N7946C is a 1944 North American B-25N. It is a fixed-wing multi-engine aircraft with 6 seats, powered by a Wright R-2600 SER rated at 1700 horsepower. The registration is active, with the registrant based in Latham, NY. Its limited airworthiness certificate was issued in Sep 1995. It has been registered to its current owner since Sep 2019. This page also carries 1 NTSB event.
- 82 years old
- Only 10 North American B-25N here
2019
1995
That's everything on file so far — TailWiki checks the FAA registry daily and adds new entries as N7946C's record changes.
On September 19, 2020, about 1925 Pacific daylight time, a North American B-25N, N7946C, was substantially damaged when it was involved in an accident near Stockton, California. The copilot and the passenger sustained serious injuries, and the pilot sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations 91 personal flight.
The airplane had made two previous flights on the day of the accident (as discussed later in this section.) For the accident flight, the pilot (who was in the right seat and not flying at the time) reported that, while the airplane was in cruise flight at 1,500 ft mean sea level (msl) and about 7 miles from its intended destination, the left engine fuel pressure fluctuated, and the left engine lost power momentarily but resumed operation. The pilot saw that the fuel pressure needle returned to normal, but he was concerned that an engine-driven fuel pump might have failed. The pilot subsequently turned the boost pumps to high and asked the passenger to open the fuel cross-feed valve. When the airplane was about 6 miles from its intended destination, both fuel pressure needles began to fluctuate. The pilot assumed that fuel starvation to the engines had occurred and decided to make an off airport landing to a field behind the airplane’s position due to residential areas between the location and the airport. The pilot stated that he took control of the airplane from the copilot (who was in the left seat) and initiated a right turn toward the field. Shortly afterward, the fuel pressure dropped below 10 pounds per square inch, and both engines lost power.
The right-seat pilot stated that, during the rollout after landing in the field, he observed ditches in front of the airplane. He was able to get the airplane airborne briefly to avoid one ditch but was not able to avoid a second large ditch. Subsequently, the airplane struck the second ditch, became airborne, and impacted the ground in a nose-low attitude. All three landing gear collapsed.
In postaccident statements, the pilot reported that he used a 150-gallons-per-hour fuel burn for flight planning purposes, which included the takeoff fuel burn. The pilot also stated that, before the accident flight, neither he nor the other airplane occupants had visually verified the fuel levels in the fuel tanks.
The copilot reported that, when he boarded the airplane before the flight, he questioned the pilot about the fuel level and was told that it was calculated to be more than 200 gallons of fuel, which was more than enough for the 20-minute flight. The copilot provided a photograph from inside the airplane before the loss of power, which showed a power setting of about 1,700 rpm and 27 inches of manifold pressure. The photograph also captured the front and aft fuel tank gauges. The front tank fuel gauges showed about 70 gallons on the left side and about 55 gallons on the right side. The aft gauges displayed 0 and were fully deflected to the bottom for both the left and right sides.
The passenger, who was also the airplane’s mechanic, reported that, when the airplane was topped off with fuel at Brown Field (SDM), San Diego, California, the fuel level was about 3 inches below the bottom of the fuel filler neck. He further reported that. when he had arrived at Vacaville Airport (VCB), Vacaville, California, he was told to board the accident airplane and prepare for departure. The passenger stated that, because he had rushed into the airplane, he did not accomplish his normal routine, which included checking fuel and oil levels. The passenger stated that he "always tops the tanks off, either to the top or maybe 2.5 inches from the top of the filler neck.”
Refueling records showed that the airplane had been last refueled on September 18, 2020, with 497.7 gallons of fuel. No evidence showed the fuel level after refueling.
Automatic dependent surveillance-broadcast (ADS-B) data showed six flights since the airplane was refueled, as shown in table 1. The ADS-B times listed do not account for operational time before takeoff and after landing.
Date
Departure
Destination
Flight Time (minutes)
September 18, 2020
North Island Naval Air Station (NZY), San Diego, California
8
September 18, 2020
Local
33
September 19, 2020
Local
19
September 19, 2020
Chino Airport (CNO), Chino, California
38
September 19, 2020
127
September 19, 2020
Stockton, California
16
Total Flight Time:
241 Minutes
Table 1. Accident airplane flights after refueling.
The airplane was equipped with two interconnected forward and aft main fuel tanks in each wing, which could hold a total of 670 gallons of fuel. The flight handbook for the accident airplane stated, in part, “useable fuel is slightly less than quantity listed.” Recovery company personnel reported that, during the recovery of the wreckage, about 1 gallon of fuel was removed from each forward and aft wing fuel tank.
The pilot provided more detailed postaccident calculations of the accident airplane’s fuel burn, which indicated that the airplane would have used 485.9 gallons of fuel after the airplane had been last refueled (not including fuel usage for taxi and runup). The pilot reported that he used power settings of 30 inches of manifold pressure and 2,000 rpm for takeoff and 20 inches manifold pressure and 1,800 rpm for cruise flight. The flight handbook for the accident airplane model contained no specific data for performance charts and fuel burn data for the pilot’s power settings in cruise flight at the altitudes flown (as shown in the ADS-B data for the accident flight).
Postaccident examination of the recovered wreckage revealed that the fuselage was substantially damaged. The left and right forward and aft main fuel tanks were undamaged. Both main forward and main aft fuel gauges were removed from the instrument panel and connected to their respective center section wiring with external power applied. Each fuel tank was subsequently filled with water, and fuel gauge indications were captured at various water levels. All four fuel gauges displayed erroneous indications at almost all levels measured. No leaks were observed throughout the fuel system. Table 2 shows the fluid levels that were captured at the top and bottom of each fuel pickup port for all four fuel tanks.
Fuel tank
Bottom of pickup port (gallons)
Top of pickup port (gallons)
Left forward
1.1
14.3
Left aft
1.5
7.0
Right forward
1.5
14.3
Right aft
1.2
7.0
Table 2. Fuel tank fluid levels during postaccident examination.
Impact damage to both carburetors precluded a functional check and a determination of the fuel flow setting.
No photos yet. Sign in to add the first one.