# N733TW: 1982 Boeing 737-2H4, registration cancelled 2014-06-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 3, 2014 - Exported to: South Korea - Status when cancelled: Valid registration - Airframe: [Boeing 737-2H4](https://openairdocs.org/model/boeing-737-2h4) (registry code 138448C) - Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049) - Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 22732 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: May 28, 1982 - Certificate issued: May 21, 2014 - Last registry action: May 21, 2014 - Mode S code: A9D7EE - Owner when cancelled: [Commercial Jet Partners LLC](https://openairdocs.org/faa-owner/COMMERCIAL%20JET%20PARTNERS%20LLC) - Location: [Garland, TX](https://openairdocs.org/faa-place/TX/Garland) - Owner type: Corporation - Owner's area on the map: 32.9289° N, 96.6198° W: Placed by OpenAirDocs at the center of ZIP code 75040, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N733TW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=733TW - Page: https://openairdocs.org/deregistered/N733TW-2014-06-03 From the FAA registry file of November 3, 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 (36) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR EE4Y20111005013](https://openairdocs.org/sdr/EE4Y20111005013), Oct 5, 2011: STRINGER SPLICE. CORRODED. AFT CARGO COMPT. BS 907 S25L WITH SPLICE CORRODED. THE PART CORRODED WAS REPLACED, WO Z10266, ITEM 1-79. - [SDR EE4Y20111005012](https://openairdocs.org/sdr/EE4Y20111005012), Oct 5, 2011: SHEAR TIE. CORRODED. AFT CARGO COMPT BS 727A FRAME WITH SHEAR TIE CORRODED BETWEEN S-21L AND S-22L. THE PART CORRODED WAS REPLACED, WO Z10226, ITEM 1-77. - [SDR EE4Y20111005011](https://openairdocs.org/sdr/EE4Y20111005011), Oct 5, 2011: STRINGER. CORRODED. AFT CARGO COMPT, BS 727A+2 WITH S22L CORRODED. THE PART CORRODED WAS REPLACED, WO Z10226, ITEM 1-78. - [SDR EE4Y20111005010](https://openairdocs.org/sdr/EE4Y20111005010), Oct 5, 2011: FITTING. CORRODED. RT WING REAR SPAR AT RSS 436 AND RSS 260 AND LT WING AT RSS 260 FLAP TRACK FITTING OTBD HOLES CORRODED. THE PARTS DAMAGED WERE REPLACEMENT, WO Z10226, ITEM'S 6- - [SDR EE4Y20111005009](https://openairdocs.org/sdr/EE4Y20111005009), Oct 5, 2011: FRAME. CRACKED. SECTION 43, FWD C/C BS 380 FRAME WITH UPPER FLANGE CRACKED AT S26R. A PERMANENT IS INSTALLED IAW SRM 51-40-3, FIG 1 GUIDELINES UNDER WO Z10226, ITEM 1-112. - [SDR EE4Y20111005008](https://openairdocs.org/sdr/EE4Y20111005008), Oct 5, 2011: SKIN. SCRATCHED. UPPER FUSELAGE BS 827 AND BS 838 BTWN S2-3L SKIN WITH SCRATCH. A PERMANENT REPAIR IS INSTALLED IAW REPAIR GUIDELINES UNDER WO Z10226, ITEM 2-134. - [SDR EE4Y20111005007](https://openairdocs.org/sdr/EE4Y20111005007), Oct 5, 2011: SKIN. SCRATCHED. UPPER FUSELAGE SKIN WITH SCRATCH AT BS 846 BETWEEN S3-2R. A PERMANENT REPAIR IS REQUIRED IAW MFG REPAIR GUIDLINES UNDER WO Z10226, ITEM 2-153. - [SDR EE4Y20110919003](https://openairdocs.org/sdr/EE4Y20110919003), Sep 19, 2011: SKIN. DENTED. LOWER FUSELAGE AT STA 819 BETWEEN STRINGER 22L AND STRINGER 23L SKIN WITH DENT. A PERMANENT REPAIR IS INSTALLED IAW REPAIR GUIDELINES UNDER WO Z10226 ITEM 1-43. - [SDR EE4Y20110919002](https://openairdocs.org/sdr/EE4Y20110919002), Sep 19, 2011: SKIN. DENTED. LOWER FUSELAGE BS 816, STRINGER 20 SKIN WITH DENT. A PERMANENT REPAIR IS INSTALLED FOLLOWING MFG REPAIR GUIDELINES UNDER WO Z10226, ITEM 1-44. - [SDR EE4Y20110919001](https://openairdocs.org/sdr/EE4Y20110919001), Sep 19, 2011: SKIN. DENTED. LOWER FUSELAGE STA 774, BETWEEN STRINGER 24L AND STRINGER 25L SKIN WITH DENT. A PERMANENT REPAIR IS INSTALLED FOLLOWING MFG REPAIR GUIDELINES UNDER WO Z10226, I - [SDR EE4Y1108003](https://openairdocs.org/sdr/EE4Y1108003), Aug 29, 2011: BEAM. CRACKED. UPPER FUSELAGE BS 578, RBL 65 STUB BEAM UPPER CHORD CRACKED. THE PART CRACKED WAS REPLACED. - [SDR EE4Y1108002](https://openairdocs.org/sdr/EE4Y1108002), Aug 29, 2011: STRINGER CLIP. CRACKED. PAX CABIN BS 1006 STRINGERS CLIP CRACKED. THE PARTS WERE REPLACED. - [SDR EE4Y1108001](https://openairdocs.org/sdr/EE4Y1108001), Aug 29, 2011: ANGLE. CRACKED. PAX CABIN BS 597 BETWEEN S-17L AND S-18L WITH ANGLE CRACKED. THE PART CRACKED WAS REPLACED. - [SDR MJYA749T1004001](https://openairdocs.org/sdr/MJYA749T1004001), Apr 3, 2010: SIGN. OUT OF POSITION. EMERGENCY EXIT SIGN IN COCKPIT FELL OUT. - [SDR EE4Y090229](https://openairdocs.org/sdr/EE4Y090229), Aug 25, 2009: SKIN. DENTED. FUSELAGE SKIN WITH DENT AT BS 1043 BETWEEN STR 16LT AND STR 17LT. - [SDR EE4Y090228](https://openairdocs.org/sdr/EE4Y090228), Aug 24, 2009: SKIN. CRACKED. AFT ENTRY DOOR UPPER HINGE SKIN CRACKED. - [SDR EE4Y090221](https://openairdocs.org/sdr/EE4Y090221), Aug 21, 2009: SKIN. CRACKED. LOWER FUSELAGE SKIN WITH CRACK AT BS 891, S-23RT. - [SDR EE4Y090220](https://openairdocs.org/sdr/EE4Y090220), Aug 21, 2009: SKIN. DELAMINATED. LEFT WING TRAILING EDGE SECTION, AILERON UPPER SURFACE SKIN DELAMINATED AT STA WBL 518.850 AND WBL 504. - [SDR EE4Y090217](https://openairdocs.org/sdr/EE4Y090217), Aug 20, 2009: STRINGER. CORRODED. LOWER FUSELAGE E&E COMPARTMENT AT BS 324, STR 28R WITH CORROSION. - [SDR EE4Y090216](https://openairdocs.org/sdr/EE4Y090216), Aug 18, 2009: BULKHEAD. CRACKED. LOWER FUSELAGE RT MAIN WHEEL WELL AFT BULKHEAD WEB WITH CRACK IN BS 727 RBL 6 WL 160. - [SDR EE4Y090215](https://openairdocs.org/sdr/EE4Y090215), Aug 18, 2009: STRINGER CLIP. CRACKED. LOWER FUSELAGE AFT CARGO COMPARTMENT BS 887 STRINGER 24 RT CLIP CRACKED. - [SDR EE4Y090213](https://openairdocs.org/sdr/EE4Y090213), Aug 18, 2009: FRAME. CORRODED. LOWER FUSELAGE FWD CARGO COMPARTMENT BS 440 BETWEEN STR 24 AND 25 RIGHT SIDE, FRAME CORRODED. - [SDR EE4Y090214](https://openairdocs.org/sdr/EE4Y090214), Aug 18, 2009: ANGLE. CORRODED. LOWER FUSELAGE AFT CARGO COMPARTMENT DOOR LOWER CUTOUT FROM BS 795 TO BS 847 ANGLE CORRODED. - [SDR 0612064](https://openairdocs.org/sdr/0612064), Dec 23, 2006: LAMP. INOPERATIVE. FORWARD ENTRY EMERGENCY EXIT LIGHT INOPERATIVE. - [SDR MJYA0606060](https://openairdocs.org/sdr/MJYA0606060), Jun 27, 2006: BATTERY PACK. DISCHARGED. AFT DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. - [SDR MJYA0602058](https://openairdocs.org/sdr/MJYA0602058), Feb 21, 2006: BATTERY PACK. DISCHARGED. CENTER AISLE EMERGENCY EXIT LIGHT AT OVERWING EXIT INOP. CHANGED BATTERY PACK. - [SDR 0601002](https://openairdocs.org/sdr/0601002), Jan 17, 2006: BATTERY PACK. DISCHARGED. FORWARD EMERGENCY AISLE LIGHT INOP. - [SDR 0601001](https://openairdocs.org/sdr/0601001), Jan 16, 2006: PUMP. MALFUNCTIONED. AFTER TAKEOFF HYDRAULIC MASTER CAUTION LIGHT ILLUMINATED, LOST A-SYSTEM HYDRAULIC QUANTITY. - [SDR 0509006](https://openairdocs.org/sdr/0509006), Sep 19, 2005: SKIN. DELAMINATED. RT WING INBOARD MID FLAP TRAILING EDGE P/N: 65-71902-42, S/N BN5, DELAMINATED AT WBL 132. - [SDR 0509004](https://openairdocs.org/sdr/0509004), Sep 19, 2005: RIB. CRACKED. RT WING, SLAT NR 4 RIB CRACKED AT SLAT STA 0.28. - [SDR 0509003](https://openairdocs.org/sdr/0509003), Sep 19, 2005: BULKHEAD. CRACKED. BS 1016 AFT PRESSURE BULKHEAD WEB TO Y-CHORD ATTACHMENT CRACKED. - [SDR 0509007](https://openairdocs.org/sdr/0509007), Sep 19, 2005: PLATE. WORN. ENGINE NR 2 PYLON FWD SECTION WITH PLATE WORN. - [SDR 0509005](https://openairdocs.org/sdr/0509005), Sep 19, 2005: PANEL. DELAMINATED. RT WING FIXED PANEL P/N: 65-50818-316, DELAMINATED AT WS 465. - [SDR 05092003](https://openairdocs.org/sdr/05092003), Sep 19, 2005: BULKHEAD. CRACKED. BS 1016 AFT PRESSURE BULKHEAD WEB TO "Y" CHORD ATTACHMENT CRACKED. - [SDR 0509002](https://openairdocs.org/sdr/0509002), Sep 19, 2005: RIB. CRACKED. RT WING AT WBL STA 364, OUTBOARD MID FLAP RIB CRACKED. - [SDR 0509001](https://openairdocs.org/sdr/0509001), Sep 19, 2005: STRINGER CLIP. CRACKED. FORWARD SERVICE DOORWAY AREA, STA 332 STRINGER 8R AREA, T-CLIP IS CRACKED. ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB CHI08IA065](https://openairdocs.org/ntsb/CHI08IA065), Jan 8, 2008: Boeing 737-2H4 (N733TW), Lincoln, NE, incident, no damage. Probable cause: The improper installation of the swivel valve fittings by the operator's mechanic leading to the total loss of both hydraulic systems. Contributing to the incident were the swivel valves leaking and… ## 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 20080108000219I](https://openairdocs.org/incident/20080108000219I), Jan 8, 2008: Boeing 7372H4 (N733TW), Lincoln, NE, No damage. (-23) N733TW, B-737-2H4, operated by ameristar charters as flight AJI9262, departed the ramp area while taxiing to the terminal. Following an uneventful… ## Other aircraft with N733TW - [Cancelled 1974-07-26](https://openairdocs.org/deregistered/N733TW-1974-07-26): Boeing 707-131, S/N 17660. Exported to Israel. Owner: [Samach Seymour R](https://openairdocs.org/faa-owner/SAMACH%20SEYMOUR%20R), Herzlia Pituach --- 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.