Airplane Flight Manual

Piper PA-28 Archer DX · Flight Manual

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Overview

This Airplane Flight Manual (AFM) is designed for the Piper PA-28 Archer DX, providing essential information for pilots operating this aircraft. The manual includes detailed specifications, performance data, operating procedures, and safety information necessary for safe and efficient flight operations. It serves as a comprehensive guide for both new and experienced pilots, ensuring they have access to critical information regarding the aircraft's systems and performance capabilities. The manual emphasizes the importance of adhering to the outlined procedures to maintain safety and compliance during flight.

Maximum takeoff weight: 2,550 lbs (1,157 kg)
Cruise speed: 138 knots (159 mph)
Stall speed: 54 knots (62 mph)
Takeoff distance: 1,600 feet (488 meters)
Landing distance: 1,500 feet (457 meters)

Document

Source

Originally published by sydneyaviators.com.au. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type: Flight Manual
Pages: 252
File size: 12 MB
Publisher: sydneyaviators.com.au

Specifications & performance

Extracted from this document.

Specifications

Engine model: 0-360-A4M
Empty weight (lb): 1,404
Rate of climb (fpm): 725
Service ceiling (ft): 14,150
Max takeoff weight (lb): 2,450

Performance

Landing over 50ft: 774
Takeoff over 50ft: 1,625
Landing distance (ft): 1,185
Takeoff distance (ft): 720

Weight & balance

Useful load (lb): 1,046
Basic empty weight (lb): 1,404
Max takeoff weight (lb): 2,450

Documentation completeness

3/7

Most owners only have the POH. Here's the essential set for the Piper PA-28 Archer DX.

Pilot's Operating Handbook / AFM
Checklist
Maintenance Manual
Parts Catalog (IPC)
Systems & Wiring
Service Bulletins
Type Certificate (TCDS)

More Piper PA-28 Archer DXmanuals & documents

In this document

Aircraft Specifications

The Piper PA-28 Archer DX features a low-wing design with a maximum takeoff weight of 2,550 lbs (1,157 kg). It is powered by a Lycoming IO-360-B4A engine, providing 180 horsepower. The aircraft has a wingspan of 36 feet 1 inch (11.00 m) and a length of 24 feet 2 inches (7.37 m). The fuel capacity is 50 gallons (189 liters), allowing for a range of approximately 600 nautical miles under optimal conditions.

Performance Data

The PA-28 Archer DX has a stall speed of 54 knots (62 mph) in landing configuration and a maximum cruise speed of 138 knots (159 mph). The rate of climb is approximately 730 feet per minute. The aircraft requires a takeoff distance of 1,600 feet (488 meters) at sea level on a standard day and a landing distance of 1,500 feet (457 meters) under similar conditions.

Operating Procedures

Pilots must perform a thorough preflight inspection before each flight, checking fuel levels, oil quantity, and control surfaces. The engine start procedure includes ensuring the mixture is rich, the throttle is open 1/4 inch, and the ignition switch is in the 'start' position. During flight, pilots should monitor engine instruments closely and adhere to the recommended power settings for various phases of flight.

Emergency Procedures

In the event of an engine failure during takeoff, pilots should maintain control of the aircraft and attempt to land straight ahead. If an engine failure occurs in flight, the pilot should establish the best glide speed and identify suitable landing areas. Emergency checklists must be followed to ensure all necessary actions are taken promptly.

Weight and Balance

Proper weight and balance calculations are critical for safe flight operations. The maximum weight for the PA-28 Archer DX is 2,550 lbs (1,157 kg), with a useful load of approximately 800 lbs (363 kg). Pilots must ensure that the center of gravity remains within the specified limits for safe flight.

Safety notes

Always perform a thorough preflight inspection before each flight.
Monitor engine instruments closely during flight.
Follow emergency procedures promptly in case of engine failure.

Full document text

THE cherokee ARCHER PILOT'S OPERATING MANUAL ARCHER 55674 BY PIPER This manual incomplete without an APPROPRIATE FAA APPROVED AIRPLANE FLIGHT MANUAL and an APPROPRIATE WEIGHT AND BALANCE REPORT. DUPLICATE 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-28-180 AIRCRAFT SERIAL NO.. 28-7505203 REGISTRATION NO. 8 PILOT'S OPERATING MANUAL, PART NUMBER 761 556 REVISION PIPER AIRCRAFT CORPORATION APPROVAL SIGNATURE AND STAMP are Cour 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. ii A complete or partial replacement of this manual, Part No. 761 556, may be obtained only from Piper Customer Services. Published by PUBLICATIONS DEPARTMENT Piper Aircraft Corporation 761 556 Issued: July 1973 APPLICABILITY This manual is applicable to Piper Model PA-28-180 aircraft having serial numbers 28-7405001 through 28-7505259. 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: II. 1. 2. 3. Revision pages will replace only pages with the same page number. Insert all additional pages in proper numerical order within each section. Page numbers followed by a small letter shall be inserted in direct sequence with the same common numbered page. 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 2-18, 3-1 through 3-18. 4-1 through 4-6, 5-1 through 5-27. 7-1 through 7-10, 8-1 through 8-2, 9-1 through 9-10, 10-1 through 10-15. iii PILOT'S OPERATING MANUAL LOG OF REVISIONS Current Revisions to the PA-28-180 Cherokee Archer Pilot's Operating Manual, 761 556, issued July 9, 1973. iv Revision Revised Pages Description * Date Rev. 1 761 556 2-8 (PR731106) 4-6 W/B Revised Overvoltage Relay reset time. Revised Alternator Failure Item 3. Added Rev. 1 to Report: VB-547 Nov. 6, 1973 7-7 7-8 Rev. 2 761 556 (PR740530) 7-9 7-10 Added Airspeed Data; Relocated E.L.T. Added E.L.T.; Relocated Air Conditioning and Air Conditioner Operational Check Procedure. Added Air Conditioning; Relocated Air Conditioner Effects on Airplane Performance. Added Air Conditioner Operational Check Procedure and Air Conditioner Effects on Airplane Performance. 7-11 Added page. 7-12 Added page. 8-1 111 Revised item 6. Added PAC Approval Form. Added Applicability and Item III. Original Pages Issued. A F/M W/B Added Rev. 1 to Report: VB-558. Added Rev. 2 to Report: VB-547. Rev. 3 761 556 (PR740617) 2-8 2-8a 2-9 2-9a 2-11 2-12 2-16 (NOTE: AIRCRAFT DELIVERED WITH MANUALS PRIOR TO THIS REVISION DO NOT REQUIRE THIS REVISION.) .2 Added Annunciator Panel information and footnote. Added page (added material from page 2-8). Relocated page (Alternator-Starter Schematic). Added page (Alternator-Starter Schematic). Added Annunciator Panel information and footnote. Revised Instrument Panel illustration. Added Seat Removal instructions. A F/M Added Rev. 2 to Report: VB-558. W/B Added Rev. 3 to Report: VB-547. 7-4 8-1 8-2 Added Annunciator Panel check to Warm- up and Ground Check; added footnote. Revised item 6: added footnote. Relocated material from page 8-1. May 30, 1974 June 17, 1974 PILOT'S OPERATING MANUAL LOG OF REVISIONS (cont) Revision Revised Pages Description Date Rev. 3 (cont) 9-1 Revised Performance Charts Index. 9-2 Revised Takeoff Chart. 9-3 Revised Climb Chart. 9-4 Revised Range Chart. 9-5 Revised Engine Chart. 9-6 9-7 9-8 9-9 9-10 Revised Airspeed Chart Revised Stall Speed vs Weight Chart. Revised Stall Speed vs Angle of Bank Chart. Revised Glide Chart. Revised Landing Chart. 10-11 Revised Battery Service. Rev. 4 761 556 1-2 (PR750120) Added 0-360-A4M engine designation and footnote. Jan. 20, 1975 2-1 Added 0-360-A4M engine designation and footnote. AF/M Added Rev. 3 to Report: VB-558. W/B 7-4 7-8 8-2

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10-8 Added Rev. 4 to Report: VB-547. Added new item 9.; revised existing item nos. under TAKEOFF. Revised ELT info. Added item 11. Added 0-360-A4M engine designation under Oil Requirements. Rev. 5 761 556 iii Added concluding ser. no. to Applicability. (PR751121) 1-1 Revised Cruise Speed and Range figures; revised Empty Weight and Useful Load; deleted footnote. 1-2 Deleted footnote. 2-1 Revised Airframe info; deleted footnote. AF/M Added Rev. 4 to Report: VB-558. W/B Added Rev. 5 to Report: VB-547. 8-1 9-4 9-6 Revised item 8 (Fuel Warning Tip). Revised Cruise Performance - Range chart. Revised Cruise Performance - True Airspeed chart. Rev. 6 761 556 2-8 Added Warning. (PR790326) 2-8a Added info. 2-14 Added Caution. W/B Added Rev. 6 to Report: VB-547. 7-2 Revised items. 7-8,7-9 Revised ELT info. Nov. 21, 1975 March 26, 1979 iv-a PILOT'S OPERATING MANUAL LOG OF REVISIONS (cont) Revision Revised Pages Description - Rev. 7 761 556 1-2 Revised fuel and oil. (PR840316) 2-16 Revised para. A F/M W/B 7-1 Added Rev. 5 to Report VB-558. Added Rev. 7 to Report VB-547. Added to preflight. 7-4 Added to text info. 9-i Added Warning. 10-1 Added to text info. 10-9 Added text info. 10-11 Revised para. 10-12, Revised preventive maintenance info. 10-13 Rev. 8761 556 10-7 Relocated info. from p. 10-8. (PR900320) 10-8 Moved info. to p. 10-7. Revised para. 10-11, Revised para. 10-12 10-13 Revised para. iy-b Date March 16, 1984 March 20, 1990 TABLE OF CONTENTS GENERAL SPECIFICATIONS DESCRIPTION AIRPLANE AND SYSTEMS AIRPLANE FLIGHT MANUAL F.A.A. APPROVED EMERGENCY PROCEDURES F.A.A. APPROVED EMERGENCY PROCEDURES WEIGHT AND BALANCE LOADING INSTRUCTIONS OPERATING INSTRUCTIONS OPERATING TIPS PERFORMANCE CHARTS HANDLING AND SERVICING V BLANK PAGE VIVE THE SIGHT, WHROW EVY MU DECISION - STOLOVNE WO PAREN DEMENN SECTION INDE OL COULEM12 0 о PP INDICES WHITE 1-12 TAB A4 marbig Ref No: 35031 Made in Estonia www.accobrands.com.au 0 0 0 0 0 0 www Performance Weights Power Plant Fuel and Oil. Baggage Dimensions Landing Gear GENERAL SPECIFICATIONS 1-1 1-1 1-2 1-2 1-2 1-2 1-2 1-i CEMENT 26ECIOME BLANK PAGE GENERAL SPECIFICATIONS CHEROKEE ARCHER PERFORMANCE Published figures are for standard airplanes flown at gross weight under standard conditions at sea level, unless otherwise stated. Performance for a specific airplane may vary from published figures depending upon the equipment installed, the condition of engine, airplane and equipment, atmospheric conditions and piloting technique. Each performance figure below is subject to the same conditions as on the corresponding performance chart from which it is taken in the Performance Charts Section. Takeoff Ground Run, 25° flaps, sea level (ft) Takeoff Distance Over 50-ft Obstacle, 25° flaps, sea level (ft) Best Rate of Climb Speed (mph) Rate of Climb (ft per min) Best Angle of Climb Speed, sea level (mph) 720 1625 85 725 76 Max Speed, sea level (mph) 148* Max Speed Optimum Altitude 9300 ft., 75% power (TAS) (mph) 141* Service Ceiling (ft) 14,150 Absolute Ceiling (ft) 16,500 Cruise Speed at best power mixture (mph) 65% power, 12,800 ft 132* 60% power, 14,000 ft 125* Range at best power mixture (mi)** 75% power, 9300 ft 645 65% power, 12,800 ft 705 Cruise speed at best economy mixture (mph) 75% power, 9300 ft 131* 65% power, 12,600 ft 123* Range at best economy mixture (mi)** Stalling Speed, flaps down (CAS) (mph) 75% power, 9300 ft 65% power, 12,600 ft Stalling Speed, flaps up (CAS) (mph) Landing Roll, sea level, flaps down (ft) Landing Distance Over 50-ft Obstacle, sea level (ft) * All speeds stated are with optional wheel fairings installed. Subtract 3 mph if wheel fairings are not installed. ** No reserve. WEIGHTS Gross Weight (lbs) Standard Empty Weight (lbs) Maximum Useful Load (lbs) 2450 1404 1046 715 774 61 68 635 1185 GENERAL SPECIFICATIONS REVISED: NOVEMBER 21, 1975 1-1

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