FOR TRAINING PURPOSES ONLY!
Piper PA-23 Apache · Pilot's Operating Handbook
Overview
This document serves as a Pilot's Operating Handbook (POH) for the Piper PA-23 Apache. It is intended for training purposes, providing essential information for pilots operating this aircraft model. The handbook includes critical operational data, performance specifications, and procedural guidelines necessary for safe and effective flight operations. It is designed to assist both new and experienced pilots in understanding the aircraft's systems and capabilities.
- Maximum takeoff weight: 3,800 lbs (1,724 kg)
- Cruise speed: approximately 180 knots
- Stall speed: 60 knots
- Range: about 700 nautical miles
- Fuel capacity: 60 gallons (227 liters)
Document
Source
Originally published by duboisaviation.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Pilot's Operating Handbook
- Pages
- 64
- File size
- 16 MB
- Publisher
- duboisaviation.com
Common. Rarer than 8% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Piper PA-23 Apache.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the PA-23 Apache 150 to your watchlist and track it in one place.
More Piper PA-23 Apachemanuals & documents
- SERVICE BULLETIN NO. 1299Service Bulletins
- INSTALLATION INSTRUCTIONS FOR HEATER KIT #1 P/N CD11005K1Weight And Balance
- SERVICE LETTER NO. 1141Maintenance Manual
- PIPER PA-23-150/160 ApacheSystems Description
- AAIB Bulletin: 1/2007 G-MOLY EW/G2006/07/24Other Documents
- Piper Parts CatalogChecklist
- Specifications for the Piper PA-23 ApacheSpecifications
- Piper PA-23 Apache Supplemental Type CertificateSupplemental Type Certificate
- Airplane Flight ManualFlight Manual
- Piper Apache 235 SpecsChecklist
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In this document
Aircraft Specifications
The Piper PA-23 Apache features a twin-engine configuration with a maximum takeoff weight of 3,800 lbs (1,724 kg). The aircraft is powered by two Lycoming O-360 engines, each producing 180 horsepower. The wingspan measures 38 feet 0 inches (11.58 m), and the overall length is 27 feet 6 inches (8.38 m).
Performance Data
The PA-23 Apache has a maximum cruise speed of approximately 180 knots and a stall speed of 60 knots. The aircraft has a range of about 700 nautical miles with a maximum fuel capacity of 60 gallons (227 liters). The climb rate is approximately 1,200 feet per minute under standard conditions.
Operating Procedures
Pilots must perform a thorough preflight inspection before each flight, including checks of fuel levels, control surfaces, and engine oil. The engine start procedure involves ensuring the mixture is rich, the throttle is set to idle, and the ignition switch is in the 'both' position.
Emergency Procedures
In the event of an engine failure, pilots should maintain control of the aircraft and attempt to land straight ahead. If time permits, the pilot should identify a suitable landing area and execute a controlled descent.
Weight and Balance
Proper weight and balance calculations are critical for safe flight operations. The maximum weight for the PA-23 Apache is 3,800 lbs, and pilots should ensure that the center of gravity remains within specified limits for optimal performance.
Safety notes
- Always perform a preflight inspection before each flight.
- Maintain weight and balance within specified limits.
- In case of engine failure, prioritize control and landing area selection.
Full document text
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