# N818EA: DJI MATRICE 600 PRO - Status: Valid registration - Airframe: [DJI MATRICE 600 PRO](https://openairdocs.org/model/dji-matrice-600-pro) (registry code 06101ZF) - Serial number: DL121816558125 - Type: Rotorcraft - Engine type: Electric - Certificate issued: May 15, 2017 - Expires: May 31, 2027 - Mode S code: AB2779 - Registered owner: [Alaska Aerial Survey LLC](https://openairdocs.org/faa-owner/ALASKA%20AERIAL%20SURVEY%20LLC) - Location: [Wasilla, AK](https://openairdocs.org/faa-place/AK/Wasilla) - Owner type: LLC - Owner's area on the map: 61.6051° N, 149.4227° W: Placed by OpenAirDocs at the center of ZIP code 99654, 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=818EA - Page: https://openairdocs.org/aircraft/N818EA 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 MATRICE 600 PRO) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N818EA. ## FAA accident and incident reports None matched to N818EA. ## 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 N818EA not matched to an aircraft (28) They name N818EA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR C1HA200478002](https://openairdocs.org/sdr/C1HA200478002), Feb 18, 2004: UPLOCK SENSOR. MALFUNCTIONED. ON APPROACH TO MSP WITH LANDING GEAR EXTENDED RIGHT MAIN GEAR HAD BOTH RED AND GREEN INDICATIONS. COMPLIED WITH COM PROCEDURES. REMOVED AND REPLACED MAIN GEAR U - [SDR C1HA200478001](https://openairdocs.org/sdr/C1HA200478001), Feb 9, 2004: MOTOR. INOPERATIVE. INBOARD TRAILING EDGE FLAPS WOULD NOT EXTEND HYDROLICLY OR ELECTRICALLY ON LANDING. FOUND INBOARD ALTERNATE FLAP MOTOR BINDING INSTALLED SERVICEABLE ALTERNATE F - [SDR 0202002709](https://openairdocs.org/sdr/0202002709), Jun 18, 2002: PUMP. FAILED. DURING CLIMBOUT, THE LEFT ENGINE EXPERIENCED A FLAME-OUT. AIRCRAFT RETURNED TO TPA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE FUE - [SDR 0102622709](https://openairdocs.org/sdr/0102622709), Jun 10, 2001: RIB. CORRODED. During M check, found corrosion in the vertical stabilizer tension tie rib mount hole. Repaired per EA27-182234. - [SDR 0102632709](https://openairdocs.org/sdr/0102632709), Jun 4, 2001: NUT PLATE. CORRODED. During M check, found corrosion under nut plates installed under cargo floor support. Repaired per EA27-182243. - [SDR 0102642709](https://openairdocs.org/sdr/0102642709), Jun 2, 2001: FLOORBEAM. CORRODED. DURING M CHECK, FOUND CORROSION ON FLOORBEAM. REPAIRED PER EA27-182241. - [SDR 0102652709](https://openairdocs.org/sdr/0102652709), May 30, 2001: KEELBEAM. CORRODED. During M check, found corrosion on outboard flange of LH keel beam. Repaired per EA27-182237. - [SDR 0003572709](https://openairdocs.org/sdr/0003572709), Sep 12, 2000: FLANGE. CRACKED. DURING L CHECK, FOUND CRACK ON UPPER FLANGE OF BULLNOSE 2 INCHES INBOARD OF CENTER HINGE ON NUMBER 2 KRUEGER FLAP. REPAIRED PER EA 27-178740. - [SDR 0003512709](https://openairdocs.org/sdr/0003512709), Sep 12, 2000: FRAME. CORRODED. DURING L CHECK, FOUND CORROSION ON THE UPPER SURFACE OF BULKHEAD REINFORCEMENT CHORD AT BS 1176 RBL 45. REPAIRED PER EA 27-178739. - [SDR 0001262709](https://openairdocs.org/sdr/0001262709), Apr 6, 2000: LIGHT. INOPERATIVE. DURING LINE CHECK, PHL MAINTENANCE FOUND AFT SECTION OF EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY BATTERY, OPERATIONAL CHECK OK. - [SDR 9803552709](https://openairdocs.org/sdr/9803552709), Feb 20, 1998: LIGHT. INOPERATIVE. DURING PREFLIGHT, FOUND FORWARD CABIN EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK OK. - [SDR 9723642709](https://openairdocs.org/sdr/9723642709), Dec 21, 1997: BATTERY. DISCHARGED. DURING LINE MAINTENANCE CHECK, FOUND AFT CABIN EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK OK. - [SDR 9723632709](https://openairdocs.org/sdr/9723632709), Dec 21, 1997: BATTERY. DISCHARGED. DURING LINE MAINTENANCE, FOUND BOTH OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS. OPERATIONAL CHECK OK. - [SDR 9719972709](https://openairdocs.org/sdr/9719972709), Oct 20, 1997: STRUT. REQD SERVICE. ON LANDING GEAR RETRACITON, NOSE GEAR INDICATION LIGHT REMAINED ON. CYCLED GEAR WITH NO CHANGE IN INDICATION. AIRCRAFT CONTINUED TO ABQ AND LANDED WITHOUT INCID - [SDR 9714612709](https://openairdocs.org/sdr/9714612709), Jul 26, 1997: HYD PUMP. FAILED. DURING CLIMB-OUT FROM MSP, LOSE SYSTEM 'B' HYDRAULICS. AIRCRAFT RETURNED TO CITY OF ORIGINATION AND LANDED WITHOUT INCIDENT. REPLACED NR 1 SYSTEM 'B' HYDRAULIC - [SDR 9626552709](https://openairdocs.org/sdr/9626552709), Dec 13, 1996: GASPER FAN. FAILED. DURING TAKEOFF ROTATION, A STRONG SMELL OF ELECTRICAL FUMES WAS EVIDENT. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED GASPER FAN MOTOR, OPERAT - [SDR 9619892709](https://openairdocs.org/sdr/9619892709), Sep 13, 1996: ACTUATOR. FAILED. DURING TAKEOFF ON FLAP RETRACTION, THE NR 3 LEADING EDGE SLAT INDICATED DOWN. AIRCRAFT RETURNED TO MKE AND LANDED WITHOUT INCIDENT. REPLACED NR 3 LEADING EDGE F - [SDR 9617832709](https://openairdocs.org/sdr/9617832709), Aug 15, 1996: OIL TEMP IND. MALFUNCTIONED. DURING CLIMBOUT, THE RIGHT ENGINE OIL TEMPERATURE BEGAN STEADILY RISING. CREW PERFORMED A PRECAUTIONARY SHUTDOWN OF THE RIGHT ENGINE. AIRCRAFT RETURNED TO DTW A - [SDR 9609492709](https://openairdocs.org/sdr/9609492709), Apr 30, 1996: FLAP INDICATOR. MALFUNCTIONED. DURING CLIMB ON RETRACTION, OUTBOARD FLAPS STAYED AT 5 DEGREES WITH THE INBOARD FLAPS WENT TO 2 DEGREES AND STOPPED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT - [SDR 9520462709](https://openairdocs.org/sdr/9520462709), Dec 13, 1995: BATTERY PACK. DISCHARGED. DURING PRE-FLIGHT, FOUND COCKPIT EMERGENCY EXIT SIGN INOPERATIVE. REPLACED LIGHT BATTERY PACK AND BATTERIES. CHECKED OK. - [SDR 9510352709](https://openairdocs.org/sdr/9510352709), Jul 1, 1995: DOOR. OUT OF RIG. DURING CLIMB MSP-GEG, FOUND THAT THE AIRCRAFT WOULD NOT PRESSURIZE. FURTHER INVESTIGATION REVEALED AN AIR LEAK AT THE MAIN CABIN DOOR. DOOR WARNING INDICATED TH - [SDR 9510932709](https://openairdocs.org/sdr/9510932709), Jun 9, 1995: CHORD. CRACKED. DURING PERIODIC CHECK, FOUND CRACKS IN THE WING-TO-BODY RIB UPPER CHORD, BOTH UPPER AND LOWER FORWARD FASTENER HOLES BS 760, LBL 70.5. REPAIRED PER EA 27-98428. - [SDR 9509552709](https://openairdocs.org/sdr/9509552709), Jun 9, 1995: FRAME. CRACKED. DURING H-CHECK, FOUND TWO, 2 INCH CRACKS IN THE BS 1303 FRAME BETWEEN THE LEFT AND RIGHT TORQUE BOXES AT THE LOWER LEFT AND RIGHT CORNERS. REPAIRED THE FRAME (P - [SDR 9509302709](https://openairdocs.org/sdr/9509302709), Jun 8, 1995: CHORD. CORRODED. DURING H-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WELL LEFT SIDE PANEL CHORD FS 336. REPAIRED CHORD (P/N 65-19861-7) PER EA 27-98463. - [SDR 9509292709](https://openairdocs.org/sdr/9509292709), Jun 8, 1995: LONGERON. CORRODED. DURING H-CHECK, FOUND CORROSION ON STR 29L FROM FS 950B TO 1000. REPAIRED STRINGER (P/N 65-56441-4) PER EA 27-98455. - [SDR 9509282709](https://openairdocs.org/sdr/9509282709), Jun 8, 1995: LONGERON. CRACKED. DURING H-CHECK, FOUND CORROSION AND CRACKS ON STR 29R FROM BS 950E TO 985. REPAIRED STRINGER (P/N 65-56441-4) PER EA 27-98461. - [SDR 9509542709](https://openairdocs.org/sdr/9509542709), Jun 7, 1995: RIB. CRACKED. DURING H-CHECK, FOUND CRACKS IN THE RIGHT WING-TO-BODY UPPER RIB CHORD BS 760 AT RBL 70.5. REPAIRED CHORD (P/N 65-18522-14) PER EA 27-98434. - [SDR 9509122709](https://openairdocs.org/sdr/9509122709), Jun 2, 1995: MOUNT. CORRODED. DURING 'H' CHECK, FOUND CORROSION IN THE NR 2 ENGINE AFT MOUNT FITTING, AFT FLANGE. REPLACED FITTING PER SRM 54-40-1, PG.1-2. ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other DJI MATRICE 600 PRO aircraft: https://openairdocs.org/model/dji-matrice-600-pro/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.