# Service difficulty reports: N237US, cancelled Nov 24, 2000

A list on [N237US, cancelled Nov 24, 2000](https://openairdocs.org/deregistered/N237US-2000-11-24.md).

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

- [SDR USAA991026](https://openairdocs.org/sdr/USAA991026.md): Stringer · corroded · Sep 25, 1999 · N237US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > TPA - DURING A CX-4 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA LOCATED UNDER STR 27R, STA 930, CORROSION LEVEL 1. REPLACED CORRODED AREA PER SRM 53-10-3 FIG 1. (X)
- [SDR USAA991025](https://openairdocs.org/sdr/USAA991025.md): Skin · cracked · Sep 25, 1999 · N237US · Boeing 737201 · Service Doors
  > TPA - DURING A CX-4 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK IN UPPER AFT CORNER OF TOP HINGE CUT-OUT SERVICE DOOR SKIN. INSTALLED DOUBLER PER TR 52-40-03A FIG 2. (X)
- [SDR USAASB99045](https://openairdocs.org/sdr/USAASB99045.md): Coalescer · dirty · Feb 19, 1999 · N237US · Boeing 737201 · Humidity Control System
  > PHL - FLT 712 - FLIGHT RETURNED TO FIELD AT PHL DUE TO A SMOKE SMELL IN THE COCKPIT. THE SMELL OF SMOKE WAS PRESENT AND TO WORSE ON TAKEOFF ROLL. CAPTAIN DECIDED TO TAKEOFF AND RETURN BACK TO FIELD. NO EMERGENCY WAS DECLARED. THE FLIGHT LANDED WITHOUT FURT
- [SDR USAASB98250](https://openairdocs.org/sdr/USAASB98250.md): Battery Pack · discharged · Sep 22, 1998 · N237US · Boeing 737201 · Emergency Lighting
  > CMH - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS AT THE AFT SERVICE DOORS DIM. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT M572. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB97347](https://openairdocs.org/sdr/USAASB97347.md): Window · cracked · Dec 23, 1997 · N237US · Boeing 737201 · Flight Compartment Windows
  > CLT 851 - EN ROUTE PIT-BHM - WHEN AT FL3100, F/O'S NR 1 WINDOW SHATTERED. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED F/O'S R1 WINDOW ASSEMBLY. OPERATIONAL CHECKS GOOD. (M)
- [SDR USAASB97068](https://openairdocs.org/sdr/USAASB97068.md): Battery Pack · discharged · Mar 2, 1997 · N237US · Boeing 737201 · Emergency Lighting
  > PIT - MAINTENANCE FOUND THE LEFT INTERIOR OVERWING EMERGENCY EXIT LIGHT ON SIDEWALL PANEL INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)
- [SDR USAASB97061](https://openairdocs.org/sdr/USAASB97061.md): Power Supply · failed · Feb 22, 1997 · N237US · Boeing 737201 · Emergency Lighting
  > PHL - MAINTENANCE FOUND THE LEFT INTERIOR AND EXTERIOR OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE M192 POWER SUPPLY. OPS CHECK GOOD. (M)
- [SDR USAA960753](https://openairdocs.org/sdr/USAA960753.md): Doubler · cracked · Nov 21, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK SKIN DOUBLER BS 377.5 TO BS 379 LBL 3 WL 148.5. FABRICATED AND INSTALLED NEW DOUBLER, REPAIRED PER SRM 53-30-2 AND SRM 51-10-1. (M)
- [SDR USAA960752](https://openairdocs.org/sdr/USAA960752.md): Skin · cracked · Nov 21, 1996 · N237US · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK WL 148.5 LBL 4, BS 279 SKIN. INSTALLED EXT DOUBELR WT ADDED 9.4 LBS AT BS 279, REPAIRED PER TR 53-30-4. (M)
- [SDR USAA960751](https://openairdocs.org/sdr/USAA960751.md): Web · cracked · Nov 21, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND.75 INCH CRACK BS 708 STRINGER 18R, SHEAR BEAM WEB. INSTALLED REPAIR KIT, REPAIRED PER EO NR 5393G256 AND BOEING DRAWING NR 65C29228. (M)
- [SDR USAA960750](https://openairdocs.org/sdr/USAA960750.md): Chord · cracked · Nov 21, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING Q-3 CHECK NDT INSPECTION, FOUND.25 INCH CRACK INBOARD AT FORWARD OUTBOARD HOE AT INTERSECTION OF STRINGER 18 A OUTBOARD STRAP AND BS 727 CHORD (RIGHT SIDE). INSTALLED REPAIR/MOD, REPAIRED PER EO 5394G068. (M)
- [SDR USAA960749](https://openairdocs.org/sdr/USAA960749.md): Skin · cracked · Nov 21, 1996 · N237US · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH CRACK IN SKIN STATION 1156, LBL 12. INSTALLED DOUBLER (REPLACED DOUBLER), REPAIRED PER SRM 53-30-3, FIG 6. (M)
- [SDR USAA960748](https://openairdocs.org/sdr/USAA960748.md): Skin · corrosion · Nov 21, 1996 · N237US · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORRODED AREA BS 967 BETWEEN STRINGER 27L AND STRINGER 27R SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. CORROSION TASK NR C53--202-01, CORROSION LEVEL 1. (M)
- [SDR USAA960747](https://openairdocs.org/sdr/USAA960747.md): Bulkhead · corrosion · Nov 21, 1996 · N237US · Boeing 737201 · Fuselage Main, Bulkhead
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND.5 INCH BY 2 INCH CORRODED AREA AT BULKHEAD BS 1023 RBL 1 INCH WL 195. INSTALLED EXT REPAIR, REPAIRED PER SRM 53-10-4/53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M)
- [SDR USAA960746](https://openairdocs.org/sdr/USAA960746.md): Splice · corrosion · Nov 21, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND.5 INCH BY 2 INCH CORRODED AREA STRINGER SPLICE BS 362 TO 363, STRINGER 27L. INSTALLED NEW SPLICE WITH 2 ADDITIONAL FASTENER ROWS, REPAIRED PER EA NR 41756. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M)
- [SDR USAA960745](https://openairdocs.org/sdr/USAA960745.md): Chord · crack · Nov 21, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND.25 INCH CRACK INDICATION INSIDE FORWARD UPPER FASTENER HOLE OUTSIDE CHORD BS 727, STRINGER 18 A STRAP. INSTALLED REPAIR MOD, REPAIRED PER EO 5394G068. (M)
- [SDR USAA960744](https://openairdocs.org/sdr/USAA960744.md): Frame · corrosion · Nov 21, 1996 · N237US · Boeing 737201 · Fuselage Main, Frame
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION AT FRAME, BS 967. INSTALLED REPAIR ANGLE, REPAIRED PER SRM 53-10-4. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M)
- [SDR USAA960743](https://openairdocs.org/sdr/USAA960743.md): Stringer · cracked · Nov 21, 1996 · N237US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 5 INCH CORRODED AREA STRINGER 27R, BS 373 TO BS 378 (STRINGER). INSTALLED STRINGER REPAIR AND REPAIRED PER SRM 53-10-3, FIG 1. CORROSION LEVEL 1, CORROSION TASK NR C53-202-01. (M)
- [SDR USAASB96230](https://openairdocs.org/sdr/USAASB96230.md): Static Line · disconnected · Nov 18, 1996 · N237US · Boeing 737201 · Altimeter, Barometric/Encoder
  > MYR - FL 8033 - ON T/O AT INT, BOTH THE CAPTAINS AND F/O ALTIMETERS FROZE AT 1,200 FT ANT TRIPPED TO STANDBY. TRIED BOTH STANDBY STATIC SOURCES WITH NO RECOVERY OF EITHER ALTIMETER. ALTIMETERS APPEARED TO OPERATE NORMALLY UPON PASSING THROUGH 1,200 FT. FLIG
- [SDR USAASB96087](https://openairdocs.org/sdr/USAASB96087.md): Light Emergency · failed · May 9, 1996 · N237US · Boeing 737201 · Emergency Lighting
  > FLT 916 - PHL - COCKPIT EMERGENCY LIGHT INOP. MX REPLACED COCKPIT EMERGENCY LIGHT ASSY. OPS CHECK SATISFACTORY. (M)
- [SDR USAA960191](https://openairdocs.org/sdr/USAA960191.md): Skin · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK SKIN BS 347 AT STRINGER 17L. INSTALLED DOUBLERS. REPAIRED PER EO 5391G-694. (M)
- [SDR USAA960190](https://openairdocs.org/sdr/USAA960190.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK TIE CLIP, STRINGER 3R, BS 727. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)
- [SDR USAA960189](https://openairdocs.org/sdr/USAA960189.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN VISUAL INSPECTION, FOUND.125 INCH CRACK IN EACH OF 2 CLIPS BS 767 AT STRINGER 5L AND STRINGER 10L, STRINGER TIE CLIPS. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)
- [SDR USAA960188](https://openairdocs.org/sdr/USAA960188.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK BS 685 STRINGER 3 RIGHT STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)
- [SDR USAA960187](https://openairdocs.org/sdr/USAA960187.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN VISUAL INSPECTION, FOUND.125 INCH CRACK IN EACH OF 2 CLIPS, BS 727B AT STRINGER 2L AND STRINGER 7L, STRINGER TIE CLIPS. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)
- [SDR USAA960186](https://openairdocs.org/sdr/USAA960186.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN VISUAL INSPECTION, FOUND.125 INCH CRACK BS 767 AT STRINGER 10 RIGHT, STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-3535214. (M)
- [SDR USAA960185](https://openairdocs.org/sdr/USAA960185.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN VISUAL INSPECTION, FOUND.125 INCH CRACK BS 767 AT STRINGER 6 RIGHT STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)
- [SDR USAA960184](https://openairdocs.org/sdr/USAA960184.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK BS 747 STRINGER 5 RIGHT, STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)
- [SDR USAA960183](https://openairdocs.org/sdr/USAA960183.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK BS 578 AT STRINGER 3 LEFT STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)
- [SDR USAA960182](https://openairdocs.org/sdr/USAA960182.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK IN 2 STRINGER TIE CLIPS BS 616 AT STRINGER 2L AND STRINGER 4L. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)
- [SDR USAA960181](https://openairdocs.org/sdr/USAA960181.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK STRINGER TIE CLIP STATION 639 STRINGERS 4L, 6L. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)
- [SDR USAA960180](https://openairdocs.org/sdr/USAA960180.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK STRINGER TIE CLIP STATION 685, STRINGER 2L AND STRINGER 5L. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)
- [SDR USAA960179](https://openairdocs.org/sdr/USAA960179.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK STRINGER TIE CLIP BS 706, STRINGER 10L. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)
- [SDR USAA960178](https://openairdocs.org/sdr/USAA960178.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK STRINGER TIE CLIP STATION 727 A STRINGERS 3L, STRINGER 4L, STRINGER 5L. REPAIRED PER EO 5393G227. MODIFIED PER NR 69-35352-14. (M)
- [SDR USAA960177](https://openairdocs.org/sdr/USAA960177.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK STRINGER TIE CLIP BS 747 STRINGER 7L AND STRINGER 10L. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)
- [SDR USAA960176](https://openairdocs.org/sdr/USAA960176.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK STRINGER TIE CLIP BS 787 STRINGER 10L. REPAIRED PER EO 5353G227. MODIFIED PART NR 69-35352-14. (M)
- [SDR USAA960175](https://openairdocs.org/sdr/USAA960175.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK STRINGER TIE CLIP BS 827 STRINGER 5 LEFT. REPAIRED PER EO 5393G227. MODIFIED PER NR 69-35352-14. (M)
- [SDR USAA960173](https://openairdocs.org/sdr/USAA960173.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK STRINGER TIE CLIP BS 578 STRINGER 3 RIGHT. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)
- [SDR USAA960172](https://openairdocs.org/sdr/USAA960172.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK STRINGER TIE CLIP BS 639 STRINGER 4 RIGHT. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)
- [SDR USAA960171](https://openairdocs.org/sdr/USAA960171.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK AT STRINGER TIE CLIP BS 727A STRINGER 4 RIGHT. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M)
- [SDR USAA960170](https://openairdocs.org/sdr/USAA960170.md): Tie Clip · cracked · Jan 30, 1996 · N237US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK BS 727 B S-1, STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR INSTALLED 69-35352-14. (M)
- [SDR USAA951428](https://openairdocs.org/sdr/USAA951428.md): Skin · cracked · Dec 30, 1995 · N237US · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND.125 INCH CRACK SHEET METAL AT LOWER CORNER MED. INSTALLED INTERIM REPAIR PER EA 31854 AND TBC. REPAIRED PER EA 31854SB 737-53-1083. (M)
- [SDR USAA950927](https://openairdocs.org/sdr/USAA950927.md): Stringer · corroded · Jul 28, 1995 · N237US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > ROA - DURING 'BX CHECK' VISUAL INSPECTION, FOUND 13.125 INCH LONG STRINGER CORRODED FUSELAGE STATION 967 JUST TO THE LEFT OF WATER TANK. REMOVED CORRODED STRINGER AREA AND INSTALLED SPLICED STRINGER PER SRM. REPAIRED PER SRM 53-10-3 FIG 1 FUSELAGE STRINGER
- [SDR USAA950029](https://openairdocs.org/sdr/USAA950029.md): Eel · inoperative · Jan 15, 1995 · N237US · Boeing 737201 · Emergency Lighting
  > PHL - COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY. (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 = 'N237US' AND deregistration_id = 'N237US-2000-11-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N237US-2000-11-24/reports

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