# Service difficulty reports: N305AW, cancelled Jan 12, 2012

A list on [N305AW, cancelled Jan 12, 2012](https://openairdocs.org/deregistered/N305AW-2012-01-12.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 · 254 reports

- [SDR USAA2011072800018](https://openairdocs.org/sdr/USAA2011072800018.md): Slide · unserviceable · Jul 16, 2011 · N305AW · Boeing 7373G7 · Escape Slide
  > C21 CHECK - L-1 DOOR ESCAPE SLIDE GIRT BAR NOT ATTACHED TO GIRT. REPLACED L-1 DOOR ESCAPE SLIDE PACK ASSEMBLY IAW B737 AMM 25-61-35-002-005.
- [SDR USAA2011072800015](https://openairdocs.org/sdr/USAA2011072800015.md): Closeout Panel · worn · Jul 12, 2011 · N305AW · Boeing 7373G7 · Nacelle/Pylon, Plate/Skin
  > C21 CHECK - NR 1 PYLON MID FAIRING CLOSE OUT PANEL IS WORN AT FORWARD END UNDER INBOARD AND OUTBOARD ANGLE BRACKETS AT NAC STA 282.67. REPAIRED NR 1 PYLON MID FAIRING CLOSE OUT PANEL IAW EA 130639.
- [SDR USAA2011072000021](https://openairdocs.org/sdr/USAA2011072000021.md): Shear Web · broken · Jul 11, 2011 · N305AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > C21 CHECK - RIGHT SIDE SHEAR WEB HAS ATTACH HOLES BROKEN OUT AT BS 1017 & BS 1024, BL 0. REPLACED SHEAR WEB IAW B737 SRM 51-40-02 FIG 3, 8, 9, 10 & 12.
- [SDR USAA2011072000019](https://openairdocs.org/sdr/USAA2011072000019.md): Strap · cracked · Jul 11, 2011 · N305AW · Boeing 7373G7 · Fuselage Main, Floor Beam
  > C21 CHECK - CRACKS IN CABIN FLOORBEAM STABILIZER STRAP AT BS 328, LBL 4. REPAIRED CABIN FLOORBEAM STABILIZER STRAP AT BS 328, LBL 4 IAW B737 SRM 53-10-51 FIG 201 REPAIR 4.
- [SDR USAA2011072000018](https://openairdocs.org/sdr/USAA2011072000018.md): Strap · cracked · Jul 11, 2011 · N305AW · Boeing 7373G7 · Fuselage Main, Floor Beam
  > C21 CHECK - CRACK IN FLOORBEAM STABILIZING STRAP AT BS 314.5, LBL 17. REPAIRED FLOORBEAM STABILIZING STRAP AT BS 314.5, LBL 17 IAW B737 SRM 53-10-51 FIG 201 REPAIR 4.
- [SDR USAA2011072600009](https://openairdocs.org/sdr/USAA2011072600009.md): Shear Web · corroded · Jul 8, 2011 · N305AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > C21 CHECK - LEVEL 2 FILIFORM CORROSION ON SHEAR WEB AT BS 1016 BETWEEN BL 0 TO LBL 39. REPLACED SHEAR WEB AT BS 1016 BETWEEN BL 0 TO LBL 39 IAW B737 SRM 51-40-02.
- [SDR USAA2011072600008](https://openairdocs.org/sdr/USAA2011072600008.md): Structure · corroded · Jul 8, 2011 · N305AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > C21 CHECK - LEVEL 2 EXFOLIATION CORROSION ON INNER CHORD BETWEEN BS 947 TO BS 998, LBL 42. REPLACED INNER CHORD BETWEEN BS 947 TO BS 998, LBL 42 IAW B737 SRM 51-40-02.
- [SDR USAA2011072000001](https://openairdocs.org/sdr/USAA2011072000001.md): Attach Angle · cracked · Jul 8, 2011 · N305AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > C21 CHECK - CRACKS ON CABIN FLOOR STRUCTURE WEB UPPER ATTACH ANGLE BETWEEN BS 927 TO BS 947.5, BL 0. REPLACED CABIN FLOOR STRUCTURE WEB UPPER ATTACH ANGLE IAW B737 SRM 51-40-02.
- [SDR USAA2011072800017](https://openairdocs.org/sdr/USAA2011072800017.md): Pressure Deck · cracked · Jul 7, 2011 · N305AW · Boeing 7373G7 · Fuselage Main, Bulkhead
  > C21 CHECK - CRACK IN LEFT MAIN WHEEL WELL PRESSURE DECK AT BS 665, LBL 40. REPAIRED LEFT MAIN WHEEL WELL PRESSURE DECK IAW EA 130643.
- [SDR USAA2011072000020](https://openairdocs.org/sdr/USAA2011072000020.md): Door Frame · cracked · Jul 7, 2011 · N305AW · Boeing 7373G7 · Fuselage Main, Structure
  > C21 CHECK - CRACK IN R1 DOOR UPPER FORWARD REVEAL STUB FRAME AT BS 297, S8R. REPLACED R1 DOOR UPPER FORWARD REVEAL STUB FRAME IAW B737 SRM 51-40-02 FIG 3, 8 & 12.
- [SDR USAA2011072000017](https://openairdocs.org/sdr/USAA2011072000017.md): Skin · cracked · Jul 7, 2011 · N305AW · Boeing 7373G7 · Spoilers
  > C21 CHECK - CRACK ON BOTTOM OF NR 6 SLAT SKIN BETWEEN SS254.4 TO SS255.0. REPAIRED NR 6 SLAT SKIN BETWEEN SS254.4 TO SS255.0 IAW B737 SRM 57-43-01 FIG 201.
- [SDR USAA2011050991797](https://openairdocs.org/sdr/USAA2011050991797.md): Skin · cracked · May 6, 2011 · N305AW · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > PHX - DAILY - CRACK IN FUSELAGE SKIN AT 2.5 INCHES FORWARD OF AFT CARGO DOOR AT BS 747, S18R. REPAIRED FUSELAGE SKIN AT 2.5 INCHES FORWARD OF AFT CARGO DOOR AT BS 747, S18R IAW B737 SRM 53-00-01.
- [SDR USAA20100617SB104](https://openairdocs.org/sdr/USAA20100617SB104.md): Uplock Sensor · faulty · Jun 16, 2010 · N305AW · Boeing 7373G7 · Landing Gear Position and Warning
  > PHX - ON CLIMBOUT FROM PHX, CREW REPORTED THE RIGHT MAIN LANDING GEAR RED LIGHT FLASHED OFF AND ON INTERMITTENTLY AFTER GEAR RETRACTION. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO FIELD AT PHX WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLA
- [SDR USAA2010050390883](https://openairdocs.org/sdr/USAA2010050390883.md): Flap · delaminated · Apr 30, 2010 · N305AW · Boeing 7373G7 · Trailing Edge Flaps
  > MCN - C20 - MAJOR REPAIR - DELAMINATION ON RIGHT OUTBOARD FORE FLAP 40 INCHES FROM INBOARD END. REPLACED RIGHT OUTBOARD FORE FLAP IAW JOB CARDS O3R27002 & C3R27002.
- [SDR USAA2010042990868](https://openairdocs.org/sdr/USAA2010042990868.md): Frame · cracked · Apr 6, 2010 · N305AW · Boeing 7373G7 · Fuselage Main, Frame
  > MCN - C20 - MAJOR REPAIR - CRACK IN FRAME WEB AT BS 303.9, S16L FORWARD OF L-1 DOOR. REPAIRED FRAME WEB AT BS 303.9, S16L FORWARD OF L-1 DOOR IAW JOB CARD M1L53001.
- [SDR USAA2010043090873](https://openairdocs.org/sdr/USAA2010043090873.md): Seat Track · corroded · Apr 3, 2010 · N305AW · Boeing 7373G7 · Fuselage, Seat/Cargo Attach Fittings
  > MCN - C20 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT BS 328, RBL 25. REPLACED SEAT TRACK AT BS 328, RBL 25 IAW B737 SRM 53-00-52.
- [SDR USAA2010042190808](https://openairdocs.org/sdr/USAA2010042190808.md): Channel · cracked · Apr 3, 2010 · N305AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > MCN - C20 - MAJOR REPAIR - CRACK IN CHANNEL AT BS 329, LBL 47. REPLACED CHANNEL AT BS 329, LBL 47 IAW B737 SRM 51-40-02.
- [SDR USAA2010041990805](https://openairdocs.org/sdr/USAA2010041990805.md): Stiffener · cracked · Apr 3, 2010 · N305AW · Boeing 7373G7 · Fuselage Main, Floor Beam
  > MCN - C20 - MAJOR REPAIR - CRACKS ON VERTICAL STIFFENER ON AFT SIDE OF FLOORBEAM AT BS 329, LBL 47. REPLACED VERTICAL STIFFENER ON AFT SIDE OF FLOORBEAM AT BS 329, LBL 47 IAW B737 SRM 51-40-02.
- [SDR USAA2010043090871](https://openairdocs.org/sdr/USAA2010043090871.md): Skin Panel · cracked · Apr 1, 2010 · N305AW · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > MCN - C20 - MAJOR REPAIR - CRACK ON FUSELAGE SKIN AT MAIN ENTRY DOOR UPPER / LOWER HINGE CUTOUTS AT BS 312 BETWEEN S9L TO S15L. REPAIRED FUSELAGE SKIN AT MAIN ENTRY DOOR UPPER / LOWER HINGE CUTOUTS IAW EA 130391.
- [SDR USAA2010042990866](https://openairdocs.org/sdr/USAA2010042990866.md): Door Frame · cracked · Mar 31, 2010 · N305AW · Boeing 7373G7 · Passenger/Crew Doors
  > MCN - C20 - MAJOR REPAIR - 2 CRACKS IN L-1 DOOR AFT FRAME AT BS 344 BETWEEN S9L TO S10L. REPAIRED L-1 DOOR AFT FRAME AT BS 344 BETWEEN S9L TO S10L IAW EA 130394.
- [SDR USAA2010042990865](https://openairdocs.org/sdr/USAA2010042990865.md): Frame · cracked · Mar 31, 2010 · N305AW · Boeing 7373G7 · Fuselage Main, Frame
  > MCN - C20 - MAJOR REPAIR - CRACK IN FUSELAGE FRAME AT BS 360, S13R. REPAIRED FUSELAGE FRAME AT BS 360, S13R IAW TYPICAL REPAIR 53-10-21B.
- [SDR USAA2010042690838](https://openairdocs.org/sdr/USAA2010042690838.md): Skin · cracked · Mar 31, 2010 · N305AW · Boeing 7373G7 · Horizontal Stabilizer, Plate/Skin
  > MCN - C20 - MAJOR REPAIR - CRACK ON RIGHT HORIZONTAL STABILIZER LOWER SKIN AT SS125. REPAIRED RIGHT HORIZONTAL STABILIZER LOWER SKIN AT SS125 IAW TYPICAL REPAIR 55-10-07 REV D.
- [SDR USAA2010042690839](https://openairdocs.org/sdr/USAA2010042690839.md): Stringer · corroded · Mar 30, 2010 · N305AW · Boeing 7373G7 · Fuselage Main, Longeron/Stringer
  > MCN - C20 - MAJOR REPAIR - CORROSION ON STRINGER 27R AT BS 946. REPAIRED STRINGER 27R AT BS 946 IAW B737 SRM 53-00-03.
- [SDR USAA2010021290350](https://openairdocs.org/sdr/USAA2010021290350.md): Slat · debonded · Feb 9, 2010 · N305AW · Boeing 7373G7 · Leading Edge Devices
  > PHX - B4 - MAJOR REPAIR - NR 4 SLAT DISBONDED AT INBOARD CORNER BETWEEN SLAT STA 12 TO SLAT STA 16. REPAIRED NR 4 SLAT AT INBOARD CORNER BETWEEN SLAT STA 12 TO SLAT STA 16 IAW B737 SRM 57-43-02 & 51-70-10.
- [SDR USAA2010021290349](https://openairdocs.org/sdr/USAA2010021290349.md): Wedge · debonded · Feb 9, 2010 · N305AW · Boeing 7373G7 · Leading Edge Devices
  > PHX - B4 - MAJOR REPAIR - NR 3 SLAT DISBONDED ON THE TRAILING EDGE WEDGE END CAP AFT CORNER BETWEEN SLAT STA 115 TO SLAT STA 124.4. REPAIRED NR 3 SLAT SKIN IAW B737 SRM 57-43-02 & 51-70-10.
- [SDR USAA2010021290348](https://openairdocs.org/sdr/USAA2010021290348.md): Skin · cracked · Feb 9, 2010 · N305AW · Boeing 7373G7 · Fuselage Main, Plate/Skin
  > PHX - B4 - MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT FORWARD LEFT CORNER OF GROUND AIR CONDITIONING SERVICE DOOR CUTOUT AT BS 530, S28L. REPAIRED FUSELAGE SKIN AT FORWARD LEFT CORNER OF GROUND AIR CONDITIONING SERVICE DOOR CUTOUT AT BS 530, S28L IAW B737 SRM 5
- [SDR USAA2009101992800](https://openairdocs.org/sdr/USAA2009101992800.md): Flap · debonded · Oct 18, 2009 · N305AW · Boeing 7373G7 · Trailing Edge Flaps
  > PHX - DAILY - MAJOR REPAIR - RIGHT WING AFT OUTBOARD TRAILING EDGE FLAP DISBONDED ON INBOARD CORNER. REPLACED RIGHT OUTBOARD TRAILING EDGE FLAP IAW CARD R3M27034.
- [SDR USAA20090828SB143](https://openairdocs.org/sdr/USAA20090828SB143.md): Warning System · malfunctioned · Aug 27, 2009 · N305AW · Boeing 7373G7 · Leading Edge Slat Position Indicating System
  > PHX - DURING APPROACH, AS FLAPS WERE SELECTED FROM FLAPS 1 TO 5, CREW RECEIVED A LEADING EDGE FLAPS TRANSIT LIGHT ALONG WITH THE NR 2 SLAT. CREW EXECUTED A MISSED APPROACH AND ACCOMPLISHED A GO-AROUND. PRIOR TO LANDING WITH FLAPS AT 15, THE LEADING EDGE FLAP
- [SDR USAA20090622SB104](https://openairdocs.org/sdr/USAA20090622SB104.md): Wire · broken · Jun 21, 2009 · N305AW · Boeing 7373G7 · Light System Wiring
  > PHX - MAINTENANCE REPORTED THE EMERGENCY EXIT SIGN AT MID CABIN CEILING WAS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE ON THE EMERGENCY EXIT SIGN. DISCOVERED THAT BROKEN WIRE SHORTED OUT POWER SUPPLY. REPLACED BOTH THE EMERGENCY EXIT SIGN AND POWER SUPPLY
- [SDR USAA20090601SB092](https://openairdocs.org/sdr/USAA20090601SB092.md): Wire · broken · Jun 1, 2009 · N305AW · Boeing 7373G7 · Light System Wiring
  > DFW MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEATS 10 AND 11, LEFT-HAND SIDE, ARE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE IN ASSOCIATION WITH SWPM 20-30-12. OPERATIONAL CHECK GOOD.
- [SDR USAA20090512SB078](https://openairdocs.org/sdr/USAA20090512SB078.md): Power Supply · faulty · May 11, 2009 · N305AW · Boeing 7373G7 · Emergency Lighting
  > PHX - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS FLASH ON AND OFF INTERMITTENTLY. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT POWER SUPPLY IN ASSOCIATION WITH MM 33-51-00, PAGE BLOCK 401. OPERATIONAL CHECK GOOD.
- [SDR USAA20090402SB046](https://openairdocs.org/sdr/USAA20090402SB046.md): Transformer · faulty · Feb 11, 2009 · N305AW · Boeing 7373G7 · DC Rectifier/Converter
  > ON SHORT FINAL INTO PDX, FULLY CONFIGURED, TR1 CIRCUIT BREAKER POPPED. AS A PRECAUTION, CAPTAIN REQUESTED TO HAVE THE EMERGENCY EQUIPMENT STANDING BY. AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT INCIDENT. CONTRACT MAINTENANCE WAS CALLED TO EVALUATE PROBL
- [SDR 2009F00032](https://openairdocs.org/sdr/2009F00032.md): Snubber · misinstalled · Jan 23, 2009 · N305AW · Boeing 7373G7 · Emergency Exits
  > ON CLIMB OUT, L1 EMERGENCY EXIT DOOR SEAL LEAKING, NOISE LEVEL UNACCEPTABLE, PRESSURIZATION OK. ACFT 13,000 LBS OVERWEIGHT FOR LANDING, DECLARED AN EMERGENCY UNSCHEDULED LANDING, & LANDED 5000LBS OVERWEIGHT. MX FOUND L1 DOOR LWR SNUBBER INSTALLED BACKWARDS
- [SDR USAA2009012190109](https://openairdocs.org/sdr/USAA2009012190109.md): Fitting · corroded · Jan 6, 2009 · N305AW · Boeing 7373G7 · Horizontal Stabilizer Miscellaneous Structure
  > SAL - C19 - MAJOR REPAIR - CORROSION ON UPPER, LOWER, & MIDDLE CLEVIS JOINT OF LEFT HORIZONTAL STABILIZER AT ELEVATOR HINGE LINE 113.25. REPAIRED UPPER, LOWER, & MIDDLE CLEVIS JOINT OF LEFT HORIZONTAL STABILIZER AT ELEVATOR HINGE LINE 113.25 IAW B737 55-10-10
- [SDR USAA2009010890051](https://openairdocs.org/sdr/USAA2009010890051.md): Web · corroded · Jan 5, 2009 · N305AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > SAL - C19 - MAJOR REPAIR - NR 6143586 - GALVANIC CORROSION ON WEB BETWEEN BS 1016 TO BS1030, LBL17. REPAIRED WEB BETWEEN BS 1016 TO BS1030, LBL17 IAW B737 SRM 51-70-13.
- [SDR USAA2009010890052](https://openairdocs.org/sdr/USAA2009010890052.md): Battery · discharged · Jan 4, 2009 · N305AW · Boeing 7373G7 · Emergency Equipment
  > SAL - C19 - EMERGENCY LIGHT - NR 6142265 - LOW BATTERY IN FLASHLIGHT ON FORWARD CABIN ATTENDANTS SEAT. REPLACED BATTERY IN FLASHLIGHT ON FORWARD CABIN ATTENDANTS SEAT IAW B737 AMM 25-60-00-0.
- [SDR USAA2009012190110](https://openairdocs.org/sdr/USAA2009012190110.md): Bulkhead · cracked · Dec 29, 2008 · N305AW · Boeing 7373G7 · Fuselage Main, Bulkhead
  > SAL - C19 - MAJOR REPAIR - CRACK AT BS 178 BULKHEAD ON WEB SURFACE OF VERTICAL BEAM, RBL 5.7, BETWEEN WL 180 & WL 190. REPAIRED BS 178 BULKHEAD ON WEB SURFACE OF VERTICAL BEAM, RBL 5.7, BETWEEN WL 180 & WL 190 IAW US AIRWAYS EA 132193.
- [SDR USAA2009012190106](https://openairdocs.org/sdr/USAA2009012190106.md): Skin · delaminated · Dec 29, 2008 · N305AW · Boeing 7373G7 · Trailing Edge Flaps
  > SAL - C19 - MAJOR REPAIR - DELAMINATION ON UPPER SKIN OF RIGHT OUTBOARD AFT FLAP WBL 350 TO WBL 368. REPAIRED UPPER SKIN OF RIGHT OUTBOARD AFT FLAP WBL 350 TO WBL 36 IAW B737 SRM 51-70-10.
- [SDR USAA2009012390132](https://openairdocs.org/sdr/USAA2009012390132.md): Channel · corroded · Dec 27, 2008 · N305AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > SAL - C19 - MAJOR REPAIR - CORROSION ON CHANNEL BETWEEN BS 787 TO BS 947, LBL 12.5. REPAIRED CHANNEL BETWEEN BS 787 TO BS 947, LBL 12.5 IAW B737 SRM 53-00-53.
- [SDR USAA2009012190113](https://openairdocs.org/sdr/USAA2009012190113.md): Frame · cracked · Dec 27, 2008 · N305AW · Boeing 7373G7 · Fuselage Main, Frame
  > SAL - C19 - MAJOR REPAIR - CRACK ON FRAME AT BS 380 BETWEEN S8R & S9R. REPAIRED FRAME AT BS 380 BETWEEN S8R & S9R IAW US AIRWAYS TASK CARD M1C53002.
- [SDR USAA2009011690083](https://openairdocs.org/sdr/USAA2009011690083.md): Frame · cracked · Dec 27, 2008 · N305AW · Boeing 7373G7 · Fuselage Main, Frame
  > SAL - C19 - MAJOR REPAIR - CRACK ON FRAME AT BS 500C, BETWEEN S8L TO S9L. REPAIRED FRAME AT BS 500C, BETWEEN S8L TO S9L IAW AMERICA WEST AIRLINES TASK CARD M1C53002.
- [SDR USAA2009011590078](https://openairdocs.org/sdr/USAA2009011590078.md): Frame · cracked · Dec 27, 2008 · N305AW · Boeing 7373G7 · Fuselage Main, Frame
  > SAL - C19 - MAJOR REPAIR - NR 6192125 - FRAME CRACKED AT BS480, BETWEEN S-8L & S9L. REPAIRED FRAME AT BS480, BETWEEN S-8L & S9L IAW AMERICA WEST AIRLINES TASK CARD M1C53002.
- [SDR USAA2009012190107](https://openairdocs.org/sdr/USAA2009012190107.md): Web · corroded · Dec 26, 2008 · N305AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON UPPER WEB AT S26R BETWEEN BS 847 TO BS 867. REPAIRED UPPER WEB AT S26R BETWEEN BS 847 TO BS 867 IAW B737 SRM 51-40-02.
- [SDR USAA2009012190117](https://openairdocs.org/sdr/USAA2009012190117.md): Floorbeam · corroded · Dec 26, 2008 · N305AW · Boeing 7373G7 · Fuselage Main, Floor Beam
  > SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT BS 967, BETWEEN LBL 18 TO LBL 44. REPAIRED FLOORBEAM AT BS 967, BETWEEN LBL 18 TO LBL 44 IAW B737 SRM 53-00-51.
- [SDR USAA2009012190114](https://openairdocs.org/sdr/USAA2009012190114.md): Support · corroded · Dec 26, 2008 · N305AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON INTERCOSTAL SUPPORT BETWEEN BS 947 TO BS 967, LBL 18. REPAIRED INTERCOSTAL SUPPORT BETWEEN BS 947 TO BS 967, LBL 18 IAW B737 SRM 51-10-02-06.
- [SDR USAA2009012190112](https://openairdocs.org/sdr/USAA2009012190112.md): Cover · corroded · Dec 26, 2008 · N305AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > SAL - C19 - MAJOR REPAIR - CORROSION ON COVER SHEET BETWEEN BS 767 TO BS 787, S26R. REPLACED COVER SHEET BETWEEN BS 767 TO BS 787, S26R IAW B737 SRM 51-40-02.
- [SDR USAA2009011390068](https://openairdocs.org/sdr/USAA2009011390068.md): Seat Track · corroded · Dec 26, 2008 · N305AW · Boeing 7373G7 · Fuselage, Seat/Cargo Attach Fittings
  > SAL - C19 - MAJOR REPAIR - NR 6142261 - GALVANIC CORROSION ON SEAT TRACK AT BS919, RBL45. REPAIRED SEAT TRACK AT BS919, RBL45 IAW B737 SRM 53-00-52.
- [SDR USAA2009012390131](https://openairdocs.org/sdr/USAA2009012390131.md): Web · cracked · Dec 24, 2008 · N305AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > SAL - C19 - MAJOR REPAIR - CRACK ON WEB AT BS 987.5, RBL 40. REPAIRED WEB AT BS 987.5, RBL 40 IAW B737 SRM 51-10-02-0G.
- [SDR USAA2009012190116](https://openairdocs.org/sdr/USAA2009012190116.md): Support · corroded · Dec 24, 2008 · N305AW · Boeing 7373G7 · Fuselage Miscellaneous Structure
  > SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON STRAP ANGLE SUPPORT AT BS 1006, RBL 41. REPAIRED STRAP ANGLE SUPPORT AT BS 1006, RBL 41 IAW B737 SRM 51-40-02 & 51-10-02.
- [SDR USAA2009012190115](https://openairdocs.org/sdr/USAA2009012190115.md): Floorbeam · corroded · Dec 24, 2008 · N305AW · Boeing 7373G7 · Fuselage Main, Floor Beam
  > SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM UPPER FLANGE AT BS 986.5, BL 0 TO RBL 54. REPAIRED FLOORBEAM UPPER FLANGE AT BS 986.5, BL 0 TO RBL 54 IAW B737 SRM 53-00-51.

Next page: https://openairdocs.org/deregistered/N305AW-2012-01-12/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 = 'N305AW' AND deregistration_id = 'N305AW-2012-01-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N305AW-2012-01-12/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.