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.
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
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 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.SDR FDEA2020072761667Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231KG WAS DELAMINATED AT CORNER. REPAIRED FLOOR PANEL BY FABRICATION IAW SRZ-25-005 REV R. MAJOR REPAIR.SDR 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.SDR 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.SDR FDEA2020072761664Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231HG IS CRACKED. REPAIRED FLOOR PANEL 231HG BY FABRICATION IAW SRZ-25-005 REV R. MAJOR REPAIR.SDR FDEA2020072751650Panel · crackedNR 1 PYLON PANEL 413BL OB LOUVERS CRACKED. NR 1 PYLON PANEL 413BL OB LOUVERS REPAIRED PER EA 6-5450-T0355371 P1.SDR 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.SDR FDEA202007211608Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241PF WAS DELAMINATED . FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.SDR FDEA2020072311607Floor Panel · crackedMAIN CABIN FLOOR PANEL 241KJ WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.SDR FDEA2020072311606Floor Panel · crackedMAIN CABIN FLOOR PANEL 242AK WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.SDR FDEA2020072311605Floor Panel · crackedMAIN CABIN FLOOR PANEL 241BK WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.SDR FDEA202007211604Floor Panel · crackedMAIN CABIN FLOOR PANEL 241ZH IS CRACKED FABRICATE NEW FLOOR PANEL IAW SRZ-25-005SDR FDEA202007211602Floor Panel · crackedMAIN CABIN FLOOR PANEL 241YH WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZZ-25-005.SDR FDEA2020072301588Panel · delaminatedNR 1 PYLON PANEL 471AL HAS DELAMINATION. REPAIRED THE NR 1 PYLON PANEL 471AL IAW EA 6-5480-T0354751-P1.SDR FDEA2020072301597Floor Panel · crackedMAIN CABIN FLOOR PANEL 242QF WAS CRACKED, FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.SDR FDEA202007201596Floor Panel · crackedMAIN CABIN FLOOR PANEL 242LH WAS PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005SDR 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.SDR 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.SDR FDEA2020072391580Panel · delaminatedNR 1 PYLON PANEL 474BR WAS DELAMINATED. REPAIRED THE PYLON PANEL IAW EA 6-5451-T0354951-P1.SDR FDEA2020071081473Floor Panel · delaminatedAFT CARGO COMPARTMENT FLOOR PANEL 151DF HAS DENT AND CORNER DAMAGESDR FDEA2020071081472Floor Panel · crushedFWD CARGO COMPARTMENT L/H FLOOR PANEL 131RF HAS DAMAGED EDGE FILLER AND CRUSHED HONEYCOMBSDR FDEA2020071081471Floor Panel · gougedFWD CARGO COMPARTMENT L/H FLOOR PANEL 132YF HAS DAMAGED EDGE FILLER AND GOUGED TOP SKINSDR FDEA2020071081469Floor Panel · delaminatedAFT CARGO COMPARTMENT FLOOR PANEL 152JF HAS DISBONDED LOWER SKIN AND DAMAGED EDGE FILLERSDR FDEA2020071081468Floor Panel · damagedAFT CARGO COMPARTMENT FLOOR PANEL 152AF HAS DAMAGE TO EDGE FILLER AND LOWER SKINSDR FDEA2020071081467Floor Panel · damagedAFT CARGO COMPARTMENT FLOOR PANEL 151BF HAS DAMAGED EDGE FILLER AND TORN LOWER SKINSDR FDEA2020071081466Floor Panel · puncturedAFT CARGO COMPARTMENT FLOOR PANEL 152HF HAS PUNCTURES IN LOWER SKINSDR FDEA2020070871457Floor Panel · damagedMAIN CABIN FLOOR PANEL 221PF IS CRACKED AND PUNCTURED FAB NEW PANEL PER FEDEX SRZ-25-005 REV RSDR FDEA2020070871456Floor Panel · brokenMAIN CABIN FLOOR PANEL 221RF HAS BROKEN CORNER FAB NEW PANEL 221RF IAW FEDEX SRZ-25-005 REV RSDR FDEA2020070871455Floor Panel · puncturedMAIN CABIN FLOOR PANEL 222RF HAD PUNCTURES ON BOTTOM SIDE. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005 REV R.SDR 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.SDR FDEA202006301392Floorboard · brokenMAIN CABIN FLOORBOARD 251ZG HAS CORNER BROKEN OFF. FABRICATED NEW PANEL 251ZG IAW FED EX SRZ 25-005 REV R.SDR FDEA202006301391Floorboard · crackedMAIN CABIN FLOORBOARD 261KF HAS CORNER BROKEN OFF. FABRICATED NEW PANEL 261KF IAW SRZ 25-005 REV R.SDR 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 51-40-21SDR 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.SDR 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. NOSDR 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.SDR 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.SDR 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 SDR 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 SDR 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.SDR 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.SDR 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, FABRISDR 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 SDR 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 51-40-2SDR 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 SDR 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 SRSDR 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 SDR 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 SSDR 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.SDR 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.
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