N774AX
Service difficulty reports · 137
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 = 'N774AX' 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 = 'N774AX' 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 ABXA20160329062Stiffener · crackedAFT BULK CARGO, STATION 1417, ABOVE STRINGER 36L, FLOORBEAM STIFFENER CRACKED. R & R STIFFENER IAW SRM 51-40-02 4B & 7D, DWG 146T1216, CRACKED 1.5". PN 146T1261425, PART NAME STIFFENER, SN N/A, FS & BS LOCATION FROM 1417, STRINGER & WS LOCATION FROM 36L. ACSDR ABXA20160329052Rib · corrodedRIGHT WING LE AIR LOAD RIB CORRODED AT WS 479. R & R RT WING LE AIR LOAD RIB AT WS 479 IAW SRM 51-40-02. CORRODED LEVEL 2, PN 114T2203-14, PART NAME STRUT RIB, SN NSN, WS LOCATION FROM WS 479 - 479. ACFT WAS GNDED.SDR ABXA20160323051Rib · corrodedLEFT WING LE AIR LOAD RIB LOWER STRUT AT APPROX OSS 575, OTBD OF NR 4 SLAT INBD AUX TRACK HAS CORROSION UNDER NUTPLATE. R & R AIR LOAD RIB AT OSS 575 IAW SRM 51-40-02. CORRODED LEVEL 2, PN 114T2209-17, PART NAME AIR LOAD STRUT, SN NSN, WS LOCATION FROM 575 -SDR ABXA20160318061Floorbeam · corrodedAFT BULK CARGO, BILGE STATION 1417, STRINGERS 32R & 33R, INTERSECTION OF TOP OF FLOORBEAM & FLOOR SUPPORT CORROSION. R & R FLOORBEAM IN ALC BULK CARGO STATION 1417, STRINGER 32R - 33R, AT TOP OF FLOORBEAM & FLOOR SUPPORT IAW SRM 51-40-02. PN 452T3230-14, PARSDR ABXA20160317057Beam · crackedBEAM BELOW HYD BAY ACCESS DOOR 447BR CHAFED & CRACKED AT FWD END. REMOVED OLD BEAM & INSTALLED NEW BEAM IAW 51-40-02. CRACKED 1", PN 313T1380-209, SN NSN, PART NAME BEAM, EXACT FS & BS LOCATION ON ACFT, ENG BS O.OO - 10.0, EXACT STRINGER & WS LOCATION ON ACFSDR ABXA20160317055Structure · crackedINNER CHORD HAS 0.125 CRACK AT LFS 859.5, LBL 89. REFERENCE JC NEA53000045-001 FOR DETAILS. REPAIRED INNER CHORD AT LFS 859.5, LBL 89 IAW JC NEW 53000045-01 & EA 53000047-101. CRACKED LENGTH .125", PN 145T1001-1, SN NSN, PART NAME INNER CHORD, EXACT FS & BS SDR ABXA20160316066Spar · gougedNUMBER 8 FLAP SUPPORT RIB AT REAR SPAR, PERFORMED FASTENER HOLE INSPECTION AT NR 4 POSITION IAW ES02540 STEP 2, DEFECT NOTED. HOLE WILL BE REPAIRED IAW REA B65731981-MR. GOUGE, PN 113T1345-20, PART NAME FLAP SUPPORT SPAR, HOLE SIZE .749 RT WING FS LOCATION WSDR ABXA20160316065Spar · gougedNUMBER 8 FLAP SUPPORT RIB AT REAR SPAR. PERFORMED FASTENER HOLE INSPECTION AT NR 3 POSITION IAW ES02540 STEP 2, DEFECT NOTED. HOLE WILL BE REPAIRED FOR REA B657 -61981-MR. GOUGE, PN 113T1345-20, PART NAME FLAP SUPPORT SPAR, HOLE SIZE .749 RT WING, FS LOCATISDR ABXA20160316064Spar · gougedNUMBER 8 FLAP SUPPORT RIB AT REAR SPAR. PERFORMED FASTENER HOLE INSPECTION AT NR 2 POSITION IAW ES02540 STEP 2, DEFECT NOTED. HOLE WILL BE REPAIRED FOR REA B657-31981 MR. GOUGE PN 113T1345-22, PART NAME FLAP SUPPORT SPAR, HOLE SIZE .749 RT WING FS LOCATION: SDR ABXA20160316063Spar · gougedNUMBER 8 FLAP SUPPORT RIB AT REAR SPAR. PERFORMED FASTENER HOLE INSPECTION AT NR 1 POSITION IAW ES02540 STEP 2, DEFECT NOTED. HOLE WILL BE REPAIRED IAW REA B657-61981-MR. GOUGE, PN 113T1345-22, PART NAME FLAP SUPPORT SPAR, HOLE SIZE 749 RT WING, FS & BS LOCSDR ABXA20160315056Structure · crackedINNER CHORD HAS 0.250 CRACK AT RFS 883.5, RBL 89. REFERENCE JC NEA 53000048-001 FOR DETAILS. REPAIRED CRACK ON INNER CHORD AT RFS 883.5, RBL 89 IAW NEA 53000048-001 & EA 60361. CRACKED, LENGTH 0.250", PN 145T1004-2, PART NAME INNER CHORD, SN NSN, FS & BS LOCSDR ABXA20160307050Rib · corrodedLEFT WING LE AIR LOAD RIB LOWER STRUT AT APPROX OSS 884, OTBD OF NR 2 SLAT INBD AUX TRACK HAS CORROSION UNDER NUTPLATE. R & R RIB IAW SRM 51-40-02 7D & DWG 114T222. CORRODED LEVEL 2 PN 114T2222-15, PART NAME AIR LOAD STRUT, SN NSN, WS LOCATION FROM 884 - 88SDR ABXA20140725254Stringer · crackedSTATION 676 18L STRINGER CRACKED. REPAIRED CRACKED STRINGER 18L AT STATION 676 IAW REA B653-61104-MR. PN 143T3001-12, PART NAME STRINGER 18L, CRACKED 1 INCH, EXACT FS FROM 682, EXACT STR LOC ON ACFT 18L. ACFT WAS GNDED.SDR ABXA20140725253Beam · corrodedRIGHT WING TE TRANSVERSE BEAM AT WS 285 CORRODED SEVERAL SPOTS ALONG INBD EDGE JUST UNDER PANEL 651MT. R & R RT WING TE TRANSVERSE BEAM IAW SRM 51-40-02 & REA NR B657-61111. SDR INFO PN 113T1623-126, PART NAME UPPER CHORD, SN NA, CORRODED LEVEL 2. ACFT WAS SDR ABXA20140723256Stringer · crackedSTATION 676 8L STRINGER CRACKED. R & R STRINGER 8L STATION 676 IAW SRM 53-00-03 & REA B653-61104-MR. CRACKED 1.75 INCHES, PN 143T3001-6, SN NSN, PART NAME STRINGER, FS & BS LOC ON ACFT FS 682, STR & WS LOC ON ACFT STR 8L. ACFT WAS GNDED.SDR ABXA20140723255Stringer · crackedSTATION 676 19L STRINGER CRACKED. R & R STRINGER 19L STATION 682 IAW SRM 53-00-03 & REAS B653-61104-MR. CRACKED 1 INCH. PN 143T3001-17, SN NSN, PART NAME STRINGER, FS & BS LOC ON ACFT FS 682, STR & WS LOC ON ACFT STR 19L. ACFT WAS GNDED.SDR ABXA20140723251Rib · corrodedRIGHT WING LE RIB CORRODED AT WS 478. REMOVED CORRODED RIB & INSTALLED FABRICATED RIB IAW REA B657-61105 & SRM 51-40-02. CORRODED LEVEL 2, PN 114T2203-16 PART NAME AIR LOAD RIB STRUT, SN NSN, STR & WS LOC RT WING STATION OSS 479.854 TO OSS 479.854 LE. ACFT SDR ABXA20140721252Spar Web · corrodedFRONT SPAR WEB CORRODED AFT OF NR 5 SLAT AT LES 450. REPAIRED FRONT SPAR WEB AFT OF NR 5 SLAT AT LES 450 IAW REA B657-61106-MR. PN 112T2007-1, PART NAME SPAR WEB, SN NSN, CORRODED LEVEL 2, EXACT WS LOC ON ACFT 448 TO 452. ACFT WAS GNDED.SDR ABXA20130810503Failsafe · crackedFRAME FAILSAFE CRACKED AND CORRODED. CRACK VERIFIED WITH HFEC IAW NDTM, PART 6 51-00-19 AND VISUALLY VERIFIED. FAILSAFE REPAIRED ON JC EA53500013-003. ACFT WAS GROUNDED.SDR ABXA20130805504Failsafe · crackedFAILSAFE CRACKED 1.7", LEFT FS 955, LBL 85.9. AIRCRAFT WAS GROUNDED. REPAIRED IAW REA B653-60654-MR.SDR ABXA20130730505Pressure Panel · crackedOTBD FWD CORNER OF PRESSURE WEB CRACKED JUST AFT OF SIDE FRAME ATTACH FLANGE. FABRICATED NEW WEB IAW DWG 145T8752 INSTALLED IAW EA 53500013-003, PG. 10, STEP 25.SDR ABXA20130410423Skin · separatedRIGHT OUTBOARD AILERON UPPER SURFACE SKIN SEPERATED AND PEELED BACK. RIGHT OUTBOARD AILERON REPLACED. REMOVED AND REPLACED RIGHT OUTBOARD AILERON, ACFT WAS GROUNDED.SDR ABXA20121108295Angle · corrodedDURING A HEAVY MAINTENANCE INSPECTION, TWO RAISED AREAS NOTED ON TOP SURFACE OF WING TRAILING EDGE FORWARD OF NUMBER 6 SPOILER. AREA OF THE LEFT WING UPPER CHORD (PN113T1406-7) FORWARD OF THE NR 6 SPOILER (WS 227 TO WS 314) FOUND CORRODED. FABRICATED REPAIR SDR ABXA201011170153Skin · crackedFUSELAGE SKIN CRACKED AT FS 1702, STRINGER 6L. CRACK IS .25 INCH LONG. REPAIRED DAMAGE AT FUSELAGE STA 1702, STRINGER 6L IAW B767 SRM 53-00-01. PRIMED AREA IAW B767 51-21-10-7.SDR ABXA201011160152Fireseal · crackedNR 2 ENGINE OUTBOARD REVERSER INBOARD AFT FIRE SEAL MATING SURFACE IS CRACKED. REPAIRED AREA IAW B767 SRM 51-70-13.SDR ABXA201011150151Mount · corrodedNR 1 ENG AFT MOUNT HAS SURFACE CORROSION. REMOVED AND REPLACED NR 1 ENGINE AFT MOUNT FROM STEP G1 TO G3 IAW AMM 71-2-04.SDR ABXA070120Floorbeam · corrodedFLOOR SUPPORT CORRODED AT FS 1402, LEFT BUTT LINE 21. REMOVED, REPAIRED AND REINSTALLED FLOOR SUPPORT IAW B767 51-70-12 AND 51-40-O2.SDR ABXA070119Beam · crackedLOWER FORWARD CORNER OF THE R1 DOOR HAD A CRACKED BEAM. REPAIRED AREA IAW REA B652-55550-MR.SDR ABXA070027O-Ring · leakingHYDRAULIC QUANTITY DECREASED TO .46 QTY STABLE WITH EDP DEPRESSURIZED ACMP OFF. OPENED COWLINGS, SERVICED RIGHT HYDRAULIC SYSTEM IAW B767 MM. RIGHT ENGINE FOUND FLUID LEAK AT STRUT DISCONNECTOR, REPLACED O-RING. NO LEAKS NOTED.SDR ABXA060154Circuit Card · faultyMAIN CARGO SMOKE DETECTION SYSTEM FAILS SELF TEST. REMOVED AND REPLACED AFOLTS CARD M2026 IAW FIM 26-14-00 AND OPS CHECK GOOD IAW MM 26-14-00.SDR ABXA050241Rib · corrodedLT WING LEADING EDGE RIB AT STA. WA 920 (APPROXIMATELY) HAD EXFOLIATED CORROSION AT FORWARD END AND LOWER FLANGE LOWER SURFACE. REMOVED AND REPLACED RIB IAW B767 SRM 51-40-01.SDR ABXA050122Slide · deployedLIFE RAFT SLIDE DEPLOYED WITHOUT BEING ARMED. THE LOWER FORWARD ENTRY DOOR HUNG WHILE TRYING TO CLOSE IT. WHEN THE DOOR WAS RAISED FOR RE-CLOSURE, THE SLIDE DEPLOYED. INSPECTED DOOR AND GIRT BAR ATTACHMENTS. NO DEFECTS NOTED. REMOVED AND REPLACED SLIDE ASSDR ABXA040298Structure · vibrationAIRCRAFT HAD AN UNUSUAL VIBRATION. COCKPIT WAS OSCILLATING UP AND DOWN APPROXIMATELY 3 CYCLES IAW SECOND. SLOWED AC TO 280 KIAS, NO CHANGE. AFTER TRANSITION TO MACH NR, OSCILLATION ABATED AS THE IAS DECREASED THROUGH 270 KNOTS. ALL ENGINE INDICATIONS WERE NORMSDR ABXA030280Battery Pack · dischargedWHEN TESTED EMERGENCY LIGHTS, LIGHT OVER COCKPIT DOOR WAS INOP. TWO EACH LIGHTS AT ENTRANCE DOOR GOOD. ALSO, SPARE LIGHT SUPPLY INOP. REPLACED MAIN EMERGENCY BATTERY POWER SUPPLY IAW B767 AMM 33-51-07. OPS CHECKED GOOD.SDR ABXA010876Battery Pack · dischargedDURING MAINTENANCE TEST OF EMERGENCY LIGHTING SYSTEM, FOUND STANDBY BATTERY INOPERATIVE. INSTALLED NEW BATTERY PACK IAW B767 MM 33-51-07-02. OPS CHECKED GOOD.SDR ABXA010875Power Supply · dischargedDURING MAINTENANCE INSPECTION, FOUND BOTH EMERGENCY LIGHTS INOPERATIVE. REPLACED PRIMARY EMERGENCY LIGHT POWER SUPPLY AND TESTED IAW B767 MM 33-51-07. PRIMARY SUPPLY OPS CHECKED GOOD. LIGHTS ILLUMINATED.SDR DL76A010663Slat · delaminatedNR 1 SLAT T/E WEDGE IS DELAMINATED ON THE INBD EDGE. REPAIR PER ER/A 380633-14AD
Back to N774AX