# Service difficulty reports: N353US, cancelled Sep 6, 2006

A list on [N353US, cancelled Sep 6, 2006](https://openairdocs.org/deregistered/N353US-2006-09-06.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 · 97 reports

- [SDR SB06007](https://openairdocs.org/sdr/SB06007.md): Light · inoperative · Jan 22, 2006 · N353US · Boeing 737301 · Emergency Lighting
  > MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT ROW 20, LEFT-HAND SIDE, INOPERATIVE. MAINTENANCE FOUND THE EMERGENCY LIGHT BASE ASSEMBLY BAD. REPAIRED BASE ASSEMBLY. OPERATIONAL CHECK GOOD.
- [SDR SB06006](https://openairdocs.org/sdr/SB06006.md): Wire · broken · Jan 22, 2006 · N353US · Boeing 737301 · Light System Wiring
  > MAINTENANCE REPORTED THE EMERGENCY LIGHTS ON SEAT ROWS 12 THRU 16, LEFT-HAND SIDE, INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE UNDER SEAT ROW 12, LEFT-HAND SIDE. OPERATIONAL CHECK GOOD.
- [SDR SB06002](https://openairdocs.org/sdr/SB06002.md): Light · inoperative · Jan 10, 2006 · N353US · Boeing 737301 · Emergency Lighting
  > CLT - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT ROW 20 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.
- [SDR USAA051554](https://openairdocs.org/sdr/USAA051554.md): Skin · dented · Dec 14, 2005 · N353US · Boeing 737301 · Fuselage Main, Plate/Skin
  > LOCATION: BETWEEN B STA 847 AND 867 ABOVE STRINGER S-20L. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-00-01 REPAIR 31 DETAIL 10, 19, DEFECT SIZE: 1.0 IN.
- [SDR USAA051503](https://openairdocs.org/sdr/USAA051503.md): Skin · chafed · Dec 12, 2005 · N353US · Boeing 737301 · Fuselage Main, Plate/Skin
  > FOUND CHAFING STA 860-880 S1L-S1R. INSTALLED DOUBLER IAW EA 97199, DEFECT SIZE: 14" AND 11".
- [SDR SB05150](https://openairdocs.org/sdr/SB05150.md): Battery Pack · discharged · Nov 20, 2005 · N353US · Boeing 737301 · Emergency Lighting
  > FLL - MAINTENANCE REPORTED THE AFT EMERGENCY LIGHT BATTERY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTERY. OPERATIONAL CHECK GOOD.
- [SDR SB05109](https://openairdocs.org/sdr/SB05109.md): Indicator · faulty · Sep 4, 2005 · N353US · Boeing 737301 · Trailing Flap Position Indicating System
  > ORD - FLT551 - ON APPROACH TO ORD, CREW EXTENDED FLAPS FROM 5 TO 10 UNITS AND A SPLIT FLAP INDICATION OF L-5 AND R-10 WAS DISPLAYED. FLAPS LOCKED OUT. CREW ACCOMPLISHED A GO-AROUND AND ON SUBSEQUENT APPROACH, FLAPS OPERATED NORMAL. FLIGHT LANDED WITHOUT FURT
- [SDR SB05103](https://openairdocs.org/sdr/SB05103.md): Light · inoperative · Aug 30, 2005 · N353US · Boeing 737301 · Emergency Lighting
  > CLT - MAINTENANCE REPORTED THE CABIN SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 13 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.
- [SDR SB05102](https://openairdocs.org/sdr/SB05102.md): Connector · disconnected · Aug 30, 2005 · N353US · Boeing 737301 · Light System Wiring
  > CLT - MAINTENANCE REPORTED THE CABIN MOUNTED EMERGENCY LIGHTS FROM SEAT ROWS 12 THRU 16 WERE INOPERATIVE. MAINTENANCE SECURED A CONNECTOR BENEATH SEAT ROW 12. OPERATIONAL CHECK GOOD.
- [SDR USAA200508002](https://openairdocs.org/sdr/USAA200508002.md): Pressure Panel · cracked · Aug 13, 2005 · N353US · Boeing 737301 · Fuselage Main, Bulkhead
  > A.75 INCH CRACK FOUND IN LT MLG WHEEL WELL PRESSURE FLOOR WEB STA 665/LBL 30. INSTALLED DOUBLER PER TYPICAL REPAIR 53-60-04A & EA 81311.
- [SDR SB05081](https://openairdocs.org/sdr/SB05081.md): Door Seal · out of position · Jul 11, 2005 · N353US · Boeing 737301 · Cargo/Baggage Doors
  > DURING CRUISE, AT APPROX FL320, CABIN PRESSURE WENT TO 10,000 FT WITH CABIN ALT WARNING HORN SOUNDING. CREW ACCOMP EMERGENCY DESCENT TO 10,000 FT AND RETURNED TO FIELD. FLT LANDED W/O FURTHER INCIDENT. NO OXYGEN MASKS WERE DEPLOYED. FLT WAS MX FERRIED FOR
- [SDR SB05045](https://openairdocs.org/sdr/SB05045.md): Light · inoperative · Apr 5, 2005 · N353US · Boeing 7373B7 · Emergency Lighting
  > PIT LEFT AFT GALLEY EMERGENCY LIGHT FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY.
- [SDR SB05016](https://openairdocs.org/sdr/SB05016.md): Light · failed · Jan 26, 2005 · N353US · Boeing 737301 · Flight Compartment Lighting
  > CLT - FLT1435 - DURING DESCENT INTO CLT FROM ORD, CREW REPORTED SMOKE ENTERING COCKPIT FROM BEHIND FIRST OFFICER "PULL UP" ANNUNCIATOR LIGHT ON FIRST OFFICER'S INSTRUMENT PANEL. ALSO, ALL LIGHTS ASSOCIATED WITH THE LIGHT TEST SWITCH ILLUMINATED. MOVING TEST
- [SDR USAA050058](https://openairdocs.org/sdr/USAA050058.md): Skin · cracked · Jan 13, 2005 · N353US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 1 INCH, STATION 727D AT STRINGER 23L. INSTALLED DOUBLER IAW SRM 53-00-01. (M)
- [SDR USAA040842](https://openairdocs.org/sdr/USAA040842.md): Skin · cracked · Nov 5, 2004 · N353US · Boeing 737301 · Fuselage Main, Plate/Skin
  > SKIN, 2 INCH CRACK (SHEAR WRINKLE), STA 727D AT STR 23R. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 229.
- [SDR SB04135](https://openairdocs.org/sdr/SB04135.md): Control Panel · faulty · Sep 28, 2004 · N353US · Boeing 737301 · Autopilot System
  > DURING A HEADING CHANGE, THE AUTOPILOT ROLLED THE AIRCRAFT INTO A 40 DEGREE BANK BEFORE THE PILOT COULD DISCONNECT IT. MAINTENANCE REPLACED THE MODE CONTROL PANEL.
- [SDR SB04132](https://openairdocs.org/sdr/SB04132.md): Iru · out of alignment · Sep 26, 2004 · N353US · Boeing 737301 · Inertial Guidance System
  > PVD - FLT491 - DURING TAKEOFF FROM PVD, THE ATTITUDE FLAG CAME INTO VIEW. BOTH THE FMC AND PMC WERE INOPERATIVE AND ON MEL AT THE TIME. FLIGHT RETURNED TO FIELD AT PVD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REALIGNED BO
- [SDR SB04130](https://openairdocs.org/sdr/SB04130.md): Control Panel · faulty · Sep 21, 2004 · N353US · Boeing 737301 · Autopilot System
  > DURING CRUISE, EN ROUTE FROM PHL TO DFW, CREW REPORTED THE CHANNEL A AUTOPILOT DROPPED OFF FOLLOWED BY THE AUTOPILOT MODE CONTROL WINDOW DISPLAYING 50,000 FEET. THE LEFT NAV THEN DROPPED OFF LINE. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT.
- [SDR USAA040050](https://openairdocs.org/sdr/USAA040050.md): Skin · cracked · Feb 20, 2004 · N353US · Boeing 737301 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRACKED 2.5 INCHES, BS 520 S12R. INSTALLED DOUBLER PER EA 95192. (M)
- [SDR USAASB03220](https://openairdocs.org/sdr/USAASB03220.md): Switch · failed · Dec 23, 2003 · N353US · Boeing 737301 · Cabin Cooling System
  > PHL - FLT 579 - AFTER TAKEOFF FROM PHL, EN ROUTE TO IND, RT PACK WOULD NOT PRESSURIZE THE AIRCRAFT. LT PACK WAS ALREADY ON MEL 21-1A. CAPTAIN ELECTED TO RETURN TO FIELD AT PHL. LANDED WITHOUT INCIDENT. NO EMERGENCY DECLARED. MAINTENANCE OPERATIONALLY CHEC
- [SDR USAASB03219](https://openairdocs.org/sdr/USAASB03219.md): Connector · inoperative · Dec 22, 2003 · N353US · Boeing 737301 · Emergency Lighting
  > MAINTENANCE REPORTED THE SEAT EMERGENCY LIGHTS, AT ROWS 12 THROUGH 16, INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR AT SEAT ROW 12 LOOSE. RESEATED CONNECTOR. OPS CHECK GOOD. (M)
- [SDR USAA030186](https://openairdocs.org/sdr/USAA030186.md): Skin · cracked · Sep 8, 2003 · N353US · Boeing 737301 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRACKED 1.250 INCH, FUSELAGE SKIN FS 727E JUST ABOVE S23L. INSTALLED DOUBLER PER SRM 53-00-01. (M)
- [SDR USAA030185](https://openairdocs.org/sdr/USAA030185.md): Skin · cracked · Sep 8, 2003 · N353US · Boeing 737301 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRACKED.750 INCH, FUSELAGE SKIN FS 727D AT S23R. INSTALLED DOUBLER PER EA 94676. (M)
- [SDR USAASB03136](https://openairdocs.org/sdr/USAASB03136.md): Uplock Sensor · failed · Aug 11, 2003 · N353US · Boeing 737301 · Landing Gear Position and Warning
  > PHL - FLT 1948 - AFTER TAKEOFF AND GEAR RETRACTION FROM PHL, THE RIGHT MAIN LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE IN UP OR OFF POSITION. CREW CYCLED THE GEAR DOWN AND RECEIVED ALL THREE GREEN LIGHTS. CREW DECIDED TO RETURN TO FI
- [SDR USAASB03097](https://openairdocs.org/sdr/USAASB03097.md): Wire · inoperative · Jul 2, 2003 · N353US · Boeing 737301 · Light System Wiring
  > PHL - PILOT REPORTED THE EMERGENCY LIGHT AT SEAT 5C INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT SEAT 5C. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB03017](https://openairdocs.org/sdr/USAASB03017.md): Window · cracked · Feb 2, 2003 · N353US · Boeing 737301 · Flight Compartment Windows
  > CLT - FLT 1122 - DURING CRUISE, EN ROUTE FROM PIT TO ATL, THE FIRST OFFICERS SLIDING WINDOW CRACKED. FLGIHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS SLIDING WINDOW PER
- [SDR USAASB03007](https://openairdocs.org/sdr/USAASB03007.md): Sensor · out of adjust · Jan 13, 2003 · N353US · Boeing 737301 · Landing Gear Position and Warning
  > PIT - FLT 1228 - AFTER TAKEOFF FROM MKE, CREW WAS UNABLE TO RETRACT THE LANDING GEAR WITH NORMAL GEAR HANDLE MOVEMENT. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND USED THE LANDING GEAR OVERRIDE LEVER TO RAISE THE GEAR. FLIGHT CONTINUED TO PIT AND L
- [SDR USAASB01345](https://openairdocs.org/sdr/USAASB01345.md): Battery Pack · discharged · Dec 20, 2001 · N353US · Boeing 737301 · Emergency Lighting
  > CLT - MAINTENANCE FOUND THE END BAY EMERGENCY LIGHT AT THE AFT SEAT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT BATTERY PACK. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB00348](https://openairdocs.org/sdr/USAASB00348.md): Gcu · loose · Dec 14, 2000 · N353US · Boeing 737301 · AC Regulator
  > MSY - FLT 796 - PRIOR TO DEPARTURE, THE RT GENERATOR WAS PLACED ON MEL BECAUSE IT WOULD NOT COME ON LINE. SHORTLY AFTER TAKEOFF FROM MSY, THE APU FAILED TO POWER THE RIGHT SIDE, THEN THE TRANSFER BUS FAILED. FLIGHT RETURNED TO FIELD AT MSY AND LANDED WITHOUT
- [SDR USAA001230](https://openairdocs.org/sdr/USAA001230.md): Angle · cracked · Aug 10, 2000 · N353US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND ANGLE CRACKED.5 INCH, STATION 178 VERTICAL STIFFENING BEAM LBL 5.5, WL 184. INSTALLED REPAIR ANGLE PER SRM 53-10-08. (M)
- [SDR USAA001229](https://openairdocs.org/sdr/USAA001229.md): Angle · cracked · Aug 10, 2000 · N353US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND ANGLE CRACKED.5 INCH, STATION 178 VERTICAL STIFFENING BEAM LBL 6, WL 184. INSTALLED REPAIR ANGLES PER SRM 53-10-08. (M)
- [SDR USAA001235](https://openairdocs.org/sdr/USAA001235.md): Door Frame · corroded · Aug 10, 2000 · N353US · Boeing 737301 · Fuselage Main, Structure
  > CLT - FOUND DOOR FRAME CORRODED.25 INCH, RBL 24, FS 793 FORWARD LOWER DOOR FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 201 AND SRM 51-70-11. (M)
- [SDR USAA001234](https://openairdocs.org/sdr/USAA001234.md): Intercostal · corroded · Aug 10, 2000 · N353US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND CORROSION ON INTERCOSTAL 1 INCH BY 18 INCHES, FS 767-787 AT STRINGER 25R. REPLACED INTERCOSTAL PER SRM 51-10-2. (M)
- [SDR USAA001220](https://openairdocs.org/sdr/USAA001220.md): Skin · cracked · Aug 8, 2000 · N353US · Boeing 737301 · Nacelle/Pylon, Plate/Skin
  > CLT - FOUND PYLON SKIN CRACKED 1 INCH, STATION 260, WL 132 INBOARD PYLON SKIN PANEL 5724L. INSTALLED DOUBLER PER TR 54-50-07, EA 67725 AND EA 67746. (M)
- [SDR USAA001219](https://openairdocs.org/sdr/USAA001219.md): Beam · cracked · Aug 8, 2000 · N353US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND SHEAR BEAM SHELF CRACKED.75 INCH, STRINGER 18A SHEAR BEAM WEB STATION 726, LBL 60.5, WL 188. INSTALLED NEW SHELF PER EA 67690 DWG 65 46877. (M)
- [SDR USAA001218](https://openairdocs.org/sdr/USAA001218.md): Track · corroded · Aug 8, 2000 · N353US · Boeing 737301 · Fuselage, Seat/Cargo Attach Fittings
  > CLT - FOUND TIE DOWN TRACK CORRODED 6 INCHES BY 2 INCHES, FS 787 TO 947 TRACK TIE DOWN, RBL 13. REMOVED AND REPLACED PER SRM 53-00-53. (M)
- [SDR USAA001152](https://openairdocs.org/sdr/USAA001152.md): Skin · corroded · Aug 4, 2000 · N353US · Boeing 737301 · Passenger/Crew Doors
  > CLT - FOUND INNER DOOR SKIN CORRODED 1 INCH BY 4 INCH AREA, FS 847 STRINGER 25R. CORROSION LEVEL 1. REMOVED AND REPLACED PER SRM 53-00-07 AND SRM 51-40-02. (M)
- [SDR USAA001151](https://openairdocs.org/sdr/USAA001151.md): Door Frame · corroded · Aug 4, 2000 · N353US · Boeing 737301 · Fuselage Main, Structure
  > CLT - FOUND FRAME CORRODED 2 INCHES BY 6 INCHES, STATION 787 PLUS 6 AFT CARGO DOOR FRAME. CORROSION LEVEL 1, C53-208-01. INSTALLED DOUBLER PER SRM 51-70-11 AND 53-00-07 FIG 201. (M)
- [SDR USAA001150](https://openairdocs.org/sdr/USAA001150.md): Door Frame · corroded · Aug 4, 2000 · N353US · Boeing 737301 · Fuselage Main, Structure
  > CLT - FOUND FRAME CORRODED 2 INCHES BY 5 INCHES, FORWARD SERVICE DOOR AFT FRAME BELOW FLOOR LEVEL. CORROSION LEVEL 1, C53-107-02. REMOVED AND REPLACED Z-ANGLE PER DWG 65 45875. (M)
- [SDR USAA001156](https://openairdocs.org/sdr/USAA001156.md): Frame · cracked · Aug 4, 2000 · N353US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME WEB CRACKED.25 INCH, STATION 807 STRINGER 9RT. INSTALLED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA001155](https://openairdocs.org/sdr/USAA001155.md): Frame · cracked · Aug 4, 2000 · N353US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME WEB CRACKED.25 INCH, STATION 887 FRAME WEB STRINGER 9 RT. INSTALLED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA001154](https://openairdocs.org/sdr/USAA001154.md): Frame · cracked · Aug 4, 2000 · N353US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME WEB CRACKED.25 INCH, STATION 847 FRAME WEB STRINGER 9 LT. INSTALLED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA001153](https://openairdocs.org/sdr/USAA001153.md): Frame · cracked · Aug 4, 2000 · N353US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME WEB CRACKED.25 INCH, STATION 827 FRAME WEB STRINGER 9 LT. INSTALLED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA001142](https://openairdocs.org/sdr/USAA001142.md): Frame · cracked · Aug 2, 2000 · N353US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.25 INCH, UPPER FORWARD CORNER FORWARD SERVICE DOOR CUTOUT. REMOVED AND REPLACED DAMAGE PART PER SRM 51-10-02. (M)
- [SDR USAA001120](https://openairdocs.org/sdr/USAA001120.md): Stringer · corroded · Aug 1, 2000 · N353US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER CORRODED 2 INCHES, STATION 969, STRINGER 29L. CORROSION LEVEL 1. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-03. (M)
- [SDR USAA001119](https://openairdocs.org/sdr/USAA001119.md): Shear Tie · corroded · Aug 1, 2000 · N353US · Boeing 737301 · Fuselage Main, Structure
  > CLT - FOUND FRAME SHEAR TIE CORRODED 1 INCH BY 2 INCHES, FRAME 947 OUTBOARD OF STRINGER 27L. REPLACED SHEAR TIE PER 51-10-02. CORROSION LEVEL 1. (M)
- [SDR USAA001118](https://openairdocs.org/sdr/USAA001118.md): Frame · corroded · Aug 1, 2000 · N353US · Boeing 737301 · Fuselage Main, Frame
  > CLT - FOUND CORROSION 5 INCHES BY 8 INCHES, STATION 727 BETWEEN STRINGER 27R AND 27L. CORROSION LEVEL 1 C53-208-01. REPLACED CHORD ANGLE PER SRM 53-00-01. (M)
- [SDR USAA001117](https://openairdocs.org/sdr/USAA001117.md): Floorbeam · corroded · Aug 1, 2000 · N353US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM CORRODED 15 INCHES, STATION 344 FROM RBL 2 TO LBL 13 FLOOR LEVEL. REPLACED T-CAP PER SRM 53-10-51. CORROSION LEVEL 1. (M)
- [SDR USDAA001116](https://openairdocs.org/sdr/USDAA001116.md): Floor Support · cracked · Aug 1, 2000 · N353US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - FOUND FLOOR SUPPORT WITH 3 INCH CRACKS, STATION 380-400, 0 BBL. REPLACED FLOOR SUPPORT PER REPAIR 51-10-02. (M)
- [SDR USAA001115](https://openairdocs.org/sdr/USAA001115.md): Stringer · cracked · Aug 1, 2000 · N353US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER FLANGE.375, STATION 360, STRINGER 14L. REPLACED STRINGER SPLICE PER DWG 65-61777-503. (M)

Next page: https://openairdocs.org/deregistered/N353US-2006-09-06/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 = 'N353US' AND deregistration_id = 'N353US-2006-09-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N353US-2006-09-06/reports

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