# Service difficulty reports: N351US, cancelled Oct 21, 2004

A list on [N351US, cancelled Oct 21, 2004](https://openairdocs.org/deregistered/N351US-2004-10-21.md).

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

- [SDR USAASB01287](https://openairdocs.org/sdr/USAASB01287.md): Uplock Sensor · defective · Oct 8, 2001 · N351US · Boeing 737301 · Landing Gear Position and Warning
  > PHL - FLT 8959 - AFTER TAKEOFF AND GEAR RETRACTION FROM MCO, EN ROUTE TO PHL, THE LEFT MAIN LANDING GEAR RED UNSAFE LIGHT ILLUMINATED STEADY, THEN INTERMITTENTLY AND THEN EXTINGUISHED. CREW RECYCLED GEAR AND GEAR INDICATION WAS NORMAL. FLIGHT CONTINUED ONTO
- [SDR USAASB01234](https://openairdocs.org/sdr/USAASB01234.md): Bolt · worn · Aug 18, 2001 · N351US · Boeing 737301 · Empennage Flight Control Surfaces, Attach Fittings
  > DCA - FLT 360 - ON CLIMB-OUT FROM DCA, EN ROUTE TO ROC, CREW FELT A RUMBLE/AIRFRAME VIBRATION THROUGHOUT THE CABIN. DUE TO PREVIOUS FILGHT SEGMENT EXPERIENCING THE SAME PROBLEM, FLIGHT RETURNED TO FIELD AT DCA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EME
- [SDR USAASB01222](https://openairdocs.org/sdr/USAASB01222.md): Transmitter · faulty · Aug 4, 2001 · N351US · Boeing 737301 · Trailing Flap Position Indicating System
  > ORD - FLT 537 - A TRAILING EDGE FLAP ASYMMETRY OCCURRED ON APPROACH TO ORD FROM CLT. LEFT FLAP INDICATED 1 UNIT WHILE RIGHT FLAP INDICATED 1.5 UNITS. CREW DECLARED AN EMERGENCY, ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES AND COMPLETED A FLAPS 1 LANDING WITHO
- [SDR USAASB01005](https://openairdocs.org/sdr/USAASB01005.md): Door · not closed · Jan 13, 2001 · N351US · Boeing 737301 · Service Doors
  > PHL - FLT 1228 - ON CLIMB-OUT FROM PHL, EN ROUTE TO CLT, CAPTAIN REPORTED THAT THE AIRCRAFT CABIN PRESSURE CONTINUED TO CLIMB ALONG WITH OUTSIDE PRESSURE. MIX VALVE APPEARS TO BE WORKING FINE. HOWEVER, FLIGHT ATTENDANT REPORTED THAT THE SEAL FOR THE AFT RIGH
- [SDR USAASB01002](https://openairdocs.org/sdr/USAASB01002.md): Indicator · failed · Jan 2, 2001 · N351US · Boeing 737301 · Leading Edge Slat Position Indicating System
  > PIT - FLT 1950 - ON DESCENT TO PIT, THE TRAILING EDGE FLAPS WOULD NOT EXTEND. AS CREW POSITIONED FLAPS TO ONE DEGREE FLAPS, THE LEFT FLAP INDICATOR STOPPED AT ONE QUARTER DEGREE WHILE THE RIGHT FLAP INDICTOR STOPED AT JUST LESS THAN ONE DEGREE. CREW ACCOMPLI
- [SDR USAASB00236](https://openairdocs.org/sdr/USAASB00236.md): Sensor · failed · Aug 30, 2000 · N351US · Boeing 737301 · Ground Proximity System
  > SAV - FLT 2382 - EN ROUTE FROM CLT TO SAV, AT FL220, THE CABIN BEGAN TO LOSE PRESS AND THE A/C EXPERIENCED SEVERAL INFLIGHT PROBLEMS WHICH SEEMED TO INDICATE AN AIR/GROUND SENSE FAULT. ACARS, TCAS, FLIGHT DIRECTOR, TRANSPONDER AND LNAV WERE AFFECTED. CAPTAIN
- [SDR USAA000654](https://openairdocs.org/sdr/USAA000654.md): Skin · cracked · May 1, 2000 · N351US · Boeing 737301 · Cargo/Baggage Doors
  > CLT - FOUND SKIN CRACKED.25 INCH, AFT UPPER RADIUS EXIT HANDLE CLOSEOUT. INSTALLED REPAIRED DOUBLER PER SRM 52-00-01 PAGE 203. (M)
- [SDR USAA000601](https://openairdocs.org/sdr/USAA000601.md): Frame · corroded · Apr 26, 2000 · N351US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND CHORD CORRODED 2 INCHES BY 4 INCHES, STATION 500 AND 500A CHORD ANGLE AT STRINGER 26R. INSTALLED REPAIR ANGLE PER EA 67007 AND SRM 51-70-12. CORROSION LEVEL 2. (M)
- [SDR USAA000602](https://openairdocs.org/sdr/USAA000602.md): Web · corroded · Apr 26, 2000 · N351US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CORRODED 2 INCHES BY 4 INCHES, STATION 500 AND 500A WEB ADJACENT TO STRINGER 26R. REPAIRED PER SRM 51-10-02. CORROSION LEVEL 2. (M)
- [SDR USAA000603](https://openairdocs.org/sdr/USAA000603.md): Floorbeam · corroded · Apr 26, 2000 · N351US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 344, LBL 42 - RBL 9 TOP OF FLOORBEAM. INSTALLED NEW SECTION PER SRM 51-40-02. (M)
- [SDR USAA000604](https://openairdocs.org/sdr/USAA000604.md): Floorbeam · corroded · Apr 26, 2000 · N351US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH, BS 328, RBL TO SERV DOOR SILL. INSTALLED NEW T-CAP PER SRM 53-10-51. (M)
- [SDR USAA000605](https://openairdocs.org/sdr/USAA000605.md): Stringer · cracked · Apr 26, 2000 · N351US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER CRACKED.5 INCH, STATION 500 AND 500A END OF STRINGER 26R. STRINGER REPAIR PER EA 67007 AND SRM 51-70-12. (M)
- [SDR USAA000606](https://openairdocs.org/sdr/USAA000606.md): Fitting · cracked · Apr 26, 2000 · N351US · Boeing 737301 · Horizontal Stabilizer Structure
  > CLT - FOUND FITTING/STABILIZER CRACKED 4.5 INCH, HORIZ STABILIZER CENTER SECTION AFT JACK SCREW. REMOVED AND REPLACED FITTING/STABILIZER PER SRM 51-10-02. (M)
- [SDR USAA000583](https://openairdocs.org/sdr/USAA000583.md): Stiffener · cracked · Apr 24, 2000 · N351US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND STIFFENER WITH TWO CRACKS 2 INCHES AND.5 INCHES, STATION 312 AND 314, RBL 32. REPLACED STIFFENER PER SRM 51-10-02. (M)
- [SDR USAA000584](https://openairdocs.org/sdr/USAA000584.md): Support Fitting · cracked · Apr 24, 2000 · N351US · Boeing 737301 · Main Landing Gear Attach Section
  > CLT - FOUND SUPPORT FITTING CRACKED.250 INCH, MLG BEAM SUPPORT FITTING OUTBOARD BOLT HOLE RT WING. REPAIRED PER TR 57-40-13. (M)
- [SDR USAA000585](https://openairdocs.org/sdr/USAA000585.md): Web · cracked · Apr 24, 2000 · N351US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CRACKED.5 INCH, AFT INBOARD RIVET IN WEB S 18AR SHELF STA 726, LBL 53. REPAIRED PER SRM 51-10-02. (M)
- [SDR USAA000586](https://openairdocs.org/sdr/USAA000586.md): Stringer · cracked · Apr 24, 2000 · N351US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER CRACKED.5 INCH, AFT INBOARD RIVET IN WEB S 18AR SHELF, STATION 726, RBL 53. REPAIRED PER SRM 51-10-02. (M)
- [SDR USAA000587](https://openairdocs.org/sdr/USAA000587.md): Tie Clip · cracked · Apr 24, 2000 · N351US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND TIE CLIP CRACKED.125 INCH, BS 663, STRINGER 10L. REPAIRED PER SRM 51-10-02. (M)
- [SDR USAA000588](https://openairdocs.org/sdr/USAA000588.md): Clip · cracked · Apr 24, 2000 · N351US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND CLIP CRACKED.125 INCH, BS 663, STRINGER 10R CLIP. REPAIRED PER SRM 51-10-02. (M)
- [SDR USAA000589](https://openairdocs.org/sdr/USAA000589.md): Skin · cracked · Apr 24, 2000 · N351US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 1 INCH, STATION 664, LBL 31. INSTALLED REPAIR PER TR 53-60-04. (M)
- [SDR USAA000590](https://openairdocs.org/sdr/USAA000590.md): Frame · cracked · Apr 24, 2000 · N351US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.25 INCH, LHG FUSE FRAME STATION 827 BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000591](https://openairdocs.org/sdr/USAA000591.md): Frame · cracked · Apr 24, 2000 · N351US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED 1 INCH, STATION 294.5, JUST ABOVE ZEE FORWARD SERVICE DOOR. INSTALLED REPAIR DOUBLER PER SRM 51-70-11. (M)
- [SDR USAA000592](https://openairdocs.org/sdr/USAA000592.md): Support Fitting · cracked · Apr 24, 2000 · N351US · Boeing 737301 · Main Landing Gear Attach Section
  > CLT - FOUND SUPPORT FITTING CRACKED.25 INCH, LEFT MLG BEAM SUPPORT FITTING. REPAIRED PER TR 57-40-13. (M)
- [SDR USAA000593](https://openairdocs.org/sdr/USAA000593.md): Strap · cracked · Apr 24, 2000 · N351US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND STABILIZER STRAP CRACKED 2 INCHES, STATION 312, RBL 46 BOTTOM OF FLOORBEAM. INSTALLED DOUBLER PER SRM 51-10-02. (M)
- [SDR USAA000594](https://openairdocs.org/sdr/USAA000594.md): Floorbeam · cracked · Apr 24, 2000 · N351US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND LOWER FLOORBEAM 1 INCH CRACKED, BL 0, STATION 312-328 LOWER FLOORBEAM SUPPORT. REPAIRED PER SRM 51-10-02. (M)
- [SDR USAA000564](https://openairdocs.org/sdr/USAA000564.md): Bulkhead · cracked · Apr 17, 2000 · N351US · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - FOUND SKIN CRACKED 1.5 INCHES, FORWARD BULKHEAD AT STATION 178.6, RBL 5. INSTALLED DOUBLER PER TR 53-10-07. (M)
- [SDR USAA000565](https://openairdocs.org/sdr/USAA000565.md): Frame · cracked · Apr 17, 2000 · N351US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.5 INCH, FORWARD UPPER SERVICE DOOR CUTOUT. REPAIRED PER SRM 51-10-02. (M)
- [SDR USAA000566](https://openairdocs.org/sdr/USAA000566.md): Bulkhead · cracked · Apr 17, 2000 · N351US · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - FOUND SKIN CRACKED 1 INCH, BL 0, WL 187, BULKHEAD 178. INSTALLED FILLER AND DOUBLER PER SRM 53-10-08. (M)
- [SDR USAA000567](https://openairdocs.org/sdr/USAA000567.md): Bulkhead · cracked · Apr 17, 2000 · N351US · Boeing 737301 · Fuselage Main, Bulkhead
  > CLT - FOUND WEB FOR BULKHEAD CRACKED 1 INCH, STATION 178 LBL 5, 9 INCHES BELOW FLOOR LEVEL. INSTALLED DOUBLER PER TR 53-10-07. (M)
- [SDR USAA000568](https://openairdocs.org/sdr/USAA000568.md): Frame · cracked · Apr 17, 2000 · N351US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.25 INCH, STATION 480 BETWEEN STRINGER 8L AND 9L LEFT FUSELAGE. REPAIR DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000570](https://openairdocs.org/sdr/USAA000570.md): Frame · cracked · Apr 17, 2000 · N351US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.25 INCH, STATION 827 BETWEEN STRINGER 8R AND 9R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)
- [SDR USAA000571](https://openairdocs.org/sdr/USAA000571.md): Frame · cracked · Apr 17, 2000 · N351US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.25 INCH, STATION 480 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14A. (M)
- [SDR USAA000569](https://openairdocs.org/sdr/USAA000569.md): Floorbeam · corroded · Apr 17, 2000 · N351US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOOR FRAME CORRODED 1 INCH, STATION 312, BL 0, RBL 8, RBL 36. INSTALLED NEW T-CAP PER SRM 53-10-51. (M)
- [SDR USAA000557](https://openairdocs.org/sdr/USAA000557.md): Skin · cracked · Apr 14, 2000 · N351US · Boeing 737301 · Passenger/Crew Doors
  > CLT - FOUND SKIN CRACKED.500 INCH, AFT ENTRY DOOR UPPER HINGE FITTING. INSTALLED DOUBLER PER TR 53-10-11. (M)
- [SDR USAA000530](https://openairdocs.org/sdr/USAA000530.md): Floorbeam · corroded · Apr 7, 2000 · N351US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED.5 INCH, STATION 1016, LBL 15 FLOORBEAM. INSTALLED REPAIR PER SRM 53-00-51 FIG 203. (M)
- [SDR USAASB99245](https://openairdocs.org/sdr/USAASB99245.md): Harness · failed · Oct 9, 1999 · N351US · Boeing 737301 · AC Generation System
  > ORD - FLT 1817 - EN ROUTE FROM PHL/MSP, CAPTAIN REPORTED THE NR 2 AND NR 3 TRANSFORMER RECTIFIERS HAD TRIPPED AND THE CAPTAIN'S WINDOW OVERHEAT LIGHT WAS ON. CAPTAIN RESET T/R'S, BUT THEY BOTH TRIPPED AGAIN. LOSS OF ELECTRIC TRIM, AUTOSPEED BRAKE AND RIGHT
- [SDR USAASB98177](https://openairdocs.org/sdr/USAASB98177.md): Valve · failed · Jul 10, 1998 · N351US · Boeing 737301 · Cabin Cooling System
  > CLT - FLT 1065 - AFTER TAKEOFF FROM CLT, THE AUTO PRESSURIZATION SYSTEM FAILED. CREW WAS UNABLE TO PRESSURIZE AIRCRAFT OR CONTROL CABIN IN STANDBY OR MANUAL OPERATION. DECISION WAS MADE TO RETURN TO FIELD AT CLT. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENC
- [SDR USAA980273](https://openairdocs.org/sdr/USAA980273.md): Skin · cracked · Jun 8, 1998 · N351US · Boeing 737301 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 1.75 INCH CRACK IN THE SKIN AFT OF THE EQUIPMENT EXHAUST AT STATION 380 BETWEEN STRINGER 28L AND BL 0. INSTALLED DOUBLER PER REPAIR DOCUMENT EA NR 44097. (M)
- [SDR USAASB98047](https://openairdocs.org/sdr/USAASB98047.md): Light · inoperative · Feb 24, 1998 · N351US · Boeing 737301 · Emergency Lighting
  > ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER SEAT ROW 10ABC WOULD NOT ILLUMINATE DURING OPERATIONAL TEST OF EMERGENCY LIGHTS. MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT WAS SHORTED. REMOVED AND REPLACED THE LIGHT ASSEMBLY, EXIT SIGN, BATTERY PACK AN
- [SDR 98ZZZM321](https://openairdocs.org/sdr/98ZZZM321.md): Charger · failed · Feb 24, 1998 · N351US · Boeing 737301 · Emergency Lighting
  > ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER SEAT ROW 10ABC WOULD NOT ILLUMINATE DURING OPERATIONAL TEST OF EMERGENCY LIGHTS. MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT WAS SHORTED. REMOVED AND REPLACED THE LIGHT ASSEMBLY, EXIT SIGN, BATTERY PACK AN
- [SDR 98ZZZM320](https://openairdocs.org/sdr/98ZZZM320.md): Battery Pack · discharged · Feb 24, 1998 · N351US · Boeing 737301 · Emergency Lighting
  > ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER SEAT ROW 10ABC WOULD NOT ILLUMINATE DURING OPERATIONAL TEST OF EMERGENCY LIGHTS. MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT WAS SHORTED. REMOVED AND REPLACED THE LIGHT ASSEMBLY, EXIT SIGN, BATTERY PACK AN
- [SDR 98ZZZM319](https://openairdocs.org/sdr/98ZZZM319.md): Sign · inoperative · Feb 24, 1998 · N351US · Boeing 737301 · Emergency Lighting
  > ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER SEAT ROW 10ABC WOULD NOT ILLUMINATE DURING OPERATIONAL TEST OF EMERGENCY LIGHTS. MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT WAS SHORTED. REMOVED AND REPLACED THE LIGHT ASSEMBLY, EXIT SIGN, BATTERY PACK AN
- [SDR USAASB97275](https://openairdocs.org/sdr/USAASB97275.md): Oven · dirty · Oct 5, 1997 · N351US · Boeing 737301 · Buffet/Galleys
  > MIA - FLT 2182 - AFTER TAKEOFF, THERE WAS A STRONG SMELL FOLLOWED BY VISIBLE BLACK SMOKE THAT CAME OUT OF THE COCKPIT DUCT VENTS. THE COCKPIT FILLED WITH ENOUGH SMOKE THAT THE CREW USED GOGGLES AND OXYGEN. THE SMOKE SMELLED LIKE SOMETHING BURNING IN THE GALL
- [SDR USAASB97253](https://openairdocs.org/sdr/USAASB97253.md): Battery Pack · discharged · Sep 14, 1997 · N351US · Boeing 737301 · Emergency Lighting
  > ALB - FOUND NUMEROUS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS AT POSITIONS 1, 2 AND 4. OPERATIONAL CHECKED OK. (M)
- [SDR USAA960474](https://openairdocs.org/sdr/USAA960474.md): Floor Beam · corrosion · Jun 14, 1996 · N351US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION ON TOP OF FLOORBEAM LOCATED AT STATION 986.5 RBL 12 AND RBL 14. INSTALLED NEW CHORD AND REPAIR ANGLES AS PER T/R 53-10-05. (M)

## 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 = 'N351US' AND deregistration_id = 'N351US-2004-10-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N351US-2004-10-21/reports

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