N802FD
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.
25 reports on file, 2005-05-06 – 2009-08-14.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 38,893 hrs · 11,638 cycles
FWD CABIN FLOOR STRUCTURE - SUPPORT FLOOR AT Y730 BTW FR12A AND 13A FOUND CORRODED. SUPPORT FLOOR REPLACED IAW SRM 51-72-10.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,893 hrs · 11,638 cycles
AFT CARGO BAY- FLOORBEAM CORROSION AT FR60 AT POSITION Y1470. REPLACED IAW SRM 51-40-21.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,893 hrs · 11,638 cycles
AFT CARGO BAY- FLOORBEAM CORROSION AT FR60 AT POSITION Y-140. BEAM REPLACED IAW SRM 51-40-21.
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 38,893 hrs · 11,638 cycles
LT WING FLAP INBD WITH DEBONDING ON T/E. T/E WAS REPLACED IAW EA 6-5710-131046 AND SRM 51-72-10.
Part: STRUCTURE — CRACKED (ZONE 100) · airframe 38,893 hrs · 11,638 cycles
COCKPIT FLOOR STRUCTURE - UPPER PANEL AT RT TORSION BOX FOUND CRACKED BETWEEN FR1 AND FR2 AT Y1004. THE TORSION BOX WAS REPAIRED IAW EA 6-5310-131043.
Part: STRUCTURE — CRACKED (ZONE 100) · airframe 38,893 hrs · 11,638 cycles
COCKPIT FLOOR STRUCTURE - UPPER PANEL AT RT TORSION BOX FOUND CRACKED BETWEEN FR1 AND FR2 AT Y-1004. THE TORSION BOX WAS REPAIRED IAW EA 6-5310-131043.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 38,893 hrs · 11,638 cycles
RIGHT WING - SPOTS OF CORROSION AT UPPER SKIN SURFACE AT REAR SPAR LOCATION, BTW RIBS 4 AND 5. CORROSION WAS BLENDED OUT AND REMAINING THICKNESS FOUND ACCEPTABLE AS PER EA 6-5710-131042.
Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,893 hrs · 11,638 cycles
FWD CARGO COMPT - MANHOLE FITTING - CORROSION FOUND BTW FR38.1&FR38.2. CORROSION REMOVED IAW SRM 51-74-10. MANHOLE WAS REPAIRED IAW A310 SRM 53-14- 12 FIG.203.
Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,893 hrs · 11,638 cycles
AFT CARGO COMPT, CORROSION ON BEAM OF CARGO COMPT FLOOR AT FRAME 63 BTW Y805 AND Y1740. THE BEAM WAS REPLACED IAW SRM 51-72-10.
Part: TRUNNION — DAMAGED (MLG) · airframe 38,893 hrs · 11,638 cycles
LT WING - NR 1 EXTERIOR TRUNNION FOUND DAMAGED. THE AFFECTED TRUNNION WAS REPAIRED IAW CMM 57-53-12.
Part: TRUNNION — DAMAGED (MLG) · airframe 38,893 hrs · 11,638 cycles
LT WING - NR 3 EXTERIOR TRUNNION FOUND DAMAGED. TRUNNION NR 3LH WAS REPAIRED IAW CMM 57-53-12.
Part: BRAKE — BURNED (ZONE 700) · airframe 38,888 hrs · 11,637 cycles
NR 8 BRAKE TAXING INTO GATE WENT ABOVE 300 DEGS WITH ALL OTHER TEMPS BETWN 50-75 DEGS. ON ARRIVAL, WERE INFORMED BY GRD CREW THE BRAKES WERE VERY HOT, SMOKING AND LATER CAUGHT FIRE. ECAM SHOWED TEMP ABOVE 600 DEGREES. BRAKE FANS WERE ACTIVATED BEFORE GATE ARRIVAL. OTHER THAN BRAKE TEMP,THERE WAS NO OTHER INDICTION OF PROBLEM. IE STEERING, BRAKE GRAB ETC.
Earlier reports · 2005–2008 · 13 reports
2008
Part: WINDOW — CRACKED (COCKPIT) · airframe 36,971 hrs · 10,508 cycles
CAPT FRONT COCKPIT WINDOW CRACKED REMOVED AND REPLACED WINDOW HEAT PROTECTION NR 1 IAW MM 30-42-11-4. PERFORMED OPS CHECK AS PER MM 30-42-00-5. ALL TEST PASSED.
2007
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 36,768 hrs · 10,400 cycles
LT WING, FLAP INBD W/ DBONDS AT THE T/E BETWEEN RIB 2 AND RIB 8 REPLACE TRAILING EDGE IAW FEDEX EA 6-5710-115293.
Part: ARM — CORRODED (RUDDER HINGE) · corrosion level 2 · airframe 36,768 hrs · 10,400 cycles
NR 3 RUDDER HINGE ARM WITH CORROSION AT LUG BORES. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FEDEX EA 6-5510-115292.
Part: ARM — CORRODED (RUDDER HINGE) · corrosion level 2 · airframe 36,768 hrs · 10,400 cycles
NR 2 RUDDER HINGE ARM WITH CORROSION IN LUG BORE. REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5510-115292.
Part: ARM — CORRODED (RUDDER HINGE) · airframe 36,768 hrs · 10,400 cycles
NR 4 RUDDER HINGE ARM WITH CORROSION AT LUG BORES. REPAIR ACCOMPLISHED IN ACCORDANCE WITH 6-5510-115292.
Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 36,768 hrs · 10,400 cycles
RT WING INBD FLAP T/E W/ VARIOUS DEBONDS TRAILING EDGE WAS REPLACED IAW SRM 51-72-10 AND EA 6-5710-115293.
2006
Part: SKIN — DAMAGED (NR 2 INLET) · airframe 35,226 hrs · 9,307 cycles
ACCOMPLISH MAINTENANCE B-CHECK. NR 2 ENGINE CRK FOUND WITH ABOUT 4 INCHES ON AIR INLET INTERIOR SKIN SURFACE BETWEEN NR 5 AND NR 6 HOURS. REPAIRED PER CMM 71-11-05 FIG 603. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.
Part: SKIN — CRACKED (NACELLE) · airframe 35,226 hrs · 9,307 cycles
ACCOMPLISH MAINTENANCE B-CHECK. NR 2 ENG SMALL CRACKS FOUND ON AIR INLET EXTERIOR SKIN SURFACE AT ZONE BETWEEN NR 5 AND NR 6 HOURS (LIP INLET). REPAIRED PER CMM 71-11-05 FIG 603. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.
Part: CONVERTER — NO TEST (E/E BAY) · airframe 35,136 hrs · 9,236 cycles
REMOVED AND REPLACED SDAC IAW AMM 31-55-22-4. OPERATIONAL TEST FOUND SATISFACTORY. A/C OK TO CONTINUE. PREMATURE REMOVAL/INSTALLATION.
2005
Part: SPOILER — DAMAGED (LT WING) · airframe 34,348 hrs · 8,690 cycles
DURING C2 CHECK, FOUND AN EXISTING REPAIR ON LEFT WING NR 1 SPOILER TRAILING EDGE. REPAIRED PER SRM 57-70-00.
Part: FLAP — DAMAGED (RT WING) · airframe 34,348 hrs · 8,690 cycles
DURING C2 CHECK, FOUND AN EXISTING REPAIR ON RIGHT INBOARD FLAP LOWER TRAILING EDGE. NEW REPAIR WAS PERFORMED IAW FEDEX EA 6-5710-84120.
Part: SKIN — DAMAGED (T/E FLAP) · airframe 34,348 hrs · 8,690 cycles
DURING C2 CHECK, 2 EXISTING FLUSH COMPOSITE REPAIRS WHERE FOUND ON LEFT INBOARD FLAP TRAILING EDGE. REPAIRED IAW EA 6-5750-84119.
Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 34,348 hrs · 8,690 cycles
DURING C2 CHECK, AN EXISTING REPAIR WAS FOUND ON LEFT ELEVATOR TOP SURFACE OUTBOARD OF RIB 17. NEW REPAIR ACCOMPLISHED PER SRM 55-20-00.