# N225US: 1979 Boeing 737-201, registration cancelled 2017-03-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 6, 2017 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Boeing 737-201](https://openairdocs.org/model/boeing-737-201) (registry code 1384454) - Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 21667 - Year built: 1979 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: March 10, 2005 - Certificate issued: March 1, 2005 - Last registry action: June 18, 2008 - Mode S code: A1F567 - Owner when cancelled: [Savanna Aviation LLC](https://openairdocs.org/faa-owner/SAVANNA%20AVIATION%20LLC) - Location: [Horseshoe Bay, TX](https://openairdocs.org/faa-place/TX/Horseshoe%20Bay) - Owner type: Corporation - Owner's area on the map: 30.5258° N, 98.3759° W: Placed by OpenAirDocs at the center of ZIP code 78657, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N225US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=225US - Page: https://openairdocs.org/deregistered/N225US-2017-03-06 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 737-201: https://openairdocs.org/model/boeing-737-201.md ## Service difficulty reports (35) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR RYNA200600002](https://openairdocs.org/sdr/RYNA200600002), Feb 3, 2006: ENGINE. BIRD INGESTION. 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 - [SDR RYNA200500022](https://openairdocs.org/sdr/RYNA200500022), Jul 6, 2005: OIL SYSTEM. OVERTEMP. 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 PRESS - [SDR RYAN200500020](https://openairdocs.org/sdr/RYAN200500020), Jul 3, 2005: SPEED BRAKE. WORN. 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 AD - [SDR RYNA200500011](https://openairdocs.org/sdr/RYNA200500011), Apr 2, 2005: SEAL. OUT OF ADJUST. 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. ADJUST - [SDR RYNA200500010](https://openairdocs.org/sdr/RYNA200500010), Apr 2, 2005: AUTOPILOT SYS. MALFUNCTIONED. 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 C - [SDR USAA011301](https://openairdocs.org/sdr/USAA011301), Sep 12, 2001: STRINGER. CORRODED. 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), Jun 5, 2000: SKIN. CRACKED. 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), Apr 8, 2000: GEARBOX. LEAKING. 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 - [SDR USAA000388](https://openairdocs.org/sdr/USAA000388), Mar 21, 2000: STRINGER. CRACKED. 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), Mar 21, 2000: SKIN. CRACKED. 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), Jan 25, 2000: BATTERY PACK. DISCHARGED. SYR - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT, IN THE FORWARD CEILING, CYCLING ON AND OFF. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHE - [SDR USAA991028](https://openairdocs.org/sdr/USAA991028), Sep 24, 1999: STRINGER. CORRODED. 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 - [SDR USAA991027](https://openairdocs.org/sdr/USAA991027), Sep 24, 1999: SKIN. CORRODED. 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 DOUBL - [SDR USAA990673](https://openairdocs.org/sdr/USAA990673), Jul 10, 1999: SKIN. CRACKED. 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), Jul 3, 1999: SEAT TRACK. CORRODED. 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 FABRI - [SDR USAASB98215](https://openairdocs.org/sdr/USAASB98215), Aug 13, 1998: BATTERY PACK. DISCHARGED. 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), Jan 10, 1998: SKIN. CRACKED. 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), May 7, 1997: FUEL PUMP. FAILED. 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 ENG - [SDR USAA960680](https://openairdocs.org/sdr/USAA960680), Oct 18, 1996: STRINGER. CORROSION. 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, REPAIR - [SDR USAA960679](https://openairdocs.org/sdr/USAA960679), Oct 18, 1996: SKIN. CRACKED. 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), Oct 18, 1996: FRAME. CRACK. 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), Oct 18, 1996: WEB. CRACKED. 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 PE - [SDR USAA960676](https://openairdocs.org/sdr/USAA960676), Oct 18, 1996: WEB. CRACKED. 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 - [SDR USAA960675](https://openairdocs.org/sdr/USAA960675), Oct 18, 1996: SKIN. CRACKED. 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 DOUB - [SDR USAA960674](https://openairdocs.org/sdr/USAA960674), Oct 18, 1996: FORMER. CORRODED. 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- - [SDR USAA960673](https://openairdocs.org/sdr/USAA960673), Oct 18, 1996: FRAME. CRACKED. 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 - [SDR USAA960672](https://openairdocs.org/sdr/USAA960672), Oct 18, 1996: SKIN. CRACKED. 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 E - [SDR USAA960671](https://openairdocs.org/sdr/USAA960671), Oct 18, 1996: KEEL BEAM. CORROSION. 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 - [SDR USAASB96167](https://openairdocs.org/sdr/USAASB96167), Aug 23, 1996: DOOR TAPE. DETACHED. 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 T - [SDR USAA960427](https://openairdocs.org/sdr/USAA960427), May 8, 1996: SKIN. CRACKED. 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 5 - [SDR USAA951335](https://openairdocs.org/sdr/USAA951335), Dec 15, 1995: SKIN. DELAMINATION. 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 S - [SDR USAASB95003](https://openairdocs.org/sdr/USAASB95003), Oct 23, 1995: FUEL PUMP. FAILED. 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. - [SDR USAA950926](https://openairdocs.org/sdr/USAA950926), Jul 20, 1995: STRINGER. CORRODED. 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 - [SDR USAA950925](https://openairdocs.org/sdr/USAA950925), Jul 20, 1995: STRINGER. CORRODED. 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 - [SDR USAA950212](https://openairdocs.org/sdr/USAA950212), Mar 5, 1995: EEL ASSEMBLY. INOPERATIVE. GSO - EMERGENCY LIGHT OVER DOOR 2L INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY. (Z) ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19950610018409I](https://openairdocs.org/incident/19950610018409I), Jun 10, 1995: Boeing 737200 (N225US), Kansas City, MO, Minor damage. Narrative: us air flight US317 was enroute to kci, when the copilots window started to crack. The aircraft was in level flight at 22,000 ft. when this incident… - [Incident 19920212006499I](https://openairdocs.org/incident/19920212006499I), Feb 12, 1992: Boeing 737201 (N225US), Cleveland, OH. NR1 engine fire warning on descent. Shut engine down. Landed safely. No fire. Faulty fire detection unit. --- 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.