# N302WA: Boeing 737-347, registration cancelled 2018-01-17 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 17, 2018 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Boeing 737-347](https://openairdocs.org/model/boeing-737-347) (registry code 138447U) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 23182 - Type of aircraft: Fixed wing multi engine - Certificate issued: January 26, 2010 - Last registry action: January 26, 2010 - Mode S code: A328B5 - Owner when cancelled: [Mec Group LLC](https://openairdocs.org/faa-owner/MEC%20GROUP%20LLC) - Location: [Tucson, AZ](https://openairdocs.org/faa-place/AZ/Tucson) - Owner type: Corporation - Owner's area on the map: 32.3353° N, 111.0418° W: Placed by OpenAirDocs at the center of ZIP code 85741, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N302WA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=302WA - Page: https://openairdocs.org/deregistered/N302WA-2018-01-17 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 737-347: https://openairdocs.org/model/boeing-737-347.md ## Service difficulty reports (24) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL733050107](https://openairdocs.org/sdr/DL733050107), Feb 14, 2005: CONNECTOR. DAMAGED. EMERGENCY PATH LIGHTING INOP AT 22D/E/F. FOUND ON ROUTINE MAINTENANCE INSPECTION. REPAIRED DAMAGED SIDEWALL CONNECTOR AT 22D/E/F. - [SDR DL733040604](https://openairdocs.org/sdr/DL733040604), Jun 26, 2004: ODOR. DETECTED. FLIGHT ATTENDANT SMELLS BURNING ODOR IN AFT GALLEY. INSPECTED AFT GALLEY EQUIPMENT FOR DEFECTS, NONE NOTED. NO SMELL PRESENT. APPLIANCES AND LIGHTS ALL CHECK NO - [SDR DL733040060](https://openairdocs.org/sdr/DL733040060), Jan 17, 2004: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND WITH A CRACK JUST BELOW STRINGER 23R ALONG THE EDGE OF THE BONDED SKIN WAFFLE DOUBLER BETWEEN FS 727D & 727E. THE DAMAGE WAS REMOVED - [SDR DL733040007](https://openairdocs.org/sdr/DL733040007), Jan 4, 2004: TIRE. CUT. ON L/O FOUND NR 2 MLG TIRE CUT BEYOND LIMITS. REMOVED AND REPLACED NR 2 MLG TIRE PER MM. - [SDR DL733030852](https://openairdocs.org/sdr/DL733030852), Sep 17, 2003: WIRE HARNESS. INOPERATIVE. WHILE REPOSITIONING HARNESS AT SEAT ROW 27 PINS PULLED OUT OF HARNESS AND SHORTED POWER SUPPLY. REPLACED HARNESS AT SEAT ROW 27 AND POWER SUPPLY/BATTERY PER M/M - [SDR DL733020273](https://openairdocs.org/sdr/DL733020273), Mar 8, 2002: ATTACH FITTING. CORRODED. THE VERTICAL STABILIZER ATTACH LUGS AND THE FUSELAGE CLEVIS LUGS WERE FOUND TO BE CORRODED DURING AN INSPECTION. THE LUG BORES WERE OVERSIZED AND THE FACES SPOT - [SDR DL733011356](https://openairdocs.org/sdr/DL733011356), Aug 18, 2001: SAFETY SWITCH. OUT OF ADJ. UPON DEPARTURE ATL LDG WOULD NOT RETRACT. GEAR HANDLE WOULD ONLY RAISE TO THE OFF POSITION. ADJUSTED AND TESTED GROUND SPOILER INTERLOCK AND SAFETY SWITCHES. RE - [SDR DL733010437](https://openairdocs.org/sdr/DL733010437), Mar 15, 2001: SKIN. CRACKED. INSPECTIONS OF THE HORIZONTAL STABILIZER CUTOUT SURROUND STRUCTURE REVEALED A CRACK IN THE STRINGER 12L STRAP. ADDITIONAL TOOLING DAMAGE WAS FOUND ON THE STRING - [SDR DL733000922](https://openairdocs.org/sdr/DL733000922), May 7, 2000: BULKHEAD. CRACKED. THE FS 178 BULKHEAD WEB WAS FOUND WITH TYPICAL FASTENER CRACKING IN THE WEB AT WL 234 AT LBL AND RBL 9. THE CRACKS ARE TYPICAL OF BAC S/B 737-53A1173. THE CRACK - [SDR DL733000258](https://openairdocs.org/sdr/DL733000258), Feb 3, 2000: VALVE. FAILED. HYD SYS B PRESS DROPPED TO ZERO WITH ASSOCIATED LOW PRESS LIGHTS ILLUMINATED. REPLACED B SYSTEM PRESSURE RELIEF VALVE. - [SDR DL733991981](https://openairdocs.org/sdr/DL733991981), Sep 7, 1999: CONTROL PANEL. FAILED. ON DESCENT, AUTO PRESS FAIL MADE UNPRESSURIZED LANDING. REPLACED PRESS CONTROL PANEL. CKS NORMAL. - [SDR DL733990506](https://openairdocs.org/sdr/DL733990506), Mar 10, 1999: LINE. LEAKING. AFTER INITIAL GEAR RETRACTION, NOSE GEAR RE-EXTENDED WITH GEAR HANDLE IN THE UP POSITION. RECYCLED GEAR HANDLE HAD NO EFFECT. NOSE GEAR REMAINED DOWN AND LOCKED - [SDR DL733990247](https://openairdocs.org/sdr/DL733990247), Feb 4, 1999: SKIN. CRACKED. THE FUSELAGE SKIN AND UNDERLYING STEEL GUSSET WERE FOUND WITH A .20 INCH CRACK AT THE UPPER AFT CORNER OF THE L1 COCKPIT WINDOW CUTOUT. THE CRACK WAS ROUTED OUT - [SDR DL733981991](https://openairdocs.org/sdr/DL733981991), Sep 26, 1998: WIRE. DAMAGED. EMERGENCY TRACK LIGHT WIRE AT SEAT ROW 25DEF FOUND DAMAGED. PERFORMED APPROVED REPAIR PER BOEING STANDARD WIRING MANUAL. SYSTEM OPERATES NORMAL. - [SDR DL733981006](https://openairdocs.org/sdr/DL733981006), May 12, 1998: BULKHEAD WEB. CRACKED. FOUR CRACKS FOUND IN THE BLKHD WEB AT FS 178. THE CRACKS ARE LOCATED AT WL 200 AND WL 188, BETWEEN LBL 5.7 AND RBL 5.7. REPAIRED PER ERA 331672-14. - [SDR DL733981005](https://openairdocs.org/sdr/DL733981005), May 12, 1998: BULKHEAD WEB. CORRODED. AFT PRESSURE BLKHD AT FS 1016 WAS FOUND CORRODED AND CRACKED AT BL 0. REPAIRED PER ERA 331673-14. - [SDR DL733981004](https://openairdocs.org/sdr/DL733981004), May 12, 1998: SKIN. WORN. FUSELAGE SKIN AT THE BLADE SEAL FUSELAGE INTERFACE WAS FOUND TO HAVE AN EXISTING REPAIR (REF 5-72770-3). WEAR WAS FOUND FWD OF THE REPAIR. REPAIRED PER ERA 3316 - [SDR DL733972182](https://openairdocs.org/sdr/DL733972182), Oct 24, 1997: BOOT SEAL. FAILED. LOST ALL PRESSURIZATION AT 30000 FEET, NORMAL DUCT PRESS. NO BLEED OR PACK TRIP. FOUND RUPTURED BOOT SEAL ON APU P DOME PRESSURE DUCT. REPLACED SEAL. PRESSURIZE - [SDR DL733970233](https://openairdocs.org/sdr/DL733970233), Feb 7, 1997: POWER SUPPLY. INOPERATIVE. WHILE PERFORMING NR 5 AD SVC CK ON SHIP 202, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP FROM ROW 1 IN F/CLASS TO ROW 12 IN Y/CLASS INOP. FOUND POWER SUPPLY FOR E - [SDR DL733961628](https://openairdocs.org/sdr/DL733961628), Apr 6, 1996: SKIN. CRACKED. THE SKIN AT THE COOLING DUCT CUTOUT, FS 379 BL 0, WAS FOUND CRACKED AT THE AFT EDGE OF THE CUTOUT. THE CRACK IS APPROX .5 IN LENGTH AND IS TYPICAL OF CRACKS DES - [SDR DL733960710](https://openairdocs.org/sdr/DL733960710), Mar 30, 1996: BALLAST. SMOKING. SIDEWALL LIGHTS ROW 23 TO 25 MOMENTARILY WENT OUT AND SMOKED. PULLED AND COLLARED C/B FOR RT SIDE, FWD TO MCO. REPLACED BALLAST AND RELAMPED, OPERATION NORMAL. - [SDR DL733960416](https://openairdocs.org/sdr/DL733960416), Feb 13, 1996: DOOR. CRACKED. DURING OVERHAUL, THE AFT LOWER FRAME ON THE C1 DOOR WAS DISCOVERED TO HAVE A 1.5 INCH CRACK IN THE RADIUS. IN ACCORDANCE WITH BACO S/B 737-52-1100 REV 2, THE CR - [SDR DL733960062](https://openairdocs.org/sdr/DL733960062), Jan 10, 1996: CONTROL CABLE. LOOSE. GEAR DOWN 3 RED AND 3 GREEN LIGHTS. RECYCLED OK 3 GREEN, HAPPENED ON 2 APPROACHS. CORRECTED CABLE TENSION FOR LANDING GEAR ACTUATOR, GEAR SWING NORMAL. - [SDR DL733954382](https://openairdocs.org/sdr/DL733954382), Nov 11, 1995: DOOR FRAME. CRACK. THE AFT CARGO DOOR OPENING FORWARD FRAME WAS FOUND WITH A .5 INCH CRACK AT THE NR 5 STOP FITTING. THE FRAME IS MADE FROM A 0.071 7075-T6 CLAD MATERIAL. THIS ER/ ## 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 19990307012819I](https://openairdocs.org/incident/19990307012819I), Mar 7, 1999: Boeing 737347 (N302WA), Salt Lake City, UT, Minor damage. Slc to san jose, struck 6-8 birds on departing runway 34L, damage to radome, repaired in san jose. - [Incident 19940107003099I](https://openairdocs.org/incident/19940107003099I), Jan 7, 1994: Boeing 737347 (N302WA), Mazatlan, Mexico, Minor damage. Narrative: at FL 350, in clear weather, enroute from Mexico city to los angeles, the #2 engine was shut down due to a loss of power, and the aircraft diverted… ## Other aircraft with N302WA - [Registered now](https://openairdocs.org/aircraft/N302WA): Piper PA-46-701TP, S/N 46020102, built 2026 --- 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.