Piper Cherokee Arrow II PA-28R-200 1973 User manual

I
WARNING
I
EXTREME CARE MUST BE EXERCISED TO LIMIT THE USE OF THIS MANUAL.
TO APPLICABLE AIRCRAFT THIS MANUAL REVISED AS lNDICATED BELOW
OR StJBSEQUENTLY REVISED IS VALID FOR USE WITH THE AIRPLANE
IDENTIFIED BELOW WHEN APPROVED BY PIPER AIRCRAFT CORPORATION.
SUBSEQUENT REVISIONS SUPPL.IED BY PIPER AIRCRAFT CORPORATION
MUST BE PROPERLY INSERTED.
MODEL PA-28R-200
AIRCRAFT SERIAL NO. 28R-7535277 REGISTRATION NO. N1lRB
PR750128
PILOT'S OPERATING MANUAL., PART NIJMBER 761 578 REVISION 1
- 28 - 75
PIPER AIRCRAFT CORPORATION
APPROVAL.SIGNATURE AND STAMP
G&#&4%
T.W. Reed, ~rw
Assurance that the airplane is in an airworthy condition is the responsibility of the owner.
The pilot in command is responsible for determining that the airplane is safe for flight. The pilot
is also responsible for remaining within the operating limitations outlined by the Airplane Flight
.g
Manual, instrument markings, and placards
This Pilot's Operating Manual is not designed as a substitute for adequate and competent
flight instruction, knowledge of the current airworthiness directives, applicable federal air
regulations, or advisory circulars. It is not intended to be a guide for basic flight instruction or a
training manual for tr
an
sition from single to multiengine flying.
It an inconsistency of information exists between the Pilot's Operating Manual and the
Airplane Flight Manual approved by the FAA, the Airplane Flight Manual shall be the
authority.
A complete or partial replacement of this manual, Part No.
761 578, may be obtained only from Piper Customer Services.
Published by
PUBL.ICATIONSDEPARTMENT
Piper Aircraft Corporation
761 578
Issued: July 1973

APPLICABILITY
This manual is applicable to Piper Model PA - 28R - 200 aircraft having serial numbers commencing with
28R
- 7435001 through 28R - 7635545. Contact Piper Customer Services for specific information on the
application of this manual.
WARNING
INSPECTION, MAINTENANCE
AND PARTS REQUIlU3MENTS FOR ALL NON - PIPER
APPROVEDSTC INSTALLATIONS
ARE NWINCLUDED IN THISHANDBOOK. WHEN
A NON - PIPER APPROVED STC INSTALLATION IS INCORPORATED ON THE
AIRPLANE, THOSE PORTIONS OF THE AIRPLANE AFFECTED BY THE
INSTALLATION MUST BE INSPECTED IN ACCORDANCE WITH THE INSPECTION
PROGRAM PUBLISRED
BY THE OWNER OF THESTC. SINCE NON - PIPER APPROVED
STC INSTALLATIONS MAY CHANGE SYSTEMS INTERFACE, OPERATING
CHARACTERISTICS AND COMPONENT LOADS OR STRESSES ON ADJACENT
STRUCTlJRES,PIPER PROVIDED INSPECTION CRITERIA MAY NOT BE VALID FOR
AIRPLANES
WITH NON - PIPER APPROVED STC INSTALLATIONS.
REVISIONS
The information compiled in the Pilot's Operating Manual will be kept current by revisions
distributed to the airplane owners.
Revision material will consist of information necessary to update the text of the present manual
and/or to add information to cover added airplane equipment.
L. Revisions
Revisions will be distributed whenever necessary as complete page replacements oradditions and shall
be inserted into the manual in accordance with the instructions given below:
1. Revision pages will replace only pages with the same page number.
2. Insert all additional pages in proper numerical order within each section.
3. Page numbers followed by a small letter shall be inserted in direct sequence with the same
common numbered page.
II. Identification of Revised Material
Revised text and illustrations shall be indicated by a black vertical line along the left hand margin of
the page, opposite revised, added or deleted material.
A line opposite the page number or section title and
printing date, will indicate that the text or illustration was unchanged but material was relocated to a
different page or that an entire page was added.
Black lines will indicate only current revisions with changes and additions to ordeletions of existing
text and illustrations. Changes in capitalization, spelling, punctuation or the physical location of material
on a page will not be identified by symbols.
III. Original Pages Issued
The original pages issued for this manual prior to revision are given below:
1
- 1 through 1 - 3, 2 - 1 through 2 - 24, 3 - 1 through 3 - 10, 4 - 1 through 4-8, 5 - 1 through 5 - 32, 7 - 1 through
7
- 10, 8 - 1 through 8-2.9-1 through 9 - 10, 10 - 1 through 10-15.
REVISED: FEBRUARY 7,2005

PILOT'S OPERATING MANUAL LOGOFREVISIONS
Current Revisions to the PA
- 28R - 200 Arrow I1 Pilot's Operating Manual, 761 578, issued July
Description
1 Date I
Rev. 1 - 761 578
I wJB I
Added Rev. 1 to Report:VB - 549. Oct. 29,1973
(PR731029)
Rev.
2 - 761 578
(PR740325)
Rev. 3 - 761 578
(PR740618)
2 - 20
A FJM
4 - 8
Added PAC Approval Form.
Added Applicability and Item
Ill. Original
Pages Issued.
Added Rev.
1 to Report VB-560.
Added Rev. 2 toReport VB - 549.
(NOTE:
AIRCRAFT DELIVERED WITH
MANUALS PRIOR TO THIS REVISION
DO NOT REQUIRE
THIS REVISION.)
Added MixtureControl Lock and Footnote.
Added MixtureControl Lock to Throttle
Quadrant Illustration.
Added AnnuncintorPanel and Footnote;
added Landing
Gear Light Dimming
Warning.
Revised AlternatorandStarterSchematic.
Added Alternatorand StarterSchematic
for 1975Models.
Added IntentionallyLeft Blank Page.
Added Annunciator Panel and Footnoteto
VacuumSystemDescription.
Added AnnunciatorPanel and Footnoteto
InstrumentPanel Description.
Added Annunciator Panel and Mixture
ControlLock to InstnunentPanel Illus
-
tration.
Added Rea~SeatRemoval Instiuctions.
Added Revision 2 to Report: VB - 560.
Revised Alternator FailureEmergency
March 25,1974 1
June18.1974
Procedures.
I I
Added Revision 3 to Report: VB - 549.
Revised Operating InstructionsIndex;
added Airspeed Data.
1 7-4 1
Revised Aii Conditioner Ground Check;
added AnnunciatorPanel
Check and Foot -
7 - 5 note; relocated info.
Added info from Page 7-4relocated
Cruisinginfo.

PI1,OT'S OPE,RATING MANUAI. LOG OF REVISIONS (cont)
1
Datc
- - -
.Jan 28. 1975
Description
Added Cruising info;added Mixture
Control Lock and Footnote;relocated
Approach and L.andinginfb.
Added Approach and Landing infb;added
Mixture Control Lock and Footnote;
relocated Moorings and Weight and Balance
infb.
Added Airspeed Data;added Moorings, and
Weight and Balance info; relocated ELT
info.
Added infb from Page 7
- 8; relocated Air
Conditioning info.
Added Air Conditioning info;relocated
info.
Added page; added relocated info.
Added Annunciator Panel to item
I I ;
moved Item 13 toPage 8-2.
Added Item 13 from Page 8-1.
Revised Performance Charts Index.
Revised Takeoff Chart.
Revised Climb Chart
Revised Airspeed Chart.
Revised Range Chart.
Revised Glide Chart.
Revised L.andingChart.
Added gear warning info.
Revised Stall Warning info.
Revision
Rev
3 (cont)
Rcv 4 - 761 578
(PR750178)
Revised
Pages
7
- 6
7
- 7
7
- 8
7
- 9
7
- 10
7
- 1 1
8 - 1
8 - 2
9
- i
9
- 2
9-.3
9 - 4
9
- 5
9
- 8
9
- 9
2
- 6
2-2 1

ARROW I1
THIS PAGE. INTENTIONALLY LEFT BLANK

ARROW 11
PILOT'S OPERATING MANUAL LOG OF REVISIONS (cont)
Revised Description
10
- 9 Added info. from page 10-8.
10-11 Revised Service Bulletin info.
...
U1
1 - 2
2
- 21
AFM
W/B
9 - i
10
- 7
2
- 5
2
- 6
2
- 16
AFM
4
- 2
Added includingserial number.
Revised fuel and oil info.
Revised para.
Added Rev. 6 toReport: VB
- 560.
Added Rev. 9 to~eport:VB
- 549.
Added Warning.
Added info., and fuel gradechart,
moved info. to page 10
- 8.
Relocated info. from pg. 10-7.moved
info. to page
10 - 9.
Relocated info. from page 10 - 8.
Revised para.
Revised preventivemaintenancepara.,
relocatedinfo. from page 10
- 13.
Moved info. topage 10
- 12.
Revised LandingGear.
Relocated Warning
Revised ThrottleQuadrant and
Consolefigures.
Revised Schematic.
Revised para. Added info.
Revised InstrumentPanelfig.
Added Rev.
7 to Report: VB - 560.
Revised Engine PowerLoss During
Takeoff para.
Revised EnginePowerLoss During
Takeoff.
Revised Power
Off Landing. Gear
Down Landing, and Gear Up Landing paras.
Moved info. from page
4-5.
Revised Emergency GearExtension para.
Moved info. to page 4-4.
Revised Note.
Revised footnote.
Revised item 12.
Revised Note.
Added Note.
Added note reference.
Date
--
Feb. 29,1984
Jan. 31,1987

PII,OT9SOPERATING MANUAL LOG OF REVISIONS (cont)
Revised
Pages
Revision
Rev. 12
- 761 578
(PR900730)
Rev. 13 - 761 - 578
(PR050207)
Rev..14 - 761 - 578
(PRO5 1 010)
Description
-
--"
Revised Oil info. Moved Dimensionsand
LandingGear to page 1-4.
Added page. Relocated Dimensions and
Landing Gearfrom page 1
- 2.
Revised Table of Contents.
Revised Oil Requirements.Moved info..
to page 10
- 8.
Relocated info..from page 10
- 7. Moved
Tire Inflation and Battery Sevice info. to
page 10
- 9.
Relocated Tire inflation and Battery Sevice
info. from page 10-8.
Revised Facts You Should Know.
Revised Preventive Maintenance.
Revised Required Serviceand
inspection
Periods.
Added Warning.
Added Rev.
8 to Report: VB - 560.
Revised Emergency Landing GearExtension.
Revised Table of Contents.
Added Warnings and moved info. to page
10-2.
Moved info.from page 10 - 1.
Revised Required Service And Inspection
Periods.
Added Rev. 9 to Report: VB
- 560
'Q=M -1 ....u---..p

TABLE OF CONTENTS
GENERAL SPEClFlCATlONS
DESCRIPTION - AIRPLANE AND SYSTEMS
AIRPLANE FUGR (TUAL F.A.W. APPROVED
EMERGENCY PROCEDURES F.A.A. APPROVED
EMERGENCY PROCEDURES
WEIGHT AND BALANCE
LOADING INSTRUCTIONS
OPERATING INSTRUCTlONS
OPERATING TIPS
PERFORMANCE CHARTS
HANDLING AND SIEWWCING

GENERAL SPECIFlCATlONS
Performance ............................................ 1 - 1
Weights
................................................ 1 - 2
Power Plant ............................................. 1 - 2
Fuel and Oil ............................................... 1 - 2
Baggage
............................................... 1 - 2
Dimensions
............................................... 1 - 2
.............................................
Landing Gear 1 - 2