PIPER CHEYENNE IIXL PA-31
PIPER CHEYENNE IIXL · Checklist
Overview
This document is a checklist for the Piper Cheyenne IIXL aircraft, detailing operational limitations, emergency procedures, and performance specifications. It serves as a quick reference for pilots to ensure safe operation and adherence to guidelines.
- Maximum takeoff weight is 9,474 lbs.
- Total fuel capacity is 374 U.S. gallons.
- Vne is 242 KIAS.
- Va is 184 KIAS.
- Emergency procedures include engine securing and fire response.
- C.G. limits vary based on weight.
- Minimum fuel pressure is 5 PSI.
- Maximum fuel pressure is 50 PSI.
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Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at gob.cl. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Checklist
- File size ·
- 21 KB
- Copy found at ·
- gob.cl
- Language ·
- es
Specifications & performance
Extracted from this document.
Specifications
- Baggage aft (lb) ·
- 200
- Baggage fwd (lb) ·
- 300
- Max takeoff weight (lb) ·
- 9474
- Fuel capacity total (gal) ·
- 374
- Fuel capacity useable (gal) ·
- 366
Performance
- V1 kias ·
- 91
- Va kias ·
- 184
- Vs kias ·
- 86
- Vx kias ·
- 95
- Vy kias ·
- 116
- Vmo kias ·
- 242
- Vne kias ·
- 242
- Vso kias ·
- 77
- Vmca kias ·
- 91
- Vsse kias ·
- 118
- Vxse kias ·
- 113
- Vyse kias ·
- 118
- Vfe 15 deg kias ·
- 181
- Vlo retraction kias ·
- 139
- Vapp flaps 40 deg kias ·
- 104
- Vle vlo extension kias ·
- 153
V-speeds
- V1_KIAS ·
- 91
- VA_KIAS ·
- 184
- VS_KIAS ·
- 86
- VX_KIAS ·
- 95
- VY_KIAS ·
- 116
- VMO_KIAS ·
- 242
- VNE_KIAS ·
- 242
- VSO_KIAS ·
- 77
- VMCA_KIAS ·
- 91
- VSSE_KIAS ·
- 118
- VXSE_KIAS ·
- 113
- VYSE_KIAS ·
- 118
- VFE_15_DEG_KIAS ·
- 181
- VLO_RETRACTION_KIAS ·
- 139
- VAPP_FLAPS_40_DEG_KIAS ·
- 104
- VLE_VLO_EXTENSION_KIAS ·
- 153
Weight & balance
- Baggage aft (lb) ·
- 200
- Baggage fwd (lb) ·
- 300
- Cg fwd 5850 lbs (in) ·
- 124.0
- Cg fwd max ramp (in) ·
- 129.6
- Cg rwd 5850 lbs (in) ·
- 136.0
- Cg rwd max ramp (in) ·
- 136.0
- Cg fwd max landing (in) ·
- 128.8
- Cg fwd max takeoff (in) ·
- 129.5
- Cg rwd max landing (in) ·
- 136.0
- Cg rwd max takeoff (in) ·
- 136.0
- Max takeoff weight (lb) ·
- 9474
Common. More common than 91% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the PIPER CHEYENNE IIXL.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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—In this document
Operations Limitations
Details speed limits, weight limits, fuel capacities, and C.G. limits for the Piper Cheyenne IIXL.
Emergency Procedures
Outlines steps for handling engine failure, fires, and other emergencies during flight and on the ground.
Weight and Balance
Specifies maximum weights and corresponding center of gravity limits for various configurations.
Fuel Specifications
Describes the type of fuel to be used and its pressure requirements.
Engine Failure Procedures
Provides specific actions to take in the event of engine failure during takeoff and in-flight.
Electrical Emergencies
Details procedures for handling electrical fires and battery overtemperature situations.
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Safety notes
- Maintain directional control after engine failure during takeoff.
- Do not feather the prop on the second engine during flameout.
- Check electrical load during battery overtemperature.
- Use oxygen system in case of smoke or fumes in the cabin.
- Perform emergency descent with gear and flaps retracted or extended as specified.
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Full document text
1 DEPARTAMENTO “SEGURIDAD OPERACIONAL” SUBDEPARTAMENTO “LICENCIAS” SECCIÓN EVALUACIONES “PIPER CHEYENNE IIXL PA-31” “AGROSUPER” CC-CPR” A.- Operations Limitations 1.- Speed (Kias) Va 184 Vne 242 Vmo 242 Vfe 15° 181 Vle/Vlo (Extension) 153 Vlo (Retraction) 139 Vmca 91 Vs 86 Vso 77 Vx 95 Vy 116 Vsse 118 Vxse 113 Vyse 118 V1 91 Vapp (flaps 40°) 104 3.- Weight (Lbs) Máximo TAKE-OFF 9.474 Baggage FWD 300 Baggage AFT 200 4.- Start 30 Seconds On 1 Minute Off 30 Seconds On 1 Minute Off 30 Seconds On 30 Minutes Cooling 5.- C.G. PESOS FWD RWD 5.850 or less 124.0 136.0 9.474 (max takeoff) 129.5 136.0 9.000 (max landing) 128.8 136.0 9.540 (max Ramp) 129.6 136.0 2.- Fuel (U.S. GAL) Tipo a Utilizar JET-A Capacidad Total 374 Capacidad Utilizable 366 Presión Combustible (PSI) Mínima 5 Máxima 50 2 B.- EMERGENCIES PROCEDURES 1.- ENGINE SECURING PROCEDURE Power Lever IDLE Prop Control FEATHER Condition Lever STOP Generator OFF 2.- ENGINE FIRE OR DAMAGE a.- In Flight: Firewall Shutoff PULL Condition Lever STOP Prop Control FEATHER Generator OFF b.- On Ground: Firewall Shutoff (Af. Eng.) PULL Condition Lever STOP 3.- ENGINE FAILURE DURING TAKEOFF a.- BEFORE ROTATION (Below 91 Kias) Power Levers IDLE Brakes AS REQUIRED If Insufficient Runway for safe stop: Condition Lever STOP Fire wall shutoff valves CLOSE Battery Master OFF 3 b.- AFTER ROTATION (101 Kias or above) Airspeed 101 KIAS MIN Directional control MANTAIN Power Lever MAXIMUN (620 SHP) Landing Gear RETRACT Inoperative Engine IDENTIFY AND VERIFY Prop (Inop. Engine) FEATHER 4.- ENGINE FIRE ON GROUND Condition Lever STOP Fire wall shutoff valve CLOSE Bleed air (inop. Engine) OFF ENGINE FIRE IN FLIGHT Affected engine IDENTIFY AND VERIFY Power (affected engine) IDLE Generator switch OFF Bleed air (affected engine) OFF Prop (affected engine) FEATHERED Condition lever OFF Fire wall shutoff valve (unless Practicing) OFF 5.- ENGINE FLAMEOUT (2ND ENGINE) Power Lever IDLE Prop Control DO NOT FEATHER Condition Lever STOP 6.- OVERSPEED PROPELER Power Lever IDLE Prop control FEATHER Condition lever STOP 4 7.- BATTERY OVERTEMP Electrical load CHECKED Battery Master OFF 8.- ELECTRICAL FIRE Oxigen System ON DON MASK Flashlight (at night) LOCATE Dome Lights (at night) ON Battery master OFF Generators OFF 9.- SMOKE OR FUMES IN CABIN Oxygen System ON DON MASK Cabin Press DUMP 10.- EMERGENCY DESCENT a.- Gear And Flaps Retracted: Power Lever IDLE Prop Control FORWARD b.- Gear And Flaps Extended: Power Lever IDLE Prop Control FULL FORWARD










