Piper Arrow IV Turbo User Manual

ELECTRICAL SCHEMATIC INDEX (cont.)
FIGURE NO. SCHEMATIC GRID NO.
FUEL SYSTEMS
Fuel Pump
91-15 PA-28RT-201 3I17
Fuel Pump/Diverter Valve/Aux. Fuel Ind.
91-17 PA-28RT-201T 3I17
INDICATORS
Annunciator (See Annunciator Systems)
Ammeter (See Alternator Systems)
Clock - Analog/Hourmeter/Digital Options
91-l8 PA-28RT-201/201T 3I18
Engine Instruments
91-19 PA-28RT-201 3I18
91-20 PA-28RT-201T: Early Models 3I19
91-21 PA-28RT-201T: Later Models 3I19
Fuel Aux. - Indicator
91-17 PA-28RT-201T 3I17
Gear Position Indicators
91-22 PA-28 RT-201/201T: Early Models 3I20
91-23 PA-28 RT-201/201T: Later Models 3I21
Turn and Bank
91-16 PA-28RT-201/201T 3I17
LANDING GEAR
Landing Gear
91-22 PA-28RT-201/201T: Early Models 3I20
91-23 PA-28RT-201: S/N’s: 28R-7X37025 and up 3I21
91-23 PA-28RT-201T: S/N’s: 28R-7X03057 and up 3I21
LIGHTING - EXTERNAL
Anti-Collision - Beacon
91-24 PA-28RT-201 only 3I22
Anti-Collision - Strobe
91-25 PA-28RT-201/201T 3I22
Landing Light
91-26 PA-28RT-201/201T 3I22
Navigation Lights
91-27 PA-28RT-201: S/N’s: 28R-79180001 to 8118039 3I22
91-28 S/N’s: 28R-8118040 and up 3I23
91-27 PA-28RT-201T: S/N’s: 28R-7931001 to 8131041 3I22
91-28 S/N’s: 28R-8131042 and up 3I23
91 - Elec. Sch. Index
Page - 2
Added: August 17, 1982
3I4
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

Piper Arrow IV Turbo Specifications

General

Manufacturer	Piper Aircraft
Model	Arrow IV Turbo
Horsepower	200 hp
Seating Capacity	4
Landing Gear	Retractable tricycle
Range	773 nautical miles
Service Ceiling	20, 000 ft
Fuel Capacity	72 gallons
Propeller	2-blade constant speed
Max Takeoff Weight	2, 900 lb (1, 315 kg)
Stall Speed (Flaps Down)	55 knots
Rate of Climb	1, 000 ft/min