Piper PA-39 Twin Comanche C/R - Page 87

TWIN COMANCHE C/R
Item
Item
D. Electrical Eauinment
One Battery 12 V, 35 Ampere
Hour
a. Wisco
X
b. Reading R-35
c. Bowers B-34
Two Landing Lights
a. G.E. Model 4509
x b. Westinghouse Model 4509
Rotating Beacon, Whelen
Z Model WRML- 12
Dual Alternators 12 V, 70
Amp., Presto&e ALX8403 With
x
Regulators, Brackets and Relay
Auxiliary Power Receptacle
Installation Per PAC Dwg. 26743
(Includes Power Cable in
*
X
Baggage Area)
*
Red Strobe Anti-Collision Light
Installation in accordance with
Whelen STC SA615EA and Piper
Dwg. 27040. Delegation Option
Authorization EA-1 Approved
Supplement E to Airplane Flight
Manual, Piper Report No. 1605,
required.
White Strobe Anti-Collision Light
Installation in accordance with
Whelen STC SA6 15EA and Piper
Dwg. 27045. Delegation Option
Authorization EA-1 Approved
Supplement E to Airplane Flight
Manual, Piper Report No. 1605,
* ,x required.
ISSUED: November 28,1969
REISSUED: June 1.1970
Weight
Arm Aft
Lbs.
Datum
Cert.
Basis
27.0 16.75 TC AlEA
1 .O ea.
1 .O ea.
86.0 TC AlEA
86.0 TC AlEA
1.4 275.0 TC AlEA
32.0 38.10
TC lE12
6.5 113.34 ,. TCAlEA
3.1
4.8
175.2 STC SA6 15EA
134.4 STC SA6 15EA
REPORT: 1605 PART II PAGE 17
MODEL: PA-39