# N8617E: 2013 Boeing 737-8H4, registration cancelled 2025-12-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 9, 2025
- 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: 36912
- Year built: 2013
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 24, 2013
- Certificate issued: November 3, 2025
- Last registry action: November 3, 2025
- Mode S code: ABD5E0
- Owner when cancelled: [Umb Bank Na Owner Trustee](https://openairdocs.org/faa-owner/UMB%20BANK%20NA%20OWNER%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/N8617E
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8617E
- Page: https://openairdocs.org/deregistered/N8617E-2025-12-09

From the FAA registry file of November 7, 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 (208, newest 50)

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

- [SDR SWAA2025102124073](https://openairdocs.org/sdr/SWAA2025102124073), Oct 13, 2025: SKIN. DELAMINATED. RT OB AFT FLAP IB END UPPER SURFACE HAS SPOT DELAMINATED. REMOVED AND REPLACED R/H OUTBD AFT FLAP IAW AMM 27-51-22-400-801 - AMM 27-51-22-400-801 -ADJUSTMENT AN
- [SDR SWAA2025100917821](https://openairdocs.org/sdr/SWAA2025100917821), Sep 24, 2025: BALANCE WEIGHT. CORRODED. RUDDER FWD COUNTERBALANCE WEIGHT SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED RUDDER FWD COUNTERBALANCE WEIGHT IAW CMM 55-40-09.
- [SDR SWAA2025091000030](https://openairdocs.org/sdr/SWAA2025091000030), Aug 10, 2025: PIN. CORRODED. PITTING CORROSION ON LOWER ATTACHMENT PIN REAR SPAR AT RT HORIZONTAL STABILIZER. REPLACED LOWER ATTACHMENT PIN AT RT HORIZONTAL STABILIZER IAW AMM 27-41-11-401-
- [SDR SWAA2025091000028](https://openairdocs.org/sdr/SWAA2025091000028), Aug 9, 2025: ANGLE. CRACKED. CRACK ANGLE, LOCATED BS 500I AT LEVEL STR28L AT FWD CARGO COMPARTMENT. REPLACED ANGLE LOCATED BS 500I AT LEVEL STR28L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 
- [SDR SWAA2025091000029](https://openairdocs.org/sdr/SWAA2025091000029), Aug 9, 2025: ANGLE. CRACKED. CRACK ANGLE LOCATED 500I AT LEVEL STR28R AT FWD CARGO COMPARTMENT. REPLACED ANGLE LOCATED 500I AT LEVEL STR28R AT FWD CARGO COMPARTMENT IAW SRM 51-40-02 AND DWG
- [SDR SWAA2025091199671](https://openairdocs.org/sdr/SWAA2025091199671), Aug 8, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLE ACCESS PANEL 561CB TRAILING EDGE AT LT WING REPAIRED ACCESS PANEL 561CB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-9.
- [SDR SWAA2025091199670](https://openairdocs.org/sdr/SWAA2025091199670), Aug 8, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLE ACCESS PANEL 551BT TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 551BT TRAILING EDGE AT LT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2025091099779](https://openairdocs.org/sdr/SWAA2025091099779), Aug 8, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 360, STRINGERS 27R - 28R IN E & E BAY. REPLACED SUPPORT ANGLE IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02. MEASUREMENT OF CRACK IS L=0.63
- [SDR SWAA2025091199282](https://openairdocs.org/sdr/SWAA2025091199282), Aug 7, 2025: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED BS540 AT LEVEL RBL 6 AT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET LOCATED BS540 AT LEVEL RBL 6 AT AIR CONDITIONING BAY IAW B7
- [SDR SWAA2025091099289](https://openairdocs.org/sdr/SWAA2025091099289), Aug 7, 2025: DOOR. CORRODED. CORROSION ON EXTERNAL SKIN TOILET SERVICE DOOR 145AL AT LOWER FUSELAGE. EVALUATED REWORK AREA LOC. ON EXTERNAL SKIN TOILET SERVICE DOOR 145AL AT LOWER FUSELAGE 
- [SDR SWAA2025091099281](https://openairdocs.org/sdr/SWAA2025091099281), Aug 7, 2025: SUPPORT BRACKET. CRACKED. CRACK SUPPORT BRACKET LOCATED BS540 AT LEVEL LBL 6 AT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET LOCATED BS540 AT LEVEL LBL 6 AT AIR CONDITIONING BAY IAW SR
- [SDR SWAA2025091098895](https://openairdocs.org/sdr/SWAA2025091098895), Aug 6, 2025: SUPPORT ANGLE. CRACKED. CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 WL 208.1. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-10-02 ITEM 9;SRM 51-40-02 AND DWG 143A5
- [SDR SWAA2025091098906](https://openairdocs.org/sdr/SWAA2025091098906), Aug 6, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 500I - 520, BL 0, WL 208.1. REPLACED SUPPORT ANGLE AND FASTENERS IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, & DWG:143A5400, SHEET 177, REV
- [SDR SWAA2025091098898](https://openairdocs.org/sdr/SWAA2025091098898), Aug 6, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 380 - 400, RBL 40, WL 208.1. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 
- [SDR SWAA2025091098893](https://openairdocs.org/sdr/SWAA2025091098893), Aug 6, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 380 - 400, LBL 13, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 142, REV -, & 
- [SDR SWAA2025091098892](https://openairdocs.org/sdr/SWAA2025091098892), Aug 6, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 380 - 400, LBL 50, WL 208.1. REPLACED SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A5400, SHEET 141,
- [SDR SWAA2025091099099](https://openairdocs.org/sdr/SWAA2025091099099), Aug 6, 2025: ANGLE. CRACKED. CRACKED ANGLE BTW BS 291.5 - 294.5, STR 17R IN FWD GALLEY. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 141A8310, SHEET 33, REV -, DWG 140A9810, SHEET 35, REV A
- [SDR SWAA2025091098404](https://openairdocs.org/sdr/SWAA2025091098404), Aug 5, 2025: FLOOR SUPPORT. CRACKED. CRACK ON INTERCOSTAL LOC BTW BS 947 TO BS 967 RBL 53 APPROX WL 208.1 AT AFT GALLEY AREA. REPLACED INTERCOSTAL AND FASTENERS LOC BTW BS 947 TO BS 967 RBL 53 APPR
- [SDR SWAA2025091098730](https://openairdocs.org/sdr/SWAA2025091098730), Aug 5, 2025: DOOR FRAME. CRACKED. CRACK FRAME AT FWD ENTRY DOOR CUT OUT BS 312 BTW STRINGERS 5L TO STRINGER 6L PASSENGER CABIN. REPAIRED FRAME AT FWD ENTRY DOOR CUT OUT BS 312 BTW STRINGERS 5L T
- [SDR SWAA2025091098731](https://openairdocs.org/sdr/SWAA2025091098731), Aug 5, 2025: NUT PLATE. CORRODED. CORROSION ON RAIL NUT-PLATE LOCATED LEADING EDGE INTERNAL CAVITY ORSS 406 AT LT WING. REPLACED RAIL NUT-PLATE LOCATED LEADING EDGE INTERNAL CAVITY ORSS 406 AT L
- [SDR SWAA2025091098403](https://openairdocs.org/sdr/SWAA2025091098403), Aug 5, 2025: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL, BS 947 - 967, LBL 53, WL 208.1. REPLACED INTERCOSTAL IAW SRM 51-10-02 ITEM 9, AND DWG 147A5650, SHEETS 54 & 55, REV A.
- [SDR SWAA2025091098557](https://openairdocs.org/sdr/SWAA2025091098557), Aug 5, 2025: ANGLE. CRACKED. CRACKED ANGLE TRAILING EDGE, IRSS 199 PLUS 12 INCHES, RT WING. REPLACED ANGLE TRAILING EDGE, IRSS 199, PLUS 12 INCHES, RT WING IAW SRM 51-10-02, ITEM 9, SRM 51-
- [SDR SWAA2025091098733](https://openairdocs.org/sdr/SWAA2025091098733), Aug 5, 2025: PLATE. CRACKED. CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 219, LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 219 LT WING IAW SRM 51-10-02, SRM 51-40-02,
- [SDR SWAA2025091098729](https://openairdocs.org/sdr/SWAA2025091098729), Aug 5, 2025: ELEVATOR. OUT OF BALANCE. DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR LT FOUND BALANCE WEIGHTS P/N: 183A0210-14 (1 E/A) ON BAY 2; P/N: 183A0210-14 (1 E/A) AND P/N: 69-53211-2 (2 E/A)
- [SDR SWAA2025091198401](https://openairdocs.org/sdr/SWAA2025091198401), Aug 4, 2025: STRAP. CORRODED. CORRODED STRAP LOCATED BTW BS794.3 TO BS807 RBL22 WL156 AT AFT CARGO COMPARTMENT. REPLACED STRAP AND FASTENERS LOCATED BTW BS767 TO BS867 RBL22 WL156 AT AFT CAR
- [SDR SWAA2025091198400](https://openairdocs.org/sdr/SWAA2025091198400), Aug 4, 2025: STRAP. CORRODED. CORROSION STRAP LOCATED BS794.3 RBL22 WL156 AT AFT CARGO COMPARTMENT. REPLACED STRAP LOCATED BS794.3 RBL22 WL156 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40
- [SDR SWAA2025091198397](https://openairdocs.org/sdr/SWAA2025091198397), Aug 4, 2025: SUPPORT. CRACKED. CRACK ANGLE - SUPPORT LOCATED BS947.5 LBL11 AT AFT CARGO COMPARTMENT . INSTALLED NEW ANGLE - SUPPORT LOCATED STA947.5 AND LBL11 AT AFT CARGO COMPARTMENT IAW B73
- [SDR SWAA2025091098395](https://openairdocs.org/sdr/SWAA2025091098395), Aug 4, 2025: WEB. CRACKED. CRACK WEB - INTERCOSTAL LOCATED BTW BS927 TO BS947.5 RBL22 AT AT AFT CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL LOCATED BTW BS927 TO BS947.5 RBL22 AT AT AFT 
- [SDR SWAA2025091098393](https://openairdocs.org/sdr/SWAA2025091098393), Aug 4, 2025: SHIELD. CORRODED. CORROSION SHIELD WEB LOCATED BTW BS767 TO BS787 RBL22 WL156 AT AFT CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS LOCATED BTW BS767 TO BS787 RBL22 WL156 A
- [SDR SWAA2025090998396](https://openairdocs.org/sdr/SWAA2025090998396), Aug 4, 2025: SUPPORT. CORRODED. CORROSION SUPPORT ZEE LOCATED BTW BS727D TO BS767 RBL22 WL156 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS767 RBL22 WL156 AT AFT CARGO
- [SDR SWAA2025090998392](https://openairdocs.org/sdr/SWAA2025090998392), Aug 4, 2025: SUPPORT. CORRODED. CORRODED SUPPORT ZEE LOCATED BETWEEN BS 727C & 807, LBL 22, WL 156 IN AFT CARGO BAY. PERFORMED CATEGORY A REPAIR ON SUPPORT ZEE IAW SRM 53-00-53-2R-6, REPAIR 6,
- [SDR SWAA2025090998394](https://openairdocs.org/sdr/SWAA2025090998394), Aug 4, 2025: KEELBEAM. CRACKED. CRACK KEELBEAM LOCATED BTW BS 727 & 727A, STRINGER 27R IN AFT CARGO BAY. PERFORMED PERMANENT REPAIR CATEGORY -A- IAW SRM 51-40-02, SRM 53-60-12-2R-1, REPAIR 1, 
- [SDR SWAA2025091098041](https://openairdocs.org/sdr/SWAA2025091098041), Aug 3, 2025: SUPPORT BEAM. CRACKED. CRACK SUPPORT BEAM #4 LOCATED FWD GALLEY DOOR. REPLACED SUPPORT BEAM #4 LOCATED FWD GALLEY DOOR IAW SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 141A6516 SHEET 144 REV
- [SDR SWAA2025091097863](https://openairdocs.org/sdr/SWAA2025091097863), Aug 3, 2025: INTERCOSTAL. CRACKED. CRACKED WEB LOCATED BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV. INSTALLED A NEW WEB INTERCOSTAL IAW SRM 51-40-02-0G AND DRAWING 141A5400 SHEET 20 REV-.
- [SDR SWAA2025091097862](https://openairdocs.org/sdr/SWAA2025091097862), Aug 3, 2025: WEB. CRACKED. CRACKED WEB BS 312 - 328, RBL 31 IN FWD GALLEY AND LAV. REPLACED WEB INTERCOSTAL AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02-0G, AND DRAWING 141A5400, 
- [SDR SWAA2025091097742](https://openairdocs.org/sdr/SWAA2025091097742), Aug 2, 2025: FLOORBEAM. CRACKED. CRACK BRAKE PANEL ASSY LOCATED BS540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN. EVALUATED CRACK ON BRAKE PANEL LOCATED BS540 BETWEEN BL 0 TO LBL 24.75 AT PAS
- [SDR SWAA2025091097741](https://openairdocs.org/sdr/SWAA2025091097741), Aug 2, 2025: ANGLE. CRACKED. CRACK ANGLE LOCATED BS 695 AND BL 0 AT PASSENGER CABIN. REPLACED ANGLE LOCATED BS 695 AND BL 0 AT PASSENGER CABIN IAW B737-800 SRM 51-10-02 ITEM 9 AND SRM 51-40
- [SDR SWAA2025091097736](https://openairdocs.org/sdr/SWAA2025091097736), Aug 2, 2025: SUPPORT ANGLE. CORRODED. CORRODED SUPPORT ANGLE, BS 500I, STRINGERS 26L - 26R IN FWD CARGO BAY. REPLACED THE SUPPORT ANGLE AND NEW FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DW
- [SDR SWAA2025090997737](https://openairdocs.org/sdr/SWAA2025090997737), Aug 2, 2025: SUPPORT. CORRODED. CORROSION SUPPORT ZEE ON FLOOR STRUCTURE LOCATED BS 500C - 500I, STRINGER 26R IN FWD CARGO BAY. REPLACED THE SUPPORT ZEE, BS 500A - 500I, S26R & THE DAMAGE WAS 
- [SDR SWAA2025091197597](https://openairdocs.org/sdr/SWAA2025091197597), Aug 1, 2025: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 661AB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661AB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10.
- [SDR SWAA2025091097603](https://openairdocs.org/sdr/SWAA2025091097603), Aug 1, 2025: BATTERY PACK. INOPERATIVE. DONT WORK CORRECTLY BATTERY PACK LOCATED BTW STA 559 AND STA 579 LH SIDE AT PASSENGER CABIN (1EA). REPLACED BATTERY PACK LOCATED BTW STA 559 AND STA 579 LH SIDE
- [SDR SWAA2025091097604](https://openairdocs.org/sdr/SWAA2025091097604), Aug 1, 2025: BATTERY PACK. INOPERATIVE. DONT WORK CORRECTLY BATTERY PACK LOCATED BTW STA 559 AND STA 579 RH SIDE AT PASSENGER CABIN (1EA). REPLACED BATTERY PACK LOCATED BTW STA 559 AND STA 579 RH SIDE
- [SDR SWAA2025091097491](https://openairdocs.org/sdr/SWAA2025091097491), Aug 1, 2025: LENS. DETERIORATED. DETERIORATED GALLEY 1 COVER LENS ON EMERGENCY EXIT LIGHT AT FWD GALLEY AREA. REPLACED GALLEY 1 COVER LENS ON EMERGENCY EXIT LIGHT AT FWD GALLEY AREA IAW AMM 33-
- [SDR SWAA2025091097611](https://openairdocs.org/sdr/SWAA2025091097611), Aug 1, 2025: HANDLE. DETERIORATED. DETERIORATED NUT ON ASSIST HANDLE AFT ENTRY DOORWAY LINNING AT AFT GALLEY AREA (2EA) . REPLACED NUT ON ASSIST HANDLE AFT ENTRY DOORWAY LINNING AT AFT GALLEY ARE
- [SDR SWAA2025091097606](https://openairdocs.org/sdr/SWAA2025091097606), Aug 1, 2025: HANDLE. DETERIORATED. DETERIORATED NUT ON ASSIST HANDLE AFT SERVICE DOORWAY LINNING AT AFT GALLEY AREA (2EA). REPLACED NUT ON ASSIST HANDLE AFT SERVICE DOORWAY LINNING AT AFT GALLEY 
- [SDR SWAA2025091097602](https://openairdocs.org/sdr/SWAA2025091097602), Aug 1, 2025: ACCESS PANEL. DELAMINATED. DELAMINATED ACCESS PANEL 193B AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 193B AT LOWER FUSELAGE IAW SRM 51-70-05-2R-6 REPAIR 6.
- [SDR SWAA2025091197254](https://openairdocs.org/sdr/SWAA2025091197254), Jul 31, 2025: ANGLE. CRACKED. CRACK ON GUSSET ANGLE LOCATED BS 500I AT LEVEL STR 21L AT FWD CARGO COMPARTMENT. REPLACED GUSSET LOCATED BS 500I AT LEVEL STR 21L AT FWD CARGO COMPARTMENT IAW B
- [SDR SWAA2025091097255](https://openairdocs.org/sdr/SWAA2025091097255), Jul 31, 2025: ANGLE. CRACKED. CRACK ON ANGLE LOCATED AFT FACE BS 500H AT LEVEL STR 26L AT FWD CARGO COMPARTMENT. REPLACED ANGLE LOCATED AFT FACE BS 500H AT LEVEL STR 26L AT FWD CARGO COMPART
- [SDR SWAA2025091096897](https://openairdocs.org/sdr/SWAA2025091096897), Jul 31, 2025: SCUFF PLATE. CRACKED. CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED THE AFT CORNER SCUFF PLATE OF FWD CARGO COMPARTMENT IAW BOEING SRM 53-30-15-2R-1 REPAIR 1 AND BA
- [SDR SWAA2025091097103](https://openairdocs.org/sdr/SWAA2025091097103), Jul 31, 2025: ANGLE. CRACKED. CRACK ANGLE LOCATED AFT FACE BS 500H AT LVEL STR 26R AT FWD CARGO COMPARTMENT. REPLACED ANGLE - CLIP LOCATED AFT FACE BS 500H AT STR 26R AT FWD CARGO COMPARTMEN

All 208: https://openairdocs.org/deregistered/N8617E-2025-12-09/reports.md

## Other aircraft with N8617E

- [Cancelled 1976-04-01](https://openairdocs.org/deregistered/N8617E-1976-04-01): Piper PA-34-200T, S/N 34-7670162, built 1976. Owner: [Interflight Inc](https://openairdocs.org/faa-owner/INTERFLIGHT%20INC), [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale)

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