# N588AA: DJI PHANTOM 4

- Status: Valid registration
- Airframe: [DJI PHANTOM 4](https://openairdocs.org/model/dji-phantom-4) (registry code 06101UI)
- Serial number: 07DDD5J0A10223
- Type: Rotorcraft
- Engine type: Electric
- Certificate issued: February 10, 2017
- Expires: February 28, 2027
- Mode S code: A793A1
- Registered owner: [Green Mountain Power Corp](https://openairdocs.org/faa-owner/GREEN%20MOUNTAIN%20POWER%20CORP)
- Location: [Rutland, VT](https://openairdocs.org/faa-place/VT/Rutland)
- Owner type: Corporation
- Owner's area on the map: 43.6246° N, 72.9102° W: Placed by OpenAirDocs at the center of ZIP code 05701, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=588AA
- Page: https://openairdocs.org/aircraft/N588AA

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 4)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N588AA.

## FAA accident and incident reports

None matched to N588AA.

## 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 N588AA not matched to an aircraft (68, newest 50)

They name N588AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR AALA20120419023](https://openairdocs.org/sdr/AALA20120419023), Apr 19, 2012: SKIN. CRACKED. FUSELAGE CRACKED AT FASTENER ABOVE PYLON AT STATION 1380 ABOVE LONGERON 14 LEFT. INSTALLED DOUBLER AND FILLER PER SRM 53-01-00 AND AARD 53-30-00-02.
- [SDR AALA20120419022](https://openairdocs.org/sdr/AALA20120419022), Apr 19, 2012: SKIN. CRACKED. FUSELAGE SKIN IS CRACKED AT 2 EACH RIVETS IN THE SHEAR TIE AT STATION 1380 LONGERON 14 RIGHT ABOVE THE ENGINE PYLON. INSTALLED DOUBLER AND FILLER PER SRM 53-01-
- [SDR AALA20120119TUL14](https://openairdocs.org/sdr/AALA20120119TUL14), Jan 19, 2012: SKIN. DAMAGED. DAMAGE TO EXTERIOR SKIN STATION 583 LONGERON 18 LEFT. INSTALLED REPAIR DOUBLER PER SRM 53-04-07.
- [SDR AALA20110522DFW05](https://openairdocs.org/sdr/AALA20110522DFW05), May 20, 2011: CONNECTOR. DEFECTIVE. SEAT MOUNTED EMERGENCY LIGHT AT 14D INOPERATIVE. REMOVED AND REPLACED SIDEWALL TO SEAT CONNECTOR AT 14DEF. OPS CHECK NORMAL.
- [SDR AALA20110110DFW01](https://openairdocs.org/sdr/AALA20110110DFW01), Jan 10, 2011: PISTON. DEFECTIVE. DFW - CREW REPORTED AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT AND CABIN PRESSURIZATION WENT INTO STANDBY. EMERGENCY DECLARED LANDED DFW WITHOUT INCIDENT. REPLAC
- [SDR AALA20100408LAX01](https://openairdocs.org/sdr/AALA20100408LAX01), Apr 7, 2010: ADC. MALFUNCTIONED. LAX - CREW REPORTED AFTER TAKEOFF THE AUTOPILOT AUTOTHROTTLES DISENGAGED AND THE CAPTAINS FLIGHT MANAGEMENT ANNUNCIATOR/ALTIMETER WENT BLANK. EMERGENCY DECLARED
- [SDR AALA20090814TUL03](https://openairdocs.org/sdr/AALA20090814TUL03), Aug 13, 2009: FRAME. CRACKED. FRAME STATION 1446 OUTBOARD OF LONGERON 2L IS CRACKED. REPAIRED FRAME UNDER EA MD80-53-007119 AND SRM 53-03-00.
- [SDR AALA20090814TUL10](https://openairdocs.org/sdr/AALA20090814TUL10), Aug 11, 2009: SHEAR TIE. CRACKED. SHEAR TIE IS CRACKED L1-L2L. REPLACED SHEAR TIE UNDER SRM 51-30-05.
- [SDR AALA20090811TUL23](https://openairdocs.org/sdr/AALA20090811TUL23), Aug 8, 2009: FRAME. CRACKED. FRAME IS CRACKED AT STATION 1418 LONGERON 2R AND LONGERON 2L. INSTALLED REPAIR UNDER EA MD80-53-007027 AND SRM 53-03 FIGURE 31A.
- [SDR AALA20090811TUL21](https://openairdocs.org/sdr/AALA20090811TUL21), Aug 8, 2009: LONGERON. CRACKED. LONGERON 2R IS CRACKED AT STATION 1418 APPROXIMATELY .75 INCHES LONG. REPLACED SECTION ON LONGERON 2R UNDER AARD 53-30-002.
- [SDR AALA20090811TUL17](https://openairdocs.org/sdr/AALA20090811TUL17), Aug 8, 2009: MOUNT. CORRODED. GALLEY NUMBER TWO INBOARD FORWARD TIE DOWN FITTING HAS CORROSION. INSTALLED NEW GALLEY MOUNT UNDER SRM 51-30.
- [SDR AALA20090811TUL14](https://openairdocs.org/sdr/AALA20090811TUL14), Aug 8, 2009: SHEAR TIE. CRACKED. SHEAR TIE CRACKED AT STATION 1451 FROM STRINGER L1L TO L2L. REPLACED SHEAR TIE UNDER AARD 51-00-00-12.
- [SDR AALA20090811TUL15](https://openairdocs.org/sdr/AALA20090811TUL15), Aug 7, 2009: SPLICE. CORRODED. LEFT TRACK SPLICE HAS CORROSION. INSTALLED NEW TRACK SPLICE UNDER SRM 51-30-05.
- [SDR AALA20090811TUL20](https://openairdocs.org/sdr/AALA20090811TUL20), Aug 7, 2009: CUSP WEB. CORRODED. CUSP CORROSION AT STATION 200 RIGHT BUTTLINE 10. INSTALLED DOUBLER UNDER AARD 53-20-00-16.
- [SDR AALA20090821TUL08](https://openairdocs.org/sdr/AALA20090821TUL08), Aug 6, 2009: BEAM. CORRODED. AFT CARGO DOOR BEAM CORRODED. INSTALLED DOUBLER REPAIR UNDER AARD 53-10-00-3
- [SDR AALA20090811TUL07](https://openairdocs.org/sdr/AALA20090811TUL07), Aug 6, 2009: CARGO TRACK. CORRODED. RIGHT AFT TIE DOWN TRACK HAS CORROSION BETWEEN STATION 1212-1320 OUT OF LIMITS. INSTALLED NEW TIE DOWN TRACK UNDER AARD 51-00-00-012.
- [SDR AALA20090811TUL02](https://openairdocs.org/sdr/AALA20090811TUL02), Aug 6, 2009: FLOOR SUPPORT. CORRODED. REMOVED FLOORBOARD SUPPORT AT RIGHT BUTTLINE 8. FOUND FLANGE CORRODED BEYOND LIMITS. INSTALLED NEW FLOORBOARD SUPPORT UNDER SRM 51-01.
- [SDR AALA20090806TUL02](https://openairdocs.org/sdr/AALA20090806TUL02), Aug 6, 2009: CUSP WEB. CORRODED. CORROSION ON RIGHT CUSP MEMBRANE STATION 160-200. INSTALLED DOUBLER REPAIR UNDER AARD 53-20-00-16.
- [SDR AALA20090811TUL25](https://openairdocs.org/sdr/AALA20090811TUL25), Aug 5, 2009: PAN. CORRODED. CORROSION BELOW NUMBER ONE GALLEY AT DRAIN PAN AREA BETWEEN FLOORBEAMS STATION 148-160. INSTALLED DOUBLER UNDER AARD 53-20-00-16.
- [SDR AALA20090811TUL22](https://openairdocs.org/sdr/AALA20090811TUL22), Aug 5, 2009: WEB. CORRODED. CORROSION ON WEB ABOVE AFT CARGO DOOR BEAM STATION 1209. INSTALLED DOUBLER UNDER SRM 51-70-04.
- [SDR AALA20090811TUL05](https://openairdocs.org/sdr/AALA20090811TUL05), Aug 5, 2009: STRUCTURE. CORRODED. SUB FLOOR STATION 200 FORWARD OF NUMBER SIX TRACK IS CORRODED. INSTALLED DOUBLER UNDER AARD 53-20-00-16.
- [SDR AALA20090806TUL24](https://openairdocs.org/sdr/AALA20090806TUL24), Aug 5, 2009: CUSP WEB. CORRODED. CUSP CORROSION FROM STATION 1250 TO 1309 OUT OF LIMITS. INSTALLED NEW CUSP PER AARD 53-20-00-16.
- [SDR AALA20090806TUL23](https://openairdocs.org/sdr/AALA20090806TUL23), Aug 5, 2009: CUSP WEB. CRACKED. LEFT CUSP STATION 1285 CRACKED. INSTALLED CUSP DOUBLER REPAIR PER AARD 53-20-00-16.
- [SDR AALA20090806TUL22](https://openairdocs.org/sdr/AALA20090806TUL22), Aug 5, 2009: CUSP WEB. CRACKED. LEFT CUSP STATION 1290 CRACKED. INSTALLED CUSP DOUBLER REPAIR PER AARD 53-20-00-16.
- [SDR AALA20090806TUL21](https://openairdocs.org/sdr/AALA20090806TUL21), Aug 5, 2009: WEB. DAMAGED. WEB INBOARD OF CARGO BEAM HAS DEEP TOOL MARKS. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR UNDER SRM 51-70-04 FIGURE 2 SHEET 2.
- [SDR AALA20090806TUL17](https://openairdocs.org/sdr/AALA20090806TUL17), Aug 4, 2009: STRAP. DAMAGED. MID CARGO AFT DOOR FRAME AFT STRAP IS DAMAGED BELOW THE RIGHT TIE DOWN TRACK INBOARD LANDING AT STATION 702 LONGERON 30R-26R. REPLACED STRAP UNDER AARD 53-00-00
- [SDR AALA20090806TUL20](https://openairdocs.org/sdr/AALA20090806TUL20), Aug 4, 2009: CARGO TRACK. CORRODED. AFT CARGO LEFT AFT TIE DOWN TRACK CORRODED. INSTALLED NEW LEFT TIE DOWN TRACK STATION 1079-1320 UNDER SRM 51-30-01.
- [SDR AALA20090806TUL19](https://openairdocs.org/sdr/AALA20090806TUL19), Aug 4, 2009: CUSP WEB. CRACKED. LEFT CUSP CRACKED STATION 225. REPLACED CUSP SHEET UNDER AARD 53-20-00-16.
- [SDR AALA20090806TUL18](https://openairdocs.org/sdr/AALA20090806TUL18), Aug 4, 2009: CUSP WEB. CRACKED. RIGHT SIDE CRACK IN CUSP AT FASTENER HOLE STATION 844. REPAIRED CRACK WITH DOUBLER UNDER AARD 53-20-00-16.
- [SDR AALA20090806TUL16](https://openairdocs.org/sdr/AALA20090806TUL16), Aug 4, 2009: WEB. CORRODED. SUB FLOOR HAS CORROSION STATION 180-160 INBOARD OF NUMBER 5 SEAT TRACK AND UNDER NUMBER 1 GALLEY. INSTALLED DOUBLER UNDER AARD 53-20-00-16.
- [SDR AALA20090803TUL04](https://openairdocs.org/sdr/AALA20090803TUL04), Aug 3, 2009: SKIN. GOUGED. AFT CARGO DOOR EXTERIOR SKIN HAS DENT AND GOUGE 14 INCHES FROM TOP EDGE AND 18 INCHES FROM AFT EDGE. REMOVED DENTED AND GOUGED SKIN FROM OUTER SKIN, FABRICATED 
- [SDR AALA20090803TUL03](https://openairdocs.org/sdr/AALA20090803TUL03), Aug 3, 2009: STOP FITTING. CRACKED. AFT CARGO DOOR NUMBER ONE BEAM AFT STOP FITTING CRACKED. REMOVED AND REPLACED AFT STOP FITTING PER ESO 80174.
- [SDR AALA20090803TUL02](https://openairdocs.org/sdr/AALA20090803TUL02), Aug 3, 2009: STOP FITTING. CRACKED. AFT CARGO DOOR NUMBER ONE BEAM FORWARD STOP FITTING CRACKED. REMOVED AND REPLACED STOP FITTING PER ESO 80174.
- [SDR AALA20090803TUL01](https://openairdocs.org/sdr/AALA20090803TUL01), Aug 3, 2009: RIB. CRACKED. HIGH FREQUENCY EDDY CURRENT INDICATES CRACKS ON RIGHT WING LEADING EDGE NUMBER FIVE SLAT AT BOTH OUTBOARD AND SECOND FROM OUTBOARD MOST SLAT RIBS. REPLACED BOTH
- [SDR AALA20090806TUL13](https://openairdocs.org/sdr/AALA20090806TUL13), Aug 2, 2009: SKIN. DENTED. TWO DENTS OUT OF LIMITS DUE TO BEING IN THE SAME BAY NOT MEETING SEPARATION REQUIREMENTS UNDER SRM 53-04-00 FIGURE 3B. INSTALLED DOUBLER UNDER SRM 53-04 FIGURE 
- [SDR AALA20090731TUL07](https://openairdocs.org/sdr/AALA20090731TUL07), Jul 31, 2009: STOP FITTING. CRACKED. TUL - FORWARD CARGO DOOR AFT STOP PAD FITTING AT NUMBER ONE BEAM CRACKED. REMOVED AND REPLACED STOP PAD FITTING PER ESO 80174.
- [SDR AALA20090731TUL06](https://openairdocs.org/sdr/AALA20090731TUL06), Jul 31, 2009: STOP FITTING. CRACKED. TUL - FORWARD CARGO DOOR FORWARD STOP BRACKET (STOP PAD FITTING) AT NUMBER THREE BEAM CRACKED. REMOVED AND REPLACED STOP BRACKET (STOP PAD FITTING) UNDER ESO 80
- [SDR AALA20090806TUL14](https://openairdocs.org/sdr/AALA20090806TUL14), Jul 30, 2009: PAN. CRACKED. LEFT HAND WINDOW PAN STATION 1060 HAS THE UPPER AFT EAR CRACKED. INSTALLED REPAIR ANGLE UNDER AARD 53-10-00-25.
- [SDR AALA20090806TUL12](https://openairdocs.org/sdr/AALA20090806TUL12), Jul 30, 2009: WEB. CRACKED. WEB CRACKED AT STATION 207 L-15L. INSTALLED DOUBLER UNDER AARD 53-10-00-11.
- [SDR AALA2009060200007](https://openairdocs.org/sdr/AALA2009060200007), Jun 2, 2009: HYDRAULIC LINE. LOOSE. DFW - LANDING GEAR SLOW TO LOWER AND RIGHT HYDRAULIC PRESS LIGHT ILLUMINATED. LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND HYDRAULIC LEAK I
- [SDR AALA200803107](https://openairdocs.org/sdr/AALA200803107), Dec 13, 2008: GENERATOR. FAULTED. LGA INFLIGHT - CREW REPORTED NR 1 ENGINE DRIVEN GENERATOR CYCLED ON AND OFF AFTER TAKEOFF FOLLOWED BY NAVIGATION DATA AND DISPLAY GUIDANCE COMPUTER INPUT LOST. 
- [SDR AALA200802657](https://openairdocs.org/sdr/AALA200802657), Oct 2, 2008: LIGHT. INOPERATIVE. MIA - EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA200802450](https://openairdocs.org/sdr/AALA200802450), Sep 26, 2008: LIGHT. INOPERATIVE. MIA EMERGENCY LIGHT AT SEAT 33D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 33D. SYSTEM GROUND CHECKED NORMAL OPS.
- [SDR AALA200801145](https://openairdocs.org/sdr/AALA200801145), Apr 28, 2008: WEB. CORRODED. TUL - LOWER WEB AT AFT LAVATORY SERVICE COMPARTMENT AFT END AFT CARGO HAS CORROSION AT STATION 1300 TO 1320. REPLACED FOUR INSIDE DOUBLERS IN ACCORDANCE WITH EN
- [SDR AALA200801146](https://openairdocs.org/sdr/AALA200801146), Apr 28, 2008: BULKHEAD. DEFORMED. TUL - AFT PRESSURE BULKHEAD WEB DEFORMED AT STATION 1338. AREA OF DISCREPANCY IS 45 INCHES BY 28.5 INCHES. REPAIRED BULKHEAD DOME PER SRM 53 03 FIGURE 33 VIEW C
- [SDR AALA20072242](https://openairdocs.org/sdr/AALA20072242), Nov 18, 2007: HOSE. LEAKING. AUS INFLIGHT T1960/18NOV, RIGHT HYDRAULIC SYSTEM LOST FLUID AT CRUISE. NORMAL GEAR EXTENSION WAS USED. LANDED AUS WITHOUT INCIDENT. FOUND RIGHT HYDRAULIC RETURN
- [SDR AALA20070230](https://openairdocs.org/sdr/AALA20070230), Jan 31, 2007: CONNECTOR. DISCONNECTED. SFO - FOUND EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. REPINNED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20070229](https://openairdocs.org/sdr/AALA20070229), Jan 31, 2007: CONNECTOR. DISCONNECTED. SFO - FOUND EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. REPINNED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20050731](https://openairdocs.org/sdr/AALA20050731), Nov 8, 2005: BATTERY PACK. INOPERATIVE. LGA - FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR TAILCONE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20040199](https://openairdocs.org/sdr/AALA20040199), Feb 6, 2004: BATTERY PACK. INOPERATIVE. DFW CEILING EMERGENCY LIGHTS AT ROWS 3 TO 7 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROWS 3 TO 7. SYSTEM GROUND CHECKED NORMAL OPERATI

All 68: https://openairdocs.org/aircraft/N588AA/unmatched-reports.md

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other DJI PHANTOM 4 aircraft: https://openairdocs.org/model/dji-phantom-4/aircraft.md

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