AAIB Bulletin: 1/2014
Beechcraft G36 Bonanza · Other Documents
Overview
This document is an accident report from the AAIB regarding the Beech A36TP Bonanza, registration N7205T. It details an incident that occurred on August 30, 2013, during a private flight. The report outlines the circumstances leading to the accident, including the pilot's observations and actions during takeoff, as well as the aircraft's performance metrics. The report serves as a factual account of the events, providing insights into the aircraft's operational parameters and the pilot's experience. It is intended for aviation professionals, safety analysts, and enthusiasts interested in understanding the factors contributing to the accident.
- Aircraft Model: Beech A36TP Bonanza
- Maximum Take Off Weight (MTOW): 3,833 lbs
- Basic Weight: 2,630 lbs
- Fuel Capacity: Increased from 74 USG to 114 USG due to wingtip tanks
- Pilot's Total Flying Experience: 2,766 hours, with 1,635 hours on type
Document
Source
Originally published by assets.publishing.service.gov.uk. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Other Documents
- Year
- 2014
- Pages
- 2
- File size
- 158 KB
- Publisher
- assets.publishing.service.gov.uk
Common. Rarer than 24% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Beechcraft G36 Bonanza.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Aircraft Description
The Beech A36TP Bonanza is a turboprop conversion of the original piston-engined Beech A36 Bonanza. This conversion includes wingtip tanks that increase fuel capacity from 74 US gallons (USG) to 114 USG. The aircraft has a Maximum Take Off Weight (MTOW) of 3,833 lbs and a basic weight of 2,630 lbs.
Flight History
The flight took off from Tatenhill Airfield with the pilot and five passengers. Witnesses reported an unusually long takeoff roll, followed by the aircraft leveling off at about 100 ft before climbing. The pilot noticed a zero reading on the engine torque gauge shortly after takeoff, leading to a forced landing attempt.
Incident Summary
During the takeoff, the pilot observed birds on the runway and throttled back. After passing the birds, he increased power but later noticed a loss of engine power indicated by the torque gauge. Unable to return to the airfield, he executed a wheels-up forced landing in a field, resulting in significant damage to the aircraft but no injuries to the occupants.
Safety notes
- The engine torque gauge reading zero indicated a potential loss of engine power during climb, which is critical for flight safety.
Full document text
37 © Crown copyright 2014 AAIB Bulletin: 1/2014 N7205T EW/G2013/08/36 ACCIDENT Aircraft Type and Registration: Beech A36TP Bonanza, N7205T No & Type of Engines: 1 Rolls-Royce/Allison 250B-17F2 turboprop engine Year of Manufacture: 1984 (Serial no: E-2182) Date & Time (UTC): 30 August 2013 at 1630 hrs Location: Near Tatenhill Airfield, Staffordshire Type of Flight: Private Persons on Board: Crew - 1 Passengers - 4 Injuries: Crew - None Passengers - None Nature of Damage: Damaged beyond economic repair Commander’s Licence: Private Pilot’s Licence Commander’s Age: 53 years Commander’s Flying Experience: 2,766 hours (of which 1,635 were on type) Last 90 days - 23 hours Last 28 days - 9 hours Information Source: Aircraft Accident Report Form submitted by the pilot Synopsis The aircraft was taking off when the pilot reportedly saw birds on the runway ahead. Shortly after takeoff he saw that the engine torque gauge was reading zero. He performed a forced landing in a field with the landing gear retracted which resulted in major damage to the aircraft but without injury to the occupants. No physical evidence of bird impact was found either on the airframe or the engine. Description of the aircraft The A36TP model is a turboprop conversion of the original, piston-engined Beech A36 Bonanza aircraft. The US Supplemental Type Certificate (STC), which introduced the conversion, also added wingtip tanks to increase the fuel capacity from 74 USG to 114 USG. Performance figures supplied by the pilot showed that the aircraft had a Maximum Take Off Weight (MTOW) of 3833 lbs and a basic weight of 2630 lbs. He had allowed 544 lbs for 81 USG of fuel and 596 lbs for himself and his four passengers. With 10 lbs allowed for baggage, this gave a weight at takeoff of 3,780 lbs History of the flight The pilot and five passengers were taking off from Tatenhill Airfield for a destination in North Yorkshire. Witnesses on the ground said they saw the aircraft lift off after an unusually long takeoff roll. It then levelled off at about 100 ft and flew level for a short time before pitching 38 © Crown copyright 2014 AAIB Bulletin: 1/2014 N7205T EW/G2013/08/36 nose-up into a climbing attitude, following which they observed what appeared to them to be the right wing dropping before the aircraft descended out of sight. The pilot has stated that after performing the normal pre-takeoff checks, he started the takeoff roll and, shortly afterwards, he was aware of birds on the runway ahead. He throttled back as the birds passed either side of the aircraft and then increased power and rotated to a climbing attitude. He initially levelled out at about 100 ft whilst the landing gear was retracted. However, having resumed a climbing attitude again, at a height of 300-400 ft he noticed that the torque gauge was reading zero. The pilot attempted to turn the aircraft back towards the airfield but realised that he had insufficient height and airspeed to achieve this. Instead, he prepared for a wheels-up forced landing in what appeared to be the nearest and most appropriate field, although it contained a crop of tall maize. The subsequent impact was described as “heavy” but there was no fire and both he and his passengers were able to exit the aircraft normally and without injury. At the time of preparation of this Bulletin, the engine had not been subjected to a detailed examination, although the maintenance company reports that a visual examination of the airframe and the engine intake and compressor did not reveal any evidence of birdstrike or ingestion. The pilot’s opinion is that the engine lost power during the climb, that the sequence of events as reported by the eyewitnesses was consistent with his recollection and was as a result of the presence of birds.


