# Boeing 737-8AS - Type: Aircraft model (FAA registry) - Registry code: 13844DI - Manufacturer (registry): BOEING - Model: 737-8AS - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 ยท Turbo-fan - Seats: 149 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 5 - Page: https://openairdocs.org/model/boeing-737-8as 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 (5) - [N6516U](https://openairdocs.org/aircraft/N6516U): [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), S/N 33814 - [N8093A](https://openairdocs.org/aircraft/N8093A): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), S/N 29938 - [N8111A](https://openairdocs.org/aircraft/N8111A): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2002, S/N 33544 - [N916BR](https://openairdocs.org/aircraft/N916BR): [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 1999, S/N 29916 - [N9242Y](https://openairdocs.org/aircraft/N9242Y): [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 29931 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (16) As reported by operators and repair stations, by the model named in the report. - [SDR 3CEY2026100200001](https://openairdocs.org/sdr/3CEY2026100200001), Sep 29, 2026: MANIFOLD. CHAFED. DURING THE INCOMING INSPECTION THE FOLLOWING FINDINGS WERE OBSERVED FUEL MANIFOLD TUBE CHAFED WITH HOLE AT 11 O'CLOCK POSITION AFT LOOKING FORWARD, WEAR TO THE - [SDR SCNA20260818366](https://openairdocs.org/sdr/SCNA20260818366), Aug 17, 2026: BATTERY. NO DISCREPANCY. EMERGENCY LIGHTS LOW BATTERY. VERIFIED ACFT BATTERY POWER IS WITHIN NORMAL OPERATING LIMITS AND WAITED 90 MINUTES FOR CHARGE IAW AMM 33-51-06, AND AMM 33-51-00. - [SDR SCNA20260702275](https://openairdocs.org/sdr/SCNA20260702275), Jul 1, 2026: DETECTION SYS. NO TEST. MAIN DECK CARGO FIRE SYSTEM TEST WILL NOT PASS. PERFORMED MAIN SYS CHECK OF CARGO FIRE REF FIM 26-23 TASK 805. NO DEFECTS NOTED. - [SDR SCNA20260522210](https://openairdocs.org/sdr/SCNA20260522210), May 22, 2026: ATTACH FITTING. CORRODED. MAIN CABIN L1 DOOR FWD GIRT BAR ATTACHMENT FITTINGS HOLES HAVE CORROSION. - [SDR K11A2024113000293](https://openairdocs.org/sdr/K11A2024113000293), Nov 30, 2024: SWITCH. OUT OF POSITION. MAIN CARGO DOOR LIGHT ILLUMINATED PASSING FL 33 EXTINGUISHED PASSING 9500 FT AND REMAINED OFF FOR THE DURATION OF THE FLIGHT. ADJUSTED FWD DOOR CLOSED SWITCH IA - [SDR K11A2024092400287](https://openairdocs.org/sdr/K11A2024092400287), Sep 24, 2024: FUEL FILTER. FAULTED. ON CLIMB OUT THE #1 ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED THEN WENT OUT CONTINUED TO CLIMB AND LIGHT ILLUMINATED AGAIN. REMOVED AND REPLACED #1 ENGINE FUE - [SDR K11A2024071800270](https://openairdocs.org/sdr/K11A2024071800270), Jul 18, 2024: INDICATOR. FAULTED. ON TAKEOFF CAPT. AIRSPEED READ 45 WHEN FO CALLED 80 KTS. THEN CAPT. AIRSPEED JUMPED TO 85 KTS. THE AUTO THROTTLES DISCONNECTED AT 85 KTS FO TRIED TO RECONNECT T - [SDR I5EA2023051100001](https://openairdocs.org/sdr/I5EA2023051100001), May 7, 2023: UNKNOWN. UNKNOWN. CABIN ALT LIGHT ILLUMINATED AT FL390, PRESS CONTROLLER IN ALT MODE PER MEL 21-14-03, CABIN CONTINUED TO CLIMB TO 10,000, CONTINUED TO 11,000 CABIN CONTROLLER IN - [SDR TX9220201228001](https://openairdocs.org/sdr/TX9220201228001), Dec 28, 2020: SKIN. CORRODED. DURING THE CONVERSION OF 737-800 PASSENGER AIRPLANE TO THE FREIGHTER TO DATUM AIRPLANE N239GE(MSN33717), TERRIBLE CORROSION DAMAGE WERE FOUND AT FUSELAGE SKIN A - [SDR CA150106002](https://openairdocs.org/sdr/CA150106002), Dec 31, 2014: SHAFT. SHEARED. (CAN) CREW NOTICED ENGINE NUMBER TWO N1 WAS 87.7% AND ENGINE NUMBER ONE N1 WAS 95% DURING TAKEOFF ROLL. AIRCRAFT WAS UNABLE TO CREATE ENOUGH POWER ON NR 2 FOR C - [SDR CA140924005](https://openairdocs.org/sdr/CA140924005), Sep 19, 2014: TIE BOLT. BROKEN. (CAN) AFTER A REMOVAL WHERE THE TIRE WAS NOTED TO BE DEFLATED, A WHEEL AND TIRE ASSY WAS SENT TO SHOP FOR INSPECTION. THE WHEEL WAS FOUND TO HAVE 5 TIE BOLTS, P - [SDR CA140818003](https://openairdocs.org/sdr/CA140818003), Aug 12, 2014: WIRE. CHAFED. (CAN) ON DEPARTURE, FORWARD PANEL INDICATION LIGHTS BEGAN TO FLICKER THEN ALL STAYED ON PERMANENTLY. LIGHTS INCLUDED ANTI SKID INOP, LE FLAP TRANSIT/EXT, AUTOBR - [SDR CA130204011](https://openairdocs.org/sdr/CA130204011), Feb 1, 2013: CONNECTOR. BURNED. (CAN) TROUBLESHOOTING WAS BEING CONDUCTED ON THE SUBJECT ACFT DUE TO A DEFECT ON AN IFE DISPLAY. DURING TROUBLESHOOTING, THE J1 CONNECTOR AT LRU50-110 OF THE SV - [SDR CA121220003](https://openairdocs.org/sdr/CA121220003), Dec 18, 2012: ARM. SHEARED. (CAN) DURING THE CREW`S PREFLIGHT CHECKS, IT WAS DISCOVERED THAT THE L1 FORWARD CABIN DOOR GUIDE ARM ROD END WAS SHEARED OFF. THE ACFT WAS TAKEN OUT OF SERVICE - [SDR CA130114003](https://openairdocs.org/sdr/CA130114003), Nov 28, 2012: RIB. WORN. (CAN) THE RT DEFLECTION CONTROL RIB AT T/E WING STA 278, WHERE THE TURNBUCKLE ATTACHES TO THE RIB WAS FOUND WORN AND TORN OPEN. - [SDR CA120502002](https://openairdocs.org/sdr/CA120502002), Apr 28, 2012: WIRE. BROKEN. (CAN) REF CADORS REPORT NR: 2012O1034. FROM CREW INCIDENT/SAFETY REPORT: - "ON SELECTION OF FLAP 1, FLAP INDICATORS STOPPED PRIOR TO REACHING FLAP 1 AMBER FLAP --- 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.