# N713AA: DJI AGRAS T40

- Status: Valid registration
- Airframe: [DJI AGRAS T40](https://openairdocs.org/model/dji-agras-t40) (registry code 06102D3)
- Serial number: 64TBK8L00100RS
- Type: Rotorcraft
- Engine type: Electric
- Certificate issued: October 21, 2024
- Expires: October 31, 2031
- Mode S code: A98733
- Registered owner: [Junior Enterprises LLC](https://openairdocs.org/faa-owner/JUNIOR%20ENTERPRISES%20LLC)
- Location: [La Quinta, CA](https://openairdocs.org/faa-place/CA/La%20Quinta)
- Owner type: LLC
- Owner's area on the map: 33.6634° N, 116.3100° W: Placed by OpenAirDocs: center of La Quinta, CA, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=713AA
- Page: https://openairdocs.org/aircraft/N713AA

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 T40)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N713AA.

## FAA accident and incident reports

None matched to N713AA.

## 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 N713AA not matched to an aircraft (135, newest 50)

They name N713AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR C8GA20120427006](https://openairdocs.org/sdr/C8GA20120427006), Apr 24, 2012: ACTUATOR. DAMAGED. RT RAM AIR DOOR AND LOWER ACTUATOR ROD MISSING ON POST FLIGHT INSPECTION. NO DAMAGE TO FUSELAGE NOTED. R & R RIGHT RAM AIR DOOR ACTUATOR, INSTALLED RAM AIR DOOR
- [SDR C8GA2011000007](https://openairdocs.org/sdr/C8GA2011000007), Jun 22, 2011: SHAFT. SHEARED. DURING CRUISE OPERATION AT FL 300, THE NR 1 ENGINE HYD SYS "A" LOW PSI LIGHT ILLUMINATED. ACFT DIVERTED WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS P
- [SDR FOTR2019813815](https://openairdocs.org/sdr/FOTR2019813815), Dec 3, 2010: STRUCTURE. CRACKED. RT SIDE OF AFT AIRSTAR TORQUE BOX UPPER CORD IS CRACKED AT AIRSTAIR ACTUATOR FITTING. REMOVED UPPER CHORD FROM RT SIDE AFT AIRSTAIR TORQUE BOX STA BS 1263 IAW 5
- [SDR FOTR2019813123](https://openairdocs.org/sdr/FOTR2019813123), Dec 1, 2010: HINGE. CRACKED. MCD UPPER AFT MOST SEGMENT FUSELAGE SIDE AFT LOBE IS CRACKED. REMOVED MAIN CARGO DOOR AFT SEGMENT HINGE IAW FREIGHTER MM, FIG 5201B, REV F. FABRICATED NEW SECTI
- [SDR FOTR2019813835](https://openairdocs.org/sdr/FOTR2019813835), Dec 1, 2010: SHEAR TIE. CORRODED. (FOTR) CORROSRION ON SHEAR TIE AT BS 720 BETWEEN STR 28L-28R. REMOVED CORRODED SHEAR TIE FROM STA 720 BETWEEN STR 28L & 28R IAW SRM 51-30-2. FABRICATED SHEAR TI
- [SDR FOTR2019813414](https://openairdocs.org/sdr/FOTR2019813414), Nov 30, 2010: FLOORBEAM. CRACKED. (FOTR) MAIN CABIN OVERWING FLOORBEAM T-CORD CRACKED AT RADIUS BS 760, LBL 45.50. REMOVED DAMAGED T-CORD FROM BS 760 LBL 45.50 IAW SRM 51-30-2. FABRICATED NEW T-
- [SDR FOTR2019813281](https://openairdocs.org/sdr/FOTR2019813281), Nov 30, 2010: FRAME. DAMAGED. (FOTR) STA 950B FRAME HAS 2 FASTENERS W/NO ED AT GILLINER SUPPORT IN WINDOW AREA ON RT SIDE. CUT OUT DAMAGE AREA 1" X .7500" IAW SRM 53-10-4, FIG 1. FABRICATED 
- [SDR FOTR2019813419](https://openairdocs.org/sdr/FOTR2019813419), Nov 30, 2010: INTERCOSTAL. CORRODED. (FOTR) CORROSION ON LOWER FLANGE OF INTERCOSTAL AT BS700 BETWEEN STR 28R - 27R. REMOVED INTERCOSTAL AT STA 700 BETWEEN STR 28R AND 27R IAW SRM 51-30-2. FABRICAT
- [SDR FOTR2019813838](https://openairdocs.org/sdr/FOTR2019813838), Nov 30, 2010: INTERCOSTAL. CORRODED. (FOTR) CORROSION ON INTERCOSTAL BETWEEN BS 720-700 STR 27R-28R. REMOVED CORRODED INTERCOSTAL FROM BETWEEN STA 720-700, STR 27R-28R IAW SRM 51-30-2. FABRICATED N
- [SDR FOTR2019813745](https://openairdocs.org/sdr/FOTR2019813745), Nov 29, 2010: FLOORBEAM. DAMAGED. BS 420, RBL 60, FLOORBEAM HAS DOUBLE DRILL. CUT OUT DAMAGE AREA DIM 10.5" X 1" IAW SRM 53-410-8, FIG 8. FAB 2 EA ANGLES REPAIRS FROM 7075-0 .090" PO 9009880 DIM
- [SDR FOTR2019813790](https://openairdocs.org/sdr/FOTR2019813790), Nov 29, 2010: SKIN. CORRODED. UPON REMOVAL OF INTERCOSTAL FOUND FUSELAGE SKIN TO BE CORRODED BETWEEN BS 700-720 STR 28R-27R. REMOVED 8" BODY FAIRINGS FROM 710 TO 720 LT AND RT IAW SRM 51-30-
- [SDR FOTR2019813278](https://openairdocs.org/sdr/FOTR2019813278), Nov 29, 2010: FRAME. DAMAGED. BS 950F, FRAME HAS 2 RIVETS W/NO E.D. IN WINDOW BELT AREA. CUT OUT DAMAGE AREA 1" X .7500" IAW SRM 53-10-4, FIG 1. FABRICATED FRAME REPAIR 2 EA PARTS MAT USED 7
- [SDR FOTR2019813426](https://openairdocs.org/sdr/FOTR2019813426), Nov 29, 2010: FRAME. DAMAGED. STA 720F FRAME HAS FASTENERS W/NO E.D. IN WINDOW AREA. CUT OUT DAMAGE AREA DIM. 1" X .7500" IAW SRM 53-10-4, FIG 1. FABRICATED FRAME REPAIR MAT, USED 7075-0 .07
- [SDR FOTR2019813280](https://openairdocs.org/sdr/FOTR2019813280), Nov 26, 2010: FRAME. DAMAGED. BS 910 FRAME HAS 2 FASTENERS W/NO E.D. AT GILLINER SUPPORT IN WINDOW AREA ON RT SIDE. CUT OUT DAMAGE AREA DIM 1" X .7500" IAW SRM 53-10-4, FIG 1. FABRICATED FRA
- [SDR FOTR2019813744](https://openairdocs.org/sdr/FOTR2019813744), Nov 26, 2010: FRAME. DAMAGED. BS 440, RBL 60 FRAME HAS DOUBLE DRILL AT FLOOR LEVEL. CUT DAMAGE AREA AT STA 440 RT FRAME DIM 1.2500" X 1" IAW SRM 51-40-3. FAB NEW REPAIR FRAME FROM 7075-0 .06
- [SDR FOTR2019813439](https://openairdocs.org/sdr/FOTR2019813439), Nov 26, 2010: FRAME. DAMAGED. STA 720E, FRAME HAS FASTENERS W/NO ED IN WINDOW AREA ON LT SIDE. CUT OUT DAMAGE AREA DIM 1" X .7500" FAB FRAME REPAIR 2EA PARTS MAT. USED 7075-0 .071" PO 900163
- [SDR FOTR2019813696](https://openairdocs.org/sdr/FOTR2019813696), Nov 26, 2010: FLOORBEAM. CRACKED. (FOTR) CRACK AROUND BOLT HOLE, FLOORBEAM RBL 12 AT FS 950D. C/W HFEC INSPECTED IAW NDTM PT6. 51-00-00, FIG 23. CRACK NOTED AT FASTENER HOLE. TRIMMED OUT DAMAGE 
- [SDR FOTR2019813282](https://openairdocs.org/sdr/FOTR2019813282), Nov 26, 2010: FRAME. DAMAGED. BS 950A FRAME HAS 2 FASTENERS W/NO ED IN WINDOW AREA ON RT SIDE. CUT OUT DAMAGED AREA DIM. 1" X .7500" IAW SRM 53-10-4, FIG 1 FABRICATED FRAME REPAIR 2 EA PARTS
- [SDR FOTR2019813832](https://openairdocs.org/sdr/FOTR2019813832), Nov 26, 2010: FRAME. DAMAGED. REMOVAL OF GILLINER ATTACH ANGLE ON LT SIDE OF FUSELAGE AT TOP OF WINDOW LEVEL REVEALED DOUBLE DRILL HOLES IN FRAME AT FS 720D. CUT DAMAGED AREA DIM. .800" X .8
- [SDR FOTR2019813831](https://openairdocs.org/sdr/FOTR2019813831), Nov 26, 2010: FRAME. DAMAGED. REMOVAL OF GILLINER ATTACH ANGLE ON LT SIDE OF FUSELAGE AT TOP OF WINDOW LEVEL REVEALED DOUBLE DRILL HOLES IN FRAME AT FS 720C. CUT OUT DAMAGED AREA DIM. .800" 
- [SDR FOTR/20198/13725](https://openairdocs.org/sdr/FOTR%2F20198%2F13725), Nov 26, 2010: FRAME. DAMAGED. (FOTR) BWS 910, FRAME LT SIDE OF FUSELAGE HAS A DOUBLE DRILL AT FLOOR LEVEL. CUT OUT DAMAGED AREA DIM .700" X .500" ON FRAME STA 910 LT FLOOR LEVEL IAW SRM 51-4
- [SDR FOTR/20198/13818](https://openairdocs.org/sdr/FOTR%2F20198%2F13818), Nov 24, 2010: SKIN. DENTED. EVALUATE DENTS 2EA AT LT INBD FORE FLAP LOWER SURFACE 62" FROM INBD EDGE. REMOVED DAMAGE SANDED, CLEANED, AND PREPPED AREA IAW SRM 51-40-20. FABRICATED DOUBLER 
- [SDR FOTR20198/13413](https://openairdocs.org/sdr/FOTR20198%2F13413), Nov 24, 2010: FLOOR SUPPORT. CRACKED. MAIN CABIN OVERWING FLOORBEAM T-CORD CRACKED AT RADIUS BS 760 45.5. REMOVED DAMAGED T-CORD FROM STA 760-870, RBL 45 IAW SRM 51-30-2. FABRICATED NEW T-CORD FROM 
- [SDR FOTR2019813376](https://openairdocs.org/sdr/FOTR2019813376), Nov 24, 2010: SKIN. CORRODED. CORROSION ON RT OTBD FWD FLAP. REMOVED DAMAGE, SANDED, CLEANED PREPPED AREA IAW SRM 51-40-20. FABBED DOUBLES FROM 2024-T3 .020" PO 9009917, APPROX 12" X 3". HOT
- [SDR FOTR2019813418](https://openairdocs.org/sdr/FOTR2019813418), Nov 24, 2010: SHEAR TIE. CORRODED. CORROSION ON SHEAR TIE AFT SIDE OF BS 700 BETWEEN STR 28L-27L. CUT OUT DAMAGED AREA AT STA 700 BETWEEN STR 27L - 28L DIM 5.5" X 1" IAW SRM 51-10-1. FAB NEW AFT 
- [SDR FOTR2019813834](https://openairdocs.org/sdr/FOTR2019813834), Nov 24, 2010: SHEAR TIE. CORRODED. SHEAR TIE CORRODED AT BS 685 BETWEEN STR 25L & 26L. REMOVED SHEAR TIE AT STA 685 BETWEEN STR 25L-26L IAW 51-30-2. FABRICATED NEW SHEAR TIE FROM 7075-T6 .040" DI
- [SDR FOTR2019813839](https://openairdocs.org/sdr/FOTR2019813839), Nov 24, 2010: STRINGER. CORRODED. (FOTR) CORROSION ON STR 28L AT BS 68-720. REMOVED STR 28L AT STA 680-720 IAW SRM 51-30-2. FAB NEW STRINGER FROM PN 1498-145 7075-T6 PO 90010545 DIM 41" IAW SRM 
- [SDR FOTR2019813833](https://openairdocs.org/sdr/FOTR2019813833), Nov 24, 2010: SHEAR TIE. CORRODED. (FOTR) BETWEEN STR 27R-28R, BS 720 SHEAR TIE CORRODED. CUT OUT DAMAGED AREA AT SHEAR TIE STA 720, STR 27R - 28R 5.5" X 1" IAW SRM 53-10-4, FIG 15 FAB REPAIR SHE
- [SDR FOTR2019813535](https://openairdocs.org/sdr/FOTR2019813535), Nov 24, 2010: STRINGER SPLICE. CORRODED. CORROSION ON STRINGER SPLICE AT BS 720, STR 28R. REMOVED STRINGER SPLICE FROM STA 680-720, STR SPLICE 28R IAW SRM 51-30-2. FAB STRINGER SPLICE FROM PN BAC1498-1
- [SDR FOTR2019813837](https://openairdocs.org/sdr/FOTR2019813837), Nov 24, 2010: INTERCOSTAL. CORRODED. CORROSION ON ITERCOSTAL BETWEEN BS 700-720 & STR 27L - 28L. REMOVED INTERCOSTAL AT BS 700-720 BETWEEN STR 27L-28L IAW SRM 51-30-2. FAB NEW INTERCOSTAL FROM 7075
- [SDR FOTR2019813836](https://openairdocs.org/sdr/FOTR2019813836), Nov 24, 2010: SHEAR TIE. CORRODED. CORROSION ON SHEAR TIE AT BS 700 BETWEEN STR 27L & 28L. CUT OUT DAMAGE AREA AT SHEAR TIE BS 700 STR 27L-28L DIM. 5.5" X 1" IAW SRM 53-10-4 FIG 5. FABRICATED SHE
- [SDR FOTR/20198/13727](https://openairdocs.org/sdr/FOTR%2F20198%2F13727), Nov 23, 2010: SEAT TRACK. DAMAGED. BS 850-870, LBL 45, SEAT TRACK HAS DOUBLE DRILLED HOLES, REMOVED SEAT TRACK SECTION BS 850 TO 870 LBL45 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION FROM 
- [SDR FOTR/20198/13607](https://openairdocs.org/sdr/FOTR%2F20198%2F13607), Nov 23, 2010: SEAT TRACK. CORRODED. CABIN SEAT TRACK IS CORRODED & PIECE IS BROKEN OFF AT RBL 45.5 BETWEEN BS 520 AND 540. REMOVED SEAT TRACK SECTION FROM STA 480 TO 690 RBL 45 IAW SRM 51-30-2, FA
- [SDR FOTR/20198/13786](https://openairdocs.org/sdr/FOTR%2F20198%2F13786), Nov 23, 2010: SEAT TRACK. DAMAGED. BS 850-870 LBL24 SEAT TRACK HAS DOUBLE DRILLED HOLES. REMOVED SEAT TRACK SECTION BS 850 TO 870 LBL 24 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION FROM BA
- [SDR FOTR/20198/13825](https://openairdocs.org/sdr/FOTR%2F20198%2F13825), Nov 23, 2010: SEAT TRACK. DAMAGED. BS 740-760, RBL 45.5 FLOATING SEAT TRACK ATTACH HOLE IS ELONGATED. REAMED HOLE TO A .5625" DIAMETER IAW SRM 51-20-01. REPLACED BUSHING PN NAS538B7P150 PO 342522
- [SDR FOTR/20198/13620](https://openairdocs.org/sdr/FOTR%2F20198%2F13620), Nov 23, 2010: SEAT TRACK. CHAFED. FWD EDGE OF LBL24 SEAT TRACK CHAFED AT BS 870. C/A REMOVED SEAT TRACK FROM STA 870 TO 960 LBL 24.75. FAB NEW SEAT TRACK FROM BAC1520-792 7178-T6511 PO NR 900105
- [SDR FOTR2019813712](https://openairdocs.org/sdr/FOTR2019813712), Nov 23, 2010: SEAT TRACK. CORRODED. SEAT TRACK IS CORRODED AT LBL 24. CA/ REMOVED DAMAGED SEAT TRACK FROM STA 950+10 TO 1130 LBL 24 IAW SRM 51-30-2. FAB NEW SEAT TRACK FROM BAC1520-792-T65 PO NR 9
- [SDR FOTR2019813611](https://openairdocs.org/sdr/FOTR2019813611), Nov 22, 2010: FRAME. DENTED. CABIN HAS FRAME DENTED AT BS 440, STR 7R. CUTOUT DAMAGE AREA DIM. 1" X 2.3750" AT BS 440, STR 7R IAW SRM 53-10-4, FIG 1. FABRICATED PARTS FROM 7075-0 .050" DIM 
- [SDR FOTR2019813754](https://openairdocs.org/sdr/FOTR2019813754), Nov 22, 2010: FRAME. DENTED. BS 380, FRAME HAS DENT AT STR 5R. CUTOUT DAMAGED AREA 1" X 1.2500" AT BS 380 FRAME STR 5R IAW SRM 53-10-4. FABRICATED REPAIR PARTS FROM 7075-0 .050" PO 20006220
- [SDR FOTR2019813610](https://openairdocs.org/sdr/FOTR2019813610), Nov 22, 2010: FRAME. DENTED. CABIN FRAME IS DENTED AT BS 420, STR 7R. CUTOUT DAMAGED AREA DIM. 1" X 1.7500" ON FRAME STA 420, STR 7R IAW SRM 53-10-4, FIG 1, FABRICATED REPAIR PARTS FROM 707
- [SDR FOTR2019813804](https://openairdocs.org/sdr/FOTR2019813804), Nov 22, 2010: FRAME. DAMAGED. BS 360 BEWTEEN STR 5L & 6L FRAME SPLICE HAS DRILL HOLE THROUGH RADIUS. REMOVED DAMAGED ANGLE IAW SRM 51-30-2 LOCATED & DRILLED NEW ANGLE PN AE727-2-360-11 IAW S
- [SDR FOTR2019813582](https://openairdocs.org/sdr/FOTR2019813582), Nov 22, 2010: FRAME. CRACKED. BS 985, RBL 24, FRAME SUPPORT IS CRACKED AT LIGHTNING HOLE. REMOVED FLOOR SUPPORT FROM BS 950E-990 BETWEEN RBL 8 TO RBL 16 IAW SRM 51-30-2. REMOVED FRAME IAW SR
- [SDR FOTR2091813273](https://openairdocs.org/sdr/FOTR2091813273), Nov 22, 2010: FRAME. DAMAGED. BS 1148 AT STR 14R FRAME HAS 2EA DRILL STARTS UNDER GILLINER SUPPORT. CUT OUT DAMAGE AREA DIM. 1.3750" X 1" IAW SRM 51-40-3, FIG 1. FABRICATED ANGLE FROM 7075-0
- [SDR FOTR2019813445](https://openairdocs.org/sdr/FOTR2019813445), Nov 22, 2010: BEAM. CORRODED. LT HORIZ STAB EXFOLIATED CORROSION AT T/E BETWEEN ELEV STA 99.97 AND ELEV STA 136.50. REMOVED CORROSION DAMAGE FROM LT HORIZ STABILIZER UPPER T/E BEAM AT SS 132
- [SDR FOTR2019814000](https://openairdocs.org/sdr/FOTR2019814000), Nov 22, 2010: INTERCOSTAL. CRACKED. BS 360 BETWEEN STRINGER 6 & 7 LT INTERCOSTAL IS CRACKED. CUT OUT DAMAGED AREA .2500" X .5" ON INTERCOSTAL STA 360 BETWEEN STR 6 & 7L IAW SRM 51-40-3, FIG 1. FAB
- [SDR FOTR2019813715](https://openairdocs.org/sdr/FOTR2019813715), Nov 21, 2010: FRAME. MISINSTALLED. BS 890 FRAME HAS FASTENER WITH NO ED IN WINDOW AREA, LT SIDE. CUTOUT DAMAGED AREA DIM .75" X .5' ON STA 890 FRAME IAW SRM 53-10-4 FIG 1. FABRICATED 2 EA DOUBLER
- [SDR FOTR2019813714](https://openairdocs.org/sdr/FOTR2019813714), Nov 21, 2010: FRAME. DAMAGED. BS 930 FRAME HAS FASTENER WITH NO ED AT WINDOW AREA, LT SIDE. CUTOUT DAMAGED AREA DIM .75" X .5" ON STA 930 FRAME LT IAW SRM 53-10-4, FIG 1 FABRICATED 2 EA DOUB
- [SDR FOTR2019813713](https://openairdocs.org/sdr/FOTR2019813713), Nov 21, 2010: FRAME. DAMAGED. BS 950A, FRAME HAS FASTENERS WITH NO ED IN WINDOW AREA. LT SIDE. CUTOUT DAMAGED AREA DIM. .75" X .5" ON STA 950A FRAME LT IAW SRM 53-10-4, FIG 1 FABRICATED 2 EA
- [SDR FOTR2019813689](https://openairdocs.org/sdr/FOTR2019813689), Nov 20, 2010: SEAT TRACK. CORRODED. BS 1070-1010, SEAT TRACK LBL 48 IS CORRODED. REMOVED CORROSION ON UPPER FLANGE OF LBL 48, SEAT TRACK SECTION EVALUATED ARE FOUND AREA TO BE OUT OF LIMITS. REMOV
- [SDR FOTR2019813724](https://openairdocs.org/sdr/FOTR2019813724), Nov 20, 2010: SEAT TRACK. CORRODED. BS 960, RBL 24, SEAT TRACK HAS GOUGE. REMOVED CORROSSION FOUND TO BE OUT OF LIMITS IAW SRM 51-10-6 & 53-10-1 FIG 3. FABRICATED SEAT TRACK AND SPLICE FROM BAC150

All 135: https://openairdocs.org/aircraft/N713AA/unmatched-reports.md

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other DJI AGRAS T40 aircraft: https://openairdocs.org/model/dji-agras-t40/aircraft.md

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