# N8671D: 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: 36715 - Year built: 2015 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 5, 2015 - Certificate issued: December 19, 2024 - Expires: December 31, 2031 - Mode S code: ABEB57 - 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=8671D - Page: https://openairdocs.org/aircraft/N8671D 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 N8671D. ## FAA accident and incident reports None matched to N8671D. ## Service difficulty reports (98, 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 SWAA2026082689480](https://openairdocs.org/sdr/SWAA2026082689480), Aug 22, 2026: LIGHT. INTERMITTENT. AFT EMERGENCY EXIT FLUORESCENT LIGHT ON F/O SIDE FLICKERS. PERFORMED OPS CHECK OF AFT RIGHT OVERWING EMERGENCY EXIT SIDE WALL LIGHT REF AMM 33-21-00. OPS CHECK - [SDR SWAA2026081296229](https://openairdocs.org/sdr/SWAA2026081296229), Aug 8, 2026: LENS. DETACHED. CENTER EMERGENCY EXIT LIGHT FELL OFF, SECURED EMERGENCY LIGHT LENS ON IAW AMM 33-51-01. - [SDR SWAA2026010959153](https://openairdocs.org/sdr/SWAA2026010959153), Jan 7, 2026: LIGHT. DETACHED. EMERGENCY LIGHT AT ROW 23 SEAT C, FELL OUT OF CEILING. REINSTALLED LIGHT ASSEMBLY AT ROW 23 SEAT C IAW AMM 33-51-03 - [SDR SWAA2025121043206](https://openairdocs.org/sdr/SWAA2025121043206), Dec 5, 2025: BATTERY PACK. INOPERATIVE. R1 DOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND INSTALLED EMERGENCY BATTERY PACK FOR R1 DOOR AMM 33-51-06-960-805 AND OPS CHECK GOOD. REMOVED AND INSTALLED EM - [SDR SWAA2025110631204](https://openairdocs.org/sdr/SWAA2025110631204), Nov 3, 2025: GIRT BAR. LOOSE. FWD SERVICE DOOR GIRT BAR BRACKET RIVETS LOOSE. OK TO CONTINUE PER TLD EA M-23-125-01839. - [SDR SWAA2025071491117](https://openairdocs.org/sdr/SWAA2025071491117), Jul 13, 2025: ENGINE. FAILED. ENGINE FAILURE AFTER DEPARTURE AT 3000. R&R #1ENGINE IN REF MT 771-00-01. OPS & LEAK CHECK GOOD. AIRCRAFT OK TO CONTINUE IN SERVICE. - [SDR SWAA2025071590378](https://openairdocs.org/sdr/SWAA2025071590378), Jul 11, 2025: ENGINE. FAILED. ENGINE FAILURE AFTER DEPARTURE @ 3000' - [SDR SWAA2025071089127](https://openairdocs.org/sdr/SWAA2025071089127), Jul 8, 2025: FLASHLIGHT. INOPERATIVE. AFT LEFT OUTBOARD FLASH LIGHT INOPERATIVE. R&R FLASHLIGHT & BATTERY PER AMM 25-64-00. - [SDR SWAA2025071090042](https://openairdocs.org/sdr/SWAA2025071090042), Jul 8, 2025: BATTERY. INOPERATIVE. AFT LEFT OUTBOARD FLASH LIGHT INOPERATIVE. R & R FLASHLIGHT & BATTERY IAW AMM 25-64-00. - [SDR SWAA2024122680637](https://openairdocs.org/sdr/SWAA2024122680637), Dec 24, 2024: SEAT TRACK. LOOSE. PASSENGER SEAT ROWS LOOSE IN TRACK AT 15ABC; 16DEF; 22DEF AND 23 ABC.<[01] SECURED LOOSE SEAT TRACKS AT SEAT ROWS 15ABC;16DEF;22DEF AND 23ABC PER AMM 25-22-00 - [SDR SWAA2024121777693](https://openairdocs.org/sdr/SWAA2024121777693), Dec 15, 2024: DOOR. OUT OF ADJUST. FWD SERVICE DOOR DIFFICULT TO CLOSE<[01] ADJUSTED FORWARD SERVICE DOOR. REFERENCE M/M 52-41-21. OPS CHECKS OK - [SDR SWAA2024110649672](https://openairdocs.org/sdr/SWAA2024110649672), Oct 17, 2024: WEDGE. DELAMINATED. LEFT WING #1 SLAT TRAILING EDGE WEDGE LOWER SURFACE IS DELAMINATED ON OUTBOARD END.<[01] REMOVED #1 SLAT IN REF TO AMM 27-81-21;[02] REMOVED #1 SLAT BOTH MAIN T - [SDR SWAA2024110649673](https://openairdocs.org/sdr/SWAA2024110649673), Oct 17, 2024: WEDGE. DELAMINATED. RIGHT WING #8 SLAT TRAILING EDGE WEDGE LOWER SURFACE IS DELAMINATED ON OUTBOARD END.<[01] REMOVED #8 SLAT WITH THE TRACK PER AMM 27-81-21;[02] OK TO INSTALL THE - [SDR SWAA2024110649940](https://openairdocs.org/sdr/SWAA2024110649940), Oct 17, 2024: FLOOR SUPPORT. CRACKED. CABIN FLOOR INTERCOSTAL CRACKED AT STA 540 LBL 1.<[01] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02;[02] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02; - [SDR SWAA2024110649941](https://openairdocs.org/sdr/SWAA2024110649941), Oct 17, 2024: FLOOR SUPPORT. CRACKED. CABIN FLOOR INTERCOSTAL CRACKED AT STA 540 RBL 1. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02 - [SDR SWAA2024110648128](https://openairdocs.org/sdr/SWAA2024110648128), Oct 13, 2024: SKIN. DELAMINATED. LEFT WING OUTBOARD AFT FLAP; THE INBOARD UPPER SURFACE HAS AN AREA OF DELAMINATION. (MARKED)<[01] REMOVED L/H OUTBD AFT FLAP PER AMM 27-51-22;[02] INSTALLED SER - [SDR SWAA2024110747347](https://openairdocs.org/sdr/SWAA2024110747347), Oct 10, 2024: SKIN. DELAMINATED. LEFT WING INBOARD MAIN FLAP TRAILING EDGE WEDGE IS DELAMINATED ON TRAILING EDGE.<[01] REMOVED LEFT WING INBOARD MAIN FLAP TRAILING EDGE WEDGE PER SRM 51-40-02.; - [SDR SWAA2024110746936](https://openairdocs.org/sdr/SWAA2024110746936), Oct 9, 2024: ANGLE. CRACKED. LT WING L-ANGLE CRACKED AT DEFLECTION RIB O/B #3 FLAP TRACK AT FWD WEB SUPPORT<[01] REMOVED ANGLE FROM AIRCRAFT I.A.W SRM 51-40-02.;[02] REMOVED AND REPLACED DE - [SDR SWAA2024110646344](https://openairdocs.org/sdr/SWAA2024110646344), Oct 8, 2024: VAPOR BARRIER. CRACKED. L/H A/C BAY AFT WALL UPPER ANGLE TO VAPOR BARRIER CRACKED AT FASTENER HOLE AT APPROX. STA.663; LBL-9'.<[01] REMOVED FASTENERS FOR VAPOR BARRIER ANGLE REPAIR IAW - [SDR SWAA2024110646343](https://openairdocs.org/sdr/SWAA2024110646343), Oct 8, 2024: VAPOR BARRIER. CRACKED. R/H A/C BAY AFT WALL UPPER ANGLE TO VAPOR BARRIER CRACKED AT FASTENER HOLE AT APPROX. STA.663; RBL-9'.<[01] SIGNED STEPS 1;2;3 AND 5;[02] INSPECTED WORK ACCOMPL - [SDR SWAA2024100343541](https://openairdocs.org/sdr/SWAA2024100343541), Sep 30, 2024: LIGHT. INOPERATIVE. FWD R/H EMERGENCY LIGHT INOP AND AFT R/H SIDE EMERGENCY LIGHT INOP<[01] RELAMPED RH FWD & AFT RH EMERGENCY LIGHTS IAW AMM 33-51-04 OP CHECK GOOD. - [SDR SWAA2024091034840](https://openairdocs.org/sdr/SWAA2024091034840), Sep 6, 2024: BATTERY PACK. INOPERATIVE. MULTIPLE EMERGENCY LIGHTS INOP (LH 4;5;6 AREA LIGHT; LH WING TO BODY)<[01] R&R EMERGENCY LIGHT CHARGER AND BATTERY PACK AT M1670 OPS OK IAW AMM 33-51-06. - [SDR SWAA2024050983962](https://openairdocs.org/sdr/SWAA2024050983962), May 9, 2024: FAIRING. CRACKED. #2 ENGINE STRUT AFT FAIRING STRUCTURE CRACK. STARTED REMOVAL OF #2 ENGINE AFT FAIRING WEDGE PER SRM 51-40-02. R & R RT STRUT AFT FAIRING IB PANEL IAW SRM 51-40- - [SDR SWAA2024050983474](https://openairdocs.org/sdr/SWAA2024050983474), May 8, 2024: WEB. CRACKED. #2 ENGINE AFT PYLON TE WEDGE FWD WEB CRACKED. CRACK TERMINATES AT EDGE OF MATERIAL AND UNDER OVERLAP; APPR 2.5 IN LENGTH<[01] 04 - REPAIRED PER EA-GENERAL 24-15 - [SDR SWAA2024050983479](https://openairdocs.org/sdr/SWAA2024050983479), May 8, 2024: SEAL. CRACKED. LEFT HORIZONTAL STABILIZER UPPER FORWARD SLIDER CRACKED.<[01] R/R LEFT HORIZ STAB FORWARD UPPER SPAR SLIDING SEAL REF AMM 53-31-31. - [SDR SWAA2024050380836](https://openairdocs.org/sdr/SWAA2024050380836), Apr 29, 2024: SENSING ELEMENT. SHORTED. WHEEL WELL FIRE LIGHT ON DECENT. INDICATION EXTINGUISHED ON GEAR EXTENTION. NO ABNORMAL SMELLS NOTED.<[01] OK TO CONTINUE PER MEL 26-4-01 SP#1 & SP#3;[02] PERFO - [SDR SWAA2024041774682](https://openairdocs.org/sdr/SWAA2024041774682), Apr 14, 2024: BATTERY. INOPERATIVE. AFT GALLEY FLASHLIGHT WILL NOT TURN OFF<[01] 01 - REMOVED AND REPLACED PER [AMM 25-64-00-900-806-NG (FLASHLIGHT BATTERY REPLACEMENT - PERMANENT)]
RR?D AFT GA - [SDR SWAA2024010336791](https://openairdocs.org/sdr/SWAA2024010336791), Jan 1, 2024: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS MID CABIN LEFT SIDE INOP<[01] REMOVED AND REPLACED M1670 EMERGENCY LIGHT POWER SUPPLY BATTERY PACK PER AMM 33-51-06; SYSTEM OPT CHECKS GOOD - [SDR SWAA2023091499623](https://openairdocs.org/sdr/SWAA2023091499623), Sep 13, 2023: GAUGE. OUT OF POSITION. PLASTIC COVER OVER AFT SLIDE PRESSURE GAGE OUT OF POSITION. INSTALLED NEW R2 SLIDE GAUGE WINDOW IAW SIP. NO DEFECTS NOTED. PLACARDS REMOVED AND MX PROCEDURES C/ - [SDR SWAA2023082390447](https://openairdocs.org/sdr/SWAA2023082390447), Aug 18, 2023: BATTERY PACK. DAMAGED. AFT GALLEY R/H EMERGENCY BATTERY PACK CHARGER PUSH TO TEST BUTTON IS DAMAGED<[01] REMOVED AND REPLACED AFT GALLEY EMERGENCY LIGHT BATTERY CHARGER AND PERFORMED - [SDR SWAA2023082288726](https://openairdocs.org/sdr/SWAA2023082288726), Aug 12, 2023: LIGHT. BROKEN. AFT CEILING EXIT LIGHT IS BROKEN.<[01] R&R AFT CEILING EXIT LIGHT BALLAST PER AMM 33-51-01.;[02] AFT CEILING EXIT LIGHT NEEDS OPS CHECK.;[03] INSPECTION C/W C/A - [SDR SWAA2023082288843](https://openairdocs.org/sdr/SWAA2023082288843), Aug 12, 2023: SIGN. BROKEN. AFT ENTRY DOOR EXIT SIGN BALLAST IS BROKEN.<[01] R&R AFT ENTRY DOOR EXIT SIGN BALLAST.;[02] AFT ENTRY DOOR EXIT SIGN NEEDS OPS CHECK.;[03] INSPECTION C/W C/A#1 - [SDR SWAA2023082387651](https://openairdocs.org/sdr/SWAA2023082387651), Aug 10, 2023: STRAP. CORRODED. AFT CARGO FLOOR BOARD STRAP DAMAGED AT 727-I<[01] REMOVED STRAP AND REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (REMAINING THICKNESS 0.052'). STRAP IS OUT - [SDR SWAA2023083095000](https://openairdocs.org/sdr/SWAA2023083095000), Aug 5, 2023: FLOOR PANEL. CORRODED. PNL 120CF HAS CORROSION ALONG THE SIDES.<[01] REMOVED AND REPLACED WITH NEW PANEL PER AMM 25-52-10;[02] C/W INSPECTION - [SDR SWAA2023082286270](https://openairdocs.org/sdr/SWAA2023082286270), Aug 5, 2023: FLOOR PANEL. CORRODED. PNL 120DF HAS CORROSION ALONG THE SIDES.<[01] REPLACED AND INSTALLED NEW FLOOR PANEL PER AMM 25-52-10 SEE TASK TTG8Q00MN032 FOR FLOOR PANEL SEALANT;[02] VERIFIE - [SDR SWAA2023082487016](https://openairdocs.org/sdr/SWAA2023082487016), Aug 3, 2023: WEB. CRACKED. #1 ENGINE; I/B FAN COWL; WEB CRACKED BELOW OIL SERVICE DOOR<[01] REMOVED AND REPLACED WEB IAW SRM 51-40-02 - [SDR SWAA2023082383853](https://openairdocs.org/sdr/SWAA2023082383853), Jul 30, 2023: ANGLE. CORRODED. AFT CARGO R/H TRANSITION ANGLE CORROSION STA 727D-727E<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVED TO BE .002 INCHES IN DEPTH. DAMAGE FOUND - [SDR SWAA2023082383850](https://openairdocs.org/sdr/SWAA2023082383850), Jul 30, 2023: ANGLE. CORRODED. AFT CARGO R/H TRANSITION ANGLE CORROSION STA 727J-747<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVAL TO BE .022 INCHES IN DEPTH. DAMAGE FOUND T - [SDR SWAA2023082383872](https://openairdocs.org/sdr/SWAA2023082383872), Jul 30, 2023: ANGLE. CORRODED. AFT CARGO R/H TRANSITION ANGLE CORROSION STA 727I-727J<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVAL TO BE .008 INCHES IN DEPTH. DAMAGE FOUND - [SDR SWAA2023082383851](https://openairdocs.org/sdr/SWAA2023082383851), Jul 30, 2023: ANGLE. CORRODED. AFT CARGO R/H TRANSITION ANGLE CORROSION STA 727G-727H<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVED TO BE .002 INCHES IN DEPTH. DAMAGE FOUND - [SDR SWAA2023082383873](https://openairdocs.org/sdr/SWAA2023082383873), Jul 30, 2023: ANGLE. CORRODED. AFT CARGO R/H TRANSITION ANGLE CORROSION STA 727F-727G<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVED TO BE .003 INCHES IN DEPTH. DAMAGE FOUND - [SDR SWAA2023082383852](https://openairdocs.org/sdr/SWAA2023082383852), Jul 30, 2023: ANGLE. CORRODED. AFT CARGO R/H TRANSITION ANGLE CORROSION STA 727E-727F<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVED TO BE .001 INCHES IN DEPTH. DAMAGE FOUND - [SDR SWAA2023082383854](https://openairdocs.org/sdr/SWAA2023082383854), Jul 30, 2023: ANGLE. CORRODED. AFT CARGO L/H TRANSITION ANGLE CORROSION STA 787-807<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVED TO BE .003 INCHES IN DEPTH. DAMAGE FOUND TO - [SDR SWAA2023082383875](https://openairdocs.org/sdr/SWAA2023082383875), Jul 30, 2023: ANGLE. CORRODED. AFT CARGO L/H TRANSITION ANGLE CORROSION STA 747-767<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVED TO BE .006 INCHES IN DEPTH. DAMAGE FOUND TO - [SDR SWAA2023082383855](https://openairdocs.org/sdr/SWAA2023082383855), Jul 30, 2023: ANGLE. CORRODED. AFT CARGO L/H TRANSITION ANGLE CORROSION STA 767-787<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVED TO BE .001 INCHES IN DEPTH. DAMAGE FOUND TO - [SDR SWAA2023082383856](https://openairdocs.org/sdr/SWAA2023082383856), Jul 30, 2023: ANGLE. CORRODED. AFT CARGO L/H TRANSITION ANGLE CORROSION STA 727I-727J<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVAL TO BE .008 INCHES IN DEPTH. DAMAGE FOUND - [SDR SWAA2023082383876](https://openairdocs.org/sdr/SWAA2023082383876), Jul 30, 2023: ANGLE. CORRODED. AFT CARGO L/H TRANSITION ANGLE CORROSION STA 727H-727I<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVAL TO BE .002 INCHES IN DEPTH. DAMAGE FOUND - [SDR SWAA2023082383877](https://openairdocs.org/sdr/SWAA2023082383877), Jul 30, 2023: ANGLE. CORRODED. AFT CARGO L/H TRANSITION ANGLE CORROSION STA 727G-727H<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVAL TO BE .003 INCHES IN DEPTH. DAMAGE FOUND - [SDR SWAA2023082383878](https://openairdocs.org/sdr/SWAA2023082383878), Jul 30, 2023: ANGLE. CORRODED. AFT CARGO L/H TRANSITION ANGLE CORROSION STA 727F-727G<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVAL TO BE .003 INCHES IN DEPTH. DAMAGE FOUND - [SDR SWAA2023082383879](https://openairdocs.org/sdr/SWAA2023082383879), Jul 30, 2023: ANGLE. CORRODED. AFT CARGO L/H TRANSITION ANGLE CORROSION STA 727E-727F<[01] REMOVED DAMAGE I.A.W SRM 51-10-02. MEASURED DAMAGE REMOVAL TO BE .001 INCHES IN DEPTH. DAMAGE FOUND All 98: https://openairdocs.org/aircraft/N8671D/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 N8671D The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N8671D before. - [Cancelled 1976-06-24](https://openairdocs.org/deregistered/N8671D-1976-06-24): Piper PA-18A, S/N 18-6267. Exported to Canada. Owner: [Wings North Inc](https://openairdocs.org/faa-owner/WINGS%20NORTH%20INC), [Stillwater I, MN](https://openairdocs.org/faa-place/MN/Stillwater%20I) ## 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.