Weight & Balance for Piper PA-28R Arrow III

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THE CHEROKEE DUPLICATE Arrow II PILOT'S OPERATING MANUAL 52297 BY ☐ PIPER This manual is incomplete without an APPROPRIATE FAA APPROVED AIRPLANE FLIGHT MANUAL and an APPROPRIATE WEIGHT AND BALANCE REPORT. W WARNING EXTREME CARE MUST BE EXERCISED TO LIMIT THE USE OF THIS MANUAL TO APPLICABLE AIRCRAFT. THIS MANUAL REVISED AS INDICATED BELOW OR SUBSEQUENTLY REVISED IS VALID FOR USE WITH THE AIRPLANE IDENTIFIED BELOW WHEN APPROVED BY PIPER AIRCRAFT CORPORATION. SUBSEQUENT REVISIONS SUPPLIED BY PIPER AIRCRAFT CORPORATION MUST BE PROPERLY INSERTED. MODEL PA-28R-200 AIRCRAFT SERIAL NO. 28R-7335366 PILOT'S OPERATING MANUAL, PART NUMBER 761 493 REVISION, PIPER AIRCRAFT CORPORATION APPROVAL SIGNATURE AND STAMP REGISTRATION NO. PR900720 че 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 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 transition from single to multi-engine flying. If 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. 761 493, may be obtained only from Piper Customer Services. Published by PUBLICATIONS DEPARTMENT Piper Aircraft Corporation 761 493 Issued: November 1971 APPLICABILITY This manual is applicable to Piper Model PA-28R-200 aircraft having serial numbers 28R-7235001 through 28-7335446. Contact Piper Customer Services for specific information on the application of this manual. 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. I. 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: Revision pages will replace only pages with the same page number. 1. 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. 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 2-22, 3-1 through 3-14, 4-1 through 4-8, 5-1 through 5-32, 6-1 through 6-8, 7-1 through 7-2, 8-1 through 8-9, 9-1 through 9-15. REVISIONS ISSUED Current Permanent and Temporary Revisions to the PA-31 Pilot's Operating Manual issued April, 1971 are as follows: 761 493 (PR720204) Permanent Revision Dated February 4, 1972 761 493 (PR720210) Permanent Revision Dated February 10, 1972 761 493 (PR720330) Permanent Revision 761 493 (PR720615) 761 493 (PR720911) 761 493 (PR720802) Permanent Revision Permanent Revision Permanent Revision to W/B Permanent Revision to W/B Dated March 30, 1972 Dated June 15, 1972 Dated September 11, 1972 Dated August 2, 1972 Dated November 14, 1972 761 493 (PR721114) 761 493 (PR730115) 761 493 (PR730330) 761 493 (PR730830) 761 493 (PR741018) 761 493 (PR751205) 761 493 (PR790410) 761 493 (PR840327) 761 493 (PR851125) 761 493 (PR860418) 761 493 (PR870131) 761 493 (PR900720) Permanent Revision to W/B Permanent Revision to F/M & P/O/M Permanent Revision to F/M & P/O/M Permanent Revision to F/M, W/B & P/O/M Permanent Revision to F/M, W/B & P/O/M Permanent Revision to F/M, W/B & P/O/M Permanent Revision to F/M, W/B & P/O/M Permanent Revision to F/M & P/O/M Permanent Revision to F/M Permanent Revision to F/M & P/O/M Permanent Revision to P/O/M Dated January 15, 1973 Dated March 30, 1973 Dated August 30, 1973 Dated October 18, 1974 Dated December 5, 1975 Dated April 10, 1979 Dated March 27, 1984 Dated November 25, 1985 Dated April 18, 1986 Dated January 31, 1987 Dated July 20, 1990 TABLE OF CONTENTS 1 GENERAL SPECIFICATIONS 2 DESCRIPTION-AIRPLANE AND SYSTEMS 3 FLIGHT MANUAL FAA APPROVED 4 EMERGENCY PROCEDURE 5 WEIGHT AND BALANCE 6 OPERATING INSTRUCTIONS 7 OPERATING TIPS 8 PERFORMANCE CHARTS 9 HANDLING AND SERVICING Performance. Weights Power Plant Fuel and Oil Baggage Dimensions Landing Gear GENERAL SPECIFICATIONS 1-1 1-1 1-1 1-2 1-2 1-2 IIIZZZZ 1-2 SPECIFICATIONS ARROW II PERFORMANCE Performance figures are for airplanes equipped for cross-country transportation and flown at gross weight under standard conditions at sea level or stated altitude. Any changes in equipment may result in changes in performance. Take-off Run (maximum effort, 25° flap) (ft) Take-off Over 50-ft Barrier (maximum effort, 25° flap) (ft) Best Rate of Climb Speed (gear retracted) (mph) Rate of Climb (ft per min) Service Ceiling (ft) Absolute Ceiling (ft) Top Speed (mph)