# N8642E: 2014 Boeing 737-8H4, registration cancelled 2026-05-15

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 15, 2026
- Exported to: Nigeria
- 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: 42525
- Year built: 2014
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 31, 2014
- Certificate issued: April 23, 2026
- Last registry action: April 23, 2026
- Mode S code: ABE056
- Owner when cancelled: [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE)
- Location: [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake)
- Owner type: Corporation
- Owner's area on the map: 40.8386° N, 111.9179° W: Placed by OpenAirDocs at the center of ZIP code 84054, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N8642E
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8642E
- Page: https://openairdocs.org/deregistered/N8642E-2026-05-15

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 (113, newest 50)

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

- [SDR SWAA2026012764140](https://openairdocs.org/sdr/SWAA2026012764140), Jan 24, 2026: LAMP. BURNED OUT. EXTERIOR FUSELAGE, AFT OF L2 DOOR, EMERGENCY LIGHT BURNED OUT. REPLACED THE LAMP IAW AMM 33-51-04-960-801.
- [SDR SWAA2026012860575](https://openairdocs.org/sdr/SWAA2026012860575), Jan 12, 2026: ACCESS PANEL. CRACKED. CRACKED ACCESS PANEL 551GB, TRAILING EDGE LT WING. REPAIRED THE ACCESS PANEL 551GB IAW SRM 51-70-05-2R-10, REPAIR 10.
- [SDR SWAA2026012757979](https://openairdocs.org/sdr/SWAA2026012757979), Jan 4, 2026: ANGLE. CRACKED. CRACKED ANGLE ON ACCCESS PANEL 834DZ OF THE ENTRY DOOR. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 411A2119, SHEET 72, REV-. MEASUREMENT O
- [SDR SWAA2026012757980](https://openairdocs.org/sdr/SWAA2026012757980), Jan 4, 2026: ANGLE. CRACKED. CRACKED ANGLE OF ACCESS PANEL 844DZ OF DOOR GALLEY AT AFT GALLEY AREA. REPLACED THE ACCESS PANEL ANGLE ON GALLEY DOOR AREA DUE TO NO FOUND ALLOWABLE DAMAGE FOR 
- [SDR SWAA2026012856545](https://openairdocs.org/sdr/SWAA2026012856545), Dec 29, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 500I, STR 28L REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, & DWG 143A7902, SHEET 320, REV-.
- [SDR SWAA2026012756542](https://openairdocs.org/sdr/SWAA2026012756542), Dec 29, 2025: SUPPORT ANGLE. CRACKED. CRACK SUPPORT ANGLE, BS 500I, STR 28R IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE, AND FASTENERS IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 
- [SDR SWAA2026012856337](https://openairdocs.org/sdr/SWAA2026012856337), Dec 28, 2025: ACCESS PANEL. CRACKED. CRACKED ACCESS PANEL 551GB T/E LT WING. REPAIRED THE ACCESS PANEL 551GB IAW SRM 51-70-05-2R-10, REPAIR 10.
- [SDR SWAA2026012756056](https://openairdocs.org/sdr/SWAA2026012756056), Dec 28, 2025: LENS. BROKEN. BROKEN LENS OF EMERGENCY LIGHT, STRONGHBACK ROW 24-25 RT SIDE. REPLACED THE LENS IAW AMM 33-51-03-960-803, STEP 4.D, ITEM (1) & (2).
- [SDR SWAA2026012856045](https://openairdocs.org/sdr/SWAA2026012856045), Dec 27, 2025: WEB. CRACKED. CRACKED WEB, ORSS 271 RT WING T/E. REPLACED THE WEB IAW SRM 51-10-02, STEP 9, SRM 51-40-02-0G-0, & DWG 115A2512, SHEET 16, REV-.
- [SDR SWAA2026012855730](https://openairdocs.org/sdr/SWAA2026012855730), Dec 26, 2025: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, BS 867, S26 - 27L. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 149A8102, SHEET 19, REV A.
- [SDR SWAA2026012755838](https://openairdocs.org/sdr/SWAA2026012755838), Dec 26, 2025: INTERCOSTAL. CORRODED. CORRODED WEB - INTERCOSTAL BS 747 - 767, RBL 21, WL 155 IN THE AFT CARGO BAY. REPLACED THE WEB - INTERCOSTAL IAW SRM 51-10-02, ITEM 9, AND DWG 146A7500, SHEET 2
- [SDR SWAA2026012755839](https://openairdocs.org/sdr/SWAA2026012755839), Dec 26, 2025: SUPPORT. DAMAGED. ELONGATED HOLES ON SUPPORT ZEE BTW BS 727C - 747, RBL 21 IN THE AFT CARGO BAY. TOOK INITIAL MEASUREMENTS OF HOLES ON THE SUPPORT ZEE, HOLE NR 1: D=0.246, HOLE N
- [SDR SWAA2026012755729](https://openairdocs.org/sdr/SWAA2026012755729), Dec 26, 2025: SHIELD. CORRODED. CORRODED SHIELD WEB, BTW BS 767 - 794.3, RBL 21, WL 155 IN THE AFT CARGO BAY. REPLACED THE SHIELD WEB IAW SRM 51-40-02, & DWG 146A0081, SHEET 49, REV A.
- [SDR SWAA2026012854842](https://openairdocs.org/sdr/SWAA2026012854842), Dec 22, 2025: CROSSBEAM. CRACKED. CRACKED CROSSBEAM, BS 540, BL 0 - LBL 24.75. REPLACED CROSSBEAM IAW SRM 51-40-02, AND DWG 143A0060, SHEET 64, REV-.
- [SDR SWAA2026012754840](https://openairdocs.org/sdr/SWAA2026012754840), Dec 22, 2025: FLOOR SUPPORT. CRACKED. CRACKED PAX CABIN FLOOR SUPPORT BTW BS 380 - 400, LBL 51. REPLACED THE FLOOR SUPPORT & FASTENERS IAW SRM 51-40-02-0G, SRM 51-10-02 PARAGRAPH 9, & DWG 143A5400, 
- [SDR SWAA2026012853686](https://openairdocs.org/sdr/SWAA2026012853686), Dec 18, 2025: ANGLE. CORRODED. CORRODED ANGLE, BS 986.5 + 10, RBL 42, WL 208.1. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02, DWG 147A5700, SHEET 123, REV A, SRM 51-10-02, STEP 9 ITEM A.
- [SDR SWAA2026012853009](https://openairdocs.org/sdr/SWAA2026012853009), Dec 16, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 400, LBL 21, IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A7505,SHEET 137, REV-.
- [SDR SWAA2026012853010](https://openairdocs.org/sdr/SWAA2026012853010), Dec 16, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, LBL 21 IN THE FWD CARGO BAY. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02, DWG 143A7505, SHEET 138, REV -.
- [SDR SWAA2026012853011](https://openairdocs.org/sdr/SWAA2026012853011), Dec 16, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 440, LBL 21. IN THE CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 138, REV -.
- [SDR SWAA2026012853013](https://openairdocs.org/sdr/SWAA2026012853013), Dec 16, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 500G, RBL 21, IN THE CARGO BAY. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 137, REV-.
- [SDR SWAA2026012853016](https://openairdocs.org/sdr/SWAA2026012853016), Dec 16, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 500G, RBL 21 AFT SIDE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, & DWG 143A7505, SHEET 137, 138, & 139, REV-.
- [SDR SWAA2026012853014](https://openairdocs.org/sdr/SWAA2026012853014), Dec 16, 2025: GUSSET ANGLE. CRACKED. CRACKED GUSSET ANGLE, BS 500I, S19R. REPLACED THE GUSSET & FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & DWG 143A7902, SHEET 256, REV B.
- [SDR SWAA2026012753015](https://openairdocs.org/sdr/SWAA2026012753015), Dec 16, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, RBL 21 FWD SIDE IN THE FWD CARGO BAY. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 137, REV-.
- [SDR SWAA2026012753012](https://openairdocs.org/sdr/SWAA2026012753012), Dec 16, 2025: ANGLE. CRACKED. CRACKED ANGLE, BS 500H, RBL 21 AFT SIDE IN THEFWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-10-02-0G, SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 137,
- [SDR SWAA2026012752633](https://openairdocs.org/sdr/SWAA2026012752633), Dec 15, 2025: SCUFF PLATE. CRACKED. CRACKED SCUFF PLATE AFT CORNER IN THE FWD CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, PARAGRAPH 4. B, STEPS 2 & 4 - 7.
- [SDR SWAA2026012752637](https://openairdocs.org/sdr/SWAA2026012752637), Dec 15, 2025: STRAP. CORRODED. CORRODED FLOOR STRAP, AFT POSITION BULKHEAD IN THE FWD CARGO BAY. REPLACED THE FLOOR STRAP IAW SRM 51-40-02-0G-0.
- [SDR SWAA2025062584648](https://openairdocs.org/sdr/SWAA2025062584648), Jun 23, 2025: SLIDE. OUT OF POSITION. PULL HANDLE EXPOSED ON AFT SERVICE DOOR SLIDE<[01] FOUND VELCRO PULL HANDLE COVER TUCKED UP IN SLIDE COVER ;PULLED DOWN AND PUT INTO PLACE PER SIP
- [SDR SWAA2025042226156](https://openairdocs.org/sdr/SWAA2025042226156), Apr 18, 2025: SLIDE. DISLODGED. R2 DOOR SLIDE FELL OUT OF COVER. REINSTALLED SLIDE IAW AMM 25-66-00 AND TASK CARD 725-61-06
- [SDR SWAA2025041422739](https://openairdocs.org/sdr/SWAA2025041422739), Apr 8, 2025: BATTERY PACK. FAILED. EMERGENCY EXIT LIGHT BATTERY PACK M1695 FAILS TO CHARGE<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD.;[02]
- [SDR SWAA2025041422735](https://openairdocs.org/sdr/SWAA2025041422735), Apr 8, 2025: BATTERY PACK. NO TEST. EMERGENCY EXIT LIGHT BATTERY PACK M1694 FAILS TO CHARGE<[01] REMOVED & REPLACED EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD.<BR><BR
- [SDR SWAA2025041422736](https://openairdocs.org/sdr/SWAA2025041422736), Apr 8, 2025: BATTERY PACK. FAILED. EMERGENCY EXIT LIGHT BATTERY PACK M1673 FAILS TO CHARGE<[01] REMOVED & REPLACED EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD.<BR>WN5
- [SDR SWAA2025041422737](https://openairdocs.org/sdr/SWAA2025041422737), Apr 8, 2025: BATTERY PACK. FAILED. EMERGENCY EXIT LIGHT BATTERY PACK M1671 FAILS TO CHARGE<[01] REMOVED & REPLACED EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD.<BR><BR
- [SDR SWAA2025041419414](https://openairdocs.org/sdr/SWAA2025041419414), Mar 29, 2025: BRACKET. CRACKED. 040-001 BRACKET ON AFT SIDE OF # 1 ENGINE O/B COWL IS WORN AND CRACKED. HAS STREAMER ATTACHED.<[01] REMOVED WORN AND CRACKED BRACKET ON AFT SIDE OF #1 ENG O/B C
- [SDR SWAA2025041409944](https://openairdocs.org/sdr/SWAA2025041409944), Mar 26, 2025: HANDLE. LOOSE. R1 DOOR LINER ASSIST HANDLE IS LOOSE<[01] RESECURED R1 DOOR LINER ASSIST HANDLE IAW AMM-52-41-31-400-802 PG 3 STEP F ITEM 2;[02] VERIFIED ITEM 1<BR>C/W
- [SDR SWAA2025041409945](https://openairdocs.org/sdr/SWAA2025041409945), Mar 26, 2025: HANDLE. LOOSE. R2 DOOR LINER ASSIST HANDLE IS LOOSE<[01] RESECURED R2 DOOR LINER ASSIST HANDLE IAW AMM-52-41-31-400-802 PG 3 STEP F ITEM 2;[02] VERIFIED ITEM 1<BR>C/W
- [SDR SWAA2025031405292](https://openairdocs.org/sdr/SWAA2025031405292), Mar 13, 2025: GIRT BAR. OUT OF ADJUST. L1 DOOR EMERGENCY SLIDE AFT GIRL BAR HOLDER LOOSE <[01]. REPLACED FWD L1 DOOR SLIDE AFT GIRT BAR HOLDER FWD RIVET PER SIP. REF AMM 25-66-01. OK FOR SVC.
- [SDR SWAA2024092741838](https://openairdocs.org/sdr/SWAA2024092741838), Sep 25, 2024: LENS. BROKEN. OVERHEAD EMERGENCY LIGHT LENS COVER 4-5 ABC BROKE<[01] 05 - OK TO CONTINUE PER [MEL 33-15-02;INTERIOR EMERGENCY EXIT LIGHTING SYSTEM - EMERGENCY AISLE LIGHTS]. 
- [SDR SWAA2024092741137](https://openairdocs.org/sdr/SWAA2024092741137), Sep 24, 2024: BATTERY PACK. INOPERATIVE. LEFT AFT OVER WING EXIT EMERGENCY LIGHTS INOP.<[01] REMOVED AND REPLACED M1670 EMERGENCY LIGHT BATTERY PER AMM 33-51-06.
- [SDR SWAA2024072415165](https://openairdocs.org/sdr/SWAA2024072415165), Jul 22, 2024: BATTERY PACK. INOPERATIVE. THE FOLLOWING EXTERNAL EMERGENCY EXIT LIGHTS ARE INOP: LH OWE AFT; RH OWE AFT; L2 DOOR; RH AFT FUSELAGE; LH AFT FUSELAGE.<[01] REMOVED BATTERY PACKS M1670; M167
- [SDR SWAA2024072312975](https://openairdocs.org/sdr/SWAA2024072312975), Jul 15, 2024: SKIN. DELAMINATED. R/H O/B AFT FLAP DELAMINATED ON I/B END<[01] REMOVED; REPLACED; AND ADJUSTED R/H O/B AFT FLAP PER AMM 27-51-22.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH ST
- [SDR SWAA2024072309199](https://openairdocs.org/sdr/SWAA2024072309199), Jul 4, 2024: RIB. CRACKED. BODY RIB CRACKED ON RH A/C BAY AT BS 540+18; RBL37.WL136(APPROX.)<[01] 'REPAIRED PER EA 24-157-01843 WITH AN INSPECTION THRESHOLD DEFINED IN 24-157-01843-DTI1 A
- [SDR SWAA2024072509195](https://openairdocs.org/sdr/SWAA2024072509195), Jul 3, 2024: SHIELD. CRACKED. #1 ENGINE I/B FAN COWL OIL TANK ACCESS DOOR SHIELD CRACKED<[01] REMOVED AND REPLACED ACCESS DOOR SHIELD IAW SRM 51-40-02.;[02] PARTS REMOVED / INSTALLED;[03] RE
- [SDR SWAA2024072408786](https://openairdocs.org/sdr/SWAA2024072408786), Jul 3, 2024: SUPPORT. CRACKED. PANEL BREAK AT BS 540 LBL 2 IS CRACKED<[01] REMOVED CRACKED PANEL BREAK AT BS 540 LBL 2 IAW SRM 51-40-02-0G-0.<BR>OBTAINED AND INSTALLED NEW PANEL BREAK AT BS 5
- [SDR SWAA2024072408787](https://openairdocs.org/sdr/SWAA2024072408787), Jul 3, 2024: SUPPORT. CRACKED. PANEL BREAK AT BS 540 RBL 2 IS CRACKED<[01] REMOVED AND REPLACED PANEL BREAK PER SRM 51-40-02-0G-0 AND DWG 143A0060;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03]
- [SDR SWAA2024022655345](https://openairdocs.org/sdr/SWAA2024022655345), Feb 3, 2024: SKIN. DELAMINATED. LEFT OUTBOARD AFT FLAP INBOARD SIDE UPPER AND LOWER SURFACE DELAMINATED.<[01] REMOVED AND REPLACED LEFT OUTBOARD AFT FLAP REF AMM 27-51-11. REQUIRES OPS CHECK.;
- [SDR SWAA2023122032438](https://openairdocs.org/sdr/SWAA2023122032438), Dec 16, 2023: LIGHT. DAMAGED. PHOTO ILLUMINATION STRIP AT ROW 1 FED DAMAGED<[01] OK TO CONTINUE PER MEL 33-19-01; SP #1;[02] REPLACED PHOTO ILLUMINATION STRIP AT ROW 1DEF PER AMM 33-51-15. M
- [SDR SWAA2023120627454](https://openairdocs.org/sdr/SWAA2023120627454), Dec 4, 2023: MEGAPHONE. INOPERATIVE. FWD MEGAPHONE IS INOP.<[01] REMOVED AND REPLACED FWD MEGAPHONE PER AMM 25-64-00. OPS CHECK NORMAL.
- [SDR SWAA2023101109326](https://openairdocs.org/sdr/SWAA2023101109326), Oct 10, 2023: BATTERY PACK. INOPERATIVE. L/H FWD EMERGENCY EXIT LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY AT L/H FWD CEILING AND BATTERY PACK AT 8 ABC AIR GRILLE LOCATIONS; PE
- [SDR SWAA2023101109862](https://openairdocs.org/sdr/SWAA2023101109862), Oct 10, 2023: POWER SUPPLY. INOPERATIVE. L/H FWD EMERGENCY EXIT LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY AT L/H FWD CEILING AND BATTERY PACK AT 8 ABC AIR GRILLE LOCATIONS; PE
- [SDR SWAA2023082492939](https://openairdocs.org/sdr/SWAA2023082492939), Aug 23, 2023: SLIDE. OUT OF ADJUST. CREW REPORTS FWD SLIDE L1 DOOR FELL OUT OF CONTAINER<[01] REINSTALLED L1 DOOR SLIDE PER MT 725-61-06

All 113: https://openairdocs.org/deregistered/N8642E-2026-05-15/reports.md

## 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 DCA22LA012](https://openairdocs.org/ntsb/DCA22LA012), Oct 9, 2021: Boeing 737-8H4 (N8642E), Lexington, VA, no damage. Probable cause: The airplane’s inadvertent encounter with convective turbulence.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20211008017909A](https://openairdocs.org/incident/20211008017909A), Oct 8, 2021: Boeing 737-8H4 (N8642E), Lexington, VA, No damage. As the flight attendants were beginning drink service, the aircraft encountered severe turbulence. The ?c? Position flight attendant injured her ankle and was…

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.