# Service difficulty reports: N342AX, cancelled Sep 29, 2026

A list on [N342AX, cancelled Sep 29, 2026](https://openairdocs.org/deregistered/N342AX-2026-09-29.md).

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

- [SDR CNMA2025020001](https://openairdocs.org/sdr/CNMA2025020001.md): Fuel Filter · faulted · Feb 11, 2025 · N342AX · Boeing 767328 · Fuel Controlling System
  > R ENG FUEL FILT EICAS MESSAGE ON MOMENTARILLY DURING CLIMB. STATUS MESSAGE R ENG FUEL FILT DISPLAYED.
- [SDR CNMA202501210002](https://openairdocs.org/sdr/CNMA202501210002.md): Pump · failed · Jan 18, 2025 · N342AX · Boeing 767328 · Fuel Boost Pump
  > PASSING THROUGH FL240 DURING CLIMB, LEFT CENTER FUEL PUMP FAILED.
- [SDR CNMA202501210001](https://openairdocs.org/sdr/CNMA202501210001.md): Pump · failed · Jan 17, 2025 · N342AX · Boeing 7673S2F · Hydraulic Pump (Electric/Engine), Main
  > DURING CLIMB, RIGHT HYDRAULIC DEMAND PUMP FAILED
- [SDR CNMA2024020001](https://openairdocs.org/sdr/CNMA2024020001.md): O-Ring · cut · Feb 19, 2024 · N342AX · Boeing 767328 · Engine Starter
  > RIGHT ENGINE OIL PRESSURE IN CAUTION RANGE AT TOP OF CLIMB. RIGHT ENGINE OIL QUANTITY ZERO. SHUT DOWN ENGINE AT OIL PRESSURE IN THE RED.
- [SDR CNMA2023FA0000380](https://openairdocs.org/sdr/CNMA2023FA0000380.md): Drive Unit · failed · Jul 23, 2023 · N342AX · Boeing 767300 · Weather Radar System
  > BOTH WX RADARS FAILED IN FLIGHT - REMOVED AND REPLACED WX RADAR ANTENNA AND R WX (?) IAW B763 AMM CHP 34-43 OPS CHECKS GOOD
- [SDR 2022FA0000182](https://openairdocs.org/sdr/2022FA0000182.md): Eec · failed · Mar 14, 2022 · N342AX · Boeing 767300 · Fuel Control/Turbine Engines
  > R ENG CONTROL STATUS MESSAGE. RIGHT ENGINE EEC PWR CH B CIRCUIT BREAKER POPPED. CORRECTIVE ACTION: R&R R ENGINE ECU IAW AMM 73-21-15 OPS CHECK GOOD
- [SDR CNMA201911070002](https://openairdocs.org/sdr/CNMA201911070002.md): Processor · intermittent · Oct 18, 2019 · N342AX · Boeing 767328 · Fuel Indicating System
  > STATUS MESSAGE FUEL QTY IND L MAIN INDICATOR BLANK, RETURNED AND WENT BLANK SEVERAL TIMES. CORRECTIVE ACTION: TROUBLSHOT PER FIM 28-41 FAULT TREE 851 RANG OUT HIZ WIRES TO FTYS, NO DEFECTS FOUND. INSPECTED WIRING BEHIND FUEL QTY PROCESSOR BULK HEAD RACK NO DEF
- [SDR CNMA201811210001](https://openairdocs.org/sdr/CNMA201811210001.md): Actuator · leaking · Nov 15, 2018 · N342AX · Boeing 767328 · Aileron Control System
  > CENTER HYDRAULIC QUANTITY EICAS IN FLIGHT DROPPED TO 0.33 WITH CENTER SYSTEM TURNED OFF. CORRECTIVE ACTION: FOUND RH INBOARD ELEVATOR PCA LEAKING. REMOVED AND REPLACED RH INBOARD ELEVATOR PCA IAW B767 AMM 27-31-05. OPS AND LEAK CHECK GOOD AT THIS TIME.
- [SDR CNMA2016010001](https://openairdocs.org/sdr/CNMA2016010001.md): Idg · disconnected · Jan 8, 2016 · N342AX · Boeing 767300 · AC Generator-Alternator
  > INFLIGHT THE RT IDG DRIVE LIGHT ILLUMINATED FOLLOWED BY RT GENERATOR CONTROL LIGHT EICAS MESSAGES RT GEN DRIVE & RT GEN OFF. DRIVE DISCONNECTED IAW CHECKLIST. C/W FIM 24-20, FT 801 AND 24-20, TASK 804 SYSTEM IS OK. SERVICED RT IDG IAW AMM 12-13 C/W FIM 2
- [SDR CNMA2014120001](https://openairdocs.org/sdr/CNMA2014120001.md): Oven · fire · Dec 16, 2014 · N342AX · Boeing 767328 · Buffet/Galleys
  > AFTER LEVEL OFF, F/A REPORTED FIRE IN AFT NR 3 GALLEY OVEN. PERFORMED INSPECTION OF AFT GALLEY OVEN. FOUND FOOD TRAYS AND FOOD BURNED. COMPLIED WITH OPS CHECKS OF OVEN NR 3 AND NR 1, 2, 4 AND NR 5 OVENS IAW CMM 25-36-22, NO FAULTS NOTED AT THIS TIME. OK F
- [SDR CNMA2014040001](https://openairdocs.org/sdr/CNMA2014040001.md): Lanyard · inoperative · Apr 14, 2014 · N342AX · Boeing 767328 · Escape Slide
  > DURING OPS CHECK OF ESCAPE SLIDE SYSTEM, ESCAPE SLIDE OPERATED AS REQUIRED, BUT THE SLIDE LIGHTS DID NOT ACTIVATE DURING REVIEW. IT WAS FOUND THAT THE ACTIVATION LANYARD APPEARED TO BE TOO LONG WHEN THE SLIDE WAS FULLY DEPLOYED TO ACTIVATE THE LIGHTS. REPLAC
- [SDR CNMA2013100001](https://openairdocs.org/sdr/CNMA2013100001.md): Control Panel · failed · Oct 8, 2013 · N342AX · Boeing 767328 · Landing and Taxi Aids
  > ILS TUNING KNOB NOT SECURE. SLIGHT BUMP WILL CHANGE COURSE BY 10 DEGREE. UNABLE TO PROCEED WITH ETOPS FLIGHT. R & R ILS CONTROL PANEL IAW MM 34-31. OPS CHECKS GOOD.
- [SDR CNMA2012080002](https://openairdocs.org/sdr/CNMA2012080002.md): Wire Harness · shorted · Aug 16, 2012 · N342AX · Boeing 767328 · Engine Indicating System Wiring
  > OIL TEMP INDICATING SYSTEM OIL TEMP LT ENGINE HIGH, OIL PRESSURE NORMAL. SHUTDOWN LT ENGINE IAW QRH. R & R NR1 ENGINE SEC IAW AMM 73-21 (GROUND TEST OF EEC CHECKED OK AT THIS TIME) R & R ECM CABLE W13 IAW GE ESM 72-00, R & R NR 1 ENG OIL TEMP SENSOR REF AMM
- [SDR CNMA2012080001](https://openairdocs.org/sdr/CNMA2012080001.md): Engine · overtemp · Aug 7, 2012 · N342AX · Boeing 767328 · Engine (Turbine/Turboprop)
  > TEMP LT ENGINE HIGH 179 ON BOTH LT AND RT EICAS COMPUTERS QRH FOLLOWED THRUST ON LT ENGINE REDUCED TO IDLE DUE TO OTHER INDICATIONS NORMAL ENGINE SHUTDOWN AND SECURE.
- [SDR CNMA20110028](https://openairdocs.org/sdr/CNMA20110028.md): Lamp · burned out · May 10, 2011 · N342AX · Boeing 767328 · Emergency Lighting
  > RIGHT 2ND FROM AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT ASSY, OPS CHECK NORMAL AT THIS TIME IAW AMM 33-51.
- [SDR CNMA20110027](https://openairdocs.org/sdr/CNMA20110027.md): Charger · defective · May 10, 2011 · N342AX · Boeing 767328 · Emergency Lighting
  > LEFT 3RD FROM AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R BATTERY CHARGER. OPS CHECK NORMAL AT THIS TIME IAW AMM 33-51.
- [SDR CNMA20110025](https://openairdocs.org/sdr/CNMA20110025.md): Floorbeam · corroded · Mar 26, 2011 · N342AX · Boeing 767328 · Fuselage Main, Floor Beam
  > FLOORBEAM UPPER FLANGE IS CORRODED ON UPPER SURFACE AT BS 287, APPROX BL 48. CUTOUT DAMAGED FLOORBEAM IAW SRM CH 53-00-51, FIG 201. EDDY CURRENT INSP. REQUIRED-EDDY CURRENT CUTOUT AREA IAW NDT MANUAL PART 6 51-00-19. NO DEFECTS NOTED. FLOORBEAMS REQUIRES REPA
- [SDR CNMA2011](https://openairdocs.org/sdr/CNMA2011.md): Floorbeam · corroded · Mar 26, 2011 · N342AX · Boeing 767328 · Fuselage Main, Floor Beam
  > FLOORBEAM AT STA 1480, RBL 48-57 IS CORRODED ON UPPER FLANGE. AREA UNDER F4 LAV. REPAIRED CORRODED FLOORBEAM IAW REA 46824, REA 01.
- [SDR CNMA20110021](https://openairdocs.org/sdr/CNMA20110021.md): Strap · corroded · Mar 26, 2011 · N342AX · Boeing 767328 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED JUST INBD OF R2 CUT OUT. REMOVED AND FABRICATED AND REPLACED FLOOR SUPPORT GUSSET STRAP IAW SRM 51-40-02 PARA 4 & 7.
- [SDR CNMA20110020](https://openairdocs.org/sdr/CNMA20110020.md): Attach Angle · corroded · Mar 26, 2011 · N342AX · Boeing 767328 · Fuselage Main, Attach Fittings
  > STA 742, UPPER ATTACH ANGLE FOR CURTAIN CORRODED AT CURTAIN ATTACH POINTS. REMOVED UPPER ATTACH ANGLE AT STA 742FLC IAW SRM 51-40-02-06-0, PARA 4, FABRICATED NEW UPPER ATTACH ANGLE IAW DWG NR453T1742 INSTALLED NEW ATTACH ANGLE IAW SRM 51-40-02-06-0, PARA 4.
- [SDR CNMA20110019](https://openairdocs.org/sdr/CNMA20110019.md): Floorbeam · corroded · Mar 26, 2011 · N342AX · Boeing 767328 · Fuselage Main, Floor Beam
  > FLOORBEAM AT FS 1518 AND BL -0- IS CORRODED AT LOWER END. REPAIRED LOWER FLANGE OF FLOORBEAM, PN 146T5143-1 IAW SRM 51-70-12, REF RFTS T-46825. REMOVED NUTPLATES ON FLOORBEAM AT STA 1518 AT LOCATION 12L AND 24L. REMOVED CORROSION. REMOVED CORROSION IAW SR
- [SDR CNMA20110018](https://openairdocs.org/sdr/CNMA20110018.md): Floor Panel · corroded · Mar 26, 2011 · N342AX · Boeing 767328 · Fuselage Floor Panel
  > F1 LAV FLOOR STRUCTURE CORRODED ON INBD SIDE. REPAIRED DAMAGED AREA IAW SRM 53-00-51, REPAIR 1.
- [SDR CNMA20110017](https://openairdocs.org/sdr/CNMA20110017.md): Bracket · corroded · Mar 26, 2011 · N342AX · Boeing 767328 · Fuselage Miscellaneous Structure
  > BRACKET CORRODED AT FS 1197, S 6 LT. R & R BRACKET AT FS 1197, STR 6L IAW SRM 51-40-02-0G-0 PARA 7.D.
- [SDR CNMA20110016](https://openairdocs.org/sdr/CNMA20110016.md): Stringer Clip · corroded · Mar 26, 2011 · N342AX · Boeing 767328 · Fuselage Main, Attach Fittings
  > ANGLE CORRODED AFT OF FRAME RT FS 1285 AT FLOOR LINE. REMOVED CORRODED ANGLE FOR REPLACEMENT-FABRICATED NEW STRINGER CLIP IAW DWG 146T1510. INSTALLED NEW STRINGER CLIP IAW SRM 51-40-02, PAR 7.
- [SDR CNMA20110015](https://openairdocs.org/sdr/CNMA20110015.md): Frame · corroded · Mar 26, 2011 · N342AX · Boeing 767328 · Fuselage Main, Frame
  > RIGHT FS 1270 FRAME CORRODED AT BASE. REMOVED CORROSION BLENDED AREA BEYOND LIMITS IAW SRM 53-00-15, FIG 101, PG 113, DETAIL XII. INSPECTED AREA IAW NDT PART 4 51-00-10, FOUND THICKNESS AROUND BLEND TO BE.175. REPAIRED AREA IAW EO B7653-04.
- [SDR CNMA20110014](https://openairdocs.org/sdr/CNMA20110014.md): Fitting · corroded · Mar 26, 2011 · N342AX · Boeing 767328 · Fuselage Miscellaneous Structure
  > LOWER PORTION OF LAV "E" IS CORRODED AROUND TIE DOWN AREAS (AFT SIDE). MFG END WALL FITTING IAW ESO 25-34. ALODINED FITTING IAW MM 51-21-04. PRIMED FITTING IAW MM 51-21-10. INSTALLED HELICOILS IAW SOPM 20-50-22 REV 5 INSTALLED END WALL FITTINGS IAW CMM 25
- [SDR CNMA20110013](https://openairdocs.org/sdr/CNMA20110013.md): Fitting · gouged · Mar 26, 2011 · N342AX · Boeing 767328 · Ailerons
  > INBD AILERON OTBD UPPER END HEAVILY GOUGED BY T/E SEAL. R & R FAIL-SAFE FITTING IAW SRM 51-40-02.
- [SDR CNMA20110012](https://openairdocs.org/sdr/CNMA20110012.md): Angle · corroded · Mar 26, 2011 · N342AX · Boeing 767328 · Fuselage Miscellaneous Structure
  > ANGLE CORRODED RT FS 1329 ON MOST OTBD WEB (M). BLENDED AREA OUT OF LIMITS IAW SRM 53-00-15, FIG 101, PG 113, DETAIL XII. REPAIRED AREA IAW SRM 51-70-11, FIG 1, PG 6 USING 7075-T6,.050.
- [SDR CNMA20100033](https://openairdocs.org/sdr/CNMA20100033.md): Skin · dented · Nov 27, 2010 · N342AX · Boeing 767328 · Trailing Edge Flaps
  > BIRD STRIKE ON RT WING OTBD FLAP LOWER SURFACE OTBD OF INBD FLAP VORTELON BY 42" AND 10" FROM T/E WITH SURFACE CRACK 9" PARALEL TO SEAM. DENT AREA 5" RND. R & R RT OTBD FLAP IAW MM 27-11 & SB 767-27A0155.
- [SDR CNMA20100029](https://openairdocs.org/sdr/CNMA20100029.md): Structure · damaged · Aug 29, 2010 · N342AX · Boeing 767328 · Landing Gear Doors
  > ON POST FLIGHT WALKAROUND INSP, FOUND RT STRUT GEAR DOOR DETATCHED FROM MOUNTS AND DAMAGED ALSO CAUSING DAMAGE TO TRUNNION DOOR. SHOCK STRUT DOOR & TRUNNION DOOR REPLACED REF SAL MX ORDER 152030292C4-0010 FOR WORK PERFORMED AND CERTIFICATION FOR RTS IAW LOG.
- [SDR CNMA20090154](https://openairdocs.org/sdr/CNMA20090154.md): Iru · inaccurate · Nov 21, 2009 · N342AX · Boeing 767328 · Inertial Guidance System
  > C IRS FAULT LIGHT ON LOCALIZER MAP WAS 7.5 MILES LT 34-21-1 SIT NR 3 NOTE( R IRS PREVIOUSLY DEFERRED). REPLACED CTR IRU IAW MM 34-21. OPS CHECK GOOD TEST NR 40, ALSO ACC.
- [SDR CNMA20090018](https://openairdocs.org/sdr/CNMA20090018.md): Slide · partial inflate · Aug 11, 2009 · N342AX · Boeing 767328 · Escape Slide
  > L-1 DOOR DID NOT OPEN FULLY DURING SLIDE DEPLOYMENT. OPS CKD L-1 DOOR DURING SLIDE DEPLOYMENT WITH FAA CKS GOOD.
- [SDR CNMA20090017](https://openairdocs.org/sdr/CNMA20090017.md): Light · burned out · Aug 11, 2009 · N342AX · Boeing 767328 · Escape Slide
  > R-2 SLIDE LIGHTS DID NOT OPERATE WHEN SLIDE WAS DEPLOYED. R-2 DOOR SLIDE REPLACED ON LOG PAGE 92473 ITEM 4 (REPLACED R-2 SLIDE IAW W/C 76SWF-002).
- [SDR CNMA20090016](https://openairdocs.org/sdr/CNMA20090016.md): Cover · missing · Aug 10, 2009 · N342AX · Boeing 767328 · Turbine Engine Oil System
  > OIL QTY AND PRESSURE LOSS ON RT ENG, NO TEMP OR ENG EXCEEDENCES, NO INFLIGHT SHUTDOWN. OIL PRESSURE DROPPED TO 10 PSI PRIOR TO RT ENG SHUTDOWN. FOUND CRANK PAD COVER NOT INSTALLED. INSTALLED CRANK PAD COVER IAW 72-00-00-982-007-H00. PERFORMED NO OIL PRESSU

## 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 = 'N342AX' AND deregistration_id = 'N342AX-2026-09-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N342AX-2026-09-29/reports

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