Piper PA-28 Cadet Pilot's Operating Handbook
Piper PA-28 Cadet · Pilot's Operating Handbook
Overview
This Pilot's Operating Handbook (POH) is specifically designed for the Piper PA-28 Cadet, providing essential information for pilots operating this aircraft. It includes detailed specifications, operating procedures, and performance data necessary for safe and efficient flight. The handbook serves as a comprehensive reference for both new and experienced pilots, ensuring they have access to critical information regarding the aircraft's systems, limitations, and emergency procedures. The document is structured to facilitate quick reference during flight operations and training, making it an invaluable resource for anyone flying the PA-28 Cadet.
- Wingspan: 36 ft 0 in (10.97 m)
- Maximum Takeoff Weight: 2,550 lbs (1,157 kg)
- Maximum Speed: 125 knots (144 mph)
- Stall Speed: 50 knots (58 mph)
- Fuel Capacity: 50 gallons (189 liters)
Document
Source
Originally published by wayman.edu. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Pilot's Operating Handbook
- Pages
- 235
- File size
- 31 MB
- Publisher
- wayman.edu
Most owners only have the POH. Here's the essential set for the Piper PA-28 Cadet.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
More Piper PA-28 Cadetmanuals & documents
See all 22 →- WARRIOR PA-28-161 PILOT’S CHECKLISTChecklist
- EMERGENCY PROCEDURESEmergency Procedures
- Piper PA28-161 CHECKLIST Warrior IIChecklist
- Piper PA-28 ChecklistChecklist
- AAIB Bulletin: 10/2013Other Documents
- PA-28-161 Warrior II Emergency Procedures ChecklistChecklist
- PA-28-161/181 Private Pilot and Commercial Pilot Operations and ManeuversV Speeds Reference
- CADET AIRPLANE PARTS CATALOGParts Catalog
- warrior-iii-section-6.pdfWeight And Balance
- Piper PA-28-161 Pilot's Operating HandbookPilot's Operating Handbook
- Piper Aircraft PA-28-161 Cadet Airplane Maintenance ManualV Speeds Reference
- EMERGENCY PROCEDURES PIPER PA28/161 WARRIOR II (AFM 13.08.1982)Emergency Procedures
In this document
Aircraft Specifications
The Piper PA-28 Cadet features a low-wing design with a wingspan of 36 feet 0 inches (10.97 m) and a length of 24 feet 0 inches (7.32 m). The maximum takeoff weight is 2,550 lbs (1,157 kg), and it is powered by a Lycoming O-320 engine, producing 150 horsepower.
Operating Limitations
The aircraft has a maximum speed of 125 knots (144 mph) and a stall speed of 50 knots (58 mph). The service ceiling is 14,000 feet (4,267 m), and the fuel capacity is 50 gallons (189 liters), with 48 gallons (182 liters) usable.
Emergency Procedures
In the event of an engine failure during takeoff, the recommended procedure is to maintain control of the aircraft, pitch for best glide speed, and select a suitable landing area. Pilots should also be familiar with the emergency checklist for engine failure and other critical situations.
Weight and Balance
Proper weight and balance calculations are crucial for safe flight operations. The handbook provides detailed charts and formulas to determine the center of gravity and ensure the aircraft is within its weight limits.
Performance Data
The PA-28 Cadet has a takeoff distance of approximately 1,600 feet (488 m) at sea level under standard conditions. The landing distance is around 1,500 feet (457 m) under similar conditions.
Safety notes
- Always perform a preflight inspection before each flight.
- Ensure weight and balance calculations are completed prior to takeoff.
- Be familiar with emergency procedures and checklists.