Emergency Procedures for the Piper PA-32R Saratoga II HP
Piper PA-32R Saratoga II HP · Emergency Procedures
Overview
This document outlines the emergency procedures specifically for the Piper PA-32R Saratoga II HP. It is intended for pilots and crew members to ensure safety during critical situations. The procedures cover various scenarios such as engine power loss during takeoff and in flight, as well as handling engine fires. Each procedure is designed to guide the pilot through the necessary steps to manage emergencies effectively, ensuring the safety of the aircraft and its occupants.
- Maximum Take-Off Weight: 3,600 lbs
- Va: 134 KIAS
- Vne: 191 KIAS
- Engine Power Loss Procedures: Throttle CLOSED, Mixture IDLE CUT OFF
- Engine Fire Procedures: Mixture IDLE CUT OFF, Fuel Selector OFF
- Minimum Airspeed for Power Loss in Flight: 83 KIAS
Document
Source
Originally published by www.dgac.gob.cl. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Emergency Procedures
- Pages
- 3
- File size
- 20 KB
- Publisher
- www.dgac.gob.cl
Most owners only have the POH. Here's the essential set for the Piper PA-32R Saratoga II HP.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
More Piper PA-32R Saratoga II HPmanuals & documents
- SERVICE LETTER NO. 1331Service Manual
- Exhaust Systems Engine Mounts Carb Air Boxes Shrouds Seats Piston Turbine Radial Vintage And More...Systems Description
- Weight & Balance, Performance CalculationWeight And Balance
- Piper Aircraft PA-32R-301/301T Maintenance ManualPilot's Operating Handbook
- Specifications/Performance Standard Equipment Saratoga/Turbo Saratoga PA 32-301/301TSpecifications
- Piper Saratoga PA-32R-301T Normal and Emergency ChecklistsEmergency Procedures
- Performance Data for the Piper PA-32R Saratoga II HPPerformance Data
- EMERGENCY PROCEDURESEmergency Procedures
- Performance Data for the Piper PA-32R Saratoga II HPPerformance Data
- Airworthiness Directives for the Piper PA-32R Saratoga II HPAirworthiness Directives
In this document
Limitations of Operation
This section details the operational limitations for the Piper PA-32R Saratoga II HP, including airspeeds (KIAS) for various phases of flight such as Va (134 KIAS), Vne (191 KIAS), and Vso (63 KIAS). It also specifies weight limits, including a maximum take-off weight of 3,600 lbs and a maximum baggage weight of 200 lbs. Additionally, it outlines engine power limits, including a maximum continuous power of 300 HP and maximum RPM of 2,700.
Emergency Procedures
The emergency procedures section provides critical steps for pilots to follow in case of engine power loss during takeoff, both on the ground and in flight. It includes specific actions such as closing the throttle, applying brakes, and switching fuel tanks. For engine fires, it details the necessary actions to take during start and in flight, emphasizing the importance of shutting off fuel and managing the throttle.
Safety notes
- Always maintain awareness of airspeeds and weight limits during flight operations.
- In case of engine failure, prioritize maintaining control and preparing for a safe landing.
Full document text
1 DEPARTAMENTO “SEGURIDAD OPERACIONAL” SUBDEPARTAMENTO “LICENCIAS” SECCIÓN EVALUACIONES “PIPER PA-32R SARATOGA” “LUIS SPOERER G.” A.- Limitaciones de Operación 1.- Limitaciones KIAS) 3.- Pesos (LBS) Va 3.600 lbs 134 Máximo TAKE-OFF 3.600 Vne 191 Máximo Equipaje 200 Vno 160 Vfe 111 4.- Motor (Potencia Máxima Continua) Vle 132 Limitaciones Operativas de Motor Vlo UP & DN 132/110 Razón HP o BHP 300 Vs 67 Máximas RPM 2.700 Vso 63 Vx 80 Temperatura Cabeza de Cilindros (°F) Vy 93 Máxima 500 Vr 70 Mínima 200 Vapp (Flaps DN) 80 Vplaneo 83 Presión de Aceite (PSI) Max Cross Wind 17 Máxima 115 Mínima 25 2.- Combustible (U.S. GAL) Temperatura de Aceite (°F) Tipo a Utilizar 100/130 Máxima 245 Capacidad Total 107 Mínima 100 Capacidad Usable 102 Presión de Combustible 5.- Limites de Maniobras (Cat. Normal) Máxima 14 Spin (Flaps UP) Prohibido Mínima 0 Escarpados 134 2 B.- Emergency Procedure 1.- ENGINE POWER LOSS DURING TAKEOFF (Airplane on ground) a.- If sufficient runway remains: Throttle CLOSED Brakes APPLY Land straight ahead b.- If not sufficient runway remains: Throttle CLOSED Mixture IDLE CUT OFF Master/ALT OFF Fuel Selector CLOSED Magnetos OFF Brakes AS REQUIRED 2.- ENGINE POWER LOSS DURING TAKEOFF (Airplane in Flight) a.- If sufficient runway remains: Flaps FULL Throttle CLOSED Land straight ahead b.- If not sufficient runway remains: Airspeed 82 KIAS Landing Gear UP Fuel Selector SWITCH OTHER TANK Electric Fuel Pump ON Mixture RICH Alternate Air OPEN 3 3.- ENGINE POWER LOSS IN FLIGHT a.- If at low altitude: Airspeed MAINTAIN 83 KIAS MIN Prepare for power off landing b.- If altitude permite: Fuel Selector SWITCH TO TANK CONTAINING FUEL Electrical fuel pump ON Mixture RICH Alternate Air OPEN Engine Gauge CHECK FOR INDICATION OF CAUSE OF POWER LOSS 4.- ENGINE FIRE DURING START Starter CRANK ENGINE Mixture IDLE CUT OFF Throttle OPEN Electric Fuel Pump OFF Fuel selector OFF Abandon if fire continues 5.- ENGINE FIRE IN FLIGHT Source of fire CHECK Fuel selector OFF Throttle CLOSED Mixture IDLE CUT OFF Electrical Fuel Pump OFF Heater and Defroster OFF Proceed with power off landing procedure.