20050118001369I

Incident

FAA incident report · Blanca 17-30A · Lititz, PA · January 18, 2005

Date
January 18, 2005 · 17:56 local
Place
Lititz, PA
Phase of flight
Climb
Operating rules
General operating rules (Part 91)
Aircraft
N28085
Reported as
Blanca 1730A
Reported engine
Continental IO520K
People aboard
1
Fatal injuries
0
Pilot’s flight hours
4,970 total2,100 in this make and model25 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry 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.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) The subject aircraft was on a night VFR flight instruction flight, climbing thru 6,000 feet, when the engine began to surge. The pilot was able to restore smooth engine operation by using the fuel boost pump. At a location 12 miles south east of lancaster airport the pilot declared an emergency to ATC and received vectors to land at lancaster airport. An uneventful landing was made and the aircraft was towed to the ramp. Maintenance personnel at (lns) determined the engine driven fuel pump caused the malfunction. A malfunction and defect report was submitted to this office. No further action is required.

As the FAA filed it

(-23) THE SUBJECT AIRCRAFT WAS ON A NIGHT VFR FLIGHT INSTRUCTION FLIGHT, CLIMBING THRU 6,000 FEET, WHEN THE ENGINE BEGAN TO SURGE. THE PILOT WAS ABLE TO RESTORE SMOOTH ENGINE OPERATION BY USING THE FUEL BOOST PUMP. AT A LOCATION 12 MILES SOUTH EAST OF LANCASTER AIRPORT THE PILOT DECLARED AN EMERGENCY TO ATC AND RECEIVED VECTORS TO LAND AT LANCASTER AIRPORT. AN UNEVENTFUL LANDING WAS MADE AND THE AIRCRAFT WAS TOWED TO THE RAMP. MAINTENANCE PERSONNEL AT (LNS) DETERMINED THE ENGINE DRIVEN FUEL PUMP CAUSED THE MALFUNCTION. A MALFUNCTION AND DEFECT REPORT WAS SUBMITTED TO THIS OFFICE. NO FURTHER ACTION IS REQUIRED.

Other reports on N28085 · 2

Matched to the same aircraft by N-number and date.