PIPER AIRCRAFT CORPORATION PA-28RT-201T, TURBO ARROW IV
PIPER PA-28RT-201T Turbo Arrow · Pilot's Operating Handbook
Overview
The Pilot's Operating Handbook for the Piper PA-28RT-201T Turbo Arrow IV serves as a comprehensive guide for pilots, detailing operational procedures, limitations, and performance data. It emphasizes the importance of flight instruction and airworthiness, while providing structured sections for quick reference during flight.
- Designed for pilot operational guidance.
- Not a substitute for flight instruction.
- Pilot is responsible for airworthiness.
- Handbook includes emergency procedures.
- Sections are organized for quick reference.
- Contains manufacturer-supplied supplemental data.
- Pilot should familiarize with all sections before flight.
- Provisions for handbook expansion are included.
Document
Source
Originally published by fliegen.ch. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Pilot's Operating Handbook
- Year ·
- 1978
- File size ·
- 365 KB
- Publisher ·
- fliegen.ch
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Entry width (in) ·
- 17
- Entry height (in) ·
- 14
- Wing area sq (ft) ·
- 170.0
Performance
- Max ramp weight (lb) ·
- 2912
- Max landing weight (lb) ·
- 2900
- Max takeoff weight (lb) ·
- 2900
Weight & balance
- Max baggage weight (lb) ·
- 200
- Wing loading lbs per sq (ft) ·
- 14.5
What is the PIPER AIRCRAFT CORPORATION PA-28RT-201T, TURBO ARROW IV?
The PIPER AIRCRAFT CORPORATION PA-28RT-201T, TURBO ARROW IV is a pilot's operating handbook for the PIPER PA-28RT-201T Turbo Arrow, dated 1978.
Where does the PIPER AIRCRAFT CORPORATION PA-28RT-201T, TURBO ARROW IV come from?
This copy of the PIPER AIRCRAFT CORPORATION PA-28RT-201T, TURBO ARROW IV was originally published by fliegen.ch and is hosted on Sprinkle as a free, searchable reference copy.
What year was the PIPER AIRCRAFT CORPORATION PA-28RT-201T, TURBO ARROW IV published?
The PIPER AIRCRAFT CORPORATION PA-28RT-201T, TURBO ARROW IV — the PIPER PA-28RT-201T Turbo Arrow pilot's operating handbook on file — is dated 1978.
Most owners only have the POH. Here's the essential set for the PIPER PA-28RT-201T Turbo Arrow.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More PIPER PA-28RT-201T Turbo Arrowmanuals & documents
In this document
Introduction
The handbook is intended for maximum utilization as an operating guide for pilots, including required material and supplemental data.
Engines
Details about the engine include manufacturer, model, rated horsepower, and specifications such as bore and stroke.
Propellers
Information on propeller specifications including manufacturer, model, number of blades, and diameter.
Fuel
Covers fuel capacity, usable fuel, and fuel grades required for operation.
Standard Airplane Weights
References standard empty weight and useful load, along with maximum weights for takeoff, landing, and ramp.
Baggage Space
Details on baggage compartment volume and entry dimensions.
Safety notes
- Pilot must ensure the airplane is airworthy.
- Operational limitations must be adhered to.
- Emergency procedures are prioritized in the handbook.
- The handbook should not be used as a sole reference during flight.
- Current status of the handbook is essential for safe operation.
Full document text
PIPER AIRCRAFT CORPORATION PA-28RT-201T, TURBO ARROW IV SECTION 1 GENERAL SECTION I GENERAL 1.1 INTRODUCTION 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 CAR 3 and FAR Parl2l SubpartJ.It also contains supplemental data supplied by the airplane manufacturer. This handbook is not designed as a substitute for adequate and compe- tent flight instruction, knowledge of current airworthiness directives, appli- cable 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 responsi- bility 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 proce- dures, performance and other sections to provide easier access to informa- tion 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 ofthe 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: VB-940 1-1 ISSUED: NOVEMBER 30, 197t SECTION 1 GENERAL PIPER AIRCRAFT CORPORATION PA-28RT-201T, TURBO ARROW IV I 2'6.m" a I Wing Area (sq. ft.) 170.0 Min. Turning Radius (ft.) (from pivot point to wingip) 31.0 THREE VIEW Figure l-l REPORT: VB-940 1-2 ISSUED: NOVEMBER 30, 197t PIPER AIRCRAFT CORPORATION pn-zrnr-zolT, TURBO ARROW lv SECTION I GENERAL I.3 ENGINES (a) Number of Engines (b) Engine Manufacturer (c) Engine Model Number (d) Rated HorsePower (e) Rated SPeed (rPm) (f) Maximum Manifold Pressure (in. Hg) (g) Bore (in.) (h) Stroke (in') ii) Disptacement (cu. in.) 0) ComPression Ratio (k) Engine TYPe ISSUED: NOVEMBER 30, 1978 REVTSED: SEPTEMBER 14' 1979 I Teledyne Continental TSIO-360-FB 200 Sea Level to 12,000 Ft. DensitY Altitude 2575 4t 4.438 3.875 360 7.5:l Six CYlinder, Direct Drive, HorizontallY Opposed, Air Cooled, Turbosupercharged and Fuel lnjected l Hartzell F8459A-8R 2 BHC-C2YF-l( )F 7b 75 Constant SPeed, HydraulicallY Actuated REPORT: VB-940 l-3 I.5 PROPELLERS STANDARD (a) Number of ProPellers (b) ProPeller Manufacturer (c) Blade Model (d) Number of Blades (e) Hub Modcl (f) Propellcr Diamcter (in.) (l) Maximum (2) Minimum (g) ProPeller TYPc SEC'I'ION I GENERAI- I'I I'ER A ITICTIA IIT' CORPOR A'TION t,A-28I1't-201't, TURBO ARROW tV ot,'l'toNAl_ (a) Nurnllcl ol' l)r'opcllcrs (b) l'r'opcllcl N4arrrrlircturcr' (c) lllatlc Motlcl (d) Nunrbcr ol'llladcs (c) Hub Motlcl (l) l'ropcllcr I )ianrctcr (in.) (l) Maxinrrrrn (2) Mirrirrrunr (g) l'ropc'llcl l ypc I.7 FUEI, AVCAS ONI.Y (a) l"ucl Capacity (U.S. gal.) (total) (b) tJsablc fjucl (U.S. gal.) (total) (c) I;ucl Gradc. Aviation (l) Minirnurn Crade (2) Altcrnatc liucls 1.9 OlL (a) Oil Capacity (U.S. qts.) (b) Oil Spccilication (c) Oil Viscosity RIil'0ll'l': V8-940 l-4 I l'l a rtzcll Ir766l-2 tt ^t PHC-C3YF-r( )F t6 72 Constant Spced, I lyd raulically Actuatccl 100 Grecn or l00l-t lllue Aviation Gratte Itefer to latest rcvision o[ Continental Service Ilulletin "Fuel and Oil Grades" IJ M l.ts-244 llefer to Section 8 - paragraph S.19. ISSUED: NOVIiMBItR 30, 1978 REVISIID; Jl.Jl,Y 16, l9ll4 77 72 PIPER AIRCRAFT CORPORATION PA-28RT-201T, TURBO ARROW IV SECTION I GENERAL I.13 STANDARD AIRPLANE WEIGHTS Refer to Figure 6-5 for the Standard Empty Weight and the Useful Load. 1.I5 BAGGAGE SPACE (a) Compartment Volume (cu. ft.) (b) Entry width (in.) (c) Entry Height (in.) 1.T7 SPECIFIC LOADINGS r.1I MAXIMUM WEIGHTS (a) Maximum Takeoff Weight (lbs.) (b) Maximum Landing Weight (lbs.) (c) Maximum Ramp Weight (lbs.) (d) Maximum Weights in Baggage Compartment (a) Wing Loading (lbs. per sq. ft.) (b) Power Loading (lbs. per hp) ISSUED: NOVEMBER 30, 1978 REYISED: JULY 15, 1982 2900 2900 2912 200 l7 r4.5 REPORT: VB-940 1-5 24 22 20