Crash of a Cessna 421B Golden Eagle II off Boston: 2 killed

Date & Time: Mar 2, 1972 at 2011 LT
Registration:
N456CB
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Boston - Teterboro
MSN:
421B-0112
YOM:
1971
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
2559
Circumstances:
The pilot initiated the flight in poor weather conditions. After takeoff from Boston-Logan Airport, while climbing in darkness, foggy conditions and rain falls, the pilot lost control of the airplane that crashed into the Boston harbor. The aircraft sank and both occupants were killed.
Probable cause:
The pilot initiated flight in adverse weather conditions and suffered a spatial disorientation during initial climb. The following factors were reported:
- Low ceiling and fog,
- Visibility below minimums,
- Took off in near zero zero conditions.
Final Report:

Crash of a Cessna 411 in Teterboro: 1 killed

Date & Time: Jan 19, 1971 at 1221 LT
Type of aircraft:
Registration:
N7386U
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Teterboro - Elmira
MSN:
411-0086
YOM:
1965
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
6450
Circumstances:
Shortly after takeoff from Teterboro Airport, while in initial climb, the pilot lost control of the airplane that stalled and crashed in a huge explosion near the runway end. The aircraft was destroyed and the pilot, sole on board, was killed.
Probable cause:
Uncontrolled descent after takeoff following a powerplant failure for undetermined reasons. The following factors were reported:
- The pilot failed to obtain/maintain flying speed,
- The pilot failed to follow the approved procedures,
- Improper emergency procedures,
- Inadequate preflight preparation,
- Complete engine failure on one engine,
- No engine malfunction found,
- Possibly insufficient warm up time,
- The pilot did not maintain single engine speed.
Final Report:

Crash of a Cessna 411 in Teterboro

Date & Time: Dec 6, 1968 at 1702 LT
Type of aircraft:
Operator:
Registration:
N162A
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
411-0219
YOM:
1966
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4900
Captain / Total hours on type:
150.00
Circumstances:
Shortly after takeoff from Teterboro Airport, while in initial climb, one of the engine failed. The pilot lost control of the airplane that crashed in a huge explosion on the apron. The pilot was seriously injured while the Cessna 411 was destroyed by a post crash fire as well as five other aircraft, a Piper PA-28 (N6416W), two Beechcraft 33 (N8822H & N5715V), a Beechcraft 35 (N9575Q) and a fifth aircraft registered N7167N. A sixth airplane registered N8390N was seriously damaged.
Probable cause:
Powerplant failure for undetermined reasons. The following factors were reported:
- The pilot failed to obtain/maintain flying speed,
- Improper emergency procedures,
- Improper single engine procedure.
Final Report:

Crash of a Douglas C-47A-15-DL in Teterboro

Date & Time: Sep 26, 1968 at 1422 LT
Operator:
Registration:
N64423
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
9251
YOM:
1943
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
11345
Captain / Total hours on type:
3808.00
Aircraft flight hours:
52844
Circumstances:
Shortly after takeoff from Teterboro Airport, while climbing, the airplane stalled and crashed near the runway end. The airplane was destroyed and both pilots were injured.
Probable cause:
The accident was probably caused by an inadequate preflight preparation and/or planning on part of the crew. The following factors were considered as contributing:
- The cargo shifted during initial climb to the rear, modifying the CofG,
- The cargo was improperly secured.
Final Report:

Crash of a Lockheed C-60A-1-LO LodeStar in Teterboro

Date & Time: Jan 5, 1954
Type of aircraft:
Operator:
Registration:
N3138
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
18-2262
YOM:
1942
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
At lift off, the right engine failed. The aircraft stalled and crashed. There were no casualties but the airplane owned by Walker P. Inman was destroyed by a post crash fire.
Probable cause:
Failure of the right engine during take off.

Crash of a Douglas C-47A-90-DL in Saint Louis: 6 killed

Date & Time: May 24, 1953 at 0418 LT
Operator:
Registration:
N53596
Flight Type:
Survivors:
Yes
Schedule:
Teterboro – Saint Louis
MSN:
20433
YOM:
1944
Crew on board:
5
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
4641
Captain / Total hours on type:
1361.00
Copilot / Total flying hours:
2729
Copilot / Total hours on type:
789
Aircraft flight hours:
10923
Circumstances:
Meteor Air Transport is an irregular carrier, and in this instance was transporting a Pratt and Whitney R-2800 engine and four company employees from Teterboro, New Jersey, to Oklahoma City, Oklahoma, where the engine was to be installed in a company C-46 aircraft. The flight departed Teterboro for St. Louis, Missouri, at approximately 2300, May 23, 1953, on a VFR Flight Plan filed by Captain Harold Carr with an estimated flight time of six and one-half hours. An instrument flight plan filed en route was approved from over Troy, Ohio, intersection via Green Airways 4 to St. Louis, Missouri, cruising at 4,000 feet. The flight proceeded in a routine manner and reported over Terre Haute, Indiana, at 0259, May 24, and at 0324 the following clearance was given to Vandalia radio for delivery to the flight: "ATC clears N 53596 to the Alton intersection to cross Alton at 3,000, Maintain 3,000, no delay expected, contact approach control approaching Alton." At 0357, N 53596 made its initial contact with the St. Louis Tower with the information that it was approaching Alton intersection at 3,000. In reply to an inquiry, N 53596 advised the tower that it carried ILS equipment and was recleared to the ILS Outer Marker 2 to maintain 3,000 with no expected delay and to report when over the Alton intersection. The flight was given the current St. Louis weather: ceiling measured 400 overcast, visibility 3 miles, fog and smoke, altimeter 29.93. It was cleared for an ILS approach to Runway 24 or l2, 3 wind south variable 5, to report leaving 3,000, passing Alton and the Outer Marker. N 53596 reported leaving 3,000 at 0408, passing Alton intersection at 0410 1/2 and inbound over the Outer Marker at 0414. While the controller was watching the approach end of Runway 24 expecting N 53596 to come into view at any moment, a surging of engines was heard; and almost simultaneously a message was received from the flight stating that it was over the field with an engine out. The time as noted by the controller was 0415 at which time all runny and approach lights were turned up to full intensity and the standby emergency alarm sounded. The pilot of the aircraft was advised that the surface winds were calm and to use any runway he could make. Shortly thereafter, the controller for the first and only time observed N 53596 at a position south of the field flying on a southeasterly heading above Natural Bridge Highway which runs parallel to Runway 12. The altitude of the aircraft was estimated at 300 feet and it appeared to be descending with the landing gear in a down position. Upon reaching an altitude of 200 feet, according to the controller, it started a climbing left turn and disappeared in the overcast. Repeated efforts to contact the flight were unsuccessful. It was learned shortly thereafter through the county sheriff's office that the aircraft had crashed adjacent to Brown Road near the McDonnell Aircraft Plant gate number 6. Navy emergency equipment was immediately dispatched to the scene. There was no fire. The occupants of the aircraft were Senior Captain S. J. Rankin, Captain Harold Carr, First Officers Edward J. Raftery and Arthur A. Ravitz, Stewardess Anne Marie Delicata, Superintendent of Maintenance John Swart and Floyd Evans, mechanic. Mr. John Swart was the only survivor.
Probable cause:
The Board determines that the probable cause of this accident was mismanagement of fuel resulting in loss of power and control while circling the field preparatory to an approach for landing. The following findings were pointe out:
- The St. Louis weather given the pilot as he approached the Alton intersection was ceiling 400 overcast, visibility 3 miles, fog and smoke, wind south 5, altimeter 29.93,
- The flight circled the airport in an attempt to remain contact below the authorized minima,
- Mismanagement of fuel resulted in the right engine stopping,
- Ample fuel remained for continued flight at the time of the accident,
- When the pilot was executing a left turn near the southeast corner of the airport, the right engine stopped and the aircraft fell striking the ground on the right wing.
Final Report:

Crash of a Curtiss C-46F-1-CU Commando in Jamaica: 5 killed

Date & Time: Apr 5, 1952 at 0827 LT
Type of aircraft:
Operator:
Registration:
N1911M
Flight Type:
Survivors:
No
Site:
Schedule:
Fort Lauderdale – Charleston – Raleigh – Teterboro
MSN:
22464
YOM:
1945
Flight number:
US4-2
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Captain / Total flying hours:
4760
Captain / Total hours on type:
2225.00
Copilot / Total flying hours:
2000
Copilot / Total hours on type:
246
Aircraft flight hours:
4293
Circumstances:
The flight was designated as No. 4-2 because it was being operated as the second section of a regularly scheduled cargo flight that left Fort Lauderdale, Florida, on April 4. Flight 4-2 departed Fort Lauderdale April 5, 1952, at 0055, with a crew consisting of Captain William B. Crockett, Jr., and Copilot Jack L. Woerderhoff. The destination was Teterboro, New Jersey, with intermediate stops at Charleston. South Carolina, and Raleigh-Durham, North Carolina. The gross weight of the aircraft upon departure was less than the maximum of 48,000 pounds permitted in cargo operations, and the load was placed so that the aircraft's center of gravity was within prescribed limits. This first segment of the flight was conducted according to visual flight rules. It was entirely routine with a landing at Charleston at 0328. Fuel was added but no cargo was loaded or discharged at Charleston. Takeoff from Charleston was at 0410, with a flight plan calling for instrument flight rules. Again the gross weight was less than the allowable and the center of gravity was within prescribed limits. This segment of the flight was also routine, with a landing at Raleigh-Durham at 0524. Again the cargo remained unchanged although 284 gallons of fuel were added. At Rale-gh-Durhan the pilots were briefed at the office of the U. S. Weather Bureau on current and forecast weather conditions over the route. It was indicated that no difficulty should be encountered en route to the New York area, but the ceilings and visibilities there and at Philadelphia, the alternate, would be 800 feet and live miles with heavy rain upon arrival. At 0554 the crew filed a flight plan according to instrument flight rules to cruise from Raleigh-Durham to new York International Airport (Idlewild) at 3,000 feet. The original destination, Teterboro, was changed because of worsening weather there, and the alternate was Philadelphia International Airport. The estimated time en route was two hours and ten minutes. The aircraft carried fuel for four hours' flight. The 0528 weather sequence reported Idlewild, the destination, as 2,100 feet ceiling and 4-mile visibility, and Philadelphia, the alternate, as also above minimums. Upon departure from Raleigh-Durham at 0608 the aircraft's gross weight was about 172 pounds less than its maximum allowable of 48,000 pounds, and its center of gravity was within prescribed limits. The flight proceeded uneventfully at its planned altitude of 3,000 feet. Routine position reports were made through Air Route Traffic Control and arrival over the Idlewild range station was estimated at 0810. At 0809 the flight was instructed by ARTC (Air Route Traffic Control) to climb to 3,500 feet and to contact Idlewild Approach Control when over Scotland Intersection (where the south-west leg of the Idlewild range intersects the southeast leg of the Newark range). The next instruction to the flight was from Idlewild Approach Control and directed it to hold at Scotland at 3,500 feet, and to expect approach clearance at 0828. The flight reported over Scotland at 3,500 feet at 0817. Immediately following the flight was given Idlewild weather as follows: "Weather 0804 time now 0817, measured 500 broken, 1800 overcast, visibility 1 1/2 miles in heavy rain, the altimeter 29.82." The approach controller first saw the flight on the airport surveillance radar (ASR) when it was approaching Scotland. He asked the flight if it could make a straight-in approach from its present position and the flight replied affirmatively. It was then cleared for a straight-in approach, instructed to descend immediately, and to report passing through 2,500 feet. The flight acknowledged and subsequently reported leaving 2,500 feet, and then leaving 2,000 feet. The controller then cleared the flight to continue descent, to advise upon reaching 1,500 feet, and then cleared it to "pass over Runway 4 and make left turn into Runway 13 left." The next contact with the flight was at 0825, when it reported "contact" over the outer marker, located at the Idlewild range station, 2.9 miles from the approach end of Runway No. 4. The local controller then took over control of the flight and advised it to "bear left and make a right turn into Runway 13L, that's the big runway on the north side of the airport, and call base leg coming up on the Federal Building. Go ahead and you'll probably De west of the Federal Building when you call." This was acknowledged by the flight, which presumably intended to comply because the message was not questioned. At 0827 the local controller saw the aircraft below the overcast and at an estimated altitude of 500 feet, between the tower and Runway 4. 2 He at once transmitted, "Just saw you pass over the airport. You should be passing those hangars now. If you start your left turn and watch the hangers on your left wing, you'll be able to make a left turn into Runway One Three. Go ahead, sir." The landing gear appeared to be fully extended, but the flap position was not noticed. A few seconds later the aircraft disappeared from view on a northerly heading and still at an estimated altitude of 500 feet. The local controller at once asked the flight if it had started the left turn, and the flight replied that it was pilling up to execute a missed approach. The tower gave immediate instruction to turn right and proceed to Long Beach intersection (the SE leg of the Idlewild Range and the SW leg of the Hempstead Range, about 10 miles SE of Idlewild) at 1,500 feet altitude. This transmission was acknowledged. This was the last communication from the flight. A very short time later the aircraft crashed at the intersection of 169th Street and 89th Avenue, Jamaica, New York, about 4.4 miles north of the Idlewild control tower.
Probable cause:
The Board determines that the probable cause of this accident was loss of control following sudden engine failure caused by a deteriorated fuel feed valve diaphragm during an attempted missed approach. The following findings were pointed out:
- As the flight approached Idlewild it was given the local weather including a measured ceiling of 500 feet and a visibility of one and one-half miles,
- This ceiling and visibility were the minimums for the subject flight,
- The captain elected not to follow the tower's suggestions due to limited forward visibility at his altitude,
- During power application for a missed approach the fuel feed valve diaphragm of the left engine either completely failed or an existing failure became worse, this diaphragm had not been replaced at the time of engine over-haul, as required,
- The left engine then acted erratically with surging, intermittently cutting out,
- At the time the flight was on instruments in turbulent air,
- Control was lost and the aircraft descended rapidly in a sharply nose-down right slip taking on aspects of a spin, and crashed.
Final Report:

Crash of a Curtiss C-46F-1-CU Commando in Teterboro: 1 killed

Date & Time: May 27, 1950 at 1729 LT
Type of aircraft:
Operator:
Registration:
N9406H
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Teterboro – Fort Wayne – Detroit
MSN:
22582
YOM:
1945
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
3200
Captain / Total hours on type:
200.00
Copilot / Total flying hours:
2800
Copilot / Total hours on type:
160
Circumstances:
At 1727 the aircraft was cleared to Runway 19 for takeoff toward the south. The engines were run up to a manifold pressure of 15 inches of mercury and ignition was checked on both magnetos of each engine. Takeoff was then started and the manifold pressure was increased to 52 inches of mercury. Ground witnesses estimated that the takeoff run as somewhat longer than usual for this model aircraft. Tower personnel and several ground witnesses saw puffs of black smoke coming from the left engine immediately after the takeoff. At an altitude estimated as 200-300 feet, the left engine started to misfire. The landing gear had been raised and was checked for position. The left engine continued misfiring and shortly became worse. The left propeller as feathered. Ahead, the terrain as flat, unobstructed and marshy. Full power was maintained on the right engine and a left turn was started as if to return to the airport. At this point the altitude was estimated to be 400-500 feet. During the turn the air speed fell to 85-90 1 PH and the aircraft settled. This turning and settling continued until the aircraft neared the ground, when it was leveled laterally. It struck while about level, both laterally and longitudinally, and slid along the omen ground in a generally northeasterly direction for some 620 feet where it struck some large trees and turned to the left about 180 degrees. Both captain and copilot were thrown clear of the wreckage. The captain later died from his injuries. The weather was good and was not a factor in the accident.
Probable cause:
The Board determines that the probable cause of the accident was overloading of the aircraft due to faulty loading end dispatch procedures coupled with engine malfunctioning due to inadequate maintenance.
The following factors were noted:
- The aircraft's was leaded above its maximum gross weight by approximately 5,000 pounds,
- The aircraft had been flown in excess of its 80-hour inspection period,
- Both engines were inadequately maintained,
- The ignition systems of both engines were found to be defective,
- The left engine malfunctioned and its propeller was feathered shortly after takeoff at an air speed of 130-135 miles per hour,
- A left turn was made and the air speed fell sharply to 85-90 miles per hour,
- The aircraft settled to the ground in a near stalled condition.
Final Report:

Crash of a Douglas C-47B-DK in Haines Cay

Date & Time: Oct 4, 1948
Operator:
Registration:
NC58121
Flight Phase:
Survivors:
Yes
Schedule:
Teterboro – Miami – San Juan
MSN:
17086/34353
YOM:
1945
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
19
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The airplane departed Teterboro Airport on a flight to San Juan with an intermediate stop in Miami. After passing Atlantic City, it continued to the south to Miami over the sea along the coast. The Florida coast was not sighted however. After heading west, the crew observed the Berry Group Islands (Bahamas). Since they didn't have enough fuel to reach Nassau, a forced belly landing was carried out on a beach. The surf later damaged the aircraft beyond repair. Although it cannot be proven, it was thought that the crew were asleep during part of the flight and that the autopilot processed and turned the plane westward.

Crash of a Curtiss T-18 Condor I in Troy: 1 killed

Date & Time: Oct 21, 1935 at 1100 LT
Type of aircraft:
Registration:
NC725K
Survivors:
Yes
Schedule:
Troy – Teterboro
MSN:
G-2
YOM:
1930
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
Shortly after takeoff, while in initial climb, the left engine failed. The crew decided to return to Troy Airport but during the last turn, just passing over a small hill, the aircraft lost altitude, impacted a tree and swung into another before dropping to the ground, bursting into flames. All six occupants were seriously injured and the aircraft was destroyed by impact forces and a post crash fire. The captain died few hours later resulting from his injuries. It appears that the aircraft was carrying two couples and was originally planned as a sky wedding flight over New York City. The captain killed in the accident was Harry Hublitz, aged 42. The famous ace feminine pilot Ruth Nichols was among the passengers and was seriously injured.
Probable cause:
There was no structural or mechanical-failure of the aircraft or controls. The cause of the left engine failing could not be determined due to damage sustained by fire. Whether or not the right engine was delivering full power could not be determined. It is evident, however, that the airplane could not maintain its altitude after the left engine failed. It is possible also that a downdraft was encountered while crossing the hill on the return flight to the airport, which caused the airplane to lose further altitude. Turning toward the disabled engine for the return flight necessitated considerably more loss of altitude than would a turn in the direction of the functioning engine. It is the opinion of the Bureau of Air Commerce that the probable cause of this accident was poor judgment on the part of the pilot in his handling of the airplane following an engine failure.