# Service difficulty reports: N881YV, cancelled Aug 22, 2026

A list on [N881YV, cancelled Aug 22, 2026](https://openairdocs.org/deregistered/N881YV-2026-08-22.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [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 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 21GA20240513013](https://openairdocs.org/sdr/21GA20240513013.md): Skin · corroded · May 13, 2024 · N881YV · Boeing 767231 · Wing, Plate/Skin
  > CORROSION FOUND ON LH WING UPPER SKIN BETWEEN STR U-2 AND U-4 AND SPLICE AND BODY STATION 97.42.
- [SDR 21GA20240513012](https://openairdocs.org/sdr/21GA20240513012.md): Skin · corroded · May 13, 2024 · N881YV · Boeing 767231 · Wing, Plate/Skin
  > CORROSION BEYOND LIMITS FOUND ON RH WING LOWER SKIN BETWEEN WS 1045.0 & WS 1070.59 AND THE REAR SPAR.
- [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 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 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 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

## 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 = 'N881YV' AND deregistration_id = 'N881YV-2026-08-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N881YV-2026-08-22/reports

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