N748FD
Service difficulty reports · 211
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 = 'N748FD' 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 = 'N748FD' 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 FDEA202607291057Shear Pin · damagedWHILE PERFORMING FREE FALL CHECK, FOUND "NLG" FREE FALL QUADRANT 3 TO MOVE MORE ON SHAFT THAN ADJACTENT MLG FREE FALL QUADRANT 1 DOES ON SHAFT. INSTALLED BUSHING & SHEAR PIN INTO NLG FREE FALL AMM 32-33-00-05, EA 6-3230-T0388190A, COMPLETED OPS CHECK OF LASDR FDEA202607220985Uplock · leakingGREEN HYD RSVR LO LEVEL ECAM ON DEPARTURE. QUANTITY WAS AT ORANGE DOT IN YELLOW BAND. COMPLIED WITH ECAM/QRH. CAPTAIN REPORTED THE ALTERNATE GEAR EXTENSION PROCEDURE WAS USED AS DIRECTED BY RED TABS. RESTORE THE GEAR IAW AMM 32-33-00-02-0. REMOVED AND RESDR FDEA202606180772Slide · fouledPER CREW DEBRIEF, R1 DOOR SLIDE HANDLE HARD TO ARM/DISARM, DOOR OPENING/CLOSING AND LATCHING NOT AFFECTED, DOOR OPERATES NORMAL. RELEASED FOR SERVICE IAW MEL : 52-11-01-01, CREW ENTRY DOOR ESCAPE SLIDE R1 INOP. SLIDE REMAINS INSTALLED ON DOOR. AMM: 25-61SDR FDEA202602210249Girt Bar · unsecureR1 DOOR SLIDE WOULD NOT DISARM . PBI RELEASED FOR SERVICE PER MEL : 52-11-01-01 CATEGORY C. CREW ENTRY DOOR ESCAPE SLIDE R1 - INOP. SLIDE REMAINS INSTALLED ON DOOR." MEL: 52-11-01-001 OK FOR SERVICE. AMM: 12-22-52-00-01, AMM: 25-61-22-04-02, AMM: 52SDR FDEA202602190236Bottle · leakingR1 DOOR ASSIST BOTTLE REQUIRES DIAPHRAGM REPLACEMENT AND SERVICE PER AMM 52_10_14_03_10. REMOVED AND REPLACED R1 DOOR ASSIST BOTTLE DIAPHRAGM. SERVICED NITROGEN TO PLACARD ONBOARD. NO LEAK NOTED. CHECKS GOOD. OKAY FOR SERVICE.SDR FDEA202602130237Bottle · damagedFOUND ON SERVICE CHECK L 1 EMERGENCY OPERATION CYLINDER LOW PER SERVICE CHART. AMM: 52-10-14-03-10 SERVICED L 1 EMERGENCY OPERATION CYLINDER PER REF.SDR FDEA202602050136Gearbox · failedON DEPARTURE, NR 1 ENG REV UNLOCK. RAN QRH, DECLARED EMERGENCY AND RETURNED TO ORF WITHOUT INCIDENT. AMM 78-31-35-04, AMM 78-32-11-05 IAW MOCC REQ (MTSI#78-31/9965) REPLACE ENG 1 SPLITTER GEARBOX. R & R ENG 1 SPLITTER GEARBOX. OPS CK OK. R & R SPLITTERSDR FDEA202601110022Apu · leakingPRIOR TO PUSHBACK, WITH ALL DOORS CLOSED EXCEPT CREW ENTRANCE DOOR, RECEIVED AN ECAM ALERT FOR MAIN DECK CARGO SMOKE DETECTED MID & EXPERIENCED SMOKE IN COCKPIT FROM GASPERS. SMOKE ON SET RAPID & HIGHLY CONCENTRATED. SMOKE CLEARLY VISIBLE IN COCKPIT, APSDR FDEA202508111420Skin · contaminatedEMPENNAGE - RH ELEVATOR UPPER COMPOSITE MATERIAL FOUND ENTRAPPED WATER (LOC: L/E ER13) REPAIRED EMPENNAGE RH ELEVATOR UPPER L/E ER13 ENTRAPPED WATER COMPOSITE MATERIAL PER A300-600 SRM55-21-12-201 PARA.5.J & SRM51-77-12-201. THIS IS CAT B REPAIR AND THE SDR FDEA202508111419Skin · contaminatedEMPENNAGE - LH ELEVATOR UPPER COMPOSITE MATERIAL FOUND ENTRAPPED WATER (LOC: L/E ER2) REPAIRED EMPENNAGE LH ELEVATOR UPPER L/E ER2 ENTRAPPED WATER COMPOSITE MATERIAL PER A300-600 SRM55-21-12-201 PARA.5.J & SRM51-77-12-201. THIS IS CAT B REPAIR AND THE FOSDR FDEA202508011359Longeron · crackedMAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR22 AND FR25 FOUND CRACK SIGNAL ON 4EA FASTENER HOLES REPAIRED THE MAIN DECK CARGO DOOR UPR EDGE PT1 BETWEEN FR22 AND FR25 4EA CRACKED FASTENER HOLES PER EA 6-5230-T0384376, MAJOR REPAIR IAW FEDEX GMM 6-2-100SDR FDEA202507251336Skin · delaminatedLH WING #5 SPOILER CENTER I/B & O/B HINGE ARM UPR SKIN FOUND DELAMINATION. SIZE: (1)30MM*18MM, DEPTH: 2.32MM (2) 82MM*39MM, DEPTH: 1.98MM COMPLIED WITH EA 6-5750-T0384253 REPAIRED LH WING #5 SPOILER CENTER I/B & O/B HINGE ARM UPR DELAMINATED SKIN. MAJOR RESDR FDEA202507251335Skin · delaminatedLH WING #5 SPOILER CENTER I/B & O/B HINGE ARM O/B SIDE SKIN FOUND DELAMINATION. SIZE: (1)30MM*11MM, DEPTH: 1.60MM (2)150MM*15MM, DEPTH: 1.81MM COMPLIED WITH EA 6-5750-T0384253 REPAIRED LH WING #5 SPOILER CENTER I/B & O/B HINGE ARM O/B SIDE DELAMINATED SKISDR FDEA202507251334Skin · delaminatedLH WING #4 SPOILER CENTER I/B & O/B HINGE ARM O/B SIDE SKIN FOUND DELAMINATION. SIZE: (1)40MM*16MM, DEPTH: 1.76MM (2)30MM*22MM, DEPTH: 1.83MM COMPLIED WITH EA 6-5750-T0384250 REPAIRED LH WING #4 SPOILER CENTER I/B & O/B HINGE ARM O/B SIDE DELAMINATED SKINSDR FDEA202507251333Skin · delaminatedRH WING #3 SPOILER CENTER O/B HINGE ARM O/B SIDE SKIN FOUND DELAMINATION. SIZE: 50MM*15MM, DEPTH: 1.80MM COMPLIED WITH EA 6-5750-T0384249 REPAIRED RH WING #3 SPOILER CENTER O/B HINGE ARM O/B SIDE DELAMINATED SKIN. TITLE: WING - FLIGHT SURFACES - RH #3 SPOISDR FDEA202507201360Web · crackedMAIN DECK CARGO COMPARTMENT - UNDER FLOOR FR47 WEB CRACKED BETWEEN Y0 AND -Y450 REPAIRED THE MAIN DECK CARGO COMPARTMENT UNDER FLOOR FR47 CRACKED WEB BETWEEN Y0 AND -Y450 PER A300-600 SRM 53-15-15-201 PARA.5A. THIS IS A CAT B REPAIR. THE FIRST INSPECTION WSDR FDEA202507181362Door Frame · crackedRIGHT FWD PAX DOOR - FRAME SEGMENT AT FR14C FOUND 1EA CRACK REPAIRED THE RH FWD PAX DOOR FRAME FR14C CRACKED SEGMENT PER SRM 51-40-21 AND DWG F52181297 ISSUE: K AND DWG F52181299 ISSUE: G. THIS IS A CAT A REPAIR AND RSC TRACKING EA 6-5210-T0384405 WAS ISSUSDR FDEA202507131361Fitting · damagedCARGO DOOR / HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24 COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MSDR FDEA202502140226Outflow Valve · failedNUMBER 1 OUTFLOW VALVE DEFERRED. AFTER TO #2 OUTFLOW STUCK FULL OPEN. COMPLIED WITH QRH REQUIRED MANUAL CONTROL TO OPEN ON TAXI IN. REMOVED AND REPALACED THE FWD OUTFLAW VALVE ASSY (202HM) I.A.W AMM 21-31-12-04 OPS CHECK PER AMM 21-31-00-5 OPS CHECK PASSSDR FDEA202501220120Electronic Unit · failedIN SYS 1 LANDING GEAR POSITION DETECTOR, TOOK OFF AND ATTEMPTED TO RAISE GEAR. UNABLE. WENT TO SYSTEM 2, GEAR CAME UP, BUT WE GOT MULTIPLE FAILURES. PITCH TRIM 1, ATS, CAPT PITOT OVERHEAT, FO PITOT OVERHEAT, STBY PITOT OVERHEAT, CAPT TAT HEAT FAILURE, CABSDR FDEA202410211569Power Supply · failedON MX PREFLIGHT: JUMPSEAT AREA EMERGENCY LIGHTS INOP. REPLACED EMERG. SUPPLY BATTERY IAW A300-600 AMM CH. REF. LISTED ABOVE. OPS CKS GOOD. A/C OK FOR SERVICE.SDR FDEA202407311071Warning Light · inoperativeON POSTFLIGHT, R1 DOOR ESCAPE SLIDE RELEASE WARNING LIGHT INOP, BUZZER OPERATES NORMALLY. RELEASED FOR SERVICE PER MEL : 52-XX-XX-XX CAT C EXP : AUG24 - R1__ CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM LIGHTS - INOP." R1 DOOR BUZZER OPERATES NORMAL, SDR FDEA202407100980Hydraulic System · lowREJECTED TAKE OFF AT 40KTS FOR BLUE HYDRAULIC LOW ECAM CAUTION.SDR FDEA202401230128Selector · inoperativePERFORMED CAT III AUTOLAND WITH LOW BRAKES. DURING ROLLOUT PHASE, AIRCRAFT PULLED TO THE RIGHT WHEN AUTO BRAKES APPLIED. REQUIRED TO DISCONNECT AUTOPILOT AND RECENTER AIRCRAFT. WHEEL ECAM PAGE SHOWED RIGHT MAIN GEAR TEMPERATURE BETWEEN 450-500 DEGREES DEGRESDR FDEA202304200865Skin · dentedFUSELAGE SKIN FOUND 1EA DENT AT FR99 PLUS 5",S-4L PLUS 5" REPAIRED THE DAMAGE AREA WITH DOUBLER, THIS IS CAT.A REPAIR I.A.W A300-600 SRM 53-19-12- 201, PARA.5, FIG.201, PAGE.204~208 "MAJOR REPAIR"SDR FDEA202304200794Skin · delaminated1EA WATER TRAPPED AREA(140MM X 180MM) WAS FOUND AT L/H ELEVATOR UPPER SKIN PANEL T/E NO.26 SCREW. ACCOMPLISHED THE COMPOSITE REPAIR, THIS IS CAT.B REPAIR I.A.W A300-600 SRM 55-21-12-201- 2, PARA.5F(REPAIR NO.6) PAGE.239-243, FIG.209(SHEET1-2) & SRI:55-21-SDR FDEA202201080025Warning Message · false activationON FINAL APPROACH ON RW 27, KMEM AT 3000 FT, GOT A SPOILER FAULT WITH #7 SPOILER SHOWING UP. DID ECAM & QRH PROCEDURE AND COULD NOT GET IT TO GO DOWN. DECLARED AN EMERGENCY AND LANDED ON RW 36C, BRAKES WERE NOT SHOWING HOT. TAXIED BACK TO THE RAMP. SSDR FDEA202112283154Sensor · faultedHI ENG OIL TEMP #1, GOT INITIAL ADVISORY AT CRUISE LEVELOFF 35,000; 168C. FOLLOWED QRH ADVISORY WHICH LED TO ENG OIL HI TEMP QRH PROCEDURE. TEMPERATURE PEAKED AT 176C, SHOWED 36C TO 40C HOTTER THAN #2 ENG DURING DESCENT AT FLIGHT IDLE. EMERGENCY DECLARED,SDR FDEA202107051678Spar · damagedDURING THE EO NO: E 6-5710-E0342809 B P3 PARA. 5, FOUND THE HOLE "I" HAD BEEN ENLARGE ACCOMPLISHED THE WORK: REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE/FRAME 47 FASTENER HOLE I REPAIR I.A.W. A300-600 EA NO: T6-5710-T0362021 P1, SEQ NO: 001077SDR FDEA202107021649Frame · crackedDURING EA NO: T 6-5710-T0307375 P2, FOUND HOLE "S" DEVIATION. ACCOMPLISHED THE WORK: REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE/FRAME 47 FASTENERS HOLES CRACK REPAIR I.A.W. A300-600 EA NO: T6-5710- T0307375 A P3, SEQ NO: 001079.SDR FDEA202106171559Panel · crackedPFM E.O. NACELLES /PYLONS INSP FOUND NO.2 PYLON O/B SIDE PNL AT RIB 8 HAS CRACK ALONG FRONT SCREW HOLE IAW WORK CARD SEQ 000960 INSPECTION OF PYLON SIDE PANELS AT RIB 8 AIRBUS SBA300-54- 6015 R03 & A310-54-2018 R03 E.O. 6-5450-7-5003 H PT4 SUBSTEP A. THRUSDR FDEA202106121517Floor Panel · damagedTHE #232RG FLOOR PANEL OF MDC WAS FOUND EDGE BROKEN REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201, PAGE 205-206, PARA 9.A, FIG 201.SDR FDEA202106121516Floor Panel · damagedTHE #232CF FLOOR PANEL OF MDC WAS FOUND EDGE BROKEN REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201, PAGE 205-206, PARA 9.A, FIG 201.SDR FDEA202106121515Floor Panel · damagedTHE #241PH FLOOR PANEL OF MDC WAS FOUND EDGE BROKEN REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201, PAGE 205-206, PARA 9.A, FIG 201.SDR FDEA202106121514Floor Panel · damagedTHE #262XF FLOOR PANEL OF MDC WAS FOUND EDGE BROKEN REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201, PAGE 205-206, PARA 9.A, FIG 201.SDR FDEA202106121513Floor Panel · damagedTHE #152GF FLOOR PANEL OF LOWER AFT CARGO COMPARTMENTS WAS FOUND EDGE BROKEN REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201, PAGE 205-206, PARA 9.A, FIG 201.SDR FDEA202106121512Floor Panel · brokenTHE #132RF FLOOR PANEL OF LOWER FWD CARGO COMPARTMENTS WAS FOUND EDGE BROKEN REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201, PAGE 205-206, PARA 9.A, FIG 201.SDR FDEA202106121511Floor Panel · damagedTHE #162HF FLOOR PANEL WAS FOUND SOFTEN & SERIOUS DAMAGED OVER HALF AREA FABRICATED THE FLOOR PNL I.A.W. FEDEX DWG. SRZ-25-005, REV. R AND SRZ25-011, REV. E.SDR FDEA202106071453Seat Track · gougedMAIN DECK SEAT TRACK CROWN AREA GOT A GOUGE AT FR 59,-Y450 PERFORM CUT OUT DAMAGE TRACK ( LENGTH 30.6") & REINFORCED REPAIR PART AND SPLICE U- SECTION WORK INSTUCTION I.A.W A300-600 SRM SUPPLEMENT 53-10-16-201, PARA 5 FG 202, P. 209-214SDR FDEA202106071451Seat Track · gougedMAIN DECK FLOOR SEAT TRACK CROWN FOUND GOUGE BTWN FR26 16" AND FR26 18". ACCOMPLISHED THE FLOOR SEAT TRACK REPAIR I.A.W. A300-600 SRM 53-10-16-201, PARA. 10, FIG. 208 (SHEET 1) P. 243-248.SDR FDEA202106071454Skin · delaminated2EA DELAMINATIONS WERE FOUND. AREA 1 (80CM2) NEAR O/B HINGE ARM OF RH SPOILER 4. AREA 2 (82CM2) NEAR I/B HINGE ARM OF RH SPOILER 4. ACCOMPLISHED THE WORK: WING - FLIGHT SURFACES - RH 4# SPOILER LOWER SKKIN DELAMINATION NEAR CENTER HINGE ARM REPAIR I.A.W.SDR FDEA202106071452Seat Track · gougedM/D Y1456 SEAT TRACK CROWN GOUGE AT FR66 12.5" ACCOMPLISHED THE SEAT TRACK REPAIR I.A.W. A300-600 SRM SUPPLEMENT 53-10-16-201, PARA. 5, FIG. 202, P. 209-214.SDR FDEA202106021432Skin · dentedLH WING O/B FLAP L/E NOSE GOT A DENT AT RIB17 5". ACCOMPLISHED THE DENTED AREA REPAIR I.A.W. A300-600 SRM 57-50-00-201, PARA. 4H, P. 230- 234, FIG. 208. THIS IS CAT. B REPAIR I.A.W. A300-600 SRM 57-50-00-201, P. 202 AND SRI 57-50-00-201 IIR 57-50- 00-2- 00SDR FDEA201906291441Power Supply · inoperativeMDIS 748 52-70 3083 29JUN19 MEM FACT U WHILE TROUBLESHOOTING R1 DOOR, PERFOMED BITE TEST OF ASPSU REF AMM 52-73-00-05-01 AND FOUND TEST TO BE FAILING. SHOWS BAT 1 AND BAT 2 FAILURE. REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: POS: ONSDR FDEA201906161314Switch · chafedRT SIDE ENTRY DOOR, IN FLIGHT, MAKING LOUD SQUEAL AND HAS A FLASHING RED LIGHT. INDICATIONS WERE NORMAL WHEN ARMED ON THE GRD. COCKPIT INDICATIONS NORMAL. DURING FLIGHT. CORRECTED ITSELF AFTER LANDING WITH NO PRESSURIZATION IN CABIN AREA. TROUBLESHOT REF SDR FDEA201905291181Limit Switch · out of adjustAFTER FLIGHT, JUMPSEATER REPORTED THAT RIGHT CREW ENTERY DOOR (R1) WAS BEEPING AND PRESSURE LIGHT WAS ON ABOVE 10,000 FEET. THERE WERE NO INDICATIONS IN THE COCKPIT. ADJUST R1 DOOR LIMIT SWITCH 10WN REF. MM 52-73-13-05-01 FIGURE 501. OPS CHECKED GOOD, RETURN SDR FDEA2019042520880Floor Panel · delaminatedFLOOR PANEL P/N A5398408500600 IS CRUSHED ON THE INBOARD SIDE OF TOP PANEL AND MISSING A SECTION OF PANEL. FABRICATED NEW FLOOR PANEL PER DWG SRZ-25-005 REV PSDR FDEA2019041630791Indicator · malfunctionedREJECTED TAKE-OFF TO STAGNATED AIRSPEED @ 100 KIAS BOTH CAPT AND F\O AIRSPEED INDICATORS. PERFORMED RTO CHECK LIST. NO BRAKE FANS INSTALLED ON THIS AIRCRAFT, TAXI BACK TO GATE 823 WITH HOT BRAKES, MOST TEMPS ON BRAKES WERE ABOVE 440 ON RIGHT ECAM. TRSDR FDEA201903130586Selector Valve · inoperativeON GEAR EXTENSION GEAR DID NOT COME DOWN RECYCLEED GEAR 3 REDS PROC "MAIN GEAR EXT"ACCOMPLISHED PER QRH. POS DET 1& 2. GOT TOWED TO RAMP. HYD SYST NORMAL IN FLIGHT AFTER BLOCK IN GREEN SYST OFF SCALE HIGH. RESET MANUAL GEAR EXTENSION TO NORMAL POSITION IAW AMMSDR FDEA201811103179Restrictor Valve · dirtyLEFT MAIN GEAR TOOK AN EXTRA 20 SECONDS TO COME DOWN WE ALMOST HAD TO GO AROUND. REMOVED AND CHECKED LEFT MAIN GEAR VALVE AND GEAR DOOR RESTRICTOR VALVES. FOUND DIRT IN GEAR RESTRICTOR VALVE. REPLACED GEAR RESTRICTOR PER AMM 32-31-57-04 AND GEAR DOOR RESTRICTO
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