N204FR
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.
16 reports on file, 2010-03-04 – 2014-10-31.
Part: PANEL — DETERIORATED (LT ELEVATOR) · airframe 32,278 hrs · 12,670 cycles
LEFT ELEVATOR THERMOGRAPH INSPECTION. REVEALED INDICATIONS UPPER PANEL IRREGULAR SHAPE & BLACK IN COLOR. REPAIRED LT ELEVATOR IAW SRM 55-20-00 PB 201 STEP 2A & SRM 55-21-11 PB 201 PAR 4 FIG 204.
Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,278 hrs · 12,670 cycles
MAIN CABIN LT SHEAR PLATE HAS CORROSION AT FRAME 70. R & R SHEAR PLATE IAW SRM 51-42-11 PAR 6D & 6B.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,278 hrs · 12,670 cycles
L2 DOOR FLOOR THRESHOLD ATTACH POINT HAS CORROSION. CORROSION OUT OF LIMITS. R & R SHAPE SILL IAW SRM 51-42-11 PAR 6D & 6B.
Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,278 hrs · 12,670 cycles
MAIN CABIN RT LATERAL SHEAR PLATE HAS CORROSION AT FRAME 70. R & R SHEAR PLATE IAW SRM 51-42-11 PAR 6D & 6B.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,278 hrs · 12,670 cycles
AIRCRAFT DUE C7-S2 INSPECTION. MAIN CABIN FLOORBEAM AT FRAME 66 TO 67 OTBD OF Y-765 HAS CORROSION. BLENDED CORROSION ON FLOORBEAM, FOUND TO BE 100% MATERIAL LOSS, OUT OF LIMITS. R & R FLOORBEAM AT FRAME 66 OTBD OF Y-765 IAW SRM 51-42-11 PAR 5 A-D. ACFT DUE OUT OF C CHECK 11/1/2014.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,278 hrs · 12,670 cycles
AIRCRAFT DUE C7-S2 INSPECTION. MAIN CABIN FLOORBEAM TRACK AT FRAME 20 Y-765 HAS CORROSION. BLENDED CORROSION ON FLOORBEAM, FOUND TO BE 50% MATERIAL LOSS OUT OF LIMITS. R & R FLOORBEAM TRACK IN MAIN CABIN AT FRAME 20 Y-765 IAW SRM 51-42-11, PAR 5 A-C, PAR 7 B. ACFT DUE OUT OF C CHECK 11/1/2014.
Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,278 hrs · 12,670 cycles
AIRCRAFT DUE C7-S2 INSPECTION. MAIN CABIN FLOOR LATERAL PLATE IS CRACKED, OUT OF LIMITS. LOCATED 7 INCHES AFT OF FRAME 68, Y1292. R & R MAIN CABIN FLOOR LATERAL PLATE IAW SRM 51-42-11 PAR 5 A-C. ACFT DUE OUT OF C CHECK 11/1/2014.
Part: CONTAINER — DEFECTIVE (CABIN) · airframe 32,032 hrs · 12,555 cycles
O2 MASK DROPPED IN ROW 8 ABC. MASKS WERE REPACKED & PLACED ON MEL. WHEN MX TESTED THE O2 MASK RELEASE TO CLEAR MEL LP 703180, ROW 8 ABC FAILED TO RELEASE. R & R ROW 8 ABC EMER OXYGEN CONTAINER. OPERATIONS CHECKED NORMAL IAW AMM 35-21-41 PB 401.
Earlier reports · 2010–2013 · 8 reports
2013
Part: HYDROMECH UNIT — FAILED (NR 1 ENGINE) · airframe 29,241 hrs · 11,379 cycles
LEVEL AT FL 270 ON DESCENT, ENG NR 1 & GEN NR 1 DISCONNECTED, FOLLOWED BY ENG 1 ROLL BACK WITH ENG FAIL, ECAM ACTION. STARTED ECAM ACTION & ENG RESTARTED. NO INDICATION THAT THIS HAPPEN ON ECAM EXCEPT ENG 1 HP FUEL VLV PULLS UPON WHEN RECALL BUTTON PUSHED AFTER UNEVENTFUL LANDING. R & R NR1 ENG HMU. OPERATIONAL TEST MINIMUM IDLE LEAK CHECKED NORMAL IAW AMM 73-21-10-PB 401.
Part: COMPUTER — INOPERATIVE (ZONE 200) · airframe 28,579 hrs · 11,084 cycles
APPROACHING TOP OF CLIMB, VENT AVIONICS FAULT ECAM. FOLLOWED SHORTLY BY VENT BLOWER FAULT AND VENT EXTRACT FAULT. ACCOMPUSHED ALL ECAM ACTIONS. TROUBLESHOT VENT AVIONICS FAULT AND ASSOCIATED BLOWER AND EXTRACT INDICATIONS REF TSM 21-26-00-810-812, REPLACED AVIONIC EQUIPMENT VENT COMPUTER.
2012
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,242 hrs · 10,107 cycles
AFT EMERGENCY LIGHT BATTERY FAILED TEST, R & R EMERGENCY LIGHT BATTERY 13WL AFT LEFT. REFAMM 33-51-38-000-002A AND 33-51-38-400-002A.
2011
Part: STUD — FAILED (SLIDE PACK) · airframe 21,479 hrs · 8,363 cycles
FWD DOOR (1L) SLIDE PACK FELL OFF DOOR. INSTALLED NEW STUD ASSY'S IN L1 SLIDE PACK IAW AMM 25-62-44-400-007.
Part: PROXIMITY SWITCH — FALSE ACTIVATION (OVERWING EXIT) · airframe 20,918 hrs · 8,016 cycles
C-CHECK: LT OVERWING EXIT DOOR SLICE ARMED LIGHT, ON SIDEWALL PANEL, WILL NOT GO OUT WITH THE DOOR REMOVED. R & R FWD LT EMERGENCY EXIT PROX SWITCH, OPS CHECKS GOOD AMM 52-73-11-00-003 AND 52-73-11-400-003. R & R LT SLICE ARMED INDICATOR LIGHT, OPS CHECKED GOOD IAW AMM 52.73-21-400-003. ALSO FOUND FWD EMERGENCY EXIT DOOR SLICE SWITCH TARGET NOT ALIGNED PROPERLY. RE-ALIGNED REF 52-73-21-003-400-003.
2010
Part: PACKING — DAMAGED (BRAKE VALVE) · airframe 18,408 hrs · 7,097 cycles
PILOT REPORT, YELLOW SYS HYD FAILURE. FOUND DAMAGED PACKING AT THE PARKING BRAKE VALVE UNION. REPLACED PACKING, NO LEAKS NOTED.
Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 17,334 hrs · 6,700 cycles
DISCOVERED ON OVERNIGHT MX LOGPAGE 508598 ITEM NR 2. LT FWD EMERGENCY POWER SUPPLY UNIT (EPSU) BATTERY FAULTS DURING EMERGENCY LIGHT TEST. REPLACED FWD LT EMERGENCY POWER SUPPLY UNIT (EPSU) BATTERY. OPS CHECK GOOD IAW AMM 33-51-38-000-002 AND AMM 33-51-400-00.
Part: MANIFOLD — BROKEN (BRAKE SERVO) · airframe 16,770 hrs · 6,499 cycles
DURING CLIMB OUT THE FLIGHT CREW RECEIVED A WARNING OF AN OVERHEAT OF 600 DEGRESS CELCIUS OF BRAKES 3 AND 4. MX R & R NORMAL BRAKE SERVO VALVE MANIFOLD ON THE RT GEAR IAW AMM 32-42-16 PB 401.