# N235US: Boeing 737-201, registration cancelled 2007-03-20

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 20, 2007
- Exported to: Pakistan
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-201](https://openairdocs.org/model/boeing-737-201) (registry code 1384454)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 22275
- Type of aircraft: Fixed wing multi engine
- Certificate issued: March 1, 2005
- Last registry action: March 1, 2005
- Mode S code: A21CE6
- 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/N235US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=235US
- Page: https://openairdocs.org/deregistered/N235US-2007-03-20

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 (26)

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

- [SDR RYNA200600001](https://openairdocs.org/sdr/RYNA200600001), Jan 10, 2006: LINK. BROKEN. ON CLIMB FROM UTA, POP AND VIBRATION WAS HEARD UNDER PILOT SEAT. AIRCRAFT DIVERTED TO MEM, LANDED WITHOUT INCIDENT. GEAR INSPECTED FOR SUSPECTED BIRD STRIKE, NO
- [SDR RYNA200500014](https://openairdocs.org/sdr/RYNA200500014), Apr 9, 2005: POTABLE WATER. LEAKING. DURING CRUISE AT FL 28.0, EXPERIENCED MULTIPLE MALFUNCTIONS. AUTO-PILOT FAILED, PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED, MACH TRIM FAIL LIGHT ILLUMINATED, AL
- [SDR USAA001015](https://openairdocs.org/sdr/USAA001015), Jul 20, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .5 INCH, AT FS 747 AND STRINGER 17L LT EXTERIOR SKIN. REPAIRED DOUBLER PER SRM 53-30-3 FIG 1, 17 AND EA 67683. (M)
- [SDR USAA000851](https://openairdocs.org/sdr/USAA000851), Jun 15, 2000: SKIN. CRACKED. TPA - FOUND FUSELAGE SKIN CRACKED 3.5 INCHES, LT FUSELAGE SKIN STATION 727A PLUS 13 JUST BELOW STRINGER 17. INSTALLED REPAIR DOUBLER PER SRM 53-30-03 FIG 1. (M)
- [SDR USAA000680](https://openairdocs.org/sdr/USAA000680), May 10, 2000: SKIN. CRACKED. CLT - SKIN CRACKED 3.125 INCHES, LT FUSELAGE EXT SKIN BETWEEN BS 770 AND BS 773, STR 17L. INSTALLED DOUBLER PER SRM 53-30-3, FIGURE 6. (X)
- [SDR USAA000261](https://openairdocs.org/sdr/USAA000261), Feb 24, 2000: SKIN. CRACKED. SKIN HAS A 3 INCH CRACK AT BS 727B STRINGER 17R. INSTALLED REPAIR DOUBLER PER SRM 53-30-6 FIG 6. (M)
- [SDR USAASB00035](https://openairdocs.org/sdr/USAASB00035), Feb 8, 2000: HARNESS. CHAFED. DTW - FLT 517 - INBOUND TO DTW FROM CLT, THE NR 1 GENERATOR BUS OFF LIGHT ILLUMINATED WITH LOSS OF ASSOCIATED SYSTEMS. THE AIRCRAFTS APU WAS ON MEL FOR NOT BEIN
- [SDR USAA990953](https://openairdocs.org/sdr/USAA990953), Sep 10, 1999: SKIN. CRACKED. CLT - DURING WALKAROUND CHECK, VISUAL INSPECTION, FOUND A .625 INCH CRACK IN SKIN AT STATION 380 2 INCHES LEFT OF CENTER LINE. INSTALLED REPAIR DOUBLERS PER TR 
- [SDR USAA990850](https://openairdocs.org/sdr/USAA990850), Aug 15, 1999: SHEAR TIE. CORRODED. TPA - DURING CX-4 CHECK VISUAL AND EDDY CURRENT, FOUND CORROSION ATTACH ANGLE SHEAR TIP STRINGER 26L STATION 967 FRAME. CORROSION LEVEL 1. REINSTALLED STRINGER 
- [SDR USAA990849](https://openairdocs.org/sdr/USAA990849), Aug 15, 1999: SKIN. CRACKED. TPA - DURING CX-4 CHECK VISUAL AND EDDY CURRENT, FOUND A 1 INCH CRACK IN SKIN AT STATION 727A PLUS 7 AND STRINGER 19L. REPAIRED PER SRM 53-30-3 FIG 1. (M)
- [SDR USAA990848](https://openairdocs.org/sdr/USAA990848), Aug 15, 1999: SKIN. CRACKED. TPA - DURING CX-4 CHECK VISUAL AND EDDY CURRENT, FOUND A 4 INCH CRACK IN SKIN AT STATION 727B PLUS 14 AND STRINGER 18L. REPAIRED PER SRM 53-30-3 FIG 25. (M)
- [SDR USAA980398](https://openairdocs.org/sdr/USAA980398), Sep 12, 1998: SKIN. CRACKED. CLT - DURING CHECK VISUAL INSPECTION, FOUND A 2 INCH SKIN CRACK 1 INCH ABOVE STR 16L 1 INCH TO 3 INCHES FORWARD OF STA 727B ON SKIN. INSTALLED DOUBLER PER SRM 5
- [SDR USAASB98217](https://openairdocs.org/sdr/USAASB98217), Aug 21, 1998: INDICATOR. MALFUNCTIONED. TYS - FLT 1797 - AT 29,000 FT, THE NR 1 ENGINE OIL QTY SLOWLY DROPPED TO ONE GALLON AND EVENTUALLY TO A HALF GALLON. ALL OTHER INDICATIONS WERE NORMAL. FLIGHT D
- [SDR 98ZZZM819](https://openairdocs.org/sdr/98ZZZM819), Aug 21, 1998: TRANSMITTER. MALFUNCTIONED. TYS - FLT 1797 - AT 29,000 FT, THE NR 1 ENGINE OIL QTY SLOWLY DROPPED TO ONE GALLON AND EVENTUALLY TO A HALF GALLON. ALL OTHER INDICATIONS WERE NORMAL. FLIGHT D
- [SDR USAASB98175](https://openairdocs.org/sdr/USAASB98175), Jul 10, 1998: BATTERY PACK. DISCHARGED. ALB - MAINTENANCE FOUND THE AFT ENTRY AND AFT SERVICE DOOR EXTERIOR EVACUATION LIGHTS AND THE INTERIOR SIDEWALL EMERGENCY EXIT SIGNS BY EACH DOOR INOP. MAINTENA
- [SDR USAA980281](https://openairdocs.org/sdr/USAA980281), Jun 23, 1998: ANGLE. CRACKED. INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 727 RBL 6.5 ATTACH ANGLE. REPAIRED PER SRM 51-10-1. (M)
- [SDR USAA980280](https://openairdocs.org/sdr/USAA980280), Jun 23, 1998: BEAM. FRETTED. INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 20 INCH FRETTED AREA BETWEEN BS 663-727 BEAM. INSTALLED REPAIR STRAP AND REPAIRED PER EA 44092. (M)
- [SDR USAA980297](https://openairdocs.org/sdr/USAA980297), Jun 22, 1998: FLOORBEAM. CORRODED. CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1.3750 INCH AREA OF CORROSION ON FLOORBEAM STA 106 LBL 18. INSTALLED T-CAP PER TR 53-10-05C. (X)
- [SDR USAA980017](https://openairdocs.org/sdr/USAA980017), Jan 16, 1998: SKIN. CRACKED. ROA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER SKIN. DOUBLER REPAIR INSTALLED, REPAIRED PER EA 61143
- [SDR USAA980016](https://openairdocs.org/sdr/USAA980016), Jan 16, 1998: SKIN. CRACKED. ROA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK STRINGER 24L, STATION 945 SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)
- [SDR USAASB97250](https://openairdocs.org/sdr/USAASB97250), Sep 11, 1997: PROXIMITY SENSOR. DEFECTIVE. PHL (FL 993) - DURING CLIMB-OUT WITH FLAPS RETRACTED,THE NR 4 LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED. AIRCRAFT RETURNED TO FIELD (PHL). NO EMERGENCY WAS DE
- [SDR USAASB96228](https://openairdocs.org/sdr/USAASB96228), Nov 16, 1996: OIL GAUGE. FAILED. BWI - FL 322 - AFTER TAKEOFF, THE NR 2 ENGINE OIL PRESSURE WENT FROM LOWER GREEN LINE TO MID YELLOW BAND. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FUR
- [SDR 96ZZZM1563](https://openairdocs.org/sdr/96ZZZM1563), Nov 16, 1996: OIL TRANSMITTER. FAILED. BWI - FL 322 - AFTER TAKEOFF, THE NR 2 ENGINE OIL PRESSURE WENT FROM LOWER GREEN LINE TO MID YELLOW BAND. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FUR
- [SDR USAA960689](https://openairdocs.org/sdr/USAA960689), Oct 20, 1996: SKIN. CRACKED. INT - DURING B-CHECK, EDDY CURRENT INSPECTION, FOUND .120 INCH CRACK LOWER FORWARD CORNER OF FORWARD SERVICE DOOR LOWER CUT OUT IN RADIUS SKIN. INSTALLED DOUBLE
- [SDR USAA960608](https://openairdocs.org/sdr/USAA960608), Sep 13, 1996: SKIN. CRACKED. CLT - INSPECTION VISUALLY FOUND 1 INCH AND 1.4 INCH SKIN CRACKS LOCATED AT STATION 727A, 2 INCH AND PLUS 7 INCH IN THE FUSELAGE SKIN, RIGHT BL 70 BETWEEN STRING
- [SDR USAASB96148](https://openairdocs.org/sdr/USAASB96148), Aug 6, 1996: SNUBBER. MISINSTALLED. PHL - FL 351 - DURING CLIMB-OUT, FLIGHT ATTENDANT REPORTED AN EXCESSIVE NOISE COMING FROM THE FORWARD MAIN ENTRANCE DOOR. THE CAPTAIN INDICATED THE CABIN WAS PR

---
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.