NYC00MA201

NTSB accident investigation · Grumman G-159 · Linneus, ME · July 19, 2000

Accident · FatalMajor investigationFinal report
Date
July 19, 2000, 00:31 local (04:31 UTC)
Place
Linneus, ME
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
CGNAKGrumman G-159
Weather
Instrument (IMC) · Night/dark
Status
Completed · report September 27, 2001
Report
Approved by Office Director
Case key
54159

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The pilot-in-command's failure to maintain minimum control airspeed, which resulted in a loss of control. Factors in this accident were clouds, and a loss of engine power for undetermined reasons, while in cruise flight above the airplane's single engine service ceiling.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine powerCruise
1 engine - undeterminedFactor
Loss of control - in flightCruise
Weather condition - cloudsFactor
Airspeed(vmc) - not maintainedPilot in commandCause
Aircraft performance,engine out capability - exceededFactor
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - water
Terrain condition - ground

Analysis

The airplane was in cruise flight at 16,000 feet, in instrument meteorological conditions. About two minutes after the crew ceased cross-feeding due to a fuel imbalance, the left engine experienced a total loss of power. About one minute later, the co-pilot indicated to the pilot-in-command (PIC) that the airplane was losing airspeed, and about 15 seconds later, the co-pilot remarked "keep it up, keep it up." Shortly thereafter, the airplane departed controlled flight and impacted terrain. The airplane was destroyed by fire and impact forces. Examination of the left engine revealed no evidence of any pre-impact failures that would have accounted for an uncommanded in-flight shut-down. A SIGMET for potential severe clear icing was effective for airplane's flight path; however, the flight crew did not report or discuss any weather related problems around the time of the accident. At the time of the accident, the airplane was above its single-engine service ceiling. The PIC had accumulated approximately 6,000 hours of total flight experience, of which, about 500 hours were as PIC in make and model. The co-pilot had approximately 600 hours of total fight experience, of which, 300 hours were in make and model.

Factual narrative

History of flight

On July 19, 2000, about 0031 eastern daylight Time (EDT), a Grumman G-159 (G-1), Canadian registry C-GNAK, operated by Airwave Transport as flight 9807, was destroyed when it impacted terrain in Linneus, Maine. The Canadian certificated airline transport pilot-in-command (PIC) and the commercial rated co-pilot were fatally injured. Night instrument meteorological conditions prevailed and an instrument flight rules flight plan had been filed for the flight that departed the Moncton Airport (CYQM), Moncton, New Brunswick, Canada, destined for Dorval International Airport (CYUL), Montreal, Quebec, Canada. The flight was conducted under Canadian Aviation Regulation (CAR) 704 as a scheduled courier flight.

According to a Moncton Air Traffic Control (ATC) transcript, the flight departed CYQM, about 2348. Approximately 0005, the flight crew provided the following pilot report (PIREP):

"OK we're now 50 miles west going through 10,000 feet ah we've got a good ride now looks like we're well past it ah there was some pretty good icing around 9,000 feet between 40 DME and 50 DME from Moncton and pretty heavy rain but ah nothing on the airway...no thunderstorms that is." They further described the icing as "moderate to severe between nine and ten thousand but it uh only lasted for about five minutes."

The airplane leveled at 14,000 feet msl, and at 0015:15, the flight crew requested and received a "block" altitude clearance between 14,000 and 15,000 feet msl, because they were "sitting on the tops." The flight was instructed to contact the Boston Air Route Traffic Control Center (ARTCC) at 0016:06.

According to a Federal Aviation Administration (FAA) transcript, the flight crew made initial contact with the Boston ARTCC at 0017:54. Additionally, they requested and received "direct dorval." At 0025:16, the flight crew requested to climb to 16,000 feet, and was subsequently cleared to maintain the "block" altitude, up to 16,000 feet. At 0029:56, the flight crew declared an emergency, requested vectors for the nearest airport and stated, "cannot maintain altitude." At 0030:10, the flight crew stated that they had "lost control." There were no further known communications with the airplane.

Witnesses near the accident site reported being awakened by the loud sound of an airplane overhead. They described the sound as "surging," or "struggling" and one witness stated the noise repeatedly changed "like [the airplane] was getting closer then further." Witnesses then described hearing a loud explosion.

The accident occurred during the hours of night approximately 46 degrees, 7 minutes north latitude, and 67 degrees, 48 minutes west longitude.

Personnel information

The PIC was the owner and president of the company that operated the airplane. He held a Canadian airline transport pilot certificate, with ratings for single and multi-engine land airplanes. He was also certified for Group I instrument privileges. Additionally, the PIC was type rated in G-1, C-550, and Boeing 727 airplanes.

The PIC received his initial training for the G-1, in September 1995. The company reported he had accumulated approximately 6,000 hours of total flight experience, of which, about 500 hours were as PIC in the G-1. Additionally, he accumulated about 26 and 49 hours of flight experience in the G-1, during the 30 and 90 days prior to the accident, respectively.

The PIC completed a G-1 Recurrent Course at Flight Safety International, Savannah, Georgia, on October 16, 1999. Additionally, he received a pilot proficiency check (PPC), on October 16, 1999.

The PIC held a current Category I Canadian Medical Certificate, which was issued on April 3, 2000.

The PIC also held an aircraft maintenance engineers certificate with ratings for the Convair 580, Convair 640, and the G-1.

The co-pilot was hired on May 1, 1999, as a dispatcher, and began to transition to the G-1 in November 1999. He held a Canadian commercial pilot certificate, with ratings for single and multi-engine land airplanes. He was also certified for Group I instrument privileges and held a G-1 type rating.

The company reported that the co-pilot had accumulated approximately 600 hours of total fight experience, of which, 300 hours were in make and model. He accumulated about 39 and 86 hours of flight experience in the G-1, during the 30 and 90 days prior to the accident, respectively.

The co-pilot completed a G-1 Initial Training Course at Flight Safety International, Savannah, Georgia, on December 10, 1999. He received a PPC on January 14, 2000.

The co-pilot held a current Category I Canadian Medical Certificate, which was issued on November 26, 1999.

Aircraft information

Review of the airplane maintenance records revealed that Airwave Transport purchased the accident airplane from North American Airlines, Ltd., Calgary, Alberta, Canada, in November 1999. On November 6, 1999, the airplane was flown for 4.5 hours from the Calgary International Airport, Calgary, Alberta, Canada, to Toronto. Prior to that flight, the airplane's most recent flight was conducted on July 17, 1998.

The airplane was maintained by Airwave Transport under an approved manufacturer inspection program, and was most recently inspected on July 10, 2000. The airplane had an accumulated total airframe time of 22,046.7 hours, and 15,452 cycles.

The accident airplane was equipped with two Rolls-Royce Dart 529-8X model turbo-propeller engines and two Dowty CR184-4-30-4-50 model propellers.

The left engine and right engines were installed on the accident airplane on July 18, 1990, and May 6, 1997, respectively. The propellers were installed on the left and right accident engines on June 1, 2000, and April 21, 1998, respectively.

At the time of the accident, the left engine and right engine had accumulated about 3,861 and 5,389 hours since overhaul, respectively.

Review of the engine logbook records revealed an engine performance run was completed on July 7, 2000. No anomalies were reported on either engine.

On July 11 and 15, 2000, the airplane was test flown by the PIC of the accident flight for 1 hour each.

A company dispatch agent occupied the co-pilot seat during the July 15 test flight. The company dispatch agent stated that he held a commercial pilot's license and he had received 2-weeks of ground instruction and 5 hours of simulator training for the G-1. He did not hold a G-1 type rating. The dispatch agent stated that the test flight lasted about an hour and he did not observe any discrepancies with the airplane; nor did the PIC give any indication of any problems. Additionally, he recalled that the weather radar was tested and worked properly.

The accident flight occurred during the third leg of the airplane's first courier trip. The accident flight crew departed Toronto, on July 17, 2000, and arrived Halifax, Nova Scotia, about 0300. Airwave Transport maintained an apartment in Halifax for flight crew personnel. The flight crew departed Halifax about 2145, and landed in Moncton about 2210.

While in Halifax, the PIC informed company personnel that he had experienced no problems during the flight and was "very happy" with the airplane's performance.

Meteorological information

Prior to the flight, the accident flight crew received a weather-briefing package via fax, which included in-flight advisories, PIREPS, wind and temperature aloft forecasts, weather observations and forecasts for selected Canadian and U.S airports.

A weather observation taken at the Houlton International Airport (HUL), Houlton, Maine, at 0049, reported: wind from 230 degrees at 5 knots, visibility 8 miles, ceiling 600 feet overcast, temperature and dew point 57 degrees Fahrenheit, altimeter 29.71 in/hg.

A Safety Board Meteorology Factual Report was prepared for this accident.

According to the Meteorologist's Factual Report, Geos

Aircraft

Registration
CGNAK
Reported as
Grumman G-159
Category
Airplane
Serial number
154
Airframe hours
22,050
Engine
Rolls-Royce 529-8X, 1,910 horsepower, turbo prop
Damage
Destroyed
Fire
On-Ground
Flight
Non-U.S., commercial
Registered owner
Airwave Transport
Airworthiness certificate
Standard, Transport
Last inspection
Continuous airworthiness · July 10, 2000 · 5 hours before
Departed
YQM · Moncton
Destination
YUL · Montreal
Flight plan
IFR

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
46
Certificate
Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
6,000 total · 500 in this make and model

Weather

Conditions
Instrument (IMC) · Night/dark
Wind
230° at 5 knots
Visibility
8 statute miles
Lowest ceiling
600 ft overcast
Temperature
135 °F, dew point 135 °F
Altimeter
29.00 inHg
Observed at
HUL, 8 nm away