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 FDEA202511142182Diaphragm · damagedL1 DOOR EMERGENCY ASSIST BOTTLE PRESSURE LOW. REPLACED DIAPHRAGM (PN# FE240-221-001, SN# N/A) IN THE PERCUSSION MECHANISM OF THE L1 DOOR ASSIST CYLINDER. NO PRESSURE DROP AFTER 4 HRS. LEAK CKS GOOD. REMOVED FROM MEL.SDR FDEA202508121409Selector Valve · faultedLANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF. L/G RETRACTION FAULT ON ECAM. EMERGENCY DECLARED. COMPLIED WITH ECAM AND QRH. EMERGENCY DECLARED. AMM: 32-31-12-04, REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE 3GA, OPS AND LEAK CHECK GOOD IAW ABOVE AMSDR FDEA202506050846Slide Raft · not reportedLH #1 PASSENGER / CREW DOOR SLIDE / RAFT REPLACEMENT. PER AMM 25-61-22-04-01 REMOVED THE SLIDE / RAFT OF L1 PASSENGER / CREW DOOR (CPN: 2513882 MPN: D30546-509FX SN: A5687 POS: L1) PER AMM 25-61-22-04-01 INSTALLED THE SLIDE / RAFT OF L1 PASSENGER / CRSDR FDEA202505290890Rib · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND CRACK AT RIB15 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA: 6-5750-T0383581 P1, TITLE: WINGS - FLIGHT SURFACES - RH CENTER FLAP RIB 15 UPPER FLANGE AND BOTTOM SKIN REPAIR - RSC TRACKING. AND PER A300-600 SRM 57-50-SDR FDEA202505290889Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND CRACK AT RIB13 BETWEEN STGR2.6 AND STGR2.7 COMPLIED WITH EA: 6-5730-T0336655 A P2, TITLE: WINGS - PLATES AND SKINS - LH WING CENTER FLAP - SRM REPAIRS - RSC TRACKING. AND PER A300-600 SRM 57-50-00-201 FIG.201 REPAIRSDR FDEA202505290888Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB26 B/W STGR2.6 AND STGR2.8 COMPLIED WITH EA: 6-5730-T0336655 A P2, TITLE: WINGS - PLATES AND SKINS - LH WING CENTER FLAP - SRM REPAIRS - RSC TRACKING. AND PER A300-600 SRM 57-50-00-201 FIG.201 REPAIRESDR FDEA202505290817Fitting · failed inspMAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR23 AND FR24 FOUND CRACK SIGNAL ON 4EA FASTENER HOLES COMPLIED WITH EA: 6-5230-T0383430. TITLE: DOORS - CARGO DOOR/HYD SYS - CRACKED HOLES ON MAIN DECK CARGO DOOR UPPER LONGERON. REPAIRED THE MAIN DECK CARGO SDR FDEA202505290816Fitting · failed inspCOMPLY WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24. COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - CARGSDR FDEA202505290815Door Frame · crackedLH FWD PAX DOOR FRAME SEGMENT AT FR14C FOUND 1EA CRACK REPLACED LH FWD PAX DOOR CRACKED FRAME SEGMENT AT FR14C WITH A FABRICATED PART PER A300-600 SRM51-40-21 AND DWG: F52181297 (ISSUE.K), F52181299(ISSUE: A). RSC TRACKING EA 6-5210-T0383529 RAISED AND ACCSDR FDEA202505290814Door Frame · crackedRT FWD PAX DOOR FRAME SEGMENT AT FR14C FOUND 1EA CRACK REPLACED RH FWD PAX DOOR CRACKED FRAME SEGMENT AT FR14C WITH A FABRICATED PART PER A300-600 SRM51-40-21 AND DWG: F52181297 (ISSUE.K), F52181299(ISSUE: A). RSC TRACKING EA 6-5210-T0383528 RAISED AND ACCSDR FDEA202505260812Skin · delaminatedLH WING #5 SPOILER CENTER O/B HINGE ARM UPPER SKIN FOUND DELAMINATION. SIZE: 63MM* 40MM, DEPTH: 1.56MM COMPLIED WITH EA: 6-5750-T0383369 P1 , TITLE: WING - FLIGHT SURFACES - LH #5 SPOILER TOP SKIN UPPER SURFACE DELAMINATION ABOVE CENTER HINGE ARM. AND PER SDR FDEA202505260811Skin · delaminatedRH WING #5 SPOILER CENTER I/B HINGE ARM UPPER SKIN FOUND DELAMINATION. SIZE: 35MM* 13MM, DEPTH: 1.50MM; CENTER O/B HINGE ARM UPPER SKIN FOUND DELAMINATION. SIZE: 95MM*45MM, DEPTH: 1.45MM COMPLIED WITH EA: 6-5750-T0383370 P1 , TITLE: WING - FLIGHT SURFACES SDR FDEA202505200781Skin · damagedNDT INSP FOUND RH ELEVATOR INBD UPPER SURFACE TRAPPED WATER AS MARK COMPLIED WITH EA: 6-5520-T0383449 P1, EA TITLE: STABILIZERS - ELEVATORS - RH ELEVATOR UPPER SKIN WATER INGRESS REPAIR, AND A300-600 SRM55-21-12-201 PARA.5.J FIGURE 212 REPAIRED RH ELEVATORSDR FDEA202505200780Skin · damagedNDT INSP FOUND RH ELEVATOR MID UPPER SURFACE TRAPPED WATER AS MARK COMPLIED WITH EA: 6-5520-T0383449 P1, EA TITLE: STABILIZERS - ELEVATORS - RH ELEVATOR UPPER SKIN WATER INGRESS REPAIR, AND A300-600 SRM55-21-12-201 PARA.5.J FIGURE 212 REPAIRED RH ELEVATOR SDR FDEA202501130062Bottle · low pressureR-1 DOOR DAMPER NEEDS TO BE SERVICE. SERVICED R1 DOOR DAMPER TO WITHIN LIMITS PER AMM 52-10-14-03-01 STEP 3.D.(12).SDR FDEA202501100056Bottle · no testWHILE OPENING R1 DOOR HEAR SIGNIFICANT POP SOUND. CLOSER INSPECTION FOUND BOLT THAT ATTACHES ASSIST CYLINDER TO FITTING FOR SNAPPED OFF( APPEARS TO HAVE AXIAL FATIGUE CRACK SEE PIC), ASSIST BOTTLE IS IN NORMAL OPPERATION RANGE, AND NO OTHER DEFECTS NOTED.SDR FDEA202501070031Bottle · low pressureL1 EMERGENCY DAMPER CYLINDER BELOW MIN CHARGE. AMM 52-10-14-03-01 SERVICED L1 DAMPER CYLINDER PER PLACARD AND ABOVE AMM 52-10-14-03-01 STEP 3.D.(12)SDR FDEA202412201821Battery · no testCOURIER AREA "EMERGENCY TEST" SW. 25WL DOESN'T ILLUMNIATE FOR 30 SEC. DURING OPS TEST OF EMERGENECY POWER SUPPLY UNITS. R & R EPSU AND BATTERY, REF AMM 33-51-14-04, OP'S CHECKS GOOD.SDR FDEA202311210104Switch · inoperativeDURING PREFLIGHT CHECKS, EMERGENCY LIGHT TOGGLE SWITCH WAS STUCK IN OFF POSITION AND BROKE OFF WHEN MOVED TO ARM POSITION. NO REFERENCE REQUIRED PLACED EMERGENCY LIGHT SWITCH TO OFF/DISARM POSITION. LRD U IDENTIFIED PARTS TOGGLE SWITCH. COURIER COMPASDR FDEA202302080348Firewall · noneAPU BULKHEAD FIRE WALL FOUND 4EA RIVETS LOOSEN. REPAIRED THE DAMAGE AREA WITH DOUBLER AND FILLER I.A.W EA NO:6-5310-T0372952 P1 , SEQ NO:000818 , TITLE:FUSELAGE-MAINFRAME-FR95 FIREWALL WEB ELONGATED FASTENER HOLES AND DOUBLER REPAIR.SDR FDEA202301200343Flap · dentedFOUND DENTS ON LOWER SKIN OF LH INNER FLAP O/B T/E. ACCOMPLISHED THE EXTERNAL DOUBLER REPAIR (CAT.A) I.A.W EA NO:6-5750-T0372824 P1, SEQ NO:000815, TITLE:WING-FLIGHT SURFACES-LH INNER FLAP TRAILING EDGE LOWER SKIN REPAIR NEAR RIB28A. MAJOR REPAIRSDR FDEA202301150208Floor Panel · damagedTHE #143DF KEEL BEAM FLOOR WAS FOUND SOFTEN AND CAUSE BY HYD FLUID CONTAMINATION FABRICATED NEW FLOOR PANEL I.A.W FEDEX STANDARD REPAIR DRAWING - FLOOR PANEL REPLACEMENT NO: SRZ-25-005 REV.R MAJOR REPAIRSDR FDEA202206071392None · unknownPDIS 744 32-40 3862 07JUN22 MEM FACT U WHEN THE LANDING GEAR WAS EXTENDED FOR LANDING AT KMEM, THE LEFT BRAKE INDICATED 600LBS AND THE RIGHT BRAKE INDICATED 250LBS. STILL SHOWS 600 LEFT, 250 RIGHT. ***EMERGENCY DECLARED*** IDENTIFIED PARTSSDR FDEA202204130955Packing · damagedAT FL 270 RECEIVED ECAM HYD GRN SYS LO PSI, THEN LO RESERVOIR. IMMEDIATELY TURNING OFF GRN SYS PUMPS TO PREVENT PUMP DAMAGE. CONFIRMED BOTH ECAM & OVERHEAD GRN SYS RES LOW. MANUAL GEAR EXTENSION QRH CHECKLIST. DURING DESCENT & DURING FINAL CONTINUED TO SDR FDEA202204070886None · nonePDIS 744 32-30 3672 07APR22 MEM OPEN U LANDING GEAR WOULD NOT COME DOWN. REFERENCED QRH. L/G GRAVITY EXTENSION ACCOMPLISHED. GEAR CAME DOWN. FOUND PROXIMITY DETECTOR PROCESSING UNIT (PDPU, 54GB) WITH RED FAULT LIGHT ON. RECALLED MEMORY ANDSDR FDEA202008181922Skin · delaminatedVERTICAL LEADING EDGE DAMAGE REPAIR VERTICAL LEADING EDGE. MULTPLIE SPOTS OF COMPOSITE SEPARATED AND EXPOSED, 10 AREAS OF DAMAGE ON THE RT SIDE OF VERTICAL STAB, REPAIRED THE VERTICAL LEADING EDGE 10EA AREA IAW SRM 55-31-12-20-2, PARA 2.A, SRM 51-77-11, FIGSDR FDEA2020081821888Skin · crackedLEFT WING LE PANEL 513AB ACCESS LAND IS CRACKED AT AFT IB AREA ACCOMPLISHED REPAIR DOUBLER ON L/W L/E PANEL LAND IAW A300-600SRM 53-15-63, FIG.201SDR FDEA2020081421869Frame · damaged10 EA FASTENER IS LEAKING FUEL AT FRAME 47 WING ROOT AREA FRAME 47 WING ROOT AREA 10EA FASTENERS REPAIRED PER EA # 6-5710-T0355031 P1.
SDR FDEA2020081211862Skin · dentedWHILE ACCOMPLISHING REPAIR OF DENT AFT OF L-1 DOOR, FASTENER HOLES DRILLED INTO CHEM MIL. COMPLIED WITH EA 6-5330-T0355104-P1.SDR FDEA202008081835Spoiler · gouged#2 SPOILER HAS GOUGE ON O/B FACE OF SPAR AROUND NUTPLATE HOLE REPAIRED RIGHT WING #2 SPOILER IAW FEDEX EA 6-5750-T0355493-P1, TITLE: WINGS - FLIGHT SURFACES - RH WING - NO. 2 SPOILER, SPAR OUTBD END, GOUGESDR FDEA2020081081835Spar · gougedNR 2 SPOILER WAS GOUGED ON THE OTBD FACE OF THE SPAR AROUND NUTPLATE HOLES. REPAIRED IAW EA 6-5750-T0355493-P1.SDR FDEA202008071798Seat Track · gougedMAIN CABIN SEAT TRACK WAS GOUGED AT FRAME 60, RBL 78. REMOVED AND REPLACED THE SECTION OF SEAT TRACK IAW SRM 53-10-16, FIG 208.SDR FDEA202008071797Seat Track · gougedMAIN CABIN SEAT TRACK WAS GOUGED AT FRAME 58, RBL 78. REMOVED AND REPLACED THE SEAT TRACK SECTION IAW SRM 53-10-16, FIG 208.SDR FDEA2020080751771Bulkhead · crackedNO.1 ENG INLET, O/B SIDE, AFT BULKHEAD CRACKED AROUND SENSE LINE ELBOW. REPAIRED #1 ENG INLET, O/B SIDE, AFT BULKHEAD AT SENSE LINE PER P&W SRM 54-10-00 FIG. 201.SDR FDEA202008031763Skin · corrodedNR 4 LIGHTNING STRIP, OUTBOARD OF NR 3, RT ELEVATOR HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED THE NR 4 LIGHTNING STRIP IAW SRM:55-21-12 PARA 5.E.SDR FDEA202008031762Skin · corrodedNR 3 LIGHTNING STRIP, OUTBOARD OF NR 2, RT ELEVATOR HAS SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED NR 3 LIGHTNING STRIP IAW SRM 55-21-12 PARA 5.E.SDR FDEA202008031761Skin · corrodedNR 2 LIGHTNING STRIP, OUTBOARD OF NR 1, RT ELEVATOR HAS SEVERAL AREAS OF CORROSION REMOVED AND REPLACED NR 2 LIGHTNING STRIP IAW SRM: 55-21-12 PARA 5.ESDR FDEA202008031760Skin · corrodedNR 1 LIGHTNING STRIP, MOST INBOARD. RT ELEVATOR HAS SEVERAL AREAS OF CORROSION REMOVED AND REPLACED THE NR 1 LIGHTNING STRIP INBD RT ELEVATOR IAW SRM: 55-21-12, PARA 5.ESDR FDEA2020082001752Skin · delaminatedRIGHT ELEVATOR UPPER SKIN CONDUCTOR STRIP AT RIB ER2 DELAMINATED. REPAIRED THE AREA AT RIB ER2 ADJACENT TO THE RT ELEVATOR UPPER SKIN IAW SRM: 55-20-00, & 55-21-12 PARA 5.E. REMOVED & REPLACED THE LIGHTNING CONDUCTOR STRIP IAW SRM: 55-21-12, PARA 5.E. MAJORSDR FDEA2020080321757Panel · crackedNR 1 PYLON PANEL 413BL FWD INSIDE IB CORNER CRACKED UNDER SEAL. REPAIRED NR 1 PYLON PANEL 413BL FWD INSIDE IB CORNER IAW SRM 54-52-51.SDR FDEA202008021756Panel · crackedNR 1 PYLON PANEL 473BL FWD INSIDE OB CORNER CRACKED UNDER SEAL. REPLACED THE NR 1 PYLON PANEL 713AL FWD OB CORNER IAW SRM 54-52-51SDR FDEA2020080321752Skin · delaminatedRIGHT ELEVATOR UPPER SKIN CONDUCTOR STRIP AT RIB ER2 DELAMINATED REPAIRED DELAMINATED AREA AT RIB ER2 ADJACENT TO RH ELEVATOR UPPER SKIN IAW A300- 600 SRM: 55-20-00 & 55-21-12 PARA 5.E. REMOVED & REPLACED LIGHTNING CONDUCTOR STRIP IAW A300-600 SRM: 55-21-12SDR FDEA2020080311739Panel · crackedNR 2 PYLON PANEL 423BL FOUND TO BE CRACKED ON THE OUTBOARD SIDE NR 2 PYLON PANEL 423BL. REPAIR IAW EA 6-5450-T0355366, P1.SDR FDEA202007271679Floor Panel · delaminatedAFT CARGO COMPARTMENT FLOOR PANEL 152FF HAS DISBONDED UPPER SKIN AND DAMAGED EDGE FILLER FABRICATED PANEL IAW SRZ-25-005 REV:R MAJOR REPAIRSDR FDEA202007271678Floor Panel · delaminatedAVIONICS FLOOR PANEL 122JF HAS CORNER DAMAGE FABRICATED PANEL 122JF IAW FEDEX SRZ-25-005 REV: R MAJOR REPAIRSDR FDEA202007271677Floor Panel · delaminatedAFT CARGO COMPARTMENT FLOOR PANEL 152EF HAS DISBANDED UPPER SKIN AND CORNER DAMAGE FABRICATED PANEL 152EF IAW FEDEX SRZ-25-005 REV: R MAJOR REPAIRSDR FDEA202007271676Floor Panel · delaminatedAVIONICS FLOOR PANEL 121JF HAD CORNER DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005, REV R. MAJOR REPAIR.SDR FDEA2020072761671Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231LG WAS CRACKED AT THE CORNER. REPAIRED THE FLOOR PANEL BY FABRICATION IAW SRZ-25-005, REV R. MAJOR REPAIR.SDR FDEA2020072761670Floor Panel · puncturedMAIN CABIN FLOOR PANEL 231UG HAS 2 EA. PUNCTURES ON BOTTOM SIDE. REPAIRED FLOOR PANEL BY FABRICATION IAW SRZ-25-005, REV R, MAJOR REPAIR.SDR FDEA2020072761669Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231JG WAS CRACKED. REPAIRED THE FLOOR PANEL BY FABRICATION IAW SRZ-25-005, REV R. MAJOR REPAIR.
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