Pilot's Operating Handbook
PIPER ARCHER II · Pilot's Operating Handbook
Overview
The Pilot's Operating Handbook for the Piper Archer II serves as an operational guide for pilots, detailing essential information required for safe flight operations. It includes specifications, performance data, and limitations, while emphasizing the importance of flight instruction and airworthiness.
- The handbook is not a substitute for flight instruction.
- Pilots must ensure the aircraft is airworthy before flight.
- Emergency procedures are prioritized for quick reference.
- The handbook is structured for easy navigation with tab dividers.
- It includes both manufacturer data and regulatory requirements.
- The pilot is responsible for adhering to operational limitations.
- The handbook should be kept current for operational use.
- Specific sections are intentionally left blank for future expansion.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at fliegen.ch. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Pilot's Operating Handbook
- Year ·
- 1979
- File size ·
- 366 KB
- Copy found at ·
- fliegen.ch
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Wing area sq (ft) ·
- 170.0
- Entry width (in) ·
- 22
- Entry height (in) ·
- 20
- Min turning radius (ft) ·
- 30.0
- Oil capacity u s quarts ·
- 8
- Baggage compartment volume cubic feet ·
- 24
Performance
- Takeoff power bhp ·
- 180
- Max continuous power bhp ·
- 180
- Max continuous engine speed rpm ·
- 2700
Weight & balance
- Max ramp weight (lb) ·
- 2558
- Max landing weight (lb) ·
- 2550
- Max takeoff weight (lb) ·
- 2550
What is the Pilot's Operating Handbook?
The Pilot's Operating Handbook is a pilot's operating handbook for the PIPER ARCHER II, dated 1979.
What year was the Pilot's Operating Handbook published?
The Pilot's Operating Handbook — the PIPER ARCHER II pilot's operating handbook on file — is dated 1979.
Common. One of the most common aircraft types we track.
Most owners only have the POH. Here's the essential set for the PIPER ARCHER II.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
PIPER ARCHER II for sale now
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In this document
Introduction
The handbook is designed for maximum utilization as an operating guide and includes material required by regulations and supplemental data from the manufacturer.
Engines
Details about the engine specifications including manufacturer, model, power limits, and engine type are provided.
Propellers
Information on the propeller specifications including manufacturer, model, number of blades, and type is included.
Fuel
The handbook specifies fuel capacity, usable fuel, and minimum octane requirements.
Maximum Weights
Maximum ramp, takeoff, and landing weights are outlined along with baggage compartment weight limits.
Baggage Space
Specifications for baggage compartment volume and entry dimensions are provided.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Safety notes
- The pilot is responsible for determining the aircraft's safety for flight.
- The handbook should not be used for operational purposes unless current.
- Emergency procedures are critical and should be reviewed before flight.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
PIPER AIRCRAFT CORPORATION PA-2&lu, ARCHER II SECTION T GENERAL SECTION 1 GENERAL 1.1 INTRODUCTION This Pilot's Operating Handbook is designed for maximum utilization as an op€rating guide for the pilot. It includes the material required to be furnished to the pilot by C.A.R. 3 and FAR Part2l, Subpart J. It also contains sripplemental data supplied by the airplane manufacturer. This handbook is not designed as a substitutc 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 thc 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 lbr 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 intentionally left blank. REPORT: VF1120 1-l ISSUED: JULY 2,1979 SECTION 1 GENERAL PIPER AIRCRAFT CORPORATION PA-2&1t1, ARCHER II I \ t2' te' !.0t" THREE VIEW Figure l-l Wing Area (sq. ft.) Min. Turning Radius (ft.) (from pivot point to wingtip) z', 170.0 30.0 I' 8.20" I' Lll" REPORT: VB-1120 t-2 ISSUED: JULY 2,1979 PIPER AIRCRAFT CORPORATION PA-28-181, ARCHER II SECTION 1 GENERAL I.3 ENGINES (a) Number of Engines (b) Engine Manufacturer (c) Engine Model Number (d) Takeoff Power - 5 Minute Limit (BHP) (e) Takeoff Engine Speed - 5 Minute Limir (RPM) (f) Maximum Continuous Power (BHP) (g) Maximum Continuous Engine Speed (RPM) (h) Bore (inches) (i) Stroke (inches) 0) Displacement (cubic inches) (k) Compression Ratio (l) Engine Type I.5 PROPELLERS (a) Number of Propellers (b) Propeller Manufacturer (c) Model (d) Number of Blades (e) Propeller Diamete r (inches) (l) Maximum (2) Minimum (f) Propeller Type I.7 FUEL AVCAS ONLY (a) Fuel Capacity (U.S. gal.) (rorat) (b) Usable Fuel (U.S. gal.) (total) (c) Fuel (l) Minimum Octane (2) Alternate Fuel' ISSUED: JULY 2,1979 REVfSED: JUNE 29,1984 2650 5.t25 4.375 36 r.0 8.5: I Four Cylinder, Direct Drive, Horizontally Opposed, Air Cooled I Sensenich 76EM8S5-0-62 2 76 76 Fixed Pitch 100 Green or l00LL Blue Aviation Grade Refer to latest issue of Lycoming lnstruction No. 1070. REPORT: VB-I120 '1-3 I Lycoming 0-360-44M or o-360-A4A t80 2700 t78 50 48 SECTION 1 GENERAL PIPER AIRCRAFT CORPORATION PA-28-181, ARCHER II r.9 orl, (a) Oil Capacity (U.S. quarts) (b) Oil Specification (c) Oil Viscosity per Average Ambient Temp. for Starting (l) Above 600F (2) 30'F to 90oF (3) 0oF to 70oF (4) Below l0oF 1.11 MAXIMUM WEIGHTS (a) Maximum Ramp Weight (lbs.) (b) Maximum Takeoff Weight (lbs.) (c) Maximum Landing Weight (lbs.) (d) Maximum Weights in Baggage Compartment (lbs.) REPORT: VB-1120 l-4 200 0 ISSUED: JULY 2,1979 REVISED: JULY 21,1982 8 Refer to latest issue of Lycoming Service Instruction 1014. Single s.A.E. 50 s.A.E.40 s.A.E. 30 s.A.E. 20 Multi S.A.E. 40 or 50 s.A.E.40 S.A.E.40 or 20w-30 s.A.E.20W-30 Normal 2558 2550 2550 Utility 2138 2130 , 2130 1.13 STANDARD AIRPLANE WEIGHTS Refer to Figure 6-5 for the Standard Empty Weight and the Useful Load. PIPER AIRCRAFT CORPORATION PA-2t-1t1, ARCHER II SECTION 1 GENERAL 1.I5 BAGGAGE SPACE (a) Compartment Volume (cubic feet) (b) Entry Width (inches) (c) Entry Height (inches) r.17 SPECIFIC LOADINGS (a) Wing Loading (lbs. per sq. ft.) (b) Power Loading (lbs. per hp) 24 22 20 15.0 14.2 REPORT: VB-1120 1-5 ISSUED: JULY 2,1979