# Boeing 737-2T4 - Type: Aircraft model (FAA registry) - Registry code: 1384492 - Manufacturer (registry): BOEING - Model: 737-2T4 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-jet - Seats: 134 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 1 - Page: https://openairdocs.org/model/boeing-737-2t4 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft (1) - [N737CS](https://openairdocs.org/aircraft/N737CS): [Trans Executive Airlines Of Hawaii Inc](https://openairdocs.org/faa-owner/TRANS%20EXECUTIVE%20AIRLINES%20OF%20HAWAII%20INC), [Honolulu, HI](https://openairdocs.org/faa-place/HI/Honolulu), S/N 23272 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports (10) 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 20010307003689I](https://openairdocs.org/incident/20010307003689I), Mar 7, 2001: Boeing 7372T4 (N808AL), Lanai City, HI, Minor damage. (-23) After applying takeoff power and as the a/c accelerated to approx. 20 knots, a loud bang was heard from the no. 1 engine. Engine was secured and a/c… - [Incident 19970709022739I](https://openairdocs.org/incident/19970709022739I), Jul 9, 1997: Boeing 7372T4 (N807AL), Honolulu, HI. Loud bang yaw and roll on climbout returned. Unable to find source. Replaced yaw damper and dfdr. - [Incident 19961203043609I](https://openairdocs.org/incident/19961203043609I), Dec 3, 1996: Boeing 7372T4 (N703S), Denver, CO, Minor damage. Narrative: sierra pacific spa 35 approved to depart runway 17L. At 125 knots, approximately halfway down the runway, the tower contacted spa 35 to abort… - [Incident 19960228006919I](https://openairdocs.org/incident/19960228006919I), Feb 28, 1996: Boeing 7372T4 (N722WN), Omaha, NE. Narrative: on February 28, 1996, N722WN, a Boeing 737-2T4, was operated by southwest airlines co., as flight 496 from st. louis, Missouri to Omaha, Nebraska.… - [Incident 19941128047479I](https://openairdocs.org/incident/19941128047479I), Nov 28, 1994: Boeing 7372T4 (N703S), Elko, NV. Landed on runway closed for snow removal ground crew cleared runway for 737. Mix up on NOTAM. ATC advised rwy open. - [Incident 19920604023169I](https://openairdocs.org/incident/19920604023169I), Jun 4, 1992: Boeing 7372T4 (N4569N), Covington - Cin, OH. Right generator failed in flight. APU fire warning on start up. Shut down. Used fire bottles. Replaced fire loop. - [Incident 19920514016859I](https://openairdocs.org/incident/19920514016859I), May 14, 1992: Boeing 7372T4 (N702ML), San Francisco, CA. Threat to aircraft while preparing for departure. Taxied to remote location. Evacuated by forward door slide. - [Incident 19880512053029I](https://openairdocs.org/incident/19880512053029I), May 12, 1988: Boeing 7372T4 (N702ML), Cleveland, OH. Inflight disturbance by a passenger. Emergency landing at Cleveland. Police took custody of irrational passenger. - [Incident 19870910062609I](https://openairdocs.org/incident/19870910062609I), Sep 10, 1987: Boeing 737200 (N130SW), Kansas City, MO, Minor damage. Nose tire threw its tread on rotation. Returned. Tread punched a hole in the e and e compartment door and skin dent. - [Incident 19870610036219I](https://openairdocs.org/incident/19870610036219I), Jun 10, 1987: Boeing 7372T4 (N4569N), Kansas City, MO. The left engine flamed out during climb. Aircraft safely returned to airport. Cause still under investigation. ## Service difficulty reports (1,269, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR FY4Y202105015](https://openairdocs.org/sdr/FY4Y202105015), May 5, 2021: SPAR. CRACKED. CRACK FOUND ON NO.5 FASTENER HOLE AT AFT SUPPORT FITTING AND REAR SPAR UPPER CHORD OF RH WING RSS 222 - [SDR FY4Y202105014](https://openairdocs.org/sdr/FY4Y202105014), May 5, 2021: SPAR. CRACKED. CRACK FOUND ON NO.5 FASTENER HOLE AT REAR SPAR UPPER CHORD OF LH WING AS MARKED. (STA RSS 222) - [SDR FY4Y202105019](https://openairdocs.org/sdr/FY4Y202105019), May 3, 2021: SPAR. CORRODED. CORROSION AT FWD UPPER L/H HORIZONTAL STABILIZER FRONT SPAR AT STAB. STA. 68~79 - [SDR FY4Y202105018](https://openairdocs.org/sdr/FY4Y202105018), May 3, 2021: SPAR. CORRODED. CORROSION AT FWD UPPER R/H HORIZONTAL STABILIZER FRONT SPAR AT STAB. STA. 68~75 - [SDR FY4Y202105013](https://openairdocs.org/sdr/FY4Y202105013), May 3, 2021: SKIN. CORRODED. CORROSION AT L/H WING SURGE TANK DRAIN VALVE (W STA 536) - [SDR FY4Y202105017](https://openairdocs.org/sdr/FY4Y202105017), May 1, 2021: SPAR. CORRODED. BULGE AT UPPER SKIN OF LH HORIZONTAL STABILIZER AT STAB. STA. 71~79 AND FROM REAR SPAR +1" - [SDR FY4Y202105016](https://openairdocs.org/sdr/FY4Y202105016), Apr 29, 2021: BEAM. CORRODED. CORROSION AT LH SIDE THRUST BEAM UPPER SURFACE AT STA. 1105 ~ 1130. (5EA) - [SDR FY4Y202105012](https://openairdocs.org/sdr/FY4Y202105012), Apr 28, 2021: SPAR. CORRODED. CORROSION AT L/H WING L/E FRONT SPAR LOWER CHORD HORIZONTAL LEG BETWEEN FSS 431 AND FSS 452 - [SDR JRAA202009110005](https://openairdocs.org/sdr/JRAA202009110005), Sep 4, 2020: EPR SYSTEM. FALSE INDICATION. UPON APPLYING T/O THRUST NR 2 EPR GAUGE DID NOT RESPOND. T/O CLEARANCE CANCELLED, EXITED RUNWAY FOR TROUBLESHOOTING, NO RELIEF. CHECKED MEL, NO RELIEF, RETURNED - [SDR JRAA20190501](https://openairdocs.org/sdr/JRAA20190501), Mar 27, 2019: WARNING SYSTEM. ACTIVATED. PILOT OBSERVED #2 ENGINE LOW OIL PRESSURE LIGHT IN FLIGHT AND PERFORMED IN FLIGHT SHUT DOWN PROCEDURES - [SDR SPAA2018060400502](https://openairdocs.org/sdr/SPAA2018060400502), May 30, 2018: LIGHT. INOPERATIVE. AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. - [SDR SPAA201806040001](https://openairdocs.org/sdr/SPAA201806040001), May 30, 2018: LIGHT. INOPERATIVE. OVERWING EMERGENCY EXITS LIGHTS INOPERATIVE. - [SDR SPAA201704030001](https://openairdocs.org/sdr/SPAA201704030001), Apr 26, 2017: LIGHT. INOPERATIVE. L1 AND R1 DOOR EMERGENCY ESCAPE SLIDE LIGHTS FAIL TO ILLUMINATE. - [SDR SPAA20170427001](https://openairdocs.org/sdr/SPAA20170427001), Apr 26, 2017: POWER SUPPLY. INOPERATIVE. L-1 AND R-1 DOOR EMERGENCY ESCAPE SLIDE LIGHTS FAIL TO ILLUMINATE - [SDR SPAA201704020002](https://openairdocs.org/sdr/SPAA201704020002), Apr 21, 2017: LIGHT. INOPERATIVE. CABIN AISLE EMERGENCY LIGHT FAILS TO ILLUMINATE. - [SDR SPAA201611002](https://openairdocs.org/sdr/SPAA201611002), Nov 7, 2016: POWER SUPPLY. INOPERATIVE. MID CABIN EMERGENCY CEILING LIGHT INOPERATIVE. - [SDR SPAA20161108001](https://openairdocs.org/sdr/SPAA20161108001), Nov 7, 2016: BATTERY PACK. DISCHARGED. MID CABIN EMERGENCY EXIT CEILING LIGHT INOP. - [SDR JRAA20160525003](https://openairdocs.org/sdr/JRAA20160525003), May 24, 2016: SELECTOR VALVE. STICKING. UNCOMMANDED LT MLG EXTENSION IN FLIGHT AT 315 KNOTS. REDUCED AIRSPEED AND REDUCED ALTITUDE. CORRECTED SEVERE YAW. SELECTED GEAR DOWN, 3 DOWN & LOCKED. CONTINUE - [SDR SPAA2016041200001](https://openairdocs.org/sdr/SPAA2016041200001), Apr 8, 2016: LIGHT. INOPERATIVE. PORTABLE EMERGENCY EXIT LIGHT AT R2 DOOR, FORWARD SERVICE DOOR, FAILS TO ILLUMINATE. REPLACED EMERGENCY EXIT LIGHT ASSY. - [SDR SPAA2016032300001](https://openairdocs.org/sdr/SPAA2016032300001), Mar 21, 2016: LIGHT. INOPERATIVE. FORWARD R2 SERVICE DOOR PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. - [SDR SPAA2016011400002](https://openairdocs.org/sdr/SPAA2016011400002), Jan 13, 2016: POWER SUPPLY. INOPERATIVE. MID CABIN OVERHEAD EMERGENCY EXIT LIGHT FAILS TO ILLUMINATE. FOUND POWER SUPPLY INOPERATIVE. - [SDR SPAA2016011400001](https://openairdocs.org/sdr/SPAA2016011400001), Jan 13, 2016: BATTERY PACK. INOPERATIVE. MID CABIN OVERHEAD EMERGENCY EXIT LIGHT FAILS TO ILLUMINATE. - [SDR 33AY2016FA0000063](https://openairdocs.org/sdr/33AY2016FA0000063), Jan 7, 2016: KEELBEAM. CORRODED. INSPECTION FOUND LT KEEL BEAM LOWER CHORD, LBBL 6.30, CORRODED BETWEEN BS 540-BS 580. THE CORRODED HORIZONTAL FLANGE SECTION WAS BLENDED AND TRIMMED OUT. INSTAL - [SDR 33AY2016FA0000053](https://openairdocs.org/sdr/33AY2016FA0000053), Jan 6, 2016: KEELBEAM. CUT. INSPECTION FOUND LT KEEL BEAM LOWER CHORD, LBL 6.30, CORRODED AND CRACKED BETWEEN BS 668 - 672. THE KEEL BEAM LOWER CHORD WAS CUT AT BS 625 AND THE KEEL BEAM AF - [SDR 33AY2016FA0000071](https://openairdocs.org/sdr/33AY2016FA0000071), Dec 21, 2015: FITTING. CORRODED. INSPECTION FOUND STRINGER FITTING AT S-27L, BS 1016 BULKHEAD CORRODED. THE DAMAGED STRINGER FITTING WAS R & R BY INSTALLING A NEW FITTING IAW SRM 51-3-02, REV 1 - [SDR 33AY2016FA0000070](https://openairdocs.org/sdr/33AY2016FA0000070), Dec 21, 2015: FITTING. CORRODED. INSPECTION FOUND STRINGER FITTING AT S26R, STA 1016 BULKHEAD CORRODED. THE DAMAGED STRINGER FITTING WAS R & R BY INSTALLING A NEW FITTING IAW SRM 51-3-02, REV 1 - [SDR 33AY2016FA0000069](https://openairdocs.org/sdr/33AY2016FA0000069), Dec 21, 2015: FITTING. CORRODED. INSPECTION FOUND STRINGER FITTING AT S-26L, BS 1016 BULKHEAD CORRODED. THE DAMAGED STRINGER FITTING WAS R & R BY INSTALLING A NEW FITTING IAW SRM 51-3-02, REV 1 - [SDR 33AY2016FA0000068](https://openairdocs.org/sdr/33AY2016FA0000068), Dec 21, 2015: FITTING. CORRODED. INSPECTION FOUND STRINGER FITTING AT S-25R, STA 1016 BULKHEAD CORRODED. THE DAMAGED STRINGER FITTING WAS R & R BY INSTALLING A NEW FITTING IAW SRM 51-3-02, REV - [SDR 33AY2016FA0000066](https://openairdocs.org/sdr/33AY2016FA0000066), Dec 21, 2015: FUEL CELL. CORRODED. INSPECTION FOUND CENTER TANK LOWER SKIN CORRODED BETWEEN S-9C TO S-10C, LBBL 6.30 TO RBBL 6.30. THE CORRODED SKIN AREAS WERE BLENDED. THE AREA WAS FOUND OUT OF - [SDR 33AY2016FA0000065](https://openairdocs.org/sdr/33AY2016FA0000065), Dec 21, 2015: FITTING. CORRODED. INSPECTION FOUND STRINGER FITTING AT STRINGER 27R, BS 1016 BULKHEAD CORRODED. THE DAMAGED STR FITTING WAS R & R BY INSTALLING A NEW FITTING IAW SRM 51-3-02, REV - [SDR 33AY2016FA0000064](https://openairdocs.org/sdr/33AY2016FA0000064), Dec 21, 2015: FUEL TANK. CORRODED. INSPECTION FOUND CENTER TANK LOWER SKIN CORRODED BETWEEN S-4C TO S-5C, LBBL 6.30 TO RBBL 6.30. THE CORRODED SKIN AREAS WERE BLENDED. THE AREA WAS FOUND OUT OF S - [SDR 33AY2016FA0000057](https://openairdocs.org/sdr/33AY2016FA0000057), Nov 14, 2015: FRAME. CORRODED. INSPECTION FOUND FRAME UPPER FLANGE AT BS 500B BETWEEN STR 25R TO STR 26R CORRODED OUT OF SRM ALLOWABLE LIMIT. THE DAMAGED SECTION WAS TRIMMED OUT AND REPAIR FI - [SDR 33AY2016FA0000056](https://openairdocs.org/sdr/33AY2016FA0000056), Nov 14, 2015: SKIN. CORRODED. INSPECTION FOUND CORROSION ON UPPER SKIN FAYING SURFACE AT LAP JOINT STR 26R BETWEEN BS 500 TO BS 500A. THE CORRODED UPPER SKIN SECTION WAS TRIMMED OUT AND EXTE - [SDR 33AY2016FA0000055](https://openairdocs.org/sdr/33AY2016FA0000055), Nov 14, 2015: FRAME. CORRODED. INSPECTION FOUND FRAME UPPER FLANGE AT BS 492 BETWEEN STR 25R CORRODED OUT OF SRM ALLOWABLE LIMIT. THE DAMAGED SECTION WAS TRIMMED OUT AND REPAIR FILLER AND FRA - [SDR 33AY2016FA0000054](https://openairdocs.org/sdr/33AY2016FA0000054), Nov 14, 2015: SKIN. CORRODED. INSPECTION FOUND CORROSION ON UPPER SKIN FAYING SURFACE AT LAP JOINT STR 26R BETWEEN BS 370 TO BS 400. THE CORRODED UPPER SKIN SECTION WAS TRIMMED OUT AND EXTER - [SDR 33AY2016FA0000062](https://openairdocs.org/sdr/33AY2016FA0000062), Oct 30, 2015: SKIN. DENTED. AIRCRAFT FOUND WITH DENT AND GOUGE DAMAGE TO THE SKIN ABOVE THE FWD CARGO DOOR CUTOUT, AT APPROXIMATELY BS 450, STR 18R. THIS DAMAGE IS WITHIN 10" OF THE DOOR A - [SDR 33AY2016FA0000073](https://openairdocs.org/sdr/33AY2016FA0000073), Oct 29, 2015: KEELBEAM. CORRODED. INSPECTION FOUND RT KEEL BEAM LOWER CHORD HORIZONTAL FLANGE CORRODED BETWEEN BS 540-BS 580, RBL 6.30. THE CORRODED FLANGE SECTION WAS BLENDED AND TRIMMED OUT. I - [SDR 33AY2016FA0000059](https://openairdocs.org/sdr/33AY2016FA0000059), Oct 28, 2015: FRAME. CORRODED. INSPECTION FOUND FRAME AT BS 787, BETWEEN STR 25L TO STR 26L CORRODED OUT OF SRM ALLOWABLE LIMIT. THE DAMAGED SECTION WAS TRIMMED OUT AND FRAME REPAIR DOUBLER W - [SDR 33AY2016FA0000058](https://openairdocs.org/sdr/33AY2016FA0000058), Oct 28, 2015: FRAME. CORRODED. INSPECTION FOUND FRAME UPPER FLANGE AT BS 887 ABOVE STRINGER STR 26L CORRODED OUT OF SRM ALLOWABLE LIMIT. THE DAMAGED SECTION WAS TRIMMED OUT AND FRAME REPAIR D - [SDR 33AY2016FA0000067](https://openairdocs.org/sdr/33AY2016FA0000067), Oct 26, 2015: SPLICE. CORRODED. INSPECTION FOUND KEEL BEAM SPLICE CORRODED AT LBBL 6.30, BS 727-BS727A. THE DAMAGED SPLICE WAS R & R IAW SRM 51-30-02. - [SDR SPAA2016110900001](https://openairdocs.org/sdr/SPAA2016110900001), Oct 15, 2015: SHEAR TIE. CORRODED. CORRODED SHEAR TIE AT BS 727A, STRINGER 23L, AFT CARGO BAY AREA - [SDR 33AY2016FA0000072](https://openairdocs.org/sdr/33AY2016FA0000072), Oct 15, 2015: SKIN. CORRODED. INSPECTION FOUND LT WING LOWER T/E SKIN CORRODED BETWEEN WBL 254 TO WBL 279.25 . THE CORRODED SKIN AREA WAS BLENDED AND REPAIRED IAW REPAIR PLAN 121083-R039, RE - [SDR 33AY2016FA0000060](https://openairdocs.org/sdr/33AY2016FA0000060), Sep 2, 2015: DOOR FRAME. CORRODED. INSPECTION FOUND AFT CARGO DOORWAY AFT FRAME AT BS 847 CORRODED. REPAIRED IAW AD 93-14-10 AND SB 737-53-1096, REV 5 BY REMOVING THE DAMAGED FRAME SEGMENT AND IN - [SDR SPAA2015051800001](https://openairdocs.org/sdr/SPAA2015051800001), May 15, 2015: BATTERY PACK. INOPERATIVE. CENTER PASSENGER CABIN OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EXIT LIGHT BATTERY PACK IAW AMM 33-51-81. - [SDR SPAA2015F00062](https://openairdocs.org/sdr/SPAA2015F00062), May 15, 2015: BATTERY PACK. DISCHARGED. CENTER, PASSENGER CABIN, OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. - [SDR SPAA2015032300002](https://openairdocs.org/sdr/SPAA2015032300002), Mar 20, 2015: POWER SUPPLY. INOPERATIVE. MID CABIN FIXED EMERGENCY EXIT SIGN FAILS TO ILLUMINATE. REPLACED EXIT SIGN POWER SUPPLY IAW AMM 33-51-101. FUNCTIONALLY TESTED IAW AMM 33-51-11 - [SDR SPAA2015032300001](https://openairdocs.org/sdr/SPAA2015032300001), Mar 20, 2015: BATTERY. INOPERATIVE. MID CABIN FIXED EMERGENCY EXIT SIGN FAILS TO ILLUMINATE. REPLACED EXIT SIGN BATTERY IAW AMM 33-51-8. FUNCTIONALLY TESTED IAW AMM 33-51-11. - [SDR SPAA201501050004](https://openairdocs.org/sdr/SPAA201501050004), Dec 31, 2014: BATTERY PACK. INOPERATIVE. MID CABIN EMERGENCY LIGHT FAILED TO ILLUMINATE DURING TEST. REPLACED THE BATTERY PACK IAW AMM 33-51-11. TESTED SATISFACTORY. - [SDR SPAA201501050003](https://openairdocs.org/sdr/SPAA201501050003), Dec 31, 2014: POWER SUPPLY. INOPERATIVE. FWD CABIN EMERGENCY EXIT LIGHT FAILED TO TEST. REPLACED THE POWER SUPPLY IAW AMM 33-51-01. TESTED SATISFACTORY. - [SDR SPAA2015010500002](https://openairdocs.org/sdr/SPAA2015010500002), Dec 31, 2014: BATTERY PACK. INOPERATIVE. MID CABIN EMERGENCY EXIT LIGHT FAILS TO ILLUMINATE ON TEST. REPLACED BATTERY PACK IAW AMM 33-51-81. TESTED SATISFACTORY. All 1,269: https://openairdocs.org/model/boeing-737-2t4/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.