# N309WA: 1986 Boeing 737-347, registration cancelled 2006-11-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 2, 2006 - Exported to: Bermuda - Status when cancelled: Triennial form not returned - Airframe: [Boeing 737-347](https://openairdocs.org/model/boeing-737-347) (registry code 138447U) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 23442 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 13, 1986 - Certificate issued: August 5, 2002 - Last registry action: January 17, 2006 - Mode S code: A342B6 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N309WA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=309WA - Page: https://openairdocs.org/deregistered/N309WA-2006-11-02 From the FAA registry file of November 4, 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 737-347: https://openairdocs.org/model/boeing-737-347.md ## Service difficulty reports (42) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL733050659](https://openairdocs.org/sdr/DL733050659), Oct 20, 2005: SKIN. CRACKED. A CRACK WAS FOUND IN THE FUSELAGE SKIN. CRACK IS APPROX 2 INCHES LONG AFT OF BS 727D, JUST BELOW STR 23L. REPAIRED WITH DOUBLER PER ER/A 451209-14AD, REF AD 200 - [SDR DL733050637](https://openairdocs.org/sdr/DL733050637), Oct 19, 2005: SKIN. CRACKED. FUSELAGE SKIN CRACK WAS FOUND AT CHEM MILL LINE AT BS 727E, STR 24R. CRACK IS 3 INCHES LONG. DOULBER INSTALLED PER ER/A 451199-14AD, AD 2004-18-06, AND SRM 53-0 - [SDR DL733050497](https://openairdocs.org/sdr/DL733050497), Aug 29, 2005: INDICATOR. UNSERVICEABLE. DURING T/O ROLL AFTER 80 KTS NR 2 OIL PRESS ROLLED BACK TO BELOW THE RED DIAL. ALL OTHER IND NORMAL. CONTINUED T/O AND PERFORMED LOP CK LIST PROCEDURE PER QRH. - [SDR DL733050214](https://openairdocs.org/sdr/DL733050214), Apr 11, 2005: CIRCUIT BREAKER. TRIPPED. ON CLIMBOUT, BATTERY ON DC- IRS LIGHTS ILLUMINATED. BATTERY VOLTS ZERO. RETURNED TO SLC. MTC IN WORK. FOUND HOT BATTERY BUS C/B POPPED P18 PNL. RESET C/B. PERFO - [SDR DL733050137](https://openairdocs.org/sdr/DL733050137), Feb 27, 2005: APU. FUSES. CREW REPORTS FUMES IN CABIN WHILE AT THE GATE. DEPLANED PASSENGERS AND TURNED OVER TO MAINTENANCE. REPLACED APU PER MM. - [SDR DL733040617](https://openairdocs.org/sdr/DL733040617), Jun 30, 2004: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT STA 767 AND STR 22R AT A CHEM MILL LOCATION. REPAIRED IN ACCORDANCE WITH ERA 091533-14. - [SDR DL733040616](https://openairdocs.org/sdr/DL733040616), Jun 30, 2004: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT CHEM MILL LINE AT STA 727E BETWEEN STR 23L AND 25L. REPAIRED IAW 091565-14. - [SDR DL733040311](https://openairdocs.org/sdr/DL733040311), Apr 5, 2004: PSU. INOPERATIVE. PAX SEAT 19DEF 02 MASKS DID NOT DEPLOY WHEN SWITCH IN COCKPIT PUSHED. REPLACED PSU. - [SDR DL733040216](https://openairdocs.org/sdr/DL733040216), Mar 5, 2004: WIRE. SHORTED. AFT OVEN RIGHT SIDE DOUBLE HAD SMOKE COMING FROM BEHIND OVEN CONTROL. REMOVED OVEN, FOUND BURNED WIRES. REPAIRED SAME. - [SDR DL733030331](https://openairdocs.org/sdr/DL733030331), Apr 2, 2003: SKIN. GOUGED. DURING HMV INSPECTIONS, THREE (3) DENTS WERE FOUND IN THE FUSELAGE SKIN BETWEEN FS 757 AND 767 IN THE BAY BETWEEN STRINGERS 20R AND 21R. ADDITIONALLY, FOUR (4) - [SDR DL733030330](https://openairdocs.org/sdr/DL733030330), Apr 2, 2003: FITTING. MISALIGNED. VERTICAL STABILIZER REAR TERMINAL FITTING LUGS WERE DETERMINED TO HAVE UNDERGONE PREVIOUS REWORK WHICH LEFT THE LUG THICKNESS LESS THAN BLUEPRINT SPECIFICATIONS - [SDR DL733030328](https://openairdocs.org/sdr/DL733030328), Apr 1, 2003: SKIN. CRACKED. DURING ACCOMPLISHMENT OF PERMANENT REPAIR OF FUSELAGE SKIN/DOUBLER CRACKING, ADDITIONAL CRACK WAS FOUND IN BOTH. THE DAMAGE WAS TRIMMED OUT AND TWO EXTERNAL DOU - [SDR DL733030322](https://openairdocs.org/sdr/DL733030322), Apr 1, 2003: SKIN. DENTED. A DENT WAS FOUND IN THE FUSELAGE SKIN BETWEEN STA 1000 AND 1016 AND BETWEEN STRINGERS 13L AND 14L THE DENT IS CUT OUT AND EXTERNAL DOUBLER AND FILLER ARE INSTAL - [SDR DL733030321](https://openairdocs.org/sdr/DL733030321), Apr 1, 2003: SKIN. DENTED. REPAIR OF DENTA DENT WAS FOUND IN THE FUSELAGE SKIN BETWEEN STRINGER 17L AND 18L AT STA 360. THE DENTED MATERIAL WAS CUT OUT AND TWO EXTERNAL ALUMINUM DOUBLERS - [SDR DL733030320](https://openairdocs.org/sdr/DL733030320), Mar 31, 2003: SKIN. WORN. THE FUSELAGE SKIN WITH AN AREA OF WEAR BETWEEN FS 857 & 877 NEAR STRINGER 1. THE DAMAGE WAS BLENDED SMOOTH AND AN AREA CUTOUT. THE DAMAGE WAS REPAIRED WITH AN A - [SDR DL733030317](https://openairdocs.org/sdr/DL733030317), Mar 30, 2003: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND DENTED AND CRACKED AT THE LOWER FWD CORNER OF THE C2 DOOR OPENING. THE DAMAGE WAS REMOVED WITH A 1.5 X 1 INCH CUTOUT TO THE CORNER T - [SDR DL733030314](https://openairdocs.org/sdr/DL733030314), Mar 29, 2003: SKIN. DENTED. THE FUSELAGE SKIN WAS FOUND DENTED NEAR FS 470 BETWEEN STRINGERS 22L & 23L. THE DENT WAS REMOVED WITH A 7 INCHES CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM R - [SDR DL733030313](https://openairdocs.org/sdr/DL733030313), Mar 29, 2003: FITTING. CORRODED. THE AFT LUG OF THE CROWN BEAM FITTING ON THE NR 2 ENGINE PYLON WAS FOUND WITH CORROSION IN THE HOLE BORE. THE BORE WAS OVERSIZED TO 3.10 INCH TO REMOVE THE CORR - [SDR DL733020608](https://openairdocs.org/sdr/DL733020608), May 30, 2002: PROXIMITY SENSOR. FAULTY. FWD CARGO DOOR LIGHT CAME ON DURING T/O AT 130 KTS. CONTINUED T/O AND RETURNED TO AIRPORT. CARGO DOOR IND LIGHT INTERMITTENT. REPLACED FWD CARGO DOOR SENSOR PER - [SDR DL733001656](https://openairdocs.org/sdr/DL733001656), Aug 26, 2000: BUSHING. WORN. THE STRUT CROWN BEAM ON THE NR 1 ENGINE PYLON WAS FOUND WITH A MIGRATED BUSHING. THE BUSHING WAS REMOVED AND WEAR DAMAGE DISCOVERED IN THE BORE. THE BORE WAS OV - [SDR DL733990437](https://openairdocs.org/sdr/DL733990437), Mar 3, 1999: SKIN. CRACKED. FUSELAGE SKIN WAS FOUND CRACKED AROUND THE AFT EDGE OF THE E/E COMPT COOLING AIR EXHAUST DUCT CUTOUT AT BS 380, BL 0.0. THE CRACK EXTENDS AFT FROM THE EDGE OF C - [SDR DL733990436](https://openairdocs.org/sdr/DL733990436), Mar 3, 1999: BULKHEAD WEB. CRACKED. BS 178 BLKHD WEB WAS FOUND WITH 6 CRACKS, MAX CRACK CUTOUT WAS 1.6 BY 1. REPAIRED PER ERA 332820-14. - [SDR DL733990387](https://openairdocs.org/sdr/DL733990387), Feb 24, 1999: INTERCOSTAL. CRACKED. R1 DOOR INTERCOSTAL AT STRINGER 8A FOUND CRACKED AT STA 334. CRACK REPAIRED PER S/B 737-53A1108 (REF ERA 332823-14AD). ACTION TAKEN, 332823-14AD. - [SDR DL733990386](https://openairdocs.org/sdr/DL733990386), Feb 23, 1999: SKIN. CRACKED. CRACK IN NR 1 PYLON STRUT SKIN AT THE ACCESS OPENING 5727L. ACTION TAKEN, 332810-14. - [SDR DL733971795](https://openairdocs.org/sdr/DL733971795), Sep 13, 1997: OVEN CONTROLLER. MALFUNCTIONED. ELECTRICAL SMELL AND SMOKE EMITTING FROM F/C GALLEY. COTNTRACT MTC CHECKING SAME. REPLACED BOTH CONTROLLERS. - [SDR DL733960632](https://openairdocs.org/sdr/DL733960632), Mar 21, 1996: TRACK LIGHTS. INOPERATIVE. ON AIRCRAFT ARRIVAL, EMERGENCY PATH TRACK LIGHTING INOP. CONTRACT MTC CALLED OUT, PARTS SENT BUT WERE UNABLE TO CORRECT PROBLEM. FLIGHT FERRIED TO DFW. REPLACED - [SDR DL733961622](https://openairdocs.org/sdr/DL733961622), Feb 22, 1996: SKIN. WORN. FUSELAGE SKIN (0.036 CLAD 2024-T3) UNDERNEATH THE VERTICAL STABILIZER FORWARD FAIRING FROM FS 870 TO 890 WAS FOUND WORN BEYOND B737-300 SRM 53-00-01 LIMITATIONS - [SDR DL733960043](https://openairdocs.org/sdr/DL733960043), Jan 6, 1996: ENGINE. FOD. SHORTLY AFTER T/O, AN ELEC ODOR DEVELOPED IN THE CABIN. COMPLIED WITH CHECKLIST. REMOVED SMALL AMOUNT OF COMPUTER PAPER FROM NR 2 ENG. RAN ENGINE PER PFHB, NO O - [SDR DL733970009](https://openairdocs.org/sdr/DL733970009), Jan 3, 1996: FIRE DETECTOR. SHORTED. LAV FIRE WARNING LIGHT AND CHIME CAME ON TWICE DURING FLIGHT WITHOUT CAUSE. REPLACED FORWARD LAV DETECTOR UNIT, OPERATIONAL TEST NORMAL. - [SDR DL733950825](https://openairdocs.org/sdr/DL733950825), Feb 20, 1995: FLOOR SUPPORT. CRACKED. AT HMV, FOUND AFT B/B FLOOR SUPPORT CRACKED AT TIE DOWN FITTING STA 727B LT AND 727D RT. REPAIRED PER SRM 53-00-53 FIG 202. - [SDR DL733950766](https://openairdocs.org/sdr/DL733950766), Feb 20, 1995: SEAT TRACK. CORRODED. FOUND AT H.M.V. RT I/B SEAT TRACK CORRODED AT FS 328. REPAIRED PER SRM 53-00-52 PG 202. - [SDR DL733950765](https://openairdocs.org/sdr/DL733950765), Feb 20, 1995: SEAT TRACK. CORRODED. FOUND AT H.M.V. RT CTR SEAT TRACK CORRODED BETWEEN STA 328 AND 344. REPAIRED PER SRM 53-00-52 PG 202. - [SDR DL733950893](https://openairdocs.org/sdr/DL733950893), Feb 18, 1995: SKIN. DENTED. DURING ROUTINE INSPECTION, SEVERAL SMALL DENTS AND ONE SKIN PUNCTURE WERE FOUND ON INSIDE SKIN OF I/B SPOILER. DAMAGE WAS CAUSED FROM DEBRIS THROWN FROM THE MAI - [SDR DL733950770](https://openairdocs.org/sdr/DL733950770), Feb 17, 1995: SKIN. CRACKED. LT ELEVATOR TAB HINGE OPENINGS CRACKED SEVERAL PLACES. FOUND AT H.M.V. REPAIRED PER SRM 55-20-01. - [SDR DL733950772](https://openairdocs.org/sdr/DL733950772), Feb 16, 1995: SKIN. DAMAGED. RT ELEVATOR TAB HAS COMPOSITE BROKEN OUT AT HINGE OPENINGS. FOUND AT H.M.V. REPAIRED PER SRM 51-40-15. - [SDR DL733950769](https://openairdocs.org/sdr/DL733950769), Feb 16, 1995: SKIN. DAMAGED. FOUND AT H.M.V. RT ELEVATOR HAS SCAB PATCH ON BOTTOM SURFACE OF COMPOSITE. REPAIRED PER SRM 51-70-17. - [SDR DL733950768](https://openairdocs.org/sdr/DL733950768), Feb 16, 1995: TE SKIN. DAMAGED. LT ELEVATOR HAS INBOARD TRAILING EDGE DAMAGED. FOUND AT H.M.V. REPAIRED PER SRM 55-20-01. PART DAMAGED DURING ROUTING. - [SDR DL733950767](https://openairdocs.org/sdr/DL733950767), Feb 16, 1995: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED LBL 25 FS 947-967. FOUND AT H.M.V. REPAIRED PER SRM 53-00-52 FIG 204. - [SDR DL733950764](https://openairdocs.org/sdr/DL733950764), Feb 16, 1995: SEAT TRACK. CORRODED. LT I/B SEAT TRACK CORRODED AT F.S. 947. FOUND AT H.M.V. REPAIRED PER SRM 53-00-52. - [SDR DL733950711](https://openairdocs.org/sdr/DL733950711), Feb 16, 1995: FLOOR BEAM. CORRODED. FOUND AT HMV, FLOOR BEAM CORRODED AT FS 328. CORROSION AT BL 0 AND RIGHT OF BL. REPAIRED PER SRM 53-00-51 FIG 205. - [SDR DL733953045](https://openairdocs.org/sdr/DL733953045), Feb 15, 1995: LE SKIN. WORN. NR 1 FOREFLAP, L/E WORN 14 INCHES FROM O/B END AND 56 INCHES FROM I/B END. REPAIRED PER SRM 57-53-01 FIG 201, AT HMV SHOP INSPECTION. - [SDR DL733950783](https://openairdocs.org/sdr/DL733950783), Feb 15, 1995: WEDGE. DELAMINATED. AT HMV, FOUND FLAP TRAILING EDGE WEDGE DELAMINATED AT ITS OUTBOARD END. REPAIRED PER SRM 57-53-02. ## FAA accident and incident reports (3) 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 19930829038939I](https://openairdocs.org/incident/19930829038939I), Aug 29, 1993: Boeing 737347 (N309WA), Jackson, WY. Cabin pressure exceeded 14000FT. Passenger oxygen masks deployed. Continued to salt lake city. Crew mismanaged system - [Incident 19900729055849I](https://openairdocs.org/incident/19900729055849I), Jul 29, 1990: Boeing 737347 (N309WA), Jackson, WY. Landed long and departed end of runway. - [Incident 19890817052289I](https://openairdocs.org/incident/19890817052289I), Aug 17, 1989: Boeing 737347 (N309WA), Burbank, CA. Electrical failure on final. Landed safely. NR2 and 3 transformer rectifier circuit breakers had tripped. --- 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.