BOMBARDIER CRJ near Tallahassee, FL — 2009-02-28
- Date
- 2009-02-28
- Location
- Tallahassee, FL, USA
- Airport
- TLH
- Aircraft
- BOMBARDIER CRJ
- Registration
- N830AS
- Category
- Airplane
- Highest injury
- None
- Fatalities
- 0
- Phase of flight
- Ground
Probable cause
An electrical anomaly in the top portion of the JB-1 junction box resulting in ignition of adjacent combustible materials, including insulation blankets, and a flexible oxygen line.
NTSB narrative
A fire initiated in the top portion of the JB-1 junction box, which contains components associated with the distribution of electrical power from the APU or an external AC power supply. The fire ignited combustible materials, including insulation blankets and spread upwards toward a flexible oxygen line mounted above the JB-1 junction box. The flexible oxygen line ignited when exposed to the fire, and the fire burned through the aircraft's fuselage. Evidence suggests that the fire initiated as a result of an electrical anomaly in the top portion of the JB-1 junction box, near bus bar and contactor components. This evidence includes melting of one side of the bus bar along the periphery of its connection to a terminal stud and severe thermal damage to the internal and, to a lesser degree, external surfaces of the K1XB contactor case. Despite the damage to the contactor case, the internal contacts did not appear to be stuck or exhibit signs of melting or excessive pitting. There were no other signs of arcing near any of these components. Numerous maintenance difficulties had occurred on the aircraft involving the external AC power supply system beginning approximately 10-weeks before the accident. To attempt to remedy the anomalies, several relays, electrical contactors, the AC power switch, the external ground power receptacle, and other electrical components were removed and replaced with new components. Several of these components were located in the upper section of the JB-1 junction box. The last of these actions occurred about 5-weeks before the accident.
Analysis
- Primary failure mode
- Mechanical failure
- First missed decision gate
- Addressing electrical anomalies before applying external power.
NTSB coding
Evidence available
- CVR
- 24 docket documents
Docket documents24
- Cockpit Voice Recorder 12 - Specialist's Factual Reportcvr
- Maintenance Records 11 - Attachment 11 - Oxygen System Maintenance Informationform
- Maintenance Records 11 - Attachment 12 - Electrical System Maintenance Informationform
- Maintenance Records 11 - Attachment 2 - Engine and APU Component Informationform
- Maintenance Records 11 - Attachment 7 - Weight and Balance Informationform
- Captain Statementinterview
- Bombardier SB 601R-35-017Aother
- Bombardier SL-35-005other
- Comments from Accredited Representative's Technical Advisorother
- FAA SAIB NM-10-06other
- Maintenance Records 11 - Attachment 1 - Air Carrier Certificateother
- Maintenance Records 11 - Attachment 10 - Time Limit Control Component Listingother
- Maintenance Records 11 - Attachment 3 - Deferred and Carry Over Maintenance Logsother
- Maintenance Records 11 - Attachment 4 - Supplemental Type Certificate Listingother
- Maintenance Records 11 - Attachment 5 - Airworthiness Directive and Service Bulletin Listingother
- Maintenance Records 11 - Attachment 6 - Aircraft Flight Discrepancy Logsother
- Maintenance Records 11 - Attachment 9 - Major Repairs and Alterations Listingother
- TC AD CF-2011-23other
- TC SDA AL-2009-05other
- Fire Investigation Factual Report 09-102report
- Maintenance Records 11 - Attachment 8 - Service Difficulty Reports and Mechanical Interruption Summary Reportreport
- Maintenance Records 11 - Factual Report of Group Chairmanreport
- Materials Laboratory Factual Report 09-103report
- Systems 9 - Factual Report of Group Chairmanreport
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