N926FD
Service difficulty reports · 95
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 = 'N926FD' 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 = 'N926FD' 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 FDEA202304130639Unknown · unknownUPON SELECTING FLAPS 25, TE FLAP DISAGREE MESSAGE. COMPLIED WITH QRH. LANDED WITH FLAPS 20, LANDING SPEED 138. EMERGENCY DECLARED. ACCOMPLISHED FSEU BITE CHECKS AND FOUND FSEU 1 WITH A FLAP DISAGREE FAULT. INSPECTED TE FLAP SYSTEM AND FOUND L/H OUTBD FLASDR FDEA202208061907Connector · not seatedPDIS 926 27-50 0370 06AUG22 FAT OPEN U WHEN SELECTING FLAPS 25 FOR LANDING WE RECEIVED THE TE FLAP DISAGREE EICAS MESSAGE. WE INITIATED A GO AROUND, COMPLIED WITH THE CHECKLIST AND COMPLETED A FLAPS 20 LANDING. THE MESSAGE REMAINED UNTIL MSDR FDEA202204060880Collar · damagedON ARRIVAL FOUND R1 DOOR GUST LOCK BROKEN. COLLAR ASSY MPN: 654N0244-7 CPN: 5214377 QTY: 1 REMOVED AND REPLACED R1 DOOR GUST LOCK DOOR HOLD OPEN COLLAR WITH ANOTHER PART FROM STOCK AND IT FIT ALL OPSSDR FDEA202203260700None · unknownTE FLAP DISAGREE ON FINAL. QRH COMPLIED WITH. PERFORMED BITE OF ALL 3 FSEU'S FOUND NO CURRENT FAULTS. ATTEMPTED TO DUPLICATE FAULT, OPERATED FLAP/SLATS FROM FAIRED TO 40 UNITS SEVERAL TIMES COULD NOT RECREATE FAULT. SUSPECT FLAP LEVER OUT OF DETENT FORSDR FDEA202108202048Frame · damagedREPAIR INSTRUCTIONS REQUIRED FOR THE ACCOMPLISHMENT OF FEDEX E.A. F-5310-147693, PART 10, SPLICE REPAIR AT STA 1640, S9R TO S20R COMPLIED WITH E.A F-5310-147693 BS 1640 FRAME I-9F - S-20R, FRAME SPLICESDR FDEA202108112001Skin · dentedFUSELAGE SKIN @ STA 1730, BETWEEN STR 29L - STR 29R, HAS 2EA DENTS. REPAIRED SKIN IAW FEDEX EA # F-5330-146539-P3SDR FDEA202105081161Line · leakingA SLOW LOSS OF RIGHT HYDRAULIC SYSTEM FLUID LED TO RIGHT HYDRAULIC SYSTEM FAILURE. COMPLIED WITH QRH, DECLARED AN EMERGENCY. AIRCRAFT WAS AIRBORNE FOR APPROXIMATELY 7-10 MINUTES AFTER RECEIVING THE HYDRAULIC SYSTEM FAILURE INDICATIONS. INSTALLED PRESSURESDR FDEA202103090608Drive Unit · failedWHEN CONFIGURING TO LAND AT SLC IT WAS VERY DIFFICULT TO MOVE FLAP LEVER FROM 20 TO 25 DETENT. WHEN I FINALLY WAS ABLE TO MOVE FLAP LEVER TO 25, WE RECEIVED A TE FLAP DISAGREE EICAS AND LIGHT. FOLLOWED QRH. EMERGENCY DECLARER. FACT 09MAR21 15:45 SLC U SDR FDEA202101290236Actuator · inoperativeMAIN CARGO DOOR WILL NOT CLOSE. FOUND BOTH LINKS ON AFT MAIN CARGO DOOR ACTUATOR BROKEN. RAISED CARGO DOOR WITH SLING REF B757 AMM CH 52-32-00-4 SO CARGO COULD BE OFFLOADED. REMOVED, REPLACED MAIN CARGO DOOR FWD ACTUATOR SUPPORT LINK ASSY, REF EO F-5230-E03SDR FDEA202012063050Skin · damagedLOWER FUSELAGE SKINS BETWEEN STA 1540 AND STA 1640 STRINGERS S-30 TO S-26L HAS NUMEROUS PLACES OF DAMAGE. COMPLIED WITH EA F-5330-T0358203 TITLED: FUSELAGE-SECTION 46 LOWER SECTION-REPAIR OF FUSELAGE SKIN INPACT DAMAGE AT STA 1624; S-29L AND EA F-5330-T035820SDR FDEA202012063049Strap · damagedAFT CARGO COMPARTMENT FUSELAGE CIRCUMFERENTIAL STRAP AT STA 1620 FROM STRINGER S-28L TO S-29R PUNCTURED, DEFORMED WITH SURFACE CORROSION. REMOVED AND REPLACED CIRCUMFERENTIAL SPLICE STA 1620 S-27L TO S27R, IAW SRM 51-40-02 AND DWG 146N3810. MAJOR REPAIR.SDR FDEA202012063048Stringer Clip · damagedAFT CARGO COMPARTMENT STRINGER CLIP AT S30 STA 1616 TO STA 1623 SEPARTED FROM SKIN AND HAS SHEARED FASTENERS AND SURFACE CORROSION. REMOVED AND REPLACED SPLICE STA 1616 TO STA 1623 S-30, IAW SRM 51-40-02 AND DWG 146N3821. MAJOR REPAIR.SDR FDEA202012063047Stringer Splice · damagedAFT CARGO COMPARTMENT STRINGER S-29L STRINGER SPLICE AT STA 1620 PUNCTURED AND STRINGER FROM STA 1623 TO STA 1630 DEFORMED. REMOVED AND REPLACED STRINGER SPLICE AT STA 1620 S-29L, IAW SRM 51-40-02 AND DWG 146N3820. FOUND STRINGER NOT TO BE DEFORMED IT WAS PRSDR FDEA202012053034Stringer · bentAFT CARGO COMPARTMENT STRINGER S-27L BETWEEN STA 1588 TO STA 1600 BENT AND DEFORMED. REPAIRED STRINGER S-27L AT STA 1570, IAW SRM 53-00-03-2R. REPAIR BETWEEN STA 1570-STA 1620. MAJOR REPAIR.SDR FDEA202012043030Skin · damagedFUSELAGE SKIN HAS DENT AND CREASE DAMAGE BETWEEN STA 1520 AND STA 1540 STRAINGERS S-25L TO S-26L. COMPLIED WITH EA F-5330-T0358196 PART 1 TITLE: FUSELAGE-SECTION 46 LOWER SECTION REPAIR OF FUSELAGE SKIN INPACT DAMAGE AT STA 1520-1540 S-26L. MAJOR REPAIR.SDR FDEA202012043029Shear Tie · crackedAFT CARGO COMPARTMENT SHEAR TIE AT STA 1600 STRINGER S-27L TO S-28L SHEARED/CRACKED. REMOVED AND REPLACED SHEAR TIE STA 1600 S-27L TO S-28L, IAW SRM 51-40-02. FABED ON VTMAE TRAVELER T20/1524173 AND DRAWING 140N2002. MAJOR REPAIR.SDR FDEA202012043028Shear Tie · crackedAFT CARGO COMPARTMENT SHEAR TIE AT STA 1620 FROM STRINGER S-28L TO S-29L SHEARED, CRACKED. REMOVED AND REPLACED SHEAR TIE STA 1620 S-28L TO S-29L, IAW SRM 51-40-02. FABED SHEAR TIE ON VT MAE TRAVELER T20/1524174. PART MARKED AS FX-140N2002-248, IAW GMM 7-0-SDR FDEA202012043027Shear Tie · bentAFT CARGO COMPARTMENT SHEAR TIE AT STRINGER S-29L TO S-30 DEFORMED WITH SURFACE CORROSION. REMOVED AND REPLACED SHEAR TIE, IAW SRM 51-40-02. FABED ON VTMAE TRAVELER T20/1525019 STA 1620 AND DRAWING 140N2002. MAJOR REPAIR.SDR FDEA202007171565Crease Beam · corrodedMAIN DECK, BS 765 RT INBD CREASE BEAM WAS CORRODED. REMOVED THE CORROSION IAW SRM 51-10-02. EVALUATED 100% MATERIAL LOSS, AND OUT OF LIMITS IAW SRM 53-30-13, FIG 101. REPAIRED THE CREASE BEAM IAW SRM 53-00-13-2R, REP 1, ALT 1.SDR FDEA2020030970501Unknown · malfunctionedPDIS 926 27-50 8236 07MAR20 RNO FACT U LOGPAGES:3215684 EXTENDING FLAPS FROM 15*- 20* RECEIVED TE FLAP DISAGREE CAUTIN MESSAGE. FLAPS STOPPED MOVING AT 17*. COMPLIED WITH QRH, LANDED UNEVENTFULLY. FACT 07MAR20 14:20 RNO U RETURNED A/C BACSDR FDEA202001110158Skin · damagedTHE LH SIDE OF THE FUSELAGE FROM STA 510-515 2"-4" DOWN FROM STR 26L HAS SEVERAL DEEP PITS FROM LIGHTNING STRIKE. REPAIRED DAMAGE IN FUSELAGE SKIN CAUSED BY LIGHTNING STRIKE. INSTALLED DOUBLER REPAIR PER EA F-5330- T0351859.SDR FDEA201907251695Frame · crackedFORWARD CARGO COMPARTMENT, BS 740 JUST ABOVE STRINGER 22R FRAME IS CRACKED AT TOOLING HOLE. VERIFIED BY HFEC (OPEN HOLE) INSPECTION, CIRCLED HOLE IN BLACK.SDR FDEA201907241678Door · crackedPOSSIBLE CRACK ON L2 DOOR UPPER HINGE CUTOUT ALL WORK ACCOMPLISHED IAW EA F-5210-T0348085 P1 DOORS - PASSENGER/CREW - CARGO - L -2 DOOR FORWARD FRAME UPPER HINGE CUT-OUT SRM REPAIR - RSC TRACKING.SDR FDEA201907231668Filler · corrodedAFT CARGO COMPT STA 1440 AT STR 29R TAPERED FILLER ON STRINGER HAS EXFOLIATING CORROSION. FOUND TAPERED FILLER AT STA 1440 STR 29R OUT OF LIMITS DUE TO 100% MATERIAL LOSS IAW SRM 53-00-03-1A FIG 101. FABRICATED NEW TAPERED FILLER IAW DWG 146N3821 REV P AND REVSDR FDEA201907111527Stringer · corrodedAFT PIT - BS 1440, STR. 29 RT HAS CORROSION ON I/B SIDE.SDR FDEA201907101520Seat Track · corrodedMAIN CABIN BETWEEN STA 1180-1200 LBL44.5 SEAT TRACK FANGE CORRODED EVALUATED SEAT TRACK STA 1180-1200 LBL 44.5 ORIG MAT .070 REM .00 LOSS .070 OUT OF LIMITS IAW SRM 53-00-52-1A FIG 101. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SEAT TRACK IAW SRM 51-40-02,SDR FDEA201907101519Seat Track · corrodedMAIN CABIN BETWEEN STA 1040-1055 BLO CORROSION ON SEAT TRACK FLANGE. REMOVED CORR ON SEAT TRACK (FLANGE) SUPPORT STA 1040-1055 BL0 IAW SRM 51-10- 02. ORIG MAT.070 REM .054 LOSS .016 OUT OF LIMITS IAW SRM 53-00-52 FIG 101. REMOVED, LOCATED, DRILLED, TRIMMED ANSDR FDEA201907101521Seat Track · corrodedMAIN CABIN STA 1195 BL0 SEAT TRACK FLANGE CORRODED.SDR FDEA201907091513Skin · dentedLT FUSELAGE OUTER SKIN AT FS 215 AROUND S-21L HAS A DENT. EVALUATED DENT ON SKIN STA. 215 AROUND S-21L A\Y FOUND TO BE IN LIMITS IAW SRM 53-00-01-1A. HFEC IAW NDTM PT6 51-00-19 CRACK NOTED. CUT OUT DAMAGED AREA, FABRICATED DOUBLER, AND INTALLED DOUBLER IAW SRMSDR FDEA201907061494Shear Plate · corrodedMAIN CABIN BETWEEN STA. 1680 - 1720, BL0 RBL53 FLOOR WEB CORRODED ALL WORK ACCOMPLISHED IAW EA F-5310-T0348184 P1 FUSELAGE - MAINFRAME - AFT SHEAR DECK PLATE CORROSION REPAIR FROM STA 1681 TO 1720 NEAR RBL 51.SDR FDEA201907061492Floorbeam · corrodedMAIN CABIN BETWEEN STA. 920 - 1040 RBL 24.75 FLOOR BEAM T CHORD CORRODED REMOVED CORR ON T-CHORD STA 920-1040 RBL 24.75 IAW SRM 51-10-02. ORIG MAT .090 REM .045 LOSS .045 OUT OF LIMITS IAW SRM 53-00-51-1A FIG 101 REMOVED, LOCATED, DRILLED, TRIMMED AND INSTALSDR FDEA201907061491Seat Track · corrodedMAIN CABIN BETWEEN STA. 1620 - 1640 RBL 44.5 SEAT TRACK FLANGE CORRODED REMOVED CORR ON SEAT TRACK FLANGE STA 1620-1640 RBL 44.5 IAW SRM 51-10-02. ORIG MAT. .070 100% MATERIAL LOSS OUT OF LIMITS IAW SRM 53-00-52-1A. REMOVED, TRIMMED, LOCATED AND DRILLED NEW SESDR FDEA201907061493Floorbeam · corrodedMAIN CABIN BETWEEN STA. 1015 - 1021 BLB 24.75 FLOORBEAM T CHORD CORRODED.SDR FDEA201901120106Seat Track · gougedREMOVE AND REPLACE LBL 45.50 SEAT TRACK FROM BS440 TO BS680 COMPLIED WITH - EQUIP AND FURNISH - CARGO - LOADING SYSTEM - INTERIM REPAIR FOR DAMAGE SEAT TRACK LOBE, STA 579.95 LBL 45.50 EA# TF - 2550-T0343358 P3.SDR FDEA2018080321896Thermal Switch · failedLT ENG STRUT OH DET 1 EICAS MESSAGE ON STATUS PAGE DURING CLIMB OUT TO 360. FOUND THERMAL SWITCH S10196 GIVING AN OVERHEAT DETECTION INDICATION BEFORE TEMPERATURE THRESHOLD. REMOVED AND REPLACED THERMAL SWITCHES S10194, S10195, AND S10196 FOR THE LEFT STRUTSDR FDEA2018080311873Circuit Card · failedWHILE CLIMBING THROUGH FL340 TO 360, LT ENGINE OVHT EICAS MESSAGE ON. PERFORMED QRH, LIGHT EXTINGUISHED AT 1.28 EPR. IAW FIM R&R AFOLDS CARD IAW AMM 26-10-01-4 AND PERFORMED TEST TEST GOOD.SDR FDEA201808171644Unknown · malfunctionedAT SPEEDBRAKE DEPLOYMENT A ROLE TO THE LEFT OCCURS WITH A DISPLACEMENT OF THE YOKE TO THE RIGHT. AT DEPLOYMENT YOKE DISPLACES 1.5 UNITS ON AILERON TRIM INDICATOR, ONCE DEPLOYED THE YOKE IS DISPLACE 1.0 UNITS TO THE RIGHT. PERFORMED OPERATIONAL TEST OF SPOILER/SDR FDEA201806071417Power Supply · inoperativeRT R1 DOOR EXTERIOR SLIDE LIGHT INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY M00730 PER MM CH 33-51-07-2. A/C READY FOR CONT SERVICE.SDR FDEA201708172251Bracket · looseFLAP FAIRING BRACKET FOR 573HB IS LOOSE. REPAIRED THE LT, INBD MAIN FLAP IAW SRM 57-53-02-2R, REPAIR 3, AND EA F-5750-T0334988, PI.SDR FDEA201708082146Skin · dentedLEFT WING NR 3 SLAT UPPER SURFACE HAS A DENT AT CENTER OF SLAT AT T\E. REPAIRED THE LT WING SLAT IAW SRM 51-70-10-2R, PARAG 8 AND 20.SDR FDEA201708082142Seat Track · corrodedMAIN CABIN, BS 1640 - 1680, LBL45, SEAT TRACK HAS CORROSION ON FLANGE. REMOVED THE CORROSION IAW SRM 51-10-02 WITH 100 PERCENT MATERIAL LOSS. FABRICATED A NEW SEAT TRACK IAW SRM 51-40-05. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02-0G.SDR FDEA201708082141Seat Track · corrodedMAIN CABIN, BS 1640 - 1660, RBL 45, SEAT TRACK HAS CORROSION ON FLANGE. REMOVED CORROSION IAW SRM 51-10-02-0G, 100 PERCENT LOSS. FABRICATED A NEW SEAT TRACK IAW SRM 51-40-05. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02, AND SRM 51-40-02.SDR FDEA201708082140Seat Track · corrodedMAIN CABIN SEAT TRACK BS 365 - 345, LBL 6 HAS CORROSION. REMOVED THE CORROSION AND FOUND 100% LOSS IAW SRM 51-10-02, & 53-00-52-1A. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02 AND SRM 51-40-02-OG. FABRICATED THE NEW SEAT TRACK IAW DWG 3504-NC-2.SDR FDEA201705191457Sight Gauge · cloudyLEFT ENTRY DOOR INSPECTION WINDOW FOR SLIDE PRESSURE GAUGE IS HAZED, MAKING IT DIFFICULT TO READ. CLEANED THE SIGHT WINDOW IAW AMM: 20-30-02-2. OK FOR SERVICE.SDR FDEA201702020380Computer · out of adjustAIRCRAFT PITCH CONTROL HAS LAG ON PREFLIGHT CONTROL CHECK AND ON ARRIVAL PITCH AXIS WAS STIFF AND SEEMED TO HAVE A DELAY IN CONTROL. ADJUSTED AND TESTED OF ELEVATOR FEEL COMPUTER IAW AMM 27-31-19-4. LEAK AND OPS CHECKED NORMAL. ACFT OK FOR SERVICE.SDR FDEA201701050053Warning Bell · false activationTRIED TO SWITCH TO GROUND POWER AFTER BLOCKIN, THE FIRE BELL SOUNDED FOR 10 SECONDS. NO FIRE LIGHTS ILLUMINATED. NO OTHER INDICATIONS OF FIRE OR ANY OTHER MALFUNCTION. STARTED THE APU AND SHUTDOWN THE LEFT ENGINE. FIRE DETECTION SYSTEM OPS CHECKED NORMAL SDR FDEA201510283395Circuit Card · faultyFIRE BELL ACTIVATED AT LIFTOFF, NO VISUAL INDICATIONS OF FIRE, COULD NOT CANCEL BELL. R & R BELL CHIME WARNING CARD AS REQUIRED.SDR FDEA201507242380Skin · dentedPROTRUDING DENTS, BS 630 STRINGER 26L. COMPLIED WITH EA F-5330-T0319058 PT 1.SDR FDEA201507242379Skin · dentedPROTRUDING DENTS, STATION 643, STRINGER 26L. COMPLIED WITH EA F-5330-T0319058 PT 1.SDR FDEA201507242377Skin · gougedLEFT WING INBD FLAP, UPPER SURFACE HAS 2 EACH DEEP GOUGE AT WS 258. WORK ACCOMPLISHED IAW EA F-5750-T0318998 P 2.
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