# Service difficulty reports: Boeing 767-375

A list on [Boeing 767-375](https://openairdocs.org/model/boeing-767-375.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 28 · 1,386 reports

- [SDR UIEA2026102300995](https://openairdocs.org/sdr/UIEA2026102300995.md): Battery · inoperative · Oct 22, 2026 · N649GT · Boeing 767375 · Emergency Equipment
  > EMERGENCY FLASHLIGHT NEXT TO LAV LED NOT FLASHING. R & R FLASHLIGHT BATTERY IAW AMM 25-64-02. OPS CHECK GOOD.</P>)
- [SDR ABXA20261018474](https://openairdocs.org/sdr/ABXA20261018474.md): A/C Pack · warning message · Oct 18, 2026 · N1709A · Boeing 767375 · Cabin Cooling System
  > DURING TAXI OUT, L PACK OFF EICAS MSG AFTER ENGINE START. A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C,MTX DEFERRED LH PACK IAW ABX MEL 21-51-1-1. AND RETURNED A/C TO SERVICE
- [SDR UIEA2026101500987](https://openairdocs.org/sdr/UIEA2026101500987.md): Limit Switch · failed · Oct 12, 2026 · N649GT · Boeing 767375 · Stabilizer Control System
  > REJECTED T/O AT 60KTS DUE TO EICAS MESSAGE. UNSCHEDULED STAB TRIM MESSAGE ALSO APPEARED TWICE DURING TAXI OUT(<P>RIGHT STAB TRIM LIMIT SWITCH/POSITION INDICATOR EXPERIENCED AN INTERNAL SHORT. R&R R/H STAB TRIM LIMIT SWITCH AND POSITION TRANSMITTER MODULE PER A
- [SDR UIEA2026100900972](https://openairdocs.org/sdr/UIEA2026100900972.md): Failsafe · damaged · Oct 10, 2026 · N649GT · Boeing 767375 · Fuselage Main, Structure
  > DETECTED DEFECT INDICATION DURING EO 6753A070 (SB 767-53A0100 R3/AD 2021-09-04) STA 955 REAR SPAR BULKHEAD SIDE FITTING FAILSAFE STRAP ULTRASONIC INSPECTION. DEFECT SIGNAL LOCATION: FAILSAFE STRAP (RH)(<P>REMOVED PLATE ASSY OF R/H MAIN L/G W/W LONGN AND L/G BE
- [SDR UIEA2026100900973](https://openairdocs.org/sdr/UIEA2026100900973.md): Skin · cracked · Oct 10, 2026 · N649GT · Boeing 767375 · Fuselage Main, Plate/Skin
  > DURING EO 6753A070 (SB 767-53A0100 R3/AD 2012-09-04 TERMINATING ACTION) OPEN-HOLE HFEC AT STA 955 R/H, A CRACK INDICATION WAS FOUND AT THE FAIL-SAFE STRAP, AND CORROSION WAS FOUND ON THE T-FITTING AND SKIN PANEL (P/N 145T3321-4) NEAR STR 22AR. REMAINING THICK
- [SDR UIEA2026100900974](https://openairdocs.org/sdr/UIEA2026100900974.md): Tee Fitting · cracked · Oct 10, 2026 · N649GT · Boeing 767375 · Fuselage Main, Structure
  > DURING EO 6753A070 PART 4 (SB 767-53A0100 R3 / AD 2012-09-04 TERMINATING ACTION) AT STA 955 R/H, CRACKS WERE FOUND AT THE 10 O'CLOCK (0.5Â€?) AND 4 O'CLOCK (NOT MEASURABLE) POSITIONS FROM THE LOWEST FAIL-SAFE STRAP HOLE PER 767 NDTM 51-00-16 / 51-00-19.(<P>STR
- [SDR UIEA2026100900975](https://openairdocs.org/sdr/UIEA2026100900975.md): Skin · corroded · Oct 10, 2026 · N649GT · Boeing 767375 · Trailing Edge Flaps
  > CORROSION FOUND ON R/H INBOARD MAIN FLAP LOWER SKIN (DAMAGE SIZE: L=11.2", W=1.7")(<P>REPAIRED THE R/H INBD MAIN FLAP LOWER PANEL (P/N 113T2243-2) SKIN IN ACCORDANCE WITH BMN SP1-TLS-26-0036, WHICH WAS APPROVED BY FAA FORM 8100-9 DATED 08OCT2026. NO FURTHER DE
- [SDR UIEA2026100900976](https://openairdocs.org/sdr/UIEA2026100900976.md): Structure · corroded · Oct 10, 2026 · N649GT · Boeing 767375 · Trailing Edge Flaps
  > CORROSION FOUND ON L/H INBOARD MAIN FLAP LOWER CHORD (DAMAGE SIZE: L=19")(<P>PER BOEING RDR SP1-TLS-26-0037-05B, INSTALLATION OF CHORD (P/N 113T2225-401) ON THE FLAP (P/N 113T2201-23A) FOR AIRCRAFT N649GT HAS BEEN APPROVED AS STRUCTURALLY ACCEPTABLE. REMOVED L
- [SDR UIEA2026100900977](https://openairdocs.org/sdr/UIEA2026100900977.md): Flap · damaged · Oct 10, 2026 · N649GT · Boeing 767375 · Trailing Edge Flaps
  > CORROSION FOUND ON RT INBD MAIN FLAP LOWER CHORD (DAMAGE SIZE: L=12") REMOVED RT INBD MAIN FLAP LOWER CHORD AND REPLACED WITH NEW CHORD PER SRM 51-40-02. HOLE COPIED PER SRM 51-40-05. NUT-PLATES INSTALLED PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.
- [SDR UIEA2026100900978](https://openairdocs.org/sdr/UIEA2026100900978.md): Skin · corroded · Oct 10, 2026 · N649GT · Boeing 767375 · Leading Edge Devices
  > L/H WING LEADING EDGE NR 1 SLAT SKIN, FOUND DENSE CORE CORROSION (DAMAGE SIZE: L = 2.5", W=5.4") REPAIRED LT WING LEADING EDGE NR 1 SLAT SKIN IAW SRM 51-70-10 AND BMN SP1-TLS-26-0028. NO FURTHER DEFECTS NOTED.
- [SDR ABXA20261009464](https://openairdocs.org/sdr/ABXA20261009464.md): A/C Pack · inoperative · Oct 9, 2026 · N1709A · Boeing 767375 · Cabin Cooling System
  > DURING TAXI, L PACK WILL NOT TURN ON WITH R PACK OPERATING. A/C RETURNED TO GATE (BTB). MX DEFERRED LEFT HAND PACK IAW MEL 21-51-1-1. A/C RETURNED TO SERVICE.
- [SDR ABXA20260926435](https://openairdocs.org/sdr/ABXA20260926435.md): Starter · defective · Sep 26, 2026 · N1709A · Boeing 767375 · Engine Starter
  > DURING TAXI, #2 ENG WOULD NOT ROTATE. CREW RETURNED TO THE GATE (BTB). MTC REMOVED AND REPLACED RH ENG STARTER IAW AMM 80-11-01. LEAK CHK GOOD OPS CHECK GOOD. PERFORMED POWERPLANT TEST 3 GND IDLE LEAK NFF AT THIS TIME, AC RELEASED E180. A/C RETURNED TO SERVICE
- [SDR ABXA20260915408](https://openairdocs.org/sdr/ABXA20260915408.md): Starter · defective · Sep 15, 2026 · N1709A · Boeing 767375 · Engine Starter
  > DURING TAXI OUT LH ENGINE STARTER, NO START. A/C RETURNED TO THE GATE AND MTX GROUNDED A/C. MTX REMOVED AND REPLACED LH STARTER IAW AMM 80-11-01. OPS CHECK GOOD.A/C REMAINS NO ETOPS. RETURNED A/C TO SERVICE
- [SDR ABXA20260907397](https://openairdocs.org/sdr/ABXA20260907397.md): Warning Message · illuminated · Sep 7, 2026 · N1709A · Boeing 767375 · Central Warning
  > PRE-DEPARTURE FOUND CARGO DET AIR MESSAGE SHOWING (FWD DET FAN ON ECS MSG), MTX DEFERRED FOR DEPARTURE IAW ABX MEL 26-16-1-3-1 MX ACTION C/W PLACARD INSTALLED A/C REMAINS ETOPS 180. AND RETURNED A/C TO SERVICE.
- [SDR UIEA2026072800658](https://openairdocs.org/sdr/UIEA2026072800658.md): Seal · broken · Jul 27, 2026 · N649GT · Boeing 767375 · Emergency Locator Beacon
  > GALLEY ELT TAMPER TAPE BROKEN. REMOVED AND REPLACED GALLEY ELT IAW AMM 25-63-03. OPS CHK OK.
- [SDR ABXA20260614256](https://openairdocs.org/sdr/ABXA20260614256.md): Tube · chafed · Jun 14, 2026 · N1709A · Boeing 767375 · Fire Bottle, Fixed
  > DURING MTC/INSP, NR 2 ENG FIRE EXTINGUISHING DISCHARGE TUBE FOUND CHAFED IN UPPER PYLON UNDER PANEL 611PT. INSTALLED NEW FIRE EXTINGUISHING TUBE FOR NR 2 ENG IN PYLON UNDER PANEL 611PT PER B767 AMM 20-11-00. ACFT REMAINS NO ETOPS. ACFT RETURNED TO SERVICE.
- [SDR UIEA2026060900455](https://openairdocs.org/sdr/UIEA2026060900455.md): Circuit Card · faulted · Jun 9, 2026 · N649GT · Boeing 767375 · Engine RPM Indicating System
  > RAT DEPLOYED RIGHT AFTER ROTATION ON TAKE-OFF. GREEN PRESSURE LIGHT ILLUMINATED(<P>REMOVED AND REPLACED LH ENG SPEED CARD & STOWED RAT PER AMM 73-21-54. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2026060300430](https://openairdocs.org/sdr/UIEA2026060300430.md): Oxygen Mask · inoperative · Jun 2, 2026 · N649GT · Boeing 767375 · Crew Oxygen System
  > CENTER SUPERNUMERARY SEAT O2 MASK INOPERATIVE. REMOVED AND REPLACED CENTER SUPERNUMERARY O2 MASK IAW AMM 35-11-51. OPS CHECK GOOD. NO LEAKS NOTED.
- [SDR UIEA2026060100424](https://openairdocs.org/sdr/UIEA2026060100424.md): Stowage Box · no test · May 30, 2026 · N649GT · Boeing 767375 · Crew Oxygen System
  > CAPTAIN SIDE O2 MASK AUDIO INTERCOM WILL NOT TEST. R & R CAPT SIDE O2 MASK STOWAGE IAW AMM 35-11-51 AND IPC 35-11-52-15. OPS CHECK GOOD. NO DEFECTS NOTED.
- [SDR UIEA2026052600364](https://openairdocs.org/sdr/UIEA2026052600364.md): Tag · broken · May 26, 2026 · N649GT · Boeing 767375 · Standard Practices/Structures
  > FLIGHT DECK ELT RH DO NOT REMOVE TAG BROKEN (PORTABLE ELT)(<P>REMOVED AND REPLACED FLIGHT DECK RH PORTABLE ELT IAW B767 AMM 25-63-03 & AIPC 25-63-52-97 AND EO 6725A129. NO FURTHER DEFECTS NOTED</P>)
- [SDR ABXA20260517208](https://openairdocs.org/sdr/ABXA20260517208.md): Generator · disengaged · May 17, 2026 · N1709A · Boeing 767375 · AC Generator-Alternator
  > RIGHT GEN OFF MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF BELOW 80KTS.TURNED OFF ONTO TAXI WAY CREW DEFERRED RH GEN. FOR DEPARUTRE,PER MEL 24-00-0-1.AND A/C TOOK OFF.
- [SDR UIEA2026051800341](https://openairdocs.org/sdr/UIEA2026051800341.md): Window · noisy · May 16, 2026 · N649GT · Boeing 767375 · Flight Compartment Windows
  > LOUD WHISTLING NOISES ON BOTTOM OF L1 WINDOW. PER CREW DEBRIEF, ACTUAL WINDOW IS L2 ( SLIDING WINDOW). CLEANED AND INSPECTED L2 WINDOW AERODYNAMIC ALONG WITH L1 WINDOW IAW AMM 12-16-02 AND 56-11-00 W/ NO DEFECTS NOTED. ALSO CLEANED AND INSPECTED L2 BULB SEAL
- [SDR ABXA20260515206](https://openairdocs.org/sdr/ABXA20260515206.md): Module · faulted · May 15, 2026 · N1709A · Boeing 767375 · Engine Bleed Air System
  > DURING TAXI, (L) PACK OFF CAUTION MSG. CREW RETURNED TO THE GATE (BTB). PERFORMED BITE TEST AND RESET OF BLEED SUPPLY MODULE FOR PER FIM 21-51 FT 844 NO FAULTS NOTED. PERFORMED ENG RUN PER AMM 71-00-00 ALL OPS CKS GOOD AT THIS TIME. AIRCRAFT REMAINS ETOPS 180.
- [SDR ABXA20260515205](https://openairdocs.org/sdr/ABXA20260515205.md): Module · faulted · May 15, 2026 · N1709A · Boeing 767375 · Engine Bleed Air System
  > DURING TAXI, (L) ENGINE BLEED OFF MSG. CREW RETURNED TO THE GATE (BTB). PERFORMED BITE TEST AND RESET OF BLEED SUPPLY MODULE PER FIM 36-10 FT 847 NO FAULT NOTED, PERFORMED ENG RUN PER AMM 71-00-00 ALL OPS CKS GOOD AT THIS TIME. AIRCRAFT REMAINS ETOPS 180. A/C
- [SDR UIEA2026040500127](https://openairdocs.org/sdr/UIEA2026040500127.md): Fan · vibration · Apr 5, 2026 · N649GT · Boeing 767375 · Turbine Engine Air Inlet Section
  > DURING CLIMB, RIGHT ENGINE FAN VIBRATION REACHED 4.3. DURING CRUISE, VIB 0.8. PERFORMED BLADE LUBE PER AMM 72-31-02. SPINNER RE-TORQUED PER AMM 72-31-01. TRIM BALANCE AND VIBRATION SURVEY PER AMM 72-31-00. #1 BEARING CHECKS GOOD. N2 VIBE AT POWER 2.0, FAN VI
- [SDR UIEA2026032700110](https://openairdocs.org/sdr/UIEA2026032700110.md): Handle · out of adjust · Mar 27, 2026 · N649GT · Boeing 767375 · Flight Compartment Windows
  > EMERGENCY WINDOW OUTSIDE HANDLE POPS OUT. ADJUSTED SPRING LOADED BALL LATCH OF WINDOW R2 EXTERIOR EMERGENCY ESCAPE HANDLE IAW AMM 56-11-04. OPS CHK GOOD AT THIS TIME.
- [SDR ABXA20260312094](https://openairdocs.org/sdr/ABXA20260312094.md): Warning Message · false activation · Mar 12, 2026 · N1709A · Boeing 767375 · Central Display
  > DURING TAXI, L ENG BLEED OFF EICAS MESSAGE APPEARED. A/C RETURNED TO BLOCKS (BTB). MAINTENANCE PERFORMED OPS TEST OF L ENG PRSOV IAW AMM 36-11-09. NO DEFECTS AT THIS TIME. A/C REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA20260306087](https://openairdocs.org/sdr/ABXA20260306087.md): Hydraulic System · low · Mar 6, 2026 · N1709A · Boeing 767375 · Hydraulic System, Main
  > BEFORE TAKEOFF CHECKLIST, NOTICED R HYD SYS RF@ 0.73 QRH FLOW COMPLETED MX CONTROL ADVISED TO BLACK BACK IN TO REFILL. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE TRANSFERRED AND LEVEL RIGHT HYD SYSTEM. RT SYSTEM INDICATING 1.03 AT THIS TIME. REF B767 AMM
- [SDR ABXA20260301080](https://openairdocs.org/sdr/ABXA20260301080.md): Door · defective · Mar 1, 2026 · N1709A · Boeing 767375 · Landing Gear Door Retract Section
  > AT 3000 AGL DURING THE AFTER-TAKEOFF CHECKLIST, THE GEAR LEVER WAS MOVED TO THE OFF POSITION, DURING WHICH THE RT MLG EXTENDED, & GEAR DISAGREE LIGHT ILLUMINATED GEAR EXTENDED NORMALLY WILL PLACE GEAR ON MEL 32-30-1.MTX DEFERRED LANDING GEAR RETRACTION SYSTEM
- [SDR ABXA20260216068](https://openairdocs.org/sdr/ABXA20260216068.md): Transducer · damaged · Feb 16, 2026 · N1709A · Boeing 767375 · Landing Gear Brake System
  > ON DEPARTURE, BRAKE TEMP DISCRETE LIGHT ILLUMINATED. FOLLOWED QRH PROCEDURE. RESUMED NORMAL OPERATION. UPON LANDING, FOUND #7 TIRE FLAT. #7 WHEEL SPEED TRANSDUCER DAMAGED. AXLE UNDER #7 TIRE/BRAKE SHOWS SIGNS OF SCORING AND DISCOLORATION. MAINTENANCE REPL
- [SDR ABXA20260214067](https://openairdocs.org/sdr/ABXA20260214067.md): Spoiler · damaged · Feb 14, 2026 · N1709A · Boeing 767375 · Spoilers
  > DURING DESCENT, USED SPEEDBRAKES AND HAD A SYMETRICAL DEPLOYMENT CAUSING ACFT TO TURN RIGHT. RESET SPEEDBRAKES AND TRIED AGAIN, IT HAPPENED AGAIN. LANDING WAS UNEVENTFUL. AFTER FLT CONTROL INSPECTION FOUND #3 SPOILER DAMAGED. REMOVED AND REPLACED #3 SPOILER
- [SDR UIEA2025111801297](https://openairdocs.org/sdr/UIEA2025111801297.md): Lanyard · unsecure · Nov 16, 2025 · N649GT · Boeing 767375 · Emergency Locator Beacon
  > ELT BY LAVATORY HAS STRING HANGING. SECURED THE ELT STRING IAW AMM 25-63-03. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.
- [SDR ABXA20251111297](https://openairdocs.org/sdr/ABXA20251111297.md): Unknown · vibration · Nov 11, 2025 · N1709A · Boeing 767375 · Main Landing Gear
  > ON TAXI OUT, RIGHT GEAR SHAKING. ABORTED TAKE-OFF. (ATO). PERFORMED AIRCRAFT TAXI WITH FLIGHT CREW ASSISTANCE. NO ABNORMAL VIBRATIONS NOTED PER AMM 71-00-00 AND 09-21-00. A/C OK FOR SERVICE.
- [SDR UIEA2025102401278](https://openairdocs.org/sdr/UIEA2025102401278.md): Skin · damaged · Oct 24, 2025 · N649GT · Boeing 767375 · Nacelle/Pylon, Plate/Skin
  > AIRCRAFT STRUCK BY LIGHTNING. LIGHTNING STRIKE DAMAGE FOUND ON R/H INLET COWL 3:00 POSITION(<P>PERFORMED PHASE 1 LIGHTNING STRIKE INSPECTION IAW B767 AMM 05-51. R/H ENGINE COWL DAMAGE FOUND WITHIN LIMITS IAW SRM 54-15-01-1A-1. NO FURTHER DEFECTS NOTED</P>)
- [SDR ABXA20251107290](https://openairdocs.org/sdr/ABXA20251107290.md): Link · damaged · Oct 7, 2025 · N1709A · Boeing 767375 · Main Landing Gear Attach Section
  > DURING TAXI, AIRCRAFT VIOLENTLY SHAKING FROM RT MAIN LANDING GEAR STRUT. A/C RETURNED TO BLOCKS. (BTB). T/S LED TO RMLG UPPER AND LOWER TORSION LINKS. REMOVED OLD, THEN INSTALLED NEW LOWER AND UPPER R MLG TORSION LINKS PER AMM 32-11-22, REF LP 39269-53/3.
- [SDR UIEA2025100401256](https://openairdocs.org/sdr/UIEA2025100401256.md): Hf Comm · abnormal · Oct 4, 2025 · N649GT · Boeing 767375 · HF Communications System
  > BOTH HF COMM RADIO INOP AND SELCAL INOP(<P>T/S WITH FIM 23-11 FT 804. RESECURED CONNECTIONS AT HF ANTENNA. OPS CHK GOOD PER AMM 23-11-00</P>)
- [SDR UIEA2025092601246](https://openairdocs.org/sdr/UIEA2025092601246.md): Cover · detached · Sep 26, 2025 · N649GT · Boeing 767375 · Emergency Lighting
  > EMERGENCY EXIT LIGHT COVER FELL OFF L1 DOOR. INSTALLED EMERGENCY EXIT LIGHT COVER IAW AMM 33-51-03. NO FURTHER DEFECTS NOTED.
- [SDR ABXA20250905213](https://openairdocs.org/sdr/ABXA20250905213.md): Sequence Valve · inoperative · Sep 5, 2025 · N1709A · Boeing 767375 · Landing Gear Door Retract Section
  > GEAR DOOR S EICAS MESSAGE AFTER TAKEOFF,WHEN GEAR LEVER WAS MOVE FROM UP TO OFF. LIGHT WENT BLUE AFTER ACCOMPLISH (GEAR DISSAGREE) QRH NNC.14.17. FINISHED FLIGHT AND LANDED WITH NO OTHER COMPLICATIONS.MTX GROUNDED A/C. PERFORMED ADJUST OF RT MLG UPLOCK REL
- [SDR UIEA2025071400949](https://openairdocs.org/sdr/UIEA2025071400949.md): Bracket · damaged · Jul 14, 2025 · N649GT · Boeing 767375 · Fuselage Main, Attach Fittings
  > FLIGHT DECK FIRE EXTINGUISHER HOLDING BRACKET INOPERATIVE. RE-ADJUSTED FLIGHT DECK FIRE EXTINGUISHING BRACKET IAW B767 AMM 26-26-02. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR ABXA20250619132](https://openairdocs.org/sdr/ABXA20250619132.md): Panel · departed · Jun 19, 2025 · N1709A · Boeing 767375 · Aerodynamic Fairings
  > ON MAINTENANCE POST FLIGHT INSP, FOUND ON RT WING TO FUSELAGE PANEL MISSING 196CR. MAINTENANCE INSTALLED RT WING TO FUSELAGE PANEL 196CR IAW AMM 20-11-00. AIRCRAFT RETURNED TO SERVICE.
- [SDR UIEA2025062100789](https://openairdocs.org/sdr/UIEA2025062100789.md): Latch · out of adjust · Jun 19, 2025 · N649GT · Boeing 767375 · Fuselage Main, Structure
  > ON LANDING, FO WINDOW NR 2 EXTERNAL EMERGENCY ESCAPE HANDLE UNLATCHING. ADJUSTED FO WINDOW #2 EMERGENCY ESCAPE HANDLE LATCH & PERFORMED SYSTEM OPS CHECK OF EXTERNAL ESCAPE HANDLE IAW AMM 56-11-04. OPS CHECK GOOD AT THIS TIME. NO OTHER DEFECTS NOTED.
- [SDR UIEA2025052900705](https://openairdocs.org/sdr/UIEA2025052900705.md): Skin · cracked · Jun 7, 2025 · N649GT · Boeing 767375 · Fuselage Main, Plate/Skin
  > SERVICE DOOR CUTOUT, AFT LOWER CORNER FUSELAGE FOUND CRACKS INDICATION, ON OPEN HOLES: #4, POSITION 8 O'CLOCK (SKIN AND BEAR STRAP) APPROX AND HOLE #5, POSITION 8 O'CLOCK (SKIN) AND 2 O'CLOCK (BEAR STRAP) APPROX.(<P>CRACKS WERE REPAIRED PER SRM 53-10-01-2R-1 R
- [SDR UIEA2025052900706](https://openairdocs.org/sdr/UIEA2025052900706.md): Bear Strap · cracked · Jun 7, 2025 · N649GT · Boeing 767375 · Fuselage Main, Plate/Skin
  > FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER WITH TWO CRACK INDICATIONS AT HOLE #5: 1. ON SKIN AT 3 OÂ´CLOCK POSITION. 2. ON BEAR STRAP AT 9 OÂ´CLOCK POSITION.(<P>CRACKS WERE REPAIRED PER SRM 53-10-01-2R-1 FIGURE 201 DETAIL III. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025060300722](https://openairdocs.org/sdr/UIEA2025060300722.md): Skin · dented · Jun 7, 2025 · N649GT · Boeing 767375 · Spoilers
  > LH WING, SPOILER #3, LOWER SURFACE, DENT AT 10.5" FROM AFT EDGE AND 6" FROM OUTBD EDGE.(<P>AFFECTED AREA WAS REPAIRED IN ACCORDANCE WITH B767 SRM 57-70-01-2R-1 PAG 2-5 FIG 201 SHEET 4 AND SRM 51-70-03-0G-0 PAR 5. L FIG 16. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025060300723](https://openairdocs.org/sdr/UIEA2025060300723.md): Wedge · damaged · Jun 7, 2025 · N649GT · Boeing 767375 · Leading Edge Devices
  > LH WING, SLAT# 1, UPPER SIDE, WEDGE WITH HAIL DAMAGE.(<P>LH WING, SLAT# 1, TRAILING WEDGE, UPPER SURFACE WITH DENTS (9 EAS) WERE EVALUATED AND FOUR DENTS WERE REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 SHEET 2 PAG.2-3 AND SRM 51-70-10-2R-4 PAG.1,3,7 FIG-.201 SHEE
- [SDR UIEA2025060300724](https://openairdocs.org/sdr/UIEA2025060300724.md): Bushing · corroded · Jun 7, 2025 · N649GT · Boeing 767375 · Engine Mount Section
  > FRETTING CORROSION ON BUSHING P/N BACB28X20E085 INSTALLED IN THE FWD SHEAR PIN HOLE OF THE FWD ENGINE MOUNT (P/N 311T2211-7), RH SIDE.(<P>BUSHING WAS REPLACED (P/N BACB28X20E085) PER DWG 311T2211-7 ID SHEET 1. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025060300725](https://openairdocs.org/sdr/UIEA2025060300725.md): Fuel Tank · leaking · Jun 7, 2025 · N649GT · Boeing 767375 · Fuel Storage
  > FUEL LEAK AT CENTER TANK BETWEEN STGR L-6 AND LBL 97.5.(<P>THE SEALANT IN THE FUEL TANK STRUCTURE WAS REPAIRED PER AMM 28-11-00-308-013. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025060300726](https://openairdocs.org/sdr/UIEA2025060300726.md): Wedge · damaged · Jun 7, 2025 · N649GT · Boeing 767375 · Leading Edge Devices
  > LH WING, SLAT# 4, UPPER SIDE, WEDGE WITH HAIL DAMAGE.(<P>LH WING, SLAT# 4, TRAILING WEDGE, UPPER SURFACE WITH DENTS (11 EAS) WERE EVALUATED AND FOUR DENTS WERE REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 SHEET 2 PAG.2-3 AND SRM 51-70-10-2R-4 PAG.1,3,7 FIG.201 SHEET
- [SDR UIEA2025060300728](https://openairdocs.org/sdr/UIEA2025060300728.md): Wedge · damaged · Jun 7, 2025 · N649GT · Boeing 767375 · Leading Edge Devices
  > LH WING, SLAT# 3, UPPER SIDE, WEDGE WITH HAIL DAMAGE.(<P>LH WING, SLAT# 3, TRAILING WEDGE, UPPER SURFACE WITH DENTS (7 EAS) WERE EVALUATED AND TWO DENTS WERE REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 SHEET 2 PAG.2-3 AND SRM 51-70-10-2R-4 PAG.1,3,7 FIG-.201 SHEET
- [SDR UIEA2025060700735](https://openairdocs.org/sdr/UIEA2025060700735.md): Skin · corroded · Jun 7, 2025 · N649GT · Boeing 767375 · Horizontal Stabilizer, Plate/Skin
  > RH OUTBD HORIZONTAL STABILIZER, UPPER SURFACE, AT REAR SPAR WITH CORROSION.(<P>RH OUTBD HORIZONTAL STABILIZER, UPPER SURFACE, AT REAR SPAR WITH CORROSION LEVEL 2 WAS REPAIRED IAW CMA-TLS-25-0045. NO FURTHER DEFECTS NOTED.</P>)

Next page: https://openairdocs.org/model/boeing-767-375/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 = '767375'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-767-375/reports

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