Piper PA-30 Twin Comanche — Other Documents
6 other documents references for the Piper PA-30 Twin Comanche.
This document is an AAIB (Air Accidents Investigation Branch) bulletin detailing the investigation of an accident involving the Piper PA-30 Twin Comanche, registration G-ATMT. The incident occurred on August 14, 2011, during a private flight from Alderney to Maypole Airfield. The report outlines the circumstances leading to the accident, including the pilot's experience, flight details, and the conditions at the time of landing. It highlights the factors contributing to the hard landing, such as low airspeed and the landing distance required as per the aircraft flight manual. The report serves as a critical resource for understanding the accident and improving safety protocols for similar aircraft operations.
- Aircraft: Piper PA-30 Twin Comanche, G-ATMT
- Takeoff weight: 3,484 lb; Landing weight: approximately 3,300 lb
- Recommended approach speed: 76 KIAS at landing weight
- Minimum landing distance required: 972 m; Available runway length: 700 m
- Pilot's total flying experience: 10,400 hours, with 2,000 hours on type
- 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