# N8608N: 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: 36638
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 24, 2013
- Certificate issued: December 17, 2024
- Expires: December 31, 2031
- Mode S code: ABD254
- 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=8608N
- Page: https://openairdocs.org/aircraft/N8608N

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 (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 DCA19CA168](https://openairdocs.org/ntsb/DCA19CA168), Jun 17, 2019: Boeing 737-8H4 (N8608N), Pittsburgh, PA, substantial damage. Probable cause: a provisioning truck that impacted the airplane resulting in substantial damage.

## FAA accident and incident reports

None matched to N8608N.

## Service difficulty reports (142, 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 SWAA2026080433342](https://openairdocs.org/sdr/SWAA2026080433342), Jul 31, 2026: GLOWSTRIP. DAMAGED. PHOTOLUMINESCENT STRIP AT 13C DAMAGED. OK TO CONTINUE PER MEL 25-10-01 SP1. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP AT 13C PER AMM 33-51-15. FUNCTION TEST G
- [SDR SWAA2026073061286](https://openairdocs.org/sdr/SWAA2026073061286), Jul 26, 2026: SLIDE. PARTIAL DEPLOY. SLIDE PACK ON L1 DOOR PARTIALLY DEPLOYED ON OPENING OF L1 DOOR AT THE GATE RE INSTALLED SLIDE PER MT725-61-06.
- [SDR SWAA2026060106452](https://openairdocs.org/sdr/SWAA2026060106452), May 26, 2026: LIGHT. LOOSE. EMERGENCY LIGHTS BY ROW 12 ARE NOT SECURED TO THE FLOOR. REATTACTED STRIP AT ROW 12 PER SIP.
- [SDR SWAA2026041789970](https://openairdocs.org/sdr/SWAA2026041789970), Apr 15, 2026: LIGHT. DETACHED. F/A REPORTS 12C FLOOR LIGHT COMING UP. ATTACHED FLOOR PHOTOLUMINESCENT LIGHT AT 12C PER AMM 33-51-15.
- [SDR SWAA2026041589124](https://openairdocs.org/sdr/SWAA2026041589124), Apr 13, 2026: SLIDE. OUT OF POSITION. F/A REPORTS THAT R1 DOOR SLIDE IS OUT OF POSITION IN BUSTLE. ADJUSTED R1 SLIDE PACK WITHIN BUSTLE PER SIP
- [SDR SWAA2026041387888](https://openairdocs.org/sdr/SWAA2026041387888), Apr 9, 2026: SLIDE. OUT OF POSITION. L1 DOOR SLIDE FLAP SHOWING. SECURED L1 DOOR SLIDE CAUTION FLAP IAW AMM 25-66-00. OK FOR SERVICE
- [SDR SWAA2026040886209](https://openairdocs.org/sdr/SWAA2026040886209), Apr 4, 2026: LAMP. INOPERATIVE. FORWARD SERVICE DOOR LIGHT ASSEMBLY L1186 DOES NOT ILLUMINATE DURING EMERGENCY LIGHTING TEST. TROUBLESHOT TO FAULTY FUSE IN M2816 POWER SUPPLY. REPLACED FUSE CO
- [SDR SWAA2026040887233](https://openairdocs.org/sdr/SWAA2026040887233), Apr 4, 2026: FUSE. INOPERATIVE. FORWARD SERVICE DOOR LIGHT ASSEMBLY L1186 DOES NOT ILLUMINATE DURING EMERGENCY LIGHTING TEST.<[01] TROUBLESHOT TO FAULTY FUSE IN M2816 POWER SUPPLY; REPLACED FU
- [SDR SWAA2026040886411](https://openairdocs.org/sdr/SWAA2026040886411), Apr 1, 2026: HANDLE. BROKEN. FWD GALLEY ASSIST HANDLE IS BROKEN<[01] REMOVED AND REPLACED BROKEN G1 ASSIST HANDLE IAW SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2026021369768](https://openairdocs.org/sdr/SWAA2026021369768), Feb 10, 2026: RADOME. DELAMINATED. NOSE RADOME HAS A DELAMINATION AT 4 O`CLOCK, 4 INCHES FROM AFT EDGE, MEASURES 9 INCHES BY 14 INCHES. R & R NOSE RADOME IAW AMM 53-52-00.
- [SDR SWAA2025120442045](https://openairdocs.org/sdr/SWAA2025120442045), Dec 3, 2025: ANGLE. CRACKED. LEFT WING OTBD ANGLE UNDER UPPER INBD FIXED TRAILING EDGE PANEL CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02-0G-0-B00069.
- [SDR SWAA2025051267810](https://openairdocs.org/sdr/SWAA2025051267810), May 6, 2025: LENS. WRONG PART. R1 DOOR EMERGENCY EXIT LIGHT LENS DOESNT MATCH<[01] R&R R1 DOOR EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01
- [SDR SWAA2025051267809](https://openairdocs.org/sdr/SWAA2025051267809), May 6, 2025: LENS. WRONG PART. L1 DOOR EMERGENCY EXIT LIGHT LENS DOESNT MATCH<[01] R&R L1 DOOR EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01
- [SDR SWAA2025022898243](https://openairdocs.org/sdr/SWAA2025022898243), Feb 22, 2025: HANDLE. OUT OF ADJUST. CR RR R2 DOOR ASSIST HANDLE AIRFRAME SIDE NEEDS SECURED. <[01] SECURED R2 DOOR ASSIST HANDLE IAW B737-800 AMM 25-21-420-801; [02] SECURED R2 DOOR ASSIST HANDLE 
- [SDR SWAA2025022797269](https://openairdocs.org/sdr/SWAA2025022797269), Feb 18, 2025: BATTERY PACK. FAILED. FORWARD RIGHT-HAND EMERGENCY LIGHTS INOP <[01]. REMOVED AND REPLACED FORWARD R/H BATTERY PACK M02816 AND OPS CHECK GOOD IAW B737-800 AMM 33-51-06-960-805.; [02]
- [SDR SWAA2025022690572](https://openairdocs.org/sdr/SWAA2025022690572), Jan 29, 2025: INTERCOSTAL. CRACKED. FWD CARGO COMPARTMENT INTERCOSTAL CLIP STA 500H R/H CRACKED P/N#143A7502-158<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT INTERCOSTAL CLIPS STA 500H R/H WITH
- [SDR SWAA2025022690573](https://openairdocs.org/sdr/SWAA2025022690573), Jan 29, 2025: INTERCOSTAL. CRACKED. FWD CARGO COMPARTMENT INTERCOSTAL CLIP STA 500H R/H CRACKED P/N 143A7502-154<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT INTERCOSTAL CLIP STA 500H R/H P/N 1
- [SDR SWAA2025022890570](https://openairdocs.org/sdr/SWAA2025022890570), Jan 28, 2025: BAFFLE. CRACKED. FWD CARGO COMPARTMENT INTERCOSTAL/BAFFLE STA 500F - STA 500G R/H CRACKED (DOT K570) <[01]. REMOVED AND REPLACED BAFFLE STA 500F IAW B737-800 SRM 51-40-02 AND BO
- [SDR SWAA2025022690568](https://openairdocs.org/sdr/SWAA2025022690568), Jan 28, 2025: INTERCOSTAL. CRACKED. FWD CARGO COMPARTMENT INTERCOSTAL STA 500D - STA 500E R/H CRACKED (DOT K569)<[01] REMOVED FWD CARGO COMPARTMENT INTERCOSTAL AT STA 500D - STA 500E R/H IAW B737-
- [SDR SWAA2025022690127](https://openairdocs.org/sdr/SWAA2025022690127), Jan 28, 2025: TRANSITION PANEL. CORRODED. FWD CARGO COMPARTMENT R/H TRANSITION PANEL CORRODED AT FASTENER HOLES THROUGHOUT FROM STA 500C TO STA 500I<[01] EVALUATED FWD CARGO COMPARTMENT R/H TRANSITION P
- [SDR SWAA2025022789739](https://openairdocs.org/sdr/SWAA2025022789739), Jan 26, 2025: FRAME. CRACKED. (CR - VERNON) FOUND FRAME CRACK AT STA 312 BETWEEN S-5L AND S-6L ABOVE L-1 DOOR<[01] REMOVED DAMAGE; FORMED; LOCATED; DRILLED; HFEC CUT OUT; OPEN HOLES AND FPI 
- [SDR SWAA2025030387860](https://openairdocs.org/sdr/SWAA2025030387860), Jan 21, 2025: PANEL. CORRODED. [DOT: Z041] AFT CARGO FLOOR BETWEEN STA 727C AND STA 807; LEFT TRANSITION PANEL CORRODED NUMEROUS PLACES AS MARKED. <FOUND TO BE OUT OF LIMITS ORGINAL MATERIAL 
- [SDR SWAA2025022787861](https://openairdocs.org/sdr/SWAA2025022787861), Jan 21, 2025: TRANSITION PANEL. CORRODED. [DOT: Z042] AFT CARGO FLOOR FROM FWD BULKHEAD TO STA 767; RIGHT TRANSITION PANEL CORRODED NUMEROUS PLACES AS MARKED. <[01] REMOVED CORROSION FROM R/H TRANSITION
- [SDR SWAA2025022687863](https://openairdocs.org/sdr/SWAA2025022687863), Jan 21, 2025: ANGLE. CORRODED. [DOT: B726] AFT CARGO FLOOR BETWEEN STA 767 AND STA 793; RIGHT SUPPORT Z-ANGLE CORRODED AS MARKED.<[01] REMOVED AND REPLACED &NBSP;&NBSP;&NBSP;&NBSP;&NBSP;AFT C
- [SDR SWAA2025022687865](https://openairdocs.org/sdr/SWAA2025022687865), Jan 21, 2025: SPLICE STRAP. CORRODED. [DOT: B727] AFT CARGO FLOOR AT STA 847; RBL 19 HAS RAIL SPLICE STRAP CORRODED AS MARKED.<[01] REMOVED AND REPLACED NEW STRAP IAE B737-800 SRM 51-40-02 AAND BAC 
- [SDR SWAA2025022887747](https://openairdocs.org/sdr/SWAA2025022887747), Jan 20, 2025: INTERCOSTAL. CORRODED. MAIN CABIN FWD WET AREA INTERCOSTA AT STA.294.5-312 BL0 IS CORR0DED <[01]. REMOVED DAMAGE; ORIG. .063; MATERIAL LOSS .063; REMAINING 0.0; FOUND TO BE OUT OF LIM
- [SDR SWAA2025030391075](https://openairdocs.org/sdr/SWAA2025030391075), Jan 19, 2025: PANEL. CORRODED. FWD PIT TRANSITON PANELS CORRODED AT FASTENER HOLES FROM STA 500C TO 500I <[01]. L/H TRANSITION PANEL FROM STA 500C TO STA 500I EVALUATED ORIG. MAT. THK. = 0.04
- [SDR SWAA2025022887419](https://openairdocs.org/sdr/SWAA2025022887419), Jan 19, 2025: SEAL. CRACKED. R-HORIZONTAL UPPER SLIDING SEAL CRACKED DOT# J149 <[01] REMOVED; LOCATED; DRILLED; AND INSTALLED NEW R/H HORIZONTAL UPPER SLIDING SEAL REF B737-NG AMM 53-31-31-
- [SDR SWAA2025022887417](https://openairdocs.org/sdr/SWAA2025022887417), Jan 18, 2025: SEAL. CRACKED. L/H HORIZ. STAB TRAILING EDGE; UPPER BLADE SEAL DELAMINATED APPROX. EL STA. 155. <[01] REMOVED AND REPLACED BLADE SEAL P/N 185A1621-115 PO 1111955.1 REF BAC DWG
- [SDR SWAA2025022887154](https://openairdocs.org/sdr/SWAA2025022887154), Jan 18, 2025: TAIL CONE. CRACKED. R-WING FLAP FAIRING #6 AT TAILCONE IS CRACKED AND HAS A HOLE DOT# J148 <[01]. REPAIRED RH WING TAILCONE ON FLAP FAIRING #6 IAW 737-800 SRM 51-70-04-2R-1 REPAIR 
- [SDR SWAA2025022887138](https://openairdocs.org/sdr/SWAA2025022887138), Jan 17, 2025: INTERCOSTAL. CORRODED. AFT WET AREA BS 967 TO 987 LBL 15 +/- INTERCOSTAL CORRODED AS MARKED. <[01] REMOVED DAMGED ON LBL 15 +/- INTERCOSTAL STA 967-987 FOUND TO BE OUT OF LIMITS IAW B
- [SDR SWAA2025022887140](https://openairdocs.org/sdr/SWAA2025022887140), Jan 17, 2025: FLOOR SUPPORT. CORRODED. AFT WET AREA; BS 995 LBL 38 +/- WEB CORRODED AT FASTENER. AS MARKED. <[01] REMOVED AND REPLACED FLOOR SUPPORT PN:147A5710U1 AT STA. 995 LBL 38. IAW B737-800 SRM
- [SDR SWAA2025022787139](https://openairdocs.org/sdr/SWAA2025022787139), Jan 17, 2025: FLOORBEAM. CORRODED. AFT WET AREA; BS 987 LBL 47 +/- FLOORBEAM T CAP CORRODED AT DOME NUT FASTENER. AS MARKED. <[01] REMOVED CORROSION FROM AFT WET AREA; BS 987 LBL 47 +/- FLOOR BEA
- [SDR SWAA2025022787142](https://openairdocs.org/sdr/SWAA2025022787142), Jan 17, 2025: WEB. CORRODED. AFT WET AREA; BS 947 RBL 52 TO LBL 5 +/- FLOORBEAM T CAP CORRODED. WIDE SPREAD AND AS MARKED.<[01] REMOVED DAMAGE; ORIG. .180; MATERIAL LOSS .090. REMAINING .09
- [SDR SWAA2025022787136](https://openairdocs.org/sdr/SWAA2025022787136), Jan 17, 2025: SUPPORT. CORRODED. MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344 APPROX. LBL-24. MARKED <[01]. MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN 
- [SDR SWAA2025022787129](https://openairdocs.org/sdr/SWAA2025022787129), Jan 17, 2025: SUPPORT. CORRODED. MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344 APPROX. LBL-45. <[01] MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 A
- [SDR SWAA2025022886807](https://openairdocs.org/sdr/SWAA2025022886807), Jan 16, 2025: STRUCTURE. CRACKED. STA540 R/H FLOORBOARD SUPPORT STRUCTURE CRACKED 2EA AREAS DOT T743 <[01]. REMOVED AND REPLACED PANEL BREAK#143A5240-64 PO#1111708.1 AT STA540 R/H IAW B737-800 S
- [SDR SWAA2025022885827](https://openairdocs.org/sdr/SWAA2025022885827), Jan 14, 2025: FLAP. DELAMINATED. RIGHT WING OUTBOARD AFT FLAP INBOARD LOWER CORNER IS DELAMINATED <[01]. REMOVED AND REPLACED RIGHT WING OUTBOARD AFT FLAP IAW B737-800 AMM 27-51-22-401-NG.; [02
- [SDR SWAA2025022785833](https://openairdocs.org/sdr/SWAA2025022785833), Jan 14, 2025: BATTERY PACK. INOPERATIVE. R/H AFT EMERGENCY LIGHTS ON R2 DOOR INOP <[01]. REMOVED AND REPLACED R/H AFT EMERGENCY BATTERY AND OPS CHECK GOOD IAW B737-800 AMM 33-51-00-710-801; [02] REMOVE
- [SDR SWAA2025030385504](https://openairdocs.org/sdr/SWAA2025030385504), Jan 13, 2025: STAND OFF. CORRODED. L/H WING FIXED L/E; 3 EACH STIAND OFFS FOR OVER HEAT DETECTOR CORRODED BETWEEN RIB #3 AND RIB #4. <[01] REMOVED AND REPLACED 3 EACH STAND OFFS # BACN10TL3A12 PO
- [SDR SWAA2024031462046](https://openairdocs.org/sdr/SWAA2024031462046), Mar 12, 2024: SKIN. CRACKED. #2 ENGINE I/B FAN COWL IS CRACKED 17' LONG AT FWD LOWER FWD END.<[01] REMOVED AND REPLACED #2 ENGINE INBOARD FAN COWL REF. AMM 71-11-02. INSTALLED VORTEX CONTRO
- [SDR SWAA2024021351466](https://openairdocs.org/sdr/SWAA2024021351466), Feb 11, 2024: ACTUATOR. FAULTY. ON APPROACH LDG GEAR WAS LOWERED AND LT MAIN DISAGREED WITH HANDLE POSITION. NOSE & RT MAIN GREEN/ LEFT MAIN RED AND NO GREEN GEAR LT ON OVERHEAD FOR LT MAIN. R
- [SDR SWAA2023122634741](https://openairdocs.org/sdr/SWAA2023122634741), Dec 21, 2023: MEGAPHONE. INOPERATIVE. FWD BULLHORN INOP<[01] R & R?D FWD GALLEY MEGAPHONE PER AMM 25-64-00.
- [SDR SWAA2023022104967](https://openairdocs.org/sdr/SWAA2023022104967), Feb 20, 2023: BATTERY. INOPERATIVE. RIGHT SIDE PASSENGER EMERGENCY LIGHTS INOP<[01] T/S PER FIM 33-50 TASK 801; RR?D BATTER PACK AT ASSY# M1695 PER AMM 33-51-06. NO HELP. RETURNED BACK TO ORIGINAL
- [SDR SWAA2023012693543](https://openairdocs.org/sdr/SWAA2023012693543), Jan 20, 2023: BATTERY PACK. INOPERATIVE. R/H EMERGENCY EXIT LIGHTS INOP<[01] REMOVED AND REPLACED 2EA EMERGENCY LIGHT BATTERY PACKS PER AMM 33-51-06. OPERATIONAL CHECK NORMAL OF EMERGENCY LIGHTS PER AM
- [SDR SWAA2023012693544](https://openairdocs.org/sdr/SWAA2023012693544), Jan 20, 2023: BATTERY PACK. INOPERATIVE. R/H AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP<[01] REMOVED AND REPLACED 2EA EMERGENCY LIGHT BATTERY PACKS PER AMM 33-51-06. OPERATIONAL CHECK NORMAL OF EMERGEN
- [SDR SWAA2023012692942](https://openairdocs.org/sdr/SWAA2023012692942), Jan 18, 2023: BALANCE WEIGHT. CORRODED. EVIDENCE OF CORROSION ON THE RUDDER BALANCE WEIGHT.<[01] REMOVED RUDDER WEIGHT PER CMM 55-40-09;[02] INSTALLED RUDDER WEIGHT PER CMM 55-40-09;[03] C/W INSPECTIO
- [SDR SWAA2023012692410](https://openairdocs.org/sdr/SWAA2023012692410), Jan 18, 2023: TRACK. CRACKED. R/T HORIZONTAL PANEL 343AT FWD TRACK IS CRACKED<[01] R&R TRACK PER SOPM 20-50-01;[02] INSPECTED WORK PERFORMED.
- [SDR SWAA2023012688618](https://openairdocs.org/sdr/SWAA2023012688618), Jan 5, 2023: SUPPORT BEAM. CRACKED. L/H WING FIXED TRAILING EDGE SUPPORT BEAM FWD FASTENER HOLE ADJACENT TO L/H DEFLECTION RIB HAS AN HFEC INDICATION OF A CRACK AT THE FWD SIDE OF THE HOLE SEE ATT
- [SDR SWAA2023012687231](https://openairdocs.org/sdr/SWAA2023012687231), Jan 3, 2023: FLOOR SUPPORT. CRACKED. CENTER CABIN STA. 540 LBL 1 FLOOR PANEL SUPPORT ANGLE IS CRACKED AT FASTENER HOLE. MRKD<[01] REMOVED AND REPLACED CABIN FLOOR SUPPORT PER SRM 51-40-02.

All 142: https://openairdocs.org/aircraft/N8608N/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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