# N753NA: DJI PHANTOM 3 PROFESSION

- Status: Valid registration
- Airframe: [DJI PHANTOM 3 PROFESSION](https://openairdocs.org/model/dji-phantom-3-profession) (registry code 06101C2)
- Serial number: P76DCE26010402
- Type: Rotorcraft
- Engine type: Electric
- Certificate issued: June 13, 2016
- Expires: June 30, 2029
- Mode S code: AA265B
- Registered owner: [Ecamsecure Inc](https://openairdocs.org/faa-owner/ECAMSECURE%20INC)
- Location: [Long Beach, CA](https://openairdocs.org/faa-place/CA/Long%20Beach)
- Owner type: Corporation
- Owner's area on the map: 33.8089° N, 118.1785° W: Placed by OpenAirDocs at the center of ZIP code 90806, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=753NA
- Page: https://openairdocs.org/aircraft/N753NA

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 PHANTOM 3 PROFESSION)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N753NA.

## FAA accident and incident reports

None matched to N753NA.

## 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 N753NA not matched to an aircraft (27)

They name N753NA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR NOCA00810](https://openairdocs.org/sdr/NOCA00810), Jan 22, 2010: SILL. CORRODED. 4L DOOR SILL CORROSION AT BS 1674 LBL 56. REPLACED GUTTER SUPPORT BRACKET PER SRM 51-10-02.
- [SDR RYNA200700026](https://openairdocs.org/sdr/RYNA200700026), Dec 3, 2007: SKIN. DAMAGED. LOWER FUSELAGE HAS EVIDENCE OF LIGHTNING STRIKE AT BS 510 AND BETWEEN STR 26R - 27R. REPAIRED FUSELAGE SKIN IAW B757-200 SRM 5I-00-01.
- [SDR RYNA200700022](https://openairdocs.org/sdr/RYNA200700022), Nov 23, 2007: FLOOR SUPPORT. CORRODED. PASSENGER CABIN FLOOR SUPPORT CORRODED AT BS 324-377 AND BETWEEN BL 0 AND RBL 3, WATER LINE 208. REPLACED CABIN FLOOR SUPPORT.
- [SDR RYNA200700023](https://openairdocs.org/sdr/RYNA200700023), Nov 23, 2007: FLOOR SUPPORT. CORRODED. PASSENGER CABIN FLOOR SUPPORT CORRODED AT BS 1640-1661 AND RBL 13, WATER LINE 208. REPLACED CABIN FLOOR SUPPORT BOTH INTERCOSTALS WHICH ARE FABRICATED FROM BOC1
- [SDR RYNA200700015](https://openairdocs.org/sdr/RYNA200700015), Nov 22, 2007: SKIN. DENTED. FUSELAGE SKIN HAS AN OUT OF LIMIT DENT AT BS 405 AND BETWEEN STG 24R AND 25R. REPAIRED IAW EO C00-5-53-483-07.
- [SDR RYNA200700019](https://openairdocs.org/sdr/RYNA200700019), Nov 21, 2007: SKIN. WORN. UPPER FUSELAGE SKIN TAIL CONE AREA HAS EVIDENCE OF WEAR AT BS 1800 BETWEEN STR 15L AND 16L. REPAIRED IAW EO C00-5-53-499-07.
- [SDR RYNA200700020](https://openairdocs.org/sdr/RYNA200700020), Nov 21, 2007: FLOORBEAM. CORRODED. PASSENGER CABIN FLOORBEAM IS CORRODED AT BS 1640 BETWEEN LBL 48 AND LBL 58. REPAIRED IAW EO C00-5-53-507-07.
- [SDR RYNA200700021](https://openairdocs.org/sdr/RYNA200700021), Nov 19, 2007: FLOORBEAM. CORRODED. PASSENGER CABIN FLOORBEAM IS CORRODED AT BS 1640 BETWEEN RBL 38 AND RBL 60, WATER LINE 208. REPAIRED IAW EO C00-5-53-502-07.
- [SDR RYNA200700018](https://openairdocs.org/sdr/RYNA200700018), Nov 19, 2007: SKIN. DENTED. FUSELAGE SKIN HAS A OUT OF LIMIT DENT AT BS 431 AND STG 4L. REPAIRED IAW EO C00-5-53-490-07.
- [SDR RYNA200700013](https://openairdocs.org/sdr/RYNA200700013), Nov 19, 2007: SKIN. DENTED. FUSELAGE SKIN HAS A DENT AT BS 1691-1693 & BETWEEN STR 12L - 13L. REPAIRED DENT IAW EO COO-5-53-487-07.
- [SDR RYNA200700009](https://openairdocs.org/sdr/RYNA200700009), Nov 19, 2007: SKIN. DENTED. FUSELAGE SKIN HAS A OUT OF LIMIT DENT AT BS 596 - 603 & BETWEEN STR 27LT AND 27RT. REPAIRED IAW EO C00-5-53-492-07.
- [SDR RYNA200700006](https://openairdocs.org/sdr/RYNA200700006), Nov 19, 2007: SKIN. DAMAGED. UPPER FUSELAGE SKIN HAS "BLEND OUT" AT BS 444.5 & STR 4LT. REPAIRED FUSELAGE SKIN AT BS 444.5 & STR 4LT PER SRM 53-00-01 FIGURE 201 SECTION I & II.
- [SDR RYNA200700011](https://openairdocs.org/sdr/RYNA200700011), Nov 18, 2007: FLOORBEAM. CORRODED. PASSENGER CABIN FLOORBEAM IS CORRODED AT BS 1661 & BETWEEN LBL 45 - RBL 58 & WL 208. REPAIRED IAW EO C00-5-53-494-07.
- [SDR RYNA200700024](https://openairdocs.org/sdr/RYNA200700024), Nov 17, 2007: SKIN. DAMAGED. LOWER FUSELAGE HAS EVIDENCE OF LIGHTNING STRIKE AT BS 1348 AND BETWEEN STR 25L - 26L. REPAIRED FUSELAGE SKIN IAW B757-200 SRM 5I-00-01, REPAIR 4.
- [SDR RYNA200700016](https://openairdocs.org/sdr/RYNA200700016), Nov 13, 2007: SKIN. DENTED. FUSELAGE SKIN HAS A OUT OF LIMIT DENT AT BS 1356 AND BETWEEN STG 25R AND 37R. REPAIRED IAW EO C00-5-53-493-07.
- [SDR RYNA200700017](https://openairdocs.org/sdr/RYNA200700017), Nov 13, 2007: SKIN. DENTED. FUSELAGE SKIN HAS AN OUT OF LIMIT DENT AT BS 1420 AND BETWEEN STG 26R AND 27R. REPAIRED IAW EO C00-5-53-495-07.
- [SDR RYNA200700014](https://openairdocs.org/sdr/RYNA200700014), Nov 13, 2007: SKIN. DENTED. FOUND FUSELAGE SKIN HAS A OUT OF LIMIT DENT AT BS 541-543 AND BETWEEN STG 20R AND 23R. REPAIRED IAW EO C00-5-53-486-07.
- [SDR RYNA200700012](https://openairdocs.org/sdr/RYNA200700012), Nov 13, 2007: SKIN. DENTED. FUSELAGE SKIN HAS A DENT AT BS 620 - 634 & BETWEEN STR 15L - 18L. REPAIRED DENT IAW EO C00-5-53-489-07.
- [SDR RYNA200700010](https://openairdocs.org/sdr/RYNA200700010), Nov 13, 2007: SKIN. DENTED. FUSELAGE SKIN HAS A DENT AT BS 620 - 634 & BETWEEN STR 15L - 16L. REPAIRED IAW EO C00-5-53-489-07.
- [SDR RYNA200700025](https://openairdocs.org/sdr/RYNA200700025), Jan 17, 2007: SKIN. DAMAGED. LOWER FUSELAGE HAS EVIDENCE OF LIGHTNING STRIKE AT BS 1483 AND BETWEEN STR 21R - 22R. REPAIRED FUSELAGE SKIN IAW B757-200 SRM 5I-00-01, REPAIR 6.
- [SDR RYNA200600009](https://openairdocs.org/sdr/RYNA200600009), Sep 15, 2006: SKIN. DAMAGED. EVIDENCE OF LIGHNTING STRIKE AT FS 224.870 (24.5") LBL 14.5. INSTALLED DOUBLER REPAIR AT FS 224.870 AS PER B757 SRM 53-00-01 FIG 201. IAW AVBORNE RES 26449-2, D
- [SDR RYNA200600008](https://openairdocs.org/sdr/RYNA200600008), Sep 15, 2006: SKIN. DAMAGED. EVIDENCE OF LIGHNTING STRIKE AT FS 237.620 (37.25") LBL 17 (37.25"). INSTALLED DOUBLER REPAIR AT FS 237.620 AS PER B757 SRM 53-00-01 FIG 201, IAW AVBORNE RES 26
- [SDR RYNA200600003](https://openairdocs.org/sdr/RYNA200600003), Feb 9, 2006: CIRCUIT CARD. FAULTY. DURING CRUISE, RECEIVED A CABIN ALTITUDE WARNING EICAS MESSAGE . CAPTAIN AND FIRST OFFICER WENT ON OXYGEN, ADVISED ATC, AND BEGAN EMERGENCY DESCENT TO 10000 FT.
- [SDR RYNA200500029](https://openairdocs.org/sdr/RYNA200500029), Sep 16, 2005: LINE. LEAKING. EICAS MESSAGE LEFT HYDRAULIC QUANTITY AND PRESSURE LOST. QUANTITY LEVEL 0.10 LT. REMOVED AND REPLACED RIGHT DOWNLOCK ACTUATOR RETURN LINE. LEAK CHECK GOOD, ALSO
- [SDR RYNA200500015](https://openairdocs.org/sdr/RYNA200500015), Apr 29, 2005: WARNING LIGHT. ILLUMINATED. AFTER TAKEOFF FROM NKW, EXPERIENCED AN APU FIRE WARNING INDICATION WITH ALL FIRE WARNING LIGHTS BUT NO HORN DURING CLIMB. APU WAS SHUTDOWN BEFORE TAXI. CREW FOL
- [SDR RYNA200500012](https://openairdocs.org/sdr/RYNA200500012), Apr 8, 2005: TRANSMITTER. INOPERATIVE. DURING CLIMB-OUT ABOVE 14,000, THE CREW NOTICED AN ABNORMAL SPLIT IN ENGINE PARAMETERS WITH THRUST LEVERS MATCHED UP. WHEN TRYING TO MATCH EPR, THERE WAS A HUGE
- [SDR RYNA200500013](https://openairdocs.org/sdr/RYNA200500013), Apr 8, 2005: TUBE. CRACKED. DURING CLIMB FROM ORD, THE NR 2 ENGINE N1 WAS INDICATING .16 LOWER THAN THE NR 1 ENGINE. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REMOVED AND R

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other DJI PHANTOM 3 PROFESSION aircraft: https://openairdocs.org/model/dji-phantom-3-profession/aircraft.md

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