N751FD

Service difficulty reports · 308

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 = 'N751FD' 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 FDEA202009092163Power Supply · inoperativeRT CABIN DOOR SLIDE ECAM DOES NOT SHOW "SLIDE" WHEN ARMED. REMOVED AND REPLACED AUTONOMOUS STANDBY SUPPLY UNIT USING AIRBUS 300 MM 52-73-18-04-0. OPERATIONS CHECKED GOOD.Sep 9, 2020 · N751FD · Airbus A300B4622R · Emergency EquipmentSDR FDEA202007211616Drain · not seatedDURING TAKEOFF ROLL, F/O CALLED 80KNOTS, CAPTAIN SAW 50 KNOTS - 30 KNOT AIRSPEED DIFFERENCE. AT100 KNOTS ON F/O AIRSPEED, CAPTAIN SAW 70 KNOTS. REJECTED THE TAKOFF AND COMPLIED WITH QRH PURGED CAPTAINS PITOT LINES AND PROBE IAW AMM 34-10-00-03 FOUND NO BLOJul 21, 2020 · N751FD · Airbus A300B4622R · Pitot/Static SystemSDR FDEA202007211611Pitot Line · leakingDURING TAKEOFF ROLL, F/O CALLED 80 KNOTS, CAPTAIN SAW 50 KNOTS, 30 KNOT AIRSPEED DIFFERENCE. AT 100 KNOTS ON F/O AIRSPEED, CAPTAIN SAW 70 KNOTS. REJECTED THE TAKOFF AND COMPLIED WITH QRH. INSPECTED BRAKES AND TIRES DUE TO REJECTED TAKEOFF IAW AMM 05-Jul 21, 2020 · N751FD · Airbus A300B4622R · Pitot/Static SystemSDR FDEA201911223046Warning Message · false activationPDIS 751 31-42 0747 22NOV19 OKC FACT U LOGPAGES:3169398 DURING CLIMBOUT RECEIVED ECAM WARNING OF EXCESSIVE AFT CG. FOLLOWED QRH PROCEDURES AND MOVED WHAT FUEL WAS IN TRIM TNK FWD. CG STABILIZED AT 30.8. HIGHEST AFT CG OBSERVED ON ECAM PANEL WNov 22, 2019 · N751FD · Airbus A300B4622R · Central WarningSDR FDEA201905131041Skin Panel · contaminatedPERFORM NDT INSPECTION RUDDER FOUND RT SIDE PONDING AS MARK REPAIRED THE RUDDER RT SIDE AS MARK PER SRM55-41-12/201 PARA31 & EA: 6-5540-T0346748 P1, TITLE: STABILIZERS - RUDDER - WATER INGRESS WAS FOUND ON RUDDER RH PANEL AROUND TRAILING EDGE SCREW. THE REPAIRMay 13, 2019 · N751FD · Airbus A300B4622R · Rudder, Plate/SkinSDR FDEA201904170818Spar · crackedPERFORM ROTATING PROBE INSP TO "C" HOLE OF RT FR47 REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE AND CRACK FOUND COMPLIED WITH EA: 6-5710-T0346583 A P1, TITLE: WINGS - BASIC WING STRUCTURE - EO 6-5710-7-3305 E3 WIC PT4 _ HOLE C CRACK AT FR47 RT _ SB 57Apr 17, 2019 · N751FD · Airbus A300B4622R · Wing SparSDR FDEA201904160808Structure · crackedRH SIDE CENTER WING JOINT AT FR40 SKIN UPPER HOLE FOUND CRACK SIGNAL REPAIRED THE RH SIDE CENTER WING JOINT AT FR40 UPPER CRACKED HOLE PER FEDEX EA: 6-5710-T0346356 P1, TITLE: WINGS - BASIC WING STRUCTURE - CRACK IN THE UPPER HOLE AT FR40 RHS CENTER WING JApr 16, 2019 · N751FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201904120783Beam · crackedNDT FOUND CRACK ON MDCC LHS OF GANTRY RH #5 AT FR52A REPAIRED THE CRACKED RH #5 GANTRY ON MDCC AT FR52A PER A300-600 SRM51-40-21 & AIRBUS DWG:R53810583 ISSUE:D, MAJOR REPAIR IAW FEDEX GMM 6-2-100Apr 12, 2019 · N751FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201904120782Beam · crackedNDT FOUND CRACK ON MDCC LHS OF GANTRY LH #4 AT FR52A. REPAIRED THE CRACKED LH #4 GANTRY ON MDCC AT FR52A PER A300-600 SRM 51-40-21 & DWG:R53810581 ISSUE:C, MAJOR REPAIR IAW GMM 6-2-100.Apr 12, 2019 · N751FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201903280740Stringer · corrodedFWD CARGO STRINGER CORRODED B/W FR38.2-FR39, STR 44R REPAIRED THE CORRODED STRINGER AT FWD CARGO B/W FR38.2-FR39, STR 44R PER SRM 53-10-14 FIG.201. THE REPAIR WAS CATEGORY "B" AND WAS CLASSIFIED AS MAJOR PER GMM 6-2-100. THE FIRST INSPECTION THRESHOLD WAS 5100Mar 28, 2019 · N751FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA201903280741Tee Fitting · corrodedFWD CARGO SKIN T-SECTION CORRODED B/W FR38.2-FR39, STR 52R-STR 54R COMPLIED WITH EA: 6-5310-T0346455 P1, TITLE: FUSELAGE - MAINFRAME - FR39 LOWER TEE BEAM CORROSION BETWEEN S-52R AND S-54R. REPAIRED THE FWD CARGO SKIN CORRODED T-SECTION B/W FR38.2-FR39, STR 52Mar 28, 2019 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201708212292Smoke Detector · failedAVIONICS SMOKE WARNING IN CRUISE. 80 MILES FROM GTF NO SMOKE DETECTED WARNING WAS INTERMITTENT. SUSPECT WATER CONTAMINATION. REMOVED AND REPLACED SMOKE DETECTORS IAW AMM 26-15-12-04. SYSTEM OPS CHECKED GOOD IAW AMM 26-15-00-05.Aug 21, 2017 · N751FD · Airbus A300B4622R · Smoke DetectionSDR FDEA201708212291Smoke Detector · failedAVIONICS SMOKE WARNING DURING CRUISE. NO SMOKE DETECTED WARNING WAS INTERMITTENT. SUSPECT WATER CONTAMINATION. REMOVED AND REPLACED THE SMOKE DETECTORS 11WA, 12WA, & 13WA IAW AMM: 26-15-12-04. SYSTEM OPS CHECKED GOOD IAW AMM 26-15-00-05.Aug 21, 2017 · N751FD · Airbus A300B4622R · Smoke DetectionSDR FDEA201708212287Smoke Detector · false activationAVIONICS SMOKE WARNING DURING CRUISE. NO SMOKE DETECTED, WARNING WAS INTERMITTENT. SUSPECT WATER CONTAMINATION. REMOVED AND REPLACED THE SMOKE DETECTORS 11WA, 12WA, & 13WA IAW AMM: 26-15-12-04. SYSTEM OPS CHECKED GOOD IAW AMM 26-15-00-05.Aug 21, 2017 · N751FD · Airbus A300B4622R · Smoke DetectionSDR FDEA201708192275Unknown · unknownON ROTATION, A DEFINITE THUMP FROM REAR OF AIRCRAFT. RETURNED TO DEPARTURE TO INVESTIGATE POSSIBLE CAUSE. PERFORMED GVI OF AIRCRAFT IAW SERVICE CHECK ON W/C, ALSO INSPECTED MCD FOR LOOSE CANS, NONE FOUND. NO CARGO PRESENT IN LOWER FWD, AFT OR BULK COMPARAug 19, 2017 · N751FD · Airbus A300B4622R · Fuselage Structure (General)SDR FDEA201707252040Pump · leakingGREEN HYDRAULIC SYSTEM LOW DURING CRUISE. COMPLIED WITH ECAM AND QRH. FOUND HYD PUMP LEAKING BETWEEN MATING SURFACE BETWEEN FRONT AND AFT HALF OF PUMP. REMOVED AND REPLACED THE NR 1 ENG HYD PUMP IAW MM 29-11-32-04-01. OPS AND LEAK CHECKED GOOD.Jul 25, 2017 · N751FD · Airbus A300B4622R · Hydraulic Pump (Electric/Engine), MainSDR FDEA201610163644Skin · gougedLT WING INBD FLAP UPPER L/E SKIN IS GOUGED. ACCOMPLISHED REPAIR ON LT WING INBD FLAP UPPER SKIN BETWEEN RIB 17 AND 18 STR 2.1 AND 2.2 PER EA 6-5750-T0329033Oct 16, 2016 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201610153640Flap · crackedREMOVE RT FLAP FOR MAINTENANCE ON CARRIAGE BUSHINGS. R&R RT CENTER FLAP IN REFERENCE AMM 27-50-12-04. FLAP FOUND UNSERVICIEABLE DUE FOUND CRACK ON XRAY INSPECTION.Oct 15, 2016 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201610153639Flap · crackedREMOVE LT CENTER FLAP ON CARRIAGE BUSHINGS. R&R LT CENTER FLAP IN REFERENCE AMM 27-50-12-04. FLAP FOUND UNSERVICEABLE DUE FOUND CRACK ON X-RAY INSPECTION.Oct 15, 2016 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201610153638Skin · puncturedRT WING NR 2 SPOILER LOWER SKIN HAS PUNCTURE DAMAGE. REMOVED AND REPLACED RT WING NR 2 SPOILER PER AMM 27-64-11-04 AND AMM 27-61-54-04.Oct 15, 2016 · N751FD · Airbus A300B4622R · SpoilersSDR FDEA201610043453Cargo Track · chafedMAIN CARGO TRACK IS GOUGED AT UPPER SURFACE BETWEEN FRAMES 42 AND 43, Y-450. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 51-40-21.Oct 4, 2016 · N751FD · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609293392Skin · damagedRIGHT WING NR 1 SLAT INNER SKIN HAS CHAFFING DAMAGE ABOVE NR 3 SLAT TRACK REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER ON RT WING NR 1 SLAT INNER SKIN ABOVE NR 3 SLAT TRACK IAW EA 6-5750-T0328570.Sep 29, 2016 · N751FD · Airbus A300B4622R · Leading Edge Slat Control SystemSDR FDEA201609253360Floorboard · damagedMAIN CABIN FLOORBOARD 231CF IS DELAMINATED AND CRACKED. REMOVED DAMAGED AND INSTALLED REPAIR DOUBLER ON UPPER AND LOWER SKIN OF MAIN CABIN FLOORBOARD IAW SRM 53-10-20 PARA 9C FIG 203.Sep 25, 2016 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201609253358Skin · damagedFWD LOWER FUSELAGE SKIN BETWEEN FR 0 AND FR 1 .500 RH OF CENTERLINE HAS LIGHTNING STIKE DAMAGE REMOVED DAMAGE ON FWD LWR FUSELAGE SKIN BETWEEN FR 0 AND FR 1, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER PER A300-600 SRM 53-10-12 FIG 202 AND SRM 53-Sep 25, 2016 · N751FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201609223348Floorboard · damagedMAIN CABIN FLOORBOARD 231CF IS DAMAGED ON UPPER AND LOWER SKIN. REMOVED DAMAGE AND INSTALLED CORE REPAIR DOUBLER IAW SRM 53-10-20 PARA 9C.Sep 22, 2016 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201609213328Floor Panel · delaminatedFLOOR PANEL 242LK LOCATED IN THE MAIN CABIN IS DELAMINATED. REMOVED DELAMINATION AND APPLIED REPAIR PATCHS IAW SRM 53-10-20 PARA 9B, FIGURE 202.Sep 21, 2016 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201609213327Floorboard · delaminatedMAIN CABIN FLOORBOARD 242RJ IS DELAMINATED. REMOVED DELAMINATION IAW SRM 53-10-20 PARA 9B FIG 202.Sep 21, 2016 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201509152882Windshield · crackedCAPTAINS FRONT WINDSHIELD CRACKED ECAM ALERT, LT FRONT WINDOW HEAT INOPERATIVE, FAULT. FOLLOWED QRH PROCEDURES. WINDOW CRACK EXTENDS INTO FIELD OF VIEW OUT OF LIMITS. R & R CAPTAINS FRONT WINDSHIELD IAW MM 56-11-11-04. OPERATIONS CHECKED NORMAL. OK FOR SESep 15, 2015 · N751FD · Airbus A300B4622R · Flight Compartment WindowsSDR FDEA201505211609Switch · defectiveLEFT GEAR OPEN LIGHT STAYED ON WHEN LG EXTENDED FOR LANDING. AT MAIN GEAR TOUCH DOWN LIGHT OUT. IAW CAPTAIN REPEAT ON DOOR INDICATION & THAT HE HAD TRIED BOTH SYS 1 & 2. FOUND LT MAIN GEAR DOOR MICRO SWITCH 31GB BAD. ALSO FOUND SYS 2 LT MAIN GEAR DOOR MIMay 21, 2015 · N751FD · Airbus A300B4622R · Landing Gear Position and WarningSDR FDEA201407131754Smoke Detector · faultyHAD AN INTERMITTENT 2 SEC MIN EQUIP BAY SMOKE ALARM AT CRUISE FLIGHT. WENT AWAY WITH NO INDICATIONS OF SUBSEQUENT SMOKE OR FIRE. REPLACED MIN EQUIPMENT BAY SMOKE DETECTOR.Jul 13, 2014 · N751FD · Airbus A300B4622R · Smoke DetectionSDR FDEA201405311234Floor Panel · damagedMCD FLOOR PANEL 231 DAMAGED. REPAIRED MCD FLOOR PANEL 231 CH, IAW SRM 53-10-20, CLASSIFIED AS MAJOR CAT A REPAIR FROM FRAME 19 - 27, Y2462LT - Y2462LT.May 31, 2014 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201405301232Floorboard · puncturedBULK CARGO COMPARTMENT PNL 172BF PUNCTURED AT TWO PLACES. FABRICATED FLOORBOARD 172BF ON STAM TRAVELER T14 1069490 IAW DWG SRZ-25-005, MAJOR REPAIR, CLASSIFIED AS CATEGORY A REPAIR.May 30, 2014 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201405261192Floorbeam · corrodedAFT CARGO BAY FLOORBEAM ANGLE AT FRAME 60, Y805 CORRODED ON BOTTOM SURFACE. PERFORMED REPAIR AT FLOORBEAM SECTION IAW SRM 53-10-15 FIGURE 207. FABRICATED REPAIR PARTS. CLASSIFIED AS MAJOR REPAIR CAT A.May 26, 2014 · N751FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA201405251188Floorboard · crackedFORWARD CARGO BAY FLOORBOARD 132YF TOP SURFACE PUNCTURED. FABRICATED NEW FLOORBOARD IAW DWG SRZ-25-005. MAJOR REPAIR CAT A REPAIR.May 25, 2014 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201405231151Floor Panel · damagedFORWARD CARGO FLOOR PANEL 131QF DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL 131QF ON STAM TRAVELER T14 1066340 IAW DWG SRZ-25-005. CLASSIFIED AS CAT A MAJOR REPAIR.May 23, 2014 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201405231150Floor Panel · damagedFORWARD CARGO FLOOR PANEL 132ZF DAMAGED. FABRICATED REPLACEMENT FLOOR PANEL ON STAM TRAVELER T14 1066342 IAW DWG SRZ- 25-005. CLASSIFIED AS CAT A MAJOR REPAIR.May 23, 2014 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201405231145Shear Tie · corrodedFORWARD CARGO COMPARTMENT BILGE AREA AT FRAME 32 BETWEEN STRINGER 54L - STRINGER 55 SHEAR TIE HAS SURFACE CORROSION. REMOVED & INSTALLED FABRICATED SHEAR TIE IN FWD CARGO COMPARTMENT BILGE AREA AT FRAME 32 IAW SRM 51-40-21. TREATED & PRIMED IAW SRM 51-21-10.May 23, 2014 · N751FD · Airbus A300B4622R · Fuselage Internal Mounting StructureSDR FDEA201405211186Floor Panel · brokenMCD FLOOR PANEL 261VF BROKEN. FABRICATED FLOORBOARD PANEL 261VF IAW STAM TRAVELER T14 1071641 MATERIAL USED A402N 48X144 BATCH 1972508 PO 26684 PART MARK AS FX-R532B387100000 IAW DWG SRZ-25-005. MAJOR REPAIR CAT A REPAIR.May 21, 2014 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201405171061Web · damagedFORWARD CABIN FLOOR SUPPORT, EDGE EXTRUSION, UNDER FWD LAVATORY SIDEWALL AREAS BETWEEN FRAME 11 & FRAME 12 HAS DAMAGE. R & R WEB PN A5361031838500 IAW SRM 51-40-21. FABRICATED NEW WEB ON STMAE TRAVELER T14/1068488 MAT 2024-0 050C BATCH 00249077664642 01 PO MMay 17, 2014 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201405151308Frame · corrodedAVI COMPARTMENT LT SIDE FRAME 11A CORRODED ON LOWER SURFACE. R & R FRAME 11A ARCH SECTION PN A5361032420200 BATCH 0002633151 IAW SRM 51-72-10. CLASSIFIED AS MAJOR REPAIR CAT A.May 15, 2014 · N751FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201405151166Floor Panel · damagedMCD FLOOR PANEL 232CF AFT EDGE BROKEN. FABRICATED NEW FLOOR PANEL 232CF ON TRAVELER T14 1069960 IAW DWG SRZ-25-005. CLASSIFIED AS MAJOR CAT A REPAIR.May 15, 2014 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201405151041Skin · damagedCOMPLIED WITH EA 6-5330-167815 PART 2. REPAIRED FUSELAGE CUT OUT BETWEEN FRAMES 66 - 67 STRINGER 1R - 1L IAW SRM-53-10-12, FIG. 225, CLASSIFIED AS MAJOR CAT B REPAIR.May 15, 2014 · N751FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201405061176Floor Panel · damagedAFT CARGO FLOOR PANEL 151JF HAS CHIPPED CORNER. FABRICATED FLOOR PANEL 151JF IAW DWG SRZ-25-005. CLASSIFIED AS MAJOR CAT A REPAIR.May 6, 2014 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201405061206Floor Panel · crackedAFT CARGO PNL 151LF CORNER CRACKED. FABRICATED FLOORBOARD PNL 151LF IAW STAM TRAVELER T14 1069605. MATERIAL USED A402H 48X144 BATCH 1972508 PO 26684 PART MARK AS FX-A2577203100000 IAW DWG SRZ-25-005. MAJOR REPAIR CAT A REPAIR.May 6, 2014 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201405061187Floor Panel · puncturedFLOOR PANEL 241TH LOWER SURFACE PUNCTURED. FABRICATED FLOOR PANEL 241TH ON TRAVELER T14 1071600 IAW DWG SRZ-25-005. CLASSIFIED AS MAJOR CAT A REPAIR.May 6, 2014 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201405061182Floor Panel · damagedAFT CARGO PANEL 152DF DAMAGED ALONG THE SIDES. FABRICATED FLOORBOARD 152DF ON STAM TRAVELER T14 1069590 IAW DWG SRZ-25-005. MAJOR REPAIR CATEGORY A REPAIR.May 6, 2014 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201405061181Floor Panel · damagedAFT CARGO PANEL 152FF DAMAGED ALONG THE SIDES. FABRICATED FLOORBOARD PANEL 152FF IAW STAM TRAVELER T14 1069602 IAW DWG SRZ-25-005. MAJOR REPAIR CAT A REPAIR.May 6, 2014 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201405061180Floor Panel · damagedAFT CARGO PANEL 151EF PUNCTURED AROUND FASTENER HOLES. FABRICATED FLOORBOARD PANEL 151EF IAW STAM TRAVELER T14 1069958 IAW DWG SRZ-25-005. MAJOR REPAIR CAT A REPAIR.May 6, 2014 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201405061179Floor Panel · damagedAFT CARGO PANEL 152LF DAMAGED ALONG THE SIDES. FABRICATED FLOORBOARD 152LF IAW STAM TRAVELER T14 1069601 IAW DWG SRZ-25-005. MAJOR REPAIR CAT A REPAIR.May 6, 2014 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201405061178Floor Panel · damagedAFT CARGO PANEL 152JF DAMAGED ALONG THE SIDES FABRICATED FLOOR BOARD 152JF ON STAM TRAVELER T14 1069604 IAW DWG SRZ-25-005. MAJOR REPAIR CAT A REPAIR.May 6, 2014 · N751FD · Airbus A300B4622R · Fuselage Floor Panel
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