N803JL
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.
6 reports on file, 2004-02-13 – 2011-08-29.
Part: PUMP — LOW PRESSURE (APU) · airframe 11,866 hrs · 7,476 cycles
THE CREW HAS BEEN REPORTING DURING APU START THAT IT WOULD HANG AT ABOUT 45% FOR ABOUT 5-6 SECONDS AND THEN LET OUT A LOUD "POP" AND THEN CONTINUE ONTO START AND RUN NORMALLY, NOTE: DURING THE START SEQUENCE IT WAS NOTED A FOG OF FUEL WAS BEING EXPELLED FROM THE APU EXHAUST. TROUBLSHOOTING INCLUDED THE REPLACEMENT OF THE FUEL START NOZZLE AND THE IGNITOR WITH NO CHANGE TO THE START. A FUEL PRESSURE CHECK AT THE START NOZZLE INDICATED A VERY LOW READING (100 PSI) THE ENGINE DRIVEN FUEL PUMP WAS FOUND TO BE DEFECTIVE P/N 4950037 S/N UNK. NOTE: HAMILTON SUNSTRAND T-62T-40C8D1 INSTALLED
Part: PRESSURE SWITCH — DEFECTIVE (HYDRAULIC SYS) · airframe 11,710 hrs · 7,376 cycles
THE FLIGHT CREW REPORTED THE "HYD 1 LO PRESS" ILLUMINATED AFTER THE FINAL FLAP SETTING AND REMAINED ON. TROUBLESHOOTING FOUND THE NR 1 HYD PRESSURE SWITCH P/N 15185-4SN1 TO BE DEFECTIVE. A NEW SWITCH WAS INSTALLED, FUNCTIONAL CHECKS SATISFACTORY.
Part: PUMP — FAILED (FUEL SYSTEM) · airframe 11,181 hrs · 7,045 cycles
(TM2R) CREW REPORTED THE "ENG NR1 FUEL" ANNUNCIATOR ILLUMINATED DURING FLIGHT.
Part: BULB — IMPROPER PART (CABIN LIGHTING)
A SELA FLORESCENT BULB WAS FOUND IN THE CABIN LIGHTING SYSTEM. THIS SYSTEM IS AN ALC SYSTEM. THE SELA BULB HAD IMPROPER CONNECTORS ON IT AS WELL. WE CHANGED OUT THE SELA BULB WITH AN ALC BULB AND USED THE PROPER CONNECTORS WHEN INSTALLING IAW AD 95-22-01 AND IB 90-001. (K)
Part: CARBON SEAL — DAMAGED (RT ENGINE)
ON DESCENT TO KBCT, ENGINE POWER WAS REDUCED TO IDLE. OIL PRESSURE ON NR 2 ENGINE DROPPED TO RED LINE. POWER INCREASED ON NR 2 ENGINE AND OIL PRESSURE INCREASED. FOUND NR 1 CARBON SEAL RUNNER RETAINER DAMAGED. REPLACED RETAINER AND CARBON SEAL WITH NEW. INSTALLED NEW OIL PUMP. PERFORMED GROUND RUN, OIL PRESSURE ADJUSTMENT, VIBE SURVEY, AND OIL SYSTEM FLUSH.
Part: OIL CAP — MISINSTALLED (LT ENGINE) · airframe 7,063 hrs · 4,660 cycles
DURING CRUISE FLIGHT, NOTICED FLUCTUATION IN OIL PRESSURE INDICATION ON LT ENGINE. INITIATED PRECAUTIONARY SHUTDOWN AND PROCEEDED WITHOUT INCIDENT. MAINTENANCE OPENED LOWER COWL AND FOUND IB OIL TANK SERVICE CAP DISLODGED AND LAYING IN LOWER COWLING. INSTALLED CAP AND LOCKWIRED, SERVICED OIL LEVEL AND WASHED ENGINE. PERFORMED ENGINE GROUND RUN, NO DISCREPANCIES FOUND.