Bonanza A36 Checklist

ONE Bonanza-A36 Normal Takeoff ONE

1. Seats -- POSITION AND LOCK Seat Backs -- UPRIGHT2. Seat Belts and Shoulder Harnesses -- FASTEN3. Parking Brake -- SET4. All Avionics -- OFF5. Circuit Breakers -- IN6. Landing Gear Handle -- DOWN; Safety System - CHECK ( if installed )7. Flaps -- UP8. Cowl Flaps -- OPEN9. Light Switches -- Rotating Beacon -- ON; LIGHTS AS REQUIRED10. Fuel Selector Valve -- CHECK DETENT OPERATION; Select Fullest Tank11. Fuel Tip Crossfeed -- OFF12. Battery & Alternator Switches -- ON If External Power is Used turn Alt. Sw. -- OFF13. Fuel Quantity Indicators ( Fuel Gages ) -- CHECK QUANTITY

*** CAUTION ***Do not Engage Starter for More Than 30 Seconds in any 4 Minute Period.

NOTE: During Hot Starts, The Auxiliary Fuel Pump Is Turning on Momentary AfterStarting to Purge System, Then Turn OFF.1. Mixture -- FULL RICH2. Propeller -- HIGH RPM3. Throttle -- FULL OPEN4. Auxiliary Fuel Pump -- ON until FUEL FLOW PEAKS then OFF (Approximately 5 Secs)5. Throttle -- Approximately 3 TURNS OPEN6. Propeller Area -- CLEAR7. Magneto/Start Switch--START POSITION; release to on position when engine starts

NOTE: If Engine Has Been Overprimed, Mixture -- Idle Cut Off, Throttle -- Open, Magneto Start SwitchStart Position, As Engine Starts Reduce -- Throttle to Idle and Advance Mixture control to FULL RICH8. Throttle -- 1000 ~1200 RPM9. Oil Pressure -- CHECK (Min 30 PSI / Max 100 PSI) 9a. Ext. Power -- (if used) DISCONNECT10. Ammeter -- Check for CHARGING11. All Engine Gauges -- CHECK12. Panel Annuciators -- CHECK

*** CAUTION ***The Ammeter Indication should be less than 25% of Full Charge at 1000 to 1200 RPM Within Two Minutes,

With no Additional Electrical Equipment on. If Not, Turn off the Battery and Alt. Switches, DON'T TAKE OFF!

1. Brakes -- RELEASE AND CHECK2. Avionics Equipment -- ON, AS REQUIRED3. Lights -- AS REQUIRED

*** CAUTION ***Do not Operate Engine Above 1200 RPM Until Oil Temperature Reaches 75*F

1. Seat Belts & Shoulder Harness -- CHECKNOTE: All Seats Must Be in The Upright Position

2. Parking Brake -- SET3. Radios -- CHECK4. Engine Instruments -- CHECK5. Flight Instruments -- CHECK AND SET CONT.

ONE This Check List is not to be used as a Substitution for the Owners Manual ONECopyright: R. Hebert 2004

BEFORE STARTING

STARTING ENGINE

AFTER STARTING & TAXI

BEFORE TAKEOFF

TWO Bonanza-A36 Normal Takeoff TWO6. Ammeter -- CHECK; for stabilized indication between 0 & 25% of full charge @ 1000 to 1200 RPM7. Auxiliary Fuel Pump -- CHECK OFF8. Throttle -- 1700 RPM 8a. Vacuum Gauge -- 4.3 to 5.9 in HG9. Propeller -- EXERCISE to obtain approx. 300 to 400 RPM drop; return to high RPM10. Magneto -- CHECK at 1700 RPM (RIGHT First, difference not to exceed 50 RPM, Max. drop 150 RPM)11. Trim Set A) AILERON -- NEUTRAL

B) ELEVATOR -- 3* (6* IF ONLY FRONT SEATS ARE OCCUPIED)12. Flaps -- UP13. Door and Window -- SECURED14. Flight Controls -- CHECK FOR PROPER DIRECTION AND FREEDOM OF MOVEMENT15. Mixture -- FULL RICH (or as required by field elevation)16. Brakes -- RELEASED17. Auto-Pilot -- CHECK AP TEST LIGHTS, AP Heading, AP NAV/Speaker, AP VS UP/DOWN18. Instruments -- CHECK (make final check of manifold pressure, fuel flow, and RPM)

at the start of takeoff run.)

1. Power -- SET TAKE-OFF POWER ( Mixture - SET as Required by Field Elevation )2. Brakes -- RELEASE THEN ACCELERATE to Recommended Speeds

NOTE: Prior to Rotation: Last Check ALL GREEN3. Landing Gear -- RETRACT (when Positive rate of climb is established and insufficient

runway remains for landing.)

Maximum Continuous-- Full Throttle, 2700 RPMCruise Climb -- 25 in. Hg (or full throttle) 2500 RPM1. Engine Temperatures - MONITOR2. Power -- SET AS DESIRED3. Mixture -- SET FUEL FLOW

1. Cowl Flaps -- CLOSED2. Power -- SET3. Mixture -- SET FUEL FLOW

Lean the Mixture and Note the Point on the Indicator that the Temperature peaks andStarts to Fall

A. Cruise (lean) Mixture -- Increase the Mixture until the EGT Shows a Drop of25*F Below Peak on the Rich side of Peak

B. Best Power Mixture -- Increase the Mixture Until the EGT Shows a Drop of100*F Below Peak on the Rich Side of peak

QuickCruise Altitude RPM/MP KTAS RPM/MP KTAS RPM/MP KTAS

Info 4,000 Ft. 25/23.5 166 23/22.9 154 21/22.6 1416,000 Ft. 25/23.0 168 23/22.4 157 21/22.1 1438,000 Ft. 25/21.7 165 23/21.7 158 21/21.6 144

10,000 Ft. 25/20.0 163 23/20.0 154 21/20.2 14112,000 Ft. 25/18.3 161 23/18.4 150 21/18.5 134

Standard Conditions Zero WindSee Page Four for the Complete Power Setting List.

TWO This Check List is not to be used as a Substitution for the Owners Manual TWO

75% POWER 65% POWER 55% POWER

BEFORE TAKEOFF

Normal TAKE-OFF

Normal CLIMB

Normal CRUISE

Leaning using EGT

POWER SETTINGS

ONEIFR Bonanza-A36 IFR Takeoff ONEIFR

1. Normal Outside Pre-Flight plus IFR-Instrument Specifics2. Pitot-Static System -- HEAT ON, Port Clear, No Blockage (Airspeed, Altimeter, VSI)3. Antennas -- ADF, Transponder, Beacon, VOR, ELT, Comms, GPS (Secure)4. Fuel -- Check NO WATER/CONTAMINATION, CORRECT COLOR, CAPS Secure5. VOR Equipment Check/IFR Operations - Sec 91.171 = Check LOGBOOK [Ground +- 40 ] [Air +- 60 ]

1. Seats -- POSITION AND LOCK Seat Backs -- UPRIGHT2. Seat Belts and Shoulder Harnesses -- FASTEN3. Parking Brake -- SET4. All Avionics -- OFF5. Circuit Breakers -- IN6. Landing Gear Handle -- DOWN; Safety System - CHECK ( if installed )7. Flaps -- UP8. Cowl Flaps -- OPEN9. Light Switches -- Rotating Beacon -- ON; NAV, STROBE LIGHTS AS REQUIRED10. Fuel Selector Valve -- CHECK DETENT OPERATION; Select Fullest Tank11. Fuel Tip Crossfeed -- OFF12. Master Battery & Alternator Switches -- ON (If External Power is Used turn Alt. Sw. -- OFF)13. Electric Turn Coordinator -- GYRO ON, No Mechnical Noise/Grinding14. Fuel Quantity Indicators ( Fuel Gages ) -- CHECK QUANTITY

*** CAUTION ***Do not Engage Starter for More Than 30 Seconds in any 4 Minute Period.

NOTE: During Hot Starts, The Auxiliary Fuel Pump Is Turning on Momentary AfterStarting to Purge System, Then Turn OFF.1. Mixture -- FULL RICH2. Propeller -- HIGH RPM3. Throttle -- FULL OPEN4. Auxiliary Fuel Pump -- ON until FUEL FLOW PEAKS then OFF (Approximately 5 Secs)5. Throttle -- APPROXIMATELY 3 TURNS OPEN6. Propeller Area -- CLEAR7. Magneto/Start Switch--START POSITION; release to on position when engine starts

NOTE: If Engine Has Been Overprimed, Mixture -- Idle Cut Off, Throttle -- Open, Magneto Start SwitchStart Position, As Engine Starts Reduce -- Throttle to Idle and Advance Mixture control to FULL RICH8. Throttle -- 1000 ~1200 RPM9. Oil Pressure -- CHECK (Min 30 PSI / Max 100 PSI) 9a. Ext. Power -- (if used) DISCONNECT10. Ammeter -- CHECK for Charging11. All Engine Gauges -- CHECK

*** CAUTION ***The Ammeter Indication should be less than 25% of Full Charge at 1000 to 1200 RPM Within Two Minutes,

With no Additional Electrical Equipment on. If Not, Turn off the Battery and Alt. Switches, DON'T TAKE OFF!

1. Airspeed Indicator -- ZERO, Needle at 12:00 within 5 Minutes2. Attitude Indicator -- HORIZON BAR Erect within 5 Minutes, SET Miniature Airplane3. Altimeter -- SET with ATIS, within 75 feet field elevation4. Turn Cordinator -- WINGS LEVEL, BALL Centered, NO RED FLAG5. Heading Indicator -- Set to match MAGNETIC COMPASS6. Vertical Speed Indicator -- ZERO, Gently TAP, Not More than 100' Difference/Note Difference7. Magnetic Compass -- NO LEAKS, FLUID NORMAL, NO BUBBLES/DIP, FREE FLOWING Movement 8. Digital Clock -- CLOCK Working

ONEIFR This Check List is not to be used as a Substitution for the Owners Manual ONEIFR

OUTSIDE PRE-FLIGHT

BEFORE STARTING

STARTING ENGINE

AFTER STARTING - INSTRUMENT CHECK "6 Pack"

TWOIFR Bonanza-A36 N9365Q IFR Takeoff TWOIFR

1. Brakes -- RELEASE AND CHECK, ATTITUDE INDICATOR -- Slight NOSE DOWN ( < 5 o )2. Turn Coordinator -- ON TURNS, WINGS DIP In Direction of TURN, BALL Move to Outside Turn3. Magnetic Compass & Heading Indicator -- SHOULD AGREE-Numbers Smaller/Smaller or Larger/Larger

*** CAUTION ***Do not Operate Engine Above 1200 RPM Until Oil Temperature Reaches 75*F

1. Seat Belts & Shoulder Harness -- CHECKAll Seats Must Be in The Upright Position2. Parking Brake -- SET3. Radios -- CHECK4. Engine Instruments -- CHECK5. Flight Instruments -- CHECK AND SET CONT.6. Ammeter -- CHECK; for stabilized indication between 0 & 25% of full charge @ 1000 to 1200 RPM7. Auxiliary Fuel Pump -- CHECK OFF8. Throttle -- 1700 RPM 8a. Vacuum Gauge -- 4.3 to 5.9 in HG9. Propeller -- EXERCISE to obtain approx. 300 to 400 RPM drop; return to high RPM10. Magneto -- CHECK at 1700 RPM ( RIGHT First , difference not to exceed 50 RPM, Max. drop 150 RPM)11. Throttle -- LOW IDLE at 700 RPM 11a. Auxillary Vacuum Gauge -- CHECK 4.3 to 5.9 in HG11. Trim Set A) AILERON -- NEUTRAL

B) ELEVATOR -- 3* (6* IF ONLY FRONT SEATS ARE OCCUPIED)12. Flaps -- UP13. Door and Window -- SECURED14. Flight Controls -- CHECK FOR PROPER DIRECTION AND FREEDOM OF MOVEMENT15. Mixture -- FULL RICH (or as required by field elevation)16. Brakes -- RELEASED17. Auto-Pilot -- CHECK AP TEST LIGHTS, AP Heading, AP NAV/Speaker, AP VS UP/DOWN18. Instruments -- CHECK & SET (check Marker Beacon Lights, Nav, Marker Beacon, DME, ADF) 19. Pitot Heat -- ON (Anytime visible moisture or flying through clouds)

1. Power -- SET TAKE-OFF POWER ( Mixture - SET as Required by Field Elevation )2. Brakes -- RELEASE THEN ACCELERATE to Recommended Speeds

NOTE: Prior to Rotation: Last Check ALL GREEN (final check of Manifold Pressure, Fuel Flow, and RPM)3. Landing Gear -- RETRACT (when Positive rate of climb is established and insufficient

runway remains for landing.)

NOTE: Maximum Continuous-- Full Throttle, 2700 RPM (Not more than 2 minutes)Cruise Climb -- 25 in. Hg (or full throttle) 2500 RPM1. Engine Temperatures - MONITOR2. Power -- SET AS DESIRED3. Mixture -- SET FUEL FLOW

1. Cowl Flaps -- CLOSED2. Power -- SET3. Mixture -- SET FUEL FLOW

QuickCruise Altitude RPM/MP KTAS RPM/MP KTAS RPM/MP KTAS

Info 4,000 Ft. 25/23.5 166 23/22.9 154 21/22.6 1416,000 Ft. 25/23.0 168 23/22.4 157 21/22.1 1438,000 Ft. 25/21.7 165 23/21.7 158 21/21.6 14410,000 Ft. 25/20.0 163 23/20.0 154 21/20.2 14112,000 Ft. 25/18.3 161 23/18.4 150 21/18.5 134

Standard Conditions Zero WindSee Page Four for the Complete Power Setting List.

TWOIFR This Check List is not to be used as a Substitution for the Owners Manual TWOIFR

75% POWER 65% POWER 55% POWER

IFR TAXI CHECK

BEFORE IFR TAKE-OFF

Normal IFR TAKE-OFF

Normal IFR CLIMB

Normal IFR CRUISE

POWER SETTINGS

THREE Beechcraft A36 Landing Procedures THREE

1. Altimeter -- SET Use Local ATIS/ASOS or Local Weather2. Cowl Flaps -- CLOSED3. Power -- AS REQUIRED Avoid Prolong Idle Settings and Low Cylinder Head Temperatures.4. Mixture -- ENRICH AS REQUIRED

1. Seats, Belts, Harness -- ADJUST and LOCKNOTE: All Reclining Seats Must be in the Upright Position During Landing.

2. Fuel Selector Valve -- SELECT THE TANK WITH THE MOST FUEL3. Cowl Flaps -- AS REQUIRED4. Mixture -- FULL RICH (Or as Required for Field Elevation)5. Landing Gear -- DOWN & CHECK --- 3 GREEN (Observe Max. Extension Speed). VLE = 153 kts/176 mph6. Landing and Taxi Lights -- AS REQUIRED7. Flaps -- DOWN (Observe Maximum Extension Speed). VFE = 123 kts/141 mph8. Establish Landing Approach Speed -- 90 kts / 104 mph9. Propeller -- High RPM

1. Airspeed -- 90 kts - 104 mph ( With Flaps and Gear Down )2. Wing Flaps -- LOWERED4. Trim -- ADJUST5. Touchdown -- MAIN WHEELS FIRST6. Landing Roll -- LOWER NOSE WHEEL GENTLY7. Braking -- MINIMUM REQUIRED

1. Power -- FULL THROTTLE and 2700 RPM2. Airspeed -- 76 kts / 87 mph Until Clear of Objects, Then Trim to Normal Climb Speed3. Wing Flaps -- UP4. Landing Gear -- UP5. Cowl Flaps -- OPEN

1. Landing and Taxi Lights -- AS REQUIRED2. Wing Flaps -- UP3. Trim Tab -- SET TO "U"4. Cowl Flaps -- OPEN

1. Parking Brake -- SET2. Avionics Power Switch - Electrical Equipment -- OFF3. Throttle -- CLOSE4. Mixture -- IDLE CUT OFF (pull full out)5. Ignition Switch -- OFF After Engine Stops6. Master Switch -- OFF7. Control Lock -- INSTALL8. Install Wheel Chocks & Release Brakes (if left unattended)

THREE This Check List is not to be used as a Substitution for the Owners Manual THREE

After Landing

Shutdown

Descent

Before Landing - GUMPS

Normal Landing - GUMPS

Balked Landing

FOUR FOURKIAS/MPH

VA 140 / 161VNO 166 / 191VNE 204 / 235VFE 123 / 142VLO 153 / 176VS1 56 / 64VR 70 / 81 VX 78 / 90VY 96 / 110

MARKING KIAS/MPH RangeWhite Arc 56 - 123 64 - 142 Full Flap Operating Range. Lower Limit is Max. Weight VSO in

landing configuration. Upper Limit Max. w/Flaps ExtendedWhite Triangle 153 176 Maximum Speed for Approach Flaps 10 Degrees OnlyGreen Arc 62-166 62-166 Normal Operating Range. Lower Limit is Max. Weight VS at

forward CG. Upper limit Is Maximum Structural Cruising SpeedYellow Arc 166-204 166-204 Operation must be conducted with CAUTION

and only in SMOOTH airRed Line 204 204 Maximum Speed for ALL operations.

Pressure Alt. ISA-36F STANDARD ISA+36F ISA-36F STANDARD ISA+36F75%Power GPH GPH GPH 75%Power GPH GPH GPH2500 RPM MP ^ KTS MP ^ KTS MP ^ KTS 2500 RPM MP ^ KTS MP ^ KTS MP ^ KTS

1000 ft. 23.6/15.3/158 24.3/15.2/161 24.8/15.2/164 7000 ft. 22.0/15.2/166 22.6/14.9/168 22.6/14.4/1682000 ft. 23.4/15.2/160 24.1/15.2/162 24.6/15.2/165 8000 ft. 21.7/15.0/166 21.7/14.5/166 21.7/14.0/1663000 ft. 23.1/15.2/160 23.8/15.2/164 24.3/15.2/167 9000 ft. 20.8/14.4/164 20.9/14.0/168 20.8/13.8/1654000 ft. 22.8/15.2/162 23.5/15.2/166 24.0/15.2/168 10000 ft. 20.0/13.9/163 20.0/13.6/163 20.0/13.0/1635000 ft. 22.5/15.2/163 23.2/15.2/166 23.7/15.1/169 11000 ft. 19.2/13.2/162 19.2/13.1/162 19.2/12.7/1616000 ft. 22.2/15.2/164 23.0/15.2/168 23.5/15.0/169 12000 ft. 16.3/13.1/161 18.3/12.7/161 18.3/12.7/161

65%Power GPH GPH GPH 65%Power GPH GPH GPH2300 RPM MP ^ KTS MP ^ KTS MP ^ KTS 2300 RPM MP ^ KTS MP ^ KTS MP ^ KTS






FOUR FOUR

Beechcraft A36 Airspeed LimitationsManeuvering Speed No Abrupt Movements

Maximum Landing Gear Operation Do not operate landing gear above this speed

This Check List is not to be used as a Substitution for the Owners Manual

Never Exceed in Any Operation

Do Not Extend Flaps (20-300) Above this Speed

Delivers Gain in Altitude in Shortest Time

NORMAL CRUISE POWER SETTINGS

Best Rate-of-Climb

Speed at which the Airplane Lifts Off

Best Angle-of-Climb Delivers Gain in Altitude in Shortest Distance

Max. Structural Cruising SpeedNever Exceed SpeedMax. Flaps Extend Speed

Design Speeds

In Smooth Air Only

Stalling Speed Speed at which the Airplane StallsRotation Speed

AIRSPEED INDICATOR MARKINGSDescription

FIVE FIVE

1. Throttle -- CLOSED ABORT TAKEOFF2. Braking -- MAXIMUM3. Fuel Selector Valve -- OFF4. Battery and Alternator Switches -- OFF

NOTE: Landing Straight Ahead is usually advisable. If sufficient altitude is available for maneuvering,accomplish the following procedure:1. Fuel Selector Valve -- SELECT OTHER TANK (Feel for Detent)2. Auxiliary Fuel Pump -- ON3. Mixture -- FULL RICH, then LEAN AS REQUIRED4. Magnetos -- CHECK LEFT, RIGHT, THEN BOTH

NOTE: The most probable cause of engine failure would be loss of FUEL FLOW or Improper Functioning of the ignition system.

NOTE: If No Restart:1. SELECT Most Favorable LANDING SITE.2. The use of LANDING GEAR is dependent on the terrain where landing must be made.

1. Mixture -- FULL RICH, then LEAN as required2. Magneto/Start Switch -- "BOTH" Position (Check to Verify)

1. Fuel Flow Gauge -- CHECKNOTE: If fuel flow is abnormally low:

A) Mixture -- FULL RICHB) Auxiliary Fuel Pump -- ON (then OFF if Performance does not improve in a few moments)2. Fuel Quantity Indicator -- CHECK for fuel supply in tank being used

NOTE: If fuel tank being used is empty:A) Fuel Tank Selector Valve -- SELECT OTHER FUEL TANK (feel for detent)

1. Fuel Selector Valve -- SELECT TANK MORE NEARLY FULL (feel for detent)2. Throttle -- RETARD3. Mixture Control -- FULL RICH4. Auxiliary Fuel Pump -- ON until power is regained, then OFF

(Leave ON if Engine Driven Fuel Pump is inoperative)5. Throttle -- ADVANCE to desired power6. Mixture -- LEAN as required

1. Power -- IDLE (1300 rpm)2. Propeller -- HIGH RPM (2500 rpm)3. Landing Gear -- DOWN4. Airpeed -- ESTABLISH 153 KIAS/176 MPH

1. Landing Gear -- UP2. Flaps -- UP3. Cowl Flaps -- CLOSED 4. Propeller -- PULL for LOW RPM 5. Airspeed -- GLIDE 110 KIAS/126 MPH

NOTE: Glide distance is approximately 1.7 nautical miles (2 statute miles), per 1000 feet of altitude above the terrain.

FIVE FIVE

Beechcraft A36 Emergency Procedures


ENGINE FAILURE - DURING TAKEOFF ROLL

ENGINE FAILURE - AFTER LIFTOFF IN FLIGHT

ENGINE CHECKS - ROUGH RUNNING ENGINE

ENGINE CHECKS - LOSS OF ENGINE POWER

ENGINE - AIR START PROCEDURE

EMERGENCY DESCENT

MAXIMUM GLIDE CONFIGURATION

SIX SIX

NOTE: When assured of reaching the landing site selected, and on Final Approach:1. Airspeed -- ESTABLISH 76 TO 81 KTS2. Fuel Selctor Valve -- OFF3. Mixture -- IDLE CUT-OFF4. Magneto/Start Switch -- OFF5. Flaps -- AS REQUIRED6. Landing Gear -- DOWN or UP (Depending on Terrain)7. Battery and Alternator Switches -- OFF

NOTE: If possible, choose firm sod or foamed runway. Make a normal approach, using flaps as necessary.When sure of reaching the selected landing spot:1. Throttle -- CLOSED2. Mixture -- IDLE CUT-OFF3. Battery, Alternator and Magneto/Start Switches -- OFF4. Fuel Selctor Valve -- OFF5. Keep Wings Level During Touchdown6. Get Clear of Airplane as soon as possible after it stops

1. Throttle -- RETARD TO RED LINE2. Airspeed -- REDUCE3. Oil Pressure -- CHECK

NOTE: If loss of oil pressure was the cause of overspeed, the engine will seize after a short period of operation4. Land -- SELECT NEAREST SUITABLE SITE and follow LANDING EMERGENCIES procedure.

NOTE: An inoperative alternator will place the entire electrical operation of the airplane except engineignition on the battery. An alternator failure will be indicated by the illumination of the ALT OUTwarning light, located on the instrument panel below the flight instruments.The warning light will not illuminate until the alternator output is almost zero. A verification ofalternator malfunction would be a discharge shown on the ammeter.There is no indication of overvoltage except that the warning light will illuminate as thoughthe alternator is out.

1. Verify Alternator Out with Ammeter -- AMMETER WILL SHOW DISCHARGENOTE: If the ammeter does not show a discharge, a malfunction in the Warning Light System is indicated,

and the Alternator Switch should be left ON.2. If Ammeter Shows a Discharge: ALTERNATOR SWITCH -- OFF MOMENTARILY, THEN ON (this resets the overvoltage relay)If the warning light does not illuminate, continue to use the Alternator.3. If the Warning Light Illuminates, Alternator Switch -- OFF4. Nonessential Electricl Equipment -- OFF to conserve battery power

NOTE: If the cabin door is not locked it may unlatch in flight. This may occur during or just after takeoff.The door will trail open approximately 3 inches but the flight characteristics of the airplane will not be affected, except the rate of climb will be reduced.1. Unlatched Door in Flight -- Cabin Door Panel Annuciator will ILLUMINATE2. Door trail open -- RETURN TO FIELD in a NORMAL MANNER3. During Landing flare-out -- Have Passenger HOLD DOOR to PREVENT it SWINGING OPEN4. Once Landed -- Passenger CLOSE DOOR/LATCH LOCKED5. Pilot Cross-check -- Cabin Door Panel Annuciator OFF

SIX SIX



LANDING WITHOUT POWER

LANDING GEAR RETRACTED - WITH POWER

SYSTEMS EMERGENCIES - PROPELLER OVERSPEED

SYSTEMS EMERGENCIES - ALTERNATOR-OUT

ALTERNATOR WARNING LIGHT ILLUMINATED

UNLATCHED DOOR IN FLIGHT

SEVEN SEVEN

NOTE: Manual extension of the landing gear is facilitated by first reducing speed, then proceed as follows:1. Landing Gear Motor -- CIRCUIT BREAKER OFF (pull-out, Right Subpanel)2. Landing Gear Switch Handle -- DOWN Position3. Handcrank Handle Cover -- REMOVE (at rear of front seats)4. Gear Handcrank -- ENGAGE and TURN COUNTERCLOCKWISE AS FAR AS POSSIBLE (approximately 50 turns)5. If Electrical Sys Operative -- CHECK LANDING GEAR POSITION LIGHTS AND WARNING HORN (check LANDING GEAR RELAY circuit breaker engaged)6. Handcrank -- DISENGAGE. (Always keep it stowed when not is use)

CAUTION: The manual gear extension system is designed to lower the landing gear only.

NOTE: DO NOT ATTEMPT TO RETRACT THE GEAR MANUALLY.

Do not operate the Landing Gear electrically with the handcrank engaged as damage to themechanism could occur. After emergency landing gear extension, do not move any landing gearcontrols or reset any switches or circuit breakers until the airplane is on jacks as failuremay have been in the gear up circuit and gear might retract on the ground.

NOTE: After practice manual extension of the landing gear - gear can only be retracted etectrically, as follows:1. Handcrank -- CHECK, STOWED2. Landing Gear Motor Circuit Breaker -- IN (right Subpanel)3. Landing Gear Switch Handle -- UP (gear up red-light)

NOTE: An alternate induction air door, spring-loaded to the closed position, is located downstream fromthe induction air filter. If the induction air filter becomes blocked (e.g., ice, etc.), the differential airpressure normally opens the alternate induction air door to provide induction air from the bottomof the engine compartment. If the alternate induction air door becomes stuck in the closed position,it can be opened by pulling and releasing the T-HANDLE located directly below the Propeller Control Knob. This T-HANDLE is placarded: ALTERNATE AIR PULL AND RELEASE

NOTE: THE EMERGENCY STATIC AIR SOURCE SHOULD BE USED FOR CONDITIONS WHERE THE NORMAL STATICSOURCE HAS BEEN OBSTRUCTED.When the airplane has been exposed to moisture and/or icing conditions especially on the ground,the possibility of obstructed static ports should be considered. Partial obstruction will result in therate of climb indication being sluggish during a climb or descent. Verification of suspectedobstruction is possible by switching to the emergency system and noting a sudden sustainedchange in rate of climb. This may be accompanied by abnormal indicated airspeed and altitudechanges beyond normal calibration differences.

NOTE: Whenever any obstruction exists in the Normal Static Air System or the Emergency Static Air Systemis desired for use:1. Pilot's Emergency Static Air Source -- Switch to ON EMERGENCY2. For Airspeed Calibration and Altimeter Correction -- REFER to PERFROMANCE Section in POH

NOTE: The Emergency Static Air Valve - in the NORMAL position when the system is not in use or needed.

WARNING: Spins are prohibited. If a SPIN is entered inadvertently:Immediately move the Control Column FULL FORWARD and simultaneouslyApply FULL RUDDER OPPOSITE the Direction of the SPIN.Continue to hold this control position until ROTATION STOPS and thenNEUTRALIZE ALL CONTROLS and execute a Smooth PULLOUT.AILERONS should be NEUTRAL and THROTTLE in IDLE Position at all times during recovery.

SEVEN SEVEN



LANDING GEAR - MANUAL EXTENSION

LANDING GEAR WARNING

LANDING GEAR - RETRACTION AFTER PRACTICE EXT.

INDUCTION SYSTEM BLOCKAGE

EMERGENCY STATIC AIR SOURCE SYSTEM

SPINS

EIGHT EIGHT

NOTE: If your not flying a published holding pattern, your holding instructions from the controller willalways tell you three key things:1. The FIX to HOLD AT (Standard Holding Pattern Circuit ~ 3 Minutes)2. The DIRECTION of HOLDING including Radial or Airway3. The Time - called the EFC, or EXPECT FURTHER CLEARANCE TIME to get further ATC instructions4. The ALTITUDE to MAINTAIN, if different from current altitude5. The DIRECTION of TURNS -- Assumed STANDARD RIGHT Unless otherwise instructed6. The LEG LENGTH in miles if asked for distance instead of time

NOTE: Begin Timer: Abeam the Station or Wings Level

NOTE: Procedure Turn Review: Common form of Course Reversal , make turn on side of course shownby barbed arrow to stay in protected airspace. (Turn Away From Barb)Standard Procedure Turn: 450 - 1800 - 450 Radial1. Fly 2 minutes out -- Execute 450 Turn to Protected Side Help2. Fly 1 minutes out -- Execute 1800 Turn back towards course3. As needle nears approach heading -- Turn 450 to intercept final approach course

Tear-Drop Procedure Turn: 300 - 2100 to Intercept1. Fly 2 minutes out -- Execute 300 Turn to Protected Side2. Fly 1 minutes out -- Execute 2100 Turn to intercept course

Holding Pattern in lieu of Procedure Turn:1. The holding pattern is completed when aircraft is established on the inbound course

800 Procedure Turn: 800-Then 2600

1. Fly 2 minutes out -- Execute 800 Turn to Protected Side2. Fly 1 minutes out -- Execute 2600 Turn back to intercept approach course

NoPT = No Procedure Turn requiredEIGHT EIGHT

Beechcraft A36 NOTES


HOLDING PATTERNS

PROCEDURE TURN REVIEW

ReciprocalHelp

360 180010 190020 200030 210040 220050 230060 240070 250080 260090 270100 280110 290120 300130 310140 320150 330160 340170 350180 360

Bonanza A36 Checklist

Documents

Transcript of Bonanza A36 Checklist