ANC14CA012

NTSB accident investigation · Douglas DC-6 · Nuiqsut, AK · November 25, 2013

Accident · No injuriesData collectionFinal report
Date
November 25, 2013, 10:21 local (14:21 UTC)
Place
Nuiqsut, AK
Injuries
3 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N100CEDouglas DC-6
Defining event
Takeoff: Miscellaneous/other
Weather
Visual (VMC) · Night
Status
Completed · report April 23, 2014
Report
Approved by Office Director
NTSB office
Alaska Regional Office
Parties
FAA
FAA report
20131125025379A
Case key
88574

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

On this page

Probable cause

A load shift during takeoff, which resulted in substantial damage to the aft bulkhead and associated structures.

Findings · 1

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Equipment/furnishings: cargo compartmentsAircraft › Aircraft systems · Incorrect use/operationDouglas C-118A: 1 caseAll aircraft: 2 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

According to the operator, the purpose of the short, 22 minute flight was to deliver a load of oversized, oil drilling tools to a remote oil production site. The flightcrew reported that shortly after takeoff the first officer noticed that the airplane's elevator control movements appeared to be "momentarily stiff." While en route to the destination, the flight engineer was asked to inspect the cargo, and he subsequently discovered that two of the four, 31-foot long oil drilling tools had shifted aft, damaging the aft pressure bulkhead. The captain did not declare an emergency, and the airplane landed at the destination without incident. A postflight inspection revealed substantial damage to the aft pressure bulkhead assembly, as well as various frames, stringers and structural longerons. In addition, several attachments for the elevator flight control pulleys and flight control cable guides were damaged. The operator noted that the airplane's pressurization system had been removed years ago, when the airplane was converted to a cargo configuration. The operator reported that after loading the airplane, just before departure, the crew inspected the five nylon strapping mechanisms that secured the four drilling tools to the floor of the airplane. The crew reported that all five of the nylon straps were tight before departure, but gathered that one or more had loosened slightly during taxi and takeoff, allowing two of the tools to shift aft during takeoff. The crew also noted that the drilling tools were covered with ice and snow, which likely aided in the tools sliding along the aluminum, diamond plate-covered floor of the airplane.

Factual narrative

According to the operator, the purpose of the short, 22 minute flight was to deliver a load of oversized, oil drilling tools to a remote oil production site. The flightcrew reported that shortly after takeoff the first officer noticed that the airplane's elevator control movements appeared to be "momentarily stiff." While en route to the destination, the flight engineer was asked to inspect the cargo, and he subsequently discovered that two of the four, 31-foot long oil drilling tools had shifted aft, damaging the aft pressure bulkhead. The captain did not declare an emergency, and the airplane landed at the destination without incident. A postflight inspection revealed substantial damage to the aft pressure bulkhead assembly, as well as various frames, stringers and structural longerons. In addition, several attachments for the elevator flight control pulleys and flight control cable guides were damaged. The operator noted that the airplane's pressurization system had been removed years ago, when the airplane was converted to a cargo configuration. The operator reported that after loading the airplane, just before departure, the crew inspected the five nylon strapping mechanisms that secured the four drilling tools to the floor of the airplane. The crew reported that all five of the nylon straps were tight before departure, but gathered that one or more had loosened slightly during taxi and takeoff, allowing two of the tools to shift aft during takeoff. The crew also noted that the drilling tools were covered with ice and snow, which likely aided in the tools sliding along the aluminum, diamond plate-covered floor of the airplane.

Aircraft

Registration
N100CE
Reported as
Douglas DC-6
Category
Airplane
Serial number
44662
Built
1953
Airframe hours
32,042
Engine
Pratt & Whitney R-2800, 2,000 horsepower, reciprocating
Damage
Substantial damage
Flight
Part 121
Operator
Tatonduk Outfitters Ltd, doing business as Everts Air Cargo
Registered owner
Tatonduk Outfitters Ltd
Airworthiness certificate
Standard, Transport
Last inspection
Continuous airworthiness · November 21, 2013
Departed
AK15 · Nuiqsut, AK
Destination
PASC · Deadhorse, AK
Flight plan
IFR
Airport
AK15 · Alpine Airstrip, runway 03, 5,005 × 100 ft, gravel

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew · 3

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
50
Injuries
None
Certificates
Airline transport, Flight engineer
Airplane ratings
Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, Without waivers/limitations
Last flight review
November 1, 2013
Seat
Left
Restraint
4-point
Flight hours
14,100 total · 12,100 in this make and model · 9,100 as pilot in command · 115 in the last 90 days · 47 in the last 30 days · 2 in the last 24 hours
Role
Co-pilot
Age
52
Injuries
None
Certificates
Airline transport, Flight engineer
Airplane ratings
Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, With waivers/limitations
Last flight review
June 13, 2013
Seat
Right
Restraint
4-point
Flight hours
4,516 total · 968 in this make and model · 160 in the last 90 days · 45 in the last 30 days · 2 in the last 24 hours
Role
Flight engineer
Injuries
None
Certificates
Flight engineer, Commercial
Seat
Center
Restraint
4-point

Weather

Conditions
Visual (VMC) · Night
Wind
210° at 10 knots
Visibility
4 statute miles
Lowest ceiling
1,100 ft overcast
Temperature
-6 °F, dew point -8 °F
Altimeter
30.32 inHg

Docket · 2

The files NTSB released with the investigation on April 7, 2014, on NTSB’s docket system: statements, records, photos and specialists’ reports. 767 KB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.