# Boeing 737-45D - Type: Aircraft model (FAA registry) - Registry code: 13844B9 - Manufacturer (registry): BOEING - Model: 737-45D - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-fan - Seats: 190 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/boeing-737-45d 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 None matched to aircraft with this model. ## Service difficulty reports (30) As reported by operators and repair stations, by the model named in the report. - [SDR K11A2026081300384](https://openairdocs.org/sdr/K11A2026081300384), Aug 13, 2026: ELEC CONNECTOR. INTERMITTENT. RIGHT WING BODY OVERHEAT ILLUMINATED WHILE CLIMBING THROUGH FL185 AND REMAINED ON EVEN WITH BLEED AIR OFF. LEFT WING BODY OVERHEAT ILLUMINATED WHILE TAXING IN W - [SDR K11A2026071600383](https://openairdocs.org/sdr/K11A2026071600383), Jul 16, 2026: OVERHEAT SENSOR. DIRTY. WHEEL WELL FIRE LIGHT IN FLIGHT. CLEANED WHEEL WELL OVERHEAT DETECTOR ELEMENT IAW AMM 26-17-11. PERFORMED OPERATIONAL CHECK OF WHEEL WELL OVERHEAT DETECTION ELE - [SDR K11A2026051500380](https://openairdocs.org/sdr/K11A2026051500380), May 15, 2026: DUCT. CRACKED. PROBLEM DESCRIPTION: LEFT PACK ILLUMINATED FOUR TIMES IN FLIGHT. FOLLOWED CHECK LIST UNABLE TO RESET PACK. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: TRAN - [SDR K11A2025103000358](https://openairdocs.org/sdr/K11A2025103000358), Oct 30, 2025: WINDOW. CRACKED. CRACKED L1 WINDOW IN FLIGHT. REMOVED AND REPLACED L1 WINDOW IAW AMM 56-11-11 REF AOG RO AOG4060253 AND KAIR WO 940600962. - [SDR K11A2024112700292](https://openairdocs.org/sdr/K11A2024112700292), Nov 27, 2024: SENSOR. OUT OF ADJUST. TAKE OFF CONFIG LIGHT & AURAL HORN CAME ON IN FLIGHT. ADJUSTED AIR SAFETY SENSOR & GROUND SAFETY SENSOR IAW B737 AMM 32-09-01, OPS CHECK PASSES WITH NO DEFECTS - [SDR K11A2024103000290](https://openairdocs.org/sdr/K11A2024103000290), Oct 30, 2024: MODULE. INOPERATIVE. REJECTED TAKE OFF ALPHA VANE HEATER LIGHT ILLUMINATED. R&R MASTER DIM MODULE M564 IAW AMM 20-40-12. MASTER CAUTION LIGHT SYSTEM OPS CHECKS GOOD IAW AMM 33-15-00 - [SDR K11A20240624264](https://openairdocs.org/sdr/K11A20240624264), Jun 25, 2024: SENSOR. FAILED. ENGINE #1 DID NOT ACCELERATE BEYOND 36%N1 DURING TAKEOFF ROLL. R&R T-2 SENSOR IAW B737 AMM 73-21-09, R&R CIT SENSOR IAW B737 AMM 73-21-02 PERFORMED IDLE LEAK CH - [SDR K11A202405210026](https://openairdocs.org/sdr/K11A202405210026), May 21, 2024: WARNING HORN. FALSE ACTIVATION. TAKEOFF CONFIG LIGHT ILLUMINATED, AND HORN SOUNDED DURING TAKEOFF ROLL. ALL TAKEOFF CONFIGURATIONS WERE IN THE PROPER POSITIONS AND WARNING DID NOT ACTIVATE DUR - [SDR I5EA2024010500005](https://openairdocs.org/sdr/I5EA2024010500005), Jan 5, 2024: POWER SUPPLY. NO TEST. BATTERY PACK AT M1576 WILL NOT HOLD CHARGE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY M1576 AT STA. 727+11 IAW B737-400 AMM 33-51-51. OPS CHECK GOOD. - [SDR I5EA2024010500004](https://openairdocs.org/sdr/I5EA2024010500004), Jan 5, 2024: POWER SUPPLY. NO TEST. L/H AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY M1134 AT STA. 628 IAW B737-400 AMM 33-51-51. OPS CHECK GOOD. - [SDR I5EA2024010500003](https://openairdocs.org/sdr/I5EA2024010500003), Jan 5, 2024: POWER SUPPLY. NO TEST. R/H FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY M1468 AT STA. 500C10 IAW B737-400 AMM 33-51-51. OPS CHECK GOOD. - [SDR I5EA2024010400002](https://openairdocs.org/sdr/I5EA2024010400002), Jan 4, 2024: POWER SUPPLY. NO TEST. POWER SUPPLY M1479 REQUIRES REPLACEMENT. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY M1479 AT STA. 598 IAW B737-400 AMM 33-51-51. TEST GOOD. - [SDR I5EA2024010400001](https://openairdocs.org/sdr/I5EA2024010400001), Jan 4, 2024: BATTERY PACK. NO TEST. MID AISLE EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1479 AT STA. 598 IAW B737-400 AMM 33-51-51. TEST GOOD. - [SDR I5EA2023091500005](https://openairdocs.org/sdr/I5EA2023091500005), Sep 15, 2023: BATTERY PACK. NO TEST. EMERGENCY LIGHT FOR AISLE AT STA 704R INOP. REMOVE AND REPLACE BATTERY PACK AT M1435 STA 747R IAW B737-400 AMM 33-51-51. OPS CHECK GOOD. - [SDR I5EA2023091500004](https://openairdocs.org/sdr/I5EA2023091500004), Sep 14, 2023: BATTERY PACK. DISCHARGED. EMERGENCY LIGHT AISLE LIGHT AT STA. 339R INOP. REMOVED AND REPLACED BATTERY PACK M1132 STA. 330R IAW B737-400 AMM 33-51-51 - [SDR MASA2023071900094](https://openairdocs.org/sdr/MASA2023071900094), Jul 20, 2023: UNKNOWN. UNKNOWN. CABIN ALTITUDE WARNING - [SDR I5EA2021073000005](https://openairdocs.org/sdr/I5EA2021073000005), Jul 28, 2021: CHARGER. INOPERATIVE. BATTERY CHARGER INOP AT LOCATION M1479 STA 598 RBL39. REMOVE AND REPLACE BATTERY CHARGER AT M1479 AT STA 598 AND TEST IAW B737-400 AMM 33-51-51, TEST OK - [SDR I5EA2021073000004](https://openairdocs.org/sdr/I5EA2021073000004), Jul 28, 2021: BATTERY PACK. DISCHARGED. RIGHT HAND OVERWING EMERGANCY LIGHT INOP. REMOVE AND REPLACE EMERGENCY LIGHT BATTERY M1479 AT STA 598, AND TEST IAW B737-400 AMM 33-51-51, TESTS OK - [SDR I5EA2021073000003](https://openairdocs.org/sdr/I5EA2021073000003), Jul 28, 2021: BATTERY PACK. DISCHARGED. LEFT HAND OVERWING EMERGENCY LIGHT INOP. REMOVE AND REPLACE EMERGENCY LIGHT BATTERY M1134 AT STA 628AND TEST IAW B737-400 AMM 33-51-51, TESTS OK - [SDR I5EA2021050300001](https://openairdocs.org/sdr/I5EA2021050300001), May 2, 2021: CHARGER. INOPERATIVE. LEFT OVER WING EXIT IDENTIFIER INOP. REMOVED AND REPLACED POWER SUPPLY (BATTERY CHARGER) M1468 AT STA 500C +10 WIH SERVICEABLE UNIT AND TEST IAW B737-400 AMM 33 - [SDR MASA20210407157](https://openairdocs.org/sdr/MASA20210407157), Mar 30, 2021: FRAME. DAMAGED. FORWARD CARGO COMPARTMENT, REINFORCEMENT FRAMES INSTALLED PER IAI CARGO CONVERSION STA 400+9.000” AND STA 400+13.500” WITH DOUBLE HOLES (2EA). THE FRAMES WERE R - [SDR MASA20210407158](https://openairdocs.org/sdr/MASA20210407158), Mar 21, 2021: ACOUSTIC PANEL. CORRODED. ENGINE #2, INLET COWL RH LWR ACOUSTIC PANEL WITH BULKHEAD BETWEEN 6 AND 7 O’CLOCK POSITION. NOTE: THE AREA WERE REPAIRED PER STS EA 72-2021-007 REV IR(REFE:JOB - [SDR I5EA2021031500008](https://openairdocs.org/sdr/I5EA2021031500008), Mar 14, 2021: BATTERY PACK. DISCHARGED. RH INTERIOR AND EXTERIOR EMERGENCY EXIT LIGHTS INOP AT R1. REMOVED AND REPLACED BATTERY PACK AT M1132, STA 330R. IAW B737-400 AMM 33-51-51 - [SDR I5EA2021031500007](https://openairdocs.org/sdr/I5EA2021031500007), Mar 14, 2021: BATTERY PACK. DISCHARGED. LH INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP AT OVER WING EXIT. REMOVED AND REPLACED BATTERY PACL AT M1576, STA 727B, STR 1L, IAW B737-400 AMM33-51-51 - [SDR EE4Y201910119892](https://openairdocs.org/sdr/EE4Y201910119892), Oct 11, 2019: FRAME. DAMAGED. UPPER CARGO CABIN AT BS 907 STR 17R LEVEL FRAME NOTCH WITH HOLE ENLONGATE.WAS REPAIRED PER AERONAUTICAL ENGINEERS EO9670 REV P2,REPAIR INSTRUCTIONS (REF:JOB:A1H - [SDR EE4Y201910119891](https://openairdocs.org/sdr/EE4Y201910119891), Oct 11, 2019: SKIN. DAMAGED. FUSELAGE SKIN FROM BS500F+10 TO BS540, BETWEEN S-16LH AND S-19LH WING TO BODY FAIRING AREA, EXTERNAL SURFACE WITH EXISTING BLENDOUT.WAS REPAIRED PER AERONAUTICA - [SDR EE4Y201910029890](https://openairdocs.org/sdr/EE4Y201910029890), Oct 2, 2019: STRINGER. DAMAGED. FWD CARGO COMPARTMENT AT STA 440 STRINGER 21LH WITH DOUBLE HOLE. HE STRINGER WAS REPAIRED PER EO9640 REPAIR INSTRUCTIONS. - [SDR EE4Y201910019889](https://openairdocs.org/sdr/EE4Y201910019889), Oct 1, 2019: SKIN. PUNCTURED. RIGHT ELEVATOR TOP SKIN SURFACE PUNCTURED AT ELEV. STA 30.5. THE ELEVATOR SKIN WAS REPAIRED IAW SERVICE REQUEST ID: 4-4567857880 AND MANUFACTURER REPAIR INSTRUC - [SDR EE4Y201910019887](https://openairdocs.org/sdr/EE4Y201910019887), Oct 1, 2019: SUPPORT FITTING. CRACKED. RH WING RSS 224.14 REAR SPAR UPPER CHORD, MLG SUPPORT BEAM - AFT SUPPORT FITTING OPEN FASTENER HOLE WITH CRACK. NOTE: THE AFT SUPPORT FITTING WAS REPAIRED PER S - [SDR EE4Y2019100109886](https://openairdocs.org/sdr/EE4Y2019100109886), Oct 1, 2019: SPAR. CRACKED. RH WING RSS 224.14 REAR SPAR UPPER CHORD OPEN FASTENER HOLE CRACKED. NOTE: REAR SPAR UPPER CHORD WAS REPAIRED AS PER SRM 57-20-10 REPAIR 4 INSTRUCTIONS. --- 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.