# N8673F: 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: 36937 - Year built: 2015 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 1, 2015 - Certificate issued: December 18, 2024 - Expires: December 31, 2031 - Mode S code: ABEB9F - 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=8673F - Page: https://openairdocs.org/aircraft/N8673F 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 N8673F. ## NTSB investigations on N8673F not matched to an aircraft (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB LAX80DUJ06](https://openairdocs.org/ntsb/LAX80DUJ06), Oct 23, 1979: Hughes 369D (N8673F), Phoenix, AZ, substantial damage ## FAA accident and incident reports None matched to N8673F. ## Reports on N8673F not matched to an aircraft (1) They name N8673F, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Accident 19791023031539A](https://openairdocs.org/incident/19791023031539A), Oct 23, 1979: Hughes 369D (N8673F), Phoenix, AZ, Substantial damage. Engine stopped. Pilot made hard autorotate landing. Found failed turbine seals. Caused bearing failure. ## Service difficulty reports (126, 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 SWAA2026092148874](https://openairdocs.org/sdr/SWAA2026092148874), Sep 17, 2026: HANDLE. BROKEN. FO`S GRAB HANDLE BROKEN. REPLACED FO`S GRAB HANDLE IAW STANDARD INDUSTRY PRACTICES. OPS CHKD GOOD. - [SDR SWAA2026082568398](https://openairdocs.org/sdr/SWAA2026082568398), Aug 18, 2026: SENSE LINE. FAULTED. ATB DUE TO RH LOW BLEED & LT PACK FLUCTUATING. O/W LANDING._ R & R NR 2 ENGINE PRECOOLER BRAIDED SENSE LINE PER MM 36-12-00 - [SDR SWAA2026072705973](https://openairdocs.org/sdr/SWAA2026072705973), Jul 24, 2026: ENGINE. FAILED. AT APPOX 30 KTS ON T/O ROLL WITH T/O PWR SET NR 2 ENG FAILED WITH AUDIBLE BANG AND RIGHT SWERVE. PERFORMED RTO. HAD ENG FAILED ON NR 2 EGT DISPLAY. AIRPORT OPS - [SDR SWAA2026081891593](https://openairdocs.org/sdr/SWAA2026081891593), Jul 23, 2026: ENGINE. FAILED. AT APPOX 30 KTS ON T/O ROLL WITH T/O PWR SET NR 2 ENG FAILED WITH AUDIBLE BANG AND RIGHT SWERVE. PERFORMED RTO. HAD ENG FAILED ON #2 EGT DISPLAY. AIRPORT OPS RE - [SDR SWAA2026012062750](https://openairdocs.org/sdr/SWAA2026012062750), Jan 19, 2026: LIGHT. INOPERATIVE. 15 ABC EMERGENCY EXIT INDICATOR LIGHT INOPERATIVE. REMOVED AND REPLACED 15 ABC EMERGENCY EXIT ASSEMBLY IAW AMM 33-51-01. - [SDR SWAA2025121750999](https://openairdocs.org/sdr/SWAA2025121750999), Dec 10, 2025: WIRE. CUT. EMERGENCY EXIT LIGHT ATTACHED TO RT SIDEWALL PANEL 242ZAW, FOUND TO HAVE CUT WIRES. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-14-960-802. PERFORMED - [SDR SWAA2025121849219](https://openairdocs.org/sdr/SWAA2025121849219), Dec 7, 2025: RETAINER. MISSING. RIGHT EMERGENCY EXIT FWD LENS RETAINER FOUND MISSING. FOUND AND INSTALLED THE MISSING RT, FWD LENS RETAINER IAW AMM 33-21-00-960-804. - [SDR SWAA2025121643747](https://openairdocs.org/sdr/SWAA2025121643747), Dec 7, 2025: RETAINER. MISSING. RIGHT EMERGENCY EXIT FWD LENS RETAINER FOUND MISSING. - [SDR SWAA2025110330438](https://openairdocs.org/sdr/SWAA2025110330438), Oct 30, 2025: LIGHT. UNSECURE. F/A REPORTS 4 INCH TRIPPING HAZARD, THE PHOTO LUMINESCENT STRIP IS STICKING UP ABOUT 4 INCHES AND IS A POTENTIAL TRIPPING HAZARD. ATTACHED AS NECESSARY IAW AMM - [SDR SWAA2025012288070](https://openairdocs.org/sdr/SWAA2025012288070), Jan 21, 2025: BATTERY PACK. INOPERATIVE. FWD AND AFT LH OVERWING EMERGENCY LIGHTS INOP<[01] CHANGED REASON CODE FOR REMOVAL FROM ROB TO CAUSE BY REQUEST FROM TRAVIS MCCLESTER X316070;[02] CERTIFIED;[03 - [SDR SWAA2025012287761](https://openairdocs.org/sdr/SWAA2025012287761), Jan 20, 2025: LATCH. MISSING. CR AH - RH EMERGENCY EXIT ROW SEATS 13DEF 14DEF MISSING ONE-WAY TRAY TABLE LATCHES<[01] REMOVED AND REPLACED 6 EACH SEAT TRAY TABLE LATCHES FOR ONE WAY LOCKING - [SDR SWAA2025012383733](https://openairdocs.org/sdr/SWAA2025012383733), Jan 7, 2025: SEAL. CRACKED. LEFT STABILIZER UPPER SLIDING SEAL WORN / CRACKED.<[01] REMOVED AND REPLACED SLIDING SEAL IAW B737-NG AMM 53-31-31;[02] VERIFIED REMOVED AND REPLACED SLIDING SE - [SDR SWAA2025012383732](https://openairdocs.org/sdr/SWAA2025012383732), Jan 7, 2025: SEAL. CRACKED. RIGHT HORIZONTAL STABILIZER UPPER SLIDING SEAL WORN / CRACKED.<[01] REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER UPPER SLIDING SEAL IAW B737NG AMM 53-31-31; - [SDR SWAA2025012382980](https://openairdocs.org/sdr/SWAA2025012382980), Jan 4, 2025: FLOOR SUPPORT. CRACKED. MAIN CABIN; 1 EACH FLOOR SUPPORT CRACKED AT BS 540 APPROX LBL-1. MARKED<[01] REMOVED; LOCATED; DRILLED; AND INSTALLED FLOOR SUPPORT REF B737-NG SRM 51-40-02 AND - [SDR SWAA2025012382976](https://openairdocs.org/sdr/SWAA2025012382976), Jan 4, 2025: FLOOR SUPPORT. CRACKED. MAIN CABIN; 1 EACH FLOOR SUPPORT CRACKED AT BS 540 APPROX RBL-1. MARKED<[01] REMOVED; LOCATED; DRILLED AND INSTALLED FLOOR SUPPORT REF BAC DWG 143A5240-63 REV A - [SDR SWAA2025012382572](https://openairdocs.org/sdr/SWAA2025012382572), Jan 3, 2025: SKIN. DELAMINATED. L/H O/B AFT FLAP DELAMINATED AT UPPER AND LOWER SKINS BETWEEN 72' INCHES AND 110' INCHES FROM I/B EDGE.<[01] 01 - REMOVED AND REPLACED PER [AMM 27-51-22-400-801 - [SDR SWAA2025012282750](https://openairdocs.org/sdr/SWAA2025012282750), Jan 3, 2025: STRAP. CORRODED. L/H EMERGENCY EXIT HATCH ESCAPE STRAP HOOK HAS CORROSION.<[01] REMOVED AND REPLACED L/H EMERGENCY EXIT HATCH ESCAPE STRAP IAW B737-800 SRM 51-40-02 & AMM 25-61- - [SDR SWAA2025012282564](https://openairdocs.org/sdr/SWAA2025012282564), Jan 2, 2025: HANDLE. MISSING. FWD CARGO DOOR ASSIST HANDLE IS MISSING UPPER CHORD<[01] INSTALLED FWD CARGO DOOR ASSIST HANDLE UPPER CHORD PN: 69-41730-85; PO#: 1110113.1 PER B737-800 AMM 52- - [SDR SWAA2025012282566](https://openairdocs.org/sdr/SWAA2025012282566), Jan 2, 2025: HANDLE. MISSING. AFT CARGO DOOR ASSIST HANDLE IS MISSING UPPER CHORD<[01] INSTALLED AFT CARGO DOOR ASSIST HANDLE UPPER CHORD PN:69-41730-86; PO#:1104656.2 PER B737-800 AMM 52-31 - [SDR SWAA2025012487078](https://openairdocs.org/sdr/SWAA2025012487078), Dec 31, 2024: BRACKET. DAMAGED. [DOT: Z047] RIGHT WING L/E CAVITY INBD OF PYLON HAS PNEUMATIC DUCT OTBD SUPPORT BRACKET HAS ELONGATED HOLES. (STREAMER ATTACH)<[01] REMOVED AND REPLACED R/W L/E - [SDR SWAA2025012487079](https://openairdocs.org/sdr/SWAA2025012487079), Dec 31, 2024: BRACKET. DAMAGED. [DOT: Z048] RIGHT WING L/E CAVITY INBD OF PYLON HAS PNEUMATIC DUCT INBD SUPPORT BRACKET HAS ELONGATED HOLE. (STREAMER ATTACH)<[01] REMOVED & REPLACED R/W L/E I/ - [SDR SWAA2025012282111](https://openairdocs.org/sdr/SWAA2025012282111), Dec 31, 2024: CAP. MISSING. AFT CARGO COMPARTMENT FWD BULKHEAD FLOOR CAP STRIP MISSING<[01] RECVD. AND INSTALLED NEW CAP STRIP PT.# 435A2511-2 IAW B737-800 SRM 51-40-02;[02] VERIFIED RECVD - [SDR SWAA2025012181905](https://openairdocs.org/sdr/SWAA2025012181905), Dec 31, 2024: LIGHT. INOPERATIVE. FLT DECK ENTRY EMERGENCY WHITE LIGHT ON BAR STRIP LIGHT INOP<[01] RE-LAMPED AND OP CHECKED LIGHT BAR IN EMERGENCY LIGHT IAW SWA 737-800 AMM 33-51-01-960-801. LI - [SDR SWAA2025012181904](https://openairdocs.org/sdr/SWAA2025012181904), Dec 31, 2024: LIGHT. BURNED OUT. R2 DOOR EMERGENCY LIGHT STRIP HAS BURNED OUT LIGHT<[01] REPLACED LAMP AT R2 DOOR EMERGENCY LIGHT STRIP AND PERFORMED A GOOD TEST OF THE R2 DOOR EMERGENCY LIGHT - [SDR SWAA2024061300431](https://openairdocs.org/sdr/SWAA2024061300431), Jun 10, 2024: SIGN. DETACHED. OVERWING EXIT SIGN COVER FELL OFF<[01] R&R?D OVERHEAD OVERWING EXIT SIGN ASSY PER M/M 33-51-01 OPS NORMAL. - [SDR SWAA2024030760334](https://openairdocs.org/sdr/SWAA2024030760334), Mar 7, 2024: COVER. DETACHED. OVER -WING EXIT SIGN COVER POPPED OFF<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-201-NG (EXIT SIGNS - MAINTENANCE PRACTICES - PERMANENT)]

REINSTALL - [SDR SWAA2024021251439](https://openairdocs.org/sdr/SWAA2024021251439), Feb 11, 2024: BATTERY PACK. INOPERATIVE. FO SIDE OVER WING EMERGENCY EXIT EMERGENCY LIGHTS INOP<[01] R&R BATTERY PACK REF AMM 33-51-06 OPS CHECK NORMAL - [SDR SWAA2023112020316](https://openairdocs.org/sdr/SWAA2023112020316), Nov 10, 2023: CAP. CORRODED. AFT PIT R/H CAP STRIP AFT OF DOOR HAS CORROSION. AFT PIT R/H CAP STRIP AFT OF DOOR HAS CORROSION<[01] REMOVED AND REPLACED AFT PIT R/H CAP STRIP PER SOPM 20-50- - [SDR SWAA2023111719950](https://openairdocs.org/sdr/SWAA2023111719950), Nov 10, 2023: FAIRING. DELAMINATED. NO. 7 FLAP TRACK SUPPORT FAIRING HAS A SMALL TEAR WITH DELAMINATION I/B SIDE OUTER SKIN<[01] REMOVED DAMAGE PER SRM 57-53-70-2R-1;[02] VERIFIED CORRECTIVE ACTIO - [SDR SWAA2023112019867](https://openairdocs.org/sdr/SWAA2023112019867), Nov 9, 2023: PANEL. DAMAGED. RH WING TRAILING EDGE SEAL PANEL 344EB HAS ELONGATED HOLES<[01] REMOVED AND REPLACED TRAILING EDGE SEAL PANEL #344EB;[02] RH HORIZONTAL STABILIZER IS WHERE 344E - [SDR SWAA2023112019056](https://openairdocs.org/sdr/SWAA2023112019056), Nov 7, 2023: BATTERY PACK. INOPERATIVE. RH FWD EMERGENCY LIGHT IN THE CABIN INOP<[01] REPLACED BATTERY PACK; LIGHTS TEST GOOD IAW AMM 33-51-06;[02] VERIFIED - [SDR SWAA2023112019057](https://openairdocs.org/sdr/SWAA2023112019057), Nov 7, 2023: BATTERY PACK. INOPERATIVE. LH AFT CABIN EMERGENCY LIGHTS INOP<[01] REPLACED BATTERY PACK; LIGHTS TEST GOOD IAW AMM 33-51-06;[02] VERIFIED - [SDR SWAA2023112019942](https://openairdocs.org/sdr/SWAA2023112019942), Nov 3, 2023: NUT PLATE. WRONG PART. LEFT HORIZONTAL STABILIZER LOWER TRAILING EDGE BEAM HAS INCORRECT NUT PLATE INSTALLED AT ELEVATOR STA 181.64 OUTBOARD OF NO.5 ELEVATOR HINGE. ADDITIONAL HOLE DR - [SDR SWAA2023112016525](https://openairdocs.org/sdr/SWAA2023112016525), Nov 1, 2023: TAIL CONE. ELONGATED. LH WING #3 CANOE FAIRING TAIL CONE BOLT HOLES ELONGATED<[01] REMOVED AND REPLACED TAIL CONE PER AMM 27-51-18 - [SDR SWAA2023112015139](https://openairdocs.org/sdr/SWAA2023112015139), Oct 26, 2023: SCUFF PLATE. CRACKED. AFT CARGO AFT CORNER SCUFF PLATE CRACKED.<[01] REMOVED AND REPLACED AFT CARGO; AFT CORNER SCUFF PLATE I.A.W AMM 53-11-02.;[02] REMOVED AND REPLACED AFT CARGO; A - [SDR SWAA2023112015218](https://openairdocs.org/sdr/SWAA2023112015218), Oct 26, 2023: TAIL CONE. DELAMINATED. TAIL CONE HAS 2EA. SMALL AREAS OF DELAMINATION R/H SIDE UPPER AFT MKD.<[01] REMOVED DAMAGE PER SRM 51-70-05 REPAIR 1.;[02] VERIFIED REMOVED DAMAGE PER SRM 51-70 - [SDR SWAA2023112014406](https://openairdocs.org/sdr/SWAA2023112014406), Oct 24, 2023: ANGLE. CORRODED. FWD CARGO HAS SURFACE CORROSION ON RT. TRANSITION ANGLE BS436-440<[01] CLEAN CORROSION PER SRM 51-10-02. REWORKED AREA IS OUT OF LIMIT PER SRM 53-00-53-1A-2 FIG - [SDR SWAA2023112014408](https://openairdocs.org/sdr/SWAA2023112014408), Oct 24, 2023: ANGLE. CORRODED. AFT CARGO STA. 727C-727G; CORROSION AROUND NUT=PLATE HOLES ON RT TRANSITION ANGLE.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (REMAINING THICKNESS 0.036'). TR - [SDR SWAA2023112014385](https://openairdocs.org/sdr/SWAA2023112014385), Oct 24, 2023: ANGLE. CORRODED. AFT CARGO STA. 727G-767; CORROSION AROUND NUT=PLATE HOLES ON RT TRANSITION ANGLE.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (REMAINING THICKNESS 0.036'). TRA - [SDR SWAA2023112014386](https://openairdocs.org/sdr/SWAA2023112014386), Oct 24, 2023: ANGLE. CORRODED. AFT CARGO STA. 727-727H; CORROSION AROUND NUT-PLATE HOLES ON LT TRANSITION ANGLE.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (REMAINING THICKNESS 0.034'). TRA - [SDR SWAA2023112014387](https://openairdocs.org/sdr/SWAA2023112014387), Oct 24, 2023: ANGLE. CORRODED. AFT CARGO STA. 727H-847; CORROSION AROUND NUT-PLATE HOLES ON LT TRANSITION ANGLE.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (REMAINING THICKNESS 0.022'). TRA - [SDR SWAA2023112014388](https://openairdocs.org/sdr/SWAA2023112014388), Oct 24, 2023: WEB. CORRODED. AFT CARGO STA. 767-790; CORROSION ON TOP AND BOTTOM SURFACES OF RT TRANSITION ANGLE AROUND NUT-PLATE HOLES.<[01] REMOVED CORROSION PER SRM 53-60-15-1A-1 (REMAIN - [SDR SWAA2023112014390](https://openairdocs.org/sdr/SWAA2023112014390), Oct 24, 2023: NUT PLATE. CORRODED. AFT CARGO STA.727D+4 LBL24-RBL2; CORROSION ON FLOORBOARD NUT-PLATE STRAP.<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2. (REMAINING THICKNESS 0.066'). STRAP IS O - [SDR SWAA2023112014391](https://openairdocs.org/sdr/SWAA2023112014391), Oct 24, 2023: NUT PLATE. CORRODED. AFT CARGO STA.767+4 LBL24-RBL24; CORROSION ON FLOORBOARD NUT-PLATE STRAP.<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2. (REMAINING THICKNESS 0.058'). - [SDR SWAA2023112014413](https://openairdocs.org/sdr/SWAA2023112014413), Oct 24, 2023: THRESHOLD. CORRODED. AFT CARGO ENTRY DOOR THRESHOLD STA. 790-847; CORROSION AROUND NUT-PLATE HOLES.<[01] REMOVED CORROSION FROM AREA PER SRM 53-60-15-1A-1 (REMAINING THICKNESS 0.042 - [SDR SWAA2023112014395](https://openairdocs.org/sdr/SWAA2023112014395), Oct 24, 2023: SUPPORT ANGLE. CRACKED. AFT CARGO STA. 867 LBL 16; LAV TANK POST HAS A CRACKED SUPPORT ANGLE AT BOTTOM INSIDE SURFACE.<[01] REMOVED SUPPORT ANGLE PER SRM 51-40-02; LOCATED AND DRILL NE - [SDR SWAA2023112013963](https://openairdocs.org/sdr/SWAA2023112013963), Oct 24, 2023: SUPPORT ANGLE. CORRODED. FWD GALLEY THRESHOLD SUPPORT ANGLE HAS CORROSION AT 3EA. N/P HOLES STA. 300 STA. 315 AND STA. 319 RBL 57-58. MRKD<[01] REMOVED CORROSION; FOUND OUT OF LIMITS PE - [SDR SWAA2023112013957](https://openairdocs.org/sdr/SWAA2023112013957), Oct 24, 2023: INTERCOSTAL. CRACKED. BETWEEN STATION 380 AND STATION 400; THE INTERCOSTAL AT LBL 51 HAS AN UPPER SURFACE CRACK.<[01] REMOVED DAMAGED PART FROM AIRCRAFT. DRILLED FASTENERS HOLES IN R - [SDR SWAA2023112013958](https://openairdocs.org/sdr/SWAA2023112013958), Oct 24, 2023: INTERCOSTAL. CRACKED. BETWEEN STATION 380 AND STATION 400; THE INTERCOSTAL AT LBL 13 HAS AN UPPER SURFACE CRACK.<[01] REMOVED DAMAGED PART FROM AIRCRAFT. DRILLED FASTENERS HOLES IN R - [SDR SWAA2023112014274](https://openairdocs.org/sdr/SWAA2023112014274), Oct 24, 2023: TAIL CONE. DELAMINATED. TAIL CONE HAS MULTIPLE DELAMINATED DENTS BETWEEN MULTIPLE COMPOSITE REPAIRS ON UPPER ON L/H SURFACES<[01] REMOVED DAMAGE IN AREAS OF DENTS MARKED PER SRM 51-70- All 126: https://openairdocs.org/aircraft/N8673F/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 ## 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.