N907FR
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.
17 reports on file, 2003-11-14 – 2007-06-23.
Part: ATTACH ANGLE — DAMAGED (FUSELAGE) · airframe 18,398 hrs · 7,827 cycles
DURING C4/S1 CHECK, INSPECTION REPORTED ANGLE AT FR67 JUST BELOW L2 DOOR SILL WHICH ATTACHES DOOR SILL TO FRAME WAS FOUND DAMAGED.
Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 18,398 hrs · 7,827 cycles
DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBOARD 231EF DELAMINATED AROUND ONE OF THE FWD SCREW HOLES. REPAIRED DAMAGE TO TOP SKIN OF FLOORBOARD 231EF IAW EA NR A9-53R-11965.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 18,398 hrs · 7,827 cycles
DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 221PF DELAMINATED NEAR THE LAV MOUNTS AND A PUNCTURE NEAR THE LAV DOOR AREA. REPAIRED DAMAGE TO THE TOP SKIN PANEL OF FLOOR PANEL 221PF IAW A319 SRM 53-02-00, PARA 8A, FIG 201 AND 202. DELAMINATION WAS DETERMINED TO BE A DENSITY CHANGE IN THE PANEL DUE TO THE INSERTS INTEGRATED INTO THE SANDWICH STRUCTURE.
Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 18,398 hrs · 7,827 cycles
DURING C4/S1 CHECK, INSPECTION REPORTED PUNCTURE IN LT CORNER AREA OF FLOORBOARD 231MF. REPAIRED SMALL PUNCTURE TO THE TOP SKIN, FWD LT CORNER SURFACE OF FLOORBOARD PANEL 231MF IAW A319 SRM 53-02-00, PARA 8A, FIG 201 AND 202.
Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,398 hrs · 7,827 cycles
DURING C4/S1 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR FRAME 61 COVER SHEET FOR NUT PLATES CORRODED AROUND SEVERAL RIVET HEADS. REMOVED AND REPLACED WEB IAW A319 SRM 51-42-11 AND 51-44-21.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,398 hrs · 7,827 cycles
DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON UNDERSIDE OF FLOOR PANEL 262FF. REPLACED FLOOR PANEL 262FF AND R2 DOOR THRESHOLD IAW SRM 53-42-12, PB 401.
Part: NUT PLATE — CORRODED (GIRT BAR) · corrosion level 2 · airframe 18,398 hrs · 7,827 cycles
DURING C4/S1 CHECK, INSPECTION REPORTED R1 GIRT BAR FITTING NUT PLATE ASSY CORRODED, FWD AND AFT. REPLACED FWD AND AFT GIRT BAR FITTINGS AND NUT PLATE ASSEMBLIES IAW SRM 51-42-11, PAGE 44, STEP 7D AND PARA 7.
Part: GIRT BAR — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,398 hrs · 7,827 cycles
DURING C4/S1 CHECK, INSPECTION REPORTED LIGHT CORROSION ON L2 DOOR GIRT BAR FITTING AFT OF C66, JUST FWD AND INBD OF SCREW HOLE. FOUND L2 DOOR SILL TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 101. REPLACED L2 DOOR SILL IAW SRM'S 51-42-11, 51-44-11, 51-41-11 AND EA NR A0-51T-11976.
Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,398 hrs · 7,827 cycles
DURING C4/S1 CHECK, INSPECTION REPORTED HEAVY CORROSION ON TOP FLANGE OF DUMMY RAIL AT Y81, BETWEEN FR12 AND FR14. REPLACED DUMMY RAIL IAW SRM 51-42-11, PARA. 8, AND SRM 51-41-11, PARA 3.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,398 hrs · 7,827 cycles
DURING C4/S1 CHECK, INSPECTION REPORTED TWO AREAS OF CORROSION ON FLOORBEAM +Y1292 AT FR68. REPLACED FLOORBEAM IAW SRM 51-42-11, SRM 51-44-11 AND EA #A0-53T-11472.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,398 hrs · 7,827 cycles
DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 261FF CORRODED AT FWD INBD CORNER ON UNDERSIDE OF PANEL. REPLACED FLOOR PANEL IAW AMM 53-32-12-400-002.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,398 hrs · 7,827 cycles
DURING C4/S1 CHECK, INSPECTION REPORTED ONE AREA OF CORROSION ON FLOORBEAM +Y1292 AT FR67. REPLACED FLOORBEAM IAW SRM 51-42-11, SRM 51-44-11, AND EA #A0-53T-11472.
Earlier reports · 2003–2006 · 5 reports
2006
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,337 hrs · 5,667 cycles
DURING C3-CHECK, INSPECTION REPORTED GALLEY BEAM BETWEEN FR 66 AND FR 68, LBL Y1292, CORRODED. FOUND GALLEY BEAM TO BE OUT OF LIMITS. REPLACED FLOORBEAM PER SRM 51-42-11, 51-44-11 AND EA A9-53R-11257.
Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,337 hrs · 5,667 cycles
DURING C3-CHECK, INSPECTION REPORTED RT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 IN AFT GALLEY CORRODED. REPLACED RT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 IAW SRM 51-42-11.
Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,337 hrs · 5,667 cycles
DURING C3-CHECK, INSPECTION REPORTED LT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 IN AFT GALLEY CORRODED. REPLACED LT LATERAL SHEAR PLATE BETWEEN FR 68 AND FR 70 IN AFT GALLEY PER SRM 51-42-12.
2004
Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 8,215 hrs · 3,577 cycles
BLOCK TURNBACK. FLIGHT CREW REPORTED MAIN CABIN DOOR WOULD NOT ARM. REMOVED, ADJUSTED AND REINSTALLED L1 DOOR SLIDE. OPS CHECK GOOD PER MM 25-62-44-000-062.
2003
Part: CONTROL UNIT — INOPERATIVE · airframe 5,002 hrs · 2,217 cycles
EN ROUTE TO DEN, ECAM STATUS SHOWED FOLLOWING MESSAGE: INOP SYS: ANTI SKID, N/W STRG/ BRK SYS 1, BRK SYS 2. N/W STEERING SWITCH WAS ON. FLIGHT CREW DECLARED AN EMERGENCY AND AIRCRAFT LANDED IN DEN WITHOUT INCIDENT. AIRCRAFT HAD NO N/W SHEERING AND NO SYS 1 OR SYS 2 BRAKING. BRAKING ACCOMPLISHED PER ABNORMAL PROCEDURES. AFTER TROUBLESHOOTING, REPLACED BSCU AND OPS CHECKED GOOD PER AMM 32-42-34. REPLACED BRAKE SELECTOR VALVE AND PERFORMED HYD LEAKAGE TEST PER AMM 32-42-11-000-001. PERFORMED OPERATIONAL TEST OF BSCU PER AMM 32-46-00-001 AND CHECKED GOOD.