N750FD
Service difficulty reports · 260
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 = 'N750FD' 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 = 'N750FD' 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 FDEA201412134210Floor Panel · damagedFLOOR PANEL 251NG DAMAGED FRAME 55 - 57.1 MAIN DECK. FLOOR PANEL 251NG FABRICATED ON T14 1110364 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.SDR FDEA201412134209Floor Panel · damagedFLOOR PANEL 242TG DAMAGED FRAME 54 - 54.2 MAIN DECK. FLOOR PANEL 242TG FABRICATED ON T14 1110362 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.SDR FDEA201412134208Floor Panel · crackedFLOOR PANEL 241EJ DAMAGE, CRACK, FRAME 54 MAIN DECK. FLOOR PANEL 241EJ FABRICATED ON T14 1110361 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.SDR FDEA201412134207Floor Panel · damagedFLOOR PANEL 251BH HAS EDGE & CORE DAMAGE FRAME 65 & 69 MAIN DECK. FLOOR PANEL 251BH FABRICATED ON T14 1110360 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR.SDR FDEA201412124206Floor Panel · puncturedBULK CARGO FLOOR PANEL 162HF HAS .5 INCH DEEP PUNCTURES ON UPPER SURFACE, FRAME 66 - 70. FLOOR PANEL 162HF FABRICATED ON T14 1109907 IAW DWG SRZ-25-011. REPAIR CLASSIFIED AS CAT A MAJOR.SDR FDEA201412124205Floor Panel · puncturedBULK CARGO FLOOR PANEL 161JF HAS .5 INCH DEEP PUNCTURES ON UPPER SURFACE, FRAME 66 - 70. FLOOR PANEL 161JF FABRICATED ON T14 1109908 IAW DWG SRZ-25-011. REPAIR CLASSIFIED AS CAT A MAJOR.SDR FDEA201412124204Floor Panel · puncturedBULK CARGO FLOOR PANEL 161GF HAS SEVERAL PUNCTURES ON UPPER SURFACE APPROX .5 INCH DEEP, FRAME 66 - 70, FLOOR PANEL 161GF. FABRICATED ON T14 1109906 IAW DWG SRZ-25-011. REPAIR CLASSIFIED CAT A MAJOR.SDR FDEA201208213094Uplock · failedON FINAL APPROACH, THE RT MAIN GEAR DID NOT EXTEND. ALL INDICATIONS WERE THE RT GEAR NOT DOWN AND LOCK, WHICH WAS CONFIRMED BY TOWER. COMPLIED WITH QRH, DECLARED EMERGENCY. R & R RT DOOR UPLOCK IAW MM 32-31-33-04. INSPECTION/CHECK OF MAIN GEAR DOOR UPLOCKSDR FDEA201208183071Flap System · malfunctionedON DEPARTURE HAD A SLATS FLAPS FAULT ON RETRACTING SLATS/ FLAPS. RECYCLED AND WOULD NOT CLEAR. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. FLAPS WERE RETRACTED WHEN ACFT ARRIVED AT GATE IAW TSM 27-50-00. CLEARED FAULTS ON SFCC 1 AND 2 CYCLED FLAPSSDR FDEA201208092908Uplock · failedON FINAL, AT GEAR EXTENSION, RT MAIN GEAR FAILED TO EXTEND - WENT AROUND AND RAN MANUAL GEAR EXT CHECKLIST GEAR CAME DOWN, LANDED. REMOVED AND REPLACED RIGHT MAIN GEAR UPLOCK ASSYSDR FDEA201111224995Skin · dentedLWR FUSELAGE SKIN FR57.3-58 S44-45R FOUND A DENT 6" IN LENGTH. PERFORMED A DVI AND ENSURED THE DENT IS IN SMOOTH CONTOUR WITHOUT SHARP EDGE. THE SCRATCH HAD BEEN REWORKED TO SMOOTH CONTOUR IAW SRM 51-73-10. PERFORMED A ROTO TEST INSPECTION OF OPENED FASTSDR FDEA201111064771Skin · chafedFUSELAGE SKIN CHAFED AT C34 S43R. STRIPPED THE PAINT PER SRM 51-75-20. REMAINING THICKNESS IS 0.051" PER NTM 51-10-04. NO CRACK FOUND PER NTM 51-10-08. ORIGINAL THICKNESS IS 0.063", OUT OF LIMITS PER SRM 53-10-12/101 PARA 7. REPAIRED SKIN PER SRM 53-10-12/SDR FDEA201111064770Skin · chafedFUSELAGE SKIN CHAFED AT C32-C33 S43R. STRIPPED THE PAINT PER SRM 51-75-20. REMAINING THICKNESS IS 0.044" PER NTM 51-10-04 NO CRACK FOUND PER NTM 51-10-08. ORIGINAL THICKNESS IS 0.063", OUT OF LIMITS PER SRM 53-10-12/101 PARA 7. REPAIRED SKIN PER SRM 53-1SDR FDEA201111064769Skin · chafedFUSELAGE SKIN CHAFED AT C31-C32, STR 43R. STRIPPED PAINT PER SRM 51-75-20 2. REMAINING THICKNESS IS 0.036" PER NTM 51-10-04 3. NO CRACK FOUND PER NTM 51-10-08 4. ORIGINAL THICKNESS IS 0.063" , OUT OF LIMITS PER SRM 53-10-12/101 PARA 7 5. REPAIRED SKIN PERSDR FDEA201011114317Landing Gear · malfunctionedLG WOULD NOT RETRACT. HANDLE WENT TO RETRACT POSITION BUT LG NEVER CAME UP. COMPLIED WITH TEST OF PROXIMITY DETECTOR PROCESSING UNIT (54GB) IAW TSM 32-61-00. NO FAULTS NOTED AT THIS TIME. GEAR PINS INSTALLED. PERFORMED TEST OF LANDING GEAR ELECTROVALVE (3GASDR FDEA201011104316Selector Valve · inoperativeLG WOULD NOT RETRACT. HANDLE WENT TO RETRACT POSITION BUT LG NEVER CAME UP. JACKED A/C VERIFIED VALVE 3GA FAULTY REMOVED AND REPLACED VALVE IAW MM 32-31-12-04. ALSO REMOVED AND REPLACED MODULE LANDING GEAR CONTROL HANDLE (2GA) IAW MM 32-32-11-04-0. PERFORMSDR FDEA201008022780Idg · malfunctionedABORTED TAKEOFF AT 100 KNOTS, DUE CHIME AND LOW OIL ON NR 1 IDG OR LOW OIL ON NR 1 ENG. RELEASED FOR SERVICE IAW MEL: 24-11-01-A CATEGORY: B EXPIRATION: "MEL 24-11-01-A: GEN NR 1 - INOP. APU GEN MUST BE USED TO POWER AFFECTED BUS THROUGHOUT FLIGHT. VERIFYSDR FDEA200905241778Electronic Unit · faultedON FINAL FULL CONFIGURATION (GEAR AND FLAPS 40), THERE WAS NO INDICATION OF BRAKE RELEASE (RELEASE BARS NOT IN VIEW). EXECUTED A GO AROUND TO TROUBLESHOOT. RELEASE BARS CAME BACK FOR NO APPARENT REASON, WENT OFF AGAIN, BUT ALL INDICATIONS NORMAL AT 500 FT, LSDR FDEA200904201340Shroud · corrodedCORROSION ON OUTER SHROUD BOX RT REPAIR PERFORMED IAW EA 6-5720-120231 AND RAS/BAE/1009111/2008.SDR FDEA200904201339Skin · crackedOLD EXTERNAL DOUBLER PATCH REPAIR WITH CRACKED HOLES. REPAIR PERFORMED IAW EA 6-5730-129153.SDR FDEA200904201337Shroud · delaminatedDAMAGE ON OUTER SHROUD BOX LT WING REPAIR PERFORMED IAW EA 6-5750-120235 AND RAS/BAE/1009297/2009.SDR FDEA200904201336Skin · corrodedSEVERAL CORROSION SPOTS BETWEEN RIB 9 IN LEVEL OF CENTER SPAR TOP SKIN PANEL UPPER SURFACE REPAIR PERFORMED IAW EA 6-5730-129154 AND RAS/BAE/1009557/2009.SDR FDEA200904201335Skin · corrodedSEVERAL CORROSION SPOTS BETWEEN RIB 14 AND 29 TOP SKIN PANEL UPPER SURFACE REPAIR PERFORMED IAW EA 6-5730-129154 AND RAS/BAE/1009557/2009.SDR FDEA200904201334Skin · misinstalledIRREGULARLY BOLT HOLE AT LT WING TOP SKIN RIB 8 STRINGER 14 SKIN REINFORCING REPAIR PERFORMED IAW EA 6-5730-129154 AND RAS/BAE/1009557/2009.SDR FDEA200904201333Skin · corrodedSEVERAL CORROSION SPOTS LT WING TOP SKIN PANEL BETWEEN RIB 1 AND 14 UPPER SURFACE REPAIR PERFORMED IAW EA 6-5730-129154 AND RAS /BAE/1009557/2009.SDR FDEA200904201332Skin · corrodedMULTIPLE CORROSION, TOP SKIN, TE OVERHANG, RIB 25-29, LEFT WING CORROSION REMOVED BY BLENDING AND NEW FASTENERS INSTALLED IAW EA 6-5720-129141. FABRICATION NEW PANEL IAW EA 6-5750-129151.SDR FDEA200904201331Rib · crackedRT WING CRACK IN RIB 7 UPPER FWD FLANGE INBOARD SIDE FLANGE BLENDED TO A SMOOTH PROFILE IAW EA 6-5710-129160.SDR FDEA200904161323Stringer · unknownSTRINGERS RIB 14 WITH RUN-OUTS REPROFILED INCORRECTLY. REPAIR PERFORMED IAW EA 6-5710-129150 AND RAS/BAE/1009505/2009 ISSUE "A".SDR FDEA200904161315Skin · corrodedSEVERAL CORROSION SPOTS AND CORROSION AROUND FASTENERS ON THE RT WING UPPER SURFACE BETWEEN RIB 1 AND 14. REPAIR PERFORMED IAW EA 6-5730-129139 AND RAS/BAE/1009447/2009 ISSUE "A".SDR FDEA200904161312Skin · corrodedCORROSION AND CHAFING, BOTTOM SKIN PANEL 1 AND 2, PYLON AND FLAP TRACK 2 REINFORCEMENT PLATE. REPAIR PERFORMED IAW EA 6-5720-129136, TD/J1/S1/09343/2009 ISSUE "A", TD/J1/S1/09620/2009 ISSUE "A" AND RAS/BAE/1009343/2009 ISSUE "A".SDR FDEA200904161311Rib · crackedCRACK AT LEADING EDGE SLAT JACK RIB 4A REPAIR PERFORMED IAW EA 6-5740-129105 AND RAS/BAE/1009425/2009 ISSUE "A".SDR FDEA200904161309Plate · chafedCHAFING MARKS IN THE LOWER WING PYLON REINFORCING PLATE. REPAIR PERFORMED IAW EA 6-5710-129142, TD/J1/S1/09291/2009 ISSUE "C" AND RAS /BAE/1009291/2009 ISSUE "A".SDR FDEA200904161321Skin · corrodedSEVERAL CORROSION SPOTS AROUND SOME FASTENERS AT TOP SKIN JOINT EXTERNAL SURFACE IN THE AREA OF RIB 9 FRONT AND REAR SPAR REPAIR PERFORMED IAW. EA 6-5730-129139 AND RAS/BAE/100944/2009 ISSUE "A"SDR FDEA200904161320Skin · corrodedSEVERAL CORROSION SPOTS RT WING TOP SKIN PANEL SURFACE FRONT SPAR ATTACHMENT BETWEEN RIB 1 AND 14 AND REAR SPAR ATTACHMENT BETWEEN RIB 1 AND 9 REPAIR PERFORMED IAW. EA 6-5730-129139 AND RAS/BAE/100944/2009 ISSUE "A"SDR FDEA200904161319Skin · corrodedSEVERAL CORROSION SPOTS AND CORROSION AROUND FASTENER RT WING TOP SKIN PANEL UPPER SURFACE BETWEEN RIB 14 AND 29 REPAIR PERFORMED IAW. EA 6-5730-129139 AND RAS/BAE/100944/2009 ISSUE "A"SDR FDEA200904161318Skin · corrodedCORROSION SPOT BETWEEN RIB 14 AND 15 / BETWEEN FRONT SPAR AND STRINGER 9 AT RT WING TOP SKIN, ARROUND FASTENER EXTERNAL SURFACE REPAIR PERFORMED IAW EA 6-5730-129139 AND RAS/BAE/100944/2009 ISSUE "A"SDR FDEA200904161316Skin · corrodedCORROSION SPOTS AROUND FASTENERS ON THE RT WING TOP SKIN RIB 8 REPAIR PERFORMED IAW EA 6-5730-129139 AND RAS/1009447/2009 ISSUE "A"SDR FDEA200904161313Rib · dentedDENT IN LEADING EDGE RIB 26-27 NOSE RIB REPLACED BY NEW ONE IAW SRM 57-50-00/201/FIG 208.SDR FDEA200904151303Rib · crackedDEVIATION RT INNER FLAP, ELONGATED AND CRACKED ATTACHMENT HOLES WITH RIB 25A REPLACEMENT. REPAIR PERFORMED IAW EA 6-5750-120193 , TD FOK/001/2009 ISSUE "C" AND RAS/FOK/001/2009 ISSUE "A" .SDR FDEA200904151302Rib · damagedDEVIATION LT INNER FLAP, ELONGATED AND CRACKED ATTACHMENT HOLES WITH RIB 25A REPLACEMENT. REPAIR PERFORMED BY REPLACEMENT OF RIB 25A AND MODIFICATION IAW OF RIB AS PER SB A300-57-6098. INSTALLED IAW SRM 51-72-10 AND TD FOK/359/2008 ISSUE "C" .SDR FDEA200904151300Skin · corrodedFOUND HEAVY CORROSION UNDER OUTER STATIC DISCHARGER OUTER FLAP LT REPAIR PERFORMED IAW EA 6-5750-129109, RAS/FOK/043/2009 ISSUE "B" AND RAS/FOK/043/2009 ISSUE "A"SDR FDEA200904091235Beam · crackedFOUND CRACK INDICATION ON BEAM 4 RT, C 49 OUTBOARD. REPAIR PERFORMED IAW DRAWING R538-10581, INSTALLATION OF REINFORCING ANGLE, SHIMS AND REPAIR STRAP.SDR FDEA200904091234Stiffener · corrodedFOUND CORRODED STIFFENERS ON FIRE WALL C 95. REPAIR PERFORMED BY REPLACEMENT OF PART IAW RAS/EFW/9000159/2009 ISS A, APPROVED BY EA 6-5310-120205.SDR FDEA200904091233Rib · chafedFOUND OLD DRILLING MARKS IN RT WING REAR SPAR RIBS IN THE TRAILING EDGE AREA. REPAIR PERFORMED BY BLEND OUT, NDT FOR CRACK FREE CONDITION IAW RAS/BAE/1009148/2009 ISS A, APPROVED BY EA 6-5710-129140.SDR FDEA200904091232Skin · delaminatedFOUND DELAMINATION ON RUDDER DURING NTM INSPECTION. REPAIR PERFORMED BY RUDDER REPLACEMENT IAW AMM 272121PB 400.SDR FDEA200904091231Skin · wornFOUND ELONGATED HOLES ON LT PYLON/WING SUPPORT BRACKET AND BOTTOM SKIN RIB 8. REPAIR PERFORMED IAW DRAWING R571-50532 AND RAS/BAE/1009499/2009 ISS A, APPROVED BY EA 6-2900-129110.SDR FDEA200904091230Skin · wornFOUND ELONGATED HOLES ON RT PYLON/WING SUPPORT BRACKET AND BOTTOM SKIN RIB 8. REPAIR PERFORMED IAW DRAWING R571-50532 AND RAS/BAE/1009499/2009 ISS A, APPROVED BY EA 6-2900-129110.SDR FDEA200904081221Structure · corrodedFOUND CORROSION ON FWD PAX DOOR LT UNDER DOOR STOP FITTINGS REPAIR PERFORMED BY REPLACEMENT OF DAMAGED PART IAW RAS 705178676/027/2009 ISS A, APPROVED BY 6-5210-129128.SDR FDEA200904081219Rib · damagedFOUND SEVERAL HOLES DAMAGED ON LT INNER FLAP, RIB 7 TOP AND BOTTOM SKIN. REPAIR PERFORMED BY REPLACEMENT OF RIB 7 AND REPAIR ALL DAMAGED PARTS IAW RAS/FOK/351/2008 ISS A, APPROVED BY EA 6-5750-120184.SDR FDEA200904081218Rib · damagedFOUND SEVERAL HOLES DAMAGED ON RT INNER FLAP, RIB 7 TOP AND BOTTOM SKIN REPAIR PERFORMED BY REPLACEMENT OF RIB 7 AND REPAIR ALL DAMAGED PARTS IAW, RAS/FOK/352/2009 ISS B, APPROVED BY EA 6-5750-120182.
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