
| Variant | Engine | MTOW | Range | Cruise | Pax |
|---|---|---|---|---|---|
PAY3 | — | 5,100 kg | 1,670 nm | 250 kt | 11 |
TCDS A23SO · Rev 19 · issued 2009-06-26
2 United Aircraft of Canada, Ltd., or Pratt & Whitney PT6A-61 (turboprop)
FAR Part 23, effective February 1, 1965, as amended by Amendment 23-16, effective February 14, 1975, and subsequent amendments as listed
Registry, flight-tracking and market data on the Piper Aircraft PA-42-720 fleet — updated daily.
42 yearsmedian age
Of the 24 registered Piper Aircraft PA-42-720 with a known build year (89% of the 27 we track), the median age is 42 years.
18 documents for the Piper Aircraft PA-42 family — Pilot's Operating Handbook · Checklist · Systems Description · Parts Catalog · Service Bulletins · Specifications · Other Documents · Training Manual · Weight And Balance · Supplemental Type Certificate · Performance Data · Airworthiness Directives. PDFs served from cdn.sprinkle.com.
No documents are catalogued for the PA-42-720 specifically; these are the Piper Aircraft PA-42 family documents.
No PA-42-720-specific manual on file — this overview is from the Piper Aircraft PA-42 family documentation.
This document serves as the Pilot's Operating Handbook for the Piper PA-42 Cheyenne IIIA, detailing its specifications, operational procedures, and safety features. It is intended for pilots and aviation enthusiasts who require comprehensive information about the aircraft's performance, systems, and handling characteristics. The handbook provides critical data on engine specifications, weight limits, fuel capacities, and performance metrics, ensuring that operators can safely and effectively manage the aircraft in various flight conditions. Additionally, it covers emergency procedures and training recommendations to enhance pilot proficiency and safety.
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 .
The Piper Aircraft PA-42-720 has a maximum range of 1,670 nautical miles across variants.
The Piper Aircraft PA-42-720 seats up to 11 across its variants.
The Piper Aircraft PA-42-720's maximum take-off weight is 5,100 kg.
The Piper Aircraft PA-42-720's ICAO type designator is PA42.
Sprinkle tracks 27 registered Piper Aircraft PA-42-720 airframes worldwide.
Individual PA-42-720 airframes by tail number — registration history, operator and lineage.