# Service difficulty reports: N752AX

A list on [N752AX](https://openairdocs.org/aircraft/N752AX.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR ABXA20221026297](https://openairdocs.org/sdr/ABXA20221026297.md): Engine · hung start · Sep 22, 2022 · N752AX · Boeing 767281 · Engine (Turbine/Turboprop)
  > HUNG START AFTER STARTER CUTOUT. EGT CONTINUED TO RISE TWD THE LIMIT. N2 AND N1 NORMAL WITH NO INCREASE IN SPEED WITH THE INCREASING EGT. FOLLOWED QRH PROCEDURE FOR THE ABORTED START AND ELECTED TO RETURN TO BLOCK. AIRCRAFT GROUNDED BY MAINTENANCE. MAINTENANCE
- [SDR ABXA2020090283168](https://openairdocs.org/sdr/ABXA2020090283168.md): Actuator · worn · Aug 30, 2020 · N752AX · Boeing 767281 · Aileron Control System
  > AFTER PUSHBACK AND ENGINES STARTED EICAS MESSAGE AILERON LOCKOUT DISPLAYED, AIRCRAFT RETURNED TO BLOCK. AIRCRAFT WAS GROUNDED. T/S IAW B767 FIM 27-11 FT 804 FAULT CONFIRMED BAD LT AILERON LOCKOUT ACTUATOR. REMOVED AND REPLACED LT AILERON LOCKOUT ACTUATOR, I
- [SDR ABXA20200813163](https://openairdocs.org/sdr/ABXA20200813163.md): Aileron Sys · lack of lube · Aug 12, 2020 · N752AX · Boeing 767281 · Aileron Control System
  > AILERON'S STIFF AND WILL NOT RETURN TO CENTER. AIRCRAFT WAS GROUNDED. CLEANED AND LUBE ROD BEARING. C/W INSPECTION FOR AILERON PULLEYS, ALL CHECKS NORMAL. LUBED AILERON PULLEYS AS PRECAUTIONARY. C/W OPS CHECK. AILERON ZERO OUT ON BOTH LH AND RH YOLK. REF AMM 2
- [SDR ABXA202006296098](https://openairdocs.org/sdr/ABXA202006296098.md): Warning Light · illuminated · Jun 26, 2020 · N752AX · Boeing 767281 · Rudder Control System
  > RUDDER RATIO LIGHT AND MESSAGE DISPLAYED ON PUSH BACK. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA20200720129](https://openairdocs.org/sdr/ABXA20200720129.md): Warning Message · illuminated · May 17, 2020 · N752AX · Boeing 767281 · Leading Edge Slat Control System
  > EICAS MESSAGE FOR THE LE SLAT ASSYM DURING APPROACH WHEN FLAPS 5 SELECTED. AIRCRAFT WAS GROUNDED.
- [SDR ABXA201808043085](https://openairdocs.org/sdr/ABXA201808043085.md): Bulkhead Web · canning · Aug 3, 2018 · N752AX · Boeing 767281 · APU Cowling/Containment
  > OIL CANNING ON APU BULKEAD WEB REPAIR AT BS 1832. THE WEB WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201808043084](https://openairdocs.org/sdr/ABXA201808043084.md): Spar · corroded · Aug 3, 2018 · N752AX · Boeing 767281 · Wing Spar
  > CORROSION ON THE LEFT WING LOWER FRONT SPAR WEB AT OUTBOARD FRONT SPAR STATION 865. THE SPAR WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201808043082](https://openairdocs.org/sdr/ABXA201808043082.md): Keelbeam · corroded · Aug 3, 2018 · N752AX · Boeing 767281 · Fuselage Main, Keel
  > CORROSION ON THE KEEL BEAM AT BS 964. THE KEEL BEAM WAS REPAIRED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201808043081](https://openairdocs.org/sdr/ABXA201808043081.md): Support · corroded · Aug 3, 2018 · N752AX · Boeing 767281 · Wing Miscellaneous Structure
  > CORROSION ON THE LEFT WING UPPER TRAILING EDGE PANEL SUPPORT AT WING STATION 318. THE PANEL SUPPORT RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201808043080](https://openairdocs.org/sdr/ABXA201808043080.md): Support · corroded · Aug 3, 2018 · N752AX · Boeing 767281 · Wing Miscellaneous Structure
  > CORROSION FOUND ON THE LEFT WING FALSE SPAR, UPPER TRAILING EDGE PANEL SUPPORT, WING STATION 360. THE SUPPORT RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA201808043079](https://openairdocs.org/sdr/ABXA201808043079.md): Intercostal · corroded · Aug 3, 2018 · N752AX · Boeing 767281 · Wing Miscellaneous Structure
  > CORROSION FOUND ON THE LEFT WING TRAILING EDGE INTERCOSTAL ABOVE THE LEFT MAIN LANDING GEAR AFT TRUNNION. THE INTERCOSTAL WAS REPLACED. THE AIRPLANE WAS GROUNDED.
- [SDR ABXA20150203010](https://openairdocs.org/sdr/ABXA20150203010.md): Skin · corroded · Feb 3, 2015 · N752AX · Boeing 767200 · Trailing Edge Flaps
  > LEFT 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
- [SDR ABXA20150203009](https://openairdocs.org/sdr/ABXA20150203009.md): Support · corroded · Feb 3, 2015 · N752AX · Boeing 767200 · Wing Miscellaneous Structure
  > LEFT 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
- [SDR ABXA20150130012](https://openairdocs.org/sdr/ABXA20150130012.md): Skin · cracked · Jan 30, 2015 · N752AX · Boeing 767200 · Fuselage Main, Plate/Skin
  > SKIN 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
- [SDR ABXA20150116007](https://openairdocs.org/sdr/ABXA20150116007.md): Beam · corroded · Jan 16, 2015 · N752AX · Boeing 767200 · Wing Miscellaneous Structure
  > RIGHT 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.
- [SDR ABXA20150115011](https://openairdocs.org/sdr/ABXA20150115011.md): Rib · cracked · Jan 15, 2015 · N752AX · Boeing 767200 · Engine Cowling System
  > NUMBER 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.
- [SDR ABXA20150109008](https://openairdocs.org/sdr/ABXA20150109008.md): Beam · corroded · Jan 9, 2015 · N752AX · Boeing 767200 · Wing Miscellaneous Structure
  > RIGHT 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 114T2300-292
- [SDR ABXA20141201345](https://openairdocs.org/sdr/ABXA20141201345.md): Switch · failed · Dec 1, 2014 · N752AX · Boeing 767200 · Exterior Lighting
  > INTERMITTENT 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
- [SDR ABXA20131008576](https://openairdocs.org/sdr/ABXA20131008576.md): Gpu · malfunctioned · Oct 8, 2013 · N752AX · Boeing 767281 · Fuel Controlling System
  > LEFT ENGINE VERY SLOW TO RESPOND WITH THROTTLE ADVANCEMENT. ON BLOCK IN, LT ENGINE ADVANCED UNCOMMANDED, THROTTLE IN IDLE POSITION, TO APPROXIMATELY 80 PERCENT, N2. PERFORMED ENGINE RUN IAW 74-00-00-2, NO DEFECTS NOTED. AS FAR AS ENGINE GOING TO FLIGHT IDLE
- [SDR ABXA20130423426](https://openairdocs.org/sdr/ABXA20130423426.md): Tee Fitting · corroded · Apr 23, 2013 · N752AX · Boeing 767281 · Wing Miscellaneous Structure
  > CORROSION ON UPPER RIGHT WING TRAILING EDGE PANEL ATTACH TEE-CAP FROM WING REAR SPAR TO TRAILING EDGE AT WING STA 434. INSTALLED NEW WING CHORD IAW B767 SRM 51-40-02 PARA 4, 7 AND 9. AIRCRAFT WAS GROUNDED.
- [SDR ABXA20121203309](https://openairdocs.org/sdr/ABXA20121203309.md): Battery · defective · Dec 3, 2012 · N752AX · Boeing 767281 · Emergency Lighting
  > EMERGENCY LIGHT SPARE BATTERY M736 WILL NOT HOLD A CHARGE. REPLACED EMERGENCY LIGHT SPARE BATTERY (M736) IAW B767 AMM 33-51-07-2, ACFT WAS GROUNDED.
- [SDR ABXA20121203308](https://openairdocs.org/sdr/ABXA20121203308.md): Battery · discharged · Dec 3, 2012 · N752AX · Boeing 767281 · Emergency Lighting
  > EMERGENCY LIGHT SPARE BATTERY M735 WILL NOT HOLD A CHARGE. REPLACED SPARE EMERGENCY LIGHT BATTERY. REPLACED EMERGENCY LIGHT SPARE BATTERY (M735) IAW B767 AMM 33-51-07-2, ACFT WAS GROUNDED.
- [SDR ABXA20111019129](https://openairdocs.org/sdr/ABXA20111019129.md): Bracket · cracked · Oct 19, 2011 · N752AX · Boeing 767281 · Wing Miscellaneous Structure
  > T-BRACKET CRACKED AT LOWER SUPPORT BRACE FWD OF RT INBD AILERON UNDERNEATH PANEL 661BB. REMOVED AND REPLACED T-BRACKET IN LWR SUPPORT BRACE BELOW PANEL 661BB IAW B767 DWG 113T1944, AWG.
- [SDR ABXA20111019128](https://openairdocs.org/sdr/ABXA20111019128.md): Plate · corroded · Oct 19, 2011 · N752AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > CORROSION ON BULK CARGO DOOR FLOOR PLATE BY AFT DOUBLER UNDER SCUFF PLATE. REMOVED & REPLACED CORRODED FLOOR PLATE IAW B767-200 SRM 51-40-02, AWG.
- [SDR ABXA20111019127](https://openairdocs.org/sdr/ABXA20111019127.md): Fitting · corroded · Oct 19, 2011 · N752AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > CORROSION ON FITTING AT FORWARD LOWER END OF CARGO DOOR CUTOUT BEHIND SEAL DEPRESSOR. REPAIRED IAW REA B653-595330-MR, AWG.
- [SDR ABXA2011031809](https://openairdocs.org/sdr/ABXA2011031809.md): Pbe · unserviceable · Mar 18, 2011 · N752AX · Boeing 767281 · Emergency Equipment
  > CREW REPORTED VACUUM SEAL ON PBE BROKEN. DEFERRED 68232 IAW B767 SERVICE CHECK AND GMM 07.04 FOR TRACKING MUST BE CLEARED BY 36 HOURS. PLACARD INSTALLED. CODE 15. AIRCRAFT WAS NOT GROUNDED.
- [SDR ABXA201011290166](https://openairdocs.org/sdr/ABXA201011290166.md): Warning System · false activation · Nov 26, 2010 · N752AX · Boeing 767281 · Leading Edge Slat Position Indicating System
  > EICAS MESSAGE "L/E SLAT ASYMMETRY" AND L/E DISCRETE LIGHT ILLUMINATED ON APPROACH TO LANDING. EMERGENCY DECLARED. PERFORMED FIM PROCEDURE IAW 27-81-00-1 FIG 107 SYSTEM CHECK'S OK.
- [SDR ABXA201003260020](https://openairdocs.org/sdr/ABXA201003260020.md): Skin · cracked · Dec 14, 2009 · N752AX · Boeing 767200 · Trailing Edge Flaps
  > LEFT OUTBOARD FLAP AFT SKIN IS CRACKED AT INBOARD END CAP. REPAIRED DAMAGED AREA IAW 767 SRM 51-70-03.
- [SDR ABXA201003260019](https://openairdocs.org/sdr/ABXA201003260019.md): Support Beam · cracked · Dec 9, 2009 · N752AX · Boeing 767200 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 ENGINE PYLON SUPPORT BEAM IS CRACKED AND HAS LOOSE / MISSING NUT PLATES CON TO PANEL 437ERX. REPAIRED SUPPORT BEAM IAW REA B654-58641-MR.
- [SDR ABXA200911170063](https://openairdocs.org/sdr/ABXA200911170063.md): Mec · malfunctioned · Nov 16, 2009 · N752AX · Boeing 767281 · Auto Throttle System
  > LEFT ENGINE FLAMED OUT AT APPROXIMATELY 1,000 AGL AFTER VNAV SELECTED. RE-LIGHT OF LEFT ENGINE SUCCESSFUL. (WHEN VNAV IS SELECTED THIS CHANGES THE THRUST PROFILE. FLAME OUT OCCURRED AS THROTTLES CAME BACK.) INSPECTED SUMPS AND FOUND NO WATER. FUEL FILTERS
- [SDR ABXA080131](https://openairdocs.org/sdr/ABXA080131.md): Strap · cracked · Mar 14, 2008 · N752AX · Boeing 767200 · Wing Spar
  > STRAP ON UPPER CAP OF FRONT SPAR WAS CRACKED LES 485. REMOVED AND REPLACED UPPER SPAR CAP STRAP SECTIONS IAW B767 SRM.
- [SDR ABXA080130](https://openairdocs.org/sdr/ABXA080130.md): Keelbeam · corroded · Mar 14, 2008 · N752AX · Boeing 767200 · Fuselage Main, Keel
  > LOWER RIGHT KEEL BEAM APPROXIMATELY STA 970 CORRODED. BLENDED CORROSION ON LOWER RIGHT KEEL BEAM STA 970 IAW B767 SRM.
- [SDR ABXA080129](https://openairdocs.org/sdr/ABXA080129.md): Keelbeam · corroded · Mar 14, 2008 · N752AX · Boeing 767200 · Fuselage Main, Keel
  > LOWER RIGHT KEEL BEAM CORD APPROXIMATELY STA 1030 - CORRODED. BLENDED CORROSION ON LOWER RIGHT KEEL BEAM STA 1030 IAW B767 SRM.
- [SDR ABXA080137](https://openairdocs.org/sdr/ABXA080137.md): Skin · cracked · Mar 13, 2008 · N752AX · Boeing 767200 · Fuselage Main, Plate/Skin
  > L1 DOOR CUTOUT LOWER AFT CORNER INTERIOR DOUBLER HAD 2 EACH.25 INCH CRACKS AT THE FASTENER HOLE AND THE EXTERIOR SKIN HAD A.125 INCH CRACK AT SAME HOLE. REPAIRED L1 DOOR CUTOUT LOWER AFT CORNER IAW REA B653-57165-MR.
- [SDR ABXA080128](https://openairdocs.org/sdr/ABXA080128.md): Skin · cracked · Mar 13, 2008 · N752AX · Boeing 767200 · Fuselage Main, Plate/Skin
  > CRACK IN SKIN APPROXIMATELY 1.375" LONG AT FASTENER FS 1654 AT STRINGER 6 LEFT. REPAIRED AREA IAW B767 SRM 53-80-01.
- [SDR ABXA080127](https://openairdocs.org/sdr/ABXA080127.md): Skin · cracked · Mar 13, 2008 · N752AX · Boeing 767200 · Fuselage Main, Plate/Skin
  > L1 DOOR CUTOUT LOWER AFT CORNER INTERIOR DOUBLER HAD 2 EACH.25 INCH CRACKS AT THE FASTENER HOLE AND THE EXTERIOR SKIN HAD A.125 INCH CRACK AT THE SAME HOLE. REPAIRED L1 DOOR CUTOUT LOWER AFT CORNER IAW REA B653-57165-MR.
- [SDR ABXA080126](https://openairdocs.org/sdr/ABXA080126.md): Door Frame · cracked · Mar 13, 2008 · N752AX · Boeing 767200 · Fuselage Main, Structure
  > R1 DOOR CUTOUT LOWER AFT CORNER INTERIOR DOUBLER HAD A.125 INCH CRACK AT THE FASTENER HOLE. REPLACED R1 DOOR CUTOUT LOWER AFT CORNER IAW REA 13653-57164-MA.
- [SDR ABXA070266](https://openairdocs.org/sdr/ABXA070266.md): Actuator · failed · Aug 11, 2007 · N752AX · Boeing 767200 · Stabilizer Actuator
  > DURING MAINTENANCE, REF JOB CARD 12-003-C1, STABILIZER TRIM BALL NUT UPPER SEAL APPEARED TO HAVE FAILED - STEP (23) (B) NOTE 2 (BEAVER UNIT). REMOVED AND REPLACED TRIM BALL SCREW ACTUATOR IAW B767 MM 27-41-10.
- [SDR ABXA070048](https://openairdocs.org/sdr/ABXA070048.md): Control Unit · malfunctioned · Feb 15, 2007 · N752AX · Boeing 767200 · Fuel Control/Turbine Engines
  > AS CREW WAS ON FINAL AT ILN, GOING THROUGH 27K, NR 2 ENGINE HAD AN UNCOMMANDED SHUTDOWN. CREW RESTARTED ENGINE WITHOUT ANY FURTHER ISSUES. NO EMERGENCY DECLARED. NO EN ROUTE DELAY. REMOVED AND REPLACED NR 2 ENGINE MAIN ENGINE CONTROL IAW B767 AMM 73-21-01-

## 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 = 'N752AX' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N752AX/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.