N963FD
Service difficulty reports · 122
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 = 'N963FD' 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 = 'N963FD' 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 FDEA202608281246Window · arcedAFTER INITIATING DESCENT FROM FL300, WITH PRESENCE OF ST. ELMO S FIRE, L1 WINDOW ARCING OCCURRED FOLLOWED BY SHATTERING. QRH ACTIONED AND EMERGENCY DECLARED. REMOVED AND REPLACED L1 WINDSHIELD IAW AMM 56-11-01-4-0 SECTION E, STEP 13, FIRST TORQUE APPLIED SECSDR FDEA202606100692Holder · inoperativeL1 DOOR EMERGENCY EXIT LIGHT AND SLIDE LIGHT WILL NOT TEST. A/C HAS BEEN POWERED FOR ALMOST 3 HOURS, NO HELP. REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT POWER SUPPLY M731. RADIANT POWER CORP, MPN 2013-1A, MSN 111794 POWER SUPPLY REMOVED. OPS CHECKS GOSDR FDEA202605050558Light · no discrepancyFO SIDE SLIDE LIGHT INOP. PERFORMED OPERATIONAL TEST OF R1 GIRT BAR ENGAGED LIGHT, GIRT BAR ENGAGED WARNING LIGHT ILLUMINATES OVER SEVERAL CYCLES OF MODE SELECT LEVER.SDR FDEA202601050005Skin · crackedLEFT AFT FUSELAGE BS 1459-1461 (02EA) FASTENERS AFT OF BUTT SEAM BS 1459 ABOVE STR 20 AND DOUBLER THAT HAVE (02) POSSIBLE CRACKS INDICATION UNDER FASTENERS RUNNING PARALLEL OF THE DOUBLER DURING NDT HFEC INSPECTION COMPLIED WITH EA # F5330-T0385962 TITTLESDR FDEA202601030003Repair · not reportedEXISTING REPAIR FOUND AT # 2 CARGO DOOR AFT LOWER CORNER CUTOUT AREA COMPLIED WITH EA # F-5330-T0305556 B TITLE: FUSELAGE PLATES & SKINS - REPLACEMENT OF EXISTING STA 1440 FUSELAGE SKIN REPAIR AT 24R-25R (# 2 CARGO DOOR OPENING)SDR FDEA202512292294Stringer · corrodedAFT CARGO COMPARTMENT, DURING REMOVAL OF PRODUCTION STRINGER SPLICE TO GAIN ACCESS FOR STRINGER REPAIR FOUND STRINGER 21L, BS 1460 - 1465 EXFOLIATED. REPAIRED THE STRINGER IAW SRM 53-00-03-2R, REPAIR 2, FIG 201, DETAIL I, SHEET 6, AND SRM 51-40-02-OG.SDR FDEA202512292293Stringer · crackedAFTER DVI OF THE LAPPED AND OVERLAPPING SKIN UNDERNEATH OF THE EXISTING REPAIR DOUBLER BETWEEN BS 1430 TO BS 1475, STR 20L TO STR 21L FOUND STRINGER 21L CRACKED AT BS 1454. REPAIRED STRINGER 21L BETWEEN STA 1426 TO STA 1456 IAW B 757 SRM 53-00-03-2R REPAIR SDR FDEA202512262290Fitting · looseNR 1 ENGINE NACELLE STRUT R/H SIDE AFTER. HINGE FITTING BOLT HEAD BROKEN OFF. REMOVED AND REPLACED BOLT AT NO 1 ENGINE NACELLE STRUT R/H SIDE AFT. HINGE FITTING IAW SRM 51-40-02-0G AND E.A # F-5440-T0385898 P1.SDR FDEA202512232285Floor Support · damagedAFT CARGO COMPARTMENT STRINGER AT B.S. 1260 LBL 10.45 WITH SEVERAL PERFORATIONS (MISDRILLED) AFT CARGO COMPARTMENT STRINGER AT BS.1260 LBL 10.45 WAS REPAIRED IAW B757 SRM 53-00- 53-2R. REPAIR1.SDR FDEA202512212275Shear Plate · corrodedGALLEY AREA BS 375 BTW LBL 20.00 TO LBL 26.00 SHOW PLATE CORRODED. REMOVED AND REPLACED SHEAR PLATE SEAT TRACK SUPPORT (U CHANNEL) AND (2EA) FLEXURE ANGLE IAW VENTURA AEROSPACE DWG 3471 REV # B DWG 3480 REV # B AND BOEING DWG PL 141N5131 REV # V.SDR FDEA202512202272Stringer · corrodedAFT CARGO BAY, STRINGER 30 BTW BS 1440 TO 1460 FOUND CORRODED. REPAIRED THE STRINGER IAW SRM 53-00-03-2R, SRM 51-40-02-0G, & DWG 146N3110, REV B.SDR FDEA202512202271Shear Tie · corrodedAFT CARGO BAY, BS 1460 SHEAR TIE BTW STR-29L TO STR-30, FOUND CORRODED. REPLACED SHEAR TIE IAW SRM 51-40-02-0G, AND DWG 140N2002, REV C.SDR FDEA202512202270Shear Tie · corrodedLOWER HALF OF FUSELAGE BS 1460 BETWEEN S28L AND S29L HAS POSSIBLE CORROSION. REPLACED THE SHEAR TIE IAW SRM 51-40-02-0G, AND DWG 140N2002, REV C.SDR FDEA202512202269Stringer Splice · corrodedAFT CARGO COMPARTMENT BS 1460 SPLICE STRINGER 30 CORRODED. REPLACED SPLICE STRINGER LOCATED BS 1460 IAW SRM 51-40-02-0G, AND DWG 146N3820, REV C.SDR FDEA202512202268Stringer · corrodedAFT CARGO BAY, STRINGER 30L BTW BS 1460 - 1480, FOUND CORRODED. REPAIRED THE STRINGER IAW SRM 51-40-02-0G, & DWG 146N3110, REV C.SDR FDEA202512202267Stringer Splice · corrodedAFT CARGO BAY, BS 1460 STRINGER SPLICE 29L CORRODED. REPLACED THE STRINGER SPLICE IAW SRM 51-40-02-0G, DWG 146N3820, REV C.SDR FDEA202512202266Stringer · corrodedAFT CARGO BAY STRINGER 29L BTW BS 1460 TO 1480, FOUND CORRODED. REPAIRED THE STRINGER IAW SRM 51-40-020-G, AND DWG 146N3110, REV B.SDR FDEA202512202265Skin Panel · crackedRIGHT WING OTBD LEADING EDGE SLAT NR 10 INTERNAL LOWER MAIN TRACK SLAT HAS POSSIBLE CRACKED. REMOVED DAMAGED COVE SKIN AT RT WING OTBD LEADING EDGE SLAT 10 IAW SRM 51-40-02-0G, AND INSTALLED NEW FORMED COVE SKIN IAW B. DRAWING 114N4075 REV -, AND PL 114N40SDR FDEA202512182261Stringer · corrodedBULK AREA BETWEEN STA 1700 TO 1720 STR 23L CORRODED ACCOMPLISHED REPAIR ON STRINGER BTW STA 1685 TO STR 1720 IAW B757 SRM 53-00-03-2R, 51- 40-02-0GSDR FDEA202512112236Seat Track · corrodedMAIN CABIN SEAT TRACK BETWEEN BS 900 TO BS 1180.0 LBL 58.22 HAS MULTIPLE SPOTS WITH CORROSION. REMOVED AND EVALUATED MAIN CABIN SEAT TRACK BTW BS 900-1180, LBL 58.22 FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52-1A, DETAIL V, 51-40-02-0G. TRIMMED, LOCATED AND DRSDR FDEA202510172049Pitot Tube · failedSTARTED TAKEOFF. POWER WAS SET. SHORTLY THEREAFTER BETWEEN 30 AND 40 KNOTS, RECEIVED ABOUT 3 TO 5 CAS MESSAGES. AUTOTHROTTLE DISCONNECT, SOME PROBE WARNING AND A COUPLE OTHERS THAT WE CAN`T RECALL. REJECT WAS INITIATED AROUND 40 KNOTS AND THE MESSAGES DISAPPSDR FDEA202505100745Slide · failedRAMP PERSONNEL OPENED L1 AFTER DOORS WERE ARMED AND THE SLIDE FELL OUT OF THE DOOR WITHOUT INFLATING. L1 DOOR ASSIST BOTTLE BLOWN, SLIDE DID NOT DEPLOY. REPLACED THE L-1 EMERGENCY POWER RESERVOIR AND THE L1 SLIDE ASSYSDR FDEA202503210469Computer · faultedMADE 2 TAKEOFF ATTEMPTS , MAX POWER FOR WIND SHEAR, EACH TIME REJECTED TAKEOFF DUE TO AIRCRAFT VEERING TO THE RIGHT OF CENTERLINE. NO EICAS MESSAGES OR WARNINGS RECEIVED. ENGINES APPEARED TO SPOOL UP NEARLY EVEN. RAN QRH REJECTED TAKEOFF AND AFTER LANDINGSDR FDEA202307071182Unknown · unknownWITH OUR BEACON ON, A MECHANIC OPENED L FWD ENT DOOR FROM OUTSIDE THE AIRCRAFT WHEN THE SLIDE WAS ARMED. THE SLIDE FELL OUT OF THE DOOR WITHOUT INFLATING. OLD SLIDE FOUND IN MAIN CARGO IN NET. REMOVED DOOR LINERS FROM DOOR, VERIFIED CORRECT OPS OF DOOR DSDR FDEA202206171458Hose · malfunctionedRIGHT ENGINE PROBLEM AT CRUISE. RIGHT EPR SHOWED MAX ON SCALE. FUEL FLOW APPRX 1/2 OF LEFT ENGINE. ALL RIGHT INSTRUMENTS WERE SIGNIFICANT THEN LEFT. HAD TO DESCEND FROM CRUISE F380 TO FL 320 TO HOLD AIRSPEED. HAD RIGHT SIGNIFICANT RIGHT THROTTLE VIBRATIONSDR FDEA202204120932Girt Bar · misalignedMDIS 963 52-10 7334 12APR22 PDX FACT U L-1 DOOR WILL NOT ARM FACT 12APR22 21:02 AFW U INSPECTED AND VERIFIED GIRT BAR ALLIGNMENT IN REF TO AMM 25-66-10-2. PERFORMED L1 DOOR GIRT BAR INSPECTION/CHECK IN REF TO AMM 25-66-10-2 SECTION 4. DOSDR FDEA202202160422Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR BEAM - UPPER CAP AFT FLANGE CRACKED, AT STA580, LBL45.5 COMPLIED WITH FEDEX EA: F-5310-T0367280 PT1, EA TITLE: FUSELAGE - MAINFRAME - STA 580 FLOOR BEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR- REPAIR DOCUMENTATION SDR FDEA202201260143Life Raft · damagedR1 DOOR WAS OPENED FROM THE OUTSIDE WHILE STILL ARMED, SLIDE FELL OFF OF DOOR RAR R1 SLIDE/RAFT, REF B757 AMM 25-66-01-4. NO DEFECTS NOTED AT THIS TIME. MEL ITEM RESTORED.SDR FDEA202110272644None · noneFOUND LIGHTING STRIKE DAMAGE TO SKIN 1.5" AFT OF STA 520 2.75" IB OF STR S29L WRITTEN ON WRI 53-00-6918 WORKED ON SEQ 5 UNDER W/O 81650 CARD WRITTEN FOR RDR/SDR. REPAIRED LIGHTING STRIKE DAMAGE TO SKIN 1.5" AFT OF STA 520 2.75" I/B OF STR S29L REF 757 SRM 5SDR FDEA202110272643None · noneFOUND LIGHTING STRIKE DAMAGE ON SECTION 43, ON STA 580, 4.5" IB OF STR 29R DAMAGE WRITTEN UP ON WRI 53-00-6925 REPAIR WORKED ON SEQ 6 W/O 81650. CARD WRITTEN FOR RDR/SRD REPAIRED LIGHTING STRIKE DAMAGE ON SECTION 43 ON STA 580 4.5" I/B OF STR 29R REF 757 SRMSDR FDEA202107071697Battery Pack · inoperativeRIGHT SIDE EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AND TESTED OK IAW AMM: 33-51-07-2-2.SDR FDEA202004300862Transition Panel · crackedBULK PIT AT BS 1550 & L/H TRANSITION PANEL PUNCHED (CRACKED). TRANSITION PANEL REPAIR ACCOMPLISHED IAW B757-200 SRM 53-00-53-2R REPAIR 2.SDR FDEA202004300860Access Panel · cracked#2 PYLON, OUTBOARD, HINGED PANEL 443AR, INNER SURFACE CRACKED. REPAIRED INNER SURFACE OF #2 PYLON, OUTBOARD, HINGED PANEL 443AR IAW B757 SRM 51- 70-17-0G RESTORED FINISH IAW B757 AMM 51-21-14 B757 AMM 51-21-15. MINOR REPAIRSDR FDEA2020043080815Seat Track · corrodedR/H SUPERNUMERARY SEAT TRACK CORRODED REMOVED AND REPLACED SEAT TRACK IAW VENTURA AEROSPACE DWG 3470 REV GSDR FDEA2020043080814Seat Track · corrodedL/H SUPERNUMERARY SEAT TRACK CORRODED REMOVED AND REPLACED SEAT TRACK IAW VENTURA AEROSPACE DWG 3470 REV GSDR FDEA202004260795Strap · gougedFUSELAGE EXTERIOR AFT CAGO DOOR CONTROL ANEL CUT OUT LOWER EDGE IS GOUGED ACCOMPLISHED BLEND REPAIR PER FEDEX EA F-5330-T0305556-P2SDR FDEA2020042760795Strap · gougedFUSELAGE EXTERIOR AFT CAGO DOOR CONTROL ANEL CUT OUT LOWER EDGE IS GOUGED ACCOMPLISHED BLEND REPAIR PER FEDEX EA F-5330-T0305556-P2SDR FDEA2020042760792Seal · cracked#2 EXHAUST NOZZLE 6 OCLOCK POSITION CASE DRAIN SUPPORT PLATE CRACKED REMOVED AND REPLACED SEAL PER B757 SRM 51-40-02-OG AND RR EIPC 78-11-04-03SDR FDEA2020042750785Filler · wornDURING AGING AIRCRAFT INSPECTION OF EXISTING REPAIR ON RIGHT WING OUTBOARD FLAP INBOARD LEADING EDGE SKIN FOUND FLUSH SKIN FILLER TO BE WORN REMOVED WORN FILLER IAW B757 SRM 51-40-02. FABRICATED AND INSTALLED NEW REPAIR FILLER IAW B757 SRM 57-53-01-2R REPASDR FDEA2020042740782Mount Bracket · crackedAILERON A2B CABLE PULLEY MOUNT BRACKET CRACKED AT STA 358 RBL25. STREAMER ATTACHED REMOVED, FABRICATED AND INSTALLED NEW STIFFENER, P/N 251N6133 IAW DWG 251N6133 REV B, EA # F-2710-T0353742-P1 FLIGHT CONTROLS-AILERON AND TABS-PULLEY BRACKET ASSY STA 345,SDR FDEA2020042310767Skin · dentedLOWER FUSELAGE EXTERNAL SKIN ,STA 1592.7 BETWEEN S22R-S23R DENTED REPAIRED PER B757 SRM 53-00-01-2R REPAIR 29SDR FDEA2018081402006Cover · damagedL1 DOOR SLIDE COVER DAMAGED. REPAIRED L1 DOOR SLIDE COVER IAW AMM 25-00-00-8. ACFT OK FOR SERVICE.SDR FDEA2018051871251Heater · failedAPPOACHING THE BEGINNING OF THE HITHR 2 RNAV, ARRIVAL AT 340 LIGHT SMOKE AND AN ELECRICAL BURNING ODOR WAS IMMEDIATELY NOTICED IN THE COCKPIT. THE SOURCE SEEMED TO ORIGINATE ON THE CAPTAIN`S SIDE AROUND THE CONTROL COLUMN. THE SMOKE AND ODOR SEEMED TO DISSAPSDR FDEA201804050858Stringer · damagedFOUND STRINGER 16L AT BS 1710 DAMAGED. CUT-OUT THE DAMAGED SECTION OF THE STRINGER, DRILLED A NEW STRINGER AND SPLICE. A REPAIR WAS INSTALLED IAW SRM 53-00-03-2R, REPAIR 2, TYPE I, DETAIL I, FIG 201.SDR FDEA201802220467Adc · failedAT APPROXIMATELY 7000 FT, LOST THE LT AIR DATA COMPUTER. SPEED TAPE, ALTITUDE, ALL INDICATIONS ON CAPTAIN`S SIDE, ROLLING ERRATICLY UP AND DOWN. DURING TROUBLESHOOTING FOUND THE LT AIR DATA COMPUTER FAULT BALL LATCHED. RETURNED CAPTAIN'S SOURCE SELECT SSDR FDEA201706061571Connector · damagedDURING DESCENT, LT ENGINE HYD PUMP EICAS MESSAGE DISPLAYED. TURNED OFF PUMP IAW QRH. PINNED THE NR 2 WIRE ON THE CONNECTOR IAW SWPM. DRY MOTORED THE NR 1 ENGINE IAW JRH. NO FAULTS FOUND, HYDRAULIC PRESSURE NORMAL. COMPLIED WITH PART 1 OF EA F-2930- T03335SDR FDEA201705021325Girt Bar · lack of lubeR1 DOOR WOULD NOT OPEN AT BLOCK IN. R1 DOOR GIRT BAR LOCK PLATES DIRTY AND DRY. LUBED GIRT BAR. OPS NORMAL.SDR FDEA201702170580Liner · out of positionWHILE ARMING THE RIGHT CREW ENTRY DOOR THE KNUCKLEBUSTER FAILED TO ARM IN THE CORRECT POSITION. REMAINED FLUSH WITH THE DOOR AND THE RED ARM WAS NOT VISIBLE. ADJUSTED LOWER DOOR LINING ON THE R1 DOOR IAW AMM 52-11-02-4. PERFORMED ADJUSTMENT TEST OF THE RSDR FDEA201609103187Light · intermittentBOTTOM ONE THIRD OF OVERHEAD PANEL LIGHTS WERE INTERMITTENT. REF WDM 23-71-11, 33-13-31 & CMM 23-70-43 CVR MPN 980-6116-002 DOES NOT CONTAIN CONTACTS FOR INTEGRAL PANEL LIGHTING.SDR FDEA201604211334Lock Sensor · failedAFTER TAKEOFF, RECEIVED GEAR DISAGREE EICAS ALERT. FOLLOWED CHECKLIST & PERFORMANCE TABLES & CONTINUED. DURING APPROACH WE EXTENDED GEAR EARLY AT APPROX 210 KTS. AT 170 KTS WE HEARD A CLUNK IN NOSE GEAR AREA. LANDING UNEVENTFUL, SWUNG GEAR & GOT LG MONITOR
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