N744FD

Service difficulty reports · 271

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 = 'N744FD' 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 FDEA2020072761668Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 232LG HAD DELAMINATION ON THE CORNER. REPAIRED THE FLOOR PANEL BY FABRICATION IAW SRZ-25-005, REV R. MAJOR REPAIR.Jul 26, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020072761667Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231KG WAS DELAMINATED AT CORNER. REPAIRED FLOOR PANEL BY FABRICATION IAW SRZ-25-005 REV R. MAJOR REPAIR.Jul 26, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020072761666Floor Panel · puncturedMAIN CABIN FLOOR PANEL 231QG HAS CRACK ON FWD SIDE AND MULTIPLE PUNCTURES. REPAIRED FLOOR PANEL 231QG BY FABRICATION IAW SRZ-25-005 REV R. MAJOR REPAIR.Jul 26, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020072761665Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231VG CRACKED AT MIDDLE CUTOUT. REPAIRED THE FLOOR PANEL BY FABRICATION IAW SRZ-25-005 REV R. MAJOR REPAIR.Jul 26, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020072761664Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231HG IS CRACKED. REPAIRED FLOOR PANEL 231HG BY FABRICATION IAW SRZ-25-005 REV R. MAJOR REPAIR.Jul 26, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020072751650Panel · crackedNR 1 PYLON PANEL 413BL OB LOUVERS CRACKED. NR 1 PYLON PANEL 413BL OB LOUVERS REPAIRED PER EA 6-5450-T0355371 P1.Jul 25, 2020 · N744FD · Airbus A300B4622R · Nacelle/Pylon, Plate/SkinSDR FDEA2020081271856Floorbeam · corrodedAFT CARGO FLOORBEAM AT FRAME 62 CORRODED THROUGH. REMOVED AND REPLACED THE AFT CARGO FLOORBEAM IAW DWG A53974288, REV.K, AND SRM 51-40-21.Jul 22, 2020 · N744FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA202007211608Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241PF WAS DELAMINATED . FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.Jul 21, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020072311607Floor Panel · crackedMAIN CABIN FLOOR PANEL 241KJ WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.Jul 21, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020072311606Floor Panel · crackedMAIN CABIN FLOOR PANEL 242AK WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.Jul 21, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020072311605Floor Panel · crackedMAIN CABIN FLOOR PANEL 241BK WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.Jul 21, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA202007211604Floor Panel · crackedMAIN CABIN FLOOR PANEL 241ZH IS CRACKED FABRICATE NEW FLOOR PANEL IAW SRZ-25-005Jul 21, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA202007211602Floor Panel · crackedMAIN CABIN FLOOR PANEL 241YH WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZZ-25-005.Jul 21, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020072301588Panel · delaminatedNR 1 PYLON PANEL 471AL HAS DELAMINATION. REPAIRED THE NR 1 PYLON PANEL 471AL IAW EA 6-5480-T0354751-P1.Jul 20, 2020 · N744FD · Airbus A300B4622R · Nacelle/Pylon, Plate/SkinSDR FDEA2020072301597Floor Panel · crackedMAIN CABIN FLOOR PANEL 242QF WAS CRACKED, FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.Jul 20, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA202007201596Floor Panel · crackedMAIN CABIN FLOOR PANEL 242LH WAS PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005Jul 20, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020072391582Access Panel · delaminatedVERTIAL STAB PANEL 325CR DELAMINATED ON THE CENTER OF TOP SURFACE. REPAIRED VERT STAB PANEL 325CR IAW EA 6-5530-T0354979-P1 STABILIZERS-V VERTICAL STABILIZER-TRAILING EDGE ACCESS PANEL 325CR DELAM.Jul 19, 2020 · N744FD · Airbus A300B4622R · Vertical Stabilizer, Plate/SkinSDR FDEA2020072391581Bulkhead · delaminatedAC BAY BULKHEAD PANEL 147CZ HAS DELAMINATION AND DISBOND THROUGHOUT. REPAIRED A/C BAY BULKHEAD PANEL 147CZ FOUND DELAMINATED AND DIBONDED THROUGHOUT IAW EA 6-2570-T0354955-P1 EQUIPT AND FUNISH-ACCESSORY COMPTS- WHEEL WELL PANEL 147CZ,DELAMINATION.Jul 19, 2020 · N744FD · Airbus A300B4622R · Fuselage Main, BulkheadSDR FDEA2020072391580Panel · delaminatedNR 1 PYLON PANEL 474BR WAS DELAMINATED. REPAIRED THE PYLON PANEL IAW EA 6-5451-T0354951-P1.Jul 19, 2020 · N744FD · Airbus A300B4622R · Nacelle/Pylon, Plate/SkinSDR FDEA2020071081473Floor Panel · delaminatedAFT CARGO COMPARTMENT FLOOR PANEL 151DF HAS DENT AND CORNER DAMAGEJul 8, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020071081472Floor Panel · crushedFWD CARGO COMPARTMENT L/H FLOOR PANEL 131RF HAS DAMAGED EDGE FILLER AND CRUSHED HONEYCOMBJul 8, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020071081471Floor Panel · gougedFWD CARGO COMPARTMENT L/H FLOOR PANEL 132YF HAS DAMAGED EDGE FILLER AND GOUGED TOP SKINJul 8, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020071081469Floor Panel · delaminatedAFT CARGO COMPARTMENT FLOOR PANEL 152JF HAS DISBONDED LOWER SKIN AND DAMAGED EDGE FILLERJul 8, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020071081468Floor Panel · damagedAFT CARGO COMPARTMENT FLOOR PANEL 152AF HAS DAMAGE TO EDGE FILLER AND LOWER SKINJul 8, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020071081467Floor Panel · damagedAFT CARGO COMPARTMENT FLOOR PANEL 151BF HAS DAMAGED EDGE FILLER AND TORN LOWER SKINJul 8, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020071081466Floor Panel · puncturedAFT CARGO COMPARTMENT FLOOR PANEL 152HF HAS PUNCTURES IN LOWER SKINJul 8, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020070871457Floor Panel · damagedMAIN CABIN FLOOR PANEL 221PF IS CRACKED AND PUNCTURED FAB NEW PANEL PER FEDEX SRZ-25-005 REV RJul 7, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020070871456Floor Panel · brokenMAIN CABIN FLOOR PANEL 221RF HAS BROKEN CORNER FAB NEW PANEL 221RF IAW FEDEX SRZ-25-005 REV RJul 7, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020070871455Floor Panel · puncturedMAIN CABIN FLOOR PANEL 222RF HAD PUNCTURES ON BOTTOM SIDE. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005 REV R.Jul 7, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020070601443Skin · dentedFUSELAGE EXTERNAL SKIN RT SIDE FWD OF FRAME 26, BETWEEN STRINGERS 38R-39R SKIN DENTED AND SCRATCHED. ACCOMPLISHED REPAIR DOUBLER ON FUSELAGE EXTERNAL SKIN RT SIDE FWD OF FRAME 26, BETWEEN STRINGERS 38R-39R IAW SRM 53-10-12, FIG 225 SHEET 1.Jun 30, 2020 · N744FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA202006301392Floorboard · brokenMAIN CABIN FLOORBOARD 251ZG HAS CORNER BROKEN OFF. FABRICATED NEW PANEL 251ZG IAW FED EX SRZ 25-005 REV R.Jun 30, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA202006301391Floorboard · crackedMAIN CABIN FLOORBOARD 261KF HAS CORNER BROKEN OFF. FABRICATED NEW PANEL 261KF IAW SRZ 25-005 REV R.Jun 30, 2020 · N744FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020081261855Floorbeam · gougedAFT PIT FLOOR, A 16" INCH (40.6CM) SCRATCH ON THE FLOOR BEAM AT FR60 Y130 TO Y720 REMOVED AND REPLACED AFT PIT FLOOR BEAM AT FR60 IAW AIRBUS DWG A53974286, REV. J, AND A300-600SRM 51-40-21Jun 23, 2020 · N744FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA201903260718Smoke Detector · malfunctionedON CLIMBOUT RECEIVED AN AVIONICS SMOKE LIGHT AND ECAM MESSAGE, DECLARED AN EMERGENCY AND RETUREND TO KORF. ISOLATED FAULT USING ASMFX3 26-15-00 TO 11WA SMOKE DETECTOR, R&R SAME PER AMM: 26-15-12-04 & SAME OP CHECKS NORMAL.Mar 26, 2019 · N744FD · Airbus A300B4622R · Smoke DetectionSDR FDEA201903230702Skin · crackedMDIS 744 54-30 0821 23MAR19 MEM FACT U SKIN CRACKED ON LT SIDE OF NR 2 AFT PYLON BOAT TAIL. SHGN 23MAR19 21:15 MEM REMOVED CRACKED AREA OF SKIN PER SRM 54-55-51, FIGURE 208. SHGN 23MAR19 22:00 MEM ACCOMPLISHED HFEC OF CUTOUT FOR REMOVED DAMAGE. NOMar 23, 2019 · N744FD · Airbus A300B4622R · Nacelle/Pylon, Plate/SkinSDR FDEA201803010549Rod · damagedFLIGHT CREW REPORTED A KRUEGER FAULT DURING LANDING. FOUND THE RT KRUEGER FLAP HANGING DOWN AND DAMAGED. INSTALLED A KRUGER FLAP MOVABLE VANE AND SPRING ROD IAW MM 27-87-12-04. OPS TESTED GOOD.Mar 1, 2018 · N744FD · Airbus A300B4622R · Leading Edge Slat Control SystemSDR FDEA201802140396Bottle · low pressureR1 DOOR ASSIST BOTTLE PRESS LOW INSTALLED RIGHT FWD ENTRY DOOR (R1) DAMPER AND EMERGENCY OPERATION CYLINDER REF 52-10-14-04-01. NO LEAKS NOTED. ACCOMPLISHED ADJ/TEST 52-10-14-05-01. DOOR CHECKS NORMAL.Feb 14, 2018 · N744FD · Airbus A300B4622R · Passenger/Crew DoorsSDR FDEA201802060308Brake · seizedAFTER DEPARTURE DURING CLIMB, RECEIVED AN ECAM FOR HOT BRAKE NR 6. LEVELED AT FL250, SLOWED BELOW GEAR SPEED. TEMPERATURE WENT FROM 300 DEGREES. 305 , 310, AND 315, 320 DEGREES BY THE TIME ACFT WAS SLOW ENOUGH TO PULL GEAR DOWN TO COOL. DIVERTED. THE NR Feb 6, 2018 · N744FD · Airbus A300B4622R · Landing Gear Brake SystemSDR FDEA201712203419Smoke Detector · false activationDURING CLIMB, RECEIVED AN INTERMITTANT AVIONICS SMOKE WARNING AND LIGHTS ON ECAM AND OVERHEAD. THIS LASTED A COUPLE OF MINUTES. CONFIMRED NO SMOKE INDICATION WITH QRH. IT HAD BEEN RAINING DEPARTURE BUT NO PUDDLES SEEN DURING PREFLIGHT. FOUND ALL ULDS WET Dec 20, 2017 · N744FD · Airbus A300B4622R · Smoke DetectionSDR FDEA201711193277Rib · crackedLT CENTER FLAP INTERNAL RIB NR 26 CRACKED AT UPPER SKIN ATTACHMENT 6TH FASTENER FWD OF REPAIR SPAR. REPAIRED THE RIB IAW SRM 57-50-00. CLASSIFIED AS A MAJOR REPAIR.Nov 19, 2017 · N744FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201711193276Rib · crackedLEFT CENTER FLAP INTERNAL RIB NR 27, CRACKED AT UPPER SKIN ATTACHMENT 6TH FASTENER FWD OF REAR SPAR. REPAIRED THE RIB IAW SRM 57-50-00. CLASSIFED AS A MAJOR REPAIR.Nov 19, 2017 · N744FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201711113227Crossbeam · wornMAIN DECK FRAME 64 CROSS TRACK BETWEEN SEAT TRACKS -Y1456 AND -Y1959 THE LOBES ARE WORN. BLENDED AREA IAW SRM 51-74-10, CHECKED LIMITS MAXIMUM MATERIAL REWORK IS 0.021" AFTER REWORK L=0.8", W=0.600", D=0.039" FOUND OUT OF LIMIT IAW SRM 53-10-15, FIG 101, FABRINov 11, 2017 · N744FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA201711113226Seat Track · wornMAIN CARGO DECK SEAT TRACK AT FR 17 -Y953 HAS ELONGATED HOLE AS MARKED. REMOVED FLOOR SUPPORT AND 3 EA BRACKETS IAW SRM 51-40-21, RECEIVED NEW SEAT TRACK BACH 0003212483, LOCATED, DRILLING IAW SRM 51-40-44, INSTALLED NEW SEAT TRACK IAW SRM 51-40-21, NO LIMITS Nov 11, 2017 · N744FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201711113225Floor Support · wornFLOOR SUPPORT BETWEEN FR 11-13 AT Y1456 MAIN CARGO DECK HAS ELONGATED HOLE AS MARKED. EVALUATED LIMITS ON FLOOR SUPPORT BETWEEN FR11-13 AT Y1456, NO LIMITS PER SRM, REMOVED 2 EA FLOOR SUPPORT CHANNELS FOR ACCESS AND REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-40-2Nov 11, 2017 · N744FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201711103217Floor Support · corrodedFLOOR SUPPORT AT FR 14, Y450 MAIN CARGO DECK HAS CORROSION TOP SURFACE AS MARKED. REMOVED CORROSION IAW SRM 51-73-10. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-21. CLASSIFIED AS CAT "A" REPAIR . CORROSION DIM L=2.5, W=1.75, D=.009. NO LIMITS FOUND PER Nov 10, 2017 · N744FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201711103216Floor Support · corrodedFLOOR SUPPORT AT FR 14, Y450 MAIN CARGO DECK HAS CORROSION TOP SURFACE AS MARKED. REMOVED CORROSION IAW SRM 51-73-10. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-21. CLASSIFIED AS CAT "A" REPAIR. CORROSION DIM L=2.5, W=1.75, D=.009. NO LIMITS FOUND PER SRNov 10, 2017 · N744FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201711103215Floor Support · corrodedFLOOR SUPPORT AT FR 14, Y450 MAIN CARGO DECK HAS CORROSION TOP SURFACE AS MARKED. REMOVED CORROSION IAW SRM 51-73-10. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-21. CLASSIFIED AS CAT "A" REPAIR. CORROSION DIM L=2.5, W=1.75, D=.009. NO LIMITS FOUND PER Nov 10, 2017 · N744FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201711103214Floor Support · corrodedFLOOR SUPPORT AT FR 14, Y450 MAIN CARGO DECK HAS CORROSION TOP SURFACE AS MARKED. REMOVED CORROSION IAW SRM 51-73-10. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-21. CLASSIFIED AS CAT "A" REPAIR. CORROSION DIM L=2.5, W=1.75, D=.009. NO LIMITS FOUND PER SNov 10, 2017 · N744FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201711093209Web · crackedFWD CARGO COMPT FR 38.2, -Y 1470 JUST BELOW ROLLER TRAY, WEB HAS CRACK. REMOVED AND REPLACED WEB IAW SRM 51-40-21 FWD CARGO COMPT FR 38.2 - 38.1, -Y 1470. CAT "A" REPAIR, MAJOR.Nov 9, 2017 · N744FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201711093208Web · crackedCRACK ON FLOOR STRUCTURE WEB IN FWD CARGO CMPT FR 20 TO FR 21, Y 1430. REMOVED AND REPLACED WEB ON FWD CARGO CMPT FROM FRAME 20-21 AT SEAT TRACK Y 1430 IAW SRM 51-40-21. CAT "A" REPAIR, MAJOR REPAIR.Nov 9, 2017 · N744FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
Back to N744FD