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.

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.Dec 13, 2014 · N750FD · Airbus A300B4622R · Fuselage Floor PanelSDR 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.Dec 13, 2014 · N750FD · Airbus A300B4622R · Fuselage Floor PanelSDR 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.Dec 13, 2014 · N750FD · Airbus A300B4622R · Fuselage Floor PanelSDR 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.Dec 13, 2014 · N750FD · Airbus A300B4622R · Fuselage Floor PanelSDR 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.Dec 12, 2014 · N750FD · Airbus A300B4622R · Fuselage Floor PanelSDR 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.Dec 12, 2014 · N750FD · Airbus A300B4622R · Fuselage Floor PanelSDR 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.Dec 12, 2014 · N750FD · Airbus A300B4622R · Fuselage Floor PanelSDR 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 UPLOCKAug 21, 2012 · N750FD · Airbus A300B4622R · Landing Gear Retraction/Extension SystemSDR 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 FLAPSAug 18, 2012 · N750FD · Airbus A300B4622R · Trailing Edge Flap Control SystemSDR 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 ASSYAug 9, 2012 · N750FD · Airbus A300B4622R · Landing Gear Retraction/Extension SystemSDR 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 FASTNov 22, 2011 · N750FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 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/Nov 6, 2011 · N750FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 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 53-1Nov 6, 2011 · N750FD · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR 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 PERNov 6, 2011 · N750FD · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR 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 (3GANov 11, 2010 · N750FD · Airbus A300B4622R · Landing Gear Retraction/Extension SystemSDR 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. PERFORMNov 10, 2010 · N750FD · Airbus A300B4622R · Landing Gear Retraction/Extension SystemSDR 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. VERIFYAug 2, 2010 · N750FD · Airbus A300B4622R · AC Generator-AlternatorSDR 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, LMay 24, 2009 · N750FD · Airbus A300B4622R · Landing Gear Brake SystemSDR FDEA200904201340Shroud · corrodedCORROSION ON OUTER SHROUD BOX RT REPAIR PERFORMED IAW EA 6-5720-120231 AND RAS/BAE/1009111/2008.Apr 20, 2009 · N750FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA200904201339Skin · crackedOLD EXTERNAL DOUBLER PATCH REPAIR WITH CRACKED HOLES. REPAIR PERFORMED IAW EA 6-5730-129153.Apr 20, 2009 · N750FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200904201337Shroud · delaminatedDAMAGE ON OUTER SHROUD BOX LT WING REPAIR PERFORMED IAW EA 6-5750-120235 AND RAS/BAE/1009297/2009.Apr 20, 2009 · N750FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR 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.Apr 20, 2009 · N750FD · Airbus A300B4622R · Wing, Plate/SkinSDR 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.Apr 20, 2009 · N750FD · Airbus A300B4622R · Wing, Plate/SkinSDR 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.Apr 20, 2009 · N750FD · Airbus A300B4622R · Wing, Plate/SkinSDR 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.Apr 20, 2009 · N750FD · Airbus A300B4622R · Wing, Plate/SkinSDR 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.Apr 20, 2009 · N750FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200904201331Rib · crackedRT WING CRACK IN RIB 7 UPPER FWD FLANGE INBOARD SIDE FLANGE BLENDED TO A SMOOTH PROFILE IAW EA 6-5710-129160.Apr 20, 2009 · N750FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA200904161323Stringer · unknownSTRINGERS RIB 14 WITH RUN-OUTS REPROFILED INCORRECTLY. REPAIR PERFORMED IAW EA 6-5710-129150 AND RAS/BAE/1009505/2009 ISSUE "A".Apr 16, 2009 · N750FD · Airbus A300B4622R · Wing, Longeron/StringerSDR 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".Apr 16, 2009 · N750FD · Airbus A300B4622R · Wing, Plate/SkinSDR 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".Apr 16, 2009 · N750FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200904161311Rib · crackedCRACK AT LEADING EDGE SLAT JACK RIB 4A REPAIR PERFORMED IAW EA 6-5740-129105 AND RAS/BAE/1009425/2009 ISSUE "A".Apr 16, 2009 · N750FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR 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".Apr 16, 2009 · N750FD · Airbus A300B4622R · Wing, Plate/SkinSDR 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"Apr 16, 2009 · N750FD · Airbus A300B4622R · Wing, Plate/SkinSDR 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"Apr 16, 2009 · N750FD · Airbus A300B4622R · Wing, Plate/SkinSDR 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"Apr 16, 2009 · N750FD · Airbus A300B4622R · Wing, Plate/SkinSDR 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"Apr 16, 2009 · N750FD · Airbus A300B4622R · Wing, Plate/SkinSDR 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"Apr 16, 2009 · N750FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200904161313Rib · dentedDENT IN LEADING EDGE RIB 26-27 NOSE RIB REPLACED BY NEW ONE IAW SRM 57-50-00/201/FIG 208.Apr 16, 2009 · N750FD · Airbus A300B4622R · Trailing Edge FlapsSDR 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" .Apr 15, 2009 · N750FD · Airbus A300B4622R · Trailing Edge FlapsSDR 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" .Apr 15, 2009 · N750FD · Airbus A300B4622R · Trailing Edge FlapsSDR 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"Apr 15, 2009 · N750FD · Airbus A300B4622R · Leading Edge DevicesSDR 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.Apr 9, 2009 · N750FD · Airbus A300B4622R · Fuselage Main, StructureSDR 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.Apr 9, 2009 · N750FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 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.Apr 9, 2009 · N750FD · Airbus A300B4622R · Wing SparSDR FDEA200904091232Skin · delaminatedFOUND DELAMINATION ON RUDDER DURING NTM INSPECTION. REPAIR PERFORMED BY RUDDER REPLACEMENT IAW AMM 272121PB 400.Apr 9, 2009 · N750FD · Airbus A300B4622R · Rudder, Plate/SkinSDR 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.Apr 9, 2009 · N750FD · Airbus A300B4622R · Wing, Plate/SkinSDR 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.Apr 9, 2009 · N750FD · Airbus A300B4622R · Wing, Plate/SkinSDR 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.Apr 8, 2009 · N750FD · Airbus A300B4622R · Passenger/Crew DoorsSDR 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.Apr 8, 2009 · N750FD · Airbus A300B4622R · Trailing Edge FlapsSDR 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.Apr 8, 2009 · N750FD · Airbus A300B4622R · Trailing Edge Flaps
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