# N911VV: DJI INSPIRE 1

- Status: Valid registration
- Airframe: [DJI INSPIRE 1](https://openairdocs.org/model/dji-inspire-1) (registry code 061008I)
- Serial number: W13DCB06020187
- Type: Rotorcraft
- Engine type: Electric
- Certificate issued: August 19, 2015
- Expires: August 31, 2028
- Mode S code: AC9C51
- Registered owner: [Weaver Cliff A](https://openairdocs.org/faa-owner/WEAVER%20CLIFF%20A)
- Location: [Evansville, IN](https://openairdocs.org/faa-place/IN/Evansville)
- Owner type: Individual
- Owner's area on the map: 37.9725° N, 87.4797° W: Placed by OpenAirDocs at the center of ZIP code 47715, 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=911VV
- Page: https://openairdocs.org/aircraft/N911VV

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 INSPIRE 1)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N911VV.

## FAA accident and incident reports

None matched to N911VV.

## Reports on N911VV not matched to an aircraft (1)

They name N911VV, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19940730030809I](https://openairdocs.org/incident/19940730030809I), Jul 30, 1994: Doug DC932 (N911VV), Montgomery, AL. Narrative: suspected galley fire. Electrical in nature. Later determined to be an electrical short in coffee maker.

## 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 N911VV not matched to an aircraft (23)

They name N911VV, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR VJ9800514](https://openairdocs.org/sdr/VJ9800514), Sep 28, 1998: SKIN. CHAFED. VERTICAL SKIN ON LT AND RT UPPER AND LOWER BANANA FAIRING CHAFED. RT UPPER BANANA FAIRING SKIN CHAFED OUT OF LIMIT IAW DC9 SRM 55-01. REMOVED SKIN, FABRICATED A
- [SDR VJ9800445](https://openairdocs.org/sdr/VJ9800445), Sep 25, 1998: SKIN. GOUGED. GOUGE IN FUSELAGE SKIN AT FS 967, L21-22R, BEYOND LIMIT IAW DC9 SRM 53-04, FIG 8. BLENDED AREA, FABRICATED AND INSTALLED DOUBLER REPAIR IAW DC9 SRM 51-10-3, 53-
- [SDR VJ9800482](https://openairdocs.org/sdr/VJ9800482), Sep 23, 1998: SPAR. MAGNETIZED. REPAIR ON AFT SIDE REAR SPAR LWR CAP XRS 525 DETERMINED TO BE MAGNETIC WITHIN 5 FEET FLUX VALVE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-3, 51
- [SDR VJ9800513](https://openairdocs.org/sdr/VJ9800513), Sep 20, 1998: TAB. CORRODED. RT ELEVATOR GEAR TAB HAS 1 INCH DIAMETER CORROSION SPOT. CUT OUT CORROSION, CLEANED AREA, FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 51-70-2.
- [SDR VJ9800538](https://openairdocs.org/sdr/VJ9800538), Sep 19, 1998: FITTING. CORRODED. AFT CABIN FLOORBEAM AT FS 996 RIGHT SIDE FITTING CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-5, 51-10-4, 51-10-3 AND 53-01 FIG 1.
- [SDR VJ9800547](https://openairdocs.org/sdr/VJ9800547), Sep 17, 1998: PANEL. LIGHTNING STRIKE. LIGHTNING STRIKE LT WINDOW PANEL AT 465 TO 484. REMOVED PANEL, CUT OUT SECTION, FABRICATED DOUBLERS AND FILLERS PLUS TWO INTERNAL DOUBLERS. INSTALLED REPAIR PAR
- [SDR VJ9800512](https://openairdocs.org/sdr/VJ9800512), Sep 17, 1998: WINDOW  PANEL. LIGHTNING STRIKE. RT WINDOW PANE HAS LIGHTNING STRIKE OUT OF LIMIT AT FS 813 TO 869. REPLACED WINDOW PANEL IAW DC9 SRM 51-30-2, 51-10-4, 51-10-3 AND 53-05, FIG 111.
- [SDR VJ9800479](https://openairdocs.org/sdr/VJ9800479), Sep 17, 1998: SPAR. CORRODED. RT WING LOWER REAR SPAR XW 530 VERTICAL LEG CORRODED. FABRICATED, INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-30-1, 51-10-4, 53-22-1, AND AIRTRAN RES 981582.
- [SDR VJ9800548](https://openairdocs.org/sdr/VJ9800548), Sep 16, 1998: BULKHEAD DOUBLER. CORRODED. UPPER RT DOUBLER AT BULKHEAD WEB FS 996 CORRODED. REMOVED CORRODED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER IAW DC9 SRM 51-10-3, 51-10-2 AND 53-02 FIG 2.
- [SDR VJ9800444](https://openairdocs.org/sdr/VJ9800444), Sep 15, 1998: SKIN. GOUGED. SKIN AT FS 962, L25R, GOUGED BEYOND LIMIT IAW DC9 SRM 53-04, FIG 38. CUT OUT GOUGE, FABRICATED AND INSTALLED EXTERNAL AND FINGER DOUBLERS IAW DC9 SRM 53-04, FIG
- [SDR VJ9800549](https://openairdocs.org/sdr/VJ9800549), Sep 12, 1998: SKIN. CORRODED. FUSELAGE SKIN AT FS 579, L30, CORRODED. CUT OUT SECTION OF SKIN, FABRICATED AND INSTALLED EXTERNAL DOUBLER AND FINGER DOUBLERS IAW DC9 SRM 53-04 FIG 12B, 51-10-
- [SDR VJ9800478](https://openairdocs.org/sdr/VJ9800478), Sep 12, 1998: FRAME. CRACKED. MAIN FRAME RT FS 966 CRACKED. REPLACED FRAME IAW AIRTRAN EO 12-5311-29-B1044 AND RES 981533.
- [SDR VJ9800551](https://openairdocs.org/sdr/VJ9800551), Sep 11, 1998: FLOORBEAM. CORRODED. AFT RT LAV FLOORBEAM AT FS 996 CORRODED FROM FUSELAGE TO LAV ENTRANCE. REMOVED RT CABLE RUN AND RT O/B PULLEY TOWER. CUT OUT CORRODED SECTION, TREATED AREA, FAB
- [SDR VJ9800550](https://openairdocs.org/sdr/VJ9800550), Sep 11, 1998: Z SECTION. CORRODED. AFT CABIN CENTER Z SECTION AT FS 945, RBL 2-20 AND LBL 2-20, CORRODED FROM BULKHEAD TO BULKHEAD. CORROSION OUT OF LIMIT IAW DC9 SRM 53-01, FIG 1. BROKE CABLE TE
- [SDR VJ9800554](https://openairdocs.org/sdr/VJ9800554), Sep 10, 1998: SKIN. DENTED. THE AFT VENTRAL STAIRS CONTAINED 27 DENTS TOO CLOSE TOGETHER IAW DC9 SRM 51-50-1, FIG 1-2A. REPLACED LOWER SKIN AND CORRODED FITTING IAW DC9 SRM 51-30-5, 51-30-
- [SDR VJ9800553](https://openairdocs.org/sdr/VJ9800553), Sep 10, 1998: FLOOR. CORRODED. AFT GALLEY FLOOR PANEL CORRODED. REMOVED FLOOR PANEL, FABRICATED AND INSTALLED NEW HAT SECTIONS AND FLOOR PANEL IAW DC9 SRM 51-20-0, 51-30-2, 53-21-0, FIG 4 AND
- [SDR VJ9800552](https://openairdocs.org/sdr/VJ9800552), Sep 10, 1998: LONGERON. CORRODED. FORWARD PIT UNDER AUX TANK AT FS 579, L30, CORRODED. REPLACED L30 AT FS 579 IAW DC9 SRM 53-02 FIG 14.
- [SDR VJ9800511](https://openairdocs.org/sdr/VJ9800511), Sep 10, 1998: SKIN. CORRODED. AFT VENTRAL STAIRS HAD DENTS TOO CLOSE TOGETHER IAW DC9 SRM 51-50-1, FIG 1-2A. REPLACED LOWER SKIN AND CORRODED FITTING IAW DC9 SRM 51-30-5, 51-30-0, 51-10-4 AN
- [SDR VJ9800555](https://openairdocs.org/sdr/VJ9800555), Sep 9, 1998: SEAT TRACK. CORRODED. FOUND CORROSION AROUND FASTENER HOLES ON SEAT TRACK AT FS 917 TO 996 LT. REPLACED SEAT TRACK IAW DC9 SRM 53-01 FIG 1, 51-10-4, 51-30-1 AND 51-10-3.
- [SDR 96ZZZM998](https://openairdocs.org/sdr/96ZZZM998), Apr 22, 1996: OXYGEN LINE. LOOSE. ON FLT 230 - DFW-ATL - THE CABIN OXYGEN SYSTEM MANUALLY SURGED, OXYGEN MASKS DOORS DID NOT OPEN. CONNECTED SUPPLY LINE TO AFT FLIGHT ATTENDANT PSU AND OPERATED 
- [SDR 96ZZZM997](https://openairdocs.org/sdr/96ZZZM997), Apr 22, 1996: CONTROLLER. MALFUNCTIONED. ON FLT 230 - DFW-ATL - THE CABIN ALTITUDE ROSE TO 12000 FEET AND WAS UNCONTROLLABLE AT FLIGHT LEVEL 330 FEET, INITIATED EMERGENCY DESCENT. THE FLIGHT HAD BEEN I
- [SDR 96ZZZM822](https://openairdocs.org/sdr/96ZZZM822), Apr 2, 1996: CSD. MALFUNCTIONED. FLT 520 - ATL-ATL, AIR RETURN FOR MTC CONVENIENCE, THE RIGHT CSD ROSE INTO THE CAUTION RANGE, APPROACHING THE RED LINE. LEFT GENERATOR PREVIOUSLY ON MEL. CLEARE
- [SDR 95ZZZX4173](https://openairdocs.org/sdr/95ZZZX4173), Jul 18, 1995: COFFEE MAKER. OVERHEATING. ATL - FLT 166 - SMOKE IN COCKPIT ON APPROACH TO ATL. FOUND TO BE FORWARD GALLEY COFFEE MAKER OVERHEATING. REMOVED COFFEE MAKER AND PLACED ON MEL.

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other DJI INSPIRE 1 aircraft: https://openairdocs.org/model/dji-inspire-1/aircraft.md

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