Skip to main content
Sell

Piper PA-28RT Arrow IV Turbo Model Guide

Piper PA-28RT Arrow IV Turbo · Model Guide

Free account — keep the POHs & checklists you reference in one place.

Overview

The Piper PA-28RT Arrow IV Turbo is a four-seat, single-engine piston airplane built from 1979 to 1982. It has a 200 hp Continental TSIO-360-FB, a six-cylinder, turbosupercharged, fuel-injected engine. The engine drives a Hartzell constant-speed, hydraulically actuated propeller. Maximum takeoff weight is 2900 lbs.

  • Four seats, 1979-1982 production, turbosupercharged fuel-injected Continental TSIO-360-FB rated at 200 hp.
  • Maximum takeoff and landing weight are both 2900 lbs. Maximum ramp weight is 2912 lbs. Baggage limit is 200 lbs.
  • FAA AD 82-06-11 R1 requires nose landing gear inspection, rigging and modification on listed serial numbers.
  • Wing removal is governed by AD 87-08-08, and the wing spar must be inspected whenever a wing is removed.

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 sprinkle.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

View original at sprinkle.com

Report a problem or request removal

Document details

Type
·
Model Guide
Year
·
2026
File size
·
48 KB
Copy found at
·
sprinkle.com

Specifications & performance

Extracted from this document.

Specifications

Max ramp weight (lb)
·
2,912
Rated horsepower (hp)
·
200
Max baggage weight (lb)
·
200
Max landing weight (lb)
·
2,900
Max takeoff weight (lb)
·
2,900
Propeller diameter max (in)
·
76
Propeller diameter min (in)
·
75
About this document
What engine does the Piper PA-28RT Arrow IV Turbo use?

The Piper PA-28RT Arrow IV Turbo uses a Continental TSIO-360-FB. It is a six-cylinder, direct-drive, air-cooled, turbosupercharged, fuel-injected engine rated at 200 hp at 2575 rpm.

What is the maximum takeoff weight?

The Piper PA-28RT Arrow IV Turbo has a maximum takeoff weight of 2900 lbs. Maximum landing weight is also 2900 lbs and maximum ramp weight is 2912 lbs. The baggage compartment is limited to 200 lbs.

Which airworthiness directives should a buyer check on the Piper PA-28RT Arrow IV Turbo?

Check AD 82-06-11 R1 for nose landing gear inspection and rigging, within 100 hours of its effective date. Check AD 87-08-08 for the wing spar inspection. Review the logbooks for compliance with both.

What is the Piper PA-28RT Arrow IV Turbo Model Guide?

The Piper PA-28RT Arrow IV Turbo Model Guide is a model guide for the Piper PA-28RT Arrow IV Turbo, dated 2026.

What year was the Piper PA-28RT Arrow IV Turbo Model Guide published?

The Piper PA-28RT Arrow IV Turbo Model Guide — the Piper PA-28RT Arrow IV Turbo model guide on file — is dated 2026.

Documentation completeness
3/7

Most owners only have the POH. Here's the essential set for the Piper PA-28RT Arrow IV Turbo.

This aircraft
Browse all aircraft modelsAircraft directory
For sale
Browse all aircraft for saleAircraft wanted ads
Your library
All Piper PA-28RT Arrow IV Turbo manuals20All Piper manualsFull manuals libraryMy hangar
Tools
Identify an aircraftTail number lookupAircraft matcherCompare aircraftCan I land here?Where can it land?
Explore Sprinkle
Aircraft directoryManufacturersAirlinesEnginesAircraft for sale
For professionals
List an aircraft for salePost a wanted adDealer & broker directoryData & API licensingData sources

More Piper PA-28RT Arrow IV Turbomanuals & documents

See all 19 →

In this document

Engine and propeller

The Continental TSIO-360-FB is rated 200 hp at 2575 rpm, with a 41 in. Hg maximum manifold pressure. It has 360 cu in displacement and a 7.5:1 compression ratio. It is direct drive, air cooled and horizontally opposed. The standard Hartzell propeller is two-bladed, 76 in. maximum and 75 in. minimum diameter. Fuel is 100 green or 100LL blue avgas only.

Weights and dimensions

Maximum takeoff weight is 2900 lbs and maximum landing weight is 2900 lbs. Maximum ramp weight is 2912 lbs and the baggage compartment is limited to 200 lbs. Wing area is 170.0 sq ft and minimum turning radius, pivot point to wingtip, is 31.0 ft. Check the standard empty weight and the current weight and balance record for the actual airplane before working out useful load.

Documents and parts support

The Turbo Arrow IV Information Manual is the pilot's handbook. A combined PA-28RT-201/201T maintenance manual and parts catalog (P/N 761 693) also cover the airplane. The maintenance manual lists a Program Inspection Manual, P/N 761 736. The model is listed with the PA-28 family under FAA Type Certificate 2A13 in the New Zealand CAA airworthiness directive schedule.

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

  • AD 82-06-11 R1 covers PA-28RT-201T serials 28R-7931001 through 28R-8131193. Confirm nose gear inspection, rigging and modification per Piper SB 724A is logged.
  • Confirm AD 87-08-08 wing spar inspection compliance. Service Letter 997 gives the wing removal and reinstallation procedure.
  • The handbook is valid only for the airplane named on its title page and only if kept current. Verify the copy matches the airplane's serial number.

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 PA-28RT Arrow IV Turbo Model Guide The Piper PA-28RT Arrow IV Turbo is a four-seat, single-engine piston airplane built from 1979 to 1982. It has a 200 hp Continental TSIO-360-FB, a six-cylinder, turbosupercharged, fuel-injected engine. The engine drives a Hartzell constant-speed, hydraulically actuated propeller. Maximum takeoff weight is 2900 lbs. • Four seats, 1979-1982 production, turbosupercharged fuel-injected Continental TSIO-360-FB rated at 200 hp. • Maximum takeoff and landing weight are both 2900 lbs. Maximum ramp weight is 2912 lbs. Baggage limit is 200 lbs. • FAA AD 82-06-11 R1 requires nose landing gear inspection, rigging and modification on listed serial numbers. • Wing removal is governed by AD 87-08-08, and the wing spar must be inspected whenever a wing is removed. Engine and propeller The Continental TSIO-360-FB is rated 200 hp at 2575 rpm, with a 41 in. Hg maximum manifold pressure. It has 360 cu in displacement and a 7.5:1 compression ratio. It is direct drive, air cooled and horizontally opposed. The standard Hartzell propeller is two-bladed, 76 in. maximum and 75 in. minimum diameter. Fuel is 100 green or 100LL blue avgas only. Weights and dimensions Maximum takeoff weight is 2900 lbs and maximum landing weight is 2900 lbs. Maximum ramp weight is 2912 lbs and the baggage compartment is limited to 200 lbs. Wing area is 170.0 sq ft and minimum turning radius, pivot point to wingtip, is 31.0 ft. Check the standard empty weight and the current weight and balance record for the actual airplane before working out useful load. Documents and parts support The Turbo Arrow IV Information Manual is the pilot's handbook. A combined PA-28RT-201/201T maintenance manual and parts catalog (P/N 761 693) also cover the airplane. The maintenance manual lists a Program Inspection Manual, P/N 761 736. The model is listed with the PA-28 family under FAA Type Certificate 2A13 in the New Zealand CAA airworthiness directive schedule. Safety notes: • AD 82-06-11 R1 covers PA-28RT-201T serials 28R-7931001 through 28R-8131193. Confirm nose gear inspection, rigging and modification per Piper SB 724A is logged. • Confirm AD 87-08-08 wing spar inspection compliance. Service Letter 997 gives the wing removal and reinstallation procedure. • The handbook is valid only for the airplane named on its title page and only if kept current. Verify the copy matches the airplane's serial number.

All Piper PA-28RT Arrow IV Turbo model guide