# Service difficulty reports: N425US, cancelled Oct 19, 2016

A list on [N425US, cancelled Oct 19, 2016](https://openairdocs.org/deregistered/N425US-2016-10-19.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 5 · 209 reports

- [SDR USAA2013090400005](https://openairdocs.org/sdr/USAA2013090400005.md): Lens · missing · Sep 3, 2013 · N425US · Boeing 737401 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS MISSING LENS ON SEATS 8C & 9E. R & R EMERGENCY EXIT LIGHTS ON SEATS 8C & 9E.
- [SDR USAA2013041200014](https://openairdocs.org/sdr/USAA2013041200014.md): Wire · shorted · Apr 10, 2013 · N425US · Boeing 737401 · Light System Wiring
  > MAINTENANCE REPORTED LEFT SEAT ROWS 24 & 25 SEAT MOUNTED EMERGENCY LIGHTS INOP. MAINTENANCE FOUND WIRES SHORTED AT ROW 25A SEAT CONNECTOR. REPLACED CONNECTOR IAW SWPM 20-64-17. OPS CHECK GOOD.
- [SDR USAA2013021300004](https://openairdocs.org/sdr/USAA2013021300004.md): Wire · loose · Feb 13, 2013 · N425US · Boeing 737401 · Light System Wiring
  > MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT AT PASSENGER SEAT 6C INOP. MAINTENANCE FOUND WIRE LOOSE AT SPLICE. RE-SPLICED WIRE. CHECKS OK.
- [SDR USAA2013010800021](https://openairdocs.org/sdr/USAA2013010800021.md): Battery Pack · discharged · Jan 8, 2013 · N425US · Boeing 737401 · Emergency Lighting
  > MAINTENANCE REPORTED DOOR 2L OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED RIGHT AFT BATTERY PACK IAW 33-51-51. OPS CHECK GOOD.
- [SDR USAA2012112700001](https://openairdocs.org/sdr/USAA2012112700001.md): Battery · discharged · Nov 26, 2012 · N425US · Boeing 737401 · Emergency Lighting
  > OVERNIGHT CHECK - ALL EMERGENCY LAMPS WORKING OFF CHARGER ASSEMBLY M1137 ARE INOP. REPLACED BATTERY ASSEMBLY, CHECKS OK IAW B373 AMM 33-51-02.
- [SDR USAA2012090400003](https://openairdocs.org/sdr/USAA2012090400003.md): Skin · cracked · Aug 29, 2012 · N425US · Boeing 737401 · Fuselage Main, Plate/Skin
  > C6 CHECK - CRACK IN FUSELAGE SKIN AT BS 882 APPROX 1 INCH ABOVE S25R. REMOVED DAMAGE, FABRICATED AND INSTALLED TEAR STRAP, FILLERS AND DOUBLER IAW B737 SRM 53-00-01-2R-31, DETAIL XIX.
- [SDR USAA2012080800016](https://openairdocs.org/sdr/USAA2012080800016.md): Charger · inoperative · Aug 8, 2012 · N425US · Boeing 737401 · Emergency Lighting
  > MAINTENANCE REPORTED THE OVERWING EMERGENCY LIGHT INOPERATIVE - LEFT SIDE. MAINTENANCE REPLACED CHARGER ASSEMBLY (INCLUDING BATTERY PACK) PER AMM 33-51-51-962. OPS CHECKS OK.
- [SDR USAA2012061800012](https://openairdocs.org/sdr/USAA2012061800012.md): Flashlight · defective · Jun 15, 2012 · N425US · Boeing 737401 · Emergency Equipment
  > RON - AFT GALLEY LOWER FLASHLIGHT WON'T CHARGE. REPLACED AFT GALLEY LOWER FLASHLIGHT PER B737-400 AMM 25-60-00, OPERATIONAL CHECKED GOOD.
- [SDR USAA2012061300002](https://openairdocs.org/sdr/USAA2012061300002.md): Slide · out of position · Jun 13, 2012 · N425US · Boeing 737401 · Escape Slide
  > CREW REPORTED DOOR 1L SLIDE PACK FALLING DOWN. MAINTENANCE REPOSITIONED 1L SLIDE PACK. CHECKS GOOD.
- [SDR USAA2012032100006](https://openairdocs.org/sdr/USAA2012032100006.md): Fuse · blown · Mar 21, 2012 · N425US · Boeing 737401 · Emergency Lighting
  > MAINTENANCE REPORTED SEAT ROWS 6 THRU 9 EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED PICO FUSE IN EMERGENCY LIGHT POWER SUPPLY. OPS CHECKS OK.
- [SDR USAA2012022300008](https://openairdocs.org/sdr/USAA2012022300008.md): Oil System · overserviced · Feb 22, 2012 · N425US · Boeing 737401 · APU Oil System
  > FLIGHT ATTENDANT REPORTED A STRONG ODOR ON APPROACH. ODOR WAS STRONG AT FORWARD FLIGHT ATTENDANT JUMPSEAT AREA, COCKPIT NORMAL. MAINTENANCE FOUND APU OVERSERVICED. CLEANED AREA AND SERVICED APU. ACCOMPLISHED CABIN ODOR TROUBLESHOOTING J/C 03L00021001. OK
- [SDR USAA2011111100006](https://openairdocs.org/sdr/USAA2011111100006.md): Seat Track · lack of lube · Nov 10, 2011 · N425US · Boeing 737401 · Fuselage, Seat/Cargo Attach Fittings
  > CREW REPORTED THE FIRST OFFICER'S SEAT IS HARD TO SLIDE FORE AND AFT. MAINTENANCE LUBED AS REQUIRED. OPS CHECK GOOD PER AMM 25-11-00.
- [SDR USAA2011093000004](https://openairdocs.org/sdr/USAA2011093000004.md): Seat Track · dirty · Sep 29, 2011 · N425US · Boeing 737401 · Fuselage, Seat/Cargo Attach Fittings
  > CREW REPORTED THE FIRST OFFICER'S SEAT VERY DIFFICULT TO ADJUST FORE AND AFT. MAINTENANCE CLEANED SEAT TRACK FOR FIRST OFFICER'S SEAT AND REMOVED FOOD ITEMS. SEAT OPERATES OK. AIRCRAFT OK FOR SERVICE.
- [SDR USAA2011091900013](https://openairdocs.org/sdr/USAA2011091900013.md): Seat Track · dirty · Sep 17, 2011 · N425US · Boeing 737401 · Fuselage, Seat/Cargo Attach Fittings
  > CREW REPORTED THE CAPTAIN'S SEAT IS VERY DIFFICULT TO ADJUST FORE AND AFT. MAINTENANCE CLEANED AND LUBED THE SEAT TRACKS. OPS CHECK NORMAL. OK FOR SERVICE.
- [SDR USAA2011090700023](https://openairdocs.org/sdr/USAA2011090700023.md): Stiffener · cracked · Sep 7, 2011 · N425US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q5 CHECK - CRACK IN VERTICAL STIFFENER AT BS 328, RBL 32. REPLACED VERTICAL STIFFENER AT BS 328, RBL 32 IAW BOEING DRAWING 65-45812 & B737 SRM 51-10-02.
- [SDR USAA2011090700017](https://openairdocs.org/sdr/USAA2011090700017.md): Floor Support · cracked · Sep 7, 2011 · N425US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q5 CHECK - CRACK ON FLOOR SUPPORT AT BS 330, LBL 46. REPLACED FLOOR SUPPORT AT BS 330, LBL 46 IAW B737 SRM 51-20-02.
- [SDR USAA2011090700019](https://openairdocs.org/sdr/USAA2011090700019.md): Shear Tie · corroded · Sep 4, 2011 · N425US · Boeing 737401 · Fuselage Internal Mounting Structure
  > Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FRAME SHEAR TIE AT BS 747, RBL 5. REPAIRED FRAME SHEAR TIE AT BS 747, RBL 5 IAW B737 SRM 53-00-02R-4 REPAIR 4.
- [SDR USAA2011090700022](https://openairdocs.org/sdr/USAA2011090700022.md): Door Frame · cracked · Sep 3, 2011 · N425US · Boeing 737401 · Fuselage Main, Structure
  > Q5 CHECK - CRACK IN FORWARD LEFT ENTRANCE DOOR FORWARD CUTOUT FRAME WEB AT BS 303.9, S16L. REPLACED FORWARD CUTOUT FRAME WEB AT BS 303.9, S16L IAW EO 5311-01025.
- [SDR USAA2011090700012](https://openairdocs.org/sdr/USAA2011090700012.md): Frame · corroded · Sep 2, 2011 · N425US · Boeing 737401 · Fuselage Main, Frame
  > Q5 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FRAME AT BS 727G, BETWEEN S27L TO S27R, BL 0. REPAIRED FRAME AT BS 727G, BETWEEN S27L TO S27R, BL 0 IAW B737-400 SRM 53-00-07 REPAIR 4.
- [SDR USAA2011090800001](https://openairdocs.org/sdr/USAA2011090800001.md): Floorbeam · corroded · Sep 1, 2011 · N425US · Boeing 737401 · Fuselage Main, Floor Beam
  > Q5 CHECK - LEVEL 2 GALVANIC CORROSION ON AFT CARGO FLOOR TRACK/BEAM BS 747, RBL 14. REPAIRED AFT CARGO FLOOR TRACK/BEAM IAW BOEING DRAWING 65-53844 & B737 SRM 51-10-02 & 53-00-53 REPAIR 2.
- [SDR USAA2011090700013](https://openairdocs.org/sdr/USAA2011090700013.md): Frame · corroded · Sep 1, 2011 · N425US · Boeing 737401 · Fuselage Main, Frame
  > Q5 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FRAME AT BS 747, BETWEEN S26L TO S27L, LBL 8. REPAIRED FRAME AT BS 747, BETWEEN S26L TO S27L, LBL 8 IAW B737-400 SRM 53-00-07-2R-4 REPAIR 2.
- [SDR USAA2011090700020](https://openairdocs.org/sdr/USAA2011090700020.md): Stringer Clip · corroded · Sep 1, 2011 · N425US · Boeing 737401 · Fuselage Main, Attach Fittings
  > Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON STRINGER TIE CLIP AT BS847, S25R. REPLACED STRINGER TIE CLIP AT BS847, S25R IAW B737 SRM 51-40-02.
- [SDR USAA2011090700021](https://openairdocs.org/sdr/USAA2011090700021.md): Stringer · corroded · Aug 31, 2011 · N425US · Boeing 737401 · Fuselage Main, Longeron/Stringer
  > Q5 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON STRINGER AT BS 927, S21R. REPAIRED STRINGER BETWEEN BS 907 TO BS 935, S21R IAW B737 SRM 53-00-03, FIG 201, REPAIR 1.
- [SDR USAA2011090100027](https://openairdocs.org/sdr/USAA2011090100027.md): Intercostal · corroded · Aug 31, 2011 · N425US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL WEB BETWEEN BS 767 TO BS 787, RBL 6. REPLACED INTERCOSTAL WEB BETWEEN BS 767 TO BS 787, RBL6 IAW B737 SRM 51-40-02.
- [SDR USAA2011090100026](https://openairdocs.org/sdr/USAA2011090100026.md): Shear Tie · corroded · Aug 31, 2011 · N425US · Boeing 737401 · Fuselage Internal Mounting Structure
  > Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE AT BS 907 BETWEEN S27L TO S27R. REPLACED SHEAR TIE AT BS 907 BETWEEN S27L TO S27R IAW B737 SRM 51-00-07 REPAIR 3.
- [SDR USAA2011090100024](https://openairdocs.org/sdr/USAA2011090100024.md): Shear Tie · corroded · Aug 31, 2011 · N425US · Boeing 737401 · Fuselage Internal Mounting Structure
  > Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE AT BS 787 BETWEEN BL 0 TO LBL 4. REPLACED SHEAR TIE AT BS 787 BETWEEN BL 0 TO LBL 4 IAW B737 SRM 51-00-07 REPAIR 4.
- [SDR USAA2011090700009](https://openairdocs.org/sdr/USAA2011090700009.md): Door Frame · corroded · Aug 30, 2011 · N425US · Boeing 737401 · Fuselage Main, Structure
  > Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON AFT FRAME AT AFT CARGO DOOR CUTOUT AT BS 847, RBL 22. REPLACED AFT FRAME AT AFT CARGO DOOR CUTOUT AT BS 847, RBL 22 IAW B737-400 SRM 51-10-02.
- [SDR USAA2011083100048](https://openairdocs.org/sdr/USAA2011083100048.md): Stiffener · cracked · Aug 27, 2011 · N425US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q5 CHECK - CRACK ON VERTICAL STIFFENER AT BS 328, LBL 47. REPLACED VERTICAL STIFFENER AT BS 328, LBL 47 IAW SRM 51-10-02 & BOEING DRAWING 65-45812.
- [SDR USAA2011083100038](https://openairdocs.org/sdr/USAA2011083100038.md): Strap · corroded · Aug 27, 2011 · N425US · Boeing 737401 · Fuselage Main, Plate/Skin
  > Q5 CHECK - CORROSION ON FUSELAGE SKIN STRAP BETWEEN BS 907 TO BS 927 & BETWEEN S26L TO S26R. REPLACED FUSELAGE SKIN STRAP BETWEEN BS 907 TO BS 927 & BETWEEN S26L TO S26R IAW B737 SRM 53-00-01 REPAIR 31, DETAIL XXI.
- [SDR USAA2011090700025](https://openairdocs.org/sdr/USAA2011090700025.md): Doubler · corroded · Aug 26, 2011 · N425US · Boeing 737401 · Fuselage Main, Plate/Skin
  > Q5 CHECK - LEVEL 2 GALVANIC CORROSION ON DOUBLER FOR PHONE ANTENNA AT BS 786 + 6 INCHES. DOUBLER FOR PHONE ANTENNA AT BS 786 + 6 INCHES IAW B737 SRM 53-00-01 FIG 101.
- [SDR USAA2011090100023](https://openairdocs.org/sdr/USAA2011090100023.md): Stringer · cracked · Aug 26, 2011 · N425US · Boeing 737401 · Fuselage Main, Longeron/Stringer
  > Q5 CHECK - CRACK ON STRINGER AT BS 1011, S7L. REPLACED STRINGER AT BS 1011, S7L IAW BOEING DRAWING 65-52988 & SRM 51-10-02.
- [SDR USAA2011090700016](https://openairdocs.org/sdr/USAA2011090700016.md): Floorbeam · corroded · Aug 25, 2011 · N425US · Boeing 737401 · Fuselage Main, Floor Beam
  > Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON AFT CARGO FLOORBEAM/TRACK CHANNEL AT BS 727F + 6 INCHES, LBL 3. REPAIRED AFT CARGO FLOORBEAM/TRACK CHANNEL IAW EA 103284.
- [SDR USAA2011083100031](https://openairdocs.org/sdr/USAA2011083100031.md): Frame · cracked · Aug 24, 2011 · N425US · Boeing 737401 · Fuselage Main, Frame
  > Q5 CHECK -.50 INCH CRACK ON FRAME AT BS 500E, BETWEEN S20L TO S21L, WL 182.5. REPAIRED FRAME AT BS 500E, BETWEEN S20L TO S21L, WL 182.5 IAW SRM 53-00-07, REPAIR 13.
- [SDR USAA2011083100032](https://openairdocs.org/sdr/USAA2011083100032.md): Frame · cracked · Aug 23, 2011 · N425US · Boeing 737401 · Fuselage Main, Frame
  > Q5 CHECK -.75 INCH CRACK ON FRAME AT BS 500F, BETWEEN S20L TO S21L, WL 182. REPAIRED FRAME AT BS 500F, BETWEEN S20L TO S21L, WL 182 IAW SRM 53-00-07.
- [SDR USAA2011083100025](https://openairdocs.org/sdr/USAA2011083100025.md): Frame · cracked · Aug 22, 2011 · N425US · Boeing 737401 · Fuselage Main, Frame
  > Q5 CHECK - 0.5 INCH CRACK ON FRAME AT BS 500C, BETWEEN S20R TO S21R, WL 182.5. REPAIRED FRAME AT BS 500C, BETWEEN S20R TO S21R, WL 182.5 IAW SRM 53-00-07, REPAIR 13.
- [SDR USAA2011090100022](https://openairdocs.org/sdr/USAA2011090100022.md): Flap · delaminated · Aug 21, 2011 · N425US · Boeing 737401 · Trailing Edge Flaps
  > Q5 CHECK - DELAMINATION ON LEFT OUTBOARD MID FLAP AT LOWER TRAILING EDGE 18 INCHES FROM EDGE OF AFT FLAP & 13 INCHES FROM LEADING EDGE. REPLACED LEFT OUTBOARD MID FLAP IAW JOB CARD 03C30727030.
- [SDR USAA2011083100049](https://openairdocs.org/sdr/USAA2011083100049.md): Stiffener · corroded · Aug 20, 2011 · N425US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q5 CHECK - LEVEL 2 GALVANIC CORROSION ON STIFFNER AT BOTH LOWER CORNERS OF APU INLET CUTOUT AT INBOARD SIDE BETWEEN BS 1116 TO BS 1126, S17R. REPLACED STIFFENER AT BOTH LOWER CORNERS OF APU INLET CUT-OUT IAW BOEING DRAWING 65-46579.
- [SDR USAA2011083100043](https://openairdocs.org/sdr/USAA2011083100043.md): Shear Tie · corroded · Aug 19, 2011 · N425US · Boeing 737401 · Fuselage Internal Mounting Structure
  > Q5 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SHEAR TIE AT BS 947 BETWEEN S19L TO S20L, LBL 49. REPLACED SHEAR TIE AT BS 947 BETWEEN S19L TO S20L, LBL49 IAW B737 SRM 51-20-01.
- [SDR USAA2011083100035](https://openairdocs.org/sdr/USAA2011083100035.md): Skin · cracked · Aug 19, 2011 · N425US · Boeing 737401 · Fuselage Main, Plate/Skin
  > Q5 CHECK - 2 CRACKS ON FUSELAGE SKIN AT MAIN ENTRY LOWER DOOR HINGE CUTOUT AT BS 303.9 BELOW S9L. REPAIRED FUSELAGE SKIN AT MAIN ENTRY LOWER DOOR HINGE CUTOUT IAW TEMPORARY REVISION SRM 53-30 & B737-400 SRM 53-10-01 REPAIR 14.
- [SDR USAA2011083100034](https://openairdocs.org/sdr/USAA2011083100034.md): Skin · cracked · Aug 19, 2011 · N425US · Boeing 737401 · Fuselage Main, Plate/Skin
  > Q5 CHECK - CRACK ON FUSELAGE SKIN AT AFT ENTRY UPPER DOOR HINGE CUTOUT AT BS 948, S20L. REPAIRED FUSELAGE SKIN AT AFT ENTRY UPPER DOOR HINGE CUTOUT IAW B737 SRM 53-60-01.
- [SDR USAA2011090700018](https://openairdocs.org/sdr/USAA2011090700018.md): Skin · cracked · Aug 18, 2011 · N425US · Boeing 737401 · Fuselage Main, Plate/Skin
  > Q5 CHECK - CRACK ON FUSELAGE SKIN AT FORWARD SERVICE DOOR LOWER HINGE CUTOUT AT BS 291.5. REPAIRED FUSELAGE SKIN AT FORWARD SERVICE DOOR LOWER HINGE CUTOUT IAW EA 103271.
- [SDR USAA2011083100041](https://openairdocs.org/sdr/USAA2011083100041.md): Intercostal · corroded · Aug 17, 2011 · N425US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q5 CHECK - CORROSION ON FLOOR SUPPORT INTERCOSTAL BETWEEN BS 328 TO BS 344, RBL 11. REPLACED FLOOR SUPPORT INTERCOSTAL BETWEEN BS 328 TO BS 344, RBL 11 IAW B737 SRM 53-10-51 & SRM 51-10-02.
- [SDR USAA2011083100036](https://openairdocs.org/sdr/USAA2011083100036.md): Floorbeam · corroded · Aug 17, 2011 · N425US · Boeing 737401 · Fuselage Main, Floor Beam
  > Q5 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN BS 335 TO BS 339, RBL 23. REPLACED FLOORBEAM BETWEEN BS 335 TO BS 339, RBL 23 IAW B737 SRM 53-00-52.
- [SDR USAA2011091200011](https://openairdocs.org/sdr/USAA2011091200011.md): Trim Tab · delaminated · Aug 16, 2011 · N425US · Boeing 737401 · Aileron Tabs
  > Q5 CHECK - RIGHT AILERON TAB AFT CORNER DELAMINATED. REPLACED RIGHT AILERON TAB IAW B737 AMM 27-11-11.
- [SDR USAA2011090700011](https://openairdocs.org/sdr/USAA2011090700011.md): Frame · cracked · Aug 16, 2011 · N425US · Boeing 737401 · Fuselage Main, Frame
  > Q5 CHECK - CRACK ON FRAME AT BS 500F BETWEEN S20R TO S21R, WL 182.5. REPAIRED FRAME AT BS 500F, BETWEEN S20R TO S21R, WL 182.5 IAW B737-400 SRM 53-00-07 REPAIR 13.
- [SDR USAA2011090700010](https://openairdocs.org/sdr/USAA2011090700010.md): Frame · cracked · Aug 16, 2011 · N425US · Boeing 737401 · Fuselage Main, Frame
  > Q5 CHECK - CRACK ON FRAME AT BS 500E, BETWEEN S20R TO S21R, WL 182.5. REPAIRED FRAME AT BS 500E, BETWEEN S20R TO S21R, WL 182.5 IAW B737-400 SRM 53-00-07 REPAIR 13.
- [SDR USAA2011090100020](https://openairdocs.org/sdr/USAA2011090100020.md): Skin · delaminated · Aug 15, 2011 · N425US · Boeing 737401 · Rudder, Plate/Skin
  > Q5 CHECK - DELAMINATION ON RIGHT SIDE OF RUDDER EXTERIOR SKIN 38 INCHES FROM BOTTOM & 4 INCHES AFT OF FORWARD SPAR. REPAIRED RIGHT SIDE OF RUDDER EXTERIOR SKIN IAW EA 103256B & B737 SRM 51-70-17.
- [SDR USAA2011083100050](https://openairdocs.org/sdr/USAA2011083100050.md): Stiffener · corroded · Aug 12, 2011 · N425US · Boeing 737401 · Fuselage Miscellaneous Structure
  > Q5 CHECK - CORROSION ON VERTICAL STIFFENER AT AFT SIDE OF APU INLET AT BS 1147, RBL 15. REPLACED VERTICAL STIFFENER AT AFT SIDE OF APU INLET IAW B737 SRM 51-10-02.
- [SDR USAA2011083100026](https://openairdocs.org/sdr/USAA2011083100026.md): Frame · cracked · Aug 11, 2011 · N425US · Boeing 737401 · Fuselage Main, Frame
  > Q5 CHECK - 0.5 INCH CRACK ON FRAME AT BS 520, BETWEEN S20L TO S21L, WL 182.5. REPAIRED FRAME AT BS 520, BETWEEN S20L TO S21L, WL 182.5 IAW SRM 53-00-07, REPAIR 13.
- [SDR USAA2011090100021](https://openairdocs.org/sdr/USAA2011090100021.md): Stringer · corroded · Aug 10, 2011 · N425US · Boeing 737401 · Fuselage Main, Longeron/Stringer
  > Q5 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON STRINGER AT BS 847, S22R. REPLACED STRINGER BETWEEN BS 847 TO BS 905, S22R IAW B737 SRM 53-60-03, FIG 1, DETAIL II & SRM 51-10-02.

Next page: https://openairdocs.org/deregistered/N425US-2016-10-19/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 = 'N425US' AND deregistration_id = 'N425US-2016-10-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N425US-2016-10-19/reports

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