# Service difficulty reports: N155AW, cancelled Mar 6, 2012

A list on [N155AW, cancelled Mar 6, 2012](https://openairdocs.org/deregistered/N155AW-2012-03-06.md).

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

Page 1 of 6 · 272 reports

- [SDR USAA20110314SB039](https://openairdocs.org/sdr/USAA20110314SB039.md): Panel · delaminated · Mar 10, 2011 · N155AW · Boeing 7373G7 · Wing, Plate/Skin
  > PHX - EN ROUTE TO PHX FROM ONT, THE AIRCRAFT SUFFERED SIGNIFICANT DELAMINATION OF AN UNDERWING PANEL CAUSING SIGNIFICANT PORTIONS OF THE PANEL TO SEPARATE FROM THE AIRCRAFT. FLIGHT LANDED WITHOUT INCIDENT. PANEL WAS REPORTED MISSING ON WALK AROUND FOR DAILY
- [SDR USAA2011031091010](https://openairdocs.org/sdr/USAA2011031091010.md): Skin · cracked · Mar 9, 2011 · N155AW · Boeing 7373G7 · Leading Edge Devices
  > PHX - B2 - MAJOR REPAIR - RIGHT WING NR 6 SLAT OUTBOARD TRACK AREA - LOWER SURFACE IS CRACKED. REPAIRED NR 6 SLAT OUTBOARD TRACK AREA - LOWER SURFACE IAW B737 SRM 57-43-01 REPAIR 6.
- [SDR USAA20110125SB015](https://openairdocs.org/sdr/USAA20110125SB015.md): Wire · damaged · Jan 25, 2011 · N155AW · Boeing 7373G7 · Light System Wiring
  > PHX - MAINTENANCE REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT 12C INOPERATIVE. MAINTENANCE REPAIRED WIRE AT SEAT 12C IN ASSOCIATION WITH SWPM 20-10. OPERATIONAL CHECK GOOD.
- [SDR USAA20101227SB208](https://openairdocs.org/sdr/USAA20101227SB208.md): Circuit Breaker · tripped · Dec 27, 2010 · N155AW · Boeing 7373G7 · Stabilizer Control System
  > DFW - ON CLIMBOUT FROM DFW, CREW REPORTED THE STAB OUT OF TRIM LIGHT CAME ON AND WITH AUTO PILOT ON, WOULD NOT TRIM. WITH AUTO PILOT OFF, STAB TRIM WILL WORK. FLIGHT RETURNED TO FIELD AT DFW AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. M
- [SDR USAA2010122393220](https://openairdocs.org/sdr/USAA2010122393220.md): Skin · cracked · Dec 21, 2010 · N155AW · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > PHX - MAJOR REPAIR - LAPSEAM INSPECTION, CRACKED FUSELAGE SKIN AT BS 727E, S22R. REPAIRED FUSELAGE SKIN AT BS 727E, S22R IAW B737 SRM 53-00-01 REPAIR 31.
- [SDR USAA2010081791696](https://openairdocs.org/sdr/USAA2010081791696.md): Light · inoperative · Aug 12, 2010 · N155AW · Boeing 7373G7 · Emergency Lighting
  > MIA - C20 - EEL - R-1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REPLACED R-1 DOOR LOWER EMERGENCY EXIT LIGHT ASSEMBLY IAW B737 AMM 33-51-11.
- [SDR USAA2010081791695](https://openairdocs.org/sdr/USAA2010081791695.md): Skin · cracked · Aug 12, 2010 · N155AW · Boeing 7373G7 · Cargo/Baggage Doors
  > MIA - C20 - MAJOR REPAIR - FORWARD CARGO DOOR INNER SKIN IS CRACKED AT LIGHTNING HOLE 22 INCHES FROM TOP EDGE 13 INCHES FROM FORWARD EDGE BETWEEN BS 442.55 TO BS 489.90 & BETWEEN S20R TO S21R. REPAIRED FORWARD CARGO DOOR INNER SKIN IAW EA 139885.
- [SDR USAA2010081791694](https://openairdocs.org/sdr/USAA2010081791694.md): Skin · cracked · Aug 11, 2010 · N155AW · Boeing 7373G7 · Leading Edge Devices
  > MIA - C20 - MAJOR REPAIR - RIGHT WING NR 5 SLAT HAS A CRACK AT THE TRAILING EDGE ON THE LOWER SURFACE 22 INCHES FROM INBOARD END. REPLACED RIGHT WING NR 5 SLAT IAW B737 AMM 27-81-21.
- [SDR USAA2010081291646](https://openairdocs.org/sdr/USAA2010081291646.md): Skin · cracked · Aug 10, 2010 · N155AW · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > MIA - C20 - MAJOR REPAIR - HORIZONTAL STABILIZER LEFT AFT ATTACH POINT AREA FOUND CRACK ON INTERNAL RE-ENFORCEMENT SKIN AT BS1138, S12L. REPLACED HORIZONTAL STABILIZER FRAME STRAP AT BS1138, S12L IAW B737 SRM 53-00-01 & B737 SRM 51-40-02.
- [SDR USAA2010081291645](https://openairdocs.org/sdr/USAA2010081291645.md): Skin · cracked · Aug 10, 2010 · N155AW · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > MIA - C20 - MAJOR REPAIR - HORIZONTAL STABILIZER LEFT AFT ATTACH POINT AREA HAS FORWARD SLIDING SEAL TORN (SKIN) BETWEEN BS 1138 TO BS 1143, S12L. REPLACED FORWARD SLIDING SEAL (SKIN) BETWEEN BS 1138 TO BS 1143, S12L IAW B737 SRM 51-40-02.
- [SDR USAA2010081891705](https://openairdocs.org/sdr/USAA2010081891705.md): Attach Angle · corroded · Aug 8, 2010 · N155AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > MIA - C20 - MAJOR REPAIR - ATTACH FITTING CORRODED STA 1016 BETWEEN S27R AND S27L. REPLACED ATTACH FITTING AT BS 1016 BETWEEN S27R AND S27L IAW B737 SRM 51-40-02.
- [SDR USAA2010081791698](https://openairdocs.org/sdr/USAA2010081791698.md): Shear Tie · cracked · Jul 26, 2010 · N155AW · Boeing 7373G7 · Fuselage Internal Mounting Structure
  > MIA - C20 - MAJOR REPAIR - CRACKS FOUND ON SHEAR TIE CLIP AT BS 360 BETWEEN S14R & S15R JUST AFT OF FORWARD SERVICE DOOR. REPAIRED SHEAR TIE CLIP AT BS 360 BETWEEN S14R & S15R IAW B737 SRM 53-00-07.
- [SDR USAA2010081791697](https://openairdocs.org/sdr/USAA2010081791697.md): Battery Pack · discharged · Jul 26, 2010 · N155AW · Boeing 7373G7 · Emergency Equipment
  > MIA - C20 - EEL - FORWARD EMERGENCY FLASH LIGHT FAILED "FLASH" TEST. REPLACED FORWARD EMERGENCY FLASH LIGHT BATTERY PACK IAW B737 AMM 25-60-00.
- [SDR USAA2010060991094](https://openairdocs.org/sdr/USAA2010060991094.md): Slat · debonded · Jun 6, 2010 · N155AW · Boeing 7373G7 · Leading Edge Devices
  > PHX - B4 - MAJOR REPAIR - LEFT WING NR 2 LEADING EDGE SLAT ASSEMBLY DISBONDED/SPLIT AT OUTBOARD TRAILING EDGE AFT CORNER. REPLACED LEFT WING NR 2 LEADING EDGE SLAT ASSEMBLY IAW B737 AMM 27-81-21.
- [SDR USAA2010060891086](https://openairdocs.org/sdr/USAA2010060891086.md): Panel · debonded · Jun 6, 2010 · N155AW · Boeing 7373G7 · Spoilers
  > PHX - B4 - MAJOR REPAIR - LEFT WING NR 3 SPOILER PANEL DISBONDED FROM INBOARD TO MID SPAN OF AFT TRAILING EDGE OF PANEL. REPLACED LEFT WING NR 3 SPOILER PANEL IAW B737 AMM 27-61-11-4.
- [SDR USAA2010060791072](https://openairdocs.org/sdr/USAA2010060791072.md): Skin · cracked · Jun 6, 2010 · N155AW · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > PHX - B4 - MAJOR REPAIR - FUSELAGE SKIN CRACK APPROX 1 INCH LONG BETWEEN BS 727E AND BS 747 RIGHT SIDE APPROX 27 INCHES BELOW LOWER LAP SEAM. REPAIRED FUSELAGE SKIN BETWEEN BS 727E & BS 747, S22R IAW B373 SRM 53-00-01 REPAIR 31.
- [SDR USAA2010060791071](https://openairdocs.org/sdr/USAA2010060791071.md): Skin · cracked · Jun 5, 2010 · N155AW · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > PHX - B-CHECK - MAJOR REPAIR - 2.5 INCH FUSELAGE SKIN CRACK AT BS 937, S25R. REPAIRED FUSELAGE SKIN CRACK AT BS 937, S25R IAW B737 SRM 53-00-01 REPAIR 31.
- [SDR USAA20100421SB055](https://openairdocs.org/sdr/USAA20100421SB055.md): Light · not seated · Apr 20, 2010 · N155AW · Boeing 7373G7 · Emergency Lighting
  > PHX - MAINTENANCE REPORTED THE MAIN CABIN SEAT MOUNTED EMERGENCY LIGHTS, AT ROWS 4L AND 15L, FAIL TO ILLUMINATE. MAINTENANCE FOUND THE LAMPS AT ROWS 4L AND 15L WERE NOT PROPERLY SEATED. REPOSITIONED LAMPS AS REQUIRED. OPERATIONAL CHECK NORMAL.
- [SDR USAA20100119SB007](https://openairdocs.org/sdr/USAA20100119SB007.md): Wire · loose · Jan 16, 2010 · N155AW · Boeing 7373G7 · Light System Wiring
  > MAINTENANCE REPORTED THE EMERGENCY ESCAPE PATH LIGHTS AT ROW 22L AISLE SEAT WIRING IS LOOSELY HANGING DISCONNECTED FROM TERMINAL. MAINTENANCE RECONNECTED WIRING TO TERMINAL. OPERATIONAL TEST GOOD IN ASSOCIATION WITH MM 33-51-02-715-001 AND WDM 33-51-21.
- [SDR USAA2010010490008](https://openairdocs.org/sdr/USAA2010010490008.md): Skin · cracked · Dec 31, 2009 · N155AW · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > PHX - OVERNIGHT - MAJOR REPAIR - CRACK IN FUSELAGE SKIN BETWEEN BS 747 & BS 747E, S25R. REPAIRED FUSELAGE SKIN BETWEEN BS 747 & BS 747E, S25R IAW B737 SRM 53-00-01 REPAIR 31.
- [SDR USAA2009101492768](https://openairdocs.org/sdr/USAA2009101492768.md): Wire · loose · Oct 13, 2009 · N155AW · Boeing 7373G7 · Light System Wiring
  > SEAT ROW 1 ACFT EMERGENCY EXIT LIGHT INOPERATIVE. WIRE PULLED OUT OF TERMINAL SPLICE. REPAIRED WIRING SEAT ROW 1. ACFT EMERGENCY EXIT LIGHT IAW STANDARD WIRING PRACTICES 20-30-12. (K)
- [SDR USAA2009101492769](https://openairdocs.org/sdr/USAA2009101492769.md): Wire · loose · Oct 13, 2009 · N155AW · Boeing 7373G7 · Light System Wiring
  > ROW 16 ABC EMERGENCY EXIT LIGHT INOPERATIVE. WIRE PULLED OUT OF TERMINAL SPLICE. REPAIRED WIRING ROW 16 ABC EMERGENCY EXIT LIGHT IAW STANDARD WIRING PRACTICES 20-30-12. (K)
- [SDR USAA2009082592247](https://openairdocs.org/sdr/USAA2009082592247.md): Skin · cracked · Aug 25, 2009 · N155AW · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > PHX - OVERNIGHT - MAJOR REPAIR - CRACK AT LAP SEAM ON FUSELAGE SKIN AT BS 727G, S25L. REPAIRED LAP SEAM ON FUSELAGE SKIN AT BS 727G, S25L IAW B737 SRM 53-00-01 REPAIR 31.
- [SDR USAA20090619SB101](https://openairdocs.org/sdr/USAA20090619SB101.md): Cable · frayed · Jun 19, 2009 · N155AW · Boeing 7373G7 · Emergency Equipment
  > PHX - MAINTENANCE REPORTED THE R2 DOOR GIRT BAR TO TRIGGER CABLE HAS STRANDS BROKEN. MAINTENANCE REMOVED AND REPLACED THE CABLE.
- [SDR USAA2009050891120](https://openairdocs.org/sdr/USAA2009050891120.md): Hinge Pin · corroded · Apr 23, 2009 · N155AW · Boeing 7373G7 · Horizontal Stabilizer, Plate/Skin
  > SAL - C19 - MAJOR REPAIR - CORROSION ON OUTER STABILIZER HINGE PIN, LEFT SIDE CENTER SECTION HINGE. REPLACED OUTER STABILIZER HINGE PIN, LEFT SIDE CENTER SECTION HINGE IAW B737 AMM 27-41-31-4.
- [SDR USAA2009050891121](https://openairdocs.org/sdr/USAA2009050891121.md): Web · cracked · Apr 22, 2009 · N155AW · Boeing 7373G7 · Horizontal Stabilizer, Plate/Skin
  > SAL - C19 - MAJOR REPAIR - CRACK ON WEB AT HORIZONTAL STABILIZER CENTER SECTION BETWEEN STA 1088 & STA 1104 LBL 22. REPAIRED WEB AT HORIZONTAL STABILIZER CENTER SECTION BETWEEN STA 1088 & STA 1104 LBL 22 IAW B737 SRM 51-70-13.
- [SDR USAA2009042390962](https://openairdocs.org/sdr/USAA2009042390962.md): Frame · cracked · Apr 12, 2009 · N155AW · Boeing 7373G7 · Fuselage Main, Frame
  > SAL - C19 - MAJOR REPAIR - CRACK ON UPPER FRAME FLANGE AT BS 344.2 BETWEEN S23L TO S24L. REPAIRED UPPER FRAME FLANGE AT BS 344.2 BETWEEN S23L TO S24L IAW B737 SRM 51-70-11.
- [SDR USAA2009050791116](https://openairdocs.org/sdr/USAA2009050791116.md): Skin Panel · cracked · Apr 9, 2009 · N155AW · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > SAL - C19 - MAJOR REPAIR - 6207024 - CRACK ON FUSELAGE SKIN BETWEEN BS 500C + 10 INCHES TO BS 520 + 10 INCHES & BETWEEN S11R TO S13R. REPAIRED FUSELAGE SKIN BETWEEN BS 500C + 10 INCHES TO BS 520 + 10 INCHES & BETWEEN S11R TO S13R IAW US AIRWAYS EA 132376.
- [SDR USAA2009050791115](https://openairdocs.org/sdr/USAA2009050791115.md): Skin Panel · cracked · Apr 9, 2009 · N155AW · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > SAL - C19 - MAJOR REPAIR - 6207023 - CRACK ON FUSELAGE SKIN BETWEEN BS 500D TO BS 530 & BETWEEN S11L TO S13L. REPAIRED FUSELAGE SKIN BETWEEN BS 500D TO BS 530 & BETWEEN S11L TO S13L IAW US AIRWAYS EA 132375.
- [SDR USAA2009042490971](https://openairdocs.org/sdr/USAA2009042490971.md): Seat Track · corroded · Apr 9, 2009 · N155AW · Boeing 7373G7 · Fuselage, Seat/Cargo Attach Fittings
  > SAL - C19 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT BS 797, LBL 45.5. REPAIRED SEAT TRACK AT BS 797, LBL 45.5 IAW B737 SRM 53-00-52.
- [SDR USAA2009042390966](https://openairdocs.org/sdr/USAA2009042390966.md): Seat Track · corroded · Apr 9, 2009 · N155AW · Boeing 7373G7 · Fuselage, Seat/Cargo Attach Fittings
  > SAL - C19 - MAJOR REPAIR - CORROSION ON SEAT TRACK AT BS 912, LBL 45.5. REPAIRED SEAT TRACK AT BS 912, LBL 45.5 IAW B737 SRM 53-00-52.
- [SDR USAA2009042991028](https://openairdocs.org/sdr/USAA2009042991028.md): Hinge Fitting · cracked · Apr 7, 2009 · N155AW · Boeing 7373G7 · Spoilers
  > SAL - C19 - MAJOR REPAIR - CRACK ON NR 5 GROUND SPOILER HINGE FITTING UPPER SURFACE WBL 117. REPLACED NR 5 GROUND SPOILER HINGE FITTING UPPER SURFACE AT WBL 117 IAW B737 SRM 57-56-61.
- [SDR USAA2009042991027](https://openairdocs.org/sdr/USAA2009042991027.md): Intercostal · corroded · Apr 4, 2009 · N155AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON INTERCOSTAL WEB BETWEEN BS 847 TO BS 867, S25R. REPLACED INTERCOSTAL BETWEEN BS 847 TO BS 867, S25R IAW B737 SRM 51-10-02.
- [SDR USAA2009042891020](https://openairdocs.org/sdr/USAA2009042891020.md): Web · corroded · Apr 4, 2009 · N155AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > SAL - C19 - MAJOR REPAIR - CORROSION ON WEB BETWEEN BS 847 TO BS 867, ALSO BETWEEN S25R TO S26R. REPAIRED WEB BETWEEN BS 847 TO BS 867, ALSO BETWEEN S25R TO S26R IAW B737 SRM 51-10-02 & BOEING DRAWING 65-47957.
- [SDR USAA2009042891019](https://openairdocs.org/sdr/USAA2009042891019.md): Channel · corroded · Apr 4, 2009 · N155AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > SAL - C19 - MAJOR REPAIR - CORROSION ON CHANNEL AT BS 859.5, RBL 8.10. REPAIRED CHANNEL AT BS 859.5 RBL 8.10 IAW B737 SRM 53-00-53.
- [SDR USAA2009042790986](https://openairdocs.org/sdr/USAA2009042790986.md): Tie Clip · cracked · Apr 4, 2009 · N155AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > SAL - C19 - MAJOR REPAIR - CRACK ON TIE CLIP AT BS 947, LBL 26. REPLACED TIE CLIP AT BS 947, LBL 26 IAW B737 SRM 51-10-02.
- [SDR USAA2009042790982](https://openairdocs.org/sdr/USAA2009042790982.md): Tie Clip · cracked · Apr 4, 2009 · N155AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > SAL - C19 - MAJOR REPAIR - CRACK ON TIE CLIP AT BS 927, LBL 27. REPAIRED TIE CLIP AT BS 927, LBL 27 IAW B737 SRM 51-10-02 & BOEING DRAWING 69-35350.
- [SDR USAA2009042790981](https://openairdocs.org/sdr/USAA2009042790981.md): Bulkhead · canning · Apr 4, 2009 · N155AW · Boeing 7373G7 · Fuselage Main, Bulkhead
  > SAL - C19 - MAJOR REPAIR - OIL CANNING ON AFT FACE OF WEB DOME ON AFT PRESSURE BULKHEAD AT BS 1023, S8L, LBL 51 & S10L, LBL 58. REPAIRED BULKHEAD WEB AT BS 1023, S8L, LBL 51 & S10L, LBL 58 IAW B737 SRM 53-80-08 REPAIR 11.
- [SDR USAA2009042390963](https://openairdocs.org/sdr/USAA2009042390963.md): Skin · cracked · Apr 4, 2009 · N155AW · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > SAL - C19 - MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT LOWER HINGE CUTOUT OF FORWARD ENTRY DOOR AT BS 312, S10L. REPAIRED FUSELAGE SKIN AT LOWER HINGE CUTOUT OF FORWARD ENTRY DOOR AT BS 312, S10L IAW B737 SRM 53-10-01.
- [SDR USAA2009050491078](https://openairdocs.org/sdr/USAA2009050491078.md): Skin · cracked · Apr 3, 2009 · N155AW · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > SAL - C19 - MAJOR REPAIR - CRACK ON LOWER LOBE OF FUSELAGE SKIN AT BS 522 BETWEEN S28L TO S28R. REPAIRED LOWER LOBE OF FUSELAGE SKIN AT BS 522 BETWEEN S28L TO S28R IAW US AIRWAYS EA 132360.
- [SDR USAA2009043091045](https://openairdocs.org/sdr/USAA2009043091045.md): Frame · cracked · Apr 3, 2009 · N155AW · Boeing 7373G7 · Fuselage Main, Frame
  > SAL - C19 - MAJOR REPAIR - FRAME CRACKED AT BS 787 BETWEEN S8L TO S9L. REPAIRED FRAME AT BS 787 BETWEEN S8L TO S9L IAW US AIRWAYS TASK CARD M1C53002.
- [SDR USAA2009043091044](https://openairdocs.org/sdr/USAA2009043091044.md): Frame · cracked · Apr 3, 2009 · N155AW · Boeing 7373G7 · Fuselage Main, Frame
  > SAL - C19 - MAJOR REPAIR - FRAME CRACKED AT BS 480 BETWEEN S8R TO S9R. REPAIRED FRAME AT BS480 BETWEEN S8R TO S9R IAW US AIRWAYS TASK CARD M1C53002.
- [SDR USAA2009043091043](https://openairdocs.org/sdr/USAA2009043091043.md): Frame · cracked · Apr 3, 2009 · N155AW · Boeing 7373G7 · Fuselage Main, Frame
  > SAL - C19 - MAJOR REPAIR - FRAME CRACKED AT BS 480 BETWEEN S8L TO S9L. REPAIRED FRAME AT BS 480 BETWEEN S8L TO S9L IAW US AIRWAYS TASK CARD M1C53002.
- [SDR USAA2009043091042](https://openairdocs.org/sdr/USAA2009043091042.md): Frame · cracked · Apr 3, 2009 · N155AW · Boeing 7373G7 · Fuselage Main, Frame
  > SAL - C19 - MAJOR REPAIR - FRAME CRACKED AT BS 380 BETWEEN S8R TO S9R. REPAIRED FRAME AT BS 380 BETWEEN S8R TO S9R IAW US AIRWAYS TASK CARD M1C53002.
- [SDR USAA2009042891014](https://openairdocs.org/sdr/USAA2009042891014.md): Floorbeam · corroded · Apr 3, 2009 · N155AW · Boeing 7373G7 · Fuselage Main, Floor Beam
  > SAL - C19 - MAJOR REPAIR - INTERGRANULAR CORROSION ON FLOORBEAM UPPER FLANGE AT BS 986.5 BETWEEN LBL 43 TO RBL 43. REPAIRED FLOORBEAM AT BS 986.5 BETWEEN LBL 43 TO RBL 43 IAW US AIRWAYS TYPICAL REPAIR 53-10-05B.
- [SDR USAA2009042790987](https://openairdocs.org/sdr/USAA2009042790987.md): Web · corroded · Apr 3, 2009 · N155AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON UPPER WEB BETWEEN BS986 TO BS1016, LBL39.5. REPAIRED UPPER WEB BETWEEN BS 986 TO BS1016, LBL39.5 IAW B737 SRM 51-10-02.
- [SDR USAA2009042490973](https://openairdocs.org/sdr/USAA2009042490973.md): Beam · corroded · Apr 3, 2009 · N155AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > SAL - C19 - MAJOR REPAIR - INTERGRANULAR CORROSION ON BEAM UPPER FLANGE BETWEEN BS 967 TO BS 986.5, RBL 18. REPLACED BEAM BETWEEN BS 967 TO BS 986.5, RBL 18 IAW B737 SRM 51-10-02.
- [SDR USAA2009042490972](https://openairdocs.org/sdr/USAA2009042490972.md): Beam · corroded · Apr 3, 2009 · N155AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > SAL - C19 - MAJOR REPAIR - INTERGRANULAR CORROSION ON BEAM UPPER FLANGE BETWEEN BS 986.5 TO BS 1006, LBL 8. REPLACED BEAM BETWEEN BS 986.5 TO BS 1006, LBL 8 IAW B737 SRM 51-10-02.
- [SDR USAA2009042390965](https://openairdocs.org/sdr/USAA2009042390965.md): Beam · corroded · Apr 3, 2009 · N155AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > SAL - C19 - MAJOR REPAIR - INTERGRANULAR CORROSION ON UPPER BEAM FLANGE BETWEEN BS 986.5 TO BS 1006, RBL 15. REPLACED BEAM BETWEEN BS 986.5 TO BS 1006, RBL 15 IAW B737 SRM 51-10-02.
- [SDR USAA2009042390964](https://openairdocs.org/sdr/USAA2009042390964.md): Beam · corroded · Apr 3, 2009 · N155AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > SAL - C19 - MAJOR REPAIR - INTERGRANULAR CORROSION ON BEAM BETWEEN BS 986.5 TO BS 1006, RBL 27. REPLACED BEAM BETWEEN BS 986.5 TO BS 1006, RBL 27 IAW B737 SRM 51-10-02.

Next page: https://openairdocs.org/deregistered/N155AW-2012-03-06/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 n_number = 'N155AW' AND deregistration_id = 'N155AW-2012-03-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N155AW-2012-03-06/reports

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