Take Flight G-BSCY PA-28-151 1981 Owner's manual

Pilot’s Operating Handbook
G-BSCY
Take
A V I A T I O N . c o m

Disclaimer
Take
A V I A T I O N . c o m
This pdf scan of the Pilots Operating
Handbook (POH) is for information,
and to aid flight planning only.
It should not replace reference to the
original documents, due to possible
updates since publication.
These are available for inspection at
Take Flight Aviation Limited on
request.

A0
AIRCRAFT
MODIFICATIONS
INC.
F.A.A.
APPROVED
AIRPLANE
SUPPLEMENTAL
FLIGHT
MANUAL
For
PIPER
CHEROKEE
MODEL
PA-28-151
With
LYCOMING0-320-D2A,
-D2B,
-D2C,
or
-D3G
PENGINE
INSTALLED
REGISTRATION
NUMBER
G3
fSS
C
Y
SEIA
NUMER761
So0
This
Supplemental
Flight
Manual
is
F.A.A.
approved
material
and
must
be
in
the
airplane
for
all
operations
when
Lycoming
0-320-D2A,
0-320-D2B,
0-320-D2C
or
0-320-D3G
engine
is
installed
in
accordance
with
STC
SA2969SW.
The
information contained
herein
supplements
or
supersedes
the
information
in
the
form
of
placards,
markings,
and
approved4tnanual
material.
For
limitations,
procedures
and
performance
information
not
contained
in
this
Supplemental
Flight
Manual
consult
the
basic
airplane
placards,
markings
and
approved
manual
material.
F.A.A.
AP
R
#4VED~f~
on
P.
Watson,
Chief,
Engineering
&
Manufacturing
Branch
FEDERAL
AVIATION
ADMINISTRATION
Southwest
Region
Fort
Worth,
Texas
76101
DATE:
October
21,
1981
S.T.C.
No.
SA2969SW
Page
1
of
2
pages
Waco-Madison
Cooper
Airport
*
P.O.
Box
5219
* Waco,
Texas
76708
* 817-752-8381

AIRCRAFT
MODIFICATIONS
INC.
PIPER
CHEROKEE MODEL PA-28-151
SUPPLEMENTAL
FLIGHT
MANUAL
I. GENERAL
1.
ENGINE:
Lycoming
0-320-D2A
or
Lycoming 0-320-D2B
or
/-"
Lycoming
0-320-D2C
or
Lycoming O-320-D3G
2.
PROPELLER:
Sensenich
74DM6-0-60
or
Sensenich
74DM6-0-58
II.
LIMITATIONS
1.
ENGINE
LIMITS:
Maximum
Continuous:
150
H.P.
- 2650
RPM
Takeoff
(Five
(5)
Minutes)
160 H.P. - 2700 RPM
2.
PROPELLE
LIMITS:
Static
RPM
at
maximum
throttle
setting:
Not
over
2450,
Not
under
2350
Diameter:
Maximum
= 74
inches
Minimum
=
72 inches
I' 3.
ENGINE
INSTRUMENT
TACHOMETER:
(0
MARKINGS:
Green Arc
2200
-
2650
RPM
Yellow
Arc
2650
- 2700'RPM
Red
Radial
- 2700
RPM
III.
PROCEDURES
No
Change
IV.
PERFORMANCE
The
performance
of
this
airplane
equipped
with
a
Lycoming
0-320-D2A,
0-320-D2B,
0-320-D2C,
or
0-320-D3G
engine
is
equal
to
or
better
than
the
original
F.A.A.
approved
performance.
F.A.A.
APPROVED
S.T.C.
No.
SA2969SW
DATE:
10/21/81
Page
2
of
2
pages
Waco-Madison
Cooper
Airport
- P.O.
Box
5219
* Waco,
Texas
76708
*
817-752-8381

P IPER
A
IR
AFI
C P
REPORT
vB-575
P_I
MODEL
PA-28-151
OEYIOPLII
UNI1T,
VERO
H[ACH,
RtA.
____________
AGE TITLE
A
P P
ROV
E D AEROPLANE FLIGtT
MA
NUA
L
FOR
TItE
P
I
P
ER MODEL
PA-28-151
tO-
Iff$D
PREPARED
IN
ACCORDANCE
WITH
BRITISH
CIVIL
AIRWORTHINESS
REQUIRENENYS
SERIAL
NUMBER:
28-7415001
TO
28-7615999
BY:
SheehanBY*
CHECKED
BY:
.
(__
R.
K.
Kirby
APPROVED
BY
:
>Lt-
-'
"
John
Fmat
rict:
Manager,
Flight
Test
IS
ST
DATE"::
/
/ 0
,:,.. l'n
U
"
"/ -"
I
"~i
,,L[
P
AA
l.'f.\
/
1,,:
...
7 , l ; : . . .. . . .. . .. . ... .... . .

PIPER
AIRCRAFT
CORP
REPORT
VB-575
SAMODEL PA-28-151
§EYE.IPUENT
CENTER,
YER0
BEACH,
RtA.
_____
°'his
is
th This
is tho Flighi
Manual which
forms
partoliho
3-. U CSL
r7'I
-0 a 2
C
nific
te
o
Conifc
ca
Airwo
hinss
for
aircaf
.............
..
'........
.... /
SECTION
I.
GENERAL
A.
Registration Particulars
i.
Airplane
designation:
PIPER Model
PA-28l151
2. Registration
Marks:
&
C3
GY
3.
Constructor's
Serial
Number:
.'g-76 506.
4.
Designed
and
Constructed
by:
Piper
Aircraft
Corporation
Vero
Beach,
Florida,
U.S.A.
32960
5.
F.A.A.
Certificate
of
Airworthiness
for
Export:
Number:
Date
of
Issue:
6.
Model
PA-28-151
British
Flight
Manual,
Piper
Aircraft
Corporation
Report
VB-575,
Approved
by
the
Secretary,
CiVil
Aviation Authority
on:
7.
This
airplane
shall
be
operated
in
accordance
with
the
limitations
in
Section
II
and any
additional limitations
in
the
Supplements
contained
in
Section
VI.

PIPER AIRCRAFT CORP. REPORT VB-575
X"
BEY[OP
IRT
CENTER,
YERO
BEACH,
FLA.
MODEL
PA-28-151
FAtE
2
SECTION
1.
GENERAL
(continued)
B.
Table
of
Contents
PAGE
SECTION
I.
GENERAL
A.
Registration
particulars
...........................................
I
B.
Table
of
Contents
..................................................
2
C.
Amendment
System...................................................6
D.
General
Arrangement
Drawing
.......................................
9
E.
Determination
of
Temperature
in
Relation
to
i.S.A
...............
10
F.
Definitions
.................
...................................
SECTION
II. LIMITATIONS
A.
Maximum
Weight
Limitations
.......................................
14
B.
Baggage
Loading
...................................................
14
C..
Fuel
System
....................................................
D.
Centre
of
Gravity
........................
E.
Power
Plant
Limitations
...........
..............................
.1
F.
Airspeed
Limitations
...........................
.........
......
G.
Miscellaneous
Limitations........................................ 21
SECTION
111.
EMERGENCY
PROCEDURES
A.
Introduction
.................................................
2"
B.
Engine
Fire
During
Start
.........................................
28
C.
Engine Power Loss
During
Take-off
................................
28
D.
Engine
Power
Loss
In
Flight
...
.................................
30
E.
Power-off
Landing
......
.
.......................................
.31
F. F
ire
.........
..................................................
3Z

I
PIPER
AIRCRAFT
CORP.
REPORT
VB-575
Eo
"YELEOP
UIT
CE
R,
YEIRO
BEACH,
R
A.
MODEL
rA-28-151
F AtE
3
SECTION
.GENERAL
(continued)
PAGE
G.
Lo
S
of
Oil
Pressure
............................................
It.
Loss
of
Fuel
Pressure
............................................
34
1.
High Oil
Temperature
...................................
........
35
J. Alternator
Failure
.............................................
35
K.
Engine
Roughness
................................................
36
..... .. ... 37
~~L,
Spins
.. ............
M.
Open
Door
............
....
...................................
37
SECTION
IV.
NORMAL
PROCEDURES
•A.
Preflight
.........................
..............................
39
B.
Walk-around
Inspection
..........................
..............
39
C.
Before
Starting
Engine
..........
.............................
42
D. Starting.Engine
When
Cold
......................................
E Starting
Engine
When
Hot
..................................
43
F.
Starting
Engine
When
Flooded
................................
..... 44
a.
General
Information
for
Starting
Engine
.....................
44
H.
Taxi
............... ........................................
45
I.
Before
Takeoff.
.................................................
45
j.
Normal
Take-off
(Flaps
up).......................................
K.
Crosswind Component...............................................
48
L..
Takeoff
Climb..................................................
48
M.
Normal
Climb
....................................................
.. 48
N.
Normal
Cruise...................................................48
0.
Approach
and
Lndin
...........................................
49
p
Post
Landing
.......................................................
51

PIPER
AIRCRAFT
CORP.
REPORT
VB-575
*MODEL PA-28-151
11EL~OPUEIRT
BEIER,.
VERO
BEACH,
FLA.
"n---0
PACE
4 ,
SECTION
I.
GENERAL (continued)
PAGE
Q.
Engine
Shut-down ...................................
,
.............
51
R.
Rough
Air
Flight
............
..................................
51
SECT
ION
V.
PERFORMANCE
A. General
.............
...........................
............ .52
B.
Maximum
Take-off
and
LAnding Weight
for
Altitude
and
Temperature
.......
................................
58
C.
Take-off
Procedures
and
Speeds ...................................
60
D.
Take-off
Field Lengths
.
........................................
61
E.
Net
Take-off
Flight
Path
...........................................
67
F.
En
Route
Performance
...............................................
70
G.
Landing
Procedures
and
Speeds .....................................
73
H.
Landing
Field
Lengths
...
.....................
...................
74
I.
Net
Glide
Range
..
..............................................
77
SECTION
VI.
SUPPLEMENTS
Explanation
of
the
Supplemen System
................................
79
Record
of
Supplements
.......
....
...................................
80

PIPER
AIRCRAFT
CORP.
REPORT VB-575
. DEYEtPUEPI
CEUTE!,
YEl
BEACH,
FIA.
MODET.
PA-28-151
SECTION
I-
GENERAL
(
continued
PAGE
LIST
OF
ILLUSTRATIONS
Figure
1.
General
Arrangement Drawing
................................
9
Figure
2.
Determination
of
Temperature
in
relation
to
I.S.A
........
Lo
Figure
3.
Centre
of
Gravity
Envelope
.
..............................
16
Figure
4.
Conversion
of
Wind
Velocities
............
...............
53
Figure
5.
Pitot Head
Location
...........................
;
......... 54
Figure 6. Position
Error Correction to
Obtain E.A.S. (MP) ........
55
Figure
7.
Position
Error Correction
to
Obtain
E.A.S.
(Knots)
...... 56
Figure
8.
Maximum
Take-off
and
Landing
Weight
for
Altitude
and
Temperature
.
................................
59
Figure
9.
Take-off Run Required
....................................
63
Figure
10.
Take-off
Distance
Required
................................
66
Figure
II°:
Net
Take-off
Flight
Path
...........
.....................
69
"
Figure
12.
En
Route
Perfor'mance
Ceiling.
and
Cross
Rate
of
Climb
....
.72
Figure
13.
Landing
Distance R~quired
.......
..........................
76
Figure
14.
Net.
Glide
Range ............................................
78