# N345UA: DJI AGRAS T30 - Status: Valid registration - Airframe: [DJI AGRAS T30](https://openairdocs.org/model/dji-agras-t30) (registry code 06102BX) - Serial number: 3U5BJ6L0010010 - Type: Rotorcraft - Engine type: Electric - Certificate issued: May 5, 2022 - Expires: May 31, 2029 - Mode S code: A3D1A4 - Registered owner: [Elk Creek Properties LLC](https://openairdocs.org/faa-owner/ELK%20CREEK%20PROPERTIES%20LLC) - Location: [Falcon, MO](https://openairdocs.org/faa-place/MO/Falcon) - Owner type: LLC - Owner's area on the map: 37.5437° N, 92.3966° W: Placed by OpenAirDocs at the center of ZIP code 65470, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=345UA - Page: https://openairdocs.org/aircraft/N345UA 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 T30) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N345UA. ## FAA accident and incident reports None matched to N345UA. ## 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 N345UA not matched to an aircraft (31) They name N345UA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR 2002UALA01315](https://openairdocs.org/sdr/2002UALA01315), Aug 15, 2002: SKIN. DENTED. DENT FOUND IN RIGHT HAND SIDE OF FUSELAGE BELOW FWD LAV SERVICE PANEL AND ABOUT 3 INCHES AFT OF RED STEERING LIMIT STRIPE. MAJOR REPAIR ACCOMPLISHED. DOUBLER RE - [SDR 2002UALA01310](https://openairdocs.org/sdr/2002UALA01310), Aug 15, 2002: BEAR STRAP. DAMAGED. AFT PIT DOOR CUTOUT SKIN BEAR STRAP BLENDED BEYOND LIMITS AT STATION 796 STR 21-24R. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED. - [SDR 2002UALA01293](https://openairdocs.org/sdr/2002UALA01293), Aug 11, 2002: WEB. GOUGED. AFT PIT DOOR SILL VERTICAL WEB GOUGED BETWEEN STATION 793 - 821 RBL 23 (APPROX) BELOW FLOOR TRACK. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW WEB. - [SDR 2002UALA01284](https://openairdocs.org/sdr/2002UALA01284), Aug 7, 2002: DOUBLER. GOUGED. EXTERNAL EXISTING FUSELAGE SKIN REPAIR STATION 845, 1 INCH BELOW STR 22R GOUGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER REPAIR. - [SDR 2002UALA01274](https://openairdocs.org/sdr/2002UALA01274), Aug 2, 2002: SKIN. DAMAGED. EXTERNAL FUSELAGE GOUGED STATION 299 BETWEEN STRINGER 25R AND 26R. ALSO GOUGED STATION 305 BETWEEN STRINGER 25R AND 26R. LIGHTNING STRIKES STATION 313 AT STRING - [SDR 2002UALA01269](https://openairdocs.org/sdr/2002UALA01269), Aug 1, 2002: DOOR FRAME. CRACKED. CABIN, STATION 294, FUSELAGE STUB FRAME CRACKED AT UPPER DOOR STOP FITTING, AT STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STUB FRAME. - [SDR 2002UALA01259](https://openairdocs.org/sdr/2002UALA01259), Aug 1, 2002: FRAME. CRACKED. CABIN BODY FRAME INBOARD CHORD IS CRACKED BODY STATION 294, RBL 53, WL 209. MAJOR REPAIR ACCOMPLISHED. SPLICED FRAME INBOARD CHORD. - [SDR 2002UALA01258](https://openairdocs.org/sdr/2002UALA01258), Jul 31, 2002: FLOORBEAM. CORRODED. AFT CABIN LEFT HAND SIDE FLOORBEAM UPPER SURFACE CORRODED AROUND NUT PLATE HOLES STATION 927 BETWEEN LBL 14 AND LBL 44. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED - [SDR 2002UALA01247](https://openairdocs.org/sdr/2002UALA01247), Jul 30, 2002: FRAME. DAMAGED. STATION 294.5 FRAME JUST INBOARD OF STRINGER 4R IS BLENDED BEYOND LIMIT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. - [SDR 2002UALA01228](https://openairdocs.org/sdr/2002UALA01228), Jul 29, 2002: FLOORBEAM. DAMAGED. CABIN STATION 947.5 BETWEEN LBL 5 & LBL 20 UPPER SURFACE OF FLOORBEAM HAS EXCESSIVE MATERIAL REMOVED. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER REPAIRS - [SDR 2002UALA01227](https://openairdocs.org/sdr/2002UALA01227), Jul 29, 2002: FRAME. CRACKED. STATION 400 FRAME CRACKED OUT OF UPPER RIVET HOLE FOR STOW BIN ATTACH CLIP JUST ABOVE STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED FRAME D - [SDR 2002UALA01216](https://openairdocs.org/sdr/2002UALA01216), Jul 29, 2002: FRAME. CRACKED. CABIN BODY FRAME WEB IS CRACKED BODY STATION 440 STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. SPLICED BODY FRAME WEB. - [SDR 2002UALA01215](https://openairdocs.org/sdr/2002UALA01215), Jul 28, 2002: FRAME. CRACKED. CABIN STATION 827 STRINGER 4R FRAME WEB WAS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER REPAIR. - [SDR 2002UALA01214](https://openairdocs.org/sdr/2002UALA01214), Jul 28, 2002: FRAME. CRACKED. CABIN STATION 847 FRAME WEB AT STRINGER 9R IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER REPAIR. - [SDR 2002UALA01213](https://openairdocs.org/sdr/2002UALA01213), Jul 28, 2002: FRAME. CRACKED. CABIN STATION 887 FRAME WEB CRACKED AT STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER REPAIR. - [SDR 2002UALA01212](https://openairdocs.org/sdr/2002UALA01212), Jul 28, 2002: FRAME. CRACKED. STATION 400 FRAME CRACKED OUT OF UPPER RIVET HOLE FOR STOW BIN ATTACH CLIP JUST ABOVE STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED. - [SDR 2002UALA01211](https://openairdocs.org/sdr/2002UALA01211), Jul 28, 2002: FRAME. CRACKED. STATION 440 FRAME CRACKED OUT OF UPPER RIVET HOLE FOR STOW BIN ATTACH CLIP JUST ABOVE STRINGER 9R. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED. - [SDR 2002UALA01209](https://openairdocs.org/sdr/2002UALA01209), Jul 27, 2002: FRAME. CRACKED. STATION 480 FRAME CRACKED OUT OF UPPER RIVET HOLE FOR STOW BIN ATTACH CLIP JUST ABOVE STRINGER 9L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. - [SDR 2002UALA01208](https://openairdocs.org/sdr/2002UALA01208), Jul 27, 2002: FRAME. CRACKED. STATION 520 FUSELAGE FRAME CRACKED IN WEB AND INBOARD FLANGE RADIUS BELOW STRINGER 14R OUT OF INSULATION STANDOFF HOLE JUST BELOW FRAME SPLICE. MAJOR REPAIR ACC - [SDR 2002UALA01068](https://openairdocs.org/sdr/2002UALA01068), Jun 22, 2002: FLAP. MALFUNCTIONED. AFTER DEPARTURE ON FLAP RETRACTION FROM FLAPS 1 TO FLAPS UP, THE FLAPS SPLIT ACCORDING TO THE FLAP POSITION INDICATOR. RETURNED TO THE FIELD AND MADE A FLAPS UP - [SDR 2002UALA00010](https://openairdocs.org/sdr/2002UALA00010), Jan 3, 2002: BULKHEAD. CRACKED. WEB CRACKED AT BODY STATION 178, WL 218, LBL 12. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR. - [SDR 2002UALA00002](https://openairdocs.org/sdr/2002UALA00002), Jan 2, 2002: BULKHEAD. CRACKED. BODY STATION 178, WL 211, LBL 17 IS CRACKED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR. - [SDR 2002UALA00001](https://openairdocs.org/sdr/2002UALA00001), Jan 2, 2002: BULKHEAD. CRACKED. BODY STATION 178, WL 200, LBL 5.7 WEB IS CRACKED. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED DOUBLER REPAIR. - [SDR 2000UALA00621](https://openairdocs.org/sdr/2000UALA00621), Oct 24, 2000: FUEL CELL. LEAKING. SUSPECTED FUEL LOSS FROM NUMBER 2 MAIN TANK. *S/D* FOUND CENTER SHIELDED CONNECTOR SHIELD BROKEN ON NR 2 MAIN FUEL GAUGE. REPLACED SHIELDED SOCKET AND CENTER PI - [SDR 2001UALA00638](https://openairdocs.org/sdr/2001UALA00638), Sep 11, 2000: CONTROL ROD. CHAFED. RUDDER POWER CONTROL UNIT CONTROL ROD AFT END OUTBOARD SIDE CHAFED, WORN AND KINKED. *S/D* CONTROL ROD REPLACED WITH SERVICEABLE CONTROL ROD. OFF UNIT FOUND TO - [SDR 2000UALA00328](https://openairdocs.org/sdr/2000UALA00328), Jun 9, 2000: SENSOR. MALFUNCTIONED. YELLOW LEADING EDGE FLAP TRANSIT LIGHT REMAINED ON AND LEFT INBOARD FLAP INDICATOR GREEN LIGHT ON. EXCEEDED 230KTS BY 5-10 KTS. *S/D* REPLACED LEADING EDGE FLAP - [SDR 99UAL900271](https://openairdocs.org/sdr/99UAL900271), May 13, 1999: SENSOR. FAILED. EXHAUST FAN INOP. *S/D* EQUIPMENT COOLING LOW FLOW SENSOR FAILED. REPLACED EQUIPMENT COOLING LOW FLOW SENSOR, OPS CHECK OK. - [SDR 98UAL900133](https://openairdocs.org/sdr/98UAL900133), Mar 31, 1998: EAU FORK. FRACTURED. BOTH THRUST REVERSER UNLOCK LIGHTS ILLUMINATED AFTER TAKEOFF. *S/D* FOUND ENGINE ACCESS UNIT RETAINING FORK ON RADIO RACK FRACTURED AND MISSING PIN. EAU WAS LOO - [SDR 97UAL900420](https://openairdocs.org/sdr/97UAL900420), Jun 5, 1997: FIRE LOOP. OUT OF POSITION. EXPERIENCED RT WING BODY OVERHEAT WARNING. OVERHEAT LIGHT ON INTERMITTENT DURING CLIMB. *S/D* THE CAUSE WAS ATTRIBUTED TO THE POSITIONING OF THE FIRE DETECTION - [SDR 97UAL900276](https://openairdocs.org/sdr/97UAL900276), Apr 8, 1997: CHARGER. FAILED. EEL LIGHT FLOOR STRIPS INOP AT ROW 11 THROUGH 17. AFT EMERGENCY EXIT INDICATOR LIGHT INOP. BULLNOSE EMERGENCY EXIT LIGHT INOP. THE EEL LIGHTS AT ROWS 11 THROUGH - [SDR 96UAL900585](https://openairdocs.org/sdr/96UAL900585), Jul 30, 1996: ACTUATOR. BROKEN. THE LEADING EDGE FLAPS TRANSIT LIGHT IS ON AND THE NR 6 SLAT LIGHT IS ON STEADY. REPLACED SLAT ACTUATOR. SHOP FOUND THE ACTUATOR ROD END BROKEN. SENT ROD END TO ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Earlier aircraft with N345UA The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N345UA before. - [Cancelled 2016-10-19](https://openairdocs.org/deregistered/N345UA-2016-10-19): Griffon Aerospace SEAHUNTER, S/N 042-010001-08. Assigned, pending cancellation ## Related - Other DJI AGRAS T30 aircraft: https://openairdocs.org/model/dji-agras-t30/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.