The Piper PA-17 (ICAO type PA17) is an aircraft of United States origin, certificated in the Normal and Utility category. It has a maximum take-off weight of 500 kg. It offers a maximum range of 220 nm, a cruise speed of 76 knots, a service ceiling of 12,500 ft and seating for up to 2 across its variants.
Piper PA-17

Fleet & certification
- Built
- 126
- Active
- 124
- Origin
- United States
Per-variant specifications
| Variant | Engine | MTOW | Range | Cruise | Pax |
|---|---|---|---|---|---|
| PA-17 PA-17 | — | 500 kg | 220 nm | 76 kt | 2 |
The FAA paperwork
TCDS A-805 · Rev 12 · issued 2006-08-07
- Category
- Normal and Utility
- MTOW
- 522 kg
- Seats
- 1 crew · 1 passengers
- Fuel
- 45 L
Continental A-65-8 or -8F, 65 hp, 2300 r.p.m.
Type Certificate No. 805 (CAR 3)
Where to look next
Piper PA-17 market & fleet intelligence
Registry, flight-tracking and market data on the Piper PA-17 fleet — updated daily.
78 yearsmedian age
Of the 93 registered Piper PA-17 with a known build year (74% of the 126 we track), the median age is 78 years.
7changed registration in 12 months
7 of the 126 registered Piper PA-17 we track changed registration in the last 12 months (6% of the fleet), across 7 registration events. Registration changes include ownership transfers, re-registrations and address updates — not all are sales.
Piper PA-17 manuals & documents
4 documents for the Piper PA-17 — Training Manual · Systems Description · Weight & Balance · Other Documents. PDFs served from cdn.sprinkle.com.
This document serves as a training manual specifically for the Piper PA-17 Vagabond Trainer. It is designed to provide pilots and aviation enthusiasts with essential information regarding the operation, maintenance, and safety procedures associated with this aircraft model. The manual includes detailed instructions on preflight checks, in-flight operations, and emergency procedures, ensuring that users are well-prepared to handle the aircraft safely and efficiently. It is an invaluable resource for both new and experienced pilots looking to enhance their knowledge and skills related to the Piper PA-17.
- Wingspan: 35 ft 6 in; Length: 22 ft 8 in; Max Takeoff Weight: 1,600 lbs.
- Engine: Lycoming O-235, 108 hp.
- Cruising Speed: 75 knots; Max Speed: 100 knots.
- Preflight inspection is mandatory before each flight.
- Maintain glide speed of 65 knots in case of engine failure.
Training Manual
Systems Description
Weight & Balance
Documents are sourced from publicly available references. Sprinkle does not host OEM-restricted materials; if you are a rights-holder and want a document removed, email .
What is the range of the Piper PA-17?
The Piper PA-17 has a maximum range of 220 nautical miles across variants.
How many people can the Piper PA-17 carry?
The Piper PA-17 seats up to 2 across its variants.
What is the MTOW of the Piper PA-17?
The Piper PA-17's maximum take-off weight is 500 kg.
What is the ICAO type designator for the Piper PA-17?
The Piper PA-17's ICAO type designator is PA17.
How many Piper PA-17 aircraft are registered worldwide?
Sprinkle tracks 126 registered Piper PA-17 airframes worldwide.
Registered PA-17 aircraft
Individual PA-17 airframes by tail number — registration history, operator and lineage.
- N4149H· 1966
- N4881H· 1949
- C-YZN· 1949
- N4865H· 1949
- N5056H· 1949
- N4886H· 1948
- N4601H· 1948
- N4639H· 1948
- N4681H· 1948
- N4612H· 1948
- N4879H· 1948
- N4824H· 1948
- N4882H· 1948
- N4619H· 1948
- N4610H· 1948
- N4845H· 1948
- C-NOD· 1948
- N4594H· 1948
- N4642H· 1948
- C-FGTZ· 1948
- N4623H· 1948
- N4660H· 1948
- N4854H· 1948
- N5004H· 1948