# N63SW: 1980 Boeing 737-2H4, registration cancelled 2004-04-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 27, 2004
- Exported to: Cambodia
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-2H4](https://openairdocs.org/model/boeing-737-2h4) (registry code 138448C)
- Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048)
- Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 22061
- Year built: 1980
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: March 26, 1980
- Certificate issued: December 30, 2003
- Last registry action: December 31, 2003
- Mode S code: A83D08
- Owner when cancelled: [Jet Midwest Inc](https://openairdocs.org/faa-owner/JET%20MIDWEST%20INC)
- Location: [Kansas City, KS](https://openairdocs.org/faa-place/KS/Kansas%20City)
- Owner type: Corporation
- Owner's area on the map: 39.1483° N, 94.6051° W: Placed by OpenAirDocs at the center of ZIP code 66115, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N63SW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=63SW
- Page: https://openairdocs.org/deregistered/N63SW-2004-04-27

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 737-2H4: https://openairdocs.org/model/boeing-737-2h4.md

## Service difficulty reports (61, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR SWAA000437](https://openairdocs.org/sdr/SWAA000437), Mar 7, 2000: ENGINE. LEAKING. AFTER TAKEOFF, WITH RT A/C PACK SELECTED, STRONG OIL FUMES IN CABIN. REMOVED AND REPLACED NR 2 ENG AND BOTH AIR CYCLE MACHINES.
- [SDR SWAA000409](https://openairdocs.org/sdr/SWAA000409), Mar 6, 2000: RELIEF VALVE. FAILED. AIR TURNBACK, HYD FUMES IN COCKPIT AND CABIN. REMOVED AND REPLACED A-SYSTEM RESERVOIR AIR PRESS REGULATOR AIR SUPPLY FILTER. REMOVED AND REPLACED RESERVOIR RELI
- [SDR SWAA000413](https://openairdocs.org/sdr/SWAA000413), Mar 4, 2000: BATTERY PACK. INOPERATIVE. DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.
- [SDR SWAA990870](https://openairdocs.org/sdr/SWAA990870), May 13, 1999: BATTERY PACK. DISCHARGED. DURING SCHEDULED C4 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
- [SDR SWAA990869](https://openairdocs.org/sdr/SWAA990869), May 13, 1999: SLIDE. OUT OF POSITION. DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESSURE GAUGE OUT OF VIEW. REPOSITIONED GAUGE PER MM.
- [SDR SWAA981874](https://openairdocs.org/sdr/SWAA981874), Aug 27, 1998: ENGINE. BIRD STRIKE. AIR TURNBACK DUE TO BIRD STRIKE, NR 2 ENGINE DURING TAKEOFF ROLL. AIRCRAFT MADE AN UNEVENTFUL LANDING. AIRCRAFT INSPECTED, NR 2 ENGINE AND PS3 FILTER. NO DAMAGE
- [SDR SWAA980082](https://openairdocs.org/sdr/SWAA980082), Jan 21, 1998: STRINGER. DAMAGED. DURING SCHEDULED D-CHECK, FOUND STRINGER DAMAGED WITH A HOLE AT BS 500B+13, S16L. REPLACED DAMAGED SECTION PER BOEING SRM.
- [SDR SWAA980081](https://openairdocs.org/sdr/SWAA980081), Jan 21, 1998: CHANNEL. CRACKED. DURING SCHEDULED D-CHECK, FOUND STRINGER CHANNEL CRACKED AT BS 500B, S16R. REPAIRED PER BOEING SRM.
- [SDR SWAA980080](https://openairdocs.org/sdr/SWAA980080), Jan 21, 1998: SKIN. CORRODED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN LAP CORROSION AT BS 908 TO 1016 AT S4L. REPAIRED PER SWA ACO 6717-53.
- [SDR SWAA980079](https://openairdocs.org/sdr/SWAA980079), Jan 21, 1998: SKIN. CRACKED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 1011, S4R AND 988, S4R, AT BS 491, S14R, AT BS 727+11, S4L, AT BS 727B+1, S4L, AT BS 767+4 AT S4L, AT
- [SDR SWAA980078](https://openairdocs.org/sdr/SWAA980078), Jan 21, 1998: SKIN. HOLE. DURING SCHEDULED D-CHECK, FOUND AN OBLONG HOLE IN LOWER ROW OF LAP JOINT, BS 500+2, AT S14L. REPAIRED PER BOEING SRM.
- [SDR SWAA980077](https://openairdocs.org/sdr/SWAA980077), Jan 21, 1998: BULKHEAD. CRACKED. DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 5, LBL 8 - LBL 16, AND RBL 1- 2. REPAIRED PER BOEING SRM.
- [SDR SWAA980076](https://openairdocs.org/sdr/SWAA980076), Jan 21, 1998: SPLICE. CORRODED. DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT S27L AND R, BS 907. REPLACED DAMAGED SECTION PER BOEING SRM.
- [SDR SWAA980075](https://openairdocs.org/sdr/SWAA980075), Jan 21, 1998: FRAME. CRACKED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, S20R. REPLACED DAMAGED SECTION PER BOEING SRM.
- [SDR SWAA980074](https://openairdocs.org/sdr/SWAA980074), Jan 21, 1998: STRINGER. CORRODED. DURING SCHEDULED D-CHECK, FOUND STRINGER CORRODED AT BS 350, S25R. REPAIRED PER BOEING SRM.
- [SDR SWAA980073](https://openairdocs.org/sdr/SWAA980073), Jan 21, 1998: SKIN. GOUGED. DURING SCHEDULED D-CHECK, FOUND SKIN GOUGED AT FWD SERVICE DOOR HINGE CUTOUT AT BS 289.5, AND AT BS 358, BETWEEN S4 AND 5L. REPAIRED PER BOEING SRM.
- [SDR SWAA980072](https://openairdocs.org/sdr/SWAA980072), Jan 21, 1998: WEB. CRACKED. DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 710. REPLACED DAMAGED SECTION PER BOEING SRM.
- [SDR SWAA980071](https://openairdocs.org/sdr/SWAA980071), Jan 21, 1998: SPLICE. CRACKED. DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT S 4L, BS 908. REPLACED DAMAGED SECTION PER BOEING SRM.
- [SDR SWAA980070](https://openairdocs.org/sdr/SWAA980070), Jan 21, 1998: STRINGER. CRACKED. DURING SCHEDULED D-CHECK, FOUND STRINGER S16R CRACKED AT BS 596. REPLACED DAMAGED SECTION PER BOEING SRM.
- [SDR SWAA980069](https://openairdocs.org/sdr/SWAA980069), Jan 21, 1998: SKIN. DENTED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 287 2 ABOVE S18R, AND AT BS 307, AT RBL 1.75. REPAIRED PER BOEING SRM.
- [SDR SWAA980068](https://openairdocs.org/sdr/SWAA980068), Jan 21, 1998: SKIN. DAMAGED. DURING SCHEDULED D-CHECK, FOUND COCKPIT WINDOW POST SKIN LIGHTNING STRIKE DAMAGED AT BS 198, WL 253. RESKINNED POST PER BOEING SRM.
- [SDR SWAA980067](https://openairdocs.org/sdr/SWAA980067), Jan 21, 1998: STRINGER. DAMAGED. DURING SCHEDULED D-CHECK, FOUND STRINGER 16R DAMAGED AT BS 522. REPLACED DAMAGED SECTION PER BOEING SRM.
- [SDR SWAA980066](https://openairdocs.org/sdr/SWAA980066), Jan 21, 1998: STRAP. CRACKED. DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STRAP CRACKED AT BS 1140, ABOVE S12R. REPLACED DAMAGED SECTION PER BOEING SRM.
- [SDR SWAA980065](https://openairdocs.org/sdr/SWAA980065), Jan 21, 1998: STRAP. CRACKED. DURING SCHEDULED D-CHECK, FOUND VERTICAL STRAP CRACKED AT BS 1140, ABOVE S12L. REPLACED DAMAGED SECTION PER BOEING SRM.
- [SDR SWAA980064](https://openairdocs.org/sdr/SWAA980064), Jan 21, 1998: SUPPORT. CORRODED. DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 299, LBL 11. REPLACED DAMAGED SECTION PER BOEING SRM.
- [SDR SWAA980063](https://openairdocs.org/sdr/SWAA980063), Jan 21, 1998: FRAME. DENTED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 807, LBL 27. REPAIRED PER BOEING SRM.
- [SDR SWAA980051](https://openairdocs.org/sdr/SWAA980051), Jan 20, 1998: RIB. CRACKED. DURING SCHEDULED D CHECK, LT HORZ STAB L/E PANEL CRACKED RIB AT STA 105.26. REPLACED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER BOEING SRM.
- [SDR SWAA980050](https://openairdocs.org/sdr/SWAA980050), Jan 20, 1998: CLIP. CRACKED. DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, S24L. REPLACED PER BOEING SRM.
- [SDR SWAA980049](https://openairdocs.org/sdr/SWAA980049), Jan 20, 1998: FRAME. DENTED. DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME DENTED AT BS 787. REPLACED DAMAGED SECTION PER BOEING SRM.
- [SDR SWAA980048](https://openairdocs.org/sdr/SWAA980048), Jan 20, 1998: SHEAR TIE. CORRODED. DURING SCHEDULED D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 947, BETWEEN S24 AND 25. REPLACE SHEAR TIE PER BOEING SRM.
- [SDR SWAA980047](https://openairdocs.org/sdr/SWAA980047), Jan 20, 1998: STRINGER. DAMAGED. DURING SCHEDULED D CHECK, FOUND STRINGER 24R WITH A HOLE AT BS 941. REPLACED DAMAGED SECTIONS PER BOEING SRM.
- [SDR SWAA980046](https://openairdocs.org/sdr/SWAA980046), Jan 20, 1998: STRINGER. DAMAGED. DURING SCHEDULED D CHECK, FOUND STRINGER 24R DAMAGED AT BS 867-878. REPLACED DAMAGED SECTIONS PER BOEING SRM.
- [SDR SWAA980045](https://openairdocs.org/sdr/SWAA980045), Jan 20, 1998: STRINGER. CORRODED. DURING SCHEDULED D CHECK, FOUND STRINGER 27L CORRODED AT BS 1004, AND AT S27R AT BS 1009. REPLACED DAMAGED SECTIONS PER BOEING SRM.
- [SDR SWAA980029](https://openairdocs.org/sdr/SWAA980029), Jan 8, 1998: FRAME. CRACKED. DURING SCHEDULED D-CHECK, FOUND I/B FRAME CHORD CRACKED AT FASTENER HOLE LT, S16, BS 639. REPLACED PER BOEING SRM.
- [SDR SWAA980028](https://openairdocs.org/sdr/SWAA980028), Jan 8, 1998: SKIN. DENTED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 993 TO 1006, ABOVE S14L. REPAIRED PER BOEING SRM.
- [SDR SWAA980027](https://openairdocs.org/sdr/SWAA980027), Jan 8, 1998: FRAME. CRACKED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 663, AT S5L, AT BS 304, LBL 65, AND AT BS 291, S12R. REPAIRED PER BOEING SRM.
- [SDR SWAA980026](https://openairdocs.org/sdr/SWAA980026), Jan 8, 1998: CHANNEL. CRACKED. DURING SCHEDULED D-CHECK, FOUND U-CHANNELS CRACKED AT BS 361 S3L, AT BS 360, LBL 254, 69 AND 63. REPLACED PER BOEING SRM.
- [SDR SWAA980025](https://openairdocs.org/sdr/SWAA980025), Jan 8, 1998: SHEAR TIE. CRACKED. DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACK INDICATION AT BS 520, AT S16L-17L, AND AT BS 967, AT S8L. REPAIRED PER BOEING SRM.
- [SDR SWAA980024](https://openairdocs.org/sdr/SWAA980024), Jan 8, 1998: SKIN. CRACKED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACK INDICATION AT BS 400, AT S5L TO 6L. REPAIRED PER BOEING SRM.
- [SDR SWAA980016](https://openairdocs.org/sdr/SWAA980016), Jan 7, 1998: SKIN. DENTED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT 446, 4 BELOW S17R, AT BS 205, 10 BELOW S19R, AT BS 270, LBL 24 TO 34, AND AT B S227, 6 BELOW S24R. REPAI
- [SDR SWAA980015](https://openairdocs.org/sdr/SWAA980015), Jan 7, 1998: SKIN. DENTED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AND CREASED AT 392 TO 400, AND AT BS 387, AT S23R. REPAIRED PER BOEING SRM.
- [SDR SWAA980014](https://openairdocs.org/sdr/SWAA980014), Jan 7, 1998: SKIN. DENTED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT 308, 3 BELOW S19R, AT BS 893, BETWEEN S22 AND 23L, AT BS 197, 10 BELOW S19R, AT BS 500B+5, AND AT BS 890
- [SDR SWAA980013](https://openairdocs.org/sdr/SWAA980013), Jan 7, 1998: CHORD. CRACKED. DURING SCHEDULED D-CHECK, FOUND BS 178 SIDE CHORD CRACKED AT BS 178 LT SIDE, WL 195 TO 194. REPAIRED PER BOEING SRM.
- [SDR SWAA980012](https://openairdocs.org/sdr/SWAA980012), Jan 7, 1998: CLIP. CRACKED. DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 360, S9L, AT BS 520, S19L AT BS 294, LBL 52, AT BS 400, AT S28L, AT BS 277, WL 223, AND AT BS 500A,
- [SDR SWAA980011](https://openairdocs.org/sdr/SWAA980011), Jan 7, 1998: FRAME. GOUGED. DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME AT BS 500A GOUGED. REPAIRED PER BOEING SRM.
- [SDR SWAA980010](https://openairdocs.org/sdr/SWAA980010), Jan 7, 1998: FRAME. DENTED. DURING SCHEDULED D-CHECK, FOUND MULTIPLE DENTS IN FUSELAGE FRAME AT BS 500. REPAIRED PER BOEING SRM.
- [SDR SWAA980009](https://openairdocs.org/sdr/SWAA980009), Jan 7, 1998: STRINGER. CRACKED. DURING SCHEDULED D-CHECK, FOUND STRINGER 22R CRACKED AT BS 494. REPLACED DAMAGED SECTION PER BOEING SRM.
- [SDR SWAA980008](https://openairdocs.org/sdr/SWAA980008), Jan 7, 1998: BULKHEAD. CRACKED. DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED BELOW FASTENER AT WL 234, LBL 15.5 AND AT RBL 9.5. REPAIRED PER BOEING SRM.
- [SDR SWAA980005](https://openairdocs.org/sdr/SWAA980005), Jan 3, 1998: LIGHT. INOPERATIVE. DURING SCHEDULED D-CHECK, FOUND FWD LT EMERGENCY FLASHLIGHT INOP. REPLACED PER BOEING M/M.
- [SDR SWAA970984](https://openairdocs.org/sdr/SWAA970984), Nov 7, 1997: FRAME. CRACKED. DURING SCHEDULED C4 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328 AT RBL 54, WL 183. REPAIRED PER BOEING SRM.

All 61: https://openairdocs.org/deregistered/N63SW-2004-04-27/reports.md

## 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 19810523034049I](https://openairdocs.org/incident/19810523034049I), May 23, 1981: Boeing 737* (N63SW), Houston, TX. During descent left engine secured due to fire alarm. Landed ok. Inspection found no fire signs. Replaced system.

## Other aircraft with N63SW

- [Registered now](https://openairdocs.org/aircraft/N63SW): Cubcrafters CC11-160, S/N CC11-00279

---
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.
