# Service difficulty reports: N232US, cancelled Apr 11, 2003

A list on [N232US, cancelled Apr 11, 2003](https://openairdocs.org/deregistered/N232US-2003-04-11.md).

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

- [SDR USAA010642](https://openairdocs.org/sdr/USAA010642.md): Skin · cracked · Jun 11, 2001 · N232US · Boeing 737201 · Fuselage Structure (General)
  > TPA - FOUND SKIN CRACKED BETWEEN STATION 727A AND 727B BELOW 13L. INSTALLED DUOBELR PER SRM USING BLIND FASTENERS PER SRM 53-30-3 FIG 1 AND MPP 308-25. (M)
- [SDR USAA010643](https://openairdocs.org/sdr/USAA010643.md): Skin · cracked · Jun 11, 2001 · N232US · Boeing 737201 · Fuselage Main, Plate/Skin
  > TPA - FOUND SKIN CRACKED 2.5 INCH AND 2.75 INCH, STATION 873 AND 885 ABOVER 19R. INSTALLED DOUBLER.063 INCH CLAD 2024TB USING BLIND FASTENERS PER SRM 53-30-3 FIG 1. (M)
- [SDR USAA010679](https://openairdocs.org/sdr/USAA010679.md): Skin · cracked · Jun 10, 2001 · N232US · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND SKIN CRACKED 1 INCH, BETWEEN BS 727A AND 727B, BELOW S13L. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER USING BLIND FASTENERS PER SRM 53-30-3 FIG 1. (M)
- [SDR USAASB00302](https://openairdocs.org/sdr/USAASB00302.md): Battery · discharged · Oct 25, 2000 · N232US · Boeing 737201 · Emergency Lighting
  > BWI - FLT 2981 - PILOT REPORTED THAT THE EMERGENCY EXIT LIGHT OVER THE RIGHT FORWARD SERVICE DOOR HAD FALLEN OUT AND THE BATTERIES HAD FULLY DISCHARGED. MAINTENANCE REPLACED THE BATTERIES AND REINSTALLED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA001280](https://openairdocs.org/sdr/USAA001280.md): Skin · cracked · Aug 17, 2000 · N232US · Boeing 737201 · Fuselage Main, Plate/Skin
  > TPA - FOUND SKIN CRACKED 1.5 INCH, BETWEEN 727A AND 727B STRINGER 17L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 25. (M)
- [SDR USAA000802](https://openairdocs.org/sdr/USAA000802.md): Skin · cracked · Jun 5, 2000 · N232US · Boeing 737201 · Fuselage Main, Plate/Skin
  > TPA - FOUND SKIN CRACKED 2.125 INCH, STATION 747, BELOW STRINGER 17 LT. REMOVED AND REPLACED PER SRM 53-30-3 FIG 1. (M)
- [SDR USAASB99306](https://openairdocs.org/sdr/USAASB99306.md): Wire · failed · Dec 28, 1999 · N232US · Boeing 737201 · Light System Wiring
  > SYR - PILOT REPORTED THAT SEVERAL ROWS OF SEAT MOUNTED EMERGENCY LIGHTS, IN THE FORWARD CABIN, ILLUMINATED WITH SWITCH IN THE ARMED POSITION AND NORMAL POWER ON AIRCRAFT. MAINTENANCE REPAIRED WIRE AT EMERGENCY LIGHT CONNECTOR LOCATED AT SEAT ROW 12ABC. OPERA
- [SDR USAA990992](https://openairdocs.org/sdr/USAA990992.md): Skin · cracked · Sep 16, 1999 · N232US · Boeing 737201 · Service Doors
  > TPA - DURING A CX-CHECK VISUAL INSPECTION, FOUND A.250 INCH LONG CRACK AT AFT SERVICE DOOR BOTTOM HINGE AFT CORNER DOOR SKIN. INSTALLED REPAIR DOUBLER PER TR 52-40-03A AND EA 65097. (M)
- [SDR USAA990732](https://openairdocs.org/sdr/USAA990732.md): Tie Clip · cracked · Jul 18, 1999 · N232US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - DURING C-CHECK, FOUND.25 INCH CRACK IN TIE CLIP AT STATION 480 STRINGER 24L (TOP LEFT CORNER). REPLACED TIE CLIP PER SRM 51-40-02. (M)
- [SDR USAA980384](https://openairdocs.org/sdr/USAA980384.md): Skin · cracked · Sep 8, 1998 · N232US · Boeing 737201 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A.50 INCH CRACK IN EXTERNAL SKIN STA 380 BL 3.01. INSTALLED DOUBLER OF.100 INCH 2024 T-3 PER TR 53-30-04 SB 737-53-1117. (X)
- [SDR USAASB98179](https://openairdocs.org/sdr/USAASB98179.md): Switch · failed · Jul 11, 1998 · N232US · Boeing 737201 · Engine Oil Indicating System
  > BOS - FLT 921 - ON CLIMB-OUT FROM BOS, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. ENGINE WAS BROUGHT BACK TO IDLE AND AN EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS SHUT DOWN AFTER LANDI
- [SDR USAA980299](https://openairdocs.org/sdr/USAA980299.md): Skin · cracked · Jul 7, 1998 · N232US · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - DURING DROP IN VISUAL INSPECTION, FOUND A 1 INCH CRACK ON FUSELAGE SKIN 1 INCH FORWARD OF BS 727B.5 INCH ABOVE STRINGE R16R. INSTALLED EXTERNAL REPAIR DOUBLER PER EA 62067. (M)
- [SDR USAASB98160](https://openairdocs.org/sdr/USAASB98160.md): Adc · failed · Jun 26, 1998 · N232US · Boeing 737201 · Air Data Computer
  > CLT - FLT 8036 - DURING CRUISE, CREW REPORTED A TOTAL NR 1 AIR DATA COMPUTER FAILURE. CREW PULLED AND RESET RN 1 CADC CIRCUIT BREAKERS. SYSTEM RESETS, THEN FAILS AGAIN. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED.
- [SDR USAA980265](https://openairdocs.org/sdr/USAA980265.md): Skin · cracked · Jun 10, 1998 · N232US · Boeing 737201 · Fuselage Main, Plate/Skin
  > PHL - DURING RON FOUND 2 INCH CRACK IN FUSELAGE SKIN RIGHT SIDE BETWEEN STATION 400 AND STATION 420 BETWEEN STRINGER 23RT AND 24RT. INSTALLED TEMPORARY EXTERNAL DOUBLER PER SRM 53-30-3 PAGE 2E, FIG 1. (M)
- [SDR USAA980264](https://openairdocs.org/sdr/USAA980264.md): Skin · cracked · Jun 10, 1998 · N232US · Boeing 737201 · Fuselage Main, Plate/Skin
  > PHL - DURING RON, FOUND 2 CRACKS, IN EACH LONG RIGHT SIDE FUSELAGE SKIN BETWEEN STATION 797 AND 767 BETWEEN STRINGER 18RT AND 19RT. INSTALLED TEMPORARY EXTERNAL DOUBLER PER SRM 53-30-3 PAGE 2E, FIG 1. (M)
- [SDR USAA980168](https://openairdocs.org/sdr/USAA980168.md): Skin · cracked · Apr 20, 1998 · N232US · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DUIRNG A-CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND 1.75 INCH CRACK BS 947, STR 24L, FUSELAGE SKIN. INSTALLED REPAIR WITH BLIND FASTENERS/SOLID FASTENERS TO BE INSTALLED NEXT Q-CHECK. REPAIRED PER SRM 53-30-3, PAGE 2C. (X)
- [SDR USAA970288](https://openairdocs.org/sdr/USAA970288.md): Frame · cracked · Sep 26, 1997 · N232US · Boeing 737201 · Fuselage Main, Frame
  > INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CRACK.50 INCH STA 351, STR 27R FRAME. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (X)
- [SDR USAA970287](https://openairdocs.org/sdr/USAA970287.md): Skin · cracked · Sep 26, 1997 · N232US · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK APPROXIMATELY 1.50 INCHES, STA 727A, STR 17R SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (X)
- [SDR USAA970286](https://openairdocs.org/sdr/USAA970286.md): Bulkhead Skin · crack · Sep 26, 1997 · N232US · Boeing 737201 · Fuselage Main, Bulkhead
  > INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND.50 INCH CRACK BS 178 BULKHEAD SKIN RIGHT UPPER ANTENNA (RADAR) MOUNT. INSTALLED REPAIR, REPAIRED PER SRM 53-10-11, FIGURE 1. (X)
- [SDR USAA970285](https://openairdocs.org/sdr/USAA970285.md): Keel Beam · corrosion · Sep 26, 1997 · N232US · Boeing 737201 · Fuselage Main, Keel
  > INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION 3 INCHES BY 1 INCH KEEL BEAM STA 727 + 3 INCHES, STR 27R. INSTALLED DOUBLER, REPAIRED PER EA 43120. CORROSION TASK NR: C53-201-01. CORROSION LEVEL: 2. (X)
- [SDR USAASB97168](https://openairdocs.org/sdr/USAASB97168.md): Battery Charger · failed · Jun 14, 1997 · N232US · Boeing 737201 · Emergency Lighting
  > ALB - MAINTENANCE FOUND THE EXIT SIGN ON THE CEILING BETWEEN OVERWING EXIT HATCHES INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB97082](https://openairdocs.org/sdr/USAASB97082.md): O-Ring · leaking · Mar 19, 1997 · N232US · Boeing 737201 · Turbine Engine Oil System
  > PHL - FL 1243, DURING CLIMB AT 10,000 FEET, THE NR 1 ENGINE OIL QTY DROPPED RAPIDLY TO ZERO, FOLLOWED BY A DROP IN OIL PRESSURE AND A RISE IN OIL TEMPERATURE. CAPTAIN DECLARED AN EMERGENCY AND SHUT DOWN THE NR 1 ENGINE IN FLIGHT. FLIGHT RETURNED TO FIELD AT
- [SDR USAASB97034](https://openairdocs.org/sdr/USAASB97034.md): T-Fitting · leaking · Jan 31, 1997 · N232US · Boeing 737201 · Hydraulic System, Main
  > PHL - FL 319 - AT 1,000 FT, MASTER CAUTION LIGHT AND THE 'A' SYSTEM FLIGHT CONTROL LOW PRESSURE LIGHT ILLUMINATED. THE 'A' SYSTEM HYDRAULIC QTY INDICATED ZERO. FLIGHT RETURNED TO FIELD AT PHL. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER
- [SDR USAASB97032](https://openairdocs.org/sdr/USAASB97032.md): Battery Pack · discharged · Jan 9, 1997 · N232US · Boeing 737201 · Emergency Lighting
  > CMH - MAINTENANCE FOUND THE FORWARD ENTRY AND SERVICE DOOR EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT POWER SUPPLY M571. OPS CHECK GOOD. (M)
- [SDR USAASB96268](https://openairdocs.org/sdr/USAASB96268.md): Battery Pack · discharged · Dec 25, 1996 · N232US · Boeing 737201 · Emergency Lighting
  > CLE - MAINTENANCE FOUND THE FORWARD SERVICE DOOR AND THE MAIN ENTRANCE DOOR INTERIOR AND EXTERIOR EXIT LIGHTS INOP. ALSO, THE MAIN ENTRANCE DOOR UPPER EMERGENCY LIGHT WAS FOUND TO BE VERY DIM. MAINTENANCE REMOVED AND REPLACED THE MAIN ENTRANCE DOOR UPPER EME
- [SDR USAA960805](https://openairdocs.org/sdr/USAA960805.md): Skin · cracked · Dec 24, 1996 · N232US · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 2.1250 INCH CRACK STRINGER 17 L, BS 760 FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1. (M)
- [SDR USAA960804](https://openairdocs.org/sdr/USAA960804.md): Skin · cracked · Dec 24, 1996 · N232US · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT, INSPECTION FOUND.75 INCH CRACK AT FUSELAGE SKIN STRINGER 17L, BS 740. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1. (M)
- [SDR USAA960803](https://openairdocs.org/sdr/USAA960803.md): Stringer · corrosion · Dec 24, 1996 · N232US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > ROA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 10 INCH CORROSION STRINGER 27L, BS 1000 TO 1016. SPLICED IN STRINGER, REPAIRED PER CD 25G00984A, SRM 53-10-3 FIG 1. (M)
- [SDR USAA960802](https://openairdocs.org/sdr/USAA960802.md): Skin · cracked · Dec 24, 1996 · N232US · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 3 INCH CRACK STRINGER 16 BS 727A PLUS 8 L FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)
- [SDR USAA960801](https://openairdocs.org/sdr/USAA960801.md): Stringer · cracked · Dec 24, 1996 · N232US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > ROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 1.75 INCH CRACK STRINGER 18A, SHEAR BEAM BS 727 LEFT. INSTALLED REPAIR KIT 65C29228-3, REPAIRED PER EO 5393G256/EA 59193. (M)
- [SDR USAA960800](https://openairdocs.org/sdr/USAA960800.md): Skin · cracked · Dec 24, 1996 · N232US · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND.3125 INCH CRACK FORWARD ENTRY DOOR CUT OUT FORWARD UPPER HINGE CUT OUT FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1 AND TR 53-30-11. (M)
- [SDR USAA960799](https://openairdocs.org/sdr/USAA960799.md): Skin · cracked · Dec 24, 1996 · N232US · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT, FOUND 2.5 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER (STRINGER 17 R BS 328) FUSELAGE SKIN, TEAR STRAP AND BEAR STRAP. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)
- [SDR USAASB96200](https://openairdocs.org/sdr/USAASB96200.md): Battery Pack · discharged · Sep 17, 1996 · N232US · Boeing 737201 · Emergency Lighting
  > PHL - MAINTENANCE FOUND THE OVERHEAD EMERGENCY EXIT IDENTIFIER LIGHT INOP AT ROW 2. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. (M)
- [SDR USAA950527](https://openairdocs.org/sdr/USAA950527.md): Fitting · cracked · May 17, 1995 · N232US · Boeing 737201 · Engine Thrust Reverser
  > JFK - FLT 968 - ON INITIAL CLIMB-OUT OF LGA, 'A' SYSTEM HYDRAULICS FAILED. FLIGHT DIVERTED INTO JFK WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED TEE FITTING AT RIGHT THRUST REVERSER PRESSURE SWITCH, 'A' SYSTEM HYDRAULICS RETURN, PRESSURE
- [SDR USAA950143](https://openairdocs.org/sdr/USAA950143.md): Wire · broken · Feb 16, 1995 · N232US · Boeing 737201 · Light System Wiring
  > LGA - EMERGENCY EXIT LIGHTING AT SEATS REMAIN ON WHENEVER SWITCH IS PLACED IN ARM POSITION. MAINTENANCE FOUND CHARGE/ON WIRE BROKEN. SPLICED IN NEW WIRE. OPS CHECKS OK. (Z)

## 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 = 'N232US' AND deregistration_id = 'N232US-2003-04-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N232US-2003-04-11/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.