20020906026229I

Incident · Minor damage

FAA incident report · Aerosp ATR 72-212A · Orlando, FL · September 6, 2002

Date
September 6, 2002 · 06:30 local
Place
Orlando, FL
Airport
Orlando International
Phase of flight
Other Ground Ops
Operating rules
Air carrier (Part 121)
Operator
SIMA
Damage
Minor damage
Aircraft
N538AT
Reported as
Aerosp ATR72212A
People aboard
24
Fatal injuries
0
Pilot’s flight hours
8,226 total3,829 in this make and model232 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) Flight crew reported fire on no.2 engine at gate 10 ramp at Orlando airport. Precautionary measure passengers deplaned on ramp via entrance door stairs then walked to terminal. One injury reported. This inspector interviewed American eagle maintenance and they determined the pilot disengaged the propeller brake by electrical switch that signals the multi function computer to disengage the propeller brake. When the pilot increased engine power the propeller started to rotate and after several minutes the propeller brake was so hot the brake started a fire. Disassembly of the propeller brake indicated the brake was on and the propeller brake reduction gear was sheared off. American eagle maintenance believes the multifunction computer failed by failure to release propeller brake.

As the FAA filed it

(-23) FLIGHT CREW REPORTED FIRE ON NO.2 ENGINE AT GATE 10 RAMP AT ORLANDO AIRPORT. PRECAUTIONARY MEASURE PASSENGERS DEPLANED ON RAMP VIA ENTRANCE DOOR STAIRS THEN WALKED TO TERMINAL. ONE INJURY REPORTED. THIS INSPECTOR INTERVIEWED AMERICAN EAGLE MAINTENANCE AND THEY DETERMINED THE PILOT DISENGAGED THE PROPELLER BRAKE BY ELECTRICAL SWITCH THAT SIGNALS THE MULTI FUNCTION COMPUTER TO DISENGAGE THE PROPELLER BRAKE. WHEN THE PILOT INCREASED ENGINE POWER THE PROPELLER STARTED TO ROTATE AND AFTER SEVERAL MINUTES THE PROPELLER BRAKE WAS SO HOT THE BRAKE STARTED A FIRE. DISASSEMBLY OF THE PROPELLER BRAKE INDICATED THE BRAKE WAS ON AND THE PROPELLER BRAKE REDUCTION GEAR WAS SHEARED OFF. AMERICAN EAGLE MAINTENANCE BELIEVES THE MULTIFUNCTION COMPUTER FAILED BY FAILURE TO RELEASE PROPELLER BRAKE.