# N509DC: DJI AGRAS T50 - Status: Sale reported - Airframe: [DJI AGRAS T50](https://openairdocs.org/model/dji-agras-t50) (registry code 06102HG) - Serial number: 1581F6BUB235N001002T - Type: Rotorcraft - Engine type: Electric - Mode S code: A65BAD - Location: [Henderson, KY](https://openairdocs.org/faa-place/KY/Henderson) - Owner type: Individual - Owner's area on the map: 37.7992° N, 87.5161° W: Placed by OpenAirDocs at the center of ZIP code 42420, within about 8 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=509DC - Page: https://openairdocs.org/aircraft/N509DC 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 T50) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N509DC. ## FAA accident and incident reports None matched to N509DC. ## 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 N509DC not matched to an aircraft (53, newest 50) They name N509DC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR AWXA200100525](https://openairdocs.org/sdr/AWXA200100525), Oct 8, 2001: TRANSMITTER. ARCED. ON APPROACH T/E FLAPS LOCKED OUT AT 5 UNITS, APPROACH WAS ABORTED. CREW FOLLOWED QRH CHECKLIST. ON RETURN FLAP POS INDICATOR NEEDLES MARRIED UP, CREW SELECTED F - [SDR AWXA200100452](https://openairdocs.org/sdr/AWXA200100452), Sep 18, 2001: FLAP. MALFUNCTIONED. SFO - FLAP LOCKOUT - FLT 815 - C - ON APPROACH TO SFO FLAPS 5 WAS SELECTED AND THE FLAP POSITION INDICATOR NEEDLES SPLIT AT FLAPS 1 AND THE FLAPS STOPPED AT FLA - [SDR AWXA0002077](https://openairdocs.org/sdr/AWXA0002077), Aug 5, 2001: CYLINDER. FAULTY. PHX-EMERGENCY LANDING -FLT 229- ON LANDING GEAR EXTENSION THE CREW HEARD A LOUD NOISE AND THE ACFT YAWED TO THE LEFT. ALL INDICATIONS WERE NORMAL AND ALL PRESSU - [SDR AWXA0001297](https://openairdocs.org/sdr/AWXA0001297), Feb 8, 2001: SKIN. CRACKED. R-1 DOOR FRAME LOWER AFT CORNER SKIN IS CRACKED; EMINATING FROM FASTENER TRAVELING TOWARD RADIUS. STOP DRILLED CRACK; FABED REPAIR DOUBLERS; DRILLED, TREATED, P - [SDR AWXA0001296](https://openairdocs.org/sdr/AWXA0001296), Feb 8, 2001: SKIN. CHAFED. RT WING O/B MID FLAP HAS A CHAFED AREA AT I/B FLAP TRACK ON LOWER SKIN. REPAIRED IAW AWA ER 03-5754-01027. - [SDR AWXA0001295](https://openairdocs.org/sdr/AWXA0001295), Feb 8, 2001: SKIN. CHAFED. LT WING O/B MID FLAP HAS A CHAFED AREA AT I/B FLAP TRACK ON LOWER SKIN. REPAIRED IAW AWA ER 03-5754-01027. - [SDR AWXA0001294](https://openairdocs.org/sdr/AWXA0001294), Feb 8, 2001: DOUBLER. CRACKED. CRACK IN RT WING INBOARD L/E SKIN JUST ABOVE INBOARD END OF L/E FLAP SEAL DOOR. CUT OUT CRACKED AREA; HFEC PERFORMED; FABED FILLER AND INTERNAL DOUBLER; INSTALL - [SDR AWXA0001293](https://openairdocs.org/sdr/AWXA0001293), Feb 8, 2001: FLOOR SUPPORT. DAMAGED. SUSPECT CRACK IN LEFT W/W AT STA 664.75 BL 33 UPPER PRESSURE PANEL. HFEC PERFORMED; CUTOUT DAMAGED AREA; FABED REPAIR DOUBLER, FILLER AND STIFFENER; INSTALLED I - [SDR AWXA0001292](https://openairdocs.org/sdr/AWXA0001292), Feb 8, 2001: SKIN. CRACKED. L-2 DOOR UPPER HINGE CUTOUT SKIN IS CRACKED.CUTOUT DAMAGED FUSELAGE SKIN; FABED REPAIR DOUBLER AND FILLER; DRILLED ATTACHMENT LOCATIONS; TREATED AND PRIMED REPA - [SDR AWXA0001291](https://openairdocs.org/sdr/AWXA0001291), Feb 8, 2001: FLOOR SUPPORT. DAMAGED. FLOOR SUPPORT END FITTING AT BS 328 HAS A HOLE DRILLED IN THE RADIUS. DRILLED HOLE TO .159 THROUGH INTERNAL DOUBLER AND EXTERNAL SKIN; COUNTERSUNK SKIN; INSTALL - [SDR AWXA0001290](https://openairdocs.org/sdr/AWXA0001290), Feb 8, 2001: SKIN. DENTED. HORIZONTAL STABILIZER LEADING EDGE SKIN DENTED STA 258.28. REPAIRED DENT IN LEADING EDGE SKIN OF LEFT HORIZONTAL STABILIZER IAW B737-300 SRM 55-10-01 FIG 203 WI - [SDR AWXA0001289](https://openairdocs.org/sdr/AWXA0001289), Feb 8, 2001: FLOORBEAM. CORRODED. CORROSION ON UPPER SURFACE OF TRANSVERSE FLOORBEAM AT BS 312 RBL 3 - 9. REMOVED UPPER T-ANGLE OF TRANSVERSE FLOORBEAM; REMOVED LT SPLICE ANGLES; FABED SPLICE PL - [SDR AWXA0001288](https://openairdocs.org/sdr/AWXA0001288), Feb 8, 2001: BULKHEAD. CRACKED. HFEC AND VISUAL (10X) CONFIRMS CRACK OF UNDETERMINED LENGTH UNDER STRAP AT BS 178 RBL 4 7/8 WL 199.5 TO 201.5. REMOVED STIFFENERS, RADOME ATTACH BRACKETS AND BA - [SDR AWXA0001287](https://openairdocs.org/sdr/AWXA0001287), Feb 8, 2001: BULKHEAD. CRACKED. ULTRASONIC INSPECTION REVEALED CRACK INDICATION BS 178 BULKHEAD WEB AT RBL 1.3 TO UNDETERMINED POINT BENEATH STRAP AT WL 205.7; CONFIRMED HFEC. REMOVED LOWER L- - [SDR AWXA0001226](https://openairdocs.org/sdr/AWXA0001226), Jan 4, 2001: LIGHT. INOPERATIVE. SEAT EMERGENCY LIGHT AT SEAT 21C INOP. RESECURED LOOSE WIRE; LIGHT OPS CHECKS GOOD - [SDR AWXA9900352](https://openairdocs.org/sdr/AWXA9900352), Oct 11, 1999: APU. MALFUNCTIONED. FAINT BURNING SMELL IN COCKPIT. T/S AIR CONDITIONING SYSTEM, DETERMINED TO BE APU BLEED. PLACED ON MEL 49-01, CNTL NR 121373. - [SDR AWXA9900026](https://openairdocs.org/sdr/AWXA9900026), Jan 20, 1999: EGT GAUGE. MALFUNCTIONED. NR 1 ENG EGT GAUGE VERY ERRATIC. NEEDLE FOLLOWS DIGITAL INDICATION WHICH INTERMITTENTLY BLANKS. BEGAN WORKING NORMAL FOR ABOUT THE LAST 15 MIN OF APPROACH. INSP - [SDR AWXA9700610](https://openairdocs.org/sdr/AWXA9700610), Oct 1, 1997: FRAME. CORRODED. DURING SCHEDULED C-13 INSPECTION, FOUND CORROSION IN RT 685 FRAME UPLOCK SUPPORT SHAFT BORE UNDER BUSHINGS. LINE BORED 685 FITTING PER ER 3-32-33-05 STEP 1, 2.3 - [SDR AWXA9700609](https://openairdocs.org/sdr/AWXA9700609), Oct 1, 1997: TRUNNION. CORRODED. DURING SCHEDULED C-13 INSPECTION, FOUND MINOR SURFACE CORROSION AT NLG RT TRUNNION BEARING BORE AT 2:30 POSITION. REMOVED ALL CORROSION FROM BORE AND BORE ID TO - [SDR AWXA9700608](https://openairdocs.org/sdr/AWXA9700608), Oct 1, 1997: FRAME. CORRODED. DURING SCHEDULED C-13 INSPECTION, FOUND PITTING CORROSION AND MINOR GOUGES UPON REMOVAL OF BUSHINGS FROM LT 685 FRAME. REMOVED ALL CORROSION AND LINE BORED 685 - [SDR AWXA9700403](https://openairdocs.org/sdr/AWXA9700403), Jul 19, 1997: ACTUATOR. LEAKING. AIR TURNBACK APPROXIMATELY 20 MINUTES AFTER TAKEOFF, NOTICED B-SYSTEM HYDRAULIC SLOWLY MOVING DOWN PASSED HALF FULL. REMOVED AND REPLACED PLUG AND O-RING ON NR - [SDR AWXA9600673](https://openairdocs.org/sdr/AWXA9600673), Nov 18, 1996: FLOOR BEAM. CORRODED. PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM UPPER CHORD BS 312, LBL 15 - RBL 15, WL 208. FABRICATED AND REPAIRED FLOOR BEAM - [SDR AWXA9600686](https://openairdocs.org/sdr/AWXA9600686), Nov 14, 1996: GALLEY TRACK. CORRODED. PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON INBOARD GALLEY TRACK STATION 294.5, WL 208, RBL 16. INSTALLED FABRICATED SEAT TRACK AT BS - [SDR AWXA9600685](https://openairdocs.org/sdr/AWXA9600685), Nov 14, 1996: SEAT TRACK. CORRODED. PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK FLANGE STATION 328, RBL 45, WL 208. INSTALLED FABRICATED SEAT TRACK AT BS 328-3 - [SDR AWXA9600684](https://openairdocs.org/sdr/AWXA9600684), Nov 14, 1996: GALLEY TRACK. CORRODED. PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON OUTBOARD GALLEY TRACK STATION 328, RBL 55, WL 208. INSTALLED FABRICATED SEAT TRACK AT BS 3 - [SDR AWXA9600677](https://openairdocs.org/sdr/AWXA9600677), Oct 30, 1996: SKIN. DISBONDED. PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND GRAVEL DAMAGE ON LOWER SURFACE INBOARD END, R/W INBOARD FOREFLAP. REPAIRED GRAVEL DAMAGE PER IAW SRM 51 - [SDR AWXA9600676](https://openairdocs.org/sdr/AWXA9600676), Oct 30, 1996: SKIN. DISBONDED. PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND GRAVEL DAMAGE ON INBOARD END LOWER SURFACE OF L/W INBOARD FOREFLAP. REPAIRED GRAVEL DAMAGE PER IAW SRM - [SDR AWXA9600675](https://openairdocs.org/sdr/AWXA9600675), Oct 30, 1996: STRINGER. CORRODED. PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND TWO AREAS OF CORROSION ON BOTH LOWER CORNERS OF THE APU INLET DOOR OPENING IN APU CAVITY. LOWER STRINGE - [SDR AWXA9600674](https://openairdocs.org/sdr/AWXA9600674), Oct 28, 1996: FLOOR BEAM. CORRODED. PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM STATION 328, RBL 24-55, WL 208. REMOVED, FABRICATED AND INSTALLED REPAIR PARTS - [SDR AWXA9600672](https://openairdocs.org/sdr/AWXA9600672), Oct 25, 1996: SEAT TRACK. CORRODED. PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION IN SEAT TRACK WELL, STATION 498 TO 500 AND 500 A PLUS 10 INCH, LBL 45, WL 208. REMOVED AND RE - [SDR AWXA9600671](https://openairdocs.org/sdr/AWXA9600671), Oct 25, 1996: FLOOR BEAM. CORRODED. PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM STATION 294.5, LBL 12 TO RBL 12, WL 208. FABRICATED REPAIR AND INSTALLED PER IA - [SDR AWXA960477](https://openairdocs.org/sdr/AWXA960477), Jul 8, 1996: WIRE. BROKEN. PHX - FLT 0543 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE AT ROW 16. REPAIRED BROKEN WIRE. OSP CHECK GOOD. (X) - [SDR AWXA9500835](https://openairdocs.org/sdr/AWXA9500835), Dec 30, 1995: SKIN. DENTED. PHX/SNA - FLT 0661 - DENT FOUND IN LT HORIZONTAL STABILIZER 8 FEET INBOARD OF TIP. PERFORMED INTERIM REPAIR PER SRM 55-10-01. (X) - [SDR AWXA9500812](https://openairdocs.org/sdr/AWXA9500812), Dec 13, 1995: WIRE. BROKEN. PHX - FLT NR 0202 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT OUT AT ROW 4. BROKEN WIRE, REPINNED, OPS CHECK GOOD. (M) - [SDR AWXA9500785](https://openairdocs.org/sdr/AWXA9500785), Nov 22, 1995: FUSE. FAILED. PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE, FROM ROW 3ABC THROUGH ROW 6ABC. REMOVED AND REPLACED FUSE IN BATTERY CHARGER AS - [SDR AWXA9500784](https://openairdocs.org/sdr/AWXA9500784), Nov 20, 1995: FUSE. FAILED. PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE, FROM ROW 3 THROUGH ROW 6. REMOVED AND REPLACED FUSE AT FORWARD OVERHEAD BATTERY - [SDR AWXA9500709](https://openairdocs.org/sdr/AWXA9500709), Oct 10, 1995: BRACKET. CRACKED. PHX - DURING SCHEDULED C11 INSPECTION, FOUND SUPPORT BRACKET CRACKED UNDER NOSE GEAR VIEWING WINDOW PANEL. FABRICATED AND INSTALLED NEW ANGLE BRACKET AND DOUBLE - [SDR AWXA9500708](https://openairdocs.org/sdr/AWXA9500708), Oct 10, 1995: THRESHOLD. CORRODED. PHX - DURING SCHEDULED C11 INSPECTION, FOUND R2 DOOR THRESHOLD CHORD NUT PLATE HOLE CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 51-7 - [SDR AWXA9500707](https://openairdocs.org/sdr/AWXA9500707), Oct 10, 1995: THRESHOLD. CORRODED. PHX - DURING SCHEDULED C11 INSPECTION, FOUND L2 DOOR THRESHOLD CHORD NUT PLATE HOLE CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 51-7 - [SDR AWXA9500706](https://openairdocs.org/sdr/AWXA9500706), Oct 10, 1995: SKIN. CRACKED. PHX - DURING SCHEDULED C11 INSPECTION, FOUND FORWARD GALLEY DOOR OUTER SKIN CUTOUT FOR UPPER HINGE CRACKED IN LOWER AFT RADIUS CORNER. FABRICATED AND INSTALLED - [SDR AWXA9500705](https://openairdocs.org/sdr/AWXA9500705), Oct 10, 1995: SKIN. CRACKED. PHX - DUIRNG SCHEDULED C11 INSPECTION, FOUND FORWARD CARGO DOOR OUTER SKIN CRACKED AT DOOR HANDLE FLAPPER DOOR CUTOUT. REPAIRED PER ER 1-52-30-01B. (M) - [SDR AWXA9500704](https://openairdocs.org/sdr/AWXA9500704), Oct 10, 1995: FLOOR BEAM. CORRODED. PHX - DURING SCHEDULED C11 INSPECTION, FOUND FLOOR BEAM CORRODED AT NUT PLATE HOLES, STATION 986.5 RBL 23.5 TO RBL 40. (M) - [SDR AWXA9500703](https://openairdocs.org/sdr/AWXA9500703), Oct 10, 1995: KEEL BEAM. CRACKED. PHX - DURING SCHEDULED C11 INSPECTION, FOUND TWO CRACKS IN KEEL BEAM SKIN BETWEEN WHEEL WELL. REPAIRED CRACKS PER SRM 53-60-12, FIGURE 202. (M) - [SDR AWXA9500524](https://openairdocs.org/sdr/AWXA9500524), Aug 11, 1995: EEL CONNECTOR. LOOSE. PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 18 THROUGH ROW 22. RESECURED LIGHT CONNECTOR AT ROW 18, OPS CHECK OK. ( - [SDR AWXA9500515](https://openairdocs.org/sdr/AWXA9500515), Aug 8, 1995: ENGINE. OVERTEMP. COS - DURING CLIMB, CREW REPORTED BOTH ENGINES EXCEEDED ALLOWABLE EGT LIMITS, E1 GOING TO 980 DEGREES AND E2 TO 960 DEGREES. CREW CONTINUED TO PHX AND LANDED WI - [SDR 95ZZZM366](https://openairdocs.org/sdr/95ZZZM366), Aug 8, 1995: ENGINE. OVERTEMP. COS - DURING CLIMB, CREW REPORTED BOTH ENGINES EXCEEDED ALLOWABLE EGT LIMITS, E1 GOING TO 980 DEGREES AND E2 TO 960 DEGREES. CREW CONTINUED TO PHX AND LANDED WI - [SDR AWXA9500490](https://openairdocs.org/sdr/AWXA9500490), Aug 1, 1995: EEL CONNECTOR. LOOSE. PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATAIVE IN CABIN. RECONNECTED LOOSE CONNECTOR AT ROW 14, OPS CHECK GOOD. (M) - [SDR AWXA9500486](https://openairdocs.org/sdr/AWXA9500486), Jul 31, 1995: EEL WIRE. INOPERATIVE. PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE ROW 14 THROUGH ROW 18. REPAIRED WIRING, OPS CHECK GOOD. (M) - [SDR AWXA9500425](https://openairdocs.org/sdr/AWXA9500425), Jul 6, 1995: EEL LAMP. INOPERATIVE. PHX - DURING ROUTINE MAINTENANCE CHK, FOUND AFT, 4 EACH, FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BROKEN WIRE AND RELAMPED 2 ASSEMBLIES, OPS - [SDR AWXA9500259](https://openairdocs.org/sdr/AWXA9500259), May 3, 1995: EEL WIRE. BROKEN. PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY LIGHTS INOPERATIVE AT ROWS 18 THROUGH 20. CRIMPED NEW CONNECTOR ON BROKEN WIRE, OPS CHECK GOOD. (W All 53: https://openairdocs.org/aircraft/N509DC/unmatched-reports.md ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Earlier aircraft with N509DC The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N509DC before. - [Cancelled 2011-04-12](https://openairdocs.org/deregistered/N509DC-2011-04-12): Bombardier CL-600-2D24, S/N 15001. Exported to Canada. Owner: [Bombardier Capital Inc](https://openairdocs.org/faa-owner/BOMBARDIER%20CAPITAL%20INC), [Colchester, VT](https://openairdocs.org/faa-place/VT/Colchester) ## Related - Other DJI AGRAS T50 aircraft: https://openairdocs.org/model/dji-agras-t50/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.