# N346BC: DJI AGRAS T100 - Status: Valid registration - Airframe: [DJI AGRAS T100](https://openairdocs.org/model/dji-agras-t100) (registry code 06102L0) - Serial number: 1858 - Type: Rotorcraft - Engine type: Electric - Certificate issued: January 9, 2026 - Expires: January 31, 2033 - Mode S code: A3D3B4 - Registered owner: [Nuway Ag LLC](https://openairdocs.org/faa-owner/NUWAY%20AG%20LLC) - Location: [Dundee, OH](https://openairdocs.org/faa-place/OH/Dundee) - Owner type: LLC - Owner's area on the map: 40.6222° N, 81.6593° W: Placed by OpenAirDocs at the center of ZIP code 44624, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=346BC - Page: https://openairdocs.org/aircraft/N346BC 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 (DJI AGRAS T100) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N346BC. ## FAA accident and incident reports None matched to N346BC. ## 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 N346BC not matched to an aircraft (55, newest 50) They name N346BC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DALA2016010400042](https://openairdocs.org/sdr/DALA2016010400042), Dec 31, 2015: WEDGE. DAMAGED. REPAIR INBD RT FLAP T/E WEDGE, DO TO FLAP TRACK FAIRING NOT FITTING IN PLACE. ACCOMPLISHED REPAIR OF THE DISCREPANT AREA, APPROXIMATELY 15.5" X 10.5", ON RT INB - [SDR DALA2015123107782](https://openairdocs.org/sdr/DALA2015123107782), Dec 30, 2015: WEDGE. DAMAGED. INBD LT FLAP T/E WEDGE, DO TO FLAP TRACK FAIRING NOT FITTING IN PLACE. REPAIRED IAW SRM 51-70-10. - [SDR DALA2015123107781](https://openairdocs.org/sdr/DALA2015123107781), Dec 30, 2015: SKIN. DAMAGED. LEFT INBD MAIN FLAP UPPER PANEL FROM MF BS 74.0 TO MF BS 209 FOUND DAMAGE CORE FROM INBD TO OTBD END AND FWD TO AFT SIDES AND ONE HOLE IN CORE. REPAIRED IAW SRM - [SDR DALA2015122007693](https://openairdocs.org/sdr/DALA2015122007693), Dec 19, 2015: FLOORBEAM. CORRODED. CP53-251-01-MAIN CABIN, CORROSION ON FRAME UNDER NUTPLATES BS 1681 AND BETWEEN RBL 57-LBL 57. REMOVED CORROSION UNDER NUTPLATES ON MAIN CABIN FRAME, FLOOR BEAM, - [SDR DALA2015121907692](https://openairdocs.org/sdr/DALA2015121907692), Dec 16, 2015: SEAT TRACK. CORRODED. CORROSION ON MAIN CABIN FLOOR STRUCTURE, SEAT TRACK FLANGE, BS 680 TO BS 740, RBL 45.5. REMOVED CORROSION ON MAIN CABIN FLOOR STRUCTURE SEAT TRACK FLANGE BS TO - [SDR DALA2015112207187](https://openairdocs.org/sdr/DALA2015112207187), Nov 21, 2015: SEAT TRACK. CORRODED. CORROSION ON MAIN CABIN FLOOR SEAT TRACK FLANGE/AROUND FASTENER HOLES AT BS 641, LBL 45.5. ACCOMPLISHED PERMANENT REPAIR ON SEAT TRACK FLANGE, AROUND FASTENER H - [SDR DALA2015121407591](https://openairdocs.org/sdr/DALA2015121407591), Nov 17, 2015: SHUTOFF VALVE. CORRODED. APU BLEED AIR SHUTOFF VALVE HAS SURFACE CORROSION VIEWED THRU ACCESS DOOR 313AL RLO14. R & R APU BLEED SHUTOFF VALVE IAW AMM 36-11 -10-401. LEAK AND OPS CHECK D - [SDR DALA2015110406746](https://openairdocs.org/sdr/DALA2015110406746), Nov 3, 2015: SUPPORT. CORRODED. FWD CARGO BS 900 BULKHEAD VERTICAL SUPPORT AT RBL-7.5 HAS CORROSION AT BOTTOM. UPON EVALUATION, FOUND BULKHEAD VERTICAL SUPPORT BS 900, RBL 7.5 TO HAVE AN EXFOL - [SDR DALA2015103106679](https://openairdocs.org/sdr/DALA2015103106679), Oct 30, 2015: FRAME. CORRODED. CORROSION ON FWD CARGO DOOR AFT LOWER FRAME. REPAIRED IAW ERA 538381-14, REV ORIGINAL. - [SDR DALA2015103106678](https://openairdocs.org/sdr/DALA2015103106678), Oct 30, 2015: FRAME. CORRODED. CORROSION ON AFT CARGO DOOR AFT LOWER FRAME. ACCOMPLISHED PERMANENT REPAIR ON AFT CARGO DOOR AFT LOWER FRAME IAW ER/A 538385-14, REV ORIGINAL. - [SDR DALA2015101406137](https://openairdocs.org/sdr/DALA2015101406137), Oct 13, 2015: KEELBEAM. CORRODED. CORROSION ON LOWER KEEL STRUCTURE TEE FITTING ABOVE LT MLG DOOR AT BS 1100 - 1120, LBL7. FOUND OUT OF LIMITS IAW SRM 53-00-71, FIG 101, DETAIL VII. REMOVED, FAB - [SDR DALA2015092105749](https://openairdocs.org/sdr/DALA2015092105749), Sep 18, 2015: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK FLANGE AROUND FASTENER HOLE, BS 640, RBL 45. BLENDED CORROSION ON SEAT TRACK FLANGE & ACCOMPLISHED PERMANENT REPAIR IAW ER/A 538371-14, - [SDR DALA2015091905747](https://openairdocs.org/sdr/DALA2015091905747), Sep 18, 2015: SKIN. DENTED. DURING INSPECTION OF DENT ON N/R 100-3 FOUND DENT AT EXT FUSELAGE 1" FWD OF BS 460 BELOW LAP AT STR 26R. MECHANICALLY MEASURED DENT ON FUS SKIN FWD OF BS 460 BE - [SDR DALA2015091005563](https://openairdocs.org/sdr/DALA2015091005563), Sep 9, 2015: FRAME. DENTED. TWO DENTS ON AFT CARGO FRAME AT BS 1340 BETWEEN STRINGERS 25-26L. REPAIRED IAW SRM 53-00-07, REPAIR 5. - [SDR DALA2015090705486](https://openairdocs.org/sdr/DALA2015090705486), Sep 5, 2015: GATE. CORRODED. R1 DOOR LOWER GATE LOWER EDGE CORRODED. REMOVED CORROSION IAW SRM 52-10-02, FIG 101 100 PERCENT EXFOLIATED FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02, FIG 101, - [SDR DALA2015082605231](https://openairdocs.org/sdr/DALA2015082605231), Aug 25, 2015: DOOR SILL. CORRODED. FWD CARGO DOOR SILL LOWER REPAIR ANGLE HAS CORROSION BETWEEN BS 580 - 600. FOUND THE REPAIR TO BE 100 PERCENT CORRODED. REMOVED, FABRICATED & INSTALLED REPLACEM - [SDR DALA2015082605230](https://openairdocs.org/sdr/DALA2015082605230), Aug 24, 2015: FLOORBEAM. CORRODED. CORROSION ON MAIN CABIN FLOORBEAM UPPER TEE BS 377, BETWEEN BL 0 AND LBL 24, FOUND TO BE OUT OF LIMITS. TRIMMED-OUT THE SECTION ON MAIN CABIN FLOORBEAM LBL 32.5 - [SDR DALA2015082505229](https://openairdocs.org/sdr/DALA2015082505229), Aug 23, 2015: FLOOR SUPPORT. CORRODED. CORROSION ON AFT CARGO FLOOR SUPPORT AROUND NUPLATES AT BS 1510, LBL 7.55. ACCOMPLISHED ER/A 332525-14MA, REV E. - [SDR DALA2015082505228](https://openairdocs.org/sdr/DALA2015082505228), Aug 23, 2015: FLOOR SUPPORT. CORRODED. CORROSION ON AFT CARGO FLOOR SUPPORT AROUND NUTPLATES AT BS 1510, RBL 2.9. REMOVED CORROSION IAW SRM 53-00-51, REPAIRED IAW ER/A 332525-14MA, REV E. - [SDR DALA2015082505227](https://openairdocs.org/sdr/DALA2015082505227), Aug 23, 2015: FLOOR SUPPORT. CORRODED. CORROSION ON AFT CARGO FLOOR SUPPORT AROUND NUTPLATES AT BS 1510, RBL 7.55. ACCOMPLISHED ERA 332525-14MA, REV E. - [SDR DALA2015082405205](https://openairdocs.org/sdr/DALA2015082405205), Aug 23, 2015: DECK PLATE. CORRODED. MAIN CABIN-CORROSION ON LT SIDE OF DECK PLATE BETWEEN BS 1681-1720 AND BETWEEN BL 0-LBL 57. REMOVED CORROSION ON MAIN CABIN DECK PLATE BS 1681 TO BS 1720, BL-0- - [SDR DALA2015082505208](https://openairdocs.org/sdr/DALA2015082505208), Aug 20, 2015: SEAT TRACK. CORRODED. CORROSION ON MAIN CABIN SEAT TRACK FLANGE FWD END, BS 365, RBL 45.5. ORIGINAL MAT. THICKNESS: .070", MAT LOSS: 3"X 1"X .021". FOUND OUT OF LIMITS IAW SRM 53-00- - [SDR DALA2015082105204](https://openairdocs.org/sdr/DALA2015082105204), Aug 20, 2015: FLOOR SUPPORT. CORRODED. CORROSION ON AFT CARGO FLOOR SUPPORT AROUND NUTPLATES AT BS 1510, LBL-12. REMOVED NUT PLATES FOR ACCESS REMOVED CORROSION IAW SRM 51-40-02. REMOVED CORROSION FR - [SDR DALA2015082105117](https://openairdocs.org/sdr/DALA2015082105117), Aug 20, 2015: FRAME. DENTED. AFT CARGO FRAME BS 1340 STR 25R FOUND DENTED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. TRIMED DAMAGE OUT OF FRAME INBD FLANGE AFT CARGO FRAME IAW SRM 53-00-0 - [SDR DALA2015082105116](https://openairdocs.org/sdr/DALA2015082105116), Aug 20, 2015: DECK PLATE. CORRODED. CORROSION FOUND ON RT SIDE OF DECK PLATE BETWEEN BS 1681 - 1720 AND BETWEEN BL 0 & RBL 57. REMOVED CORROSION IN AREA AND FOUND AREAS TO BE OUT OF LIMITS IAW SRM - [SDR DALA2015082105115](https://openairdocs.org/sdr/DALA2015082105115), Aug 20, 2015: FLOOR SUPPORT. CORRODED. CORROSION ON AT CARGO FLOOR SUPPORT AROUND NUTPLATES AT BS 1510, LBL 2.9. ACCOMPLISHED ERA 332525-14MA, REV E DUE TO 100 PERCENT MATERIAL LOSS AT THIS LOCATION. - [SDR DALA2015082105114](https://openairdocs.org/sdr/DALA2015082105114), Aug 17, 2015: STRAP. CRACKED. FLOOR SUPPORT STABILIZATION STRAP BS 365.25 - 377.7 LBL 24 CRACKED IN THREE PLACES AND BETWEEN TWO PREVIOUS REPAIR DOUBLERS. R & R DAMAGED SECTION OF STABILIZAT - [SDR DALA2015081805023](https://openairdocs.org/sdr/DALA2015081805023), Aug 17, 2015: SEAT TRACK. CORRODED. CORROSION ON MAIN CABIN SEAT TRACK FLANGE FWD END, BS 365, RBL 24.7. REMOVED CORROSION ON MAIN CABIN SEAT TRACK SUPPORT AT BS RBL 24.5, L=1.4", W=.9", D=.012" O - [SDR DALA2015081705021](https://openairdocs.org/sdr/DALA2015081705021), Aug 16, 2015: FRAME. DENTED. THREE DENTS ON AFT CARGO LT FRAME AT BS 1440 BETWEEN STRINGERS 25-26L. CUT OUT DENTS, FABRICATED AND INSTALLED PERMANENT REPAIR IAW SRM 53-00-07-R5, FIG 201. - [SDR DALA2015082905343](https://openairdocs.org/sdr/DALA2015082905343), Aug 15, 2015: INTERCOSTAL. CORRODED. CORROSION FOUND ON AFT CARGO INTERCOSTALT BS 1380, RBL 26. REMOVED CORROSION IAW SRM 51-10-02 AND 53-00-04 ALLOWABLE DAMAGE 1. FOUND OUT OF LIMITS IAW SRM 53-00 - [SDR DALA2015081404958](https://openairdocs.org/sdr/DALA2015081404958), Aug 13, 2015: STRINGER. CORRODED. CORROSION ON STR 30 END FITTING IN AFT CARGO BS 1620. REMOVED CORROSION IAW SRM 53-00-03. FOUND OUT OF LIMITS IAW SRM 53-00-03. R & R THE STRINGER END FITTING I - [SDR DALA2015081204910](https://openairdocs.org/sdr/DALA2015081204910), Aug 11, 2015: FRAME. DENTED. DENT ON FWD CARGO LT FRAME AT BS 780 JUST ABOVE STR 24L. DENT ON FWD CARGO LT FRAME AT BS 780, STR 24L, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101. TRI - [SDR DALA2015081404960](https://openairdocs.org/sdr/DALA2015081404960), Aug 7, 2015: FRAME. DENTED. THREE DENTS ON FWD CARGO FRAME BS 600 STRINGERS 24-25L. TRIMMED OUT THE DENTS IAW SRM 53-00-07, REP 5. ACCOMPLISHED PERMANENT CAT "B" REPAIR IAW SRM 53-00-07, R - [SDR DALA2015080704901](https://openairdocs.org/sdr/DALA2015080704901), Aug 6, 2015: FRAME. DENTED. TWO DENTS ON FWD CARGO LT FRAME AT BS 800 BETWEEN STRINGERS 23 - 25L. TRIMED OUT DENTS, ACCOMPLISHED PERMANENT MAJOR REPAIR IAW SRM. - [SDR DALA2015080704899](https://openairdocs.org/sdr/DALA2015080704899), Aug 6, 2015: FLOORBEAM. CORRODED. CORROSION ON MAIN CABIN FLOORBEAM UPPER TEE BS 365, BL 0 TO RBL 62. ACCOMPLISHED PERMANENT CAT"A" MAJOR REPAIR IAW SRM. - [SDR DALA2015080504897](https://openairdocs.org/sdr/DALA2015080504897), Aug 4, 2015: FLOORBEAM. CORRODED. CORROSION ON MAIN CABIN FLOORBEAM UPPER TEE BS 377, BETWEEN BL 0 AND LBL 24. OUT OF LIMITS. - [SDR DALA2015081404957](https://openairdocs.org/sdr/DALA2015081404957), Jul 31, 2015: INTERCOSTAL. CORRODED. CORROSION ON AFT CARGO INTERCOSTAL AT BS 1413, LBL 16 ON INBD SIDE OF WEB. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-04, FIG 101. DETAIL II. FABRI - [SDR DALA2015080404928](https://openairdocs.org/sdr/DALA2015080404928), Jul 31, 2015: INTERCOSTAL. CORRODED. CORROSION ON AFT CARGO INTERCOSTAL BETWEEN BS 1600-1620, LBL-2.9 AT BOTTOM ON OTBD SIDE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, R & R INTERCOSTAL IAW - [SDR DALA2015080204783](https://openairdocs.org/sdr/DALA2015080204783), Jul 31, 2015: CREASE BEAM. CORRODED. CORROSION ON LEFT CREASE BEAM BS 438. REMOVED SECTION OF CREASE BEAM BETWEEN BS 430 - 450 IAW SRM 51-40-02, PG 7. FABRICATED, LOCATED AND DRILLED THE NEW SECTIO - [SDR DALA2015080104782](https://openairdocs.org/sdr/DALA2015080104782), Jul 31, 2015: SKIN. DENTED. BS 443 BELOW STRINGER 25R, FUSELAGE SKIN HAS APPROXIMATELY A ONE INCH DENT. REPAIRED IAW ER/A 536965-14, REV ORIGINAL. - [SDR DALA2015080104781](https://openairdocs.org/sdr/DALA2015080104781), Jul 29, 2015: SEAT TRACK. CORRODED. CORROSION ON MAIN CABIN SEAT TRACK FLANGE, BS 640, LBL 24.7. REMOVED DAMAGED SEAT TRACK SECTION . FABRICATED A REPLACEMENT SEAT TRACK SECTION AND FABRICATED CHA - [SDR DALA2015072804700](https://openairdocs.org/sdr/DALA2015072804700), Jul 27, 2015: TEE FITTING. CORRODED. CORROSION ON AFT ATTACH POINT OF LOWER KEEL STRUCTURE TEE FITTING AT BS 1120 - 1140, LBL 5.5. R & R THE TEE FITTING IAW SRM 51-40-02, PAR 9. - [SDR DALA2015072604699](https://openairdocs.org/sdr/DALA2015072604699), Jul 25, 2015: FLOORBEAM. CORRODED. CORROSION ON UPPER CAP ON FRAME BS 1661, RBL 54. TRIMMED-OUT DAMAGED SECTION OF FLOORBEAM BETWEEN RBL 49 - 65 AND ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00- - [SDR DALA2015072604698](https://openairdocs.org/sdr/DALA2015072604698), Jul 25, 2015: CREASE BEAM. CORRODED. CORROSION FOUND ON RT CREASE BEAM BS 1237, RBL 65. CUTOUT DAMAGED SECTION OF CREASE BEAM FROM BS 1230 - 1250, RT & ACCOMPLISHED A PERMANENT SPLICE REPAIR IAW SR - [SDR DALA2015072604697](https://openairdocs.org/sdr/DALA2015072604697), Jul 24, 2015: CREASE BEAM. CORRODED. CORROSION ON CREASE BEAM BS 1600 - 1607, LBL 62. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-60-13, 1 FIG 101, DETAIL III. R & R THE SECTION OF THE CRE - [SDR DALA2015072504696](https://openairdocs.org/sdr/DALA2015072504696), Jul 24, 2015: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT, BS 332 - 336, RBL 3. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, AD1, FIG 101, DETAIL VI. R & R THE FLOOR SUPP - [SDR DALA2015072504695](https://openairdocs.org/sdr/DALA2015072504695), Jul 24, 2015: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BS 365 - 377, BL 0. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. R & R THE FLOOR SUPPORT IAW SRM 51-40-02, PG 6 A - [SDR DALA2015072404624](https://openairdocs.org/sdr/DALA2015072404624), Jul 23, 2015: FRAME. DENTED. DENT ON FWD CARGO RT FRAME AT BS 700 ABOVE STR 24R. TRIMMED-OUT DENT ON FWD CARGO RT FRAME AT BS 700 ABOVE STR 24R AND ACCOMPLISHED A PERMANENT CAT"B" REPAIR IA - [SDR DALA2015072404623](https://openairdocs.org/sdr/DALA2015072404623), Jul 23, 2015: FRAME. DENTED. DENT ON FWD CARGO RT FRAME AT BS 800 ABOVE STR 23R. ACCOMPLISHED A PERMANENT CAT"B" REPAIR IAW SRM 53-00-07, REPAIR 5, FIG 201. TRIMOUT SIZE 1.08" X 0.94" X 0.5 - [SDR DALA2015072304622](https://openairdocs.org/sdr/DALA2015072304622), Jul 21, 2015: SKIN. DAMAGED. LEFT WING INBD FLAP T/E WEDGE PANEL LOWER SURFACE IS DAMAGED, DENTED, PUNCTURED, AND CRACKED MF BS 223 TO MF BS 240. ACCOMPLISHED REPAIR OF THE DISCREPANT AREA All 55: https://openairdocs.org/aircraft/N346BC/unmatched-reports.md ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Earlier aircraft with N346BC The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N346BC before. - [Cancelled 1996-05-30](https://openairdocs.org/deregistered/N346BC-1996-05-30): S N I A S AS350D ASTAR, S/N 1470. Exported to Brazil. Owner: [Arrow Trading Inc](https://openairdocs.org/faa-owner/ARROW%20TRADING%20INC), [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale) ## Related - Other DJI AGRAS T100 aircraft: https://openairdocs.org/model/dji-agras-t100/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.