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N586P accident description

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Crash location Unknown
Nearest city Florence, KY
38.998950°N, 84.626611°W

Tail number N586P
Accident date 13 Aug 2004
Aircraft type Convair Div. of Gen. Dynamics CV-340 (580)
Additional details: None

NTSB description

The Board's full report is available at, AAR-06/03, PB2006-910403.

On August 13, 2004, about 0049 eastern daylight time,1 Air Tahoma, Inc., flight 185, a Convair 580, N586P, crashed about 1 mile south of Cincinnati/Northern Kentucky International Airport (CVG), Covington, Kentucky, while on approach to runway 36R. The first officer was killed, and the captain received minor injuries. The airplane was destroyed by impact forces. The flight was operating under the provisions of 14 Code of Federal Regulations (CFR) Part 121 as a cargo flight for DHL Express2 from Memphis International Airport (MEM), Memphis, Tennessee, to CVG. Visual meteorological conditions prevailed for the flight, which operated on an instrument flight rules flight plan.

The flight crew was scheduled to fly the accident airplane on a roundtrip sequence from MEM to CVG.3 Flight 185 departed MEM about 2329. The first officer was the flying pilot, and the captain performed the nonflying pilot duties. During postaccident interviews, the captain stated that the takeoff and climb portions of the flight were normal.

According to the cockpit voice recorder (CVR) transcript, at 0017:49, the captain stated that he was just going to "balance out the fuel here."4 The first officer acknowledged. From 0026:30 to 0027:08, the CVR recorded the captain discussing the airplane's weight and balance with the first officer. Specifically, the captain stated, "couldn't figure out why on the landing I was out and I was okay on the takeoff." The captain added, "the momentum is one six six seven and I…put one zero six seven and I couldn't work it." He then stated, "so…we were okay all along."

At 0030:40, the first officer stated, "weird." At 0032:31, the captain stated, "okay just let me finish this [the weight and balance paperwork] off and…I'm happy," and, about 2 minutes later, he stated, "okay, back with you here." At 0037:08, the captain contacted Cincinnati Terminal Radar Approach Control (TRACON) and reported an altitude of 11,000 feet mean sea level.6 About 1 minute later, the first officer stated, "something's messed up with this thing," and, at 0039:07, he asked "why is this thing?" At 0041:21, the first officer stated that the control wheel felt "funny." He added, "feels like I need a lot of force. it is pushing to the right for some reason. I don't know why…I don't know what's going on." The first officer then repeated twice that it felt like he needed "a lot of force." The CVR did not record the captain responding to any of these comments.

At 0043:53, when the airplane was at an altitude of about 4,000 feet, the captain reported to Cincinnati TRACON that he had the runway in sight. The approach controller cleared flight 185 for a visual approach to runway 36R and added, "keep your speed up." The captain acknowledged the clearance and the instruction. The first officer then stated, "what in the world is going on with this plane? sucker is acting so funny." The captain replied, "we'll do a full control check on the ground." At 0044:43, the approach controller again told the captain to "keep your speed up" and instructed him to contact the CVG Air Traffic Control Tower (ATCT).

At 0045:11, the captain contacted the CVG ATCT and requested clearance to land on runway 36R, and the local control west controller issued the landing clearance. Flight data recorder (FDR) data indicated that, shortly afterward, the airplane passed through about 3,200 feet, and its airspeed began to decrease from about 240 knots indicated airspeed. At 0045:37, when the airplane was at an altitude of about 3,000 feet, the captain started the in-range checklist,8 stating, "bypass is down. hydraulic pressure. quantity checks. AC [alternating current] pump is on. green light. fuel panel. boost pumps on."

About 0046, the first officer stated, "I'm telling you, what is wrong with this plane? it is really funny. I got something all messed up here." The captain replied, "yeah." The first officer then asked, "can you feel it? it's like swinging back and forth." The captain replied, "we've got an imbalance on this…crossfeed I left open." The first officer responded, "oh, is that what it is?" A few seconds later, the first officer stated, "we're gonna flame out." The captain responded, "I got the crossfeed open. just keep power on."

At 0046:45, the CVR recorded a sound similar to decreasing engine rpm. Immediately thereafter, the first officer stated, "we're losing power." At 0046:52, the first officer stated, "we've lost both of them. did we?" The captain responded, "nope." FDR data showed that, about 1 second later, a momentary electrical power interruption occurred when the airplane was at an altitude of about 2,400 feet. At 0046:55, the CVR stopped recording. Airplane performance calculations indicated that, shortly after the power interruption, the airplane's descent rate was about 900 feet per minute (fpm).

According to air traffic control (ATC) transcripts, at 0047:12, the captain reported to the CVG ATCT that the airplane was "having engine problems." The local control west controller asked, "you're having engine problems?" The captain replied, "affirmative." At 0047:28, the controller asked the captain if he needed emergency equipment, and the captain replied, "negative.'" This was the last transmission received by ATC from the accident flight crew. The FDR continued recording until about 0049. The wreckage was located about 1.2 miles short of runway 36R.


1. The captain and first officer were properly certificated and qualified under Federal regulations.

2. No evidence indicated that flight crew fatigue was a factor in this accident, and no evidence indicated any preexisting medical or behavioral conditions that might have affected the accident flight.

3. The airplane was properly maintained in accordance with Federal regulations and approved company procedures.

4. The recovered components showed no evidence of any preexisting powerplant, system, or structural failures. No evidence indicated that any of the airplane's cargo shifted during the flight.

5. Neither the weather nor the inoperative distance measuring equipment on the Cincinnati/Northern Kentucky International Airport very high frequency omnidirectional range was a factor in this accident.

6. Sufficient fuel was on board the airplane for the flight from Memphis International Airport to Cincinnati/Northern Kentucky International Airport.

7. The captain's preflight weight and balance calculations indicated that the airplane was not within takeoff limits; therefore, he should not have allowed the airplane to take off. However, the captain's calculations were incorrect, and the airplane's weight and balance were within limits.

8. The captain did not recognize the importance of the cues provided by the first officer, and he failed to perform expected pilot-in-command duties.

9. The captain was preoccupied with the weight and balance calculations during critical portions of the flight and, as a result, he did not monitor the fuel crossfeed operations, which resulted in a fuel imbalance and unusual airplane handling characteristics.

10. The flight crew did not monitor the fuel quantity gauges or respond properly to the airplane's changing handling characteristics, and the captain did not start the in-range checklist at the appropriate altitude; as a result, the crew missed several opportunities to identify the ongoing fuel crossfeed operations and determine that the airplane's fuel was imbalanced.

11. Although fuel transfer is prohibited on the Convair 580 airplane, fuel transfer can occur during fuel crossfeed operations if the fuel tank shutoff valve for the tank not being used is left open.

12. All of the fuel from the airplane's left tank that was not used by the engines transferred into the right tank because the captain intentionally kept the right fuel tank shutoff valve open during fuel crossfeed operations, which was not in accordance with approved fuel crossfeed procedures.

13. During the airplane's descent to landing, the fuel in the left fuel tank, which was providing fuel to both engines, was exhausted because both engine-driven fuel pumps drew air from the left tank into the fuel system instead of fuel from the right tank, resulting in a dual-engine flameout.

14. Fuel transfer can occur on the Convair 580 airplane if it is operated with different fuel boost pump output pressure settings and with the fuel crossfeed valves unintentionally left open.

15. The accident investigation would have benefited from the retrofit of an independent cockpit voice recorder power source and a cockpit image recorder.

(c) 2009-2018 Lee C. Baker / Crosswind Software, LLC. For informational purposes only.