Piper PA-39 Twin Comanche C/R User Manual

TWIN COMANCHE C/R
Weight Arm Aft
Lbs.
Datum
Cert.
Basis
E. Interior Equipment
Heater, Janitrol Model 20D35
X
Per PAC Dwg. 2672 1
29.0
15.0
FAA TSO C20
AutoControl III, Autopilot
Inst. Mitchell AK 16 1, in
accordance with Piper Dwg.
26733, Delegation Option
Authorization, EA-1 Approved
Supplement B to Airplane Flight
Manual, Piper Report No. 1605,
*
required.
4.0 113.0 TC AlEA
AltiMatic IIIB, Autopilot
Installation in accordance with
Piper Dwg. 26884, Delegation
Option Authorization EA-1.
Approved Supplement D to
Airplane Flight Manual, Piper
* ,Y Report No. 1605, required.
19.3 119.0 TC AlEA
Glar Ban Lights Per PAC
* I Dwg. 2687 1
Delegation Option Authorization
Approved Airplane Flight
Manual, Piper Report No. 1605
Dated November 28, 1969, Reissued
Neglect Wt. Change
i’
TC AIEA
.i
X
Yune 1, 1970 (Serial No. 39-l
and UP)
Delegation Option Authorization
Approved Supplement A, Dated
November 28, 1969 to Airplane
Flight Manual, Piper Report No.
*
1605. Required when Oxygen
System installation is installed.
ISSUED: November 28,1%9
REISSUED: June 1,197O
TC-AlEA
TC AlEA
REPORT: 1605 PART II PAGE 19
MODEL: PA-39

Piper PA-39 Twin Comanche C/R Specifications

General

Manufacturer	Piper Aircraft
Model	PA-39 Twin Comanche C/R
Type	Light twin-engine aircraft
Engines	2
Crew	1
Seating Capacity	4
Max Takeoff Weight	3, 600 lb (1, 633 kg)
Powerplant Output	160 hp each
Capacity	4
Wingspan	36 ft 0 in (10.97 m)
Service Ceiling	20, 000 ft (6, 100 m)
Fuel Capacity	100 US gal (379 L)