# N768QT: DJI PHANTOM 2 VISION +

- Status: Valid registration
- Airframe: [DJI PHANTOM 2 VISION +](https://openairdocs.org/model/dji-phantom-2-vision-plus) (registry code 061004I)
- Serial number: PH645490714
- Type: Rotorcraft
- Engine type: Electric
- Certificate issued: July 25, 2016
- Expires: July 31, 2029
- Mode S code: AA60B0
- Registered owner: [Truman State University](https://openairdocs.org/faa-owner/TRUMAN%20STATE%20UNIVERSITY)
- Location: [Kirksville, MO](https://openairdocs.org/faa-place/MO/Kirksville)
- Owner type: Corporation
- Owner's area on the map: 40.1663° N, 92.5912° W: Placed by OpenAirDocs at the center of ZIP code 63501, 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=768QT
- Page: https://openairdocs.org/aircraft/N768QT

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 2 VISION +)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N768QT.

## FAA accident and incident reports

None matched to N768QT.

## 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 N768QT not matched to an aircraft (66, newest 50)

They name N768QT, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 2DYA20140518002](https://openairdocs.org/sdr/2DYA20140518002), May 16, 2014: PROXIMITY SWITCH. FAULTY. AFTER FLAP RETRACTION, FLAP NEEDLES JUMPED BETWEEN 0 & 1. EICAS MSG LE SLAT ASYMMETRICAL & LE ANNUNCIATOR ILLUMINATED. DURING PSEU BITE IAW BFIM 32-09-03, FOUND
- [SDR 2DYA20140518001](https://openairdocs.org/sdr/2DYA20140518001), May 16, 2014: WARNING SYSTEM. FALSE ACTIVATION. FLAP & SLAT RETRACTION FROM F1 TO 0 SETTING EICAS MSG LE SLAT ASYMMETRICAL. TROUBLESHOOTING IAW BFIM 27-81 FAULT TREE 808 REVEALED NO FAULTS.
- [SDR 2012F00080](https://openairdocs.org/sdr/2012F00080), May 5, 2012: VALVE. OPEN. DURING CRUISE, WITH EQUIPMENT COOLING SWITCH IN STANBY, EICAS MESSAGE " FWD EQPT OVHT" DISPLAYED AND OVERHEAT LIGHT ILLUMINATING. IAW AMM TASK CARD 21-58-29-004
- [SDR TAMF2011FA0000166](https://openairdocs.org/sdr/TAMF2011FA0000166), Oct 4, 2011: ELECTRONIC UNIT. MALFUNCTIONED. AFTER ACFT ROTATION EICAS DISPLAYED L/E SLAT DISAGREE WITH THE FLAP LEVER IN 5. OVERWEIGHT LANDING, 1000KG LW 1293 KG NO HARD LANDING. HARD LANDING INSPECTION W
- [SDR TAMF2011FA0000164](https://openairdocs.org/sdr/TAMF2011FA0000164), Sep 30, 2011: WARNING LIGHT. ILLUMINATED. DURING CLIMB, EICAS MESSAGE L/E SLAT ASSYM DISPLAYED L/E LIGHT ILLUMINATED WITH FLAP LEVER IN 1. BOTH FLAP POINTERS WERE CORRECT. AIR TURN BACK, AN OVERWEIGHT L
- [SDR TAMF2011FA0000162](https://openairdocs.org/sdr/TAMF2011FA0000162), Jul 11, 2011: ROTARY ACTUATOR. CORRODED. DURING WALK AROUND ON ACFT, FOUND AT LT WING NR 5 SLAT HANGING DOWN FROM ONE SIDE. THE SLAT REMAINED SUPPORTED FROM ONE TRACK WHICH CAUSED HOLES OF SOME PANELS 
- [SDR TAMF2011FA0000161](https://openairdocs.org/sdr/TAMF2011FA0000161), May 31, 2011: ROTARY ACTUATOR. CORRODED. DURING CLIMBING STAGE L/E SLAT ASSY APPEARS. AIR TURNBACK. GROUND INSP FINDINGS: DURING VISUAL INSP WAS FOUND SLAT NR 12 HANGING DOWN FROM ONE SIDE. THE SLAT RE
- [SDR TAMF20100062S](https://openairdocs.org/sdr/TAMF20100062S), Aug 15, 2010: SKIN. CORRODED. DURING SVC C4, FOUND CORROSION ON LWR SKIN BETWEEN RIB 19, WS 668.2 AND RIB 23 WS 772.2 AFTER BLENDING REMAINING THICKNESS WAS FOUND OUT OF LIMITS, REPAIR WAS P
- [SDR TAMF20100061S](https://openairdocs.org/sdr/TAMF20100061S), Aug 15, 2010: RIB. CORRODED. DURING SVC C4, FOUND CORROSION ON RT INBD FLAP RIB ASSY AT HOLE (LODGING ON TORQUE TUBE) STA IFS 108.5 RIBS PN 113T2237-2/14, REPAIR ACCOMPLISHED IAW EWO 767-57
- [SDR TAMF20100060S](https://openairdocs.org/sdr/TAMF20100060S), Aug 15, 2010: SPAR. DAMAGED. DURING SVC C4, FOUND RT WING FRONT SPAR BETWEEN RIB 32 TO 31 WITH A HOLE, REPAIR WAS ACCOMPLISHED IAW EWO 767-57-066 AND SR 1-1660377939.
- [SDR TAMF20100059S](https://openairdocs.org/sdr/TAMF20100059S), Aug 15, 2010: SEAT TRACK. CORRODED. DURING SVC C4, FOUND CORROSION ON TRACKS RBL 11.00 BETWEEN STA 478-588. REPAIR ACCOMPLISHED IAW EWO 767-53-115 AND EO TAC-100823.
- [SDR TAMF20100058S](https://openairdocs.org/sdr/TAMF20100058S), Aug 15, 2010: SEAT TRACK. CORRODED. DURING SVC C4, FOUND CORROSION ON TRACKS LBL 54.75 STA 566-663.45, REPAIR ACCOMPLISHED WITH EWO 767-53-0114 AND EO TAC-100824
- [SDR TAMF20100057S](https://openairdocs.org/sdr/TAMF20100057S), Aug 15, 2010: CARGO TRACK. CORRODED. DURING SVC C4, MAIN DECK CARGO TRACKS RBL 33.00, STA 1480-1605 WAS FOUND WITH CORROSION, REPAIR ACCOMPLISHED IAW EWO 767-53-113 AND IAAC PARTS EO TAC-100824.
- [SDR TAMF20100056S](https://openairdocs.org/sdr/TAMF20100056S), Aug 15, 2010: LATCH. CORRODED. DURING SVC C4, WAS FOUND CORROSION ON LATCH FITTING PN 368-53-00-95345 (12 POSITION) MAIN CARGO DOOR, REPAIR ACCOMPLISHED IAW EWO 767-53-112 AND IAI DOC CS-2380
- [SDR TAMF20100055S](https://openairdocs.org/sdr/TAMF20100055S), Aug 15, 2010: CARGO TRACK. CORRODED. DURING SVC C4, FOUND MAIN DECK CARGO TRACKS BETWEEN STA RBL 54.75 TO 1605.5 AND BETWEEN 1518-1605 HAS CORROSION.
- [SDR TAMF20100054S](https://openairdocs.org/sdr/TAMF20100054S), Aug 15, 2010: SKIN. CORRODED. DURING SVC C4, FOUND ON FUSELAGE EXTERIOR SKIN STA 742, STR 33L-34L AFTER BLENDING CORROSION OUT OF LIMITS, REPAIR WAS ACCOMPLISHED IAW EWO 767-53-110R1 AND SR 
- [SDR TAMF20100053S](https://openairdocs.org/sdr/TAMF20100053S), Aug 15, 2010: FRAME. BENT. DURING SVC C4, FOUND NOSE RADOME 7 O'CLOCK, 10 O'CLOCK, 12 O'CLOCK AND 1 O'CLOCK FRAME HAS BEND. REPAIR WAS ACCOMPLISHED IAW EWO 767-53-109 AND SR 1-1660613312.
- [SDR TAMF20100052S](https://openairdocs.org/sdr/TAMF20100052S), Aug 15, 2010: KEELBEAM. CORRODED. DURING SVC C4, FOUND KEELBEAM HORIZ WEB, BS 1000 TO BS 1010 HAS CORROSION, REPAIR WAS ACCOMPLISHED IAW EWO 767-53-108R1 AND SR 1-1660618916.
- [SDR TAMF20100051S](https://openairdocs.org/sdr/TAMF20100051S), Aug 15, 2010: KEELBEAM. CORRODED. DURING SVC C4, FOUND KEELBEAM, BS 1070, LT MID SECTION CHORD HAS CORROSION, REPAIR WAS ACCOMPLISHED IAW EWO 767-53-106R1 AND SR 1-1657143102.
- [SDR TAMF20100050S](https://openairdocs.org/sdr/TAMF20100050S), Aug 15, 2010: SKIN. DENTED. DURING SVC C4, FOUND 2 DENTS ON EXTERNAL SKIN FWD LARGE CARGO DOOR STA 533.60-542.4 BETWEEN INTERCOSTAL PLANE 3-4, REPAIR WAS ACCOMPLISHED IAW EWO 767-52-23R1 A
- [SDR TAMF20100049S](https://openairdocs.org/sdr/TAMF20100049S), Aug 15, 2010: SKIN. DAMAGED. DURING SVC C4, FOUND AT FWD CARGO COMPARTMENT DOOR, INNER SKIN, AFT SIDE FLANGE HOLE BEND, REPAIR WAS ACCOMPLISHED UNDER EWO 767-52-022 AND SR 1-1665185720.
- [SDR 2009FA0000724](https://openairdocs.org/sdr/2009FA0000724), Aug 16, 2009: ENGINE. AUTO SHUTDOWN. DURING CRUISE LEVEL AT FL 360, 65 NM MILES SOUTH OF INTERSECTION, THE RT ENG OIL FILTER EICAS ANNUNCIATION DISPLAYED. ACCORDING TO CHECK LIST, REDUCED THRUST TO
- [SDR TAMF20090027S](https://openairdocs.org/sdr/TAMF20090027S), Mar 23, 2009: SILL. CORRODED. DURING C3 CHECK INSPECTION, FOUND FWD CARGO DOOR SURROUND STRUCTURE LOWER SILL BETWEEN STA 500 TO STA 610 LATCH FITTINGS WITH CORROSION. REPAIR ACCOMPLISHED IAW
- [SDR TAMF20090019S](https://openairdocs.org/sdr/TAMF20090019S), Mar 23, 2009: SKIN. CORRODED. DURING C3 CHECK FOUND CORROSION ON SKIN COMMON TO ATC ANTENNA, STA 448 STRINGER 39R/39L. REPAIR ACCOMPLISHED IAW EWO 767 53-088 AND BOEING SR 1-1249400131.
- [SDR TAMF20090024S](https://openairdocs.org/sdr/TAMF20090024S), Mar 22, 2009: SKIN. CORRODED. DURING C3 CHECK INSPECTION WAS FOUND CORROSION ON WING LOWER SKIN STA WS 694.2 WITH REAR SPAR, LT. REPAIR ACCOMPLISHED IAW EWO 767 57-053 AND BOEING SR 1-125134
- [SDR TAMF20090026S](https://openairdocs.org/sdr/TAMF20090026S), Mar 21, 2009: SKIN. CORRODED. DURING C3 CHECK INSPECTION, FOUND RT WING OTBD T/E FLAP LWR SURFACE AT STA OTEF 119 AND BETWEEN STA OTEF 265.69 TO OTEF 371.88 HAS CORROSION. REPAIR ACCOMPLISHE
- [SDR TAMF20090025S](https://openairdocs.org/sdr/TAMF20090025S), Mar 20, 2009: FRAME. CRACKED. DURING C3 CHECK INSPECTION WAS FOUND A CRACK ON NR 2 ENGINE CORE COWL FRAME STA NAC 303.75. REPAIR ACCOMPLISHED IAW EWO 54-055 AND CV09-0833-04.
- [SDR TAMF20090023S](https://openairdocs.org/sdr/TAMF20090023S), Mar 20, 2009: FRAME. CRACKED. DURING C3 CHECK INSPECTION WAS FOUND A CRACK ON NR 2 ENGINE CORE COWL FRAME STA NAC 303.75. REPAIR ACCOMPLISHED IAW EWO 54-054 AND CV09-0811-02.
- [SDR TAMF20090022S](https://openairdocs.org/sdr/TAMF20090022S), Mar 20, 2009: FRAME. CRACKED. DURING C3 CHECK INSPECTION WAS FOUND A CRACK ON NR 1 ENGINE CORE COWL FRAME STA NAC 303.75. REPAIR ACCOMPLISHED IAW EWO 767 54-087 AND ROHR CV09-0810-03.
- [SDR TAMF20090020S](https://openairdocs.org/sdr/TAMF20090020S), Mar 20, 2009: DOOR. CORRODED. DURING C3 CHECKS INSPECTION WAS FOUND A CORROSION ON FWD CARGO DOOR EXTERNAL REPAIR DOUBLER STA 606 - 617 INTERCOSTAL PLANE 7. REPAIR ACCOMPLISHED IAW EWO 767 5
- [SDR TAMF20070033S](https://openairdocs.org/sdr/TAMF20070033S), Aug 29, 2007: SKIN. DENTED. DURING INSPECTION OF (C2) CHECK WAS FOUND A DENT A/Y=25 ON SKIN STA 1307-1329 STR 32-33 - LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-052 AND SRM 53-00-01 REPA
- [SDR TAMF20070024S](https://openairdocs.org/sdr/TAMF20070024S), Aug 28, 2007: SPAR. DAMAGED. DURING C CHECK INSPECTION (TASK CARD 57-650-00) WAS FOUND LOOSE MATERIAL ON SPLICE PLATE AT FRONT SPAR STA ISS 864.92 873.13 RT. DAMAGED AREA WAS REPAIRED IAW E
- [SDR TAMF20070037S](https://openairdocs.org/sdr/TAMF20070037S), Aug 27, 2007: STRAP. CORRODED. DURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON CARGO DOOR SURROUND STRUCTURE, SAFE FAIL STRAP P/N 146T8048-3. REMOVED, FABRICATED AND INSTALLED A NEW 
- [SDR TAMF20070025S](https://openairdocs.org/sdr/TAMF20070025S), Aug 27, 2007: SPAR. DAMAGED. DURING C CHECK INSPECTION (TASK CARD 06-102-01-1) WAS FOUND A LOOSE MATERIAL ON SPLICE PLATE AT FRONT SPAR STA ISS 1009 - 1017 LT. DAMAGED AREA WAS REPAIRED IAW
- [SDR TAMF20070036S](https://openairdocs.org/sdr/TAMF20070036S), Aug 26, 2007: SKIN. CORRODED. DURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON PRESSURE SKIN STA 582 BETWEEN STRINGER 34-35 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-058 AND SERVI
- [SDR TAMF20070035S](https://openairdocs.org/sdr/TAMF20070035S), Aug 26, 2007: SILL. CORRODED. DURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON CARGO DOOR SURROUND STRUCTURE, MAIN SILL, OUTER CHORD STA 569.65 RT. DAMAGED AREA WAS REPAIRED IAW EWO 
- [SDR TAMF20070034S](https://openairdocs.org/sdr/TAMF20070034S), Aug 26, 2007: SILL. CORRODED. DURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON CARGO DOOR SURROUND STRUCTURE, MAIN SILL, OUTER CHORD STA 632 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767
- [SDR TAMF20070017S](https://openairdocs.org/sdr/TAMF20070017S), Aug 26, 2007: BEAM. CRACKED. DURING C-CHECKS INSPECTION WAS FOUND A CRACK ON FIXED LEADING EDGE NOSE BEAM WEB STA OSS 644.58-694.55 - RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-025 AND SR
- [SDR TAMF20070032S](https://openairdocs.org/sdr/TAMF20070032S), Aug 25, 2007: SKIN. CHAFED. DURING INSPECTION OF (C) CHECK WAS FOUND A WEAR ON RUB STRIPS SKIN STA 1725.50 STRINGER 22 - RT/LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-054 AND MFG SERVICE
- [SDR TAMF20070031S](https://openairdocs.org/sdr/TAMF20070031S), Aug 25, 2007: SKIN. WRINKLED. DURING (C) CHECKS INSPECTION WAS FOUND AN EXISTING REPAIR WRINKLED ON LEADING EDGE SLAT NR 2 UPPER SKIN. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-029 AND MFG SE
- [SDR TAMF20070029S](https://openairdocs.org/sdr/TAMF20070029S), Aug 25, 2007: SILL. CORRODED. FWD CARGO COMPARTMENT LOWER MAIN SILL, THE UPPER EXTERIOR EXTRUDED SECTION HAS CORROSION AT STA 610. REMOVED AND REPLACED MAIN SILL IN FWD CARGO COMPARTMENT UPP
- [SDR TAMF20070028S](https://openairdocs.org/sdr/TAMF20070028S), Aug 25, 2007: SKIN. DENTED. DURING INSPECTION OF (C2) CHECK WERE FOUND SEVERAL DENTS ON FUSELAGE SKIN STA 1417-1436 STRINGER 33 -36-LT. DAMAGED AREAS WERE REPAIRED IAW EWO 767-53-055 AND S
- [SDR TAMF20070023S](https://openairdocs.org/sdr/TAMF20070023S), Aug 25, 2007: COWLING. DAMAGED. DURING C CHECK INSPECTION WAS FOUND CORE COWL P/N: 224-2301-513 S/N: 0130 WITH ELONGATED HOLE AT FRAME STA NAC 294 - CF6-80C2. DAMAGED AREA WAS REPAIRED IAW CV0
- [SDR TAMF20070020S](https://openairdocs.org/sdr/TAMF20070020S), Aug 25, 2007: RIB. CHAFED. DURING C-CHECK INSPECTION WAS FOUND A WEAR OUT OF LIMITS ON IB AILERON RT - OB CLOSURE RIB WEB.DAMAGED AREA WAS REPAIRED IAW EWO 767 57-026 AND SERVICE REQUEST 
- [SDR TAMF20070019S](https://openairdocs.org/sdr/TAMF20070019S), Aug 25, 2007: SKIN. DENTED. DURING INSPECTION OF (C2) CHECK WAS FOUND A DENT A/Y=40 ON LAP SKIN STA 1536 STR 36 - LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-049 AND SRM 53-00-01 REPAIR 1
- [SDR TAMF20070018S](https://openairdocs.org/sdr/TAMF20070018S), Aug 25, 2007: SKIN. DENTED. DURING INSPECTION OF (C2) CHECK WAS FOUND A DENT A/Y=20 ON FUSELAGE SKIN AT STA 1506, STR 31-32 -LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-048 AND SRM 53-00-
- [SDR TAMF20070015S](https://openairdocs.org/sdr/TAMF20070015S), Aug 25, 2007: SKIN. DENTED. DURING INSPECTION OF (C2) CHECK WAS FOUND A DENT OVER REPAIR DOUBLER AT SKIN STA 676-698 STRINGER 37-38 - RT. THE DOUBLER NEEDS TO BE REPLACE. DAMAGED AREA WAS 
- [SDR TAMF20070030S](https://openairdocs.org/sdr/TAMF20070030S), Aug 24, 2007: FAIRING. CORRODED. DURING C CHECK INSPECTION WAS FOUND A CORROSION ON HORIZONTAL STABILIZER TIP LT NOSE IB - LT.DAMAGED AREA WAS REPAIRED IAW EWO 767-57-030 AND MFG SERVICE REQUES
- [SDR TAMF20070022S](https://openairdocs.org/sdr/TAMF20070022S), Aug 22, 2007: SKIN. DENTED. DURING INSPECTION OF C2 CHECK WAS FOUND A DENT ON LAP SKIN STA 212.5, STR 30-RT. DENT ON LIMITS IAW EWO 767-53-051 AND MFG SERVICE REQUEST 1-526586182. FAA FORM
- [SDR TAMF20070021S](https://openairdocs.org/sdr/TAMF20070021S), Aug 22, 2007: SKIN. DENTED. DURING INSPECTION OF (C2) CHECK WAS FOUND A DENT ON LAP SKIN STA 1339 STR 17 - LT. DAMAGE ON LIMITS IAW EWO 767-53-05 AND BOEING SERVICE REQUEST 1-526586182. FA

All 66: https://openairdocs.org/aircraft/N768QT/unmatched-reports.md

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other DJI PHANTOM 2 VISION + aircraft: https://openairdocs.org/model/dji-phantom-2-vision-plus/aircraft.md

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