Boeing 767-200

Service difficulty reports · 568

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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 = '767200'
  ORDER BY difficulty_date DESC"

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SDR CNMA2018010002Windshield · crackedR1 WINDOW CRACKED IN FLIGHT AT FLIGHT LEVEL 360. R FWD WINDSHIELD HEAT INOP AFTEFRWARDS REMOVED & REPLACED R1 WINDOW IAW 767 AMM 56-11-01. OPS CK NORMALFeb 12, 2018 · N234AX · Boeing 767200 · Flight Compartment WindowsSDR ABXA20160718117Skin · corrodedREMOVED CORROSION IAW SRM 57-51-02, FIG 101. INITIAL THICKNESS .094, REMAINING THICKNESS .061. BLENDED AREAS REQUIRED REPAIR AND WERE REPAIRED ON REA B657-62130. CORRODED LEVEL 2, PN 113T1621-58, SKIN, FS/BS LOCATION: FROM R/W T/E TO UPPER STR, WS LOCATION: Jul 18, 2016 · N797AX · Boeing 767200 · Fuselage Main, Plate/SkinSDR ABXA20160718116Skin · corrodedFOUND SKIN CORROSION COMMON TO THE TRIMMED OUT SECTION OF THE FAIL SAFE. CORROSION IS ISOLATED TO THE LOWER HOLE. COMPLIED WITH TASK CARD EA 53500014-004 AND DOCUMENT 470080RD10 CORROSION WAS REMOVED, WITHIN THE ALLOWABLE LIMITS. CORRODED, LEVEL 2, PN 145T34Jul 18, 2016 · N797AX · Boeing 767200 · Fuselage Main, Plate/SkinSDR ABXA20160718115Failsafe · crackedCOMPLIED WITH TC S53-050·04-2. RT WHEEL WELL STA 955, RT FAIL-SAFE HAS HFEC DEFECT INDICATION AT LOWER HOLE COMMON TO FAIL-SAFE AND TEE FITTING. REF: SB 767-53A0100, FIG 2, SH 1. COMPLIED WITH FAIL SAFE TRIM OUT AT TC EA 53500014-003 AND DOCUMENT 47008 AND 04Jul 18, 2016 · N797AX · Boeing 767200 · Fuselage Main, FrameSDR ABXA20160216008Rib · corrodedLEFT WING LE CORROSION ON RIB AT LES 436. REMOVED LT WING TAI DUCT, CORROSION OUT OF LIMITS ON RIB. R & R RIB IAW SRM 51-40-02 PARA 7 & 4B. REINSTALLED TAI DUCT IAW MM 20-11-00, LEAK CHECKED GOOD IAW MM 3071-00. CORRODED LEVEL 2, PN 114T2200-17, PART NAME Feb 16, 2016 · N798AX · Boeing 767200 · Wing, Rib/BulkheadSDR ABXA20160212031Beam · corrodedWING TE UPPER PANEL ATTACH BEAM RUNNING LENGTH WAYS, CORRODED ON FWD SIDE AT WS .273, INBD OF NR 6 SPOILER, AS SEEN THRU PANEL 551VB OPENING. REMOVED ATTACH BEAMS & INSTALLED SERVICEABLE ATTACH BEAMS, PN 113T1633-157 IAW SRM 51-40-02. CORRODED LEVEL 2, PN 11Feb 12, 2016 · N797AX · Boeing 767200 · Wing Miscellaneous StructureSDR ABXA20160212013Frame · crackedSTATION 883.5, LBL 89 LT SIDE FRAME INNER CHORD CRACKED 1/4" AT TRANSITION RAD II. IAW WS02568 FIG 1 SH 2 FOR LOCATION. INNER CHORD CRACK WILL BE REPAIRED ON JC EA 53000049-101. CRACKED LENGTH .25", PN 145T1004-1, PART NAME, INNER CHORD, SN NSN, BS LOCATIONFeb 12, 2016 · N798AX · Boeing 767200 · Fuselage Main, FrameSDR ABXA20160211028Structure · corrodedUPPER WING TE PANEL, ATTACH CHORD AT WING TO FUSELAGE JUNCTION, ABOVE UPLOCK CYLINDER, CORRODED AROUND NUTPLATES. REMOVED ATTACH CHORD & INSTALLED SERVICEABLE ATTACH CHORD, PN 113T1621-55 IAW SRM 51-40-2. CORRODED LEVEL 2, PN 113T1621-55, PART NAME ATTACH COFeb 11, 2016 · N797AX · Boeing 767200 · Fuselage Main, Attach FittingsSDR ABXA20160210030Structure · corrodedUPPER CHORD CORRODED ON REAR SPAR TO WING TE BEAM, AT STATION 285, AT AFT END AS SEEN UNDER INBD END OF NR 6 SPOILER. REMOVED TE BEAM ASSEMBLY, R & R UPPER CHORD, PN 113T1623-141, WITH SERVICEABLE CHORD, INSTALLED TE BEAM ASSEMBLY IAW SRM 51-40-2. CORRODED LFeb 10, 2016 · N797AX · Boeing 767200 · Wing Miscellaneous StructureSDR ABXA20160210027Structure · corrodedSTATION 859.5, RBL 89 INNER CHORD CRACKED .450" APPROX AT TRANSITION RADIUS, IAW ES02568 FIG 1 SH 2 ATTACHED TO NEA 53000045-001 FOR CRACK LOCATION. REPAIRED INNER CHAP AT STRINGER 859.5, RBL 89. IAW EA 53000048-101 & REA B653-61905-513. CORROSION LEVEL 2, PFeb 10, 2016 · N797AX · Boeing 767200 · Fuselage Miscellaneous StructureSDR ABXA20160210009Bear Strap · corrodedRIGHT OVERWING EXIT CUT OUT FWD SIDE HAS CORROSION. REPAIRED CORRODED AREA AT RT OVERWING EXIT CUT OUT FORWARD SIDE, BETWEEN STATION 859 - 862, STRINGER 16R - 17R IAW REA B653-61943-MR. CORRODED, PN 145T28320-10, PART NAME UPPER BEAR STRAP, SN NSN, FS & BS LFeb 10, 2016 · N798AX · Boeing 767200 · Fuselage Main, Plate/SkinSDR ABXA20160209019Stringer · crackedSTATION 676, AFT STRINGER 19L, LOWER HAT FLANGE CRACKED, AT 4 SPLICE FITTING FLANGE FASTENER LOCATIONS. REPAIR IAW NEA53100137-201 STEP 27 B B 2 & ENGINEERING. COMPLETED M-289, REPAIRED STRINGER 19L TO STATION 676 IAW ENGINEERING SKETCH ES 02821. CRACKED 4"Feb 9, 2016 · N798AX · Boeing 767200 · Fuselage Main, Longeron/StringerSDR ABXA20160209017Stringer Splice · crackedSTATION 676, STRINGER 4L SPLICE HAS 3/4" CRACK ON VERTICAL LEG FWD SIDE OF FRAME. CONTACT ENGINEERING FOR REPAIR. COMPLETE M 289, REF NEA53100137-201. R & R SPLICE IAW B767 SRM 51-40-02 REA B653-61924MR. CRACKED LENGTH .650, PN 368-53-00-95387, SN N/A, PARTFeb 9, 2016 · N798AX · Boeing 767200 · Fuselage Main, Longeron/StringerSDR ABXA20160208029Beam · corrodedWING TE AFT LOWER CHORD FOR PANEL 552HB AT TE WS 418 SPLIT ON EDGE. R & R CHORD AT STATION 418 IAW SRM 51-40-02. FABRICATED CHORD, PN 133T1407-1, IAW REA B657-61929MR. CORRODED LEVEL 2, PN 113T1407-1, SN NSN, PART NAME, SPOILER BEAM CHORD LOWER, EXACT FS & Feb 8, 2016 · N797AX · Boeing 767200 · SpoilersSDR ABXA20160208020Stringer · crackedSTATION 676 AFT STRINGER 24L, UPPER HAT FLANGE CRACKED, APPROX 5". REPAIR IAW NEA 53100137-201 STEP 27 B B 2 & ENGINEERING. COMPLETED M-289, REPAIRED 524L IAW SRM 53-00-03 & NEA5310037-201 STEP 27B. CRACKED LENGTH 4.75", PN 143T3001-32, PART NAME STRINGER 24Feb 8, 2016 · N798AX · Boeing 767200 · Fuselage Main, Longeron/StringerSDR ABXA20160205026Shear Tie · corrodedAFT BULK CARGO COMPARTMENT, BILGE AREA, STATION 1562, CORROSION. R & R REQUIRED PARTS & HARDWARE IAW SRM 51-40-02 PARA 4 & PARA 9. CORRODED LEVEL 2, PN 146T1223-23, PART NAME SHEAR TIE, EXACT FS & BS LOCATION ON ACFT 1562. EXACT STRINGER & WS LOCATION ON ACFeb 5, 2016 · N797AX · Boeing 767200 · Fuselage Internal Mounting StructureSDR ABXA20160205018Stringer · crackedSTATION 676, AFT STRINGER 8L, UPPER HAT FLANGE CRACKED APPROX 4", LOWER HAT FLANGE CRACKED APPROX 5 1/2". REPAIR IAW NEA53100137-201 STEP 16 B B 2 & ENGINEERING. COMPLETE M-289 IAW NEA53100137-201. PERFORMED REPAIR IAW ENGINEERING SKETCH E502821 FIG 7. INSFeb 5, 2016 · N798AX · Boeing 767200 · Fuselage Main, Longeron/StringerSDR ABXA20160204021Floor Support · corrodedFLOOR SUPPORT AT STATION 610, APPROX RBL 20 CORRODED. R & R SUPPORT ANGLE FROM STATION 615 - 532. INSTALLED SUPPORT CLIP IAW SRM 51-40-02 FIG 12. CORRODED LEVEL 2, PN 143T5000-36AX, SN NA, PART NAME SUPPORT, EXACT FS & BS LOCATION ON ACFT FROM STATION 615 Feb 4, 2016 · N798AX · Boeing 767200 · Fuselage Miscellaneous StructureSDR ABXA20160204014Frame · crackedSTATION 883.5, RBL 89 RT SIDE FRAME INNER CHORD CRACKED 1/4" AT TRANSITION RADII. EF ES02568 FIG 1 SH 2 FOR LOCATION. REPAIR WILL BE ACCOMPLISHED & DOCUMENTED ON JC EA 53000050-101. CRACKED LENTH .25", PN 145T1004-2, PART NAME, INNER CHORD, SNS NSN, FS & BSFeb 4, 2016 · N798AX · Boeing 767200 · Fuselage Main, FrameSDR ABXA20160203035Bulkhead · corrodedFORWARD SIDE OF APB, BETWEEN RS 18 & 21, OS TS1 HAS SEVERAL AREAS OF CORROSION. REPAIRED APB IAW SRM 53-80-08 REPAIR 2 DETAIL II FIG 201. CORRODED LEVEL 2, PN PO-06072803, PART NAME APB DOUBLER, FS & BS LOCATION RS 18 - 21, STRINGER & WS N/A TO N/A. ACFT WAFeb 3, 2016 · N797AX · Boeing 767200 · Fuselage Main, BulkheadSDR ABXA20160202024Splice Plate · corrodedRIGHT WING CORRODED, BETWEEN NUTPLATE CHANNEL & WING LOWER SURFACE AT LE STATION 1070, FWD OF FRONT SPAR. R & R DAMAGED AREA IAW REA B657-61897 REV IR 01-06-2016. CORRODED LEVEL 2, PN 114T0222, SN N/A, PART NAME, LOWER SPLICE PLATE, EXACT FS & BS LOCATION ONFeb 2, 2016 · N797AX · Boeing 767200 · Wing Miscellaneous StructureSDR ABXA2016020223Beam · corrodedNUMBER 8 SUPPORT 123 BEAM, C FASTENER ONE EACH SHOWS CRACK INDICATION & CORROSION IN BOTTOM. REQUEST TECHNICAL ENGINEERING ASSISTANCE, REPAIRED HOLE ON THE NR 8 FLAP SUPPORT 1 - 3 BEAM IAW REA CO57-61926-MR. CORRODED LEVEL 2, PN 113T1313-8, PART NAME 1-3 BEFeb 2, 2016 · N798AX · Boeing 767200 · Wing Main, Frame StructureSDR ABXA20160202022Beam · gougedNUMBER 2 FLAP SUPPORT 1-3, BEAM HAS A GOUGE AROUND FASTENER HOLE. REPAIRED HOLE ON THE NR 2, 1 - 3 BEAM FOR THE NR 2 FLAP SUPPORT IAW REA CO57-61933-MR. PN 113T1314-15, PART NAME 1 - 3 BEAM. SN ABXV654, WS LOCATION, 616.2 - 616.2. ACFT WAS GNDED.Feb 2, 2016 · N798AX · Boeing 767200 · Wing Main, Frame StructureSDR ABXA20160129034Floorbeam · corrodedCORRODED T CAP STATION 246, UNDER FWD LAVATORY AREA. REMOVED & FABRICATED NEW FLOORBEAM USING PO 0077887 7075-T6 .050, EXTRUSION IAW SRM 53-10-51 FIG 201. CORRODED, PN 141T5814-78, PART NAME CHORD, SN NSN, EXACT FS & BS LOCATION ON ACFT, FROM STATION 246, LBJan 29, 2016 · N797AX · Boeing 767200 · Fuselage Main, Floor BeamSDR ABXA20160129011Rib · corrodedNUMBER 5 SLAT UPPER RIB ON INBD SIDE OF TELESCOPING DUCT CORRODED. R & R NR 5 SLAT UPPER RIB ON INBD SIDE OF TELESCOPING DUCT IAW DWG 114T2202 & SRM 51-40-02. CORRODED LEVEL 2, PN 114T2202-23, PART NAME RIB, SN NSN, WS LOCATION, FROM 456 TO 456. ACFT WAS GNJan 29, 2016 · N798AX · Boeing 767200 · Leading Edge DevicesSDR ABXA20160129006Rib · corrodedLEFT WING LE CORROSION IN TWO PLACES ON RIB AT LES 779. R & R RIB IAW REA B657-61902 & SRM 51-40-02. CORRODED LEVEL 2, PN 114T2217-15, SN N/A, PART NAME RIB, EXACT STRINGER & WS LOCATION ON ACFT FROM WS 779. ACFT WAS GNDED.Jan 29, 2016 · N798AX · Boeing 767200 · Wing, Rib/BulkheadSDR ABXA20160128016Frame · corrodedLOWER FRAME CORRODED, AT STATION 742L, BETWEEN STRINGER 34L & 36L, IN THREE PLACES. BLENDED CORROSION, SHEAR TIE OUT OF LIMITS, TO BE REPAIRED ON NON-ROUTINE 0822. BLENDED WEB STATION 742L, STRINGER 34 - 35L. ORIGINAL MT .032, REMOVED .003, REMAIN .029 WITHJan 28, 2016 · N798AX · Boeing 767200 · Fuselage Main, FrameSDR ABXA20160126025Frame · corrodedNUMBER 1 SLAT INBD IDLER TRACK, OTBD FRAME, CORROSION. REMOVED EXISTING FRAME, PN 114T2227-15 & INSTALLED SERVICEABLE FRAME IAW SRM 51-40-2. SDR INFO, CORRODED LEVEL 2, PN 114T2277-15, PART NAME: FRAME RIB STRUT, STRINGER & WS LOCATION. OSS1029 - OSS1029. AJan 26, 2016 · N797AX · Boeing 767200 · Leading Edge DevicesSDR ABXA20160126015Support · corrodedREFERENCE CARRY OVER ITEM 62398-001, PERMANENT TRUNNION SUPPORT RE. PN 112T1711-8, PART NAME, SUPPORT ASSEMBLY, SN NSN, CORRODED LEVEL 2, EXACT STRINGER & WS LOC ON ACFT, RT TE WS310 TO WS310. ACFT WAS GNDED.Jan 26, 2016 · N798AX · Boeing 767200 · Wing, Landing Gear Attach FittingsSDR ABXA20160120012Rib · corrodedNUMBER 8 FLAP SUPPORT, OTBD SPAR FITTING HAS PITTING IN CRANK ARM BUSHING BORE. REPAIRED IAW REA B657-61911-MR. LEVEL 2 PN 113T1345-20, PART NAME, RIB ASSEMBLY, SN NSN, STRINGER & WS LOCATION FROM, WS 798 - 798. ACFT WAS GNDED.Jan 20, 2016 · N798AX · Boeing 767200 · Wing, Rib/BulkheadSDR ABXA20160119033Shear Tie · corrodedCORRODED SHEAR TIE, AT STATION 1329, RBL 93. REMOVED SHEAR TIE, REPLACED WITH SERVICEABLE SHEAR TIE, PN 368-53-16 -94465-209 IAW SRM 51-40-2. CORRODED LEVEL 2, PN 368-53-16-94465-209, PART NAME CLIP, CARGO HEADING, EXACT FS & BS LOCATION ON ACFT, FROM STATIOJan 19, 2016 · N797AX · Boeing 767200 · Fuselage Internal Mounting StructureSDR ABXA20160114010Doubler · corrodedFORWARD NLG BAY FWD BULKHEAD FOUND CORRODED DOUBLER. R & R DOUBLER IN NLG BAY IAW SRM 51-40-02. FABRICATED FROM SRM 53-10-14 FIGURE 1 DWG 141T290 METAL 2024-T3-090 PO 1473909. CORRODED LEVEL 2, PN 141T2912-2, SN NSN, PART NAME STRAP, EXACT FS BS LOCATION ONJan 14, 2016 · N798AX · Boeing 767200 · Fuselage Main, BulkheadSDR ABXA20160111007Web · corrodedLEFT WING LE SHIM, CORRODED AT LES 582, FRONT INBD CORNER OF BAY. FOUND CORROSION TO BE ON NOSE BEAM, FOUND CORROSION TO BE OUT OF LIMITS. REMOVED NOSE BEAM & FABRICATED NEW NOSE BEAM FROM 7075-T6 050 IAW DWG 114T2300 & SAMPLE PO 0069430. INSTALLED NEW NOSEJan 11, 2016 · N798AX · Boeing 767200 · Wing Miscellaneous StructureSDR 2DYA20151210022Computer · failedDURING CLIMB OUT, CREW REPORTED INITIALLY, LOSS OF BOTH EPR INDICATIONS & NO SPEED INDICATION, DECIDED TO RETURN. DID NOT DECLARE AN EMER & RETURNED, LANDED WITHOUT FURTHER INCIDENT. UPON ARRIVAL, THE LOGBOOK DISCREPANCY WAS SPD INDICATION ON THE ADI & LOSS Dec 10, 2015 · N767DA · Boeing 767200 · Engine Pressure Ratio (EPR)SDR ABXA20150203010Skin · corrodedLEFT OTBD FLAP UPPER SURFACE AT APPROXIMATELY STATION 367 - 377, HAS CORROSION, BULGING SKIN & ALSO HAS CORRODED SHIMS AT ACCESS 566MT OPENING EDGE. FLAP REPLACED ON NON-ROUTINE 0037. SDR INFO, CORRODED, PN 113T3100-63, PART NAME LT OTBD FLAP, SN 000355, FS Feb 3, 2015 · N752AX · Boeing 767200 · Trailing Edge FlapsSDR ABXA20150203009Support · corrodedLEFT WING UPPER TE EDGE PANEL SUPPORT TEE CORRODED ALONG ENTIRE LENGTH. VIEWED THROUGH PANELS 561AB & 552HB. REMOVED LT WING UPPER TE PANELS FWD INBD AILERON. REMOVED TE PANEL SUPPORT. REINSTALLED SERVICEABLE SUPPORT TE PN 113T1510-33 & TE PANELS IAW SRM CH Feb 3, 2015 · N752AX · Boeing 767200 · Wing Miscellaneous StructureSDR ABXA20150130012Skin · crackedSKIN UNDER THE FWD ADF ANTENNA HAS A 0.50 IN CRACK AT FS 1125, STRINGER 1L. FABRICATED & INSTALLED REPAIR TRIPLER & DOUBLER FOR SKIN UNDER FWD ADF ANTENNA AT FS 1125, STRINGER IL IAW DWG 146T3110 & SRM 53-00-01. SDR INFO, CRACKED 0.5 INCHES, PN 146T3110, SN Jan 30, 2015 · N752AX · Boeing 767200 · Fuselage Main, Plate/SkinSDR ABXA20150116007Beam · corrodedRIGHT WING LE OSS 1007.5 NOSE BEAM EXFOLIATED AT NUTPLATE AREA. R & R NOSE BEAM SECTION ON RT WING LE OSS 1007.5 IAW SRM 51-40-02. ACCOMPLISHED SB-60 351084. SDR INFO, CORRODED, PN 114T2330, PART NAME NOSE BEAM, SN NSN, STRINGER & WS LOCATION FROM OSS 1007.Jan 16, 2015 · N752AX · Boeing 767200 · Wing Miscellaneous StructureSDR ABXA20150115011Rib · crackedNUMBER 2 INBD CORE COWL NR 3 RIB FROM AFT CRACKED. REMOVED NR 3 RIB & LOWER DOUBLER. WELDED RIB IAW PSM 900-7-2-1 NR 1 REV 50. REINSTALLED IAW SRM 51-40-02. SDR INFO, CRACKED LENGTH 2.5 INCHES, PN 314T1210-17, SN NSN, PART NAME RIB. ACFT WAS GNDED.Jan 15, 2015 · N752AX · Boeing 767200 · Engine Cowling SystemSDR ABXA20150109008Beam · corrodedRIGHT WING LE OSS 695 NOSE BEAM EXFOLIATED AT LE PANEL ATTACH FLANGE. REPLACED RT WING LE 055 695 NOSE BEAM PART 114T2300-292 & NR 10 INBD SLAT CURTAIN. RE-FINISHED NOSE BEAM IAW SRM 51-40-02, SRM 51-20-01 & AMM 27-81-31. SDR INFO, CORRODED, PN 114T2300-292Jan 9, 2015 · N752AX · Boeing 767200 · Wing Miscellaneous StructureSDR ABXA20141201345Switch · failedINTERMITTENT BURNING RUBBER SMELL DURING FLIGHT. AFTER LANDING, THE RUNWAY TURNOFF LIGHT SWITCH WAS CYCLED & VISIBLE SMOKE & FIRE APPEARED AT OVERHEAD PANEL. RT RUNWAY TURNOFF LIGHT REMAINED ILLUMINATED WITH THE SWITCH IN THE OFF POSITION. PERFORMED VISUAL Dec 1, 2014 · N752AX · Boeing 767200 · Exterior LightingSDR ABXA20140721245Structure · corrodedPER CUSTOMER REQUEST CANN RT WING UPPER BEAM PN 113T1623-126 FOR USE ON ACFT. REMOVED RT WING UPPER BEAM PN 113T1623-126 IAW CUSTOMER REQUEST INSTALL T ANGLE IAW SRM 51-40-02. FABRICATED NEW SHIMS IAW DWG 113T1623, TREATED SHIMS IAW AMM 51-21-04. INSTALLED NJul 21, 2014 · N792AX · Boeing 767200 · Wing Miscellaneous StructureSDR ABXA20140718246Stiffener · corrodedDURING REPLACEMENT OF RT WING UPPER BEAM ON NR 0983 FOUND ANGLE STIFFENER CORRODED. FABRICATED PART IAW DWG 113T1623 & SAMPLE PO 0052750 PN BAC 1503-100442-7075-T6511 ANGLE BARE ALUM EXTRUDED. CORRODED, PN 113T1623-18, SN NA, PART NAME STIFFENER, STR & WS LOJul 18, 2014 · N792AX · Boeing 767200 · Wing Miscellaneous StructureSDR ABXA20140714250Skin · corrodedCORROSION FOUND RT WING LE SPAR AT STATION 247. CORROSION WAS REMOVED & AREA WAS REPAIRED ON REA B657-61093 MR. SEE PARTIAL WORK ACCOMPLISHED AND PWS 57 PG 1. CORRODED L2, PN 112T3101-6, SN NA, PART NAME WING SKIN, FS & BS WS 248, RT WING TE LOWER SURFACESJul 14, 2014 · N792AX · Boeing 767200 · Wing, Plate/SkinSDR ABXA20140714249Skin · corrodedCORROSION FOUND RT WING TE STATION 273. CORROSION WAS REMOVED & AREA WAS REPAIRED ON REA B657-61093MR STEPS 21 - 25. CORRODED L2, PN 112T3101-6, SN NA, PART NAME WING SKIN, FS & BS LOC ON ACFT WS 273, RT WING TE SKIN LOWER SURFACE. ACFT WAS GNDED.Jul 14, 2014 · N792AX · Boeing 767200 · Wing, Plate/SkinSDR ABXA20140714248Skin · corrodedCORROSION FOUND AT RT WING STATION 288 UNDER TE WING SUPPORT. CORROSION WAS REMOVED & AREA WAS REPAIRED AT RT WING STATION 288 UPPER SURFACE IAW REA B657-61093MR STEPS 26 - 31. CORRODED L2, PN 112T3101-6, SN N/A, PART NAME WING SKIN, FS & BS LOC ON ACFT WS 2Jul 14, 2014 · N792AX · Boeing 767200 · Wing, Plate/SkinSDR ABXA20140714247Skin · corrodedFOUND CORROSION ON RT WING TE SPAR WHILE WORKING NR 0983. CORROSION WAS REMOVED & AREAS WERE REPAIRED ON THE RT WING UPPER TE SURFACE AT WS 248 & 273 IAW REA B657-61093MR. M-287 WERE COMPLIED WITH ON NR 1074 & 1076. CORRODED L2, PN 112T3101-6, SN N/A, PART Jul 14, 2014 · N792AX · Boeing 767200 · Wing, Plate/SkinSDR ABXA20140630236Window · faultyRED GLOWING BURNING NOTED AT BOTTOM EDGE OF LT FWD WINDOW. STOPPED WHEN LT FWD WINDOW HEAT TURNED OFF. REPLACED L1 WINDOW ASSEMBLY. WINDOW ASSEMBLY EXCHANGED WITH NEW ASSEMBLY.Jun 30, 2014 · N773AX · Boeing 767200 · Windshield/Door Rain/Ice RemovalSDR ABXA20140624240Splice Plate · corrodedRIGHT WING LOWER LE FALSE SPAR CRACKED AT NR 9 SLAT AREA NEAR OTBD AUX TRACK. REMOVED DAMAGED SECTION OF RT WING LE LOWER SPLICE PLATE AT LES 612 - 708. FABRICATED NEW SECTION IAW REA B654-61068, INSTALLED NEW SECTION AT SPLICE PLATE IAW SRM 51-40-02 & REA BJun 24, 2014 · N792AX · Boeing 767200 · Wing SparSDR ABXA20140624239Strut · corrodedALL NUTPLATES RUSTED ON INBD AIR LOAD STRUT NR 10 SLAT INBD AUX TRACK AREA. R & R INBD AIR LOAD STRUT AT NR 10 SLAT INBD AUX TRACK IAW SRM 51-40-02. R & R NUTPLATES WITH RIB. CORRODED, PN 114T2215-16, SN NA, PART NAME STRUT, EXACT FS & BS LOCATION ON ACFT FJun 24, 2014 · N792AX · Boeing 767200 · Wing, Rib/Bulkhead
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