# Service difficulty reports: N745AX

A list on [N745AX](https://openairdocs.org/aircraft/N745AX.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 6 · 268 reports

- [SDR ABXA20260919414](https://openairdocs.org/sdr/ABXA20260919414.md): Door · no discrepancy · Sep 19, 2026 · N745AX · Boeing 767232 · Passenger/Crew Doors
  > RIGHT ENTRY DOOR EICAS ON TAXI. ACFT RETURNED TO THE GATE (BTB). MTC PERFORMED OPS CHECK RT ENTRY DOOR CLOSED & LOCKED OK IAW AMM 52-11-00. NO DISCREPANCIES NOTED, LIGHT OFF, DOOR VERIFIED CLOSED & LOCK. ACFT RETURNED TO SERVICE.
- [SDR ABXA20260917413](https://openairdocs.org/sdr/ABXA20260917413.md): Warning Message · activated · Sep 17, 2026 · N745AX · Boeing 767232 · Central Warning
  > ON TAKEOFF, THRUST LEVER ADVANCED THEN RED SPOILERS EICAS MESSAGE. COMPLETED QRH AND ABORTED TAKE OFF (ATO). CREW RETURNED TO THE GATE (BTB). MTC PERFORMED SPOILER CONTROL MODULE BITE PROCEDURE IAW FIM 27-09 FT 807. NO FAULTS ON ANY BOX. OPS CHECKED GOOD OF SP
- [SDR ABXA20260916410](https://openairdocs.org/sdr/ABXA20260916410.md): Engine · fluctuates · Sep 16, 2026 · N745AX · Boeing 767232 · Engine (Turbine/Turboprop)
  > DURING TAKEOFF FROM MIA, RT ENG STARTED TO ROLL BACK 2-3 PER N1. AFTER TAKEOFF FLUCUATED BETWEEN 2-3 TO 6-8%. BY 500FT IT WAS BOUNCING BETWEEN 95% & 68%. UPON THRUST REVERSER APPLICATION R ENGINE WAS 8% LOWER. CREW DECLARED EMERGENCY (EDC) AND PERFORMED AIR TU
- [SDR ABXA20260901378](https://openairdocs.org/sdr/ABXA20260901378.md): Module · leaking · Sep 1, 2026 · N745AX · Boeing 767232 · Hydraulic System, Main
  > ON DEPARTURE WHILE CLIMBING THROUGH 9000-10000 FEET THE CREW NOTICED A LOW HYDRAULIC FLUID MESSAGE. WHEN THEY CHECKED THE HYDRAULIC FLUID LEVEL THE CENTER SYSTEM WAS DROPPING RAPIDLY AND WITHIN ABOUT 5-10 SECONDS WAS AT ZERO. ATC DECLARED AN EMERGENCY ON THE C
- [SDR ABXA20260819369](https://openairdocs.org/sdr/ABXA20260819369.md): Wire · damaged · Aug 19, 2026 · N745AX · Boeing 767232 · Fire Protection System Wiring
  > FOUND WIRES W606-575R-20, W614-532R-20, W614-912R-20 & W614-020R-20 DAMAGED. REFERENCE WDM 26-16-31. REPAIRED WIRES PER BSWPM 20-10-13. SYSTEM CHECKS NORMAL PER AMM 26-16-00. ACFT RETURNED TO SERVICE.
- [SDR ABXA20260817366](https://openairdocs.org/sdr/ABXA20260817366.md): Circuit Card · faulted · Aug 17, 2026 · N745AX · Boeing 767232 · Fire Protection System Wiring
  > FWD CARGO DET 2 EICAS MSG. PERFORMED TROUBLESHOOTING IAW FIM 26-10-00-990-803 FAULT TREE 803. R & R FIRE DET. CARD, PROBLEM STILL EXISTED, REINSTALLED OLD CARD IAW AMM 26-10-1, R & R FWD NR 2 SMOKE DET. PROBLEM STILL EXISTED. TRANSFERRED TO NEW MEL 26-16-1-1-
- [SDR ABXA20260810354](https://openairdocs.org/sdr/ABXA20260810354.md): Circuit Board · defective · Aug 10, 2026 · N745AX · Boeing 767232 · Fire Protection System Wiring
  > ON ARRIVAL, AFT CARGO DETECTOR 1 & AFT CARGO DETECTOR 2 STATUS MSGS DISPLAYED. R & R M10427 CARD IAW AMM 26-10-01, OPS CHKD GOOD. ACFT RETURNED TO SERVICE.
- [SDR ABXA20260805349](https://openairdocs.org/sdr/ABXA20260805349.md): Control Panel · faulted · Aug 5, 2026 · N745AX · Boeing 767232 · Auto Throttle System
  > DURING TAXI, TMCP DOES NOT ALLOW FOR POWER SETTING. ALSO RCVD A/T AMBER MESSAGE. A/C RETURNED TO BLOCKS (BTB). MTC DEFERRED THRUST MANAGEMENT SYSTEM PER MEL 22-30-1. PLACARDS INSTALLED. A/C RELEASED CAT I OPERATIONAL. A/C RETURNED TO SERVICE.
- [SDR ABXA20260608250](https://openairdocs.org/sdr/ABXA20260608250.md): Module · defective · Jun 8, 2026 · N745AX · Boeing 767232 · Leading Edge Slat Control System
  > AFTER PUSHBACK, FLAP/SLAT ELEC STATUS MSG. REPLACED FLAP/SLAT SHUTOFF VALVE MODULE PER B767 AMM 27-51-48 LEAK & OPS CK GOOD AT THIS TIME A/C RELEASED CAT I PENDING 30/40 TEST PLACARD ROTATED. A/C RETURNED TO SERVICE.
- [SDR ABXA20260608249](https://openairdocs.org/sdr/ABXA20260608249.md): Shutoff Valve · faulted · Jun 8, 2026 · N745AX · Boeing 767232 · Trailing Flap Position Indicating System
  > ON LANDING, CREW RECEIVED FLAP/SLAT ELEC WARN STATUS MSG. PERFORMED FIM 27-51 FT 836. FOUND PREV FAULT # 27810047. CHECKED FLAP/SLAT SHUTOFF VALVE CONDITION IAW AMM 27-51-48. OPS CHECK GOOD. NO FAULTS NOTED. A/C RETURNED TO SERVICE.
- [SDR ABXA20260530235](https://openairdocs.org/sdr/ABXA20260530235.md): Battery · discharged · May 30, 2026 · N745AX · Boeing 767232 · Emergency Lighting
  > DURING SERVICE CHECK INSPECTION FOUND EMERGENCY LIGHT BY L1 DOOR INOP MTX REMOVED AND REPLACED EMERGENCY BATTERY M735 AND OPS CHECK GOOD IAW AMM 33-51-07. AND RETURNED A/C TO SERVICE
- [SDR ABXA20260528232](https://openairdocs.org/sdr/ABXA20260528232.md): Escape Reel · defective · May 28, 2026 · N745AX · Boeing 767232 · Emergency Equipment
  > DURING INSPECTION, FOUND NR 1 DESCENT DEVICE INOPERATIVE. REMOVED AND REPLACED NR 1 DESENT DEVICE IAW 25-61-03. ACFT RETURNED TO SERVICE.
- [SDR ABXA20260528231](https://openairdocs.org/sdr/ABXA20260528231.md): Antenna · defective · May 28, 2026 · N745AX · Boeing 767232 · Ground Proximity System
  > WHILE DESCENDING THRU FL 280 AND BELOW, GEAR NOT DOWN EICAS WARNING AND CONFIG LIGHT CAME ON WHEN THRUST LEVERS ARE AT IDLE. REMOVED AND REPLACED LH RA RCVR AND XMTR ANTENNAS IAW 767 AMM 34-33-02. OPS CHECK GOOD. A/C DOWNGRADED CAT I PENDING 30/40 TESTS REF LP
- [SDR ABXA20260425175](https://openairdocs.org/sdr/ABXA20260425175.md): Wire · broken · Apr 25, 2026 · N745AX · Boeing 767232 · Light System Wiring
  > DURING SERVICE CHECK FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP, MTX GROUNDED A/C AND ATTEMPTED TO REMOVE & REPLACE, FOUND BROKEN WIRE PUT BACK TO ORIGINAL IAW AMM 33-51-01 REPAIRED THE WIRE IAW SWPM 20-30-00 OPS CHECKED GOOD. RETURNED A/C TO SERVICE
- [SDR ABXA20260410156](https://openairdocs.org/sdr/ABXA20260410156.md): Warning Message · illuminated · Apr 10, 2026 · N745AX · Boeing 767232 · Fuel Boost Pump
  > DURING TAXI, CTR R FUEL PUMP EICAS MESSAGE ILLUMINATED AFTER PUSHBACK. T/S IAW FIM 28-22 FT 805. FOUND UFI INDICATION. RESET UFI IAW SUP AMM 28-23-00. OPS CHECK GOOD. ACFT REMAINS NO ETOPS. ACFT RETURNED TO SERVICE.
- [SDR ABXA20260217070](https://openairdocs.org/sdr/ABXA20260217070.md): Elec Connector · unsecure · Feb 17, 2026 · N745AX · Boeing 767232 · Fire Protection System Wiring
  > ON CREW PREFLIGHT, FOUND FIRE DET SYS INDICATION B# LINE WAS YELLOW (AMBER). MAINTENANCE RESECURED ELEC CONNECTOR ON CARGO FIRE PANEL IAW B767 AMM 26-11-00 AND PERFORMED AFOLTS TEST IAW B767 AMM 26-10-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA2026013029040](https://openairdocs.org/sdr/ABXA2026013029040.md): Valve · defective · Jan 29, 2026 · N745AX · Boeing 767232 · Air Distribution System
  > FWD EQUIP VALVE EICAS MESSAGE AFTER BLOCK OUT. NO OTHER LIGHTS OBSERVED. AIRCRAFT RETURNED TO BLOCKS (BTB). REPLACED MANIFOLD INTERCONNECT VALVE IAW AMM 21-58-01. LEAK CHECK GOOD. OPS CHECKED GOOD.
- [SDR ABXA20260128034](https://openairdocs.org/sdr/ABXA20260128034.md): Circuit Card · defective · Jan 28, 2026 · N745AX · Boeing 767232 · Air Conditioning System Wiring
  > DURING TAXI OUT, FWD EQUIP VALVE MSG ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). REMOVED & REPLACED EQUIP COOLING INDICATION CARD I.A.W AMM 21-58-24 OPS CHECK GOOD I.A.W AMM 21-58-00 MESSAGE CLEARED, A/C NO ETOPS. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA20260128032](https://openairdocs.org/sdr/ABXA20260128032.md): Warning Message · false activation · Jan 28, 2026 · N745AX · Boeing 767232 · Central Warning
  > ON TAXI OUT, FWD EQPT VALVE MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE PERFORMED FIM 21-58, TASK 805. MSG CLEARED, A/C OK FOR SERVICE.
- [SDR ABXA202601187017](https://openairdocs.org/sdr/ABXA202601187017.md): Pump · faulted · Jan 17, 2026 · N745AX · Boeing 767232 · Hydraulic Pump (Electric/Engine), Main
  > DURING TAXI OUT C HYD DEM PUMP PRESSURE WHEN FLAPS ARE IN TRANSITION, ACFT RETURNED TO GATE (BTB) AND MTX GROUNDED ACFT. DEFERRED ADP MTX TRANSFERRED TO DI# 69856 IAW MEL 29-11-3, MBCB 01/27/26, PULLED AND COLLARED C/B, MX PROCEDURES C/W, PLACARD INSTALLED
- [SDR ABXA20251015271](https://openairdocs.org/sdr/ABXA20251015271.md): Smoke Detector · no test · Oct 15, 2025 · N745AX · Boeing 767232 · Smoke Detection
  > DURING MAINTENANCE INSPECTION, A1 SMOKE DETECTOR FAILED INDICATION ON CARGO FIRE PANEL. REMOVED AND REPLACED A1 MCD SMOKE DETECTOR IAW IAI SUPP AMM 26-14-01. OPS CECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA20251014270](https://openairdocs.org/sdr/ABXA20251014270.md): Smoke Detector · failed · Oct 14, 2025 · N745AX · Boeing 767232 · Smoke Detection
  > DURING CREW PRE-FLIGHT, 1B MCD CARGO DECK SMOKE DETECTOR FAILED. MAINTENANCE DEFERRED DI# 67028 IAW MEL 26-16-2-2. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA20251009262](https://openairdocs.org/sdr/ABXA20251009262.md): Elec Connector · not seated · Oct 9, 2025 · N745AX · Boeing 767232 · Light System Wiring
  > DURING MAINTENANCE INSPECTION, EMERGENCY LIGHTS NOT ILLUMINATING. RE-SEATED CANNON PLUGS IAW FIM 33-51 FT 803. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA20250922235](https://openairdocs.org/sdr/ABXA20250922235.md): Elec Connector · defective · Sep 22, 2025 · N745AX · Boeing 767232 · Engine Indicating System Wiring
  > ON TAKE OFF, LT ENGINE EGT FLUCTUATED. AIRCRAFT ABORTED TAKE OFF AND RETURNED TO BLOCKS. (BTB). MAINTENANCE C/W HIGH ENERGY STOP INSPECTION IAW AMM 05-51-14. NO DISCREPANCIES NOTED AT THIS TIME. REMOVED AND REPLACED D4208P AND D4208J (PYLON CONNECTORS), D9
- [SDR ABXA20250917231](https://openairdocs.org/sdr/ABXA20250917231.md): Detection Sys · faulted · Sep 17, 2025 · N745AX · Boeing 767232 · Fire Detection
  > DURING THROUGH FLIGHT, MAIN CARGO FIRE DETECTION AMBER LIGHT IN SECTION 3B. MAINTENANCE DEFERRED IAW 26-16-2-1 MEL MAINTENANCE PROCEDURES C/W PLACARD INSTALLED MBCB 9/27/25 REPETITIVE INSPECTION REQUIRED BEFORE EACH DEPARTURE 26-16-2-1 IAW MEL 26-16-2-1. AI
- [SDR ABXA20250908217](https://openairdocs.org/sdr/ABXA20250908217.md): Elec Connector · detached · Sep 8, 2025 · N745AX · Boeing 767232 · Light System Wiring
  > DURING MAINTENANCE INSPECTION, FOUND FLIGHT DECK EMERGENCY EXIT SIGN LIGHT INOP. CLEANED AND REINSTALLED CONNECTOR FOR POWER SUPPLY. LIGHT OPS CHECKS GOOD IAW AMM 33-51-00. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA20250908216](https://openairdocs.org/sdr/ABXA20250908216.md): Elec Connector · detached · Sep 8, 2025 · N745AX · Boeing 767232 · Light System Wiring
  > DURING MAINTENANCE INSPECTION, FOUND L1 DOOR EMERGENCY EXIT SIGN LIGHT INOP. CLEANED AND REINSTALLED CONNECTOR FOR POWER SUPPLY. LIGHT OPS CHECKS GOOD IAW AMM 31-51-00. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA20250812182](https://openairdocs.org/sdr/ABXA20250812182.md): Battery · inoperative · Aug 12, 2025 · N745AX · Boeing 767232 · Emergency Lighting
  > DURING INSPECTION, EMERGENCY LIGHTS POWER SUPPLY BATTERY M737 INOP BATTERY M735 ALSO INOP. FOUND CONNECTORS D170 AND D1088 NOT SEATED CORRECTLY FER WDM 33-51-01 AND AMM 33-51-00 ALL LIGHTS OPERATE NORMALLY. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA20150826150](https://openairdocs.org/sdr/ABXA20150826150.md): Skin · corroded · Aug 26, 2015 · N745AX · Boeing 767232 · Fuselage Main, Plate/Skin
  > COMPLIED WITH DETAILED INSPECTION OF SURFACE OF SKIN AT STATION 955 FAIL-SAFE CUT OUT. FOUND CORROSION & MINOR TOOLING MARKS. REMOVED & SPOT FACED SKIN CORROSION IAW REA B653-61707-MR & 47008ORD10. SDR INFO CORRODED, PN 145T3420, SN NSN, PART NAME RT SKIN,
- [SDR ABXA20150825145](https://openairdocs.org/sdr/ABXA20150825145.md): Doubler · corroded · Aug 25, 2015 · N745AX · Boeing 767232 · Fuselage Main, Bulkhead
  > LEFT PRESS DECK FWD DOUBLER IS CORRODED BEYOND LIMITS. REFERENCE DWG 145T8752. NEW FWD LT PRESS DECK FWD DOUBLER, PN 145T8754-33 INSTALLED ON JC 53500013-003 & DOCUMENT 47008ORD03, TAG 1409197. SDR INFO CORRODED, PN 14578754-33, PART NAME DOUBLER, SN NSN, F
- [SDR ABXA20150821146](https://openairdocs.org/sdr/ABXA20150821146.md): Stringer · corroded · Aug 21, 2015 · N745AX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > LEFT FWD I BEAM STRINGER AT LBL 85.90 IS CORRODED BEYOND LIMITS. REFERENCE DWG 145T8752. FABRICATED NEW SECTION OF I BEAM FROM BAC 1518-751 2024-73511, PO 0037419 IAW REA B653-61698. SDR INFO CORRODED, PN 14578752-37, SN NSN, PART NAME STRINGER, FROM STATIO
- [SDR ABXA20150821144](https://openairdocs.org/sdr/ABXA20150821144.md): Pressure Deck · corroded · Aug 21, 2015 · N745AX · Boeing 767232 · Fuselage Main, Bulkhead
  > LEFT PRESS DECK WEB IS CORRODED BEYOND LIMITS IAW DWG 145T8752. FABRICATED NEW WEB FROM 2024-T3.125" PO 0057631. MACHINED EDGES ANODIZED, PRIMED & PAINTED IAW DWG 145T8752 & MIL-A-8625 TYPE I CLASS 1 & SRM 51-40-05. SDR INFO CORRODED L2, PN 14578752-235, P
- [SDR ABXA20150820124](https://openairdocs.org/sdr/ABXA20150820124.md): Angle · corroded · Aug 20, 2015 · N745AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > FOUND FWD LT BILGE PANEL, AFT MOUNT ANGLE CORRODED & NUTPLATES CORRODED. R & R UPPER CHORD ASSEMBLY AT STATION 544 IAW SRM 51-40-02 PAR 4B 1-5 & SRM 51-40-02 PARA 4 & PARA 7, SOPM 20-50-01, AMM 25-53-03 4, THROUGH COMP AMM 53-01-05 3C 3 TO 3C 4 & AMM 25-53-01
- [SDR ABXA20150817143](https://openairdocs.org/sdr/ABXA20150817143.md): Web · corroded · Aug 17, 2015 · N745AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > FLOOR WEBBING AT FS 550, RBL 36 HAS A HOLE CORRODED THROUGH WEB, WEB IS APPROX 5 FEET IN LENGTH. R & R FLOOR WEB AT FS 550, RBL 36 IN FLC IAW SRM 51-40-02. SDR INFO CORRODED LEVEL 2, PN 451T2504-17, NAME PANEL, FS & BS FS 522 - 642, EXACT STRINGER & WS RBL 3
- [SDR ABXA20150815148](https://openairdocs.org/sdr/ABXA20150815148.md): Strap · corroded · Aug 15, 2015 · N745AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > DURING DETAILED VISUAL INSPECTION OBSERVED CORROSION & CRACKS AROUND HOLES COMMON TO FAILSAFE STRAP & T FITTING. PREVIOUSLY MENTIONED ON NON-ROUTINE 1369. TRIMMED OUT CRACKED & CORRODED AREA OF FAILSAFE STRAP AS WRITTEN IAW EA 53500013-003 & DOCUMENT 47008OR
- [SDR ABXA20150815147](https://openairdocs.org/sdr/ABXA20150815147.md): Strap · cracked · Aug 15, 2015 · N745AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > DURING ROTARY HOLE SCAN, FOUND 2 CRACKS IN HOLES COMMON TO THE FAIL SAFE STRAP. ACCOMPLISHED TRIM OUT IAW EA5350013-003 & DOCUMENT 47008ORD03. CRACKED 1/4", PN 145T2524, PART NAME, LEFT FAIL SAFE STRAP, SN NSN, FS & BS LOCATION STATION 955. ACFT WAS GNDED.
- [SDR ABXA20150814149](https://openairdocs.org/sdr/ABXA20150814149.md): Strap · cracked · Aug 14, 2015 · N745AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > DURING HFEC SURFACE SCAN FOUND END OF CRACKS MENTIONED ON NON-ROUTINE 1369 & MARKED END OF CRACK LOCATIONS WITHIN TRIM OUT LIMITS. ACCOMPLISHED TRIM OUT OF FAIL-SAFE IAW EA 53500013-003 & DOCUMENT 47008ORD03. SDR INFO 1/4" CRACKED, PN 145T2524, PART NAME, LE
- [SDR ABXA20150803125](https://openairdocs.org/sdr/ABXA20150803125.md): Skin · damaged · Aug 3, 2015 · N745AX · Boeing 767232 · Fuselage Main, Plate/Skin
  > SKIN HAS A LARGE CREASE GOING THROUGH LAP SPLICE AT LT FS 1395, STRINGER 36L. REPAIRED LAP SPLICE CREASE IAW REA B653-61583-MR & SRM 53-00-21. SDR INFO, PN 146T3240 & 146T3230, SN N/A, PART NAME FUSELAGE SKINS, FS & BS LOCATION ON ACFT FS 1395 TO 1417, STRIN
- [SDR ABXA20150731131](https://openairdocs.org/sdr/ABXA20150731131.md): Skin · corroded · Jul 31, 2015 · N745AX · Boeing 767232 · Fuselage Main, Plate/Skin
  > DDR ITEM NR 21, REINFORCED REPAIR DOUBLER FOUND ON LT FUSELAGE, STATION 1654, STRINGER 33L - 34L. REPAIRED DAMAGED SKIN IAW SRM 53-00-01 REPAIR 29. SDR, CORRODED, PN 148T3211, PART NAME SKIN, SN NSN, FS & BS LOCATION 1651 TO 1661, STRINGER & WS LOCATION, STR
- [SDR ABXA20150731130](https://openairdocs.org/sdr/ABXA20150731130.md): Skin · corroded · Jul 31, 2015 · N745AX · Boeing 767232 · Fuselage Main, Plate/Skin
  > DDR ITEM NR 8, REINFORCED DOUBLER REPAIR FOUND ON LT FUSELAGE, STATION 441 - 451, STRINGER 32L. DDR NR 8 DOC REPAIR LT FUSELAGE HAS BEEN COMPLIED WITH IAW REA B653-61674-MR. CORRODED LEVEL 2, PN 143T3210-1, PART NAME SKIN, SN N/A, FS & BS FROM 442 TO 453, ST
- [SDR ABXA20150724142](https://openairdocs.org/sdr/ABXA20150724142.md): Angle · corroded · Jul 24, 2015 · N745AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > ANGLE FOUND CORRODED, AFT LOWER CARGO APPROX STATION 1263, RBL 42.0. R & R ANGLE IAW SRM 51-40-02 PARA 7D & E. CORRODED L2, PN 146T5050-84, PART NAME ANGLE, SN N/A, FS & BS FROM 1263 TO 1280, STRINGER & WS FROM STRINGER 33R, RBL 42. ACFT WAS GNDED.
- [SDR ABXA20150724141](https://openairdocs.org/sdr/ABXA20150724141.md): Support · corroded · Jul 24, 2015 · N745AX · Boeing 767232 · Wing Miscellaneous Structure
  > BEAM UNDER OTBD ROTARY ACTUATOR FOR INBD FLAP HAS AREA OF EXFOLIATION AT OTBD END OF BEAM. R & R RT WING CHORD PANEL SUPPORT T AT OTBD ROTARY ACTUATOR IAW SRM 51-40-2. SDR CORRODED L2, PN 113T1407-6, PART NAME CHORD, SN NSN, STRINGER & WS RT WING STATION 226
- [SDR ABXA20150723136](https://openairdocs.org/sdr/ABXA20150723136.md): Skin · corroded · Jul 23, 2015 · N745AX · Boeing 767232 · Fuselage Main, Plate/Skin
  > MULTIPLE SPOTS OF CORROSION ALONG THE STRINGER 37L LAP JOINT FROM LFS 412 - 434. COMPLIED WITH REA B653-61659-MR TO REPAIR FUSELAGE SKIN CORROSION. CORRODED L2, PN 141T3230, PART NAME SKIN, EXACT FS & BS LOCATION ON ACFT STATION 412 - 434, EXACT STRINGER & W
- [SDR ABXA20150720133](https://openairdocs.org/sdr/ABXA20150720133.md): Fireseal · cracked · Jul 20, 2015 · N745AX · Boeing 767232 · Nacelle/Pylon, Bulkhead/Firewall
  > AFT PYLON FIRE SEAL IS CRACKED AT MARKED LOCATION. REMOVED, FABRICATED, HEAT TREATED & INSTALLED AFT NR 1 PYLON FIRE SEAL IAW DWG 313T1380. SDR INFO, CRACKED LENGTH 1/4", PN 313T1380, PART NAME HEAT SHIELD, NAC LOCATION NR 1 NACELLE, STATION 308.5. ACFT WAS
- [SDR ABXA20150720127](https://openairdocs.org/sdr/ABXA20150720127.md): Support Beam · corroded · Jul 20, 2015 · N745AX · Boeing 767232 · Wing Miscellaneous Structure
  > LEFT WING INBD TE PANEL SUPPORT BEAM ON LWW CEILING, NEAR WS 249, IS CORRODED NEAR FWD END. R & R LT WING CEILING INBD TE PANEL SUPPORT BEAM WS 249 IAW SRM 51-40-2. FABRICATED PARA TO REA B757-61588. SDR INFO, CORRODED L2, PN 113T1622-110, PART NAME CHORD,
- [SDR ABXA20150716135](https://openairdocs.org/sdr/ABXA20150716135.md): Doubler · dented · Jul 16, 2015 · N745AX · Boeing 767232 · Fuselage Miscellaneous Structure
  > LARGE DENT ON DOUBLER AT LOWER FUSELAGE 390, STRINGER 20L. REPAIRED DENT IAW REA B653-61656-MR. SDR INFO PN 368-53-11-90699-287, SN NSN, PART NAME REINFORCING STRAP, FS & BS LOCATION ON ACFT 390L STRINGER & WS LOCATION ON ACFT STRINGER 20L. ACFT WAS GNDED.
- [SDR ABXA20150716123](https://openairdocs.org/sdr/ABXA20150716123.md): Angle · cracked · Jul 16, 2015 · N745AX · Boeing 767232 · Nacelle/Pylon Miscellaneous Structure
  > WHEN INSTALLING THE ARROWHEAD PANEL, FOUND STRUT DOOR LOWER SEAL RETAINER MOUNT, Z ANGLE, CRACKED ON AFT END. R & R Z ANGLE IAW SRM 51-40-02. SDR INFO, CRACKED 3", PN 313T1380-111, SN 1389552, PART NAME NR 2 PYLON, STATION 880 - 883. ACFT WAS GNDED.
- [SDR ABXA20150710138](https://openairdocs.org/sdr/ABXA20150710138.md): Support Beam · cracked · Jul 10, 2015 · N745AX · Boeing 767232 · Trailing Edge Flaps
  > NUMBER 1 FLAP SUPPORT 1 - 3, BEAM HAS 7 HOLES WITH DEFECT INDICATIONS WITH HFEC ROTARY SCAN. REPAIRED FLAP SUPPORT 1-3 BEAM IAW REA CO57-61601-MR. SDR INFO CRACK UNKNOWN, PN 113T1313-7, PART NAME 1 - 3 BEAM, SN ABXT883, LOCATION STRINGER & WS FROM LWS 798.2.
- [SDR ABXA20150710122](https://openairdocs.org/sdr/ABXA20150710122.md): Stringer Clip · corroded · Jul 10, 2015 · N745AX · Boeing 767232 · Fuselage Main, Attach Fittings
  > TWO STRINGER CLIPS & SHEAR TIE AT FS 1329, BETWEEN STRINGER 33L & 34L CORRODED. FABRICATED & INSTALLED 452T2706-4 ANGLES IAW DWG 452T27006. SDR INFO, CORRODED L2, PN 452T2706-4, SN NA, PART NAME ANGLE, FS & BS ON ACFT 1280L & 1324L, STRINGER LOCATION ON ACFT
- [SDR ABXA20150710121](https://openairdocs.org/sdr/ABXA20150710121.md): Longeron · cracked · Jul 10, 2015 · N745AX · Boeing 767232 · Nacelle/Pylon, Longeron/Stringer
  > NUMBER 2 ENG OTBD CORE COWL LOWER FRAME CRACKED BY NR 3 LATCH. REMOVED & REINSTALLED NR 3 LATCH & LOWER FRAME IAW SRM 51-40-02 D. WELD REPAIR LOWER FRAME IAW PROCESS STANDARDS MANUAL CH 900-7-2-1. PRIMED & PAINTED LOWER FRAME IAW AMM 51-21-02 & 51-21-10. C

Next page: https://openairdocs.org/aircraft/N745AX/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 = 'N745AX' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N745AX/reports

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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.