# Service difficulty reports: N714AX, cancelled Mar 12, 2025

A list on [N714AX, cancelled Mar 12, 2025](https://openairdocs.org/deregistered/N714AX-2025-03-12.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 · 61 reports

- [SDR IXXA20230313022](https://openairdocs.org/sdr/IXXA20230313022.md): Unknown · unknown · Mar 13, 2023 · N714AX · Boeing 767223 · Passenger/Crew Doors
  > PRE-FLIGHT CREW REPORTED L1 ENTRY DOOR CAME OFF TRACKS. ADJUSTED L1 ENTRY DOOR INTO CORRECT POSITION OF TRACK IAW B767 AMM 52-11-00.
- [SDR IXXA20230221017](https://openairdocs.org/sdr/IXXA20230221017.md): None · none · Feb 18, 2023 · N714AX · Boeing 767223 · Hydraulic System, Main
  > CENTER HYDRAULIC PRESSURE EICAS ON APPROACH. QUANTITY IN CENTER REACHED 0.08. ALTERNATE FLAP AND GEAR EXTENSION ENGAGED. HYDRAULIC QTY WAS FULL AT TOP OF DESCENT AND EMPTY WHEN FLAPS 5 SELECTED. DUE TO IRREGULAR OPERATIONS CREW ELECTED AN EMERGENCY DESCENT. L
- [SDR IXXA20230211016](https://openairdocs.org/sdr/IXXA20230211016.md): Flashlight · inoperative · Feb 11, 2023 · N714AX · Boeing 767223 · Emergency Equipment
  > FOUND COCKPIT EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW B767 AMM 25-05-03. OPERATIONAL CHECK GOOD.
- [SDR IXXA20221101143](https://openairdocs.org/sdr/IXXA20221101143.md): Pump · damaged · Oct 28, 2022 · N714AX · Boeing 767223 · Turbine Engine Oil System
  > DESCENT THRU FL190, OIL PSI RT ENGINE DECREASING. ENG NEAR IDLE & SHUTDOWN BEFORE OIL WENT TO 0. SINGLE ENG APPR & LDG PROCEDURES COMPLIED WITH. DECLARED EMERGENCY. OIL PSI AT 6 PSI AT SHUTDOWN & #2 ENG WINDMILLED APROX 7 MIN. LANDING UNEVENTFUL. ACFT RF
- [SDR IXXA2022050501](https://openairdocs.org/sdr/IXXA2022050501.md): Vent · cracked · May 5, 2022 · N714AX · Boeing 767223 · Nacelle/Pylon Structure
  > CORE COWL VENT CRACKED
- [SDR IXXA2022050408](https://openairdocs.org/sdr/IXXA2022050408.md): Thrust Reverser · chafed · May 4, 2022 · N714AX · Boeing 767200 · Engine Thrust Reverser
  > #2 ENGINE OUTBD THRUST REVERSER HAS A GOUGE AT THE 12 O'CLOCK POSITION
- [SDR IXXA202205040008](https://openairdocs.org/sdr/IXXA202205040008.md): Support Angle · cracked · May 4, 2022 · N714AX · Boeing 767200 · Leading Edge Devices
  > #6 SLAT LOWER EDGE HAS A CRACKED SUPPORT ANGLE. LOCATED BETWEEN THE CENTER AND THE OUTBD AUX TRACK
- [SDR IXXA2022050407](https://openairdocs.org/sdr/IXXA2022050407.md): Thrust Reverser · gouged · May 4, 2022 · N714AX · Boeing 767223 · Engine Thrust Reverser
  > THRUST REVERSER HAS GOUGE ON INTERNAL FAIRING
- [SDR IXXA2022050406](https://openairdocs.org/sdr/IXXA2022050406.md): Cowl Latch · worn · May 4, 2022 · N714AX · Boeing 767223 · Nacelle/Pylon Structure
  > CORE COWL AFT LATCH HAS WEAR
- [SDR IXXA2022050405](https://openairdocs.org/sdr/IXXA2022050405.md): Thrust Reverser · bent · May 4, 2022 · N714AX · Boeing 767200 · Engine Thrust Reverser
  > THRUST REVERSER TRAILING EDGE BENT
- [SDR IXXA2022050403](https://openairdocs.org/sdr/IXXA2022050403.md): Bracket · cracked · May 4, 2022 · N714AX · Boeing 767200 · Nacelle/Pylon Structure
  > BRACKET CRACKED ON SKIRT FAIRING
- [SDR IXXA2022050402](https://openairdocs.org/sdr/IXXA2022050402.md): Thrust Reverser · cracked · May 4, 2022 · N714AX · Boeing 767223 · Engine Thrust Reverser
  > THRUST REVERSER TRAILING EDGE CRACKED
- [SDR IXXA2022050304](https://openairdocs.org/sdr/IXXA2022050304.md): Sleeve · deteriorated · May 3, 2022 · N714AX · Boeing 767 · Powerplant System
  > #1 ENGINE EXHAUST SLEEVE LEADING EDGE WEAR COATING CHIPPED AND DETERIORATED.
- [SDR IXXA2022050303](https://openairdocs.org/sdr/IXXA2022050303.md): Sleeve · worn · May 3, 2022 · N714AX · Boeing 767200 · Powerplant System
  > #1 ENGINE EXHAUST SLEEVE HAS A HOLE WORN ON THE LEADING EDGE AT 7 O'CLOCK POSITION
- [SDR IXXA2022050302](https://openairdocs.org/sdr/IXXA2022050302.md): Cowling · chafed · May 3, 2022 · N714AX · Boeing 767200 · Engine Cowling System
  > LOWER CLOSE OUT CHANNEL CHAFED IN MULTI AREAS WHERE STOP PADS MATE UP ON #1 ENGINE O/B CORE COWL LOWER END
- [SDR IXXA2022050301](https://openairdocs.org/sdr/IXXA2022050301.md): None · cracked · May 3, 2022 · N714AX · Boeing 767 · Engine Cowling System
  > #1 ENGINE I/B CORE COWL UPPER LOUVER EXHAUST ON AFT FLANGE CRACKED
- [SDR IXXA2022043001](https://openairdocs.org/sdr/IXXA2022043001.md): Torque Tube · corroded · Apr 30, 2022 · N714AX · Boeing 767200 · Wing Structure
  > RH FLAP IB TORQUE TUBE PITTED
- [SDR IXXA20220427002](https://openairdocs.org/sdr/IXXA20220427002.md): Panel · corroded · Apr 27, 2022 · N714AX · Boeing 767200 · Fuselage Miscellaneous Structure
  > ALC PANEL SUPPORT ON BILGE PANEL RBL16 AT STATION 1281 CORRODED
- [SDR IXXA2022042201](https://openairdocs.org/sdr/IXXA2022042201.md): Floor Panel · cracked · Apr 22, 2022 · N714AX · Boeing 767200 · Fuselage Structure (General)
  > FLOOR PANEL 122C CRACKED
- [SDR IXXA2022041502](https://openairdocs.org/sdr/IXXA2022041502.md): Seal Bracket · cracked · Apr 15, 2022 · N714AX · Boeing 767 · Engine (Turbine/Turboprop)
  > FAN COWL SEAL RETAINER BRACKET CRACKED
- [SDR IXXA202204290002](https://openairdocs.org/sdr/IXXA202204290002.md): Beam · corroded · Apr 14, 2022 · N714AX · Boeing 767223 · Trailing Edge Flaps
  > R/W TRAILING EDGE FLAP #8 SUPPORT 1-2-3 BEAM HAS TWO FASTENERS COMMON TO THE SIDE BRACE ATTACH FITTING WITH DEFECT INDICATION WITH HFEC HOLE SCAN
- [SDR IXXA2022050502](https://openairdocs.org/sdr/IXXA2022050502.md): Support Bracket · corroded · Apr 12, 2022 · N714AX · Boeing 767223 · Cargo Compartments
  > L/H BILGE PANEL SUPPORT BRACKET (L-2) AT STA 1270 CORRODED
- [SDR IXXA2022050305](https://openairdocs.org/sdr/IXXA2022050305.md): Torque Tube · worn · Apr 11, 2022 · N714AX · Boeing 767223 · Trailing Edge Flaps
  > L/H I/B FLAP #4 TORQUE TUBE FOUND PITTED AND WORN BEYOND LIMITS
- [SDR IXXA2022042801](https://openairdocs.org/sdr/IXXA2022042801.md): Torque Tube · worn · Apr 11, 2022 · N714AX · Boeing 767223 · Trailing Edge Flaps
  > RH I/B FLAP TORQUE TUBE REQUIRES REMOVAL FOR INSPECTION IAW J/C ATI-57-793-12-02 #5 TORQUE TUBE FOUND TO BE PITTED AND WORN
- [SDR IXXA2022050201](https://openairdocs.org/sdr/IXXA2022050201.md): Retainer Seal · cracked · Apr 8, 2022 · N714AX · Boeing 767223 · Trailing Edge Flap Control System
  > I/B FLAP FAIRING 671FB INSIDE O/B SEAL RETAINER CRACKED
- [SDR IXXA20210522038](https://openairdocs.org/sdr/IXXA20210522038.md): Battery Pack · inoperative · May 17, 2021 · N714AX · Boeing 767223 · Emergency Lighting
  > MULTIPLE EMERGANCY EXIT SIGN LIGHTS INOPERATIVE. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. REMOVED AND REPLACED BATTERY PACK IAW BOEING 767 AMM 33-51-07. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RELEASED TO SERVICE.
- [SDR IXXA20210405014](https://openairdocs.org/sdr/IXXA20210405014.md): Connector · damaged · Apr 2, 2021 · N714AX · Boeing 767223 · Light System Wiring
  > DURING SERVICE CHECK, FOUND LEFT ENTRY DOOR EXIT SIGN LIGHT NOT ON WITH FLIGHT DECK EMERGENCY LIGHT SWITCH IN THE ON POSITION. TROUBLESHOT IAW B767 IAI WDM 33-51-11 & 33-51-13, IDENTIFIED CRACKED PIN IN FEMALE END CONNECTOR D1084 PIN 2 CAUSING INTERMITTENT FUN
- [SDR IXXA20201202444](https://openairdocs.org/sdr/IXXA20201202444.md): Warning Message · illuminated · Nov 29, 2020 · N714AX · Boeing 767223 · Door Warning System
  > PRE-DEPARTURE: CREW REPORTS L1 DOOR INDICATION AFTER ENGINE START. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE, WORK IN PROGRESS.
- [SDR IXXA20200519010](https://openairdocs.org/sdr/IXXA20200519010.md): Mount Bracket · gouged · May 5, 2020 · N714AX · Boeing 767223 · Nacelle/Pylon Miscellaneous Structure
  > AIRCRAFT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-54-408-00-02 " GVI - EXTERNAL - NO. 2 NACELLE STRUT" LEFT AFT PRECOOLER MOUNT BRACKET CRACKED VIEWED BENEATH #2 LEFT CORE COWL. REMOVED AND REPLACED LEFT AFT PRECOOLER MOUNT BRACKET IAW B767 SRM
- [SDR ABXR2020050600026](https://openairdocs.org/sdr/ABXR2020050600026.md): Bracket · cracked · May 5, 2020 · N714AX · Boeing 767223 · Engine Cowling System
  > L/H AFT PRECOOLER MOUNT BRACKET CRACKED VIEWED BENEATH #2 L/H CORE COWL. REMOVED AND REPLACED L/H AFT PRECOOLER MOUNT BRACKET IAW B767 SRM 51-40-02 PARA 9 AND IAW 47404FAB04.
- [SDR ABXR2020050600027](https://openairdocs.org/sdr/ABXR2020050600027.md): Tee Fitting · corroded · Apr 27, 2020 · N714AX · Boeing 767223 · Cargo/Baggage Doors
  > CORROSION ON INTERIOR "T" SECTION OF ALC DOOR 10" FROM AFT EDGE, 24" FROM TOP EDGE.REMOVED AND REPLACED INTERIOR "T" SECTION OF ALC 3RD FROM TOP USING 140T2604-3 IAW BOEING DWG# 140T2604.
- [SDR IXXA20200519015](https://openairdocs.org/sdr/IXXA20200519015.md): Floor Support · corroded · Apr 24, 2020 · N714AX · Boeing 767223 · Fuselage Miscellaneous Structure
  > AIRCRAFT GROUNDED FOR CHECK-C24. IN COMPLIANCE OF TASK CARD ATI-53-572-00-01 "GVI - INTERNAL - BULK CARGO COMPARTMENT BULK FLOOR SUPPORT" F.S. 1417 HAS CORROSION ALONG LENGTH OF THE SUPPORT TOP SIDE. REMOVED AND INSTALLED "Z" BEAM IAW BOEING DWG 452T3260 REV E
- [SDR IXXA20200519012](https://openairdocs.org/sdr/IXXA20200519012.md): Skin · corroded · Apr 24, 2020 · N714AX · Boeing 767223 · Doors
  > AIRCRAFT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-20-073-00-01, ALC DOOR HAS LIGHT CORROSION AT INTERIOR PANEL MOUNTING SCREW LOCATIONS. REPLACED SKIN ON ALC DOOR IAW B767 51-40-02 PAR 4 BOEING DWG 140T2640 AND DOC 47404FAB02.
- [SDR ABXR2020050600028](https://openairdocs.org/sdr/ABXR2020050600028.md): Web · corroded · Apr 24, 2020 · N714AX · Boeing 767223 · Cargo/Baggage Doors
  > ALC DOOR HAS LIGHT CORROSION AT INTERIOR PANEL MOUNTING SCREW LOCATIONS.REPLACED SKIN ON ALC DOOR IAW B767 51-40-02 PAR 4 BOEING DWG 140T2640 AND DOC 47404FAB02
- [SDR IXXA20200519014](https://openairdocs.org/sdr/IXXA20200519014.md): Skin · cracked · Apr 22, 2020 · N714AX · Boeing 767223 · Fuselage Main, Plate/Skin
  > AIRCRAGT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-53-730-00-02 "GVI - EXTERNAL - EXTERIOR SECTION 48 - RIGHT SIDE", THE FOLLOWING FINDINGS WERE NOTED: AFT RIGHT EXTERIOR FUSELAGE SKIN IS CRACKED STA 1654.5 BETWEEN STRINGERS 4R-5R. REPAIRED EXTE
- [SDR IXXA20200519013](https://openairdocs.org/sdr/IXXA20200519013.md): Web · broken · Apr 22, 2020 · N714AX · Boeing 767223 · Nacelle/Pylon Miscellaneous Structure
  > AIRCRAFT GROUNDED FOR C-CHECK-24. IN COMPLIANCE OF TASK CARD ATI-20-105-00-01 "DET - FORWARD NACELLE STRUT FAIRING - NACELLE 2 (EZAP)" THE FOLLOWING FINDINGS WERE NOTED: NUMBER 2 PYLON - WEB AND BRACKET WHICH THE NOSE COWL ANTI-ICE DUCT ATTACHES TO AT FORWARD
- [SDR ABXR2020050600030](https://openairdocs.org/sdr/ABXR2020050600030.md): Stringer Splice · corroded · Apr 22, 2020 · N714AX · Boeing 767223 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE AT STA. 434 S31R CORRODED.REMOVED AND REPLACED CORRODED SPLICE AT STA 434 S31R IAW B767 SRM 51-40-02.
- [SDR ABXR2020050600029](https://openairdocs.org/sdr/ABXR2020050600029.md): Web · cracked · Apr 22, 2020 · N714AX · Boeing 767223 · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 2 PYLON - WEB AND BRACKET THAT NOSE COWL ANTI-ICE DUCT ATTACHES TO AT FORWARD END OF PYLON AT PASS THRU ARE WORN/BROKEN.REPLACE WORE BRACKET IAW B767 SRM 51-40-02, NEW WEB REPLACEMENT DONE ON AMES REA 47404FAB01 ON #2 PYLON FWD END.
- [SDR ABXR2020050600031](https://openairdocs.org/sdr/ABXR2020050600031.md): Skin · cracked · Apr 17, 2020 · N714AX · Boeing 767223 · Fuselage Main, Plate/Skin
  > AFT R/H EXTERIOR FUSELAGE SKIN IS CRACKED STA 1654.5 BETWEEN STRINGERS 4R-5R. (VERIFIED WITH HFEC SURFACE SCAN).REPAIRED EXTERIOR FUSELAGE SKIN STA 1654.5 S3R-S8R IAW B767 SRM 53-80-01 REPAIR 4.
- [SDR IXXA20200519017](https://openairdocs.org/sdr/IXXA20200519017.md): Stringer · corroded · Apr 15, 2020 · N714AX · Boeing 767223 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT GROUNDED FOR CHECK-C24. IN COMPLIANCE OF TASK CARD ATI-53-454-00-01, "GVI - INTERNAL - BULK CARGO COMPARTMENT" THE FOLLOWING FINDINGS WERE NOTED: FLC - CORROSION ON STRINGER 32R JUST FORWARD OF STA.434. REPAIRED STRINGER 32R STA. 412-434 IAW B767 SRM
- [SDR IXXA20200519016](https://openairdocs.org/sdr/IXXA20200519016.md): Stringer · corroded · Apr 15, 2020 · N714AX · Boeing 767223 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT GROUNDED FOR CHECK-C-24.IN COMPLIANCE OF TASK CARD ATI-53-454-00-01,"GVI - INTERNAL - BULK CARGO COMPARTMENT" FLC - CORROSION ON STRINGER 31R AT STA.412. REPAIRED STRINGER 31R STA 412-434 IAW B767 SRM 53-00-03 REPAIR 2.
- [SDR IXXA20200519009](https://openairdocs.org/sdr/IXXA20200519009.md): Slat · bulged · Apr 14, 2020 · N714AX · Boeing 767223 · Leading Edge Devices
  > AIRCRAFT GROUNDED FOR C-CHECK 24. IN COMPLIANCE OF TASK CARD ATI-57-806-00-02, "GVI - ZONAL - INBOARD SLAT NO. 7" THE FOLLOWING FINDINGS WERE NOTED: 7 SLAT - LOWER LEADING EDGE HAS BULGE 93 INCHES FROM OUTBOARD END AND 7 INCHES FROM TRAILING EDGE.
- [SDR ABXR2020050600025](https://openairdocs.org/sdr/ABXR2020050600025.md): Slat · corroded · Apr 14, 2020 · N714AX · Boeing 767223 · Leading Edge Devices
  > NUMBER 7 SLAT - LOWER LEADING EDGE HAS BULGE 93 INCHES FROM OUTBOARD END AND 7 INCHES FROM TRAILING EDGE.REPAIRED #7 SLAT LOWER LEADING EDGE IAW REA# 47404REA02
- [SDR IXXA20180515023](https://openairdocs.org/sdr/IXXA20180515023.md): Failsafe · cracked · Apr 11, 2018 · N714AX · Boeing 767223 · Fuselage Main, Structure
  > RIGHT WING FAILSAFE STRAP AT WS 955, REAMED HOLES IAW SRM 51-40-02. LOWER HOLE DAMAGE EXTENDED BEYOND ALLOWABLE LIMITS AND WAS REPAIRED IAW 47317REA01.
- [SDR IXXA20180515022](https://openairdocs.org/sdr/IXXA20180515022.md): Bulkhead · dented · Apr 6, 2018 · N714AX · Boeing 767223 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD WAS FOUND DENTED. REPAIRED THE BULKHEAD IAW REA 47317, REA 05, REV IR.
- [SDR IXXA20180515021](https://openairdocs.org/sdr/IXXA20180515021.md): Skin · bulged · Apr 6, 2018 · N714AX · Boeing 767223 · Fuselage Main, Plate/Skin
  > BULGING FUSELAGE SKIN BS 462, STRINGER 23R. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-01, REPAIR 1.
- [SDR IXXA20180515020](https://openairdocs.org/sdr/IXXA20180515020.md): Seat Track · cracked · Apr 2, 2018 · N714AX · Boeing 767223 · Fuselage, Seat/Cargo Attach Fittings
  > FIRST OFFICER'S RIGHT FORWARD SEAT TRACK WAS CRACKED. REMOVED AND REPLACED THE SEAT TRACK IAW IAW AMM 25-11-01-822-095-001
- [SDR IXXA20180515019](https://openairdocs.org/sdr/IXXA20180515019.md): Failsafe · cracked · Mar 30, 2018 · N714AX · Boeing 767223 · Fuselage Main, Structure
  > LT FAILSAFE STRAP LOWER HOLE COMMON TO THE TEE FITTING CRACKED. THE FAILSAFE WAS REPAIRED.
- [SDR IXXA20170726253](https://openairdocs.org/sdr/IXXA20170726253.md): Escape Reel · failed · Jul 13, 2017 · N714AX · Boeing 767223 · Emergency Equipment
  > EMERGENCY DESCENT DEVICE NUMBER 5 PARTIALLY EXTENDED. REMOVED AND REPLACED THE EMERGENCY DESCENT DEVICE IAW MMS 25-61-03. AIRCRAFT RELEASED TO SERVICE.
- [SDR IXXA20170726252](https://openairdocs.org/sdr/IXXA20170726252.md): Escape Reel · inoperative · Jul 13, 2017 · N714AX · Boeing 767223 · Emergency Equipment
  > EMERGENCY DESCENT DEVICE NUMBER 7 IN THE SUPERNUMERARY AREA WILL NOT EXTEND. REMOVED AND REPLACED THE EMERGENCY DESCENT DEVICE IAW 25-61-03. ACFT RELEASED TO SERVICE.

Next page: https://openairdocs.org/deregistered/N714AX-2025-03-12/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 = 'N714AX' AND deregistration_id = 'N714AX-2025-03-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N714AX-2025-03-12/reports

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