# Service difficulty reports: Boeing 767-241

A list on [Boeing 767-241](https://openairdocs.org/model/boeing-767-241.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 165 reports

- [SDR 21GA202605260000](https://openairdocs.org/sdr/21GA202605260000.md): Skin · delaminated · May 26, 2026 · N999YV · Boeing 767241 · Vertical Stabilizer, Plate/Skin
  > DELAMINATION LOCATED ON LEFT SIDE OF VERTICAL STABILIZER PANEL BETWEEN SPAR AND FRONT SPAR FSS 220.521 - 270-784 (MAJOR REPAIR)
- [SDR 21GA2026052623801](https://openairdocs.org/sdr/21GA2026052623801.md): Seat Track · corroded · May 26, 2026 · N999YV · Boeing 767241 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON SEAT TRACK AT STATION 1125 MAIN DECK AT LBL 11 AND RBL 11 (MAJOR REPAIR)
- [SDR 21GA2026052623806](https://openairdocs.org/sdr/21GA2026052623806.md): Window Frame · cracked · May 26, 2026 · N999YV · Boeing 767241 · Fuselage Main, Structure
  > WINDOW FRAME AT STATION 944 LH SIDE IS CORRODED AT CENTER OF LOWER EDGE. (MAJOR REPAIR)
- [SDR 21GA2026052623805](https://openairdocs.org/sdr/21GA2026052623805.md): Frame · cracked · May 26, 2026 · N999YV · Boeing 767241 · Fuselage Main, Frame
  > CRACK FOUND IN CENTER WING REAR SPAR AT STATION 953 BBL 1R
- [SDR 21GA2026052623803](https://openairdocs.org/sdr/21GA2026052623803.md): Skin · corroded · May 26, 2026 · N999YV · Boeing 767241 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON UPPER SURFACE OF CENTER SECTION AT BS 955.1 AT BL 0 (MAJOR REPAIR)
- [SDR 21GA2026052623802](https://openairdocs.org/sdr/21GA2026052623802.md): Skin · corroded · May 26, 2026 · N999YV · Boeing 767241 · Wing, Plate/Skin
  > CORROSION ON LOWER RH WING AT WS 314.30 - 372.20 STR 16-18
- [SDR 21GA20250724016](https://openairdocs.org/sdr/21GA20250724016.md): Power Supply · faulted · Jul 24, 2025 · N999YV · Boeing 767241 · Flight Control System
  > AT FL 390 BEGAN TO EXPERIENCE DUTCH ROLLS WITH AUTO PILOT AND AUTO THROTTLES ENGAGED.DISCONNECTD AP BUT HAD TO HOLD THE YOKE TO THE RIGHT TO MAINTAIN CONTROL. DELCARED EMERGENCY AND DIVERTED TO ST. LOUIS. MAINTENANCE PERSONNEL REPLACED RIGHT CSEU POWER SUPPLY.
- [SDR 21GA20250324003](https://openairdocs.org/sdr/21GA20250324003.md): Valve · faulted · Mar 22, 2025 · N999YV · Boeing 767241 · Air Distribution System
  > DURING CRUSIE RECEIVED FWD EQUIPMENT COOLING OVHT MESSAGE. DIVERTED TO OMAHA. REPLACED RH ENG PRVC.
- [SDR 21GA202503242002](https://openairdocs.org/sdr/21GA202503242002.md): Warning Message · false activation · Mar 22, 2025 · N999YV · Boeing 767241 · Central Warning
  > DURING CRUISE AT FL 370, RECEIVED EICAS MESSAGE "EQUIPMENT OVERHEAT" MESSAGE. DECENDED TO FL 310. DURING THIS DECENT, RECEIVED "CABIN ALT" MESSAGE. DECLARED EMERGENCY AND DIVERTED. MAINTENANACE PERSONNEL PLACED THE EQUIPMENT COOLING SYSTEM ON MEL AND ACCOMPLIS
- [SDR 21GA202412223021](https://openairdocs.org/sdr/21GA202412223021.md): Engine · surges · Dec 22, 2024 · N881YV · Boeing 767241 · Engine (Turbine/Turboprop)
  > RIGHT ENGINE SURGING. IT STOPPED WHEN THROTTLES REDUCED. THERE WERE NO EXCEEDENCES. ENGINE OPERATON BECAME NORMAL AGAIN. PERFORMED BORESCOPE INSPECTION. NO DEFECTS NOTED.
- [SDR 21GA20241001019](https://openairdocs.org/sdr/21GA20241001019.md): Skin · cracked · Oct 1, 2024 · N999YV · Boeing 767241 · Fuselage Main, Plate/Skin
  > DURING HEAVY CHECK, FOUND CRACKED SKIN CRACKED 1 INCH FWD AND 2.5 INCHES AFT OF IAI PG STRAP. REPAIRED IAW FLIGHT VEHICLES CONSULTING, INC EO #24151-3.
- [SDR 21GA20241001018](https://openairdocs.org/sdr/21GA20241001018.md): Skin · dented · Oct 1, 2024 · N999YV · Boeing 767241 · Fuselage Main, Plate/Skin
  > DURING HEAVY CHECK, A DENT AND CREASE WERE FOUND AT FUSELAGE SKIN STA 1279.53 BETWEEN STR 33R AND 35R. WAS REPAIRED IAW FLIGHT VEHICLES CONSULTING, INC. EO # 24151-2.
- [SDR 21GA20241001017](https://openairdocs.org/sdr/21GA20241001017.md): Skin · dented · Oct 1, 2024 · N999YV · Boeing 767241 · Fuselage Main, Plate/Skin
  > DURING HEAVY CHECK, DENTS AND CRACKS WERE FOUND BETWEEN FUSELAGE SKIN STA 347 AND 390 AT STR 19R TO 21R. WAS REPAIRED IAW FLIGT VEHICLES CONSULTING INC. EO# 24151-1.
- [SDR 21GA20240917016](https://openairdocs.org/sdr/21GA20240917016.md): Module · faulted · Sep 17, 2024 · N881YV · Boeing 767241 · Trailing Edge Flap Control System
  > ON APPROACH TO CVG SELECTED FLAPS AND GOT TRAINING EDGE FLAP DISAGREEE MESSAGE. LANDED WITH FLAPS AT 20 DEGREES.
- [SDR 21GA20240118001](https://openairdocs.org/sdr/21GA20240118001.md): Flt Controls · abnormal · Jan 17, 2024 · N881Y · Boeing 767241 · Flight Control System
  > AFTER TAKEOFF PASSING 5,000 FT, EXTREMELY LOUD BANGING NOISE ON RH SIDE OF AIRCRAFT. AIIRCRAFT WAS YAWING BACK AND FORTH. FLIGHT CONTROLS FELT LOOSE. DISCONNECTED AUTOPILOT AND RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE PERSONNEL INSPECTED THE AIRCRAFT WI
- [SDR 21GA20230228005](https://openairdocs.org/sdr/21GA20230228005.md): Skin · cracked · Feb 28, 2023 · N999YV · Boeing 767241 · Fuselage Structure (General)
  > DURING MAINTENANCE FOUND CRACK ON SKIN AT RH FUSELAGE FWD UPPER FASTENER AT STA. 1809 AT STR 12A.
- [SDR 21GA20230218003](https://openairdocs.org/sdr/21GA20230218003.md): Skin · corroded · Feb 18, 2023 · N999YV · Boeing 767241 · Horizontal Stabilizer Structure
  > CORROSION FOUND ON HORIZONTAL STABILIZER CENTER SECT. UPPER SKIN AT REAR SPAR BETWEEN BL 0.0 & RBL 10.0.
- [SDR 21GA20230202004](https://openairdocs.org/sdr/21GA20230202004.md): Skin · corroded · Feb 2, 2023 · N999YV · Boeing 767241 · Fuselage Structure (General)
  > CORROSION FOUND ON FUSELAGE SKIN SECTION 46 AT STA 1197 BETWEEN STR 39R AND STR 36L.
- [SDR 21GA20230125002](https://openairdocs.org/sdr/21GA20230125002.md): Keelbeam · corroded · Jan 25, 2023 · N999YV · Boeing 767241 · Fuselage Structure (General)
  > CORROSION FOUND ON LH KEEL BEAM LOWER CHORD BETWEEN STA 959 & 969.5 BETWEEN STA 1000 & 1017.5 LBL 9.5.
- [SDR 21GA202302150001](https://openairdocs.org/sdr/21GA202302150001.md): Skin · corroded · Jan 25, 2023 · N999YV · Boeing 767241 · Fuselage Structure (General)
  > CORROSION FOUND ON FUSELAGE SKIN SECTION 46 BETWEEN STA. 1072.75 & 1109 BETWEEN STR. 36L & 36R.
- [SDR 21GA20221003004](https://openairdocs.org/sdr/21GA20221003004.md): Keelbeam · corroded · Sep 29, 2022 · N999YV · Boeing 767241 · Fuselage Main, Keel
  > CORROSION FOUND ON FUSELAGE SECTION 43 KEEL BEAM AROUND F.S. 740 AT LBL 9.5.
- [SDR 21GA20220919003](https://openairdocs.org/sdr/21GA20220919003.md): Skin · corroded · Sep 13, 2022 · N881YV · Boeing 767241 · Horizontal Stabilizer, Plate/Skin
  > CORROSION FOUND ON RH INBOARD STABILIZER UPPER SKIN AT FRONT SPAR.
- [SDR 21GA20220919002](https://openairdocs.org/sdr/21GA20220919002.md): Skin · cracked · Aug 30, 2022 · N881YV · Boeing 767241 · Fuselage Main, Plate/Skin
  > CRACK FOUND ON RH SIDE OF LOWER FUSELAGE AT STA. 660.
- [SDR 21GA20220416001](https://openairdocs.org/sdr/21GA20220416001.md): None · none · Apr 16, 2022 · N999YV · Boeing 767241 · Cabin Pressure Control System
  > DURING CRUISE, CABIN ALTITUDE AUTO 2 STATUS MESSAGE. ZERO DUCT PRESSURE FROM ENGINE OR APU BLEEDS. PERFORMED EMERGENCY DECENT DUE TO LOSS OF CABIN PRESSURE. MAINTENANCE PERSONNEL PERFORMED A CABIN PRESSURE CONTROL SYSTEM TEST PER AMM. NO FAULTS NOTED. PERFORME
- [SDR 21GA20211119001](https://openairdocs.org/sdr/21GA20211119001.md): Cooling Duct · ruptured · Nov 19, 2021 · N881YV · Boeing 767241 · Pneumatic Distribution System
  > LEFT ENGINE FIRE MASTER WARNING MESSAGE AT FLIGHT LEVEL 260. SHUTDOWN LEFT ENGINE AND RETURNED TO AIRPORT. FOUND LEFT ENGINE LOW PRESSURE TURBINE CASE COOLING DUCT RUPTURED. REPLACED DUCT.
- [SDR 21GA20210401001](https://openairdocs.org/sdr/21GA20210401001.md): Skin · corroded · Apr 1, 2021 · N881YV · Boeing 767241 · Fuselage Main, Plate/Skin
  > CENTER WING-UPPER PLATING BETWEEN LBL 54 - LBL 43 AROUND REPAIR SPAR, CORROSION DAMAGE REPAIR.
- [SDR 21GA20210401004](https://openairdocs.org/sdr/21GA20210401004.md): Skin · corroded · Mar 31, 2021 · N881YV · Boeing 767241 · Wing, Plate/Skin
  > LEFT WING, TRAILING EDGE STRUCTURE AT UPPER FORWARD SECTION BETWEEN WBL 296 TO 283, CORROSION DAMAGE REPAIR.
- [SDR 21GA20210401003](https://openairdocs.org/sdr/21GA20210401003.md): Skin · corroded · Mar 31, 2021 · N881YV · Boeing 767241 · Wing, Plate/Skin
  > LEFT WING - UPPER PLATING BETWEEN WBL 190 TO 198 AROUND REAR SPAR, CORROSION DAMAGE REPAIR.
- [SDR 21GA20210401002](https://openairdocs.org/sdr/21GA20210401002.md): Skin · corroded · Mar 25, 2021 · N881YV · Boeing 767241 · Fuselage Main, Plate/Skin
  > CENTER WING - UPPER PLATTING BETWEEN LBL 7-LBL 9.5 AROUND REAR SPAR, CORROSION DAMAGE REPAIR.
- [SDR 21GA20191107008](https://openairdocs.org/sdr/21GA20191107008.md): Skin · cracked · Nov 5, 2019 · N999YV · Boeing 767241 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE SKIN SECTION 43 SKIN CRACKED AT STRINGER 38R AT BS786.
- [SDR 21GA20191107007](https://openairdocs.org/sdr/21GA20191107007.md): Skin · corroded · Nov 5, 2019 · N999YV · Boeing 767241 · Horizontal Stabilizer, Plate/Skin
  > MULTIPLE AREAS OF SCATTERED SURFACE CORROSION ON FASTENER HEADS ON THE UPPER SURFACE OF THE HORIZONTAL STABILIZER RH BETWEEN THE REAR SPAR AND TRAILING EDGE AT STATION 224.
- [SDR 21GA20191107006](https://openairdocs.org/sdr/21GA20191107006.md): Skin · corroded · Nov 5, 2019 · N999YV · Boeing 767241 · Wing, Plate/Skin
  > LH WING LOWER SURFACE AT WING STATION 1075 HAS A BLOWOUT (CORROSION) WHERE MARKED AT REAR SPAR.
- [SDR 21GA20191107005](https://openairdocs.org/sdr/21GA20191107005.md): Skin · corroded · Nov 5, 2019 · N999YV · Boeing 767241 · Wing, Plate/Skin
  > LH WING LOWER SURFACE AT WING STATION 715 HAS A BLOWOUT (CORROSION) WHERE MARKED AT REAR SPAR.
- [SDR 21GA20191107004](https://openairdocs.org/sdr/21GA20191107004.md): Structure · corroded · Nov 5, 2019 · N999YV · Boeing 767241 · Fuel Storage
  > RH UPPER CENTER TANK SKIN HAS CORROSION AT RBL 71 OF REAR SPAR.
- [SDR 21GA20191107003](https://openairdocs.org/sdr/21GA20191107003.md): Skin · cracked · Nov 5, 2019 · N999YV · Boeing 767241 · Fuselage Main, Plate/Skin
  > RH R1 DOOR CUTOUT AFT LOWER CORNER SKIN CRACKED 4” LONG AT STATION 347 BETWEEN STRINGERS 19 & 20 R.
- [SDR 21GA201702110001](https://openairdocs.org/sdr/21GA201702110001.md): Engine · fluctuates · Feb 9, 2017 · N999YV · Boeing 767241 · Engine (Turbine/Turboprop)
  > DURING CRUISE AT FLT LEVEL 390 LEFT ENGINE FLUCTUATED ERRATICALLY 400 DEGREES, OTHER PARAMETERS NORMAL
- [SDR 2D7A201612300001](https://openairdocs.org/sdr/2D7A201612300001.md): Battery Pack · discharged · Dec 30, 2016 · N999YV · Boeing 767241 · Emergency Lighting
  > DURING MAINTENANCE CHECK, THE EXIT SIGNS WOULD NOT ILLUMINATE. FOUND THE BATTERY PACK DISCHARGED.
- [SDR 2DYA20151109018](https://openairdocs.org/sdr/2DYA20151109018.md): Door · worn · Nov 7, 2015 · N999YV · Boeing 767241 · Electrical/Electronic Compartment Doors
  > DURING CRUISE, RECEIVED A E & E BAY DOOR EICAS MSG & DECIDED TO RETURN. NO EMER WAS DECLARED & RETURNED & LANDED SAFELY WITH NO FURTHER INCIDENT. PREVIOUS DMI 999-15-0090 WAS RE-OPENED MEL 52-71-01-01, E & E DOOR MUST BE VERIFIED CLOSED & LATCHED PRIOR TO EA
- [SDR 2DYA20151101017](https://openairdocs.org/sdr/2DYA20151101017.md): Sensor · out of adjust · Nov 1, 2015 · N881YV · Boeing 767241 · Leading Edge Slat Position Indicating System
  > AFTER TAKEOFF, CREW NOTICED DURING FLAP RETRACTION, LE SLAT DISAGREE & LE SLAT ASYMMETRICAL STATUS MESSAGE, LE SLAT SHUTDOWN AIR & GROUND DISAGREE, AFTER GEAR RETRACTION. AUTO BRAKES INOPERATIVE. CREW MADE DETERMINATION TO RETURN, DUE TO PREVIOUS DIVERT FOR
- [SDR 2DYA20151101016](https://openairdocs.org/sdr/2DYA20151101016.md): Sensor · dirty · Nov 1, 2015 · N881YV · Boeing 767241 · Leading Edge Slat Position Indicating System
  > AFTER TAKEOFF, CREW NOTICED DURING FLAP RETRACTION LE RETRACTION, LE SLAT ASYMMETRY AIR & GND DISAGREE, AFTER GEAR RETRACTION. AFTER FOLLOWING QRM PROCEDURES, CREW MADE DETERMINATION TO DIVERT. LANDED SAFELY WITH NO FURTHER INCIDENT. FOUND SENSORS VERY DIRT
- [SDR 2DYA20151009013](https://openairdocs.org/sdr/2DYA20151009013.md): Light · inoperative · Oct 8, 2015 · N881YV · Boeing 767241 · Emergency Lighting
  > DURING C CHECK INSPECTION, INSPECTORS FOUND FLIGHT DECK EMER EXIT LIGHT INOPERATIVE. R & R EXIT LIGHT ASSEMBLY IAW MM 33-51-001. OPERATIONAL CHECKED NORMAL IAW MM 33-51-00 202.
- [SDR 2DYA20150526008](https://openairdocs.org/sdr/2DYA20150526008.md): Light · inoperative · Jul 8, 2015 · N881YV · Boeing 767241 · Emergency Lighting
  > DURING A3 CHECK, INSPECTION FOUND COCKPIT DOOR EMER LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM 33-51-01. OPERATIONAL TESTED NORMAL.
- [SDR 2DYA20150526006](https://openairdocs.org/sdr/2DYA20150526006.md): Terminal · broken · May 22, 2015 · N881YV · Boeing 767241 · Fire Detection
  > AIRCRAFT ARRIVED WITH NO INBD WRITE-UPS. WHILE MX WAS DOING THE ENG START CHECKLIST TO START TROUBLESHOOTING THE LT ENG PRSOV MEL, IT WAS FOUND THAT THE LT ENG FIRE DETECT SYS WOULD NOT TEST & ONLY NR 2 OVHT LOOP WOULD TEST. AFTER OPENING THE LT ENG COWLINGS
- [SDR 2DYA2015051300004](https://openairdocs.org/sdr/2DYA2015051300004.md): Radio · failed · May 10, 2015 · N999YV · Boeing 767241 · VHF Communications System
  > DURING CRUISE JUST PRIOR TO DESCENT, THE CREW NOTICED THE CENTER VHF COMM WENT BLANK & WAS FOLLOWED BY A STRONG ELEC ODOR & SMOKE. COMPLETED NORMAL APPROACH & LANDED WITHOUT INCIDENT. SMOKE & FUMES IN COCKPIT INSPECTION WAS ACCOMPLISHED. AFTER TROUBLESHOOTI
- [SDR 2DYA20150602007](https://openairdocs.org/sdr/2DYA20150602007.md): Turbine Blades · damaged · May 6, 2015 · N881YV · Boeing 767241 · Turbine Section
  > CLIMBING THROUGH 4000' CREW HAD HIGH ENG VIBRATION WITH EGT GOING INTO YELLOW ARC ON LT ENG. ENG PULLED BACK TO IDLE THRUST & STILL HAD VIBRATION. ENG SHUTDOWN & RETURNED. VISUAL DAMAGE TO TURBINE BLADES. UPON INSPECTION, BORESCOPE, IT WAS DETERMINED THAT
- [SDR 2DYA20141030002](https://openairdocs.org/sdr/2DYA20141030002.md): Unknown · malfunctioned · Oct 21, 2014 · N999YV · Boeing 767241 · Cabin Pressure Control System
  > CABIN ALTITUDE CONTINUE TO CLIMB ABOVE 10,000 AT LEVEL FLIGHT 40,000. ACFT RETURNED FOR TROUBLESHOOTING. PERFORMED PRESSURIZATION TEST IAW AMM 21-31-00, TESTED GOOD. ACFT DEPARTED AT A LATER DATE WITHOUT EVENT.
- [SDR 2DYA20140518002](https://openairdocs.org/sdr/2DYA20140518002.md): Proximity Switch · faulty · May 16, 2014 · N768QT · Boeing 767241 · Leading Edge Slat Position Indicating System
  > AFTER FLAP RETRACTION, FLAP NEEDLES JUMPED BETWEEN 0 & 1. EICAS MSG LE SLAT ASYMMETRICAL & LE ANNUNCIATOR ILLUMINATED. DURING PSEU BITE IAW BFIM 32-09-03, FOUND PROXIMITY SWITCH 282 FAULTY. R & R PROXIMITY SWITCH IAW AMM 27-88-01. CHECKED CLEARANCE BETWEEN
- [SDR 2DYA20140518001](https://openairdocs.org/sdr/2DYA20140518001.md): Warning System · false activation · May 16, 2014 · N768QT · Boeing 767241 · Leading Edge Slat Position Indicating System
  > FLAP & SLAT RETRACTION FROM F1 TO 0 SETTING EICAS MSG LE SLAT ASYMMETRICAL. TROUBLESHOOTING IAW BFIM 27-81 FAULT TREE 808 REVEALED NO FAULTS.
- [SDR TAMF2012FA0000003](https://openairdocs.org/sdr/TAMF2012FA0000003.md): Tire · damaged · Dec 25, 2012 · N770QT · Boeing 767241 · Tire
  > DURING DAILY CHECK, FOUND MAIN TIRE NR 7 DAMAGED, TREAD LOOSE OF THE TIRE. R & R NR 7 TIRE AND WHEEL ASSY IAW AMM 32-45-01, PAGE 401-413. TIRE PRESSURE NORMAL.
- [SDR 2012F00107](https://openairdocs.org/sdr/2012F00107.md): Engine · making metal · Jun 12, 2012 · N769QT · Boeing 767241 · Engine (Turbine/Turboprop)
  > EICAS MESSAGE FOR RT OIL FILTER. DISPLAY REMAINED WHEN THRUST REDUCED. RT ENGINE SHUTDOWN. ENGINE VIBRATION DURING CLIMB. DURING INSPECTION FOUND DEBRI IN ALL MAGNETIC CHIP DETECTORS. ENGINE REPLACED.

Next page: https://openairdocs.org/model/boeing-767-241/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 = '767241'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-767-241/reports

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