Boeing 767-281

Service difficulty reports · 1,831

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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 aircraft_model_key = '767281'
  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 UIEA2015030500162Support Angle · damagedAFT ATTACH BRACKET FOR FLOOR PANEL ABOVE MEC DOOR, OPEN POSITION CHECKED. REMOVED DAMAGED SUPPORT ANGLE, FABRICATED NEW ANGLE FROM 7075-T6,0063 P0 0048004. INSTALLED NEW SUPPORT ANGLE USING SRM 51-40-02 & 51-30-01. VERIFIED MATERIAL NR 15.Mar 5, 2015 · N658GT · Boeing 767281 · Fuselage Miscellaneous StructureSDR UIEA2015030500163Skin · corrodedCORROSION ON LT WING AT FS 939. REMOVED CORROSION, BLENDED AREA IAW REA 47136REA07.Mar 5, 2015 · N658GT · Boeing 767281 · Wing, Plate/SkinSDR ABXA20150227017Smoke Detector · false activationLAVATORY SMOKE ALARM SOUNDED, NO SMOKE OBSERVED. REPLACED LAVATORY SMOKE DETECTOR.Feb 27, 2015 · N788AX · Boeing 767281 · Smoke DetectionSDR ABXA20150224031Beam · corrodedDURING OK TO CLOSE OF LE PANELS FOUND CORROSION ON NUT STRIP ON FIXED LE AT APPROX LES 590. FOUND CORROSION TO BE ON NOSE BEAM WEB COMMON TO NUTPLATES. REMOVED WEB & FABRICATED NEW ONE FROM 7075-76-050 PO 0056503. INSTALLED NEW WEB & REMOVED ASSEMBLY IAW SRFeb 24, 2015 · N788AX · Boeing 767281 · Wing Miscellaneous StructureSDR ABXA20150224029Beam · corrodedLEFT HORIZONTAL STABILIZER UPPER REAR BEAM HAS AREAS OF CORROSION FROM ELEVATOR STATION 49 - 302. OUT OF LIMITS AREA ELEVATOR STATION 146 - 150.5. REPAIRED IAW REA B655-61427. THREE BLEND LOCATIONS FOUND TO BE WITHIN ACCEPTABLE LIMITS WHEN COMBINING SRM 55-Feb 24, 2015 · N788AX · Boeing 767281 · Horizontal Stabilizer Miscellaneous StructureSDR ABXA20150224020Angle · crackedVERTICAL STABILIZER TO SKIN ANGLE LT OTBD END CRACKED, ACCESS THROUGH PANEL 324AL. REMOVED ANGLE, FABRICATED NEW ANGLE IAW DWG 173T1302 FROM 2024-T3 .040. PERFORMED HFEC INSPECTION. INSTALLED NEW ANGLE IAW SRM 5140-02. SDR INFO, CRACKED 1.900", PN 173T1302Feb 24, 2015 · N788AX · Boeing 767281 · Vertical Stabilizer, Attach FittingsSDR ABXA20150224016Module · faultyFIRE WARNING BELL CAME ON CONTINUOUSLY WITH NO OTHER INDICATIONS. TESTED FIRE WARNING, ALL INDICATIONS NORMAL. REPLACED AURAL WARNING MODULE.Feb 24, 2015 · N769AX · Boeing 767281 · Fire DetectionSDR ABXA20150222028Rib · corrodedRIGHT WING TE LOWER CHORD OF SUPPORT RIB AT WS 1080 IS CORRODED & SPLIT. R & R RT WING TE LOWER CHORD OF SUPPORT RIB WS 1080 IAW SRM 51-40-02 & DOC 113T1521 REV 6. FABRICATED ON REA B657-61431. SDR INFO, PN 113T1521-16, PART NAME CHORD, SN NSN, CORRODED LEVFeb 22, 2015 · N788AX · Boeing 767281 · Wing, Rib/BulkheadSDR ABXA20150221026Spar · corrodedLEFT HORIZONTAL STABILIZER REAR SPAR & TE BEAM ARE CORRODED AT ELEVATOR STATION 325. REPAIRED OUT OF LIMITS AREA OF LT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD ELEVATOR STATION 321.5 - 337.5 IAW REA B655-61425-MR. TE BEAM AT ELEVATOR STATION 325 FOUND TO Feb 21, 2015 · N788AX · Boeing 767281 · Horizontal Stabilizer, Spar/RibSDR ABXA20150221025Spar · corrodedLEFT HORIZONTAL STABILIZER REAR SPAR IS CORRODED AT ELEVATOR STATION 139 - 143. REPAIRED OUT OF LIMITS AREA OF LT HORIZONTAL STABILIZER REAR UPPER CHORD ELEVATOR STATION 139 - 143 IAW REA B655-61435-MR. SDR INFO, PN 182T1100-1, PART NAME REAR SPAR UPPER CHORFeb 21, 2015 · N788AX · Boeing 767281 · Horizontal Stabilizer, Spar/RibSDR ABXA20150221022Rib · corrodedLEFT HORIZONTAL STABILIZER, ELEVATOR STATION 91 UPPER CHORD OF THE TE RIB IS CORRODED. R & R CHORD PN 183T1400-5 IAW SRM 51-40-02. SDR INFO, PN 183T1400-5, PART NAME UPPER CHORD, SN NSN, CORRODED LEVEL 2, EXACT FS & BS LOCATION ON ACFT ELEVATOR STATION 91. Feb 21, 2015 · N788AX · Boeing 767281 · Horizontal Stabilizer, Spar/RibSDR ABXA20150220027Structure · crackedEA 53500009-001 NEEDS ACCOMPLISHED. REPAIRED DAMAGED CHORD RT STATION 883.5 STRINGER 18R IAW SRM 53-50-07 REPAIR 1. SDR INFO CRACKED 0.250", PN 145T8000-1, SN N/A, PART NAME CHORD, FS LOCATION ON ACFT, FS 883.5, STRINGER LOCATION ON ACFT, STRINGER 18R. ACFTFeb 20, 2015 · N788AX · Boeing 767281 · Fuselage Miscellaneous StructureSDR ABXA20150220023Rib · corrodedLEFT HORIZONTAL STABILIZER, ELEVATOR STATION 215 UPPER CHORD OF THE TE RIB IS CORRODED. INSTALLED NEW LT HORIZONTAL STABILIZER, ELEVATOR STATION 215 UPPER CHORD OF THE TE RIB IAW REA B657-61411-MR & SRM 51-40-02. SDR INFO, CORRODED LEVEL 2, PN 183T1340-29, PFeb 20, 2015 · N788AX · Boeing 767281 · Horizontal Stabilizer, Spar/RibSDR ABXA20150220021Keelbeam · corrodedRIGHT KEEL BEAM LOWER INBD FLANGE LOWER SURFACE CORROSION FS 998 - 1007. REPAIRED RT KEEL BEAM IAW REA B653-61424-MR. SDR INFO, CRACKED, CORRODED L2, PN 145T8611, SN NSN, PART NAME KEEL BEAM, FS & BS LOCATION ON ACFT RT 998 TO 1007. ACFT WAS GNDED.Feb 20, 2015 · N788AX · Boeing 767281 · Fuselage Main, KeelSDR ABXA20150219030Beam · corrodedCORROSION FOUND ON FIXED LE STRUCTURE AT APPROX LE STATION 894 AT SCREW HOLE. REMOVED NOSE BEAM WEB ASSEMBLY, FABRICATED NEW WEB & REINSTALLED ASSEMBLY WITH NEW WEB IAW SRM 51-40-02 & DWG 114T2300. SDR INFO, CORRODED L2, PN 114T2300-39, SN NSN, PART NAME NOSFeb 19, 2015 · N788AX · Boeing 767281 · Wing Miscellaneous StructureSDR ABXA20150219024Rib · corrodedLEFT HORIZONTAL STABILIZER, ELEVATOR STATION 325 UPPER CHORD OF THE TE RIB IS CORRODED. REPLACED UPPER T CHORD FITTING ON LT HORIZONTAL STATION 325. PN 183T1530-5AX IAW SRM 51-40-02. SDR INFO, CORRODED L2, PN 183T1530-5AX, SN NSN, PART NAME UPPER CHORD, FS Feb 19, 2015 · N788AX · Boeing 767281 · Horizontal Stabilizer, Spar/RibSDR ABXA20150219015Warning Light · false activationMAIN CARGO DOOR LIGHT ILLUMINATED WHILE CLIMBING OUT OF 12000 FT. INDICATION SWITCHES WERE CHECKED & MEASURED. ALL SWITCHES WERE FOUND WITHIN LIMITS. OPS CHECK OF THE MAIN CARGO DOOR FOUND NO FAULTS.Feb 19, 2015 · N792AX · Boeing 767281 · Door Warning SystemSDR ABXA20150217019Beam · corrodedHYDRAULIC LINE SUPPORT CLIP OTBD & AFT OF TOP OF LG CORRODED ON TE SUPPORT. REMOVED CLIP, FOUND BEAM TO BE CORRODED. REPLACED BEAM, REINSTALLED CLIP IAW SRM 51-40-02 & DWG 113T1633. SDR INFO, CORRODED LEVEL 2, PN 113T1633-217, PART NAME BEAM, SN NSN, STRINGFeb 17, 2015 · N788AX · Boeing 767281 · Wing Miscellaneous StructureSDR ABXA20150217018Angle · corrodedLEFT FWD KEEL BEAM FWD STATION 977, LBL 2 CORROSION FOUND, MARKED WITH NR. FOUND ANGLE AT STATION 977, LBL 2 TO BE CORRODED BEYOND LIMITS IAW SRM 53-50-12 FIG 101. R & R ANGLE IAW SRM 51-40-02. SDR INFO, CORRODED LEVEL 2, PN 145T8604-2, PART NAME ANGLE, SN Feb 17, 2015 · N788AX · Boeing 767281 · Fuselage Main, KeelSDR UIEA2015021600124Spar · corrodedCORROSION ON RT WING AFT SPAR AT WS 920. REPAIRED RT WING TE IAW REA 47142REA01. SEE REA NR 547810000 0151 & PARTIAL WORK SHEET NR 3, IN WORK ORDER 9607 FOR WORK PERFORMED.Feb 14, 2015 · N659GT · Boeing 767281 · Wing SparSDR ABXA20150209005Beam · corrodedCORROSION AROUND NUTPLATE AT APPROX LES 620. R & R WEB IAW SRM 51-40-02. SDR INFO, CORRODED, PN 114T2300-225, SN N/A, PART NAME NOSE BEAM. ACFT WAS GNDED.Feb 9, 2015 · N788AX · Boeing 767281 · Wing Miscellaneous StructureSDR ABXA20150206006Spar · corrodedCORROSION AROUND NUTPLATES ON REAR SPAR TO TE BEAM UPPER CHORD AT WS 433 NEAR TE. R & R UPPER CHORD WS 433 REAR SPAR TO TE IAW SRM 51-40-02. SDR INFO, CORRODED L2, PN 113T1510-33, SN NSN, PART NAME CHORD, AILERON SUPP STRINGER & WS LOCATION ON ACFT WS 433. Feb 6, 2015 · N788AX · Boeing 767281 · Wing SparSDR ABXA20150201002Switch · out of toleranceMAIN CARGO DOOR LIGHT & SIREN ILLUMINATED DURING CLIMB OUT AT APPROXIMATELY 2.0 TO 2.1 PSID. INDICATION SWITCHES GAP ADJUSTED TO TOLERANCE & E1-1 BURNDY BLOCK CLEANED. WORN DOOR MECHANISM CAUSING SWITCH GAP TO FALL OUT OF TOLERANCE.Feb 1, 2015 · N794AX · Boeing 767281 · Door Warning SystemSDR UIEA2015012000008Skin · corrodedLEFT WING OVERWING FILL PORT FAILED BONDING RESISTANCE CHECK, READ INFINITE RESISTANCE IAW JC A-028-018-03. REMOVED FILL PORT, CLEANED CORROSION & REINSTALLED FILL PORT IAW SRM 57-20-01 & AMM 28-11-04 REA 47135REA02 A.Jan 18, 2015 · N656GT · Boeing 767281 · Wing, Plate/SkinSDR UIEA2015012000009Skin · corrodedRIGHT WING OVERWING FILL PORT FAILED BONDING RESISTANCE CHECK, READS INFINITE RESISTANCE IAW JC A-28-018-04. REMOVED & REINSTALLED FILL PORT IAW AMM 28-11-04. REMOVED CORROSION IAW SRM 27-20-01.Jan 18, 2015 · N656GT · Boeing 767281 · Wing, Plate/SkinSDR ABXA20141022335Beam · corrodedLEFT FLAP 9 - 10 BEAM 4 AFT ATTACHMENT & 2 FWD ATTACHMENT HOLES ARE CORRODED. REMOVED & RE-ROUTE 9 - 10 BEAM TO COMPONENT SERVICES FOR REPAIR IAW REA C057-61249-MR. REINSTALLED BEAM IAW REA C057-61249-MR. CORRODED L2, PN 113T1266-25, SN NSN, PART NAME LT INOct 22, 2014 · N787AX · Boeing 767281 · Trailing Edge FlapsSDR ABXA20141021336Support · corrodedRIGHT WING PANEL 661NB AFT PANEL SUPPORT EXFOLIATED. R & R PANEL SUPPORT IAW B657-61286. CORRODED L2, PN 113T1912-29, PART NAME BEAM, SN NSN, STRINGER & WS LOCATION WS 1079.95. ACFT WAS GNDED.Oct 21, 2014 · N787AX · Boeing 767281 · Wing Miscellaneous StructureSDR ABXA20141021334Beam · corrodedRIGHT FLAP 9 - 10 BEAM FWD 4 & AFT 2 ATTACHMENT HOLES ARE CORRODED. REMOVED & RE-ROUTE 9 - 10 BEAM TO COMPONENT SERVICES FOR WORK IAW REA C057-61250-MR. REINSTALLED 9 - 10 BEAM & NEW FASTENERS IAW REA C057-6150-MR. CORRODED L2, PN 113T1226-26, SN NSN, PARTOct 21, 2014 · N787AX · Boeing 767281 · Trailing Edge FlapsSDR ABXA20141017320Support Fitting · crackedSPOILER ACTUATOR SUPPORT BRACKET CRACKED IN TWO AT RT WING STATION 700. LOCATED JUST FWD OF FLAP TORQUE TUBE SUPPORT. REMOVED & INSTALLED SERVICEABLE FITTING IAW DWG 113T1421. CRACKED 2 INCHES, PN 113T1566-26, SN NSN, PART NAME FITTING, WING SPAR WINGS, STOct 17, 2014 · N787AX · Boeing 767281 · SpoilersSDR ABXA20141016331Structure · crackedRIGHT 1809 CHORD CRACKED AREA 2 FWD LOWER LE. FWD LOWER FASTENER OF AREA 1 NEEDS REMOVED TO VERIFY DEFECT INDICATION IAW STEP 11 OF TASK CARD NEA53800003-001. REPAIRED CHORD IAW SB 767-53A0078. CRACKED, LENGTH .5, PN 015T1059-4, PART NAME CHORD, SN NSN, FSOct 16, 2014 · N787AX · Boeing 767281 · Fuselage Miscellaneous StructureSDR ABXA20141013332Rib · crackedRIGHT OTBD FLAP NR 7 SUPPORT INBD FLANGE ACTUATOR HOLE AT 1:00 LOOKING INBD HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN, ALSO OTBD FLANGE HOLE AT 12:00 HAS AN INDICATION WITH ROTARY SCAN. REAMED & RE-BUSHINGED HOLE LAW SRM 51-70-16 NDT HOLE NO DAMAGE FOUND.Oct 13, 2014 · N787AX · Boeing 767281 · Wing, Rib/BulkheadSDR ABXA20141013330Splice Plate · corrodedFRONT SPAR UPPER CHORD CORRODED ABOVE NR 8 SLAT TAI TELESCOPING DUCT. REPAIRED CORROSION ON UPPER SPLICE PLATE IAW REA B657-61236. L2 CORROSION, PN 114T023-20, PART NAME SKIN SPLICE, SN NSN, LOCATION WS 450 TO 464. ACFT WAS GNDED.Oct 13, 2014 · N787AX · Boeing 767281 · Wing, Plate/SkinSDR ABXA20141008333Splice Plate · crackedNUMBER 1 PYLON AT INBD LOWER BEAM HYD BAY DOOR AT AFT END STRUCTURE IS CRACKED ABOVE & BELOW THE BEAM. R & R SPLICE PLATE IAW SRM 51-10-2. CRACKED 2.O INCHES, PN 313T3380-59, PART NAME SPLICE PLATE, SN NSN, STRINGER & WS LOCATION 318.50 TO 318.50. ACFT WAS Oct 8, 2014 · N787AX · Boeing 767281 · Nacelle/Pylon, Plate/SkinSDR ABXA20141007321Splice Plate · corrodedFRONT SPAR UPPER CHORD CORRODED AT LES 464. REMOVED CORROSION FOUND TO BE OUT OF LIMITS WILL BE REPAIRED ON REA B657-61236. CORRODED L2, PN 114T023-20, SN NSN, PART NAME UPPER SPLICE PLATE, STRINGER & WS LOCATION LES 464. ACFT WAS GNDED.Oct 7, 2014 · N787AX · Boeing 767281 · Wing Miscellaneous StructureSDR ABXA20141006329Rib · crackedRIGHT WING NR 8 ACTUATOR SUPPORT INBD FLANGE 1 EACH HOLE OVERSIZE, 1 EACH OTBD HOLE. REPAIRED HOLES IAW REA B657-61258-MR, RFTS NR E-46238. CRACKED .0625 INCHES, PN 113T1345-22, PART NAME FLAP SUPPORT RIB NR 8, SN NSN, STRINGER & WS LOCATION WS 798.2. ACFT Oct 6, 2014 · N787AX · Boeing 767281 · Wing, Rib/BulkheadSDR ABXA20141006323Fitting · corrodedLEFT 1809 CHORD TENSION FITTING AREA 1 UPPER AFT HOLE ELONGATED. PERFORMED PERMANENT REPAIR OF THE FWD CHORD IAW SB 767-53A0078. CORRODED L2, PN 0157T1059-7, 148T904441, 015T1059-3148T2512-7, PART NAME CHORD SPLICE FITTING, TENSION FITTING. CHORD SPLICE, LOOct 6, 2014 · N787AX · Boeing 767281 · Fuselage Miscellaneous StructureSDR ABXA20141003327Rib · crackedLEFT OTBD FLAP NR 2 SUPPORT INBD FLANGE 2 ACTUATOR HOLES AT 12:00 HAVE DEFECT INDICATIONS WITH HFEC ROTARY SCAN. OTBD FLAP NR 2 SUPPORT INBD FLANGE 2 ACTUATOR HOLES AT 12:00 ARE REPAIRED ON REA B657-61257. CRACKED .01562 INCHES, PN 113T1345-25, PART NAME LT Oct 3, 2014 · N787AX · Boeing 767281 · Wing, Rib/BulkheadSDR ABXA20141002326Rib · crackedFLANGE ACTUATOR HOLE AT 12:00 HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. CLEANED OUT HOLES LAW AMM 20-10-22 SEE REA 657-61238-MR. CRACKED 1/64, PN 113T1345-19, PART NAME LT WING OTBD FLAP SUPPORT RIB NR 1, SN NSN, STRINGER & WS LOCATION WS 798.2. ACFT Oct 2, 2014 · N787AX · Boeing 767281 · Wing, Rib/BulkheadSDR ABXA20140930324Strap · crackedINSIDE ACCESS PANEL 447BR NR 2 STRUT AFT VERTICAL ROW OF FASTENERS FOR ARROWHEAD PANEL STRUCTURE IS CRACKED. R & R DOUBLER LAW SRM 51-40-02 PER 7. CRACKED 3 INCHES, PN 313T3380-245, PART NAME STRAP, SN N/A, EXACT NACELLE STATION 400, EXACT STRINGER & WS FROSep 30, 2014 · N787AX · Boeing 767281 · Nacelle/Pylon Miscellaneous StructureSDR ABXA20140929328Fitting · crackedNUMBER 2 ENG OTBD CORE COWL NR 4 LATCH FITTING CRACKED INSIDE OF POCKET & LOCK FASTENERS ARE DAMAGED. REMOVED OLD LATCH FITTING & DRILLED NEW FITTING IAW SRM 51-40-5 & SRM 51-40-0. INSTALLED NEW FITTING IAW SRM 51-40-02. CRACKED .500, PN 314T1223, PART NAMESep 29, 2014 · N787AX · Boeing 767281 · Engine Cowling SystemSDR ABXA20140928322Keelbeam · corrodedCENTER BEAM IN LT WW BS 997, LBL 8, WL 115 IS CORRODED. CORRODED AREA WAS BLENDED, FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-50-12. REPAIRED IAW REA B653-61253-MR & SRM 51-40-02. CORRODED L2, PN 145T8612-1, PART NAME WEB, KEEL BEAM, SN NSN, EXACT FS & Sep 28, 2014 · N787AX · Boeing 767281 · Fuselage Main, KeelSDR ABXA20140925325Beam · crackedNUMBER 2 STRUT OTBD LOWER BEAM IS CRACKED AT FWD END. R & R OTBD LOWER STRUT BEAM INSTALLED IAW SRM 51-40-02. INSTALLED BRACKETS IAW SRM-51-40-02. PN 313T1380-242, PART NAME OTBD BEAM, CRACKED 1.75 INCHES, SN N/A, EXACT STRINGER & WS LOCATION ON MC 310 TO 3Sep 25, 2014 · N787AX · Boeing 767281 · Nacelle/Pylon Miscellaneous StructureSDR ABXA20140925319Support · corrodedRIGHT WING UPPER PANEL SUPPORT TEE INBD END OF 651MT EXFOLIATED NEAR AFT END OF TEE. R & R UPPER CLAMP LAW SRM 51-40-2. CORRODED L2, PN 113T1623-158, PART NAME CHORD, SN NSN, EXACT STRINGER & WS LOCATION ON NC 273WS TO 275WS. ACFT WAS GNDED.Sep 25, 2014 · N787AX · Boeing 767281 · Wing Miscellaneous StructureSDR ABXA20140925311Channel · damagedWING TE PANEL ATTACH CHANNEL LOWER CHORD SPLIT ON EDGE AT WS 424.22 INCHES FROM REAR SPAR. INSTALLED NEW CHORD IAW REA B657-61210-MR & SRM 51-40-02. PANEL 552JB INSTALLED IAW SRM 51-40-02. SDR INFO PN 113T1407-1, PART NAME SPOILER BEAM CHORD, L2 CORROSION, Sep 25, 2014 · N795AX · Boeing 767281 · Wing Miscellaneous StructureSDR ABXA20140924315Bushing · wornLEFT WING NR 2 FLAP HINGE 9 - 10 BEAM HAS LOOSE BUSHINGS IN CTR OF THE BEAM. REPLACED BUSHINGS IAW REA C027-61235-MR. PN 113T1347-7, PART NAME BUSHING, WORN & LOOSE BUSHING, EXACT FS & BS LOCATION ON ACFT LT WING, EXACT WS LOCATION ON ACFT WS 616. ACFT WAS Sep 24, 2014 · N795AX · Boeing 767281 · Trailing Edge FlapsSDR ABXA20140924314Bearing · wornRIGHT FLAP HINGE POINT 9 - 10 BEAM HAS A LOOSE BEARING & A LOOSE BUSHING. R & R BEARING ON 9 - 10 BEAM AT FLAP SUPPORT NR 7 IAW CMM 27-51-97. THE 9 - 10 BEAM WILL BE INSTALLED ON NR 0037, SEE REACO27-61234-MR. PN 60B00180-236, PART NAME BEARING, WORN & LOOSSep 24, 2014 · N795AX · Boeing 767281 · Trailing Edge FlapsSDR ABXA201409243008Keelbeam · corrodedCORROSION FOUND BETWEEN STATION 999 & 1021 IN LT WW CTR BEAM. REMOVED CORROSION IAW SRM 53-50-12 & COMPLIED WITH REA NR B653-61251-MR. CORRODED L2, PN 145T8612-1, PART NAME KEEL WEB, SN N/A, LOCATION STATION 999 LBL TO 1021 LBL. ACFT WAS GNDED.Sep 24, 2014 · N795AX · Boeing 767281 · Fuselage Main, KeelSDR ABXA20140923318Skin · crackedSKIN CRACKED AROUND RIVETS AT STATION 1654 ADJACENT TO STRINGERS 3L, 4L & 5L. REPAIRED SKIN IAW SRM 53-80-01 FIG 201 REPAIR 4. CRACKED, 0.6 INCHES, PART NAME SKIN, PN 148T3111, SN NSN, LOCATION FROM 1654 STRINGER & WS, LOCATION STRINGER 3L - 8L. ACFT WAS GSep 23, 2014 · N795AX · Boeing 767281 · Fuselage Main, Plate/SkinSDR ABXA20140926316Beam · crackedLEFT WING NR 8 123 BEAM HAS 1 CRACK INDICATION. YOU CAN SEE THE DEFECT AT THE BOTTOM OF THE HOLE LOOKING FROM INBD OUT. REAMED HOLE CLEAN & ROUND IN 1/64TH INCREMENTS & COMPLIED WITH HFEC HOLE SCAN. REPAIRED NR 8 1-2-3 BEAM IAW REA CO57-61254-MR. ALSO REFESep 23, 2014 · N795AX · Boeing 767281 · Wing Miscellaneous StructureSDR ABXA20140917312Stringer · crackedAT STRINGER 17L AT STATION 676 FOUND STRINGER CRACKED. REPAIR CRACKED STRINGER 17L STATION 676 UPPER CARGO AREA IAW ARM 53-00- 03 & REA NR B653-61203MR. CRACKED 2.0 INCHES, PN 143T3001-10, PART NAME STRINGER, LOCATION 675L TO 700L, STRINGER & WS LOCATION 17LSep 17, 2014 · N795AX · Boeing 767281 · Fuselage Main, Longeron/Stringer
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