N453FE

Service difficulty reports · 49

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N453FE' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201512194038Fairing · damagedLEFT WING INBD FLAP FAIRING HANGING DOWN ON ARRIVAL. RELEASED FOR SERVICE IAW CDL 27-01, B CATEGORY. FLAP TRACK FAIRING MISSING, REFER TO CDL 27-01-B FOR RESTRICTIONS. REMOVED LT WING FARING NR 2 WITH ASSOCIATED HARDWARE & SENT TO STRUCTURES FOR POSSIBLE REDec 19, 2015 · N453FE · Airbus A310222 · Trailing Edge FlapsSDR FDEA201512023853Adapter · looseDEPARTED WITH 62,000 POUNDS OF FUEL, AT LANDING FUEL QTY INDICATES 61,400 POUNDS OF FUEL. REMOVED AND REPLACED LEFT OUTER ADAPTER PLUGS 42QT1 & 43QT1 PER AMM 28-42-37-04.Dec 2, 2015 · N453FE · Airbus A310222 · Fuel Indicating SystemSDR FDEA201511043464Computer · failedSHORTLY AFTER CLEANUP ON TAKEOFF, MULTIPLE & VARIOUS AURAL & ECAM ALERTS & WARNINGS BEGAN. DECLARED AN EMER & RETURNED, WARNINGS CONTINUED ALL THE WAY TO BLOCK IN. REPLACED NR 1 AND NR 2 FLIGHT WARNING COMPUTERS 1WW1 & 1WW2 IAW AMM 31-53-34-04. PERFORMED FWNov 4, 2015 · N453FE · Airbus A310222 · Central WarningSDR FDEA201507092174Seat Track · damagedRAMP REPORTS AFT LOCK IN POSITION 8R LOOSE IN FLOOR, LATCH N1288. LATCH RESTRAINT DEVICE N1288 AT 8R INOPERATIVE, BROKEN OR MISSING. INSTALLED NEW SEAT TRACK SECTION IN IAW SRM 53-10-16. INSTALLED FLOORING & LOADING SYS IAW SRM 51-40-20.Jul 9, 2015 · N453FE · Airbus A310222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201507092173Seat Track · damagedFOUND AT POS 8R, LOCK S1288 TO HAVE SEAT TRACK LOBE DAMAGE CAUSING LOCK TO BE LOOSE. LOBE DAMAGE AT LOCK S1288 POS 8R, LOCK INSTALLED BUT LOOSE IN FLOOR. ACFT OK FOR SERVICE. RESTRAINT HAS BEEN REMOVED IAW SR 30-53-003 & MEL HAS BEEN APPLIED. REF WRI 25-5Jul 9, 2015 · N453FE · Airbus A310222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201505221623Switch · faultyLOWERED GEAR, GOT SAFE INDICATION OF GEAR DOWN. A FEW SECONDS LATER GOT UNSAFE GEAR WARNING. LIGHT & HORN IN POS 2 SELECTED SYS 1 & THE LIGHT QAND WARNING HORN WENT OUT.. 3 GREEN DOWN INDICATIONS INSYS 1. SYS 2 HAD 2 GREEN LIGHTS FOR MAIN WHEELS AND NO GMay 22, 2015 · N453FE · Airbus A310222 · Landing Gear Position and WarningSDR FDEA201502120515Engine · vibrationON TAKEOFF, ACFT STARTED VIBRATING VERY BADLY. FELT MORE LIKE AN AIRFRAME FLUTTER RATHER THAN ENG VIBRATION. CHECKED ENG PAGE, ALL NORMAL. CLIMBING THROUGH 2500' PULLED THROTTLES BACK & FLUTTER DECREASED. AS SPEED STARTED TO INCREASE FLUTTER INCREASED. SLFeb 12, 2015 · N453FE · Airbus A310222 · Engine (Turbine/Turboprop)SDR FDEA201407131756Damper · leakingON DEPARTURE LG WOULD NOT RETRACT. TRIED BOTH SYS 1 & SYS 2 & QRH, NO HELP. RT GEAR PITCH DAMPER POPPED WITH THE REAR SEAL BLOWN ALL THE WAY OUT. R & R RT MAIN GEAR PITCH DAMPER IAW AMM 32-11-15-04-01. FOUND RT MLG BOGIE SENSOR SUPPORT BROKEN CAUSING GEAR Jul 13, 2014 · N453FE · Airbus A310222 · Landing Gear Retraction/Extension SystemSDR FDEA201406021269Skin · crackedPOSSIBLE CRACK ON LT WING INBD SLAT CUT OUT, BOTH CORNERS. PERFORMED HFEC OF AREA IAW NTM 51-10-08 BLOCK 601, TWO CRACK INDICATIONS. REPAIRED AREAS, INSTALLED FILLERS AND DOUBLER IAW EA 6-5730-T0308606.Jun 2, 2014 · N453FE · Airbus A310222 · Wing, Plate/SkinSDR FDEA201310062421Lug · damagedLEFT MLG WW RIB 5 FITTING FWD LUG DAMAGED. REPAIRED IAW EA 6-5750-T0302477 P1, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Oct 6, 2013 · N453FE · Airbus A310222 · Wing, Attach FittingsSDR FDEA201310042404Lug · corrodedCORROSION WAS FOUND ON THE LUG BORE AND AFT SPOTFACE OF RT RIB5 FWD LUG. ACCOMPLISHED CORROSION REPAIR IAW GMM 6-2-100 REPAIR CLASSIFIEID AS MINOR.Oct 4, 2013 · N453FE · Airbus A310222 · Wing Miscellaneous StructureSDR FDEA201310042403Lug · corrodedCORROSION WAS FOUND ON LUG BORE AND FWD SPOTFACE OF LT RIB 5. ACCOMPLISHED THE CORROSION REPAIR IAW GMM 6-2-100, IAW EA 6-5750-T0302477 P1. REPAIR CLASSIFED AS MINOR.Oct 4, 2013 · N453FE · Airbus A310222 · Wing Miscellaneous StructureSDR FDEA201309302338Beam · crackedTHREE CRACKS WERE FOUND AT LT INNER LONGITUDINAL BEAM FLANGE STR 11 BETWEEN FRAMES 73A AND 74A. CUT OUT DAMAGE PORTION OF BEAM AND REWORK MILLED STEP. INSTALL THE REPAIR ANGLE AND FILLER IAW SRM 53-18-18, FIG 205A.Sep 30, 2013 · N453FE · Airbus A310222 · Fuselage Miscellaneous StructureSDR FDEA201309232283Floor Panel · damagedFLOOR PANEL 132RF IN LOWER FWD CARGO BAY WAS FOUND SOFT. FABRICATED A NEW PANEL WITH INSERTS AND ADHESIVE IAW SRM 53-10-20 & IRM 9701. REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 23, 2013 · N453FE · Airbus A310222 · Fuselage Floor PanelSDR FDEA201309232282Floor Panel · dentedFLOOR PANEL 162HF IN BULK CARGO, FOUND SERIOUS DENT IN SKIN. FABRICATED A NEW PANEL WITH INSERTS AND ADHESIVE IAW SRM 53-10-20 & IRM 9701. REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 23, 2013 · N453FE · Airbus A310222 · Fuselage Floor PanelSDR FDEA201005031430Crease Beam · corrodedL-3 DOOR INBD CREASEBEAM CORRODED AT STA 1348 LBL 60. REMOVED CORROSION FROM LT SIDE IB CREASE BEAM CHORD AT STA 1290-1370 IAW SRM 51- 10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15 FIG 101 DETAIL VII. ORIG MATERIAL .100 AFTER REWORK .083 L=1.0 W=1.0. May 3, 2010 · N453FE · Airbus A310222 · Fuselage Main, StructureSDR FDEA201003240978Pressure Switch · failedT/O, 1 MIN NR 1 ENG FUEL FILTER CLOG LT ILLUMINATED FOLLOWED QRH NO RELIEF RTB LAND WT 271.5K LBS. RELEASED FOR SERVICE IAW MEL: 73-36-03-01. ONCE EACH FLIGHT DAY." NR 1 ENG FUEL FILTER INSPECTED & NO CONTAMINATION FOUND. R & R FUEL FILTER IAW AMM 73-12-0Mar 24, 2010 · N453FE · Airbus A310222 · Engine Fuel DistributionSDR FDEA201003210950Switch · inoperativeNR 1 ENG FUEL FILTER CLOG AT 19000 FT IN CLIMB - RETURNED PWR TO IDLE. WARNING REMAINING ON. MEL 21MAR10 RELEASED FOR SERVICE IAW MEL: 73-36-03-02 CATEGORY: C EXPIRATION: 31MAR10 NR1 ENG FUEL FILTER INSPECTED & NO CONTAMINATION FOUND. REPLACED FUEL FILTERMar 21, 2010 · N453FE · Airbus A310222 · Engine Fuel DistributionSDR FDEA201001210207Actuator · damagedDURING T/S FOUND RT NR 2 SPEEDBRAKE ACTUATOR'S ROD END BROKEN ALSO THE INBD FLAP NEAR THE SPEEDBRAKE ACTUATOR DAMAGED ABOUT 2IN X 1.5 IN. R & R RT INBD FLAP VANE IAW AMM 27-50-11-4. OPS CHECK NORMAL . REF DISCREPANCY 2760 9380 FOR SPEEDBRAKE ACTUATOR CHAJan 21, 2010 · N453FE · Airbus A310222 · Drag Control SystemSDR FDEA200909113287Switch · inoperative45 MINS AFTER T/O DEPARTUE AT FL 340, NR 2 OIL CLOG LIGHT ILLUMINATED. FOLLOWED QRH PROC, SHUTDOWN NR 2 ENG AND RETURNED TO DEPARTURE. REMOVED AND REPLACED NR 2 ENG OIL PRESSURE SWITCH AND OIL PRESSURE DIFFERENTIAL SWITCH. RAN NR 2 ENG IAW JRH - NO " OIL Sep 11, 2009 · N453FE · Airbus A310222 · Central WarningSDR FDEA200902250721Smoke Warning · false activationJUST BEFORE TAKEOFF, MAIN DECK CARGO SMOKE (ECAM). WORKED QRH PROCEDURE AND THEN HAD ECAM, CARGO LOOP FAULT FOR MID-DECK. WHILE RUNNING CHECKLIST FOR CARGO LOOP FAULT, BOTH A AND B ON AFT DECK, MAIN DECK CARGO SMOKE ILLUMINATED AND REMAINED ON. JUST PRIOR TFeb 25, 2009 · N453FE · Airbus A310322 · Smoke DetectionSDR FDEA200902250720Smoke Warning · false activationJUST BEFORE TAKEOFF, MAIN DECK CARGO SMOKE (ECAM). WORKED QRH PROCEDURE AND THEN HAD ECAM, CARGO LOOP FAULT FOR MID-DECK. WHILE RUNNING CHECKLIST FOR CARGO LOOP FAULT, BOTH A AND B ON AFT DECK, MAIN DECK CARGO SMOKE ILLUMINATED AND REMAINED ON. JUST PRIOR TOFeb 25, 2009 · N453FE · Airbus A310222 · Smoke DetectionSDR FDEA200812175191Control Module · malfunctionedAFTER T/O LANDING GEAR WOULD NOT RETRACT. THIS WAS CONFIRMED ON OVHD PANEL AS WELL. INTERROGATED MTP AND GOT 28V GEAR PWR SUPPLY 1 LOSS LOGGED AND LIKEWISE FOUND RELAYS AND RETRACT CTL CB OF LDG PROX DETECTOR POPPED OUT. FOLLOWED T/S PER TSM 32-30-00 FIG 1Dec 17, 2008 · N453FE · Airbus A310222 · Landing Gear Retraction/Extension SystemSDR FDEA200812175188Control Handle · failedAFTER T/O LANDING GEAR WOULD NOT RETRACT. THIS WAS CONFIRMED ON OVHD PANEL AS WELL. INTERROGATED MTP AND GOT 28V GEAR PWR SUPPLY 1 LOSS. INTERROGATED MTP AND GOT 28V GEAR POWER SUPPLY 1 LOSS LOGGED AND LIKEWISE FOUND RELAYS & RETRACT CONTROL C/B OF MLG PROX Dec 17, 2008 · N453FE · Airbus A310222 · Landing Gear SelectorSDR FDEA200811134875Attach Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING AT RIB 14 HAS CORROSION. COMPLIED WITH EA 6-5510-125488.Nov 13, 2008 · N453FE · Airbus A310222 · Vertical Stabilizer, Attach FittingsSDR FDEA200811134874Attach Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING AT RIB 13 HAS CORROSION. COMPLIED WITH EA 6-5510-125488.Nov 13, 2008 · N453FE · Airbus A310222 · Vertical Stabilizer, Attach FittingsSDR FDEA200811134873Attach Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING AT RIB 12 HAS CORROSION. REMOVED CORROSION PER SRM 51-74-10. APPLIED ALODINE TO THE REWORKED AREA PER SRM 51-21-10. FREE OF CRACK AT THE REWORKED AREA. REMAINING THICKNESS IS 0.481 INCH, IT IS WITHIN LIMIT PER SRM 55-30-0Nov 13, 2008 · N453FE · Airbus A310222 · Vertical Stabilizer, Attach FittingsSDR 08FDEA04875Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING AT RIB 14 HAS CORROSION.Nov 13, 2008 · N453FE · Airbus A310222 · Vertical Stabilizer, Attach FittingsSDR 08FDEA04874Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING AT RIB 13 HAS CORROSION.Nov 13, 2008 · N453FE · Airbus A310222 · Vertical Stabilizer, Attach FittingsSDR 08FDEA04873Attach Fitting · corrodedVERTICAL STABILIZER ATTACH FITTING AT RIB 12 HAS CORROSION.Nov 13, 2008 · N453FE · Airbus A310222 · Vertical Stabilizer, Attach FittingsSDR FDEA200811124869Bellcrank · corrodedNR 1 RUDDER SERVO ACTUATOR BELLCRANK AT RIB 12 HAS CORROSION. REPLACED WITH NEW FITTING PER SRM 51-40-21. PERFORM RUDDER MECHANICAL CONTROL OPERATIONAL AND FUNCTIONAL TEST PER AMM 27-21-00-5.Nov 12, 2008 · N453FE · Airbus A310222 · Rudder StructureSDR FDEA200811124868Attach Fitting · corrodedRUDDER, NR 1 ATTACH FITTING HAS CORROSION. REPLACED WITH NEW FITTING PER SRM 51-40-21.Nov 12, 2008 · N453FE · Airbus A310222 · Rudder/Tab, Attach FittingsSDR 08FDEA04869Bellcrank · corrodedNR 1 RUDDER SERVO ACTUATOR BELLCRANK AT RIB 12 HAS CORROSION.Nov 12, 2008 · N453FE · Airbus A310222 · Rudder Control SystemSDR 08FDEA04868Attach Fitting · corrodedRUDDER, NR 1 ATTACH FITTING HAS CORROSION.Nov 12, 2008 · N453FE · Airbus A310222 · Rudder StructureSDR FDEA200811104881Engine · inoperativeENG NR 2 FAILURE DURING CLIMB-OUT. CLIMB POWER PASSING 1800 FT, FELT SHUDDER, HEARD A BANG, HAD YAW. COMPLETED SINGLE ENGINE LANDING. NO SMOKE OR FIRE PULLED NR 2 ENG FIRE HANDLE AND AGENT 1 DISCHARGED. EGT SPIKE TO 780. R AND I NR 2 ENGINE AND PERFORMED Oct 10, 2008 · N453FE · Airbus A310222 · Engine (Turbine/Turboprop)SDR 08FDEA01206O-Ring · leakingDURING CRUISE GREEN SYSTEM LOW QUANTITY ALERT. LOSS OF GREEN HYD KRUEGER FLAP ALERT DURING APPROACH. CREW DECLARED FOR EMERGENCY LANDING. ACCORDING TO CREW THE A/C LANDED SMOOTHLY AT WSSS 02L AND NO OVERWEIGHT. THE GREEN HYD FLUID QTY INDICATION AT LOWER Mar 30, 2008 · N453FE · Airbus A310222 · Drag Control SystemSDR 07FDEA05007Switch · looseDURING TAKEOFF ROLL WITH POWER ADVANCING TO TAKEOFF POWER (MAX), THE NR 2 REV UNLOCK LIGHT ILLUMINATED. TAKEOFF WAS REJECTED. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 15DEC07, SFS BKK/06 T/S FOUND ENG NR 2 RT STOW SWITCH Dec 5, 2007 · N453FE · Airbus A310222 · Engine Thrust ReverserSDR 07FDEA02876Pitot Head · obstructedREJECTED TAKEOFF AT APPROX 90 KNOTS DUE TO NO F/O A/S. FOUND BUG DEBRIS IN F/O PITOT PROBE CLEANED. INSPECTED PROBE PER AMM 34-11-15-6, NO DEFECTS NOTED. F/O'S AIRSPEED CHECKED GOOD WITH PITOT TESTER. INSPECTED A/C BRAKES PER AMM 05-51-16-0. NO DEFECTS NOAug 14, 2007 · N453FE · Airbus A310222 · Pitot/Static SystemSDR 06FDEA2677Stringer · corrodedAVIONICS COMPART RT SIDE CORRSION ON STR 44R AT FR 17R REF N00188. REMOVED CORROSION IAW A310-200 SRM 51-74-10 FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 51-10-17 REPAIRED IAW EA 6-5310-102502.Jul 25, 2006 · N453FE · Airbus A310222 · Fuselage Main, Longeron/StringerSDR 06FDEA2625Adapter · corrodedCLS ADAPTER AT FR 46 BETWEEN SEAT TRACK R2 & R3 BENT REF N00300. REMOVED AND REPLACED CLS ADAPTER IAW A310-200 SRM 51-72-10.Jul 18, 2006 · N453FE · Airbus A310222 · Fuselage Miscellaneous StructureSDR 06FDEA2623Seat Track · gougedCLS ADAPTER AT FR 43 BETWEEN SEAT TRACK R2 & R3 HAS GOUGE IN SCALLOP REF N00298. REMOVED AND REPLACED CLS ADAPTER IAW A310-200 SRM 51-72-10.Jul 18, 2006 · N453FE · Airbus A310222 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02606Fairing · crackedSMIS 453 05-21 0003629 28JUN04 MC1 OPEN R WS-P 00026805 MOD TYPE H MOD NR C-CHECK REV NR PS ACCOMPLISH MAINTENANCE C-CHECK NR 002 ENT BY: 067708 PLND: ORIGINAL PLAN DATE WAS ENTERED ON: 28JUN04 19:47:42:3 BY:067708 S=M PLND: DATE:01AUG04 AT: LIS-VNSep 2, 2004 · N453FE · Airbus A310 · Aerodynamic FairingsSDR 04FDEA02593Seal · wornDURING C CHECK, FOUND DAMAGED DRIP PAN SEAL AND WORN SUPPORT HOLES ON PANEL 147CZ AND 148CZ. GEN ITEM 41C0508. PANELS REPAIRED ON N00056 AND N00057 PER EA 6-5315-81014.Sep 1, 2004 · N453FE · Airbus A310222 · Fuselage Miscellaneous StructureSDR 04FDEA01541Cable · out of rigON TAKEOFF NR 2 THROTTLE WOULD NOT GO PAST V2WAY, DUE TO BINDING. ABORTED BELOW 70 KTS. RETURNED TO GATE. THROTTLE LEVER FEEDBACK CABLE MECHANISM FOUND OUT OF RIGGING RANGE. T/L FEEDBACK MECHANISM RIGGED IAW MM 78-31-38-2.May 31, 2004 · N453FE · Airbus A310222 · Power LeverSDR 01FDEA00860Engine · malfunctioned01-324 ON T/O NR 2 ENGINE N1 STAGNATED & W/N ACCELERATE PAST 49 PERCENT, ALL PARAMETERS NORMAL AND PROCEEDED TO T/O.Sep 27, 2001 · N453FE · Airbus A310222 · Engine (Turbine/Turboprop)SDR 00FDEA00862Warning Light · illuminated00-344 ON T/O ROLL NR 1 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. ** S/D ** COMINGDec 8, 2000 · N453FE · Airbus A310222 · Engine Thrust ReverserSDR 00FDEA00200Skin · damagedFRAME 19/20, STR 29-31 RT DAMAGED FUSELAGE SKIN AT ACCESS DOOR CONTROL PNL CORNERS. BLEND OUT DAMAGE IAW THE REFERENCED DWG EFW 632-99 & PROTECT SURFACE AP SRM.Mar 30, 2000 · N453FE · Airbus A310222 · Fuselage Main, Plate/SkinSDR 00FDEA00199Skin · crackedFRAME 79, STR 10 LT/RT DENTS ON OUTER FUSELAGE SKIN MAX DENT DEPT 1.3 MM LT AND 0.9 MM RT. REMOVED AND REPLACED DAMAGE PER SRM DWG TD/K4/51/11742/1999.Mar 30, 2000 · N453FE · Airbus A310222 · Fuselage Main, Plate/SkinSDR 00FDEA00198Skin · crackedFRAME 54.1-54.2, STR 39-41 LT EXT FUSELAGE SKIN CRACKED. REMOVED AND REPLACED REINFORCEMENT DOUBLER (16R539H0126) PER DWG 16R539H0111, SHEET 2 IAW DWG 74626/99-04 PC.Mar 30, 2000 · N453FE · Airbus A310222 · Fuselage Main, Plate/Skin
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