N903FE
Registered owner: FEDERAL EXPRESS CORPORATION, TN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Corporate Air (HSYA) | Certificate holder | — | Matched by certificate designator |
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.
12 reports on file, 2000-05-19 – 2014-03-06.
Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 3 · airframe 11,039 hrs · 12,409 cycles
CORROSION FOUND ON INBD FLAP TRACK WEB RS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.
Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 3 · airframe 11,039 hrs · 12,409 cycles
CORROSION FOUND ON OTBD FLAP TRACK WEB RS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.
Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 3 · airframe 11,039 hrs · 12,409 cycles
CORROSION FOUND ON CTR FLAP TRACK WEB, LS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.
Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 3 · airframe 11,039 hrs · 12,409 cycles
CORROSION FOUND ON OTBD FLAP TRACK WEB, LS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.
Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 3 · airframe 11,039 hrs · 12,409 cycles
CORROSION FOUND ONCENTER FLAP TRACK WEB, R.S. FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANNULAR CORROSION.
Part: THROTTLE — MALFUNCTIONED (ENGINE) · airframe 10,814 hrs · 15,401 cycles
PILOT REPORTED HE RAN OUT OF THROTTLE AT 5800 FEET -TORQUE LIMITED WITH NORMAL ITT.
Part: THROTTLE — OUT OF RIG (ENGINE) · airframe 10,814 hrs · 15,401 cycles
PILOT REPORTED HE RAN OUT OF THROTTLE AT 5800 FEET WITH NORMAL ITT. ENGINE WAS RE-RIGGED AND OPS CHECK FLIGHT WAS SATISFACTORY.
Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 10,246 hrs · 14,253 cycles
DURING SCHEDULED PHASE INSPECTION, MX FOUND EXFOLIATION CORROSION ON CENTER SEAT TRACK BETWEEN FUSELAGE BS 329.5 AND 332. CORROSION MEASURES 2.5" IN LENGTH AND .5" IN WIDTH - WITH A MAXIMUM DEPTH PENETRATION MEASUREMENT OF 4/32". OPEN
Part: MASTER CYLINDER — DETERIORATED (BRAKES) · airframe 9,962 hrs · 13,662 cycles
PILOT TAXIED, AT HOLD SHORT LINE TO RUNWAY, THE LEFT BRAKE FAILED. PILOT APPLIED FULL RT BRAKE AND WAS ABLE TO REGAIN FULL LT BRAKE EFFECTIVENESS BY PUMPING THE BRAKE. ACFT RETURNED TO BLOCKS FOR TROUBLESHOOTING. MX TROUBLESHOT SYS TO LT BRAKE MASTER CYLINDER. LT BRAKE MASTER CYLINDER R & R IAW MM 32-40-00.
Part: UNKNOWN — SMOKE (COCKPIT) · airframe 9,014 hrs · 12,024 cycles
STRONG SMELL OF BURNING OR BURNT INSULATION AND A SLIGHT HAZE OF SMOKE IN COCKPIT. BOTH THE LEFT AND RIGHT INSTRUMENT PANELS AND WIRING WERE INSPECTED FOR OBVIOUS DAMAGE. PERFORMED GROUND RUNS WITH ALL COCKPIT INSTRUMENTS ON AND COULD NOT DUPLICATE THE PROBLEM. THE AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER INCIDENT.
Part: O-RING — FAILED (FUEL SYSTEM) · airframe 2,228 hrs
(MRR NR 01-020405) DURING DEPARTURE, PILOT NOTICED AN ENGINE POWER LOSS AND FLUCTUATION AND ABORTED THE TAKEOFF. AFTER REDUCING POWER, THE PILOT EXPERIENCED A STRONG FUEL SMELL IN THE COCKPIT. MAINTENANCE FOUND THAT THE NR 10 FUEL NOZZLE TRANSFER TUBE WAS LOOSE AND LEAKING FUEL. REPLACED ALL O-RINGS, FUEL NOZZLE GASKET AND RESCUED TRANSFER TUBE AND FUEL NOZZLE. (NM05200503118) (K)
Part: HOSE — LEAKING
HNL - FLT 8666 - ON CLIMB-OUT, PILOT REPORTED ''FUEL FUMES IN COCKPIT''. AIR TURNBACK TO HNL. FUEL ACCUMULATION IN ENGINE COWL DUE TO LOOSE FUEL LINE CONNECTION AT FIREWALL FUEL FILTER. TIGHTENED THE NOSE FITTING, FLUSHED COWLING WITH SOAP AND WATER. PERFORMED GROUND RUN-UP LEAK CHECK. AIRCRAFT RETURNED TO SERVICE. (X)