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Piper PA-39 Twin Comanche C/R Model Guide

Piper PA-39 Twin Comanche C/R · Model Guide

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Overview

The Piper PA-39 Twin Comanche C/R is a twin-engine piston airplane built from 1970 to 1972, with 4 to 6 seats. It was the final production Twin Comanche, with counter-rotating propellers and handed engines. Only 155 were built (serials 39-1 through 39-155). Gross weight is 3600 pounds, in the Normal category.

  • Final Twin Comanche version: counter-rotating props and handed engines. Only 155 PA-39s were built, against 2000 PA-30s.
  • Gross weight is 3600 pounds. The airplane is certified in the Normal category only.
  • Service Bulletin 1026 (vacuum pump flexible coupling) lists serials 39-1 through 39-155. Confirm it was done.
  • A 70-inch Hartzell replacement propeller kit lists the PA-39 as applicable, with a 2400 hour / 6 year TBO.

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.

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Document details

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

Specifications & performance

Extracted from this document.

Specifications

Max takeoff weight (lb)
·
3,600
About this document
How many Piper PA-39 Twin Comanche C/R airplanes were built?

Per the type acceptance report, only 155 examples of the Piper PA-39 Twin Comanche C/R were manufactured, serials 39-1 through 39-155, compared with 2000 PA-30 series airplanes.

What sets the Piper PA-39 Twin Comanche C/R apart from earlier Twin Comanches?

The Piper PA-39 Twin Comanche C/R was the final production version. It has counter-rotating propellers and handed engines. It was built from 1970 to 1972.

What is the gross weight of the Piper PA-39 Twin Comanche C/R?

The Piper PA-39 Twin Comanche C/R handbook lists a gross weight of 3600 pounds. The airplane is approved in the Normal category only.

Is there a known service bulletin on the Piper PA-39 Twin Comanche C/R?

Yes. Service Bulletin 1026 covers vacuum pump flexible couplings on the Piper PA-39 Twin Comanche C/R, serials 39-1 through 39-155. Piper considers compliance mandatory. Ask for proof it was done.

What is the Piper PA-39 Twin Comanche C/R Model Guide?

The Piper PA-39 Twin Comanche C/R Model Guide is a model guide for the Piper PA-39 Twin Comanche C/R, dated 2026.

What year was the Piper PA-39 Twin Comanche C/R Model Guide published?

The Piper PA-39 Twin Comanche C/R Model Guide — the Piper PA-39 Twin Comanche C/R model guide on file — is dated 2026.

How rare is it?
1,201Piper PA-39 Twin Comanche C/R registered worldwide · 1,193 active

Common. More common than 97% of the aircraft models we track.

Documentation completeness
5/7

Most owners only have the POH. Here's the essential set for the Piper PA-39 Twin Comanche C/R.

More Piper PA-39 Twin Comanche C/Rmanuals & documents

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In this document

Heritage and production

The PA-30 Twin Comanche was introduced in 1963, derived from the PA-24-400 Comanche with two 160 hp engines. The C was the last PA-30 variant, in 1969. The PA-39 C/R followed as the final production version. Production was 2000 PA-30s and only 155 PA-39s.

Engines and propellers

Type data for the PA-30/PA-39 series lists Lycoming IO-320-B1A engines and Hartzell HC-E2YL-2 series propellers. A replacement counter-rotating kit uses 70-inch two-bladed props. It is 2 pounds heavier per aircraft and replaces 72-inch props with a 2000 hour / 5 year TBO.

Documents to check

The original Piper Pilot's Operating Manual (761 453) was issued in June 1970. Revisions added a propeller synchrophaser and a fuel pump revision. The FAA-approved flight manual must stay in the airplane. The service manual (753 645) and parts catalog (753 646) cover the PA-39, so confirm the paperwork is current.

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

  • Piper considers Service Bulletin 1026 compliance mandatory. A failed vacuum pump coupling can cause loss of vacuum instruments. Due before next IFR flight, within ten hours or sixty days.
  • The operating manual is not a substitute for flight instruction, and it is not a transition guide from single-engine to multi-engine flying.
  • The owner is responsible for airworthiness. Keep the flight manual current, because the approved flight manual governs over other manual information.

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-39 Twin Comanche C/R Model Guide The Piper PA-39 Twin Comanche C/R is a twin-engine piston airplane built from 1970 to 1972, with 4 to 6 seats. It was the final production Twin Comanche, with counter-rotating propellers and handed engines. Only 155 were built (serials 39-1 through 39-155). Gross weight is 3600 pounds, in the Normal category. • Final Twin Comanche version: counter-rotating props and handed engines. Only 155 PA-39s were built, against 2000 PA-30s. • Gross weight is 3600 pounds. The airplane is certified in the Normal category only. • Service Bulletin 1026 (vacuum pump flexible coupling) lists serials 39-1 through 39-155. Confirm it was done. • A 70-inch Hartzell replacement propeller kit lists the PA-39 as applicable, with a 2400 hour / 6 year TBO. Heritage and production The PA-30 Twin Comanche was introduced in 1963, derived from the PA-24-400 Comanche with two 160 hp engines. The C was the last PA-30 variant, in 1969. The PA-39 C/R followed as the final production version. Production was 2000 PA-30s and only 155 PA-39s. Engines and propellers Type data for the PA-30/PA-39 series lists Lycoming IO-320-B1A engines and Hartzell HC-E2YL-2 series propellers. A replacement counter-rotating kit uses 70-inch two-bladed props. It is 2 pounds heavier per aircraft and replaces 72-inch props with a 2000 hour / 5 year TBO. Documents to check The original Piper Pilot's Operating Manual (761 453) was issued in June 1970. Revisions added a propeller synchrophaser and a fuel pump revision. The FAA-approved flight manual must stay in the airplane. The service manual (753 645) and parts catalog (753 646) cover the PA-39, so confirm the paperwork is current. Safety notes: • Piper considers Service Bulletin 1026 compliance mandatory. A failed vacuum pump coupling can cause loss of vacuum instruments. Due before next IFR flight, within ten hours or sixty days. • The operating manual is not a substitute for flight instruction, and it is not a transition guide from single-engine to multi-engine flying. • The owner is responsible for airworthiness. Keep the flight manual current, because the approved flight manual governs over other manual information.