# Service difficulty reports: N562AU, cancelled May 17, 2006

A list on [N562AU, cancelled May 17, 2006](https://openairdocs.org/deregistered/N562AU-2006-05-17.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 2 · 65 reports

- [SDR USAASB02067](https://openairdocs.org/sdr/USAASB02067.md): Coalescer Bag · contaminated · Mar 29, 2002 · N562AU · Boeing 737301 · Humidity Control System
  > CLT - FLT 897 - AFTER TAKEOFF FROM EWR, EN ROUTE TO CLT, A FOUL ODOR WAS REPORTED COMING FROM THE AIR CONDITION PACKS. ODOR DISSIPATED WITHIN 10-15 MINUTES. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT AT CLT. MAINTENANCE REMOVED AND REPLACED THE LE
- [SDR USAASB01309](https://openairdocs.org/sdr/USAASB01309.md): Odor · detected · Nov 6, 2001 · N562AU · Boeing 737301 · Air Distribution System
  > CLT - FLT 2135 - AFTER TAKEOFF FROM CLT, EN ROUTE TO MCO, THE FLIGHT ATTENDANTS AND PASSENGERS REPORTED A STRONG SMELL OF BURNING PLASTIC. FLIGHT ATTENDANT REPORTED THAT THE ODOR WAS INTENSIFYING. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER IN
- [SDR USAASB00181](https://openairdocs.org/sdr/USAASB00181.md): Structure · cracked · Jun 29, 2000 · N562AU · Boeing 737301 · Elevator, Tab Structure
  > PIT - FLT 9234 - EN ROUTE FROM ROC-CMH, CAPTAIN REPORTED AN AIRFRAME VIBRATION WHICH WAS FELT IN THE AFT GALLEY/LAVATORY AREA. VIBRATION WAS OF HIGH FREQUENCY AND MODERATE FROM 5,000 TO 31,000 FEET BETWEEN 220 TO 300 KNOTS. CAPTAIN ACCOMPLISHED TROUBLESHOOTI
- [SDR USAA000607](https://openairdocs.org/sdr/USAA000607.md): Pan · corroded · Apr 26, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND FLOOR PAN CORRODED 4 INCHES BY 5 INCHES, STATION 1029, LBL 27 FLOOR PAN. FABRICATED NEW STRAP PER EA 67046. (M)
- [SDR USAA000608](https://openairdocs.org/sdr/USAA000608.md): Strap · corroded · Apr 26, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND STRAP CORRODED 3 INCHES BY 6 INCHES, STATION 1016-1006, LBL 27 STRAP. REPAIRED FABRICATED STRAP PER EA 67046. (M)
- [SDR USAA000609](https://openairdocs.org/sdr/USAA000609.md): Strap · corroded · Apr 26, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND STRAP CORRODED 6 INCHES BY 3 INCHES, STATION 1006-1016, BL 0, WL 208 STRAP. FABRICATED NEW H STRAP PER EA 67046. (M)
- [SDR USAA000599](https://openairdocs.org/sdr/USAA000599.md): Keelbeam · corroded · Apr 25, 2000 · N562AU · Boeing 737301 · Fuselage Main, Keel
  > CLT - FOUND KEELBEAM CORRODED 1 INCH BY 11 INCHES, STATION 500C PLUS 17 TO 500D PLUS 8 STRINGER 28R. INSTALLED DOUBLER PER EA66939. (M)
- [SDR USAA000598](https://openairdocs.org/sdr/USAA000598.md): Fitting · cracked · Apr 24, 2000 · N562AU · Boeing 737301 · Main Landing Gear Attach Section
  > CLT - FOUND FITTING CRACKED.375 INCH, LT MLG BEAM OUTBOARD ATTACH FITTING AT UPPER BOLT ON L/B. REPAIRED PER TR 57-40-13. (M)
- [SDR USAA000582](https://openairdocs.org/sdr/USAA000582.md): Keelbeam · corroded · Apr 18, 2000 · N562AU · Boeing 737301 · Fuselage Main, Keel
  > CLT - FOUND KEELBEAM CORRODED 2 INCHES BY 6 INCHES, RIGHT KEEL BEAM STATION 500C PLUS 17 TO 500D PLUS 8 STRINGER 28. INSTALLED SPLICE ANGLES PER EA 66939. (M)
- [SDR USAA000575](https://openairdocs.org/sdr/USAA000575.md): Strap · cracked · Apr 17, 2000 · N562AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN AND BEARSTRAP CRACKED 2 INCHES, LOWER AFT CORNER OF FORWARD SERVICE DOOR CUTOUT. REPAIRED PER SRM 53-10-01. (M)
- [SDR USAA000576](https://openairdocs.org/sdr/USAA000576.md): Frame · cracked · Apr 17, 2000 · N562AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.25 INCH, BS 480, STRINGER 9L. REPAIRED DOUBLER INSTALLED PER SRM 53-00-07 AND SRM 51-30-01. (M)
- [SDR USAA000577](https://openairdocs.org/sdr/USAA000577.md): Skin · corroded · Apr 17, 2000 · N562AU · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND FUSELAGE SKIN CORRODED,.75 INCH BY.75 INCH, BS 500C PLUS 10, LBL 18. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)
- [SDR USAA000561](https://openairdocs.org/sdr/USAA000561.md): Floorbeam · corroded · Apr 14, 2000 · N562AU · Boeing 737301 · Fuselage Main, Floor Beam
  > FOUND FLOORBEAM CORRODED.500 INCH, STATION 360 RBL 52 - RBL 72. INSTALLED T-CAP PER SRM 53-00-51 AND 51-70-11. CORROSION LEVEL 2 NR C53-107-01. (M)
- [SDR USAA000562](https://openairdocs.org/sdr/USAA000562.md): Floorbeam · corroded · Apr 14, 2000 · N562AU · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 3 INCHES BY 1 INCH, STATION 328, RBL 51 TOP SURFACE. INSTALLED T-CAP PER SRM 53-10-51. CORROSION LEVEL 2 NR C53-107-01. (M)
- [SDR USAA000554](https://openairdocs.org/sdr/USAA000554.md): Frame · cracked · Apr 13, 2000 · N562AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - FRAME CRACKED.75 INCH CRACK, FS 907 JUST LEFT OF STRINGER 1 FRAME. INSTALLED FILLER AND DOUBLER PER EA 66974. (M)
- [SDR USAA000555](https://openairdocs.org/sdr/USAA000555.md): Beam · corroded · Apr 13, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND BEAM CORRODED.5 INCH, STATION 1016, LBL 6 AND LBL 10 SCREW HOLES. REPAIRED PER TR 53-20-10 AND EA 66954. (M)
- [SDR USAA000538](https://openairdocs.org/sdr/USAA000538.md): Floorbeam · cracked · Apr 10, 2000 · N562AU · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM WEB CRACKED 4 PLACES.25 INCH, BS 328, RBL 44, WL 202.5 RIVET HOLES. REMOVED DAMAGED PER EA 66993. (M)
- [SDR USAA000539](https://openairdocs.org/sdr/USAA000539.md): Tie Clip · cracked · Apr 10, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, STATION 727B, STRINGER 4L. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA000540](https://openairdocs.org/sdr/USAA000540.md): Tie Clip · cracked · Apr 10, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, STATION 727B, STRINGER 5L. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA000541](https://openairdocs.org/sdr/USAA000541.md): Frame · cracked · Apr 10, 2000 · N562AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.500 INCH, BS 887, STRINGER 9L. REMOVED CRACK, INSTALLED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA000542](https://openairdocs.org/sdr/USAA000542.md): Angle · cracked · Apr 10, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND ANGLE CRACKED.5 INCH, BS 639, LBL 45, WL 203 VERT ATTACH ANGLE. REMOVED AND REPLACED ANGLE PER SRM 51-30-02 AND DWG 65-46540. (M)
- [SDR USAA000543](https://openairdocs.org/sdr/USAA000543.md): Angle · corroded · Apr 10, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND ANGLE CORRODED 1 INCH BY 15 INCHES, AFT ENT Z-CHANNEL ANGLE. REMOVED AND REPLACED Z-ANGLE PER SRM 51-40-02. (M)
- [SDR USAA000537](https://openairdocs.org/sdr/USAA000537.md): Frame · corroded · Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CORRODED 2 INCHES, STATION 500D, LBL 18 SKIN. INSTALLED DOUBLER, T-ANGLE AND SHIM PER SRM 53-00-07. (M)
- [SDR USAA000531](https://openairdocs.org/sdr/USAA000531.md): Bulkhead · cracked · Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - FOUND WEB CRACKED.5 INCH, STATION 178, BULKHEAD WEB RBL 4.75, WL 201. INSTALLED DOUBLER PER SRM 53-10-08. (M)
- [SDR USAA000532](https://openairdocs.org/sdr/USAA000532.md): Bulkhead · cracked · Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - FOUND WEB CRACKED.5 INCH, STATION 178 BULKHEAD WEB LBL 4.75, WL 201. INSTALLED DOUBLER. (M)
- [SDR USAA000533](https://openairdocs.org/sdr/USAA000533.md): Bulkhead · cracked · Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - FOUND WEB CRACKED.5 INCH, STATION 178 BULKHEAD WEB LBL 4.75, WL 198. INSTALLED DOUBLER PER SRM 53-10-08. (M)
- [SDR USAA000534](https://openairdocs.org/sdr/USAA000534.md): Bulkhead · cracked · Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - FOUND WEB CRACKED.5 INCH, STATION 178 BULKHEAD WEB RBL 4.75, WL 198. INSTALLED DOUBLER PER SRM 53-10-08. (M)
- [SDR USAA000535](https://openairdocs.org/sdr/USAA000535.md): Stiffener · cracked · Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND VERTICAL STIFFENER CRACKED 1 INCH, STATION 178 BULKHEAD VERTICAL STIFFENER LBL 6, WL 184. INSTALLED DOUBLER AND ANGLES PER SRM 53-10-08. (M)
- [SDR USAA000536](https://openairdocs.org/sdr/USAA000536.md): Bulkhead · cracked · Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - FOUND WEB CRACKED.25 INCH LONG, STATION 178 BULKHEAD WEB RBL 1, WL 206. INSTALLED DOUBLER PER SRM 53-10-08. (M)
- [SDR USAA000528](https://openairdocs.org/sdr/USAA000528.md): Web · cracked · Apr 5, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED.25 INCH, BS 710-717, BBL 0, WL 203. INSTALLED DOUBLER PER SRM 51-70-13. (M)
- [SDR USAA000520](https://openairdocs.org/sdr/USAA000520.md): Skin · cracked · Apr 4, 2000 · N562AU · Boeing 737301 · Service Doors
  > CLT - FOUND DOOR SKIN CRACKED 5 INCHES BY 5 INCHES, FORWARD SERVICE DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 52-00-01 FIG 203. (M)
- [SDR USAA000523](https://openairdocs.org/sdr/USAA000523.md): Channel · corroded · Apr 4, 2000 · N562AU · Boeing 737301 · Service Doors
  > CLT - FOUND Z-CHANNEL CORRODED, AFT SERVICE DOOR. REPLACED WITH NEW Z-CHANNEL PER SRM 51-4-02. (M)
- [SDR USAA000524](https://openairdocs.org/sdr/USAA000524.md): Angle · corroded · Apr 4, 2000 · N562AU · Boeing 737301 · Passenger/Crew Doors
  > CLT - FOUND DOOR Z-ANGLE CORRODED 6 FT BY 3 INCHES, STATION 947-1006, LBL 60, AFT ENTRY DOOR Z-ANGLE. INSTALLED NEW Z-ANGLE PER SRM 51-40-02. (M)
- [SDR USAA000522](https://openairdocs.org/sdr/USAA000522.md): Stringer · cracked · Apr 4, 2000 · N562AU · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER CRACKED.5 INCH, STRINGER 18 SHELF AT AFT END INBOARD RIVET IN WEB. REPLACED PER SRM 51-10-02. (M)
- [SDR USAA000521](https://openairdocs.org/sdr/USAA000521.md): Frame · cracked · Apr 4, 2000 · N562AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.75 INCHES LONG, BOTTOM END OF STATION 616 INBOARD CHORD ANGLE RIGHT SIDE. FABRICATED ANGLE AND FILLER PER TR 53-62-01. (M)
- [SDR USAA000508](https://openairdocs.org/sdr/USAA000508.md): Stringer Clip · cracked · Mar 30, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, STATION 727A, STRINGER 2R TIE CLIP AFT SIDE. REPLACED TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA000509](https://openairdocs.org/sdr/USAA000509.md): Stringer Clip · cracked · Mar 30, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND STRINGER TIE CLIP WITH TWO CRACKS.5 INCH LONG, STATION 639, STRINGER 4R FUSELAGE FRAME. REPLACED TIE CLIP PER SRM 51-10-02 AND 51-40-02. (M)
- [SDR USAA000510](https://openairdocs.org/sdr/USAA000510.md): Door Frame · cracked · Mar 30, 2000 · N562AU · Boeing 737301 · Fuselage Main, Structure
  > CLT - FOUND FRAME CRACKED.25 INCH, FORWARD SERVICE DOOR FRAME LOWER FORWARD CORNER. INSTALLED DOUBLER AND FILLER PER SRM 51-10-11. (M)
- [SDR USAA000512](https://openairdocs.org/sdr/USAA000512.md): Bulkhead · cracked · Mar 30, 2000 · N562AU · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - FOUND.5 INCH CRACK IN BULKHEAD, STATION 178, WEB LBL.75, WL 188. INSTALLED DOUBLER REPAIR PER SRM 53-10-08. (M)
- [SDR USAA000507](https://openairdocs.org/sdr/USAA000507.md): Frame · cracked · Mar 30, 2000 · N562AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.250 INCH, STATION 827, STRINGER 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA000506](https://openairdocs.org/sdr/USAA000506.md): Floorbeam · corroded · Mar 30, 2000 · N562AU · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 986, RBL 14 UPPER CHORD FLOORBEAM. REPLACED NEW T-CAP PER TR 53-10-05A. (M)
- [SDR USAA000490](https://openairdocs.org/sdr/USAA000490.md): Floorbeam · corroded · Mar 29, 2000 · N562AU · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 344 AT BL 0, LBL 22. CORROSION LEVEL 1. INSTALLED FLOORBEAM TOP CAP PER SRM 51-70-12. (M)
- [SDR USAA000491](https://openairdocs.org/sdr/USAA000491.md): Beam · corroded · Mar 29, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND BEAM CORRODED.5 INCH BY.5 INCH, BS 1006, LBL 10 BEAM SCREW HOLES. REPAIRED DOUBLER PER SRM 53-00-51. (M)
- [SDR USAA000492](https://openairdocs.org/sdr/USAA000492.md): Seat Track · corroded · Mar 29, 2000 · N562AU · Boeing 737301 · Fuselage, Seat/Cargo Attach Fittings
  > CLT - FOUND SEAT TRACK CORRODED 2 INCHES BY 2 INCHES, STATION 344, LBL 25. INSTALLED NEW SEAT TRACK PER SRM 53-00-52. (M)
- [SDR USAA000464](https://openairdocs.org/sdr/USAA000464.md): Stringer Clip · cracked · Mar 27, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.25 INCH, STATION 727B, STRINGER 16. REMOVED AND REPLACED WITH NEW TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA000465](https://openairdocs.org/sdr/USAA000465.md): Beam · corroded · Mar 27, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND BEAM CORRODED.5 INCH, STATION 967, LBL 5 UPPER CHORD SCREW HOLE BEAM. INSTALLED T-CAP PER SRM 53-00-51. CORROSION LEVEL 1. (M)
- [SDR USAA000469](https://openairdocs.org/sdr/USAA000469.md): Frame · cracked · Mar 27, 2000 · N562AU · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND CHORD CRACKED.5 INCH, BS 616, WL 202 RIGHT SIDE INNER FRAME CHORD AT LOWER FAST. REPAIRED DOUBLER PER TR 53-62-01. (M)
- [SDR USAA000453](https://openairdocs.org/sdr/USAA000453.md): Angle · cracked · Mar 24, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND CHORD ANGLE CRACKED.350 INCH, BS 291.5 BETWEEN STRINGER 10R AND 11R. REPAIRED PER SRM 51-40-02. (M)
- [SDR USAA000454](https://openairdocs.org/sdr/USAA000454.md): Stringer Clip · cracked · Mar 24, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.250 INCH, BS 663 STRINGER 10L. REPAIRED PER SRM 51-10-02. (M)
- [SDR USAA000455](https://openairdocs.org/sdr/USAA000455.md): Stringer Clip · cracked · Mar 24, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.500 INCH, BS 887, STRINGER 1. REPAIRED PER SRM 51-40-02 AND 51-10-00. (M)

Next page: https://openairdocs.org/deregistered/N562AU-2006-05-17/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 = 'N562AU' AND deregistration_id = 'N562AU-2006-05-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N562AU-2006-05-17/reports

---
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