# N8611F: 2013 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: 36892
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 27, 2013
- Certificate issued: December 17, 2024
- Expires: December 31, 2031
- Mode S code: ABD50F
- 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=8611F
- Page: https://openairdocs.org/aircraft/N8611F

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 N8611F.

## NTSB investigations on N8611F 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 FTW80FPA01](https://openairdocs.org/ntsb/FTW80FPA01), Oct 9, 1979: Hughes 369D (N8611F), Dallas, TX, substantial damage

## FAA accident and incident reports

None matched to N8611F.

## Reports on N8611F not matched to an aircraft (2)

They name N8611F, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19830929062929I](https://openairdocs.org/incident/19830929062929I), Sep 29, 1983: Hughes 369D (N8611F), Overland Park, KS. RPM fluctuation during traffic survey. Landed in a field. Erratic turbine governor.
- [Accident 19791009027769A](https://openairdocs.org/incident/19791009027769A), Oct 9, 1979: Hughes 369D (N8611F), Dallas, TX, Substantial damage. Diode failed in the "fuel low" warning light.

## Service difficulty reports (205, 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 SWAA2026081964634](https://openairdocs.org/sdr/SWAA2026081964634), Aug 15, 2026: BATTERY. NO TEST. FWD FLIGHT ATTENDANT SEAT BOTH FLASH LIGHTS REQUIRES BATTERY REPLACEMENT. REMOVED AND REPLACED THE BATTERY IAW AMM 25-64-00-900-806-NG.
- [SDR SWAA2026081921111](https://openairdocs.org/sdr/SWAA2026081921111), Aug 15, 2026: BATTERY. NO TEST. AFT FLIGHT ATTENDANT SEAT BOTH STATION FLASHLIGHTS REQUIRES BATTERY REPLACEMENT. REMOVED AND REPLACED THE BATTERY IAW AMM 25-64-00-900-806-NG.
- [SDR SWAA2026081983985](https://openairdocs.org/sdr/SWAA2026081983985), Aug 15, 2026: BATTERY. NO TEST. AT FWD FLIGHT ATTENDANT SEAT, BOTH FLASHLIGHTS REQUIRES BATTERY REPLACEMENT. REMOVED AND REPLACED THE BATTERY IAW AMM 25-64-00-900-806.
- [SDR SWAA2026081915877](https://openairdocs.org/sdr/SWAA2026081915877), Aug 15, 2026: BATTERY. NO TEST. AFT FLIGHT ATTENDANT SEAT BOTH STATION FLASH LIGHTS REQUIRES BATTERY REPLACEMENT. R & R THE BATTERY IAW AMM 25-64-00-900-806.
- [SDR SWAA2026061612755](https://openairdocs.org/sdr/SWAA2026061612755), Jun 15, 2026: SLIDE. OUT OF POSITION. L1 DOOR SLIDE FELL OUT OF BUSSEL. SECURED L1 DOOR SLIDE Z-FLAP AMM 25-66-01
- [SDR SWAA2026031679605](https://openairdocs.org/sdr/SWAA2026031679605), Mar 14, 2026: LAMP. INOPERATIVE. LT FWD EMERGENCY WINDOW FWD LOWER EXIT SIGN IS DIM, BULB OUT. REPLACED THE LAMP AND PERFORMED A GOOD OPS TEST IAW AMM 33-51-01-960-801.
- [SDR SWAA2026031679607](https://openairdocs.org/sdr/SWAA2026031679607), Mar 14, 2026: HANDLE. LOOSE. FED; AED; ASD DOOR ASSIST HANDLE IS LOOSE<[01] INSTALLED FWD ENTRY DOOR ASSIST HANDLE IAW AMM 52-11-31-400-802. INSTALLED AFT SERVICE DOOR ASSIST HANDLE IAW AMM
- [SDR SWAA2026031678847](https://openairdocs.org/sdr/SWAA2026031678847), Mar 11, 2026: LAMP. INOPERATIVE. EMERGENCY EXIT SIGN LOWER AREA AFT OWE IS INOPERATIVE. RELAMPED AND PERFORMED GOOD TEST OF RH EMERGENCY EXIT SIGN LOWER AREA AFT OWE IAW AMM 33-51-01-960-801;[0
- [SDR SWAA2026031678706](https://openairdocs.org/sdr/SWAA2026031678706), Mar 11, 2026: HANDLE. LOOSE. FWD SERVICE DOOR ASSIST HANDLE IS LOOSE. TIGHTENED FWD SERVICE DOOR ASSIST HANDLE IAW AMM 52-412-31-400-802 STEPS 3. F. (2) (A-D).
- [SDR SWAA2026031678083](https://openairdocs.org/sdr/SWAA2026031678083), Mar 10, 2026: BULB. BURNED OUT. R/H SIDE G4 EMERGENCY EXIT LIGHT HAS 2 BURNT OUT BULBS. REPLACED LIGHT BULBS ON THE RIGHT SIDE G4 EMEREGENCY EXIT LIGHT, PERFORMED GOOD TEST PER AMM 33-51-01-96
- [SDR SWAA2026031676888](https://openairdocs.org/sdr/SWAA2026031676888), Mar 5, 2026: HANDLE. BROKEN. G1 DOOR ASSIST HANDLE FOUND BROKEN. REMOVED AND REINSTALLED THE GALLEY 1 DOOR ASSIST HANDLE WITH NEW PARTS IAW AMM 52-11-31-400-802; AMM SUBTASK 52-11-31-020-01
- [SDR SWAA2026031676607](https://openairdocs.org/sdr/SWAA2026031676607), Mar 4, 2026: RECEIVER. BROKEN. OWE LT FWD EMERGENCY LIGHT ASSY RECEPTACLE IS BROKEN. REMOVED AND REPLACED IAW AMM 33-21-00-960-805-NG.
- [SDR SWAA2025100220243](https://openairdocs.org/sdr/SWAA2025100220243), Oct 1, 2025: COVER. OUT OF POSITION. FA REPORTS AFT ENTRY ESCAPE SLIDEPULL HANDLE SHOWING. REPOSITIONED PULL HANDLE COVER REF MM 25-66-01.
- [SDR SWAA2025091514540](https://openairdocs.org/sdr/SWAA2025091514540), Sep 13, 2025: COVER. MISSING. EXIT ROW; RIGHT SIDE; EXIT PLACARD MISSING. REPLACED EMERGENFCY LIGHT COVER IAW AMM 33-51-01.
- [SDR SWAA2025061279607](https://openairdocs.org/sdr/SWAA2025061279607), Jun 9, 2025: TABLE. STUCK. PASSENGER SEAT TRAY TABLE STICKING SLIDE ON BACK OF SEAT LOCATIONS: 15A; 15D; 23B; 25D; 25E AND 25F.<[01] CLEANED AND RESECURED PASSENGER SEAT TRAY TABLE SLIDES
- [SDR SWAA2025061279605](https://openairdocs.org/sdr/SWAA2025061279605), Jun 9, 2025: TABLE. LOOSE. PASSENGER SEAT TRAY TABLE LOOSE AT SLIDE ATTACH SCREWS ON BACK OF SEAT LOCATIONS: 14E; 14D; 16B; 16D; 16E; 16F; 17E; 17F; 18E AND 18F.<[01] RESECURED TRAY TABLE
- [SDR SWAA2025042945992](https://openairdocs.org/sdr/SWAA2025042945992), Apr 25, 2025: HANDLE. DAMAGED. AFT ENTRY DOOR ASSIST HANDLE DAMAGED.<[01] R&R AFT ENTRY DOOR ASSIST HANDLE/NUTS IAW AMM 52-00-00.
- [SDR SWAA2025033119750](https://openairdocs.org/sdr/SWAA2025033119750), Mar 29, 2025: COVER. LOOSE. AFT EMERGENCY EXIT LIGHT LENSE COVER CAME OFF<[01] REINSTALLED LIGHT COVER IAW AMM 33-51-01
- [SDR SWAA2025020587984](https://openairdocs.org/sdr/SWAA2025020587984), Jan 21, 2025: LIGHT. CRACKED. CRACK ON PHOTOLUMINESCENT STRIPS RH SIDE 8 EA IN PASSENGER CABIN 2024-77957 2<[01]. REPLACED PHOTOLUMINESCENT STRIPS RH SIDE 8 EA IN PASSENGER CABIN IAW B737-80
- [SDR SWAA2025021086178](https://openairdocs.org/sdr/SWAA2025021086178), Jan 15, 2025: BATTERY PACK. INOPERATIVE. DOES NOT WORK CORRECTLY BATERY PACK LOCATED ON CEILING PANEL AT FWD GALLEY AREA LATERAL POSITION 1EA 2024-779533<[01] REPLACED BATERY PACK LOCATED ON CEILING PA
- [SDR SWAA2025020586179](https://openairdocs.org/sdr/SWAA2025020586179), Jan 15, 2025: BATTERY PACK. INOPERATIVE. DOES NOT WORK CORRECTLY BATTERY PACK LOCATED ON FWD CEILING PANEL AT FWD GALLEY AREA CENTER POSITION 1 EA 2024-779534<[01] REPLACED BATTERY PACK LOCATED ON FWD 
- [SDR SWAA2025020586562](https://openairdocs.org/sdr/SWAA2025020586562), Jan 15, 2025: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS500I AND STR28L AFT POSITION FWD CARGO COMPARTMENT 2024-779547<[01]. REPLACED SUPPORT ANGLE LOCATED BS500I AND STR28L AFT POSITI
- [SDR SWAA2025020586561](https://openairdocs.org/sdr/SWAA2025020586561), Jan 15, 2025: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS500I AND STR28R AFT POSITION FWD CARGO COMPARTMENT 2024-779548<[01]. REPLACED ANGLE SUPPORT LOCATED BS500I AND STR28R AFT POSITI
- [SDR SWAA2025020586563](https://openairdocs.org/sdr/SWAA2025020586563), Jan 15, 2025: PANEL. CORRODED. CORROSION ON SUPPORT PANEL LOCATED BS 992.8 BTW LBL 43 TO LBL 53 WL 208.1 AT AFT GALLEY AREA. 2024-779551<[01] REPLACED SUPPORT PANEL LOCATED BS 992.8 BTW LBL 4
- [SDR SWAA2025021185329](https://openairdocs.org/sdr/SWAA2025021185329), Jan 12, 2025: SEAL PLATE. CRACKED. CRACK SEAL - PLATE ACCESS PANEL 343AT AT RT HORIZONTAL STABILIZER 2024-779505<[01] REPLACED SEAL - PLATE LOCATED ON ACCESS PANEL 343AT AT RT HORIZONTAL STABILIZ
- [SDR SWAA2025021185332](https://openairdocs.org/sdr/SWAA2025021185332), Jan 12, 2025: ANGLE. CRACKED. CRACK SEAL - PLATE ANGLE ACCESS PANEL 343AT AT RT HORIZONTAL STABILIZER 2024-779506<[01] TASK COMPLETED FOR REPLACE SEAL - PLATE ANGLE LOCATED ON ACCESS PANEL 3
- [SDR SWAA2025020585335](https://openairdocs.org/sdr/SWAA2025020585335), Jan 12, 2025: SCUFF PLATE. CRACKED. CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2024-779511<[01]. TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N :1859843 ; DUE DATE: 10/MAR/25; [
- [SDR SWAA2025021184638](https://openairdocs.org/sdr/SWAA2025021184638), Jan 9, 2025: NUT PLATE. CORRODED. CORROSION RAIL NUT PLATES INTERNAL CAVITY LOCATED OFSS94 LEADING EDGE AT LT WING 2024-779438<[01] REPLACED RAIL NUT PLATES INTERNAL CAVITY AND FASTENERS LOCATED
- [SDR SWAA2025021184642](https://openairdocs.org/sdr/SWAA2025021184642), Jan 9, 2025: NUT PLATE. CORRODED. CORROSION RAIL NUT PLATES INTERNAL CAVITY LOCATED OFSS449 LEADING EDGE AT LT WING 2024-779439<[01] REPLACED RAIL NUT PLATES INTERNAL CAVITY LOCATED OFSS449 LEAD
- [SDR SWAA2025021184636](https://openairdocs.org/sdr/SWAA2025021184636), Jan 9, 2025: ANGLE. CRACKED. CRACK ANGLE AUXILIARY TRACK ON SLAT #8 AT RT WING 2024-779432<[01] REPLACED ANGLE LOCATED ON AUXILIARY TRACK ON SLAT #8 AT RT WING IAW B737-800 SRM 51-40-02-0G.
- [SDR SWAA2025021184633](https://openairdocs.org/sdr/SWAA2025021184633), Jan 9, 2025: SUPPORT ANGLE. CRACKED. CRACK ANGLE SUPPORT STRUCTURE WING TO BODY FAIRING LOCATED BS500I BETWEEN S-18R TO S-20R FUSELAGE EXTERIOR 2024-779428<[01] TOOL USED: POWER PACK: P/N: FMK00032
- [SDR SWAA2025021184634](https://openairdocs.org/sdr/SWAA2025021184634), Jan 9, 2025: SUPPORT ANGLE. CRACKED. CRACK ANGLE SUPPORT STRUCTURE WING TO BODY FAIRING LOCATED BS 540 AT LEVEL S-22L FUSELAGE EXTERIOR 2024-779430<[01] REPLACED ANGLE SUPPORT STRUCTURE WING TO BOD
- [SDR SWAA2025021084794](https://openairdocs.org/sdr/SWAA2025021084794), Jan 9, 2025: BALANCE WEIGHT. OUT OF BALANCE. DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR RT PN:183A0103-22 SN:0 05242 FOUND BALANCE WEIGHTS PN:183A0210-15 (1 EA) ON BAY 4 PN:183A0210 -14 (1 EA) ON BAY 
- [SDR SWAA2025020584632](https://openairdocs.org/sdr/SWAA2025020584632), Jan 9, 2025: SUPPORT BRACKET. CRACKED. CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2024-779426<[01] REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT
- [SDR SWAA2025020584640](https://openairdocs.org/sdr/SWAA2025020584640), Jan 9, 2025: GUSSET. CRACKED. CRACK ON GUSSET LOCATED BS500I AND STR21R AT FWD CARGO COMPARTMENT 2024-779435<[01]. REPLACED GUSSET AND FASTENERS LOCATED BS500I AND STR21R AT FWD CARGO COMPAR
- [SDR SWAA2025020584639](https://openairdocs.org/sdr/SWAA2025020584639), Jan 9, 2025: GUSSET. CRACKED. CRACK ON GUSSET LOCATED BS500I AND STR21L AT FWD CARGO COMPARTMENT 2024-779434 <[01]. REPLACED GUSSET LOCATED BS500I AND STR21L AT FWD CARGO COMPARTMENT IAW B73
- [SDR SWAA2025020584637](https://openairdocs.org/sdr/SWAA2025020584637), Jan 9, 2025: RAIL. CORRODED. CORROSION RAIL NUT PLATES INTERNAL CAVITY LOCATED OFSS52 LEADING EDGE AT LT WING 2024-779437<[01] REPLACED RAIL NUT PLATES INTERNAL CAVITY AND FASTENERS LOCATED
- [SDR SWAA2025020484635](https://openairdocs.org/sdr/SWAA2025020484635), Jan 9, 2025: ANGLE. CRACKED. CRACK ON ANGLE LOCATED ACCESS 844DZ AT AFT GALLEY SERVICE DOOR 2024-779431<[01]. REPLACED ANGLE LOCATED ACCESS 844DZ AT AFT GALLEY SERVICE DOOR I.A.W. B737-800 
- [SDR SWAA2025020484452](https://openairdocs.org/sdr/SWAA2025020484452), Jan 8, 2025: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 241XF AT AFT GALLEY AREA 2024-779398 <[01]. REPLACED FLOOR PANEL 241XF AT AFT GALLEY AREA IAW B737-800 AMM 53-21-00-400-801 THE INSTALLA
- [SDR SWAA2025020484453](https://openairdocs.org/sdr/SWAA2025020484453), Jan 8, 2025: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 241AAF AT AFT GALLEY AREA 2024-779399 <[01]. REPLACED FLOOR PANEL 241AAF AT AFT GALLEY AREA IAW B737-800 AMM 53-21-00-400-801. THE INSTA
- [SDR SWAA2025020484454](https://openairdocs.org/sdr/SWAA2025020484454), Jan 8, 2025: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 242UF AT AFT GALLEY AREA 2024-779400<[01] REPLACED FLOOR PANEL 242UF AT AFT GALLEY AREA IAW B737-800 AMM 53-21-00-400-801 THE INSTALLATI
- [SDR SWAA2025020484455](https://openairdocs.org/sdr/SWAA2025020484455), Jan 8, 2025: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 242E AT AFT GALLEY AREA 2024-779401<[01] REPLACED FLOOR PANEL 242E AT AFT GALLEY AREA IAW B737-800 AMM 53-21-00-400-801 THE INSTALLATION
- [SDR SWAA2025020484456](https://openairdocs.org/sdr/SWAA2025020484456), Jan 8, 2025: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 241ABF AT AFT GALLEY AREA 2024-779402<[01]. REPLACED FLOOR PANEL 241ABF AT AFT GALLEY AREA IAW B737-800 AMM 53-21-00-400-801; THE INSTAL
- [SDR SWAA2025020584039](https://openairdocs.org/sdr/SWAA2025020584039), Jan 7, 2025: FRAME. CRACKED. CRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2024-779365<[01] REPAIRED FRAME ON BS 312 BETWEEN S-5L AND S-6L AT FWD GALLEY AREA IAW B73
- [SDR SWAA2025020584038](https://openairdocs.org/sdr/SWAA2025020584038), Jan 7, 2025: ANGLE. CRACKED. CRACK ANGLE - CLIP LOCATED BS500H AND RBL21 AFT POSITION FWD CARGO COMPARTMENT 2024-779349 CORRECTED LOCATED 25 RBL. <[01] REPLACED ANGLE - CLIP AND FASTENERS L
- [SDR SWAA2025020584040](https://openairdocs.org/sdr/SWAA2025020584040), Jan 7, 2025: ANGLE. CRACKED. CRACK ANGLE - CLIP LOCATED BS500H AND LBL25 FWD POSITION FWD CARGO COMPARTMENT 2024-779354 <[01]. REPLACED ANGLE - CLIP LOCATED BS500H AND LBL25 FWD POSITION FW
- [SDR SWAA2025020584041](https://openairdocs.org/sdr/SWAA2025020584041), Jan 7, 2025: ANGLE. CRACKED. CRACK ANGLE - CLIP LOCATED BS500G AND LBL21 FWD POSITION FWD CARGO COMPARTMENT 2024-779355 <[01]. REPLACED NEW ANGLE - CLIP LOCATED BS500G AND LBL21 FWD POSITIO
- [SDR SWAA2025020584044](https://openairdocs.org/sdr/SWAA2025020584044), Jan 7, 2025: ANGLE. CRACKED. CRACK ANGLE - CLIP LOCATED BS500H AND RBL25 FWD POSITION FWD CARGO COMPARTMENT 2024-779350<[01]. REPLACED ANGLE - CLIP AND FASTENERS LOCATED BS500H AND RBL25 FW
- [SDR SWAA2025020584046](https://openairdocs.org/sdr/SWAA2025020584046), Jan 7, 2025: ANGLE. CRACKED. CRACK ANGLE - CLIP LOCATED BS500H AND LBL25 AFT POSITION FWD CARGO COMPARTMENT 2024-779352<[01]. REPLACED ANGLE - CLIP LOCATED BS500H AND LBL25 AFT POSITION FWD
- [SDR SWAA2025020584047](https://openairdocs.org/sdr/SWAA2025020584047), Jan 7, 2025: ANGLE. CRACKED. CRACK ANGLE - CLIP LOCATED BS500F AND LBL25 FWD POSITION FWD CARGO COMPARTMENT 2024-779357<[01]. REPLACED ANGLE - CLIP LOCATED BS500F AND LBL25 FWD POSITION FWD

All 205: https://openairdocs.org/aircraft/N8611F/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

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