# N240AU: Boeing 737-201, registration cancelled 2017-02-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 28, 2017 - Status when cancelled: Registration expired, pending cancellation - 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: 22355 - Type of aircraft: Fixed wing multi engine - Certificate issued: March 1, 2005 - Last registry action: June 18, 2008 - Mode S code: A23012 - 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/N240AU - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=240AU - Page: https://openairdocs.org/deregistered/N240AU-2017-02-28 From the FAA registry file of November 3, 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 (38) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR RYAN20050018](https://openairdocs.org/sdr/RYAN20050018), Jun 12, 2005: WARNING SYSTEM. ACTIVATED. DURING CLIMB, ENGINE NR 1 HAD HIGH OIL PRESSURE AND SHORTLY THEREAFTER NR 1 OIL TEMPERATURE STARTED CLIMBING TOWARDS REDLINE. ON RETURN NR 1 ENGINE WAS SHUTDOWN - [SDR RYAN200500018](https://openairdocs.org/sdr/RYAN200500018), Jun 12, 2005: BULB. FAULTY. DURING CLIMB, ENGINE NR 1 HAD HIGH OIL PRESSURE AND SHORTLY THEREAFTER NR 1 OIL TEMPERATURE STARTED CLIMBING TOWARDS REDLINE. ON RETURN, NR 1 ENGINE SHUTDOWN. - [SDR 193](https://openairdocs.org/sdr/193), Jun 12, 2005: BULB. MALFUNCTIONED. DURING CLIMB, ENGINE NR 1 HAD HIGH OIL PRESSURE AND SHORTLY THEREAFTER NR 1 OIL TEMPERATURE STARTED CLIMBING TOWARDS REDLINE. ON RETURN, NR 1 ENGINE SHUTDOWN. - [SDR RYNA200500003](https://openairdocs.org/sdr/RYNA200500003), Jan 17, 2005: INTERCOSTAL. CRACKED. MAIN CABIN FLOOR BEAM INTERCOSTAL CRACKED AT BS 328 TO 344, LBL 45. REPAIRED CRACKED INTERCOSTAL AT BS 328 TO 344, LBL 45. - [SDR RYNA200500002](https://openairdocs.org/sdr/RYNA200500002), Jan 17, 2005: FLOORBEAM. CORRODED. MAIN CABIN FLOOR BEAM, UPPER CHORD, UPPER SURFACE CORRODED AT BS 1006, LBL 29. REMOVED CORROSION ON FLOOR BEAM, FABRICATED, TREATED AND INSTALLED REPAIR PARTS. - [SDR 2004F00170](https://openairdocs.org/sdr/2004F00170), Mar 14, 2004: LINE. LEAKING. DURING CRUISE FROM GSO-ACY, EXPERIENCED A LOSS OF THE A-SYSTEM HYDRAULICS. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED AT ACY WITHOUT INCIDENT. REMOVED AND RE - [SDR USAASB00177](https://openairdocs.org/sdr/USAASB00177), Jun 23, 2000: INDICATOR. FAILED. CLE - FLT 1231 - ON APPROACH TO CLE, CREW WAS UNABLE TO EXTEND FLAPS. CREW ACCOMPLISHED GO AROUND AND QUICK REFERENCE HANDBOOK PROCEDURES. CREW RECEIVED PARTIAL - [SDR USAASB00169](https://openairdocs.org/sdr/USAASB00169), Jun 17, 2000: CONNECTOR. DAMAGED. IAD - FLT 797 - ON APPROACH TO IAD, THE FLAPS WOULD NOT EXTEND BEYOND 10 DEGREES. CRWE COMPLETED CHECK FOR FLAPS AND FIRST OFFICER WENT BACK INTO CABIN FOR VISU - [SDR USAASB00066](https://openairdocs.org/sdr/USAASB00066), Mar 6, 2000: LIGHT. INOPERATIVE. ORD - PILOT REPORTED THE EMERGENCY EVACUATION LIGHT AT SEAT ROW 16 ABC IS INOPERABLE AND THE WIRING UNDER SEAT 16C IS HANGING DOWN. MAINTENANCE REPAIRED WIRING - [SDR USAA000196](https://openairdocs.org/sdr/USAA000196), Feb 15, 2000: SKIN. CRACKED. CLT - FOUND SKIN CRACKED .5 INCH, BS 765, STRINGER 19R FUSELAGE SKIN. REPAIRED PER SRM 53-30-3 FIG 6. (M) - [SDR USAASB98156](https://openairdocs.org/sdr/USAASB98156), Jun 25, 1998: SWITCH. FAILED. PHL - FLT 452 - ON CLIMB-OUT FROM PHL, AT APPROX 5,000 FT, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. LIGHT REMAINED ON WHEN POWER WAS REDUCED TO IDLE - [SDR USAASB97327](https://openairdocs.org/sdr/USAASB97327), Nov 28, 1997: WIRE. LOOSE. PHL - FLT 461 - PILOT REPORTED THAT THE SEAT LEVEL EMERGENCY EXIT LIGHTS BRIEFLY ILLUMINATED TWICE IN FLIGHT AND EXTINGUISHED ONTHEIR OWN. MAINTENANCE INSPECTED - [SDR USAASB97320](https://openairdocs.org/sdr/USAASB97320), Nov 21, 1997: BATTERY PACK. DISCHARGED. CLT - FLT 596 - PILOT REPORTED, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS. OPS CHECK GOOD. (M) - [SDR USAASB97268](https://openairdocs.org/sdr/USAASB97268), Sep 28, 1997: BATTERY PACK. DISCHARGED. PHL - FOUND LEFT HAND ENTRY OVERHEAD EMERGENCY LIGHT INOPERABLE; BOTH EMERGENCY SLIDE LIGHTS (FORWARD LEFT) INOPERABLE AND THE LEFT HAND OVERWING EMERGENCY LIGH - [SDR USAA970264](https://openairdocs.org/sdr/USAA970264), Aug 15, 1997: SKIN. CRACKED. ROA - DURING 'A' CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK IN A/C SKIN, SKIN WAS CRACKED AT STRINGER 24L BETWEEN STATION 924 AND 947. INSTALLED REPAIR DOUBLER - [SDR USAA970263](https://openairdocs.org/sdr/USAA970263), Aug 15, 1997: STRINGER. CORRODED. ROA - DURING 'A' CHECK VISUAL INSPECTION, FOUND CORRODED AREA IN STRINGER 2 INCHES LONG STRINGER 28L, STATION 372. REPLACED DEFECTIVE PORTION OF STRINGER, REPAI - [SDR USAA970262](https://openairdocs.org/sdr/USAA970262), Aug 15, 1997: SKIN. CRACKED. ROA - DURING 'A' CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 1 INCH SKIN CRACK BS 378 BETWEEN BL 0 AND STRINGER 28L. INSTALLED DOUBLER REPAIR, REPAIRED PER TYPI - [SDR USAASB97190](https://openairdocs.org/sdr/USAASB97190), Jul 14, 1997: LINK ASSEMBLY. BROKEN. RDU - FL 607 - IMMEDIATELY FOLLOWING ROTATION, DURING GEAR RETRACTION, THE FLIGHT CREW HEARD A LOUD BANG NOISE FOLLOWED BY A VERY LOUD RUSH OF AIR. THE FIRST OF - [SDR USAASB97158](https://openairdocs.org/sdr/USAASB97158), Jun 10, 1997: POWER SUPPLY. FAILED. CLT - FL354, EMERGENCY EXIT LIGHTS ON LEFT FORWARD SEATS COME ON DURING FLIGHT AND STAY ON, EVEN IF EMERGENCY EXIT SWITCH IS TURNED OFF. MAINTENANCE REMOVED AND - [SDR USAASB97154](https://openairdocs.org/sdr/USAASB97154), Jun 8, 1997: DIODE. FAILED. PHL - AFTER ENGINE SHUTDOWN, THE SEAT MOUNTED EMERGENCY LIGHTS ILLUMINATED. MAINTENANCE REPLACED A SYSTEM DIODE. (M) - [SDR USAASB97153](https://openairdocs.org/sdr/USAASB97153), Jun 7, 1997: BATTERIES. DISCHARGED. BDL - FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE IN FORWARD AND MID CABIN AREAS. MAINTENANCE REPLACED TWO BATTERY PACKS. (M) - [SDR USAASB97136](https://openairdocs.org/sdr/USAASB97136), May 22, 1997: LIGHTS. MALFUNCTIONED. DCA - FLT 1727 - FLIGHT CREW REPORTED THAT THE EMERGENCY LIGHTS IN THE CABIN ILLUMINATED DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SWI - [SDR USAASB97133](https://openairdocs.org/sdr/USAASB97133), May 21, 1997: BATTERY. DISCHARGED. CLT - FLT 7900 - DURING TEST FLIGHT AFTER HEAVY MAINTENANCE VISIT, THE LOW LEVEL EMERGENCY EXIT LIGHTS FROM SEAT ROW 7 AND BACK ILLUMINATED. AFTER LANDING, THE - [SDR USAA970203](https://openairdocs.org/sdr/USAA970203), May 21, 1997: STRINGER. CORROSION. INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AT OUTER AREA OF STRINGER WHERE MATES W/SKIN 15 INCHES LONG BY 1 INCH WIDE, SOME AREAS COMPLETELY THRO - [SDR USAA970202](https://openairdocs.org/sdr/USAA970202), May 21, 1997: DOUBLER. CRACKED. INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND BELL CRANK CUTOUT DOUBLERS CRACKED STATION 677, RBL 25 AND LBL 25 STATION 677, RBL 25 AND LBL 25. INSTALLED NEW - [SDR USAA970201](https://openairdocs.org/sdr/USAA970201), May 21, 1997: FRAME. CRACKED. INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 639 STRINGER 16L FRAME. INSTALLED REPAIR PER DRAWING 65C31658. (M) - [SDR USAA970200](https://openairdocs.org/sdr/USAA970200), May 21, 1997: SKIN. CRACKED. INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .125 INCH AND .25 INCH CRACK LOWER HINGE CUT OUT UPPER AND LOWER CORNERS (FWD ENTRY DOOR) SKIN. INSTALLED DOUBLE - [SDR USAA970199](https://openairdocs.org/sdr/USAA970199), May 21, 1997: SKIN. CRACKED. INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK LOWER FORWARD CORNER OF FORWARD CARGO DOOR CUTOUT SKIN. INSTALLED DOUBLER, REPAIRED PER EA 42403. - [SDR USAA970198](https://openairdocs.org/sdr/USAA970198), May 21, 1997: STRINGER. CORRODED. INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH CORRODED AREA BS 919, STRINGER 25L. SPLICED STRINGER, REPAIRED PER SRM 53-10-3. (M) - [SDR USAA970197](https://openairdocs.org/sdr/USAA970197), May 21, 1997: SKIN. CRACKED. INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AFT SERVICE DOOR UPPER HINGE CUTOUT UPPER FORWARD CORNER SKIN. INSTALLED DOUBLER, REPAIRED PER S - [SDR USAA970196](https://openairdocs.org/sdr/USAA970196), May 21, 1997: SKIN. CRACKED. INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACKS 4 INCHES AND 2 INCHES AT STRINGER 18R STATION 727 A PLUS 16 INCHES AND STRINGER 18R STATION 727 A PLUS 3 - [SDR USAA970195](https://openairdocs.org/sdr/USAA970195), May 21, 1997: SKIN. CRACKED. INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK LEFT UPPER CORNER OF CAPTAINS NR 1 WINDOW FRAME FLIGHT COMPARTMENT SKIN. STOP DRILLED CRACK AND I - [SDR USAA970058](https://openairdocs.org/sdr/USAA970058), Feb 10, 1997: BRACKET. CRACKED. CLT - I NSPECTION VISUALLY FOUND A 3 INCH CRACK LOCATED AT RADIUS OF SUPPORT BRACKET, FOR NLG ACTUATOR SUPPORT BEAM AFT END. FABRICATED REPAIR BRACKET AS PER SR - [SDR USAA960693](https://openairdocs.org/sdr/USAA960693), Oct 26, 1996: SKIN. CORROSION. ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 6 INCH CORROSION STRINGER 26R BS 797 FUSELAGE SKIN. REMOVED CORROSION AND INSTALLED DOUBLER. REPAIRED - [SDR USAASB96109](https://openairdocs.org/sdr/USAASB96109), Jun 15, 1996: OIL PRESS IND. FAILED. BWI - FLT 2539 - ABOUT 50 MILES OUT OF BWI, THE CREW OBSERVED ZERO OIL PRESSURE ON THE NR 1 ENGINE. ALL OTHER INDICATIONS WERE NORMAL. FLIGHT RETURNED TO FIELD - [SDR USAA951134](https://openairdocs.org/sdr/USAA951134), Sep 18, 1995: STRINGER. CORROSION. CLT - DURING A PCI INSPECTION, A 10 INCH BY 1 INCH CORROSION WAS FOUND AT STRINGER 28R, RBL 6 BETWEEN BS 350 AND 360. REPLACED END STRINGER 28R, RBL 6. (M) - [SDR USAA951089](https://openairdocs.org/sdr/USAA951089), Sep 18, 1995: STRINGER. CORRODED. CLT - DURING A PCI INSPECTION, FOUND CORROSION 10 INCHES BY 1 INCH ON STRINGER 28R, RBL 6 BETWEEN BS 350 AND 360. CORROSION TASK NR C53-202-02/PCI 1227, CORROSI - [SDR USAA950748](https://openairdocs.org/sdr/USAA950748), Jul 8, 1995: HYDRAULIC LINE. LEAKING. ROC - FLT 2274 - UPON GEAR RETRACTION ON TAKEOFF, A-SYSTEM QUANTITY WENT TO ZERO AND A-SYSTEM LOW PRESSURE LIGHTS CAME ON. FLIGHT RETURNED TO ROC WHERE LANDING ## FAA accident and incident reports (1) 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 19950708025079I](https://openairdocs.org/incident/19950708025079I), Jul 8, 1995: Boeing 737200 (N240AU), Rochester, NY. A hydraulic system failure on takeoff. Returned. Repaired, returned to service. --- 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.