N953FR
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.
18 reports on file, 2011-06-01 – 2017-11-02.
Part: SHEAR WEB — CORRODED (RIGHT) · corrosion level 2 · airframe 25,837 hrs · 11,361 cycles
RIGHT SHEAR WEB HAS CORROSION. REMOVED AND REPLACED THE SHEAR WEB IAW SRM 51-42-11, AND 51-44-11.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,837 hrs · 11,361 cycles
FLOORBEAM AT -Y254, FR68 HAS CORROSION. EVALUATED FLOORBEAM AT -Y254, FR68 AND FOUND DAMAGE TO BE OUT OF REPAIRABLE LIMITS IAW SRM 53-00-14-283-002. REMOVED AND REPLACED FLOORBEAM -Y254 FROM FR 68 IAW SRM 51-21-00 AND 51-72-11.
Part: FLOOR SUPPORT — CORRODED (FRAMES 68-70) · corrosion level 2 · airframe 25,837 hrs · 11,361 cycles
FLOOR SUPPORT AT Y512, FRAME 68 HAS CORROSION. REMOVED AND REPLACED THE FLOORBEAM FROM FRAMES 68 - 70 IAW SRM 51-72-11-911-001, AND 51-42-11.
Part: DOOR SILL — CORRODED (FRAME 66) · corrosion level 2 · airframe 25,837 hrs · 11,361 cycles
R2 DOOR SILL FWD GIRT BAR FITTING AT FRAME 66 CORRODED. REMOVED AND REPLACED THE R2 DOOR SILL IAW SRM 51-72-11, AND 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 25,837 hrs · 11,361 cycles
FLOOR SUPPORT, -Y1292, FRAME 68 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 68 - 70 IAW SRM 51-42-11, AND 51-44-11.
Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 25,837 hrs · 11,361 cycles
FLOORBEAM -Y465 AT FRAME 68 HAS CORROSION. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, 51-72-11, AND 51-44-11.
Part: FLOORBEAM — CORRODED (FRAME 67) · corrosion level 2 · airframe 25,837 hrs · 11,361 cycles
FLOORBEAM, +Y765, FRAME 67 CORRODED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND SRM 51-44-11.
Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 25,837 hrs · 11,361 cycles
FLOORBEAM -Y465, FRAME 66 CORRODED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND 51-72-11.
Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 25,837 hrs · 11,361 cycles
FLOORBEAM -Y1292 AT FRAME 66, HARD POINT HAS CORROSION. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11, AND 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FRAME 64-66) · corrosion level 2 · airframe 25,837 hrs · 11,361 cycles
FLOOR SUPPORT OTBD FASTENER HOLE AT SPLICE -Y765 AFT OF FRAME 66 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FRAME 66) · corrosion level 2 · airframe 25,837 hrs · 11,361 cycles
FLOOR SUPPORT, -Y765, FRAME 66 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 66 TO 70 IAW SRM 51-72-11, AND 51-44-11.
Earlier reports · 2011–2016 · 7 reports
2016
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,314 hrs · 8,576 cycles
DURING C CHECK, INSPECTION NOTED FLOORBEAM Y765 WAS CORRODED AT FRAME 68. R & R FLOORBEAM Y765 AT FRAME 68 IAW SRM 51-42-11.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 19,314 hrs · 8,576 cycles
DURING C CHECK, NOTED CORROSION ON STRINGER 43 LT AFT CARGO, BETWEEN FRAME 54 & 56. REPAIRED IAW EA A9-53R-33386 & SRM 51-74-00.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 19,314 hrs · 8,576 cycles
DURING C CHECK, INSPECTION NOTED AFT CARGO STRINGER HAS CORROSION, BETWEEN FRAME 54 & 57, AT STRINGER 42 LT. REPAIRED IAW EA A9-53R-33386 & SRM 51-74-00.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,314 hrs · 8,576 cycles
DURING C CHECK, INSPECTION NOTED FLOORBEAM Y765 WAS CORRODED AT FRAME 67. R & R FLOORBEAM Y765 AT FRAME 67 IAW SRM 51-42-11.
2011
Part: TUBE — CRACKED (ENGINE OIL SYS) · airframe 3,293 hrs · 1,417 cycles
NR 1 ENGINE OIL LOSS IN FLIGHT. UPON INSPECTION, FOUND OIL LEAKING FROM A SHEARED OIL TUBE. FOUND DEBRIS IN SCAVANGE FILTER - IN PROCESS OF CHANGING ENGINE.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 3,180 hrs · 1,354 cycles
R1DOOR LOWER EXIT MARKER INOPERATIVE. R & R R-1 DOOR LOWER MARKER EMERGENCY LIGHT. OPS CHECKED GOOD IAW E A9-33T-32189,
Part: ENTERTAIN SYS — SMOKE (CABIN) · airframe 1,914 hrs · 743 cycles
CREW REPORTED SMOKE ODOR IN CABIN ROWS 9-12. NO ACTUAL SMOKE SEEN, NO ECAM. ACFT WAS DIVERTED FOR TROUBLESHOOT IAW GMM 85.07, PG 2, FOUND DIRECT TV SYS TO BE EMITTING ODOR. PLACED TV SYSTEM ON MEL 44-20-01AA.