# Service difficulty reports: N585US, cancelled Sep 12, 2006

A list on [N585US, cancelled Sep 12, 2006](https://openairdocs.org/deregistered/N585US-2006-09-12.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 2 · 62 reports

- [SDR USAA050281](https://openairdocs.org/sdr/USAA050281.md): Door Frame · cracked · Feb 11, 2005 · N585US · Boeing 737301 · Cargo/Baggage Doors
  > PIT - FOUND DOOR WITH THREE.5 INCH CRACKS, AFT CARGO DOOR FORWARD FRAME. REMOVED AND REPLACED DOOR PER JOB CARD J3-57-52301. (M)
- [SDR USAA040413](https://openairdocs.org/sdr/USAA040413.md): Skin · cracked · Aug 7, 2004 · N585US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 1.25 INCH, BS 727D S-23R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229 DETAIL XI. (M)
- [SDR USAA040414](https://openairdocs.org/sdr/USAA040414.md): Skin · cracked · Aug 4, 2004 · N585US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 1.5 INCH, BS 727E S23L. INSTALLED DOUBLERS PER SRM 53-00-01 FIG 229. (M)
- [SDR USAA040232](https://openairdocs.org/sdr/USAA040232.md): Frame · cracked · May 3, 2004 · N585US · Boeing 737301 · Fuselage Main, Frame
  > FRAME CRCKED, 1 INCH LONG CRACK, STA 616 JUST BELOW STRINGER 17L. FABRICATED FILLER IAW T/R 53-62-01, 53-60-01 AND J NR 58-53503-004.
- [SDR USAA040200](https://openairdocs.org/sdr/USAA040200.md): Stringer · cracked · May 3, 2004 · N585US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > STRINGER (.2500 INCH X.1250 INCH CRACKS) CRACKED STA 908 AND STR 4R. REPLACED STRINGER SPLICE IAW SRM 51-20-02.
- [SDR USAA040182](https://openairdocs.org/sdr/USAA040182.md): Floorbeam · corroded · May 3, 2004 · N585US · Boeing 737301 · Fuselage Main, Floor Beam
  > PIT - FOUND FLOORBEAM CORRODED, STATION 986.5. CORROSION LEVEL 1, TASK NR C53-107-01. REPLACED INTERCOSTAL STRUCTURE BETWEEN STATION 986.5 AND 100.6 PER SRM 52-10-02. (M)
- [SDR USAA040181](https://openairdocs.org/sdr/USAA040181.md): Support Fitting · cracked · May 3, 2004 · N585US · Boeing 737301 · Wing, Landing Gear Attach Fittings
  > PIT - FOUND MLG SUPPORT FITTING CRACKED.5 INCH, RT MLG SUPPORT FITTING REAR SPAR OF RIGHT WING. REPLACED RIGHT MLG SUPPORT FITTING PER EA 78221. (M)
- [SDR USAA040179](https://openairdocs.org/sdr/USAA040179.md): Web · cracked · May 3, 2004 · N585US · Boeing 737301 · Fuselage Miscellaneous Structure
  > PIT - FOUND FLOOR WEB CRACKED 1 INCH AND 1.5 INCHES, BETWEEN STATION 559 AND 578 AT STRINGER 17L. REPLACED FLOOR WEB PER SRM 51-10-2. (M)
- [SDR USAA040180](https://openairdocs.org/sdr/USAA040180.md): Support Fitting · cracked · May 3, 2004 · N585US · Boeing 737301 · Wing, Landing Gear Attach Fittings
  > PIT - FOUND MLG SUPPORT FITTING CRACKED.25 INCH LONG, LEFT MLG SUPPORT FITTING REAR SPAR OF LEFT WING. REPLACED LEFT MLG SUPPORT FITTING PER EA 78221. (M)
- [SDR USAA040160](https://openairdocs.org/sdr/USAA040160.md): Stringer Splice · cracked · Apr 9, 2004 · N585US · Boeing 737301 · Fuselage Miscellaneous Structure
  > PIT - FOUND STRINGER SPLICE WITH TWO.125 INCH CRACKS, FS 907, S4R STRINGER SPLICE. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M)
- [SDR USAASB03153](https://openairdocs.org/sdr/USAASB03153.md): Control Unit · malfunctioned · Aug 25, 2003 · N585US · Boeing 737301 · Trailing Edge Flap Control System
  > AFTER TAKEOFF FROM TPA, CREW REPORTED UNABLE TO RETRACT FLAPS BEYOND 2 UNITS. CREW RECYCLED FLAP HANDLE AND FLAPS CIRCUIT BREAKER SEVERAL TIMES WITH NO HELP. FLIGHT RETURNED TO FIELD AT TPA WITH 2 UNITS FLAPS AND FULL SLATS. FLIGHT LANDED WITHOUT INCIDENT.
- [SDR USAASB03033](https://openairdocs.org/sdr/USAASB03033.md): Indicator · failed · Mar 2, 2003 · N585US · Boeing 737301 · Trailing Flap Position Indicating System
  > CLT - FLT 953 - ON APPROACH TO CLT FROM BOS, CREW REPORTED THAT WHEN FLAPS WERE EXTENDED TO 10 UNITS, THE RIGHT TRAILING EDGE FLAP STOPPED AT 6 UNITS. CREW EXTENDED GEAR AND ATTEMPTED TO MOVE THE FLAPS TO 15 UNITS BUT FLAPS WOULD NOT MOVE. CREW DISCONTINUED
- [SDR USAA020476](https://openairdocs.org/sdr/USAA020476.md): Skin · cracked · Dec 31, 2002 · N585US · Boeing 737301 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 2 INCHES, STATION 727 STRINGER 24L. CUT OUT DAMAGE, NDT'D AREA, INSTALLED DOUBLER AND TRIPLER PER SRM 53-00-01 FIG 201 AND TR 53-60-06. (M)
- [SDR USAASB02185](https://openairdocs.org/sdr/USAASB02185.md): Wire · broken · Oct 3, 2002 · N585US · Boeing 737301 · Light System Wiring
  > EWR - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT 1C INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UNDER SEATS 2A AND C. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA020370](https://openairdocs.org/sdr/USAA020370.md): Skin · cracked · Sep 26, 2002 · N585US · Boeing 737301 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN WITH TWO CRACKED.25 INCH LONG, STATION 380 BODYLINE 0 AT RIVET FASTENER. INSTALLED DOUBLER, ROUTED OUT CRACK PER TYPICAL REPAIR 53-30-07 AND EA 74918. (M)
- [SDR USA2002F00077](https://openairdocs.org/sdr/USA2002F00077.md): Wire · broken · Aug 3, 2002 · N585US · Boeing 737301 · Light System Wiring
  > MAINTENANCE FOUND THE EMERGENCY LIGHT ON SEAT ROW 13 ABC INOPERATIVE. MAINTENANCE REPAIRED WIRING AT SEAT ROW 13 ABC. OPERATIONAL CHECK NORMAL.
- [SDR USAASB02117](https://openairdocs.org/sdr/USAASB02117.md): Solenoid · faulty · Jun 17, 2002 · N585US · Boeing 737301 · Landing Gear Retraction/Extension System
  > SYR - FLT 251 - AFTER T/O FROM SYR, COULD NOT GET THE GEAR HANDLE TO MOVE PAST THE 'OFF' POSITION. CREW DID NOT OVERRIDE THE GEAR HANDLE BECAUSE OF A FLAPPING NOISE HEARD FROM THE NLG WW. FLT RETURNED TO FIELD AT SYR AND LANDED WITHOUT FURTHER INCIDENT. AFT
- [SDR USAA020134](https://openairdocs.org/sdr/USAA020134.md): Bulkhead · cracked · Apr 11, 2002 · N585US · Boeing 737301 · Fuselage Main, Bulkhead
  > TPA - FOUND BULKHEAD WEB CRACKED TWO PLACES 2.5 INCH EACH, FS 663.75, RBL 45, W/W FORWARD BULKHEAD WEB. INSTALLED TWO DOUBLERS PER EA 94296A. (M)
- [SDR USAA020133](https://openairdocs.org/sdr/USAA020133.md): Skin · cracked · Apr 9, 2002 · N585US · Boeing 737301 · Passenger/Crew Doors
  > TPA - FOUND SKIN CRACKED.25 INCH, LOWER AFT CORNER OF LOWER HINGE CUT OUT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 52-10-12. (M)
- [SDR USA2001F00006](https://openairdocs.org/sdr/USA2001F00006.md): Panel · departed · May 31, 2001 · N585US · Boeing 737301 · Wing, Plate/Skin
  > AFTER TAKEOFF, FLIGHT ENCOUNTERED COMPLETE LOSS OF SYSTEM A HYDRAULICS AND PRESSURE. LOST LG TRIANGULAR PANEL OFF TOP OF RT WING. NOSE GEAR WOULD RETRACT BUT MAIN GEAR WOULD NOT. HYDRAULIC LINE HAD BROKEN. PANEL DEPARTED AIRCRAFT AT END OF RUNWAY. CAPTAIN
- [SDR USAASB01046](https://openairdocs.org/sdr/USAASB01046.md): Indicator · failed · Feb 10, 2001 · N585US · Boeing 737301 · Leading Edge Slat Position Indicating System
  > BUF - FLT 638 - DURING DESCENT INTO BUF, CREW EXTENDED FLAPS TO 5 DEGREES AND THEN TO 10 DEGREES BUT RECEIVED A FLAP LIGHT. FLAPS WOULD NOT EXTEND BEYOND 5 DEGREES. CAPTAIN DECLARED AN EMERGENCY AND THE FLIGHT LANDED AT BUF WITHOUT FURTHER INCIDENT. MAINTEN
- [SDR USAASB00352](https://openairdocs.org/sdr/USAASB00352.md): Jackscrew · worn · Dec 20, 2000 · N585US · Boeing 737301 · Trailing Edge Flap Control System
  > CLT - FLT 1974 - ON DESCENT INTO CLT, FROM MBJ, CAPTAIN NOTIFIED TOWER THAT THE FLAPS WOULD NOT EXTEND BEYOND FIVE DEGREES. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MX T
- [SDR USAASB00314](https://openairdocs.org/sdr/USAASB00314.md): Flap · malfunctioned · Nov 14, 2000 · N585US · Boeing 737301 · Trailing Edge Flap Control System
  > BWI - FLT 2046 - ON APPROACH TO DCA, FROM MCI, THE TRAILING EDGE FLAPS STOPPED AT 8-10 DEGREES WITH NEEDLES SPLIT ON INDICATOR. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND DIVERTED TO BWI. FLIGHT LANDED AT 5 DEGREES TRAILING EDGE FLAPS AND WITHOUT
- [SDR USAASB00243](https://openairdocs.org/sdr/USAASB00243.md): Warning Light · illuminated · Sep 3, 2000 · N585US · Boeing 737301 · Trailing Flap Position Indicating System
  > PIT - FLT 1624 - ON CLIMB-OUT FROM PIT, THE LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED AS LEADING EDGE SLATS AND FLAPS DID NOT FULLY RETRACT. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE PERFOR
- [SDR USAASB00256](https://openairdocs.org/sdr/USAASB00256.md): Battery Pack · discharged · Aug 29, 2000 · N585US · Boeing 737301 · Emergency Lighting
  > RDU - WHILE ACCOMPLISHING OVERNIGHT CHECK, MAINTENANCE FOUND THE LEFT OVERHEAD EXIT LIGHTS, THE OVERWING DOOR EXIT LIGHTS, THE SEAT MOUNTED EXIT LIGHT AT OVERWING DOOR ROW AND ONE BULLNOSE EMERGENCY LIGHT OVER SEAT ROW 14, RIGHT SIDE, WOULD NOT HOLD CHARGE AFT
- [SDR USAASB00185](https://openairdocs.org/sdr/USAASB00185.md): Control Panel · failed · Jul 4, 2000 · N585US · Boeing 737301 · Cabin Pressure Indicator
  > PHL - FLT 637 - EN ROUTE FROM BOS-PHL, AT FL280, THE CABIN PRESSURE BEGAN TO SLOWLY CREEP UP TO 10,000 FEET. THE ALTITUDE WARNING HORN SOUNDED AND THE CREW BEGAN AN IMMEDIATE DESCENT. NO EMERGENCY WAS DECLARED AND NO OXYGEN MASKS WERE DEPLOYED. FLIGHT CONTI
- [SDR USAA000888](https://openairdocs.org/sdr/USAA000888.md): Frame · worn · Jun 20, 2000 · N585US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME WORN 3 INCHES WEAR AREA CAUSED BY APU DUCT CLAMP, STATION 1040. REPAIRED PER EA 67421/SRM 53-00-03. (M)
- [SDR USAA000878](https://openairdocs.org/sdr/USAA000878.md): Angle · cracked · Jun 20, 2000 · N585US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND CHORD ANGLE CRACKED 4 INCHES, STATION 1138, STRINGER 5R INSIDE UPPER STRAP CHORD ANGLE. FABRICATED REPAIR AND INSTALLED PER SRM 53-00-01 FIG 221. (M)
- [SDR USAA000868](https://openairdocs.org/sdr/USAA000868.md): Frame · cracked · Jun 19, 2000 · N585US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.5 INCHES, STATION 480, STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER AND FILLER PER TR 53-10-14A. (M)
- [SDR USAA000869](https://openairdocs.org/sdr/USAA000869.md): Frame · cracked · Jun 19, 2000 · N585US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.5 INCH, STATION 440, STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER AND FILLER PER TR 53-10-14A. (M)
- [SDR USAA000870](https://openairdocs.org/sdr/USAA000870.md): Frame · cracked · Jun 19, 2000 · N585US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.5 INCHES, STATION 500A, STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000871](https://openairdocs.org/sdr/USAA000871.md): Frame · cracked · Jun 19, 2000 · N585US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.5 INCH, STATION 400, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000858](https://openairdocs.org/sdr/USAA000858.md): Frame · cracked · Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.5 INCH, STATION 400, STRINGER 9L AT OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER SRM 53-10-14A. (M)
- [SDR USAA000859](https://openairdocs.org/sdr/USAA000859.md): Frame · cracked · Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.5 INCH, STATION 440, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000861](https://openairdocs.org/sdr/USAA000861.md): Frame · cracked · Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.5 INCH, STATION 727D, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000862](https://openairdocs.org/sdr/USAA000862.md): Frame · cracked · Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.5 INCH, STATION 747, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000863](https://openairdocs.org/sdr/USAA000863.md): Frame · cracked · Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED, STATION 747 STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000864](https://openairdocs.org/sdr/USAA000864.md): Frame · cracked · Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.5 INCH, STATION 787, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000865](https://openairdocs.org/sdr/USAA000865.md): Frame · cracked · Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.5 INCH, STATION 827, STRINGER 9L OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000866](https://openairdocs.org/sdr/USAA000866.md): Frame · cracked · Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME.5 INCH CRACKED, STATION 827, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000867](https://openairdocs.org/sdr/USAA000867.md): Frame · cracked · Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.5 INCH, STATION 867, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000860](https://openairdocs.org/sdr/USAA000860.md): Frame · cracked · Jun 16, 2000 · N585US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.5 INCHES, STATION 480, STRINGER 9R OVERHEAD BIN SUPPORT. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000848](https://openairdocs.org/sdr/USAA000848.md): Door Frame · cracked · Jun 14, 2000 · N585US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND FRAME CRACKED.125 INCH, FORWARD SERVICE DOOR JAMB FRAME UPPER FORWARD DOOR STOP FITTING. REMOVED AND REPLACED PART PER BOEING DWG 65-55878. (M)
- [SDR USAA000815](https://openairdocs.org/sdr/USAA000815.md): Bulkhead · cracked · Jun 12, 2000 · N585US · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - FOUND TWO CRACKS IN BULKHEAD.25 INCH AND.75 INCH, WL 201, LBL 5. FABRICATED AND INSTALLED REPAIR PART PER TR 53-10-08 FIG 209. (M)
- [SDR USAA000814](https://openairdocs.org/sdr/USAA000814.md): Angle · cracked · Jun 12, 2000 · N585US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND ANGLE CRACKED 1 INCH, LOWER FORWARD WING TO BS 540 ABOVE RT RAM AIR DUCT. INSTALLED DOUBLER PER TR 53-50-03. (M)
- [SDR USAA000884](https://openairdocs.org/sdr/USAA000884.md): Channel · cracked · Jun 4, 2000 · N585US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND U-CHANNEL CRACKED.375 INCH, STRINGER 18A SHAFT LEFT W/W PLUS 727. REPLACED STRINGER 18A SHELF. (M)
- [SDR USAA000885](https://openairdocs.org/sdr/USAA000885.md): Frame · corroded · Jun 3, 2000 · N585US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND 1 INCH CORROSION, STATION 807 BETWEEN STRINER 23R-24R. FABRICATED REPLACEMENT STIFFENER PER DWG 69-38178. CORROSION LEVEL 1, TASK NR C53-202-01. (M)
- [SDR USAA000883](https://openairdocs.org/sdr/USAA000883.md): Support Bracket · cracked · Jun 3, 2000 · N585US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND DOOR SUPPORT CRACKED 2 INCHES, LOWER CORNER AT FORWARD DOOR SUPPORT. INSTALLED DOUBLER PER SRM 51-70-11. (M)
- [SDR USAA000882](https://openairdocs.org/sdr/USAA000882.md): Drag Brace · cracked · Jun 3, 2000 · N585US · Boeing 737301 · Fuselage Main, Structure
  > CLT - FOUND DRAG BRACE ANGLE CRACKED.5 INCH, BS 536, STRINGER 21L. INSTALLED FABRICATED SUPPORT ANGLE SECTION PER TR 53-50-03. (M)
- [SDR USAA000887](https://openairdocs.org/sdr/USAA000887.md): Frame · cracked · Jun 2, 2000 · N585US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.5 INCH IN FRAME AT INBOARD RIVET HOLE, STATION 787, STRINGER 9L AT OVERHEAD BIN SUPPORT. INSTALLED REPAIR DOUBLER PER TR 53-10-14A. (M)

Next page: https://openairdocs.org/deregistered/N585US-2006-09-12/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 = 'N585US' AND deregistration_id = 'N585US-2006-09-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N585US-2006-09-12/reports

---
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