# N3301: Boeing 737-347, registration cancelled 2009-08-04 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 4, 2009 - Status when cancelled: Valid registration - 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: 23181 - Type of aircraft: Fixed wing multi engine - Certificate issued: November 10, 2008 - Last registry action: November 10, 2008 - Mode S code: A3984A - 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/N3301 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=3301 - Page: https://openairdocs.org/deregistered/N3301-2009-08-04 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 (42) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL733040805](https://openairdocs.org/sdr/DL733040805), Aug 23, 2004: SKIN. CRACKED. TWO CRACKS WERE FOUND RUNNING ALONG THE BONDED SKIN DOUBLER LINE OF STRINGER 24L. ONE CRACK WAS JUST FWD AND THE OTHER JUST AFT OF A PREVIOUSLY INSTALLED SKIN R - [SDR DL733040802](https://openairdocs.org/sdr/DL733040802), Aug 23, 2004: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND CRACKED AT FOUR LOCATIONS. THE CRACKS WERE ALL LOCATED ALONG THE EDGE OF THE UNDERLYING BONDED DOUBLER. A 1 INCH VERTICAL CRACK WAS - [SDR DL733040796](https://openairdocs.org/sdr/DL733040796), Aug 23, 2004: WEDGE. DEBONDED. NR 4 FORE FLAP TE WEDGE WAS FOUND WITH A 42 INCH SECTION OF SKIN DISBONDED. REPAIRED PER ER/A 092865-14. - [SDR DL733040776](https://openairdocs.org/sdr/DL733040776), Aug 18, 2004: SKIN. CRACKED. CRACK REPAIR, THE FUSELAGE SKIN WAS FOUND WITH A CRACK AT FS 757 JUST BELOW STRINGER 19R RUNNING ALONG THE UNDERLYING BONDED DOUBLER EDGE. THE CRACK WAS REMOVED - [SDR DL733030502](https://openairdocs.org/sdr/DL733030502), May 31, 2003: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND WITH A 3 INCH CRACK JUST ABOVE STRINGER 24R AND A 2 INCH CRACK JUST BELOW STRINGER 24R. THE CRACKS RAN ALONG THE BONDED WAFFLE DOUBL - [SDR DL733030417](https://openairdocs.org/sdr/DL733030417), May 3, 2003: HEAT EXCHANGER. CRACKED. RIGHT WING BODY OVERHEAT LIGHT CAME ON DURING CLIMB RAN PROCEDURE BUT LEFT PACK WOULD NOT HOLD CABIN ALTITUDE CABIN UNDER CONTROL AT 18000 MAX CABIN ALT 9500. F - [SDR DL733030363](https://openairdocs.org/sdr/DL733030363), Apr 17, 2003: WEDGE. DELAMINATED. RT INBOARD AFT FLAP TE WEDGE DISBONDED. REPAIRED PER ER/A 422820-14 - [SDR DL733030303](https://openairdocs.org/sdr/DL733030303), Mar 31, 2003: STRUCTURE. DEBONDED. INBOARD FORE FLAP DELAMINATED. REPAIRED PER ER/A 422922-14. - [SDR DL733030082](https://openairdocs.org/sdr/DL733030082), Jan 21, 2003: SKIN. DENTED. FUSELAGE / SKIN / FS 277-290.5 / STRG. 20R-22R : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN WAS DENTED AND GOUGED BY GROUND EQUIPMENT JUST AFT OF THE LAVATOR - [SDR DL733021132](https://openairdocs.org/sdr/DL733021132), Sep 23, 2002: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT AT SEAT 10 DEF INOP. RELAMPED SAME OPS CK GOOD - [SDR DL733021056](https://openairdocs.org/sdr/DL733021056), Sep 11, 2002: SKIN. DELAMINATED. WING SPOILERS WAS FOUND WITH EXCESSIVE DELAMINATION. REPAIR PER ER/A 417560-14 AND NORDAM EWO E0038848. - [SDR DL733020870](https://openairdocs.org/sdr/DL733020870), Jul 26, 2002: SKIN. CRACKED. DURING INSPECTION PER OPN 57512 SKIN CRACK WAS FOUND AT STATION 727E+15 AND STRINGER 23L. CORRECTIVE ACTION: REPAIRED PER ER/A 383585-14. - [SDR DL733020869](https://openairdocs.org/sdr/DL733020869), Jul 26, 2002: SKIN. CRACKED. DURING INSPECTION PER OPN 57512 CRACK WAS FOUND IN THE SKIN AT STATION 727D+15 AND STR-22R. CORRECTIVE ACTION: REPAIRED PER ER/A 383586-14. - [SDR DL733020812](https://openairdocs.org/sdr/DL733020812), Jul 15, 2002: HYDRAULIC LINE. RUPTURED. LOSS OF B-SYSTEM PRESSURE IN FLIGHT. REPLACED B-PUMP HYD SUPPLY LINE IN RT WHEEL WELL . ALSO REPLACED NR 2 ENGINE HYD PUMP AND CASE DRAIN FILTER SYSTEM, OPS AND - [SDR DL733020424](https://openairdocs.org/sdr/DL733020424), Apr 10, 2002: WIRE. DISCONNECTED. EMERGENCY EXIT LIGHT ON SEAT 12D INOP. FOUND WIRES PULLED FROM CONNECTOR. REWIRED CONNECTOR, LIGHT OPNS NORMAL. - [SDR DL733020423](https://openairdocs.org/sdr/DL733020423), Apr 10, 2002: SKIN. DELAMINATED. OUTBOARD SPOILER UPPER SKIN WAS FOUND DELAMINATED. REPAIR PER ER/A 411175-14 AND NORDAM EWO E0037508 REV I/R. - [SDR DL733020307](https://openairdocs.org/sdr/DL733020307), Mar 14, 2002: ACTUATOR. LEAKING. NR 1 ENGINE LOW PRESSURE HYDRAULIC (A) SYSTEM LIGHT ILLUMINATED WITH ASSOCIATED A SYSTEM QUANTITY DECREASED TO ZERO. FOLLOWED POM PROCEDURE NO OTHER INDICATION. - [SDR DL733020227](https://openairdocs.org/sdr/DL733020227), Feb 24, 2002: POWER SUPPLY. INOPERATIVE. L2 DOOR AND AFT AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. - [SDR DL733020135](https://openairdocs.org/sdr/DL733020135), Feb 1, 2002: DOOR FRAME. CRACKED. FWD CARGO DOOR ARRIVED IN THE SHOP DUE TO CRACKING FOUND IN THE LOWER FWD AND AFT CORNER FRAMES AS WELL AS THE FWD AND AFT SECTIONS OF THE LWD STOP BEAM. REPAIR - [SDR DL733020122](https://openairdocs.org/sdr/DL733020122), Feb 1, 2002: KEELBEAM. CRACKED. CORROSION WAS FOUND ON THE LOWER KEEL CHORD AT FS 727 AND STR 27R. ADDITIONALLY, SEVERAL WEAR LOCATIONS WERE FOUND BETWEEN FS 727 AND FS 715 AND A CRACK WAS FOU - [SDR DL733020121](https://openairdocs.org/sdr/DL733020121), Feb 1, 2002: WEB. CRACKED. THE KEEL BEAM LOWER SKIN PANEL WAS FOUND CRACKED IN SEVERAL PLACES_BETWEEN FS 661 AND FS 721. THE PANEL WAS REPLACED PER S/B 737-53-1104. THE DAMAGE WAS FOUND A - [SDR DL733020062](https://openairdocs.org/sdr/DL733020062), Jan 18, 2002: SUPPORT FITTING. DAMAGED. FWD ENGINE MOUNT SUPPORT FITTING WAS FOUND WITH OVERSIZED MOUNT HOLES. REPAIR PER ER/A 410877-14AD. - [SDR DL733020061](https://openairdocs.org/sdr/DL733020061), Jan 18, 2002: SUPPORT FITTING. DAMAGED. FWD ENGINE MOUNT SUPPORT FITTING WAS FOUND WITH OVERSIZED MOUNT HOLES. REPAIR PER ER/A 410878-14AD. - [SDR DL733020059](https://openairdocs.org/sdr/DL733020059), Jan 18, 2002: BEAM. CORRODED. CORROSION WAS FOUND ON THE CROWN BEAM LUG BORES OF THE NR 1 AND NR 2 PYLONS. THE BORES WERE OVERSIZED AND REPAIR BUSHINGS INSTALLED. THE DAMAGE WAS FOUND DURING - [SDR DL733011409](https://openairdocs.org/sdr/DL733011409), Aug 26, 2001: TIRE. SEPARATED. NR 1 MAIN TIRE TREAD SEPARATED FROM TIRE ON TAKE OFF. DAMAGING LEFT I/B FLAPS AND LEFT GEAR DOOR. CA REPLACED TIRE, GEAR DOOR AND REPAIRED FLAP DAMAGE. - [SDR DL733010931](https://openairdocs.org/sdr/DL733010931), Jun 8, 2001: PIN. BURNED. ON DESCENT DFW THE APU DET INOP LIGHT ON FIRE PANEL ILLUM. FOLLOWED POM PROCEDURE. APU AND APU BLEEDS WERE OFF AT THE TIME. ON FINAL THE APU FIRE WARN ILLUM. FO - [SDR DL733010705](https://openairdocs.org/sdr/DL733010705), May 2, 2001: ATTACH FITTING. CORRODED. THE RT MLG SIDE STRUT SUPPORT FITTING AT FS 685 WAS FOUND WITH CORROSION IN THE BORE AND FACES OF THE WL 188.5 LUG. THE CORROSION WAS REMOVED BY OVERSIZING THE - [SDR DL733010454](https://openairdocs.org/sdr/DL733010454), Mar 15, 2001: BULKHEAD. CRACKED. BS 178 BULKHEAD FLOOR SUPPORT STRUCTURE WEB CRACKED AT WL 207 AND LBL 25. ER/A 380305-14AD ORIGINAL ISSUE - [SDR DL733010427](https://openairdocs.org/sdr/DL733010427), Mar 14, 2001: FRAME. CRACKED. THE LT AND RT SIDE CHORDS OF THE FS 178 BULKHEAD WERE FOUND CRACKED NEAR WL 207. THE CRACKS ARE LESS THAN 3 INCHES IN LENGTH.THE CRACKS WERE STOP DRILLED AND RE - [SDR DL733002089](https://openairdocs.org/sdr/DL733002089), Oct 20, 2000: SKIN. CRACKED. A SMALL CRACK WAS FOUND IN THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT (FS 348, S-16L). THE CRACK WAS IN THE OUTER SKIN ONLY AND WAS REMOVED WITH A 1 X .5 INCH C - [SDR DL733981955](https://openairdocs.org/sdr/DL733981955), Sep 19, 1998: WIRE. LOOSE. TRACK LIGHT AT SEAT 1-C INOP. FOUND WIRE UNHOOKED UNDER SEAT, OPS CK OK NOW. - [SDR DL733981732](https://openairdocs.org/sdr/DL733981732), Aug 21, 1998: LINE. PUNCTURED. EN ROUTE EXPERIENCED TOTAL HYD SYS-B FAILURE CONTACTED ATL. MTC AND DISPATCH ADVISED LANDING IN LAS. T/S B-HYD SYS FOUND PIN HOLE IN FLEX HOSE FROM PUMP TO PRES - [SDR DL733980853](https://openairdocs.org/sdr/DL733980853), Apr 20, 1998: SKIN. DENTED. FUSELAGE SKIN BELOW C1 DOOR CUTOUT WAS FOUND DENTED AND CREASED IN TWO PLACES. THE DAMAGE IS BETWEEN S26R AND S27R. REPAIRED PER ERA 331629-14. - [SDR DL733980852](https://openairdocs.org/sdr/DL733980852), Apr 20, 1998: BULKHEAD WEB. CORROEDED. AFT PRESSURE BLKHD AT FS 1016 WAS FOUND CORRODED AND CRACKED AT APPROX BL 0.0. THE CORROSION INCLUDED SURFACES 0 THE DOME WEB (GORE) AND BOTH THE LT AND RT 'C' - [SDR DL733980851](https://openairdocs.org/sdr/DL733980851), Apr 20, 1998: KEEL BEAM. CORRODED. S28L KEEL BEAM WAS CORRODED AT FS 500D THRU FS 520. THE CORROSION REQUIRED CUTTING AND REMOVING A SECTION FROM FS 500D+10 FWD TO FS 500C+10. REPAIRED PER ERA 33 - [SDR DL733980822](https://openairdocs.org/sdr/DL733980822), Apr 16, 1998: SKIN. WORN. THE FUSE SKIN WAS REPORTED TO BE WORN FROM BS 860 TO BS 885 TO A MAX DEPTH OF 0.013. REPAIRED PER ERA 331634-14. - [SDR DL733970463](https://openairdocs.org/sdr/DL733970463), Mar 11, 1997: UPLOCK TARGET. LOOSE. ON TAKEOFF, NOSE GEAR INDICATOR REMAINED RED ON RETRACTION. FOUND TARGET TABS OUT OF POSITION - REPAIRED. - [SDR DL733962590](https://openairdocs.org/sdr/DL733962590), Nov 25, 1996: LIGHT. INOPERATIVE. 2ND EMERGENCY TRACK LIGHT INOP IN Y/C. RELAMPED OPS CKS NML. - [SDR DL733960430](https://openairdocs.org/sdr/DL733960430), Feb 24, 1996: TARGET. RUSTED. NOSE GEAR DOWN AND LOCKED LIGHT WOULD NOT IND GREEN ON EXT OF GEAR. FOUND LOCK SENSOR TARGET BENT UP ABOVE SENSOR. REPLACED RUSTED SPRING RETAINER BOLTS, PERFOR - [SDR DL733951675](https://openairdocs.org/sdr/DL733951675), Apr 24, 1995: NOSE COWL. DENTED. DURING SHOP INSPECTION, NR 1 ENGINE NOSE COWL WAS FOUND WITH THE LEADING EDGE LIP DENTED AT THE 9 O'CLOCK POSITION. REPAIRED PER SRM 54-10-01. - [SDR DL733951249](https://openairdocs.org/sdr/DL733951249), Mar 22, 1995: NOSE COWL. DENTED. FOUND DURING LETTER CHECK, DENT INSIDE NOSE COWL, CUT OUT DAMAGED SKIN AND CORE INJECTED POTTING COMPOUND AND CURED PER SRM 54-10-01. - [SDR DL733950621](https://openairdocs.org/sdr/DL733950621), Feb 4, 1995: DETECTOR. FAULTY. DURING APPROACH HAD NR 2 ENGINE OVERHEAT/FIRE INDICATION NR 2 WAS SHUT DOWN, BOTTLE DISCHARGED. NO EVIDENCE OF FIRE WAS FOUND. SUBSEQUENT TROUBLESOOTING REPLACE ## 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 20010826025599I](https://openairdocs.org/incident/20010826025599I), Aug 26, 2001: Boeing 737347 (N3301), Kansas City, MO, Minor damage. (-23) On August 26, 2001, a delta airlines B737-300, flight number 1802, departed slc for mci, when, on takeoff roll, the crew reported hearing a noise and… --- 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.