# N307WA: 1986 Boeing 737-347, registration cancelled 2018-04-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 19, 2018 - Status when cancelled: Registration expired, pending cancellation - 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: 23440 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 16, 1986 - Certificate issued: October 13, 2011 - Last registry action: May 14, 2014 - Mode S code: A33B48 - Owner when cancelled: [Aersale 23440 LLC](https://openairdocs.org/faa-owner/AERSALE%2023440%20LLC) - Location: [Coral Gables, FL](https://openairdocs.org/faa-place/FL/Coral%20Gables) - Owner type: Corporation - Owner's area on the map: 25.7533° N, 80.2704° W: Placed by OpenAirDocs at the center of ZIP code 33134, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N307WA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=307WA - Page: https://openairdocs.org/deregistered/N307WA-2018-04-19 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 (27) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL733030066](https://openairdocs.org/sdr/DL733030066), Jan 16, 2003: FITTING. CORRODED. CORROSION WAS FOUND ON THE AFT FACE OF THE RT REAR SPAR PRIMARY FITTING LUG. THE AFT SIDE OF THE LUG WAS SPOT FACED .005 INCH TO REMOVE THE CORROSION. A REPAIR - [SDR DL733030053](https://openairdocs.org/sdr/DL733030053), Jan 13, 2003: SKIN. DEBONDED. LEFT INBOARD FORE FLAP DISBONDED. REPAIRED PER ER/A 418180-14. - [SDR DL733030032](https://openairdocs.org/sdr/DL733030032), Jan 7, 2003: FITTING. CORRODED. THE RHS MLG SIDE STRUT SUPPORT FITTING HAD CORROSION IN THE BORE AND FORWARD AND AFT FACES OF THE FITTING AT FS 685, WL 188.5. THE BORE WAS OVERSIZED AND REPAIR - [SDR DL733030028](https://openairdocs.org/sdr/DL733030028), Jan 6, 2003: SKIN. DAMAGED. THREE AREAS OF PRE-EXISTING DAMAGES WERE REPORTED. THE FIRST TWO WERE PREVIOUS BLENDS AT FS 757 AT STR 15R AND JUSTBELOW STR 14R. THE FINAL DAMAGE WAS JUST AFT - [SDR DL733030027](https://openairdocs.org/sdr/DL733030027), Jan 6, 2003: FRAME. CORRODED. CORROSION WAS FOUND ON THE INNER FLANGE OF THE R-1 DOORWAY AFT FRAME JUST ABOVE THE FLOORLINE. THE CORROSION WAS REMOVED TO A MAX DEPTH OF .017". ADDITIONALLY, - [SDR DL733021460](https://openairdocs.org/sdr/DL733021460), Dec 23, 2002: FITTING. CORRODED. CORROSION WAS FOUND IN THE BORE OF THE #1 PYLON CROWN BEAM AFT FITTING. THE BORE WAS REAMED TO A DIAMETER OF 3.102" TO REMOVE THE CORROSION. THE DAMAGE WAS FOUN - [SDR DL733020337](https://openairdocs.org/sdr/DL733020337), Mar 16, 2002: ATTACH FITTING. WORN. A BEARING WAS FOUND MIGRATED FROM THE LUG BORE OF THE AFT FITTING ON THE NR 2 PYLON CROWN BEAM. AFTER REMOVAL OF THE BEARING LIGHT GOUGES WERE FOUND IN THE LUG - [SDR DL733011709](https://openairdocs.org/sdr/DL733011709), Oct 23, 2001: GCU. FAILED. APU OVERSPEED, NR 1 GEN WAS ALREADY ON MCO. RESET OVERSPEED ON APU ACCY UNIT. APU WORKS NORMAL. REPLACED NR 1 GCU NR 1 GEN WORKS NORMAL. - [SDR DL733011297](https://openairdocs.org/sdr/DL733011297), Aug 7, 2001: WARNING SYSTEM. MALFUNCTIONED. CABIN PRESSURE WARNING SOUNDED IN FLIGHT, WOULD NOT SILENCE. PRESSURE GOOD. REPLACED AURAL WARNING UNIT AND CABIN ALT SWITCH. - [SDR DL733010229](https://openairdocs.org/sdr/DL733010229), Feb 9, 2001: BULKHEAD. CRACKED. DURING INSPECTIONS PER S/B 737-53A1173 CRACKS WERE FOUND IN THE CENTER WEB OF THE FS 178 BULKHEAD AT WL 234 AND LBL 6. THE CRACKS WERE REPAIRED PER S/B AND SRM - [SDR DL733010203](https://openairdocs.org/sdr/DL733010203), Feb 6, 2001: BULKHEAD. CRACKED. WEB CRACKS WERE FOUND IN THE FS 178 BULKHEAD AT WL 207, RBL AND LBL 25. THE WEBS WERE REPLACED PER S/B 737-53A1173 AT CV. - [SDR DL733010297](https://openairdocs.org/sdr/DL733010297), Jan 20, 2001: FRAME. CRACKED. WHILE ACCOMPLISHING INSPECTIONS PER S/B 737-53A1173 A .25 INCH CRACK WAS FOUND IN THE RADIUS OF THE RT SIDE CHORD JUST ABOVE WL 207. THE PART WAS REPAIRED PER S - [SDR DL733991002](https://openairdocs.org/sdr/DL733991002), May 6, 1999: CONNECTOR. FAILED. FLOOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROWS 18 THROUGH 22 ARE INOP. FOUND OPEN SPLICE CONNECTOR UNDER SEAT 22D. REMOVED AND REPLACED CONNECTOR SPLICE, OPS NO - [SDR DL733990278](https://openairdocs.org/sdr/DL733990278), Feb 11, 1999: FITTING. CRACKED. LT LANDING GEAR BEAM ATTACH FITTING CRACK IN FASTENER ATTACH HOLES. REPAIRED PER ERA 332754-14. - [SDR DL733990244](https://openairdocs.org/sdr/DL733990244), Feb 5, 1999: SKIN. WORN. INSPECTION OF THE VERT STAB FOUND THE FUSE SKIN AT THE BLADE SEAL INTERFACE WORN FROM BS 860 TO BS 887. GREATEST DEPTH OF WEAR WAS 0.013. REPAIRED PER ERA 33274 - [SDR DL733990242](https://openairdocs.org/sdr/DL733990242), Feb 5, 1999: SKIN. DAMAGED. AN EXISTING REPAIR WAS REMOVED AT THE C1 DOOR CUTOUT, ADDITIONAL DAMAGE FOUND. CUTOUTS ARE IN SKIN (1.25 X 3.5) AND BEAR STRAP (1.25 BY 1.5). REPAIRED PER ERA 3 - [SDR DL733990241](https://openairdocs.org/sdr/DL733990241), Feb 5, 1999: BULKHEAD WEB. CRACKED. BS 178 BLKHD WEB FOUND CRACKED IN 8 PLACES, LARGEST CUTOUT IS 5 BY 1. REPAIRED PER ERA 332734-14. - [SDR DL733990240](https://openairdocs.org/sdr/DL733990240), Feb 5, 1999: STRINGER. CRACKED. DURING ACCOMPLISHMENT OF EO 5-70166-3 OF S18A AT BS 727, A CRACK WAS FOUND BEYOND EO/SB LIMITS. REPAIRED PER ERA 332733-14. - [SDR DL733990239](https://openairdocs.org/sdr/DL733990239), Feb 5, 1999: SKIN. DENTED. FUSELAGE SKIN FOUND DENTED AT BS 947 NEAR S19L. REPAIRED PER ERA 332751-14. - [SDR DL733981421](https://openairdocs.org/sdr/DL733981421), Jul 6, 1998: SKIN. CRACKED. A .375 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN AND UNDERLYING GUSSET AT THE UPPER OUTBD CORNER OF THE L1 COCKPIT WINDOW (UPPER END OF THE C-D POST). THE CRACK - [SDR DL733972063](https://openairdocs.org/sdr/DL733972063), Oct 16, 1997: OVEN. FAILED. F/A CALLED TO SAY SHE WAS GETTING STRONG ELEC SMOKE FROM FWD GALLEY OVENS. SMOKE INCREASED, PULLED GALLEY FWD C/BS AND TURNED OFF GALLEY PWR AND SMOKE DECREASED - [SDR DL733961198](https://openairdocs.org/sdr/DL733961198), May 17, 1996: FIRE DETECTOR. SHORTED. AT FL 330 NR 1 ENG OVHT LT CAME ON, REDUCED PWR SLIGHTLY LT WENT OUT. LT CAME ON SEVERAL MINS LATER THEN FAULT LT CAME ON, OVHT LT STAYED ON, SO SHUT DWN ENG FI - [SDR DL733950578](https://openairdocs.org/sdr/DL733950578), Feb 10, 1995: SKIN. DAMAGED. DURING HMV, FOUND A DEEP GOUGE IN THE C-1 B/B DOOR IN MID-SECTION OF EXTERNAL SKIN 9 INCHES FROM AFT END. CUT OUT DAMAGE AND REPAIRED PER SRM 52-00-01. - [SDR DL733950730](https://openairdocs.org/sdr/DL733950730), Jan 28, 1995: SKIN. WORN. TOP SIDE OF LOWER SKIN WAS FOUND WORN AT SECOND FROM I/B AFT TRACK CUTOUT, OF NR 4 MID FLAP. REPAIRED PER SRM 57-53-01 WITH REF TO 51-70-10. - [SDR DL733950523](https://openairdocs.org/sdr/DL733950523), Jan 28, 1995: STRINGER. CRACKED. DURING HMV, FOUND CARGO TIEDOWN STRINGER CRACKED IN AFT B/B RT CARGO TIEDOWN AT STA 787. REMOVED DAMAGED SECTION AND REPLACED PER SRM 53-00-53 PG 201-203, 206, - [SDR DL733950458](https://openairdocs.org/sdr/DL733950458), Jan 28, 1995: SKIN. DENTED. AT HMV, FOUND FUSELAGE SKIN DENTED AT FS 360 ABOVE STRINGER 19R. REPAIRED PER SRM 53-00 -01 PG 312. - [SDR DL733950457](https://openairdocs.org/sdr/DL733950457), Jan 28, 1995: SKIN. CRACKED. AT HMV, NR 5 SLAT LOWER T/E SKIN WAS FOUND CRACKED AT RIVET HEADS ON BOTH SIDES OF SLAT ACTUATOR. REPAIRED PER SRM 57-43-01 FIG 205. ## FAA accident and incident reports (4) 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 20120519008429I](https://openairdocs.org/incident/20120519008429I), May 19, 2012: Boeing 737-347 (N307WA), Charlotte, NC, No damage. Pilot stated the SIC was flying this leg. While on approach and on a coupled g/s the SIC let the aircraft drift below the g/s when the PIC took control of the… - [Incident 20040610010059I](https://openairdocs.org/incident/20040610010059I), Jun 10, 2004: Boeing 737347 (N307WA), Salt Lake City, UT, Minor damage. (-23) Delta flight 1640 lost the tread from the right inboard main landing gear tire recap. On rotation the crew felt a vibration. Shortly after that there was… - [Incident 19941015040679I](https://openairdocs.org/incident/19941015040679I), Oct 15, 1994: Boeing 737300 (N307WA), Salt Lake City, UT, Minor damage. During pushback from gate tail cone was struck by passing catering truck. - [Incident 19901129058469I](https://openairdocs.org/incident/19901129058469I), Nov 29, 1990: Boeing 737347 (N307WA), Minneapolis, MN, Minor damage. NR1 engine tail pipe fire after pushback. Shut engine down. Taxied to gate. No malfunction found. ## Other aircraft with N307WA - [Registered now](https://openairdocs.org/aircraft/N307WA): Xag P100 PRO, S/N 1863FPEG82193451N06N --- 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.