# Service difficulty reports: Boeing 767-338

A list on [Boeing 767-338](https://openairdocs.org/model/boeing-767-338.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 27 · 1,326 reports

- [SDR ABXA20261017471](https://openairdocs.org/sdr/ABXA20261017471.md): Autothrottle Sys · faulted · Oct 17, 2026 · N317CM · Boeing 767338 · Auto Flight System
  > AUTOTHROTTLES DISCONECTED @ CRUISE WITH NO INDICATION WHICH LEAD TO STALL RECOVERY 210 KNOTS BEGAN RECOVERY AND ESTIMATE 90 SECONDS RECOVERY FROM 330 TO 280 CREW DECLARED EMERGENCY AND RETURNED TO MIA (ATB) A/C LANDED AND MTX GROUNDED A/C PERFORMED STALL (AFTE
- [SDR ABXA20261015468](https://openairdocs.org/sdr/ABXA20261015468.md): Fire Detector · illuminated · Oct 15, 2026 · N363CM · Boeing 767338 · Fire Detection
  > SECTION A AT ZONE 8 ON CARGO FIRE DETECTION LIGHT BAR IS ILLUMINATED AMBER. MX DEFERRED ZONE 8 AIR DETECTOR OF MAIN CARGO DECK PER MEL 26-16-2-2. PLACARDS INSTALLED. A/C RETURNED TO SERVICE.
- [SDR IXXA20261005091](https://openairdocs.org/sdr/IXXA20261005091.md): Light · inoperative · Oct 5, 2026 · N313AZ · Boeing 767338 · Emergency Lighting
  > SUPERNUMERARY EMERGENCY LIGHTS INOPERATIVE. PLACED ON DEFERRAL 77612 MINIMUM EQUIPMENT LIST ATI-33-51-01-01 CATEGORY D. DUE 02 FEBRUARY 2027.
- [SDR ABXA20261004456](https://openairdocs.org/sdr/ABXA20261004456.md): Oxygen Mask · no test · Oct 4, 2026 · N317CM · Boeing 767338 · Crew Oxygen System
  > DURING SCHEDULED MTC, CAPT. OXYGEN MASK DOES NOT TEST PROPERLY.MTX REMOVED AND REPLACED CAPT OXYGEN MASK STOWAGE BOX IAW AMM 35-11-51. OPS CHK AND LEAK CHK GOOD.A/C RETURNED TO SERVICE.
- [SDR IXXA2026100302](https://openairdocs.org/sdr/IXXA2026100302.md): Keelbeam · cracked · Oct 3, 2026 · N313AZ · Boeing 767338 · Fuselage Main, Keel
  > LH KEEL BEAM WEB CRACKED
- [SDR IXXA2026100301](https://openairdocs.org/sdr/IXXA2026100301.md): Keelbeam · cracked · Oct 3, 2026 · N313AZ · Boeing 767338 · Fuselage Main, Keel
  > KEEL BEAM WEB CRACKED
- [SDR ABXA20260930442](https://openairdocs.org/sdr/ABXA20260930442.md): Bleed Valve · defective · Sep 30, 2026 · N363CM · Boeing 767338 · Compressor Bleed Valve
  > DURING TAXI, R BLD ISLN VAL EICAS MESSAGE. R ISLN VAL DISCRETE LIGHT. CREW RETURNED TO THE GATE (BTB). MTX TROUBLE SHOT AND REMOVED AND REPLACED RH BLEED ISOLATION VALVE IAW B767 AMM 36-11-04. LEAKS AND OPS CHECK GOOD. AIRCRAFT REMAINS NO ETOPS. RETURNED A/C T
- [SDR ABXA20260917427](https://openairdocs.org/sdr/ABXA20260917427.md): Battery · defective · Sep 17, 2026 · N364CM · Boeing 767338 · Emergency Lighting
  > DURING INSP/MTC, 2 EACH EMERGENCY LIGHTS INOP, SUPERNUMERY AREA. REPLACED BATTERY PACK AT POSITION M736 PER B767 AMM 33-51-07. SYSTEM CHECKS NORMAL. A/C RETURNED TO SERVICE.
- [SDR ABXA20260916412](https://openairdocs.org/sdr/ABXA20260916412.md): Smoke Goggles · deteriorated · Sep 16, 2026 · N364CM · Boeing 767338 · Emergency Equipment
  > DURING INSP/MTC, FOUND FO SMOKE GOGGLES DETERIORATED. REMOVED F.O. SMOKE GOGGLES. REPLACED WITH SERV. GOGGLES IAW AMM 25-64-00. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE.
- [SDR IXXA202609140205](https://openairdocs.org/sdr/IXXA202609140205.md): Light · illuminated · Sep 14, 2026 · Boeing 767338 · Emergency Lighting
  > EMERGENCY LIGHTS UNARM LIGHT ILLUMINATED.
- [SDR ABXA20260913409](https://openairdocs.org/sdr/ABXA20260913409.md): Latch · failed · Sep 13, 2026 · N362CM · Boeing 767338 · Flight Compartment Windows
  > SHORTLY AFTER APPROACHING 80KTS ON THE RUNWAY IN KLAS, THE FIRST OFFICERS WINDOW POPPED OPEN AND THE CAPTAIN ABORTED THE TAKEOFF (ATO). CREW RESECURED THE FIRST OFFICER'S WINDOW AND LINED BACK UP FOR TAKEOFF. A/C DID NOT RETURN TO THE GATE AND MAINTENANCE WAS
- [SDR ABXA20260913404](https://openairdocs.org/sdr/ABXA20260913404.md): Controller · defective · Sep 13, 2026 · N362CM · Boeing 767338 · Cabin Pressure Controller
  > WHILE CRUISING AT FL370 BETWEEN THE CALIFORNIA AND NEVADA BORDER, THE FO AND CAPT HEARD A BEEPING NOISE COMING FROM THE MAIN DECK CARGO AREA. ABOUT 30 SECONDS AFTER THAT THEY RECEIVED A MASTER WARNING EICAS CABIN ALTITUDE. AT THAT TIME THEY BOTH DONNED OXYGEN
- [SDR IXXA20260913080](https://openairdocs.org/sdr/IXXA20260913080.md): Warning Light · illuminated · Sep 13, 2026 · N307AZ · Boeing 767338 · Emergency Lighting
  > EMERGENCY LIGHTS UNARM LIGHT ILLUMINATED.
- [SDR ABXA20260912402](https://openairdocs.org/sdr/ABXA20260912402.md): Overheat Sys · false activation · Sep 12, 2026 · N317CM · Boeing 767338 · Overheat Detection
  > FIRE/OVHT SYS ON FINAL APPROACH. AC LANDED AND MTX GROUNDED A/C. PERFORMED OPERATIONAL CHECK I.A.W A.M.M B767 26-11-00. ALL FOUND NORMAL. UNABLE TO DUPLICATE FAULT, NO STATUS MESSAGE. AIRCRAFT REMAINS NO ETOPS AND RETURNED A/C TO SERVICE.
- [SDR 2026FA0000687](https://openairdocs.org/sdr/2026FA0000687.md): Skin · damaged · Sep 9, 2026 · N373CM · Boeing 767338 · Fuselage Main, Plate/Skin
  > AT ITS ARRIVAL IN GUATEMALA, DAMAGE ON THE FUSELAGE WAS DETECTED UN WALK AROUND CHECK. SKIN SEEMED TO BE SEVERLY DAMAGE. AFTER INSPECTION FOUND SEVERAL FRAMES AND STRINGERS DAMAGED, BENT OR BROKEN. ALSO THE SKINS HAS SEVERAL CRACKS. STATION 350 TO 360 STRINGER
- [SDR ABXA20260903393](https://openairdocs.org/sdr/ABXA20260903393.md): Module · faulted · Sep 3, 2026 · N362CM · Boeing 767338 · Rudder Control System
  > RUDDER RATIO EICAS MSG APPEARED AFTER BLOCK OUT. CREW RETURNED TO THE GATE (BTB). MTC PERFORMED B767 FIM 27-09 FT 803 CLEARED FAULT BALLS ON RUDDER RATIO CHANGING MODULES. RAN BOTH ENGINES IAW B767AMM 71-00-00 MESSAGE DID NOT RETURN NO FURTHER ACTION REQUIRED
- [SDR ABXA20260901377](https://openairdocs.org/sdr/ABXA20260901377.md): Resistor · faulted · Sep 1, 2026 · N364CM · Boeing 767338 · Door System Wiring
  > DURING TAXI EMERGENCY DOORS LIGHT ILLUMINATED. CREW RETURNED TO THE BLOCKS (BTB). REMOVED AND INSTALLED RESISTOR 59032 IAW B767-WDM 52-71-12, PERFORMED PSEU BITE TEST IAW B767 FIM 32-09 FAULT TREE803, BITE TEST GOOD. A/C REMAINS NO ETOPS AND RETURNED TO SERVI
- [SDR ABXA20260901392](https://openairdocs.org/sdr/ABXA20260901392.md): Skin · dented · Sep 1, 2026 · N364CM · Boeing 767338 · Fuselage Main, Plate/Skin
  > DURING C-CHECK, INSPECTION AT FUSELAGE SKIN, LOWER SKIN PANEL, AT BS 1373, BETWEEN STR 27R AND ABOVE STR 29R WAS FOUND DENTED OUT OF SRM LIMITS 53-00-01, FIG 101, DETAIL 3 AND WHILE PERFORMING SRM 53-00-01, REPAIR 14, FOUND DOUBLER TO STOP ON AN INTERNAL DOU
- [SDR ABXA20260901391](https://openairdocs.org/sdr/ABXA20260901391.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Wing, Plate/Skin
  > DURING C-CHECK, CORROSION WAS OBSERVED ON THE RT WING UPPER SURFACE SKIN PANEL NR 1 AT WS 434 OVER UPPER RIB FLANGE PIN 113T1545-6, THE DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA IAW SRM 51-10-02 WITH MEASURED MATERIAL REMAINING OF0.112 INCHES FROM INITIAL T
- [SDR ABXA20260901390](https://openairdocs.org/sdr/ABXA20260901390.md): Skin · damaged · Sep 1, 2026 · N364CM · Boeing 767338 · Wing, Plate/Skin
  > DURING AN INSPECTION, LEFT WING LOWER SKIN EXISTING BLEND REPAIRS AT WS 110, STRINGER 10 WAS FOUND. THE AFFECTED FASTENERS WERE REMOVED, AND HFEC ROTO AND SURFACE INSPECTIONS WERE ACCOMPLISHED WITH NO ADDITIONAL DAMAGE. THE BLEND AFFECTS SKIN PANEL AND SKIN PA
- [SDR ABXA20260901389](https://openairdocs.org/sdr/ABXA20260901389.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Wing, Plate/Skin
  > DURING C-CHECK AT AMES (TPA), DURING STRUCTURAL INSPECTION OF THE RIGHT-WING TOP SKIN PANEL NO.1 UPPER SURFACE, CORROSION WAS FOUND AT WS 350 UNDER WING FIXED TRAILING EDGE PANEL 113T1609-2. CORROSION WAS REMOVED BY BLENDING AND FOUND TO BE OUT OF LIMITS PER S
- [SDR ABXA20260901388](https://openairdocs.org/sdr/ABXA20260901388.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, DURING STRUCTURAL INSPECTION THE LT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS 300.105 AND RS 323.281, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BLENDED IAW SRM. DAMAGE REPAIRED IAW FVCI EO 26099-5, & ABX-REA-5513-
- [SDR ABXA20260901387](https://openairdocs.org/sdr/ABXA20260901387.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, DURING STRUCTURAL INSPECTION THE LT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS STA 300.105 AND RS STA 323.281, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BLENDED PER SRM. ENGINEERING CONTACTED FOR FURTHER EVALUATION AN
- [SDR ABXA20260901386](https://openairdocs.org/sdr/ABXA20260901386.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, LT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX" 3" LONG AT 165" FROM FUSELAGE BODY. (AROUND FASTERNERS) FOUND WITH CORROSION BETWEEN RS STA 160 AND RS STA 180, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BLENDED PER SR
- [SDR ABXA20260901385](https://openairdocs.org/sdr/ABXA20260901385.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, LT HORIZONTAL STAB, UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX" 3" LONG AT 8" FROM FUSELAGE BODY. (AROUND FASTERNERS) LT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS STA 13.986 AND RS STA 30.605, UPPER REA
- [SDR ABXA20260901384](https://openairdocs.org/sdr/ABXA20260901384.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX 2" LONG AT 70"" O/B SIDE. (AROUND FASTERNERS) RT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION AT RS 275.605, UPPER REAR SPAR AREA STRG-1. CORROSION WAS BL
- [SDR ABXA20260901383](https://openairdocs.org/sdr/ABXA20260901383.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX" 2" LONG AT 47" FROM OTBD SIDE. (AROUND FASTERNERS) RT HORIZONTAL STAB UPPER SKIN PANEL WAS FOUND WITH CORROSION BETWEEN RS 290 & RS 310, UPPER REAR SPAR AREA STRG-1) CO
- [SDR ABXA20260901382](https://openairdocs.org/sdr/ABXA20260901382.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APPROX 3" LONG AT 22" FROM OTBD SIDE & 2.5" FWD OF REAR SPAR. (AROUND FASTERNERS). CORROSION BLENDED IAW SRM. DAMAGE REPAIRED IAW FVCI EO 26099-10 AND ABX-REA-5513-66201
- [SDR ABXA20260901381](https://openairdocs.org/sdr/ABXA20260901381.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, RT HORIZONTAL STAB. UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX 4" LONG AT 161" FROM FUSELAGE BODY. (AROUND FASTERNERS) CORROSION WAS BLENDED IAW SRM. DAMAGE REPAIRED IAW FVCI EO 26099-7, & ABX-REA-5513-66193-00.
- [SDR ABXA20260901380](https://openairdocs.org/sdr/ABXA20260901380.md): Skin · corroded · Sep 1, 2026 · N364CM · Boeing 767338 · Horizontal Stabilizer, Plate/Skin
  > DURING C-CHECK, R/H HORIZONTAL STAB UPPER SURFACE REAR SPAR HAS COROSION BLISTER OF APROX 5" LONG AT 95" FROM FUSELAGE BODY. (AROUND FASTERNERS) FOUND CORROSION BTWN RS STA 104.105, UPPER REAR SPAR AREA AND STRG 1. CORROSION WAS BLENDED IAW SRM. ENGINEERING
- [SDR ABXA20260901379](https://openairdocs.org/sdr/ABXA20260901379.md): Skin · dented · Sep 1, 2026 · N364CM · Boeing 767338 · Fuselage Main, Plate/Skin
  > DURING C-CHECK & INSPECTION, FUSELAGE SKIN, LOWER SKIN PANEL AT BS 1373, BTWN STR 27R & ABOVE STR 29R WAS FOUND WITH A DENT OUT OF SRM LIMITS 53-00-01, FIG 101, DETAIL 3, & WHILE PERFORMING SRM 53-00-01, REPAIR 14, FOUND DOUBLER TO STOP ON AN INTERNAL DOUBLER
- [SDR ABXA20260822372](https://openairdocs.org/sdr/ABXA20260822372.md): Actuator · malfunctioned · Aug 22, 2026 · N371CM · Boeing 767338 · Aircraft Fuel Distribution System
  > LEFT ENG SPAR VALVE LIGHT ILLUMINATED AFTER FUEL ADDED, START NOT SUSTAINED. ACFT RETURNED TO THE GATE (BTB). MTC REMOVED LT ENG SHUTOFF VALVE ACTUATOR IAW AMM 28-22-11. INSTALLED NEW LT ENG FUEL SPAR ACTUATOR IAW AMM 28-22-11. ALL CHECKS IN LIMITS OPS TEST GO
- [SDR ABXA20260821370](https://openairdocs.org/sdr/ABXA20260821370.md): Pitot Tube · defective · Aug 21, 2026 · N317CM · Boeing 767338 · Pitot/Static System
  > DURING TAXI OUT CAPT. PITOT LIGHT ON OVERHEAD PANEL ILLUMINATED. A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C. MTX REMOVED AND REPLACED CAPTAINS (LEFT UPPER) PITOT-STATIC PROBE PER B767 AMM 34-11-01. LEAK CHECK GOOD PER B767 AMM 34-11-00. AIRCRAFT REMA
- [SDR ABXA20260812359](https://openairdocs.org/sdr/ABXA20260812359.md): Throttle · stiff · Aug 12, 2026 · N317CM · Boeing 767338 · Power Lever
  > STIFF RESISTANCE FELT ON THROTTLE LEVERS. SLOW ACCELERATION AND RESPONSE DURING TAXI. A/C RETURNED TO THE GATE (BTB). MTX ACCOMPLISHED ACCELERATION AND DECELERATION TEST IAW B767 AMM 71-00-00. BOTH ENGINES WITHIN LIMITS. CYCLED THROTTLES MULTIPLE TIMES, NO RES
- [SDR ABXA20260811358](https://openairdocs.org/sdr/ABXA20260811358.md): Control Box · dislodged · Aug 11, 2026 · N371CM · Boeing 767338 · Fuel Controlling System
  > AT FL340, LT ENGINE N1 DROP DOWN TO IDLE, NO INDICATION OF OTHER ABNORMAL. CREW DECLARED AN EMERGENCY AND DIVERTED BACK TO CVG. AFTER TROUBLESHOOTING MTX FOUND L ENGINE PUSH-PULL CABLE CONTROL BOX DISLODGED FROM MEC AT THE HOUSING BODY. GAINED ACCESS TO, THEN
- [SDR ABXA20260806350](https://openairdocs.org/sdr/ABXA20260806350.md): Bleed Valve · defective · Aug 6, 2026 · N371CM · Boeing 767338 · Compressor Bleed Valve
  > L ISLN VALVE LIGHT ON START, L N2 INADEQUATE FOR ENGINE START. A/C RETURNED TO THE GATE (BTB). MTC REMOVED AND REPLACED LEFT ISLN VALVE OPS CHECKS NORMAL IAW B767 AMM 36-11-04. AIRCRAFT REMAINS ETOPS 180. A/C RETURNED TO SERVICE.
- [SDR IXXA20260722059](https://openairdocs.org/sdr/IXXA20260722059.md): Elec Connector · dirty · Jul 22, 2026 · N307AZ · Boeing 767338 · Light System Wiring
  > EMERGENCY LIGHTS NOT ARMING. CLEANED EMERGENCY LIGHT PANEL ELECTRICAL CONNECTOR IAW SOPM 20-60-01. OPS CHECKED GOOD.
- [SDR ABXA20260720326](https://openairdocs.org/sdr/ABXA20260720326.md): Warning Message · illuminated · Jul 20, 2026 · N362CM · Boeing 767338 · Central Warning
  > DURING TAXI AFTER START R ENG BLEED LIGHT DID NOT EXTINGUISH NO DUCT PRESSURE INDICATED. EICAS MESSAGES "R ENG BLLED" AND "R PACK OFF"A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C MTX PERFORMED GROUND TEST NR 3. IAW AMM 71-00-00 OPS TEST GOOD BOTH PACKS
- [SDR ABXA20260716323](https://openairdocs.org/sdr/ABXA20260716323.md): Controller · faulted · Jul 16, 2026 · N219CY · Boeing 767338 · Cabin Temperature Controller
  > DUIRNG TAXI OUT AFTER ENG START WE GOT AFT CABIN TEMP, FWD CABIN TEMP, FLT DECK TEMP INOP. CAME ON AND A/C RETURNED TO THE GATE (BTB). MTX GROUNDED ACFT, AND RESET ZONE TEMP CONTROLLER IAW AMM 21-51-13 OPS CK GOOD ACFT REMAINS NO ETOPS. AND RETURNED ACFT TO
- [SDR ABXA20260705303](https://openairdocs.org/sdr/ABXA20260705303.md): Bleed Air Sys · no discrepancy · Jul 5, 2026 · N363CM · Boeing 767338 · Pneumatic Distribution System
  > LEFT PACK OFF AND L ENG BLEED OFF AFTER PUSHBACK AND AFTER START CHECKLIST. L DUCT PRESSURE DROPPED TO ZERO. R DUCT PRESSURE NORMAL AC RETURNED TO THE GATE (BTB) MTX GROUNDED A/C,MTX PERFORMED LH ENGINE RUN REF AMM 71-00-00, NO FAULTS NOTED AT THIS TIME RETUR
- [SDR ABXA20260625285](https://openairdocs.org/sdr/ABXA20260625285.md): Test Switch · sticking · Jun 25, 2026 · N362CM · Boeing 767338 · Smoke Detection
  > DURING INSP/MTC, FIRE/OVERHEAT TEST FOUND SYS FAIL/RESET SWITCH STICKY. REMOVED AND REPLACED FIRE/OVHT TEST PANEL ASSY PER B767 AMM 26-11-01. OPS CHECK SATISFACTORY. ACFT REMAINS ETOPS 180. ACFT RETURNED TO SERVICE.
- [SDR IXXA20260622053](https://openairdocs.org/sdr/IXXA20260622053.md): Terminal · faulted · Jun 22, 2026 · N503AZ · Boeing 767338 · Light System Wiring
  > DURING PRE-FLIGHT CREW REPORTED RIGHT CHART LIGHT SHOCKED PILOT WHEN TOUCHED. REMOVED AND REPLACED RIGHT CHART LIGHT IN ACCORDANCE WITH B767 AMM 33-14-00. OPERATIONAL CHECK GOOD.
- [SDR ABXA20260619268](https://openairdocs.org/sdr/ABXA20260619268.md): Warning Message · illuminated · Jun 19, 2026 · N362CM · Boeing 767338 · Fuel Boost Pump
  > DURING TAXI, AFTER BLOCK OUT, L AFT FUEL PUMP EICAS MESSAGE APPEARED ACCOMPLISHED QRH. RETURNED TO GATE (BTB). DEFERRED L AFT FUEL PUMP IAW MEL 28-22-1. PLACARDS INSTALLED. ACFT DOWNGRADED TO ETOPS 120. ACFT RETURNED TO SERVICE.
- [SDR ABXA20260617266](https://openairdocs.org/sdr/ABXA20260617266.md): Start Valve · faulted · Jun 17, 2026 · N371CM · Boeing 767338 · Engine Start Valves/Controls
  > DURING ENGINE START, LT ENGINE START VALVE INOPERATIVE. ACFT RETURNED TO THE GATE (BTB). DEFERRED LT START VALVE IAW MEL 80-00-2-1. MX ACTIONS ACCOMPLISHED PLACARDS INSTALLED A/C REMAINS ETOPS 180. REMOVED AND REPLACED L ENG STARTER VALVE IAW B767 AMM 80-11-02
- [SDR ABXA20260617264](https://openairdocs.org/sdr/ABXA20260617264.md): Radar · faulted · Jun 17, 2026 · N371CM · Boeing 767338 · Ground Proximity System
  > DURING TAXI, CREW RECEIVED NO LAND 3 AND C RAD ALT INDICATION. RETURNED TO THE GATE (BTB). MTC DEFERRED RAD ALT PER MEL 34-33-1-2A-1 MX PROCEDURES APPLIED. PLACARD INSTALLED ACFT DOWNGRADED TO CAT II. ACFT RETURNED TO SERVICE.
- [SDR IXXA20260612050](https://openairdocs.org/sdr/IXXA20260612050.md): Guard · detached · Jun 12, 2026 · N313AZ · Boeing 767338 · Emergency Lighting
  > EMERGENCY LIGHT SWITCH GUARD SPRING RELEASED/DETACHED. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH GUARD IN ACCORDANCE WITH B767 AMM 20-11-00. OPERATIONAL CHECK IN ACCORDANCE WITH B767 AMM 33-51-08 NOTED NO FAULTS.
- [SDR IXXA20260609002](https://openairdocs.org/sdr/IXXA20260609002.md): Web · cracked · Jun 9, 2026 · N503AZ · Boeing 767338 · Nacelle/Pylon, Plate/Skin
  > NUMBER 2 PYLON AFT FAIRING 447DB (STINGER) INTERNAL SUPPORT WEB IS CRACKED REFERENCE AMES WO N503AZ-28 NR 193266-0400-0075
- [SDR IXXA20260609001](https://openairdocs.org/sdr/IXXA20260609001.md): Channel · cracked · Jun 9, 2026 · N503AZ · Boeing 767338 · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 2 PYLON AFT FAIRING 447DB (STINGER) INTERNAL O/B WEB STIFFENER IS CRACKED IN LOWER RADIUS REFERENCE AMES WO N503AZ-28 NR 193266-0400-0076
- [SDR IXXA20260606001](https://openairdocs.org/sdr/IXXA20260606001.md): Strut · cracked · Jun 6, 2026 · N503AZ · Boeing 767338 · Wing Miscellaneous Structure
  > LEFT WING L/E UPPER SUPPORT STRUCTURE HAS CRACKAT LOCK FASTENER AFT END, VERIFIED BY EDDY CURRENT AROUND LES 506
- [SDR ABXA20260604242](https://openairdocs.org/sdr/ABXA20260604242.md): Detection Sys · faulted · Jun 4, 2026 · N362CM · Boeing 767338 · Fire Detection
  > AFTER FIRE TEST ALL -B- MAIN DECK CARGO LIGHTS ILLUMINATED WHITE. NO EICAS INDICTATIONS MTX,MTX GROUNDED ACFT AND PERFORMED AFLOTS TEST IAW B767 26-10-00. FAULTS CLEARED NO FURTHER DEFECTS NOTED.AC RETURNED TO SERVICE

Next page: https://openairdocs.org/model/boeing-767-338/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 aircraft_model_key = '767338'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-767-338/reports

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