N732FD

Service difficulty reports · 157

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 = 'N732FD' 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 FDEA2019082872028Floor Panel · damagedMAIN DECK FLOOR PANEL 231BH DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIRAug 27, 2019 · N732FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA2019082872027Floor Panel · damagedMAIN DECK FLOOR PANEL 231RH DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Aug 27, 2019 · N732FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA2019082872026Floorboard · damagedMAIN CARGO AREA FLOORBOARD 251RH DAMAGED. FABRICATED A NEW FLOORBOARD IAW SRZ-25-005. MAJOR REPAIRAug 27, 2019 · N732FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201908272025Floor Panel · damagedMAIN CARGO AREA FLOOR PANEL 231GG DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIRAug 27, 2019 · N732FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201908272024Floor Panel · damagedMAIN CABIN AREA FLOOR PANEL 241SH DAMAGED. FABRICATED FLOOR PANEL IAW SRZ-25-005 MAJOR REPAIRAug 27, 2019 · N732FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201908272023Floor Panel · brokenCABIN FLOOR PANEL 242LK BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIRAug 27, 2019 · N732FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201908262019Floor Panel · damagedFWD CARGO FLOOR PANEL 131HG BROKEN. FLOOR PANEL 131HG FABRICATED IAW SRZ-25-005. MAJOR REPAIR.Aug 26, 2019 · N732FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201908262018Floor Panel · damagedFWD CARGO FLOOR PANEL 132HG BROKEN. FLOOR PANEL 132HG FABRICATED ON MAE TRAVELER T19/1437881 AND IAW SRZ-25-005 MAJOR REPAIRAug 26, 2019 · N732FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA2019040530759Coupling · leakingRTO L 60 KTS. NR 1 GEN FAULT. NR 1 GEN FAULT CLEARED AFTER RESET. ATTEMPTED SECOND TAKEOFF. RTO NR 1 GEN FAULT L 60KTS. AFTER AIRCRAFT BLOCK IN, FOUND NR 1 ENGINE IDG SERVICE PORT LEAKING AND OIL PUDDLING IN COWLING. LEAK APPEARS TO BE BETWEEN SERVICE POApr 3, 2019 · N732FD · Airbus A300B4605R · AC Generator-AlternatorSDR FDEA2019021180311Hose · chafedPDIS 732 29-02 1585 08FEB19 IND FACT U LOGPAGES:3050131 GREEN HYD RESERVOIR SHOWED SLOW DECREASE IN FLT. OVERHEAD GAUGE SHOWED NEEDLE ALMOST TOUCHING RED DOT. WHEN GEAR WAS LOWERED LEVEL CAME UP HALFWAY TO HAT. LEVEL WAS DROPPING ABOUT 1 NEEDFeb 8, 2019 · N732FD · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201902080288Hydraulic Line · chafedGREEN HYD RESERVOIR SHOWED SLOW DECREASE IN FLT. OVERHEAD GAUGE SHOWED NEEDLE ALMOST TOUCHING RED DOT. WHEN GEAR WAS LOWERED LEVEL CAME UP HALFWAY TO HAT. LEVEL WAS DROPPING ABOUT 1 NEEDLE WIDTH EVERY 20-30 MINUTES. HYD PRESS WAS GOOD THE ENTIRE TIME. REMOVED Feb 8, 2019 · N732FD · Airbus A300B4605R · Hydraulic System, MainSDR FDEA201811233358Skin · damagedRT I/B FLAP LOWER SKIN IS DAMAGED 47.75" FWD OF TE AND 22.875 I/B OF INNER EDGE. REPAIRED RT FLAP LOWER SKIN PER EA NR 6-5750-T03443692 P1.Nov 23, 2018 · N732FD · Airbus A300B4605R · Trailing Edge FlapsSDR FDEA201711163247Hydraulic System · malfunctionedDURING DESCENT, LOST THE GREEN SYS HYD QTY IAW ECAM/QRH. LANDED WITHOUT GREEN SYSTEM. MANUALLY EXTENDED THE LANDING GEAR. AFTER TOW IN, QTY IN THE GREEN SYS RETURNED TO NORMAL.Nov 16, 2017 · N732FD · Airbus A300B4605R · Hydraulic Pressure IndicatorSDR FDEA201704081113Warning Message · false activationDURING CRUISE AT FLT LEVEL 350, THE RT MAIN ENTRY DOOR ESCAPE ARM LIGHT & ALARM ACTIVATED DURING FLT AND AT BLOCK-IN. WARNING SYSTEM FUNCTIONED NORMAL DURING PRESSURIZATION.Apr 8, 2017 · N732FD · Airbus A300B4605R · Door Warning SystemSDR FDEA201703100842Fitting · crackedFUSELAGE WING BOX, INSPECTION OF REAR SPAR & BOTTOM PANEL. NDT CHECK HOLE NR 44 WITH A CRACK SIGNAL. COMPLIED WITH EA6-5710-T0331014, P1. MAJOR REPAIR IAW GMM 6-2-100.Mar 10, 2017 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA201703100841Fitting · crackedFUSELAGE WING BOX, INSPECTION OF REAR SPAR & BOTTOM PANEL. NDT FOUND HOLE 181 WITH CRACK A SIGNAL. COMPLIED WITH EA6-5710-T0331014, P1. MAJOR REPAIR IAW GMM 6-2-100.Mar 10, 2017 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA201703100840Fitting · crackedFUSELAGE WING BOX, INSPECTION OF REAR SPAR & BOTTOM PANEL. INSPECTION FOUND HOLE"D" WITH A CRACK SIGNAL. COMPLIED WITH EA6-5710-T0331014, P1. MAJOR REPAIR IAW GMM 6-2-100.Mar 10, 2017 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA201703100839Fitting · crackedFUSELAGE WING BOX INSPECTION OF REAR SPAR & BOTTOM PANEL. INSPECTION FOUND HOLE"A" WITH A CRACK SIGNAL. COMPLIED WITH EA6-5710-T0331014, P1. MAJOR REPAIR IAW GMM 6-2-100.Mar 10, 2017 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA201703100838Fitting · crackedFUSELAGE WING BOX INSPECTION OF REAR SPAR & BOTTOM PANEL. INSPECTION FOUND HOLE"F" WITH A CRACK SIGNAL. COMPLIED WITH EA6-5710-T0331014, P1. MAJOR REPAIR IAW GMM 6-2-100.Mar 10, 2017 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA201703100837Fitting · crackedFUSELAGE WING BOX INSPECTION OF REAR SPAR & BOTTOM PANEL. INSPECTION FOUND THE RT SIDE FOUND HOLE"E" WITH A CRACK SIGNAL. COMPLIED WITH EA6-5710-T0331014, P1. MAJOR REPAIR IAW GMM 6-2-100.Mar 10, 2017 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA201703100836Fitting · crackedFUSELAGE WING BOX INSP OF REAR SPAR & BOTTOM PANEL. INSPECTED RT SIDE AND FOUND HOLE"P" WITH A CRACK SIGNAL. COMPLIED WITH EA6-5710-T0331014, P1. MAJOR REPAIR IAW GMM 6-2-100.Mar 10, 2017 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA201703100835Fitting · crackedFUSELAGE WING BOX INSPECTION OF REAR SPAR & BOTTOM PANEL. INSPECTION RT SIDE FOUND HOLE"Q" WITH A CRACKED SIGNAL. COMPLIED WITH FEDEX EA6-5710-T0331014, P1. MAJOR REPAIR IAW GMM 6-2-100.Mar 10, 2017 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA201703100834Fitting · crackedFUSELAGE CTR WING BOX INSPECTION OF REAR SPAR & BOTTOM PANEL. NDT CHECK HOLE NR 568 HAD A CRACK SIGNAL, RT SIDE. COMPLIED WITH EA6-5710-T0331014. P1. MAJOR REPAIR IAW GMM 6-2-100.Mar 10, 2017 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA201703100833Fitting · crackedFUSELAGE CTR WING BOX INSP OF REAR SPAR & BOTTOM PANEL. NDT CHECK HOLE NR 100 WITH CRACK SIGNAL RT SIDE. COMPLIED WITH EA6-5710-T0331014, P1. MAJOR REPAIR IAW GMM 6-2-100.Mar 10, 2017 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA201703100832Fitting · crackedFUSELAGE CTR WING BOX INSP OF REAR SPAR & BOTTOM PANEL. NDT CHECK HOLE NR 102 WITH CRACK SIGNAL RT SIDE. COMPLIED WITH EA6-5710-T0331014 P1. MAJOR REPAIR IAW GMM 6-2-100.Mar 10, 2017 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA201703100831Fitting · crackedINSPECTION OF FRAME 47, FITTING FOUND CRACKED. REPAIRED IAW EO6-5710-7-3305 E1 PART3 & 4. MAJOR REPAIR IAW GMM6-2-100.Mar 10, 2017 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA201703090824Fitting · crackedINSPECTION OF THE FUSELAGE FITTING LT SIDE FOUND HOLE-C CRACKED FRAME 47. REPAIRED IAW EA6-5710-T0331014 P1. MAJOR REPAIR IAW GMM 6-2-100.Mar 9, 2017 · N732FD · Airbus A300B4605R · Fuselage Main, Attach FittingsSDR FDEA201703090825Fitting · crackedFRAME 47 FITTING PRODUCED A CRACKED SIGNAL IAW EA6-5710-T0331014, P1. REPAIRED IAW EA. MAJOR REPAIR IAW GMM 6-2-100.Mar 9, 2017 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA201702160570Rib · crackedNDT X-RAY INSPECTION FOUND LT CTR FLAP RIB20 CRACK AT AFT SECTION COMPLIED WITH EA:6-5750-T0330963 A PT1 EA TITLE:WINGS-FLIGHT SURFACES-CRACKS AT LT CENTER FLAP RIB 12.19.20.25.26 UPPER FLANGES. THIS IS A MAJOR REPAIR IAW GMM6-2-100.Feb 16, 2017 · N732FD · Airbus A300B4605R · Trailing Edge FlapsSDR FDEA201702160569Rib · crackedNDT X-RAY INSPECTION FOUND LT CTR FLAP RIB 26 CRACK AT AFT SECTION(2EA). COMPLIED WITH EA:6-5750-T0330963 A PT1 EA TITLE:WINGS-FLIGHT SURFACES-CRACKS AT LT CENTER FLAP RIB12.19.20.25.26 UPPER FLANGES THIS IS A MAJOR REPAIR IAW GMM6-2-100.Feb 16, 2017 · N732FD · Airbus A300B4605R · Trailing Edge FlapsSDR FDEA201702140552Rib · crackedNDT X-RAY INSPECTION FOUND LT CTR FLAP RIB25 CRACK AT AFT SECTION. COMPLIED WITH EA 6-5750-T0330963 A PT1 EA TITLE:WINGS-FLIGHT SURFACES-CRACKS AT LT CENTER FLAP RIB12.19.20.25.26 UPPER FLANGES. THIS IS A MAJOR REPAIR IAW GMM6-2-100.Feb 14, 2017 · N732FD · Airbus A300B4605R · Trailing Edge FlapsSDR FDEA201702140551Rib · crackedNDT X-RAY INSPECTION FOUND LT CTR FLAP RIB12 CRACK AT AFT SECTION. COMPLIED WITH EA 6-5750-T0330963 A PT1 EA TITLE:WINGS-FLIGHT SURFACES-CRACKS AT LT CENTER FLAP RIB 12.19.20.25.26 UPPER FLANGES. THIS IS A MAJOR REPAIR IAW GMM6-2-100.Feb 14, 2017 · N732FD · Airbus A300B4605R · Trailing Edge FlapsSDR FDEA201702140550Rib · crackedNDT X-RAY INSPECTION FOUND LT CTR FLAP RIB19 CRACK AT AFT SECTION(2EA). COMPLIED WITH EA 6-5750-T0330963 A PT1 EA TITLE: WINGS-FLIGHT SURFACES-CRACKS AT LT CENTER FLAP RIB 12.19.20.25.26 UPPER FLANGES. THIS IS A MAJOR REPAIR IAW GMM6-2-100.Feb 14, 2017 · N732FD · Airbus A300B4605R · Trailing Edge FlapsSDR FDEA201701280277Seat Track · chafedFRAMES 54.2 - 54.3 Y953 SEAT TRACK UPPER SECTION CHAFED. REPAIRED IAW SRM 51-40-21, DWG A53275018 AND SRM 53-10-16, FIG 207. THE REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jan 28, 2017 · N732FD · Airbus A300B4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201701280276Floor Support · corrodedFRAME 10 - 12 FLOOR SUPPORT FOUND CORRODED. .REMOVE CORROSION IAW SRM 51-74-10 . FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-12-15/201 PARA.4.G, FIG207 MAJOR REPAIR IAW 6-2-100.Jan 28, 2017 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA201701280275Support Beam · corrodedFRAMES 10 - 12 SUPPORT BEAM FOUND CORRODED. REPAIRED THE SUPPORT BEAM IAW SRM 53-12-15/201 PARA.4.G, FIG 207, CLASSIFIED AS A, MAJOR REPAIR IAW GMM 6-2-100.Jan 28, 2017 · N732FD · Airbus A300B4605R · Fuselage Main, StructureSDR FDEA201611033805Warning System · inoperativeR1 DOOR WARNING BUZZER INOPERATIVE. WARNING LIGHT WORKS FINE. REMOVED AND REPLACED R1 DOOR, WARNING HORN, IAW AMM 52-73-12-04-01. OPS CHECKED GOOD.Nov 3, 2016 · N732FD · Airbus A300B4605R · Door Warning SystemSDR FDEA201606091909Slide · out of positionRIGHT DOOR SLIDE WILL NOT ARM: 52-11-01-01, CATEGORY C, EXPIRATION MEL 52-11-01-01: CREW ENTRY DOOR ESCAPE SLIDE, R1- INOPERATIVE. SLIDE REMAINS INSTALLED ON DOOR. REPOSITIONED SLIDE, GIRT BAR OPERATED NORMALLY, REF AMM 52-22-11. OK FOR SERVICE.Jun 9, 2016 · N732FD · Airbus A300B4605R · Escape SlideSDR FDEA201606091908Slide · out of positionRIGHT DOOR SLIDE WILL NOT ARM : 52-11-01-01, CATEGORY: C, EXPIRATION MEL 52-11-01-01. CREW ENTRY DOOR ESCAPE SLIDE R1- INOPERATIVE SLIDE REMAINS INSTALLED ON DOOR. REPOSITIONED SLIDE GIRT BAR OPERATED NORMALLY REF AMM 52-22-11. OK FOR SERVICE.Jun 9, 2016 · N732FD · Airbus A300B4605R · Escape SlideSDR FDEA201604281422Nut · contaminatedDURING APPROACH WE HAD A DOUBLE FLAP, SYS 1 & 2, FAULT & FLAPS WERE STUCK AT 15, CYCLED NO HELP. COMPLIED WITH ECAM & QRH PROCEDURE, LANDED WITH FLAPS AT 15. AFTER LANDING DOUBLE FLAP FAULT DISAPPEARED. ACCOMPLISHED BITE CHECK OF SFCC 1 & 2, BOX 1 FAULT IS Apr 28, 2016 · N732FD · Airbus A300B4605R · Trailing Edge Flap ActuatorSDR FDEA201602240680Slide · unsecureON R1 DOOR APPEARS DOOR SLIDE PARTIALLY HANGING OFF THE DOOR ON THE LT SIDE. RELEASED FOR SERVICE IAW MEL 52-11-01-02 CATEGORY C EXPIRATION 05 MAR 16. IDENTIFY R1 CREW ENTRY, IDENTIFY DOOR OR ESCAPE SLIDE, ESCAPE SLIDE INOPERATIVE. IF SLIDE TO BE RETAINED OFeb 24, 2016 · N732FD · Airbus A300B4605R · Escape SlideSDR FDEA201411123646Brake Assy · failedDURING CLIMB PASSING FL 190 TO FL 350, RECEIVED A MASTER CAUTION & ECAM. WARMER OF BRAKE OVERTEMP. REFERED TO WHEEL PAGE & NR 5 INDICATES SHOWED 320 & CLIMBING. COORDINATED DESCENT TO FL190 & SLOWED TO 25 KTS, DROPPED GEAR. TEMP SLOWLY DROPPED TO BELOW 10Nov 12, 2014 · N732FD · Airbus A300B4605R · Landing Gear Brake SystemSDR FDEA201409112568Skin · delaminatedTWO EXISTING REPAIRS ON LT ELEVATOR UPPER SURFACE FROM INBD TO OTBD 20 INCHES, FROM AFT TO FWD 20 INCHES. THE EXISTING REPAIR WAS EVALUATED & FOUND IN CONFORMITY WITH SRM 55-21-12 201 PARA 5 B, BUT FOUND DELAMINATION BETWEEN REPAIRED PLIES & CORE. REPAIREDSep 11, 2014 · N732FD · Airbus A300B4605R · Elevator, Plate/SkinSDR FDEA201408302362Seat Track · brokenDURING PERFORM INSTALL LOADING SYS FOUND MDCC SEAT TRACK Y C TEETH BROKEN BETWEEN FRAME 53 & 54.1. REMOVED THE MDCC BROKEN SEAT TRACK PER A300-600 AMM20-21-12-00, MACHINED THE REPAIR SEAT TRACK FROM TRACK (P/N: A5381312720000) PER AIRBUS DRAWING: Y53829731200Aug 30, 2014 · N732FD · Airbus A300B4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201408082122Skin · crackedLEFT SIDE CTR WING JOINT AT FRAME 40 SKIN UPPER HOLE FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0310491 PT1 , TITLE: WINGS - BASIC WING STRUCTURE - CRACK HOLES IN CENTER WING JOINT - FR40 LT/RT , REPAIRED THE LT UPPER HOLE OF CENTER WING JOINT AT FRAME 40Aug 8, 2014 · N732FD · Airbus A300B4605R · Fuselage Main, Plate/SkinSDR FDEA201408082121Skin · crackedRIGHT SIDE CTR WING JOINT AT FRAME 40 SKIN LOWER HOLE FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0310491 PT1 , TITLE: WINGS - BASIC WING STRUCTURE - CRACK HOLES IN CENTER WING JOINT - FR40 LT/RT , REPAIRED THE RT LOWER HOLE OF CENTER WING JOINT AT FRAME 4Aug 8, 2014 · N732FD · Airbus A300B4605R · Fuselage Main, Plate/SkinSDR FDEA201402200378Rib · corrodedRIGHT MLG RIB 5 FWD LUG HAS CORROSION IN BORE, FWD FACE & AFT FACE. REPAIRED IAW EA 6-5710-T0306255 P-2 .Feb 20, 2014 · N732FD · Airbus A300B4605R · Wing, Landing Gear Attach FittingsSDR FDEA201402200379Rib · corrodedLEFT MLG RIB 5 FWD LUG HAS CORROSION IN THE BORE, FWD FACE & AFT FACE. REPAIRED IAW EA 6-5710-T0306255 P-1.Feb 20, 2014 · N732FD · Airbus A300B4605R · Wing, Landing Gear Attach FittingsSDR FDEA201306051202Screw · brokenFLAP HANDLE WOULD NOT RETRACT AFTER TAKEOFF. FOUND FLAP HANDLE SCREW BROKEN REPLACE REF EO 6-2750-7-5006, PART 1.Jun 5, 2013 · N732FD · Airbus A300B4605R · Trailing Edge Flap Control SystemSDR FDEA201208042844Door · out of adjustON CLIMB OUT, AT 29,000 R1 FWD ENTRY DOOR ECAM ALERTED DOOR NOT CLOSED. JUMPSEATER REPORTED DOOR CHIME WAS SOUNDING AND DOOR LOCKS WERE INDICATING "HALF" LOCKED & HALF OPEN. DECENDED TO 10,000 SLOWLY. NO PRESSURE PROBLEMS NOTED. FOUND UPPER HOOKS NOT MAKIAug 4, 2012 · N732FD · Airbus A300B4605R · Passenger/Crew Doors
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