# N8670A: 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: 36656 - Year built: 2015 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 11, 2015 - Certificate issued: December 19, 2024 - Expires: December 31, 2031 - Mode S code: ABEB31 - 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=8670A - Page: https://openairdocs.org/aircraft/N8670A 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 N8670A. ## FAA accident and incident reports None matched to N8670A. ## Service difficulty reports (100, 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 SWAA2026092146823](https://openairdocs.org/sdr/SWAA2026092146823), Sep 16, 2026: FASTENER. MISSING. LEFT ELEVATOR OTBD BALANCE WEIGHT INNER MOST TRIM WEIGHT MISSING INBD ATTACH HARDWARE. INSTALLED FASTENER IAW SRM 51-61-04, AND SRM 51-40-02-0G-0-B00387. - [SDR SWAA2026061611642](https://openairdocs.org/sdr/SWAA2026061611642), Jun 12, 2026: GIRT BAR. OUT OF ADJUST. FLIGHT ATTENDANT REPORTS AFT GALLEY FIRST OFFICER`S SIDE GRIT BAR SKIRT HANGING OUT MORE THEN USUAL. READJUSTED AFT RT SVC DOOR ESCAPE SLIDE GIRT BAR SKIRT AS R - [SDR SWAA2026060104886](https://openairdocs.org/sdr/SWAA2026060104886), May 20, 2026: ELEC CONNECTOR. BROKEN. RIGHT HAND OWE AFT DOOR LIGHT ASSEMBLY #W4142; D14724 M02838 IS BROKEN (RED CAPPED). REPLACED CONNECTOR D14724 FUNCTIONAL CHECK OF RIGHT AFT OWE EMERGENCY LIGHT - [SDR SWAA2026060104617](https://openairdocs.org/sdr/SWAA2026060104617), May 19, 2026: CARTRIDGE. CRACKED. CRACK FOUND ON LT OUTBOARD AFT FLAP INBOARD CARTRIDGE INNER SURFACE. LEFT WING OUTBOARD AFT FLAP; CARTRIDGE WAS REMOVED AND REPLACED IAW B737 CMM 57-53-08. ASSE - [SDR SWAA2026031679516](https://openairdocs.org/sdr/SWAA2026031679516), Mar 13, 2026: FILTER. ODOR. WATER SMELLS OF CHEMICALS. DRAIN POTABLE WATER TANK. R & R GALLEY FILTERS. SERVICED POTABLE WATER PER AMM 38-11-99. - [SDR SWAA2025123055653](https://openairdocs.org/sdr/SWAA2025123055653), Dec 26, 2025: LIGHT. DETACHED. CENTER AISLE EMERGENCY EXIT SIGN DETACHED. REMOVED AND REPLACED EMERGENCY AISLE LIGHT IAW AMM 33-51-03. - [SDR SWAA2025122955339](https://openairdocs.org/sdr/SWAA2025122955339), Dec 24, 2025: SIGN. DETACHED. EMERGENCY EXIT SIGN MID CABIN DETACHED. PERFORMED TIME LIMIT REPAIR AT EMERGENCY EXIT SIGN MID CABIN IAW M24-133-0096. PERFORMED TIME LIMIT REPAIR AT EMERGENCY - [SDR SWAA2025121551849](https://openairdocs.org/sdr/SWAA2025121551849), Dec 12, 2025: SLIDE. DISLODGED. AFT SERVICE DOOR SLIDE FELL OUT BUT DID NOT DEPLOY. RE-PACKED AFT SERVICE DOOR SLIDE IAW MT 725-61-06. ACFT OK FOR SERVICE. - [SDR SWAA2025032709939](https://openairdocs.org/sdr/SWAA2025032709939), Mar 27, 2025: LAMP. INOPERATIVE. FWD LEFT OVERWING INTERIOR EXIT LIGHT HAS A FEW LAMPS INOP<[01] RELAMPED FWD LEFT OVERWING INTERIOR EXIT LIGHT PER AMM 33-51-01. OPS CHECK GOOD. - [SDR SWAA2025010382711](https://openairdocs.org/sdr/SWAA2025010382711), Jan 2, 2025: LIGHT. OUT OF ADJUST. EXIT SIGN COVERS KNOCKED OFF<[01] R&R AISLE EXIT LT ASSY PER AMM 33-51-01 - [SDR SWAA2024120272623](https://openairdocs.org/sdr/SWAA2024120272623), Nov 29, 2024: PANEL. CRACKED. WING-TO-BODY FAIRING PANEL 193D GROOVE AND CRACK DAMAGE LOCATED 4.25' FROM FWD EDGE OF PANE<[01] REMOVED AND REPLACED 93D PANEL PER SOPM 20-50-01. PARTS TRANSAC - [SDR SWAA2024120272231](https://openairdocs.org/sdr/SWAA2024120272231), Nov 27, 2024: PANEL. CRACKED. PANEL 193D HAS 5.5' GROOVE .5' WIDE WITH CRACK IN FACESHEET<[01] C/W EA 24-153-03309. - [SDR SWAA2024112561582](https://openairdocs.org/sdr/SWAA2024112561582), Nov 19, 2024: COVER. MISSING. OVERHEAD XIT SIGN AT OVERWING MISSING<[01] LENSE COVER FOUND AND REFITTED IAW AMM 33-51-03 - [SDR SWAA2024111258236](https://openairdocs.org/sdr/SWAA2024111258236), Nov 9, 2024: SIGN. LOOSE. AISLE EXIT SIGN MID CAB SIGN LOOSE<[01] RESECURED EXIT SIGN PER SIP - [SDR SWAA2024110856878](https://openairdocs.org/sdr/SWAA2024110856878), Nov 4, 2024: FLAP SYSTEM. LOCKED. FLAPS WOULD NOT GO DOWN PAST 5<[01] FOUND #1 FLAP TRANSMISSION TRIP INDICATOR TRIPPED. RESET PER FIM 27-51 TASK 849.;[02] REPLACED OIL FOR TRAILING EDGE FLAP TR - [SDR SWAA2024062404817](https://openairdocs.org/sdr/SWAA2024062404817), Jun 22, 2024: LENS. DETACHED. LEFT FORWARD OVER WING EMERGENCY EXIT DOOR SIGN LENS OFF<[01] INSTALLED LENS COVER PER M/M 33-51-01 - [SDR SWAA2024061497825](https://openairdocs.org/sdr/SWAA2024061497825), Jun 3, 2024: STIFFENER. CRACKED. CRACKED STIFFENER BS 540 LBL 1.5 WL 208 (MARKED)<[01] VERIFIED STEP 2 IN PARTIAL.;[02] REMOVED AND REPLACED PASSENGER CABIN STIFFENER AT BS 540 BL0 TO LBL 25 WL - [SDR SWAA2024061497824](https://openairdocs.org/sdr/SWAA2024061497824), Jun 3, 2024: STIFFENER. CRACKED. CRACKED STIFFENER BS 540 RBL 1.5 WL 208 (MARKED)<[01] VERIFIED STEP 3 IN PARTIAL.;[02] VERIFIED STEPS 2;3 COMPLETE; STEP 1 IN PARTIAL.;[03] REMOVED AND REPLACED - [SDR SWAA2024061491364](https://openairdocs.org/sdr/SWAA2024061491364), May 29, 2024: ATTACH ANGLE. CRACKED. B.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 10 W.L. 164.<[01] VERIFIED STEPS 8;10 COMPLETE; STEP 9 IN PARTIAL.;[02] VERIFIED STEPS 9;11 COMPL - [SDR SWAA2024022957111](https://openairdocs.org/sdr/SWAA2024022957111), Feb 27, 2024: COVER. DETACHED. CREW REPORTED OVERWING AREA EMERGENCY EXIT SIGN COVER FELL OFF<[01] REPOSITIONED OVERWING EMERGENCY EXIT SIGN COVER PER AMM 33-51-01 OP CHECK OK - [SDR SWAA2024020247019](https://openairdocs.org/sdr/SWAA2024020247019), Jan 30, 2024: GLOWSTRIP. DETACHED. PHOTOLUMINESENT STRIP FO SIDE BLUE FLOOR STRIP BY ROW 12 IS COMING OFF<[01] RESEATED GLOW STRIP IAW SIP - [SDR SWAA2023082392773](https://openairdocs.org/sdr/SWAA2023082392773), Aug 23, 2023: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT IN AFT CEILING PANEL INOP<[01] FOUND CONNECTOR DISCONNECTED AND TAPED. CONNECTED TO EMERGENCY BATTERY PACK CONNECTOR PER SIP & WDM 33-51-14. - [SDR SWAA2023052450594](https://openairdocs.org/sdr/SWAA2023052450594), May 21, 2023: WEDGE. DELAMINATED. R/H INBOARD FLAP BONDED WEDGE ASSY DELAMANATED<[01] REMOVED WEDGE PER SRM 51-40-02.;[02] RII. OK TO INSTALL NEW WEDGE P/N 113A2500-14.;[03] INSTALLED SERVICABLE - [SDR SWAA2023052547785](https://openairdocs.org/sdr/SWAA2023052547785), May 11, 2023: FAIRING. DELAMINATED. L/H WING #3 FLAP FAIRING 542BB OUTER SKIN IS DELAMINATED ON LOWER OUTBOARD SIDE. (MARKED)<[01] REMOVED DELAMINATED SKIN PER SRM 57-53-70-2R-4.;[02] INSPECTED WO - [SDR SWAA2023052547435](https://openairdocs.org/sdr/SWAA2023052547435), May 11, 2023: BAFFLE. CORRODED. AFT CARGO BAFFLE AT RBL 22 STA 747-767 HAS CORROSION AROUND FASTENER HOLES.<[01] BLENDED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-00?52 - [SDR SWAA2023052447663](https://openairdocs.org/sdr/SWAA2023052447663), May 11, 2023: BATTERY PACK. INOPERATIVE. FWD GALLEY LT EMERGENCY EXIT BATTERY PACK INOP<[01] REMOVED AND REPLACED FOWARD GALLEY BATTERY PACK PER MM 33-51-06; OPS CHECKS GOOD PER MM 33-51-00 - [SDR SWAA2023052546994](https://openairdocs.org/sdr/SWAA2023052546994), May 9, 2023: SKIN. PULLED. #1 ENGINE INLET HAS FASTENER PULLED THROUGH LIP SKIN OUTER SURFACE 2 O'CLOCK POSITION.<[01] PERFORMED NDT ON FASTENER HOLE PER NDT PART 6; 51-00-00 PROCEDURE 16 - [SDR SWAA2023052547102](https://openairdocs.org/sdr/SWAA2023052547102), May 9, 2023: ANGLE. CRACKED. L/H WING UPPER TRAILING EDGE PANEL LOWER CHANNEL UNDER PANEL HAS SEVERAL CRACKS I/B OF CASTING FOR I/B FLAP DEFLECTION ROLLERS (MKD)<[01] REMOVED AND REPLACED L - [SDR SWAA2023052546187](https://openairdocs.org/sdr/SWAA2023052546187), May 6, 2023: SHIELD. CORRODED. AFT CARGO DOOR SURROUND STRUCTURE LOWER SILL FWD TRANSITION SHIELD STA 767 TO STA 795; RBL 21 TO RBL 27 HAS CORROSION AT UPPER AND LOWER SURFACES AROUND FASTENE - [SDR SWAA2023052545319](https://openairdocs.org/sdr/SWAA2023052545319), May 4, 2023: BEAM. CRACKED. AFT CARGO COMPARTMENT BILGE AREA. SUPPORT ANGLE FOR WASTE TANK ENCLOSURE BEAM IS CRACKED. LOCATED AT STA 867 LBL 13; WL 161. MARKED. AFT CARGO COMPARTMENT BILGE - [SDR SWAA2023052545316](https://openairdocs.org/sdr/SWAA2023052545316), May 4, 2023: WEB. CORRODED. AFT CARGO DOOR CUTOUT SURROUND STRUCTURE. LOWER MAIN SILL WEB HAS MINOR SURFACE CORROSION AROUND FASTENER HOLES STARTING AT STA 787 TO STA 847 RBL 21 TO RBL 27. - [SDR SWAA2023052545310](https://openairdocs.org/sdr/SWAA2023052545310), May 4, 2023: ANGLE. CORRODED. AFT CARGO LH FLOOR TRANSITION ANGLE (SIDEPLATE CHANNEL) HAS CORROSION IN NUMEROUS AREAS ON AND AROUND FASTEN HOLES STA-747 TO 787 (MARKED)<[01] BLENDED OUT CORR - [SDR SWAA2023052545614](https://openairdocs.org/sdr/SWAA2023052545614), May 4, 2023: ANGLE. CORRODED. AFT CARGO RH FLOOR TRANSITION ANGLE (SIDEPLATE CHANNEL) CORROSION OUT OF LIMITS BS727I TO 727J.<[01] COMPLIED WITH MEASUREMENTS.;[02] COMPLIED WITH TOOL REQUIRE - [SDR SWAA2023052445612](https://openairdocs.org/sdr/SWAA2023052445612), May 4, 2023: FLAP. DELAMINATED. LEFT WING OUTBOARD AFT FLAP HAS A LARGE AREA OF DELIMITATION ON THE INBOARD LOWER SURFACE. (PIC ATTACHED)<[01] REMOVED AND REPLACED OUTBOARD AFT FLAP IAW AMM 27 - [SDR SWAA2023052545067](https://openairdocs.org/sdr/SWAA2023052545067), May 3, 2023: ANGLE. CRACKED. FWD CARGO R/H SIDEPLATE HAS POSSIBLE CRACK AT I/B ATTACH FASTENER RBL 21; STA. 500B.<[01] CRACKED FOUND OUT OF LIMIT .I.A.W. SRM 53-00-53-1A-2.;[02] REMOVED RH - [SDR SWAA2023052545083](https://openairdocs.org/sdr/SWAA2023052545083), May 3, 2023: PLATE. CRACKED. FWD CARGO L/H SIDEPLATE HAS POSSIBLE CRACK AT I/B ATTACH FASTENER LBL 21; STA. 500B.<[01] FWD CARGO L/H SIDE PLATE FROM STA 440+10 TO STA 500I REPLACED ON FAULT - [SDR SWAA2023052545073](https://openairdocs.org/sdr/SWAA2023052545073), May 3, 2023: STRUCTURE. CORRODED. SURFACE CORROSION ON UPPER FLOOR STRUCTURE AROUND O/B AFT LAV MOUNT FOR AFT L/H LAV. (MKD)<[01] DRAIN INTERCOSTAL OUT OF LIMITS PER SRM 53-70-51-1A-1;[02] LOCAT - [SDR SWAA2023052545059](https://openairdocs.org/sdr/SWAA2023052545059), May 3, 2023: ANGLE. CORRODED. FWD CARGO AFT BULKHEAD PANEL LOWER ATTACH ANGLE HAS CORROSION AT FASTENER HOLES; RBL 11-RBL 24; STA. 500I<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAG - [SDR SWAA2023052545075](https://openairdocs.org/sdr/SWAA2023052545075), May 3, 2023: PLATE. CORRODED. FWD CARGO R/H SIDEPLATE HAS CORROSION AT FASTENER HOLES RBL 24; STA. 500D-500E<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .010? IN DEPT - [SDR SWAA2023052545076](https://openairdocs.org/sdr/SWAA2023052545076), May 3, 2023: PLATE. CORRODED. FWD CARGO R/H SIDEPLATE HAS CORROSION AT FASTENER HOLES RBL 24; STA. 500E-500F<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .015?. DAMAGE - [SDR SWAA2023052545061](https://openairdocs.org/sdr/SWAA2023052545061), May 3, 2023: PLATE. CORRODED. FWD CARGO R/H SIDEPLATE HAS CORROSION AT FASTENER HOLES RBL 24; STA. 500F-500G<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .009?. DAMAGE - [SDR SWAA2023052545064](https://openairdocs.org/sdr/SWAA2023052545064), May 3, 2023: THRESHOLD. CORRODED. AFT CARGO DOOR THRESHOLD CORROSION AT STA 795 TO 847; RBL 27. AFT CARGO DOOR THRESHOLD CORROSION AT STA 795 TO 847 RBL 27.<[01] BLENDED OUT CORROSION AT AFT CAR - [SDR SWAA2023052545077](https://openairdocs.org/sdr/SWAA2023052545077), May 3, 2023: PLATE. CORRODED. FWD CARGO R/H SIDEPLATE HAS CORROSION AT FASTENER HOLES RBL 24; STA. 500H-500I<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .006?. DAMAGE - [SDR SWAA2023052545062](https://openairdocs.org/sdr/SWAA2023052545062), May 3, 2023: PLATE. CORRODED. FWD CARGO R/H SIDEPLATE HAS CORROSION AT FASTENER HOLES RBL 24; STA. 500G-500H<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .009?. DAMAGE - [SDR SWAA2023052545086](https://openairdocs.org/sdr/SWAA2023052545086), May 3, 2023: THRESHOLD. CORRODED. FWD CARGO DOOR THRESHOLD WEB HAS CORROSION RBL 28; STA. 440-492.<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .006?. DAMAGE FOUND TO BE O - [SDR SWAA2023052545298](https://openairdocs.org/sdr/SWAA2023052545298), May 3, 2023: BEAM. CORRODED. CORROSION ON FLOOR BEAM AT STA 927+10; LBL +52- MARKED. FAULT #1137 CLOSED IN ERROR<[01] DRAIN INTERCOSTAL OUT OF LIMITS PER SRM 53-70-51-1A-1;[02] FAULT TO BE - [SDR SWAA2023052545078](https://openairdocs.org/sdr/SWAA2023052545078), May 3, 2023: PLATE. CORRODED. FWD CARGO L/H SIDEPLATE HAS CORROSION AT FASTENER HOLES LBL 24; STA. 500D-500E<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .018?. DAMAGE - [SDR SWAA2023052545299](https://openairdocs.org/sdr/SWAA2023052545299), May 3, 2023: INTERCOSTAL. CRACKED. LEFT INBOARD FAN COWL HAS CRACKED INTERCOSTAL ON OIL ACCESS DOOR FRAME.<[01] REMOVED AND REPLACED INTERCOSTAL PER ARM. 51-40-02;[02] INSPECTED WORK PERFORMED. - [SDR SWAA2023052545300](https://openairdocs.org/sdr/SWAA2023052545300), May 3, 2023: WEB. CRACKED. RIGHT OUTBOARD FAN COWL HAS CRACKED INTERCOSTAL ON OIL SERVICE DOOR FRAME.<[01] REMOVED AND REPLACED WEB I.A.W SRM 51-40-02.;[02] INSPECTED WORK PERFORMED - [SDR SWAA2023052446186](https://openairdocs.org/sdr/SWAA2023052446186), May 3, 2023: PANEL. MISSING. PANEL 221BF HAS FIBERS MISSING<[01] INSTALLED NEW 221BF PANEL PER AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT);[02] C/W INSPE All 100: https://openairdocs.org/aircraft/N8670A/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 N8670A The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N8670A before. - [Cancelled 1971-08-25](https://openairdocs.org/deregistered/N8670A-1971-08-25): Beech A35, S/N D2080. Owner: [Hay Frank B](https://openairdocs.org/faa-owner/HAY%20FRANK%20B) ## 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.