PA-30 160 Twin Comanche C — Piper Aircraft PA-30 160 Twin Comanche C
Fleet & certification
- Built
- 11
- Origin
- US
Per-variant specifications
| Variant | Engine | MTOW | Range | Cruise | Pax |
|---|---|---|---|---|---|
PA30 PA30 | — | 1,600 kg | 1,130 nm | 168 kt | 5 |
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Piper Aircraft PA-30 160 Twin Comanche C manuals & documents
28 documents for the Piper Aircraft PA-30 160 Twin Comanche C — Supplemental Type Certificate · V Speeds Reference · Airworthiness Directives · Weight And Balance · Normal Procedures · Service Bulletins · Wiring Diagram · Performance Data · Pilot's Operating Handbook · Checklist · Systems Description · Parts Catalog · Service Bulletins · Other Documents. PDFs served from cdn.sprinkle.com.
The Twin Comanche PA-30 Owner's Handbook is designed to assist pilots in operating the Piper PA-30 Twin Comanche safely and effectively. It provides detailed information on the aircraft's specifications, performance, systems, and operational procedures. The handbook emphasizes the importance of competent flight instruction and knowledge of airworthiness directives and regulations. It serves as a comprehensive guide to the aircraft's performance characteristics, handling, and operational procedures, ensuring that pilots are well-acquainted with their aircraft. This document is essential for both new and experienced pilots flying the Twin Comanche, offering insights into its multi-engine operation and unique features.
- Take-off run (short field): 1250 ft
- Stalling speed (gear and flaps down): 69 mph
- Best rate of climb: 1460 ft/min
- Top speed: 205 mph
- Gross weight: 3600 lbs
- Fuel capacity: 90 U.S. gallons
- Engine type: Lycoming 10-320-B, 160 hp
- Electrical system: 12-volt DC, 50-amp generator
Supplemental Type Certificate
V Speeds Reference
Airworthiness Directives
Weight And Balance
Normal Procedures
Service Bulletins
Wiring Diagram
Pilot's Operating Handbook
Checklist
Systems Description
Parts Catalog
Other Documents
- AAIB Bulletin: G-ATMT EW/G2011/08/2520123 pages· 434 KB· via assets.publishing.service.gov.uk
- Collision with terrain – 43 km east of Perth Airport, Western Australia – 28 March 2010 – VH-KDS, Piper Aircraft Corp. PA-30-160B Twin Comanche201138 pages· 3.2 MB· via www.atsb.gov.au
- AAIB Bulletin: 11/200920093 pages· 409 KB· via assets.publishing.service.gov.uk
- Engine power loss, 15 km SE Gold Coast Airport, Qld, 4 February 2007, VH-DIC, Piper Aircraft Co. PA-30 Twin Comanche200830 pages· 3.0 MB· via www.atsb.gov.au
- AIRCRAFT ACCIDENT INVESTIGATION SUMMARY REPORT19754 pages· 393 KB· via www.atsb.gov.au
- SIMULATION MODEL FOR THE PIPER PA-30 LIGHT MANEUVERABLE AIRCRAFT IN THE FINAL APPROACH197130 pages· 1012 KB· via apps.dtic.mil
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 .
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