# Boeing 737 2J8 - Type: Aircraft model (FAA registry) - Registry code: 1384489 - Manufacturer (registry): BOEING - Model: 737 2J8 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-fan - Seats: 125 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/boeing-737-2j8 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 None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports (2) 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 19960125002059I](https://openairdocs.org/incident/19960125002059I), Jan 25, 1996: Boeing 7372J8 (N235WA), Wichita, KS, Minor damage. Narrative: delta flt 846 from ict to atl on 1/25/96 a/c B-737 number N235WA at gear retraction, on takeoff at ict, left main gear remained illuminated with… - [Incident 19870821066349I](https://openairdocs.org/incident/19870821066349I), Aug 21, 1987: Boeing 7372J8 (N235WA), Las Vegas, NV. Aft lavatory smoke detector activated on approach. Fire bottle discharged and hand bottle put out fire in trash bin ## Service difficulty reports (25) As reported by operators and repair stations, by the model named in the report. - [SDR DL73E010722](https://openairdocs.org/sdr/DL73E010722), May 5, 2001: SUPPORT FITTING. CORRODED. THE WL 188.5 LUG ON THE LT MLG SIDE STRUT SUPPORT FITTING AT FS 685 WAS FOUND WITH CORROSION IN THE LUG BORE. THE CORROSION WAS REMOVED BY OVERSIZING THE LUG BO - [SDR DL73E010721](https://openairdocs.org/sdr/DL73E010721), May 5, 2001: SKIN. CRACKED. A 1.2 INCH LONG CRACK WAS FOUND IN THE BONDED SKIN ASSY AT THE LOWER FWD CORNER OF THE AFT GALLEY DOOR CUTOUT. THE CRACK WAS REMOVED WITH A CUTOUT IN THE SKIN. - [SDR DL73E010723](https://openairdocs.org/sdr/DL73E010723), May 4, 2001: SKIN. CRACKED. A TYPICAL CRACK WAS FOUND IN THE LOWER FORWARD CORNER OF THE AFT ENTRY DOOR CUTOUT. THE CRACK WAS IN THE BONDED SKIN ASSY AND THE UNDERLYING BEAR STRAP. THE CRA - [SDR DL73E002241](https://openairdocs.org/sdr/DL73E002241), Nov 14, 2000: FLOORBEAM. CRACKED. THE UPPER CAP OF THE BL 0.07 LONGITUDINAL FLOORBEAM WAS FOUND WITH CRACKS COMMON TO THE FLOOR PANEL ATTACH HOLES BETWEEN FS 660 & 664. THE CRACKS ARE TYPICAL OF - [SDR DL73E002068](https://openairdocs.org/sdr/DL73E002068), Oct 19, 2000: SWITCH. MALFUNCTIONED. AS POWER WAS PUSHED UP FOR TAKEOFF ABOVE 1.4 EPR TAKEOFF WARNING HORN SOUNDED INTERMITTENT TONE. TAKEOFF WAS DISCONTINUED AT AROUND 20 - 30 KTS. A CHECK SHOWED - [SDR DL73E000209](https://openairdocs.org/sdr/DL73E000209), Jan 27, 2000: SKIN. CRACKED. THE LOWER AFT CORNER OF THE R1 DOOR CUTOUT WAS FOUND WITH A 1.75 INCH TYPICAL CRACK IN THE SKIN AND BONDED DOUBLER AND A 1.5 INCH CRACK IN THE UNDERLYING BEAR S - [SDR DL73E991054](https://openairdocs.org/sdr/DL73E991054), May 13, 1999: OVERHEAT DET. INOPERATIVE. APU LIGHT ILLUMINATED ON T/O. PULLED HANDLE, LIGHT CONTINUED TO ILLUMINATE ON TAXI BACK. REJECTED TAKEOFF. REPLACED APU TAILPIPE OVERHEAT DET CONNECTOR D1878 AN - [SDR DL73E990468](https://openairdocs.org/sdr/DL73E990468), Mar 5, 1999: LIGHT. INOP. EMERGENCY EXIT LIGHT ABOVE L1 DOOR INOP. REPLACED LIGHT ASSY, OP CKS GOOD. - [SDR DL73E990249](https://openairdocs.org/sdr/DL73E990249), Feb 5, 1999: LIGHT. INOP. EMERGENCY LIGHT ASSY SEAT 12D INOP. REPLACED LIGHT ASSY, TEST GOOD PER MM. - [SDR DL73E981806](https://openairdocs.org/sdr/DL73E981806), Sep 1, 1998: ACTUATOR. BROKEN. ON TAXI IN, A-SYS HYD WENT TO ONE GALLON. REPLACED NR 8 SPOILER ACTUATOR. - [SDR DL73E981407](https://openairdocs.org/sdr/DL73E981407), Jul 4, 1998: ENGINE. OVER TEMP. ENGINE IN FLIGHT, SHUT DOWN DUE TO OIL TEMP EXCEEDED RED LINE. ENGINE WAS REPLACED. - [SDR DL73E972306](https://openairdocs.org/sdr/DL73E972306), Nov 10, 1997: KEEL BEAM. CRACKED. TWO 1.5 INCH CRACKS FOUND IN THE KEEL BEAM LWR SKIN AT STA 680 AND TWO ADDITIONAL AT STA 696. CRACKS LOCATED AT L/RBL 5. REPAIR PER ERA 363005-14, REV A. - [SDR DL73E972305](https://openairdocs.org/sdr/DL73E972305), Nov 10, 1997: SKIN. CRACKED. CRACK FOUND IN THE FUSELAGE SKIN AT STA 727A AND STR 16R. REPAIR PER ERA 330976-14. - [SDR DL73E972304](https://openairdocs.org/sdr/DL73E972304), Nov 10, 1997: SKIN. CRACKED. FUSELAGE SKIN FOUND WITH A SMALL CRACK IN THE UPPER AFT CORNER OF THE C2 DOOR CUTOUT. REPAIRED PER ERA 330960-14. - [SDR DL73E972303](https://openairdocs.org/sdr/DL73E972303), Nov 10, 1997: STRUCTURE. CORRODED. SKIN, FRAME AND STRINGERS 27 LT AND RT WERE FOUND WITH CORROSION AT STA 807. REPAIRED PER ERA 330955-14. - [SDR DL73E972302](https://openairdocs.org/sdr/DL73E972302), Nov 10, 1997: FRAME. CRACKED. R1 DOOR FRAME INTERCOSTAL AT STGR 8A WAS CRACKED IN TYP MANNER SHOWN IN SB 737-53A1108, R5, AT APPROX FS 334. ALSO, THE INTERCOSTAL AT STGR 11 WAS CRACKED. REPA - [SDR DL73E972301](https://openairdocs.org/sdr/DL73E972301), Nov 10, 1997: FLOORBEAM. CRACKED. FLOORBEAM AT FS 520 WAS FOUND CRACKED AT RBL 25 AND LBL 45. REPAIRED PER SB 737-53-1120, R 1. - [SDR DL73E972112](https://openairdocs.org/sdr/DL73E972112), Oct 10, 1997: SKIN. CRACKED. THE RT FUSELAGE SKIN BETWEEN FS 747 AND 767 AND S-18R AND S-19R WAS FOUND WITH TWO CRACKS. REPAIRED PER DELTA ER/A 362945-14 AND B737 SRM 53-30-3, FIG 6. - [SDR DL73E961207](https://openairdocs.org/sdr/DL73E961207), May 18, 1996: TEST MODULE. INOPERATIVE. NR 2 GENERATOR WOULD NOT HOOK UP TO BUS DUE TO NO VOLTAGE. FREQUENCY WAS NORMAL. REPLACED POWER TEST MODULE, OPS CK OK FOR SERVICE. - [SDR DL73E960757](https://openairdocs.org/sdr/DL73E960757), Apr 3, 1996: MAIN TIRE. FAILED. SHORTLY AFTER TAKEOFF, A HYD SYS PRESS FAILED AND QTY WENT TO ZERO. ACCOMPLISHED CHECKLIST AND RETURNED FOR LANDING. AFTER LANDING FOUND NR 3 MAIN TIRE HAD COME - [SDR DL73E960715](https://openairdocs.org/sdr/DL73E960715), Mar 30, 1996: BATTERY PACK. DISCHARGED. EMERGENCY PATH LIGHTS BATTERY PACK INOP. REPLACED, CHECKS GOOD. - [SDR DL73E960741](https://openairdocs.org/sdr/DL73E960741), Mar 29, 1996: BULKHEAD WEB. CRACKED. BULKHEAD 178 WAS FOUND CRACKED BENEATH THE VERTICAL STIFFENERS AT LBL 5.7 AND RBL 5.7. DAMAGE REMOVAL RESULTED IN CUT OUTS ON THE LT SIDE 3.5 AND 6 ABOVE WL 195 - [SDR DL73E960716](https://openairdocs.org/sdr/DL73E960716), Mar 27, 1996: BATTERY PACK. DISCHARGED. DURING LAYOVER, EMERGENCY LIGHTS FOR OVERWING EMERGENCY EXITS FAILED TEST. REPLACED BATTERY PACK, OPERATION NORMAL. - [SDR DL73E954725](https://openairdocs.org/sdr/DL73E954725), Dec 14, 1995: SKIN. DAMAGED. THE FUSELAGE SKIN WAS GOUGED BETWEEN FS 380 AND FS 400. THE DAMAGE CUT OUT MEASURES APPROX 4.9 BY 23.1. THE NEWLY DAMAGED SECTION IS BETWEEN 2 PREVIOUSLY DAMAGE - [SDR DL73E950771](https://openairdocs.org/sdr/DL73E950771), Jan 25, 1995: FRAME. CRACKED. DURING SHOP INSPECTION, A 0.70 INCH CRACK WAS FOUND IN THE INNER RADIUS OF THE FORWARD CARGO DOOR FRAME. THE CRACK IS LOCATED ON THE FORWARD EDGE OF THE DOOR BE --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. 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