1983-1983 Piper Aerostar 602P
PIPER AEROSTAR 602P · Pilot's Operating Handbook
Overview
The document provides detailed specifications and performance information for the Piper Aerostar 602P aircraft. It includes data on engines, weights, dimensions, performance metrics, and standard equipment.
- The Aerostar 602P is powered by two Lycoming 290 hp engines.
- Maximum take-off weight is 6000 lbs.
- Cruise speed at best power is 247 knots.
- Usable fuel capacity is 165.5 gallons.
- The aircraft features hydraulic retractable landing gear.
- Standard empty weight is 4125 lbs.
- Service ceiling is 28,000 feet.
- The aircraft includes dual automatic turbo-chargers.
Document
Source
Originally published by aeroresourcesinc.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Pilot's Operating Handbook
- Year ·
- 1983
- File size ·
- 4.5 MB
- Publisher ·
- aeroresourcesinc.com
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Cabin width (in) ·
- 45.5
- Wing area sqft ·
- 36.7
- Cabin height (in) ·
- 46.5
- Cabin length (in) ·
- 119.5
- Oil capacity (gal) ·
- 30
- Luggage capacity (lb) ·
- 240
- Maximum ramp weight (lb) ·
- 6000
- Standard useful load (lb) ·
- 1904
- Standard empty weight (lb) ·
- 4125
- Maximum landing weight (lb) ·
- 6000
- Maximum takeoff weight (lb) ·
- 6000
Performance
- Cruise range (nm) ·
- 1094
- Cruise speed (kt) ·
- 247
- Maximum speed (kt) ·
- 247
- Rate of climb (fpm) ·
- 1800
- Service ceiling (ft) ·
- 28000
V-speeds
- VS_KIAS ·
- 77
Weight & balance
- Maximum ramp weight (lb) ·
- 6000
- Standard useful load (lb) ·
- 1904
- Standard empty weight (lb) ·
- 4125
- Maximum landing weight (lb) ·
- 6000
- Maximum takeoff weight (lb) ·
- 6000
What is the 1983-1983 Piper Aerostar 602P?
The 1983-1983 Piper Aerostar 602P is a pilot's operating handbook for the PIPER AEROSTAR 602P, dated 1983.
Where does the 1983-1983 Piper Aerostar 602P come from?
This copy of the 1983-1983 Piper Aerostar 602P was originally published by aeroresourcesinc.com and is hosted on Sprinkle as a free, searchable reference copy.
What year was the 1983-1983 Piper Aerostar 602P published?
The 1983-1983 Piper Aerostar 602P — the PIPER AEROSTAR 602P pilot's operating handbook on file — is dated 1983.
Most owners only have the POH. Here's the essential set for the PIPER AEROSTAR 602P.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More PIPER AEROSTAR 602Pmanuals & documents
In this document
Engines
The Aerostar 602P is equipped with two Lycoming 10-540-AA 1A5 engines, each rated at 290 BHP at 2425 RPM.
Weights
The maximum ramp weight is 6000 lbs, with a standard empty weight of 4125 lbs and a useful load of 1904 lbs.
Dimensions
The aircraft has a wingspan of 36.7 ft, a length of 34.8 ft, and a height of 12.1 ft.
Performance
Cruise speeds range from 201 to 247 knots depending on power settings and altitude.
Standard Equipment
The aircraft includes dual flight controls, hydraulic flaps, and a complete circuit breaker panel.
Pressurization System
The cabin is equipped with a pressurization system that maintains a cabin altitude of 4.25 psi.
Safety notes
- Actual performance depends on pilot techniques and operating surfaces.
- It is the pilot's responsibility to operate within approved limits of design gross weight and center of gravity.
- Take-off and landing performance is optimum under standard conditions.
Full document text
· -),./ ••• ••• Y-..- Piper Aircraft Corporation 1983 Specifications/ Perform ance Standard Equipment Aerostar 602P Piper Aircraft Corporation Aerostar 602P Specifications 290 BHP @ 2425 RPM 1800 ENGINES Manufacturer Model Rating (hp @ rpm) Maximum Continuous Operating Power (MCOP) Recommended TBO (hrs.) WEIGHTS Maximum Ramp Weight (Ibs./kg) Maximum Take-off Weight (Ibs./kg) Maximum Landing Weight (lbs./kg) Standard Empty Weight (Ibs./~g) (Includes: unusable fuel. full operating fluids and full oil) Standard Useful Load (Ibs./kg.) WING AREA AND LOADINGS Wing Area (ft.2/m2) Wing Loading (lb./ft.2)/(kg./m2) Power Loading (Ib./hp)/(kg./hp) Lycoming 10-540- AA 1A5 6029/2734 6000/2721 6000/2721 4125/1871 1904/864 178/16.5 33.7/164.5 10.3/4.7 DIMENSIONS Wing Span (ft./m) Length (ft./m) Height (ft./m) Cabin Length (in./cm) Cabin Width (in./cm.) Cabin Height (in./cm.) Passenger Door Size (in./cm) Luggage Door Size (in./cm.) USABLE FUEL (gaL/I) OIL CAPACITY (gal./eng.) (Lleng) BAGGAGE Luggage Capacity (Ibs./kg) Luggage Space (ft.3/m3) 36.7/11.2 34.8/10.6 12.1 /3.7 119.5/303.5 45.5/115.6 46.5/118.1 28 x 45/71.1 x 114.3 22 x 24/55.9 x 61.0 165.5/626.5 3/11.4 240/108.9 30/.85 262/485 1755/535 302/92 Cruise Speed (kts)/(km/h) 247/457 242/448 226/419 228/422 224/415 210/389 203/376 201/372 191/354 Performance MAXIMUM SPEED (MCOP) (kts.)/(km/h) (TAS at Average Cruise Weight) CRUISING SPEEDS (Best Power) (TAS at Average Cruise Weight of 5500 Ibs.) Power Cruise Altitude % (ft./m) 75 25,000/7620 75 23,000/7010 75 15.000/4572 65 25.000/7620 65 23.000/701 0 65 15.000/4572 55 25,000/7620 55 23.000/7010 55 15.000/4572 CRUISE RANGE (Best Economy) for 165.5 Gallons Usable (626.5 Liters) Includes Allowance for Fuel Used During Start. Taxi, Take-off Climb. Descent and a 45 Minute Reserve at Economy Fuel Mixture. Power Cruise Altitude Range % (ft./m) (nm/km) 65 15,000/4572 1094/2026 65 23.000/7010 1098/2034 65 25,000/7620 1078/1997 55 15.000/4572 1143/2117 55 23.000/7010 1137/2106 55 25.000/7620 1112/2059 RATE OF CLIMB at 6000 Ibs. (2721 kg) Two Engines (MCOP) - Sea Level (fpm/mpm) Single Engine (MCOP) - Sea Level (fpm/mpm) RATE OF CLIMB at 5000 Ibs. (2268 kg) Two Engines (MCOP) - Sea Level (fpm/mpm) Single Engine (MCOP) - Sea Level (fpm/mpm) STALL SPEEDS - 6000 Ibs. (2721 kg) Power off, Flaps Down (kts.) (km/h) IAS SERVICE CEILING 6000 Ibs. (2721 kg) Two Engines (MCOP) (ft./m) Single Engine (MCOP) (ft./m) Single Engine (MCOP) (ft./m) @ 5000 Ibs. (2268 kg) TAKE-OFF DISTANCE Normal procedure at 6000 Ibs. (2721 kg) Ground Run (ft./m) Total distance over 50-ft. obstacle (ft./m) Normal procedure at 5000 Ibs. (2268 kg) Ground Run (ft./m) Total distance over 50 ft. obstacle (ft./m) LANDING DISTANCE - Flaps 45° Normal procedure at 6000 Ibs. (2721 kg) Ground Roll (ft./m) Total distance over 50-ft. obstacle (ft./m) Normal procedure at 5000 Ibs. (2268 kg) Ground Roll (ft./m) Total distance over 50-ft. obstacle (ft./m) 2342/714 583/178 77/143 28,000/8534 12.900/3932 20,750/6325 1800/549 2250/686 1350/411 1688/515 1217/371 2076/633 1022/312 1809/551 Standard Equipment POWER PLANT AND ACCESSORIES Two Lycoming 290 hp 10-540-AA 1A5-1 ,800 hour- TBO Engines Complete Internal Corrosion Proofing Dual Automatic Turbo-Charger System Dual Ignition System with 1200 Series Magnetos Ground Service Electrical Receptacle (Ground APU Receptacle) Hydraulic Pump Injection Type Fuel System Long Range Fuel System - 165.5 Gallons Usable Fuel Overvoltage Protector Two Electric Auxiliary Fuel Pumps Two Engine Driven Gyro Pressure Pumps Two Engine Driven Variable Orifice Fuel Pumps Two Bleed Air Coolers Two Fuel Strainers Two Full Feathering Constant Speed Hartzell 3-Bladed 78" Diameter Propellers Two Full Flow Oil Filters Two High Capacity Oil Coolers Two Sonic Venturi Flow Limiters Twenty-Four Volt DC, 24 Ampere-Hour Battery System Two 70 AMP Alternators FLIGHT DECK Airspeed Indicator Alternate Static Source Alternator Failure Warning Lights Auxiliary Fuel Pump Switches Cabin Heater, push-pull heat controls Capacitance Type Fuel Quantity System Complete Circuit Breaker Panel (resettable type push-puII breaker) Complete Dual Flight Controls including Copilot's Brakes Fuel Pressure Gauge Dual Exhaust Temperature Gauge Dual Fuel Flow Gauges, Transducer Type Dual Fuel Selectors w/Off, On, and Crossfeed Dual Gyro Pressure Gauge Dual Manifold Pressure Gauge Dual Tachometer Dual 3-Way Engine Gauges: Oil Temperature, Oil Pressure and Cylinder Head Temperature Eight Day Clock Heater Fail Light Annunciator Panel Crossfeed Annunciator Electric Elevator Trim and Panel Mounted Indicator Gauge Electric Rudder Trim and Panel Mounted Indicator Gauge Electro-Hydraulic Nose Wheel Steering and Shimmy Damper Flight Hour Meter Four Landing Gear Position Indicator Lights Full Engine Controls: Throttles, Propellers, and Mixtures High Visibility Rocker Type Electrical Switches Hydraulic Landing Gear Control Hydraulic Shut Off Switch Hydraulic Wing Flap Control with Panel Mounted Indicator Internally Lighted Magnetic Compass Low Fuel Warning System Map Light. Dual Intensity Outside Air Temperature Gauge Parking Brake Pilot and Copilot Microphone Jacks Pilot and Copilot Headset Jacks Radio Call Plaque Radio Light Dimmer Control Rate of Climb Indicator (VSI) Safety Padded Glare Shield Sensitive Altimeter Three-inch Attitude and Directional Gyros (pneumatic) Tilted Instrument Panel Turn Coordinator Variable Intensity Red and White Instrument Panel Lighting Volt-Ammeter with Individual Alternator Load Selection Windshield Defroster Pilot's Check List INTERIOR Aircraft Log Book Airplane Flight Manual Carpeted and Lighted Baggage Compartment Deluxe Curtains Double-Pane Windows Six Velour Seats w/ Armrests Pilot & Copilot Inertia Reel Shoulder Harness Full Reclining Passenger Seats Individual Cabin Air Ventilators Individual Passenger Reading Lights Key Locked Baggage Compartment Matching Velour/Vinyl Side Panels
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Pilot and Copilot Eyebrow Windows Pilot and Copilot Floor Scuff Plates Pilot and Copilot Sun Visors Super Soundproofing Thermostatically Controlled Variable Cabin Heat Tinted Passenger Windows Emergency Exit Two Engine Log Books Ventilation Fan Weight and Balance Plotter Wall to Wall Deep-Pile Color Coordinated Carpet Standard Equipment Continued EXTERIOR Aircraft Tow Bar Deluxe Polyurethane Paint Four Exterior Colors Standard. Base Color, Plus Three Trim Colors Dual Landing/Taxi lights Emergency Locator Transmitter (ELT) Heated Pitot Heavy Duty Dual Caliper Disc Brakes Hydraulic Fowler Flaps Hydraulic Retractable Landing Gear Steerable Nose Wheel 3 Convenient Quick Drain Fuel Strainers 3 Light Strobe System 3 Navigation lights PRESSURIZATION SYSTEM Cabin Altitude and Differential Pressure Indicator Cabin Rate of Climb Indicator Cabin Door Pressure Seal Cabin Outflow Pressure-Regulating Valve Cabin Pressure Safety and Dump Valve Cabin Water Drain System Emergency Exit Pressure Seal Variable Rate Cabin Pressure Controller 4.25 psi Pressurization System Cabin Altitude Warning Light PRODUCT SUPPORT Piper Warranty Form Piper Service Center Directory Inspection Form The performance information is based on an airplane flown at gross weight under standard sea level atmospheric conditions except as noted and based on the latest data available at the time of publication approval. Take-off and landing performance is optimum. Actual performance depends on pilot techniques, operating surfaces and other factors. It is the responsibility of the pilot to determine that all operations are conducted within approved limits of design gross weight, center of gravity, and in accordance with the FAA-approved Airplane Flight Manual which is the only official source of operating parameters and performance information. In accordance with GAMA format, range provides for taxi, take-off, climb at MCP, cruise at stated mixture and descent with 45-minute reserve at maximum range power. Empty weight in- cludes unusable fuel, full operating fluids and full oil. Piper Aircraft Corporation reserves the right to make changes in specifications, materials, equipment or prices at any time without prior notice or to discontinue models as required. Your Piper Aerostar Dealer has listings of a wide variety of optional equipment and avionics. Items most frequently chosen by owners are packaged for factory installation. I.PIPER AIRCRAFT CORPORATION LOCK HAVEN. PENNSYLVANIA 17745 995·3·107 10/1/82 Printed in USA @ a BANGOR PUNTA Company i) MEMBER OF GAMA