De Havilland DHC-2 N9878R
19 July 2018 · Willow, Alaska, United States · Fatal
Summary
On 19 July 2018 at about 03:00 local time, a De Havilland DHC-2 registered N9878R, operated by Alaska Skyways, Inc., was involved in an accident near Willow, Alaska, United States. 4 people were on board and one died, 3 were seriously injured. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.
The record
- Date
- at 03:00
- Classification
- Accident
- Location
- Willow, Alaska, United States
- Nearest airport
- Willow SPB (2X2)
- Coordinates
- 61.7322, -150.0480
- Aircraft
- De Havilland DHC-2
- Registration
- N9878R
- Category
- Airplane
- Year built
- 1956
- Engines
- 1
- Operator
- Alaska Skyways, Inc.
- Operating rule
- Part 135: Air Taxi & Commuter
- Phase of flight
- Not recorded
- Route
- Willow → Skwentna
- Aircraft damage
- Destroyed
- Weather
- VMC
- Light
- Day
- NTSB number
- ANC18FA055
People
1 person died.
| On board | Died | Serious | Minor | Uninjured |
|---|---|---|---|---|
| 4 | 1 | 3 | 0 | 0 |
Probable cause
The pilot's exceedance of the airplane's critical angle of attack during departure climb, which resulted in an aerodynamic stall. Contributing to the accident was the pilot's improper decision to load the airplane beyond its allowable gross weight and center of gravity limits, coupled with his lack of operational experience in the airplane make, model, and configuration.
Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.
Read the full NTSB narrative
The pilot was conducting an on-demand air taxi flight in a float-equipped airplane from a seaplane base on a public lake to a remote lakeside home, with a passenger and her young son. The passenger brought cargo to transport as well, including an unexpected 800 lbs of mortar bags. Witnesses who labored to push the airplane out after loading reported that the airplane appeared very aft heavy and the pilot said he would offload "cement blocks" if he could not take off. A review of witness videos revealed that the pilot attempted one takeoff using only 3/4 of the available waterway, then step taxied around the lake and performed a step-taxi takeoff, again not using the full length of the lake. The airplane eventually lifted off, and barely climbed over trees on the south end of the lake, before descending and impacting terrain. A home surveillance video that captured the airplane seconds before the crash revealed that 3 seconds before ground impact, the estimated altitude of the airplane was 115 ft above ground level (agl) and the groundspeed was about 64 miles per hour (mph), which was low and much slower than normal climb speed (80 mph). As the airplane banked to the left to turn on course, it rolled through 90° likely experiencing an aerodynamic stall. Analysis of the engine rpm sound revealed that the engine was operating near maximum continuous power up until impact, and a postaccident examination of the airframe and engine revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation. A calculation performed by investigators postaccident revealed the airplane's estimated gross weight at the time of the accident was 75 lbs over the approved maximum gross takeoff weight, and the airplane's estimated center of gravity was 1.76 inches aft of the rear limit. The pilot had been recently hired by the operator and he flew his first commercial flight in the same make and model, float-equipped airplane the week before the accident. He had accumulated 12.9 flight hours, and 13 sea landings/takeoffs in the accident model airplane since being hired as a part-time pilot. Although the airplane was able to takeoff, the aircraft's out-of-limit weight-and-balance condition increased its stall speed and degraded its climb performance, stability, and slow-flight characteristics. When the pilot turned the airplane left, the critical angle of attack was exceeded resulting in an aerodynamic stall at low altitude. If the pilot had performed a proper weight and balance calculation, he may have recognized the airplane was overweight and out of balance and should not have attempted the flight without making a load adjustment.
Quoted verbatim from the NTSB record.
Other De Havilland DHC-2 accidents
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 24 Sep 2018 | De Havilland DHC 2 MK. I(L20A) | Kukaklek Lake, Alaska, United States | T-Corp | Minor injuries | - |
| 5 Aug 2018 | De Havilland DHC-2 | Talkeetna, Alaska, United States | K2 Aviation | Fatal | 5 |
| 23 Jun 2018 | De Havilland DHC-2 | Dillingham, Alaska, United States | - | Serious injuries | - |
| 20 Sep 2018 | De Havilland DHC 2 | Igiugig, Alaska, United States | - | Minor injuries | - |
| 13 May 2019 | De Havilland DHC-2 | Ketchikan, Alaska, United States | Mountain Air Service LLC | Fatal | 6 |
| 20 May 2019 | De Havilland DHC 2 | Metlakatla, Alaska, United States | Venture Travel, LLC | Fatal | 2 |
Other accidents in this area
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 22 Aug 2018 | Cessna A185F | Kaktovik, Alaska, United States | - | No injuries | - |
| 30 May 2018 | Cessna 180 | Kake, Alaska, United States | - | No injuries | - |
| 16 Jul 2018 | Piper PA18S | Palmer, Alaska, United States | - | No injuries | - |
| 20 Aug 2018 | Piper PA18 | McGrath, Alaska, United States | - | No injuries | - |
| 16 Jul 2018 | Curtiss-Wright C46 | Manley Hot Springs, Alaska, United States | Everts Air Fuel Inc | Minor injuries | - |
| 3 Oct 2018 | Beechcraft 1900 | Gambell, Alaska, United States | Hageland Aviation | No injuries | - |