Cherokee SIX 260 Especificaciones técnicas
FLIGHT MAilUAL
r0R
KEE SIX 260
IYUMBERS 32.7 4O()O()I THROUGH 32.7600024
OHERO
APPLICABLE TO SERIAI,
AIRPLA}IE
,^
NOTE
THIS MANUAL MUST BE KEPT IN THE AIRPLA}IE AT ALL TIMES
FAA APPROVED FY'
PIPER AIRCRAFT CORPORATION
D. O. A. NO. SO-1
VERO BEACH, FLORIDA
DATE OF APPROVAL: MAY l4,lg73
APPROVAL BASIS: CAR 3
REPORT: VB-561
MODEL: PA-32-260
WARNING
EXTREME CARE MUST BE EXERCISED TO LTMIT THE USE OF THIS MANUAL
TO APPLICABLE AIRCRAFT. THIS MANUAL REVISED AS INDICATED BELOW
oR srrBSEeuENTLy REvrsgp rs vALrD FoR usE wrrH THE AIRpLANE
IDENTIFIED BELOW WHEN APPROVED BY PIPER AIRCRAFT CORPORATION.
SI,]BSEQUENT REVISIONS SUPPLIED BY PIPER AIRCRAFT COPJORATION
MODEL PA.32.260
32-7 400029
AIRCRAFT SERTAL NO.
AIRPLANE FLIGHT MANUAI, REPORT
PIPER AIRCRAFT CORPORATION
APPROVAL SIGNATURE AND STAIvIP
REGISTRATION NO.
ER VB.56I REVISION
.1{. BARNHOUSE
i.-
BLANK PAGE
-
v
n
AIRPTA}IE TtrcHI ilIA]IUAt
Log of Rwisions 3-iii
Limitations . .3-l
Procedures
Supplements
3-5
3-7
3-9
^
3-i
V
BLANKPAGE
CHEROKEE SIX-260
,..-
TABTE OF GO}ITE}ITS
Log of Revisions
SECIION I
Limitations
SECTIONU
Procedurts
SEqTION M
Performance
SECTION TV
Optional Equipment
A aaa
J-1ll
3-l
3-l
3-l
3-l
3-l
A. Enehe
B. Fugl ....... r...o............o.........
C. Propeller
D. Power Instnrments
E. Airspeed Limitations and Airspeed Instrument
F.
G.
H.'
r.
J.
Mukings (Calibrated Airsieed) 3-2
MaximumWeight 3-z
C. G. Ranep 3A
Manetners 34
Placards 3-3
Bear Cabin Doc or Rear Cabin Door and Cargo
DoorRemoved . ..; 34
Swenth-Passenger Operation 34
Nose Wheel Fairing Removed 94
K.
L.
3-5
3-7
A. Electric Pitdl Trim Installation
B. AutoFlite II Installation. . .
C. Piper AutoControl III and/or AutoControl IIIB Installation
D. Piper AltMatic IIIC Installation
3-g
3-1 I
3-r4
3-15
3-19
REPORT: VB-561 PAGE 3-i
MODEL: PA-32-260
FAA APPROVED MAY 14, 1973
REVISED: NOVEMBER 4, 1974
,
CHEROKEE SIX-260
V
THIS PAGE INTENTIONALLY LEFT BLANK
v
REPORT: VB-561 PAGE 3-ii
MODEL: PA-32-260 FAA APPROVE,D MAY 14, 1973
V
CHEROKEE SIX-260
n
AIRPLANE FLIGHT MANUAL LOG OF REVISIONS
Revision Revised Pages Description and Revision Efu{ Approved
Date
1
2
a
J
4
Title
3-i
3-9
3-15,3-16,
3-17,3-18
3-i
3-4
3-9
3-12
3-r3
3 -14
3-15
3-18
3-19,3-20,
3-21, 3-22"
3-23, 3-24,
3-25, 3-26
3-3,3-4
Added PAC Approval Form.
(NOTE: AIRCRAFT DELIVERED WITH
MANUALS PRIOR TO THIS REVISION
DO NOT REQUIRE THIS REVISION.)
Added Item D. (Installation of Piper Auto-
Control IIIB) to Supplements.
Added Item D. (Installation of Piper Auto-
Control IIIB).
Added pages (AutoControl IIIB Supplement).
Under Limitations - added item L. (Nose Wheel
Fairing Removed); changed Section IV title
from Supplements to Optional Equipment;
under Optional Equipment- deleted items B.
and C.; revised remaining items; added new
item D. (Piper AltiMatic IIIC Installation).
Added item L. (Nose Wheel Fairing Removed),
remove Airplane Flight Manual Supplement
Report No. VB-637 if attached to the Air-
plane Flight Manual.
Changed Section IV title from Supplements to
Optional Equipment; revised Note; deleted
items B. and C.; revised remaining items; added
new item D. (Piper AltiMatic IIIC Installation).
Deleted item B. AutoFlite Installation.
Deleted item C. AutoControl Installation.
Revised item letter (D. to B.).
Revised item letter; revised item title; added
AutoControl III to title.
Deleted IIIB designation from items c. (1) and
(2).
Added pages (AltiM atic IIIC), remove Airplane
Flight Manual Supplement Report No . YB-667
if attached to the Airplane Flight Manual.
Deleted seventh seat reference.
D. H. Trompler
June 19, 197 4
U*l €vur\.-
Ward Evans
Nov. 4, L97 4
A *J 6.,or,,
Ward Evans
Dec. 13 , L978
,ll
FAAAPPROVED MAY 14, 1973
REVISED: DECEMBER 13, 1978 REPORT: VB-561 PAGE 3-iii
MODEL: PA-32-260
/,u
D. H. Trompler
June 4, 197 4
CHEROKEE SIX-260
Revision Revised Pages Description and Revision FAA Approved
Date
5Title Added Applicable Serial Numbers.
(NOTE: AIRCRAFT DELIVERED
WITH MANUALS PRIOR TO THIS
REVISION DO NOT REQUIRE THIS
REVTSTON.)
tJ*n
Ward Evans
March 22, 1979
AIRPLAI\E FLIGHT MANUAL LOG OF REVISIONS (cont) \-
V
REPORT: VB-561 PAGE 3-iv
MODEL: PA-32-260 FAA APPROVED MAY 14, 1973
REVISED: MARCII 22, 1979
-
CHEROKEE SIX-260
/^
SECTION I
LIMITATIONS
The following limitations must be observed in the operation of this airplane:
A. ENGINE
Lycoming 0-540-E4B5
ENGINE LIMITS
For all operations 2700 RPM, 260 HP
B. FUEL
100/130 minimum aviation grade fuel
C. PROPELLER
Hartzell Model HC-C2YK-l( )18477-2 or HC-C2YK-l( )F1F8477-2, low pitch stop
12.0" +.2",high pitch stop 32" + 2o, maximum diameter 82 inches, minimum diameter
80.5 inches.
D. POWER INSTRIJMENTS
OIL TEMPERATURE,
Green Arc (Normal Operating Range)
Red Line (Maximum)
OIL PRESSI]RE,
$: i,'"li:Ji.Tfi il,3ff ;ili - R an g e )
Red Line (Minimum)
Red Line (Maximum)
FUEL PRE tiy,Hrm al operatin g Range)
Red Line (Minimum)
Red Line (Maximum)
TACHOME,TER
Green Arc (Normal Operating Range)
Red Line (Maximum Continuous Power)
REPORT: VB-561 PAGE 3-1
MODEL: PA-32-260
7 5"F to 245 "F
245"F
60 PSI to 90 PSI
25 PSI to 60 PSI
25 PSI
90 PSI
.5 PSI to 8 PSI
.5 PSI
8 PSI
500 to 2100 RPM
27OO RPM
EAA APPROVED MAY 14, 1973
CHEROKEE SIX-260
E. AIRSPEED LIMITATIONS AND AIRSPEED INSTRUMENT MARKINGS (CalibTated
Airspeed)
NE,VE,R EXCEE,D
MAXIMUM STRUCTIJRAL CRT]I SE
MANEIJVERING
FLAPS EXTENDED
MAXIMUM POSITIVE LOAD FACTOR
MAXIMIJM NE,GATIVE, LOAD FACTOR
AIRSPEED NSTRTJMENT MARKINGS
Red Radial Line (Never Exceed)
Yellow Arc (Caution Range)
(Smooth Air Only)
Green Arc (Normal Operating Range)
White Arc (Flap Down Range)
F. MAXIMI]M WEIGHT
212 MPH
168 MPH
149 MPH
125 MPH
3.8
No inverted maneuvers approved
212 MPH (184 KTS)
168 MPH to 21 2 MPH
(146 KTS to 184 KTS)
7l MPH to 168 MPH
(62 KTS to 146 KTS)
63 MPH to 125 MPH
(55 KTS to 109 KTS)
34OO LBS
wing leading edge at the intersection of the
Rearward Limit
(In. Aft of Datum)
95.5
96.2
96.2
96.2
G. C. G. RANGE
The datum used is
straight and tapered
Weight
(Pounds)
3400
3300
2900
2400
7 8.4 inches ahead of the
section.
Forward Limit
(In. Aft of Datum)
9t.4
89.0
80.0
7 6.0
V
..v
Straight line variation between points given.
NOTE
It is the responsibility of the airplane owner and the pilot to
insure that the airplane is properly loaded. See Weight and
Balance Section for proper loading instructions.
H. MANEUVERS
No acrobatic maneuvers including spins approved.
REPORT: VB-561 PAGE3-2
MODEL: PA-32-260 EAA APPROVED MAY 14, 1973 -
Este manual sirve para los siguientes modelos
3
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