N902FX
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
9 reports on file, 2005-10-10 – 2008-07-02.
Part: FAN — FAILED (NR 1 A/C PACK)
SMOKE IN ACFT FLT 8783 GTF TO GPI. DURING TAXI TO PARKING AFTER THE FLIGHT, ELECT SMOKE LIGHT ILLUMINATED AND THE CREW SMELLED SMOKE. SHUT DOWN AND TURNED OFF ALL POWER. CONTINUED TO TAXI TO PARKING AREA WITHOUT INCIDENT. REMOVED & REPLACED NR 1 GROUND COOLING FAN. (S)
Part: CONNECTOR — CONTAMINATED (TE FLAPS)
FLT 8788 -WHILE PERFORMING TAXI CHECKS AFTER A/C DEICING, CREW OBSERVED THAT THE FLAPS WOULD NOT EXTEND. THE CREW RETURNED TO RAMP. CLEANED CONNECTORS, DEICE FLUID CONTAMINATION. (M)
Part: INDICATOR — FLUCTUATES (NR 2 TORQUE)
FLT 7813 - ON TAKEOFF ROLL, THE NR 2 TORQUE GAUGE WAS FLUCTUATING BY GREATER THAN 10 PERCENT. TAKEOFF ABORTED. COULD NOT DUPLICATE DURING MAINTENANCE RUNS. (M)
Part: UNKNOWN — UNKNOWN (CABIN PRESSURE)
DURING CLIMB OUT AT CPR ON FLIGHT NR 8788 THE PILOT NOTICED THAT THE CABIN WAS NOT PRESSURIZING AT 1000 FT. THE CREW RECEIVED THE MASTER WARNING. THE CREW ELECTED TO RETURN TO DEPARTURE. NO EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. (K)
Part: WEB — CORRODED (FUSELAGE)
CARGO COMPARTMENT, PRESSURIZED ZONE BETWEEN LT MLG WHEEL WELL FRAME 25 TO 27 LOWER SIDE BOX WEB ASSEMBLY HAS SEVERAL AREAS OF LEVEL 2 SURFACE CORROSION. CORROSION SPOTS BLENDED IAW SRI DO/TS 2302/07-8813 AND ANA/E4162/2007/E-002. THIS IS PERMANENT REPAIR IAW SRAS DOTS-2302/07 4130 WITH SUPPLEMENTARY INSPECTIO TASK OF A DVI OF BLENDED AREAS EVERY 2 YEARS FOR NEW CORROSION DETECTION. (K)
Part: SKIN — CORRODED (ZONE 800)
SURFACE CORROSION (LEVEL 2) FOUND ON FUSELAGE SKIN COMMON TO NR 2 LOWER VHF ANTENNA. REMOVED CORROSION FROM DOUBLER COMMON TO VHF ANTENNA. FOUND DOUBLER TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW DOUBLER. (K)
Part: ANGLE — CORRODED (CARGO DOOR)
AFT LT CARGO DOOR LOWER CENTER ANGLE HAS LEVEL 2 CORROSION. REMOVED LOWER CENTER ANGLE. INSTALLED NEWLY FABRICATED LOWER CENTER ANGLE. (K)
Part: ANGLE — CORRODED (CARGO DOOR)
AFT LT CARGO DOOR LOWER AFT INER ANGLE HAS LEVEL 2 CORROSION. REMOVED LOWER AFT INNER ANGLE. INSTALLED NEWLY FABRICATED LOWER AFT INNER ANGLE. (K)
Part: SILL — LOOSE (FWD CARGO DOOR)
CARTGO DOOR WARNING LIGHT ILLUMINATED AFTER TAKEOFF. PILOT ELECTED TO RETURN TO DEPARTURE. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. PILOT INSPECTED CARGO DOOR AND FOUND THAT IT WAS CLOSED PROPERLY, HOWEVER THE DOOR SILL GUARD WAS PRESSING AGAINST THE CARGO DOOR, PREVENTING COMPLETE CLOSURE. THE PILOT STOWED THE SILL GUARD TO THE IB POSITION AND THE UNLOCK LIGHT EXTINGUISHED. THE CARGO STC HOLDER HAS A SB TO CORRECT THIS PROBLEM, AND THE PARTS ARE SCHEDULED TO BE AVAILABLE IN NOVEMBER. (K)