Piper PA-39 Twin Comanche C/R User Manual

TWIN COMANCHE C/R
SECTION 1
LOG OF REVISIONS
Revision Revised Pages
Description and Revision
FAA Appi oved
Date
This manual, which was completely revised June 1, 1970, applies to
Piper Model PA-39-1 and up.
1.
3
1.
I-ii
I-19
Page I-32 added
Pages I-33 & 34
added
II-2 1
II-24
I-26
I-28
I-29
II-5
II-6
II-24
II-29
Under Section V, added Item F.
Nov. 2, 1970
Added Item F.
Added information for Supplement F.
Added Supplement F.
Heated Glass Panel Installation added.
Appropriate was appropriated. March 17, 1971
Revised Supplement D - Item 2. - d.
Added to Supplement D Item 6. - f.
C. G. Chart Clarified.
Basic weight was basis weight.
Added Radair Exhaust Gas Temperature Indicator
and Delta Mixture Control Indicator.
Added Narco ATS-A Transponder and King
Digital ADF KR-85.
3.
4.
5.
6.
7.
II-29
II-29
II-I 0
II-I 1
I-3
H-9
II-IO
I-9
Added Bendix ADF-T 12D. April 19, 1971
Added Marker Beacon Installation MBT-R-I 2. June 1, 1971
Added Propeller-Synchrophaser. August 13, 1971
Added Piper Dwg. Nos. to Fuel Pumps.
Added additional Hartzell Propellers. Sept. 3, 1971
Added additional Hartzell Propellers.
Added additional Hartzell Propellers to Spinners.
Revised instructions for Voltage Regulating Nov. 1, 1971
System item e. and g.
FAA APPROVED November 28,1969
REISSUED: June 1,197O
REVISED: November 1,197l
REPORT: 1605 PART I PAGE 1’
MODEL: PA-39

Piper PA-39 Twin Comanche C/R Specifications

General

Brand	Piper
Model	PA-39 Twin Comanche C/R
Category	Aircrafts
Language	English