N749FD
Service difficulty reports · 180
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 = 'N749FD' 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 = 'N749FD' 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 FDEA202608071109Skin · corrodedAVIONICS COMPARTMENT FR 18 - 19, STRINGERS 50L - 51L INNER SKIN CORRODED. REPAIRED THE CORRODED SKIN AT AVIONICS COMPARTMENT FR18 - FR19, S50L - S51L. THIS IS CATEGORY B REPAIR DUE TO AWAITING FURTHER DAMAGE TOLERANCE ASSESSMENT(DT) APPROVAL. SOLUTION LIFE ORSDR FDEA202607301137Fitting · noneCARGO 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 C P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THSDR FDEA202607221060Skin · puncturedLH WING SLAT #2 LOWER SKIN BETWEEN INBOARD RIB AND RIB 2 FOUND PUNCTURE. COMPLIED WITH EA 6-5750-T0388161 P1. LH WING SLAT #2 LOWER SKIN PUNCTURED AREA BETWEEN INBOARD RIB AND RIB 2. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 57SDR FDEA202504110588Harness · inoperativeFO LEFT SHOULDER HARNESS WON T RELEASE LEFT SHOULDER HARNESS INERTIAL REEL DOES NOT MOVE EVEN WITH THE LOCK RELEASED. ORDER SEAT AS REQUIRED REMOVED AND REPLACED FIRST OFFICER SEAT SAFETY HARNESS PER AMM 25-11-63-04-01. OPS CHECK OKSDR FDEA202504010547Hydraulic System · faultedHYD GREEN RSVR LO LEVEL. COMPLIED WITH QRH AND ECAM. LANDED UNEVENTFULLY. ***EMERGENCY DECLARED*** MX PERFORMED A DVI OF THE THE A/C NO LEAKS NOTED. MX SPOKE WITH THE FLIGHT CREW AT 32,000 FT THE GOT A LOW LEVEL ON THEIR GREEN HYD SYSTEM AND THEY PERFORMSDR FDEA202503170450Slide · malfunctionedRIGHT SIDE SLIDE WILL NOT ARM. AMM: 52-73-00-05-01 RESET ASPSU AND C/W ADJ/TEST IAW A300-600 AMM CH. REF. LISTED ABOVE. ALL DOOR INDICATIONS AND WARNINGS OPS CK NORMAL. A/C OK FOR SERVICE.SDR FDEA202503040328Lug · corrodedRIGHT HAND WING AFT PINTLE FWD LUG HAS EVIDENCE OF CORROSION BETWEEN BUSHINGS "D" AND "E". ACCOMPLISHED REPAIR ON EA # 6-5710-T0306535 B PART 2 "WINGS - BASIC WING STRUCTURE - R/H RIB 5 LUG HAS CORROSION" STEPS 1 - 9.SDR FDEA202503040327Lug · corrodedLEFT HAND WING AFT PINTLE FWD LUG HAS EVIDENCE OF CORROSION BETWEEN BUSHINGS "D" AND "E". ACCOMPLISHED REPAIR ON STEPS 1-9 OF EA # 6-5710-T0382242 " WINGS - BASIC WING STRUCTURE - L/H MLG RIB 5, FWD LUG - CORROSION". MAJOR REPAIR.SDR FDEA202409051245Hydraulic Line · leakingAFTER DEPARTING KSDF LEFT ECAM DISPLAYED GREEN HYD SYS LO PR. AFTER RUNNING STEPS ON ECAM AND FOLLOWED QRH WHICH LED TO GRAVITY EXTENSION OF THE LANDING GEAR BECAUSE THERE WAS NO GREEN HYDRAULIC FLUID.SDR FDEA202402220246Angle · bentFUSELAGE AFT TAIL SECTION FR86 TO FR87 FOUND 2EA ANGLES DEFORMED. DEFORMED ANGLES REMOVED AND REPLACED NEW ONE INSTALLED WITH RIVETS.(2EA) I.A.W A300-600 SRM 51-72-10-001, PAGE.2 AND SRM 51-40-21-001, PARA.6, PAGE.7B-23. REPAIR CLASSIFIED AS MINOR PER GMM SDR FDEA202401300354Skin · cracked1EA CRACK INDICATION WAS FOUND AT R/H FR54, STR44 FASENTER HOLE. ACCOMPLISHED THE TRIM-OUT REPAIR AND REINFORCED WITH SHIM & EXTERNAL DOUBLER AT FR54 S-44R, THE REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 I.A.W FEDEX EA:T6-5330- T0378095 P1, SEQ NO:974, TITLSDR FDEA202401270301Fitting · cracked1EA CRACK(7MM) WAS FOUND AT LH WING FR40 LOWER OUTBOARD RADIUS AREA. ACCOMPLISHED TRIM OUT INSTALLED WITH FILLER & COVER PLATE I.A.W EO:E6-5710- E0333574 I P23, SEQ NO:955 & EA:T6-5710-T0378152 P1, SEQ NO:965, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 (AT SDR FDEA202401250302Skin · damagedAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON FWD CARGO DOOR INNER SKIN AT FR21, BEAM1 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CSDR FDEA202401250125None · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER2 PLUS 3", T/E-39" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENSDR FDEA202401250124None · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER2 PLUS 3",T/E-20" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTSDR FDEA202401240306Frame · cracked1EA CRACK WAS FOUND AT THE RIVET HEAD OF THE SEAL RETAINER RUN OUT HOLE AT FRAME 73A RH. ACCOMPLISHED THE SPLICE REPAIR AT RH DOOR FRAME FR73A I.A.W FEDEX EA NO:T6-5310- T0377912 P1, SEQ NO:971, TITLE:FUSELAGE-MAINFRAME-E0 6-5310-E0327267(SB A300-53-6175) SDR FDEA202401230277Web · crackedFWD CARGO COMPARTMENT WAS FOUND WEB CRACK AT FR21,S-44L-2" REPLACED THE CRACK WEB WITH NEW ONE AT FR21, S-44L-2" I.A.W A300-600 SRM 51-72-10-001, PAGE 2 AND SRM 51-40-21-001, PARA 6, PAGE7B-23, REPAIR CLASSIFIED AS MINOR PER GMM 6-2- 100.SDR FDEA202401230218Panel · deformedAFT CGO DOOR CUTOUT UPR FWD CORNER FOUND PANEL DEFORM FR59A~FR61, STR 28R. REPLACED THE PLATE WITH NEW PART. IAW A300-600 SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B ~ PAGE.23SDR FDEA202401230217Floorbeam · crackedFLOOR STRUCTURE CROSS BEAM SUPPORT ANGLE CRACK AT FWD E/E COMPARTMENT FR10, PLUSY953MM POS REPLACED THE ANGLE WITH NEW ONE I.A.W A300-600 SRM 51-72-10-001, PAGE.2.SDR FDEA202401230137Floorbeam · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON AFT CARGO COMPT FLOOR CROSSBEAM BTW -Y140 ~ -Y805, FR63 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING RESDR FDEA202401220212Bracket · corrodedAFT CGO COMPT FWD PARTITION LINING SUPPORT FOUND CORROSION AT FR 54 UNDER FLOOR STRUCTURE Y450~Y-450 CORROSION BRACKET REPLACED NEW PART, INSTALLED WITH RIVETS. I.A.W A300-600 SRM 51-72- 10-001, PAGE 2 AND 51-40-21-001, PARA 6, PAGE 7B-23, AS PER GMM 6-2-10SDR FDEA202401200123None · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW FR86~87,STGR 43~45L COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFRSDR FDEA202311071840Unknown · unknownPDIS 749 05-50 7037 07NOV23 MEM MULTIPLE BIRD STRIKES AT LIFTOFF. ***EMERGENCY DECLARED**** FACT 07NOV23 19:05 MEM AMM: 05-51-14-00 PERFORMED BIRD STRIKE INSPECTION REF. AMM 05-51-14-00 ,CLEANED BLOOD STAIN ON NOSE RADOME AND BOTH ENGINES, SDR FDEA202206011354Tachometer · unknownPDIS 749 32-42 5282 01JUN22 MEM FACT U ON LANDING, LEFT LANDING GEAR TRUCK BRAKE TEMP IMMEDIATELY EXCEEDED 300 DEGREES ON WHEELS 2, 5, AND 6. TEMPS ON 2 AND 5 REACHED 700 DEGREES ON TAXI IN WITH FANS RUNNING. WHEEL 1 BRAKE NEVER EXCEEDED 50SDR FDEA202108142016Fire Loop · faultedNO. 2 ENGINE LOOP B FAULTED IN FLIGHT MEL 14AUG21 23:34 ANC U RELEASED FOR SERVICE PER MEL : 26-12-01-01-A CATEGORY : C EXPIRATION : 24AUG21 "MEL 26-12-01-01-A: ENG 2 LOOP B - INOP. FLIGHT CREW MUST PERFORM FUNCTIONAL TEST OF ENG FIRE WARNING SYSTEMSDR FDEA202108091997Skin · chafedRH FWD PAX DOOR UPR CUTOUT SKIN FOUND CHAFE MARKS REPAIRED THE CHAFE MARKS AT RH FWD PAX DOOR UPR CUTOUT SKIN (FAIL SAFE RING) PER EA 6-5310-T0363353 A P1. TITLE: FUSELAGE MAINFRAME - RH FWD CREW/COURIER DOOR FAIL SAFE RING CHAFE/WEAR DAMAGE - BLEND REPAIRSDR FDEA202108011910Fitting · crackedJUNCTION BETWEEN CENTER WING BOX AND CRUCIFORM FITTING AT FR41 LH SIDE FRAME LOCATION O/B ROW FWD FASTENER HOLE FOUND CRACK SIGNAL REPAIRED THE JUNCTION BETWEEN CENTER WING BOX AND CRUCIFORM FITTING AT FR41 LH SIDE FRAME LOCATION O/B ROW FWD CRACKED FASTENSDR FDEA202108011908Frame · crackedFUSELAGE - MAIN FRAME - LH GANTRY 5 RH SIDE LWR FLANGE AT FR52.A FOUND CRACK SIGNAL REPAIRED THE CRACKED MAINFRAME LH #5 GANTRY RH SIDE LWR FLANGE AT FR52.A PER EO: 6-5310-7-5021 E PT8 & AIRBUS DWG: R53810583 ISSUE:D. THIS IS CATEGORY A REPAIR. MAJOR MAJSDR FDEA202108011911Fitting · crackedJUNCTION BETWEEN CENTER WING BOX AND CRUCIFORM FITTING AT FR42 RH SIDE FRAME LOCATION O/B ROW FWD FASTENER HOLE FOUND CRACK SIGNAL REPAIRED THE JUNCTION BETWEEN CENTER WING BOX AND CRUCIFORM FITTING AT FR42 RH SIDE FRAME LOCATION O/B ROW FWD CRACKED FASTESDR FDEA202108011909Fitting · crackedJUNCTION BETWEEN CENTER WING BOX AND CRUCIFORM FITTING AT FR41 RH SIDE FRAME LOCATION O/B ROW FWD FASTENER HOLE FOUND CRACK SIGNAL REPAIRED THE JUNCTION BETWEEN CENTER WING BOX AND CRUCIFORM FITTING AT FR41 RH SIDE FRAME LOCATION O/B ROW FWD CRACKED FASTENSDR FDEA202108011907Structure · crackedCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "E" HOLE FOUND CRACK SIGNAL REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE FASTENER "E" HOLE CRACK PSDR FDEA202108011905Web · crackedFRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, LEFT HAND, LOWER FASTENER HOLE FOUND CRACK SIGNAL REPAIRED THE FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION LEFT HAND LOWER CRACKED FASTENER HOLE PER EA 6-57SDR FDEA202108011904Skin · crackedFRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, LEFT HAND, MIDDLE FASTENER HOLE FOUND CRACK SIGNAL REPAIRED THE FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION LEFT HAND MIDDLE CRACKED FASTENER HOLE PER EA 6-SDR FDEA202108011903Skin · crackedFRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, LEFT HAND, UPPER FASTENER HOLE FOUND CRACK SIGNAL REPAIRED THE FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION LEFT HAND UPPER CRACKED FASTENER HOLE PER EA 6-5SDR FDEA202108011906Beam · crackedAFT CARGO - FR61 DOOR SILL BEAM FLAG CRACK WAS DEVEALED BY HFEC INSPECTION REPAIRED THE AFT CARGO FR61 CRACKED DOOR SILL BEAM FLAG PER EA 6-5320-T0363121 P1. TITLE: FUSELAGE - AUXILIARY STRUCTURE - SILL BEAM FLAG CRACK AT FR61 - REPAIR *THIS EA DEVIATES FRSDR FDEA202107201819Seat Track · gougedMAIN DECK FR74-FR75 -Y1137.1 SEAT TRACK FOUND GOUGE MARKS REPAIRED THE MAIN DECK FR74-FR75 -Y1137.1 SEAT TRACK PER A300-600 SRM53-10-16-201 FIG.208 SHEET 1 . THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM 6-2-100SDR FDEA202107201818Seat Track · gougedMAIN DECK FR60-FR61 Y1456 SEAT TRACK FOUND GOUGE MARKS REPAIRED THE MAIN DECK FR60-FR61 Y1456 SEAT TRACK PER A300-600 SRM53-10-16-201 FIG.208 SHEET 1 . THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM 6-2-100SDR FDEA202010112461Smoke Detector · false activationPDIS 749 26-12 3604 10OCT20 MEM FACT U. PASSING FL 200 ON CLIMB OUT, GOT MAIN DECK AFT SMOKE WARNING. WARNING STOPPED AFTER A FEW MINUTES. RETURNED TO MEM, NO EXTERIOR INDICATIONS ON GROUND FROM RESCUE ON SEAN. SHGN 10OCT20 23:39 MEM U. UPON INSPECTION, NSDR FDEA202009182249Hydraulic System · malfunctionedPDIS 749 29-30 3529 18SEP20 MEM OPEN U. DURING TAKEOFF ROLL AT 50KTS, ECAM ALERT "HYD YELLOW PUMP LO PR" AND "YELLOW SYS LO PR" REJECTED TAKEOFF. CLEARING RWY NOTICED HYD YELLOW FLUID LEVEL ABOUT 4 NEEDLE WIDTHS BELOW TOPHAT. DID FLT CONT CHECK AND YELLOW SDR FDEA201905171089Skin · crackedFWD CARGO DOOR INNER SKIN AT THE BOTH SIDE OF ACTUATOR ATTACH LUG FITTING CRACKED COMPLIED WITH EA # 6-5230-T0346774 P1, EA TITLE: DOORS - CARGO DOOR/HYD SYS - FWD CARGO DOOR INNER SKIN CRACKED AT FR22A. REPAIRED THE FWD CARGO DOOR INNER SKIN AT THE BOTH SIDE SDR FDEA201905071011Floor Support · corrodedMAIN DECK FR11-FR15A Y953 FLOOR SUPPORT CORRODED REPLACED THE HEAVILY CORRODED FLOOR SUPPORT ON MAIN DECK FR11-FR15A Y953 PER SRM 51-40-21 . MAJOR REPAIR IAW GMM6-2-100.SDR FDEA201905010974Skin · corrodedFUSELAGE SKIN EXTERIOR SURFACE CORRODED, BTW FR0 AND FR1, STR 25L AND STR 26L REPAIRED THE CORRODED FUSELAGE SKIN BTW FR0 AND FR1, STR 25L AND STR 26L PER SRM 53-11-12-201 FIG201. THIS IS A CATEGORY "B" REPAIR, MUST BE INSPECTED AT DEFINED INTERVALS PER SRI 5SDR FDEA201904280951Beam · unknownEXISTING REPAIR ON AFT CARGO COMPARTMENT CROSSBEAM AT FR60 BETWEEN -Y805 AND -Y1470 REQUIRES EVALUATION FOR
CONFORMITY THE EXISTING REPAIR ON AFT CARGO COMPARTMENT CROSSBEAM AT FR60 BETWEEN -Y805 AND -Y1470 WAS
EVALUATED AND FOUND NOT IN CONFORMITY WITH CURRSDR FDEA201904280952Doubler · corrodedEXISTING REPAIR ON FUSELAGE SKIN BETWEEN FR11A AND FR13 BELOW TOILET SERVICE DOOR REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE SKIN BETWEEN FR11A AND FR13 BELOW TOILET SERVICE DOOR FOUND IN CONFORMITY WITH RAS/AS/128/2003 ISSUE A AND FOUNSDR FDEA201904280945Doubler · wornEXISTING REPAIR ON RH I/B FLAP UPPER SKIN BETWEEN RIB1C AND RIB3 STGR2.1 AND STGR2.2 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON RH I/B FLAP UPPER SKIN BETWEEN RIB1C AND RIB3 STGR2.1 AND STGR2.2 WAS EVALUATED AND FOUND IN CONFORMITY WITH TD FOK/1SDR FDEA201901250196Pressure Switch · failedFOLLOWING T/O KMEM ECAM: (GREEN SYS LO PR) CONFERRED WITH DISPATCH / MAINT DECISION TO RETURN KMEM. FOLLOWED ECAM AND QRH PROCEDURES. GREEN HYD LVL IN GREEN BAND/PRESS ON ECAM 3100 PSI. CAPT CONFIRMED L/G WAS MANUALLY EXTENDED PER QRH. RESTORED LANDING GEAR TOSDR FDEA201707292080Windshield · failedFIRST OFFICER`S WINDSCREEN SHATTERED AFTER WINDOW HEAT FAULT. NO CRACKS INSIDE PANE. REMOVED AND REPLACED THE WINDSCREEN IAW AMM 56-11-11-04 AND PERFORMED ADJUSTMENT AND TEST IAW AMM 30-42-00-05. OK FOR SERVICE.SDR FDEA201706141663Processor · failedDURING CLIMB OUT NR 1 PITCH TRIM CLICKED OFF, NO RESET, NR 2 PITCH TRIM RETURNED TO DEPARTURE. REMOVED AND REPLACED THE PROXIMITY DETECTOR PROCESSING UNIT IAW AMM 32-31-71-04. OPS CHECKED GOOD. REPLACED THE NLG RELAYS 96GB AND 141GB IAW ESPM FOR FLAGGED FAUSDR FDEA201702180587Indicator · malfunctionedDUE TO QRH PROCEDURES LEAVING CROSSFEED OPEN WITH LOW FUEL INDICATIONS, LANDED OUT OF TANK LIMITS. LEFT TANK, 7.8 RT TANK 4.6. IAW MOCC AND ENGN STICK FUEL QTY IN TANKS BOTH OUTER TANKS READING PER INDICATION L/H OUTER 7.5 AND STICK READING WAS 30 ON STSDR FDEA201702090475Fire Loop · malfunctionedINFLIGHT WHEN LEVELING AT FLIGHT 330, LOOP A LIGHT ILLUMINATED ON NR 2 ENGINE. FOLLOWED QRH. PERFORMED BITE CHECK OF NR 2 ENGINE FIRE DETECTION CONTROL UNIT IAW MM 26-12-00-05-01, NO FAULTS , OPENED THE NR 2 ENG AND CHECKED RESISTENCE OF A LOOP RESPONDE
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