N807FR
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.
15 reports on file, 2006-08-15 – 2009-12-28.
Part: COVER — OUT OF POSITION (EMERGENCY EXIT) · airframe 18,769 hrs · 9,833 cycles
DURING CLIMB OUT, THE FLIGHT CREW RECEIVED SPURIOUS ECAM INDICATIONS RT DOOR EMERGENCY EXIT. MX REINSTALLED RT OVERWING EXIT HANDLE COVER FLAP AND ECAM INDICATION CHECKED NORMAL IAW AMM 25-23-47-420-127.
Part: CABLE — LACK OF LUBE (ESCAPE SLIDE) · airframe 15,717 hrs · 8,173 cycles
DURING C3 C-CHECK, INSPECTION NOTED THAT THE RIGHT OVERWING EMERGENCY SLIDE CABLE FAILED THE FUNCTIONAL TEST OF THE SLIDE RELEASE SIGNAL AND OPERATIONAL TEST OF THE UNLOCKING AND OPENING FROM THE OUTER SIDE IN THE ARMED MODE. MAINTENANCE INSPECTED AND LUBED CABLE PER ENGINEERING AUTHORIZATION A0-52T-30102, ALL CHECKS SATISFACTORY.
Part: SILL — CORRODED (ZONE 200) · airframe 15,717 hrs · 8,173 cycles
DURING C3 C-CHECK, INSPECTION NOTED CORROSION AT THE FASTENER HOLE OF THE AFT GIRT BAR FITTING, L2 DOOR THRESHOLD. MAINTENANCE REMOVED THE CORROSION. FABRICATED REPAIR DOUBLER AND FILLER AND COMPLETED THE REPAIR PER ENGINEERING AUTHORIZATION A8-53R-30930.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 15,717 hrs · 8,173 cycles
REFERENCE NON-ROUTINE C057562. DURING C3 C-CHECK, INSPECTION NOTED CORROSION ON FLOORBEAM -Y1292 BETWEEN FRAME 66 AND FRAME 68. MAINTENANCE REMOVED AND REPLACED FLOORBEAM -Y1292 BETWEEN FRAME 66 AND FRAME 68 IN REFERENCE TO SRM 51-42-11 PARAGRAPHS 5 AND 7.
Earlier reports · 2006–2008 · 11 reports
2008
Part: ISOLATION VALVE — CRACKED (THRUST REVERSER) · airframe 15,124 hrs · 7,864 cycles
ENROUTE AT FL330, PILOT REPORTED INDICATION OF HYDRAULIC RESERVOIR LOW LEVEL FOLLOWED BY ENGINE NR 2 PUMP LOW LEVEL AND NOTED THE YELLOW SYSTEM FLUID QUANTITY DEPLETED. MAINTENANCE INSPECTED THE NR 2 ENGINE AND FOUND THE THRUST REVERSER ISOLATION VALVE HYDRAULIC LINE CRACKED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE THRUST REVERSER ISOLATION VALVE HYDRAULIC LINE AND PERFORMED OPERATIONAL AND LEAK CHECKS IAW AMM 78-37-51-400-001 AND 78-21-00-710-042.
Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 13,788 hrs · 7,114 cycles
LINE MAINTENANCE NOTED THE AFT CARGO PIT TRANSITION PANEL 151FH HAD PUNCTURE DAMAGE IN THREE PLACES ON THE UPPER SKIN. MAINTENANCE REPAIRED DAMAGE IN ACCORDANCE WITH A318 SRM 53-02-00, FIGURE 205.
Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 13,788 hrs · 7,114 cycles
LINE MAINTENANCE NOTED THE AFT CARGO PIT TRANSITION PANEL 151FG HAS PUNCTURE DAMAGE IN THREE PLACES ON UPPER SKIN. MAINTENANCE REPAIRED DAMAGE IN ACCORDANCE WITH A318 SRM 53-02-00, FIGURE 205.
Part: COOLING FAN — BINDING (CABIN) · airframe 12,358 hrs · 6,398 cycles
DURING CRUISE, AT 35000, FLT CREW REPORTED LOUD NOISE AND VIBRATION FOLLOWED BY ACRID ODOR AND SMOKE IN COCKPIT. ECAM DISPLAYED BLOWER AND EXTRACTOR FAN FAULT. FLIGHT CREW DECLARED AN EMERGENCY, DIVERTED TO OKC AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED AVIONICS COOLING BLOWER, PERFORMED AVEC BITE TEST IN ACCORDANCE WITH AMM 21-26-51 PB 401. RII ALSO PERFORMED. TEST RESULTS WERE NORMAL. AIRCRAFT RETURNED TO SERVICE.
2007
Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 10,332 hrs · 5,346 cycles
FLIGHT CREW REPORTED GREEN HYD QTY LOW IN CRUISE. PERFORMED LANDING GRAVITY EXTENSION PER FOM VOL II. REPLACED NR 1 ENGINE T/R ISOLATION VALVE PRESSURE HYDRAULIC LINE. PERFORMED OPS AND LEAK CHECK IAW 8-37-51-PB-401. CHECKED GOOD. RESET FREE FALL EXTENSION HANDLE AND STOWED GEAR DOORS IAW AMM 32-33-00-720-001.
Part: PANEL — PUNCTURED (FUSELAGE) · airframe 10,097 hrs · 5,217 cycles
DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANELS 151FH, 151HH, AND 162SF DAMAGED. REPAIRED PUNCTURES IN PANELS IAW A318 SRM 53-20-00, PB 201, PARA 8C, FIG 204.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 10,097 hrs · 5,217 cycles
DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR PANEL 161QF DAMAGED. REPAIRED FLOOR PANEL 161QF IAW A318 SRM 53-02-00, FIG 204.
Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 10,097 hrs · 5,217 cycles
DURING C-2 CHECK, INSPECTION REPORTED PUNCTURE ON TOPSIDE OF AFT CARGO COMPARTMENT FLOOR PANEL 161QF. REPAIRED AFT CARGO COMPARTMENT FLOOR PANEL 161QF IAW SRM 53-02-00, FIG 204.
Part: PANEL — DAMAGED (FUSELAGE) · airframe 10,097 hrs · 5,217 cycles
DURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT TRANSITION PANEL 131BF DAMAGED. REPAIRED PUNCTURE IAW A318 SRM 53-20-00, PB 201, PARA 8.C., FIG. 204.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 8,576 hrs · 4,431 cycles
AIR TURN BACK, CAPTAIN'S FWD WINDSHIELD SHATTERED. REPLACED CAPTAINS FWD WINDSHIELD IAW 56-11-11, PB401.
2006
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 6,658 hrs · 3,420 cycles
ON APPROACH ECAM FLAPS LOCKED. FLAPS WOULD NOT EXTEND BEYOND F2, SLATS EXTEND NORMALLY. MAINTENANCE PERFORMED TROUBLESHOOTING PER TSM 27-51-00-810-818, OPERATIONAL TEST OK. FLAP ALIGNMENT OK. NO ALIGNMENT OR FLAP FAULT NOTED DURING TEST. PER TSM 27-51-00-810-818 CREW MONITORED FLAP OPERATION DURING THE NEXT FLIGHT. NO FURTHER DISCREPANCY NOTED.