# Service difficulty reports: N763CX, cancelled Aug 5, 2024

A list on [N763CX, cancelled Aug 5, 2024](https://openairdocs.org/deregistered/N763CX-2024-08-05.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 3 · 131 reports

- [SDR IXXA20220922134](https://openairdocs.org/sdr/IXXA20220922134.md): Battery · inoperative · Sep 18, 2022 · N763CX · Boeing 767232 · Emergency Lighting
  > PRE-DEPARTURE, EMERGENCY FLASH LIGHT INOP. SYSTEM DEFERRED-34747 MEL CAT C. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-02. NO ADDITIONAL FAULTS NOTED
- [SDR IXXA20220615118](https://openairdocs.org/sdr/IXXA20220615118.md): Flashlight · inoperative · Jun 11, 2022 · N763CX · Boeing 767232 · Flight Compartment Lighting
  > DURING ROUTINE MAINTENANCE, EMERGENCY FLASHLIGHT OPERATIVE. REMOVED AND REPLACED EMERGENCY FLASHLIGHT ASSEMBLY IAW B767 AMM 26-64-02. OPERATIONAL CHECK GOOD.
- [SDR IXXA202204117107](https://openairdocs.org/sdr/IXXA202204117107.md): Controller · arced · Apr 7, 2022 · N763CX · Boeing 767232 · Windshield/Door Rain/Ice Removal
  > ENROUTE FROM KRIV TO KIAH, CREW REPORTED A STRONG ELECTRICAL ODOR EMITTING FROM THE LEFT NUMBER 1 WINDOW ASSEMBLY ELECTRICAL CONNECTION. AIRCRAFT DIVERTED TO KPHX. LANDING WAS UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. AIRCRAFT GROUNDED FOR UNSCHEDUL
- [SDR IXXA202202127009](https://openairdocs.org/sdr/IXXA202202127009.md): None · none · Feb 8, 2022 · N763CX · Boeing 767200 · Engine (Turbine/Turboprop)
  > ENROUTE FROM KRFD TO KCLT AND CLIMBING THROUGH 12,000 WITH AUTOPILOT AND AUTOTHROTTLES ENGAGED, LEFT ENGINE CONTINUOUSLY STEADY STATE SURGE STALLED. EGT MAX INDICATION OF 959C OBSERVED. CREW CONSULTED ATI QUICK REFERENCE HANDBOOK AND ADJUSTED LEFT ENGINE TO 70
- [SDR IXXA2022012605](https://openairdocs.org/sdr/IXXA2022012605.md): Skin Panel · corroded · Jan 26, 2022 · N763CX · Boeing 767232 · Fuselage Structure (General)
  > SKIN CORRODED BEYOND LIMITS
- [SDR IXXA2022012013](https://openairdocs.org/sdr/IXXA2022012013.md): Stringer · corroded · Jan 20, 2022 · N763CX · Boeing 767232 · Fuselage Structure (General)
  > STRINGER CORRODED BEYOND LIMITS.
- [SDR IXXA2022012012](https://openairdocs.org/sdr/IXXA2022012012.md): Shear Tie · corroded · Jan 20, 2022 · N763CX · Boeing 767232 · Fuselage Structure (General)
  > SHEAR TIE CORRODED BEYOND LIMITS
- [SDR IXXA2022012011](https://openairdocs.org/sdr/IXXA2022012011.md): Shear Tie · corroded · Jan 20, 2022 · N763CX · Boeing 767232 · Fuselage Structure (General)
  > SHEAR TIE CORRODED OUT OF LIMITS
- [SDR IXXA2022010703](https://openairdocs.org/sdr/IXXA2022010703.md): Shear Tie · corroded · Jan 7, 2022 · N763CX · Boeing 767232 · Fuselage Structure (General)
  > SHEAR TIE CORRODED BEYOND LIMITS
- [SDR IXXA2021122303](https://openairdocs.org/sdr/IXXA2021122303.md): Stringer · corroded · Dec 23, 2021 · N763CX · Boeing 767232 · Fuselage Structure (General)
  > CORRODED STRINGER 36L
- [SDR IXXA20211115070](https://openairdocs.org/sdr/IXXA20211115070.md): Pressure Switch · faulted · Nov 14, 2021 · N763CX · Boeing 767232 · Leading Edge Slat Control System
  > ON FINAL APPROACH LEADING EDGE SLAT DISAGREE EICAS MESSAGE ANNUNICATED, LANDING ABORTED. CREW PERFORMED GO AROUND AND LEADING EDGE SLAT DISAGREE MESSAGE NO LONGER ANNUNCIATED WHEN FLAPS RETRACTED TO 20. ON SECOND APPROACH, GEAR DISAGREE EICAS MESSAGE AND GEAR
- [SDR IXXA20210516036](https://openairdocs.org/sdr/IXXA20210516036.md): Skin · damaged · May 5, 2021 · N763CX · Boeing 767232 · Fuselage Main, Plate/Skin
  > AIRCRAFT GROUNDED FOR C-23 CHECK. DAMAGE TO FUSELAGE SKIN SECTION 43 BETWEEN STA 522 AND STA 566, BETWEEN STR 28R TO 34R. ACCOMPLISHED PERMANENT REPAIR AT FUSELAGE SECTION 43 BETWEEN STATION 522 TO STATION 566 BETWEEN STRINGERS 28R TO 34R IAW ENGINEERING ORD
- [SDR IXXA20210516034](https://openairdocs.org/sdr/IXXA20210516034.md): Stringer · corroded · May 5, 2021 · N763CX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT GROUNDED FOR C-23 CHECK. IN ACCOMPLISHMENT OF TASK CARD ATI-53-552-01-01 STRINGER REPAIR DISCOVERED ADDITIONAL CORROSION TO STRINGER 36L 1361 TO 1336. REPAIRED STRINGER 36L ON BS 1361-1336 IAW BOEING 767-200 STRUCTURES REPAIR MANUAL 53-00-03.
- [SDR IXXA20210516033](https://openairdocs.org/sdr/IXXA20210516033.md): Stringer · corroded · May 5, 2021 · N763CX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT GROUNDED FOR C-23 CHECK. IN ACCOMPLISHMENT OF TASK CARD ATI-53-552-01-01 DOT 14 DOT 045 UNDERNEATH WASTE TANK VAVLE AT FS 1540-1582 BETWEEN STRINGER 37L AND 37R CORROSION OUT OF LIMITS ON STRINGER 37R AT STATION 1540. REPAIRED STRINGER 37R ON BS 1540
- [SDR IXXA20210516032](https://openairdocs.org/sdr/IXXA20210516032.md): Skin · scratched · May 5, 2021 · N763CX · Boeing 767232 · Fuselage Main, Plate/Skin
  > AIRCRAFT GROUNDED FOR C-23 CHECK. IN ACCOMPLISHMENT OF TASK CARD ATI-53-552-01-01 MAINTENANCE IDENTIFIED D-15 DOT 163 AFT CARGO FUSELAGE SKIN SCRATCHED BETWEEN STATION 1356 AND 1363 AND STRINGERS 31L TO 33L. MATERIAL THICKNESS IAW B767-200 SRM 53-60-01 OUT OF
- [SDR IXXA20210516031](https://openairdocs.org/sdr/IXXA20210516031.md): Plenum · cracked · May 3, 2021 · N763CX · Boeing 767232 · APU Core Engine
  > AIRCRAFT GROUNDED FOR C-23 CHECK. IN ACCOMPLISHMENT OF TASK CARD ATI-24-031-01-01, MAINTENANCE IDENTIFIED SEVERAL CRACKS IN SUPPORT PLATFORM. REMOVED AND REPLACED APU PLENUM IAW BOEING 767-200 STRUCTURES REPAIR MANUAL 51-40-02. APU PLENUM REPAIRED IAW B767-200
- [SDR IXXA20210516030](https://openairdocs.org/sdr/IXXA20210516030.md): Stringer · cracked · May 3, 2021 · N763CX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT GROUNDED FOR C-23 CHECK. IN ACCOMPLISHMENT OF TASK CARD 53-552-0101, MAINTENANCE IDENTIFIED D-15 DOT 162 AFT CARGO HAS TWO STRINGERS WITH MARKS AT STATION 1359 STRINGER 31 L AND STATION 1361 STRINGER 33L. DAMAGE REMOVED.028. OUT OF LIMITS IAW B767 SR
- [SDR IXXA20190804013](https://openairdocs.org/sdr/IXXA20190804013.md): Structure · punctured · Jul 31, 2019 · N763CX · Boeing 767232 · Fuselage Miscellaneous Structure
  > PRE DEPARTURE-PUNCTURE AFT OF LOWER CARGO DOOR BETWEEN S28R-S29R. AOG. COMPLIED WITH CONDITIONAL INSPECTION IAW B767 AMM 05-51-59/ NO FURTHER DEFECTS NOTED. TEMP REPAIRS IAW ATI ENGINEERING ORDERS 53-767-6676 COMPLIED WITH. ACFT HAS BEEN AUTHORIZED A 1 TIME F
- [SDR IXXA20190529008](https://openairdocs.org/sdr/IXXA20190529008.md): Support · corroded · May 17, 2019 · N763CX · Boeing 767232 · Wing Miscellaneous Structure
  > AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE VISIT. THE FOLLOWING FINDING WAS NOTED FOR TASK CARD, 57-564-00-02- RIGHT WING TRAILING EDGE PANEL SUPPORT CORRODED AT STA 852. REMOVED AND REPLACED PANEL SUPPORT IAW ENGINERRING ORDER REA 47369FAB02 AND SRM 51-40-02 PAR
- [SDR IXXA20190529009](https://openairdocs.org/sdr/IXXA20190529009.md): Retainer · corroded · May 15, 2019 · N763CX · Boeing 767232 · Wing Miscellaneous Structure
  > AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE VISIT. THE FOLLOWING FINDING WAS NOTED FOR TASK CARD 57-572-00-01, LOWER WING TRAILING EDGE LOWER PANEL NEAR O/B FLAP O/B FAIRING HAS A CORRODED SEAL RETAINER. REPAIRED LOWER WING TRAILING EDGE LOWER PANEL SUPPORT BEAM I
- [SDR IXXA20190529011](https://openairdocs.org/sdr/IXXA20190529011.md): Skin · corroded · May 13, 2019 · N763CX · Boeing 767232 · Wing, Plate/Skin
  > AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE VISIT. THE FOLLOWING FINDING WAS NOTED FOR TASK CARD, 55-434-00-01. BLENDED CORROSION OUT OF LIMITS. NOMINAL T=.140" REMAINING T=.080" REPAIRED BLENDED AREA IAW ENGINEERING DOC 4736REA04 REV IR AND SRM 51-10-01/FIG 201
- [SDR IXXA20190529010](https://openairdocs.org/sdr/IXXA20190529010.md): Track · cracked · May 13, 2019 · N763CX · Boeing 767232 · Engine Thrust Reverser
  > AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE VISIT. THE FOLLOWING FINDING WAS NOTED FOR TASK CARD 71-828-00-01-O/B T/R UPPER SLIDE TRACK FAIRING IS BENT AND CHAFFED. REMOVED AND REPAIRED ON ENGINEERING ORDER 47369REA03.
- [SDR IXXA20190529007](https://openairdocs.org/sdr/IXXA20190529007.md): Skin · corroded · May 8, 2019 · N763CX · Boeing 767232 · Wing, Plate/Skin
  > AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE VIST. FINDING: TASK CARD 57-572-00-02-RIGHT WING TRAILING EDGE BONDED PANEL LEADING EDGE IS BULGING WS 1050. REMOVED UPPER RIGHT WING TRAILING EDGE PANEL FOR FURTHER INSPECTION, FOUND CORROSION ON UPPER WING SKIN. CLEANE
- [SDR IXXA20170513999](https://openairdocs.org/sdr/IXXA20170513999.md): Engine · making metal · May 9, 2017 · N763CX · Boeing 767232 · Engine (Turbine/Turboprop)
  > FLIGHT ATN3706 EN ROUTE FROM DEPARTURE STATION KABE TO DESTINATION STATION KONT EICAS MESSAGE DISPLAYED "R OIL FILTER". AS DIRECTED BY QRH, THE RIGHT ENGINE WAS SHUTDOWN. NOTIFIED ATC, DECLARED EMERGENCY. DIVERSION TO KILN. LANDED WITHOUT FURTHER INCIDENT. AIR
- [SDR IXXA20170414238](https://openairdocs.org/sdr/IXXA20170414238.md): Shear Tie · corroded · Mar 28, 2017 · N763CX · Boeing 767232 · Fuselage Internal Mounting Structure
  > AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT SIDE OF FRAME AT STATION 742 OUTBOARD STRINGER 39R IS CORRODED. REMOVED AND REPLACED SHEAR TIE AND CLIP FROM FORWARD LOWER CARGO STATION 742 STRINGER 39R WITH NEW PART IN ACCORDANCE WITH DRAWING 143T1214.
- [SDR IXXA20170414236](https://openairdocs.org/sdr/IXXA20170414236.md): Keelbeam · corroded · Mar 17, 2017 · N763CX · Boeing 767232 · Fuselage Main, Keel
  > AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. UPPER KEEL WEB IN THE RIGHT MAIN LANDING GEAR WHEEL WELL HAS AREAS OF CORROSION IN THE FORWARD PASS THROUGH LOCATION. BLENDED CORROSION ON RIGHT MAIN LANDING GEAR WHEEL WELL STATION 970 RIGHT BUTT LINE 5 FOUND TO BE OUT
- [SDR IXXA20170414237](https://openairdocs.org/sdr/IXXA20170414237.md): Frame · cracked · Mar 16, 2017 · N763CX · Boeing 767232 · Fuselage Main, Frame
  > AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. STATION 859.5 LEFT BUTT LINE 89 BELOW WATER LINE 200, FRAME INNER CHORD TRANSITION RADIUS CRACKED.25" APPROXIMATELY. REMOVED FASTENERS PER JOB CARD ENGINEERING ORDER 53-767-5352 FOR HIGH FREQUENCY EDDY CURRENT. COMPLIE
- [SDR IXXA20160429018](https://openairdocs.org/sdr/IXXA20160429018.md): Shear Tie · cracked · Apr 9, 2016 · N763CX · Boeing 767232 · Fuselage Internal Mounting Structure
  > DURING MX VISIT ACCOMPLISHED PERMANENT REPAIR FOR THE SHEAR TIE ATTACHED TO THE LT LONGERON LOCATED AT STATION 1746.25 & WL 258.44. WORK WAS ACCOMPLISHED IAW ENGINEERING DOCUMENT 53-767-5445 DATED 04 08 16 REV 3, NR0001, APPROVED REPAIR ON 8110-3.
- [SDR IXXA20151107118](https://openairdocs.org/sdr/IXXA20151107118.md): Skin · cracked · Nov 7, 2015 · N763CX · Boeing 767232 · Fuselage Main, Plate/Skin
  > SKIN CRACK & PROBABLE CORROSION AT APPROX FS 1339, LONGERON 35L. REMOVED DAMAGED AREA, FABRICATED FILLER & DOUBLER, INSTALLED REPAIRED PARTS IAW SRM 51-30-01. COMPLIED WITH HFEC OF AREA WHERE DAMAGE WAS REMOVED IAW NDT PART 6 51-00-19. NO DEFECTS NOTED.
- [SDR IXXA20150320050](https://openairdocs.org/sdr/IXXA20150320050.md): Spar Cap · corroded · Mar 20, 2015 · N763CX · Boeing 767232 · Wing Spar
  > AIRCRAFT GNDED FOR HEAVY MX. WING LE FRONT SPAR UPPER CAP CORRODED AT WING LES 579. R & R SPAR CAP IAW REA 47089REA19.
- [SDR IXXA20150320049](https://openairdocs.org/sdr/IXXA20150320049.md): Cap · corroded · Mar 20, 2015 · N763CX · Boeing 767232 · Wing, Rib/Bulkhead
  > AIRCRAFT GNDED FOR HVY MX. UPPER CAP ON LE RIB AT LES 261 CORRODED 4 INCHES FROM FRONT SPAR ON INBD SIDE. REMOVED, REPAIRED & INSTALLED UPPER RIB CAP LES 261 IAW SRM 57-41-09 & 51-40-02.
- [SDR IXXA20150320048](https://openairdocs.org/sdr/IXXA20150320048.md): Spar Cap · corroded · Mar 20, 2015 · N763CX · Boeing 767232 · Wing Spar
  > WING LE FRONT SPAR UPPER CAP CORRODED AT LES 472. R & R SECTION OF UPPER SPAR CAP FROM LES 450 - 506 IAW EO 47089REA18.
- [SDR IXXA20150330071](https://openairdocs.org/sdr/IXXA20150330071.md): Skin Panel · corroded · Mar 15, 2015 · N763CX · Boeing 767232 · Wing, Plate/Skin
  > AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. UPPER WING SURFACE AT STATION 187 REAR SPAR AREA PANEL IS BULGED UP. POSSIBLE SIGNS OF CORROSION UNDER PANEL. REMOVED CORROSION IAW SRM 57-20-1 FIG 101. REMOVED & INSTALLED FASTENERS IAW AM 28-11-00. LEAK
- [SDR IXXA20150331084](https://openairdocs.org/sdr/IXXA20150331084.md): Hinge Fitting · cracked · Feb 16, 2015 · N763CX · Boeing 767232 · Landing Gear Doors
  > AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. FWD FITTING AT BODY DOOR CTR HINGE BEAM CRACKED. R & R RT MLG DOOR HINGE FITTING AT CTR BEAM TO DOOR CTR IAW SRM 51-40-02. OPERATIONAL CHECKED SATISFACTORY. NO LEAKS NOTED IAW AMM 32-32-12.
- [SDR IXXA20150406118](https://openairdocs.org/sdr/IXXA20150406118.md): Skin · damaged · Feb 13, 2015 · N763CX · Boeing 767232 · Fuselage Main, Plate/Skin
  > AOG FOR HVY MX, FAILSAFE INSPECTION. AFT LOWER CARGO COMPARTMENT DOOR CUT OUT FOR PANEL 822D HAS A DAMAGED COUNTER SINK. REPAIRED DAMAGED SCREW HOLE IAW ENGINEERING DOCUMENT 47129REA04. REINSTALLED PANEL 822D IAW SRM 51-40-02.
- [SDR IXXA20150322061](https://openairdocs.org/sdr/IXXA20150322061.md): Fitting · corroded · Feb 12, 2015 · N763CX · Boeing 767232 · Fuselage Miscellaneous Structure
  > AIRCRAFT GNDED FOR HEAVY MX. CORROSION ON LOWER PORTION OF BODY FITTING AT STATION 933 RT SIDE IN UPPER CARGO. INSTALLED NEW STUB FITTING AT RT STATION 933 IAW SRM 51-40-02.
- [SDR IXXA20150322066](https://openairdocs.org/sdr/IXXA20150322066.md): Stringer · corroded · Feb 10, 2015 · N763CX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT GNDED FOR HEAVY MX. CORROSION ON STRINGER 36R AT STATION 445. R & R STRINGER 36R STATION 434 - 466 IAW REA 47089REA08.
- [SDR IXXA20150322060](https://openairdocs.org/sdr/IXXA20150322060.md): Floorbeam · corroded · Feb 10, 2015 · N763CX · Boeing 767232 · Fuselage Main, Floor Beam
  > AIRCRAFT GNDED FOR HEAVY MX. FLOOR FRAME UPPER CHORD HAS CORROSION UNDER NUTPLATES AT STATION 676, RBL 17 TO 19 LOWER SURFACE. FABRICATED, R & R FLOOR FRAME UPPER CHORD IAW DWG 143T 1211 & SRM 53-30-07 SEC 43 FIG 1.
- [SDR IXXA20150322059](https://openairdocs.org/sdr/IXXA20150322059.md): Floorbeam · corroded · Feb 10, 2015 · N763CX · Boeing 767232 · Fuselage Main, Floor Beam
  > AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. FLOORBEAM UPPER TEE CORRODED AT BS 478, RBL 5 TO 9 AROUND NUTPLATES ON LOWER SURFACE. R & R FLOORBEAM UPPER TEE IAW DWG 143T 1202 & SRM 53-30-07 SEC 43.
- [SDR IXXA20150406114](https://openairdocs.org/sdr/IXXA20150406114.md): Stringer · cracked · Dec 26, 2014 · N763CX · Boeing 767232 · Fuselage Main, Longeron/Stringer
  > AOG FOR HVY MX, FAILSAFE INSPECTION. UPPER CARGO STATION 676 AFT OF SPLICE ON STRINGER 11L IS CRACKED. REMOVED, FABRICATED & INSTALLED NEW STRINGER IAW ENGINEERING DOCUMENT 4712REA03 & SRM 53-00-03.
- [SDR IXXA20150406116](https://openairdocs.org/sdr/IXXA20150406116.md): Floorbeam · cracked · Dec 23, 2014 · N763CX · Boeing 767232 · Fuselage Main, Floor Beam
  > AOG FOR HVY MX, FAILSAFE INSPECTION. STATION 1021 CTR FLOORBEAM FITTING CRACKED. R & R FLOORBEAM ATTACH FITTING IAW SRM 51-40-02.
- [SDR IXXA20150406115](https://openairdocs.org/sdr/IXXA20150406115.md): Attach Fitting · cracked · Dec 23, 2014 · N763CX · Boeing 767232 · Fuselage Main, Floor Beam
  > AOG FOR HVY MX, FAILSAFE INSPECTION. STATION 1043 CTR FLOORBEAM ATTACH FITTING CRACKED. R & R FLOORBEAM ATTACH FITTING IAW SRM 51-40-02.
- [SDR IXXA20150406112](https://openairdocs.org/sdr/IXXA20150406112.md): Skin · gouged · Dec 23, 2014 · N763CX · Boeing 767232 · Fuselage Main, Plate/Skin
  > AOG FOR HVY MX, FAILSAFE INSPECTION. FUSELAGE SKIN GOUGED IN TWO PLACES AT AFT END OF UPPER HORSE COLLAR FS 1804 - 1815. REPAIRED DAMAGED FWD SKIN IAW ENGINEERING DOCUMENT REA 47129REA02. REPAIRED DAMAGED AFT SKIN IAW SRM 53-80-01 & ENGINEERING DOCUMENT REA
- [SDR IXXA20150403106](https://openairdocs.org/sdr/IXXA20150403106.md): Fitting · corroded · Dec 23, 2014 · N763CX · Boeing 767232 · Fuselage Miscellaneous Structure
  > AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. RT 1809.5 OUTER CHORD LOWER TENSION FITTING, TENSION BOLT HOLE ELONGATED. REPLACED RT LOWER FWD STATION 1809.5 TENSION FITTING IAW SRM 51-40-02 & EO 53-767-4857.
- [SDR IXXA20150403105](https://openairdocs.org/sdr/IXXA20150403105.md): Structure · corroded · Dec 23, 2014 · N763CX · Boeing 767232 · Fuselage Miscellaneous Structure
  > AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. RT 1809.5 FWD OUTER CHORD SKIN HAS HFEC OPEN HOLE DEFECT INDICATION AT FWD LOWER HOLE, COMMON TO CHORD, SPLICE FITTING & TENSION FITTING. INTERIOR SURFACE AROUND HOLE HAS CORROSION. DAMAGED AREA WAS REPAIRE
- [SDR IXXA20150403104](https://openairdocs.org/sdr/IXXA20150403104.md): Fitting · corroded · Dec 23, 2014 · N763CX · Boeing 767232 · Fuselage Miscellaneous Structure
  > AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. RT 1809.5 FWD OUTER CHORD UPPER TENSION FITTING HAS DAMAGED HOLE, COMMON TO SPLICE FITTING & SKIN. RT UPPER FWD STATION 1809.5 TENSION FITTING WAS REPLACED IAW SRM 51-40-02 & EO 53-767-4857. FITTING FABRICA
- [SDR IXXA20150403103](https://openairdocs.org/sdr/IXXA20150403103.md): Fitting · corroded · Dec 23, 2014 · N763CX · Boeing 767232 · Fuselage Miscellaneous Structure
  > AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. RT 1809.5 FWD OUTER CHORD SPLICE FITTING LOWER TENSION BOLT HOLE HAS HFEC OPEN HOLE DEFECT INDICATION. R & R SPLICE FITTING IAW SRM 51-40-02 & EO 53-767-4857.
- [SDR IXXA20150330070](https://openairdocs.org/sdr/IXXA20150330070.md): Splice Plate · corroded · Dec 23, 2014 · N763CX · Boeing 767232 · Wing Spar
  > AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. WING LE FRONT SPAR UPPER SPAR CAP CORRODED AT LES 472. R & R SECTION OF UPPER SPAR CAP, UPPER SPLICE PLATE, FROM LES 450 - 506 IAW 47089REA18.
- [SDR IXXA201503220053](https://openairdocs.org/sdr/IXXA201503220053.md): Plate · corroded · Dec 19, 2014 · N763CX · Boeing 767232 · Fuselage Miscellaneous Structure
  > AIRCRAFT GNDED FOR HEAVY MX. STRUCTURE BEHIND LT PICKLE FORK SHOWS SIGNS OF CORROSION. R & R CORRODED BEARING PLATE IAW SRM 51-40-02 & EO 47008ORD11.
- [SDR IXXA20150406107](https://openairdocs.org/sdr/IXXA20150406107.md): Frame · corroded · Dec 17, 2014 · N763CX · Boeing 767232 · Fuselage Main, Frame
  > AOG FOR HVY MX, FAILSAFE INSPECTION. FLC FUSELAGE STATION 368, RBL 23 UNDERSIDE OF UPPER CHORD IS CORRODED AT NUTPLATE LOCATION. R & R UPPER CHORD IAW BDWG 143T1202 & SRM 51-40-02. PRIMED & TOP COAT FINISH APPLIED IAW AMM 51-21-10-7.

Next page: https://openairdocs.org/deregistered/N763CX-2024-08-05/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 = 'N763CX' AND deregistration_id = 'N763CX-2024-08-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N763CX-2024-08-05/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.