PENN,rAN AENOS~RVICE1INC.

Transcription

PENN,rAN AENOS~RVICE1INC.
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PENN,rAN AENOS~RVICE1
INC.
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PENN
'fJ\N,
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180 H.P. SUPERHAWK
(315) 536-2333
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FAA APPROVED
SUPPLEMENTAL AIRPLANE FLIGHT MANUAL
FOR
CESSNA
REG.
NO.
SER. NO.
172N
~
~
~
This Supplement must be carried in the aircraft when it is modified by the
installation
of a 180 HP engine and the gross weight is increased in
accordance with STCSA703GL. The information contained herein supplements or
supersedes the basic placards and markings only in tho~e areas lis~ed.
~
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FAA APPROVED:'
1
, .c..6x.',t)
{{I~ W. F Horn, Manager
Chic go Aircraft
Certification
Office
FAA Central
Region
DATE:
June 11, 1985
PaQe 1 of 4
PENN YAN AERO SERVICE INC.
FAA APPROVED
SUPPLEMENTALAIRPLANE FLIGHT MANUAL
FOR
CESSNA 172SERIESAIRCRAFT
.
..
LOG OF REVISIONS
~
Rev.
NQ.
A
NQ.
4
Description
FAA Approved
Added performance
information to
section 5 for
clarification
Renumbered pages
Irwin N Brumer
Manager, NYACO
APR ,1 3 1994
-
Page 2 of 4
\
Penn Yan Aero Service,
Inc.
Supplemental Airplane
Flight Manual for
Cessna 172N
2499 Bath Road, Airport
Penn Yan, NY 14527-9599
SECTIONI
- Limitations
A. The following placard must be displayed
in full view of the pilot:
THIS AIRCRAFT HAS BEEN MODIFIED BY THE INSTALLATION OF A 180 HP
ENGINE PER STC SA703GL.
IT MUST BE OPERATED AS A NORHALCATEGORY
AIRPLANE IN COMPLIANCE WITH THE OPERATING LIMITATIONS AS STATED
IN THE FORM OF PLACARDS, MARKINGS AND MANUALS.
B.
For the N model a"ircraft
the following
adjacent to the flap position
selector
placard
switch:
must be displayed
.
MAXIMUMFLAP TRAVEL IS 30°
C.
The following
limits
apply to the normal category
only.
-
MaximumGross Weight 2550 lbs.
C.G. Range 41.0" to 47.3" at 2550 lbs.
35.0" to 47.3" at 1950 lbs. or less
Straight line variation between points given.
-
"
FAA
APPROVED JUN 111!85
DATED:
Pag e.3 of 4-
..
Section
3
Emerqency Procedures
NO CHANGE
Section
4
Normal
Procedures
NO CHANGE
Section 5
Performance
Performance of the Cessna 172 series
aircraft, when it is modified by the
installation of a 180 HP engine and the gross
weight is increased, in accordance with STC
SA703GL, will be equal to or better than the
basic airplane
CAUTION:-
..
The fuel consumption
and range/endurance
information originally presented for this
model do not apply to this STC modification:
increased fuel consumption and reduced range/
endurance can be expected with the 180 hp
engine installed.
FAA APPROVED
DATE:
Revised: APR.13 1994
.
Page 4 Of 4
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