# Boeing 737-2S5C - Type: Aircraft model (FAA registry) - Registry code: 1384499 - Manufacturer (registry): BOEING - Model: 737-2S5C - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 ยท Turbo-fan - Seats: 130 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/boeing-737-2s5c 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 (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 19861224076319I](https://openairdocs.org/incident/19861224076319I), Dec 24, 1986: Boeing 7372S5C (N802AL), Van Nuys, CA. Ferry fuel tank developed a leak after takeoff. Returned to airport. Bottom welded seam of tank had massive leak. ## Service difficulty reports (143, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR TSAA0253214](https://openairdocs.org/sdr/TSAA0253214), Oct 16, 2002: SPAR. CRACKED. REMOVED A CRACK AND CORROSION LOCKED AT RIGHT WING FRONT SPAR WEB AT FSS 124.79 AND FSS 134.80. HFEC INSPECTED TO ENSURE THE DAMAGE COMPLETELY REMOVED. FABRICAT - [SDR TSAA0253182](https://openairdocs.org/sdr/TSAA0253182), Aug 16, 2002: SPAR. CRACKED. RIGHT WING FRONT SPAR CRACK AND CORRODED AT FSS124.79 AND FSS134.80. AIRCRAFT RETURNED TO SERVICE. - [SDR TSAA0252137](https://openairdocs.org/sdr/TSAA0252137), May 13, 2002: PROXIMITY SWITCH. INOPERATIVE. DURING CLIMB, OUT THE CABIN RATE OF CLIMB WAS 1750 FPM WITH BOTH OUTFLOW VALVES CLOSED AND ALL DOOR LIGHTS. UNABLE TO PRESSURIZE THE CABIN, THE AIRCRAFT RETURNE - [SDR TSAA0253139](https://openairdocs.org/sdr/TSAA0253139), May 13, 2002: SKIN. CRACKED. FOUND A 4 INCH CRACK AT BS 780 STRINGER 15R. TRIMMED OUT CRACK, MAINTAINING A .5 INCH MINIMUM RADIUS AND 2D EDGE MARGIN FROM FASTENERS. HFEC INSPECTED THE CUTOU - [SDR TSAA0253138](https://openairdocs.org/sdr/TSAA0253138), May 13, 2002: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT BS 275 STRINGER 15L. TRIMMED OUT THE CRACK MAINTAINING A .5 INCH MINIMUM RADIUS. HFEC INSPECTED CUT OUT. FABRICATED REPAIR PLATE FROM 2 - [SDR TSAA0251046](https://openairdocs.org/sdr/TSAA0251046), Feb 13, 2002: DOOR FRAME. CRACKED. REPAIRED .25 INCH CRACK AT MAIN CARGO DOOR FRAME EXTENDING FROM THE RIVET AT BS 390. CUTOUT AND CONFIRMED CRACK REMOVED USING HFEC METHOD. FABRICATED AND INSTAL - [SDR TSAA0253048](https://openairdocs.org/sdr/TSAA0253048), Feb 7, 2002: SEAT TRACK. DAMAGED. CUT AND REMOVED THE DAMAGED PORTION OF THE TRACK AT BS 420 TO 480. FABRICATED NEW SEAT TRACK. INSTALLED THE REPAIR PARTS IAW SRM 53-10-5, FIGURE 7. AIRCRAFT RET - [SDR TSAA0253023](https://openairdocs.org/sdr/TSAA0253023), Jan 24, 2002: BULKHEAD. CRACKED. FOUND CRACK INDICATION FORWARD SIDE OF LEFT BULKHEAD 178 CENTER WEB LBL 10.0 WI234, ADJACENT TO RIVET HEAD. REMOVED CRACK AND MAINTAINED A MINIMUM OF .038 INCH - [SDR TSAA0124102](https://openairdocs.org/sdr/TSAA0124102), Nov 16, 2001: CIRCUIT BREAKER. FAULTY. FLT 950 - HNL-ITO - AFTER TAKEOFF DURING FLIGHT, THE NR 2 THRUST REVERSER AND NR 2 AFT FUEL PUMP CIRCUIT BREAKERS POPPED/TRIPPED. RESET NORMAL AND AFTER SEVERAL - [SDR TSAA0132010](https://openairdocs.org/sdr/TSAA0132010), Aug 14, 2001: ACCESSORY UNIT. FAULTY. ON APPROACH, WITH GEAR DOWN THREE GREEN AND FLAPS AT 40 GREEN LIGHT, AURAL WARNING 'TOO LOW GEAR' SOUNDED AT APPROX 900 FT. THREE RED GEAR LIGHTS ILLUMINATED, T - [SDR TSAA0153083](https://openairdocs.org/sdr/TSAA0153083), Jul 1, 2001: FRAME. CRACKED. DISCOVERED CRACK PROPAGATING FROM FORWARD FASTENER HOLE AT BS 727 CHORD STRINGER S-18L, DURING SCHEDULED INSPECTION VERIFIED BY METHOD OF HFEC AND ULTRASONIC IN - [SDR TSAA0153084](https://openairdocs.org/sdr/TSAA0153084), Jul 1, 2001: FRAME. CRACKED. DISCOVERED CRACK PROPAGATING FROM THE AFT TO FORWARD FASTENER HOLE AT BS 727 CHORD STRINGER S18R DURING SCHEDULED INSPECTION VERIFIED BY METHOD OF HFEC AND ULTR - [SDR TSAA0021228](https://openairdocs.org/sdr/TSAA0021228), Nov 2, 2000: CONTROLLER. FAILED. FLT 942 - HNL-KOA - AFTER TAKEOFF, PRESSURIZATION IN AUTO FAILED. NOT CONTROLLABLE IN ANY MODE. RETURNED TO HNL FOR UNEVENTFUL LANDING. REMOVED AND REPLACED THE - [SDR TSAA0033257](https://openairdocs.org/sdr/TSAA0033257), Jul 25, 2000: BATTERY PACK. DISCHARGED. REPLACED NR 6 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. - [SDR TSAA0033177](https://openairdocs.org/sdr/TSAA0033177), Jul 25, 2000: BATTERY PACK. INOPERATIVE. REPLACED NR 6 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0033167](https://openairdocs.org/sdr/TSAA0033167), Jul 11, 2000: BATTERY PACK. INOPERATIVE. REPLACED NR 4 PROXIMITY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0033168](https://openairdocs.org/sdr/TSAA0033168), Apr 11, 2000: BATTERY PACK. INOPERATIVE. REPLACED CENTER AISLE NR 6 LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0033102](https://openairdocs.org/sdr/TSAA0033102), Mar 20, 2000: BATTERY PACK. INOPERATIVE. REPLACED RIGHT OVERWING EXTERIOR EMERGENCY LIGHT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0053096](https://openairdocs.org/sdr/TSAA0053096), Mar 16, 2000: SKIN. CRACKED. REPAIRED FUSELAGE SKIN AT BS 770, STRINGER 17L IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0033071](https://openairdocs.org/sdr/TSAA0033071), Mar 4, 2000: BATTERY PACK. INOPERATIVE. REPLACED RIGHT OVERWING SLIDE LIGHTS BATTERY POWER SUPPLY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0033070](https://openairdocs.org/sdr/TSAA0033070), Mar 3, 2000: LIGHT. INOPERATIVE. REPLACED THE ENTRY DOOR EMERGENCY EXIT LIGHT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0033069](https://openairdocs.org/sdr/TSAA0033069), Feb 17, 2000: BATTERY PACK. INOPERATIVE. REPLACED THE FORWARD ENTRY EXIT IDENTIFIER POWER SUPPLY DUE TO DIM LIGHT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA200057060](https://openairdocs.org/sdr/TSAA200057060), Feb 9, 2000: SPLICE PLATE. CRACKED. CENTER FUEL TANK SPLICE PLATE FOUND CRACKED. REPAIRED IAW ECO 1854. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA200055059](https://openairdocs.org/sdr/TSAA200055059), Feb 9, 2000: ATTACH FITTING. CRACKED. LEFT AND RIGHT HORIZONTAL STABILIZER UPPER ATTACH FITTINGS FOUND CRACKED. BOEING AOG TEAM REPLACED THE HORIZONTAL STABILIZER UPPER ATTACH CHORD. AIRCRAFT RETURN - [SDR TSAA9933503](https://openairdocs.org/sdr/TSAA9933503), Dec 13, 1999: LIGHT. INOPERATIVE. REPLACED NR 2 POSITION FLOOR LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9933497](https://openairdocs.org/sdr/TSAA9933497), Dec 9, 1999: BATTERY PACK. INOPERATIVE. REPLACED BATTERY PACK FOR NR 2 POSITION FLOOR LIGHT DUE TO NO TEST. OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE. (X) - [SDR TSAA9933496](https://openairdocs.org/sdr/TSAA9933496), Dec 8, 1999: BATTERY PACK. INOPERATIVE. REPLACED BATTERY PACK FOR NR 2 POSITION FLOOR LIGHT DUE TO NO TEST. OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE. (X) - [SDR TSAA9933495](https://openairdocs.org/sdr/TSAA9933495), Dec 2, 1999: BATTERY PACK. DISCHARGED. REPLACED BATTERY PACK FOR NR 4 AND NR 6 POSITION FLOOR LIGHT DUE TO LOW. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X) - [SDR TSAA9933482](https://openairdocs.org/sdr/TSAA9933482), Nov 27, 1999: BATTERY PACK. DISCHARGED. REPLACED BATTERY PACK FOR NR 5 POSITION FLOOR LIGHT DUE TO INOPERABLE. OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE. (X) - [SDR TSAA9933467](https://openairdocs.org/sdr/TSAA9933467), Oct 22, 1999: LIGHT. INOPERATIVE. REPLACED CONTROL CABIN EXIT EMERGENCY LIGHT ASSY DUE TO NOT TURNING OFF. OPS CHECK OK. AIRCRAFT RETURNED TO SERICE. (M) - [SDR TSAA9928365](https://openairdocs.org/sdr/TSAA9928365), Jul 30, 1999: CONDUIT. LEAKED. IN THE PROCESS OF ACCOMPLISHING ECO 2956, CENTER TANK FLOAT SWITCH MOD, SB 737 28A1132, AD 99-05012, MECHANICS FOUND THAT FUEL HAD LEAKED INTO THE ELECTRICAL CO - [SDR TSAA9933258](https://openairdocs.org/sdr/TSAA9933258), Jun 11, 1999: BATTERY PACK. DISCHARGED. REPLACED BATTERY PACK FOR NR 4 POSITION FLOOR LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9933257](https://openairdocs.org/sdr/TSAA9933257), Jun 9, 1999: BATTERY PACK. DISCHARGED. REPLACED BATTERY PACK FOR NR 1 POSITION FLOOR LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9953289](https://openairdocs.org/sdr/TSAA9953289), Jun 5, 1999: SKIN. CRACKED. FUSELAGE SKIN CRACK AT BS 536 AT STRINGE R15R. VERIFIED CRACK AND CRACK ENDS USING HIGH FREQUENCY EDDY CURRENT. REPAIRED PER SRM 53-30-3 FIG 1. AIRCRAFT RETURNE - [SDR TSAA9953288](https://openairdocs.org/sdr/TSAA9953288), Jun 5, 1999: SKIN. CRACKED. FUSELAGE SKIN CRACK AT BS 749 AT STRINGER 15L. VERIFIED CRACK AND CRACK ENDS USING HIGH FREQUENCY EDDY CURRENT. REPAIRED PER SRM 53-30-3 FIG 1. AIRCRAFT RETURNE - [SDR TSAA9953287](https://openairdocs.org/sdr/TSAA9953287), Jun 5, 1999: SKIN. CRACK. FUSELAGE SKIN CRACK AT BS 749 AT STRINGER 17L. VERIFIED CRACK AND CRACK ENDS USING HIGH FREQUENCY EDDY CURRENT. REPAIRED PER SRM 53-30-3 PAGE 25. AIRCRAFT RETUR - [SDR TSAA9933243](https://openairdocs.org/sdr/TSAA9933243), May 30, 1999: LIGHT. INOPERATIVE. REPLACED AFT SERVICE DOOR EMERGENCY LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9933219](https://openairdocs.org/sdr/TSAA9933219), Apr 15, 1999: BATTERY PACK. DISCHARGED. REPLACED NR 6 FLOOR LIGHT PROXIMITY BATTERY PACK DUE TO NO 'ALL IS WELL' LED. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9933218](https://openairdocs.org/sdr/TSAA9933218), Apr 15, 1999: LIGHT. INOPERATIVE. REPLACED NR 4 FLOOR PROXIMITY LIGHT ASSY DUE TO NO 'ALL IS WELL' LED. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9933203](https://openairdocs.org/sdr/TSAA9933203), Apr 6, 1999: BATTERY PACK. DISCHARGED. REPLACED LEFT OVERWING EXIT IDENTIFIER BATTERY PACK DUE TO BEING INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9933202](https://openairdocs.org/sdr/TSAA9933202), Apr 6, 1999: BATTERY PACK. DISCHARGED. REPLACED AFT EMERGENCY LIGHT TRANSMITTER BATTERY PACK DUE TO BEING INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9933020](https://openairdocs.org/sdr/TSAA9933020), Jan 12, 1999: BATTERY PACK. DISCHARGED. REPLACED EMERGENCY FLOOR LIGHT BATTERY PACKS DUE TO INOP FOR POSITIONS 1, 2, 3 AND 4. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9933018](https://openairdocs.org/sdr/TSAA9933018), Jan 11, 1999: BATTERY PACK. DISCHARGED. REPLACED NR 2 SEAT EMERGENCY LIGHT ASSY BATTERY PACK DUE TO NO 'ALL WELL' LIGHT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9833651](https://openairdocs.org/sdr/TSAA9833651), Dec 25, 1998: BATTERY PACK. DISCHARGED. REPLACED NR 2 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9833627](https://openairdocs.org/sdr/TSAA9833627), Dec 12, 1998: LIGHT. INOP. REPLACED FORWARD SERVICE DOOR OVERHEAD EMERGENCY LIGHT ASSY DUE TO BEING INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9833621](https://openairdocs.org/sdr/TSAA9833621), Dec 10, 1998: BATTERY PACK. DISCHARGED. REPLACED FORWARD EMERGENCY CENTER OVERHEAD EXIT SIGN BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9833606](https://openairdocs.org/sdr/TSAA9833606), Nov 30, 1998: BATTERY PACK. DISCHARGED. NR 2 SEAT EMERGENCY LIGHT BATTERY PACK NO LIGHT. REPLACED NR 2 BATTERY PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9833553](https://openairdocs.org/sdr/TSAA9833553), Oct 11, 1998: BATTERY PACK. DISCHARGED. REPLACED NR 3 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9833541](https://openairdocs.org/sdr/TSAA9833541), Oct 6, 1998: BATTERY PACK. DISCHARGED. REPLACED FORWARD ENTRANCE EXIT IDENTIFIER BATTERY DUE TO LOW VOLTAGE. OPERATIONAL CHECK FOUND SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA9833511](https://openairdocs.org/sdr/TSAA9833511), Sep 21, 1998: BATTERY PACK. DISCHARGED. REPLACED NR 2 POSITION EMERGENCY FLOOR PROXIMITY LIGHT BATTERY PACK DUE TO BEING INOP. REPLACED BATTERY PACK. AIRCRAFT RETURNED TO SERVICE. (M) All 143: https://openairdocs.org/model/boeing-737-2s5c/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.