N952FD
Service difficulty reports · 71
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 = 'N952FD' 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 = 'N952FD' 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 FDEA202309071552Unknown · unknownDURING APPROACH IN TO MEM, TE FLAP DISAGREE EICAS APPEARED AND FLAPS CEASED TO MOVE WHEN MOVING FLAP HANDLE TO FLAPS 25. ACCOMPLISHED THE QRH AND LANDED WITH FLAPS 20. ***EMERGENCY DECLARED*** FIM: 27-51-00-1 SDR FDEA202206021361Skin · corrodedRH PYLON BOLT HOLE #2 HAS DAMAGE INDICATION. CLEANED HOLE #2 BY REAMING TO .624 IAW SRM 51-40-05 AND EA # F-5730-T0368661 P1. PERFORMED ROTO-PROBE AT HOLE #2 IAW NTM 51-00-16. NO DAMAGE NOTED. WING- PLATES AND SKINS-RH WING, UPPER SKIN AND DRAG FITTING, HOSDR FDEA202206011355Frame · crackedBS 1640 FUSELAGE FRAME WEB AT STRINGER S-14L HAS CRACK INDICATION NOTED, IN TOP INBOARD AND OUTBOARD HOLES AND BOTTOM OUTBOARD HOLE. COMPLIED WITH EA # F-5310-T0368467 P1 "FUSELAGE-MAINFRAME-FRAME 1640 AT S-14L HAS A CRACK INDICATIONS-REPAIR" MAJOR RESDR FDEA202012313224Slide · inoperativeSLIDE RAFT DEPLOYED UPON GROUND OPENING L1 DOOR FROM THE OUTSIDE. REMOVED AND REPLACED L-1 DOOR SLIDE, IAW AMM 52-11-25-5. STILL REQUIRES GIRT BAR RIG/ADJUSTMENT AND OPERATIONS CHECK. REMOVED AND INSTALLED NEW GIRT BAR ASSEMBLY ON L1 DOOR SLIDE FOR BINDING SDR FDEA202011052808Compressor · corroded`#2 ENGINE COMPRESSOR CASING FWD MOST FRAME FLANGE HAS AREAS OF CORROSION AROUND THE REMOVED #2 ENGINE REF WORK CARD # 7180260-02-01 SEQ #172 AND REPLACED ENGINE REF WORK CARD # 7180260-02-02 SEQ # 173SDR FDEA2020051510870Skin · crackedR/H WING # 9 SLAT LOWER COVE PANEL SKIN HAS A CRACK AT WS 594. REMOVED AND REINSTALLED #9 LEADING EDGE SLAT IAW B757 AMM 27-81-02-4, FABRICATED AND INSTALLED LOWER COVE PANEL IAW B757 SRM 51-40-02-06 AND B, DWGS. 114N4003, REV. E AND REV. B, B DWG : 114NSDR FDEA2020050410870Skin · crackedR/H WING # 9 SLAT LOWER COVE PANEL SKIN HAS CRACK AT WS 594.SDR FDEA2020051390839Filler · corrodedCORROSION FORWARD WET AREA STA 375 LBL 20 FLOOR SUPPORT CORRIER AREA. REMOVED CORROSION FWD WET AREA STA 375 LBL 20 FILLER IAW B 757 SRM 51-10-02-OG ORIGINAL MATERIAL .071",MAT REM .058",MAT LOSS .013" FOUND TO BE OUT OF LIMITS IAW B 75 757 SRM 53-00-51-1SDR FDEA202004300839Filler · corrodedCORROSION FORWARD WET AREA STA 375 LBL 20 FLOOR SUPPORT CORRIER AREA. REMOVED CORROSION FWD WET AREA STA 375 LBL 20 FILLER IAW B 757 SRM 51-10-02-OG ORIGINAL MATERIAL .071",MAT REM .058",MAT LOSS .013" FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-00-51-1A FISDR FDEA2020043080816Frame · crackedFWD CARGO PIT-R/H SIDE,FRAME 846 AT STR 22 RT. CRACKED AT FASTENER HOLE. REMOVED,FABRICATED AND INSTALLED STANCHION STUB (FRAME) ON FWD CARGO PIT R/H SIDE AT STA 846 BETWEEN STR-21R TO STR-26R IAW B 757 SRM 51-40-02-OG AND B. DWG : 143N5811, REV : - , RESDR FDEA2019032760720Charger · no testDURING POST FLIGHT MX WALKAROUND FOUND THE INTERIOR EMERGENCY EXIT LIGHT ABOVE THE L1 DOOR INOP. REPLACED BATTERY CHARGER CPN 3311913 AND BATTERY CPN 3301128 IN POS M731, EMERGENCY LIGHT ABOVE L1 SDR FDEA2019032760719Charger · no testDURING POST FLIGHT MX WALKAROUND FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP AFT OF THE L1 DOOR . REPLACED BATTERY CHARGER CPN 3311913 AND BATTERY CPN 3301128 POS M731, EMERGENCY LIGHT AFT OF L1 SDR FDEA201902190451Unknown · odorAT FL 340, AIRCREW SMELLED A STRONG PUNGENT ODOR COMING FROM VENTS. IT WAS STRONG BUT NOT QUITE STRONG ENOUGH TO GO ON OXYGEN. RAN PACKS FOR 30 MINUTES AT MAX HEAT. NO UNUSUAL ODORS NOTED THROUGHOUT MAIN CARGO COMPARTMENT AND IN FLIGHT DECK. RAN BOTH ENG AT MSDR FDEA2018120653432Warning Message · false activationPDIS 952 52-10 5943 05DEC18 MEM FACT U LOGPAGES:2924671 MOMENTARY LEFT FORWARD ENTRY DOOR EICAS DURING CRUISE AT FL 360 PRESURIZATION NORMAL. FACT 05DEC18 05:50 MEM U COMPLIED WITH FIM 52-11 FAULT TREE 802. NO VISUAL DEFECTS NOTED. OPERATSDR FDEA201811173269Static Line · out of positionRIGHT DOOR DISARM LIGHT WILL NOT COME ON. IT INITIALLY CAME ON, BUT NOW IT STAYS OUT. DOOR DIDNT FEEL NORMAL DURING DISARM. REMOVED R1 DOOR SLIDE COVER. FOUND SLIDE STATIC LINE SQUARE KNOT INTERFERANCE WITH GIRT BAR HANDLING MECHANISM AT FORWARD GIRSDR FDEA2018051571183Skin · dentedLARGE DENT ON TOP OF THE NR 8 SLAT WEDGE. REPAIRED THE SLAT WEDGE IAW SRM 57-43-02-2R, FIG 201, AND SRM 51-70-10-2R, REPAIR 3 AND 4, SRM 51-70-10-2R, PARAGRAPH 20, AND EA F-5750-T0339954 P1.SDR FDEA201804040852Transmitter · failedAT 13000 FT AND 220 KNOTS, CALLED FOR FLAPS 1. RECEIVED A TE FLAP ASYM ON EICAS. RECEIVED TRAILING EDGE LIGHT ON THE PANEL, FLAP ASYM OCCURRED BETWEEN FLAPS UP AND FLAPS 1 INDICATION. COMPLETED QRH AND CONTINUED TO LANDING. ACCOMPLISHED FIM 27-51 FAULTSDR FDEA201711073188Rope · exposedDOOR L1 HAD A PIECE OF EQUIPMENT EXPOSED AFTER CLOSING. RAMP PERSONNEL HAD US RE-OPEN DOOR TO SECURE. CALLED MX. SECURED DOOR SLIDE ROPE AND SLIDE COVER REF MM CH. 25-66-01-4. OK TO CONTINUE. OPS CHECKED NORMAL.SDR FDEA201710162966Battery Pack · inoperativeR1 INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE M730 POWER SUPPLY BATTERY PACK IAW AMM 33-51-07-2, OPS CHECKED GOOD.SDR FDEA201705181454Plug · detachedAT FL 350, THE RT ENG OIL PRESSURE ALERT ACTIVATED. OIL QTY RAPIDLY DECREASED TO ZERO. WINDMILLED FOR 30 MINUTES. FOUND THE ENGINE CUP PLUG HAD FALLEN OUT OF THE HIGH SPEED GEARBOX REINSTALLED THE PLUG, SERVICED OIL TANK, INSPECTED CHIP DETECTORS, NO MSDR FDEA201703090826Guard · brokenL1 DOOR EMERGENCY LIGHT TEST SWITCH GUARD IS MISSING. TEST SWITCH OPS NORMAL. PLASTIC FLANGE ON SWITCH IS BROKEN AND WILL NOT REMAIN FASTENED IN PLACE. WHILE TESTING THE LIGHTS THE SWITCH FELL DOWN IN BEHIND THE SIDEWALL LINER. REMOVED AND REPLACED THE SDR FDEA201612294576Cover · damagedCAPTAIN`S SIDE ESCAPE ROPE COVER IS BROKEN AND LOWER LATCH HAS COME OFF. REPLACED THE ACCESS COVER IAW MM 25-61-00-0-0 PARA 2A1.SDR FDEA201612094387Sensor · inoperativeSLIDE ARM LIGHTS INOP BOTH ENTRY DOORS. T/S PER FIM 25-66 TASK 802. R&R S10216 PROX SENSOR A AND S10217 PROX SENSOR B IAW AMM CH 25-66-11-2. BOTH R1 AND L1 SLIDE LIGHTS OPS CHECKS GOOD. MEL REMOVED.SDR FDEA201610133611Unknown · odorAPPROXIMATELY 20 MINUTES BEFORE COMMENCING DESCENT, A FAIRLY STRONG SMOKE ODOR OCCURRED WHICH SEEMED ELECTRICAL IN NATURE. DONNED OXYGEN MASKS AND STARTED QRH SEARCH. DID A SNIFF TEST AFTER A COUPLE MINUTES AND THE ODOR HAD DISSIPATED. CONTINUED FLIGHTSDR FDEA201608222955Unknown · odorPASSING F360 NOTICED ELECTRICAL SMELL. PER CHECKLIST, SHUTOFF UTILITY BUSSES AND RESIRC FAN. SMELL DISAPPEARED AND PER CHECKLIST CONTINUED TO DESTINATION. PERFORMED EXAMINATION OF THE LT AIR RECIRCULATION FAN FILTERS NORMAL PER AMM 21-25-02-4. ALSO PERFORSDR FDEA201608072831Blower · failedF/O EVAS BLOWER MOTOR TEST FAILED IAW WC F-2560-E0323178 A, P2, STEP 2. RT EVAS UNIT TEST PROCEDURES, RELEASED FOR SERVICE IAW MEL: 25-60-01, CATEGORY: D, EXPIRATION: 02DEC16, MEL 25-60-01. F/O EVAS UNIT REPLACED PER AMM 25-62-00-4. PERFORMED BLOWER ND BATSDR FDEA201607072310Lifter · brokenL1 DOOR VERY HARD TO DISARM AND ARM. ALSO DIFFICULT TO OPEN & CLOSE. FOUND THE GIRT BAR STRIKE BRACKET BROKEN. R & R THE BROKEN L1 DOOR GIRT BAR LIFTER, 140N2754-9 AND PERFORMED DOOR GIRT BAR MECHANISM TEST IAW AMM52-11-25-5, SATISFIED. DMI CLEARED AND STISDR FDEA201605141586Pump · malfunctionedFLIGHT TEST FTAM 4-66, RT ENG SHUTDOWN & RE-LIGHT FL 220 AIRSPEED 300KTS. AFTER THE NORMAL SHUTDOWN OF THE RT ENG, RELIGHT WAS ATTEMPTED. WHEN THE RT FUEL CONTROL SWITCH WAS POSITIONED FROM CUT OFF TO RUN THE SPAR, VLV OPEN & THE ENG VLV ON THE RT ENG DID NOSDR FDEA201605061486Splice Plate · damagedRIGHT ENG PYLON AFT OTBD ENG MOUNT BRACKET HAS A DING. REMOVED RT ENGINE SPLICE PLATE IAW B757 SRM 51-40-02. FABRICATED NEW SPLICE PLATE IAW SRM 51-40-05 AND 51-40-08. INSTALLED NEW SPLICE PLATE IAW SRM 51-40-02. PART MARKED IWA GMM 7-0-1001-1 PAR 7SDR FDEA201507202290Latch · defectivePARTS FELL OFF CAPTAIN`S ESCAPE ROPE HATCH DURING PREFLIGHT. REINSTALLED LATCH COMPONENTS, HATCH LOCKED INTO PLACE. OK FOR SERVICE. MM 25-61-00-4.SDR FDEA201506031690Collar · wornYELLOW DOOR LOCK RELEASE ON LT ENTRY DOOR IS VERY HARD TO LIFT UP WHEN CLOSING DOOR. R & R OPEN LOCK COLLAR IAW AMM 52-11-08-8. OPERATIONS CHECKED GOOD.SDR FDEA201501160205Light · intermittentSLIDE LIGHT ON DOOR IR ILLUMINATED INTERMITTENTLY THROUGH FLIGHT. REPLACE BULBS IAW MM 33-16-02-2. OPERATIONS CHECKED GOOD.SDR FDEA201412304220Light · inoperativeR1 DOOR SLIDE LIGHT INOPERATIVE. SUSPECT BAD BULB. RELAMPED LIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-13-00-2.SDR FDEA201411023454Reservoir · unknownL1 DOOR EMER POWER RESERVOIR ASSEMBLY NEEDS TO BE REPLACED. R & R L1 DOOR EMER POWER RESERVOIR IAW AMM 52-11-30-4.SDR FDEA201304280880Bottle · out of positionDOOR ASSIST RESERVIOR GAUGE FACES IN THE UPWARD DIRECTION REQUIRING USE OF A MIRROR TO VIEW BOTTLE PRESSURE. R & R R1 EMERGENCY POWER RESERVOIR IAW AMM 52-11-30-4. ACFT OK FOR SERVICE.SDR FDEA201303070509Door · out of adjustLEFT CREW ENTRY DOOR VERY HARD TO CLOSE. INSPECTED DOOR FOR ADJUSTMENT. DOOR OPERATES NORMAL IAW MM 52-11-00-5.SDR FDEA201206282388Lamp · inoperativeR1 DOOR SLIDE ILLUMINATION LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.SDR FDEA201204231523Skin · dentedRIGHT SKIN DENTED AT BS 720 -740, STR 27. REPAIR CARRIED OUT AS PER EA F-5330-158041 PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201204191491Strap · mismanufacturedHORIZONTAL STAB LEFT SIDE LOWER SURFACE PIVOT PIN RETAINING STRAP HAS CORROSION DUE WRONG MATERIAL USED. REWORKED STRAP. REMOVED AND FABRICATED NEW RETAINING STRAP IAW DWG 182N1608, SHEET 1 REV A AND INSTALLED IAW DWG 182N1601, SHEET 2, REV. REPAIR IS CLASSDR FDEA201204191490Strap · mismanufacturedHORIZONTAL STAB RT SIDE LOWER SURFACE PIVOT PIN RETAINING STRAP HAS CORROSION DUE WRONG MATERIAL USED. REWORKED OF RETAING STRAP. STRAP REMOVED. NEW STRAP FABRICATED IAW DWG 182N1608, SHEET 1, REV A AND INSTALLED IAW DWG 182N1601, SHEET 2, REV. REPAIR IS CSDR FDEA201204021221Support · chafedFOUND KNIFE EDGE CHAFING ON LOWER END OF SUPPORT ON VERTICAL STAB. R & R WITH FAIRING SUPPORT FABRICIATED IAW DWG 173N1300-3, SHT 1, REV B AND INSTALLED IAW DWG 173N1300 SHT 1, REV B. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201204021218Skin · corrodedAFTER REMOVAL OF TCAS ANTENNA FOUND CORROSION ON SKIN AT BS 420-440 AT STRINGER 28L TO 28R. REPAIRED IAW DWG 143N3003-2, SHT 1, REV C AND DWG 143N3400, SHT 21, REV B. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201203301198Floor Skin · corrodedCABIN DECK PLATE AT BS 1717, RBL 14 TO RBL 14.5 CORRODED. REPAIR CARRIED OUT IAW SRM 53-60-51, REPAIR 2 FIG 201, REV 105. REPAIR IS CLASSIFIED MAJOR.SDR FDEA201203281157Angle · corrodedRT SIDE APU DOOR CUT OUT AREA THE ANGLE THAT THE NUTPLATES ARE ATTACHED TO ALONG STRINGER 2R IS CORRODED. REMOVED, FABRICATED IAW DWG 148N3152-2, SHT 1, REV- AND INSTALLED IAW SRM 51-40-02, REV 105 AND DWG 148N3105, SHT 1, REV C. REPAIR IS CLASSIFIED AS MAJOSDR FDEA201203271131Strap · corrodedRIGHT SIDE OF APU DOOR CUTOUT AREA, BS 1825 THE APU INLET STRAP CORRODED. CORRODED STRAP REMOVED. STRAP FABRICATED IAW DWG 148N3138-8000 SHT 1, REV C, AND INSTALLED IAW DWG 148N3105, SHT 1, REV C. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201203261103Attach Angle · corrodedRT SIDE APU INLET CUTOUT, AFTER THE APU INLET REMOVAL FOUND THE INLET ATTACH ANGLE FROM STA 1793 -1825 HAS CORROSION AT STRINGER 6, RT. CORRODED RT APU INLET CUTOUT ATTACHMENT ANGLE REMOVED. REPLACED WITH ANGLE FABRICATED IAW DWG 148N3152-1, SHT 1, REV A SDR FDEA201203261102Splice Plate · corrodedAPU DOOR CUT OUT AREA, RT SIDE. NUTPLATES ALONG THE FWD EDGE ARE CORRODED JUST AFT OF BS 1787 BULKHEAD FRAME. CORRODED SPLICE PLATE R & R IAW SRM 51-40-02, REV 105 AND DWG 148N3105, SH 1REV C. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201203261097Skin · scratchedFUSELAGE SKIN, UNDER SHORING BS 540 - 560 BETWEEN STR 26L - 26R HAS SCRATCHES. SKIN REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 16, REV 105. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201203261096Skin · scratchedFUSELAGE SKIN UNDER SHORING BS 500 -520 BETWEEN STR 26L - 26R HAS SCRATCHES. DAMAGED SKIN REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 16, REV. 105. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201203221059Rib · corrodedLEFT WING INBD T/E MAIN FLAP INBD TORQUE TUBE SUPPORT RIB LOWER AREA FOUND CORROSION. REPAIR CARRIED OUT IAW EA F-5750-158016. REPAIR IS CLASSIFIED AS MAJOR.
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