N319FC

Destroyed
Fatal

Piper PA-28-140S/N: 28-25157

Accident Details

Date
Friday, June 15, 2001
NTSB Number
LAX01FA208
Location
Lanai City, HI
Event ID
20010627X01274
Coordinates
20.882778, -156.964996
Aircraft Damage
Destroyed
Highest Injury
Fatal
Fatalities
1
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
2

Probable Cause and Findings

the CFI's inadequate in-flight planning/decision making, inadequate supervision, and his delayed remedial action, which resulted in controlled flight into terrain.

Aircraft Information

Registration
N319FC
Make
PIPER
Serial Number
28-25157
Engine Type
Reciprocating
Year Built
1968
Model / ICAO
PA-28-140P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
MUELLER JAHN P
Address
PO BOX 30523
Status
Deregistered
City
HONOLULU
State / Zip Code
HI 96820-0523
Country
United States

Analysis

HISTORY OF FLIGHT

On June 14, 2001, at 2044 Hawaiian standard time, a Piper PA-28-140, N319FC, impacted level terrain 5.4 miles northwest of the Lanai Airport (LNY), Lanai City, Hawaii. Mueller Aviation operated the airplane under the provisions of 14 CFR Part 91. The airplane was destroyed. The student pilot sustained fatal injuries; the certified flight instructor (CFI) sustained serious injuries. The instructional cross-country flight departed Honolulu International Airport (HNL), Honolulu, Hawaii, about 1945, en route to Kapalua Airport (HJH), Lahaina, on the island of Maui. Night visual meteorological conditions prevailed, and a visual flight rules (VFR) flight plan had been filed.

In a post accident interview, the CFI reported that the purpose of the flight was to do a night cross-country in preparation for the student's private pilot check ride. After receiving a weather briefing, the student pilot filed a flight plan to HJH at 3,000 feet. The intent was to execute a night landing at the Kahului Airport (OGG), Kahului, Hawaii, or LNY.

As the flight proceeded towards Lanai, weather conditions deteriorated. The CFI told the student to make a right turn. Instead, the student made a left descending turn and they entered instrument meteorological conditions (IMC). The CFI took the controls and initiated a climb on a heading of approximately 270 degrees when the airplane impacted the ground in a level attitude.

The National Transportation Safety Board investigator-in-charge (IIC) reviewed recorded radio transmissions between the pilot and the Honolulu Automated Flight Service Station (HNL AFSS).

The student contacted an air traffic control specialist at the HNL AFSS prior to the flight and requested the following information: winds aloft forecast; Notices to Airmen (NOTAM); significant weather; and Kapalua weather. The specialist provided the information and advised, "VFR flight was not recommended" on the windward and mountain sections, and on the windward coastal sections of Maui. The student queried the "VFR not recommended" advisory. The specialist gave him the advisory a second time, and again advised "VFR flight was not recommended."

The student was in radio contact during the flight with an air traffic control specialist at the HNL AFSS. The student's final position report was Heleolono Harbor. He reported reaching Heleolono Harbor, and then queried the specialist as to whether or not HJH (his filed destination) was a private or public airport. The specialist advised the student that it was a private airport. The student closed his flight plan and the specialist queried as to his destination. The student reported that he was turning around, with the intent to return to HNL. The specialist then stated, "flight plan closed."

Coast Guard rescue personnel reported that dark, moonless lighting conditions existed during the rescue operations. The accident site was located approximately 5 hours 30 minutes after it occurred.

According to a Federal Aviation Administration (FAA) inspector, the pilots were not in radio contact with Federal Aviation Administration (FAA) facilities at the time of the accident.

PERSONNEL INFORMATION

A review of FAA airman records revealed that the CFI held a commercial certificate with ratings for single engine land, multiengine land, and instrument airplanes. The CFI also held a certified flight instructor certificate with ratings for single engine and multiengine land airplanes. The CFI held a first-class medical certificate issued on March 02, 2001. It had no limitations or waivers.

An examination of the CFI's logbook indicated he had accumulated an estimated total flight time of 382 hours. He logged 63 hours in the last 90 days, and 45 hours in the last 30 days. The CFI had logged 54 hours as a CFI with 2 hours of night instruction given. He had 54 hours in this make and model.

A review of FAA airman records revealed that the second pilot was a student pilot. The student pilot held a first-class medical certificate issued on May 26, 2001. It had no limitations or waivers. The CFI described the student pilot as an excellent student. The student had about 15 hours total time, and soloed after 1 week of instruction.

AIRCRAFT INFORMATION

The airplane was a 1968 Piper PA-28-140, serial number 28-25157. A review of the airplane's logbooks revealed a total airframe time of 9,081.86 hours at the last 100-hour inspection. The 100-hour inspection was completed on May 1, 2001. At the time of the last inspection, the tachometer read 2,318.96, and the Hobbs hour meter read 1,818.0. The tachometer read 2,343.76 at the accident scene, while the Hobbs hour meter read 1,838.3. The last annual inspection was completed on February 23, 2001, at 8,883.0 hours.

The engine was a Textron Lycoming O-320-E2A engine, serial number L-14033-27. Total time on the engine at the last 100-hour inspection was 1188.0 hours.

METEOROLOGICAL INFORMATION

The closest official weather observation station was Lanai Airport (LNY), Lanai, located 5.4 miles southeast of the accident site. The elevation of the weather observation station was 1,308 feet msl. Hawaiian Airlines personnel, located at LNY, who were National Weather Service (NWS) certified, took a weather observation at 2045. It stated: winds from 040 degrees at 20 knots; visibility 10 miles; few clouds at 1,000 feet, 2,000 feet scattered, and 4,000 feet scattered; temperature 69 degrees Fahrenheit; dew point 68 degrees Fahrenheit; altimeter 29.99 InHg.

The next closest official weather observation station was Molokai Airport (HMO), Molokai, located 20 miles north-northeast of the accident site. The elevation of the weather observation station was 454 feet msl. Reported weather at 1954, was: winds from 060 degrees at 14 knots gusting to 18 knots; visibility 10 miles; few clouds at 3,500 feet, scattered clouds at 6,500 feet; temperature 74 degrees Fahrenheit; dew point 66 degrees Fahrenheit; altimeter 29.99 inHg.

The next closest official weather observation was Kahului Airport (OGG), Maui, located 29 miles east-northeast of the accident site. The elevation of the weather observation station was 54 feet msl. Reported weather at 1954 was: winds from 060 degrees at 13 knots gusting to 19 knots; visibility 10 miles; few clouds at 4,000 feet, scattered clouds at 7,000 feet; temperature 72 degrees Fahrenheit; dew point 66 Fahrenheit; altimeter 29.97 inHg.

The area forecast for the Hawaiian Islands was valid from June 14, 2001, at 1800 until June 15 at 0600. The windward coastal mountain sections of Maui, and adjacent coastal waters from 2000 were forecasted for the following: scattered clouds at 2,500 feet msl, scattered and broken clouds at 4,000 feet, and broken to scattered clouds at 6,000 feet, with tops to 8,000 feet. There were isolated broken clouds at 2,500 feet with visibility between 3 to 5 miles in light rain showers and mist.

The forecast for HNL to Maui for the same time period was as follows: expect scattered clouds at 2,500 feet msl, broken to scattered clouds at 4,500 feet with tops to 7,000 feet. An isolated broken cloud layer existed at 2,500 feet with light rain showers.

The outlook from 0700 to 1300 was for VFR conditions to prevail for the area. The terminal aerodrome forecast for LNY was issued at 1320 on June 14, 2001, valid from 1400 until 1400 on June 15. The forecast indicated wind was from 060 degrees at 8 knots; visibility better than 6 miles; scattered clouds at 2,000 feet, and 4,000 feet. A temporary condition existed between 1500 and 2100 for: broken ceilings at 2,000 feet, with a second broken layer of clouds at 6,000 feet. After 1000, the wind was forecast from 290 degrees at 8 knots; visibility better than 6 miles; scattered clouds at 2,000 feet, and a secondary layer at 4,000 feet. Temporary conditions existed between 1000 and 1500, called for broken clouds at 2,000 feet, and a broken cloud layer at 4,000 feet.

According to the United States Naval Observatory Sun and Moon information available for the day of the accident, sunset occurred at 1910, and the end of civil twilight occurred at 1934.

AIDS TO NAVIGATION

The airplane was equipped with a Very High Frequency (VHF) omni-directional range (VOR) receiver. The frequency for Koko head VOR (113.9) was in the primary receiver window and the frequency for Lanai (117.7) was in the standby window.

WRECKAGE AND IMPACT INFORMATION

Investigators from the Safety Board, the FAA, New Piper Aircraft, and Textron Lycoming, who were parties to the investigation, examined the wreckage at the accident scene. The primary wreckage was at 20 degrees 51 minutes north latitude and 156 degrees 58 minutes west longitude. The airplane came to rest upright at a global positioning system (GPS) elevation of 1,760 feet. The accident area was known as the "bombing range" on the outskirts of the "Garden of the Gods." The accident site was 5.4 miles from LNY on a 332-degree magnetic bearing.

The first identified point of impact (FIPI) was an initial ground scar, which was oriented along a 346-degree heading. The ground scar consisted of three parallel scrape marks that were separated by distances consistent with the distance between the fixed landing gear of the airplane. A portion of the nose gear was about 25 feet from the beginning of the ground scar. About 3 feet beyond the nose gear, were a series of slash marks. The slash marks continued for a distance of 36 feet. The slash marks were perpendicular to the scrape marks.

The airplane collided with a 4-foot dirt berm located 27 feet beyond the ground scar. Debris located between the berm and the main wreckage included the top rudder and vertical stabilizer fairing. The distance between the FIPC to the main wreckage was 250 feet on a 351-degree magnetic bearing.

Investigators examined the airframe and engine at the accident site on June 16, 2001.

The airplane fuselag...

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX01FA208