Cherokee SIX 260 Specifiche tecniche

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

AIRPTA}IE TtrcHI ilIA]IUAt

Log of Rwisions 3-iii

Limitations . .3-l

Procedures

Supplements

3-5

3-7

3-9

3-i

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

A. Enehe

B. Fugl ....... r...o............o.........

C. Propeller

D. Power Instnrments

E. Airspeed Limitations and Airspeed Instrument

H.'

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

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

THIS PAGE INTENTIONALLY LEFT BLANK

REPORT: VB-561 PAGE 3-ii

MODEL: PA-32-260 FAA APPROVE,D MAY 14, 1973

CHEROKEE SIX-260

AIRPLANE FLIGHT MANUAL LOG OF REVISIONS

Revision Revised Pages Description and Revision Efu{ Approved

Date

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) \-

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

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

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 -

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