N681FE
Service difficulty reports · 339
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 = 'N681FE' 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.
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 = 'N681FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201001220215Floor Support · crackedAVIONICS COMPARTMENT FLOOR SUPPORT INTERCOSTAL ATTACH ANGLE IS CRACKED AT FRAME 10. REMOVED ATTACH ANGLE. LOCATED AND DRILLED ANGLE. INSTALLED ATTACH ANGLE IAW SRM 51-72-10SDR FDEA201001200196Floor Panel · damagedMAIN CABIN FLOOR PANEL 231 YG IS DAMAGED. REPAIRED MAIN CAB CARGO COMPARTMENT FLOOR PANEL 231 YG BY FABRICATING NEW FLOOR PANEL USING OLD FLOOR PANEL 231 YG AS TEMPLATE IAW DWG SRZ 25-005, REV "H".SDR FDEA201001190176Support · crackedE & E COMPARTMENT BATTERY RACK CTR HORIZONTAL SUPPORT IS CRACKED AT THE INBD FASTENER HOLE. REMOVED BATTERY RACK SUPPORT IAW SRM 51-72-10, PARA 5, PG 2 AND SRM 51-40-21, PARA 6. INSTALLED BATTERY RACK SUPPORT IAW SRM 51-72-10, PARA 6, PG 2 AND SRM 51-40-21SDR FDEA201001190175Channel · crackedAVIONICS COMPARTMENT BATTERY RACK IS CRACKED AT THE INBD HAT CHANNEL AND CTR SUPPORT STRUCTURE ATTACH POINT AT FRAME 16. REMOVED AND RE-INSTALLED SHIPS BATTERIES AFTER REPAIR IN REFERENCE TO AMM 24-31-11-4. PERFORMED A GOOD CHECK OF THE BATTERY CHARGER BITESDR FDEA201001180171Skin · crackedAPU COMPARTMENT; RT ACCESS DOOR; AFT INBD CORNER; SKIN IS CRACKED AND A RIVET IS SHEARED. DRILLED OUT FASTENER IAW SRM 51-40-21, PARA 6. CUT OUT DAMAGE IAW SRM 52-41-41, PG 210. IAW SRM 52-41-11, FIG 202. FABRICATED REPAIR PARTS IAW SRM 52-41-11, FIG 202, PSDR FDEA201001180170Skin · damagedFWD CARGO DOOR; UPPER AFT CORNER HAS A SHEARED FASTENER AND SKIN SEPARATION. REPAIRED IAW SRM 52-31-00, FIG 203, SHEET 3. ALODINE, PRIME AND TOPCOAT IAW SRM 51-21-10, PG 4 AND SRM 51-23-10, PGS 2 & 3. INSTALLED DOUBLER IAW SRM 52-31-00, FIG 203, SHEET 3.SDR FDEA201001180169Skin · damagedFWD CARGO DOOR; UPPER FWD CORNER HAS A SHEARED FASTENER AND SKIN SEPARATION. REPAIRED CRACK IAW SRM 52-31-00, FIG 203, SHEET 3. ALODINE, PRIME AND TOPCOAT IAW SRM 51-21-10, PG 4 & SRM 51-23-10, PGS 2 & 3. INSTALLED DOUBLER IAW SRM 52-31-00, FIG 203, SHEET SDR FDEA201001140143Floorboard · puncturedMAIN CABIN CARGO COMPARTMENT FLOORBOARD NR 242 RG IS PUNCTURED. REPAIRED MAIN CAB CARGO COMPARTMENT FLOORBOARD NR 242 RG BY FABRICATING NEW FLOORBOARD USING OLD FLOORBOARD NR 242 RG AS TEMPLATE IAW DWG SRZ 25-005, REV "H".SDR FDEA201001140142Floorboard · puncturedMAIN CABIN CARGO COMPARTMENT FLOORBOARD NR 242 EK IS PUNCTURED. REPAIRED MAIN CAB CARGO COMPARTMENT FLOORBOARD NR 242 EK BY FABRICATING NEW FLOORBOARD USING OLD FLOORBOARD NR 242 EK AS TEMPLATE IAW DWG SRZ 25-005, REV "H".SDR FDEA201001140141Floorboard · puncturedMAIN CABIN CARGO COMPARTMENT FLOORBOARD NR 242 UJ IS PUNCTURED. REPAIRED MAIN CAB CARGO COMPARTMENT FLOORBOARD NR 242 UJ BY FABRICATING NEW FLOORBOARD USING OLD FLOORBOARD NR 242 UJ AS TEMPLATE IAW DWG SRZ 25-005, REV "H".SDR FDEA201001140140Floorboard · puncturedMAIN CABIN CARGO COMPARTMENT FLOORBOARD NR 240 QJ IS PUNCTURED. REPAIRED MAIN CAB CARGO COMPARTMENT FLOORBOARD NR 242 QJ BY FABRICATING NEW FLOORBOARD USING OLD FLOORBOARD NR 242 QJ AS TEMPLATE IAW DWG SRZ 25-005, REV "H".SDR FDEA201001140139Floorboard · puncturedMAIN CABIN CARGO COMPARTMENT FLOORBOARD NR 242 SF IS PUNCTURED. REPAIRED MAIN CAB CARGO COMPARTMENT FLOORBOARD NR 242 SF BY FABRICATING NEW FLOORBOARD USING OLD FLOORBOARD NR 242 SF AS TEMPLATE IAW DWG SRZ 25-005, REV "H".SDR FDEA201001140137Support · crackedRT WING T/E UPPER PANEL SUPPORT IS CRACKED FROM RIB 6A TO RIB 7. REMOVED CRACKED SUPPORT/STIFFENER IAW SRM 51-40-21, PARA 7. MACHINED NEW STIFFENER IAW DWG A57241059. ACCOMPLISHED FPI IAW DWG A57241059 IAW PROCESS 526.2501 AND ABP 6-5230. NO CRACKS NOTED. SDR FDEA201001140128Skin · crackedRT WING LOWER SKIN SURFACE IS CRACKED AT ACCESS PANEL 613 AB. REMOVED ACCESS PANEL ADJACENT TO THE REPAIR ON THE FWD SPAR IAW SRM 51-40-02, PARA 5. FABRICATED -1 AND -3 REPAIR DOUBLERS IAW SRM 53-15-63, FIG 201. ALODINED REPAIR IAW SRM 51-21-10, PARA 2-B(C)SDR FDEA200906242283Fusible Plug · blownWINDS 340/24/GUSTS 29 LANDED RUNWAY 28 MEDIUM BRAKES 20/20 FLAP, SMOOTH LANDING, ON CENTERLINE 3 LT TRUCK TIRES FUSE PLUGS BLEW ON TAXI IN. TEMP REACHED 650-700 ON 3 TIRES RT REACHED 150 MAX.SDR FDEA200808293645Ecu · failedDURING CLIMB NR 2 ENG N1, FF, EGT BECAME UNSTABLE, ASSOCIATED WITH ENGINE SURGING. FADEC GRD TEST, FOUND FAULT CODE 352-21 ON CH A. N1 SPEED SENSOR PERFORMED TSM PROCEDURE 73-21-30 352-21 FIG 102 SHEET 28. CHECKED BOTH CH A AND B SYS GOOD. SPEED SENSOR IS SDR 08FDEA03645Ecu · failedDURING CLIMB NR 2 ENG N1, FF, EGT BECAME UNSTABLE, ASSOCIATED WITH ENGINE SURGING. FOLLOWING NR 2 ENG FADEC BITE DISPLAY: BITE CHA CHB 270 84120 84120 271 99080 99080 272 20000 20000 273 274 ON 350-354. FADEC GROUND TEST: FOUND FAULT CODE 352-21 SDR 08FDEA01463Filter · cloggedNR 1 ENGINE FUEL FILTER CLOG LIGHT CAME ON DURING TAKEOFF ROLL AT 80 KTS WITH STD POWER SET. LIGHT AND ECAM WARNING WENT OUT AS SOON AS THROTTLES WERE RETARDED TO IDLE. REMOVED NR 1 ENGINE FUEL FILTER. FOUND FILTER CLOGGED WITH DEBRIS. INSTALLED NEW FUEL FSDR 08FDEA00367Seat Track · wornMAIN CARGO DECK NR 1 SEAT TRACK BETWEEN FR 41 AND FR 45N HAS SEVERAL SCALLOPS WORN REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-72-10.SDR 08FDEA00366Seat Track · damagedMDCC SEAT TRACK NR 1 BETWEEN FR 57 AND FR 57.1 HAS 2 SCALLOPS BROKEN. REMOVED DAMAGED SECTION OF TRACK AND INSTALLED SEAT TRACK REPAIR IAW A300-600 SRM 53-10-16, FIG 201.SDR 08FDEA00365Seat Track · wornSEAT TRACK AT FR 57.1, 2 LT HAS 2 EA SCALLOPS WORN REMOVED DAMAGED SEAT TRACK SECTION AND INSTALLED SEAT TRACK REPAIR IAW A300-600 SRM 53-10-16, FIG 201.SDR 08FDEA00290Adapter · crackedMAIN CARGO DECK FRAME 57.1 SEAT TRACK NR 3 LT SIDE CLS ADAPTER CRACKED APPROX 3.5 INCH IN LENGTH. REMOVED AND REPLACED CLS ADAPTER IAW A300-600 SRM 51-72-10.SDR 07FDEA00619Unknown · unsecureON T/O ROLL BELOW 80K, NR 1 T/R PRESSURIZED AS NOTED ON LEFT ECAM AND NR 1 REV UNLOCK LT ILLUMINATED. FOUND C/P FOR DPV NOT SECURED CAUSING LT, REF MEL 78-30-01-A.SDR 07FDEA00353Thrust Reverser · malfunctionedNR 1 T/R PRESSURIZED AS POWER INCREASED THROUGH 75-80 PERCENT N1. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 16FEB07 "MEL 78-30-01-A: ENGINE NR 1 TSI OPENED FOR T/S.SDR 05FDEA03402Skin · chafedLEFT WING SPOILER NR 2 O/B FWD EDGE 2 EA AREAS THAT ARE CHAFED. COMPLIED WITH EA 6-5750-92961 N00044.SDR 05FDEA03401Skin · chafedLEFT WING O/B UPPER SURFACE HAS 4 EA CHAFE MARKS. COMPLIED WITH EA 6-5750-93355 REF N00076.SDR 05FDEA03400Skin · chafedLEFT WING TRAILING EDGE SUBSTRUCTURE LOWER SURFACE 7 EA RIVET HEADS CHAFING INTO UPPER SURFACE, INTO THE O/B FLAP (LOCATED BETWEEN SPOILER 3 AND 4) DAMAGE ON SUBSTRUCTURE AND ON FLAP. COMPLIED WITH EA 6-5750-93356 REF N00077.SDR 05FDEA03397Retainer · looseSTATIC DISCHARGER RETAINER AT RT WING MOST OUTBOARD IS BAD/LOOSE. COMPLIED WITH EA6-5720-92943 REF N00232.SDR 05FDEA03398Door Frame · gougedFWD CARGO DOOR FRAME 20A SKIN IS GOUGE AND SCRATCH LWR FWD CORNER OF CARGO DOOR. COMPLIED WITH EA 6-533092960 REF N00212.SDR 05FDEA03004Seat Track · damagedFR 42- FR 43 SEAT TRACK L3 IS DAMAGED IN SCALLOP AREA. FABRICATED AND INSTALLED SEAT TRACK SECTION IAW A300-600 SRM 53-10-16. ALODINED, PRIMED, AND TOPCOATED IAW A300-600 SRM 51-75-10.SDR 05FDEA03003Seat Track · damagedMDCC - FR 37-38 SEAT TRACK L3 HAS DAMAGE IN SCALLOPS. FABRICATED AND INSTALLED SEAT TRACK SECTION IAW A300-600 SRM 53-10-16. ALODINED, PRIMED, AND TOPCOATED IAW A300-600 SRM 51-75-10.SDR 05FDEA03002Seat Track · damagedMDCC SEAT TRACK R2 FS 54.2 - FS 54.3 HAS DAMAGE IN SCALLOP AREA. FABRICATED SEAT TRACK SECTION AND INSTALLED WITH 2 EA SPLICES IAW A300-600 SRM 53-10-16. ALODINED, PRIMED, AND TOPCOATED IAW A300-600 SRM 51-75-10.SDR 05FDEA03001Seat Track · damagedSEAT TRACK L2 AT FS 54.2 - 54.3 HAS DAMAGE IN SCALLOP AREA. FABRICATED SEAT TRACK SECTION AND INSTALLED WITH SPLICES (2EA) IAW A300-600 SRM 53-10-16. ALODINED, PRIMED, AND TOPCOATED IAW A300-600 SRM 51-25-10.SDR 05FDEA03000Adapter · damagedMDCC CLAS ADAPTER AT FR 42 AND FR 44 BETWEEN S/T L4 AND L5 HAVE DAMAGE IN SCALLOP AREAS. REMOVED AND REPLACED 2 CROSSBEAMS IAW A300-600 SRM 51-72-10.SDR 04FDEA00062Pilot Valve · failedON TAKEOF ROLL WHEN PWR ADVANCED ABOVE 60 PERCENT N1 RECEIVED NR 1 ENG REVERSE PRESSURIZED ECAM. ABORTED T/O ROLL RETURNED TO GATE. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A MEL 78-30-01-A: ENGINE 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED ISDR 03FDEA01249Frame · crackedAFT CARGO FRAME (C58) 20 INCH TO THE RT OF CENTER HAS A 1 INCH CRACK IN FRAME. REPAIRED: IAW (EA6-5310-71398) BY CUTTING OUT CRACKED SECTION IAW SRM 51-27-00, NDT THE CUT OUT. REMOVED AFFECTED FASTENERS AND CABLE SUPPORTS AS REQUIRED, FLAP-PEEN AREA FABSDR 02FDEA00919Thrust Reverser · malfunctionedDURING TAKEOFF POWER APPLICATION AS POWER STABILIZED AT TOGA SETTING, ECAM ANNUNCIATED A NR 1 REVERSER PRESSURIZED WARNING. TAKEOFF WAS ABORTED AT ABOUT 60 KTS. ENGINE NR 1 THRUST REVERSER , INOPERATIVE. THRUST NR 1 (1 OR 2) REVERSER DEACTIVATED IN FORWARD SDR 01FDEA00461Warning System · activatedON T/O ECAM WARN ENG FAIL NR 2 ABORTED TAKEOFF. RETURN FOR 2ND TRY AND RECEIVED ECAM WARN ENG SHUTDOWN.SDR 00FDEA00319Engine · vibration00-133 AT ROTATION SPD NR 1 ENG START VIB LOUDLY. VIEW BIRDS ON RUNWAY ON ROTATION. PERFORMED TRIM BALANCE AND VIBRATION SURVEY PER A300 MM 72-21-00-2. VIB LEVELS WELL WITHIN LIMITS AT THIS TIME.
Back to N681FE