MIA98GA069

NTSB accident investigation · Bell UH-1H · Savannah, TN · February 3, 1998

Accident · FatalFinal report
Date
February 3, 1998, 08:50 local (14:50 UTC)
Place
Savannah, TN
Injuries
4 fatal, 1 minor; on the ground: 1 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N30TVBell UH-1H
Weather
Visual (VMC) · Day
Status
Completed · report February 15, 2001
Report
Approved by Office Director
FAA report
19980203000919A
Case key
38406

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

failure of the flight crew to maintain sufficient altitude/clearance from the pole and workman. Related factors were: the gusty wind condition, inadequate communication/coordination between the flight crew and ground personnel, and an improper external system for this type of operation.

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.

In flight collision with objectHover - out of ground effect
Weather condition - gustsFactor
Air/ground communications - inadequateFactor
Crew/group coordination - inadequateFactor
Object - pole
Altitude/clearance - not maintainedFlightcrewCause
Improper use of equipment/aircraftCompany/operator managementFactor
Propeller/rotor contact to personHover - out of ground effect
In flight collision with terrain/waterDescent - uncontrolled

Analysis

Helicopter (hel) was being used to string rope/wires with chief pilot (PIC) in left front seat, copilot in right front seat, & 2 observers behind pilots on either side. Witnesses observed hel approach 150' tall pole with a workman at the top. Workman was to connect a rope to a 17' line from the hel which had 600 lbs of weights attached. Foreman in charge of ground operations was observing on ground between his vehicle & the pole. He was not in radio contact with pilots, although vehicle was radio equipped. Witnesses saw hel approach workman & pole from above with hel's nose facing northwest. Wind was from 110 deg at 9 gusting 19 kts. Observers were watching from sides of hel; right observer was providing suggested flight directions for the copilot, who was on the controls. Hel came to a high hover over the pole; workman attempted to attach the rope. Witnesses said hel descended as it drifted left & forward of pole & workman, then it began to back up & climb. Rotor blades struck pole & workman. Hel then rolled right, descended, & impacted ground on its right side. The hook system that was normally used for this type of operation was on another hel & was not available for this mission. Instead, a 'U' shaped swivel hook with a bolt & nut arrangement was used. The normal hook system would have allowed the workman to quickly hook the rope to the hel within seconds. Video tape showed hel hovering above workman & pole for 1-1/4 min until tape stopped (just before accident). Operation Manual required 2-way radio communication between pilot & ground crew (unless otherwise authorized by Manager of Aviation Services). There was no communication between pilot & ground crew from time hel was overhead until accident occurred.

Factual narrative

History of flight

On February 3, 1998, about 0850 central standard time, a Bell UH-1H helicopter, N30TV, operated by the Tennessee Valley Authority (TVA), as a Title 14 CFR Part 91 public-use flight, impacted with a pole near Savannah, Tennessee. Visual meteorological conditions prevailed, and no flight plan was filed. The helicopter was destroyed. Two airline transport pilots, one crewmember observer, and one TVA employee working on the pole, were fatally injured. One observer (a helicopter crewmember) received minor injuries. The flight had originated from Muscle Shoals, Alabama, at 0630, en route to Savannah. The flight was conducted to support a rope stringing and wire installation operation which was being conducted by the TVA.

The helicopter departed from the TVA Air Service hangar with a crew of two, TVA's Chief Pilot and an observer. Two additional crew members, another observer, and a contract pilot, had driven to Savannah earlier and were to meet the helicopter in Savannah. After a 30 minute flight, the helicopter landed at the TVA line maintenance facility, and the crew attended a line installation briefing. The two other crew members were there and they also attended the briefing. The briefing lasted about 30 minutes, and the flight departed at 0730.

The helicopter flew about 1.2 hours stringing ropes/wires before it proceeded to the area where the accident occurred. Ground witnesses observed the helicopter approach a pole with a workman at the top, at a height of about 150 feet above the ground. The workman's task was to attach a conductor pull rope to the end of a 17-foot sling and 600 pound weights, with a shackle assembly, which were suspended from the bottom of the helicopter. Ground witnesses saw the helicopter approach the workman and the pole with the nose of the helicopter heading in a northwest direction. The helicopter came to a high hover over the pole, and the workman attempted to attach the rope. The witnesses said the helicopter began to get lower and lower until the workman could no longer reach the line coming from the helicopter. As the helicopter descended it drifted left and forward of the pole and the workman. The ground witnesses said the helicopter started to back up and climb when the main rotor blades struck the pole and the workman. The helicopter then rolled to the right, descended and impacted the ground on its right side.

The Foreman in charge of the ground operation, who was located close to the pole, identified as STR 51, at the time of the accident, said that before the mission started he talked to the workman that was to climb the pole, to make sure "he was comfortable " with hooking the ropes up. The Foreman was told by the workman, "he had done it before, he wasn't concerned." The Foreman said, "...I had my truck parked right next to STR 51 where I could see everything." He said he talked to the pilot-in-command [PIC], "whom [he] thought was flying the helicopter."

The Foreman said that the first rope that had been strung, had been picked up from a nearby field, and it was then brought to his attention that they might have "trouble" flying the next phase, the bottom, without getting "it bucked." It was decided to "...let [the workman] take [the] rope to the top of the pole to hook to the helicopter." The Foreman said he "discussed it" with the PIC and he replied, "Okay." The workman was at the top of the pole when the helicopter came to a hover over him so that he could hook the rope to the helicopter. The Foreman said, "...from where I was standing it looked like he [the workman] was having a hard time getting the rope hooked. I was still standing between the pole and my truck pacing around. I thought I saw [the workman] just stop and start hugging the pole, because the wind from the helicopter was so strong. I saw men in the helicopter leaning out, (spotters) watching what was going on. For some reason I thought they could see what was going on and they were just going to leave. When I looked back up I saw the 600 lbs. weight...bouncing off [the workman's] back and I knew something was wrong for sure." The Forman then ran to his truck and, "...got on the radio to tell [the PIC] he was too close to my man, that he needed to leave so we could regroup. No sooner than I finished I heard a noise, when I looked up the helicopter had hit the top of the pole with their main rotor...."

According to the TVA Aviation Operation Manual, under the heading External Load Operation, the last paragraph on page 26 states: "...external load operations shall not be conducted unless there are two-way radio communications between the pilot and ground crew unless otherwise authorized by the Manger of Aviation Services. Hand or light signals will not be employed except when initially hooking up or releasing load. In case of radio failure, the pilot in command shall terminate operation until the transceiver is repaired or replaced...." During this operation the Foreman said his radio was in his truck, some distance from where he was positioned. There was no evidence found, that from the time the helicopter arrived at the pole, until the accident had occurred, that there was not any radio communication between the ground and the pilot. In addition, examination of the helicopter's radios did not indicate any discrepancies.

The surviving crew member, who was in the helicopter at the time of the accident, confirmed that their mission that day was to pull rope across the Tennessee River. He said that the helicopter approached the pole centerline, from above the pole. Commands were given by the other observer, located on the right side of the helicopter, to the pilot in the right front seat of the helicopter, who was on the controls. The pilot was told by the right side observer, "...to ease the aircraft down and hold position, along with move left and move right commands. These commands were made to move [the] aircraft wire pulling rigging system even with the top of the pole where a linemen from the ground would be located to connect the rope." He further stated that the workman on the pole, "was unscrewing a pin through a swivel in order to insert [the] loop of the rope and reinstall [the] pin." The weights on the rigging "had settled" on the side of the pole with the helicopter, "drifting just past the pole." "A command was given to ease back to bring the rigging back vertical and [the] weights off the pole." The left side observer said he looked away when, "the linemen lost the swivel." When he looked back down, the helicopter had, "drifted to the left and forward of the pole." The workman and the pole were no longer visible to him from his location in the helicopter.

The surviving crew member described the following events, "...the pilot asked what he needed to do and a command was given to back off and try again...immediately followed with move left command and repeated in about two seconds. Another two seconds past and [the right side observer] yelled left, left, left, left. Immediately following the command I felt and heard both main rotor blades strike the pole. This caused the aircraft to turn 90 degrees to the left and roll hard right."

In addition, after impact the engine was still running. The surviving crew member said, "he moved behind the co-pilot's seat to look for the fuel boost pump cut off switch. The control was not visible...I placed the battery switch in the off position...grabbed the co-pilot's collective control to roll the throttle to flight idle, but it was jammed...I disconnected the battery as I ran around to the opposite side of the aircraft...I moved to where the engine was located and tried to manually move [the] throttle linkage to [the] cut off position, but it was jammed. I went to climb back in the cabin to locate the fuel shut off valve, but [was] told...that the power lines we landed on were hot...I told

Aircraft

Registration
N30TV
Reported as
Bell UH-1H
Category
Helicopter
Serial number
73-21853
Airframe hours
5,331
Engine
Lycoming T53L-13B, 1,250 horsepower, turbo shaft
Damage
Destroyed
Flight
Public aircraft · Part 91
Registered owner
Tennessee Valley Authority
Airworthiness certificate
Standard, Utility
Last inspection
100 hour · November 18, 1997 · 35 hours before
Departed
MSC · Muscle Shoals, AL

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

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
59
Certificate
Airline transport
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Helicopter, Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
12,710 total · 10,000 as pilot in command · 380 in the last 90 days · 70 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
110° at 9 knots, gusting 19
Visibility
10 statute miles
Lowest ceiling
2,400 ft broken
Temperature
48 °F, dew point 43 °F
Altimeter
29.00 inHg
Observed at
SNH, 5 nm away

FAA reports on this event · 1

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