EasyManuals Logo

Piper Arrow IV Turbo User Manual

Piper Arrow IV Turbo
752 pages
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Page #43 background imageLoading...
Page #43 background image
CHART 601. LEADING PARTICULARS AND PRINCIPAL DIMENSIONS (cont)
MODEL PA-28RT-201 PA-28RT-201T
ENGINE (cont)
Spark Plugs (Shielded):
AC SR86 SR86, S86R, HSR86
Champion REM38E REM38W, RHM38W,
RHM38EP, REM38P,
REM38E, RHM38E
Autolite SH-15 PH26, PH260
Red Seal SE270, SE270P,
SJ270, SJ270P
Spark Plug Gap Setting 0.015 to 0.021 0.15 to 0.19
Firing Order 1-3-2-4 1-6-3-2-5-4
Starter - Prestolite (12-volt) MZ4206 MCL-6501
Alternator:
Chrysler (60 AMP) 3656624 or 4111810
Prestolite (60 AMP) ALY-6422
Prestolite (65 AMP) ALX-9425
Alternator Voltage Regulator, WICO X16300B X16300B
Alternator Overvoltage Relay, WICO X16799B X16799B
PROPELLER - Constant Speed
Manufacturer McCauley Hartzell
Hub, Model B2D34C213
1
or 2D34C215
2
BHC-C2YF-1-BF
Blade, Model 90DHA-16
1
or 90DJA-14E
2
F8459A-8R
Diameter (in.) 74.0 76.0
Diameter, Minimum (in.) 73.0 75.0
Blade Angle, Low Pitch* 12.5° ± 0.2° 14.4° ± 0.2°
Blade Angle, High Pitch* 29.8° ± 0.5° 29° ± 1.0°
Governor Control and Model Hartzell F-2-7( ) Hartzell E-5 or Wood
ward G210681
Manufacturer Hartzell Hartzell
Hub, Model HC-C2YK-1BF PHC-C3YF-1( )F
Blade, Model F7666A-2R F7663-2R
Diameter (in.) 74.0 76.0
Diameter, Minimum (in.) 72.5 72.0
*MEASURED AT 30 INCH STATION
1 USED ON S/N 28R-7918001 TO 28R-7918306 INCL.
2 USED ON S/N 28R-8018001 AND UP
6-10-00
Page 6-02
Revised: August 17, 1982
1B19
PIPER AIRCRAFT
PA-28RT-201 / 201T
* MAINTENANCE MANUAL

Table of Contents

Questions and Answers:

Question and Answer IconNeed help?

Do you have a question about the Piper Arrow IV Turbo and is the answer not in the manual?

Piper Arrow IV Turbo Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelArrow IV Turbo
Horsepower200 hp
Seating Capacity4
Landing GearRetractable tricycle
Range773 nautical miles
Service Ceiling20, 000 ft
Fuel Capacity72 gallons
Propeller2-blade constant speed
Max Takeoff Weight2, 900 lb (1, 315 kg)
Stall Speed (Flaps Down)55 knots
Rate of Climb1, 000 ft/min

Related product manuals