N743AL
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, 2002-08-16 – 2004-07-01.
Part: ECU — FAILED (CARGO BAY) · airframe 8,030 hrs · 2,399 cycles
AFTER T/O, APU FAULT LIGHT CAUSED APU AUTO SHUTDOWN. LANDING GW 142.3 K, SINK RATE AT TOUCHDOWN LESS THAN 300 FPM. DIVERTED TO HNL, UNEVENTFUL LANDING. PERFORMED APU BITE CHECK, ECU INTERNAL FAULT SHOWN. REPLACED APU ELECTRONIC CONTROL UNIT PER AMM 49-61-12-00-801. STARTED APU AND PERFORMED APU BITE TEST, OPS CHECK GOOD. PERFORMED OVERWEIGHT LANDING INSPECTION IAW AMM 05-51-35-2, PAGES 1-13. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.
Part: SWITCH — FAILED (NR 1 ENGINE)
CLIMBING THROUGH ABOUT 7000 FEET THE LT ENGINE BLEED TRIP LIGHT ILLUMINATED. QRH ACCOMPLISHED. A RESET WAS ATTEMPTED THREE TIMES. RETURNED TO HNL. OVERWEIGHT LANDING AT 147,500 LBS. TOUCHDOWN RATE OF DESCENT LESS THAN 300 FPM. REMOVED AND REPLACED 390 DEGREES FAHRENHEIT PRE-COOLER VALVE SENSOR P/N 975-0172-006, IAW 36-12-03-4. OPS CHECK GOOD. VERIFIED NO BLEED TRIP OFF LIGHT ILLUMINATED. REPLACED 490 DEGREES FAHRENHEIT OVERTEMP SWITCH. RAN ENGINES OPS CHECK GOOD. ACCOMPLISHED OVERWEIGHT LANDING CONDITIONAL INSPECTION IAW 05-51-35-2. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)
Part: CIRCUIT BREAKER — MALFUNCTIONED (GALLEY)
EN ROUTE TO HNL, THE CREW COULD NOT GET THE GALLEY POWER TO COME ON. THE AIRCRAFT RETURNED TO OAK AND MADE AN OVERWEIGHT LANDING WITH NO FURTHER INCIDENT. MAINTENANCE RESET THE GALLEY POWER CIRCUIT BREAKERS ON THE P-92 PANEL LOCATED IN THE E/E COMPARTMENT. GROUND OPERATIONAL CHECK FOR THE FORWARD AND AFT GALLEYS WERE GOOD. AN OVERWEIGHT LANDING INSPECTION WAS COMPLETED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)
Part: LIGHT — INOPERATIVE (PAX CABIN)
REPLACED FORWARD ENTRY DOOR EXIT LIGHT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (COCKPIT)
RT LANDING GEAR GREEN LIGHT FAILED TO ILLUMINATE AFTER GEAR WAS SELECTED DOWN DURING APPROACH. SECONDARY GEAR INDICATOR IN OVERHEAD PANEL SHOWED NORMAL GREEN LIGHTS. CIRCUIT BREAKERS WERE CHECKED. AIRCRAFT MADE A PASS BY TOWER TO CONFIRM GEAR DOWN. A NORMAL LANDING WAS MADE WITH NO FURTHER PROBLEMS. TROUBLESHOT LANDING SYSTEM IAW FIM. LIGHT BULB FOR RIGHT MAIN GEAR INDICATOR WAS FOUND BURNT OUT. LIGHT BULB ON CENTER INSTRUMENT PANEL WAS REPLACED AND BOTH PRIMARY AND SECONDARY GEAR INDICATORS CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE.