# N8600F: 2012 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 CFM56-7B26E series](https://openairdocs.org/engine/cfm-international-cfm56-7b26e-series) (registry code 13099)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (The Boeing Company) (OpenAirDocs)
- Serial number: 39882
- Year built: 2012
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 16, 2012
- Certificate issued: May 2, 2012
- Expires: May 31, 2028
- Mode S code: ABD135
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8600F
- Page: https://openairdocs.org/aircraft/N8600F

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 CFM56-7B26E 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 CFM56-7B26E 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 N8600F.

## FAA accident and incident reports

None matched to N8600F.

## Service difficulty reports (188, 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 SWAA2026100141224](https://openairdocs.org/sdr/SWAA2026100141224), Sep 27, 2026: SIGN. DETACHED. LOWER EXIT SIGN 14ABC FELL OFF. CW EA M-21-133-00720
- [SDR SWAA2026062914555](https://openairdocs.org/sdr/SWAA2026062914555), Jun 22, 2026: ELEC CONNECTOR. DISCONNECTED. TWO RT AFT VALENCE AISLE LIGHTS INOPERATIVE. UPON INVESTIGATION; FOUND CONNECTORS D14708 AND D14832 DISCONNECTED. RECONNECTED CONNECTORS IAW WDM 33-51-14 AND PE
- [SDR SWAA2026062914070](https://openairdocs.org/sdr/SWAA2026062914070), Jun 20, 2026: BATTERY PACK. INOPERATIVE. ALL ASSOCIATED EMERGENCY LIGHTS FOR M2816 BATTERY PACK INOPERATIVE. REMOVED AND REPLACED BATTERY PACK M2816; PERFORMED GOOD OPS TEST IAW AMM TASK 33-51-00-710-8
- [SDR SWAA2026062914071](https://openairdocs.org/sdr/SWAA2026062914071), Jun 20, 2026: BATTERY PACK. INOPERATIVE. ALL ASSOCIATED LIGHT INOP FOR EMERGENCY BATTERY PACK M1672. REMOVED AND REPLACED BATTERY PACK M1672, PERFORMED GOOD OPS TEST IAW AMM 33-51-00-710-801. FUNCTIONA
- [SDR SWAA2026062914217](https://openairdocs.org/sdr/SWAA2026062914217), Jun 20, 2026: BATTERY PACK. INOPERATIVE. M2837 FWD OWE LIGHT INOPERATIVE. CHARGED BATTERY PACK AND PERFORMED A GOOD TEST OF M2837 FWD OVERWING EMERGENCY LIGHT IAW AMM 33-51-06-610-802.
- [SDR SWAA2026063011115](https://openairdocs.org/sdr/SWAA2026063011115), Jun 10, 2026: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 727F, S6L. THE STRINGER CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02-0G-0, AND DWG 146A1121, REV-.
- [SDR SWAA2026063011116](https://openairdocs.org/sdr/SWAA2026063011116), Jun 10, 2026: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 727D, S8L. THE STRINGER CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02-0G-0, AND DWG 146A1111, REV-.
- [SDR SWAA2026063011117](https://openairdocs.org/sdr/SWAA2026063011117), Jun 10, 2026: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 727D, S6L. THE STRINGER CLIP WAS REMOVED AND REPLACED IAW SRM 51-40-02-0G-0, AND DWG 146A1111, REV-.
- [SDR SWAA2026063011120](https://openairdocs.org/sdr/SWAA2026063011120), Jun 10, 2026: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 727E, S5L. THE STRINGER CLIP WAS R & R THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1112, REV 05.
- [SDR SWAA2026063011119](https://openairdocs.org/sdr/SWAA2026063011119), Jun 10, 2026: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT STA 727C, S5L. THE STRINGER CLIP WAS R & R IAW SRM 51-40-02-0G-0, AND DWG 146A1103, REV-.
- [SDR SWAA2026063011118](https://openairdocs.org/sdr/SWAA2026063011118), Jun 10, 2026: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED AT BS 727C, S6L. STRINGER CLIP REMOVED AND REPLACED IAW SRM 51-40-02-0G-0, AND DWG 146A1103, REV-.
- [SDR SWAA2026063010342](https://openairdocs.org/sdr/SWAA2026063010342), Jun 9, 2026: SKIN. DELAMINATED. RIGHT OTBD AFT FLAP LOWER INBD END DELAMINATED. RECEIVED A NEW RT OTBD AFT FLAP, INSTALLATION WILL BE ACCOMPLISHED ON CC TTG8Q01CM9EG.
- [SDR SWAA2026063010344](https://openairdocs.org/sdr/SWAA2026063010344), Jun 9, 2026: WEDGE. DELAMINATED. LEFT INBD MID FLAP OTBD T/E EDGE WEDGE DELAMINATED AT TRAILING EDGE. REMOVED AND REPLACED LEFT INBD MID FLAP OTBD T/E EDGE WEDGE IAW SRM 51-40-02-0G-0, SRM 51-4
- [SDR SWAA2026063010320](https://openairdocs.org/sdr/SWAA2026063010320), Jun 8, 2026: PANEL. DELAMINATED. DELAMINATION ON RT WING T/E PANEL 661BB. REPAIRED DELAMINATION DAMAGE ON RT WING T/E PANEL 661BB IAW SRM 51-70-04-2R-9.
- [SDR SWAA2026042792801](https://openairdocs.org/sdr/SWAA2026042792801), Apr 24, 2026: CLAMP. LEAKING. STRONG ODOR FROM FWD LAVATORY AS WELL AS BROWN FLUID ON LAVATORY FLOOR. CLEANED AREA SHUT OFF WATER TO FWD LAV. NO FURTHER LEAKS NOTED. FOUND THE FWD LAV WASTE 
- [SDR SWAA2025062383787](https://openairdocs.org/sdr/SWAA2025062383787), Jun 20, 2025: HANDLE. LOOSE. R1 DOOR ASSIST HANDLE LOOSE <[01]. TIGHTNED R1 DOOR ASSIST HANDLE IAW B 737 AMM 2-41-31-400-802-NG. TQ WRENCH T8349R DUE 23/OCT/25; [02] TIGHTNED R1 DOOR ASSIST
- [SDR SWAA2025021294930](https://openairdocs.org/sdr/SWAA2025021294930), Feb 11, 2025: SLIDE. DISLODGED. FA'S REPORT L1 SLIDE NOT PROPERLY STOWED. SLIDE IS PARTIALLY PULLED OUT<[01] REPOSITIONED SLIDE I/A/W AMM 25-66-01
- [SDR SWAA2024101748165](https://openairdocs.org/sdr/SWAA2024101748165), Oct 13, 2024: LIGHT. UNSECURE. ROW 5 LOOSE (EMERGENCY LIGHT)<[01] RESECURED ROW ABC EMERGENCY LIGHT PER SIP. CKS OK.
- [SDR SWAA2024101447055](https://openairdocs.org/sdr/SWAA2024101447055), Oct 10, 2024: LENS. CRACKED. EMERGENCY LIGHT LENS CRACKED AT 6DEF AND 29DEF.<[01] REPLACED LENSES PER S.I.P.
- [SDR SWAA2024101147056](https://openairdocs.org/sdr/SWAA2024101147056), Oct 10, 2024: SLIDE. UNPACKED. FWD ENTRY DOOR (L1) ESCAPE SLIDE NEEDS TO BE RE-PACKED (FALLING OUT) OF CONTAINER<[01] REPOSITIONED SMALL FLAP BEHIND GIRT BAR PER M.M. 25-66-01. RE-PACK OF SLI
- [SDR SWAA2024091737975](https://openairdocs.org/sdr/SWAA2024091737975), Sep 15, 2024: HANDLE. LOOSE. R1 DOOR HANDLE (OUTSIDE) CAME OFF<[01] REINSTALLED R1 DOOR HANDLE ASSY IAW AMM 52-41-11; AMM 52-41-31;
- [SDR SWAA2023122635257](https://openairdocs.org/sdr/SWAA2023122635257), Dec 24, 2023: DRAIN. BROKEN. AIRSPEED UNRELIABLE. CA SIDE APPEARED TO BE ACCURATE. F.O. SIDE WAS APPROX 20 KTS OFF. F.O. SIDE WAS ALSO 400 OFF ALTITUDE. BOTH EEC WENT TO ALTERNATE.<[01] FOU
- [SDR SWAA2023090596318](https://openairdocs.org/sdr/SWAA2023090596318), Sep 1, 2023: SIGN. MISSING. RH AFT OVER WING EXIT SIGN MISSING<[01] REPLACED RH OVER WING EXIT SIGN COVER IAW AMM 33-51-01. OPS CKS NORMAL
- [SDR SWAA2023081685346](https://openairdocs.org/sdr/SWAA2023081685346), Aug 3, 2023: BATTERY. DISCHARGED. FWD CABIN FLASHLIGHTS BATTERIES DISCHARGED.<[01] REMOVED AND REPLACED FWD CABIN FLASHLIGHTS BATTERIES; REF BOEING AMM 25-64-00-900-806.;[02] VERIFIED STEP 1
- [SDR SWAA2023081684065](https://openairdocs.org/sdr/SWAA2023081684065), Jul 30, 2023: BATTERY PACK. INOPERATIVE. SEVERAL EMERGENCY LIGHTS INOP THROUGH OUT PASSENGER CABIN.<[01] PERFORMED TROUBLESHOOTING FOR EMERGENCY LIGHTS AS PER B737 WDM 33-51-11; WDM 33-51-11; WDM 33-51
- [SDR SWAA2023081683170](https://openairdocs.org/sdr/SWAA2023081683170), Jul 28, 2023: PANEL. DELAMINATED. RIGHT HORIZONTAL STAB. T/E PANEL 343DB HAS EVIDENCE DELAMINATE IN CORNET O/B.<[01] REPAIRED DAMAGE CORNER WITH A PERMANENT REPAIR ON PANEL 343DB AS PER B737 SRM
- [SDR SWAA2023081680317](https://openairdocs.org/sdr/SWAA2023081680317), Jul 19, 2023: MOUNT. BROKEN. FWD SERVICE DOOR SLIDE BRACKET SHOCK MOUNT BROKEN<[01] REMOVED AND REPLACED FWD SERVICE DOOR SLIDE BRACKET SHOCK MOUNT BROKEN;[02] VERIFIED ALL STEPS
- [SDR SWAA2023081685098](https://openairdocs.org/sdr/SWAA2023081685098), Jul 14, 2023: ACCESS PANEL. CRACKED. R/H FWD O/B ACCESS PANEL # 193AR HAS BULGING/CRACKED FASTENER HOLES<[01] SUMMARY :ACCOMPLISHED PULSE-ECHO ULTRASONIC INSP. FOR DELAMINATION ON R/H FWD O/B ACCES
- [SDR SWAA2023081685343](https://openairdocs.org/sdr/SWAA2023081685343), Jul 14, 2023: ACCESS PANEL. CRACKED. RIGHT WING LOWER MID T/E ACCESS PANEL # 661BB HAS BULGING/CRACKED FASTENER HOLES<[01] APPLIED REPAIR AT PANEL #661BB PER B737 SRM51-70-04-2R-0 PARAGRAPH (4.L.7)
- [SDR SWAA2023081678843](https://openairdocs.org/sdr/SWAA2023081678843), Jul 14, 2023: RIB. CRACKED. L/H HORIZONTAL STAB. L/E PANEL # 331B HAS RIB # 23 CRACKED<[01] SUMMARY; REMOVED RIB AT L/H HORIZONTAL STAB L/E PANEL # 331B RIB 23 AS PER REF B/737 SRM 51-40-0
- [SDR SWAA2023081678842](https://openairdocs.org/sdr/SWAA2023081678842), Jul 14, 2023: RIB. CRACKED. R/H HORIZONTAL STAB. L/E PANEL # 341B HAS RIB # 25 CRACKED<[01] REMOVED AND INSTALLED NEW #25 RIB AT R/H HORIZONTAL STABILIZER PANEL 341B AS PER SRM 51-40-02-0G
- [SDR SWAA2023081678839](https://openairdocs.org/sdr/SWAA2023081678839), Jul 14, 2023: RIB. CRACKED. R/H HORIZONTAL STAB. L/E PANEL # 341B HAS RIB 4 CRACKED<[01] REMOVED AND REPLACED RIB # 4 AT RH HORIZONTAL STAB L/E PANEL 341B PER SRM 51-40-02-0G-0.;[02] VERIF
- [SDR SWAA2023081678840](https://openairdocs.org/sdr/SWAA2023081678840), Jul 14, 2023: RIB. CRACKED. R/H HORIZONTAL STAB. L/E PANEL # 341B HAS RIB # 23 CRACKED<[01] SUMMARY: REMOVED AT R/H HORIZONTAL STAB L/E PANEL #341B RIB 23 AS PER REF B/737 SRM 51-40-02-0G-
- [SDR SWAA2023081678841](https://openairdocs.org/sdr/SWAA2023081678841), Jul 14, 2023: RIB. CRACKED. R/H HORIZONTAL STAB. L/E PANEL # 341B HAS RIB # 24 CRACKED<[01] SUMMARY: REMOVED R/H HORIZONTAL STAB L/E #342B RIB #24 AS PER REF B/737 SRM 51-40-02-0G-0 AND DW
- [SDR SWAA2023081681886](https://openairdocs.org/sdr/SWAA2023081681886), Jul 13, 2023: ACCESS PANEL. CRACKED. LEFT FWD O/B FUSELAGE ACCESS PANEL # 193CL HAD BULGING/CRACKED FASTENER HOLES<[01] ALL STEPS COMPLETED.;[02] SUMMARY=PREPARED DAMAGED AREA FOR REPAIR AS MARKED 
- [SDR SWAA2023081678303](https://openairdocs.org/sdr/SWAA2023081678303), Jul 13, 2023: DOOR. CRACKED. CUSTOMER REQUEST: LH MAIN LANDING GEAR CENTER DOOR CRACKED.<[01] REMOVED LMLG CENTER AND INNER DOORS AS PER AMM 32-13-11-00-802 AND AMM 32-13-11-000-804; INSTAL
- [SDR SWAA2023081678302](https://openairdocs.org/sdr/SWAA2023081678302), Jul 13, 2023: ACCESS PANEL. BULGED. LOWER MID KEEL BEAM ACCESS PANEL # 192F HAS FASTENER HOLES BULGING/CRACKED<[01] ALL STEPS COMPLETED;[02] SUMMARY=PREPARED DAMAGED AREA FOR REPAIR (FASTENER HOLE
- [SDR SWAA2023081681887](https://openairdocs.org/sdr/SWAA2023081681887), Jul 13, 2023: ACCESS PANEL. BULGED. R/H OVERWING FAIRING ACCESS PANEL # 195CR HAS BULGING/CRACKED AROUND FASTENER HOLES<[01] C/W;[02] CORRECTION TO READ SUMMARY=PREPARED DAMAGED AREA FOR REPAIR (F
- [SDR SWAA2023081684064](https://openairdocs.org/sdr/SWAA2023081684064), Jul 13, 2023: ACCESS PANEL. EXPOSED. L/H UPPER AFT FAIRING ACCESS PANEL # 194FL HAS EXPOSED COMPOSITE AT PANEL AND EDGE OF APU DRAIN MAST<[01] VERIFIED STEP 1;[02] REPAIRED PANEL AT DAMAGED ARE PER
- [SDR SWAA2023081677571](https://openairdocs.org/sdr/SWAA2023081677571), Jul 12, 2023: CHANNEL. CRACKED. AFT CARGO COMPARTMENT RIGHT SIDE; FLOOR STRUCTURE 'Z CHANEL' HAS CRACK BETWEEN STA 727H TO STA 727I.<[01] EVALUATED DAMAGED CRACK AREA OUT OF LIMITS PER SRM 53-
- [SDR SWAA2023081677573](https://openairdocs.org/sdr/SWAA2023081677573), Jul 12, 2023: CHANNEL. CORRODED. AFT CARGO COMPARTMENT RIGHT SIDE; FLOOR STRUCTURE 'Z CHANEL' AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 727J TO STA 747.<[01] RH Z CHANNEL SECTION TO BE RE
- [SDR SWAA2023081677572](https://openairdocs.org/sdr/SWAA2023081677572), Jul 12, 2023: CHANNEL. CORRODED. AFT CARGO COMPARTMENT RIGHT SIDE; FLOOR STRUCTURE 'Z CHANEL' AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 727I TO STA 727J.<[01] RH Z CHANNEL SECTION TO BE R
- [SDR SWAA2023081677585](https://openairdocs.org/sdr/SWAA2023081677585), Jul 12, 2023: CHANNEL. CORRODED. AFT CARGO COMPARTMENT RIGHT SIDE; FLOOR STRUCTURE 'Z CHANEL' AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 727G TO STA 727H.<[01] RH Z CHANNEL SECTION TO BE R
- [SDR SWAA2023081677574](https://openairdocs.org/sdr/SWAA2023081677574), Jul 12, 2023: CHANNEL. CORRODED. AFT CARGO COMPARTMENT RIGHT SIDE; FLOOR STRUCTURE 'Z CHANEL' AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 747 TO STA 767.<[01] RH Z CHANNEL SECTION TO BE REP
- [SDR SWAA2023081677584](https://openairdocs.org/sdr/SWAA2023081677584), Jul 12, 2023: CHANNEL. CORRODED. AFT CARGO COMPARTMENT RIGHT SIDE; FLOOR STRUCTURE 'Z CHANEL' AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 727F TO STA 727G.<[01] RH Z CHANNEL SECTION TO BE R
- [SDR SWAA2023081677570](https://openairdocs.org/sdr/SWAA2023081677570), Jul 12, 2023: CHANNEL. CORRODED. AFT CARGO COMPARTMENT RIGHT SIDE; FLOOR STRUCTURE 'Z CHANEL' AROUND HOLES HAS EVIDENCE CORROSION BETWEEN STA 727H TO STA 727I.<[01] RH Z CHANNEL SECTION TO BE R
- [SDR SWAA2023081677985](https://openairdocs.org/sdr/SWAA2023081677985), Jul 12, 2023: ACCESS PANEL. BULGED. LOWER FUSELAGE FWD KEEL BEAM ACCESS PANEL # 192E HAS BULGING/CRACKED FASTENER HOLES<[01] PREPARED DAMAGED AREA FOR REPAIR FASTENER HOLES AS MARKET ON PANEL #192
- [SDR SWAA2023081677553](https://openairdocs.org/sdr/SWAA2023081677553), Jul 11, 2023: BATTERY. INOPERATIVE. LAVATORY D AFT WALL FLASHLIGHT INDICATION LIGHT DOES NOT FLASH.<[01] REMOVED AND REPLACED LAVATORY D AFT WALL FLASHLIGHT BATTERY IN REF WITH ASTRONICS CMM 25-60
- [SDR SWAA2023081677557](https://openairdocs.org/sdr/SWAA2023081677557), Jul 11, 2023: SUPPORT. CRACKED. PASSENGER COMPARTMENT; SUPPORT FLOOR PANEL CRACKED AT STA 540 RBL 2'<[01] ALL STEPS COMPLETED.
- [SDR SWAA2023081690185](https://openairdocs.org/sdr/SWAA2023081690185), Jul 11, 2023: FLOOR PANEL. CRACKED. PASSENGER COMPARTMENT; SUPPORT FLOOR PANEL CRACKED AT STA 540 RBL 2'<[01] ALL STEPS COMPLETED.

All 188: https://openairdocs.org/aircraft/N8600F/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 CFM56-7B26E 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 N8600F

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N8600F before.

- [Cancelled 1980-02-28](https://openairdocs.org/deregistered/N8600F-1980-02-28): Hughes Helicopters HUGHES 369D, S/N 470108D, built 1977. Exported to Australia. Owner: [Vandagriff Dwayne V](https://openairdocs.org/faa-owner/VANDAGRIFF%20DWAYNE%20V), [Coqville, OR](https://openairdocs.org/faa-place/OR/Coqville)

## Related

- Other Boeing 737-8H4 aircraft: https://openairdocs.org/model/boeing-737-8h4/aircraft.md
- The CFM International CFM56-7B26E series engine: https://openairdocs.org/engine/cfm-international-cfm56-7b26e-series.md

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