# N794AS: 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: EAVUAV502585798
- Type: Rotorcraft
- Engine type: Electric
- Certificate issued: August 7, 2025
- Expires: August 31, 2032
- Mode S code: AAC6F2
- Registered owner: [Falling Tree Drone Service LLC](https://openairdocs.org/faa-owner/FALLING%20TREE%20DRONE%20SERVICE%20LLC)
- Location: [Idaville, IN](https://openairdocs.org/faa-place/IN/Idaville)
- Owner type: LLC
- Owner's area on the map: 40.8017° N, 86.6535° W: Placed by OpenAirDocs at the center of ZIP code 47950, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=794AS
- Page: https://openairdocs.org/aircraft/N794AS

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 N794AS.

## FAA accident and incident reports

None matched to N794AS.

## 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 N794AS not matched to an aircraft (126, newest 50)

They name N794AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR ASAA2017010519267](https://openairdocs.org/sdr/ASAA2017010519267), Jan 5, 2017: SIGN. DETACHED. LEFT ROW EXIT SIGN DETACHED. ACFT GROUNDED. REINSTALLED AND SECURED THE SIGN.
- [SDR ASAA2016102618667](https://openairdocs.org/sdr/ASAA2016102618667), Oct 26, 2016: WEB. CRACKED. WHILE ACCOMPLISHING NDT OPEN HOLE INSPECTION ON LT WING WEB, UPPER ROW FASTENER HOLE AT APPROX. RSS 222.5 WAS FOUND TO BE CRACKED IN WEB. ACFT GROUNDED. REPAIRE
- [SDR ASAA2016102418538](https://openairdocs.org/sdr/ASAA2016102418538), Oct 24, 2016: SKIN. CHAFED. RIGHT WING INBD FLAP UPPER SURFACE INBD END SKIN IS CHAFED. ACFT GROUNDED. BLENDED THE FLAP SKIN AND FOUND TO BE OUT OF LIMITS. INSTALLED A REPAIR IAW SRM 57-53
- [SDR ASAA2016102218537](https://openairdocs.org/sdr/ASAA2016102218537), Oct 22, 2016: BEARING. MIGRATED. NR 4 SPOILER SECOND FROM OTBD HINGE HAS A MIGRATING BEARING. ACFT GROUNDED. REMOVED THE NR 4 SPOILER HINGE AND INSTALLED A NEW HINGE IAW SRM 51-40-04.
- [SDR ASAA2016102118663](https://openairdocs.org/sdr/ASAA2016102118663), Oct 21, 2016: SPAR. CRACKED. LEFT WING REAR SPAR UPPER CHORD CRACKED AT APPROX RSS 216. ACFT GROUNDED. REPAIRED THE WING R & R THE SPAR UPPER ANGLE IAW SRM 57-20-10-2R-4 REPAIR 4
- [SDR ASAA2016102018482](https://openairdocs.org/sdr/ASAA2016102018482), Oct 20, 2016: ATTACH ANGLE. CRACKED. INTERCOSTAL ATTACH ANGLE CRACKED BS 291 BETWEEN STRINGERS 13 AND 14R. ACFT GROUNDED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-02-0G-0.
- [SDR ASAA2016030115675](https://openairdocs.org/sdr/ASAA2016030115675), Mar 1, 2016: LENS. DETACHED. LEFT WING OVERWING, EXIT SIGN WILL NOT SECURE INTO PLACE. GROUNDED. REPLACED LT WING OVERWING EXIT SIGN IAW AMM 33-51-22.
- [SDR ASAA2015122614475](https://openairdocs.org/sdr/ASAA2015122614475), Dec 26, 2015: LENS. DETACHED. EXIT SIGN OVER EXIT ROW A/C RT HAS DETACHED. ACFT GROUNDED. REATTACHED EMERGENCY EXIT SIGN OVER EXIT ROW A/C RT. NO DEFECTS NOTED.
- [SDR ASAA2015071012721](https://openairdocs.org/sdr/ASAA2015071012721), Jul 10, 2015: FRAME. CRACKED. FRAME AT BS 747 IS CRACKED BETWEEN STRINGERS 8 - 9L. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609, 400-53-134, REV NEW.
- [SDR ASAA2015071012720](https://openairdocs.org/sdr/ASAA2015071012720), Jul 10, 2015: FRAME. CRACKED. FRAME AT BS 727D BETWEEN STR 8 - 9R IS CRACKED. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609, 400-53-134, REV NEW.
- [SDR ASAA2015071012714](https://openairdocs.org/sdr/ASAA2015071012714), Jul 10, 2015: FRAME. CRACKED. FRAME BS 787 BETWEEN STRINGERS 8 - 9R FOUND CRACKED. ACFT GROUNDED. REPAIRED THE FRAME IAW EA AD20062609, 400-53-134, REV NEW.
- [SDR ASAA2015071012713](https://openairdocs.org/sdr/ASAA2015071012713), Jul 10, 2015: FRAME. CRACKED. CABIN FRAME AT BS 827 BETWEEN STR 8L AND 9L IS CRACKED. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609, 400-53-134, REV NEW DATED 14AUG15 WORKFRONT NOTIFICATIO
- [SDR ASAA2015070812719](https://openairdocs.org/sdr/ASAA2015070812719), Jul 8, 2015: FRAME. CRACKED. FRAME AT BS 480 CRACKED BETWEEN S 8 - 9R. ACFT GROUNDED. REPAIRED THE FRAME IAW EA AD20062609, 400-53-134, REV NEW.
- [SDR ASAA2015070812718](https://openairdocs.org/sdr/ASAA2015070812718), Jul 8, 2015: FRAME. CRACKED. FRAME AT BS 440 CRACKED BETWEEN S8 - 9R. ACFT GROUNDED. REPAIRED THE FRAME IAW EA AD20062609, 400-53-134, REV NEW.
- [SDR ASAA2015070812717](https://openairdocs.org/sdr/ASAA2015070812717), Jul 8, 2015: FRAME. CRACKED. FRAME AT BS 400 CRACKED BETWEEN S8 - 9R. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609, 400-53-134, REV NEW.
- [SDR ASAA2015070714495](https://openairdocs.org/sdr/ASAA2015070714495), Jul 7, 2015: CARGO TRACK. CORRODED. AFT CARGO TRACK, RBL 13 IS CORRODED AT BS 764-877. ACFT GROUNDED. REPAIRED AFT PIT CARGO TRACK BS 764-877, RBL 13.8 IAW EA 400, 53EA 15553 AND SRM 53-00-53-2R-2
- [SDR ASAA2015070712740](https://openairdocs.org/sdr/ASAA2015070712740), Jul 7, 2015: CARGO TRACK. CORRODED. CARGO TRACK RBL 13 IS CORRODED AT BS 764-877. ACFT GROUNDED. REPAIRED THE CARGO TRACK IAW EA AND SRM.
- [SDR ASAA2015070712716](https://openairdocs.org/sdr/ASAA2015070712716), Jul 7, 2015: FRAME. CRACKED. FRAME AT BS 400 CRACKED BETWEEN S7 - 8L. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20062609, 400-53-134, REV NEW.
- [SDR ASAA2015070712715](https://openairdocs.org/sdr/ASAA2015070712715), Jul 7, 2015: FRAME. CRACKED. FRAME AT BS 360 CRACKED BETWEEN S8 - 9L. ACFT GROUNDED. REPAIRED THE FRAME IAW EA AD20062609, 400-53-134, REV NEW.
- [SDR ASAA2015070712493](https://openairdocs.org/sdr/ASAA2015070712493), Jul 7, 2015: ATTACH ANGLE. CRACKED. INTERCOSTAL TO FRAME ATTACH ANGLE CRACKED AT STA 348 AND S-14L. ACFT GROUNDED. R & R ATTACH ANGLE IAW SRM 51-40-02-0G-0.
- [SDR ASAA2015070614489](https://openairdocs.org/sdr/ASAA2015070614489), Jul 6, 2015: FITTING. CORRODED. L1 DOOR AFT GIRT BAR FITTING FLOOR BRACKET BS 344 IS CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-1. R & R GIRT 
- [SDR ASAA2015070612639](https://openairdocs.org/sdr/ASAA2015070612639), Jul 6, 2015: FLOORBEAM. CORRODED. FLOORBEAM BS 344 IS CORRODED AT LBL 11.1 AROUND FASTENER. ACFT GROUNDED. REPAIRED THE FLOORBEAM IAW EA 400 53EA 15489.
- [SDR ASAA2015070612422](https://openairdocs.org/sdr/ASAA2015070612422), Jul 6, 2015: FLOORBEAM. CORRODED. FWD FLOORBEAM, BS 312 CORRODED AT LBL 11 AND RBL 10 ON UPPER CAP. ACFT GROUNDED. CORROSION WAS FOUND TO BE OUT OF LIMITS, REMOVED DAMAGE AND REPAIRED IAW SRM 51
- [SDR ASAA2015070512670](https://openairdocs.org/sdr/ASAA2015070512670), Jul 5, 2015: FRAME. CORRODED. BS 992, FRAME CORRODED, WL 208 - 212. ACFT GROUNDED. REMOVED CORROSION, AND FOUND TO BE OUT OF LIMITS. , REPAIRED IAW EA 400, 53EA-15509.
- [SDR ASAA2014033107432](https://openairdocs.org/sdr/ASAA2014033107432), Mar 31, 2014: STOP FITTING. CRACKED. L1 DOOR UPPER AFT STOP PIN FITTING CRACKED, NDT VERIFIED, FOUND DURING LINER INSTALL. ACFT GROUNDED. R & R L1 DOOR UPPER AFT STOP IN FITTING IAW EA 400-52, EA-1
- [SDR ASAA2014032107333](https://openairdocs.org/sdr/ASAA2014032107333), Mar 21, 2014: SKIN. DELAMINATED. RT WING NR 5 SLAT INBD UPPER AFT CORNER EXISTING REPAIR IS DELAMINATED. ACFT GROUNDED. REPAIRED IAW SRM 51-70-10-2R-4, REPAIR 4.
- [SDR ASAA2014032107332](https://openairdocs.org/sdr/ASAA2014032107332), Mar 21, 2014: SKIN. DELAMINATED. RIGHT WING NR 5 SLAT OTBD UPPER CORNER IS DELAMINATED. ACFT GROUNDED. REPAIRED IAW SRM 51-70-10-2R-4, REPAIR 4.
- [SDR ASAA2014032107331](https://openairdocs.org/sdr/ASAA2014032107331), Mar 21, 2014: SKIN. CHAFED. LEFT INBD EXHAUST GATE OTBD UPPER SKIN IS CHAFED. ACFT GROUNDED. REPAIRED EXHAUST GATE UPPER SKIN IAW SRM 57-53-01-2R-10, PARA 7.
- [SDR ASAA2014032107289](https://openairdocs.org/sdr/ASAA2014032107289), Mar 21, 2014: SUPPORT ANGLE. CORRODED. AFT CARGO EQUIPMENT BAY LT AFT BS 947, L28L TRANSITION ANGLE END BACKSIDE HAS HEAVY CORROSION. ACFT GROUNDED. FABRICATED, LOCATED, DRILLED AND INSTALLED NEW SEC
- [SDR ASAA2014032107288](https://openairdocs.org/sdr/ASAA2014032107288), Mar 21, 2014: FRAME. CRACKED. LT FRAME AT BS 348 HAS A CRACKED ANGLE BELOW S15L. ACFT GROUNDED. FABRICATED NEW ANGLE IAW DWG 65-17685 AND INSTALLED IAW SRM 51-40-02-0G-0.
- [SDR ASAA2013100396099](https://openairdocs.org/sdr/ASAA2013100396099), Oct 3, 2013: ROLLER. OUT OF LIMITS. F/O WINDOW WILL NOT OPEN WHEN WINDOW LATCH IS ACTIVATED. ACFT GROUNDED. CHECKED FORCE TO OPEN AND CLOSE R2 WINDOW, FOUND TO BE OUT OF LIMITS ON HIGH SIDE IAW AM
- [SDR ASAA2013090595936](https://openairdocs.org/sdr/ASAA2013090595936), Sep 5, 2013: LENS. MISSING. AFT GALLEY L2 EXIT SIGN LENS MISSING. ACFT GROUNDED. INSTALLED EXIT LENS.
- [SDR ASAA2013081695811](https://openairdocs.org/sdr/ASAA2013081695811), Aug 16, 2013: SCREW. LOOSE. F/O R2 SLIDING WINDOW WOULD NOT SHUT. FOUND NUT AND WASHER IN WINDOW TRACK. ACFT GROUNDED. FOUND SCREW LOOSE UNDER HANDLE, R2 WINDOW. REINSTALLED HARDWARE- NO A
- [SDR ASAA2013032194215](https://openairdocs.org/sdr/ASAA2013032194215), Mar 21, 2013: STRUCTURE. GOUGED. AFT CARGO DOOR HANDLE MISSING RUBBER BUMPER AND DOOR STRUCTURE GOUGED. GOUGE IN DOOR HANDLE HOUSING IS OUT OF LIMITS REF AMM 52-31-15-801. REMOVED INTERIOR AND 
- [SDR ASAA2013021193863](https://openairdocs.org/sdr/ASAA2013021193863), Feb 11, 2013: LAMP. INOPERATIVE. EMERGENCY LIGHT EXIT LOCATOR SIGN AT RT FWD OVERWING EXIT HAS BROKEN LENS AND MULTIPLE LAMPS INOPERATIVE. REPLACED LAMP & LENS, AND TESTED IAW MM 33-51-81-962-0
- [SDR ASAA2012122093545](https://openairdocs.org/sdr/ASAA2012122093545), Dec 20, 2012: FLOOR SUPPORT. CRACKED. PAX CABIN FLOOR SUPPORT CRACKED BETWEEN STA 312 AND 328. R & R FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR ASAA2012121493601](https://openairdocs.org/sdr/ASAA2012121493601), Dec 14, 2012: CARGO TRACK. CORRODED. AFT CARGO TRACK, RBL 13.8 IS CORRODED BS 807 TO 837. REPAIRED CORRODED CARGO TRACK IAW EA -09534 .
- [SDR ASAA2012121393599](https://openairdocs.org/sdr/ASAA2012121393599), Dec 13, 2012: TRANSITION PANEL. CORRODED. AFT CARGO RT TRANSITION PANEL IS CORRODED, BS 727D, REMOVED CORROSION STA 727D, FOUND TO BE WITHIN LIMITS IAW SRM 53 60 53 1A 1, REMOVED AND INSTALLED SECTION O
- [SDR ASAA2012121293587](https://openairdocs.org/sdr/ASAA2012121293587), Dec 12, 2012: FLOOR PANEL. CORRODED. AFT CARGO BAY FLOOR PANEL FS 767 CORRODED. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53, FAB NEW FLOOR PANEL SPLICE IAW SRM 51-40-02.
- [SDR ASAA2012121293578](https://openairdocs.org/sdr/ASAA2012121293578), Dec 12, 2012: FLOOR PANEL. CORRODED. AFT CARGO BAY FLOOR PANEL, FS 767 CORRODED. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53 FAB NEW FLOOR PANEL SPLICE IAW SRM 51-40-02, W 1, O .0
- [SDR ASAA2012121193600](https://openairdocs.org/sdr/ASAA2012121193600), Dec 11, 2012: TIE DOWN. CORRODED. FWD CARGO SCUFF AFT TIE DOWN PLATE CORRODED ON LOWER SURFACE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-30-53.
- [SDR ASAA2012062692427](https://openairdocs.org/sdr/ASAA2012062692427), Jun 2, 2012: LAMP. INOPERATIVE. R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY & RELAMPED, OPS CHECKED NORMAL.
- [SDR ASAA11410359](https://openairdocs.org/sdr/ASAA11410359), Sep 13, 2011: LIGHT. INOPERATIVE. LT FORWARD OVERWING EMERGENCY EXIT IDENTIFIER HAS BULBS INOP. RELAMPED & PERFORMED GOOD OPS TEST IAW AMM 33 51 22 962 001.
- [SDR ASAA11410355](https://openairdocs.org/sdr/ASAA11410355), Sep 11, 2011: FRAME. CRACKED. BS 601 L FRAME INNER CHORD CRACKED AT LOWEST 2 EA FASTENER HOLES WL 200 MARKED. CUT OUT DAMAGE AT LOWEST 2 FASTENER HOLES AND REPAIRED CHORD IAW ASA EA 400 53EA
- [SDR ASAA11410354](https://openairdocs.org/sdr/ASAA11410354), Sep 11, 2011: FRAME. CRACKED. BS 601 RT FRAME INNER CHORD CRACKED AT 1 EA LOWEST FASTENER HOLE WL 200. FOUND DURING NDI HEEC BOTTOM SIDE OF HOLE MARKED. CUT OUT CRACKED FASTENER HOLE AND REP
- [SDR ASAA11410358](https://openairdocs.org/sdr/ASAA11410358), Sep 10, 2011: FRAME. CRACKED. BS 616 RT FRAME INNER CHORD CRACKED AT LOWEST FASTENER HOLE WL 200. FOUND DURING NDI HFEC BOTTOM POSITION OF HOLE MARKED. REPAIRED BS 616 RT FRAME INNER CHORD W
- [SDR ASAA11410344](https://openairdocs.org/sdr/ASAA11410344), Sep 7, 2011: ANGLE. CRACKED. RIGHT WING DOG HOUSE PANEL I/B ATTACH ANGLE COMMON TO NR 6 FLAP TRACK FAIRING CRACKED ON LOWER END. ACFT GROUNDED. REMOVED FABRICATED AND INSTALLED PANEL I/B AN
- [SDR ASAA11410343](https://openairdocs.org/sdr/ASAA11410343), Sep 7, 2011: PANEL. CRACKED. NR 6 FLAP TRACK FAIRING I/B PANEL CRACKED ABOVE UPPER FORWARD SCREW (NR 2 PYLON). REPLACED NR 2 PYLON PANEL.
- [SDR ASAA1047766](https://openairdocs.org/sdr/ASAA1047766), Apr 30, 2010: WEDGE. DAMAGED. RIGHT I/B MID FLAP LOWER T/E WEDGE IS DAMAGED. REPAIRED MID FLAP.
- [SDR ASAA1047765](https://openairdocs.org/sdr/ASAA1047765), Apr 30, 2010: SKIN. DELAMINATED. RIGHT I/B MID FLAP DELAMINATED IN SEVERAL AREAS. REPAIRED MID FLAP.

All 126: https://openairdocs.org/aircraft/N794AS/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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