# N319SW: 1987 Boeing 737-3H4, registration cancelled 2008-08-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 28, 2008 - 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: 23340 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 4, 1987 - Certificate issued: April 3, 2008 - Last registry action: April 3, 2008 - Mode S code: A369E5 - Owner when cancelled: [Aar Parts Trading Inc](https://openairdocs.org/faa-owner/AAR%20PARTS%20TRADING%20INC) - Location: [Wood Dale, IL](https://openairdocs.org/faa-place/IL/Wood%20Dale) - Owner type: Corporation - Owner's area on the map: 41.9744° N, 87.9865° W: Placed by OpenAirDocs at the center of ZIP code 60191, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N319SW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=319SW - Page: https://openairdocs.org/deregistered/N319SW-2008-08-28 From the FAA registry file of November 7, 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 (200, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA074017](https://openairdocs.org/sdr/SWAA074017), Aug 12, 2007: TORQUE TUBE. WORN. FLAPS SETTING FROM 25 TO 30, FLAPS LOCKED OUT. REMOVED AND REPLACED RT FLAP TORQUE TUBE PER MM. - [SDR SWAA073866](https://openairdocs.org/sdr/SWAA073866), Aug 1, 2007: SKIN. CRACKED. DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, RBL 3. REPAIRED SKIN PER EA. - [SDR SWAA073530](https://openairdocs.org/sdr/SWAA073530), Jul 18, 2007: SKIN. CRACKED. DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 801, STR 18L. REPAIRED SKIN PER SRM. - [SDR SWAA071546](https://openairdocs.org/sdr/SWAA071546), Mar 23, 2007: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT BS 475, STR 16L. REPAIRED SKIN PER SRM. - [SDR SWAA071547](https://openairdocs.org/sdr/SWAA071547), Mar 23, 2007: SKIN. CRACKED. DURING MV2 CK, FOUND FUSELAGE SKIN CRACKED AT BS 425, STR 16L. REPAIRED SKIN PER SRM. - [SDR SWAA071548](https://openairdocs.org/sdr/SWAA071548), Mar 23, 2007: SKIN. CRACKED. DURING MV2 CK, FOUND FUSELAGE SKIN CRACKED AT BS 415, STR 16L. REPAIRED SKIN PER SRM. - [SDR SWAA071549](https://openairdocs.org/sdr/SWAA071549), Mar 23, 2007: SKIN. CRACKED. DURING MV2 CK, FOUND FUSELAGE SKIN CRACKED AT BS 485, STR 16R. REPAIRED SKIN PER SRM. - [SDR SWAA071201](https://openairdocs.org/sdr/SWAA071201), Mar 3, 2007: LENS. MISSING. BULL NOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 17 DEF. INSTALLED LIGHT LENS PER MM. - [SDR SWAA071209](https://openairdocs.org/sdr/SWAA071209), Mar 1, 2007: TIRE. RUPTURED. DIVERSION / DECLARED EMERGENCY. NR 3 MAIN TIRE RUPTURED ON TAKEOFF. REMOVED AND REPLACED NR 3 WHEEL AND TIRE ASSY, RIGHT WING INBOARD GROUND SPOILER, FORE FLAP - [SDR SWAA070329](https://openairdocs.org/sdr/SWAA070329), Jan 23, 2007: LIGHT. INOPERATIVE. DURING SCHEDULED HC1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 19 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. - [SDR SWAA063969](https://openairdocs.org/sdr/SWAA063969), Oct 13, 2006: SHEAR TIE. CRACKED. DURING SCHEDULED MV4 CHECK, FOUND SHEAR TIE CRACKED AT BS 380, STR 14R. REPAIRED SHEAR TIE PER SWA EA. - [SDR SWAA063968](https://openairdocs.org/sdr/SWAA063968), Oct 13, 2006: SKIN. CRACKED. DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 376, STR 15R. REPAIRED SKIN PER SRM. - [SDR SWAA063967](https://openairdocs.org/sdr/SWAA063967), Oct 13, 2006: SKIN. CRACKED. DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 480, STR 19L. REPAIRED SKIN PER SRM. - [SDR SWAA063966](https://openairdocs.org/sdr/SWAA063966), Oct 13, 2006: SKIN. CRACKED. DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 430, STR 16L. REPAIRED SKIN PER SRM. - [SDR SWAA063254](https://openairdocs.org/sdr/SWAA063254), Aug 31, 2006: BATTERY PACK. DISCHARGED. DURING SCHEDULED MV3 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. - [SDR SWAA062507](https://openairdocs.org/sdr/SWAA062507), Jul 17, 2006: FITTING. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND LT MLG HANGER SHAFT AFT FITTING CORRODED. REMOVED AND REPLACED MLG SHAFT AFT FITTING PER MM. - [SDR SWAA062506](https://openairdocs.org/sdr/SWAA062506), Jul 17, 2006: FITTING. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND RT MLG HANGER SHAFT AFT FITTING CORRODED. REMOVED AND REPLACED MLG SHAFT AFT FITTING PER MM. - [SDR SWAA062505](https://openairdocs.org/sdr/SWAA062505), Jul 17, 2006: FITTING. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND RT MLG STABILIZER BEAM AFT FITTING CORRODED. REMOVED AND REPLACED AFT FITTING PER MM. - [SDR SWAA062504](https://openairdocs.org/sdr/SWAA062504), Jul 17, 2006: BEAR STRAP. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT FWD CARGO DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN SECTION PER ER. - [SDR SWAA062503](https://openairdocs.org/sdr/SWAA062503), Jul 17, 2006: SKIN. DELAMINATED. DURING SCHEDULED 20Y CHECK, FOUND LT ELEVATOR SKIN DELAMINATED AT UPPER SURFACE STA 84. REPAIRED ELEVATOR SKIN PER SRM. - [SDR SWAA062491](https://openairdocs.org/sdr/SWAA062491), Jul 17, 2006: FITTING. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. - [SDR SWAA062490](https://openairdocs.org/sdr/SWAA062490), Jul 17, 2006: FITTING. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. - [SDR SWAA062489](https://openairdocs.org/sdr/SWAA062489), Jul 17, 2006: SKIN. DELAMINATED. DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED INBOARD T/E. REPAIRED FORE FLAP SKIN PER SRM. - [SDR SWAA062488](https://openairdocs.org/sdr/SWAA062488), Jul 17, 2006: RIB. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND RT HORIZONTAL STAB RIB CRACKED AT STA 151.75. REMOVED AND REPLACED HORIZONTAL STAB RIB PER SRM. - [SDR SWAA062487](https://openairdocs.org/sdr/SWAA062487), Jul 17, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND STUB FRAME CRACKED AT FWD SIDE UPPER CORNER BS 296, STR 7R. REMOVED AND REPLACED STUB FRAME SECTION PER SRM. - [SDR SWAA062470](https://openairdocs.org/sdr/SWAA062470), Jul 16, 2006: STRINGER CLIP. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM. - [SDR SWAA062469](https://openairdocs.org/sdr/SWAA062469), Jul 16, 2006: FLOORBEAM. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 1016, LBL 4. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM. - [SDR SWAA062468](https://openairdocs.org/sdr/SWAA062468), Jul 16, 2006: BULKHEAD. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016, STR 4L. REPAIRED DOME CAP PER ER. - [SDR SWAA062467](https://openairdocs.org/sdr/SWAA062467), Jul 16, 2006: BULKHEAD. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016, STR 7R. REPAIRED DOME CAP PER SRM. - [SDR SWAA062466](https://openairdocs.org/sdr/SWAA062466), Jul 16, 2006: BULKHEAD. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016, FIRST FASTENER AT 7 O'CLOCK POSITION. REPAIRED DOME CAP PER SRM. - [SDR SWAA062465](https://openairdocs.org/sdr/SWAA062465), Jul 16, 2006: ANGLE. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND FWD ENTRY DOOR ZEE ANGLE CORRODED AT BS 312 TO BS 348, LBL 62. REMOVED AND REPLACED ZEE ANGLE PER SRM. - [SDR SWAA062464](https://openairdocs.org/sdr/SWAA062464), Jul 16, 2006: FLOORBEAM. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CORRODED AT BS 270, LBL 11 TO RBL 11. REMOVED AND REPLACED FLOORBEAM CHORD PER SRM. - [SDR SWAA062463](https://openairdocs.org/sdr/SWAA062463), Jul 16, 2006: BEAR STRAP. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 440, STR 19R. REPAIRED SKIN PER SRM. - [SDR SWAA062419](https://openairdocs.org/sdr/SWAA062419), Jul 12, 2006: SPAR. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND LT AND RT HORZ STAB SPARS LUG FACES CORRODED. REPAIRED HORZ STAB PER SRM. - [SDR SWAA062418](https://openairdocs.org/sdr/SWAA062418), Jul 12, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 827, LBL4, WL 154. REPAIRED FRAME SECTION PER SRM. - [SDR SWAA062417](https://openairdocs.org/sdr/SWAA062417), Jul 12, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME SECTION PER SRM. - [SDR SWAA062416](https://openairdocs.org/sdr/SWAA062416), Jul 12, 2006: FLOOR SUPPORT. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED AT BS 727B, RBL 45. REPAIRED FLOORBEAM PER ER. - [SDR SWAA062415](https://openairdocs.org/sdr/SWAA062415), Jul 12, 2006: FLOOR SUPPORT. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CRACKED AT BS 663 TO BS 671, LBL 25. REPAIRED FLOORBEAM PER ER. - [SDR SWAA062392](https://openairdocs.org/sdr/SWAA062392), Jul 10, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D. STR 25L. REMOVED AND REPLACED FRAME SECTION PER SRM. - [SDR SWAA062391](https://openairdocs.org/sdr/SWAA062391), Jul 10, 2006: STRINGER CLIP. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM. - [SDR SWAA062390](https://openairdocs.org/sdr/SWAA062390), Jul 10, 2006: STRINGER SPLICE. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 358, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. - [SDR SWAA062389](https://openairdocs.org/sdr/SWAA062389), Jul 10, 2006: BEAM. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STAB LT TRAILING EDGE BEAM CRACKED. REMOVED AND REPLACED VERTICAL STAB BEAM PER SRM. - [SDR SWAA062388](https://openairdocs.org/sdr/SWAA062388), Jul 10, 2006: LIGHT. INOPERATIVE. DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. - [SDR SWAA062387](https://openairdocs.org/sdr/SWAA062387), Jul 10, 2006: SKIN. CORRODED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 986.5, BL 0. REPAIRED SKIN PER ER. - [SDR SWAA062377](https://openairdocs.org/sdr/SWAA062377), Jul 9, 2006: SHEAR TIE. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 22L. REPAIRED SHEAR TIE PER SRM. - [SDR SWAA062376](https://openairdocs.org/sdr/SWAA062376), Jul 9, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME SECTION PER SRM. - [SDR SWAA062375](https://openairdocs.org/sdr/SWAA062375), Jul 9, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME SECTION PER SRM. - [SDR SWAA062374](https://openairdocs.org/sdr/SWAA062374), Jul 9, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME SECTION PER SRM. - [SDR SWAA062373](https://openairdocs.org/sdr/SWAA062373), Jul 9, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME SECTION PER SRM. - [SDR SWAA062372](https://openairdocs.org/sdr/SWAA062372), Jul 9, 2006: FRAME. CRACKED. DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME SECTION PER SRM. All 200: https://openairdocs.org/deregistered/N319SW-2008-08-28/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.