I I WARNING 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 G&#&4% APPROVAL. SIGNATURE AND STAMP ~rw T.W. Reed, 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 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. an A complete or partial replacement of this manual, Part No. 761 578, may be obtained only from Piper Customer Services. Published by PUBL.ICATIONS DEPARTMENT 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 APPROVED STC INSTALLATIONS ARE N W I NCLUDED IN THIS HANDBOOK. 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 THE STC. 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 or additions 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 or deletions 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 LOG OF REVISIONS Current Revisions to the PA-28R-200 Arrow I1 Pilot's Operating Manual, 761 578, issued July I 1 Description Date I I Rev. 1 - 761 578 Added Rev. 1 to Report: VB-549. Oct. 29,1973 (PR731 029) wJB 1 Rev. 2 - 761 578 Added PAC Approval Form. March 25,1974 (PR740325) Added Applicability and Item Ill. Original Pages Issued. Added Rev. 1 to Report VB-560. Added Rev. 2 to Report VB-549. (NOTE: AIRCRAFT DELIVERED WITH MANUALS PRIOR TO THIS REVISION DO NOT REQUIRE THIS REVISION.) Rev. 3 - 761 578 Added Mixture Control Lock and Footnote. June 18.1974 (PR740618) Added Mixture Control Lock to Throttle Quadrant Illustration. Added Annuncintor Panel and Footnote; added Landing Gear Light Dimming Warning. Revised Alternator and Starter Schematic. Added Alternator and Starter Schematic for 1975 Models. Added Intentionally Left Blank Page. Added Annunciator Panel and Footnote to Vacuum System Description. Added Annunciator Panel and Footnote to Instrument Panel Description. Added Annunciator Panel and Mixture Control Lock to Instnunent Panel Illus- tration. 2-20 Added ReaS~e at Removal Instiuctions. A FJM Added Revision 2 to Report: VB-560. 4-8 Revised Alternator Failure Emergency I I Procedures. Added Revision 3 to Report: VB-549. Revised Operating Instructions Index; 1 1 added Airspeed Data. Revised Aii Conditioner Ground Check; 7-4 added Annunciator Panel Check and Foot- note; relocated info. 7-5 Added info from Page 7-4 relocated Cruising info. PI1,OT'S OPE,RATING MANUAI. LOG OF REVISIONS (cont) 1 Revised Revision Description --D-atc Pages Rev 3 (cont) 7-6 Added Cruising info; added Mixture Control Lock and Footnote; relocated Approach and L.anding infb. 7-7 Added Approach and Landing infb; added Mixture Control Lock and Footnote; relocated Moorings and Weight and Balance infb. 7-8 Added Airspeed Data; added Moorings, and Weight and Balance info; relocated ELT info. 7-9 Added infb from Page 7-8; relocated Air Conditioning info. 7-1 0 Added Air Conditioning info; relocated info. 7-1 1 Added page; added relocated info. 8- 1 Added Annunciator Panel to item I I ; moved Item 13 to Page 8-2. 8-2 Added Item 13 from Page 8-1. 9-i Revised Performance Charts Index. 9- 2 Revised Takeoff Chart. 9-.3 Revised Climb Chart 9-4 Revised Airspeed Chart. 9-5 Revised Range Chart. 9-8 Revised Glide Chart. 9-9 Revised L.anding Chart. Rcv 4- 761 578 2-6 Added gear warning info. .Jan 28. 1975 (PR750178) 2-2 1 Revised Stall Warning info. ARROW I1 THIS PAGE. INTENTIONALLY LEFT BLANK ARROW 11 PILOT'S OPERATING MANUAL LOG OF REVISIONS (cont) Revised Description Date -- 10-9 Added info. from page 10-8. 10-11 Revised Service Bulletin info. ... Added including serial number. Feb. 29,1984 U1 1-2 Revised fuel and oil info. 2-21 Revised para. AFM Added Rev. 6 to Report: VB-560. W/B Added Rev. 9 to ~eportV: B-549. 9-i Added Warning. 10-7 Added info., and fuel grade chart, 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 preventive maintenance para., relocated info. from page 10-13. Moved info. to page 10-12. Revised Landing Gear. Jan. 31,1987 Relocated Warning Revised Throttle Quadrant and Console figures. 2-5 Revised Schematic. 2-6 Revised para. Added info. 2-16 Revised Instrument Panel fig. AFM Added Rev. 7 to Report: VB-560. 4-2 Revised Engine Power Loss During Take off para. Revised Engine Power Loss During Takeoff. Revised Power Off Landing. Gear Down Landing, and Gear Up Landing paras. Moved info. from page 4-5. Revised Emergency Gear Extension para. Moved info. to page 4-4. Revised Note. Revised footnote. Revised item 12. Revised Note. Added Note. Added note reference. PII,OT9SO PERATING MANUAL LOG OF REVISIONS (cont) - Revised Revision Description Pages --" - Rev. 12 761 578 Revised Oil info. Moved Dimensions and (PR900730) Landing Gear to page 1-4. Added page. Relocated Dimensions and Landing Gear from page 1-2. Revised Table of Contents. Revised Oil Requirements. Moved info.. to page 10-8. Relocated info..f rom 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 Service and inspection Periods. - Rev. 13 761-578 Added Warning. (PR050207) Added Rev. 8 to Report: VB-560. Revised Emergency Landing Gear Extension. 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. -1 Rev.. 14 - 761-578 Added Rev. 9 to Report: VB-560 'Q=M ....u---..p (PRO51 01 0 ) 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