N745AL
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
4 reports on file, 2003-11-22 – 2004-09-07.
Part: ANTENNA — FAILED (ELT) · airframe 14,594 hrs · 7,906 cycles
LAS-HNL: DURING CLIMB-OUT, A LOUD NOISE WAS HEARD FROM THE CEILING NEAR ROW 17. RETURNED TO LAS FOR OVER-WEIGHT LANDING AT 147K LBS, SMOOTH TOUCHDOWN. FOUND ELT ANTENNA DELAMINATED/DAMAGED. REMOVED DAMAGED ANTENNA AND INSTALLED BLANKING PLATE IAW AQ ECO 7-0223. DEFERRED ELT SYSTEM IAW MEL 23-12, PLACARDS INSTALLED. PERFORMED OVER-WEIGHT LANDING INSPECTION IAW AQ M-121-PART 1, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.INSTALLED ELT ANTENNA IAW AQ ECO 7-0223-PART II; OPS CHECK OK. PLACARDS REMOVED, AIRCRAFT RETURNED TO SERVICE.
Part: WINDOW — CRACKED (COCKPIT) · airframe 13,581 hrs · 7,633 cycles
CAPTAINâS NR 2 OUTER WINDOW PANE CRACKED. RETURNED TO HNL. OVERWEIGHT LANDING AT 141,000 LBS. DESCENT RATE LESS THAN 100 FEET PER MINUTE AT 140 KTS. REPLACED NR 2 CAPTAIN SIDE WINDOW IAW AMM 56-12-11-4. OPS CHECK OK. PERFORMED OVERWEIGHT LANDING INSPECTION PHASE I IAW AMM 5-51-35-2. NO DEFECTS NOTED. VERIFIED WINDOW HEAT SYSTEM OPERATIONAL IAW AMM 30-41-00-710-80, OPS CHECK NORMAL. AS PRECAUTION; REPLACED WINDOW HEAT CONTROLLER IAW AMM 30-41-11, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.
Part: ACCESS DOOR — CRACKED (EXTERNAL POWER) · airframe 12,606 hrs · 7,330 cycles
FOUND EXTERNAL POWER ACCESS DOOR DAMAGED. TRIMMED OUT CRACK OR DAMAGED AREA TO 1/2 INTERNAL RADIUS. HFEC VERIFIED TRIMMED OUT AREA. ALODINED AND PRIMED. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IN ACCORDANCE WITH ECO 7-0170. AIRCRAFT RETURNED TO SERVICE.
Part: HMU — MALFUNCTIONED (NR 1 ENGINE)
40NM EAST OF FIXED POINT FANTO, NR 1 ENGINE FAILED. ATTEMPTED IN FIGHT ENGINE RESTART SUCCESSFULLY, BUT ENGINE REMAINED AT IDLE AND OIL TEMPERATURE ROSE RAPIDLY WHEN THRUST LEVER WAS ADVANCED. REMOVED AND REPLACED HYDRO-MECHANICAL METERING UNIT AND ENGINE DRIVEN FUEL PUMP. LEAK AND OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)