# Service difficulty reports: N792AX, cancelled Nov 9, 2023 A list on [N792AX, cancelled Nov 9, 2023](https://openairdocs.org/deregistered/N792AX-2023-11-09.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 88 reports - [SDR ABXA20151022162](https://openairdocs.org/sdr/ABXA20151022162.md): Control Unit · unserviceable · Oct 22, 2015 · N792AX · Boeing 767281 · Flight Management Computing Hardware System > DURING TAKEOFF, THE RT FLIGHT MANAGEMENT CONTROL & DISPLAY UNIT FLASHED VERTICAL BRIGHT & THEN FAILED, FOLLOWED BY A STRONG SMELL OF SMOKE. THE RT CONTROL & DISPLAY UNIT WAS REPLACED. THE CAUSE OF FAILURE IS CURRENTLY UNDER INVESTIGATION. - [SDR ABXA20150219015](https://openairdocs.org/sdr/ABXA20150219015.md): Warning Light · false activation · Feb 19, 2015 · N792AX · Boeing 767281 · Door Warning System > MAIN 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. - [SDR ABXA20140721245](https://openairdocs.org/sdr/ABXA20140721245.md): Structure · corroded · Jul 21, 2014 · N792AX · Boeing 767200 · Wing Miscellaneous Structure > PER 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 N - [SDR ABXA20140718246](https://openairdocs.org/sdr/ABXA20140718246.md): Stiffener · corroded · Jul 18, 2014 · N792AX · Boeing 767200 · Wing Miscellaneous Structure > DURING 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 LO - [SDR ABXA20140714250](https://openairdocs.org/sdr/ABXA20140714250.md): Skin · corroded · Jul 14, 2014 · N792AX · Boeing 767200 · Wing, Plate/Skin > CORROSION 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 SURFACES - [SDR ABXA20140714249](https://openairdocs.org/sdr/ABXA20140714249.md): Skin · corroded · Jul 14, 2014 · N792AX · Boeing 767200 · Wing, Plate/Skin > CORROSION 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. - [SDR ABXA20140714248](https://openairdocs.org/sdr/ABXA20140714248.md): Skin · corroded · Jul 14, 2014 · N792AX · Boeing 767200 · Wing, Plate/Skin > CORROSION 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 2 - [SDR ABXA20140714247](https://openairdocs.org/sdr/ABXA20140714247.md): Skin · corroded · Jul 14, 2014 · N792AX · Boeing 767200 · Wing, Plate/Skin > FOUND 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 - [SDR ABXA20140624240](https://openairdocs.org/sdr/ABXA20140624240.md): Splice Plate · corroded · Jun 24, 2014 · N792AX · Boeing 767200 · Wing Spar > RIGHT 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 B - [SDR ABXA20140624239](https://openairdocs.org/sdr/ABXA20140624239.md): Strut · corroded · Jun 24, 2014 · N792AX · Boeing 767200 · Wing, Rib/Bulkhead > ALL 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 F - [SDR ABXA20140618238](https://openairdocs.org/sdr/ABXA20140618238.md): Strut · corroded · Jun 24, 2014 · N792AX · Boeing 767200 · Wing, Rib/Bulkhead > OUTBOARD AIR LOAD STRUT CORRODED AT NR 10 SLAT INBD AUX TRACK. DRILLED, LOCATED, & INSTALLED NEW RIB SRM 51-40-05 & 51-40-02. CIC AREA IAW SOPM 20-41-05 NR 75 900444. CORRODED L2, PN 114T2216-16AX, SN NSN, PART NAME STRUT, FS & BS LOC ON ACFT OSS 732, RT LE - [SDR ABXA20140623242](https://openairdocs.org/sdr/ABXA20140623242.md): Strut · corroded · Jun 23, 2014 · N792AX · Boeing 767200 · Wing, Rib/Bulkhead > INBOARD AIR LOAD STRUT CORRODED AT NR 3 SLAT NEAR INBD AUX TRACK. INSTALLED LOWER STRUT PN 114T2215-15 IAW SRM 51-40-02, INSTALLED ADEL CLAMPS IAW SRM 51-40-02 PARA 9 B. CORRODED, PN 114T2215-15, PART NAME STRUT, SN NSN, FS & BS LOC OSS 732.840 TO LW, STR & - [SDR ABXA20140620241](https://openairdocs.org/sdr/ABXA20140620241.md): Web · corroded · Jun 20, 2014 · N792AX · Boeing 767200 · Wing Miscellaneous Structure > LEADING EDGE WEB CORRODED AT NUMBER 2 SLAT AREA NEAR OTBD AUX TRACK WS 897. FABRICATED NEW PART FROM 7075-T6-050 CLAD ALUMINUM IAW DWG 11452300, PO 0051890. INSTALLED & LOCATED NEW PART IAW SRM 51-40-05 & 51-40-02. CORRODED PN 114T2300-157, PART NAME WEB, S - [SDR ABXA20140619244](https://openairdocs.org/sdr/ABXA20140619244.md): Support · cracked · Jun 19, 2014 · N792AX · Boeing 767200 · Wing, Control Surface Attach Fittings > RIGHT WING OUTER HALF OF NR 8 FLAP SUPPORT HAS ONE FASTENER HOLE GIVING CRACK INDICATIONS. REAMED AFFECTED HOLE CLEAN & ROUND AT.658 IAW SRM 51-10-02, HFEC INSP COMPLETED IAW NDTM PART 6, 51-00-16. NO INDICATIONS AT THIS TIME. HOLE REPAIRED REA NR 657-6108 - [SDR ABXA20140619243](https://openairdocs.org/sdr/ABXA20140619243.md): Support · corroded · Jun 19, 2014 · N792AX · Boeing 767200 · Wing, Control Surface Attach Fittings > RIGHT WING INNER HALF OF NR 8 FLAP SUPPORT HAS ONE FASTENER HOLE GIVING CRACK INDICATIONS. REAMED AFFECTED HOLE TO.674 INCHES TRUE & ROUND IAW SRM 51-10-02. HFEC INSP IAW NDTM PART 6, 51-00-16. NO INDICATIONS NOTED THIS HOLE REPAIRED REA BI, B657-61081-MR. - [SDR ABXA20140619233](https://openairdocs.org/sdr/ABXA20140619233.md): Support · corroded · Jun 19, 2014 · N792AX · Boeing 767200 · Wing, Attach Fittings > RIGHT WING OUTER HALF OF NR 7 FLAP SUPPORT ALL SIX FASTENER HOLES GIVE CRACK INDICATIONS. REAMED AFFECTED HOLE TO 0673 CLEAN & ROUND IAW RAM 51-10-02 HFEC INSP COMPLETED IAW NDTM PART 6, 51-00-16. NO INDICATIONS AT THIS TIME. HOLE REPAIRED REA NR B657-61081 - [SDR ABXA20140618226](https://openairdocs.org/sdr/ABXA20140618226.md): Support Angle · corroded · Jun 18, 2014 · N792AX · Boeing 767200 · Wing Miscellaneous Structure > RIGHT WING LOWER TE PANEL 661CB HAS AFT Z ANGLE CORRODED, INBD AILERON AREA. R & R RT WING LOWER TE PANEL 661CB SUPPORT Z ANGLE IAW SRM 51-40-02. CORRODED L2, PN 113T1944-44, SN NA, PART NAME PANEL SUPPORT BEAM, STR & WS LOC ON ACFT 534.27 TO 545. ACFT WAS - [SDR ABXA20140618219](https://openairdocs.org/sdr/ABXA20140618219.md): Rib · corroded · Jun 18, 2014 · N792AX · Boeing 767200 · Wing, Rib/Bulkhead > OUTBOARD AIR LOAD STRUT CORRODED AT NR 1 SLAT INBD AUX TRACK. R & R AIR LOAD RIB AT NR 1 SLOT INBD AUX TRACK OTBD RIB IAW SRM 51-40-02. CORRODED L2, PN 114T2227-15, SN NSN, PART NAME STRUT, STR & WS LOC ON ACFT WS 1020 LT. ACFT WAS GNDED. - [SDR ABXA20140618217](https://openairdocs.org/sdr/ABXA20140618217.md): Rib · corroded · Jun 18, 2014 · N792AX · Boeing 767200 · Wing, Rib/Bulkhead > AIR LOAD STRUT CORRODED AT NR 8 SLAT AREA BY TELESCOPING DUCT. REMOVED CORRODED AIR LOAD RIB & INSTALLED NEW AIR LOAD RIB COMPLYING WITH REA NR B657-61059 IAW SRM 51-40-02 TAI DUCTING & COMPONENTS TO BE INSTALLED ON NR 0989. CORRODED L2 1 INCH PN 114T2202-8, - [SDR ABXA20140618216](https://openairdocs.org/sdr/ABXA20140618216.md): Rib · corroded · Jun 18, 2014 · N792AX · Boeing 767200 · Wing, Rib/Bulkhead > INBOARD AIR LOAD STRUT CORRODED AT NR 8 SLAT OTBD AUX TRACK AREA. REMOVED AIR LOAD RIB. FABRICATED NEW AIR LOAD RIB IAW REA 657-61051. INSTALLED NEW AIR LOAD RIB AT NR 8 SLAT OTBD AUX TRACK INBD SIDE IAW SRM 51-40-02 PARA 7 D. CORRODED L2, PN 114T2203-16, - [SDR ABXA20140618213](https://openairdocs.org/sdr/ABXA20140618213.md): Beam · corroded · Jun 18, 2014 · N792AX · Boeing 767200 · Wing Miscellaneous Structure > LEADING EDGE WEB CORRODED NR 10 SLAT AREA INBD OF MAIN TRACK. REMOVED DAMAGED SECTION OF NOSE BEAM & REPAIRED IAW SRM 51-70-11 FIG 1. CORRODED L2 1 INCH, PN 114T2300-190, SN NSN, STR & WS LOC ON ACFT OSS 759 RT WING. ACFT WAS GNDED. - [SDR ABXA20140618209](https://openairdocs.org/sdr/ABXA20140618209.md): Rib · corroded · Jun 18, 2014 · N792AX · Boeing 767200 · Wing, Rib/Bulkhead > INBOARD AIR LOAD STRUT CORRODED AT NR 10 SLAT OTBD AUX TRACK AREA. INSTALLED NEW RIB IAW SRM 51-40-05 & 51-40-02 CIC AREA JPER SOPM 20-41- 05. CORRODED L2, PN 114T2217-18, SN N/A, PART NAME AIR LOAD RIB STRUT, STR & WS LOC ON ACFT OSS 779 WING LE AT NR 10 SL - [SDR ABXA20140617225](https://openairdocs.org/sdr/ABXA20140617225.md): Support Angle · corroded · Jun 17, 2014 · N792AX · Boeing 767200 · Wing Miscellaneous Structure > RIGHT WING TRAILING PANEL 661PB HAS A CORRODED SUPPORT ANGLE, OTBD OF AUX TANK VENT. R & R RT WING TE LOWER CHORD AT WS 1068 IAW SRM 51-40-02. CORRODED, PN 113T1683-28, PART NAME CHORD LOWER, SN N/A, STR & WS LOC WS 1068 TO TE. ACFT WAS GNDED. - [SDR ABXA20140616220](https://openairdocs.org/sdr/ABXA20140616220.md): Spar · corroded · Jun 16, 2014 · N792AX · Boeing 767200 · Wing Spar > LOWER LE PANEL SPAR CRACKED & CORRODED AT NR 1 SLAT INBD AUX TRACK AREA. REMOVED DAMAGED & CORRODED SECTION OF LOWER LE SPLICE PLATE & INSTALLED NEW SECTION OF SPLICE PLATE IAW REA B657-61054. ACFT WAS GROUNDED. - [SDR ABXA20140616218](https://openairdocs.org/sdr/ABXA20140616218.md): Rib · corroded · Jun 16, 2014 · N792AX · Boeing 767200 · Wing, Rib/Bulkhead > OUTBOARD AIR LOAD STRUT CORRODED AT NR 8 SLAT INBD AUX TRACK AREA. CLEANED AREA IAW SRM 51-10-00. REMOVED.005 ORIGINAL MATERIAL, AREA IS WITHIN IMITS IAW SRM 57-41-09. TREATED & PRIMED AREA IAW SRM 51-20- 01. PAINTED AREA IAW AMM 51-21-10. CORRODED L2, PN - [SDR ABXA20140616215](https://openairdocs.org/sdr/ABXA20140616215.md): Beam · corroded · Jun 16, 2014 · N792AX · Boeing 767200 · Wing Miscellaneous Structure > LEADING EDGE WEB CORRODED AT NR 8 SLAT OTBD AUX TRACK AREA. REMOVED NOSE BEAM WEB & NOSE FORMER AT LES 489 - 481. FABRICATED NEW NOSE BEAM WEB. INSTALLED NEW NOSE WEB BEAM IAW SRM 51-40-02. REINSTALLED NOSE FORMER IAW SRM 51-40-02. TREATED, PRIMED & PANEL - [SDR ABXA20140616211](https://openairdocs.org/sdr/ABXA20140616211.md): Channel · corroded · Jun 16, 2014 · N792AX · Boeing 767200 · Wing, Attach Fittings > LOWER SPAR SMALL NUTPLATE CHANNEL CORRODED AT NR 10 SLAT INBD AUX TRACK. INSTALLED NEW CHANNEL BAC 1493-734-2024-T42, PO 0051497 IAW SRM 51- 40-02. PAINTED IAW MM 51-21-02, CIC IAW SOPM 20-41-05. CORRODED L2, PN 114T2400-152, PART NAME NUTPLATE CHANNEL, SN - [SDR ABXA20140616210](https://openairdocs.org/sdr/ABXA20140616210.md): Channel · corroded · Jun 16, 2014 · N792AX · Boeing 767200 · Wing, Attach Fittings > LARGE NUTPLATE CHANNEL CORRODED RT WING LE LOWER SPAR AT NR 10 SLAT NEAR OTBD AUX. INSTALLED NEW CHANNEL BAC1493-734-2024-T42, PO 0051497 IAW SRM 51-40- 02. PAINTED IAW MM 51-26-02 & CIC IAW SOPM 20-41-05. CORRODED L2, PN 114T2400-254 BAC 1493-734-2024-T42, - [SDR ABXA20140616208](https://openairdocs.org/sdr/ABXA20140616208.md): Channel · corroded · Jun 16, 2014 · N792AX · Boeing 767200 · Wing, Attach Fittings > SMALL NUTPLATE CHANNEL CORRODED AT NR 10 SLAT OTBD AUX TRACK, RT WING LOWER SPAR. INSTALLED NEW CHANNEL PAPER BAC1493-734-2024-T42. PO 0051497 IAW SRM 51-40-02, PAINTED IAW MM 51-21-02 & C I C IAW SOPM 20-41-05. CORRODED L2, PN 114T2400-254, SN N/A, PART NA - [SDR ABXA20140613221](https://openairdocs.org/sdr/ABXA20140613221.md): Web · corroded · Jun 13, 2014 · N792AX · Boeing 767200 · Wing Miscellaneous Structure > LEADING EDGE WEB CORRODED AT NR 3 SLAT AREA NEAR OTBD AUX TRACK. FABRICATED IAW DWG 114T2300 & SAMPLE. INSTALLED WEB IAW SRM 51-40-02. CORRODED L2, PN 114T2300-33 & -93, SN NA, PART NAME WEB, WS LOC ON ACFT OFS782, LT WING LE NR 3 SLAT. ACFT WAS GNDED. - [SDR ABXA20140613207](https://openairdocs.org/sdr/ABXA20140613207.md): Beam · corroded · Jun 13, 2014 · N792AX · Boeing 767200 · Wing Miscellaneous Structure > RIGHT WING LE FWD WEB CORRODED NR 11 SLAT AREA INBD WS 844. REMOVED DAMAGED NOSE BEAM WEB FABRICATED NEW & INSTALLED IAW DWG 114T2300 & SAMPLE SRM 51-40-02. 2 INCHES, CORRODED LEVEL 2, PN 114T2300, PART NAME NOSE BEAM, SN NSN, FS & BS LOC RT WING, STR & WS L - [SDR ABXA20140609212](https://openairdocs.org/sdr/ABXA20140609212.md): Beam · corroded · Jun 12, 2014 · N792AX · Boeing 767200 · Wing Miscellaneous Structure > LEADING EDGE WEB CORRODED AT WS 745 NR 10 SLAT INBD AUX TRACK AREA. REMOVED DAMAGED NOSE BEAM, FABRICATED NEW BEAM FROM 7075-T6.050 INCHES PO 0048004. INSTALLED NEW BEAM IAW DWG 114T2300-178 & SRM 51-40-02. APPLIED TOP COAT IAW AMM 51-21-02. CORRODED L2, - [SDR ABXA20140611234](https://openairdocs.org/sdr/ABXA20140611234.md): Skin · corroded · Jun 11, 2014 · N792AX · Boeing 767200 · Leading Edge Devices > NUMBER 10 SLAT LE SKIN IS BULGED AT THE OTBD END. FOUND BULGE IN LOWER LE SLAT SKIN DUE TO CORROSION, REPAIRED NR 10 SLAT IAW ABX B657-61062. CORRODED, PN 114T3160, PART NAME SLAT NOSE SKIN, EXACT FS & BS LOCATION ON ACFT FROM 825.2 TO 825.2. ACFT WAS GNDED - [SDR ABXA20140611227](https://openairdocs.org/sdr/ABXA20140611227.md): Beam · corroded · Jun 11, 2014 · N792AX · Boeing 767200 · Wing Miscellaneous Structure > CORROSION ON BEAM NEAR OTBD END OF MLG SUPPORT BEAM. REMOVED, FABRICATED BEAM IAW DWG 113T1634 & INSTALLED BEAM NEAR OTBD END OF MLG. CORRODED L2, PN 113T1634-16, SN NA, PART NAME SUPPORT RIB ASSEMBLY, STR & WS LOC ON ACFT WS 368.704. ACFT WAS GNDED. - [SDR ABXA20140611203](https://openairdocs.org/sdr/ABXA20140611203.md): Retainer · corroded · Jun 11, 2014 · N792AX · Boeing 767281 · Wing Miscellaneous Structure > UNDERNEATH INBD AILERON PCA ACCESS PANEL 661BB, FWD ATTACHMENT RAIL IS CORRODED BETWEEN PCA REACTION LINK ASSEMBLIES. R & R SEAL RETAINER IAW SRM 51-40-02. FABRICATED FROM 7075 T6 032 CLAD AFTER PO 0037486. CORRODED, EXACT FS & BS LOCATION ON ACFT FROM 484 - [SDR ABXA20140610230](https://openairdocs.org/sdr/ABXA20140610230.md): Skin · corroded · Jun 10, 2014 · N792AX · Boeing 767200 · Leading Edge Devices > NUMBER 8 SLAT LOWER LE SKIN IS BULGED AT APPROX OSS 467. FOUND BULGE IN SKIN CORRODED REPAIRED SKIN IAW REA B657-61064. CORRODED L2, PN 114T3160, PART NAME SLAT NOSE SKIN, STR & WS LOC ON ACFT RT WING OSS 460.2. ACFT WAS GNDED. - [SDR ABXA20140610229](https://openairdocs.org/sdr/ABXA20140610229.md): Skin · corroded · Jun 10, 2014 · N792AX · Boeing 767200 · Leading Edge Devices > NUMBER 2 SLAT LOWER OTBD SKIN CRACKED & BULGING. FOUND BULGE IN LOWER SLAP SKIN DUE TO CORROSION REPAIRED NR 2 SLAT IAW ABX B657-61063. CORRODED, PN 114T3160, PART NAME SLAT NOSE SKIN, EXACT FS & BS LOCATION ON ACFT FROM 975.0 TO 975.0. ACFT WAS GNDED. - [SDR ABXA20140610228](https://openairdocs.org/sdr/ABXA20140610228.md): Skin · corroded · Jun 10, 2014 · N792AX · Boeing 767200 · Leading Edge Devices > RIGHT TE NR 9 SLAT LOWER LE SKIN IS BULGED AT APPROX OSS 604. FOUND BULGE IN SKIN CORRODED REPAIRED SKIN IAW REA B657-61065. CORRODED L2, PN 114T3160, PART NAME SLAT NOSE SKIN, STR & WS LOC ON ACFT RT WING OSS 590.2. ACFT WAS GNDED. - [SDR ABXA20140610222](https://openairdocs.org/sdr/ABXA20140610222.md): Rib · corroded · Jun 10, 2014 · N792AX · Boeing 767200 · Wing, Rib/Bulkhead > INBOARD AIR LOAD STRUT CORRODED AT NR 4 SLAT NEAR OTBD AUX TRACK. INSTALLED & LOCATED NEW PART IAW SRM 51-40-5 & 51-40-2. CORRODED L2, PN 114T2210-19, SN NSN, PART NAME STRUT, STR & WS LOC ON ACFT OSS 628.845, LT WING. ACFT WAS GNDED. - [SDR ABXA20140609214](https://openairdocs.org/sdr/ABXA20140609214.md): Beam · corroded · Jun 9, 2014 · N792AX · Boeing 767281 · Wing Miscellaneous Structure > LEADING EDGE WEB CORRODED AT NR 9 SLAT INBD AUX TRACK AREA. REMOVED NOSE BEAM WEB, FABRICATED NEW WEB IAW DWG 114T2300 & SRM 57-41-13, INSTALLED NEW NOSE BEAM WEB IAW SRM 51-40-02. RESTORED TOPCOAT IN AREA IAW AMM 51-21-10. CORRODED L2, PN 114T2300-136, PAR - [SDR ABXA20140605206](https://openairdocs.org/sdr/ABXA20140605206.md): Support · corroded · Jun 5, 2014 · N792AX · Boeing 767200 · Wing, Attach Fittings > NUMBER 4 SLAT OTBD AUX TRACK, FWD SUPPORT, AT THE OTBD ATTACHMENT TO STRUCTURE SUPPORT IS CORRODED AT APPROX LT WING LE STATION 633. LOCATED & INSTALLED NEW STRUT RIB IAW SRM 51-40-5 & 51-40-2. CIE WILL BE ACCOMPLISHED ON PANEL REPORT NR 2, 75 900444. CORRO - [SDR ABXA20140603231](https://openairdocs.org/sdr/ABXA20140603231.md): Support · cracked · Jun 3, 2014 · N792AX · Boeing 767200 · Fuselage Miscellaneous Structure > CRACKED GUIDE SUPPORT AT FLOORBEAM UPPER CHORD RT SIDE INBD OF PDU STATION 1219. R & R GUIDE SUPPORT UPPER WEB AT FS 1219 IAW DWG 452T2051 & SRM 51-40-02. CRACKED.750 INCHES PN 452T2055-9, SN NSN, PART NAME WEB, EXACT FS BS LOCATION ON ACFT FROM 1219. ACFT - [SDR ABXA20140602205](https://openairdocs.org/sdr/ABXA20140602205.md): Rib · corroded · Jun 2, 2014 · N792AX · Boeing 767200 · Wing, Rib/Bulkhead > THE NR 5 OTBD AUX TRACK AREA, THE LOWER INBD RIB AT STATION 476 HAS AN AREA OF CORROSION. R & R AIR LOAD RIB AT NR 5 SLAT OTBD AUX TRACK INBD RIB IAW SRM 51-40-02. CORRODED L2, PN 114T2203-15, SN NSN, PART NAME STRUT, STR & WS LOC ON ACFT LT WING, WS 479.54. - [SDR ABXA20140602204](https://openairdocs.org/sdr/ABXA20140602204.md): Rib · corroded · Jun 2, 2014 · N792AX · Boeing 767200 · Wing, Rib/Bulkhead > NUMBER 5 SLAT INBD AUX TRACK LOWER RIB AT STATION 436 HAS AN AREA OF CORROSION. R & R AIR LOAD RIB AT NR 5 SLAT INBD AUX TRACK INBD RIB IAW SRM 51- 40-02. CORRODED L2, PN 114T2202-21, SN NSN, PART NAME STRUT, STR & WS LOC ON ACFT LT WING, WS 437.39. ACFT WA - [SDR ABXA20140530232](https://openairdocs.org/sdr/ABXA20140530232.md): Intercostal · corroded · May 30, 2014 · N792AX · Boeing 767200 · Fuselage Miscellaneous Structure > CORRODED INTERCOSTAL ON EITHER END BETWEEN FLOORBEAM UPPER CHORDS STATION 1329 & 1351 RT AFT BILGE AREA. R & R CORRODED INTERCOSTAL FS 1329 - 1351 AT RT AFT BILGE IAW SRM 51-40-02. CORRODED, PN 1146T5000-120, PART NAME SUPPORT FLOOR, SN NSN, FS & BS LOC 1329 - [SDR ABXA20140530223](https://openairdocs.org/sdr/ABXA20140530223.md): Stiffener · cracked · May 30, 2014 · N792AX · Boeing 767200 · Wing, Rib/Bulkhead > LEADING EDGE UPPER RIB STIFFENER CRACKED ON AFT END AT WS 550 NR 4 SLAT AREA, INBD. INSTALLED NEW STIFFENER PART 114T2207-5 IAW SRM 51-40-05, & 51-40-02. APPLIED CIC IAW SOPM 20-41-05 NR 75 900444. CRACKED.923, PN 114T2207-5, SN NSN, PART NAME STIFFENER, S - [SDR ABXA20140529224](https://openairdocs.org/sdr/ABXA20140529224.md): Stiffener · cracked · May 29, 2014 · N792AX · Boeing 767200 · Wing, Rib/Bulkhead > LEADING EDGE UPPER RIB LOWER STIFFENER IS CRACKED ON AFT END AT WS 520 NR 5 SLAT AREA OTBD. INSTALLED NEW CHORD IAW SRM 51-40-2 & 51-40-05. TREATED & PRIMED IAW SRM 51-21-02, DINETROLED IAW SOPM 51-21-02. CRACKED 1.35 INCHES, PN 114T2206-5, SN NA, PART NAME - [SDR ABXA2014032845](https://openairdocs.org/sdr/ABXA2014032845.md): Spring · dislodged · Mar 28, 2014 · N792AX · Boeing 767200 · Emergency Lighting > EMERGENCY LIGHT SWITCH GUARD WILL NOT LET THE SWITCH REMAIN IN THE ARMED POSITION. SWITCH GUARD WAS BUMPED OUT OF POSITION BY PERSONNEL ON THE FLIGHT DECK. RE POSITIONED THE LIGHT SWITCH GUARD SPRING SO THAT IT OPERATES NORMALLY. - [SDR ABXA20130621459](https://openairdocs.org/sdr/ABXA20130621459.md): Seal · broken · Jun 21, 2013 · N792AX · Boeing 767281 · Emergency Equipment > DURING SERVICE CHECK FOUND 2 EMERGENCY DESCENT DEVICE SEAL BROKEN AND ACTIVATED. R & R TWO EMERGENCY DEVICE IAW AMM 25-61-02-2, ACFT WAS GROUNDED. - [SDR ABXA20121004280](https://openairdocs.org/sdr/ABXA20121004280.md): Structure · damaged · Oct 3, 2012 · N792AX · Boeing 767281 · Fuselage Miscellaneous Structure > SCRIBE LINE FOUND AT STATION 363 STRINGER S 17L 2.5 INCHES MEASURED AT.0069 DEEP. FORWARD EDGE WAS.100 FROM LAP JOINT REPAIRED ON REA #B653-60351-MR. NO CRACKS WERE FOUND, FINAL REPAIR PER SRM 53-00-01 REPAIR 12, ACFT WAS GROUNDED. Next page: https://openairdocs.org/deregistered/N792AX-2023-11-09/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N792AX' AND deregistration_id = 'N792AX-2023-11-09' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N792AX-2023-11-09/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.