Attch_1_C-130_FuT_PWS

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Attachment 1

C-130 Aircrew Training System

(C-130 ATS)

Performance Work Statement

C-130 Fuselage Trainer (FuT) Conversion

12 August 2010

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Attachment 1

CONTENTS

OBJECTIVE ....................................................................................................................................3

1.0 INTRODUCTION ....................................................................................................................3

1.1 Scope ...................................................................................................................................3 1.2 Government Furnished Equipment/Information/Property (GFE/GFI/GFP) ........................3

2.0 APPLICABLE DOCUMENTS ................................................................................................3

3.0 REQUIREMENTS .....................................................................................................................4

3.1 PROGRAM MANAGEMENT ..................................................................................................4

3.1.1 Risk Management .......................................................................................................4 3.1.2 Associate Contractor Agreements (ACA) ..................................................................4

3.2 Technical Requirements.......................................................................................................4 3.2.1 Reviews .......................................................................................................................5

3.2.1.1 Kick-Off Meeting (Meeting #1).........................................................................5 3.2.1.2 Meeting #2 .........................................................................................................5

3.2.1.3 Meeting #3 .........................................................................................................6 3.3 Test and Evaluation.............................................................................................................6

3.3.1 Inspection and Acceptance Testing ............................................................................6 3.3.2 Closure Criteria ...........................................................................................................6

3.3.2.1 Test Discrepancies .............................................................................................6

3.4 Quality Assurance/Quality Assurance Personnel (QAP) .....................................................7

3.5 Packing and Crating .............................................................................................................7 3.6 Safety ...................................................................................................................................7

4.0 DELIVERABLES ......................................................................................................................7

4.1 Technical Data Package .......................................................................................................7 4.1.1 Warranty and Licenses ................................................................................................7

4.2 Contractor Acquired Property ..............................................................................................7 4.3 Contract Data Requirements List (CDRL) ..........................................................................8

APPENDIX #1 FUT FUNCTIONALITY REQUIREMENTS .....................................................10

APPENDIX #2 FUT GOVERNMENT FURNISHED PROPERTY (GFP) .................................26

APPENDIX #3 INSTRUCTOR OPERATOR STATION EXAMPLE .......................................27

APPENDIX #4 C-130 ATS FUT FIDELITY REQUIREMENTS ................................................35

APPENDIX #5 FUT DRAWINGS, PHOTO’S .............................................................................38

APPENDIX #6 FUT DESIGNATED SAVE ITEMS LIST ..........................................................41

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OBJECTIVE

The overall objective of this C-130 Fuselage Trainer (FuT) Conversion effort is to provide an additional

permanent C-130 FuT at Little Rock AFB. The contractor shall manage and modify the Government

Furnished C-130E aircraft IAW the contractor provided Program Management Plan.

1.0 INTRODUCTION

1.1 Scope

This Performance Work Statement (PWS) defines the effort accomplished by the FuT conversion

contractor (herein referred to as the contractor) in providing management, labor, materials, fabrication,

test, technical data package, and Government acceptance of the C-130E Fuselage Trainer (FuT) located

at Little Rock AFB, AR. The contractor shall modify the Government Furnished C-130E aircraft by

removing the aircraft nose radome, aircraft wings, aircraft tail section and other identified components

outlined in this PWS, providing normal aircraft functionality that loadmasters would normally have in a

flight worthy, operational aircraft. The delivered FuT shall also meet all requirements in Appendix #1,

FuT Functionality Requirements upon delivery accompanied with a Technical Data Package. Using GFP

listed in appendix #2, the contractor shall perform the required task outlined throughout this PWS.

Appendix #3 provides an example of the IOS station that will be constructed by the contractor to include

photos and wiring diagrams.. Appendix #4 has a list of the pre/post modification baseline fidelity

requirements. The aircraft wings, after removal at the production breakpoint, shall be further removed as

identified in Appendix #5 and disposed of by the Contractor. The contractor shall be responsible for

shipping the aircraft nose, aircraft wings, aircraft tail section and other components listed on the SAVE

List in Appendix #6. Other aircraft components removed during the fuselage modification shall be

turned into the Air Force Supply System. This effort shall be coordinated with the ATS prime contractor

through the Government for inclusion into the ATS program Integrated Master Schedule (IMS). The

fuselage trainer will be integrated into the Air Force’s Aircrew Training System.

1.2 Government Furnished Equipment/Information/Property (GFE/GFI/GFP)

The following GFE/GFI shall be included within the scope of this modification:

C-130E Aircraft 63-7784.

Flight Line location as directed by the Government.

Aircraft Technical Orders (TO), these TO’s shall be utilized by the awarded contractor to generate

the Technical Data Package (CDRL B004).

2.0 APPLICABLE DOCUMENTS

The following Appendices form a part of this PWS to the extent specified herein.

1) Appendix #1 – FuT Functionality Requirements.

2) Appendix #2 – FuT Government Furnished Equipment.

3) Appendix #3 – FuT Instructor Operator Station (IOS) example.

4) Appendix #4 – C130 ATS FuT Fidelity Requirements

5) Appendix #5 - FuT Drawing to Indentify Responsibility

6) Appendix #6 – FuT Designated Save Items List

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3.0 REQUIREMENTS

The contractor shall provide the labor, materials, support equipment, and tools necessary to accomplish

the requirements as outlined in paragraph 3 of this PWS. The contractor, in accordance with appendix #

5, shall remove the wings (at the production breakpoint), the vertical and horizontal stabilizers, the

radome, and other aircraft components listed in the SAVE List of appendix #6. The contractor shall

construct crates, package, and ship all components identified on the SAVE List to CONUS locations

designated by the Government and turn in any remaining components to the government IAW Air Force

Supply System requirements and guidelines. The contractor shall install an Instructor Operator Station

(IOS, with an NVG compatible flood lamp/light that will illuminate the IOS station allowing operation

under night vision condition scenarios), Air Deflector Switch (at the junction box in the aft section of the

fuselage), Jump/Caution Lights switch (at the IOS and junction box in the aft section of the fuselage),

and beef-up plate in accordance with this PWS. The contractor shall be responsible for “clipping” the

wings from the production breakpoint back to the fuselage. The contractor shall correctly terminate all

electrical, fuel, pneumatic, and hydraulic lines. The contractor shall provide a sheet metal cap that is

sealed providing weather proof protection from corrosion over the wings, tail section and radar antennas

that are removed. The contractor shall provide a beef-up plate for structural support across the area

where the horizontal stabilizer was removed (see appendix # 5 for photos). The contractor shall deliver a

Technical Data Package (TDP).

3.1 PROGRAM MANAGEMENT

The Contractor shall provide program management, labor, materials, and other resources necessary to

meet the requirements of the contract. The Contractor shall establish and maintain a Program

Management Plan (CDRL A003) to include the contractor’s methodology to meet the requirements of

paragraph 3 and 4 of this PWS, planning, scheduling, directing, and controlling the administrative,

management, technical, logistical, financial production, and support functions of this contract. The

contractor’s Program Management Plan shall discuss the contractor’s Test & Evaluation and Inspection

& Acceptance Testing programs. The Contractor shall designate a management point of contact for

interface with the Government for all issues regarding this program. The Contractor shall monitor the

progress of all the work performed and costs incurred under the contract. The Contractor shall be fully

responsible to exercise due diligence in managing any subcontractors and vendors.

3.1.1 Risk Management

The Contractor shall implement its standard risk management processes and shall identify low, medium,

and high risks for the project, including cost, performance, schedule, and supportability risks. The

Contractor shall track medium risks, shall manage and mitigate high risks, shall perform a program risk

analysis, and shall report results to the Government Program Office at each review.

3.1.2 Associate Contractor Agreements (ACA)

The Contractor shall implement ACAs, as required, for the purposes of exchanging data, accessing and

using third party equipment, receiving technical support, establishing working interface issues, and/or

agreeing on equipment use and time for the modification.

3.2 Technical Requirements

The Contractor shall provide the necessary engineering, equipment, testing, technical, supervisory, and

logistics support in accordance with the requirements of this PWS. The Contractor shall comply with all

specifications in Appendix #1, FuT Functionality Requirements. Physical characteristics of any new or

modified components (Instructor Operator Station (IOS), Air Deflector Switch, Jump/Caution Lights

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switch, Beef-up plate) of the C-130 FuT shall be compatible with all other elements of the ATS, and in

accordance with best commercial practice for transportation, storage, and durability. The Contractor

shall not make unauthorized modifications to the training system or equipment. The contractor shall

comply with all Air Force Technical Orders in the disassembly and removal of all aircraft components

and parts applicable to this conversion effort. All movement of the aircraft will be by and under the

direction of the government.

The design for this modification shall mirror the configuration and operation of the existing FuT devices

and shall be structurally configured in the same manner as current FuT devices (i.e. tail stiffening beam,

wing root caps, IOS, Air Deflector Switch (junction box in the aft section of the fuselage), Jump/Caution

Lights switch (at the IOS and junction box in the aft section of the fuselage, etc.). The IOS faceplate

should closely replicate the drawing in Appendix #3 and be more consistent with other aircraft panels.

The Contractor shall have full responsibility for analyzing received data and developing work-around or

migration solutions.

3.2.1 Reviews

The Contractor shall support, participate in, or host (as appropriate) the reviews listed in the following

paragraphs. Schedule and technical status issues shall be discussed at all reviews. Contractor shall

prepare agendas and minutes for all reviews (CDRLs A001, A002).

3.2.1.1 Kick-Off Meeting (Meeting #1)

The Contractor shall conduct a Kick-Off meeting within 15 days after contract award at the

Government’s facility (Det 3, Little Rock AFB, AR). The purpose of this meeting is to review

requirements line-by-line, and to resolve any conflicts early in the program. The Kick-Off meeting shall

include a review of the following items:

Contractor Modification Program Schedule, including activities and milestones

PWS requirements

Contractor Data Requirements List (CDRL)

Supply System Turn-in process

Configuration management process

Acceptance Test Procedure (ATP) (CDRL B001)

System Safety process

Program Risk Assessment

3.2.1.2 Meeting #2

The contractor shall conduct a meeting after Kick-Off, but prior to the beginning of the conversion

effort. A date for the meeting shall be agreed upon by all parties during Kick-Off. Additionally, ATP

(CDRL B001), shall be due prior to meeting #2, which shall include, at a minimum, reviews of the

following items:

Updated Contractor Modification Program Schedule (include start/completion date)

Contractor Data Requirements List (CDRL), if revised

Supply System Turn-in process

Configuration management process review

ATP (CDRL B001) discussion and finalization

System Safety process review

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Program Risk Assessment review

3.2.1.3 Meeting #3

The Contractor shall conduct a meeting at the modification site in accordance with the Modification

Program Schedule. The Contractor shall conduct a Test Readiness Review during meeting #3, which

shall immediately precede acceptance testing with the Government. Meeting #3 shall include a thorough

review of any test discrepancies reported during the contractor’s internal testing and the actions taken to

correct those discrepancies.

3.3 Test and Evaluation

The contractor shall utilize their Test and Evaluation (T&E) Program to ensure that the FuT fulfills its

established requirements as set forth in this PWS. The contractor shall be responsible for the

performance of all inspection and test requirements for the modification. The Government reserves the

right to witness and/or perform any tests considered necessary to assure that no system degradation or

incompatibility exists after the modification is incorporated. The contractor shall disclose all known

discrepancies and support the Government and the ATS prime contractor in identification of

modification deficiencies. The contractor shall establish a pre-modification baseline to document any

pre-modification issues that may help to relieve any potential degradation claims. The Government

shall certify proper operation of the FuT after modification.

3.3.1 Inspection and Acceptance Testing

The Contractor shall utilize the Inspection & Acceptance Testing program to outline all inspection and

acceptance activities to be conducted during modification acceptance. The Contractor shall present the

System Test Plan to the Government for review at meeting #2. An ATP working group may be held in

conjunction with meeting #2 to finalize the ATP.

All requirements defined in this PWS shall be verified by the execution of the Government approved

ATP (Appendix 1 can be used for the basis of the ATP) (CDRL B001). Final Acceptance Testing shall

be conducted at Little Rock AFB, AR.

The following conditions also apply:

a. The Government may inspect all work at reasonable times and places. Contractor shall provide

all information and assistance necessary for safe and convenient inspection. No such inspection

shall relieve the Contractor of its obligation to furnish all work in accordance with the

requirements of this contract. The Government final inspection and acceptance shall be

accomplished at Little Rock AFB, AR.

b. The Contractor shall provide the Government the right to witness, examine, test, measure, and

evaluate all aspects of the modification during each test phase to assure its appropriate

performance/operation. The Government may utilize the ATS prime contractor for these actions.

3.3.2 Closure Criteria

Successful completion of the ATP (CDRL B001) and delivery of the Test/inspection Report (B002) and

TDP (B003) will result in a declaration that the device is Ready For Training (RFT).

3.3.2.1 Test Discrepancies

The Contractor shall work with the Government to identify modification deficiencies. The Contractor

shall utilize a test discrepancy tracking system and shall correct any deficiency/degradation to the trainer

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operation resulting from the modification activities. All test deficiencies shall be evaluated against the

modification requirements. The Contractor shall provide the Government a Test/Inspection Report

(CDRL B002) listing all test discrepancies and final resolution after successful completion of acceptance

testing.

3.4 Quality Assurance/Quality Assurance Personnel (QAP)

The government will evaluate the contractor’s performance by appointing a representative(s) to monitor

performance to ensure services are received. The government representative will evaluate the

contractor’s performance through intermittent on-site inspections of the contractor's quality control

program and receipt of complaints from base personnel. The government may inspect each task as

completed or increase the number of quality control inspections if deemed appropriate. Subsequent to

contract award, the identity of the QAP(s), with a letter defining their duties and authority will be

promptly furnished by the Contracting Officer to the successful contractor. The QAP(s) will inform the

Contracting Officer when discrepancies occur. The QAP(s) shall not obligate the Government.

3.5 Packing and Crating

The Contractor shall be responsible for fabricating crates to Government provided specifications as

identified in the Special Packaging Instructions website (https://spires.wpafb.af.mil/sindex.cfm). The

contractor shall provide shipping to CONUS locations as required by the government for items

identified in the Designated Save Items List identified in Appendix 6 FuT SAVE Items List.

3.6 Safety

The contractor shall provide a Safety Plan as part of the Program Management Plan (CDRL A003).

4.0 DELIVERABLES

4.1 Technical Data Package

After contract award, the government will provide to the winning Contractor, Technical Orders essential

in the development of the Technical Data Package. The Contractor shall develop and deliver a Technical

Data Package (TDP) (CDRL B004) to include applicable drawings and schematics that have been

modified as part of this conversion effort. Maximum use shall be made of existing Air Force provided

Technical Orders. The Government will evaluate any Contractor-produced TDP to ensure technical

adequacy and acceptability.

4.1.1 Warranty and Licenses

The government retains unlimited rights to any and all deliverables developed under this effort.

Contractor is notified that the end user of this product will be the United States Air Force (USAF) and

its Air Mobility Command (AMC), Air Education Training Command (AETC), and as managed by

Ogden Air Logistics Command (ALC)/GHMSA. All rights shall be transferable to the US Government,

AMC, AETC, and Ogden ALC for continued operation and maintenance of this system. The Contractor

shall provide a warranty on its portion of the FuT products and modifications for one year from the date

of DD250 sign off.

4.2 Contractor Acquired Property

The contractor shall purchase and deliver the following items:

https://spires.wpafb.af.mil/sindex.cfm

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1. Propeller Dolly: Qty 1: Please provide the following support equipment or its Air Force

Certified approved equivalent equipment. NSN 4920-00-167-0262; P/N: 34J6222-2, which is a

C-130 propeller dolly used to transport the C-130 propeller. 100 In. Long; 79.88 In. Wide; 70.25

In. High; 0.5 TN Rated Cap.; Steel body 1 propeller accommodated 13.5 Ft Maximum Diameter

W/O Tool Compartment; Wheel arrangement single axle, single wheel front and rear mount;

Parking Brakes, Pin Coupler; W/O retractable support. Predominant material manufactured

Steel.

2. Storage Containers: (various quantities); Please provide the following containers or its

equivalent. STANLEY Vidmar or its equivalent, Qty; 1Ea., Cabinet P/N (PKL071510C-

000001) 60"W X 27 3/4"D X 59"H; Qty: 1 Ea, Cabinet P/N (PKL071510C-000002), 60"W X

27 3/4"D X 35"H; Qty; 2Ea., Cabinet P/N (PKL071510C-000003), 45"W X 27 3/4"D X 59"H;

Qty; 2Ea., Cabinet P/N (PKL071510C-000005), 45"W X 27 3/4"D X 35"H; Qty: 1 Ea, Cabinet

P/N (PKL071510C-000007); Qty; 1Ea.; Cabinet P/N (PKL071510C-000008), 30"W X 21

3/8"D X 35"H; Qty; 2Ea., Cabinet P/N (PKL071510C-000009), 45"W X 27 3/4"D X 37"H;

Qty; 2Ea., Cabinet P/N (PKL071510C-000010), 60"W X 27 3/4"D X 37"H.

3. Inspection Lights: Qty 26: Please provide the following tools or its equivalent. Pelican M6

LED, Model #M6, P/N 2330-010-110; LED, Black, Batteries & Holster, water tight, equipment

Protector Case. Black, Batteries & Holster, Clam Features: - Batteries Included: Yes - Bulb:

LED, White - Burn Time: 4 Hours - Carry System: Holster - Finish: Black - Material: Aluminum

- Output (lumens): 41 - Overall Length (inches): 5.51 - Packaging: Clamshell - Power Source: 2

x CR123 - Submersible: No - Switch: Push Button Constant On/Off or Momentary - Made In:

United States.

4. High Boy Engine Trailer: Qty 2; Please provide the following support equipment or its Air

Force Certified approved equivalent equipment. NSN: 1740-00-106-8512, P/N 200-000-101;

MODEL 200-000-101 Quick Engine Change (QEC) Dolly is designed to support and transport

the T56-A-1A, T56-A-7, AND T56-A-9 Turboprop aircraft engines during change in aircraft

power packages, during storage, and for transportation of the engine; it is a towed vehicle

incorporating hand lever operated cable controlled brakes, leveling jacks, and wheel covered

splash fenders.

5. Digital Portable Radios: Qty, 3; Please provide the following support equipment or its

equivalent. Motorola ASTRO XTS 5000, Model II Receiver Typical Performance Specifications,

700/800 MHz VH1 UHF R1 UHF R2, Frequency Range/Bandsplits.

4.3 Contract Data Requirements List (CDRL)

The modification Data Item Descriptions (DIDs) in Table 4.4-1 includes the preliminary data items in

support of the FuT #4. The Contractor shall use electronic media and shall deliver data in USAF

standard office suite software when applicable. The Contractor shall deliver the following data items to

the Government in accordance with the initial delivery and frequency outlined in Table 4.4-1.

Distribution of these DIDs shall be determined after contract award.

Table 4.3-1. Data Item Deliverables

CDRL Data Deliverables DID (use as guide) Frequency

A001 Conference Agenda DI-ADMN-81249A As Required

A002 Conference Minutes DI-ADMN-81250A As Required

A003 Program Management Plan DI-MGMT-80004A As Required

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B001 Acceptance Test Procedure (ATP) DI-NDTI-80603A As Required

B002 Test/Inspection Report DI-NDTI-80809B As Required

B003 Technical Data Package DI-CMAN-80776 As Required

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APPENDIX #1 FUT FUNCTIONALITY REQUIREMENTS

Using the Instructor Operators Station (IOS) panel [constructed by the contractor] and located in the

Technical Order cabinet, will operate the Aerial Delivery System without the necessity of being on the

on the flight deck (All flight deck switches shall retain their current functionality). Appendix #3

provides an example of the current FuT devices IOS and aft junction box. The IOS shall be configured

so that it is interchangeable with the existing FuT IOS’s (see appendix 3). The functionality shall

include;

1. The ADS switch opens and closes the Ramp and Door in the same manner as the switch on the

ADS panel (Center Console).

2. The ADS Light illuminates when the Ramp and Door are in the full open position.

3. The Touchdown Relay switch allows the instructor to by-pass the relay to simulate flight.

4. The Red and Green “Jump/Caution Lights” switches operate the same as the Side Panel Switches.

5. The “Chute Release” push-button serves the same function as the center console button…bomb

rack chute release.

6. The “Aux Pump” switch turns the Auxiliary Hydraulic Pump on or off.

7. An Night Vision Goggles compatible floodlight

Additionally, two (2) switches shall be provided at the aft junction box;

1. One for operation of the Air-deflector doors.

2. One for operation of the Red and Green “Jump/Caution Lights”.

The FuT fidelity shall be such that the following checklists shall be capable of being performed. All

required equipment and systems shall be functional and operational.

** Note for Contractor - Items in light font should not be affected by the FuT conversion

modification.

PRIOR TO ENTRANCE

1. Nose landing gear pin -Installed

2. Ground wires -Installed

3. Chocks -In place

4. Armament placard

APPLYING POWER

This procedure checks only switches that many cause damage to the airplane if not in proper

position during application of external power. All other switches should be in their normal

power off position.

POWER OFF INSPECTIONS

Battery Compartment

1 AC EXT PWR CONTROL circuit breaker -Closed

2 DC EXT PWR CONTROL circuit breaker -Closed

Cargo Compartment

1 Defensive system safety pins -Installed

2 Aft fuselage junction box circuit breakers -Checked

3 Ramp and door controls, valves and switches -6N, NEUTRAL, OFF

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Flight Station (Right Side)

1. Status of airplane

a. AFTO Form 781A and K

2. Landing gear lever -Down

3. Hydraulic panel switches -Set

a. AUX pump switch -OFF

b. Anti-skid switch -ON

c. Engine pump switches -ON

d. Suction boost pump switches -OFF

4. Airdrop/Troop Jump computer-manual select -AD/TJ MAN switch

NOTE

Must be in AD/T J MANUAL to prevent depletion of the airplane battery.

5. Air deflectors switch -OFF

** - Jump Lights - Check

6. Copilot's circuit breaker panels -Checked

a. Tachometer test switch -OFF

b. Iron lung outlets -OFF

Navigation Station

1. Radar altimeter -Off

2. Radar PWR function switch -OFF

3. IFF radar transponder (some airplanes) -OFF

4. SCNS control panel -Set

a. SCNS power switch -OFF

b. INU power switches -OFF

c. GPS power switch -OFF

d. DVS power switch -OFF

5. RWR-OFF

6. Nose radome anti-icing switches (some airplanes) -OFF

7. AN/ALE-40/AN/ALE-47 CONTROL panel GND TEST/EMER switch -NORMAL

8. AN/ALE-40 CCU arming switch -OFF

9. AN/AAR-47 power indicator/switch -OFF

10. AN/ALE-47 CDU mode switch -OFF

11. AN/ALQ-131 control indicators OFF ISTBYIOPR switches (some airplanes) -OFF

12. SCNS power bypass switch -OFF, safetied

13. Circuit breakers -Checked

a. AN/ALE-40/AN/ALE-4 7 circuit breakers -As required

b. AN/ALQ-131 circuit breakers -As required

14. Aerial reconnaissance weather officer's console -Set

a. Check all switches -OFF/CLOSED

15. Test operation panel-GUARD DOWN

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Crew Bunk/Galley Area

1. Upper main AC distribution panel circuit breakers -Checked

WARNING

Use extreme care when working in or around the FS-245 area. Electrical shock hazard exists

because of uninsulated, high voltage wires.

Flight Station (Left Side)

1. Pilot's circuit breaker panels -Checked

a. Emergency INS battery bus tie switch -OFF, safetied

2. Air deflectors switch -OFF

** Jump Lights - Check

3. Air conditioning master switch -Off

4. Anti-icing panel-Set

a. NESA windshield switches -OFF

b. Nacelle preheat switches -OFF

c. Propeller and engine anti-icing master switch -AUTO

d. Pitot heat switches -OFF

e. Engine inlet air duct anti-icing switches -OFF

f. Propeller ice control switches -OFF

g. Anti-icing wing and anti-icing empennage switches -OFF

5. Bleed Air Valve switches -Set

a. Wing isolation valve switches -NORMAL

b. Engine bleed air valve switches -CLOSED

6. External AC and DC power switches -OFF

7. Fuel panel -Set

a. Dump pump switches -OFF, safetied; ~OFF

b. ~Dump valve switches -NORMAL, safetied

c. Fuel boost pump switches -OFF

d. No. 2 crossfeed valve switch -OPEN, all others CLOSED

8. ADS ramp and door control switch -OFF

Power Connection

1. Power cart -Positioned

a. Position generator a minimum of 50 feet from airplane and fuel sources, and a

minimum of 25 feet from fuel vents.

2. Power cable plug -Inspected

a. Inspect pins in power cable plug for foreign objects and remove as required.

3. Power cable - Connected to receptacle

4. Power cart - On

Power ON Inspection

1. Electrical panel -Set

NOTE

Ensure external power is OFF prior to performing electrical panel checks.

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a. INS battery charge switch -OFF

b. Generator switches -OFF

c. Generator disconnect switches -OFF, safetied

d. Inverter switches -OFF

e. Airplane battery voltage -Checked

f. External AC power light -On

g. Check voltage and frequency

(1) Check volts for A, B, and C phases are between 110 -125.

(2) Checks freqs for A, B, and C phases are between 380 -420.

h. External AC power switch -EXT AC PWR

i. DC loadmeters -Checked

(1) Ensure all four loadmeters are functional and indicating a load above zero.

FLIGHT STATION

1. Status of airplane -Checked

2. ADS control panel ramp and door control switch -OFF

3. PA system main power switch -ON, speakers as required

4. Weight and balance data -Checked, on board

CARGO COMPARTMENT (GENERAL)

1. AFTO Form 46/Emergency equipment -Checked and secured

2. Oxygen -Checked

3. Cargo floor -Checked

4. Dual rail pip pins -Checked (11 each)

5. Dual rail system/core bolts/ critical attachment bolts, roller conveyors -Checked, installed

CARGO COMPARTMENT (LEFT SIDE)

1. Emergency exit light -Checked, ARM, safe tied

2. Escape ladder -Checked, secured

3. Tiedown devices/straps -Checked, secured

4. Forward seats and seat belts -Check condition, installed, as required

5. Defensive system safety pins -Installed

6. Wheel well seats and seat belts -Check condition, if installed

7. Static-line retriever cable clips -Check condition, as required

8. Fire extinguisher -Checked, secured

9. Center seat support extensions -Stowed (FS 617)

10. Wheel well seat supports -Checked, secured

11. Center seat support beams -Checked, secured

12. Seats and seat belts -Check condition, installed as required


14. Emergency exit light -Checked, ARM, safetied

15. Left paratroop door master door warning light shutoff switch NORMAL, safe tied

16. Pistol grip remote dispenser switch -Checked, stowed

17. Paratroop door and warning light -Check for operation

18. Oxygen regulator -Checked, 100%, OFF (if not in use)

19. Tiedown container -Checked for proper contents, secured

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20. Ramp and door controls, manual control valves, and switches NEUTRAL, 6N, OFF, handle

secured

21. Latrine facilities -Checked for cleanliness, serviceable

22. Tiedown devices -Checked, secured

23. Anchor cable center support and pins -Checked, as required

24. Left and right paratroop jump platforms -Stowed, serviceable, secured

25. Auxiliary hydraulic system -Checked for leaks, reservoir level

26. Ramp locks and ADS arm -Engaged, connected/secured

27. Liquid containers (if installed) -Checked, secured

28. Litter stanchion -Checked, secured

29. Anchor cable reels -Checked, secured

30. Anchor cable aft support -Checked


32. Aft overhead escape hatch and rope -Installed, locking pin removed

33. Ground loading ramps -Checked, serviceable, secured

34. Door storage compartments -Checked for proper contents, secured

35. Static-line extension Y-cables/ Towed Parachutist Retrieval System (TPRS) -Checked, as

required

36. Cargo door locks -Engaged

37. Cargo door uplock -Unlocked

CARGO COMPARTMENT (RIGHT SIDE)


2. Anchor cable aft support -Checked

3. Anchor cable reels -Checked, secured

4. Litter stanchion -Checked, secured

5. Liquid containers (if installed) -Checked, secured

6. Tiedown containers -Checked for proper contents, secured

7. Waste container -Checked, clean, secured

8. Ramp locks and ADS arm -Engaged, connected/secured

9. Fire extinguisher and hand ax -Checked, secured

10. Latrine facilities -Checked for cleanliness, serviceable


12. Tiedown containers -Checked for proper contents, secured

13. Truck loading ramps -Checked, secured

14. Anchor cable center support braces -Check for pins, proper stowage

15. Anchor cable center support and pins -Checked, as required

16. Oxygen regulator-Checked, 100%, OFF (if not in use)

17. Life raft release handles -Checked, safetied

18. Right paratroop door, ramp and door master door warning light shutoff switches -

NORMAL, safetied

19. Paratroop door and warning light -Checked for operation


21. Pistol grip remote dispenser switch -Checked, stowed

22. Center seat support beams -Checked, secured

23. Wheel well seat supports -Checked, secured

W900KK-10-T-0043

Attachment 1

24. Paratroop retrieval bar -Checked, secured

25. Seats and seat belts -Check condition, installed as required

26. Emergency exit light (center overhead hatch) Checked, ARM, safetied

27. Arm emergency exit light if escape ladder is installed or an overwater leg is to be

accomplished.

28. Center overhead escape hatch and rope -Installed, locking pin removed

29. Oxygen bottle and smoke/quick-don mask -Checked, serviced, smoke mask attached to or

near bottle, hose disconnected/quick-don hose connected, harness checked, quick-don purge pin

30. Static-line retriever cable clips -Check condition

31. Wheel well seats and seat belts -Check condition, if installed


33. Forward seats and seat belts -Check condition, installed as required

34. Emergency exit light -Checked, ARM, safe tied

35. Side emergency exit -Checked, unobstructed, secured, safetied

36. Center seat back support beams -Checked, secured

37. Oxygen regulators -Checked, 100%, OFF

38. Oxygen bottle and smoke/quick-don mask -Checked, serviced, smoke mask attached to or

near bottle, hose disconnected/quick-don hose connected, harness checked, quick don purge pin


40. Internal portable winch snatch block(s) -Checked

41. Seat and litter stanchions -Checked, secured


43. Fire extinguisher and hand ax -Checked, secured

44. Urinal facilities -Checked for cleanliness, serviceable

POWER ON

1. Forward auxiliary control panel -Checked

2. Cargo winch (if installed) -Check operation, serviceable as required, secured

3. Aft fuselage junction box panel -Checked

4. Cargo ramp and door and warning lights -Check for proper operation

5. Aft right interphone cord -Checked

6. FWD right interphone cord -Checked

7. Galley -Checked, OFF

BEFORE TAXI

1. Crew entrance door -Closed, locked

BEFORE LEAVING AIRPLANE

1. Airplane and equipment -Cleaned, stowed, secured

2. Cargo ramp and door -Closed, ADS arms connected

3. Cargo compartment emergency exit lights switch -OFF

4. Cargo compartment oxygen regulators -Off

5. Pendulum release pivot arm cover -Installed

6. Cargo floor restraint rail detent latches -Extended

7. Electrical panel switches -Set

8. Emergency exit light off button -Pressed

W900KK-10-T-0043

Attachment 1

9. Power cart -Off

CARGO DOOR AND RAMP OPERATION

WARNING

The ADS control panel ramp and door control switch must be set to OFF and the ramp

manual control knob, above the ramp control panel must be set at the 6N (neutral) position

before operating the pump switch on the ramp control panel.

CAUTION

Wait at least 10 seconds after the auxiliary hydraulic pump is turned OFF, to allow the accumulator to

discharge before turning the pump switch back on. Failure to do this will overload the motor and open

the pump circuit breakers.

With the pump switch set to ON the cargo door is opened by holding the cargo door control switch in

the OPEN position until the door is fully opened and retained by the uplock; the ramp then is moved to

the desired position by holding the ramp control switch at LOWER.

NOTE

The ramp can be stopped at any position by releasing the ramp control switch. The cargo door will free

fall back to the closed position if the door control switch is released prior to the moment the door

reaches the up-and-locked position.

The ramp is closed by holding the ramp control switch in the RAISE position until the ramp is up and

locked.

CAUTION

Prior to raising the ramp, ensure that locks are retracted and the ramp seal area is clear.

NOTE

When being raised the ramp call be stopped in any position by releasing the ramp control switch.

On E airplanes prior to AF72-1288 H and 3> airplanes the door is closed by holding the cargo door

switch to the OPEN position and pulling the cargo door manual release until the uplock is released.

After the uplock is released allow the cargo door to free fall to the closed position. If door does not lock,

hold the cargo door switch to the CLOSE position until the door is closed and locked.

Manual Operation of Cargo Door and Ramp with Handpump Pressure

OPENING CARGO DOOR AND RAMP

To open the cargo door and lower the ramp by use of the handpump:

WARNING

Before manual handpump operation, check that the AUX hydraulic pump switches on the flight station

and the ramp control panel are in the OFF position.

W900KK-10-T-0043

Attachment 1

1. Move the cargo door manual control valve handle to OPEN and operate the handpump until the door

is up and locked.

2. Move the cargo door manual control valve handle to the NEUT (center) position.

3. Move the ramp manual control knob to the NO. I (unlock) position: operate the handpump until the

handpump pressure indicator on the ramp control panel shows 3,000 PSI and all the ramp locks are

visibly disengaged.

4. Move the ramp manual control knob to the NO. 2 (lower) position. Operate the handpump until the

ramp is lowered.

5. Move the ramp manual control knob to the 3N (neutral) position.

CLOSING CARGO DOOR AND RAMP

To close the cargo door and raise the ramp by using the handpump, proceed as follows:

WARNING

Before manual handpump operation, check that the AUX hydraulic pump switches on the flight station

and the ramp control panel arc in the OFF position.

1. Check that the pump switch on the ramp control panel is at the OFF position.

2. Move the ramp manual control knob to the NO.4 (raise) position and operate the handpump until the

ramp is fully closed.

3. Move the ramp manual control knob to the NO.5 (lock) position. Operate the handpump until the

handpump pressure indicator registers 3.000 PSI and all ramp locks are visibly engaged.

4. Move the ramp manual control knob to 6N (neutral).and leave it in that position.

5. Move the cargo door manual control valve handle to OPEN position. Operate the handpump until the

pressure indicator reads a minimum of 500 PSI, pull the aft cargo door uplock manual release to the

unlock position and move the manual control valve to NEUT. Door will free fall

6. Move the cargo door manual control valve handle to CLOSE, and operate the hand pump until the

door is locked.

7. Move the cargo door manual control valve handle to the NEUT (center) position. The handle does not

have a positive stop at the NEUT (center) position. so it should be checked to ensure that is has not been

inadvertently moved beyond this setting.

Operation of Cargo Door and Ramp from Flight Station

1. Depressurize the airplane.

2. Operate the auxiliary hydraulic system electric-driven pump by placing the pump switch. on the

hydraulic system control panel, in the ON position. Check the system pressure.

** Bypass Touchdown Relay with IOS.

3. Move the ramp and door control switch on the ADS panel to the OPEN position.

4. When the ramp and door open light and the master door warning light illuminate, move the ramp and

door control switch to the OFF position.

5. When the loadmaster signals that the cargo is dropped and the ramp and door area is clear, move the

ramp and door control switch to OPEN then CLOSE position.

6. When the ramp and door open light and the master door warning light go off, move the ramp and door

control switch to the OFF position.

7. Turn auxiliary hydraulic pump OFF.

W900KK-10-T-0043

Attachment 1

** Repeat 1 – 7 utilizing IOS controls in lieu of Flight Station controls.

AIRLAND CARGO HANDLING SYSTEM PREFLIGHT

1. Left and right control handles -Repositioned

a. LH SIMUL handle to AFT RESTRAINT RELEASE then to SIMULTANEOUS position.

b. RH EMERG REL handle to EMER then to LOAD position.

2. Left and right detents Retracted

3. Left control handles Repositioned

a. LH SIMUL handle retuned to STOWED position, stowage pin installed.

b. Sequentially unlock all left detent latched in sequence, drum counter opposite ALL OPEN, stow

handle with LOCK position on knob facing up,

4, Critical attachment bolts and roller conveyors -. Checked

a, Critical attachment bolts -Physically checked

b. Attachment bolts visually inspected

c. Roller conveyors –installed/secure

5, Left and right ramp release handles Checked

a. Engage detents and flanges

b, Pull release handles to fh1l forward position, ensure detent and flanges fully retract.

c, Release handles stowed, stowage pins installed.

6. Discrepancies Entered into AFTO Fom1 781 A

PALLETIZED AIRDROP CARGO HANDLING I

SYSTEM PREFLIGHT

1. Left control handles -Checked

a. LH SIMUL handle down, stowage pin installed.

b. SEQ LOCK handle, check that drum counter is opposite number 11 position and the handle is stowed

with LOCK position on knob facing up.

2. Right-hand master control handle and crossover linkage -Connected

a. Move RH EMERG REI handle to CHECK, ensure handle will stay in CHECK, move to NORMAL.

3. Left rails --Checked

a. Proceeding aft, check the following:

(1) Cargo compartment inboard attachment bolts and washers installed.

(2) Draw bars connected and sleeves secured in full forward position.

(3) Detent latches will not depress into rail, detent restraint arm parallel to detent body, no yellow

showing on actuator arm, and emergency release arms connected to SIMUL control rods.

(4) A-30 critical attachment bolt and washer installed. Right Rails --Checked

a. Proceeding forward, check the following:

(1) G-30 critical attachment bolt and washer installed.

(2) Cargo compartment inboard attachment bolts and washers installed.

(3) Detent latches will not depress into rail, release spacer between roller, alignment mark satisfactory,

lock out pins stowed, lock tension at minimum settings, horizontal oval point screw installed, slippage

mark satisfactory, and vertical set screw installed.

(4) Draw bars connected and sleeves secured in full forward position. Left and right control handles -

Positioned

5. Left and right control handles -Positioned

W900KK-10-T-0043

Attachment 1

a. LH SIMUL handle to AFT RESTRAINT RELEASE.

b. RH EMERG REL handle to EMERG

6, Left and right detents -Checked

a, Check for freedom of aft movement.

7, Left and right control handles Repositioned

a. LH SIMUL handle to SIMULTANEOUS,

b. RH EMERG REI, handle to LOAD,

8, Left and right detents and guard assembly doors Retracted/closed, as required

9, Left control handles Checked

a. LH SIMUL handle returned to STOWED position, stowage pin installed,

b, Sequentially unlock all left detent latches, drum counter opposite ALL OPEN, stow handle with

LOCK position on knob facing up.

10. Cargo compartment and ramp intermediate roller conveyors '.'. Checked, secure, serviceable

11. Discrepancies Entered in AFTO FORM 781 A

CARGO LOADING PREPARATION

1, Manifest/load plan Checked

2. Cargo inspection -Completed

3, Pallet and net conditions Checked

4. Pallet/vehicle safety aisles Checked, verified

5, Soil contamination and pest Checked

6, Mounted equipment/cargo -Secured to carrier or Vehicle

7, Engines and brakes Checked, if applicable

8, Fuel levels Checked, if applicable

9, Fuel, battery, and oil caps Tightened

10. Tanker-type vehicles Checked

11. Contact area pressures Computed

12. Hazardous materials Checked, properly documented

13 , Ramp support/ramp –Installed/positioned as required

14, Cargo loading preparation checklist-Completed

CARGO LOADING (PALLETIZED/FLOOR LOAD)

1. Cargo loading preparation check list Completed

2. Left-hand and right-hand locks and vertical restraint flanges Retracted, as required

3. Cargo compartment and ramp 110m area -Cleared and unobstructed

4. Load inspection ·-Completed

5. Loading team duties -Assigned, briefed

6. Vehicle chocks Positioned

7. Auxiliary truck loading ramps -Installed, as required

8. Loading chocks -Installed, (for bare tine loading only)

9. Vehicle Positioned, adjusted

10. Brakes Set

11. Bridge plates Installed, as required

12. Pallet(s)/platform(s)/cargo -Loaded

13. Dual rail detent latches/tiedown Engaged/installed

14. Remaining pallet (s}/platform(s)/cargo Loaded

W900KK-10-T-0043

Attachment 1

15. Floor retractable flanges -Engaged, as required

16. Ramp pallet, detent latches, and retractable flanges -Loaded, engaged, as required

17. Loading vehicle ---Released

18. Tiedown Computed, installed, checked

19. Cargo loading (palletized/floor loaded) checklist - complete

WINCHING CHECKLIST

1. Winch --Positioned

2. Power cable (portable winch only) Connected

3. Winch condition Checked

4. Winch oil level (portable winch only) Checked

5. Control pendant power cable not in path of cargo (HCU-9/A only) IC] --Checked

6. Operational checkout Completed

7. Winch cable condition Checked

8. Loading team duties Assigned, briefed

9. Cargo compartment and ramp floor area .. Clear

10. Steering yoke _. Installed, if required

11. Auxiliary loading ramp/bridge plates Installed/positioned, if required

12. Vehicle chocks -Positioned

13. Winching vehicle (external/self winching)

14. Cargo/vehicle to be loader – Positioned

15. Cable attached – completed

16. Cable slack removed, snatch block and cable attachment – Completed, as required

17. Ratchet brake release lever (Bulldog) – Up position

18. Vehicle/cargo – Loaded, positioned, transmission set

19. Tiedown – Computed, installed, checked

20. Winching checklist – Completed

VEHICLE LOADING

1. Cargo loading preparation checklist -Completed

2. Auxiliary loading ramps/bridge plates aligned for proper axle width Checked

3. Ventilation Checked

4. Loading team duties Assigned, briefed

5. Vehicles to be loaded/prime mover Aligned, low gear, if applicable

6. Vehicles Loaded, parked, transmission set

7. Parking brakes and ignition --Set, off

8. Tiedown Computed, installed, checked

9. Vehicle Loading Checklist --Completed

PALLETIZED/CARGO/VEHICLE OFFLOADING

1. Offloading team duties. Assigned, briefed

2. Ramp support/bridge plates/auxiliary truck loading ramps/auxiliary ground loading ramps

Installed/positioned, if required

3. Vehicle chock -Positioned, as required

4. Offloading vehicle/equipment Positioned

5. Ventilation As required

W900KK-10-T-0043

Attachment 1

6. Winch -Positioned, secured and attached to load, as required

7. Vehicle/cargo Restraints, removed

8. Cargo compartment and ramp floor area Cleared

9. Cargo ramp right-hand and left-hand detent latches Unlocked, if applicable

10. Cargo compartment vertical restraint flanges Retracted, as required

11. Cargo compartment right-hand and left-hand detent latches Unlocked, if applicable

12. Off1oad Completed

13. Offloading vehicle(s) --Released

14. Palletized/cargo/vehicle offloading checklist Completed

PASSENGER ONLOADING/OFFLOADING

1. Cargo compartment and ramp floor area Clear

2, Ramp and door/crew entrance door -Positioned/opened

3, Passengers -Boarded/deplaned

4, Seat belts - As required

5, Manifest Checked

6, Passenger briefing --Completed

7, Baggage/loose equipment –Secured/offloaded

8, Passenger onloading/offloading checklist-Completed

GENERAL AIRCRAFT PREPARATION FOR AIRDROP CHECKLIST

1. Litter stanchion brackets -Positioned (as required)

2. Static-line retriever (forward control) Checked, if required

3. CDS arming switches -Safetied/checked, dearmed,

4. Anchor cable Support arms (forward controls) --Checked, if required

5. Anchor cables, fittings, and U-bolts-Installed and checked (as required)

6. Seat/seat support beams Secured/removed

7. Anchor cable support arms (aft controls) Checked, if required

8. Aft auxiliary control panel -Checked

9. Anchor cable stowage brackets -Rotated, secured (as required)

10. Litter stanchion brackets -Taped (as required)

11. Engine exhaust covers -Secured forward of load

12. Anchor cable reels Secured/removed

13. Aft cargo door contents --checked

14. Urinal steps, toilet assembly, modesty curtains, cargo net stowage boxes, and trash containers

Stowed and secured Type III nylon cord

15. Vertical restraint flanges and ramp locks - Retracted and secured

16. Pendulum release pivot arm cover -Removed, stowed (as required)

17. Pendulum release system Checked (if required)

18. Tiedown tab 30D -Checked (if required)

19. Anchor cable stops -Positioned and taped (as required)

20. Roller conveyors Secured/removed and stowed (as required)

21. Cargo door and ramp - Opened to ADS position

22. General aircraft preparation for airdrop checklist Completed

AIRCRAFT PREPARATION FOR PARATROOP AIRDROP

W900KK-10-T-0043

Attachment 1

1. General aircraft preparation for airdrop checklist Completed, if required

2, Restraint rail sections 5B and 6B -Removed, stowed (if required)

3, Seats and safety belts –Checked

4. Center anchor cable supports Installed, checked (if required)

5, Static-line retriever extensions, V-cables. TPRS Checked (as required)

6, Paratroop retrieval bar (some aircraft) Positioned, secured

7. Jump platforms and door area - Inspected, installed, checked (if required)

8, Aircraft exterior inspection –Completed

9. Passenger onloading/offloading checklist -Completed

10, Cargo loading (palletized/floor load) checklist -Completed (as required)

11, Aircraft preparation for paratroop airdrop checklist. Completed

AIRCRAFT PREPERATION FOR EQUIPMENT AIRDROP

PRIOR TO LOADING

1. General aircraft preparation for airdrop checklist - Completed

2. Left rail lock inspection covers taped open Completed

3. Right-hand master control handle - Normal position

4. Right rail detents -Pinned-out, as required

5. Iron lung switch -On, as required

6. EPJS control box -Installed/connected and secured, as required

7. EPJS Y· connector(s) and mounting box(es) Installed and secured, as required

8. EPJS main cable Installed and secured, as required

9. EPJS interconnect cable(s) -Installed and secured, as required

10. Right-hand master control handle Load position

11. Load acceptance inspection Completed

12. Cargo loading (palletized/floor loading) checklist --Completed

AFTER LOADING

1. Left rail detents -Engaged, checked

2. Right rail detents Engaged, set

3. Vertical restraint flanges -Engaged, as required

4, EFTC actuators Installed

5. Extraction system --Installed, checked

6. EPJS platform cable (s) - Installed, as required

7, EPJS squib cable(s) Installed, as required

8. EPJS continuity check -Completed, as required

9. Emergency restraint chains --Positioned

10. Load inspection Accomplished

11. Aircraft preparation for equipment airdrop checklist -Completed

AIRCRAFT PREPARATION FOR CONTAINER DELIVERY SYSTEM (CDS) AIRDROP

PRIOR TO LOADING

1. General aircraft preparation for airdrop Checklist Completed

2. Seat support beam(s) - Removed (as required)

W900KK-10-T-0043

Attachment 1

3. Buffer stop assembly/alternate forward barrier Installed

4. Center vertical restraint (CVR) Installed (as required)

5. Detents beside and aft of load Retracted and pinned-out (as required)

6. Pulley assembly Installed

7. Retriever winch cable loop Installed (as required)

8. Load Acceptance Inspection –Completed

9. Cargo loading (palletized/f1oor load) checklist Completed

AFTER LOADING

1. Container rigging

2. Tiedown restraint --Installed and checked (if required)

3. Load inspection –Accomplished

4 Aircraft preparation for container delivery system (CDS) airdrop checklist Completed

AIRCRAFT PREPARATION FOR COMBAT RUBBER RAIDING CRAFT (CRRC) AIRDROP

1. General aircraft preparation for airdrop checklist/aircraft preparation For paratroop airdrop checklists

2. Left and right detents - Retracted and pinned out, as required

3. Retriever winch cable loop -Installed

4, Load acceptance inspection Completed

5, Cargo loading (palletized/floor load) checklist -Completed

AFTER LOADING

1. CRRC platform(s) Positioned

2. Pulley assembly Installed

3. Type VIII nylon release gate Installed

4. Static-line retriever cable --Attached to guillotine knife

5. Static-lines attached to anchor cable Completed

6. Forward barrier - Installed

7. Tiedown restraint Installed and checked

8, Load inspection – Accomplished

9. Aircraft preparation for combat rubber raiding craft (CRRC) air drop Completed

AIRCRAFT PREPARATION FOR HIGH SPEED LOW LEVEL AERIAL DELIVERY SYSTEM

(HSLLADS) AIRDROP

1. General aircraft preparation for airdrop checklist Completed

2. Sling ejection delivery system (SEDS) Checked

3. Load acceptance - inspection -Completed

4, Cargo loading (palletized/floor load) checklist -Completed

AFTER LOADING

1. Container(s) Positioned

2. Multiple container belly band (if applicable)

3. Sling ejection delivery system (SEDS)

4, Sling retention lines Attached

5, Release assembly –Attached

6. Electrical cable -Connected

W900KK-10-T-0043

Attachment 1

7, Static-line(s) –Attached

8. Load inspection Accomplished

9. Sling Disconnected

10. Tiedown restraint · Installed

11. Aircraft preparation for high speed low level aerial delivery system (HSLLADS) airdrop checklist -

Completed

AIRCRAFT PREPARATION FOR CONTAINER RELEASE SYSTEM (CRS) AIRDROP

PRIOR TO LOADING

1. General aircraft preparation for airdrop checklist -Completed

2. Release assembly - Checked

3. Load acceptance inspection Completed

4, Cargo loading (palletized/floor load) checklist Completed

AFTER LOADING

1. Container(s) Positioned

2. Multiple container belly band (if applicable) - Installed

3. Release assembly Attached

4. Forward restrain/tension strap Installed

5. Electrical cable Connected

6. Static-line(s) Attached

7. Load inspection -Accomplished

8. Tiedown restraint -installed

9. Aircraft preparation for container release system (CRS) airdrop checklist Completed

ABFDS CREW EMERGENCY JETTISONING PROCEDURES

1. Notify Pilot Notified LM

2. OXYGEN ON/l00% ALL

3. Pressurization Emergency Depressurize FE

4. DESCENT As required p

5. Forward and aft tank valves closed. 25-foot vent hose disconnected from forward vent fitting and

stowed under aft lank straps. Fuel Specialist/LM

6. 20-fool hose, disconnected from vent at

FS 642 and stowed under aft tank straps. Fuel Specialist/LM

7. 28-foot and 8-fool hose disconnected at FWD and AFT tank valves and capped. Stow the above hose

on the pump modules and secure with one 5,000 pound strap for jettisoning.

Fuel Specialist/LM

8. Cargo ramp and door -Clear to Open/OPEN and locked LM

9. Left and right ramp lock release handles Pulled LM

10. Loadmaster informs pilot Clear to jettison pump modules. Pilot will establish a slight nose high

attitude to jettison modules. LM,P

11. Vertical restraint flanges -Released/retracted LM

12. All tank restraint straps Clear LM

13. All personnel forward of load LM

14. Loadmaster informs pilot ready to jettison LM

15. Pilot will establish an approximate IO-degree nose high attitude to assist in jettisoning.

W900KK-10-T-0043

Attachment 1

16. Upon the pilot's command "JETTISON " the LM immediately positions RH EMERG REL handles

to EMERG and LH SIMUL handle to aft restraint removed position.

17. Pilot notified of load – Load clear/or condition

END OF APPENDIX # 1

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Attachment 1

APPENDIX #2 FUT GOVERNMENT FURNISHED PROPERTY (GFP)

The following is a list of Government furnished support equipment provided for this

requirement.

AGE Support Equipment

a. -86 Hobart Generator (1 Ea.)

b. Lo-Paks (up to a maximum 5 Ea.)

c. FL1D Light Carts (up to a maximum of 5 Ea.)

d. Maintenance Stands

a. B-4 (2 Ea.)

b. B-5 (2 Ea.)

c. B-1 (2 Ea.)

d. C-1 (2 Ea.)

e. Hydraulic Mule (1 Ea.)

f. Browsers (2 Ea.)

g. Fuel Foam Carts (2 Ea.)

h. Flight Control Surfaces Dollies (1 Ea.)

C-130E Aircraft 63-7784.

Flight Line location as directed by the Government.

Aircraft Technical Orders (TO), these TO’s shall be utilized by the awarded contractor to generate

the Technical Data Package (CDRL B004).

END OF APPENDIX # 2

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Attachment 1

APPENDIX #3 INSTRUCTOR OPERATOR STATION EXAMPLE

Instructor Operation Station (IOS) pictured above. Pictured

Below is the Aft Junction Box.

The Aft Fuselage

Junction Box

requires adding a

Jump/Caution

Lights switch,

beside the Air

Deflector Switch.

There is

approximately 70

feet from the IOS

to the Aft Fuselage

Junction Box.

An NVG

compatible

flood

lamp/light

will

illuminate

the IOS

Station

5.25” H;

5.25” D; 7” W

W900KK-10-T-0043

Attachment 1

ADS panel that the IOS is wired to. There is

approximately 30 feet from the IOS to the ADS

panel located on the Center Control Pedestal.

W900KK-10-T-0043

Attachment 1

W900KK-10-T-0043

Attachment 1

Jump Lights Panel that the IOS is wired to.

There is approximately 30 feet from the

IOS to the Jump Lights panel located on the

Pilot and Co-Pilot Side Panel.

W900KK-10-T-0043

Attachment 1

W900KK-10-T-0043

Attachment 1

The Male Connector attached to the IOS Control Box.

W900KK-10-T-0043

Attachment 1

APPENDIX #4 C-130 ATS FUT FIDELITY REQUIREMENTS

DEFINITIONS

Failure - A failure is defined as any C-130 FuT malfunction which results in the loss or delay of

scheduled training.

Functional - Shall be identical to the C-130 aircraft or in accordance with delivered drawings and

shall include all associated aircraft hardware in accordance with C-130 technical data and technical

orders.

Functional Non-Operational - Shall be identical to C-130 aircraft but related system(s) does not

have to function or be operational. Must, twist, switch, etc. but not operate or manipulate a system.

Operational - Shall be identical in operation to the C-130 aircraft.

An Instructor Operators Station (IOS) panel, located at the TO cabinet, shall be installed to allow Aerial

Delivery System (ADS) and Jump/Caution Light operations without the necessity of being in the cockpit

(All cockpit switches shall retain their current functionality). Appendix #3 provides an example of the

current FuT devices IOS. The functionality shall include;

1. The ADS switch opens and closes the Ramp and Door in the same manner as the switch on the ADS

panel (Center Console).

2. The ADS Light illuminates when the Ramp and Door are in the full open position.

3. The Touchdown Relay switch allows the instructor to by-pass the relay to simulate flight.

4. The Red and Green “Jump/Caution Lights” switches operate the same as the Side Panel Switches.

5. The “Chute Release” push-button serves the same function as the center console button…bomb rack

chute release.

6. The “Aux Pump” switch turns the Auxiliary Hydraulic Pump on or off.

7. An NVG compatible floodlight

Additionally, two (2) switches shall be provided at the aft junction box;

1. One for operation of the Air-deflector doors.

2. One for operation of the Red and Green “Jump/Caution Lights”.

The following is a list of aircraft equipment the contractor shall be responsible for providing the initial

inspection, diagnostic and reassembly, to convert the FuT as a learning device to meet the PWS

requirement based on the indicated state of fidelity:

Exterior

AC Exterior Power Receptacle - Operational

Flight Deck - Pilot's Station

Pilot's left side console (PA/interphone

switch, hand held microphone) - Operational

Flight Deck - Copilot Station

Auxiliary Hydraulic System panel - Operational Functional

Copilot's right side console (inter-phone panel, handheld

microphone) - Operational

Flight Deck - Center Console

Copilots ADS panel - Operational

ADS Chute Release – Functional

Flight Deck - Overhead Center Console (top)

W900KK-10-T-0043

Attachment 1

Emergency exit light switch - Functional Operational

Ceiling PA speaker and switch - Functional

Inter-phone panel - Functional

Electrical control panel top row - Functional

Battery switch - Functional Non-Operational

Bus tie switch - Operational

External power switch - Functional

Fuel panel - Functional Non-Operational

Flight Engineer and Navigator Seats and safety belts – Functional

Circuit breaker panel - Modified Functional (Some must be operational for FuT

Operations. Rest should be pulled and strapped.)

Flight Deck - Navigator Station

Inter-phone Panel - Functional Operational

Seat and safety belts - Functional

Oxygen regulators - Functional Non-Operational

Flight Deck - Other

Forward escape hatch - Functional

Wing life raft T-handles - Functional Non-Operational

All oxygen regulators - Functional Non-Operational

Crew oxygen recharger hoses - Functional Non-Operational

Cargo Compartment - Bulkhead

Crew galley (oven/CB/light/hot cup receptacle/

coffee jug receptacle) - Operational

Crew galley (refrigerator door and

bottom drawer) - Functional Non-Operational

Cargo winch (attachment points/pendent/oil

level/cable) - Functional

Crew oxygen re-charge hoses (3) - Functional Non-Operational

Instructor loadmaster station - Functional Operational

Cargo Compartment - Left Side (Fwd to Aft)

Crew entrance door - Operational

Forward PA/Inter-phone panel and cord - Functional

Cargo compartment dome light switches - Functional

Left troop door jump signal lights - Functional

Left troop door ADS control panel - Functional

Left troop door PA/Interphone panel and cord - Functional

Hydraulic system manual override selector valve system -

Functional

Aft jump signal lights - Functional

Aft anchor line arm switch - Functional

Aft anchor cable support - Functional

Cargo Compartment - Right Side (Aft to Fwd)

Aft anchor cable actuator - Functional

Aft jump signal lights - Functional

Right troop door jump signal lights - Functional

Right troop door PA/Interphone panel and cord - Functional

W900KK-10-T-0043

Attachment 1

Auxiliary Hydraulic system pump and all associated plumbing, fittings and filters -

Functional

Cargo Compartment - Right Side (Aft to Fwd)

Cargo compartment dimming switches - Functional

Oxygen manual shutoff valve - Functional Non-Operational

Oxygen regulators - Functional Non-Operational

Cargo Compartment - Other

Oxygen recharge hoses (2) - Functional Non-Operational

All cargo compartment and ramp loading lights - Functional

Escape ropes and ladders - Functional

Ramp and cargo door - Functional

All emergency exit lights - Functional

Warning bells - Functional

PA speakers - Functional

Restraint rails, left and right - Functional

Cargo compartment and ramp roller conveyors - Functional

12 each litter stanchions - Functional

Snatch blocks - Functional

Anchor cable attachment points - Functional

Wing life raft T-handles - Functional Non-Operational

Side emergency escape hatches/interior handles - Functional

Emergency escape overhead hatches/interior releases

Functional

Escape ropes - Functional

Auxiliary ground loading ramps - Functional

Strap stowage boxes - Functional

Chain storage boxes - Functional

Cargo floor (good general condition) - Functional

Pendulum release assembly (bomb rack) - Functional

Anchor cables - Functional

Cargo Compartment - Other

Aerial delivery system - Functional

Static line retriever winches - Functional

Aft retriever winch remote control assembly - Functional

Scanners cord - Functional

Protective clothing kit - Functional Non-Operational

Miscellaneous

Emergency hand ax (2) - Functional

Crew entrance door - Functional

Flight Station ladder - Functional

Restraint rail end bumpers - Functional

Door open lights - Functional

Aft anchor cable supports/motors - Functional

Air deflector doors – Functional

W900KK-10-T-0043

Attachment 1

END OF APPENDIX # 4

APPENDIX #5 FUT DRAWINGS, PHOTO’S

Legend:

"A"-Blue = Require Removal and Shipment, Blue Lined (///) = Sub-Components Require Removal and Shipment

"B"-Red/Green = Require Shipment [Currently Removed]

"C"-Orange = Wing Section To Be Cut

"D"-Yellow = FuT Completed Project

Dorsal Fin Assembly “A”

3A. Outer Wing Dry)………………………………………………………………....……………..3962 LB

4B. Aileron………………………………………………………………………………………….190 LB

5B. Outer Wing Flap…………….………………………………………………………………….217 LB

6B. Center Section Flap…………………….…..…………………………………………………..119 LB

7A. Horizontal Stabilizer Assembly……………………..…………………………………………2589 LB

8B. Elevator (Inboard Counterweight Removed)…………………………………………………...218 LB

9A. Vertical Stabilizer……………………………….……………………………………………..869 LB

10B. Rudder (Not Including Balance)…………………………….………………………………..193 LB

11A. Tail Cone……………………………………………………………………………………..72 LB

12D. Main Gear Wheel (Complete With Tire And Tube)…............................................................365 LB

13D. Main Gear Wheel (One Gear Complete With Wheel, Tire, And Brake)…………………….825 LB 14D. Nose Landing Gear……….………………………………………………………………………….….573 LB

18A. Radome………………………………………………………………………………………200 LB

19D. Cargo Ramp…………..…………………………………………………………….……….1,109 LB

20D. Aft Cargo Door………………………………………………..…………………………….731 LB

*NOTE: Weights are approximate

Wing Section

“C” To Be Cut

W900KK-10-T-0043

Attachment 1

The top photo shows an example of a the beef-up

beam, and the bottom photo shows how the beef-

up beam is attached on the tail section after the tail

sectin is removed.

W900KK-10-T-0043

Attachment 1

The picture above show an example of a combination beef-up beam/cover plate above the ramp and

cargo door after the tail section is removed.

END OF APPENDIX # 5

W900KK-10-T-0043

Attachment 1

APPENDIX #6 FUT DESIGNATED SAVE ITEMS LIST

a. DESIGNATED SAVE ITEMS LIST FOR FuT #4 DISPOSITION

*These parts require shipment (CONUS) as identified in the PWS and Attachment 5.

#'s Component Qty Turn-In/Ship Shipping Location

1 O/B Flap 1 Ship Robins AFB, GA

2 O/B Flap 1 Ship Robins AFB, GA

3 Vertical Horz Tip 1 Crate/Ship Robins AFB, GA

4 I/B Nacell Upper Access Pnl Assy 1 Turn-In LRAFB

5 O/B Wing Leading Edge 1 Crate/Ship Robins AFB, GA

6 Horz Stab Lt Leading Edge 1 Crate/Ship Robins AFB, GA




10 Wing Leading Edge 1 Crate/Ship Robins AFB, GA


12 Nose Radome Assy 1 Crate/Ship Robins AFB, GA


14 LH I/B Flap 1 Ship Robins AFB, GA

15 RH I/B Flap 1 Ship Robins AFB, GA

16 Rt Aileron 1 Ship Robins AFB, GA

17 Lt External Fuel Tank 1 Crate/Ship Robins AFB, GA

18 Rt External Fuel Tank 1 Crate/Ship Robins AFB, GA

19 Pylon ? 1 Crate/Ship Robins AFB, GA

20 Synchrophaser Assy 1 Turn-In LRAFB

21 Synchrophaser Assy 1 Turn-In LRAFB

22 Heat Exchanger 1 Turn-In LRAFB

23 Heat Exchanger 1 Turn-In LRAFB

24 Jackscrew Assy, Flap 7 Crate/Ship Robins AFB, GA

25 Jackscrew Assy, Flap 7 Crate/Ship Robins AFB, GA

26 Fire Extinguisher (Bottle) 1 Turn-in LRAFB

27 Pneumatic Valve 1 Turn-in Robins AFB, GA

28 Anti Ice Valve 20 Turn-in Tinker AFB

29 Butterfly Valve 1 Turn-in Tinker AFB

30 Butterfly Valve 5 Turn-in Tinker AFB

31 Regulating Float Valve 1 Turn-in Tinker AFB

32 Speech Security Equipment 1 Turn-in LRAFB

33 Remote Control Unit 1 Turn-in LRAFB

34 Electrical Equip Rack 1 Turn-in Robins AFB, GA

35 Radio Set 1 Turn-in LRAFB

W900KK-10-T-0043

Attachment 1

36 Amplifier 50 Turn-in LRAFB

37 Direction Control 1 Turn-in LRAFB

38 Radio Reciever 1 Turn-in LRAFB

39 Radio Reciever 1 Turn-in LRAFB

40 Radio Nav Receiver 34 Turn-in LRAFB

41 Radio Nav Receiver 53 Turn-in LRAFB

42 Radar Reciever 1 Turn-in LRAFB

43 Transmitter Reciever 1 Turn-in LRAFB



46 Radar Set Control 1 Turn-in LRAFB

47 Radar Data Computer 1 Turn-in LRAFB

48 Ground Collision Avoidance 1 Turn-in LRAFB

49 ETCAS Processor / GCA 1 Turn-in LRAFB

50 AN/APX-119 Rec Transmitter 1 Turn-in LRAFB

51 Radar Processor 1 Turn-in LRAFB

52 Countermeasure Receiver 1 Turn-in LRAFB

53 Countermeasure Receiver 1 Turn-in LRAFB

54 Countermeasures Dispenser 18 Turn-in LRAFB

55 Countermeasures Rec Control 1 Turn-in LRAFB

56 Countermeasures Processor 1 Turn-in LRAFB

57 Countermeasure Switching Unit 9 Turn-in LRAFB

58 AN/AAR-44A Signal Processor 21 Turn-in LRAFB

59 AN/AAR-44A Sensor 1 Turn-in LRAFB

60 Tuning Drive 1 Turn-in LRAFB

61 Power Supply Amplifier 1 Turn-in LRAFB

62 Amplifier Control 1 Turn-in LRAFB

63 Amplifier Detector 1 Turn-in LRAFB

64 Communications Modem 1 Turn-in LRAFB

65 Electromagnet Relay 1 Turn-in LRAFB

66 Electromagnet Relay 1 Turn-in LRAFB

67 Electrical Chassis 1 Turn-in LRAFB

68 Prop Deicer Contact Ring Assy 4 Turn-in LRAFB

69 Antenna 19 Turn-in LRAFB


71 Antenna Control 1 Turn-in LRAFB

72 Antenna Control 2 Turn-in LRAFB

73 Electronic Amplifier 1 Turn-in LRAFB

74 Power Supply Amplifier 1 Turn-in LRAFB

75 Circuit card Assy 1 Turn-in Robins AFB, GA


W900KK-10-T-0043

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81 Generator Control Unit 4 Turn-in Tinker AFB

82 Light Source Control 1 Turn-in San Antonio

83 Generator Stator 1 Turn-in Tinker AFB

84 Special Cable Assembly 1 Turn-in Robins AFB, GA

85 Light Indicating Panel 1 Turn-in San Antonio

86 Remote Magnetic Compensator 1 Turn-in Hill AFB

87 Navigation Computer 1 Turn-in Grand Rapids

88 Flight Director Computer 1 Turn-in Tinker AFB

89 Flight Controller 1 Turn-in Tinker AFB

90 Flight Controller 1 Turn-in Tinker AFB

91 Airdrop Computer 1 Turn-in LRAFB


93 ATM A/C Generator 2 Turn-in LRAFB

94 Auto Pilot Box 1 Turn-in LRAFB

95 Auxilary Tank Bladder/Foam 2 Turn-in LRAFB

96 Clam Shells Cowlings 4 Crate/Ship Robins AFB, GA

97 Flight Data Accquisition Unit 1 Turn-in LRAFB

98 Fuel Qty Totalizer/Power Supply 1 Turn-in LRAFB

99 GTC 1 Turn-in LRAFB

100 Horse Collar 4 Crate/Ship Robins AFB, GA

101 Horzontal Stabilizer 1 Crate/Ship Air Force

Academy

102 I/B Flapp Comnnecting Links 14 Crate/Ship LRAFB

103 IFF 1 Turn-in LRAFB

104 KY5-5 RCU 1 Turn-in LRAFB

105 Lt Aileron 1 Ship Robins AFB, GA

106 Lt Elevator 1 Ship Robins AFB, GA

107 Mode "C" / Rt Cargo 1 Turn-in LRAFB

108 Mode "C" Data Converter 2 Turn-in LRAFB

109 Nose Radome Antenna 1 Crate/Ship Robins AFB, GA

110 Radio Reciever/Hog Trough 1 Turn-in LRAFB

111 Radio RT 1 Turn-in LRAFB

112 Receiver Transmitter 1 Turn-in LRAFB

113 Receiver Transmitter/Hog Trough 1 Turn-in LRAFB

114 Rt Elevator 1 Ship Robins AFB, GA

115 Rudder 1 Ship Robins AFB, GA

116 SKE/KY58 Computers Turn-in LRAFB

117 TACAN Coupler 1 Turn-in LRAFB

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118 Transponder/Hog Trough 1 Turn-in LRAFB

119 Vertical Stabilizer 1 Crate/Ship Air Force

Academy

120 Aircraft Wings 2 Ship Robins AFB, GA

Total Components 421

Attch_1_C-130_FuT_PWS

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