# N8620H: 2013 Boeing 737-8H4, registration cancelled 2026-01-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 30, 2026
- Exported to: Brazil
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-8H4](https://openairdocs.org/model/boeing-737-8h4) (registry code 138440A)
- 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) (OpenAirDocs)
- Serial number: 42526
- Year built: 2013
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 3, 2013
- Certificate issued: January 6, 2026
- Last registry action: January 6, 2026
- Mode S code: ABD8A5
- Owner when cancelled: [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 was based
- The mark today: https://openairdocs.org/aircraft/N8620H
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8620H
- Page: https://openairdocs.org/deregistered/N8620H-2026-01-30

From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 737-8H4: https://openairdocs.org/model/boeing-737-8h4.md

## Service difficulty reports (148, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR SWAA2025121034545](https://openairdocs.org/sdr/SWAA2025121034545), Nov 12, 2025: SEAT. OUT OF ADJUST. SEAT 13D RECLINES. IT SHOULD NOTRECLINE INTO EXIT ROW. ADJUSTED PAX SEAT 13D RECLINE LOCK IAW AMM 25-22-00-525-801.
- [SDR SWAA2025121033754](https://openairdocs.org/sdr/SWAA2025121033754), Nov 10, 2025: LENS. FOGGED. R1 DOOR EMERGENCY LIGHT LENS FOGGY. REMOVED AND REPLACED THE R1 DOOR EMERGENCY LIGHT LENS IAW AMM 33-51-04-960-801, STEP F;3 D.
- [SDR SWAA2025121033763](https://openairdocs.org/sdr/SWAA2025121033763), Nov 10, 2025: LENS. CRACKED. ROW 2 CEILING EMERGENCY LIGHT LENS TRIM IS CRACKED AND IN POOR CONDITION. R & R IAW AMM35-51-03-960-803.
- [SDR SWAA2025120933757](https://openairdocs.org/sdr/SWAA2025120933757), Nov 10, 2025: LIGHT. DETERIORATED. RIGHT FWD CABIN EMERGENCY PHOTOLUMINESCENT LIGHT STRIPS ARE DETERIORATED. REMOVED AND REPLACED RH FWD CABIN EMERGENCY PHOTOLUMINESCENT LIGHT STRIP IAW AMM 33-51
- [SDR SWAA2025120933758](https://openairdocs.org/sdr/SWAA2025120933758), Nov 10, 2025: LIGHT. DETERIORATED. LEFT FWD CABIN EMERGENCY PHOTOLUMINESCENT LIGHT STRIPS ARE DETERIORATED. REMOVED AND REPLACED LH FWD CABIN EMERGENCY PHOTOLUMINESCENT LIGHT STRIP IAW AMM 33-51-
- [SDR SWAA2025120933769](https://openairdocs.org/sdr/SWAA2025120933769), Nov 10, 2025: LENS. WRONG PART. AFT LAV ON THE EXTERIOR EMERGENCY EXIT LIGHT LENS IS MISSING VERBIAGE (EXIT). REMOVED AND REPLACED ATF LAV EXTERIOR EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01-9
- [SDR SWAA2025110530572](https://openairdocs.org/sdr/SWAA2025110530572), Oct 31, 2025: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHT POWER SUPPLY M1695, BS 565, RT INOPERATIVE. REPLACED THE POWER SUPPLY IAW AMM 33-51-06-960-806. TESTED OK.
- [SDR SWAA2025110524435](https://openairdocs.org/sdr/SWAA2025110524435), Oct 14, 2025: WEB. CRACKED. CRACKED WEB, BS 500G - 500H, STRINGER 26R. REPLACED THE WEB & FASTENERS IAW SRM 51-40-02, AND DWG 143A7505, SHEET 123, REV-.
- [SDR SWAA2025110522763](https://openairdocs.org/sdr/SWAA2025110522763), Oct 9, 2025: LIGHT. INOPERATIVE. INOPERATIVE EMERGENCY LIGHT, REPLACED EMERGENCY LIGHT IAW AMM 33-51-03-960-805, TESTED OK.
- [SDR SWAA2025110522764](https://openairdocs.org/sdr/SWAA2025110522764), Oct 9, 2025: LIGHT. INOPERATIVE. INOPERATIVE EMERGENCY LIGHT AT ROW 16ABC. REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-03-960-805, TESTED OK.
- [SDR SWAA2025110521930](https://openairdocs.org/sdr/SWAA2025110521930), Oct 7, 2025: LENS. BROKEN. BROKEN SIDEWALL PANEL 231ZLW EMERGENCY LIGHT LENS AT PASSENGER CABIN . REPLACED SIDEWALL PANEL 231ZLW EMERGENCY LIGHT LENS AT PAX CABIN IAW AMM 33-51-01-960-802
- [SDR SWAA2025110521932](https://openairdocs.org/sdr/SWAA2025110521932), Oct 7, 2025: LIGHT. DETERIORATED. DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH AND RH SIDE IN CABIN 10 EA. REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH AND RH SIDE AT PASSE
- [SDR SWAA2025110521643](https://openairdocs.org/sdr/SWAA2025110521643), Oct 5, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE OTBD FAN COWL, NR 2 ENGINE. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02.
- [SDR SWAA2025110521416](https://openairdocs.org/sdr/SWAA2025110521416), Oct 4, 2025: HANDLE. DETERIORATED. DETERIORATED HANDLE BOX HARDWARE, FWD SERVICE DOOR. REPLACED HANDLE BOX HARDWARE IAW AMM 52-41-11-400-801, STEP 3.F, 2J,
- [SDR SWAA2025110521056](https://openairdocs.org/sdr/SWAA2025110521056), Oct 3, 2025: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED BS540 AT LEVEL RBL 6 AT RT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET AND FASTENERS LOCATED BS540 AT LEVEL RBL 6 AT RT AIR CON
- [SDR SWAA2025110520966](https://openairdocs.org/sdr/SWAA2025110520966), Oct 3, 2025: SUPPORT BRACKET. CRACKED. CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABINREPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO 3R AT PASSENGER CABIN IAW B
- [SDR SWAA2025110521063](https://openairdocs.org/sdr/SWAA2025110521063), Oct 3, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE LOCATED BODY STA 663.75 AND LBL 10 AT AIR CONDITIONING BAY. REPLACED SUPPORT ANGLE IAW SRM 51-10-02; SRM 51-40-02. AND DRAWING 111A1000; SHE
- [SDR SWAA2025110521057](https://openairdocs.org/sdr/SWAA2025110521057), Oct 3, 2025: SUPPORT BEAM. CRACKED. CRACK SUPPORT BEAM NR 4 LOCATED FWD GALLEY DOOR. REPLACED SUPPORT BEAM NR 4 AND FASTENERS IAW SRM 51-10-02; SRM 51-40-02; DWG 141A6535, SHEET 13, REV -, AND DWG
- [SDR SWAA2025110521062](https://openairdocs.org/sdr/SWAA2025110521062), Oct 3, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BODY STA 663.75 RBL 35 AT AIR CONDITIONING BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02; SRM 51-40-02 AND DRAWING 111A1000; S
- [SDR SWAA2025110520967](https://openairdocs.org/sdr/SWAA2025110520967), Oct 3, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE BTW BS 380 - 400, LBL 13, WL 208.1. REPLACED SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, DWG 143A5400, SHEET 138, REV -, & DWG 143A5400
- [SDR SWAA2025110520965](https://openairdocs.org/sdr/SWAA2025110520965), Oct 3, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 52 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 52
- [SDR SWAA2025110520968](https://openairdocs.org/sdr/SWAA2025110520968), Oct 3, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 39 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 39
- [SDR SWAA2025110520670](https://openairdocs.org/sdr/SWAA2025110520670), Oct 2, 2025: SUPPORT. CORRODED. CORROSION LOWER SILL LOCATED BTW BS 794.3 TO BS 847 RBL 22 WL 156.1. REMOVED AND REPLACED LOWER SILL AND FASTENERS LOCATED BTW BSTA 794.3 TO BSTA 847. RBL 22 AN
- [SDR SWAA2025110520667](https://openairdocs.org/sdr/SWAA2025110520667), Oct 2, 2025: SKIN. CORRODED. CORROSION INTERNAL SKIN LOCATED BTW STA 727D TO STA 727E BTW STR 27L TO STR 27R AND WL 148.5 AT AFT CARGO. GAINED ACCESS LOCATED BTW STA 727D TO STA 727E BTW ST
- [SDR SWAA2025110520561](https://openairdocs.org/sdr/SWAA2025110520561), Oct 2, 2025: TIE CLIP. CRACKED. CRACK ON TIE CLIP LOCATED BS 500I AT LEVE STR 26R AT FWD CARGO COMPARTMENT. REPLACED TIE CLIP AND FASTENERS LOCATED BS 500I ON STRINGER 26R AT FWD CARGO COMPART
- [SDR SWAA2025110520562](https://openairdocs.org/sdr/SWAA2025110520562), Oct 2, 2025: SUPPORT ANGLE. CORRODED. CORROSION ON SUPPORT ANGLE LOCATED BS 500I BTW STR26L TO STR 26R AT FWD CARGO. PERFORMED CLEAN ON AREA AND APPLIED PAINT SUPPORT ANGLE LOCATED BS 500I BTW STR26
- [SDR SWAA2025110520676](https://openairdocs.org/sdr/SWAA2025110520676), Oct 2, 2025: PLATE. CORRODED. CORROSION PLATE BTW STA 827 TO STA 847, STR 25R TO STR 26R WL 156. REPLACED THE PLATE IAW SRM 51-10-02; SRM 51-40-02 AND DWG 146A8340 SHEET 28 REV -.
- [SDR SWAA2025110520672](https://openairdocs.org/sdr/SWAA2025110520672), Oct 2, 2025: PLATE. CORRODED. CORRODED PLATE BTW STA 794.3 TO STA 807 BTW STR 25R TO STR 26R WL 156. REPLACED PLATE IAW SRM 51-10-02; SRM 51-40-02 AND DWG 146A8340 SHEET 28 REV -.
- [SDR SWAA2025110520567](https://openairdocs.org/sdr/SWAA2025110520567), Oct 2, 2025: WEB. CRACKED. CRACKED WEB, BS 500 - 500A, STRINGER 26L. REPLACED THE WEB IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 124, SHEET 125, REV -.
- [SDR SWAA2025110520665](https://openairdocs.org/sdr/SWAA2025110520665), Oct 2, 2025: SUPPORT. CORRODED. CORRODED SUPPORT ZEE, BS 727I - 807, LBL 21, WL 156.1. REPLACED SUPPORT ZEE IAW SRM-53-00-53-2R-5, REPAIR 5, SRM-51-40-02, DWG:146A7500, SHEET 233, REV-, & DWG 
- [SDR SWAA2025110520669](https://openairdocs.org/sdr/SWAA2025110520669), Oct 2, 2025: SHIELD. CORRODED. CORRODED SHIELD, BS 767 - 794.3, STRINGER 25R, WL 165. REPLACED THE SHIELD AND FASTENERS IAW SRM 51-40-02, & DWG 146A0081, SHEET 49, REV A.
- [SDR SWAA2025110520674](https://openairdocs.org/sdr/SWAA2025110520674), Oct 2, 2025: STRAP. CORRODED. CORROED STRAP, BS 767 - 787, STRINGERS 25L - 25R. REPLACED THE STRAP IAW SRM 51-10-02, ITEM 9, NO ALLOWABLE DAMAGE IN SRM.
- [SDR SWAA2025110520675](https://openairdocs.org/sdr/SWAA2025110520675), Oct 2, 2025: WEB. CRACKED. CRACKED WEB, BS 927 - 947.5, RBL 21. REPLACED THE WEB AND FASTENERS IAW SRM 51-40-02, AND DWG 147A7500, SHEET 37, REV -.
- [SDR SWAA2025110520663](https://openairdocs.org/sdr/SWAA2025110520663), Oct 2, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 867 BTW STRINGERS 26L - 27L. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, AND DRAWING 149A8102, SHEET 19, REV A.
- [SDR SWAA2025110520673](https://openairdocs.org/sdr/SWAA2025110520673), Oct 2, 2025: ANGLE. CORRODED. CORRODED ANGLE BTW BS 767 - 787, STRINGER 25R, WL 165. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02, AND DWG 146A8123, SHEET 16, REV-.
- [SDR SWAA2025110420560](https://openairdocs.org/sdr/SWAA2025110420560), Oct 2, 2025: SHIELD. CORRODED. CORRODED SHIELD WEB LOCATED BTW BS 492.4 - 500A, RBL 22, WL 208.1. REPLACED SHIELD WEB IAW SRM 51-10-02; B737-800 SRM 51-40-02 AND DRAWING 143A0080 SHEET: 39 RE
- [SDR SWAA2025110420563](https://openairdocs.org/sdr/SWAA2025110420563), Oct 2, 2025: SUPPORT. CORRODED. CORROSION ON SUPPORT ZEE LOCATED BTW BS 500F - 500I, RBL 22, FWD CARGO BAY. REMOVED DAMAGE AND EVALUATED REWORK AREA ON SUPPORT ZEE IAW SRM 53-00-53-1A-2 ALLOWA
- [SDR SWAA2025110420566](https://openairdocs.org/sdr/SWAA2025110420566), Oct 2, 2025: SUPPORT. CORRODED. CORROSION ON SUPPORT ZEE LOCATED BTW BS 500A TO 500F, RBL 22, WL 208.1 IN THE FWD CARGO BAY. REMOVED DAMAGE AND EVALUATED REWORK AREA ON SUPPORT ZEE LOCATED BTW
- [SDR SWAA2025110520293](https://openairdocs.org/sdr/SWAA2025110520293), Oct 1, 2025: NUT PLATE. CRACKED. CRACK OUTBOARD FRONT SPAR RAIL NUT PLATE OFSS 573 AT LT WING. REPLACED RAIL NUT PLATE LOCATED OUTBOARD FRONT SPAR OFSS 573 AT LT WING IAW B737-800 SRM 51-40-02-
- [SDR SWAA2025110520295](https://openairdocs.org/sdr/SWAA2025110520295), Oct 1, 2025: NUT PLATE. CRACKED. CRACK OUTBOARD FRONT SPAR RAIL NUT PLATE OFSS 491 AT LT WING. REPLACED RAIL NUT PLATE LOCATED OUTBOARD FRONT SPAR OFSS 491 AT LT WING IAW B737-800 SRM 51-40-02-
- [SDR SWAA2025110520187](https://openairdocs.org/sdr/SWAA2025110520187), Oct 1, 2025: TIE CLIP. CRACKED. CRACK TIE CLIP FRAME ON BS 277 AND STR10R AT FWD GALLEY AREA. REPLACED TIE CLIP LOCATED ON BS 277 AND STR 10R AT FWD GALLEY AREA. IAW SRM 51-10-02 ITEM 9; SRM 5
- [SDR SWAA2025110520296](https://openairdocs.org/sdr/SWAA2025110520296), Oct 1, 2025: NUT PLATE. CRACKED. CRACK OTBD FRONT SPAR RAIL NUT PLATE OFSS 333 AT LT WING. REPLACED THE NUT PLATE LOCATED OTBD FRONT SPAR OFSS 333 IAW SRM 51-40-02-0G; SRM 51-10-02-0G-0, ITEM 9
- [SDR SWAA2025110520292](https://openairdocs.org/sdr/SWAA2025110520292), Oct 1, 2025: NUT PLATE. CRACKED. CRACK ON RAIL NUT PLATE FRONT SPAR OFSS 604 AT LT WING. REPLACED THE NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 112A4402, SHEET 41, REV A.
- [SDR SWAA2025110520294](https://openairdocs.org/sdr/SWAA2025110520294), Oct 1, 2025: NUT PLATE. CRACKED. CRACK OUTBOARD FRONT SPAR RAIL NUT PLATE OFSS 506 AT LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G, & DWG 112A4402, SHEET 40, 
- [SDR SWAA2025110519729](https://openairdocs.org/sdr/SWAA2025110519729), Sep 30, 2025: SEAT TRACK. DETERIORATED. DETERIORATED SEAT TRACK SEAT ROWS 3(INB) AND 20(OUT) AT PASSENGER CABIN. REPLACED SEAT TRACK IAW CMM 25-22-46-3500 REV. 8 PAGE 3015 DISASSEMBLY STEP 3.AA.(5) AN
- [SDR SWAA2025110519408](https://openairdocs.org/sdr/SWAA2025110519408), Sep 29, 2025: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM LOCATED BS 986.5 RBL 42 WL 208.1. REPAIRED FLOORBEAM IAW SRM 53-70-51-2R-6 REPAIR 6.
- [SDR SWAA2025110519259](https://openairdocs.org/sdr/SWAA2025110519259), Sep 29, 2025: SUPPORT ANGLE. CORRODED. CORROSION ANGLE - SUPPORT LOCATED STA 500I BTW STR 24L TO STR 26L AND WL 156 AT FWD CARGO. REMOVED DAMAGE AND EVALUATED REWORK AREA (3 EA) ON ANGLE - SUPPORT LO
- [SDR SWAA2025110519250](https://openairdocs.org/sdr/SWAA2025110519250), Sep 29, 2025: ACCESS PANEL. CRACKED. CRACK ANTENNA ACCESS PANEL 192F WING TO BODY FAIRING AT FUSELAGE EXTERIOR. REMOVED AND REPLACED MARKER BEACON ANTENNA ON ACCESS PANEL 192F WING TO BODY FAIRING 
- [SDR SWAA2025110519254](https://openairdocs.org/sdr/SWAA2025110519254), Sep 29, 2025: FLOORBEAM. CRACKED. CRACKED FLOORBEAM, BS 540, BL 0 - LBL 24.75, WL 208.1. REPLACED THE FLOORBEAM IAW SRM 51-10-02 ITEM 9, SRM 51-40-02-0G, & DWG143A0060, SHEET 64, REV-.
- [SDR SWAA2025110519413](https://openairdocs.org/sdr/SWAA2025110519413), Sep 29, 2025: SUPPORT ANGLE. CRACKED. CRACK CARGO LINER SUPPORT ANGLE, CEILING AREA, BS 727J, LBL 50. REPAIRED THE SUPPORT ANGLE IAW SRM 51-70-11-2R-0.

All 148: https://openairdocs.org/deregistered/N8620H-2026-01-30/reports.md

## Other aircraft with N8620H

- [Cancelled 1973-10-18](https://openairdocs.org/deregistered/N8620H-1973-10-18): North American NAVION, S/N NAV-4-585. Owner: [Nicholas G Barry](https://openairdocs.org/faa-owner/NICHOLAS%20G%20BARRY), [Long Island, NY](https://openairdocs.org/faa-place/NY/Long%20Island)

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