Piper Cheyenne 31t1 Maintenance Manual Download

  

Piper Cheyenne III PA-42 761-523 Service Maintenance Manual 1979 thru 1998. This 1561 pages illustrated Maintenance Manual in Pdf Download for the 1979 thru 1998 Piper Cheyenne III PA-42 and Cheyenne IIIA PA-42-720 Part Number 761-523.Contents below:INTRODUCTIONAEROFICHE EXPL. If you plan on accessing your ATP publications on a mobile device, you will need to download the ATP Aviation Hub mobile app. The Hub mobile app can be downloaded from the Apple, Google, or Windows stores, at no charge. PA-31T Cheyenne PA-31T Cheyenne II PA-31T1 Cheyenne I PA-31T1 Cheyenne IA PA-31T2 Cheyenne II XL Piper Service Manual/ Piper Maintenance Manual Part Number 753-825 (PR780907) dated 1978 with revision to October 15, 1997. Has 1068 pages long. Piper PA31T Cheyenne I – Checklist Before Power-up Flight Plan LOADED Flight Controls (All Axis) TEST Brakes and Parking Break TEST and Parking Break SET Doors OPEN Battery Switch OFF Seat Belts OFF (Down) Fuel Pump Switches OFF (Middle) Avionics OFF Propeller FULL FORWARD Mixture CUTOFF Power-up Battery Switch ON. EFM, LLC is not liable for the accuracy, effectiveness or safe use of any aircraft manual or publication and does not warrant that any aircraft manual or publication contains current revisions. Aircraft manuals and publications required for any reason other than historical or research purposes should be obtained from the original equipment.

PA-31T Cheyenne
PA-31T1 Cheyenne in landing configuration
RoleTurboprop
ManufacturerPiper Aircraft
First flight29 August 1969
Produced1974–1985[citation needed]
Number built823
Developed fromPiper PA-31 Navajo
VariantsPiper PA-42 Cheyenne

The Piper PA-31T Cheyenne is a turboprop development of the earlier PA-31P Pressurized Navajo.

  • 2Operators

Development[edit]

Piper owners should subscribe to the free Piper Publication Notification Service to receive an email alerting you when new service letters, service bulletins or change notices are issued for your airplane. Aircraft Technical Publishers (ATP) is the exclusive provider and distributor of electronic publications for Piper Aircraft. FREE Aircraft Manuals Cessna, Piper. Upload them here. DOWNLOAD HERE: Models: Years: Type Of Manual: Click Here: L-21A military version of the Super Cub 125, 125 hp Lycoming 0-290-II. Revised Oct 1955: Erection and Maintenance Manual: Click Here: Piper PA-18 150 SuperCub Parts Catalog: Aug 15, 1988: Parts Manual: Click Here: Piper 180D.

Originally, the aircraft was an upgraded version of the Pressurized Navajo equipped with two Pratt & Whitney Canada PT6A-28 turboprop engines. Later, the aircraft was further refined and developed, including aerodynamic improvements and fuselage extensions. The PA-31T led to the development of the PA-42 Cheyenne III and IV.

Operators[edit]

Military operators[edit]

Mauritania
Download
  • Mauritanian Air Force[1]
United States
  • United States Department of Defense.[2]

Variants[edit]

PA-31T Cheyenne
Initial production version, powered by two 620-shp (462-kW) Pratt & Whitney Canada PT6A-28 turboprop engines.
Piper PA-31T Cheyenne
PA-31T-1
Original designation of the PT-31T Cheyenne I. Powered by 500-shp (373-kW) Pratt & Whitney Canada PT6A-II turboprop engines.
PA-31T Cheyenne II
Improved version, renamed version of original powered by two 620-shp (462-kW) Pratt & Whitney Canada PT6A-28 turboprop engines.
PA-31T2 Cheyenne IIXL
Stretched version, powered by two 750-shp (559-kW) Pratt & Whitney Canada PT6A-135 turboprop engines.

Specifications[edit]

Data from Jane's All the World's Aircraft 1976–77 [3]

General characteristics

  • Crew: 2
  • Capacity: 4–6 passengers
  • Length: 34 ft 8 in (10.57 m)
  • Wingspan: 42 ft 814 in (13.011 m) (over tip tanks)
  • Height: 12 ft 9 in (3.89 m)
  • Wing area: 229 sq ft (21.3 m2)
  • Airfoil: NACA 632-415 at root, 63A212 at tip
  • Empty weight: 4,870 lb (2,209 kg)
  • Max takeoff weight: 9,000 lb (4,082 kg)
  • Fuel capacity: 382 US gal (318 imp gal; 1,450 L) usable fuel
  • Powerplant: 2 × Pratt & Whitney Canada PT6A-28 turboprops, 620 shp (460 kW) each
  • Propellers: 3-bladed Hartzell HC-BTN-3B constant-speed propellers, 7 ft 9 in (2.36 m) diameter

Piper Cheyenne 31t1 Maintenance Manual Download Windows 7

Performance

  • Maximum speed: 326 mph (525 km/h, 283 kn) at 11,000 ft (3,400 m)
  • Cruise speed: 244 mph (393 km/h, 212 kn) at 25,000 ft (7,600 m) (econ. cruise)
  • Stall speed: 88 mph (142 km/h, 76 kn) (flaps down)
  • Range: 1,702 mi (2,739 km, 1,479 nmi) (econ. cruise, 45 min reserves)
  • Service ceiling: 29,000 ft (8,800 m)
  • Rate of climb: 2,800 ft/min (14 m/s)
  • Takeoff run to 50 ft (15 m): 1,980 ft (600 m)
  • Landing run from 15 ft (15 m): 1,860 ft (570 m)

See also[edit]

Related development

Aircraft of comparable role, configuration and era

References[edit]

Piper Cheyenne Ii

  1. ^'World Air Forces 1987 pg. 72'. flightglobal.com. Retrieved 3 April 2019.
  2. ^Tom, Kaminsky (2000). The United States military aviation directory. Airtime Publishing Inc. ISBN978-1-880588-29-1.
  3. ^Taylor, John W.R. (1976), Jane's All The World's Aircraft 1976–77, London: Jane's Yearbooks, pp. 358–359, ISBN0-354-00538-3

External links[edit]

Wikimedia Commons has media related to Piper aircraft.

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