# N344TM: 1983 Boeing 737-200, registration cancelled 2005-12-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 28, 2005 - Exported to: Nigeria - Status when cancelled: Valid registration - Airframe: [Boeing 737-200](https://openairdocs.org/model/boeing-737-200) (registry code 1384451) - Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 23044 - Year built: 1983 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: February 5, 1999 - Certificate issued: March 22, 2004 - Last registry action: March 22, 2004 - Mode S code: A3CDDF - Owners when cancelled: [Tem Enterprises DBA](https://openairdocs.org/faa-owner/TEM%20ENTERPRISES%20DBA), [Casino Express Airlines](https://openairdocs.org/faa-owner/CASINO%20EXPRESS%20AIRLINES) - Location: [Elko, NV](https://openairdocs.org/faa-place/NV/Elko) - Owner type: Corporation - Owner's area on the map: 41.1650° N, 115.7572° W: Placed by OpenAirDocs at the center of ZIP code 89801, within about 20 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N344TM - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=344TM - Page: https://openairdocs.org/deregistered/N344TM-2005-12-28 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 737-200: https://openairdocs.org/model/boeing-737-200.md ## Service difficulty reports (81, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR BJNA051201](https://openairdocs.org/sdr/BJNA051201), Dec 2, 2005: CONNECTOR. DIRTY. EMERGENCY EXIT LIGHT ILLUMINATED 2 TIMES ON DESCENT. CLEANED THE CONNECTORS ON THE COCKPIT REMOVABLE EMERGENCY EXIT LIGHT, SYSTEM CHECKS NORMAL. (K) - [SDR BJNA05021](https://openairdocs.org/sdr/BJNA05021), Feb 11, 2005: ENGINE. FAILED. NR 2 ENGINE FAILED ON THE BEGINNING OF TAKEOFF ROLL, 1.6 EPR HARD COMPRESSOR STALL AND ROLL DOWN. INSPECTION REVEALED EXTENSIVE DAMAGE TO THE T-1 THROUGH T-4 TU - [SDR BJNA050103](https://openairdocs.org/sdr/BJNA050103), Jan 26, 2005: LINE. LEAKING. NR 1 ENGINE LOST ENGINE OIL QUANTITY AND ILLUMINATED THE LOW OIL PRESSURE LIGHT. ENGINE WAS SHUTDOWN AND WIND MILLED APPROX 20 MIN. INSPECTION FOUND THE ENGINE - [SDR BJNA050102](https://openairdocs.org/sdr/BJNA050102), Jan 21, 2005: BATTERY PACK. DISCHARGED. DURING A MAINTENANCE WALK AROUND CHECK, THE LT SERVICE DOOR L2 EMERGENCY EXIT LIGHT WOULD NOR ILLUMINATE. MAINTENANCE DISCOVERED THAT THE BATTERIES WERE DISCHAR - [SDR BJNA050101](https://openairdocs.org/sdr/BJNA050101), Jan 8, 2005: BULB. BURNED OUT. DURING A MAINTENANCE WALK AROUND CHECK, THE LT SERVICE DOOR L2 EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB OF THE - [SDR BJNA041201](https://openairdocs.org/sdr/BJNA041201), Dec 15, 2004: BATTERY PACK. DISCHARGED. DURING A PREFLIGHT WALK AROUND INSPECTION THE NR 1 OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE OVERWING EMERGENCY E - [SDR BJNA041003](https://openairdocs.org/sdr/BJNA041003), Oct 10, 2004: BULB. BURNED OUT. LT AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT BULB AND CLEANED SOCKET IAW AMM 33-51-101. - [SDR BJNA040904](https://openairdocs.org/sdr/BJNA040904), Sep 19, 2004: BATTERY PACK. INOPERATIVE. FOUND CABIN EMERGENCY FLASHLIGHT CHARGE INDICATOR DOES NOT BLINK. REMOVED AND REPLACED THE FLASHLIGHT BATTERY PACK IAW AMM 25-69-00. (M) - [SDR BJNA040809](https://openairdocs.org/sdr/BJNA040809), Aug 25, 2004: FLOOR SUPPORT. CORRODED. DURING C-CHECK INSPECTION, FOUND CABIN FLOOR SUPPORT AT BS 312-328 RBL 12 WITH LEVEL 2 CORROSION. FABRICATED NEW FLOOR SUPPORT ANGLE FROM 7075-T6 BAC 1505-29222 - [SDR BJNA040807](https://openairdocs.org/sdr/BJNA040807), Aug 25, 2004: DOOR FRAME. CRACKED. DURING C-CHECK INSPECTION, FOUND C-1 DOOR LOWER FORWARD CORNER FRAME CRACKED. INSTALLED NEW LOWER FORWARD CORNER AT C1 DOOR IAW SRM 51-20-1 AND SERVICE BULLETIN - [SDR BJNA040808](https://openairdocs.org/sdr/BJNA040808), Aug 25, 2004: DOOR FRAME. CRACKED. DURING C-CHECK INSPECTION, FOUND C-1 DOOR LOWER AFT CORNER FRAME CRACKED. INSTALLED NEW LOWER AFT CORNER AT C1 DOOR IAW SRM 51-20-1 AND SB 737-52A1100 REV 4. (M - [SDR BJNA040804](https://openairdocs.org/sdr/BJNA040804), Aug 13, 2004: FLOOR SUPPORT. CORRODED. DURING C-CHECK INSPECTION, FOUND CABIN FLOOR SUPPORT AT BS 312-328 RBL 45 CORRODED. FABRICATED NEW FLOOR SUPPORT ANGLE FROM 7075-T6 BAC 1505-19222 IAW THE BOEIN - [SDR BJNA040805](https://openairdocs.org/sdr/BJNA040805), Aug 13, 2004: FLOOR SUPPORT. CORRODED. DURING C-CHECK INSPECTION, FOUND CABIN FLOOR SUPPORT AT BS 312-328 LBL 45 CORRODED. FABRICATED NEW FLOOR SUPPORT ANGLE FROM 7075-T6 BAC 1505-29222 IAW THE SRM 5 - [SDR BJNA040803](https://openairdocs.org/sdr/BJNA040803), Aug 12, 2004: INTERCOSTAL. CORRODED. DURING C-CHECK INSPECTION, FOUND FLOORBEAM INTERCOSTAL CORRODED AT BS 306 LBL 12. REMOVED AND REPLACED FLOORBEAM INTERCOSTAL AT BS 306 LBL 12 IAW THE STRUCTURAL - [SDR BJNA040901](https://openairdocs.org/sdr/BJNA040901), Aug 6, 2004: CROSSBEAM. CRACKED. DURING C-CHECK INSPECTION FOUND C-1 DOOR LOWER CROSS BEAM HAS WEB CRACK NEAR AFT CORNER. FABRICATED FILLER, .875 INCH BY 5 INCH AND 5 INCH BY 4 INCH MATERIAL US - [SDR BJNA040902](https://openairdocs.org/sdr/BJNA040902), Aug 6, 2004: SKIN. CRACKED. DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BOTTOM OF L1 DOOR CUT OUT BS 336. INSTALLED DOUBLER AND STRAP AT L1 DOOR LOWER CUTOUT IAW SB 737-53-10 - [SDR BJNA040802](https://openairdocs.org/sdr/BJNA040802), Aug 6, 2004: SKIN. CRACKED. DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACK AT LOWER AFT CORNER OF R1 DOOR CUTOUT AT BS 344. REPAIRED IAW THE BOEING 737 STRUCTURAL REPAIR MANUAL 53-30 - [SDR BJNA040801](https://openairdocs.org/sdr/BJNA040801), Aug 6, 2004: SKIN. CRACKED. DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACK AT L1 DOOR LOWER HINGE CUTOUT AT BS 304. REPAIRED IAW THE BOEING 737 STRUCTURAL REPAIR MANUAL 53-30-3 FIGUR - [SDR BJNA040503](https://openairdocs.org/sdr/BJNA040503), May 12, 2004: LIGHT. BURNED OUT. DURING A MAINTENANCE WALK AROUND CHECK, THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP OF TH - [SDR BJNA040502](https://openairdocs.org/sdr/BJNA040502), May 3, 2004: ACTUATOR. LEAKING. AFTER TAKEOFF, FLT CREW NOTICED HYD SYSTEM-A QUANTITY LOSS. A/C RETURNED TO MFE & MADE UNEVENTFUL OVERWEIGHT LANDING. B AND STANDBY HYD SYS NOT AFFECTED. MX DIS - [SDR BJNA040202](https://openairdocs.org/sdr/BJNA040202), Feb 24, 2004: WIRE. LOOSE. FORWARD FLOOR TRACK LIGHTING INOPERATIVE. INSPECTED THE EMERGENCY LIGHT POWER SUPPLY FOUND WIRE PULLED FROM THE CONNECTOR, REPLACED THE POWER SUPPLY, OPS CHECK - [SDR BJNA040203](https://openairdocs.org/sdr/BJNA040203), Feb 23, 2004: POWER SUPPLY. INOPERATIVE. DURING A MAINTENANCE WALK AROUND CHECK, THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY - [SDR BJNA040102](https://openairdocs.org/sdr/BJNA040102), Jan 28, 2004: CONNECTOR. INOPERATIVE. DURING A MAINTENANCE WALKAROUND CHECK, THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING DID NOT ILLUMINATE. MAINTENANCE CLEANED THE CONNECTORS ON THE FORWA - [SDR BJNA031101](https://openairdocs.org/sdr/BJNA031101), Nov 9, 2003: BATTERY PACK. INOPERATIVE. DURING A SCHEDULED MAINTENANCE CHECK THE EMERGENCY EXIT LIGHTS AT DOOR R-2, AND L2 DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE R-2, AND L2 EMERGENC - [SDR BJNA030801](https://openairdocs.org/sdr/BJNA030801), Aug 13, 2003: BEARING. FAILED. AT FL 310, NR 1 ENGINE OIL PRESSURE NOTICED DROPPING, OIL QUANTITY WENT TO HALF GALLON, AND OIL TEMPERATURE ROSE TO THE YELLOW BAND. ENGINE WAS SHUTDOWN, LOW OI - [SDR BJNA030700](https://openairdocs.org/sdr/BJNA030700), Jul 14, 2003: LIGHT. INOPERATIVE. DURING A MAINTENANCE PREFLIGHT INSPECTION, THE EMERGENCY EXIT LIGHT LOCATED BY THE LEFT AFT ENTRY DOOR EXTERIOR WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND RE - [SDR BJNA030601](https://openairdocs.org/sdr/BJNA030601), Jun 10, 2003: ODOR. DETECTED. BURNING ODOR IN COCKPIT AND CABIN ON TAKEOFF. INSPECTED AIRCRAFT, RAN ENGINES, CHECKED AIR CONDITIONING PACKS AND VENTILATION SYSTEM. UNABLE TO DUPLICATE, NO FA - [SDR BJNA030501](https://openairdocs.org/sdr/BJNA030501), May 6, 2003: GEARBOX. LEAKING. NR 2 ENGINE DEVELOPED OIL LEAK IN FLIGHT, ENGINE SHUT DOWN, AIRCRAFT LANDED WITHOUT INCIDENT. FOND THE ENGINE GEARBOX P-5 PORT THREADS STRIPPED, OIL LEAKING ARO - [SDR BJNA021202](https://openairdocs.org/sdr/BJNA021202), Dec 30, 2002: BATTERY PACK. DISCHARGED. LT EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE AT OVERWING EXIT. REPLACE LT EXTERIOR EMERGENCY BATTERY PACK POWER SUPPLY IN THE AFT CARGO PIT IAW MM. - [SDR BJNA021102](https://openairdocs.org/sdr/BJNA021102), Nov 10, 2002: COVER. BROKEN. HARD COMPRESSOR STALL ON NR 1 ENGINE AT 2.20 EPR - 96 PERCENT N1 - 20 KNOTS SPEED, POWER WAS PULLED TO IDLE WITHIN 300 FT OF TAKE OFF ROLL, TAKE OFF ABORTED. EN - [SDR BJNA021001](https://openairdocs.org/sdr/BJNA021001), Oct 9, 2002: CASE. DAMAGED. ON TAKEOFF ROLL AT 115 KNOTS AIRCRAFT VEERED TO THE LT, CAPTAIN REPORTED HEARING A LOUD BANG. ABORTED TAKEOFF. MAINTENANCE REPORTED MAJOR DAMAGE TO TURBINE SECT - [SDR BJNA020832](https://openairdocs.org/sdr/BJNA020832), Aug 27, 2002: SPAR. CORRODED. FOUND LT HORIZONTAL STAB CENTER SECTION REAR SPAR TOP CHORD FORWARD LUG HAS LEVEL 2 CORROSION INSIDE BORE. REMOVED CORROSION BORED I/D OF LUG TO 1.564 INCH, ROT - [SDR BJNA020828](https://openairdocs.org/sdr/BJNA020828), Aug 16, 2002: FRAME. CORRODED. FOUND LEVEL 2 CORROSION UNDER 3 EACH SCREW HOLES AT FRAME RBL 28 BETWEEN BS 955 TO BS 967. REMOVED FRAME ORDERED AND RECEIVED NEW FRAME (BEAM) DRILLED, DEBBARRD - [SDR BJNA020827](https://openairdocs.org/sdr/BJNA020827), Aug 15, 2002: BEAM. CORRODED. FOUND LEVEL 2 CORROSION 4 EACH PLACES ON UPPER SURFACE OF BEAM 294.5 BETWEEN LBL 10 TO RBL 20. REMOVED CORROSION AND TREAT. REPAINT SURFACE CHECK LIMITS. (M) - [SDR BJNA020824](https://openairdocs.org/sdr/BJNA020824), Aug 15, 2002: FRAME. CORRODED. FOUND FRAME AT STATION 328 HAS SURFACE CORROSION AROUND FASTENER HOLES ON UNDER SIDE OF FRAME. LEVEL 2 CORROSION. REMOVED CORROSION AT 328 FABRICATED REPAIR ANG - [SDR BJNA020818](https://openairdocs.org/sdr/BJNA020818), Aug 14, 2002: PANEL. CORRODED. FOUND CORROSION IN FORWARD PIT LEFT SIDE TRANSITION PANEL FROM STATION 500B TO 520, LEVEL 2 CORROSION. REMOVED OLD TRANSITION PANEL, FABRICATED NEW SECTION OF P - [SDR BJNA020833](https://openairdocs.org/sdr/BJNA020833), Aug 12, 2002: SKIN. CORRODED. FORWARD FRAME OF THE C-2 DOOR CUT OUT ABOVE TRANSITION PANEL HAS LEVEL 2 CORROSION. REMOVED CORRODED FRAME IAW 737 SRM 51-30-2 AND REO L00 588. REPAIRED FRAME I - [SDR BJNA020831](https://openairdocs.org/sdr/BJNA020831), Aug 10, 2002: FRAME. CORRODED. FOUND LEVEL 2 CORROSION FORWARD PIT STATION 500 RBL 12 FRAME LOWER LEG. CORROSION REMOVED AND FOUND REMAINING MATERIAL OUT OF LIMITS, FABRICATED, TRIMMED DRILLE - [SDR BJNA020813](https://openairdocs.org/sdr/BJNA020813), Aug 9, 2002: DOOR FRAME. GOUGED. FOUND RIGHT SIDE FORWARD EDGE OF AFT CARGO DOOR OPENING IS GOUGED AND TORN. CUT OUT DAMAGED AREA AND FABRICATED STACKED DOUBLER REPAIR PER B737 SRM 53-30-3 FIG - [SDR BJNA020810](https://openairdocs.org/sdr/BJNA020810), Aug 8, 2002: SEAT TRACK. CORRODED. SURFACE CORROSION ON SEAT TRACK AT RBL 32 AT BS 328, LEVEL 2 CORROSION. FOUND CORROSION ON SEAT TRACK OUT OF LIMITS, CUT NEW TRACK FROM BAC1520-792 16 INCH INST - [SDR BJNA020825](https://openairdocs.org/sdr/BJNA020825), Aug 7, 2002: STRINGER. CORRODED. AFT AIRCRAFT INSIDE RIGHT SIDE STRINGER 17 AT FS 986.5 UNDER CUSP LONGERON HAS LEVEL 2 CORROSION. REMOVED CORROSIN FABRICATED AND INSTALLED NEW CUSP WEB IAW B73 - [SDR BJNA020812](https://openairdocs.org/sdr/BJNA020812), Aug 6, 2002: TIE CLIP. CRACKED. FOUND TENSION TIE FITTING AT STA 104 STR 19L AND 20L CRACKED ON CORNER. LEVEL 2 CORROSION. REMOVED SECTION OF STATION 19L AT FS 104 FABRICATED REPAIR SECTION OF - [SDR BJNA020811](https://openairdocs.org/sdr/BJNA020811), Aug 6, 2002: SHEAR TIE. CORRODED. FOUND CORROSION IN FORWARD PIT AT STA 500 LBL 2 TO RBL 2 FRAME LOWER LEG, LEVEL 2 CORROSION. CUT AND REMOVED CORROSION FROM SHEAR TIE LEG. FABRICATED AND INSTAL - [SDR BJNA020820](https://openairdocs.org/sdr/BJNA020820), Aug 6, 2002: FLOOR SUPPORT. CORRODED. FORWARD PIT FLOOR SUPPORT BS 520 LBL 17 TO LBL 20 LEVEL 2 CORROSION AROUND 4 EACH NUT CLIPS AND 1 MISSING. REMOVED CORROSION FABRICATED AND INSTALLED FLOOR SUPP - [SDR BJNA020819](https://openairdocs.org/sdr/BJNA020819), Aug 6, 2002: ANGLE. CORRODED. FORWARD PIT BS 500 RBL 28 FRAME SUPPORT LOWER LEG FORWARD AND AFT HAS LEVEL 2 CORROSION. REMOVED CORROSION FABRICATED AND INSTALLED ANGLE REPAIR IAW B737 SRM 51 - [SDR BJNA020823](https://openairdocs.org/sdr/BJNA020823), Aug 6, 2002: TORQUE BOX. CORRODED. FOUND BS 1100 LEFT TOP CORNER OF TORQUE BOX NUT PLATE HAS LEVEL 2 CORROSION. CUT OUT CORRODED AREA FABRICATED AND INSTALLED FILLER ANGLE AND RADIUS BLOCK IAW B7 - [SDR BJNA020822](https://openairdocs.org/sdr/BJNA020822), Aug 6, 2002: TORQUE BOX. GOUGED. FOUND BS 1104 TORQUE BOX LEFT CENTER SIDE HAS DEEP GOUGE. CUT OUT GOUGED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR IAW B737 SRM 51-40-2 FIGURE 1 - [SDR BJNA020821](https://openairdocs.org/sdr/BJNA020821), Aug 6, 2002: STRINGER. GOUGED. TAIL COMPARTMENTS BS 1044 STRINGER 26L HAS DEEP CHAFE FROM BLEED AIR DUCT. CUT OUT CHAFED SECTION OF STRINGER, FABRICATED AND INSTALLED STRINGER REPAIR IAW 53-1 - [SDR BJNA020809](https://openairdocs.org/sdr/BJNA020809), Aug 6, 2002: STRUCTURE. CORRODED. FOUND CORROSION ON 4 SCREW HOLES AT RBL 20 BETWEEN BS 986.5 TO BS 967, CORROSION LEVEL 2. (M) - [SDR BJNA020806](https://openairdocs.org/sdr/BJNA020806), Aug 6, 2002: FRAME. CORRODED. CORROSION ON FRAME RBL 8 NEAR BEAM BS 967. REMOVED 18.8750 INCH SECTION, FABRICATED AND INSTALLED REPAIR SECTION OF FRAME IAW SRM. All 81: https://openairdocs.org/deregistered/N344TM-2005-12-28/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 20021008030219I](https://openairdocs.org/incident/20021008030219I), Oct 8, 2002: Boeing 737200 (N344TM), Elko, NV, Minor damage. (-23) At a speed of approximately 115 knots during the take-off on runway 23 at the Elko Regional Airport (eko) in Elko, NV., the aircraft veered to the left,… --- 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.