N921FD
Service difficulty reports · 121
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 = 'N921FD' 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 = 'N921FD' 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 FDEA202507221293Socket · loosePARKING BRAKE DISCRETE LIGHT DOES NOT ILLUMINATE WHEN PARKING BRAKE SET FOUND PARKING BRAKE LIGHT BASE ASSY LOOSE, TIGHTEN BASE. LIGHT OPS CKED GOOD. A/C OK FOR SERVICE.SDR FDEA202507191267Skin · damagedWHILE PERFORMING INSPECTION ON THE #2 CARGO DOOR LWR CORNERS SKIN CUTOUT FWD AND AFT, FOUND A REPAIR ON THE AFT LOWER CORNER OF THE #2 CARGO DOOR AREA. AD2006-11-11 FUSELAGE PREVIOUS REPAIR AT NO. 2 CARGO DOOR CUTOUT BS 1410-1445 STR 25- 28R. ACCOMPLISHED SSDR FDEA202507141192Floorbeam · corrodedMCD STA 1640 SUPPORT BEAM BL 0.00 TO LBL 45.50 HAS CORROSION. REMOVED CORROSION AT STA 1640 SUPPORT BEAM BL 0.00 - LBL 45050 IAW SRM 51-10-02. FOUND OUT OF LIMIT IAW SRM 53-00-51-1A. REPAIRED FLOOR BEAM AT STA 1640, LBL 45.50 IAW SRM 53- 00-51-2R. MAJOR REPSDR FDEA202507141191Crease Beam · corrodedCORROSION NOTED ON THE ATTACHMENT FRAME OF MAIN DECK FLOORBOARD # 252 MKF (RH MOST O/B) AT STA 1540 - 1620. REPAIRED FRAME ATTACHMENT (CREASE BEAM) AT MAIN CABIN R/H STA 1540 - 1620 IAW SRM 53- 00-13-2R. MAJOR REPAIR.SDR FDEA202507111182Seat Track · corrodedCORROSION NOTED ON THE SEAT TRACK BASE AT LH STA 1200-1240 I/B OF FLOOR PNL 251 MCF. REMOVED AND REPLACED SEAT TRACK AT L/H STA 1180 TO 1240 LBL 45.50 IAW SRM 51-40-02 AND SRM 53-60-52-01. MAJOR REPAIR.SDR FDEA202504040573Module · faultedDURING FIRE/OVHT TEST MASTER WARNING, MASTER CAUTION LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED MASTER WARNING MODULE (M618) REF AMM 31-51-04-4 OPS TEST GOOD. A/C OK FOR SERVICE. WEU BOARD, PN 285T0032-19, SN F20543.SDR FDEA202405250726Controller · failedAT FL400 CABIN ALT HIGH WARNING DONNED MASKS. RAN QRH. INITIATED EMERGENCY DESCENT. CABIN ALTITUDE RATE REACHED 2000 FT PER MIN DOWN AND HIGHEST ALTITUDE REACHED WAS 15 K. EMERGENCY DECLARED AMM: 21-31-02-4, AMM: 21-31-00-5, AMM: 05-51-24-2, CABIN PRESDR FDEA202304240748Cam · failedON APPROACH, GOT LT FWD ENTRY DOOR EICAS. AFTER SHUTDOWN, DOOR HANDLE HAD RAISED APPROX 4 INCHES, SLIGHTLY ABOVE DOOR ARMED KNUCKLE BUSTER. DOOR HANDLE CONFIRMED FULLY DOWN BEFORE PUSH. IAW PREVIOUS DISCREPANCIES, SEEMS THAT RESTRICTIONS TO GIRT BAR IS KEEPSDR FDEA202304200725Roller · misalignedPDIS 921 52-10 0900 20APR23 FAT FACT U L FWD ENTRY DOOR EICAS CAME ON DURING DEPARTURE PASSING APPROX 3000 . RAN QRH AND CONTINUED NORMAL OPS AS PRESSURIZATION REMAINED NORMAL. EICAS WENT OUT BEFORE REACHING CRUISE ALTITUDE. IT CAME BACK OSDR FDEA202210212637Lamp · burned outL1 DOOR INTERIOR EXIT LIGHTS 3/4 OF LIGHTS BURNED OUT. REMOVED AND REPLACED L1 DOOR INTERIOR EXIT LIGHT SIGN IAW AMM 33-51-01-2. LIGHT OPS CHECKS NORMAL. ACFT OK FOR SERVICE.SDR FDEA202206251551Oil System · low pressureLEFT ENGINE OIL QUANTITY DECREASED TO 0 ON TAKEOFF, PRESSURE DECREASED TO 0 AS WELL. L ENG OIL PRESS EICAS MESSAGE ILLUMINATED. RAN QRH AND SHUT DOWN LEFT ENGINE INFLIGHT. LANDED RNO 34L WITHOUT FURTHER INCIDENT. EMERGENCY DECLARED. REMOVED #1 ENGINE RESDR FDEA202108262107Handle · unsecureDURING A TEST FLIGHT, LT ENTRU DOOR EICAS MSG, IMMEDIATELY AFTER TAKEOFF. HANDLE HAD POPPED UP APPROX 6 INCHES AND WOULD NOT LOCK BACK DOWN. NO ABNORMAL PRESSURIZATION ISSUES. ADJUSTED THE L1 DOOR IAW AMM 52-11-00, OPS CHECKED GOOD.SDR FDEA202108232075Handle · unsecureTEST FLIGHT- L FWD ENT DOOR EICAS OCCURRED IN THE APPROACH PATTERN. THE DOOR HANDLE HAD POPPED UP APPROX 6 IN. FROM FULL LOCKED POSITION. COULD MOVE HANDLE DOWN ENOUGH TO EXTINGUISH LIGHT BUT NOT ENOUGH TO OVER-CENTER AND LOCK DOOR. REMOVED L-1 LINING DOORSDR FDEA202108232074Ram Air Turb · failedTEST FLIGHT- RAT WOULD NOT DEPLOY WITH BOTH SPEED CAD C/B PULLED. REMOVED AND REPLACED LEFT AND RIGHT ENG SPEED CARDS IAW AMM 77-12-03-4, PERFORMED RAT AUTO DROP TEST IAW AMM 29-21-00-5, TEST PASSED.SDR FDEA202108192042Frame · crackedL/H SIDE FR 1640 S-14 WEB FRAME. BOTH BOTTOM INBD AND OUTBD HOLES HAVE CRACK INDICATIONS. CLOCK POSITION FOR BOTH HOLES ARE 9 AND 3:00 O'CLOCK. ACCOMPLISHED FINAL EA F-5310-T0362919 FUSELAGE - MAIN FRAME - STA 1640 FRAME SPLICE REPAIR BETWEEN STRINGER I-9SDR FDEA202108102000Floor Panel · crackedMAIN DECK FLOOR PANEL 251MWF HAS CRACK (ADAJACENT L4 DOOR) DOT 136-51 FABRICATED MAIN DECK PANEL 251MWF ON VTMAE TRAVELER # T21/1565104 IAW DWG SRZ-25- 005 REVISION R, MAJOR REPAIR.SDR FDEA202108101999Floor Panel · crackedMAIN DECK FLOOR PANEL 251MVF HAS CRACK (ADJACENT R4 DOOR). DOT 136-58 FABRICATED MAIN DECK FLOOR PANEL 251MVF ON VTMAE TRAVELER # T21/1565102 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.SDR FDEA202105281418Controller · malfunctionedDURING CLIMB COCKPIT TEMP BECAME EXCESSIVELY HOT. RAN QRH AND AFTER TRIM AIR SWITCH TURNED OFF REGAINED TEMP CONTROL. PERFORMED BITE TEST ON CABIN ZONE TEMP CONTROLLER. NO CURRENT FAULTS OR PREVIOUS FAULTS NOTED. REMOVED AND REPLACED CABIN ZONE TEMP CONTSDR FDEA202012163169Handle · malfunctionedLEFT MAIN DOOR ARM HANDLE WILL NOT MOVE, REF FIM 52-11 TREE 802. INSPECTED DOOR LATCHING MECHANISMS FOR DEFECTS OR OBSTRUCTIONS WITH NONE FOUND. ALSO, OPERATED L1 DOOR FROM ARM/DISARM WITH SLIDE REMOVED, PER MEL WITH NO BINDING OR DEFECTS NOTED. REMAINS ON SDR FDEA202009232318Landing Gear · failedPDIS 921 32-51 8989 23SEP20 IND OPEN U. AIRCRAFT STILL PULLS HARD TO THE RIGHT. IT TAKES ALMOST 1/2 RUDDER DEFLECTION TO TRACK STRAIGHT. ALSO IT TAKES CONSIDERABLY MORE POWER TO BREAKAWAY AND GET THE JET MOVING, APPROXIMATELY 35% N1 W/BOTH ENGINES. REMOVEDSDR FDEA2019120973208Bulb · inoperativeSVC CK R-1 DOOR EMERGENCY ESCAPE SLIDE LIGHT INOP. RELAMPED R ESCAPE SLIDE LIGHT REF AMM 33-51-06-2-1, BULB GE767. OP'S NORMAL OK FOR SERVICESDR FDEA2019112202998Outflow Valve · inoperativePDIS 921 21-30 8717 20NOV19 MEM FACT U LOGPAGES:3170064 SAME PROBLEM AS YESTERDAY WITH PRESSURIZATION EXCEPT AUTO 1, AUTO 2 AND MANUAL CONTROL WORKED. HOWEVER THE PRESSURIZATION OF THE AIRCRAFT COULD NOT KEEP UP ABOVE FL 250. CABIN PRESSURE CSDR FDEA201911192993Outflow Valve · failedPDIS 921 21-30 8714 19NOV19 MCI OPEN U LOGPAGES:3170061 CABIN AUTOMATIC INOP. UNABLE TO MAINTAIN CABIN ALT IN MANUAL WITH VALVE FULLY CLOSED. REPLACED CABIN PRESSURE OUTFLOW VALVE AND TESTED PER AMM 21-31-03SDR FDEA201911192997Controller · failedCABIN AUTOMATIC INOP. UNABLE TO MAINTAIN CABIN ALT IN MANUAL WITH VALVE FULLY CLOSED. REPLACED CABIN PRESSURE OUTFLOW VALVE AND TESTED PER AMM 21-31-03-2, OPS CHECKS GOOD. REPLACED #2 AUTOMATIC PRESSURE CONTROLLERSDR FDEA2019111522934Battery · smokeSTRONG BURNING ELECTRICAL SMELL MAIN CARGO COMPARTMENT T/S FOUND APU BATTERY SMOKING WITH A HEAVY BURNT SMELL. R&R APU BATTERY REF AMM 24-31-03-4. ALSO R&R APU BATTERY CHARGER REF AMM 24-31-04-4 PRECAUTIONARY. OPS CK'D GOOD. A/C OK FOR SERVICESDR FDEA201902280547Transmitter · failedAT FLAP CONFIGURATION WE RECEIVED A TE FLAP ASYM EICAS WITH NO LE SLAT OR LE SLAT DISAGREE INDICATED. RAN QRH, DECLARED EMERGENCY AND LANDED IAW QRH GUIDANCE, FLAPS STOPPED AT LESS THAN 1 DEG. T/S PER FIM 27-51-FT803, NR 1 FSEU FAULTED LT FLAP TRANSMITTER. R&SDR FDEA201812133499Socket · damagedRIGHT FORWARD ENTRY DOOR SLIDE WILL NOT ARM. R1 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS INOP. REMOVED AND REPLACED SLIDE ANNUNCIATOR ASSY IAW SMP AND 757 WDM CH 25_66_11. SLIDE LIGHT OPS CHECKS SDR FDEA201708062125Spar · corrodedLT WING O/B FLAP MID AREA INTERIOR FRONT SPAR LOWER CHORD FOUND HEAVY CORROSION. COMPLIED WITH EA F-5750-T0334766 P1, REPAIRED LT WING O/B FLAP MID AREA INTERIOR FRONT SPAR LOWER CHORD. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201708032102Floor Support · corrodedMDCC BS 920 - 1040, LBL 45.5 FLOOR SUPPORT CORRODED. REPAIRED THE FLOOR SUPPORT IAW EA:F-5310-T0334767 P1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201708032100Seat Track · corrodedMDCC BS 1180 - 1200, LBL 24.75 SEAT TRACK CORRODED. FABRICATED A NEW SEAT TRACK IAW DWG 146N5130. REPLACED THE SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201708032103Seat Track · corrodedMDCC BS 1180 - 1200, RBL 45.5 SEAT TRACK CORRODED. FABRICATED A NEW SEAT TRACK IAW DWG 146N5130. REPLACED THE SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201708032101Seat Track · corrodedMDCC BS 1080 - 1180, LBL 45.5 SEAT TRACK CORRODED. FABRICATED A NEW SEAT TRACK IAW DWG 144N5021. REPLACED THE SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201706301788Hydraulic System · leakingINFLIGHT EICAS LT HYD QTY INDICATED 0.45. QUANTITY CONTINUED DECREASING AND LOST ENTIRE L HYDRAULIC SYSTEM AFTER LANDING ROLLOUT, NO NLG STEERING AVAILABLE. OPENSDR FDEA201704111131Flap System · malfunctionedDURING FINAL APPROACH, EXTENDED FLAPS 15 TO 20, FLAPS STUCK AT 17 DEGREES. RECEIVED A TE FLAP DISAGREE EICAS MESSAGE. DECLARED AN EMERGENCY PERFORMED QRH. UNEVENTFUL SECOND APPROACH. BITE FSEU NR 1, RECEIVED A FAULT CODE 305. FOLLOWED FIM AND PERFORMED ISDR FDEA201603291099Fseu · inoperativeAT LEVEL OFF FLIGHT 360, EICAS MSG LE SLAT ASYM MSG CAME ON. COMPLIED WITH QRH. ACFT ARRIVED WITH NO LOWER EICAS MSG OR MX MSG. LE LIGHT WAS ON ABOVE POSITION GAUGE. CREW HAD LE SLAT ASYM ORANGE ON UPPER EICAS. RESETTING FSCUE 1 BREAKER CLEARED LIGHT. BISDR FDEA201603291098Computer · inoperativeAT LEVEL OFF FLIGHT 360, EICAS MSG LE SLAT ASYM MSG CAME ON. COMPLIED WITH QRH. ACFT ARRIVED WITH NO LOWER EICAS MSG OR MX MSG. LE LIGHT WAS ON ABOVE POSITION GAUGE. CREW HAD, LE SLAT ASYM, IN ORANGE ON UPPER EICAS. RESETTING FSCUE 1 BREAKER CLEARED LIGHTSDR FDEA201511293815Slide · unsecureAFTER LANDING, FIRST OFFICER FAILED TO DISARM RT ENTRY DOOR. SLIDE & RAFT CAME OUT OF CONTAINER BUT DID NOT INFLATE, WHEN MX OPENED DOOR. REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE. REF AMM 25-66-01-4. ITEM REMOVED FROM MEL, A/C OK FOR SERVICE.SDR FDEA201508122540Skin · delaminatedLEFT WING INBD FLAP, CHIPPED PAINT, POSSIBLE DELAMINATION UPPER SURFACE. REPAIRED IAW SRM 51-70-07-00-0 PARAGRAPHS 4 D4 & 4.6.SDR FDEA201508102527Shear Plate · corrodedMAIN CABIN SHEAR PLATE HAS CORROSION BS 395 - 440, BETWEEN LBL 24.75 & 45.50. REPAIRED IAW EA F-5310-T0319429 REV NR PS P1.SDR FDEA201508102526Shear Plate · corrodedMAIN CABIN SHEAR PLATE HAS CORROSION BS 395 - 440, BETWEEN LBL 0 & 24.75. REPAIRED IAW EA F-5310-T0319384 REV NR PS P1SDR FDEA201312193024Controller · failedDURING CRUISE FL380, IN CLEAR AIR WITH ANTI-ICE OFF, RECEIVED EICAS MESSAGES FOR RT ENGINE BLEED OFF, RT PACK OFF, & RT PACK TEMP, IAW QRH TURNED RT ENGINE BLEED OFF. R & R RT PACK TEMP CONTROLLER IAW AMM 21-51-14-4, CHECKED NORMAL IAW FIM 36-10.SDR FDEA201307311708Attach Fitting · crackedFWD ENTRY AREA, FRAME BS 350, ATTACH FITTING TO L1 DOOR UPPER SILL IS CRACKED. REMOVED DAMAGED ATTACH FITTING, FABRICATED AND INSTALLED NEW ATTACH FITTING IAW DWG 141N8321, REV F AND SRM 51-40-02.SDR FDEA201307261670Skin · dentedLOWER FUSELAGE DENTED BS 510 BETWEEN STRINGERS 27-28L. FABRICATED, AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-00 AND SRM 53-00-01, REPAIR 16 FIG 201.SDR FDEA201306271408Line · leakingAFTER TAKE OFF PASSING 10K FT, LEFT HYD QTY LT ILLUMINATED, SHORTLY FOLLOWING THE LEFT HYD SYS PRESSURE LIGHT ILLUMINATED SYS QTY & SYS PRESSURE BOTH WENT TO ZERO. R & R RT MAIN GEAR DOWNLOCK ACTUATOR HYD LINE IAW AMM 32-32-02-04. UNABLE TO LEAK CHECK, DUESDR FDEA201306131272Unknown · unknownLEFT FWD ENTRY DOOR, WHEN SAFETIED AFTER SHUTDOWN "KNUCKLE KNUCKER" DID NOT RELEASE. HANDLE WENT TO GREEN AREA AND SLIDE LIGHT WENT OUT. DOOR ARMING SLIDE/ GIRT BAR, OPS CHECKED NORMAL IAW MM 52-11-25-5.SDR FDEA201305151001Indicator · failedLEFT ENGINE EPR WAS SURGING OR - 0.10 EPR DURING T/O ROLL WITH AUTOTHROTTLES ENGAGED. REJECTED T/O AT 80 KNOTS. R & R FFG CONTINUED AND ENGINE WAS REMOVED FOR THIS PROBLEM.SDR FDEA201305100956Engine · surgesLEFT ENGINE EPR SURGED. .10 EPR DURING TAKE OFF ROLL WITH AUTOTHROTTLES ENGAGED. REJECTED TAKE OFF AT 80 KNOTS. PERFORMED IP/HP COMPRESSOR AIRFLOW CONTROL TEST MM REF 71-00-00-5-3 RAN ENGINES TO HIGH POWER AND LT ENGINE EPR WAS STEADY NO SURGING ACFT OK FOSDR FDEA201305090952Compressor · stalledAFTER TAKEOFF LT ENGINE BEGAN SURGING AND HAD A NOTICABLE THUMP LIKE A COMPRESSOR STALL. ALT 2000' AGL. POWER AT CLIMB, RETARDED THROTTLE RETURNED TO DEPARTURE. PERFORMED BORESCOPE OF NR 1 ENGINE LP, IP, HP, COMPRESSOR AND LP, IP, HP, TURBINE IAW AMM 72-0SDR FDEA201212174313Light · inoperativeRT EMERGENCY SLIDE LIGHT INOPERATIVE. R & R RT EMERGENCY SLIDE LIGHT IAW SMP, OPS NORMAL.SDR FDEA201212164311Light · inoperativeRT SIDE EMERGENCY EXTERIOR LIGHT INOPERATIVE. R & R RT EMERGENCY SLIDE LIGHT IAW SMP, OPS NORMAL.
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