HIGHEST PERFORMANCE MARKET AVAILABLE AIRCRAFT

VERSATILE – MODERN - AFFORDABLE

IA-63 PAMPA III

TRAINING ANDLIGHT ATTACK CAPABILITIES IN ONE AIRCRAFT

TRAINING ANDLIGHT ATTACK CAPABILITIES IN ONE AIRCRAFT

VERSATILITYDESIGN & TECHNOLOGYPERFORMANCEPRODUCTIONMAINTENANCE

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VERSATILITYBASIC-ADVANCED TRAINING AND LIGHT ATTACK AIRCRAFT

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VERSATILITYTRAINING AIRCRAFT

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.Transition and Air Work Aerobatics

.Basic Instrument Flying

.Formation / Instrument Flying

.Tactical Mission Training

.Basic Through Advanced Training

.LIFT training

VERSATILITYLIGHT ATTACK AIRCRAFT

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.Five Stations for Weapon Delivery

.Air-to-Air; Air-to-Ground Missions

.Tactical Reconnaissance and Surveillance Light Close Air Support Missions.Low Level Interdiction.Long range stand alone surveillance.Border patrol

DESIGN & TECHNOLOGYNEXT GENERATION AIRCRAFT

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ESPECIFICACIONESTÉCNICASDESIGN & TECHNOLOGYTECHNICAL SPECIFICATIONS

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DimensionesPrincipales

WingspanHeightLength

Alar surfaceAlar max load

UndercarriageGauge

Base

9,69 m (31 ft 9 in)4.30 m (14 ft 1 in)10.90 m (35 ft 9 in)

15.63 m2 (168 ft2)320 kg/m2 (66 Lb/ft2)

2,66 m (8 ft 9 in)4.42 m (14 ft 6 in)

Propulsor

MakerType / No

static thrust (ISA)specific consumption

Honeywell Turbofan TFE 731-40-2N1780 daN (4000 Lb)(0,46 Lb/Lb/h)

Pesos

Operating empty 2,960 kgNormal TOW 3,890 kg

5,200 kg Maximum TOWComb Fuselage 327 kg

Comb Ala 755 kgInt Comb average 757 kg

Comb int Maximum 1080 kg

(6,520 Lb)(8,570 Lb)(11,038 Lb)(418 l - 720 Lb)(965 l-1665 Lb)(970 l-1670 Lb)(1383 l- 2380 Lb)

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DESIGN & TECHNOLOGYNEXT GENERATION AIRCRAFT

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.Full Glass Cockpit-Mil 1553 Integrated Digital Avionics

.Integrated NAV/COMM/ATTACK System, HOTAS.

.Integrated Stores Management System (SMS).

.Data Transfer System (DTS).

.Mission Planning Station.

.Data Link – EVA virtual avionics – TARGO Helmet

DESIGN & TECHNOLOGYAIRCRAFT

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.Structural Design based upon MIL-STD-1530A and MIL-A-8860A Standards..Quick Access Doors to Critical Equipment..Descent Touch-Down Speed at 3,6 m/seg..Fatigue Safe Life at 8.000 hs. Planned Upgrade up to 14.000 after inspection.

DESIGN & TECHNOLOGYELECTRIC AND HYDRAULICSYSTEM

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.Electrical: Primary Power Supply Generated by 11.5 KW Starter Generator. .2 in Parallel x 27 Amp-Hour Sealed Lead Acid Batteries..30 Minutes In-Flight Emergency Backup..Servo Assisted Flight Controls..Dual Redundant Hydraulic System..Ram Air Turbine for Hydraulic Emergency.

DESIGN & TECHNOLOGYRELIABLE POWER PLANT

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.Turbofan Honeywell TFE 731-40-2N.

.Digital Electronic Control (DEEC).

DESIGN & TECHNOLOGYCOCKPIT

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.Excellent Visibility from both stations.

.Pressurized Cabin.

.Anti-G System.

.Standard Zero-Zero Ejection Seats.

.Canopy Fragilization for Emergency Ground Egress.

DESIGN &TECHNOLOGYTACTICAL CAPACITY GROWTH(CONCEPT)

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Pod ISRMulti mission

Radar APG 67Modified nose

Virtual Radar

Air to Air Missiles

External Tanks

Chaff & flare

RWRData Link ACTS

HMD

IRSTModified nose

PERFORMANCEPROVEN MISSIONEFFECTIVENESS

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PERFORMANCE

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Max level speed (28,200 ft)V Long range Cruise (30,000 ft) V Stall-Flap extended (clean)V Stall – Flap ext (w/External stores)Max Operating speed

470 KTAS 870 Km/hr 350 KTAS 650 Km/hr 85 KCAS 157 Km/hr 98 KCAS 182 Km/hr M = 0.8 480 KCAS

Take off distance (ISA-S/L- Normal fuel- 8,300 lb)Landing distance (ISA-S/L- 7,710 lb)Service ceilingMax Rate of Climb (8,300 lb)Max Range (Max Internal fuel)Max roll rate

1,410 ft 430 m1,510 ft 460 m 42,300 ft 12,900 m 6,050 ft/min 1,850 m/min 1,250 n miles 2,315 Km 200° /sec

PERFORMANCEFLIGHT ENVELOPE - SPEED

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IA63-Level

IA63-Limit

Flight envelope - n=1

0

5000

10000

15000

20000

25000

30000

35000

40000

45000

50 100 150 200 250 300 350 400 450 500 550

Alt

itud

- ft

Mach Max.0.8

VD Max. 480 KCAS

V KTAS

350 KTASExternal storescruise

430 KTASMax Level speed

H=0

85 KCASMin Speed

450 KTASClean cruise

A wide range of Speeds(85 KCAS a 450 KTAS) allowsIA-63 III Pampa FulfillBasic/Advanced Training Syllabiand Light Attack Missions.

PERFORMANCELIGHT ATTACKAIRCRAFT

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.Designed to operate at +4.5/-2 G with maximum external load..Ventral station: 30 mm conformed canon pod, DEFA 553. .Four removable under wing pylons: Alkan type 6095/96 C..Each wing station can carry: inner station 970 lbs, outer station 640 Lbs..Integrated digital Attack/Nav/Attack, 1553 /ARINC 429 Buss with Data Link..Air-to- Air, Air-to-Ground capacity..Several external stores configurations up to 1200 Kg (Standard NATO)..Photographic pod..Under wing tanks are not required for long range missions (internal fuel: 1380 Lit.)..2x 300 liters external Drop-tanks (Option).

PERFORMANCELIGHT ATTACK ROLE

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1 Ventral Cannon Pack (DEFA 553 30 mm / 145 rounds).2 ETNA TMP-5 or COLIBRI Twin Gun Pack: 2x 7,62 mmmachine guns.3 MK 82 500-lb (227 Kg) HE bomb.4 Multiple ejector rack MK 81 250-lb (113 Kg) HE bomb.5 MK 81 250-lb (113 Kg) HE bomb6 2.75 in (68 mm) folding-fin-aircraft rockets (FFAR)7 Combined rocket launcher / Practice bombsdispenser, CBLS 200 type.8 4-lb (1,8 Kg) practice bomb.9 5-lb (2,27 Kg) practice bomb.10 ALKAN type 531 cartridge launcher.11 74 mm cartridges (40).12 ALKAN type 6095C inboard wing pylon(970 lb- 440kg hard point loading capability).13 ALKAN type 6096C outboard wing pylon(640 lb-290Kg hard point loading capability).

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1011

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IA63 III typical Artillery

PERFORMANCELIGHT ATTACK MISSIONS

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AIR-to-GROUND (HI-LO-HI) (Light Close Air Support)Max TOGW 11,460 lb 5,200 kgMilitary load 2,200 lb 1,000 kgArmament Cannon30 mm/ 2 X MK81; 2 X MK82(5 Minutes weapon delivery)Radius of action (Internal fuel): 420 nm (with descent leg) 340 nm (without descent leg)

AIR-to-AIRE (HI-HI) (Typical Gunnery)Max TOGW 8,815 lb 4,000 kgMilitary load 559 lb 254 kgArmament Gun pod 30 mm / 145 rounds(5 Minutes Dogfight) Radius of action (Max internal fuel): 460 nm

FERRY RANGEMax TOGW 9,300 lb 4,200 kgClean external loadMax internal fuel: 1,250n nm

30,000

ft

420 n

milla

s30 Min Reserve

30,000

ft

460 n

milla

s30 Min Reserve

30,000

ft

1,250

n m

illas

30 Min Reserve

PRODUCCIÓNPRODUCTION LINE

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.High rate production line up and running.

.Supply chain in place.

.18 IA 63 II-40 re-engined / FAA.

.40 IA 63 PAMPA III in production / FAA.

PRODUCCIÓNSUPPLY CHAIN

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Equipment supported by someof the most relevant aircraftmanufacturers worldwide(World Class).

MAINTENANCEEXCELLENT OPERATIVE PERFORMANCE AND LOW MAINTENANCE COSTS

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MAINTENANCEMAINTENANCE CONCEPT

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.Based on “On Condition” and “Inspection and Repair as necessary” Concept..90% of the Components at Ground Level..Components Grouped by Similar Functions within compartments with removable panels..Engine Inspection Schedule - TBO: MPI: 1,500 FH CZI: 3,500 FH.Requires 2.27 DMMH/FH (Direct Maintenance Man Hour per Flight Hour) up to Scheduled Maintenance (Nivel I - O)..Overall Maintenance Workload required up to Depot Maintenance Level is only 3.80 DMMH/FH.

MAINTENANCERELIABILITY ANDMAINTAINABILITY

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Design Focused on Reliability.During Design phase Off-the-Shelfcomponents were selected.

Easy Access.Design focused on easy access to everycomponent (150 Access areas).

Minimum Maintenance Time / Man Hours.Maximum use of components withBuilt-In test (BIT) capability and Autotests for failure report.

Quick Pre Flight Inspection/Access to Critical Functions.Simplified schedule for daily inspectionsQuick engine change maintenance (in lessthan one hour) (QEC).

IA-63 PAMPA IIIVERSATILE - MODERN - AFFORDABLE

.Proven Aircraft, More than 30 Years of Operation..Exceptional Visibility and Maneuverability..State-of-the-Art Integrated Digital Avionics (NAV-COM-ATTACK) (Standard Bus 1553B) with DATA LINK /TARGO helmet..New Engine: TFE 731- 40-2N / Digital Control and Maintenance Parameters Monitoring..Simplified Maintenance and Low Operative Cost. .Integrated Logistics Support. .Complete Maintenance Program, Training Included..Advanced Variants Under Development.

COMMERCIAL CONTACTPhone: (54-351) 466-8736Fax: (54-351) 466-8734Email: jofreg@fadeasa.com.arWebsite: www.fadeasa.com.ar