# N8610A: 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: 36635
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 22, 2013
- Certificate issued: December 23, 2024
- Expires: December 31, 2031
- Mode S code: ABD4E7
- 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=8610A
- Page: https://openairdocs.org/aircraft/N8610A

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 N8610A.

## FAA accident and incident reports

None matched to N8610A.

## Service difficulty reports (171, 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 SWAA2026101909356](https://openairdocs.org/sdr/SWAA2026101909356), Oct 15, 2026: BATTERY PACK. INOPERATIVE. RIGHT OVERWING EXIT INTERNAL EMERGENCY LIGHTS WERE INOPERAIVE. REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805. OPS TESTED GOOD.
- [SDR SWAA2026082514571](https://openairdocs.org/sdr/SWAA2026082514571), Aug 21, 2026: LENS. DISPLACED. L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT LENS DISPLACED. SECURED THE LENS IAW AMM 33-51-04 . LIGHT DOES NOT ILLUMINATE. OK TO CONTINUE IAW MEL 33-14-01. RELAMPED A
- [SDR SWAA2026072799239](https://openairdocs.org/sdr/SWAA2026072799239), Jul 22, 2026: LENS. MISSING. EMERGENCY EXIT SIGN AT ROW 13ABC MISSING LENS. REPLACED THE LENS IAW AMM 33-51-01
- [SDR SWAA2026071502202](https://openairdocs.org/sdr/SWAA2026071502202), Jul 11, 2026: ENGINE. SLOW. AFTER LANDING NR 1 ENGINE SLOW/ NO RESPONSE TO THRUST LEVER MOVEMENT. PERFORMED EEC BITE IAW FIM 73-00 TASK 801 NO FAULTS AND PERFORMED ENGINE RUN IAW AMM 71-00
- [SDR SWAA2026071545498](https://openairdocs.org/sdr/SWAA2026071545498), Jul 11, 2026: PUMP. FAILED. OTS, NR 1 ENGINE FAILED IN FLIGHT. ATTEMPTED RESTART WITH NO SUCCESS. LANDED SINGLE ENGINE. NO AIRFRAME OR OTHER ABNORMAL ENGINE INDICATIONS PRIOR TO FAILURE. H
- [SDR SWAA2026040784991](https://openairdocs.org/sdr/SWAA2026040784991), Mar 31, 2026: SKIN. DEBONDED. DISBOND ON LH OUTBD AFT FLAP UPPER SKIN.<[01] REMOVED LT OTBD AFT FLAP PER AMM 27-51-22. INSTALLED NEW LT OTBD AFT FLAP PER AMM 27-51-22; ACCOMPLISHED RIG PER A
- [SDR SWAA2026040184583](https://openairdocs.org/sdr/SWAA2026040184583), Mar 29, 2026: SKIN. DEBONDED. CREW REPORTS NR 1 TE FLAP UPPER FWD CORNER, DEBONDING. RELATIVE TO WS 326. PERFORMED EA 26-157-00859. ACFT OK FOR SERVICE.
- [SDR SWAA2026030976833](https://openairdocs.org/sdr/SWAA2026030976833), Mar 4, 2026: SIGN. CRACKED. FWD ENTRY DOOR EMERGENCY EXIT SIGN CRACKED. R & R FWD ENTRY DOOR EMERGENCY EXIT SIGN IAW AMM 33-51-01.
- [SDR SWAA2026030575655](https://openairdocs.org/sdr/SWAA2026030575655), Mar 1, 2026: HANDLE. LOOSE. FORWARD SERVICE DOOR ASSIST HANDLE LOOSE. TIGHTENED THE ASSIST HANDLE IAW AMM 52-41-31-400-802.
- [SDR SWAA2026030575654](https://openairdocs.org/sdr/SWAA2026030575654), Mar 1, 2026: PIN. DISENGAGED. SEAT ROW 14FED OVERHEAD EMERGENCY LIGHT INOPERATIVE. ON INVESTIGATION; FOUND PIN B NOT FULLY ENGAGED IN CONNECTOR D14816. TERMINATED IAW WDM 33-51-12 AND PERFOR
- [SDR SWAA2026030374508](https://openairdocs.org/sdr/SWAA2026030374508), Feb 26, 2026: ELEC CONNECTOR. BROKEN. AFT COVE BULLNOSE HAS BROKEN AISLE LIGHT CONNECTOR. REPLACED AISLE LIGHT CONNECTOR IAW SWPM 20-63-02, & WDM 33-51-14-13. FUNCTIONAL TEST WILL BE PERFORM IN TASK
- [SDR SWAA2026030374089](https://openairdocs.org/sdr/SWAA2026030374089), Feb 25, 2026: COVER. BROKEN. G1 EMERGENCY LIGHT COVER IS BROKEN. R & R THE EMERGENCY LIGHT COVER IAW AMM 33-51-14-960-802. FUNCTIONAL CHECK PERFORMED ON TASK CARD TTG8Q01AJFUK.
- [SDR SWAA2026030374507](https://openairdocs.org/sdr/SWAA2026030374507), Feb 25, 2026: LIGHT. CRACKED. LEFT CENTER OVER WING EXIT SIDEWALL PANEL EMERGENCY EXIT LIGHT BACKING IS CRACKED. R & R THE EMERGENCY LIGHT IAW AMM 33-51-14-960-802. FUNCTIONAL CHECK PERFORME
- [SDR SWAA2025122354586](https://openairdocs.org/sdr/SWAA2025122354586), Dec 21, 2025: SLIDE. OUT OF ALIGNMENT. FORWARD GALLEY SLIDE LOOKS MISALIGNED. RESCURED EXCESS MATERIAL AT BOTTOM OF R1 DOOR SLIDE COMPARTMENT. VERIFIED GIRT BAR OPERATION; GIRT OPS NORMAL AND SLIDE P
- [SDR SWAA2025081905343](https://openairdocs.org/sdr/SWAA2025081905343), Aug 17, 2025: SHIELD. BROKEN. AFT LT OTBD EMERGENCY FLASHLIGHT SHEILD BROKEN. R&R FLASHLIGHT SHEILD REF AMM 25-64-00.
- [SDR SWAA2025051970988](https://openairdocs.org/sdr/SWAA2025051970988), May 14, 2025: DOOR FRAME. CORRODED. AFT LEFT LAVATORY DOOR POST HAS EVIDENCE OF CORROSION AT LOWER SIDE<[01] REMOVED LH AFT LAV DOOR; AND AFT DOOR FRAME TRIM. REMOVED CORRODED SECTION OF THE AFT D
- [SDR SWAA2025041422625](https://openairdocs.org/sdr/SWAA2025041422625), Apr 8, 2025: LIGHT. INOPERATIVE. EXTERIOR EMERGENCY LIGHT AFT OF R/H WING INOP<[01] RELAMPED EXTERIOR EMERGENCY LIGHT AFT OF R/H WING IAW AMM 33-51-04
- [SDR SWAA2025031104138](https://openairdocs.org/sdr/SWAA2025031104138), Mar 11, 2025: FLAP SYSTEM. LOCKED. ON APPROACH FLAP INDICATION WAS 10 WHILE FLAP HANDLE WAS AT 30. WE EXECUTED A GO AROUND AND RAN THE TRAILING EDGE FLAP DISAGREE CHECKLIST. WE EXTENDED THE FLAPS
- [SDR SWAA2025021395098](https://openairdocs.org/sdr/SWAA2025021395098), Feb 12, 2025: HANDLE. OUT OF ADJUST. FWD GALLEY SERVICE DOOR HANDLE CAM CONTACTING LOWER 4 FASTENERS.<[01] FWD GALLEY SERVICE DOOR HANDLE ADJUSTED REF. AMM 52-41-00 AND REMOVED AND REPLACED FASTENE
- [SDR SWAA2025013191303](https://openairdocs.org/sdr/SWAA2025013191303), Jan 30, 2025: PANEL. DELAMINATED. PANEL 193AL HAS DELAMINATION<[01]. EVALUATED DAMAGE ON PANEL 193AL. FOUND PUNCTURE LENGTH .5''; WIDTH .3''; DEPTH 0.05''. APPLIED TEMPORARY SEAL PER SRM 53-40-7
- [SDR SWAA2025011582423](https://openairdocs.org/sdr/SWAA2025011582423), Jan 2, 2025: INTERCOSTAL. ELONGATED. ELONGATED HOLE WEB - INTERCOSTAL LOC BTW BS500B TO BS500C AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-764828<[01] REPLACED WEB - INTERCOSTAL LOC BTW BS500B T
- [SDR SWAA2025011582424](https://openairdocs.org/sdr/SWAA2025011582424), Jan 2, 2025: INTERCOSTAL. ELONGATED. ELONGATED HOLE WEB - INTERCOSTAL LOC BTW BS500G TO BS500H AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-764829<[01] REPLACED WEB - INTERCOSTAL LOC BTW BS500G T
- [SDR SWAA2025011582422](https://openairdocs.org/sdr/SWAA2025011582422), Jan 2, 2025: INTERCOSTAL. ELONGATED. ELONGATED HOLE WEB - INTERCOSTAL LOC BTW BS500C TO BS500D AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-764827<[01] REPLACED WEB - INTERCOSTAL LOC BTW BS500C T
- [SDR SWAA2025012381111](https://openairdocs.org/sdr/SWAA2025012381111), Dec 27, 2024: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET BODY STATION 540 AND LBL 6 AT KEEL BEAM 2024-764808<[01] REPLACED SUPPORT BRACKET LOCATED ON BS 540 AND LBL6 AT KEEL BEAM. IAW B737-800 SR
- [SDR SWAA2025012380929](https://openairdocs.org/sdr/SWAA2025012380929), Dec 26, 2024: PLATE. CRACKED. CRACK ON CORRUGATED PLATE LOCATED IRSS 215 AT TRAILING EDGE AT LT WING 2024-764797<[01] REPLACED CORRUGATED PLATE LOCATED IRSS 215 AT TRAILING EDGE AT LT WING I
- [SDR SWAA2025012480359](https://openairdocs.org/sdr/SWAA2025012480359), Dec 22, 2024: PLATE. BROKEN. BROKEN CORRUGATED PLATE LOC ON IRSS 143 AT REAR SPAR LT WING 2024-764768<[01] REPLACED CORRUGATED PLATE LOC ON IRSS 143 LT WING IAW B737-800 SRM 51-40-02 AND DR
- [SDR SWAA2025012280354](https://openairdocs.org/sdr/SWAA2025012280354), Dec 22, 2024: NUT. DETERIORATED. DETERIORATED NUT ON ASSIST HANDLE AT AFT SERVICE DOOR (2EA) 2024-764740<[01] REPLACED NUT ON ASSIST HANDLE AT AFT SERVICE DOOR (2EA) IAW SOPM 20-50-01 REV. 38 A
- [SDR SWAA2025012280353](https://openairdocs.org/sdr/SWAA2025012280353), Dec 22, 2024: NUT. DETERIORATED. DETERIORATED NUT ON ASSIST HANDLE AT FWD SERVICE DOOR 2024-764739<[01] REPLACED NUT ON ASSIST HANDLE AT FWD SERVICE DOOR IAW B737-800 AMM 52-41-31-400-802 STEP 
- [SDR SWAA2025012180357](https://openairdocs.org/sdr/SWAA2025012180357), Dec 22, 2024: RIB. CRACKED. CRACK ON DEFLECTION CONTROL RIB TRAILING EDGE AT LT WING 2024-764746<[01] TOOL USED STEP 6 EDDY CURRENT EQUIPMENT PN: NORTEC 600D SN: 240497907 DUE DATE: 27-AUG
- [SDR SWAA2025012080355](https://openairdocs.org/sdr/SWAA2025012080355), Dec 22, 2024: ANGLE. CRACKED. CRACK ANGLE TRAILING EDGE LOCATED ORSS 317 AT LT WING 2024-764745<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 317 AT LT WING IAW B737-800 SRM 51-40-02 AND DW
- [SDR SWAA2025012379911](https://openairdocs.org/sdr/SWAA2025012379911), Dec 21, 2024: RIB. CRACKED. CRACK ON RIB ACCESS PANEL 331B LOCATED LE STA105.26 AT LT HORIZONTAL STABILIZER 2024-764729<[01] REPLACED RIB AND FASTENERS LOCATED ON L/E STA 105.26 AT LT HORI
- [SDR SWAA2025012379912](https://openairdocs.org/sdr/SWAA2025012379912), Dec 21, 2024: RIB. CRACKED. CRACK ON RIB ACCESS PANEL 331B LOCATED LE STA114.55 AT LT HORIZONTAL STABILIZER 2024-764730<[01] REPLACED RIB & FASTENERS LOCATED ON L/E STA 114.55 AT LT HORIZO
- [SDR SWAA2025012379910](https://openairdocs.org/sdr/SWAA2025012379910), Dec 20, 2024: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN 2024-764690<[01] TOOLS USED TEMPERATURE CONTROLLER P/N: 38615K71; S/N: AE-40585
- [SDR SWAA2025012179559](https://openairdocs.org/sdr/SWAA2025012179559), Dec 19, 2024: SHEAR PLATE. CORRODED. CORROSION BILGE AREA SHEAR PLATE BTW BS 500 TO BS 500A AT LEVEL S 26R AND WL 154.5 AT FWD CARGO COMPARTMENT 2024-764668<[01] REPLACED SHIELD PLATE BTW BS 492.4 
- [SDR SWAA2025012179555](https://openairdocs.org/sdr/SWAA2025012179555), Dec 19, 2024: SUPPORT CHANNEL. CORRODED. CORROSION CHANNEL SUPPORT ZEE LOCATED BTW BS 500C TO BS 500G AT LEVEL S 26L AT WL 154.5 AT FWD CARGO COMPARTMENT 2024-764656<[01] THE DAMAGE WAS REPAIRED PER SR
- [SDR SWAA2025012179558](https://openairdocs.org/sdr/SWAA2025012179558), Dec 19, 2024: SHIELD. CORRODED. CORROSION WEB (SHIELD) LOCATED BTW BS794 TO 767 RBL 21 WL 156.5 AT AFT CARGO COMPARTMENT 2024-764657<[01] REPLACED WEB(SHIELD)AND FASTENERS LOCATED BETWEEN BS76
- [SDR SWAA2025012179552](https://openairdocs.org/sdr/SWAA2025012179552), Dec 19, 2024: CHANNEL. CORRODED. CORROSION CHANNEL SUPPORT ZEE LOCATED BTW BS 500H TO BS 500I AT LEVEL S 26L AND WL 154.5 AT FWD CARGO COMPARTMENT 2024-764658<[01] TOOL USED ON STEP 4 UT EQUIPM
- [SDR SWAA2025011579562](https://openairdocs.org/sdr/SWAA2025011579562), Dec 19, 2024: WEB. CORRODED. CORROSION WEB - INTERCOSTAL LOCATED BTW BS747 TO BS767 RBL21 WL 156.5 AFT CARGO COMPARTMENT. REPLACED WEB LOCATED BTW BS 747 TO BS 767 RBL 21 WL 156 AT AFT CARG
- [SDR SWAA2025011579564](https://openairdocs.org/sdr/SWAA2025011579564), Dec 19, 2024: SUPPORT ANGLE. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS867 AT LEVEL STR27L AT AFT CARGO COMPARTMENT 2024-764669<[01] REPLACED ANGLE - SUPPORT LOCATED FLOOR STRUCTURE STA 867 AT LEVEL 
- [SDR SWAA2025011579561](https://openairdocs.org/sdr/SWAA2025011579561), Dec 19, 2024: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BTW BS727F TO BS767 RBL21 WL156.5 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE AND CLIP ZEE-SUPPORT(1E/A) BTW BS727F TO BS767 RB
- [SDR SWAA2025011579563](https://openairdocs.org/sdr/SWAA2025011579563), Dec 19, 2024: STRAP. CORRODED. CORROSION STRAP LOCATED BS767 BTW LBL21 TO RBL21 WL 156.5 AT AFT CARGO COMPARTMENT 2024-764667<[01] REPLACED STRAP LOCATED BS767 BTW LBL21 TO RBL21 WL 156.5 AT 
- [SDR SWAA2025011579560](https://openairdocs.org/sdr/SWAA2025011579560), Dec 19, 2024: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BTW BS727D TO BS807 LBL21 WL156.5 AT AFT CARGO COMPARTMENT. ZEE CHANNEL SIDEPLATE ( SUPPORT ZEE) LOCATED BTW BS 727C+11 TO BS 787+
- [SDR SWAA2025012379162](https://openairdocs.org/sdr/SWAA2025012379162), Dec 18, 2024: BALANCE WEIGHT. OUT OF BALANCE. DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR LT PN: 183A0103-25 SN: 006113 FOUND BALANCE WEIGHTS PN: 183A0210-15 (1 EA) ON BAY 4 PN: 183A0210-14 (1EA) ON BAY
- [SDR SWAA2025012379163](https://openairdocs.org/sdr/SWAA2025012379163), Dec 18, 2024: BALANCE WEIGHT. OUT OF BALANCE. DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR RT PN: 183A0103-26 SN: 006328 FOUND BALANCE WEIGHTS PN: 183A0210-15 (1 EA) ON BAY 4 PN: 183A0210-14 (1EA) ON BAY
- [SDR SWAA2025012078981](https://openairdocs.org/sdr/SWAA2025012078981), Dec 18, 2024: WEB. CRACKED. CRACK FLOOR STRUCTURE WEB LOCATED BTW BS 380 TO BS 400 AT LBL 13 AT PASSENGER CABIN 2024-764625<[01] REPLACED FLOOR STRUCTURE WEB (UPPER CHORD ANGLE) LOCATED BT
- [SDR SWAA2025012378551](https://openairdocs.org/sdr/SWAA2025012378551), Dec 17, 2024: FRAME. CRACKED. CRACK FRAME ON BS 312 BETWEEN S-5L AND S-6L AT FWD GALLEY AREA 2024-764593<[01] REPAIRED FRAME ON BS 312 BETWEEN S-5L AND S-6L AT FWD GALLEY AREA IAW B737-800 E
- [SDR SWAA2025012378744](https://openairdocs.org/sdr/SWAA2025012378744), Dec 17, 2024: GUSSET. CRACKED. BROKEN ANGLE GUSSET LOCATED ON BS 500I AT STR 19R AT FWD CARGO COMPARTMENT 2024-764608<[01] REPLACED ANGLE GUSSET AND FASTENERS LOCATED ON BS 500I AT STRINGER 1
- [SDR SWAA2025012178553](https://openairdocs.org/sdr/SWAA2025012178553), Dec 17, 2024: FASTENER. DETERIORATED. DETERIORATED GIRT BAR FITTING HARDWARE ON AFT ENTRY AND GALLEY AT AFT GALLEY AREA 2024-764576<[01] REPLACED GIRT BAR FITTING HARDWARE ON AFT ENTRY AND GALLEY AT
- [SDR SWAA2025012178554](https://openairdocs.org/sdr/SWAA2025012178554), Dec 17, 2024: FASTENER. DETERIORATED. DETERIORATED HARDWARE GIRT BAR FITTING IN ENTRY AND SERVICE DOOR AT FWD GALLEY AREA 2024-764587<[01] REPLACED HARDWARE GIRT BAR FITTING IN ENTRY AND SERVICE DOO
- [SDR SWAA2025012378182](https://openairdocs.org/sdr/SWAA2025012378182), Dec 16, 2024: STIFFENER. CORRODED. CORROSION STIFFENER LOCATED BTW BS947.5 TO BS967 RBL 50 WL 208.1 AT AFT GALLEY AREA 2024-764549<[01] TOOL USED P/N: 45MG; S/N: 130066401; CAL DUE: 21-OCT-25.;[0

All 171: https://openairdocs.org/aircraft/N8610A/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 N8610A

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N8610A before.

- [Cancelled 2007-05-15](https://openairdocs.org/deregistered/N8610A-2007-05-15): Williams James R B1RD, S/N 232. Owner: [Williams James R](https://openairdocs.org/faa-owner/WILLIAMS%20JAMES%20R), [Camano Island, WA](https://openairdocs.org/faa-place/WA/Camano%20Island)
- [Cancelled 1951-04-10](https://openairdocs.org/deregistered/N8610A-1951-04-10): Beech D18S, S/N A-537. Owner: [Beech Aircraft Corp](https://openairdocs.org/faa-owner/BEECH%20AIRCRAFT%20CORP), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)

## 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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