PA-36-285 — Piper Aircraft PA-36-285

Fleet & certification
- Built
- 50
- Active
- 46
- Origin
- US
Per-variant specifications
| Variant | Engine | MTOW | Range | Cruise | Pax |
|---|---|---|---|---|---|
PA36 PA36 | — | 2,100 kg | 410 nm | 104 kt | 2 |
Other models in this family
The FAA paperwork
TCDS A9SO · 10 · issued 2006-08-07
The FAA-issued Type Certificate for this model is on file (TCDS A9SO), but we haven't yet extracted the structured spec values.
Read the TCDS (PDF) →Where to look next
Other airframes worth a look
Free — save the PA-36-285 to your watchlist and track it in one place.
Registered PA-36-285 aircraft
Individual PA-36-285 airframes by tail number — registration history, operator and lineage.
- VH-MYJ1976
- N577841976
- N578141976
- N577721976
- N577751976
- N764001976
- N577491976
- N577461976
- N578241976
- N577511976
- N410RM1975
- N9901P1975
- N575851975
- N575891975
- N9911P1975
- N577381975
- N577211975
- N653101975
- N576251975
- N577251975
- N576151975
- N576091975
- C-FPMD1975
- N9904P1975
How many Piper Aircraft PA-36-285 are there?
50 Piper Aircraft PA-36-285 are on the worldwide civil registry, of which about 46 are active. This counts registered airframes, not total production.
What is the range of the Piper Aircraft PA-36-285?
The Piper Aircraft PA-36-285 has a range of about 410 nautical miles.
How fast is the Piper Aircraft PA-36-285?
The Piper Aircraft PA-36-285 cruises at around 104 knots.
What is the Piper Aircraft PA-36-285's maximum take-off weight?
The Piper Aircraft PA-36-285 has a maximum take-off weight of 2,100 kg.
How many seats does the Piper Aircraft PA-36-285 have?
The Piper Aircraft PA-36-285 is typically configured for up to 2 occupants.
What is the ICAO type designator for the Piper Aircraft PA-36-285?
The Piper Aircraft PA-36-285 uses ICAO type designator PA36.
Is the Piper Aircraft PA-36-285 type certified?
Yes. The Piper Aircraft PA-36-285 holds a type certificate; you can read its Type Certificate Data Sheet (TCDS) and what each section means on Sprinkle.





