# N305SW: 1985 Boeing 737-3H4, registration cancelled 2011-09-01 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 1, 2011 - Status when cancelled: Valid registration - Airframe: [Boeing 737-3H4](https://openairdocs.org/model/boeing-737-3h4) (registry code 138447K) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Serial number: 22945 - Year built: 1985 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 28, 1985 - Certificate issued: January 25, 2011 - Last registry action: January 25, 2011 - Mode S code: A3338A - Owner when cancelled: [Oh Capital Assets Inc](https://openairdocs.org/faa-owner/OH%20CAPITAL%20ASSETS%20INC) - Location: [Monroe, NC](https://openairdocs.org/faa-place/NC/Monroe) - Owner type: Corporation - Owner's area on the map: 35.0660° N, 80.5091° W: Placed by OpenAirDocs at the center of ZIP code 28110, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N305SW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=305SW - Page: https://openairdocs.org/deregistered/N305SW-2011-09-01 From the FAA registry file of October 27, 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 737-3H4: https://openairdocs.org/model/boeing-737-3h4.md ## Service difficulty reports (324, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA096711](https://openairdocs.org/sdr/SWAA096711), Oct 25, 2009: FLAP. DELAMINATED. DURING SCHEDULED SPV CHECK, FOUND RT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM. - [SDR SWAA096616](https://openairdocs.org/sdr/SWAA096616), Oct 15, 2009: FLAP. DELAMINATED. DURING SCHEDULED SPV CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM. - [SDR SWAA096489](https://openairdocs.org/sdr/SWAA096489), Oct 12, 2009: STRINGER CLIP. CRACKED. DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED CLIP PER SRM. - [SDR SWAA096324](https://openairdocs.org/sdr/SWAA096324), Oct 3, 2009: BATTERY PACK. DISCHARGED. DURING SCHEDULED SPV CHECK, FOUND OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 6 TO ROW 8. REMOVED AND REPLACED BATTERY PACK PER MM. - [SDR SWAA096220](https://openairdocs.org/sdr/SWAA096220), Sep 29, 2009: LIGHT. INOPERATIVE. DURING SCHEDULED SPV CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. - [SDR SWAA096219](https://openairdocs.org/sdr/SWAA096219), Sep 29, 2009: LIGHT. INOPERATIVE. DURING SCHEDULED SPV CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. - [SDR SWAA095424](https://openairdocs.org/sdr/SWAA095424), Aug 21, 2009: SKIN. DELAMINATED. DURING SCHEDULED OTS CHECK, FOUND LT WING NR 2 L/E SLAT TOP SURFACE DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM. - [SDR SWAA094644](https://openairdocs.org/sdr/SWAA094644), Jul 21, 2009: SLIDE. OUT OF POSITION. DURING SCHEDULED CV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT. - [SDR SWAA094643](https://openairdocs.org/sdr/SWAA094643), Jul 21, 2009: SLIDE. OUT OF POSITION. DURING SCHEDULED CV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT. - [SDR SWAA094232](https://openairdocs.org/sdr/SWAA094232), Jun 30, 2009: SHEAR TIE. CORRODED. DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 927, STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM. - [SDR SWAA094231](https://openairdocs.org/sdr/SWAA094231), Jun 30, 2009: SHEAR TIE. CORRODED. DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 907, STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM. - [SDR SWAA092476](https://openairdocs.org/sdr/SWAA092476), Apr 16, 2009: SKIN. CRACKED. DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 548, STR 10R. REPAIRED SKIN PER SRM. - [SDR SWAA092475](https://openairdocs.org/sdr/SWAA092475), Apr 16, 2009: SKIN. CRACKED. DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 3 SLAT LOWER SKIN CRACKED. REPAIRED SLAT PER SRM. - [SDR SWAA092474](https://openairdocs.org/sdr/SWAA092474), Apr 16, 2009: SKIN. DELAMINATED. DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B FORE FLAP UPPER SKIN DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM. - [SDR SWAA090930](https://openairdocs.org/sdr/SWAA090930), Feb 8, 2009: LIGHT. CRACKED. DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY ESCAPE SLIDE LIGHT CRACKED. REMOVED AND REPLACED LIGHT PER MM. - [SDR SWAA090929](https://openairdocs.org/sdr/SWAA090929), Feb 8, 2009: SKIN. CRACKED. DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 345, STR 15R. REPAIRED SKIN PER SWA EA. - [SDR SWAA085457](https://openairdocs.org/sdr/SWAA085457), Oct 6, 2008: LIGHT. INOPERATIVE. DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. - [SDR SWAA085456](https://openairdocs.org/sdr/SWAA085456), Oct 6, 2008: SKIN. CRACKED. DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 905, STR 3L TO STR 4L. REMOVED AND REPLACED SKIN PER SWA EA. - [SDR SWAA085455](https://openairdocs.org/sdr/SWAA085455), Oct 6, 2008: SKIN. CRACKED. DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 905, STR 6L TO STR 7L. REMOVED AND REPLACED SKIN PER SRM. - [SDR SWAA084889](https://openairdocs.org/sdr/SWAA084889), Sep 7, 2008: SLIDE. LOW PRESSURE. L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. - [SDR SWAA081661](https://openairdocs.org/sdr/SWAA081661), Mar 26, 2008: KEELBEAM. CORRODED. DURING SCHEDULED 22Y CHECK, FOUND KEEL BEAM CHORD CORRODED BETWEEN BS 510D TO BS 540, RBL 6. REPAIRED CHORD PER SRM. - [SDR SWAA081603](https://openairdocs.org/sdr/SWAA081603), Mar 25, 2008: FITTING. CRACKED. DURING SCHEDULED 22Y CHECK, FOUND RIGHT WING NR 5 SPOILER INBOARD ACTUATOR FITTING WORN. REMOVED AND REPLACED FITTING PER MM. - [SDR SWAA081529](https://openairdocs.org/sdr/SWAA081529), Mar 19, 2008: SHEAR TIE. CORRODED. DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, RBL 11 TO RBL 13. REMOVED AND REPLACED SHEAR TIE PER SRM. - [SDR SWAA081498](https://openairdocs.org/sdr/SWAA081498), Mar 18, 2008: SLAT. DELAMINATED. DURING SCHEDULED 22Y CHECK, FOUND LT WING L/E NR 3 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM. - [SDR SWAA081473](https://openairdocs.org/sdr/SWAA081473), Mar 18, 2008: GLOWSTRIP. WORN. DURING SCHEDULED 22Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 7 DEF. REMOVED AND REPLACED STRIP PER MM. - [SDR SWAA081455](https://openairdocs.org/sdr/SWAA081455), Mar 17, 2008: SKIN. CRACKED. DURING SCHEDULED 22Y CHECK, FOUND FWD CARGO DOOR FWD UPPER SKIN CRACKED. REPAIRED SKIN PER SWA EA. - [SDR SWAA081429](https://openairdocs.org/sdr/SWAA081429), Mar 14, 2008: STRINGER CLIP. CRACKED. DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM. - [SDR SWAA081428](https://openairdocs.org/sdr/SWAA081428), Mar 14, 2008: SKIN. DELAMINATED. DURING SCHEDULED 22Y CHECK, FOUND RT WING 36 L/E SLAT UPPER SURFACE DELAMINATED. REPAIRED SLAT PER SRM. - [SDR SWAA081355](https://openairdocs.org/sdr/SWAA081355), Mar 11, 2008: CREASE BEAM. CORRODED. DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 328 AND BS 344, STR 17R. REMOVED AND REPLACED CREASE BEAM PER SRM. - [SDR SWAA081356](https://openairdocs.org/sdr/SWAA081356), Mar 11, 2008: FITTING. CORRODED. DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM. - [SDR SWAA081357](https://openairdocs.org/sdr/SWAA081357), Mar 11, 2008: FITTING. CORRODED. DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM. - [SDR SWAA081334](https://openairdocs.org/sdr/SWAA081334), Mar 10, 2008: FLOORBEAM. CORRODED. DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 5 TO RBL 46. REPAIRED FLOORBEAM PER SRM. - [SDR SWAA081343](https://openairdocs.org/sdr/SWAA081343), Mar 10, 2008: SKIN. CRACKED. DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 270, STR 16R. REPAIRED SKIN PER SRM. - [SDR SWAA081333](https://openairdocs.org/sdr/SWAA081333), Mar 10, 2008: CREASE BEAM. CORRODED. DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 952 AND BS 990, STR 17R. REMOVED AND REPLACED CREASE BEAM PER SRM. - [SDR SWAA081275](https://openairdocs.org/sdr/SWAA081275), Mar 9, 2008: FITTING. CORRODED. DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM. - [SDR SWAA081270](https://openairdocs.org/sdr/SWAA081270), Mar 9, 2008: STRINGER CLIP. CRACKED. DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM. - [SDR SWAA081271](https://openairdocs.org/sdr/SWAA081271), Mar 9, 2008: STRINGER CLIP. CRACKED. DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM. - [SDR SWAA081272](https://openairdocs.org/sdr/SWAA081272), Mar 9, 2008: STRINGER CLIP. CRACKED. DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM. - [SDR SWAA081274](https://openairdocs.org/sdr/SWAA081274), Mar 9, 2008: FITTING. CORRODED. DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM. - [SDR SWAA081273](https://openairdocs.org/sdr/SWAA081273), Mar 9, 2008: STRINGER CLIP. CRACKED. DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 204, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM. - [SDR SWAA081243](https://openairdocs.org/sdr/SWAA081243), Mar 5, 2008: MECHANISM. OUT OF ADJUST. DURING SCHEDULED 22Y CHECK, FOUND FLIGHT DECK R2 WINDOW EXTERNAL RELEASE HANDLE WILL NOT UNLOCK WINDOW. ADJUSTED RELEASE HANDLE MECHANISM PER MM. - [SDR SWAA080689](https://openairdocs.org/sdr/SWAA080689), Feb 6, 2008: SKIN. DELAMINATED. DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED FLAP PER MM. - [SDR SWAA080688](https://openairdocs.org/sdr/SWAA080688), Feb 6, 2008: SKIN. DELAMINATED. DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD FOREFLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FLAP PER MM. - [SDR SWAA080690](https://openairdocs.org/sdr/SWAA080690), Feb 6, 2008: SKIN. CRACKED. DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 346, STR 2L. REPAIRED SKIN PER SRM. - [SDR SWAA080230](https://openairdocs.org/sdr/SWAA080230), Jan 10, 2008: BATTERY PACK. DISCHARGED. DURING SCHEDULED A2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. - [SDR SWAA075731](https://openairdocs.org/sdr/SWAA075731), Nov 17, 2007: SKIN. CRACKED. DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259.5, STR 19L. REPAIRED SKIN PER SRM. - [SDR SWAA075315](https://openairdocs.org/sdr/SWAA075315), Oct 25, 2007: CASTING. CRACKED. DURING SCHEDULED C1 CHECK, FOUND RT WING INBOARD GROUND SPOILER OUTBOARD CASTING CRACKED. REMOVED AND REPLACED SPOILER PER MM. - [SDR SWAA075272](https://openairdocs.org/sdr/SWAA075272), Oct 24, 2007: LAMP. INOPERATIVE. DURING SCHEDULED C1 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. - [SDR SWAA074969](https://openairdocs.org/sdr/SWAA074969), Oct 7, 2007: BATTERY PACK. INOPERATIVE. DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. - [SDR SWAA071742](https://openairdocs.org/sdr/SWAA071742), Apr 6, 2007: SHEAR TIE. CORRODED. DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 380, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. All 324: https://openairdocs.org/deregistered/N305SW-2011-09-01/reports.md --- 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.