# Service difficulty reports: N225US, cancelled Mar 6, 2017

A list on [N225US, cancelled Mar 6, 2017](https://openairdocs.org/deregistered/N225US-2017-03-06.md).

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

- [SDR RYNA200600002](https://openairdocs.org/sdr/RYNA200600002.md): Engine · bird ingestion · Feb 3, 2006 · N225US · Boeing 737201 · Engine (Turbine/Turboprop)
  > BIRD INGESTION INTO NR 1 ENGINE OCCURRED DURING LANDING, AFTER MAIN WHEELS TOUCHED DOWN AND BEFORE NOSE WHEEL TOUCHED DOWN. THUD WAS HEARD IN COCKPIT. AIRCRAFT TAXIED TO GATE WITHOUT FURTHER INCIDENT. UPON INSPECTION FOUND NR 1 ENGINE DAMAGED BEYOND REPAIR
- [SDR RYNA200500022](https://openairdocs.org/sdr/RYNA200500022.md): Oil System · overtemp · Jul 6, 2005 · N225US · Boeing 737201 · Engine Oil Temperature
  > DURING CLIMB-OUT, NR 2 ENGINE OIL TEMP INCREASED TO 122 DEG C. DURING DESCENT, OIL TEMP INCREASED TO 140 DEG C. OIL TEMP IN YELLOW BAND FOR 5 MINUTES. OIL PRESSURE WAS NORMAL IN CLIMB AND CRUISE. NR 2 ENGINE SHUTDOWN AS A PRECAUTION BECAUSE OIL TEMP COULD NOT
- [SDR RYAN200500020](https://openairdocs.org/sdr/RYAN200500020.md): Speed Brake · worn · Jul 3, 2005 · N225US · Boeing 737201 · Engine Thrust Reverser
  > SPEED BRAKE TAKEOFF WARNING SWITCH WORN/BROKEN. SWITCH NOT MAKING CONTACT WHEN SPEED BRAKE ARMED, CAUSING A FALSE TAKEOFF WARNING TO SOUND WHEN THROTTLES ARE ADVANCED.
- [SDR RYNA200500011](https://openairdocs.org/sdr/RYNA200500011.md): Seal · out of adjust · Apr 2, 2005 · N225US · Boeing 737201 · Passenger/Crew Doors
  > AFTER TAKEOFF FROM TUS, A LOUD SQUEAL AND PRESSURIZATION LEAK WAS DETECTED AT THE L-1 DOOR. THE AIRCRAFT WAS RETURNED TO TUS AND LANDED WITHOUT INCIDENT. ADJUSTED L-1 DOOR SEAL. LEAK CHECK GOOD DURING FLIGHT TEST.
- [SDR RYNA200500010](https://openairdocs.org/sdr/RYNA200500010.md): Autopilot Sys · malfunctioned · Apr 2, 2005 · N225US · Boeing 737201 · Autopilot System
  > IMMEDIATELY AFTER TAKEOFF FROM TUS, THE AUTOPILOT PORPOISED IN PITCH. THE AIRCRAFT WAS RETURNED TO TUS AND LANDED WITHOUT INCIDENT. AMENDMENT TO BE FILED UPON COMPLETION OF TROUBLESHOOTING AND CORRECTIVE ACTION.
- [SDR USAA011301](https://openairdocs.org/sdr/USAA011301.md): Stringer · corroded · Sep 12, 2001 · N225US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER CORRODED 1.5 INCH BY 13 INCHES, STRINGER 27L BETWEEN STATION 900 AND 913. INSTALLED DOUBLER AND SECTION OF STRINGER. (M)
- [SDR USAA000801](https://openairdocs.org/sdr/USAA000801.md): Skin · cracked · Jun 5, 2000 · N225US · Boeing 737201 · Fuselage Main, Plate/Skin
  > TPA - FOUND SKIN CRACKED.25 INCH, STATION 920 PLUS 1.5 JUST ABOVE STRINGER 22L AFT FUSE. INSTALLED DOUBLER PER 53-30-3 PAGES 2C, 2D, 2E. (M)
- [SDR USAASB00108](https://openairdocs.org/sdr/USAASB00108.md): Gearbox · leaking · Apr 8, 2000 · N225US · Boeing 737201 · Turbine Engine Oil System
  > CLT - FLT 365 - ON CLIMB-OUT FROM CLT, THE NR 1 ENGINE OIL QTY WENT TO ZERO RESULTING IN AN INFLIGHT SHUTDOWN OF THE NR 1 ENGINE. CAPTAIN DECLARED AN EMERGENCY AND THE FLIGHT RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE
- [SDR USAA000388](https://openairdocs.org/sdr/USAA000388.md): Stringer · cracked · Mar 21, 2000 · N225US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER CRACKED.5 INCH, STRINGER 15L FASTENER HOLES BS 538. INSTALLED REPAIR FILLER AND DOUBLER PER EA 66891. (M)
- [SDR USAA000387](https://openairdocs.org/sdr/USAA000387.md): Skin · cracked · Mar 21, 2000 · N225US · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 1.25 INCHES, BS 538, 1 INCH BELOW STRINGER 14L. INSTALLED DOUBLER PER EA 66891. (M)
- [SDR USAASB00022](https://openairdocs.org/sdr/USAASB00022.md): Battery Pack · discharged · Jan 25, 2000 · N225US · Boeing 737201 · Emergency Lighting
  > SYR - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT, IN THE FORWARD CEILING, CYCLING ON AND OFF. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA991028](https://openairdocs.org/sdr/USAA991028.md): Stringer · corroded · Sep 24, 1999 · N225US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - DURING A RON VISUAL INSPECTION FOUND CORROSION 9 INCHES BY 2 INCHES BY.075 INCH AT BS 500B PLUS 14 INCHES, STR 28R STRINGER (KEEL BEAM). CORROSION LEVEL 2. REMOVED CORROSION, INSTALLED KEEL BEAM REPAIR ANGLES AND SHIMS PER EA 65660. (X)
- [SDR USAA991027](https://openairdocs.org/sdr/USAA991027.md): Skin · corroded · Sep 24, 1999 · N225US · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - DURING A RON VISUAL INSPECTION, FOUND CORROSION APPROXIMATELY 2 INCH BY 8 INCH AT BS 500B PLUS 14 INCHES, STR 28R SKIN. DAMAGE CUT-OUT AND INSTALLED DOUBLER AND FILLER PER SRM 53-30-03 FIG 6. (X)
- [SDR USAA990673](https://openairdocs.org/sdr/USAA990673.md): Skin · cracked · Jul 10, 1999 · N225US · Boeing 737201 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK IN SKIN AT STATION 727B AND STRINGER 18L, SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M)
- [SDR USAA990663](https://openairdocs.org/sdr/USAA990663.md): Seat Track · corroded · Jul 3, 1999 · N225US · Boeing 737201 · Fuselage, Seat/Cargo Attach Fittings
  > TPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND MINOR CORROSION AT FORWARD END OF LEFT SEAT TRACK INBOARD AND OUTBOARD, CORROSION LEVEL 1. SPLICED IN AND FABRICATED REPAIR PARTS PER SRM 53-10-5 FIG 2. (M)
- [SDR USAASB98215](https://openairdocs.org/sdr/USAASB98215.md): Battery Pack · discharged · Aug 13, 1998 · N225US · Boeing 737201 · Emergency Lighting
  > PHL - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA980008](https://openairdocs.org/sdr/USAA980008.md): Skin · cracked · Jan 10, 1998 · N225US · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DURING BX-1 CHECK VISUAL INSPECTION, FOUND 1.75 INCH CRACK STATION 935 STRINGER 24L SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M)
- [SDR USAASB97124](https://openairdocs.org/sdr/USAASB97124.md): Fuel Pump · failed · May 7, 1997 · N225US · Boeing 737201 · Engine Fuel Pump
  > CLT - FL1173, ON CLIMB-OUT AT APPROX 1,200 FT, THE NR 1 ENG LOST THRUST. THE LOW OIL PRESS LIGHT CAME ON WITH NO OTHER INDICATIONS. CAPTAIN PERFORMED SINGLE ENGINE FAILURE CHECKLIST AND SHUTDOWN THE NR 1 ENGINE. AN EMERGENCY WAS DECLARED. FLIGHT RETURNED T
- [SDR USAA960680](https://openairdocs.org/sdr/USAA960680.md): Stringer · corrosion · Oct 18, 1996 · N225US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION APPROX 2 INCH BY 2 INCH STATION 947.5 STRINGER 27L. REPLACED STRINGER FROM STATION 940 TO 1016, REPAIRED PER SRM 53-10-3. CORROSION TASK NR 53-202-01, CORROSION LEVEL 1. (M)
- [SDR USAA960679](https://openairdocs.org/sdr/USAA960679.md): Skin · cracked · Oct 18, 1996 · N225US · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.24 INCH CRACK EXT SKIN LBL 3 BS 380. INSTALLED DOUBLER, REPAIRED PER TR 53-30-04. (M)
- [SDR USAA960678](https://openairdocs.org/sdr/USAA960678.md): Frame · crack · Oct 18, 1996 · N225US · Boeing 737201 · Fuselage Main, Frame
  > DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK FRAME STATION 767 AT STRINGER 21 LEFT. INSTALLED DOUBLER, REPAIRED PER SRM 53-10-4. (M)
- [SDR USAA960677](https://openairdocs.org/sdr/USAA960677.md): Web · cracked · Oct 18, 1996 · N225US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND TWO CRACKS APPROX 1 INCH LONG EACH IN VERTICAL WEB STATION 706 LBL 24. INSTALLED DOUBLER AND ANGLES, REPAIRED PER SRM 51-40-2. (M)
- [SDR USAA960676](https://openairdocs.org/sdr/USAA960676.md): Web · cracked · Oct 18, 1996 · N225US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CRACKS APPROXIMATELY 1 INCH LONG IN VERTICAL WEB STATION 706 RBL 24. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M)
- [SDR USAA960675](https://openairdocs.org/sdr/USAA960675.md): Skin · cracked · Oct 18, 1996 · N225US · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2.875 INCH CRACK IN SKIN BS 727B AT STRINGER 17R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER. REPAIRED PER SRM 53-30-3. (M)
- [SDR USAA960674](https://openairdocs.org/sdr/USAA960674.md): Former · corroded · Oct 18, 1996 · N225US · Boeing 737201 · Fuselage Miscellaneous Structure
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH STATION 500 A STRINGER 26 R FORMER. INSTALLED DOUBLER REPAIR, REPAIRED PER SRM 51-40-3, CORROSION TASK NR C53-208-01, CORROSION LEVEL 1. (M)
- [SDR USAA960673](https://openairdocs.org/sdr/USAA960673.md): Frame · cracked · Oct 18, 1996 · N225US · Boeing 737201 · Service Doors
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 CRACKS.25 INCH AND.375 INCH FORWARD SERVICE DOOR AFT FRAME 1 AT NR 3 STOP, 1 AT NR 4 STOP. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3. (M)
- [SDR USAA960672](https://openairdocs.org/sdr/USAA960672.md): Skin · cracked · Oct 18, 1996 · N225US · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK BS 754 ABOVE STRINGER 18R FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6 AND EA 58706. (M)
- [SDR USAA960671](https://openairdocs.org/sdr/USAA960671.md): Keel Beam · corrosion · Oct 18, 1996 · N225US · Boeing 737201 · Fuselage Main, Keel
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 SCREW HOLES CORRODED.25 INCH AROUND OPENINGS, BS 720-725 RIGHT FLANGE UPPER SIDE KEEL BEAM. INSTALLED DOUBLER AFTER SPOT FACING, REPAIRED PER EA NR 41637. CORROSION TASK NR C53-212-01, CORROSION LEVEL 1. (M
- [SDR USAASB96167](https://openairdocs.org/sdr/USAASB96167.md): Door Tape · detached · Aug 23, 1996 · N225US · Boeing 737201 · Passenger/Crew Doors
  > CLT - FL 1024 - CREW AND PASSENGERS HEARD A LOUD THUMPING NOISE COMING FROM THE TOP OF THE AIRCRAFT DURING CLIMB. AT APPROX 5,000 FEET, CREW DECIDED TO RETURN TO FIELD AT CLT. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE DISCOVERED DUCT TAPE AT UPPER
- [SDR USAA960427](https://openairdocs.org/sdr/USAA960427.md): Skin · cracked · May 8, 1996 · N225US · Boeing 737201 · Fuselage Main, Plate/Skin
  > ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND.75 INCH CRACK FUSELAGE SKIN AT BS 727 A BETWEEN STRINGER 15 AND 16 LEFT. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 PAGE 01. (M)
- [SDR USAA951335](https://openairdocs.org/sdr/USAA951335.md): Skin · delamination · Dec 15, 1995 · N225US · Boeing 737201 · Fuselage Main, Plate/Skin
  > INT - DURING 'DROP IN-AV' VISUAL/ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES AND LOCATIONS, FROM BS 727-908 LEFT WINDOW BELT PANEL BS 727-908 LEFT SIDE. REPLACED UPPER ROW OF FASTENERS BS 727-908 S-14 L. REPAIRED PER EA 31780. (M)
- [SDR USAASB95003](https://openairdocs.org/sdr/USAASB95003.md): Fuel Pump · failed · Oct 23, 1995 · N225US · Boeing 737201 · Engine Fuel Pump
  > PHL - FL 330, CLIMBING OUT OF LGA, AT FL 280, THE LEFT ENGINE SHUT DOWN AND COULD NOT BE RESTARTED. FLIGHT DIVERTED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN FUEL PUMP FAILED AND REPLACED IT. (M)
- [SDR USAA950926](https://openairdocs.org/sdr/USAA950926.md): Stringer · corroded · Jul 20, 1995 · N225US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > INT - DURING 'CD-6' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BETWEEN STATION 967 AND 986.5 AT S-27L. INSTALLED REPAIR SPLICES. REPAIRED PER SRM 53-10-3. (M)
- [SDR USAA950925](https://openairdocs.org/sdr/USAA950925.md): Stringer · corroded · Jul 20, 1995 · N225US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > INT - DURING 'CX-6' CHECK VISUAL INSPECTION, FOUND 4 INCH BY 2 INCH CORRODED AREA BETWEEN STATION 947.5 AND 967 AT S-26L. INSTALLED REPAIR SPLICES. REPAIRED PER SRM 53-10-3. (M)
- [SDR USAA950212](https://openairdocs.org/sdr/USAA950212.md): Eel Assembly · inoperative · Mar 5, 1995 · N225US · Boeing 737201 · Emergency Lighting
  > GSO - EMERGENCY LIGHT OVER DOOR 2L 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 = 'N225US' AND deregistration_id = 'N225US-2017-03-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N225US-2017-03-06/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.