Crash of a Piper PA-31-350 Navajo Chieftain in Sanikiluaq

Date & Time: Jan 20, 1998
Operator:
Registration:
C-FDNF
Flight Phase:
Survivors:
Yes
Schedule:
Sanikiluaq – Iqaluit
MSN:
31-8252042
YOM:
1982
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2800
Captain / Total hours on type:
1000.00
Circumstances:
The Piper Navajo Chieftain PA-31-350, serial number 31-8252042, was on an instrument flight rules (IFR) flight from Sanikiluaq to Iqaluit, Northwest Territories. Two pilots and two passengers were on board. After checking the runway condition and weather, the pilot commenced his take-off run on runway 27. After take-off, the pilot saw flames coming out of the right engine cowl. The right engine was shut down but the aircraft could not maintain a sufficient rate of climb, and it crashed on flat, snow-covered ground about one mile from the end of the runway. The aircraft sustained substantial damage on landing. After the aircraft came to a stop, the occupants evacuated via the left front door and walked back to the airport terminal for shelter and assistance. There were no injuries. The occurrence happened at night in instrument meteorological conditions.
Probable cause:
A modification to the cabin heating unit inconsistent with the manufacturer's recommendations and aviation regulations caused an engine fire in the right engine cowl during the initial climb. The pilot shut down the engine, but the aircraft could not maintain a positive rate of climb and crashed to the ground.
Final Report:

Crash of a Swearingen SA26T Merlin IIA in Whale Cove

Date & Time: Jun 20, 1996 at 1905 LT
Type of aircraft:
Operator:
Registration:
C-GTHN
Flight Type:
Survivors:
Yes
MSN:
T26-016
YOM:
1968
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After landing at Whale Cove Airport, the aircraft deviated to the left after a course of about 1,600 feet. It veered off runway, lost its undercarriage and came to rest. Both pilots escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
The aircraft deviated from the runway centerline after landing due to strong crosswinds gusting up to 31 knots. The certification limit for the aircraft in such conditions was 22 knots.

Crash of a De Havilland DHC-6 Twin Otter 100 on Baffin Island

Date & Time: Mar 6, 1993
Operator:
Registration:
C-FQBT
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
95
YOM:
1968
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
While taking off from an icy lake, the nose gear struck an ice ridge. The aircraft went out of control and collided with the river bank before coming to rest. Both pilots were slightly injured and the aircraft was damaged beyond repair. The accident occurred at 69°58'00.0"N 76°59'00.0"W.

Crash of a Lockheed C-130 Hercules near Alert: 5 killed

Date & Time: Oct 30, 1991 at 1640 LT
Type of aircraft:
Operator:
Registration:
130322
Flight Type:
Survivors:
Yes
Schedule:
Edmonton - Thule - Alert
MSN:
4192
YOM:
1967
Flight number:
Boxtop22
Country:
Crew on board:
5
Crew fatalities:
Pax on board:
13
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
Every year, in the cold and darkness of late October, personnel at Canadian Forces Station Alert on Ellesmere Island, Nunavut, gather at a cairn near the runway to remember the crew and passengers of Hercules 130322 who lost their lives during a resupply mission to the station. On October 30, 1991, at approximately 4:40 p.m., flight 22 of Operation Boxtop – as the biannual resupply mission is called – was on its final approach to the station from Thule Air Force Base in Greenland. As the CC-130 Hercules from 435 Transport and Rescue Squadron, loaded with 3,400 litres of diesel fuel, began its descent, the pilot flying lost sight of the runway. Moments later, radar contact and communication were lost as the aircraft crashed approximately 16 km south of the station. The crew of another CC-130 Hercules, also bound for Alert, saw the fires of the crash and identified the location of Boxtop 22. The crash took the lives of five Canadian Armed Forces members – four died in the crash and one perished before help arrived – and led to the boldest and most massive air disaster rescue mission ever undertaken by the Canadian military in the High Arctic. Thirteen lives were saved. Within a half hour of the rescue call, a Hercules carrying 12 search and rescue technicians from 440 Search and Rescue Squadron in Edmonton, Alberta, was in the air. It reached the crash site seven and a half hours later, but the SAR technicians couldn’t descend due to the weather. Another Hercules from 413 Search and Rescue Squadron in Greenwood, Nova Scotia, soon joined the search. Meanwhile, search and rescue technicians formed a ground rescue team at Alert and set out overland for the crash site, guided through the darkness and horrendous weather conditions by a Hercules. The survivors, some soaked in diesel fuel, endured high winds and temperatures between -20C and -30C. Many sheltered in the tail section of the downed aircraft but others were more exposed to the elements. Finally, the 413 Squadron team finally got a break in the weather and six SAR technicians parachuted into the site more than 32 hours after the crash and began looking for survivors. They were joined soon after by more SAR technicians. When the ground rescue team finally arrived – 21 hours after it had set out – 26 rescuers were on the ground. They warmed and treated the injured and prepared them for medical evacuation. A Twin Huey helicopter from Alert made three trips to bring the survivors back to the station. Once again this year, personnel at Alert will conduct a parade on October 30 to commemorate the crash. The parade will begin at 4:30 p.m. and continue through the 4:40 p.m. timing when the crash occurred.
Those killed were:
Cpt John Couch, pilot,
Cpt Judy Trépanier, logistics officer,
M/WO Tom Jardine, regional services manager CANEX,
W/O Robert Grimsley, supply technician,
M/Cpl Roland Pitre, traffic technician.
Those who survived were:
Robert Thomson,
Susan Hillier,
Cpt Richard Dumoulin, logistics officer,
Cpt Wilma DeGroot, doctor,
Lt Joe Bales, pilot,
Lt Mike Moore, navigator,
M/WO Marc Tremblay, supply technician,
Sgt Paul West, flight engineer,
M/Cpl Tony Cobden, communications researcher,
M/Cpl David Meace, radio technician,
M/Cpl Mario Ellefsen, communications researcher,
M/S “Monty” Montgomery, communications researcher,
Pvt Bill Vance, communications researcher.
Source:
http://www.rcaf-arc.forces.gc.ca/en/article-template-standard.page?doc=remembering-the-crash-of-boxtop-flight-22/ig9v1k0t
Final Report:

Crash of a Piper PA-31-310 Navajo in Rankin Inlet: 5 killed

Date & Time: Nov 12, 1986
Type of aircraft:
Registration:
C-FBBR
Flight Phase:
Survivors:
No
MSN:
31-377
YOM:
1968
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
Crashed for unknown reasons shortly after takeoff from Rankin Inlet Airport, killing all five occupants.

Crash of a Beechcraft B90 King Air on Belcher Island: 3 killed

Date & Time: Dec 22, 1984
Type of aircraft:
Operator:
Registration:
C-GPPN
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Sanikiluaq – Churchill
MSN:
LJ-389
YOM:
1968
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The twin engine aircraft departed Sanikiluaq Airport on an ambulance flight to Churchill, MB. In unknown circumstances, it crashed on Belcher Island, about 45 km southeast of Sanikiluaq Airport. Both pilots and the medevac passenger were killed.

Crash of a Lockheed 18 Learstar II in Nanisivik

Date & Time: Aug 12, 1984
Type of aircraft:
Operator:
Registration:
C-FOZO
Survivors:
Yes
MSN:
18-2209
YOM:
1942
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The undercarriage collapsed upon landing at Nanisivik Airport. There were no casualties but the aircraft was damaged beyond repair.
Probable cause:
Undercarriage failure upon landing for unknown reasons.

Crash of a De Havilland DHC-6 Twin Otter 300 in Frobisher Bay: 9 killed

Date & Time: Aug 29, 1979 at 2305 LT
Operator:
Registration:
C-GROW
Survivors:
No
Schedule:
Brevoort Island - Frobisher Bay
MSN:
415
YOM:
1974
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
9
Captain / Total flying hours:
3729
Captain / Total hours on type:
476.00
Copilot / Total flying hours:
2600
Copilot / Total hours on type:
323
Aircraft flight hours:
5286
Circumstances:
The airplane was being used for a series of flights between Frobisher (YFB) and Brevoort Island, a distance of 119 NM. These flights were conducted under visual flight rules (VFR) with a Flight Notification filed at Frobisher. Two return flights were accomplished without incident and the aircraft was flown back to Brevoort for another round trip. On the final flight the aircraft, with the same two pilots and with seven passengers, left Brevoort at 21:57 hours local time enroute to Frobisher. The pilots contacted Frobisher Flight Service Station (FSS) at 22:31 reporting at 6000 feet altitude estimating Frobisher in 15 minutes. Upon receiving the latest weather indicating conditions below VFR limits, they requested clearance for 'Special VFR'. This clearance was granted. Another weather report was transmitted by the Frobisher FSS giving the 22:44 observation in which the ceiling had lowered to 400 ft with the visibility at 8 miles and the wind from 190 deg M at 22 knots. The pilot stated they would make a front course ILS approach to runway 36 with a landing on 18. At 22:58 they were issued a clearance for an ILS approach. They subsequently reported outbound at procedure turn altitude and at that time confirmed their planned approach for runway 36 with circling for 18. This was the last radio transmission from C-GROW. The Twin Otter was seen flying north along the runway. It then struck high ground about 1,200 feet east of the runway and about 100 feet above runway level. The aircraft was destroyed and all nine occupants were killed.
Probable cause:
The following findings were identified:
- Three other aircraft made successful downwind landings on runway 36; one before and two after the accident flight.
- For undetermined reasons, the crew of C-GROW, following their instrument landing approach, decided not to land on runway 36 with the strong tailwind and elected to circle for runway 18.
- The weather was below circling limits.
- The crew attempted a circling approach at low altitude at night on the non maneuvering side of the runway.
- The aircraft struck the ground while under control during flight in restricted visibility.
Final Report:

Crash of a De Havilland DHC-6 Twin Otter 300 in Frobisher Bay: 1 killed

Date & Time: Aug 23, 1978
Operator:
Registration:
CF-QDG
Survivors:
Yes
MSN:
246
YOM:
1969
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
On final approach to Frobisher Bay Airport, while passing 40 feet over the runway threshold, the twin engine airplane rolled to the left and descended out of control, causing the left wing to struck the ILS antenna. The left engine was torn off and the airplane crashed nose first and came to rest upside down on the left side of the runway. Five occupants were injured while one the pilot was killed.

Crash of a De Havilland DHC-6 Twin Otter 300 in Nanisivik: 8 killed

Date & Time: Dec 21, 1977 at 1504 LT
Operator:
Registration:
C-FABW
Survivors:
No
Schedule:
Pond Inlet – Nanisivik – Resolute Bay
MSN:
278
YOM:
1970
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
8
Captain / Total flying hours:
12534
Captain / Total hours on type:
3000.00
Circumstances:
The aircraft was on a return flight between Resolute Bay, Nanisivik and Pond Inlet. The first two legs of the flight had been completed and the aircraft had been refueled at Pond Inlet. The return flight to Nanisivik was flown at 8,000 feet and all reports and radio transmissions were routine. The last transmission to the radio operator at Nanisivik made by the First Officer was 'a couple of miles back on left base and will be turning final shortly', which indicated that they were doing a night visual approach. A final wind check was passed to the aircraft but no acknowledgement was received. A witness to the accident described the aircraft as 'moving in a violent fashion' before it crashed 2,200 feet short of the runway in a 45° nose down, 80° right bank attitude. All eight occupants were killed.
Probable cause:
Examination of the weather aftercast indicated that low level turbulence and vertical windshear of 10 to 12 knots per thousand feet existed at the time of the accident. Other aircraft reported varying degrees of turbulence on final approach to the- runway both before and after the accident. Technical investigation suggests that the right engine was rotating at or below flight idle at impact. Extensive laboratory analysis of the engine components ‘failed to prove conclusively that an engine failure had actually occurred and until further evidence is forthcoming the accident cause must. remain undetermined. (LP 39/78, LP 40/78, LP 78/78, LP 89/78) Note: Thirteen months after this accident occurred evidence first began to emerge pertaining to possible in-flight failure of DHC-6 flap and aileron control rods. Recovery of a failed flap rod from the bottom of Vancouver Harbour 26 Jan 1979 and a failed aileron rod recovered at Sechelt, B.C., 30 Sept 79, from two aircraft which had crashed under very similar circumstances to that of CF-ABW, led to a decision to re-open this investigation. Negotiations and financial arrangements to recover and re~examine the buried aircraft structure were initiated during February 1980 with a target date between mid July and mid-August. As the aircraft had been burned, crushed by a bulldozer, partially scattered and buried under 20 ft of shale in the Nanisivik dump the projected recovery attempt would have been futile. This decision was made on 17 July 1980. In view of the fact that the safety deficiency related to stress corrosion control rod failure had been identified and rectified by AWD action as a result of subsequent DHC-6 accidents it was deemed that no useful accident prevention purpose would be served in pursuing this accident further.
Final Report: