# N8676A: 2015 Boeing 737-8H4 - Status: Valid registration - Airframe: [Boeing 737-8H4](https://openairdocs.org/model/boeing-737-8h4) (registry code 138440A, 143 seats) - Engine: [CFM International CFM56-7B27E series](https://openairdocs.org/engine/cfm-international-cfm56-7b27e-series) (registry code 13078) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs) - Serial number: 36941 - Year built: 2015 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 14, 2015 - Certificate issued: December 31, 2024 - Expires: December 31, 2031 - Mode S code: ABEC03 - Registered owner: [Umb Bank Na Trustee](https://openairdocs.org/faa-owner/UMB%20BANK%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.6171° N, 111.6866° W: Placed by OpenAirDocs at the center of ZIP code 84121, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8676A - Page: https://openairdocs.org/aircraft/N8676A From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every CFM International CFM56-7B27E model are included. ## ADs that may apply (OpenAirDocs): 6 in force ### Matched by airframe (Boeing 737-8H4) None in force. ### Matched by engine (CFM International CFM56-7B27E series) - [AD 2023-05-05](https://openairdocs.org/ad/2023-05-05): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 98 more. Effective May 10, 2023 - [AD 2018-26-01](https://openairdocs.org/ad/2018-26-01): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jan 10, 2019 - [AD 2018-09-51](https://openairdocs.org/ad/2018-09-51): Engine · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 7, 2018 - [AD 2015-18-04](https://openairdocs.org/ad/2015-18-04): 73-tooth gearshaft located in the engine accessory gearbox (AGB) · CFM International CFM56-3, CFM56-7B20, CFM56-7B20/2 and 47 more. Effective Oct 20, 2015 - [AD 2015-04-02](https://openairdocs.org/ad/2015-04-02): Dual engine thrust instability event · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Mar 31, 2015 - [AD 2009-11-02](https://openairdocs.org/ad/2009-11-02): HPC 4-9 spools · CFM International CFM56-2, CFM56-2A, CFM56-2B and 109 more. Effective Jun 23, 2009 ### Historical (superseded or no longer in force) - [AD 2021-10-09](https://openairdocs.org/ad/2021-10-09) (historical): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 82 more. Effective Jun 24, 2021 - [AD 2018-18-01](https://openairdocs.org/ad/2018-18-01) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Oct 16, 2018 - [AD 2018-10-11](https://openairdocs.org/ad/2018-10-11) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 1, 2018 - [AD 2018-09-10](https://openairdocs.org/ad/2018-09-10) (historical): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective May 14, 2018 - [AD 2013-26-01](https://openairdocs.org/ad/2013-26-01) (historical): Oil dynamic seal assembly · CFM International CFM56-3, CFM56-3B, CFM56-3C and 52 more. Effective Feb 3, 2014 ## Information bulletins (advisory) (1 in force) - [SAIB NE-08-17R3](https://openairdocs.org/saib/NE-08-17R3): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued May 28, 2014 - [SAIB NE-08-17R2](https://openairdocs.org/saib/NE-08-17R2) (historical): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued Mar 7, 2011 ## NTSB investigations None matched to N8676A. ## FAA accident and incident reports None matched to N8676A. ## Service difficulty reports (230, newest 50) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWAA2026082401590](https://openairdocs.org/sdr/SWAA2026082401590), Aug 19, 2026: WIRE. DETACHED. L1 DOOR OUTSIDE EMERGENCY LIGHT INOPERATIVE. FOUND WIRE W3142-0151-16 REMOVED FROM GROUND BLOCK GD3876. RE-PINNED WIRE TO GROUND BLOCK AND OPS CHECK OF EMERGENC - [SDR SWAA2026082475413](https://openairdocs.org/sdr/SWAA2026082475413), Aug 12, 2026: HANDLE. LOOSE. ASSIST HANDLE ON G1 GALLEY LOOSE. SECURED ASSIST HANDLE ON G1 GALLEY IAW AMM 25-31-11-400-801 SUBTASK 25-31-11-410-016. - [SDR SWAA2026082411258](https://openairdocs.org/sdr/SWAA2026082411258), Aug 11, 2026: LENS. DAMAGED. FORWARD L1 DOOR EXIT LENS REQUIRES REPLACEMENT. REMOVED AND REPLACED THE FWD L1 DOOR EXIT LIGHT LENS IAW AMM 33-51-01-960-801. - [SDR SWAA2026082469658](https://openairdocs.org/sdr/SWAA2026082469658), Aug 11, 2026: LAMP. INOPERATIVE. L1 DOOR EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. REPLACED THE LAMPS, OPS CHECKED L1 DOOR EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-04-960-801. OPS CHECKED GOOD. - [SDR SWAA2026082446338](https://openairdocs.org/sdr/SWAA2026082446338), Aug 11, 2026: SKIN. DELAMINATED. FOUND LEFT OTBD AFT FLAP DELAMINATED. REMOVED AND REPLACED LT OTBD AFT FLAP IAW AMM 27-51-22-401. - [SDR SWAA2026082456139](https://openairdocs.org/sdr/SWAA2026082456139), Aug 11, 2026: SKIN. DELAMINATED. FOUND RT OTBD AFT FLAP DELAMINATED. REMOVED AND REPLACED RT OTBD AFT FLAP IAW AMM 27-51-22. - [SDR SWAA2026082495892](https://openairdocs.org/sdr/SWAA2026082495892), Aug 11, 2026: HANDLE. UNSECURE. L2 DOOR AIRFRAME SIDE ASSIST HANDLE NEEDS SECURED SECURED ASSIST HANDLE ON AIRFRAME SIDE AT L2 DOOR IAW AMM 25-21-25-420-801 SUBTASK 25-21-25-420-004 SECURED AS - [SDR SWAA2026082475326](https://openairdocs.org/sdr/SWAA2026082475326), Aug 11, 2026: HANDLE. UNSECURE. R2 DOOR AIRFRAME SIDE ASSIST HANDLE NEEDS SECURED. SECURED ASSIST HANDLE AT R2 DOOR AIRFRAME SIDE IAW AMM 25-21-25-420-801. - [SDR SWAA2026082440515](https://openairdocs.org/sdr/SWAA2026082440515), Aug 11, 2026: LAMP. INOPERATIVE. L2 EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. REPLACED THE LAMPS, OP CHECKED L2 DOOR EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-04-960-801. EMERGENCY LIGHT. OPS CHECK - [SDR SWAA2026082415394](https://openairdocs.org/sdr/SWAA2026082415394), Aug 11, 2026: HANDLE. UNSECURE. L1 DOOR ASSIST HANDLE NEEDS SECURED. SECURED ASSIST HANDLE AT L1 DOOR IAW AMM 52-11-31-400-802 SUBTASK 52-11-31-020-011. - [SDR SWAA2026010859154](https://openairdocs.org/sdr/SWAA2026010859154), Jan 7, 2026: RELAY. FAILED. ELECTRIC STAB TRIM FAIL DURING CLIMB OUT, AUTOPILOT WAS NOT ENGAGED. NEITHER CAP OR FO ELECTRIC STAB TRIM WAS OPERATIONAL. MANUAL TRIM OPERATED NORMALLY. R & R - [SDR SWAA2025122254054](https://openairdocs.org/sdr/SWAA2025122254054), Dec 19, 2025: COVER. LOOSE. FWD SERVICE DOOR EXIT COVER (LOWER) CAME OFF. SECURED FWD SERVICE DOOR EXIT COVER IAW MM 33-51-01 - [SDR SWAA2025121552653](https://openairdocs.org/sdr/SWAA2025121552653), Dec 13, 2025: TRIM MOTOR. INOPERATIVE. CREW REPORTS STAB TRIM INOPERATIVE, WORKS WITH AUTOPILOT. R & R STABILIZER TRIM MOTOR IAW AMM 27-41-71. TESTED GOOD IAW AMM 27-41-71-700-801. - [SDR SWAA2025103030124](https://openairdocs.org/sdr/SWAA2025103030124), Oct 30, 2025: BULB. INOPERATIVE. EXTERIOR EMERGENCY LIGHT, AFT OF L2 DOOR NO ILLUMINATION DURING EMERGENCY LIGHT OPS CHK. PLACED THE BULB IAW MM 33-51-00. - [SDR SWAA2025091614417](https://openairdocs.org/sdr/SWAA2025091614417), Sep 14, 2025: BATTERY. INOPERATIVE. LH EMERGENCY. EXIT LIGHTS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY AT LT 12CBA POSITION. - [SDR SWAA2025062384569](https://openairdocs.org/sdr/SWAA2025062384569), Jun 23, 2025: SENSOR. FAULTY. LE FLAP TRANSIT LIGHT CAME ON WHEN FLAPS 15 SELECTED AND STAYED ON <[01]. R&R #4 LEADING EDGE FLAP PROXIMITY SENSOR REF AMM 27-88-11. OPS CHECK GOOD. - [SDR SWAA2024122379900](https://openairdocs.org/sdr/SWAA2024122379900), Dec 20, 2024: LIGHT. INOPERATIVE. FORWARD ENTRY DOOR SLIDE EMERGENCY LIGHT INOP<[01] RE LAMPED FORWARD ENTRY DOOR SLIDE EMERGENCY LIGHT;OPS CHECKS GOOD PER MM 33-51-04;[02] RE LAMPED FORWARD ENT - [SDR SWAA2024122379541](https://openairdocs.org/sdr/SWAA2024122379541), Dec 19, 2024: MEGAPHONE. BROKEN. FORWARD CABIN MEGAPHONE HANDLE IS BROKEN AWAY FROM HORN.<[01] REPLACED FWD CABIN MEGAPHONE IN REFERENCE TO AMM 25-64-00.;[02] ROBERT WALESA (TECHNICIAN); 19-DEC - [SDR SWAA2024122378971](https://openairdocs.org/sdr/SWAA2024122378971), Dec 18, 2024: BATTERY PACK. INOPERATIVE. RIGHT OVER WING EXIT EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED RIGHT OVER WING EMERGENCY LIGHT BATTERY PACK;ROW 13R PER MM 33-51-06. OPS CHECKS GOOD PER M - [SDR SWAA2024122375283](https://openairdocs.org/sdr/SWAA2024122375283), Dec 9, 2024: CHANNEL. CRACKED. FLOORBOARD SUPPORT CHANNEL CRACKED AT I/B ATTACH POINT AT APPROXIMATELY STA. 540 BETWEEN FLOOR BEAM AT LBL 0.07 TO SEAT TRACK FLOOR BEAM AT RBL 24.82.<[01] REMO - [SDR SWAA2024122375284](https://openairdocs.org/sdr/SWAA2024122375284), Dec 9, 2024: CHANNEL. CRACKED. FLOORBOARD SUPPORT CHANNEL CRACKED AT I/B ATTACH POINT AT APPROXIMATELY STA. 540 BETWEEN FLOOR BEAM AT LBL 0.07 TO SEAT TRACK FLOOR BEAM AT LBL 24.82.<[01] REMO - [SDR SWAA2024122374443](https://openairdocs.org/sdr/SWAA2024122374443), Dec 5, 2024: MOUNT BRACKET. CRACKED. PANEL 551FB HAS A CRACKED MOUNTING ANGLE. REMOVED AND REPLACED MOUNTING BRACKET PER SRM 51-40-02. INSPECTED WORK PERFORMED. REMOVED AND REPLACED MOUNTING BRACKE - [SDR SWAA2024122374124](https://openairdocs.org/sdr/SWAA2024122374124), Dec 5, 2024: BRACKET. CRACKED. PANEL 414 FAN COWL ASSY. #1 ENGINE INBOARD: OIL DOOR WIND DEFLECTOR BRACKET IS CRACKED. MARKED. PANEL 414 FAN COWL ASSY. #1 ENGINE INBOARD: OIL DOOR WIND DEFLEC - [SDR SWAA2024122374442](https://openairdocs.org/sdr/SWAA2024122374442), Dec 5, 2024: ATTACH BRACKET. CRACKED. DEFLECTION RIB ATTACH BRACKET IS CRACKED<[01] REMOVED DAMAGED BRACKET PER SRM 51-40-02.;[02] REMOVED AND REPLACED DEFLECTION RIB ATTACH CLIP PER SRM 51-40-02.;[ - [SDR SWAA2024122073800](https://openairdocs.org/sdr/SWAA2024122073800), Dec 3, 2024: FLOOR PANEL. DELAMINATED. CENTER CABIN FLOOR PANEL 241 GF DELAMINATED<[01] REMOVED AND REPLACED WITH NEW SERVICEABLE FLOOR PANEL IAW AMM 53-21-00.;[02] C/W INSPECTION - [SDR SWAA2024122073801](https://openairdocs.org/sdr/SWAA2024122073801), Dec 3, 2024: FLOOR PANEL. DELAMINATED. CENTER CABIN FLOOR PANEL 241 KF DELAMINATED<[01] REMOVED AND REPLACED WITH NEW SERVICEABLE FLOOR PANEL 241KF PER AMM 53-21-00.;[02] COMPLIED WITH CORRECTIVE ACT - [SDR SWAA2024122073802](https://openairdocs.org/sdr/SWAA2024122073802), Dec 3, 2024: FLOOR PANEL. DELAMINATED. CENTER CABIN FLOOR PANEL 241 RF DELAMINATED<[01] REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00-400-801.;[02] COMPLIED WITH CORRECTIVE ACTION#1. - [SDR SWAA2024122373310](https://openairdocs.org/sdr/SWAA2024122373310), Dec 2, 2024: ATTACH ANGLE. CRACKED. RW TE COVE; FIRST RIB INBOARD OF THE DEFLECTION CONTROL RIB (ORSS 275); UPPER INBOARD SIDE OF THE RIB ATTACH ANGLE IS CRACKED RW TE COVE FIRST RIB INBOARD OF TH - [SDR SWAA2024122373311](https://openairdocs.org/sdr/SWAA2024122373311), Dec 2, 2024: ATTACH ANGLE. CRACKED. RW DEFLECTION CONTROL RIB; INBOARD AFT ATTACH ANGLE CRACKED RW DEFLECTION CONTROL RIB INBOARD AFT ATTACH ANGLE CRACKED<[01] REMOVED AND REPLACED INBOARD AFT ATT - [SDR SWAA2024122373308](https://openairdocs.org/sdr/SWAA2024122373308), Dec 2, 2024: ANGLE. CRACKED. L/H WING DEFLECTION RIB; UPPER PANEL; CENTER COVE RIB ANGLE CRACKED(BACKSIDE).<[01] REMOVED CRACKED ANGLE PER SRM 51-40-02.;[02] REMOVED AND REPLACED INBD.DEFLE - [SDR SWAA2024122372990](https://openairdocs.org/sdr/SWAA2024122372990), Nov 30, 2024: FLOOR PANEL. CRACKED. PANEL 661BB HAS SEVERAL FASTENER HOLES DAMAGED ; PULLED SURFACE & CRACKING.<[01] FILLED DAMAGED HOLES; APPLIED PRE-PREG REPAIR PLIES AND COOKED REPAIR PER SRM 5 - [SDR SWAA2024122372730](https://openairdocs.org/sdr/SWAA2024122372730), Nov 30, 2024: ATTACH ANGLE. CRACKED. L/H A/C BAY AFT WALL STA 663 AND APPROX. LBL 8 VAPOR BARRIER ATTACH ANGLE IS CRACKED AT RIVET HOLE IN VERTICAL FLANGE.<[01] CUT AND REMOVED DAMAGED SECTION OF A - [SDR SWAA2024122372727](https://openairdocs.org/sdr/SWAA2024122372727), Nov 30, 2024: ATTACH ANGLE. CRACKED. R/H A/C BAY AFT WALL STA 663 AND APPROX. RBL 8 VAPOR BARRIER ATTACH ANGLE IS CRACKED AT RIVET HOLE IN VERTICAL FLANGE.<[01] CUT AND REMOVED DAMAGED SECTION OF A - [SDR SWAA2024021551810](https://openairdocs.org/sdr/SWAA2024021551810), Feb 13, 2024: BATTERY PACK. INOPERATIVE. CEILING EMRGCY LTS INOP @ ROW 18;21 DEF<[01] R/R EMRGCY LT BATT PACK @ ROW 20 DEF PER AMM 33-51-06. LIGHT OPS - OK. - [SDR SWAA2023122732899](https://openairdocs.org/sdr/SWAA2023122732899), Dec 17, 2023: BATTERY PACK. INOPERATIVE. AFT GALLEY R/H EMERGENCY LIGHT BATTERY PACK INOP<[01] REMOVED AND REPLACED EMAERGENCY LIGHT BATTERY PACK AT STA 952R PER MM 33-51-06;[02] AFT GALLEY EMERGENCY L - [SDR SWAA2023122732985](https://openairdocs.org/sdr/SWAA2023122732985), Dec 17, 2023: BATTERY PACK. INOPERATIVE. FWD CABIN EMERGENCY LIGHTS BATTERY PACK AT STA 565L IS INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT STA 565L PER MM 33-51-06.EMERGENCY LIGHTS - [SDR SWAA2023122732986](https://openairdocs.org/sdr/SWAA2023122732986), Dec 17, 2023: BATTERY PACK. INOPERATIVE. FWD CABIN EMERGENCY LIGHT BATTERY PACK AT STA 565R IS INOP<[01] REMOVED AND REPLACE EMERGENCY LIGHT BATTERY PACK AT STA 565R PER MM 33-51-06.EMERGENCY LIGHTS OP - [SDR SWAA2023122831574](https://openairdocs.org/sdr/SWAA2023122831574), Dec 14, 2023: TRACK. CRACKED. R/H HORIZONTAL STAB UPPER AFT BLADE SEAL FWD TRACK IS CRACKED.<[01] INSTALLED R/H HORIZONTAL STAB UPPER AFT BLADE SEAL FWD TRACK PER SRM 51-40-02;[02] VERIFIED - [SDR SWAA2023122833189](https://openairdocs.org/sdr/SWAA2023122833189), Dec 7, 2023: STRINGER. INCORRECT. BS 727 INNER CHORD AT STRINGER 18A LEFT SIDE GAP IS 0.018'<[01] REPAIRED PER EO-5311-E-14577-NG.;[02] REPAIRED PER EO-5311-E-14577-NG ON FAULT #TTG8Q00Q4Y4H.;[0 - [SDR SWAA2023122833290](https://openairdocs.org/sdr/SWAA2023122833290), Dec 7, 2023: STRINGER. INCORRECT. BS 727 INNER CHORD AT STRINGER 18A RIGHT SIDE GAP IS 0.045' AT THE UPPER AND 0.040' AT THE BOTTOM<[01] REPAIRED PER EO-5311-E-14625-NG ON FAULT #TTG8Q00Q4Z2Z.;[ - [SDR SWAA2023122828959](https://openairdocs.org/sdr/SWAA2023122828959), Dec 7, 2023: ANGLE. CORRODED. FWD CARGO RH TRANSITION ANGLE HAS CORROSION FROM STA. 500E TO 500F.<[01] BLENDED AREAS; REMOVED .010' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. - [SDR SWAA2023122828480](https://openairdocs.org/sdr/SWAA2023122828480), Dec 6, 2023: NUT. INOPERATIVE. FORWARD ENTRY DOOR ESCAPE SLIDE FORWARD MOUNT BARREL NUT BAD.<[01] REPLACED BARREL NUT PER SOPM 20-50-01.;[02] C/W INSPECTION. - [SDR SWAA2023122828481](https://openairdocs.org/sdr/SWAA2023122828481), Dec 6, 2023: FASTENER. LOOSE. FORWARD ENTRY DOOR ESCAPE SLIDE RIGHT HAND GIRT BAR BRACKET LOOSE.<[01] R/R FASTENER IAW SRM 51-40-02.;[02] C/W INSPECTION. - [SDR SWAA2023122728495](https://openairdocs.org/sdr/SWAA2023122728495), Dec 6, 2023: PLATE. LOOSE. AFT SERVICE DOOR INTERNAL HANDLE CAMPLATE LOOSE.<[01] SECURED CAMPLATE PER M/M REF 52-41-11;[02] C/W INSPECTION. - [SDR SWAA2023122827970](https://openairdocs.org/sdr/SWAA2023122827970), Dec 5, 2023: FLOOR PANEL. DELAMINATED. FOLLOWING FWD WET AREA FLOOR BOARDS HAVE DENTS/DELAMINATION; 231CF; 231BF; 231AF; 222DF; 222CF; 221GF; 221FF; 221EF; 221CF; AND 221DF.<[01] REPLACED FLOOR PANEL - [SDR SWAA2023122827972](https://openairdocs.org/sdr/SWAA2023122827972), Dec 5, 2023: FLOOR PANEL. DELAMINATED. 221BF AND 221AF FWD WET AREA FLOOR BOARDS HAVE DENTS/DELAMINATION.<[01] NEW FLOOR PANEL 221BF INSTALLED ON TTG8Q00P6GMR
NEW FLOOR PANEL 221AF INSTALLED ON TT - [SDR SWAA2023122827679](https://openairdocs.org/sdr/SWAA2023122827679), Dec 5, 2023: LINER. TORN. FWD SERVICE DOOR (R-1) LINER TEDLAR COVERING TORN IN 2 AREAS. (SLIDE MOUNT FASTENER AND HANDLE AREAS MARKED)<[01] REMOVED AND REPLACED LINER PER M/M REF 52-41-3 - [SDR SWAA2024010227240](https://openairdocs.org/sdr/SWAA2024010227240), Dec 4, 2023: ANGLE. CORRODED. AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLE STA 727G+6 LBL 21 WL 156. MRKD<[01] REPAIR ACCOMPLISHED ON CARD TTG8Q00Q22QW. - [SDR SWAA2024010227232](https://openairdocs.org/sdr/SWAA2024010227232), Dec 4, 2023: ANGLE. CORRODED. AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLE STA 727G+9 LBL 21 WL 156. MRKD<[01] REPAIR ACCOMPLISHED ON CARD TTG8Q00Q22QW. - [SDR SWAA2024010227233](https://openairdocs.org/sdr/SWAA2024010227233), Dec 4, 2023: ANGLE. CORRODED. AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLE STA 727G+13 LBL 21 WL 156. MRKD<[01] REPAIR ACCOMPLISHED ON CARD TTG8Q00Q22QW. All 230: https://openairdocs.org/aircraft/N8676A/reports.md ## STCs that may be installed (OpenAirDocs) (31) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Boeing 737-8H4) - [STC ST00555AT](https://openairdocs.org/stc/ST00555AT): Installation of Airshow 210 system. AIRCRAFT RECONFIG TECHNOLOGIES, LLC. Lists 737 Series - [STC SA4842SW](https://openairdocs.org/stc/SA4842SW): Modification of air to air heat exchanger (P/N 182820-2 Series 2). Honeywell International Inc. Lists 737 Series - [STC SA270NW](https://openairdocs.org/stc/SA270NW): Installation of modified seat. Aviation Technical Services. Lists 737 Series - [STC ST01162NY](https://openairdocs.org/stc/ST01162NY): Installation of Literature Pockets. Magee Plastics Company. Lists 737 Series - [STC SA2607SO](https://openairdocs.org/stc/SA2607SO): Installation of coffee maker P/N 416-1001-29. B/E Aerospace Inc. Lists 737 Series - [STC SA2608SO](https://openairdocs.org/stc/SA2608SO): Installation of rail assembly, P/N 416-0201-15. B/E Aerospace Inc. Lists 737 Series - [STC SA3058SO](https://openairdocs.org/stc/SA3058SO): Installation of coffee maker 416-0001-23 and rail assembly 416-0201-5. B/E Aerospace Inc. Lists 737 Series - [STC ST01476AT](https://openairdocs.org/stc/ST01476AT): Installation of coffee maker. B/E Aerospace Inc. Lists 737 Series - [STC ST01778AT](https://openairdocs.org/stc/ST01778AT): Installation of espresso maker p/n 3510-0066-01. B/E Aerospace Inc. Lists 737 Series - [STC SA629GL](https://openairdocs.org/stc/SA629GL): Installation of Grimes galley, Model 1545LW unit 2 and unit 4. B/E Aerospace. Lists 737 Series - [STC ST01332AT](https://openairdocs.org/stc/ST01332AT): Installation of Galley Service Carts. Champ International, Inc. Lists 737 Series - [STC ST09870SC](https://openairdocs.org/stc/ST09870SC): Installation of Mechanical Window Shades. Lou Martin & Associates. Lists 737 Series - [STC ST00033AT](https://openairdocs.org/stc/ST00033AT): Installation of a single Mode S system and provisions for a TCAS II system. General Aerospace, Inc. Lists 737 Series - [STC SA4532NM](https://openairdocs.org/stc/SA4532NM): Installation of Coltech, CTD-80 ATSCALL, enabling company calling of selected aircraft via company selected radio. Avtech Corporation. Lists 737 Series - [STC ST4532NM](https://openairdocs.org/stc/ST4532NM): Installation of Coltech CTD-80 ATSCALL, enabling company calling of selected aircraft via company selected radio. Avtech Corporation. Lists 737 Series - [STC ST00774NY](https://openairdocs.org/stc/ST00774NY): Installation of a passenger cabin Liquor/beverage service cart P/N E500170. (757-222) (767-222) (727-222) (737 SERIES 222, 291, 322, 522) (747-100 SERIES 238B). Driessen Aircraft Interior Systems USA, Inc. Lists 737 Series - [STC ST02052AT](https://openairdocs.org/stc/ST02052AT): Installation of a single Collins GNLU910A flight management system, along with global navigation satellite system sensor. General Aerospace, Inc. Lists 737 Series - [STC SA02034AT](https://openairdocs.org/stc/SA02034AT): Manufacture of tray carrier, P/N 2282-506. BFE Services. Lists 737 Series - [STC ST01968AT](https://openairdocs.org/stc/ST01968AT): Manufacture of inserts for galley stowage. JK Aerospace, Inc. Lists 737 Series - [STC SA01916AT](https://openairdocs.org/stc/SA01916AT): Manufacture of Tray Carrier P/N 1839-501. BFE Services. Lists 737 Series - [STC SA2534SO](https://openairdocs.org/stc/SA2534SO): Installation of window shades, acoustic panes and reveals. Magee Plastics Company. Lists 737 Series - [STC ST179CH](https://openairdocs.org/stc/ST179CH): Installation of cargo container curtain. Plastic Composites Corp. Lists 737 Series - [STC SA00056LA](https://openairdocs.org/stc/SA00056LA): Installation of Weber Coffeemaker, P/N 870130-415. Monogram Systems. Lists 737 Series - [STC SA6090NM](https://openairdocs.org/stc/SA6090NM): Installation of emergency vision assurance system (EVAS). VisionSafe Corporation. Lists 737 Series - [STC SA370NW](https://openairdocs.org/stc/SA370NW): Removal of passenger interior, installation of cargo compartment liners and cargo tie down equipment. Western Metal Products. Lists 737 Series - [STC SA2589CE](https://openairdocs.org/stc/SA2589CE): Install Bennetts Seat Converter Stowage Compartment on passenger seat(s). John's Aircraft and Upholstery. Lists 737 Series - [STC SA1029NW](https://openairdocs.org/stc/SA1029NW): Installation of a cargo system. Western Metal Products. Lists 737 Series - [STC SA1258EA](https://openairdocs.org/stc/SA1258EA): Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584). Miller Stuart R. Lists 737 Series - [STC SA1052SO](https://openairdocs.org/stc/SA1052SO): Installation of GE battery P/N43B022RB36 in place of Marathon P/N CA-727-7, CA-727-20, or CA-27-20 batteries or SAFT P/N23180 batteries; or installation of GE battery P/N 43B020RB10 replacing Marathon P/N CA-727-7, CA-727-20 or CA-27-20 or SAFT P/N 23186 or 23180 batteries. General Electric Company. Lists 737 Series - [STC SA1082NW](https://openairdocs.org/stc/SA1082NW) (historical): Installation of auxiliary fuel tanks in the aft cargo compartment. (737 series -2K9A). Rogerson ATS. Lists 737 Series ### Approved for the engine (CFM International CFM56-7B27E series) - [STC SE04840NY](https://openairdocs.org/stc/SE04840NY): Installation of HarcoSemco Exhaust Gas Temperature (EGT) Electrical Harnesses in CFM56-7 engine. Kilroy Aviation LLC ## Earlier aircraft with N8676A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N8676A before. - [Cancelled 1957-02-18](https://openairdocs.org/deregistered/N8676A-1957-02-18): Beech A35, S/N D-2086. Owner: [Nathan Bakalar](https://openairdocs.org/faa-owner/NATHAN%20BAKALAR), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) ## Related - Other Boeing 737-8H4 aircraft: https://openairdocs.org/model/boeing-737-8h4/aircraft.md - The CFM International CFM56-7B27E series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b27e-series.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.