# N8675A: 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: 35976 - Year built: 2015 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 13, 2015 - Certificate issued: December 17, 2024 - Expires: December 31, 2031 - Mode S code: ABEBE0 - 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=8675A - Page: https://openairdocs.org/aircraft/N8675A 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 N8675A. ## FAA accident and incident reports None matched to N8675A. ## Service difficulty reports (130, 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 SWAA2026093046583](https://openairdocs.org/sdr/SWAA2026093046583), Sep 26, 2026: BATTERY. INOPERATIVE. LEFT AFT INBD FLIGHT ATTENDANT FLASHLIGHT BATTERY INOPERATIVE, OK TO CONTINUE PER MEL 25-12-01. R & R THE FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECKED GOOD. - [SDR SWAA2026081002003](https://openairdocs.org/sdr/SWAA2026081002003), Aug 4, 2026: ENGINE. FAILED. NR 1 ENGINE FAILED ON TAKEOFF ROLL. REMOVED AND REPLACED THE NR 1 ENG IAW MT 771-00-01. REF TTG8Q008F2S8. - [SDR SWAA2025121551604](https://openairdocs.org/sdr/SWAA2025121551604), Dec 11, 2025: BRACKET. BROKEN. FWD MEGAPHONE BRACKET BROKEN. R & R BRACKET IAW AMM 25--64-00 SIP. - [SDR SWAA2025110731884](https://openairdocs.org/sdr/SWAA2025110731884), Nov 5, 2025: TRAY. DELAMINATED. PASSENGER CABIN SEAT BACK MOUNTED TRAY TABLE DELAMINATED AT 15E. REMOVED AND REPLACED FOOD TRAY TABLE AT 15E IAW CMM 25-22-46 - [SDR SWAA2025091113312](https://openairdocs.org/sdr/SWAA2025091113312), Sep 9, 2025: BATTERY. INTERMITTENT. CREW REPORTS FWD MEGAPHONE WORK INTERMITTENTLY. R & R FWD MEGAPHONE BATTERIES IN REF TO AMM 25-64-00. NEXT INSPECTION DUE SEP 2026 - [SDR SWAA2025052772867](https://openairdocs.org/sdr/SWAA2025052772867), May 20, 2025: TAB. CRACKED. LEFT WING FIXED TRAILING EDGE DEFLECTION ROLLERS ASSEMBLYS PANEL ATTACHMENT TAB HAS A VISIBLE CRACKED 1.7 INCHES IN THE RADIUS FROM THE AFT EDGE.PICTURE ATTACHE - [SDR SWAA2025042125874](https://openairdocs.org/sdr/SWAA2025042125874), Apr 17, 2025: GIRT BAR. FAILED. FWD ENTRY DOOR GIRT BAR NOT DISARMED WHEN DOOR WAS OPENED. SLIDE CAME PARTIALLY OUT OF DOOR. SLIDE DID NOT DEPLOY. REINSTALLED FORWARD ENTRY ESCAPE SLIDE PER MT - [SDR SWAA2025012086390](https://openairdocs.org/sdr/SWAA2025012086390), Jan 15, 2025: BATTERY PACK. INOPERATIVE. RT HAND EMERGENCY EXIT DOOR LIGHTS INOP<[01] REMOVED AND REPLACED CHARGER ASSY AND BATTERY IAW AMM 33-51-06 SYSY OPERATION NORMAL;[02] INSPECTED REMOVED AND REP - [SDR SWAA2025012084581](https://openairdocs.org/sdr/SWAA2025012084581), Jan 9, 2025: ANGLE. CRACKED. IN THE LH AC BAY; L ANGLE AT STA 663; LBL12; RIVET HAS A VERTICAL CRACK EXTENDING FROM IT. VERIFIED WITH HFEC. FABRICATED REPAIR PARTS PER SRM 57-10-10-2R-5;[04 - [SDR SWAA2025012083721](https://openairdocs.org/sdr/SWAA2025012083721), Jan 7, 2025: ANGLE. CRACKED. BAFFLE ATTACH ANGLE CRACKED IN FORWARD CARGO; AFT SIDE OF BS 500H RBL 21.<[01] REMOVED ATTACH ANGLE FROM AIRCRAFT I.A.W SRM 51-40-02 FOR REPLACEMENT.;[02] LOCAT - [SDR SWAA2025012083722](https://openairdocs.org/sdr/SWAA2025012083722), Jan 7, 2025: ANGLE. CRACKED. BAFFLE ATTACH ANGLE CRACKED IN FORWARD CARGO; FWD SIDE OF BS 500H RBL 21.<[01] REMOVED ATTACH ANGLE FROM AIRCRAFT I.A.W SRM 51-40-02 FOR REPLACEMENT.;[02] LOCAT - [SDR SWAA2025012083723](https://openairdocs.org/sdr/SWAA2025012083723), Jan 7, 2025: ANGLE. CRACKED. BAFFLE ATTACH ANGLE CRACKED IN FORWARD CARGO; AFT SIDE OF BS 500G RBL 21.<[01] REMOVED ATTACH ANGLE FROM AIRCRAFT I.A.W SRM 51-40-02 FOR REPLACEMENT.;[02] LOCAT - [SDR SWAA2025012081294](https://openairdocs.org/sdr/SWAA2025012081294), Dec 28, 2024: ANGLE. CRACKED. IN THE LH AC BAY; L ANGLE AT STA 663; LBL12; RIVET HAS A VERTICAL CRACK EXTENDING FROM IT. VERIFIED WITH HFEC. FABRICATED REPAIR PARTS PER SRM 57-10-10-2R-5;[04 - [SDR SWAA2025012081291](https://openairdocs.org/sdr/SWAA2025012081291), Dec 28, 2024: PANEL. DAMAGED. PANEL 551GB PANEL HAS 2 ELONGATED FASTERNER HOLES. MARKED.<[01] REPAIRED PER SRM 51-70-06-2R-9;[02] INSPECTED REPAIR PER SRM 51-70-06-2R-9. - [SDR SWAA2025012081293](https://openairdocs.org/sdr/SWAA2025012081293), Dec 28, 2024: STRAP. FRAYED. LEFT EMERGENCY EXIT HATCH ESCAPE STRAP FRAYED<[01] REMOVED AND REPLACED EMERGENCY ESCAPE STRAP PER AMM 25-61-10-400-802.;[02] QC C/W FOR CA#1. WILLIAM DAVIS (TE - [SDR SWAA2025012081292](https://openairdocs.org/sdr/SWAA2025012081292), Dec 28, 2024: STRAP. FRAYED. RIGHT EMERGENCY EXIT HATCH ESCAPE STRAP FRAYED<[01] REMOVED AND REPLACED EMERGENCY ESCAPE STRAP PER AMM 25-61-10-400-802.;[02] QC C/W FOR CA#1. WILLIAM DAVIS (T - [SDR SWAA2025012081165](https://openairdocs.org/sdr/SWAA2025012081165), Dec 27, 2024: FLOOR SUPPORT. CRACKED. PASSENGER COMPARTMENT FLOOR SUPPORT STA. 540 BL 0-RBL 24 CRACKED ON BOTH ENDS AT ATTACHMENT FASTENERS.<[01] 01 - REMOVED AND REPLACED PER SRM 51-40-02. - [SDR SWAA2025012081166](https://openairdocs.org/sdr/SWAA2025012081166), Dec 27, 2024: FLOOR SUPPORT. CRACKED. PASSENGER COMPARTMENT FLOOR SUPPORT STA. 540 BL 0-LBL 24 CRACKED ON BOTH ENDS AT ATTACHMENT FASTENERS.<[01] 01 - REMOVED AND REPLACED PER SRM 51-40-02.;[02] COR - [SDR SWAA2025012080925](https://openairdocs.org/sdr/SWAA2025012080925), Dec 26, 2024: PANEL. DAMAGED. RIGHT WING LOWER WING L/E PANEL #621FB HAS 2EA ELONGATED HOLES.<[01] REPAIRED PER SRM 51-70-06-2R-9;[02] INSP C/W PER REPAIRED PER SRM 51-70-06-2R-9;[03] RESTOR - [SDR SWAA2025012080922](https://openairdocs.org/sdr/SWAA2025012080922), Dec 26, 2024: PANEL. DAMAGED. RIGHT WING LOWER WING L/E PANEL #621PB HAS 1EA ELONGATED HOLES.<[01] REPAIRED PER SRM 51-70-06-2R-9;[02] INSP C/W PER REPAIRED PER SRM 51-70-06-2R-9;[03] RESTOR - [SDR SWAA2025012080926](https://openairdocs.org/sdr/SWAA2025012080926), Dec 26, 2024: PANEL. DAMAGED. RIGHT WING LOWER WING L/E PANEL #621VB HAS 2EA ELONGATED HOLES.<[01] REPAIRED PER SRM 51-70-06-2R-9;[02] INSP C/W REPAIRED PER SRM 51-70-06-2R-9;[03] RESTORED F - [SDR SWAA2025012080581](https://openairdocs.org/sdr/SWAA2025012080581), Dec 24, 2024: ANGLE. CRACKED. FOUND 'L' ANGLE CRACKED AT STA 663 R/H SIDE A/C BAY FROM FASTENER HOLE. 5TH FASTENER FROM O/B BULKHEAD DIVIDER.<[01] INSPRJCT: WORK ACCOMPLISHED IN STEPS 1; 2 A - [SDR SWAA2025012080577](https://openairdocs.org/sdr/SWAA2025012080577), Dec 24, 2024: ANGLE. CRACKED. L/H WING FIXED T/E ANGLE THAT IS ATTACHED TO THE I/B SIDE OF THE DEFLECTION CONTROL RIB IS CRACKED (MARKED) AFT UPPER T/E<[01] REMOVED OLD ANGLE AND DRILLED NEW - [SDR SWAA2025012080580](https://openairdocs.org/sdr/SWAA2025012080580), Dec 24, 2024: SUPPORT BRACKET. CRACKED. FIXED TRAILING PANEL ABOVE DEFLECTION CONTROL RIB HAS SUPPORT BRACKET (FWD SIDE) CRACK LOCATED AT WBL 190.<[01] REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51- - [SDR SWAA2025012080578](https://openairdocs.org/sdr/SWAA2025012080578), Dec 24, 2024: RIB. DAMAGED. R WING TRAILING EDGE STRUCTURE DEFLECTION CONTROL RIB UPPER TAB HAS ELONGATED FASTENER HOLES.(2EA) [MARKED]<[01] CUT OUT DAMAGE IN UPPER TAB IAW SRM 57-51-02-2R - [SDR SWAA2025012080345](https://openairdocs.org/sdr/SWAA2025012080345), Dec 22, 2024: WEB. FRAYED. FWD CARGO; LEFT OF DOOR- HALF MOON CARGO WEB FRAYING<[01] REPLACED FWD CARGO; LEFT OF DOOR- HALF MOON CARGO NET PER AMM 25-52-12.;[02] 02 - INSPECTED PER [AMM 2 - [SDR SWAA2025012080346](https://openairdocs.org/sdr/SWAA2025012080346), Dec 22, 2024: WEB. FRAYED. FWD CARGO; RIGHT OF DOOR- HALF MOON CARGO WEB FRAYING<[01] REPLACED FWD CARGO; RIGHT OF DOOR- HALF MOON CARGO PER AMM 25-52-12.;[02] 02 - INSPECTED PER [AMM 25- - [SDR SWAA2024102452279](https://openairdocs.org/sdr/SWAA2024102452279), Oct 23, 2024: GIRT BAR. OUT OF ALIGNMENT. FLIGHT ATTENDANT REPORTS THAT FWD SERVICE DOOR GIRT BAR IS HARD TO STOW ON HOOKS<[01] RR?D FWD SERVICE DOOR GIRT BAR IAW AMM 25-66-01 - [SDR SWAA2024070106876](https://openairdocs.org/sdr/SWAA2024070106876), Jun 27, 2024: LENS. UNSECURE. CENTER AISLE EXIT SIGN NOT SECURE<[01] SECURED EXIT SIGN LENS COVER PER M/M 33-51-01 - [SDR SWAA2024020546548](https://openairdocs.org/sdr/SWAA2024020546548), Jan 30, 2024: PUMP. LOW PRESSURE. A HYD SYSTEM FAILURE CREW NOTED LOSS OF A SYSTEM ENGINE PUMP PRESSURE AND LOSS OF 50% OF FLUID. 'FOLLOWING CHECKLIST' RAN ELECTRIC PUMP TILL ZERO PRESSURE AND Z - [SDR SWAA2023121832365](https://openairdocs.org/sdr/SWAA2023121832365), Dec 15, 2023: FILLER. MISSING. EXTERNAL ELECTRICAL PLUG CUTOUT; EXTERNAL DOUBLER TAB IS MISSING AT THE LOWER LATCH STRIKER PLATE.<[01] REMOVED FASTENERS AT MISSING FILLER FROM PREVIOUS REPAIR - [SDR SWAA2023121531422](https://openairdocs.org/sdr/SWAA2023121531422), Dec 13, 2023: BATTERY PACK. INOPERATIVE. RIGHT AFT SERVICE DOOR EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED RIGHT AFT GALLEY EMERGENCY LIGHT BATTERY PACK PER MM 33-51-06. OPS CHECKS GOOD PER MM 33-5 - [SDR SWAA2023121830127](https://openairdocs.org/sdr/SWAA2023121830127), Dec 10, 2023: HANDLE. GOUGED. FWD SERVICE DOOR LINER UPPER ASSIST HANDLE IS GOUGED.<[01] REPLACED FWD SERVICE DOOR ASSIST HANDLE MOUNTING CUP IN REFERENCE AMM 52-41-31.;[02] REPLACED FWD SER - [SDR SWAA2023121530128](https://openairdocs.org/sdr/SWAA2023121530128), Dec 10, 2023: HANDLE. GOUGED. FWD ENTRY DOOR INTERIOR AFT ASSIST HANDLE IS GOUGED.<[01] REPLACED FWD ENTRY DOOR INTERIOR AFT ASSIST HANDLE MOUNTING CUPS IN REFERENCE AMM 25-21-31-420-802 STE - [SDR SWAA2023121529579](https://openairdocs.org/sdr/SWAA2023121529579), Dec 8, 2023: BATTERY PACK. INOPERATIVE. CABIN BULL NOSE EMERGENCY LIGHT; LEFT SIDE INOP<[01] REMOVED AND REPLACED BATTERY PACKS AT SEATS 7; 13; AND 20ABC; OPS CHECKS GOOD; CABIN BULL NOSE EMERGENCY LI - [SDR SWAA2023121529132](https://openairdocs.org/sdr/SWAA2023121529132), Dec 8, 2023: SCUFF PLATE. CRACKED. AFT CARGO AFT CORNER SCUFF PLATE IS CRACKED.<[01] REMOVED AND REPLACED AFT CARGO SCUFF PLATE PER AMM 53-11-02 - [SDR SWAA2023121825199](https://openairdocs.org/sdr/SWAA2023121825199), Nov 27, 2023: FLOORBEAM. CORRODED. FLOOR BEAM CORRODED AT STA 947 LBL 24 NEAR EDGE OF LAV MOUNT<[01] REMOVED CORROSION IAW SRM 51-10-02. THE REWORKED AREA IS OUT OF LIMIT PER SRM 53-70-51-1A-1 FI - [SDR SWAA2023121525200](https://openairdocs.org/sdr/SWAA2023121525200), Nov 27, 2023: RADOME. CRACKED. NOSE RADOME RUBBER BOOT HAS MULTIPLE CRACKS<[01] REMOVED AND REPLACED RADOME PER MM 53-52-00. SEE CARD [TTG8Q00PX78K FOR TOOLING AND SIGH OFFS. - [SDR SWAA2023121524848](https://openairdocs.org/sdr/SWAA2023121524848), Nov 26, 2023: LIGHT. INOPERATIVE. OPS CHECK EMERGENCY LIGHTS<[01] CABIN EMERGENCY LIUGHTS OPS CHECKS GOOD PER MM 33-51-00 - [SDR SWAA2023121829963](https://openairdocs.org/sdr/SWAA2023121829963), Nov 22, 2023: STRINGER. INCORRECT. BS 727 INNER CHORD AT STRINGER 18A LEFT SIDE THICKNESS OF THE GAP BETWEEN THE INNER CHORD AND STRINGER S-18A RECORDED GAP VALUE .029 (GAP MEASUREMENT IS GREATER - [SDR SWAA2023121829964](https://openairdocs.org/sdr/SWAA2023121829964), Nov 22, 2023: STRINGER. INCORRECT. BS 727 INNER CHORD AT STRINGER 18A RIGHT SIDE THICKNESS OF THE GAP BETWEEN THE INNER CHORD AND STRINGER S-18A RECORDED GAP VALUE .021 (GAP MEASUREMENT IS GREATE - [SDR SWAA2023121824197](https://openairdocs.org/sdr/SWAA2023121824197), Nov 22, 2023: ANGLE. CORRODED. CORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT 747 + 2 ' APROX AT STA 747 + 2 ' APROX<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0. - [SDR SWAA2023121824192](https://openairdocs.org/sdr/SWAA2023121824192), Nov 22, 2023: ANGLE. CORRODED. CORROSION ON AFT CARGO R/H TRANSITION ANGLE AROUND ATTACH HOLE AT STA 767 { MARK }<[01] CORROSION REMOVED PER SRM 51-10-02. DAMAGE OUT OF LIMITS PER SRM 53-00-5 - [SDR SWAA2023121824203](https://openairdocs.org/sdr/SWAA2023121824203), Nov 22, 2023: ANGLE. CORRODED. CORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT BS 727 J + 10 ' APROX<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0.037' REMAINING TH - [SDR SWAA2023121824207](https://openairdocs.org/sdr/SWAA2023121824207), Nov 22, 2023: ANGLE. CORRODED. CORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT BS 727 I + 6 ' APROX<[01] REMOVED CORROSION PER SRM 53-0-53-1A-2 (0.037' REMAINING THICKNESS). TR - [SDR SWAA2023121824208](https://openairdocs.org/sdr/SWAA2023121824208), Nov 22, 2023: ANGLE. CORRODED. CORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT BS 727 I + 14 ' APROX<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.035' REMAINING THICKNESS). - [SDR SWAA2023121824209](https://openairdocs.org/sdr/SWAA2023121824209), Nov 22, 2023: ANGLE. CORRODED. CORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT BS 727 I + 18 ' APROX<[01] REMOVED CORROSION PER SRM 53-0-53-1A-2 (0.038' REMAINING THICKNESS). T - [SDR SWAA2023121824187](https://openairdocs.org/sdr/SWAA2023121824187), Nov 22, 2023: ANGLE. CORRODED. CORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT 747 + 6 ' APROX AT STA 747 + 6 ' APROX<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0. - [SDR SWAA2023121824188](https://openairdocs.org/sdr/SWAA2023121824188), Nov 22, 2023: ANGLE. CORRODED. CORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT 747 +14 ' APROX AT STA 747 +14 ' APROX<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0. - [SDR SWAA2023121824198](https://openairdocs.org/sdr/SWAA2023121824198), Nov 22, 2023: ANGLE. CORRODED. CORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT 747 + 10 ' APROX AT STA 747 + 10 ' APROX<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.037' REM All 130: https://openairdocs.org/aircraft/N8675A/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 N8675A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N8675A before. - [Cancelled 2006-11-02](https://openairdocs.org/deregistered/N8675A-2006-11-02): Beech A35, S/N D-2085, built 1949. Triennial form not returned. Owner: [Johnson Lucien S](https://openairdocs.org/faa-owner/JOHNSON%20LUCIEN%20S), [Orlando, FL](https://openairdocs.org/faa-place/FL/Orlando) ## 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.