# Incident 20060111011569I: Piper PA28*, Lincoln Park, NJ, January 11, 2006

- Type: FAA incident report (Accident/Incident Data System), as reported
- Date: January 11, 2006, 16:00 local time
- Place: Lincoln Park, NJ
- Airport: Lincoln Park Airport
- Damage: Minor damage
- Phase of flight: Forced/Precautionary Landing
- Operating rules: General operating rules (Part 91)
- Location: 40.9476° N, 74.3145° W: Placed by OpenAirDocs at LINCOLN PARK (N07), within about a mile (OpenAirDocs)
- Nearby events: https://openairdocs.org/map.md?lat=40.9476&lon=-74.3145&mi=10
- Aircraft: N5328W, a cancelled registration (https://openairdocs.org/deregistered/N5328W-2012-12-18) (OpenAirDocs)
- Registry model: Piper PA-28 (registry code 7102801, https://openairdocs.org/model/piper-pa-28) (OpenAirDocs)
- Registry engine: Lycoming 0-320 series (registry code 41508, https://openairdocs.org/engine/lycoming-0-320-series) (OpenAirDocs)
- Reported make and model: PIPER PA28*
- Reported engine: LYC O320*
- People aboard: 1
- Fatal injuries: 0
- Pilot certificates: Student
- Pilot flight hours: 130 total, 130 in this make and model, 20 in the last 90 days
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/20060111011569I

## Narrative

As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^.

(-23) AIRCRAFT DEPARTED FROM RUNWAY 19 AT LINCOLN PARK AIRPORT (N07) AFTER PASSING THROUGH 800 FEET THE ENGINE BEGAN TO RUN ROUGH AND DID NOT PRODUCE SUFFICIENT POWER. PILOT ANNOUNCED EMERGENCY AND ATTEMPTED TO LAND ON RUNWAY 1. DUE TO THE ALTITUDE AND SPEED HE COULD NOT EXECUTE A SAFE LANDING AND ATTEMPTED A GO AROUND. THE ENGINE FAILED TO PRODUCE SUFFICIENT POWER TO GAIN ALTITUDE, AND IT WAS RUNNING VERY ROUGH. THE PILOT SAW AN OPEN FIELD APPROXIMATELY 1200 FEET PAST THE END OF RUNWAY 1 AND DECIDED TO EXECUTE AN EMERGENCY LANDING. AFTER LANDING, THE PILOT TURNED LEFT TO AVOID HITTING A DUMPSTER. THE NOSE WHEEL HIT A CURB THAT WAS FABRICATED FROM A 4 1/2 INCHES IN DIAMETER PIPE. THE NOSE GEAR STRUT AND ENGINE MOUNT WAS DAMAGED. ONE BLADE OF THE TWO BLADED PROPELLER WAS DAMAGED. MINOR DAMAGE TO THE RIGHT WING TIP.

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. For accidents, the NTSB's own investigation is the fuller record.

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