# Service difficulty reports: N242US, cancelled Apr 13, 2007

A list on [N242US, cancelled Apr 13, 2007](https://openairdocs.org/deregistered/N242US-2007-04-13.md).

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

- [SDR RYNA200500028](https://openairdocs.org/sdr/RYNA200500028.md): Pump · overheated · Aug 29, 2005 · N242US · Boeing 737201 · Hydraulic Pump, Auxiliary
  > NR 2 B-SYSTEM ELECTRIC HYDRAULIC PUMP OVERHEATED, RETURNED TO ACY DUE TO DECREASING A-SYSTEM HYDRAULIC QUANTITY. REMOVED AND REPLACED NR 2 B-SYSTEM ELECTRIC HYDRAULIC PUMP, AND SERVICED A-SYSTEM. BOTH SYSTEMS LEAKED AND OPERATIONALLY CHECKED GOOD. REF B737
- [SDR RYNA200500026](https://openairdocs.org/sdr/RYNA200500026.md): Skin · cracked · Aug 17, 2005 · N242US · Boeing 737201 · Fuselage Main, Plate/Skin
  > DURING WALKAROUND AFTER FLIGHT A SKIN CRACK AT BS 727B+18" AND JUST ABOVE STRINGER 16L WAS NOTICED. AIRCRAFT FERRIED TO FLIGHTSTAR FOR REPAIR. COMPLIED WITH FUSELAGE SKIN REPAIR AT BS 727B+18" AT STRINGER 16L PER SRM 53-30-3 FIG DETAIL VII.
- [SDR USAASB01266](https://openairdocs.org/sdr/USAASB01266.md): Power Supply · discharged · Sep 22, 2001 · N242US · Boeing 737201 · Emergency Lighting
  > BWI - THE EMERGENCY LIGHTS FOR THE LAST FIVE SEAT ROWS IN THE PASSENGER CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)
- [SDR USAA010569](https://openairdocs.org/sdr/USAA010569.md): Bulkhead · cracked · May 25, 2001 · N242US · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND PRESSURE WEB WITH CRACKS RANGING IN SIZE FROM.375 INCH TO 1.5 INCH, BS 178, WL 199 TO WL 234 LBL 10.5 TO RBL 10.5. DAMAGE REMOVED, REPAIR FILLERS AND DOUBLER INSTALLED PER EO 5300V153, EA 69712, SRM 53-10-11 FIG 1. (M)
- [SDR USAA010570](https://openairdocs.org/sdr/USAA010570.md): Frame · cracked · May 25, 2001 · N242US · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND SIDE CHORD CRACKED.5 INCHES AND 1.25 INCHES, BS 178, LEFT AND RIGHT SIDE CHORD, WL 195. DAMAGED SECTIONS CUTOUT, INSTALLED CHORD SPLICE REPAIR PER EO 5300V157 AND SRM 51-10-02. (M)
- [SDR USAA010571](https://openairdocs.org/sdr/USAA010571.md): Intercostal · cracked · May 25, 2001 · N242US · Boeing 737201 · Fuselage Structure (General)
  > CLT - FOUND INTERCOSTAL CRACKED 1.5 INCHES, BS 178, WL 195, LBL 25 AND RBL 25. REMOVED AND REPLACED INTERCOSTAL. (M)
- [SDR USAA010572](https://openairdocs.org/sdr/USAA010572.md): Bulkhead · cracked · May 25, 2001 · N242US · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND WEB CRACKED.250 INCH, BS 178 WL 195.7, LBL 23. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER PER EA 69714 AND SRM 53-10-11 FIG 2. (M)
- [SDR USAA200101173](https://openairdocs.org/sdr/USAA200101173.md): Seal · leaking · Dec 18, 2000 · N242US · Boeing 737201 · Passenger/Crew Doors
  > ON CLIMB OUT FROM TPA, A VERY LOUD SQUEAL WAS COMING FROM THE FORWARD ENTRY DOOR. AC WAS PRESSURIZING, NOISE BECAME LOUDER AS AC CLIMBED HIGHER. FLIGHT RETRUNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED.MAINTENANCE REMOVED AND REP
- [SDR USAASB00298](https://openairdocs.org/sdr/USAASB00298.md): Duct · cracked · Oct 22, 2000 · N242US · Boeing 737201 · Engine Anti-Icing System
  > LGA-MCO - FLT 2667 - DURING CRUISE, THE RIGHT ENGINE OVERHEAT LIGHT ILLUMINATED. THE LIGHT WENT OUT WHEN THE ENGINE POWER WAS REDUCED. THE AIRCRAFT DIVERTED TO BWI AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED AND NO ENGINE SHUTDOWN OCCURRED. MAIN
- [SDR USAASB00073](https://openairdocs.org/sdr/USAASB00073.md): Controller · failed · Mar 18, 2000 · N242US · Boeing 737201 · Cabin Pressure Controller
  > IAD - FLT 2808 - ON CLIMB OUT FROM IAD, AIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR STANDBY MODE. FLIGHT RETURNED TO FIELD AT IAD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED CABIN PRESSURE CONTROLLER FUNCTIONAL TEST
- [SDR USAA000046](https://openairdocs.org/sdr/USAA000046.md): Skin · cracked · Jan 17, 2000 · N242US · Boeing 737201 · Fuselage Main, Plate/Skin
  > SKIN CRACKED AT BS 727 STRINGER 16L AND 15L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M)
- [SDR USAA000038](https://openairdocs.org/sdr/USAA000038.md): Stringer · corroded · Jan 17, 2000 · N242US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > STRINGER 28R CORRODED AT BS 360. REPAIRED PER EA 66136 AND SRM 53-10-3 FIG 1. (M)
- [SDR USAA000037](https://openairdocs.org/sdr/USAA000037.md): Skin · cracked · Jan 17, 2000 · N242US · Boeing 737201 · Fuselage Main, Plate/Skin
  > SKIN CRACKED AT BS 947. INSTALLED DOUBLER PER SRM 53-30-3 FIG 34. (M)
- [SDR USAA000036](https://openairdocs.org/sdr/USAA000036.md): Stringer · corroded · Jan 17, 2000 · N242US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > STRINGER 27L CORRODED AT BS 986.5. REPAIRED PER SRM 53-10-3 FIG 1. (M)
- [SDR USAA000035](https://openairdocs.org/sdr/USAA000035.md): Skin · cracked · Jan 17, 2000 · N242US · Boeing 737201 · Fuselage Main, Plate/Skin
  > SKIN CRACKED AT BS 727 PLUS 13, AND 2 INCHES ABOVE STRINGER 18R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6 AND EA 66135. (M)
- [SDR USAASB99116](https://openairdocs.org/sdr/USAASB99116.md): Fan · failed · Apr 30, 1999 · N242US · Boeing 737201 · Air Distribution Fan
  > RIC - FLT 517 - EN ROUTE FOR CLT-DCA AT FL250, FLIGHT ATTENDANT REPORTED THAT A PASSENGER SMELLED SMOKE IN THE FIRST THREE ROWS OF CABIN. CAPTAIN TURNED GALLEY POWER OFF AND THE FLIGHT ATTENDANT WENT BACK AND CONFIRMED SMOKE COMING OUT OF THE AIR CONDITIONING
- [SDR USAA990182](https://openairdocs.org/sdr/USAA990182.md): Skin · cracked · Mar 9, 1999 · N242US · Boeing 737201 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-3 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK IN SKIN STATION 943 STRINGER 24L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6 AND EA 63860. (M)
- [SDR USAA980137](https://openairdocs.org/sdr/USAA980137.md): Stringer · corrosion · Mar 27, 1998 · N242US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 4 INCH BY 4 INCH STATION 908, STRINGER 21L. CUT OUT DAMAGE AND INSTALLED STRINGER, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)
- [SDR USAA980136](https://openairdocs.org/sdr/USAA980136.md): Stringer · corrosion · Mar 27, 1998 · N242US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > INT - DURING 'Q-4' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 20 INCHES, STA 967 TO STA 987, STR 25R. INSTALLED REPAIR ANGLES AND REPAIRED PER SRM 53-10-3. CORROSION TASK NR: C53-202-01. CORROSION LEVEL: 2. (X)
- [SDR USAA980135](https://openairdocs.org/sdr/USAA980135.md): Beam · corrosion · Mar 27, 1998 · N242US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AROUND NUT PLATES STATION 235 BL '0' TO RBL 15 NOSE W/W CEILING TRANSVERSER BEAM. REMOVED AND INSTALLED NEW PREFAB TRANSVERSER BEAM, FABRICATED AND INSTALLED ZEE STRAPS. REPAIRED PER
- [SDR USAA980134](https://openairdocs.org/sdr/USAA980134.md): Stringer · corrosion · Mar 27, 1998 · N242US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 30 INCH CORRODED AREAS CORROSION ON STRINGER 24L FROM BS 294.5 TO BS 325.3 STRINGER. INSTALLED DOUBLER REPAIR ANGLE, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)
- [SDR USAA980133](https://openairdocs.org/sdr/USAA980133.md): Stringer · corroded · Mar 27, 1998 · N242US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > INT - DURING 'Q-4' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 8 INCH CORROSION STA 1006 STR 26L. INSTALLED REPAIR ANGLES, REPAIRED PER SRM 53-10-3. CORROSION TAKE NR: C53-202-01. CORROSION LEVEL: 2. (X)
- [SDR USAA980132](https://openairdocs.org/sdr/USAA980132.md): Stringer · corroded · Mar 27, 1998 · N242US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION.5 INCH BY 30 INCH STATION 294 TO 325 STRINGER 24L. SPLICED IN NEW STRINGER SECTION, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01. CORROSION LEVEL 2. (M)
- [SDR USAASB98015](https://openairdocs.org/sdr/USAASB98015.md): Light · failed · Jan 17, 1998 · N242US · Boeing 737201 · Landing Gear Position and Warning
  > CLT - FLT 209 - ON APPROACH INTO CLT, CREW DID NOT RECEIVE A DOWN AND LOCKED INDICATION FOR THE RT MLG. CREW TESTED LIGHT AND CONFIRMED THE LIGHT WAS OPERATIONAL. CREW RECYCLED THE GEAR AND AGAIN RECEIVED NO DOWN AND LOCKED INDICATION FOR THE RIGHT MAIN GEAR
- [SDR USAA980010](https://openairdocs.org/sdr/USAA980010.md): Stringer · corroded · Jan 9, 1998 · N242US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH CORROSION STRINGER 27L, BSL 967. REMOVED CORRODED STRINGER AND INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3 FIG 1. (M)
- [SDR USAA980009](https://openairdocs.org/sdr/USAA980009.md): Skin · cracked · Jan 9, 1998 · N242US · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND.25 INCH CRACK BS 767 STRINGER 19R FUSELAGE SKIN. REMOVED CRACKED SKIN AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1. (M)
- [SDR USAASB97125](https://openairdocs.org/sdr/USAASB97125.md): Wire · broken · Apr 8, 1997 · N242US · Boeing 737201 · Light System Wiring
  > CMH - MAINTENANCE FOUND THE EMERGENCY LIGHT AT SEAT ROW 11 INOP. MAINTENANCE REPAIRED A BROKEN WIRE AT THE LIGHT SOCKET. OPS CHECK GOOD. (M)
- [SDR USAA960404](https://openairdocs.org/sdr/USAA960404.md): Stringer · corrosion · Apr 25, 1996 · N242US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > ROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 6 INCH CORROSION ON STRINGER, FORWARD OF AFT PRESSURE BULKHEAD STRINGER 26R BS 1016. INSTALLED NEW STRINGER, REPAIRED PER SRM 53-10-3. (M)
- [SDR USAASB96012](https://openairdocs.org/sdr/USAASB96012.md): Pressurization · lost · Jan 19, 1996 · N242US · Boeing 737201 · Cabin Pressure Control System
  > FLT NR 818 - PIT - FLIGHT DIVERTED DUE TO LOSS OF PRESSURIZATION. (M)
- [SDR USAA950194](https://openairdocs.org/sdr/USAA950194.md): Switch · failed · Feb 27, 1995 · N242US · Boeing 737201 · Engine Oil Indicating System
  > JAX - FLT 1606 - ON CLIMB NR 2 OIL FILTER BYPASS LIGHT ILLUMINATED. RETARDED THROTTLE AND LIGHT WENT OUT. FLIGHT DIVERTED TO JAX WHERE LANDING WAS WITHOUT FURTHER INCIDENT. REPLACED RIGHT MAIN OIL FILTER BYPASS SWITCH AND RIGHT MAIN OIL SCREEN. (W)

## 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 = 'N242US' AND deregistration_id = 'N242US-2007-04-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N242US-2007-04-13/reports

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