# Boeing 737-8CX - Type: Aircraft model (FAA registry) - Registry code: 13844IA - Manufacturer (registry): BOEING - Model: 737-8CX - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-fan - Seats: 149 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 1 - Page: https://openairdocs.org/model/boeing-737-8cx 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) - [N277EA](https://openairdocs.org/aircraft/N277EA): [Umb Bank Na Trustee](https://openairdocs.org/faa-owner/UMB%20BANK%20NA%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2001, S/N 32359 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (38) As reported by operators and repair stations, by the model named in the report. - [SDR I5EA2022110300003](https://openairdocs.org/sdr/I5EA2022110300003), Oct 26, 2022: TRANSDUCER. FAILED. ANTISKID LIGHT ILLUMINATED IN FLIGHT, EMERGENCY DECLARED INTO KIWA. REMOVED AND REPLACED #4 WHEEL TRANSDUCER AND ANTISKID CONTROL BOX IAW B737 AMM 32-42-11 AND - [SDR I5EA2021102000004](https://openairdocs.org/sdr/I5EA2021102000004), Oct 14, 2021: PUMP. FAILED. INFLIGHT #2 ENGINE HYD. B SYSTEM LOW PRESSURE LIGHT ILLUMINATED RUN QRH AFTER A PERIOD OF TIME B SYSTEM QUANTITY DROPPED TO 0 RUN QRH. UPON INSPECTION FOUND EDP - [SDR I5EA2021080400001](https://openairdocs.org/sdr/I5EA2021080400001), Aug 4, 2021: FSEU. NO TEST. DURING CLIMB AURAL WARNING AND TAKE OFF CONFIGURATION WARNING LIGHTS CAME ON WHEN PASSING FL 310. CHECKLIST PERFORMED AND LIGHTS AND SOUND WENT OFF WHEN PASSING - [SDR I5EA2021032500009](https://openairdocs.org/sdr/I5EA2021032500009), Mar 22, 2021: PUMP. INOPERATIVE. #2 EDP NO PRESSURE AND UPON ON APPROACH B SYSTEM HYDRAULIC QUANTITY LOW. REMOPVED AND REPLACED #2 ENG EDP PER AMM 29-11-11. OPS AND LEAK CHECK ARE GOOD. - [SDR I5EA201910110905](https://openairdocs.org/sdr/I5EA201910110905), Sep 23, 2019: INDICATOR. SPLIT. TRAILING EDGE FLAP INDICATOR SPLIT BETWEEN 0 UNIT RT, 3 UNIT LH DURING THE FLIGHT UNABLE TO OPERATE TRAILING EDGE FLAP FOR LANDING. - [SDR I5EA201910100904](https://openairdocs.org/sdr/I5EA201910100904), Sep 23, 2019: INDICATOR. SPLIT. TRAILING EDGE FLAP INDICATOR SPLIT BETWEEN 0RT AND 3"LH AFTER TAKE OFF. UNABLE TO OPERATED TRAILING EDGE FLAPS HIGH ENERGY CONDITION INSPECTION. - [SDR I5EA2019072909](https://openairdocs.org/sdr/I5EA2019072909), Jul 27, 2019: PIN. RECESSED. DISCREPANCY: EMERGENCY EXIT LIGHTS STAY ON WITH SWITCH IN THE ARMED POSITION. CORRECTIVE ACTION: TROUBLE SHOT THE EMERGANCY EXIT LIGHT SYSTEM IAW FIM 33-50-00 F - [SDR I5EA20190705](https://openairdocs.org/sdr/I5EA20190705), Jul 13, 2019: POWER SUPPLY. INOPERATIVE. DISCREPANCY: RT AFT EMERGANCY EXTERNAL LIGHT INOP. CORRECTIVE ACTION: TROUBLE SHOT EMERGANCY LIGHT SYSTEM PER WDM 33-51-14 FOUND THE EXTERNAL EMERGANCY LIGHT PO - [SDR I5EA2019071104](https://openairdocs.org/sdr/I5EA2019071104), Jul 10, 2019: DOOR. OUT OF POSITION. DISCREPANCY: AFTER TAKEOFF THE LANDING GEAR FAILED TO RETRACT, PILOT RETURNED TO BASE AND CONDUCTED AN OVERWEIGHT LANDING ( LANDING WEIGHT 69.5 VREF 152+5=157). - [SDR I5EA2019052800014](https://openairdocs.org/sdr/I5EA2019052800014), May 15, 2019: BLOCK. DAMAGED. DISCREPANCY: COMPLETE EO SWA-190203S, REV: IR, DATED: 02-15-2019. CORRRECTIVE ACTION: ACCOMPLISHED L/H AFT "D" LAVATORY REPAIR COMPOSITE EXTERIOR SURFACE AND FA - [SDR I5EA2019052800015](https://openairdocs.org/sdr/I5EA2019052800015), May 15, 2019: BLOCK. DAMAGED. DISCREPANCY: COMPLETE EO SWA-190203S, REV: IR, DATED: 02-15-2019. CORRRECTIVE ACTION: ACCOMPLISHED FWD "A" LAVATORY REPAIR COMPOSITE EXTERIOR SURFACE AND FABRIC - [SDR I5EA2019052800013](https://openairdocs.org/sdr/I5EA2019052800013), May 15, 2019: BLOCK. DAMAGED. DISCREPANCY: COMPLETE EO SWA-190203S, REV: IR, DATED: 02-15-2019. CORRRECTIVE ACTION: ACCOMPLISHED RT AFT "E" LAVATORY REPAIR COMPOSITE EXTERIOR SURFACE AND FAB - [SDR I5EA2019052800031](https://openairdocs.org/sdr/I5EA2019052800031), May 15, 2019: SKIN. CRACKED. DISCREPANCY: FOUND CRACK AT FUSELAGE STA 787 BETWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT LT FUSELAGE STA 787 BETWEEN STRINGERS 8L AND - [SDR I5EA20190530](https://openairdocs.org/sdr/I5EA20190530), May 15, 2019: SKIN. CRACKED. DISCREPANCY: FOUND CRACK AT RT FUSELAGE STA: 867 BETWEEN STRINGERS 8R AND 9R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT RT FUSELAGE STA 867 BETWEEN STRINGERS 8R - [SDR I5EA2019052800029](https://openairdocs.org/sdr/I5EA2019052800029), May 15, 2019: SKIN. CRACKED. DISCREPANCY: FOUND CRACK AT LT FUSELAGE STA 500A BETWEEN 8L AND 9L. CORRECTIVE ACTIONS: ACCOMPLISHED REPAIR AT LT FUSELAGE STA 500A BETWEEN STRINGERS 8L AND 9L - [SDR I5EA2019052800028](https://openairdocs.org/sdr/I5EA2019052800028), May 15, 2019: SKIN. CRACKED. DISCREPANCY: FOUND CRACK AT LT FUSELAGE STA 727D BTWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT LT FUSELAGE STA 727D BETWEEN 8L AND 9L PE - [SDR I5EA2019052500027](https://openairdocs.org/sdr/I5EA2019052500027), May 15, 2019: SKIN. CRACKED. DISCREPANCY: FOUND DAMAGE AT RT FUSELAGE STA 727D BETWEEN STRINGERS 8R AND 9R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT RT FUSELAGE STA 727D BETWEEN STRINGERS - [SDR I5EA2019052500026](https://openairdocs.org/sdr/I5EA2019052500026), May 15, 2019: SKIN. CRACKED. DISCREPANCY: FOUND CRACK AT RT FUSELAGE STA 460 BETWEEN STRINGERS 8R AND 9R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT RT FUSELAGE STA 460 BETWEEN STRINGERS 8R - [SDR I5EA2019052400025](https://openairdocs.org/sdr/I5EA2019052400025), May 15, 2019: SKIN. CRACKED. DISCREPANCY: FOUND CRACK AT LT FUSELAGE STA 400 BETWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT LT FUSELAGE STA 400 BETWEEN STRINGERS 8L - [SDR I5EA2019052400024](https://openairdocs.org/sdr/I5EA2019052400024), May 15, 2019: SKIN. DAMAGED. DISCEPANCY: FOUND DAMAGE AT LT FUSELAGE STA 440 BETWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIRS AT LT FUSELAGE STA 440 BETWEEN STRINGERS 8L - [SDR I5EA2019052300022](https://openairdocs.org/sdr/I5EA2019052300022), May 15, 2019: SKIN. CRACKED. CRACK FOUND AT STA 500 RT BETWEEN STRINGER 8R AND 9R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT RT FUSELAGE STA. 500 BETWEEN STRINGERS 8R AND 9R PER AD 2009-01- - [SDR I5EA2019052300020](https://openairdocs.org/sdr/I5EA2019052300020), May 15, 2019: SKIN. CRACKED. DISCREPANCY: FOUND CRACK AT FUSELAGE SECTION 47 LOWER PLATING AROUND FUSELAGE STA LT 1016 BETWEEN STRINGERS 20 AND 23L. CORRECTIVE ACTION: ACCOMPLISHED CRACK RE - [SDR I5EA2019052100019](https://openairdocs.org/sdr/I5EA2019052100019), May 15, 2019: LINK. NOT REPORTED. INSTALL NEW PIVOT LINK ASSEMBLYS BS 520 TO 540 IAW AD 2015-02-26 (G) 1 AND SB 737-53-12-44 R5 GROUP 4. CORRECTIVE ACTION: ACCOMPLISHED INSTALL NEW PIVOT LINK AS - [SDR I5EA2019052100018](https://openairdocs.org/sdr/I5EA2019052100018), May 15, 2019: SKIN. CRACKED. DISCREPANCY: FOUND CRACK AT FUSELAGE STA. 867 RT BETWEEN STRINGERS 8R AND 9R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT RT FUSELAGE STA. 867 BETWEEN STRINGERS 8 - [SDR I5EA2019052100017](https://openairdocs.org/sdr/I5EA2019052100017), May 15, 2019: SKIN. CRACKED. DISCREPANCY: FOUND CRACK AT LT FUSELAGE STA. 460 BETWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT LT FUSELAGE STA 460 BETWEEN STRINGERS 8L - [SDR I5EA2019052100002](https://openairdocs.org/sdr/I5EA2019052100002), May 15, 2019: DOUBLER. NOT REPORTED. DISCREPANCY: ACCOMPLISHED DET VISUAL INSPECTION OF REPAIR ON LT HORIZONTAL STABILIZER LOWER SKIN LE STA 133.15 CORRECTIVE ACTION: ACCOMPLISHED PERMANENT EXTERNA - [SDR I5EA20190512](https://openairdocs.org/sdr/I5EA20190512), May 15, 2019: SKIN. CRACKED. DISCREPANCY: FOUND CRACK AT LT FUSELAGE STA. 500F BETWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT LT FUSELAGE STA. 500F BETWEEN STRINGERS - [SDR I5EA20190511](https://openairdocs.org/sdr/I5EA20190511), May 15, 2019: SKIN. CRACKED. DISCREPANCY: FOUND CRACK AT LT FUSELAGE STATION. 360 BETWEEN STRINGERS 8L AND 9L. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT LT FUSELAGE STATION. 360 BETWEEN STR - [SDR I5EA2019052100001](https://openairdocs.org/sdr/I5EA2019052100001), May 15, 2019: SKIN. DAMAGED. DISCREPANCY: FOUND DAMAGE AT RT FUSELAGE STA. 400 BETWEEN STRINGERS 8R AND 9R. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT RT FUSELAGE STA. 400 BETWEEN STRINGERS - [SDR I5EA2019040901](https://openairdocs.org/sdr/I5EA2019040901), Apr 5, 2019: LAMP. BURNED OUT. ROW 12 L/H SIDE EMERGANCY LIGHT INOP. REMOVED LAMP ROW 12 L/H SIDE AEREA LIGHT PER AMM 33-51-03. OPS TEST WAS GOOD. - [SDR I5EA201804060001](https://openairdocs.org/sdr/I5EA201804060001), Apr 4, 2018: BATTERY PACK. DISCHARGED. MID CABIN EMERGENCY LIGHTS M1670 INOP AT STA 727C+13. REMOVED AND REPLACED BATTERY PACK (M1670) AT STA. 727C+13, TEST GOOD IAW AMM 33-51-06. - [SDR 29EA20160523001](https://openairdocs.org/sdr/29EA20160523001), May 23, 2016: BATTERY PACK. DISCHARGED. DURING INSPECTION FOUND THE EMER EXIT LIGHT BATTERY PACK NOT TESTING PROPERLY. - [SDR 29EA20160403003](https://openairdocs.org/sdr/29EA20160403003), Mar 30, 2016: LIGHT. INOPERATIVE. L1 DOOR EMER EXIT LIGHT INOPERATIVE. R & R LAMP IAW THE AMM 33-51-04. OPERATIONS CHECKED NORMAL UNDER NR 500 038 WO SRO1857. - [SDR 29EA20160403002](https://openairdocs.org/sdr/29EA20160403002), Mar 30, 2016: LIGHT. INOPERATIVE. AFT LT WING EMER EXIT LIGHT INOPERATIVE. R & R LAMP IAW THE AMM 33-51-04. OPERATIONS CHECKED NORMAL UNDER NR 500 038 WO SR O1857. - [SDR 29EA20160403001](https://openairdocs.org/sdr/29EA20160403001), Mar 30, 2016: POWER SUPPLY. INOPERATIVE. EMERGENCY POWER SUPPLY ON RT ROW 14 INOPERATIVE. R & R POWER SUPPLY IAW THE AMM 33-51-06. OPERATIONS CHECKED NORMAL UNDER NR 500 038 WO SRO1857. - [SDR ASMF201503005](https://openairdocs.org/sdr/ASMF201503005), Jan 22, 2015: FLAP. CRACKED. DURING TRANSIT CHECK, THE LT OTBD AFTER FLAP WAS DETECTED CRACKED. PERFORMED REVISION IN THE LT FLAP DETECTING A CRACK OF 8.0” LENGTH & A PUNCTURE OF 1.0” DIAME - [SDR ASMF201501020](https://openairdocs.org/sdr/ASMF201501020), Dec 14, 2014: LIGHT. INOPERATIVE. DURING FUELING, THE LT AFT EMER EXIT LIGHT WAS DETECTED INOPERATIVE. THE FUELING WAS STOPPED & THE EMER EXIT LIGHT WAS REPLACED IAW AMM 33-50-00, TESTED CORRECT - [SDR ASMF2014061706005](https://openairdocs.org/sdr/ASMF2014061706005), Apr 14, 2014: FUEL HEATER. LEAKING. DURING RT ENG TEST RUNNING, DETECTED A FUEL LEAK AT RT ENG FUEL SERVO HEATER. THE SERVO HEATER WAS REPLACED IAW AMM 73-11-07, TESTED CORRECT. --- 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.