# N838AS: Ea Vision EA J100

- Status: Valid registration
- Airframe: [Ea Vision EA J100](https://openairdocs.org/model/ea-vision-ea-j100) (registry code 06102JZ)
- Serial number: EAVUAV502585854
- Type: Rotorcraft
- Engine type: Electric
- Certificate issued: June 20, 2025
- Expires: June 30, 2032
- Mode S code: AB7623
- Registered owner: [Agri Spray Drones LLC](https://openairdocs.org/faa-owner/AGRI%20SPRAY%20DRONES%20LLC)
- Location: [Boonville, MO](https://openairdocs.org/faa-place/MO/Boonville)
- Owner type: LLC
- Owner's area on the map: 38.9107° N, 92.7239° W: Placed by OpenAirDocs at the center of ZIP code 65233, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=838AS
- Page: https://openairdocs.org/aircraft/N838AS

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.

## ADs that may apply (OpenAirDocs): 0 in force

### Matched by airframe (Ea Vision EA J100)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N838AS.

## FAA accident and incident reports

None matched to N838AS.

## Reports on N838AS not matched to an aircraft (2)

They name N838AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20130405006619I](https://openairdocs.org/incident/20130405006619I), Apr 5, 2013: Bombardier Inc CL-600-2B19 (N838AS), Charleston, WV, Minor damage. The aircraft was landing at Charleston, WV (kcrw) rwy 23, 6800 feet in length. Weather was VFR, wind 290 at 10 gusts 17. Upon landing, the right wingtip struck…
- [Incident 20070723013599I](https://openairdocs.org/incident/20070723013599I), Jul 23, 2007: Cndair CL6002B19 (N838AS), Peoria, IL, No damage. (-23) Aircraft had just departed pia enroute to atlanta, ga and was approximately 10 miles south of pia and got a glap disagreement indication. Indication…

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N838AS not matched to an aircraft (173, newest 50)

They name N838AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR ASOA2015062613181](https://openairdocs.org/sdr/ASOA2015062613181), Jun 23, 2015: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT LIGHTS INOPERATIVE AT THE RT OVERWING EXIT AND AISLE OVERHEAD. R & R NR 4 BATTERY PACK IAW AMM 33-51-04. IPC REF 33-51-04, ITEM 17. OPS CHECKED G
- [SDR ASOA2015030212314](https://openairdocs.org/sdr/ASOA2015030212314), Mar 1, 2015: ANGLE. CRACKED. INBD ANGLE CRACKED AT FS 682 AT STR 27. COMPLIED WITH EA 05-2014-036. NO FURTHER DAMAGE NOTED.
- [SDR ASOA2013110709354](https://openairdocs.org/sdr/ASOA2013110709354), Oct 19, 2013: LIGHT. FAILED. ASD HANDLE BETA LIGHT FAILED FUNCTIONAL TEST. REMOVED ASD HANDLE BETA LIGHT IAW AMM 33-51-09-000-801. INSTALLED SERVICEABLE BETA LIGHT ON ASD HANDLE IAW AMM 33-
- [SDR ASOA2013110709350](https://openairdocs.org/sdr/ASOA2013110709350), Oct 18, 2013: SKIN. BURNED. BURN ON SKIN BETWEEN BS 235 - 250 AND BETWEEN STRINGERS 22L AND 23L. COMPLIED WITH REO 601R-53-00-115.
- [SDR ASOA2013110709349](https://openairdocs.org/sdr/ASOA2013110709349), Oct 18, 2013: SKIN. DAMAGED. FASTENER HOLE IN LOWER WING PLANK IS PREVIOUSLY OVERSIZE TO .339. REPAIRED IAW REO 601R-57-21-2014. MAJOR REPAIR.
- [SDR ASOA2013110709348](https://openairdocs.org/sdr/ASOA2013110709348), Oct 16, 2013: SEAT TRACK. CORRODED. LEFT SIDE WALL SEAT TRACK CORRODED AT FS 499-544. R & R SEAT TRACK IAW SRM 51-40-11-00, AMM 53-01-11-000-802, AND 53-01-11-400-802.
- [SDR ASOA2013110709347](https://openairdocs.org/sdr/ASOA2013110709347), Oct 16, 2013: SEAT TRACK. CORRODED. RT SIDE WALL SEAT TRACK CORRODED AT BS 544- 559+80. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA2013110709346](https://openairdocs.org/sdr/ASOA2013110709346), Oct 16, 2013: SEAT TRACK. CORRODED. LT SIDE WALL SEAT TRACK CORRODED AT FS 409.16-409.112. R & R SEAT TRACK IAW SRM 51-40-11-00, AMM 53-01-11-000-802, AND 53-01-11-400-802.
- [SDR ASOA2013110709345](https://openairdocs.org/sdr/ASOA2013110709345), Oct 16, 2013: SEAT TRACK. CORRODED. LT SIDE WALL SEAT TRACK CORRODED AT FS 409+112-449.85. R & R SEAT TRACK IAW SRM 51-40-11-00, AMM 53-01-11-000-802, AND 53-01-11-400-802.
- [SDR ASOA2013110709344](https://openairdocs.org/sdr/ASOA2013110709344), Oct 16, 2013: SEAT TRACK. CORRODED. LT SIDE WALL SEAT TRACK CORRODED AT FS 449.85-499. R & R SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.
- [SDR ASOA2013110709343](https://openairdocs.org/sdr/ASOA2013110709343), Oct 16, 2013: SEAT TRACK. CORRODED. LT SIDE WALL SEAT TRACK CORRODED AT FS 554-559+80. REMOVED THEN INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-000-802, 53-01-11-400-802 AND SRM 51-40-11.
- [SDR ASOA2013110709342](https://openairdocs.org/sdr/ASOA2013110709342), Oct 16, 2013: SEAT TRACK. CORRODED. SEAT TRACK CORRODED AT FS 349-409+16. R & R SEAT TRACK IAW SRM 51-40-11-00, AMM 53-01-11-000-802, AND 53-01-11-400-802.
- [SDR ASOA2013110709341](https://openairdocs.org/sdr/ASOA2013110709341), Oct 16, 2013: SEAT TRACK. CORRODED. RT SIDE WALL SEAT TRACK CORRODED AT FS 409+16-409.00+112. REMOVED THEN INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-000-802, 53-01-11-400-801 AND SRM 51-40-11.
- [SDR ASOA2013110709340](https://openairdocs.org/sdr/ASOA2013110709340), Oct 16, 2013: SEAT TRACK. CORRODED. RT SIDE WALL SEAT TRACK CORRODED AT FS 409-449.85. R & R SEAT TRACK IAW SRM 51-40-11-00, AMM 53-01-11-000-802, AND 53-01-11-400-802.
- [SDR ASOA2013110709339](https://openairdocs.org/sdr/ASOA2013110709339), Oct 16, 2013: BULKHEAD. DAMAGED. TOOL DAMAGE AT RBL 9.0, WL 94.5 BEHIND ISOLATOR AFT PRESSURE BULKHEAD FWD FACE. REPAIRED IAW REO601R-53-61-4206, REV C. MAJOR REPAIR
- [SDR ASOA2013110709338](https://openairdocs.org/sdr/ASOA2013110709338), Oct 16, 2013: BULKHEAD. DAMAGED. TOOL DAMAGE AT LBL 9.0 WL 95.5 BEHIND ISOLATOR AFT PRESSURE BULKHEAD FWD FACE. REPAIRED IAW REO 601R-53-31-4206, REV C. MAJOR REPAIR
- [SDR ASOA2013110709337](https://openairdocs.org/sdr/ASOA2013110709337), Oct 15, 2013: INTERCOSTAL. CRACKED. CARGO DOOR, LOWER AFT CORNER INTERCOSTAL CRACKED. REMOVED CRACKED INTERCOSTAL AND DRILLED SERVICABLE, NEW, INTERCOSTAL TO FIT IAW SRM 51-40-00 AND 51-40-11. INS
- [SDR ASOA2013110509335](https://openairdocs.org/sdr/ASOA2013110509335), Oct 13, 2013: STIFFENER. CRACKED. CRACK FOUND ON STIFFENER ON INTERIOR OF RT WING L/E AT ACCESS PANEL CUT-OUT 630CZ. REMOVED DAMAGED EDGING/STIFFENER FROM RT WING LOWER L/E. DRILLED UP NEW PART 
- [SDR ASOA2013110509334](https://openairdocs.org/sdr/ASOA2013110509334), Oct 13, 2013: SUPPORT ANGLE. CRACKED. CARGO TRACK SUPPORT ANGLE CRACKED AT LBL 27 AT FS 621 BELOW FLOOR AT WL 73.50. REMOVED SUPPORT ANGLE IAW SRM 51-77-00 AND 51-42-21. INSTALLED NEW SUPPORT ANGLE 
- [SDR ASOA2013110509333](https://openairdocs.org/sdr/ASOA2013110509333), Oct 13, 2013: ANGLE. CRACKED. ANGLE CRACKED BELOW AFT CARGO DOOR PULLEY BRACKET AT FS 621. REMOVED ANGLE IAW SRM 51-42-21 AND INSTALLED NEW ANGLE IAW SRM 51-42-21, 51-42-02 AND DWG 601R35050
- [SDR ASOA2013110509332](https://openairdocs.org/sdr/ASOA2013110509332), Oct 13, 2013: BRACKET. CRACKED. CARGO DOOR FWD LOWER SUPPORT BRACKET CRACKED. REMOVED SUPPORT BRACKET IAW SRM 51-42-06. INSTALLED SUPPORT BRACKET IAW SRM 51-42-06 AND DWG 601R35050.
- [SDR ASOA2013110509331](https://openairdocs.org/sdr/ASOA2013110509331), Oct 13, 2013: STIFFENER. CRACKED. STIFFENER ON THE INTERIOR OF THE LT WING L/E AT PANEL 530DZ IS CRACKED. REMOVED DAMAGED EDGING FROM WING L/E WS 149.58 TO 247.95 IAW SRM 51-42-06 AND 51-42-13. 
- [SDR ASOA2013101709236](https://openairdocs.org/sdr/ASOA2013101709236), Oct 13, 2013: ISOLATOR. BROKEN. BROKEN ISOLATOR FOUND ON AFT PRESSURE BULKHEAD FWD FACE. R & R ISOLATOR IAW SRM 51-42-06-00 AND SRM 51-42-13-00.
- [SDR ASOA2013110509330](https://openairdocs.org/sdr/ASOA2013110509330), Oct 12, 2013: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED ON AFT SIDE PRESSURE BULKHEAD AT FS 621, STR 14L. R & R INTERCOSTAL IAW SRM 51-42-20-00 DWG NR 601-35012.
- [SDR ASOA2013110509329](https://openairdocs.org/sdr/ASOA2013110509329), Oct 12, 2013: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED ON AFT SIDE PRESSURE BULKHEAD AT FS 621 STR 14R. REMOVED & INSTALLED NEW INTERCOSTAL IAW SRM 51-42-20 DWG 601-35012.
- [SDR ASOA2013110509328](https://openairdocs.org/sdr/ASOA2013110509328), Oct 12, 2013: BRACKET. CRACKED. CRACKED BRACKET INBD SIDE FS 484, LBL 27. R & R BRACKET IAW SRM 51-42-21.
- [SDR ASOA2013110509327](https://openairdocs.org/sdr/ASOA2013110509327), Oct 12, 2013: BRACKET. CRACKED. LT BRACKET CRACKED AT FS 718, BELOW STR 11L. REPAIRED IAW REO 601R-53-61-5060.
- [SDR ASOA2013110509326](https://openairdocs.org/sdr/ASOA2013110509326), Oct 11, 2013: SILL. CORRODED. CARGO DOOR SILL CORRODED BS 574 -621. REMOVED CORROSION IAW SRM 51-21-06. FOUND OUT OF LIMITS IAW SRM 53-61-23, TR 53-27, FIG 10Z. MAJOR REPAIR.
- [SDR ASOA2013110509325](https://openairdocs.org/sdr/ASOA2013110509325), Oct 11, 2013: FLOOR SUPPORT. CORRODED. LEFT CABIN FLOOR SUPPORT CORRODED FS 409 TO 559. REPAIRED IAW REO 601R-53-41-666. MAJOR REPAIR.
- [SDR ASOA2013110509324](https://openairdocs.org/sdr/ASOA2013110509324), Oct 11, 2013: FLOOR SUPPORT. CORRODED. RT CABIN FLOOR SUPPORT CORRODED FS 409 TO 559. BLENDED CORROSION DAMAGE IAW SRM 51-21-06-00. REPAIRED IAW REO 601R-53-41-666.
- [SDR ASOA2013110509323](https://openairdocs.org/sdr/ASOA2013110509323), Oct 11, 2013: HINGE FITTING. GOUGED. LT INBD FLAP, INBD HINGE, LOWER OUTBD LUG GOUGED ON OTBD SIDE. BLENDED DAMAGE IAW SRM 51-12-00, REMOVED .007" MATERIAL IN DAMAGED AREA OF LT INBD FLAP, INBD HIN
- [SDR ASOA2013110509322](https://openairdocs.org/sdr/ASOA2013110509322), Oct 11, 2013: LIGHT. BROKEN. GALLEY CLOSE OUT PANEL HAS BROKEN EMERGENCY EXIT LIGHT. R & R EMERGENCY LIGHT SIGN ON GALLEY CLOSE OUT PANEL IAW AMM 33-51-13-000-801/33-51-13-400-801. EMERGENC
- [SDR ASOA2013110509321](https://openairdocs.org/sdr/ASOA2013110509321), Oct 10, 2013: FITTING. CRACKED. NLG DOOR ACTUATOR FITTING CRACKED AT LOWER SECTION. REMOVED RT DOOR MECHANISM ASSY IAW AMM 32-22-14-000-801 BUILT UP DOOR MECHANISM ASSY IAW ACMM 32-30-20 INSTA
- [SDR ASOA2013110709352](https://openairdocs.org/sdr/ASOA2013110709352), Oct 9, 2013: SKIN. BURNED. BURN ON SKIN BETWEEN FS 235 - 250 AND STRINGERS 22L AND 23L. REPAIRED IAW SRM 51-42-13 AND GREO 601R-53-00-115 REV E. MAJOR REPAIR.
- [SDR ASOA2013062403887](https://openairdocs.org/sdr/ASOA2013062403887), Jun 20, 2013: LENS. BROKEN. EMERGENCY OVERWING EXIT LIGHT ON THE RT SIDE. GLASS BROKEN. REINSTALLED RT EMERGENCY LIGHT COVER ON EXIT. FUSELAGE BACK INTO PLACE IAW AMM 33-51-21. OK FOR SERV
- [SDR ASOA2013032003240](https://openairdocs.org/sdr/ASOA2013032003240), Mar 16, 2013: LIGHT. INOPERATIVE. RT MIDDLE EXTERIOR EMERGENCY LIGHT INOPERATIVE.
- [SDR ASOA2012112802544](https://openairdocs.org/sdr/ASOA2012112802544), Nov 14, 2012: STRUCTURE. CRACKED. RT WING CRACKED AT WS 148 AT REAR SPAR, CONFIRMED BY EDDY CURRENT. REPAIRED IAW REO 601R-57-21-1794, REV A, REO 601R-57-21-130-01, REO 601R-57-21-130, REV J DAT
- [SDR ASOA201201006](https://openairdocs.org/sdr/ASOA201201006), Mar 1, 2012: SENSOR. FAILED. PAX DOOR OUT HANDLE CAUTION MESSAGE IN FLIGHT. DIVERTED, & EMERGENCY DECLARED. R & R PAX DOOR OUTER HANDLE SENSOR PS2MB IAW AMM 52-70-04, OPS CHECKED GOOD.
- [SDR ASOA201102017](https://openairdocs.org/sdr/ASOA201102017), Oct 20, 2011: WEB. CRACKED. FS 280 WEB HAS A 1.5" LONG CRACK AT LBL 9.0. REO 601R-53-11-2208, REV HAS BEEN ACCOMPLISHED.
- [SDR ASOA201102012](https://openairdocs.org/sdr/ASOA201102012), Oct 19, 2011: FLOOR SUPPORT. CORRODED. CORRODED FLOOR SUPPORT BETWEEN FS 439.00 AND FS 449.85 LBL 42.00. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, REV B.
- [SDR ASOA201101945](https://openairdocs.org/sdr/ASOA201101945), Oct 11, 2011: SKIN. CORRODED. FUSELAGE BELLY SKIN HAS APPROX 20 RIVETS WITH CORROSION AROUND THEM AT FS 559.1 FS 559+18, STRINGER 25L - 25R. REPAIRED IAW REO 601R-53-00-440.
- [SDR ASOA201101944](https://openairdocs.org/sdr/ASOA201101944), Oct 11, 2011: SKIN. CORRODED. FUSELAGE BELLY SKIN HAS HEAVY CORROSION AROUND FASTENERS AT FS 559+80 - 574 S25L - 25R. REPAIRED IAW REO 601R-53-00-440.
- [SDR ASOA201101930](https://openairdocs.org/sdr/ASOA201101930), Oct 10, 2011: SILL. CORRODED. PASSENGER DOOR LOWER SILL ANGLE IS CORRODED ON INBD SIDE AROUND FASTENERS AND PROXIMITY SENSOR FS 310 - 349. REPAIRED IAW SRM 51-27-19.
- [SDR ASOA201101866](https://openairdocs.org/sdr/ASOA201101866), Oct 5, 2011: WEB. CRACKED. FS 280 WEB HAS A 1.5 INCH LONG CRACK AT LBL 9.0. REPAIRED IAW REO 601R-53-11-2208.
- [SDR ASOA201101856](https://openairdocs.org/sdr/ASOA201101856), Oct 5, 2011: FRAME. CORRODED. FUSELAGE FRAME AT FS 605 IS CORRODED BETWEEN STR 25 LT & RT. REPAIRED IAW ALL SRM`S.
- [SDR ASOA201101855](https://openairdocs.org/sdr/ASOA201101855), Oct 5, 2011: FRAME. CORRODED. FUSELAGE FRAME AT FS 605 IS CORRODED. BETWEEN S25 LT & RT. REPAIRED IAW ALL SRM`S.
- [SDR ASOA201101853](https://openairdocs.org/sdr/ASOA201101853), Oct 4, 2011: WEB. CRACKED. FS 280, WEB HAS A 1.5 INCH LONG CRACK AT LBL 9. REPAIRED IAW SRM 51-42-13.
- [SDR ASOA201101846](https://openairdocs.org/sdr/ASOA201101846), Oct 3, 2011: SUPPORT ANGLE. CRACKED. LT WING INBD AFT PANEL SUPPORT ANGLE CRACKED ON AFT TOP SIDE FAR INBD SUPPORT ANGLE. R & R ANGLE IAW SRM 51-42-21. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR.
- [SDR ASOA201101831](https://openairdocs.org/sdr/ASOA201101831), Sep 29, 2011: FLOORBEAM. CORRODED. FLOORBEAM AT FS 349 IS CORRODED BETWEEN RBL 36 AND RBL 45. REPAIRED IAW REO 601R-53-21-2185.
- [SDR ASOA201101830](https://openairdocs.org/sdr/ASOA201101830), Sep 26, 2011: SILL. CORRODED. FOUND CORROSION BETWEEN FS 521 & FS 544 NEAR LBL 42 ON SILL ANGLE & SILL PANEL. REPAIRED IAW REO 601R-53-41-666.

All 173: https://openairdocs.org/aircraft/N838AS/unmatched-reports.md

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Ea Vision EA J100 aircraft: https://openairdocs.org/model/ea-vision-ea-j100/aircraft.md

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