# Service difficulty reports: N922UW, cancelled Aug 22, 2011

A list on [N922UW, cancelled Aug 22, 2011](https://openairdocs.org/deregistered/N922UW-2011-08-22.md).

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

- [SDR USAA20090206BB030](https://openairdocs.org/sdr/USAA20090206BB030.md): Light · inoperative · Feb 5, 2009 · N922UW · Boeing 757225 · Escape Slide
  > CLT - THE GIRT BAR ENGAGEMENT LIGHT WAS EXTINGUISHED WITH THE EVACUATION SLIDE ARMED LEVER IN THE ARMED POSITION AT ENTRY DOOR L2. MAINTENANCE RELAMPED THE SLIDE LIGHT CAPSULE AND CLEANED THE GIRT BAR SLIDERS AT THE L2 DOOR. OPERATIONALLY CHECKS OK.
- [SDR USAA920081251](https://openairdocs.org/sdr/USAA920081251.md): Angle · corroded · Jun 21, 2008 · N922UW · Boeing 7572B7 · Passenger/Crew Doors
  > CLT - RON - MAJOR REPAIR - CORROSION FOUND ON ANGLE IN BOTTOM OF R2 DOOR AT BS 710. REPAIRED CORROSION FOUND ON ANGLE IN BOTTOM OF R2 DOOR AT BS 710 IAW BOEING B757 DRAWING 143N6100. (S)
- [SDR USAA920080861](https://openairdocs.org/sdr/USAA920080861.md): Bracket · cracked · Apr 10, 2008 · N922UW · Boeing 757225 · Fuselage Miscellaneous Structure
  > PIT - MAJOR REPAIR - C4 CHECK - A.5" CRACK ON BRACKET AT BS 310.5. REPLACED BRACKET IAW SRM 510-10-00.
- [SDR USAA920080860](https://openairdocs.org/sdr/USAA920080860.md): Skin · cracked · Apr 9, 2008 · N922UW · Boeing 757225 · Fuselage Main, Plate/Skin
  > PIT - MAJOR REPAIR - C4 CHECK - A.3" CRACK ON FUSELAGE SKIN AT BS 1708, STR 4L. INSTALLED DOUBLER / TRIPLER REPAIR IAW EA 110816.
- [SDR USAA920080859](https://openairdocs.org/sdr/USAA920080859.md): Skin · cracked · Apr 9, 2008 · N922UW · Boeing 757225 · Fuselage Main, Plate/Skin
  > PIT - MAJOR REPAIR - C4 CHECK - A.2" CRACK ON FUSELAGE SKIN AT BS 1630, STR 4R. INSTALLED DOUBLER / TRIPLER REPAIR IAW EA 110817/.
- [SDR USAA920080857](https://openairdocs.org/sdr/USAA920080857.md): Seat Track · cracked · Apr 9, 2008 · N922UW · Boeing 757225 · Fuselage, Seat/Cargo Attach Fittings
  > PIT - MAJOR REPAIR - C4 CHECK - A 2" CORNER OF SEAT TRACK CRACKED AT BS 780. REPLACED SEAT TRACK (BS 680-790) IAW SRM 51-40-00.
- [SDR USAA920080858](https://openairdocs.org/sdr/USAA920080858.md): Slat · delaminated · Apr 8, 2008 · N922UW · Boeing 757225 · Leading Edge Devices
  > PIT - MAJOR REPAIR - C4 CHECK - NR 6 L/E SLAT HAS 4" DELAMINATION. INSTALLED DOUBLER REPAIR IAW SRM 51-70-10.
- [SDR USAA920080846](https://openairdocs.org/sdr/USAA920080846.md): Floorbeam · corroded · Apr 8, 2008 · N922UW · Boeing 757225 · Fuselage Main, Floor Beam
  > PIT- MAJOR REPAIR - C4 CHECK - CORROSION ON FLOORBEAM AT BS 1680, WL 208.1, LBL 54 - RBL 54. REPAIRED FLOORBEAM IAW SRM 51-10-00, 51-21-02 AND 53-00-51 REPAIR 3.
- [SDR USAA920080843](https://openairdocs.org/sdr/USAA920080843.md): Angle · corroded · Apr 7, 2008 · N922UW · Boeing 757225 · Fuselage Miscellaneous Structure
  > PIT - MAJOR REPAIR - C4 CHECK - Z-ANGLE CORRODED BENEATH L2 DOOR SILL PLATE AT BS 686 - 760. REPLACED Z-ANGLE IAW SRM 51-40-02.
- [SDR USAA920080854](https://openairdocs.org/sdr/USAA920080854.md): Floor Support · corroded · Apr 3, 2008 · N922UW · Boeing 757225 · Fuselage Miscellaneous Structure
  > PIT - MAJOR REPAIR - C4 CHECK - CORROSION ON FLOOR SUPPORT CHANNEL AT BS 345, WL, 208.1, LBL 36. REPLACED CHANNEL IAW SRM 53-00-51.
- [SDR USAA920080853](https://openairdocs.org/sdr/USAA920080853.md): Floor Support · corroded · Apr 3, 2008 · N922UW · Boeing 757225 · Fuselage Miscellaneous Structure
  > PIT - MAJOR REPAIR - C4 CHECK - CORROSION ON FLOOR SUPPORT ANGLE AT BS 1635, WL 208.1, LBL 64. REPLACED SUPPORT ANGLE IAW 51-40-02 AND 53-60-13.
- [SDR USAA920080851](https://openairdocs.org/sdr/USAA920080851.md): Floor Support · corroded · Apr 3, 2008 · N922UW · Boeing 757225 · Fuselage Miscellaneous Structure
  > PIT - MAJOR REPAIR - C4 CHECK - CORROSION ON FLOOR SUPPORT AT BS 1640 - 1661, WL 208.1, BL 0. REPLACED SUPPORT IAW SRM 51-40-02.
- [SDR USAA920080841](https://openairdocs.org/sdr/USAA920080841.md): Stringer · cracked · Apr 3, 2008 · N922UW · Boeing 757225 · Fuselage Main, Longeron/Stringer
  > PIT- MAJOR REPAIR - C4 CHECK - A 1" CRACK ON STRINGER 3R BETWEEN BS 1020 AND BS 1040. INSTALLED REPAIR IAW SRM 53-00-03 FIG 201.
- [SDR USAA920080850](https://openairdocs.org/sdr/USAA920080850.md): Floor Support · cracked · Apr 2, 2008 · N922UW · Boeing 757225 · Fuselage Miscellaneous Structure
  > PIT- MAJOR REPAIR - C4 CHECK - A 1" CRACK ON FLOOR SUPPORT WEB AT BS 1681, WL 208.1, RBL 10. REPLACED WEB IAW SRM 51-40-02.
- [SDR USAA920080847](https://openairdocs.org/sdr/USAA920080847.md): Floor Support · corroded · Apr 1, 2008 · N922UW · Boeing 757225 · Fuselage Miscellaneous Structure
  > PIT- MAJOR REPAIR - C4 CHECK - CORROSION ON FLOOR SUPPORT AT BS 1640 - 1661, RBL 54. REPLACED SUPPORT IAW SRM 51-40-02.
- [SDR USAA920080845](https://openairdocs.org/sdr/USAA920080845.md): Support · corroded · Apr 1, 2008 · N922UW · Boeing 757225 · Fuselage, Equipment Attach Fittings
  > PIT- MAJOR REPAIR - C4 CHECK - CORROSION ON GALLEY SUPPORT AT BS 1710 - 1720, WL 208.1, RBL 6. REPLACED SUPPORT IAW SRM 51-10-00, 51-40-02 AND DRAWING 146N5300.
- [SDR USAA920080844](https://openairdocs.org/sdr/USAA920080844.md): Support · corroded · Apr 1, 2008 · N922UW · Boeing 757225 · Fuselage, Equipment Attach Fittings
  > PIT- MAJOR REPAIR - C4 CHECK - CORROSION ON GALLEY SUPPORT AT BS 1700-1720, WL 208.1, LBL 6. REPLACED SUPPORT IAW SRM 51-10-00, 51-40-02 AND DRAWING 146N5300.
- [SDR USAA920080842](https://openairdocs.org/sdr/USAA920080842.md): Floor Support · corroded · Apr 1, 2008 · N922UW · Boeing 757225 · Fuselage Miscellaneous Structure
  > PIT- MAJOR REPAIR - C4 CHECK - A 1" X 1" AREA OF CORROSION ON FLOOR SUPPORT AT BS 1640 - 1661, LBL 54. REPLACED SUPPORT IAW SRM 51-40-02.
- [SDR USAA920080855](https://openairdocs.org/sdr/USAA920080855.md): Slat · delaminated · Mar 31, 2008 · N922UW · Boeing 757225 · Leading Edge Devices
  > PIT - MAJOR REPAIR - C4 CHECK - NR 9 SLAT HAS DELAMINATION AT I/B TRAILING EDGE CORNER (2.5" X 9.5") AND O/B TRAILING EDGE CORNER (4" X 15.75"). INSTALLED REPAIR IAW SRM 51-70-10.
- [SDR USAA920080849](https://openairdocs.org/sdr/USAA920080849.md): Angle · corroded · Mar 31, 2008 · N922UW · Boeing 757225 · Fuselage Miscellaneous Structure
  > PIT - MAJOR REPAIR - C4 CHECK - CORROSION ON Z-ANGLE R4 DOOR SILL PLATE MOUNT AT BS 1640. REPLACED Z-ANGLE MOUNT IAW SRM 51-40-02.
- [SDR USAA920080848](https://openairdocs.org/sdr/USAA920080848.md): Support · corroded · Mar 30, 2008 · N922UW · Boeing 757225 · Fuselage Miscellaneous Structure
  > PIT- MAJOR REPAIR - C4 CHECK - CORROSION ON R4 DOOR DRAIN PAN SUPPORT AT BS 1661 - 1681. REPLACED SUPPORT IAW SRM 51-40-02.
- [SDR USAA920080839](https://openairdocs.org/sdr/USAA920080839.md): Floorbeam · corroded · Mar 30, 2008 · N922UW · Boeing 757225 · Fuselage Main, Floor Beam
  > PIT - MAJOR REPAIR - C4 CHECK - A 1" X 3" AND 4" X 6" CORROSION AREAS ON FLOOR RAIL AT BS 365-395, RBL 10. MANUFACTURED AND REPLACED RAIL IAW BOEING DRAWING 141N5162-6.
- [SDR USAA920080840](https://openairdocs.org/sdr/USAA920080840.md): Skin · cracked · Mar 27, 2008 · N922UW · Boeing 757225 · Trailing Edge Flaps
  > PIT- MAJOR REPAIR - C4 CHECK - A 5" CRACK ON RIGHT O/B FLAP BOTTOM SKIN AT O/B EDGE. REPAIRED IAW SRM 57-53-01 FIG 201, REPAIR 4.
- [SDR BB08014](https://openairdocs.org/sdr/BB08014.md): Module · failed · Feb 9, 2008 · N922UW · Boeing 757225 · Stabilizer Control System
  > FLT NR 1586 - ON FINAL JUST BELOW 1,000 FT AGL 27R, A/P OFF, A/T OFF, REF 138, WIND 280 AT 14 KTS THE A/C PITCHED UP ABOUT 8 FT ROLLED RT. CREW PUSHED A/C NOSE DOWN AND BANKED BACK LEFT. 15 SECONDS LATER DID THE SAME THING DID NOT FEEL ANY WAKE TURBULENCE.
- [SDR USAA920080331](https://openairdocs.org/sdr/USAA920080331.md): Skin · cracked · Jan 31, 2008 · N922UW · Boeing 757225 · Fuselage Main, Plate/Skin
  > CLT - MAJOR REPAIR - RON - NR 4262403, CRACK FOUND ON THE R2 DOOR UPPER HINGE CUTOUT AREA. REPAIRED THE R2 DOOR UPPER HINGE CUTOUT AREA IAW USAIRWAYS EA 110574.
- [SDR BB07033](https://openairdocs.org/sdr/BB07033.md): Engine · vibration · Apr 2, 2007 · N922UW · Boeing 757225 · Engine (Turbine/Turboprop)
  > FLIGHT 1866, FLL-PHL: DURING FLIGHT, CREW REPORTED A NUMBER ONE ENGINE VIBRATION AND NO RESPONSE TO THROTTLE MOVEMENTS. DECLARED EMERGENCY AND LANDED PHL WITH NO OTHER DIFFICULTIES. ENGINE SHUT DOWN NORMALLY AFTER LANDING. MAINTENANCE REPLACED THE LEFT ENG

## 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 = 'N922UW' AND deregistration_id = 'N922UW-2011-08-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N922UW-2011-08-22/reports

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