19940208004589I

Incident

FAA incident report · Boeing 707-323C · Dallas-Ft Worth, TX · February 8, 1994

Date
February 8, 1994 · 23:15 local
Place
Dallas-Ft Worth, TX
Airport
Dallas-Fort Worth International
Phase of flight
Forced/Precautionary Landing
Operating rules
Air carrier (Part 121)
Operator
BUFA
Aircraft
N8404
Reported as
Boeing 707323C
Reported engine
Pratt & Whitney JT3D3
People aboard
3
Fatal injuries
0

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.

Narrative: during climbout the number 2 and number 3 engines hydraulic low pressure lights came on and the utility system quantity went to zero. The crew performed the hydraulic fluid shutoff procedure per the abnormal procedures checklist. The number 4 engine fire warning then came on and the crew performed the emergency procedures to shut down the engine and discharged the fire extinguisher agent to the engine. After landing the aircraft was towed to the ramp due to loss of nose wheel steering and normal brake pressure, and the unknown status of the number 4 engine. Maintenance found the leading edge flap actuator flexible line (part number BACH8AO4EN0123) just outboard of number 4 engine ruptured, which caused hydraulic fluid to enter the tailpipe area of number 4 engine. This resulted in the fire warning light illuminating. Maintenance replaced the failed hydraulic line, reserviced the hydraulic system, replaced the fire extinguisher bottles, checked the number 4 engine for damage and found no damage or evidence of fire. Aircraft returned to service. This incident is closed.

As the FAA filed it

NARRATIVE: DURING CLIMBOUT THE NUMBER 2 AND NUMBER 3 ENGINES HYDRAULIC LOW PRESSURE LIGHTS CAME ON AND THE UTILITY SYSTEM QUANTITY WENT TO ZERO. THE CREW PERFORMED THE HYDRAULIC FLUID SHUTOFF PROCEDURE PER THE ABNORMAL PROCEDURES CHECKLIST. THE NUMBER 4 ENGINE FIRE WARNING THEN CAME ON AND THE CREW PERFORMED THE EMERGENCY PROCEDURES TO SHUT DOWN THE ENGINE AND DISCHARGED THE FIRE EXTINGUISHER AGENT TO THE ENGINE. AFTER LANDING THE AIRCRAFT WAS TOWED TO THE RAMP DUE TO LOSS OF NOSE WHEEL STEERING AND NORMAL BRAKE PRESSURE, AND THE UNKNOWN STATUS OF THE NUMBER 4 ENGINE. MAINTENANCE FOUND THE LEADING EDGE FLAP ACTUATOR FLEXIBLE LINE (PART NUMBER BACH8AO4EN0123) JUST OUTBOARD OF NUMBER 4 ENGINE RUPTURED, WHICH CAUSED HYDRAULIC FLUID TO ENTER THE TAILPIPE AREA OF NUMBER 4 ENGINE. THIS RESULTED IN THE FIRE WARNING LIGHT ILLUMINATING. MAINTENANCE REPLACED THE FAILED HYDRAULIC LINE, RESERVICED THE HYDRAULIC SYSTEM, REPLACED THE FIRE EXTINGUISHER BOTTLES, CHECKED THE NUMBER 4 ENGINE FOR DAMAGE AND FOUND NO DAMAGE OR EVIDENCE OF FIRE. AIRCRAFT RETURNED TO SERVICE. THIS INCIDENT IS CLOSED.

Other reports on N8404 · 3

Matched to the same aircraft by N-number and date.