# N225NW: DJI AGRAS T100 - Status: Valid registration - Airframe: [DJI AGRAS T100](https://openairdocs.org/model/dji-agras-t100) (registry code 06102L0) - Serial number: 1489 - Type: Rotorcraft - Engine type: Electric - Certificate issued: January 6, 2026 - Expires: January 31, 2033 - Mode S code: A1F4D5 - 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=225NW - Page: https://openairdocs.org/aircraft/N225NW 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 N225NW. ## FAA accident and incident reports None matched to N225NW. ## Reports on N225NW not matched to an aircraft (1) They name N225NW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 20010830026849I](https://openairdocs.org/incident/20010830026849I), Aug 30, 2001: Doug DC1030 (N225NW), Detroit, MI, Minor damage. (-23) Takeoff was aborted due to severe vibration and loss of nosewheel steering. The nose landing gear torque link was found to be disconnected. ## 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 N225NW not matched to an aircraft (27) They name N225NW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR 0601021225](https://openairdocs.org/sdr/0601021225), May 15, 2006: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS INOP ROW 30 BACK. REPLACED POWER SUPPLY. OPERATION CHECKS GOOD. - [SDR 0500641225](https://openairdocs.org/sdr/0500641225), Apr 29, 2005: COMPRESSOR. STALLED. DURING TAKEOFF ROLL, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL WITH EGT EXCEEDING RED LINE. TAKEOFF WAS ABORTED AT 110 KTS. THE ENGINE WILL BE REPLACED. - [SDR 0401001225](https://openairdocs.org/sdr/0401001225), Jun 17, 2004: FIRE LOOP. MALFUNCTIONED. ON CLIMBOUT AT 31,000 FT, RECEIVED NR 2 ENGINE FIRE WARNING INDICATION. NR 2 ENGINE B-LOOP WAS PUT ON MEL. SHUT DOWN NR 2 ENGINE IAW COM PROCEDURE. DUMPED 90,00 - [SDR 0301611225](https://openairdocs.org/sdr/0301611225), Aug 19, 2003: GENERATOR. FAILED. DURING CRUISE, NR 2 GENERATOR TRIPPED OFF AND THEN NR 1 CSD TEMPERATURE CLIMBED AND TRIPPED OFF. FLIGHT DUMPED 70,000 LBS OF FUEL AND RETURNED TO DTW. MAINTENAN - [SDR 0203401225](https://openairdocs.org/sdr/0203401225), Oct 2, 2002: PUMP. INOPERATIVE. PUMP WAS INSTALLED IN THE LOWER AUXILIARY FUEL TANK. IT WAS REMOVED AS PART OF EO 2815-01008 WHICH DEACTIVATES THE LOWER AUXILIARY FUEL TANK. PUMP FAILED THE ST - [SDR 0104671225](https://openairdocs.org/sdr/0104671225), Nov 28, 2001: GENERATOR. DURING CRUISE ENROUTE TO HNL, THE NBR 1 GENERATOR DROPPED OFF LINE. FLIGHT CREW FOLLOWED COM PROCEDURE AND DISCONNECTED CSD AND GENERATOR. FLIGHT CONTINUED TO H - [SDR 0103151225](https://openairdocs.org/sdr/0103151225), Aug 30, 2001: TORQUE LINK. DISCONNECTED. ABORTED TAKEOFF AT 100 KNOTS DUE TO VIBRATION AND LOSS OF NOSE GEAR STEERING. FOUND NOSE LANDING GEAR TORQUE LINKS DISCONNECTED. AIRCRAFT WAS TOWED TO THE GATE. - [SDR 0003811225](https://openairdocs.org/sdr/0003811225), Oct 8, 2000: UNKNOWN. ODOR. AMS- SEVERAL PASSENGERS NOTED AN ELECTRICAL ODOR IN THE AREA OF SEATS 1AB BUT ODOR THEN DISSIPATED. AIRCRAFT CONTINUED TO AMS AND LANDED WITHOUT INCIDENT. REPLA - [SDR 9810511225](https://openairdocs.org/sdr/9810511225), Nov 24, 1998: POWER SUPPLY. SMOKING. DURING CRUISE, NOTICED SMOKE IN OVERHEAD CEILING BETWEEN FIRST GALLEY AND COAT CLOSET. ALSO, SMOKE COMING FROM EMERGENCY POWER SUPPLY. FLIGHT DIVERTED TO GEG AN - [SDR 9807591225](https://openairdocs.org/sdr/9807591225), Apr 25, 1998: CONTROL. FAILED. NR 1 GENERATOR OFF LIGHT ILLUMINATED AND NR 1 GENERATOR DROPPED OFF LINE. ON TAKEOFF ROLL, THE NR 1 GENERATOR OFF LIGHT ILLUMINATED AGAIN. RETURNED TO THE GATE. - [SDR 9807471225](https://openairdocs.org/sdr/9807471225), Mar 20, 1998: WEB. CRACKED. DURING M CHECK, FOUND CRACK IN AFT WEB IN THE RIGHT WHEEL WELL. REPAIRED PER EA 12-156163. - [SDR 9805481225](https://openairdocs.org/sdr/9805481225), Mar 18, 1998: FRAME. CRACKED. DURING M-CHECK, FOUND CRACK IN LOWER NOSE FUSELAGE FRAME AT FS 459, RBL 62. REPAIRED PER EA 12-150786. - [SDR 9805471225](https://openairdocs.org/sdr/9805471225), Mar 18, 1998: FRAME. CRACKED. DURING M-CHECK, FOUND CRACK IN LOWER NOSE FUSELAGE FRAME AT FS 459 LBL 62. REPAIRED PER EA 12-150786. - [SDR 9805491225](https://openairdocs.org/sdr/9805491225), Mar 16, 1998: FRAME. CORRODED. DURING M-CHECK, FOUND CORROSION ON FORWARD CARGO DOOR JAMB FRAME AT FS 895, STR 42R. REPAIRED PER EA 12-190781. - [SDR 9807371225](https://openairdocs.org/sdr/9807371225), Mar 11, 1998: LONGERON. CORRODED. DURING M CHECK, FOUND CORRODED LONGERON IN THE NR 1 AC COMPARTMENT AT THE EXHAUST FS 568-587. REPAIRED PER EA 12-155546. - [SDR 9804571225](https://openairdocs.org/sdr/9804571225), Mar 3, 1998: SKIN. CORRODED. DURING M CHECK, FOUND CORROSION ON BELLY SKIN AT FS 1501-1531, LONGERON 48L-48R. REPAIRED PER EA 12-154586. - [SDR 9801931225](https://openairdocs.org/sdr/9801931225), Jan 31, 1998: REGULATOR VALVE. FAILED. ON DEPARTURE, NR 1 PNEUMATIC TEMPERATURE LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE. UNABLE TO DEPRESSURIZE DUCT. REDUCED THROTTLE AND BROUG - [SDR 9714131225](https://openairdocs.org/sdr/9714131225), Jul 23, 1997: ENGINE. FAILED. WHILE CLIMBING THROUGH FL180, THE NR 2 ENGINE EGT AND FUEL FLOW SPIKED WITH AN ASSOCIATED VIBRATION. THE ENGINE STABILIZED ON ITS OWN. THIRTY MINUTES LATER THE - [SDR 9618881225](https://openairdocs.org/sdr/9618881225), Aug 29, 1996: SEAL. WORN. DURING CRUISE, CABIN PRESSURE FLUCTUATED AND UNABLE TO CONTROL NR 2 PNEUMATIC SYSTEM. FLIGHT RETURNED TO HNL. MAINTENANCE REPLACED THE CENTER E/E DOOR SEAL, REI - [SDR 9618331225](https://openairdocs.org/sdr/9618331225), Aug 25, 1996: PRESS REG VALVE. MALFUNCTIONED. DURING CLIMB, THE NR 2 MANIFOLD FAIL LIGHT ILLUMINATED AND WAS UNABLE TO CLOSE PRV PER COM. DUMPED 45,000 LBS OF FUEL AND RETURNED TO DTW. MAINTENANCE LOCKED TH - [SDR 9617161225](https://openairdocs.org/sdr/9617161225), Aug 9, 1996: PNEUM SYS. MALFUNCTIONED. DURING CRUISE, THE NR 2 MANIFOLD FAIL LIGHT ILLUMINATED. FOLLOWED COM AND SHUT OFF THE PNEUMATIC SUPPLY. DUMPED 15,000 LBS OF FUEL AND RETURNED TO HNL. MAINTENA - [SDR 9611781225](https://openairdocs.org/sdr/9611781225), May 23, 1996: POWER SUPPLY. INOPERATIVE. DURING LINE INSPECTION, FOUND THE EMERGENCY LIGHT AND STANDBY POWER CIRCUIT BREAKERS TRIPPED. MAINTENANCE REPLACED THE FORWARD BATTERY POWER SUPPLY. - [SDR 9611761225](https://openairdocs.org/sdr/9611761225), May 10, 1996: BATTERY PACK. DISCHARGED. DURING LINE INSPECTION, FOUND THE EMERGENCY LIGHT INOPERATIVE AT DOOR 1L AND 1R AND THE FIRST CLASS FLOOR LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE BATTERY - [SDR 9607331225](https://openairdocs.org/sdr/9607331225), Mar 31, 1996: INDICATION SYST. MALFUNCTIONED. DURING CRUISE, THE NR 1 PNEUMATIC TEMPERATURE WAS 220 DEGREES AND THE NR 3 PNEUMATIC TEMPERATURE LIGHT ILLUMINATED WITH NR 3 TEMPERATURE INDICATING 150 DEGREES. - [SDR 9601601225](https://openairdocs.org/sdr/9601601225), Jan 10, 1996: SKIN. CORRODED. DURING T-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN FS 1950 TO 1958, LONGERON 50L TO 52. REPAIRED SKIN (P/N AGA 7418-1) PER EA 12-104396. - [SDR 9600681225](https://openairdocs.org/sdr/9600681225), Jan 8, 1996: FITTING. CORRODED. DURING T-CHECK, FOUND CORROSION ON THE CENTER GEAR WELL STRINGER FITTINGS AT LBL 21, 14, 7, BL 0, AND RBL 21 FROM BS 1509 TO 1521. REPLACED STRINGER FITTINGS. - [SDR 9601551225](https://openairdocs.org/sdr/9601551225), Jan 3, 1996: SKIN. CORRODED. DURING T-CHECK, FOUND CORROSION ON THE MOUNTING RINGS FOR ALL 4 RADIO ALTIMETER MOUNTING RINGS. REPAIRED RINGS (P/N AYB7022-1; AYB 7053-1, -501) PER EA 12-10387 ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## 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.