N917FR
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.
13 reports on file, 2005-05-22 – 2007-08-07.
Part: FAN — SEIZED (E/E) · airframe 16,434 hrs · 7,742 cycles
DURING FLIGHT FROM KPDX TO KDEN, FLIGHT CREW REPORTED LIVE TV SMOKE DETECTION ALARM SOUNDED. AIRCRAFT DIVERTED TO KSLC AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LIVE TV EQUIPMENT FAN TO BE THE SOURCE OF LIVE TV SMOKE DETECTION. DEACTIVATED LIVE TV SYSTEM PER MEL 44-20-01AA, C/N 1029316. RAN APU AND PACKS. NO SMOKE SMELL DETECTED. PERFORMED OVERWEIGHT LANDING INSPECTION IAW MP05510-4. NO DAMAGED OR DEFECTED NOTED. REPLACED THE LIVE TV EQUIPMENT COOLING FAN IAW LTV AMM 44-25-00. OPS CHECKED GOOD. REMOVED PLACARD. REPLACED THE LIVE TV EQUIPMENT COOLING FAN IAW LTV AMM 44-25-00. OPS CHECKED GOOD. REMOVED PLACARD.
Part: LEVER — BINDING (R1 DOOR) · airframe 14,199 hrs · 6,676 cycles
DURING C-3 CHECK, INSPECTION REPORTED THE R-1 DOOR ARMED LEVER WOULD NOT MOVE TO ARMED POSITION. REMOVED EXCESS LUBRICANT AND RETORQUED NUTS IAW AMM 52-11-22-820-001, STEP 4E(E). DOOR OPERATION NORMAL.
Part: LEVER — BINDING (R1 DOOR) · airframe 14,199 hrs · 6,676 cycles
DURING C-3 CHECK, INSPECTION REPORTED THE R-1 DOOR ARMED LEVER WOULD NOT MOVE TO ARMED POSITION. REMOVED EXCESS LUBRICANT AND RETORQUED NUTS IAW AMM 52-11-22-820-001, STEP 4E(E). DOOR OPERATION NORMAL.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,199 hrs · 6,676 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON LOWER SURFACE OF FLOOR PANEL 262FF. REPLACED FLOOR PANEL PER WORK CARD C534103-2.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,199 hrs · 6,676 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON LOWER SURFACE OF FLOOR PANEL 262FF. REPLACED FLOOR PANEL PER WORK CARD C534103-2.
Part: GIRT BAR — CORRODED (L2 DOOR) · corrosion level 2 · airframe 14,199 hrs · 6,676 cycles
DURING C-3 CHECK, INSPECTION REPORTED GIRT BAR PLATES ON FWD AND AFT L2 DOOR CORRODED. REPLACED FWD AND AFT L2 DOOR GIRT BAR PLATES PER AMM 52-13-31. RIGGED AND SEALED GIRT BAR LATCHES PER AMM 52-13-00-820-001.
Part: SHEAR PLATE — CORRODED (RIGHT) · corrosion level 2 · airframe 14,199 hrs · 6,676 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON AFT CORNER OF RT LATERAL SHEAR PLATE. DETERMINED SHEAR PLATE AND SUPPORT FRAME TO BE OUT OF LIMITS. REMOVED SHEAR PLATE SUPPORT FRAME ASSY PER SRM 53-41-14, FIG 2 AND 51-42-11. REPLACED SHEAR PLATE AND SUPPORT FRAME AFT GALLEY, RT SIDE, PER SRM 51-42-11.
Part: GIRT BAR — CORRODED (L2 DOOR SLIDE) · corrosion level 2 · airframe 14,199 hrs · 6,676 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION IN FWD GIRT BAR FITTING FASTENER HOLES ON L2 DOOR FRAME SILL. REMOVED CORROSION IAW SRM 53-41-14, FIG 101. FABRICATED REPAIR DOUBLER PER EA A9-54R-11722, STEP 5.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,199 hrs · 6,676 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND FASTENER HOLE AT FR68, RT SIDE, APPROX ONE FOOT INBD OF DOOR SKIN. BLENDED CORROSION AROUND HOLE AND FOUND INTERGRANULAR CORROSION INSIDE FASTENER HOLE THAT WAS FOUND TO BE OUT OF LIMITS IAW SRM 51-74-00. REPLACED FLOORBEAM IAW SRMS 51-42-11 AND 51-44-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,199 hrs · 6,676 cycles
DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM BETWEEN FR 66 AND FR 69, ABOUT 1 FT INBD OF THE MOLD LINE ON LT SIDE NEAR L2 DOOR - CORROSION AROUND SEVERAL HOLES AND AN AREA OF CORROSION THROUGH THE FLOORBEAM. REMOVED AND REPLACED FLOORBEAM PER SRM'S 51-42-11 AND 51-44-11, AND AIRBUS DRAWINGS D53472780 AND D53472816.
Earlier reports · 2005–2006 · 3 reports
2006
Part: COMPUTER — FAULTY (AUTOPILOT SYS) · airframe 12,099 hrs · 5,609 cycles
FLIGHT CREW REPORTED A/C DISPLAYED LATERAL WOBBLE (RIGHT) DURING CLIMB ANYTIME RUDDER TRIM >.3 UNITS LEFT, A/S >270. AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT. REPLACED NO. 1 FAC AND OPERATIONAL CHECK FLIGHT SHOWED NO VIBRATION. AIRCRAFT RETURNED TO SERVICE.
2005
Part: COVER — CRACKED (GEARBOX) · airframe 8,306 hrs · 3,778 cycles
DURING C-2 CHECK, INSPECTION REPORTED CRACK IN L2 DOOR GEARBOX COVER. REPAIRED L2 DOOR GEARBOX COVER PER EA A9-52R-10886. PAINTED L2 DOOR GEARBOX COVER PER AMM 25-00-00-540.
Part: COVER — CRACKED (GEARBOX) · airframe 8,306 hrs · 3,778 cycles
DURING C-2 CHECK, INSPECTION REPORTED CRACK IN R2 DOOR GEARBOX COVER. REPAIRED R2 DOOR GEARBOX COVER PER EA A9-52R-10886. PAINTED R2 DOOR GEARBOX COVER PER AMM 25-00-00-340.