19960813026769I

Incident · Minor damage

FAA incident report · Piper PA-38-112 · Kansas City, MO · August 13, 1996

Date
August 13, 1996 · 10:45 local
Place
Kansas City, MO
Airport
Kansas City Downtown Airport
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N2466D
Reported as
Piper PA38112
Reported engine
Lycoming O235L2C
People aboard
2
Fatal injuries
0
Pilot’s flight hours
1,000 total200 in this make and model150 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.

Narrative: 1. On 08/13/96 at 1545Z time, a Piper PA-38-112 aircraft (N2466D) departed Kansas City down town (mkc) airport, Missouri en route to return back to Kansas City down town (mkc) airport, Missouri. On take-off from runway 21 at mkc, certified flight instructor (CFI) craig a. moore noted a loss of engine power on climb. Flight instructor, craig a. moore, immediately took control of the aircraft from his student jeremiah garlook and proceeded to make an emergency go-around landing. 2. Initiating emergency procedures with approximately only 100 feet above ground level (AGL), the flight instructor proceeded with an emergency landing. The flight instructor instructed his student to notify the airport tower that they were making an emergency landing on runway 1. Total engine power was lost while making the evasive turn to land on runway 1. Attempting to avoid injury to ground personnel and property, the flight instructor targeted a grassy area to land the aircraft which resulted in the left wing tip to touch the ground and receive minor damage. 3. On examination, mechanic charles drake of spirit aviation discovered water in the left wing fuel tank. Aircraft records revealed that this aircraft had not been operated for the past three days prior to this flight and had been exposed to heavy rains. It is believed that the fuel caps may not have been completely sealed resulting in rain water to have seeped into the left wing fuel tank. The left wing fuel tank was selected for use during this intended flight. 4. The aircraft fuel system will be purged by the mechanic charles drake and returned to service after a hard landing inspection is accomplished. A follow-up ramp and records inspection will be conducted by general aviation airworthiness section. This incident investigation was cordinated with general avaition operations. 5. This incident number CE96-IGA0114 is closed.

As the FAA filed it

NARRATIVE: 1. ON 08/13/96 AT 1545Z TIME, A PIPER PA-38-112 AIRCRAFT (N2466D) DEPARTED KANSAS CITY DOWN TOWN (MKC) AIRPORT, MISSOURI EN ROUTE TO RETURN BACK TO KANSAS CITY DOWN TOWN (MKC) AIRPORT, MISSOURI. ON TAKE-OFF FROM RUNWAY 21 AT MKC, CERTIFIED FLIGHT INSTRUCTOR (CFI) CRAIG A. MOORE NOTED A LOSS OF ENGINE POWER ON CLIMB. FLIGHT INSTRUCTOR, CRAIG A. MOORE, IMMEDIATELY TOOK CONTROL OF THE AIRCRAFT FROM HIS STUDENT JEREMIAH GARLOOK AND PROCEEDED TO MAKE AN EMERGENCY GO-AROUND LANDING. 2. INITIATING EMERGENCY PROCEDURES WITH APPROXIMATELY ONLY 100 FEET ABOVE GROUND LEVEL (AGL), THE FLIGHT INSTRUCTOR PROCEEDED WITH AN EMERGENCY LANDING. THE FLIGHT INSTRUCTOR INSTRUCTED HIS STUDENT TO NOTIFY THE AIRPORT TOWER THAT THEY WERE MAKING AN EMERGENCY LANDING ON RUNWAY 1. TOTAL ENGINE POWER WAS LOST WHILE MAKING THE EVASIVE TURN TO LAND ON RUNWAY 1. ATTEMPTING TO AVOID INJURY TO GROUND PERSONNEL AND PROPERTY, THE FLIGHT INSTRUCTOR TARGETED A GRASSY AREA TO LAND THE AIRCRAFT WHICH RESULTED IN THE LEFT WING TIP TO TOUCH THE GROUND AND RECEIVE MINOR DAMAGE. 3. ON EXAMINATION, MECHANIC CHARLES DRAKE OF SPIRIT AVIATION DISCOVERED WATER IN THE LEFT WING FUEL TANK. AIRCRAFT RECORDS REVEALED THAT THIS AIRCRAFT HAD NOT BEEN OPERATED FOR THE PAST THREE DAYS PRIOR TO THIS FLIGHT AND HAD BEEN EXPOSED TO HEAVY RAINS. IT IS BELIEVED THAT THE FUEL CAPS MAY NOT HAVE BEEN COMPLETELY SEALED RESULTING IN RAIN WATER TO HAVE SEEPED INTO THE LEFT WING FUEL TANK. THE LEFT WING FUEL TANK WAS SELECTED FOR USE DURING THIS INTENDED FLIGHT. 4. THE AIRCRAFT FUEL SYSTEM WILL BE PURGED BY THE MECHANIC CHARLES DRAKE AND RETURNED TO SERVICE AFTER A HARD LANDING INSPECTION IS ACCOMPLISHED. A FOLLOW-UP RAMP AND RECORDS INSPECTION WILL BE CONDUCTED BY GENERAL AVIATION AIRWORTHINESS SECTION. THIS INCIDENT INVESTIGATION WAS CORDINATED WITH GENERAL AVAITION OPERATIONS. 5. THIS INCIDENT NUMBER CE96-IGA0114 IS CLOSED.

Other reports on N2466D · 2

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