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Piper Aircraft PA-42-720R
PA42
Photo via Wikipedia: Piper PA-42 Cheyenne
Year
—
Owner
—
Last seen
—
MTOW
5,100 kg
Range
1,670 nm
Seats
11
PA-42-720R
Piper Aircraft · PA-42-720R
Model overview
Fleet & certification
- Built
- 1
- Active
- 1
- Origin
- United States
Certifying authorities
FAA
Variants
Per-variant specifications
| Variant | Engine | MTOW | Range | Cruise | Pax |
|---|---|---|---|---|---|
PAY3 | — | 5,100 kg | 1,670 nm | 250 kt | 11 |
Same family
Other models in this family
Type certification
The FAA paperwork
TCDS A32SO · Rev 3 · issued 2014-10-13
- Category
- Restricted Category Only
- MTOW
- 6,100 kg
- MZFW
- 4,463 kg
- Seats
- 1 crew · 5 passengers
- Fuel
- 2,279 L
- Ceiling
- 35,000 ft
Approved fuelJP-4JP-5commercial keroseneJet AA-1B fuels conforming to P&W Specification 522 or Service Bulletin 13044MIL-G-5572 Grades 80/87, 91/98, 100/130 and 115/145 (limited time)
Engine
2 United Aircraft of Canada, Ltd., or Pratt & Whitney, PT6A-61 (turboprop)
Certification basis
FAR Part 23, effective February 1, 1965, as amended by Amendment 23-16, effective February 14, 1975, with specified deletions and additions; FAR Part 25, effective February 1, 1965…
Safety & ops history
Where to look next
Detailed safety & ops history coming soon — view this model's FAA Airworthiness Directives at FAA.gov.
This aircraft
Tools
Explore Sprinkle
Piper Aircraft PA-42-720R manuals & documents
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-42-720R specifically; these are the Piper Aircraft PA-42 family documents.
Overview
CHEYENNE IIIA · 1987
No PA-42-720R-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.
- Maximum takeoff weight: 11,200 lbs
- Cruise speed at 25,000 ft: 310 KTAS
- Rate of climb at sea level: 2,380 fpm
- Maximum operating altitude: 35,840 ft
- Fuel capacity: 3,820 lbs (3,753 lbs usable)
Pilot's Operating Handbook
Systems Description
Service Bulletins
Weight And Balance
Supplemental Type Certificate
Performance Data
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 .
PA-42-720R — frequently asked
What is the range of the Piper Aircraft PA-42-720R?
The Piper Aircraft PA-42-720R has a maximum range of 1,670 nautical miles across variants.
How many people can the Piper Aircraft PA-42-720R carry?
The Piper Aircraft PA-42-720R seats up to 11 across its variants.
What is the MTOW of the Piper Aircraft PA-42-720R?
The Piper Aircraft PA-42-720R's maximum take-off weight is 5,100 kg.
What is the ICAO type designator for the Piper Aircraft PA-42-720R?
The Piper Aircraft PA-42-720R's ICAO type designator is PA42.
How many Piper Aircraft PA-42-720R aircraft are registered worldwide?
Sprinkle tracks 1 registered Piper Aircraft PA-42-720R airframes worldwide.
Registered PA-42-720R aircraft
Individual PA-42-720R airframes by tail number — registration history, operator and lineage.