# NTSB FTW01LA047: Nord 1101, N208BF, McKinney, TX, January 9, 2001 - Type: NTSB accident investigation - Classification: Accident · Serious injuries · Limited investigation · Final report - Date: January 9, 2001, 17:00 local (23:00 UTC) - Place: McKinney, TX - Coordinates: 33.214168, -96.747779 - Nearby events: https://openairdocs.org/map.md?lat=33.2142&lon=-96.7478&mi=10 - Phase of flight: [Initial climb](https://openairdocs.org/ntsb-phases/350) (OpenAirDocs' grouping) - Highest injury: Serious injuries - Injuries: 1 serious, 1 uninjured - Status: Completed, report July 30, 2001 - Report: Approved by Office Director - Parties: FAA FSDO - NTSB case key (mKey): 50917 - NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=FTW01LA047 - NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/50917/pdf - Page: https://openairdocs.org/ntsb/FTW01LA047 ## Probable cause the loss of engine power during takeoff resulting from the inadequate engagement of the throttle torque tube rod end into the support bushing by unknown maintenance personnel. ## Sequence of events In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf). - Loss of engine power(partial) - mech failure/malf, takeoff - initial climb - maintenance - improper, unknown (cause) - throttle/power lever,push/pull rod - disconnected (cause) - Forced landing, takeoff - initial climb - In flight collision with terrain/water, landing - flare/touchdown - terrain condition - ground ## Analysis The pilot reported that during the takeoff/initial climb the engine "smoothly throttled back to a low power setting although throttle lever was at full position." During the ensuing forced landing in a soft field, the airplane's fuselage sustained damage. Examination of the engine revealed that the throttle linkage assembly's push/pull rod separated from the support bushing. The FAA inspector, who examined the airplane, stated that the rod end was "inadequately" engaged in the support bushing "due to improper installation." ## Factual narrative On January 9, 2001, at 1700 central standard time, a Nord 1101, single-engine experimental airplane, N208BF, sustained substantial damage during a forced landing following a loss of engine power during the takeoff/initial climb from the Aero Country Airport, near McKinney, Texas. The airplane was owned and operated by the pilot under 14 Code of Federal Regulations Part 91. The airline transport pilot received serious injuries and his pilot-rated passenger was not injured. Visual meteorological conditions prevailed for the local flight, and a flight plan was not filed. The personal flight was originating at the time of the accident. The pilot reported that the airplane was at 250 feet agl when the engine "smoothly throttled back to a low power setting although throttle lever was at full position." The pilot performed the emergency procedures; however, the engine power was not restored. The airplane would not maintain altitude, and the pilot landed the airplane in a soft field southeast of the airport. The FAA inspector, who responded to the site, found the right aileron separated at its outboard hinge. The fuselage structure was wrinkled and buckled. Examination of the engine revealed that the aft throttle linkage assembly's push/pull rod separated from the support bushing. The FAA inspector stated that the rod end was "inadequately" engaged in the support bushing "due to improper installation." The pilot/owner reported that the airplane had accumulated 2.4 flight hours since the last annual inspection. ## Aircraft - Registration: [N208BF](https://openairdocs.org/deregistered/N208BF-2013-05-14), registration cancelled 2013-05-14, S/N 154 (OpenAirDocs) - Reported make and model: Nord 1101 - Registry model: [Nord 1101](https://openairdocs.org/model/nord-1101) (registry code 6380108) (OpenAirDocs) - Registry engine: [Renault 6Q10B](https://openairdocs.org/engine/renault-6q10b) (registry code 52501, reciprocating) (OpenAirDocs) - Category: Airplane - Serial number: 154 - Airframe hours: 3472.4 - Engines: Renault 6Q10A 230 horsepower reciprocating - Damage: Substantial damage - Flight: Personal, Part 91 - Registered owner: Richard M. Barrett - Airworthiness certificate: Special, Experimental (Special) - Last inspection: Annual, August 14, 2000, 2.4 hours before - Departed: T31, McKinney, TX - Airport: T31, Aero Country, runway 17, 3,000 × 75 ft, asphalt ## Flight crew As NTSB recorded them. NTSB leaves out names. - Pilot; age 67; injuries: serious; airline transport, flight engineer, flight instructor; airplane ratings: multi-engine land, single-engine land, single-engine sea; instrument ratings: airplane; medical: class 1, valid medical--w/ waivers/lim; last flight review November 30, 2000; seat: left; flight hours: 33,600 total, 12 in this make and model, 30,000 as pilot in command, 1 in the last 90 days ## Weather - Conditions: Visual (VMC), Day - Wind: 90° at 10 knots - Visibility: 10 statute miles - Lowest ceiling: none - Temperature: 61 °F, dew point 39 °F - Altimeter: 30.00 inHg ## FAA reports on this event (1) The FAA's own accident and incident reports, matched to the aircraft by N-number and date (OpenAirDocs). - [Accident 20010109000509A](https://openairdocs.org/incident/20010109000509A), Jan 9, 2001: Nord 1101, Port Isabel, TX, No damage. (-23) On January 9, 2001, at 1700 CST, a Nord mod. 1101, (experimental), reg. Number N208BF, owned and operated by richard m. barrett of mckinney, TX.,… From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.