N744AX

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 = 'N744AX' 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.

SDR ABXA20161102169Support Angle · corrodedUPPER ATTACH STRUCTURE CORRODED UNDER APU INTAKE DOOR. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II. FABRICATED A NEW ATTACH STRUCTURE IAW DRAWING 148T3120, AND INSTALLED IAW DRAWING 148T3210, AND SRM 51-40-02 PAR 4,7. Nov 2, 2016 · N744AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20161018168Skin · corrodedLEFT APU DOOR INNER SKIN CORRODED JUST AFT OF 5TH FRAME FROM FORWARD END. REPAIRED IAW SRM 52-40-01 FIG 201 REPAIR 5. AIRCRAFT GROUNDED.Oct 18, 2016 · N744AX · Boeing 767232 · Auxiliary Power Unit (APU) DoorsSDR ABXA20161017156Keelbeam · corrodedTHREE AREAS OF CORROSION ON KEEL BEAM LOWER CHORD (TOP AND BOTTOM) APPROXIMATE STATION 956-970, LBL9 ACCESSED BETWEEN MAIN LANDING GEAR DOORS. REPAIRED LOWER KEEL BEAM AT STATION 956-970 LBL9 IN ACCORDANCE REA-B653-62220-MR. ACFT GROUNDED.Oct 17, 2016 · N744AX · Boeing 767232 · Fuselage Main, KeelSDR ABXA20161017155Keelbeam · corrodedCORROSION ON KEEL BEAM LOWER CHORD APPROXIMATE BS 990-996, LBL9 ACCESSED BETWEEN MAIN LANDING GEAR DOORS. REPAIRED LOWER KEEL BEAM CHORD AT STATION 990-996 LBL9 IN ACCORDANCE WITH REA- B653-62220-MR. ACFT GROUNDED.Oct 17, 2016 · N744AX · Boeing 767232 · Fuselage Main, KeelSDR ABXA20161017154Angle · corrodedCORROSION ON KEEL BEAM LOWER ANGLE BS 1002 - 1015, LBL 9. REPAIRED IAW REA-B653-622220-MR. AIRCRAFT WAS GROUNDED.Oct 17, 2016 · N744AX · Boeing 767232 · Fuselage Main, KeelSDR ABXA20161017153Angle · corrodedCORROSION ON KEEL BEAM LOWER ANGLE BS 1025 - 1030, LBL 9. REPAIRED IAW REA B653-62220-MR. AIRCRAFT WAS GROUNDED.Oct 17, 2016 · N744AX · Boeing 767232 · Fuselage Main, KeelSDR ABXA20161014163Frame · crackedBS 883.5 LBL 89, SIDE FRAME AT LOWER TRANSITION CRACKED BELOW FLOOR LINE. REPAIRED IAW EA 53000049-101 AND REA B653-62233-SB. AIRCRAFT WAS GROUNDED.Oct 14, 2016 · N744AX · Boeing 767232 · Fuselage Main, FrameSDR ABXA20161012166Frame · crackedBS 859.5 LBL 89, SIDE FRAME AT LOWER TRANSITION RADII CRACKED (BELOW FLOOR LINE). REF: J/C NEA 53000045-001 ES02570 PG 2 AIRCRAFT WAS GROUNDED.Oct 12, 2016 · N744AX · Boeing 767232 · Fuselage Main, FrameSDR ABXA20161011167Angle · crackedANGLE CRACKED ON OUTBOARD PYLON JUST ABOVE AND FORWARD OF STRUT ACCESS DOOR. REMOVED AND REPLACED THE ANGLE IAW DRAWING 313T3310 AND SRM 51-40-02 PAR 7.Oct 11, 2016 · N744AX · Boeing 767232 · Nacelle/Pylon, Attach FittingsSDR ABXA20161007165Frame · crackedBS 859.5 RBL 89, SIDE FRAME LOWER TRANSITION CRACKED BELOW FLOOR LINE. REPAIRED IAW EA 53000048-101. AIRCRAFT WAS GROUNDED.Oct 7, 2016 · N744AX · Boeing 767232 · Fuselage Main, FrameSDR ABXA20161007164Frame · crackedBS 883.5 RBL 89, SIDE FRAME AT LOWER TRANSITION CRACKED BELOW FLOOR LINE. REPAIRED IAW EA53000050-101. AIRCRAFT WAS GROUNDED.Oct 7, 2016 · N744AX · Boeing 767232 · Fuselage Main, FrameSDR ABXA20161007162Rib · crackedNR 4 SLAT INBOARD DRIVE ROD CUTOUT, INBOARD NOSE RIB CRACKED. REMOVED AND REPLACED INBOARD NOSE RIB ON NR 4 SLAT IAW SRM 51-40-02. AIRCRAFT WAS GROUNDED.Oct 7, 2016 · N744AX · Boeing 767232 · Wing, Rib/BulkheadSDR ABXA20161007161Beam · corrodedLEFT WING LEADING EDGE BS 698 FORWARD LOWER PANEL ATTACH NUT PLATE STRIP CORRODED. NOSE BEAM AT NUT PLATE LOCATIONS WAS FOUND CORRODED BEYOND ALLOWABLE DAMAGE LIMITS. REMOVED NOSE BEAM WEB AND FABRICATED REPLACEMENT NOSE BEAM WEB FROM 7075T-6 .050 PO# 008909Oct 7, 2016 · N744AX · Boeing 767232 · Wing Main, Frame StructureSDR ABXA20161007160Angle · crackedBS 1702 STRINGER 3R FRAME ANGLE CRACKED. REMOVED AND REPLACED FRAME ANGLE IAW SRM 51-40-02. AIRCRAFT WAS GROUNDED.Oct 7, 2016 · N744AX · Boeing 767232 · Fuselage Main, StructureSDR ABXA20161007159Angle · crackedBS 1678 STRINGER 3R FRAME ANGLE CRACKED. REMOVED AND REPLACED FRAME ANGLE IAW SRM 51-40-07. AIRCRAFT WAS GROUNDED.Oct 7, 2016 · N744AX · Boeing 767232 · Fuselage Main, FrameSDR ABXA20160928157Support Angle · corrodedCORROSION ON SUPPORT ANGLE AT THE AFT LEFT CORNER OF THE INNER KEEL BEAM AREA ACCESSED THRU PANEL 139FZ. REMOVED CORROSION ON SUPPORT ANGLE WITHIN ALLOWABLE DAMAGE LIMITS OF SRM 53-50-12 FIGURE 101 DETAIL II AND TALE I. REMOVED .010 OF MATERIAL, ORIGINAL THICKSep 28, 2016 · N744AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA2016225005Torque Tube · crackedDURING PREPARATION OF FLAP REMOVAL, WHILE INSTALLING NR 3 SPOILER LOCK, FOUND ACTUATOR TO WING OTBD ATTACH LUG BROKEN OFF & INBD LUG BADLY WORN. R & R NR 3 SPOILER ACTUATOR TORQUE TUBE IAW AMM 27-61-01, & 27-61-02. SDR CRACK 3 INCHES, PN 1134T1440-1, SN NSN,Feb 25, 2016 · N744AX · Boeing 767232 · Drag Control SystemSDR ABXA20141110341Web · crackedSTRUCTURAL WEB IS CRACKED AT THE FWD MOST NOSE COWL ANTI-ICE DUCT SUPPORT ROD BRACKET. REMOVED DAMAGED WEB, FABRICATED & INSTALLED NEW WEB IAW SRM 51-40-02 & DWG 311T1510. CRACKED 3.2 INCHES, PN 311T1510-59, SN N/A, PART NAME WEB, FS & BS LOCATION ON ACFT NANov 10, 2014 · N744AX · Boeing 767232 · Nacelle/Pylon Miscellaneous StructureSDR ABXA20141107344Support · damagedFASTENER HOLE ON NR 1 SUPPORT 1, 2, 3 BEAM RT SIDE FWD OF NR 2 JOINT UPPER HOLE HAS DAMAGE IN HOLE. REAMED HOLE & INSTALLED OVERSIZED FASTENER IAW REA-C027-61321-MR. HOLE DAMAGE, PART NR 113T1313-7, PART NAME FLAP SUPPORT, 1 - 3 BEAM, EXACT LOCATION 800, SN Nov 7, 2014 · N744AX · Boeing 767232 · Wing, Control Surface Attach FittingsSDR ABXA20141106343Support · corrodedRIGHT WING NR 7 FLAP SUPPORT 1,2, 3 BEAM HAS HFEC DEFECT INDICATION IN OTBD STUD HOLE. NR 7 SUPPORT 1, 2, 3 BEAM REROUTED TO COMPONENT REPAIR SHOP FOR REPAIR IAW CMM IAW REA C057-61311-MR. CORRODED LEVEL 2, PART NR 113T1314-16, PART NAME NR 7 SUPPORT 1 - 3 ANov 6, 2014 · N744AX · Boeing 767232 · Wing, Control Surface Attach FittingsSDR ABXA20141106342Support · corrodedRIGHT WING NR 8 FLAP SUPPORT MECHANISM 1, 2, 3 BEAM INBD STUD HOLE HAS HFEC DEFECT INDICATION. CORROSION VISIBLE. NR 8 SUPPORT 1, 2, 3 BEAM REROUTED TO COMPONENT REPAIR SHOP FOR REPAIR IAW CMM IAW REA C057-61312-MR. CORRODED LEVEL 2, PART NR 113T1313-8, PARNov 6, 2014 · N744AX · Boeing 767232 · Wing, Control Surface Attach FittingsSDR ABXA20141030340Doubler · damagedTOOLING MARKS ON REPAIR DOUBLER AT STATION 1373 IN BETWEEN STRINGER 29R & 30R. R & R DOUBLERS IAW ERA 379839-14. FABRICATED DOUBLERS FROM 2024-T3 .100 IAW ERA 379839-14. REPLACED DOUBLERS BECAUSE OF TOOLING MARKS ON LOWER DOUBLER. TOOLING MARKS, PN 146T3531Oct 30, 2014 · N744AX · Boeing 767232 · Fuselage Main, Plate/SkinSDR ABXA20141027337Support Angle · crackedCRACKED SUPPORT ANGLE AT AFT END OF FORE TO AFT LOWER BEAM AT REAR SPAR APPROX RBL 42. FABRICATED NEW SUPPORT ANGLE FROM 2075-0-090 PO 0055105. HEAT TREATED TO 2075-T6 IAW DWG 111T1000. CRACKED 4.7 INCHES, PN 111T1000, PART NAME ANGLE, SN NSN, FS & BS LOCATOct 27, 2014 · N744AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20141022338Structure · corrodedPANEL 552CB AFT ATTACH CHORD SPLIT ON EDGE. R & R CHORD. REINSTALLED PANEL 552EB & 551YBX IAW SRM 51-40-02. CORRODED L2, PN 654T0391-35, SN NSN, PART NAME CHORD, STRINGER & WS 180 TO 314. ACFT WAS GNDED.Oct 22, 2014 · N744AX · Boeing 767232 · Wing Miscellaneous StructureSDR ABXA20141017339Crossmember · corrodedPANEL ATTACH CROSS MEMBER AT STATION 968 CORRODED AROUND NUTPLATE ON LT SIDE. R & R ATTACH CROSS MEMBER AT STATION 968 IAW SRM 51-40-08, 51-40-05 & 51-40-02. PN 145T8629-3, PART NAME CROSS MEMBER, SN NSN, CORRODED L2, EXACT FS LOCATION ON ACFT 968 TO 968 LOWOct 17, 2014 · N744AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20130321422Fitting · crackedL1 DOOR HAS A POSSIBLE CRACK ON THE LOWER FRONT AND AFT FITTINGS OF THE DOOR, IN THE BACK POCKET OF THE FITTINGS. INSTALLED NEW LOWER BEAM IAW B767 SRM 51-40-02 AND DWG 141T6109, ACFT WAS GROUNDED.Mar 21, 2013 · N744AX · Boeing 767232 · Passenger/Crew DoorsSDR ABXA20130320421Skin · corrodedLEFT SIDE SKIN UNDER FAILSAFE CUTOUT SHOWS SIGNS OF CORROSION. REPAIRED AREA, ACFT WAS GROUNDED.Mar 20, 2013 · N744AX · Boeing 767232 · Fuselage Main, Plate/SkinSDR ABXA20130320420Failsafe · crackedSTA 955 S22L FAILSAFE CUTOUT CENTER HOLE SHOWS CRACK INDICATION. REAMED HOLE IAW B767-200 SRM 51-10-02. NDT VERIFIED. NO DEFECTS, INSTALLED 2ND OVERSIZE FASTENER IAW AMES DOCUMENT 47043REA02, ACFT WAS GROUNDED.Mar 20, 2013 · N744AX · Boeing 767232 · Fuselage Main, FrameSDR ABXA20130319416Strap · crackedRIGHT SIDE FAILSAFE STRAP FOUND WITH .50" CRACK RADIATING FROM LOWER HOLE AT APPROX 9 O'CLOCK POSITION. FRETTING CORROSION ON OPPOSITE SIDE OF FITTING WILL BE CLEANED UP BY TRIM OUT PROCEDURE. TRIM OUT OF FAILSAFE AND CORRECTIVE ACTION ACCOMPLISHED, ACFT WASMar 19, 2013 · N744AX · Boeing 767232 · Fuselage Main, FrameSDR ABXA20130319418Failsafe · corrodedSTA 955 LEFT FAILSAFE, INBOARD SIDE, CORROSION AT TEE FITTING REMOVAL LOCATION. FAILSAFE TRIM OUT ACCOMPLISHED ON DOCUMENT 470080RD03, ACFT WAS GROUNDED.Mar 19, 2013 · N744AX · Boeing 767232 · Fuselage Main, FrameSDR ABXA20130314419Failsafe · crackedLEFT FAILSAFE INBD, CRACKED AT CENTER HOLE TEE FITTING REMOVAL LOCATION, CORRECTIVE ACTION (FAILSAFE TRIMOUT) ACCOMPLISHED ON AMES DOCUMENT 470080RD03. ACFT WAS GROUNDED.Mar 14, 2013 · N744AX · Boeing 767232 · Fuselage Main, FrameSDR ABXA20130314417Tee Fitting · corrodedAT STA 955 LEFT TEE FITTING COMMON TO THE FAILSAFE STAP IS CORRODED. DRILLED NEW TEE FITTING IAW B767 SRM 51-40-05 TEE FITTING INSTALLED ON DOCUMENT 47008ORD03 STEP 15, ACFT WAS GROUNDED.Mar 14, 2013 · N744AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20130314415Tee Fitting · corrodedAT STA 955 RIGHT RIGHT SIDE TEE FITTING COMMON TO FAILSAFE, FWD LOWER HOLE OUT BOARD SURFACE CORRODED. DRILLED NEW TEE-FITTING IAW B767 SRM 51-40-05. TEE-FITTING INSTALLED ON DOCUMENT 47008ORD04, ACFT WAS GROUNDED.Mar 14, 2013 · N744AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20130312414Doubler · crackedRIGHT WING LEADING EDGE ATTACHING FLANGE (DOUBLER) CRACKED FOR WING TIP FAIRING. REMOVED AND REPLACED RIGHT SIDE WING TIP FWD ATTACH DOUBLER P/N 112T5360-44 USING 2024T3 .063" THICK IAW BOEING DWG 112T5360 AND B767-200 SRM 51-40-02, ACFT WAS GROUNDED.Mar 12, 2013 · N744AX · Boeing 767232 · Wing, Plate/SkinSDR ABXA20130306413Skin · corrodedHORIZONTAL CENTER SECTION LOWER SKIN BETWEEN S-9 AND S-10 HAS HEAVY CORROSION JUST OUTBOARD RIB 2R-3R. BLENDED AREA ON LOWER SKIN BETWEEN S9 & S10 IAW B767 SRM 55-10-01. FOUND TO BE WITHIN LIMITS IAW REA B655-60486-MR, AIRCRAFT WAS GROUNDED.Mar 6, 2013 · N744AX · Boeing 767232 · Horizontal Stabilizer, Plate/SkinSDR ABXA20130303411Sill · corrodedUNDER BULK CARGO DOOR SILL LOWER SILL FS 1407-1480 BELOW S32L HAS THE UPPER CHORD OF THE SILL FRAME CORRODED (METAL WAS EXFOLIATED). REMOVED AND REPLACED BULK CARGO DOOR UPPER CHORD OF FLOOR FRAME WITH SERVICEABLE UNIT IAW BOEING SRM 51-40-02 AT FS 1407-1480 Mar 3, 2013 · N744AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20130228405Structure · corrodedHORIZONTAL CENTER SECTION UPPER S-7 VERTICAL LEG HAS HEAVY CORROSION JUST OUTBOARD OF RIB 1L. BLENDED AREA OF CORROSION, BLENDED AREA WAS REWORKED AND FOUND TO BE PERMANENT REPAIR IAW REA B655-60485-MR, ACFT WAS GROUNDED.Feb 28, 2013 · N744AX · Boeing 767232 · Horizontal Stabilizer StructureSDR ABXA20130228403Fastener · corrodedHORIZONTAL BOX, AT S11 UPPER FWD BETWEEN RIB 2-R AND RIB -1-R BRACKET HAVE HARDWARE CORR. BLENDED AREA OF CORROSION, BLENDED AREA WAS REWORKED AND FOUND TO BE A PERMANENT REPAIR IAW REA B655-60485-MR. REMOVED ADN REPLACED CORRODED HARDWARE IAW B767-200 SRM 5Feb 28, 2013 · N744AX · Boeing 767232 · Horizontal Stabilizer Miscellaneous StructureSDR ABXA20130227410Angle · corrodedCORROSION ANGLE UNDER BULK CARGO DOOR SILL AT FWD EDGE AT STA 1417. REMOVED AND REPLACED NEW ANGLE UNDER BULK CARGO DOOR SILL IAW B767 SRM 51-40-02, ACFT WAS GROUNDED.Feb 27, 2013 · N744AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20130226408Splice · crackedMAIN CARGO DOOR SURROUND CIRCUMFERENTIAL SPLICE SKIN STA 434 CRACKED AT FASTENER FWD 2ND ROW 2" LEFT OF STRINGER 1R LEFAIVE 350125. REPAIRED AREA AT STA 434 UPPER SKIN SPLICE IAW B653-60479-MR. ACFT WAS GROUNDED.Feb 26, 2013 · N744AX · Boeing 767232 · Fuselage Main, Plate/SkinSDR ABXA20130226406Structure · corrodedHORIZONTAL CENTER SECTION LOWER RBL 41.5 STR 5 BETWEEN RIBS 2 & 3 HAS HEAVY CORROSION JUST OUTBOARD RIB 2R. CORRODED AREA FOUND TO BE OUT OF LIMITS, REPAIRED AREA IAW REA B655-60481-MR, ACFT WAS GROUNDED.Feb 26, 2013 · N744AX · Boeing 767232 · Horizontal Stabilizer Miscellaneous StructureSDR ABXA20130226404Slat · corrodedNR 8 SLAT NEEDS REMOVED AND REPLACED DUE TO CORROSION FINDING. REMOVED & REPLACED NR 8 SLAT IAW B767 AMM 27-81-02, ACFT WAS GROUNDED.Feb 26, 2013 · N744AX · Boeing 767232 · Leading Edge DevicesSDR ABXA20130223401Spar · corrodedCORROSION ON RIGHT WING UPPER SURFACE FORWARD SPAR ATTACH AREA. REMOVED CORROSION IAW B767 SRM 51-10-02 & 57-20-01. C/W REA 657-60480-MR, ACFT WAS GROUNDED.Feb 23, 2013 · N744AX · Boeing 767232 · Wing SparSDR ABXA20130223399Skin · corrodedRIGHT WING UPPER SKIN HAS AREA OF CORROSION AT FWD SPAR ATTACH POINT WS 433 APROX FORWARD OF VORTEX GENERATORS. REMOVED CORROSION IAW B767 SRM 51-10-02 & 57-20-01. C/W REA 657-60480-MR, ACFT WAS GROUNDED.Feb 23, 2013 · N744AX · Boeing 767232 · Wing, Plate/SkinSDR ABXA20130222409Intercostal · crackedINTERCOSTAL CRACKED AND CORRODED RIGHT SIDE OF LOWER CARGO FLOOR BETWEEN STA 1263 AND STA 1285. REMOVED AND REPLACED LOWER CARGO FLOOR INTERCOSTAL ON RIGHT SIDE STA 1263 AND STA 1285 IAW B767 SRM 51-40-02 STEP 7(D), ACFT WAS GROUNDED.Feb 22, 2013 · N744AX · Boeing 737232 · Fuselage Miscellaneous StructureSDR ABXA20130222407Intercostal · corrodedINTERCOSTAL BEHIND LOWER CARGO DOOR AFT HINGE IS CORRODED. BLENDED AREA, .040" MATERIAL REMAINED FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED INTERCOSTAL, ALL WORK DONE IAW B767 SRM 53-00-04, 51-40-02 PARA 7 & BOEING DWG 435T535-8, ACFT WAS GROUNDED.Feb 22, 2013 · N744AX · Boeing 767232 · Fuselage Miscellaneous StructureSDR ABXA20130218402Support Beam · corrodedRIGHT WING AFT OF REAR SPAR WING STATION 360 HAS CORROSION ON SUPPORT BEAM BELOW ANGLE DRIVE FLAP GEARBOX FOR INBD FLAP. REMOVED AND REPLACED CORRODED BEAM IAW B767 SRM 51-40-02. RIGHT WING TRAILING EDGE WS 375 FUSELAGE STA 1043, ACFT WAS GROUNDED.Feb 18, 2013 · N744AX · Boeing 767232 · Wing Miscellaneous StructureSDR ABXA20130223400Skin · corrodedRIGHT WING UPPER SKIN HAS AREA OF CORROSION AT FWD SPAR ATTACH POINT WS 490 APROX FWD OF VORTEX GENERATORS. REMOVED CORROSION IAW B767 SRM 51-10-02 & 57-20-01. C/W REA 657-60480-MR, ACFT WAS GROUNDED.Feb 3, 2013 · N744AX · Boeing 767232 · Wing, Plate/SkinSDR ABXA20121126296Socket · dirtyL1 EXTERIOR EMERGENCY LIGHT FAIL TO TEST. REMOVED EXT EMERGENCY LIGHT, AND CLEANED LAMP HOLDER SOCKET PER AMM 33-51-16-2. OPERATIONAL CHECK OK, ACFT WAS GROUNDED.Nov 26, 2012 · N744AX · Boeing 767232 · Emergency LightingSDR ABXA20111004118Stringer · crackedSTRINGER S7L IS CRACKED JUST AFT OF STA 676. REMOVED STRINGER SECTION, FABRICATED REPAIR FOR S7L STA 676 AND SPLICED IN REPLACEMENT SECTION IAW B767 200 SRM 53-00-03 FIG 201 REPAIR 1 AND REA B653-59499 MR, AWG.Oct 4, 2011 · N744AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
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