NC92857
1949-JUN-07 · Off Punta Salinas, Puerto Rico

Strato-Freight — Flight NC92857

A Curtiss C-46D crashed into the Atlantic Ocean shortly after takeoff from San Juan due to a combination of severe engine power loss and a significant overweight condition. The right engine failed because maintenance personnel had installed unapproved spark plugs and left the magneto switch in a position that only fired the rear plugs, which subsequently overheated. The aircraft was also carrying 3,709 pounds more than its maximum certified weight, preventing it from maintaining altitude on a single engine.

Aircraft
Curtiss C-46D-5-CU Commando
Registration
NC92857
Phase
Takeoff
Cause
Human Factors (Maintenance)
Souls on Board
81
Fatalities
53
Origin → Dest
San Juan-Isla Grande Airport, Puerto Rico → Miami International Airport, Florida, USA
Report
Final

Investigation Summary

The investigation revealed a systemic disregard for safety regulations by Strato-Freight. The aircraft was configured with only 65 seats but carried 75 passengers, forcing many to share seats or sit on laps. The weight manifest was falsified to show 44,500 lbs, while the actual weight was 48,709 lbs. Maintenance performed just days before the crash involved the installation of AC-LS-87 spark plugs, which were explicitly prohibited for use in the Pratt and Whitney engines of the C-46. During the accident flight, the right engine began backfiring at an altitude of only 250 feet. Post-crash inspection found the right magneto switch set to 'Left', meaning only the rear row of spark plugs was firing. These plugs, already unapproved, suffered extreme heat damage and fused, leading to total power loss. The crew did not attempt to feather the propeller, and the overloaded airframe could not maintain flight, resulting in a ditching 200 yards offshore.

Final Conclusions

The Civil Aeronautics Board determined the probable cause was the loss of power in the right engine before reaching optimum single-engine climb speed, exacerbated by the aircraft's overloaded condition. Contributory factors included the use of unapproved spark plugs, improper magneto switch positioning, and the operator's general indifference toward civil air regulations.

Video Analysis

No video analysis linked for this case file yet.

Airframe & Maintenance

Airframe Hours
2,002

Crew Experience

Captain

Total hours
6,400
On type
3,200

Alfred Cockrill was acting as pilot during the accident flight.

First Officer

Total hours
3,860
On type
2,000

John Connell was acting as copilot.

Systems & Failure Modes

i

Pratt & Whitney R-2800 Engines

The powerplants required specific approved spark plugs; the use of unapproved AC-LS-87 plugs led to overheating and failure.

i

Magneto Ignition System

The ignition switch was improperly set to the 'Left' position, isolating the front row of spark plugs and overloading the rear row.

i

Weight and Balance Manifest

The manifest was inaccurately prepared, underreporting the aircraft's weight by over 4,000 pounds.

Interesting Facts

  • 01The aircraft was 3,709 pounds over its maximum certified takeoff weight of 45,000 pounds.
  • 0230 of the 36 spark plugs in the right engine were AC-LS-87 models, which were not approved for the C-46.
  • 03The cabin contained only 65 seats for 75 passengers, leading to seat-sharing.
  • 04The right engine magneto switch was found in the 'Left' position, firing only the rear spark plugs.
  • 05At the time, this was the deadliest accident in the history of commercial aviation.
  • 06None of the passengers had received instructions on the location or use of emergency equipment prior to the ditching.

Safety Actions & Advisories

Revocation of Operating Certificate

Strato-Freight's operating license was suspended immediately after the crash and permanently revoked effective November 8, 1949, due to a pattern of safety violations and indifference to regulations.

Location

Off Punta Salinas, Puerto Rico · 18.4690, -66.2040

Related Cases

Case ID · strato-freight-1949Last updated · Filed

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