# N103DA: 2002 Aircraft Sales & Parts SUMMIT II

- Status: Valid registration
- Airframe: [Aircraft Sales & Parts SUMMIT II](https://openairdocs.org/model/aircraft-sales-parts-summit-ii) (registry code 05904WN, 2 seats)
- Engine: [Rotax 582SER](https://openairdocs.org/engine/rotax-582ser) (registry code 55556)
- Serial number: 3086
- Year built: 2002
- Type: Powered parachute
- Engine type: 2 cycle
- Airworthiness: Experimental, registered before 01/31/08
- Airworthiness date: November 26, 2007
- Certificate issued: August 28, 2007
- Expires: April 30, 2028
- Mode S code: A01025
- Registered owner: [Allen Dallas R](https://openairdocs.org/faa-owner/ALLEN%20DALLAS%20R)
- Location: [Plant City, FL](https://openairdocs.org/faa-place/FL/Plant%20City)
- Owner type: Individual
- Owner's area on the map: 28.0859° N, 82.1481° W: Placed by OpenAirDocs at the center of ZIP code 33565, 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=103DA
- Page: https://openairdocs.org/aircraft/N103DA

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 (Aircraft Sales & Parts SUMMIT II)

None in force.

### Matched by engine (Rotax 582SER)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N103DA.

## FAA accident and incident reports

None matched to N103DA.

## Reports on N103DA not matched to an aircraft (2)

They name N103DA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20000718027079I](https://openairdocs.org/incident/20000718027079I), Jul 18, 2000: Boeing 767232 (N103DA), Memphis, TN. (-23)A/c dispatched with lt pack inop. Due to faulty isolation valve, a/c could not maintain pressurization with rt pack.
- [Incident 19870630040879I](https://openairdocs.org/incident/19870630040879I), Jun 30, 1987: Boeing 767232 (N103DA), Los Angeles, CA. Both engines were shut down during climb. Pilot failed to coordinate with copilot and inadvertently shut off fuel.

## 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 N103DA not matched to an aircraft (34)

They name N103DA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DL767050518](https://openairdocs.org/sdr/DL767050518), Sep 6, 2005: BULKHEAD. CRACKED. DAMAGE FOUND ON FS 1582 BULKHEAD AT STIFFENER 14L LAPJOINT BETWEEN TEAR STRAPS 4 AND 5. REPAIRED USING DOUBLER/STRUCTURAL SHIMS ON AFT SIDE OF BULKHEAD. BOEING 
- [SDR DL767040637](https://openairdocs.org/sdr/DL767040637), Jul 7, 2004: VALVE. INOPERATIVE. ACFT WOULD NOT PRESSURIZE AFTER TAKEOFF. REPLACED FWD EQUIPMENT COOLING OVERBOARD EXHAUST VALVE.
- [SDR DL767040507](https://openairdocs.org/sdr/DL767040507), Mar 4, 2004: WIRE. CORRODED. DURING HMV IN GSO FOUND NR 2 PYLON AND ENGINE WIRING CORRODED AT CANNON PLUGS. REPLACED WIRES AND PLUGS.
- [SDR DL767040506](https://openairdocs.org/sdr/DL767040506), Mar 4, 2004: WIRE. CORRODED. DURING HMV IN GSO FOUND NR 1 PYLON AND ENGINE WIRING CORRODED AT CANNON PLUGS. REPLACED WIRING AND PLUGS.
- [SDR DL767030687](https://openairdocs.org/sdr/DL767030687), Jul 22, 2003: CHARGER. INOPERATIVE. MID LEFT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER, OPS GOOD.
- [SDR DL767030283](https://openairdocs.org/sdr/DL767030283), Mar 27, 2003: WEDGE. DEBONDED. RIGHT WING SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 422819-14.
- [SDR DL767021462](https://openairdocs.org/sdr/DL767021462), Dec 23, 2002: COUPLING. LEAKING. LEFT DUCT LEAK ON CLIMBOUT. RESEALED COUPLING ON BODY CROSSOVER DUCT IN LEFT AC BAY. RAN TO TAKEOFF POWER PER PFHB. OK FOR SERVICE.
- [SDR DL767021395](https://openairdocs.org/sdr/DL767021395), Dec 1, 2002: ENGINE. FAILED. LEFT ENG SURGE IN FLIGHT AND ON LANDING. ENG SHUT ITSELF DOWN ON LANDING AT 5 THOUSAND FT. ENG CHANGE IS IN WORK
- [SDR DL767020496](https://openairdocs.org/sdr/DL767020496), May 1, 2002: PANEL. UNRELIABLE. CAPTAINS VHF FREQUENCY SELECT PANEL LEFT DISPLAY 4TH DIGIT CHANGED_WITHOUT INPUT. 118.97 SWITCHED BACK AND FORTH TO 118.17 CA RPLD PANEL, OP CKS GD.
- [SDR DL767020443](https://openairdocs.org/sdr/DL767020443), Apr 16, 2002: LIGHT. INOPERATIVE. COCKPIT PORTABLE EMERGENCY LIGHT WILL NOT ILLUM. REPLACED SAME.
- [SDR DL767011723](https://openairdocs.org/sdr/DL767011723), Oct 26, 2001: TARGET. OUT OF ADJ. ON T/O, LEADING EDGE LIGHT FLICKERED AND STICK SHAKER AFTER T/O LIGHT CAME ON STBY FLAPS WERE RETRACTED BUT STUCK BETWEEN UP AND 1 HAD ASSOCIATED L/E SLAT ASYM 
- [SDR DL767011717](https://openairdocs.org/sdr/DL767011717), Oct 24, 2001: SKIN. DELAMINATED. DELAMINATION TO THE UPPER SKIN OF THE SPOILER. REPAIRED PER ER/A 410579-14.
- [SDR DL767011350](https://openairdocs.org/sdr/DL767011350), Aug 17, 2001: FUEL LINE. CRACKED. FLUID LEAKING FROM RIGHT ENGINE ON PUSHBACK AFTER START. T/S LEAK PER M/M FOUND FUEL TUBE ON FUEL NOZZLE FEEDER MANIFOLD AT 5'OCLOCK POSITION CRACKED. REPLACED 
- [SDR DL767011305](https://openairdocs.org/sdr/DL767011305), Aug 7, 2001: FRAME. CRACKED. INSPECTION OF THE FS 1809.5 OUTER CHORDS PER AD 2001-09-13 AND BAC S/B 767-53-0078 REVEALED CRACKS EMANATING FROM TWO FASTENER HOLES IN THE RT FWD CHORD AND ONE
- [SDR DL767010742](https://openairdocs.org/sdr/DL767010742), May 9, 2001: BATTERY. DISCHARGED. LEFT OVERWING EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY AND BATTERY ASSEMBLY PER M/M.
- [SDR DL767010740](https://openairdocs.org/sdr/DL767010740), May 9, 2001: POWER SUPPLY. INOPERATIVE. LEFT OVERWING EXTERIOR EMERGENCY LIGHTING INOP. REMOVED AND REPLACED POWER SUPPLY AND BATTERY ASSEMBLY PER M/M.
- [SDR DL767002283](https://openairdocs.org/sdr/DL767002283), Nov 13, 2000: ENGINE. LEAKING. SMOKE IN CABIN SOURCE UNKNOWN SMOKE CLEARED AFTER PERFORMINGSMOKE AND FUME REMOVAL CHK LIST._HAPPENED AT FL370 DESCENDED TO FL230 ALSO SMOKE ALARM IN MID LAV WE
- [SDR DL767002134](https://openairdocs.org/sdr/DL767002134), Oct 25, 2000: SKIN. CORRODED. CORROSION FOUND ON CENTER SECTION WING SKIN. THE DAMAGE WAS ON THE OUTER SURFACE OF THE UPPER SKIN AT STRINGER U-17 AT LBL 88. ER/A 334963-14 REPAIRED DAMAGE.
- [SDR DL767002132](https://openairdocs.org/sdr/DL767002132), Oct 25, 2000: PRESSURE PANEL. CORRODED. CORROSION FOUND ON THE RT MLG WHEEL WELL CANTED PRESSURE WEB. CORROSION LOCATED AT STA 960 BETWEEN RBL 85 AND RBL 90. ER/A 334987-14 REMOVED CORROSION.
- [SDR DL767001894](https://openairdocs.org/sdr/DL767001894), Sep 27, 2000: SKIN. DENTED. GROUND DAMAGE AT STA 1250 STR 30R. SKIN AND STRINGER DENTED LOCALLY. SKIN AND STRINGER ARE TRIMMED OUT AND REPAIRED. ER/A 369288-14 REV A.
- [SDR DL767001859](https://openairdocs.org/sdr/DL767001859), Sep 25, 2000: SKIN. CORRODED. CORROSION WAS FOUND ON THE FUSELAGE SKIN AT THE FOLLOWING LOCATIONS; FS 1175 AND S-39L, FS 1197 AND S-39L, AND FS 1197AND S-39R. THE CORROSION WAS CUT OUT AND E
- [SDR DL767001781](https://openairdocs.org/sdr/DL767001781), Sep 15, 2000: SKIN. GOUGED. OUTER SKIN OF THE L-1 DOOR HAS BEEN GOUGED. REPAIR PER ER/A 388030-14.
- [SDR DL767001349](https://openairdocs.org/sdr/DL767001349), Jul 18, 2000: VALVE. MALFUNCTIONED. AT FL350 WITH RT PACK ON GOT CABIN ALT EICAS MSG. TURNED LT PACK ON AND DID EMER DESCENT AND DIVERTED TO MEM. RT PACK TESTED GOOD. LT PACK VALVE INDICATION ON P
- [SDR DL767991716](https://openairdocs.org/sdr/DL767991716), Jul 31, 1999: IDG. REQUIRED SERVICE. RT GEN FIELD TRIPPED ON T/O ROLL, ABORTED T/O AT 80 KNOTS. RAN NR 2 ENG, DISCONNECTED RT IDG. VERIFIED NO VOLTS AND FREQS. SERVICED IDG WITH OIL.
- [SDR DL767981757](https://openairdocs.org/sdr/DL767981757), Aug 22, 1998: LIGHT. DAMAGED. EMERGENCY TRACK LIGHTING DAMAGED BY 2L DOOR. INSPECTED ALL EMERGENCY TRACK LIGHTING, REPAIRED DAMAGE, CKS OK.
- [SDR DL767981374](https://openairdocs.org/sdr/DL767981374), Jul 1, 1998: ENGINE. FAILED. AS POWER CAME UP FROM IDLE A BANG WAS HEARD AND LT ENG REMAINED AT IDLE PWR. NO CONTROL OF LEFT ENG FROM COCKPIT. NO ENG EXCEEDANCE NOTED AND NO INDICATIONS IN 
- [SDR DL767980207](https://openairdocs.org/sdr/DL767980207), Jan 21, 1998: PRESSURE DECK. CRACKED. THE WHEEL WELL PRESSURE DECK WAS FOUND WITH A CRACK AT 977 ON THE LEFT HAND SIDE AT LBL 35, THE CRACK IS 12 INCHES LONG. THE CRACK WAS REPAIRED PER 767-200 SRM 
- [SDR DL767971445](https://openairdocs.org/sdr/DL767971445), Jun 19, 1997: TE WEDGE. DELAMINATED. THE NR 5 SLAT TRAILING EDGE WEDGE UPPER SURFACE WAS FOUND DELAMINATED ON THE AFT INBOARD CORNER. THE DELAMINATION IS APPROX 3 BY 3.5. THIS AREA WAS REPAIRED PER
- [SDR DL767962000](https://openairdocs.org/sdr/DL767962000), Aug 28, 1996: POWER SUPPLY. INOPERATIVE. FWD PART OF AFT CABIN EMERGENCY PATH LIGHTING INOP DURING L/O. REPAIRED SHORTED WIRES AT SIDEWALL 35FG AND REPLACED M9009 BATTERY MODULE.
- [SDR DL767961900](https://openairdocs.org/sdr/DL767961900), Aug 14, 1996: BATTERY PACK. DISCHARGED. FOUND ON L/O, AFT THREE EXTERIOR EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY M738 AND BATTERY PACK, LIGHT OPS NORMAL.
- [SDR DL767961161](https://openairdocs.org/sdr/DL767961161), May 15, 1996: COFFEEMAKER. FAILED. SMOKE IN REAR GALLEY REPORTED COMING FROM AIR VENT. INSPECTED AFT GALLEY AREA AND ABOVE CEILING AREA FOR EVIDENCE OF BURNING OR SMELL, NONE FOUND AND ALL WIRING
- [SDR DL767961046](https://openairdocs.org/sdr/DL767961046), May 1, 1996: RETRACT MECH. MALFUNCTIONED. AIRCRAFT'S ATB RIGHT MLG WOULD NOT RETRACT. PRESSURE GOOD. JACKED AIRCRAFT, CYCLED GEAR SERVERAL TIMES PER MM. CHECKS NORMAL. TILTED TRUCK, TURNED ON HYDRAULIC,
- [SDR DL767954374](https://openairdocs.org/sdr/DL767954374), Nov 14, 1995: SPRING. BROKEN. ON TAXI OUT, CHECKING CONTROLS F/O SIDE AILERONS EXTREMELY STIFF, VERY DIFFICULT TO MOVE. AFTER INSPECTION FOUND SPRING (P/N 69881284-2), BROKEN ON F/O AILERON 
- [SDR DL767950116](https://openairdocs.org/sdr/DL767950116), Jan 10, 1995: POWER SUPPLY. FAULTY. DURING LAYOVER, RIGHT SIDE OVERWING EMERGENCY ESCAPE SLIDE SQUIB TEST 2 INOP. REPLACED RIGHT SQUIB POWER SUPPLY TEST NORMAL.

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Aircraft Sales & Parts SUMMIT II aircraft: https://openairdocs.org/model/aircraft-sales-parts-summit-ii/aircraft.md
- The Rotax 582SER engine: https://openairdocs.org/engine/rotax-582ser.md

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