N744AL
Registered owner: ERLANDSEN ALLAN, WA (owner ≠ operator)
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.
5 reports on file, 2002-12-23 – 2005-08-14.
Part: SENSOR — FAILED (CABIN AIR)
FLIGHT 493 SNA-OGG. AFTER DEPARTURE FROM SNA CREW NOTED EQUIPMENT COOLING SUPPLY OFF LIGHT ILLUMINATED STEADY IN NORMAL POSITION FLICKERING IN ALTERNATE POSITION. CREW RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LOW AIRFLOW SENSOR, OPS AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. FLIGHT CREW CONDUCTED IN-FLIGHT VERIFICATION OF EQUIPMENT COOLING AND FOUND SYSTEM OPERATING NORMALLY.
Part: ECU — FAILED (APU)
FLT 441 - OAK-HNL - APU FAULT LIGHT ILLUMINATED ON FINAL APPROACH, AUTO SHUTDOWN. REPLACED APU ECU. SYSTEM OPS CHECK GOOD IAW MM 49-61-12-4. AIRCRAFT RETURNED TO SERVICE. (M)
Part: WARNING LIGHT — FALSE INDICATION (COCKPIT)
ON TAKEOFF ROLL, ABORTED TAKEOFF AT 70 KTS DUE TO ENGINE MASTER CAUTION LIGHT, DIDN'T NOTE SOURCE OF LIGHT. ONLY ABNORMAL INDICATION WAS 99 CELSIUS TAT. SMOKE OBSERVED FROM BRAKES, NORMAL TAXI TO GATE. PERFORMED HIGH ENERGY STOP/HEAT DAMAGE CONDITION INSPECTION IAW GMM 05-51-07-2. AIRCRAFT OK FOR SERVICE. PERFORMED ENGINE 1 AND 2 BITE TEST IAW 73-00-801. FOUND PITOT PROBE HEAT WAS OFF. PERFORMED ADIRS BITE 34-21 TAT PROBE SIGNAL FIM 34-21-00-810. FOUND NO FAULT. PHYSICALLY CHECK PITOT PROBLE FOR PROPER OPERATION. AIRCRAFT RETURNED TO SERVICE. (M)
Part: PRESSURE SWITCH — FAILED ('A' HYD SYS)
AFTER TAKEOFF THE 'A' SYSTEM HYDRAULIC PUMP LIGHT CAME ON. THE AIRCRAFT RETURNED TO HNL AND MADE AN OVERWEIGHT LANDING WITH NO FURTHER INCIDENT. MAINTENANCE VERIFIED THE LOW PRESSURE LIGHT. THE 'A' SYSTEM ELECTRIC PUMP PRESSURE SWITCH, NR 2 ELECTRIC MOTOR DRIVEN PUMP AND SYSTEM FILTERS WERE REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. AN OVERWEIGHT LANDING INSPECTION WAS COMPLETED AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: PUMP — FAILED (NR 1 & 2 ENG)
NR 2 EDP LOW PRESSURE LIGHT CAME ON 2.5 HOURS INTO FLT. SUSPECT PUMP FAILURE AS PRESSURE FOR SYS 'A' BEGAN DROPPING WHEN NR 2 ENGINE HYD PUMP MOMENTARILY TURNED OFF, DETERMINED NORMAL AFTER EVALUATION. NR 1 EDP LOW PRESSURE LIGHT ILLUMINATED ABOUT 3.5 HOURS INTO FLT. NR 2 DEP LOW PRESSURE LIGHT ILLUMINATED 4.5 HOURS INTO FLT. DIVERTED TO HNL FOR MAINT & LANDED WITH NO FURTHER INCIDENT. REPLACED NR 1 & NR 2 EDP. REPLACED CASE DRAIN FILTERS FOR NR 1, 2 EDP & NR 2 EMP. AS A PRECAUTION, 'A' & 'B' SYSTEM PRESSURE MODULE & RETURN MODULE FILTERS REPLACED. INCORPORATED EA 700-29-001R1 TO REMOVE 'A' & 'B' SYS DEPRESSURIZATION VALVES FROM HYD SYS. HYD SYS TESTED CHECKED GOOD. A/C RETURNED TO SERVICE. (M)