# N858AS: 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: EAVUAV502585750 - Type: Rotorcraft - Engine type: Electric - Certificate issued: June 23, 2025 - Expires: June 30, 2032 - Mode S code: ABC521 - 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=858AS - Page: https://openairdocs.org/aircraft/N858AS 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 N858AS. ## FAA accident and incident reports None matched to N858AS. ## Reports on N858AS not matched to an aircraft (1) They name N858AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 20100205026789I](https://openairdocs.org/incident/20100205026789I), Feb 5, 2010: Bombardier CL-600-2B19 (N858AS), Cleveland, OH, No damage. During the takeoff roll, after crew acknowledged their 80 kt call out, the aircraft had begun to shake violently. The captain knew either one or both of the… ## 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 N858AS not matched to an aircraft (141, newest 50) They name N858AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR ASOA201705301633](https://openairdocs.org/sdr/ASOA201705301633), May 30, 2017: WHEEL. BROKEN. SUPPORT WHEEL BROKEN. PASSENGER DOOR ASSEMBLY REMOVED AND REPLACED, OPS CHECKED GOOD . ACFT OK FOR CONTINUED SERVICE. - [SDR ASOA2015121814232](https://openairdocs.org/sdr/ASOA2015121814232), Dec 18, 2015: WIRE. DAMAGED. EXIT LIGHT ON F/A STATION INOPERATIVE. R & R WIRE SPLICE CONNECTOR ON EMERGENCY LIGHT, DS10LN, IAW ESPM 20-17-31. OPS TEST GOOD. - [SDR ASOA2015121714231](https://openairdocs.org/sdr/ASOA2015121714231), Dec 17, 2015: WIRE. BROKEN. EXIT LIGHT TRIM PANEL NEXT TO GALLEY 1 HAS A BROKEN WIRE. TERMINATED FEMALE SPLICE CONNECTOR FOR EXIT LIGHT ON RT FWD DOOR TRIM IAW ESPM 20-17-31. PERFORMED OPS - [SDR ASOA2015112914227](https://openairdocs.org/sdr/ASOA2015112914227), Nov 29, 2015: FLOOR SUPPORT. CORRODED. FLOORBEAM CAP CORRODED BETWEEN FS 554.00 +64 AND FS 559.0+45 AT RBL9. REMOVED CORROSION FROM FLOORBEAM AT RBL 9 BETWEEN FS 559.00+48-559.00+64 IAW SRM 51-21-06. - [SDR ASOA2015112914185](https://openairdocs.org/sdr/ASOA2015112914185), Nov 29, 2015: FLOORBEAM. CORRODED. FLOORBEAM CORRODED AT FS 621.00, RBL9. REMOVED CORROSION FROM FLOORBEAM AT FS621 AT RBL9 IAW SRM 51-21-06. DAMAGED FOUND TO BE OUT OF LIMITS IAW SRM 53-61-43 AN - [SDR ASOA2015112814226](https://openairdocs.org/sdr/ASOA2015112814226), Nov 28, 2015: FLOORBEAM. CORRODED. CORROSION ON RBL 9 FLOORBEAM CAP FWD OF FS 409.00 + 16. REMOVED CORROSION ON RBL9 FLOORBEAM CAP FWD PF FS 409.00+16 IAW SRM 51-21-06. REPAIRED IAW SRM 53-00-43. - [SDR ASOA2015112814225](https://openairdocs.org/sdr/ASOA2015112814225), Nov 28, 2015: SEAT TRACK. CORRODED. RBL9 SEAT TRACK CORRODED AND OUT OF LIMITS BETWEEN FS 409 +112 AND FS 394. REMOVED CORRODED SEAT TRACK AT RBL9, FS 394-FS 409+112 IAW TASK 53-01-11-000-802. DRI - [SDR ASOA2015112814224](https://openairdocs.org/sdr/ASOA2015112814224), Nov 28, 2015: SEAT TRACK. CORRODED. LBL9 SEAT TRACK CORRODED AND OUT-OF-LIMITS AT FS 394 TO FS 409 + 112. REMOVED SEAT RAIL AT FS 394 - FS 409+112 IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT RAIL - [SDR ASOA2015112814179](https://openairdocs.org/sdr/ASOA2015112814179), Nov 28, 2015: SEAT TRACK. CORRODED. RBL9, SEAT TRACK CORRODED AND OUT-OF-LIMITS BETWEEN FS 364 TO 394. R & R SEAT TRACK IAW AMM 53-01-11-00-802 AND 53-01-11-400-802. - [SDR ASOA2015112814178](https://openairdocs.org/sdr/ASOA2015112814178), Nov 28, 2015: SEAT TRACK. CORRODED. LBL 9 SEAT TRACK CORRODED AND OUT OF LIMITS BETWEEN BS 364 - 394. R & R SEAT TRACK IAW AMM 53-01-11-00-802 AND 53-01-11-400-802. - [SDR ASOA2015112714177](https://openairdocs.org/sdr/ASOA2015112714177), Nov 27, 2015: INTERCOSTAL. CORRODED. BAY DOOR INTERCOSTAL AT BS 349-409 BETWEEN STR 26 AND 27L IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06. INTERCOSTAL AT FS 394-FS 409 BETWEEN STR 27-26L IS OU - [SDR ASOA2015112714176](https://openairdocs.org/sdr/ASOA2015112714176), Nov 27, 2015: SEAT TRACK. CORRODED. RIGHT SIDEWALL SEAT TRACK FS409+16-409+112 HAS CORROSION. REMOVED CORROSION ON RT SIDE SEAT RAIL BETWEEN FS 409+16-409+112 IAW SRM 51-21-06. DAMAGE FOUND TO BE - [SDR ASOA2015112714175](https://openairdocs.org/sdr/ASOA2015112714175), Nov 27, 2015: SEAT TRACK. CORRODED. RIGHT SIDEWALL SEAT TRACK FS364-409.16 HAS CORROSION. REMOVED CORROISON ON RT SIDE SEAT RAIL BETWEEN FS364-409+16 IAW SRM 51-21-06. DAMAGE FOUND TO BE OUT OF LI - [SDR ASOA2015112414223](https://openairdocs.org/sdr/ASOA2015112414223), Nov 24, 2015: SKIN. CRACKED. FUSELAGE SKIN IS CRACKED AT FS 235.00 S26R. RECIEVED AND COMPLIED WITH REO 601R-53-11-2844. COMPLIED WITH EC/TC REO 601R-53-11-0048 IAW REO 601R-53-11-0048, REV - [SDR ASOA2015112414222](https://openairdocs.org/sdr/ASOA2015112414222), Nov 24, 2015: FLOOR PANEL. CRACKED. BS 193 ELECTIRCAL BAY FLOOR CRACKED RT SIDE. REPAIRED ELECTRICAL BAY FLOOR AT BS 193.0, RT SIDE, IAW GREO 601R-53-11-111. UPON FURTHER EVALUATION FOUND GREO 601 - [SDR ASOA2015102813980](https://openairdocs.org/sdr/ASOA2015102813980), Oct 28, 2015: HANDLE. FOULED. F/A REPORT MAIN AIR SERVICE DOOR IS HARD TO OPEN. FOUND FOD AT MAIN PAX DOOR LEVEL HANDLE. REMOVED FOD. OPS CHECK TEST GOOD, REF AMM 52-11-21. - [SDR ASOA2015102013934](https://openairdocs.org/sdr/ASOA2015102013934), Oct 20, 2015: INVERTER. UNSERVICEABLE. RT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. R & R INVERTER NR 3 IAW AMM 33-51-07. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION. - [SDR ASOA2015101113886](https://openairdocs.org/sdr/ASOA2015101113886), Oct 11, 2015: LAMP. BURNED OUT. EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21. SYSTEM OPS CHECKED GOOD. - [SDR ASOA2015100513869](https://openairdocs.org/sdr/ASOA2015100513869), Oct 5, 2015: FITTING. DAMAGED. UPPER ATTACH FITTINGS HAD TOOL DAMAGE ON BOTH INBD FACES. BLENDED IAW SRM 51-12-00. FOUND TO BE OUT OF LIMITS IAW SRM 55-11-27. REPAIRED IAW REO 601R-55-11-522. - [SDR ASOA2015030412317](https://openairdocs.org/sdr/ASOA2015030412317), Mar 2, 2015: SIGN. MISSING. CEILING EXIT SIGN MISSING. INSTALLED CEILING EXIT SIGN IAW AMM 33-51-14. - [SDR ASOA2014073010984](https://openairdocs.org/sdr/ASOA2014073010984), Jul 27, 2014: LENS. MISSING. FWD CABIN ENTRANCE EMERGENCY FLOOR FLOOD LIGHT COVER MISSING. INSTALLED LENS IAW AMM 33-51-19. OP'S CHECKED GOOD. - [SDR ASOA2014062310715](https://openairdocs.org/sdr/ASOA2014062310715), Jun 19, 2014: BULB. BURNED OUT. RT EXTERIOR NR 6 EMERGENCY LIGHT INOPERATIVE. PERFORMED OPS TEST OF EXTERIOR EMERGENGY LIGHTS, REPLACED THE BULBS AS REQUIRED IAW AMM 33-51-00. OPS CHECKED GOOD - [SDR ASOA2014031910157](https://openairdocs.org/sdr/ASOA2014031910157), Mar 10, 2014: SKIN. DAMAGED. A HOLE IS IN THE SKIN OF THE AC RT SIDE AT THE FWD END OF THE FLAP STUB FAIRING THIS WAS FOUND WHILE GIVING AN OK TO INSTALL THE RT FLAP STABILIZER FAIRING. COM - [SDR ASOA2014031910156](https://openairdocs.org/sdr/ASOA2014031910156), Feb 27, 2014: WINDOW FRAME. CRACKED. WINDSHIELD CENTER POST LOWER RT FITTING CRACKED. REMOVED FITTING ON W/S CENTER POST LWR RT SIDE IAW SRM 51-42-21. DRILLED UP NEW FITTING IAW SRM 51-40-11. THIS - [SDR ASOA2014031910155](https://openairdocs.org/sdr/ASOA2014031910155), Feb 24, 2014: FLOOR SUPPORT. CORRODED. UPPER LT FLOOR SUPPORT FITTING CORRODED. LOCATED & DRILLED NEW UPPER LT FLOOR SUPPORT FITTING IAW DWG 601RR38672-7 & SRM 51-42-06. INSTALLED NEW SERVICEABLE FIT - [SDR ASOA2014031910154](https://openairdocs.org/sdr/ASOA2014031910154), Feb 20, 2014: STRAP. CRACKED. LEFT WING LOWER TIE STRAP FOR LOWER SKIN AT WS 148.019 CRACKED. REMOVED STRAP IAW SRM 51-42-20-00 AND SRM 51-42-06-00. INSTALLED IAW SRM 51-42-06, 51-42-20 DWG - [SDR ASOA2014031910153](https://openairdocs.org/sdr/ASOA2014031910153), Feb 19, 2014: INSERT. DAMAGED. FLOOR PANEL 282HRF HAS DAMAGED SCREW INSERTS. REMOVED AND INSTALLED NEW INSERTS IAW C AND D RPM 25-6000-1. - [SDR ASOA2014031910152](https://openairdocs.org/sdr/ASOA2014031910152), Feb 19, 2014: FRAME. CORRODED. FRAME BS 349 CORRODED BETWEEN S25L AND 26R. R & R FRAME SECTOR IAW SRM 51-42-06-00, 51-42-21-00 AND DWG 601R32005. MAJOR REPAIR. - [SDR ASOA2014031910151](https://openairdocs.org/sdr/ASOA2014031910151), Feb 19, 2014: FRAME. CORRODED. FRAME BS 333 CORRODED BETWEEN S26 - 27L. REMOVED CORROSION IAW SRM 51-21-06 AND 51-12-00. COMPLIED WITH PERMANENT REPAIR EA 12-2014-046 NDTM PT-1, 51-20-06. - [SDR ASOA2014031910150](https://openairdocs.org/sdr/ASOA2014031910150), Feb 19, 2014: FLOOR SUPPORT. CORRODED. LEFT CABIN FLOOR SUPPORT CORRODED IN SEVERAL AREAS BETWEEN BS 439-544. COMPLIED WITH ECTC REO 601R-53-41-666. - [SDR ASOA2014031910149](https://openairdocs.org/sdr/ASOA2014031910149), Feb 19, 2014: FLOOR SUPPORT. CORRODED. RIGHT CABIN FLOOR SUPPORT CORRODED IN SEVERAL AREAS BETWEEN BS 439 - 516. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, REV C. MAJOR REPAIR. - [SDR ASOA2014031910148](https://openairdocs.org/sdr/ASOA2014031910148), Feb 19, 2014: BULKHEAD. GOUGED. SCREW DAMAGE ON REAR PRESSURE BULKHEAD FORWARD FACE BETWEEN LBL 18.00 & LBL 27.50 JUST ABOVE WL 73.50. BLEND OUT DAMAGED AREA IAW SRM 51-12-00. COMPLIED WITH ST - [SDR ASOA2014031910147](https://openairdocs.org/sdr/ASOA2014031910147), Feb 19, 2014: BULKHEAD. GOUGED. SCREW DAMAGE ON REAR PRESSURE BULKHEAD FORWARD FACE AT RBL 36.20 BETWEEN 2ND AND 3RD ISOLATOR FROM BOTTOM. BLEND OUT DAMAGED AREA IAW SRM 51-12-00. COMPLIED WIT - [SDR ASOA2014031910146](https://openairdocs.org/sdr/ASOA2014031910146), Feb 19, 2014: BULKHEAD. GOUGED. SCREW DAMAGE ON REAR PRESSURE BULKHEAD FWD FACE AT RBL 27.50 BETWEEN 2ND AND 3RD ISOLATOR FROM BOTTOM. BLEND OUT DAMAGED AREA IAW SRM 51-12-00. COMPLIED WITH RE - [SDR ASOA2014031910145](https://openairdocs.org/sdr/ASOA2014031910145), Feb 19, 2014: BULKHEAD. GOUGED. SCREW DAMAGE ON REAR PRESSURE BULKHEAD FWD FACE AT RBL 18.00 BETWEEN 2ND AND 3RD ISOLATOR FROM BOTTOM. COMPLIED WITH REO 601R-53-61-2155. - [SDR ASOA2014031910144](https://openairdocs.org/sdr/ASOA2014031910144), Feb 19, 2014: PANEL. DAMAGED. STAB TIP PANEL 343AR ERODED. REPAIRED ERODED TIP ON TAB PANEL 343AR IAW SRM 51-15-52 AND SRM 51-74-02. REPAIRED LIGHTING PROTECTION STRIP IAW D/G DOCUMENT 71015 - [SDR ASOA2014031910143](https://openairdocs.org/sdr/ASOA2014031910143), Feb 19, 2014: HINGE. GOUGED. PASSENGER DOOR HINGE FUSELAGE SIDE 15TH LUG FROM FRONT IS GOUGED. COMPLIED WITH REO 601R-53-21-814, REV. MAJOR REPAIR. - [SDR ASOA2014031910142](https://openairdocs.org/sdr/ASOA2014031910142), Feb 18, 2014: ANGLE. CORRODED. PAX DOOR SILL LOWER ATTACH ANGLE MISSING. INSTALLED SILL ANGLE IAW DWG 601R-31-527-221, 51-42-21, 51-42-13, 51-42-06, SRM 51-22-00. MAJOR REPAIR - [SDR ASOA2014031910141](https://openairdocs.org/sdr/ASOA2014031910141), Feb 18, 2014: STRAP. CRACKED. RT WING LOWER TIE STRAP FOR LOWER SKIN AT WS 148.019 CRACKED. REMOVED AND REPLACED STRAP IAW SRM 51-42-20-00 & SRM 51-42-06-00 & DWG 601R10336. - [SDR ASOA2014031910140](https://openairdocs.org/sdr/ASOA2014031910140), Feb 18, 2014: STRUCTURE. CRACKED. TRU SHELF CRACKED LT SIDE OTBD OF SERVICING GAUGE, BS 193. COMPLIED WITH REO 601R53-11-081. RECEIVED AND COMPLIED WITH REO 601R-53-2634. MAJOR REPAIR. - [SDR ASOA2014031710139](https://openairdocs.org/sdr/ASOA2014031710139), Feb 18, 2014: FLOOR SUPPORT. CRACKED. COCKPIT FLOOR SUPPORT AFT LT CORNER CRACKED. REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-42-06. LOCATED AND DRILLED HOLES ON NEW FLOOR SUPPORT ANGLE IAW SRM 51-42-06 - [SDR ASOA2014031710138](https://openairdocs.org/sdr/ASOA2014031710138), Feb 18, 2014: ATTACH ANGLE. CRACKED. AFT BULKHEAD ZEE MEMBER TO SKIN ATTACH ANGLE APPEARS CRACKED. REMOVED ATTACH ANGLE AT FS 625 & STR16L IAW SRM 51-42-06 & SRM 51-42-21. REMOVED & DRILLED UP NEW - [SDR ASOA2014031410137](https://openairdocs.org/sdr/ASOA2014031410137), Feb 18, 2014: LUG. GOUGED. PAX DOOR HINGE LUG 2, 5, 8, 14, 19 & 25 GOUGED. COMPLIED WITH REO 601R-52-11-1347. COMPLIED WITH ECTC REP 601R-52-11-1347. MAJOR REPAIR. - [SDR ASOA2014031410136](https://openairdocs.org/sdr/ASOA2014031410136), Feb 18, 2014: ANGLE. CRACKED. LT FS 625 ANGLE BROKEN ON T/E. REMOVED AND REPLACED ANGLE IAW SRM 51-42-21, DWG 601R350126 AND 601-35012. - [SDR ASOA2014031410135](https://openairdocs.org/sdr/ASOA2014031410135), Feb 18, 2014: PANEL. DAMAGED. PANEL 121AL HAS ERROSION DAMAGE. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. COMPLETED REPAIR OF PANEL 121AL IAW SRM 51-74-02. - [SDR ASOA2014022710029](https://openairdocs.org/sdr/ASOA2014022710029), Feb 18, 2014: FLOORBEAM. CRACKED. UPPER RADIUS OF FLOORBEAM ANGLE CRACKED, RBL 9 BS 280. R & R FLOORBEAM ANGLE IAW SRM 51-42-21. - [SDR ASOA2013122009673](https://openairdocs.org/sdr/ASOA2013122009673), Dec 19, 2013: FLASHLIGHT. INTERMITTENT. CAPTAIN`S FLASHLIGHT GOES IN AND OUT. R & R FLASHLIGHT IAW AMM 25-61-02. - [SDR ASOA2013022803082](https://openairdocs.org/sdr/ASOA2013022803082), Feb 24, 2013: LAMP. BURNED OUT. CABIN CEILING EMERGENCY LIGHT 2ND FROM AFT INOP. RELAMPED CABIN CEILING EMERGENCY LIGHT AT 4-5CD IAW AMM 33-51-16, OPS CHECKED GOOD. - [SDR ASOA201200504](https://openairdocs.org/sdr/ASOA201200504), Feb 15, 2012: WIRE. DAMAGED. LEFT 14TH STAGE BLEED DUCT WARNING MESSAGE. EMERGENCY DECLARED. REPAIRED WIRE AT LT PYLON IAW ESPM 20-16-00, PERFORMED OPS TEST OF BLEED LEAK DETECTION SYS IAW - [SDR ASOA2012012500333](https://openairdocs.org/sdr/ASOA2012012500333), Jan 25, 2012: ANGLE. CORRODED. AFT CORNER OF ASD ON HINGE END IS CORRODED. REMOVED AFT CORNER OF ASD AT HINGE END CORRODED. INSTALLED AFT CORNER OF ASD HINGE END IAW SRM 51-42-06, 51-42-13. R All 141: https://openairdocs.org/aircraft/N858AS/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 --- 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.