Piper PA28-181 Archer II Pilot's Operating Handbook POH INSTANT *

PILOT’S OPERATING HANDBOOK PIPER CHEROKEE ARCHER II FAA APPROVED IN NORMAL AND UTILITY CATEGORIES BASED ON CAR 3 AND FAR PART 21, SUBPART J. THIS HANDBOOK INCLUDES THE MATERIAL REQUIRED TO BE FURNISHED TO THE PILOT BY CAR 3 AND FAR PART 21, SUBPART J AND MUST BE CARRIED IN THE AIRPLANE AT ALL TIMES. AIRPLANE SERIAL NO. _____________________________ AIRPLANE REGISTRATION NO. ______________________ PA-28-181 REPORT: VB-760 FAA APPROVED BY: _______________________________ WARD EVANS D.O.A. NO. SO-1 PIPER AIRCRAFT CORPORATION VERO BEACH, FLORIDA DATE OF APPROVAL: AUGUST 15, 1975

Published by PUBLICATIONS DEPARTMENT Piper Aircraft Corporation Issued: August 15, 1975 REPORT: VB-760 ii 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 ON THE FACE OF THE TITLE PAGE WHEN OFFICIALLY APPROVED. SUBSEQUENT REVISIONS SUPPLIED BY PIPER AIRCRAFT CORPORATION MUST BE PROPERLY INSERTED. MODEL PA-28-181, CHEROKEE ARCHER II PILOT’S OPERATING HANDBOOK, REPORT: VB-760 REVISION_________________________________ PIPER AIRCRAFT CORPORATION APPROVAL SIGNATURE AND STAMP ________________________________________________________

APPLICABILITY The aircraft serial number eligibility bracket for application of this handbook is 28-7690001 through 28-7690467. The specific application of this handbook is limited to the Piper PA-28-181 model airplane designated by serial number and registration number on the face of the title page of this handbook. This handbook cannot be used for operational purposes unless kept in a current status. REVISIONS The information compiled in the Pilot's Operating Handbook 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 handbook and/or to add information to cover added airplane equipment. 1. Revisions Revisions will be distributed whenever necessary as complete page replacements or additions and shall be inserted into the handbook 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 outside margin of the page. opposite revised, added or deleted material. A line along the outside margin of the page opposite the page number will indicate 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. ORIGINAL PAGES ISSUED The original pages issued for this handbook prior to revision are given below: Title, ii through v, 1-1 through 1-14, 2-1 through 2-8, 3-1 through 3-12, 4-1 through 4-16, 5-1 through 5-26,6-1 through 6-52, 7-1 through 7-26, 8-1 through 8-16, 9-1 through 9-14. 10-1 through 10-2. REPORT: VB-760 iii

PIL OT' S OPERATING HANDBOOK LOG OF REVISIONS Current Revisions to the PA·28·I S1 Cherokee Archer 11 Pilot's Operating Handbook, REPOR T: VB-760 issued Augus t 15 . 1975. Revision Number and Code Rev. I ·7616 19 (PR760106) Rev.2·761619 (PR761112) Rev.3-761619 (PR770601) Rev. 4-76l619 (PR790316) RE PORT: VB·760 iv Revised Pages 6-i 6·37 6·44 6·46 7·25 8·5 3·3 3·8 3·9 4·14 5·4 5·9 5·13 5·14 5-143 5·14b 5-25 5-26 6· 35 6-36 6·46 7· 25 4·1 4·4 4·9 '" 1·4 4·5 5·5 5·14 5·14b 6·1 6·3 7·10 FAA Approval Description of Revi sion SignalUre and Date Re!vised wording of 6. 9 (a). Re moved Pi pe r Dwg. No. from item 1 55. Adde d items 236 and 238. c. .) ,w.! .. Revised item 263. Revised ELT pilot's re mote swit ch info. Ward Eva ns Revised 8.7 (a), items (I), (2), and (3), lan. 6. 1976 Revised chec klist. Revised word ing of 3. 11. Revised 3.15 inf o. Rev i se d ap proach speed in 4.29. Rev ised takeoff perfonn ance. Added Fig. 5·6. 5· 8, and 5·30. Revised Fig . 5-5. Added Fig. 5-6 (Fl aps Up Ground Roll ). Added page (added revised Fig. 5-7), Added page (added Fig. 5-8 - 25° Ground Ro ll ). Revised Fig. 5-29. Added Fig. 5- 30 (Landing Ground Roll ). Added i!ems 114 and 116. ... Relocated items 127 and 129, added items 131 and 133. A.dded PAL transmitter item 263 (c), revised item 263 (0) to 263 (d ). Revised ELT transmiuer info. Ward Evans Revised ELT pil ot's remo te sw itch info. Nov. 12, 1 976 Revised item 4.3 (c). Revised St ar li ng Engine When Hot. Ward Evans Revised item 4, 13 (b) June I, 1977 Added serial no. effectivity. Revised para. 1.13 and footnote. Revised para. 4.5. Revised para. 5.5. Revised Fig. 5-6. Revised Fig. 5-8. Revised para. 6. 1. Added Caution to para. 6.3. Added Warning to par a. 7.15.

Revi sion Number and Code Rev. 4 -761619 (pR790316) (cont) Rev. 5 - 76 1 61 9 (PR900608) PILOT'S OPERATING HANDBOOK LOG OF REVISIONS (conI) Revised Pages Desa1ption of Revision 7-11 Revised para 7.15. 7-21 Added Caullon to para. 7.23. 7-24 Revised para. 7.37. 8-13 Added Caution 10 pon. 8.21 ; re10cated info to pg . 8-14 . 8-14 Added info. from pg. 8-13; relocated info. 10 pg . 8-15 . 8- 15 Added info. from pg. 8-14. 1- 3 Revised para , 1.9. Item (c). 8- 1 Revised para. 8. t. 8-3 Revised para. 8.3. 8-4 Revised para. 8.5. 8-1 J Revised para 8.19. Revised para 8.21, item b. Relocated para . 8.21, item (c) to pg .8 -12. 8-11 a Added page. 8-1l b Added page. Added Fuel Comparison Chart. Added info. 10 para. 8.21. item (b). 8-12 Added rel ocated para. 8.21, item (c) from pg . 8-11 FAA Approval Signature and Date Ward Evans March 16, 1979 D.H. Trompler Jul y 30. 1990 REPORT: VB-760 iv-a

SECTION 1 SECTION 2 SECTION 3 SECTION 4 SECTION 5 SECTION 6 SECTION 7 SECTION 8 SECTION 9 SECTION 10 TABLE OF CONTENTS GENERAL LIMITATIONS EMERGENCY PROCEDURES NORMAL PROCEDURES PERFORMANCE WEIGHT AND BALANCE DESCRIPTION AND OPERATION OF THE AIRPLANE AND ITS SYSTEMS AIRPLANE HANDLING} SERVICING AND MAINTENANCE SUPPLEMENTS SAFETY TIPS REPORT: VB-760 v

Paragraph No. TABLE OF CONTENTS SECTION! GENERAL Page No. 1.1 Introduction ............... ......... ................................................................................................................. I-I 1.3 Engines................................................................................................................................................ 1-3 1.5 Propellers ....... ............... ...................................................................................................................... 1- 3 1.7 Fuel ..................................................................................................................................................... 1-3 1.9 Oil ....................................................................................................................................................... 1-3 1.11 Maximum Weights. ............................................................................................................................. 1-4 1.13 Standard Airplane Weights ................................................................................................................. 1-4 1.15 Baggage Space .......... .......................................................................................................................... 1-4 1.17 Specific Loadings................................................................................................................................ 1-4 1.19 Symbols, Abbreviations and Terminology .......................................................................................... 1-5 1.21 Conversion Factors ............................................................................................................................. I-II REPORT: VB-760 l-i

PIPER AIRCRAFT CORPORATION PA-28-181, CHEROKEE ARCHER II 1.1 INTRODUCTION SECTION 1 GENERAL SECTION 1 GENERAL This Pilot's Operating Handbook is designed for maximum utilization as an operating guide for the pilot. It includes the material required to be furnished to the pilot by C.A.R. 3 and FAR Part 21, Subpart J. It also contains supplemental data supplied by the airplane manufacturer. This handbook is not designed as a substitute for adequate and competent flight instruction, knowledge of 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 and should not be used for operational purposes unless kept in a current status. 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 as outlined by instrument markings, placards, and this handbook. Although the arrangement of this handbook is intended to increase its in-flight capabilities, it should not be used solely as an occasional operating reference. The pilot should study the entire handbook to familiarize himself with the limitations, performance, procedures and operational handling characteristics of the airplane before flight. The handbook has been divided into numbered (arabic) sections, each provided with a "finger-tip" tab divider for quick reference. The limitations and emergency procedures have been placed ahead of the normal procedures. performance and other sections to provide easier access to information that may be required in flight. The "Emergency Procedures" Section has been furnished with a red tab divider to present an instant reference to the section. Provisions for expansion of the handbook have been made by the deliberate omission of certain paragraph numbers. figure numbers. item numbers and pages noted as being left blank intentionally. ISSUED: AUGUST 15, 1975 REPORT: VB-760 1-1

SECTION 1 GENERAL 1-----12' IU."-----t PIPER AIRCRAFT CORPORATION PA-28-181, CHEROKEE ARCHER II t'L'" Wing Area (sq. ft.) 170.0 Min. Turning Radius (ft.) 30.0 (from pivot point to wingtip) n----"--------.:==nn- 3' '.20" I --L-L_----li 1-1 ._----------35' 0.0 ... -------------1 REPORT: VB-760 1-2 1-1.--10' U."----i ;--------23' UI" \ THREE VIEW Figure 1-1 1'3.10" ISSUED: AUGUST 15, 1975

PIPER AIRCRAFT CORPORATION PA-28-181, CHEROKEE ARCHER II 1.3 ENGINES (a) Number of Engines (b) Engine Manufacturer (c) Engine Model Number (d) Rated Horsepower (e) Rated Speed (rpm) (f) Bore (inches) (g) Stroke (inches) (h) Displacement (cubic inches) (i) Compression Ratio U) Engine Type 1.5 PROPELLERS (a) Number of Propellers (b) Propeller Manufacturer (c) Model (d) Number of Blades (e) Propeller Diameter (inches) (I) Maximum (2) Minimum (f) Propeller Type 1.7 FUEL AVGAS ONLY (a) Fuel Capacity (U.S. gal.) (total) (b) Usable Fuel. (U.S. gal.) (total) (c) Fuel Grade. Aviation (min. octane) 1.9 OIL (a) Oil Capacity (U.S. Quarts) (b) Oil Specification SECTION 1 GENERAL Lycoming 0-360-A4M 180 2700 5.125 4.375 361.0 8.5: 1 Four Cylinder, Direct Drive Horizontally Opposed, Air Cooled Sensenich 76EM8S5-0-60 2 76 76 Fixed Pitch 50 48 100/130 Green 8 Refer to latest issue of Lycoming Instruction No. 1014. (c) Oil Viscosity per Average Ambient Temp. for Starting () ) All Temperatures (2) Above 80°F (3) Above 60°F (4) 30°F to 90°F (5) O°F to 70°F (6) O°F to 90°F (7) Below 10°F MIL-L-6082B Mineral SAE Grade 60 50 40 30 20W-50 20 MIL-L-22851 Ashless Dispersant SAE Grades 15W-50 or 20W-50 60 40 or 50 40 30,40 or 20W-40 20W-50 or JSW-50 30 or 20W-30 When operating temperatures overlap indicated ranges, use the lighter grade oil. ISSUED: AUGUST 15, 1975 REVISED: JUNE 8, 1990 REPORT: VB-760 1-3

Piper PA28-181 Archer II Pilot's Operating Handbook POH INSTANT *

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