Accident Lockheed L-188A Electra N9705C,
ASN logo
ASN Wikibase Occurrence # 333936
 

Date:Tuesday 29 September 1959
Time:23:09
Type:Silhouette image of generic L188 model; specific model in this crash may look slightly different    
Lockheed L-188A Electra
Owner/operator:Braniff International Airways
Registration: N9705C
MSN: 1090
Year of manufacture:1959
Total airframe hrs:132 hours
Engine model:Allison 501-D13
Fatalities:Fatalities: 34 / Occupants: 34
Aircraft damage: Destroyed, written off
Category:Accident
Location:6 km ESE of Buffalo, TX -   United States of America
Phase: En route
Nature:Passenger - Scheduled
Departure airport:Houston International Airport, TX (HOU/KHOU)
Destination airport:Dallas-Love Field, TX (DAL/KDAL)
Investigating agency: CAB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
Braniff International Airways Flight 542, a Lockheed L-188A Electra, departed the ramp at Houston International Airport at 22:37, 22 minutes behind schedule. The delayed departure was due to a mechanical discrepancy involving No. 3 generator. This generator was inoperative on arrival of N9705C at Houston. Prior to departure from Houston the Nos. 3 and 4 voltage regulators were interchanged. The estimated time en route to Dallas was 41 minutes.
The flight was given an IFR clearance which was to the Leona omni, via Victor Airway 13 west to the Gulf Coast intersection, direct to Leona, to maintain 2,300 feet altitude to Gulf Coast, then to climb to and maintain 9,000. At approximately 22:40 the flight was cleared for takeoff and at 22:44 the crew reported airborne.
After takeoff Houston departure control advised that it had the flight in radar contact and requested it to report when established outbound on the 345-degree radial of the Houston omni. Flight 542 complied and subsequently was cleared to 9,000 feet and advised to contact San Antonio Center upon passing the Gulf Coast intersection.
At approximately 22:52 Flight 542 reported to San Antonio Center as being over Gulf Coast intersection at 9,000 feet. The flight was then issued its destination clearance to the Dallas Airport and it was cleared to climb to its cruising altitude of 15,000 feet. After the Electra had passed Leona at 23:05, the crew contacted company radio with a message for maintenance, advising that the generators were then OK but that there had been insufficient time for maintenance to insulate the terminal strip on No. 3 propeller at Houston and it would like to have it done in Dallas.
At 23:09 the left wing and the No. 1 gear box propeller separated. The horizontal stabilizer then broke up under the impact of parts coming from the wing; wing planking from the right wing tip came free; the No. 4 powerplant tore loose; and the right wing outboard of engine No. 4 separated. All of these events happened in a short period of time. Somewhat later, at much lower altitudes, the fuselage broke in two separate portions at a point about halfway back near fuselage station No. 570.
All 34 on board were killed in the accident.

On March 17, 1960, while the investigation into this accident was still ongoing, a second Lockheed Electra crashed under similar circumstances near Cannelton, Indiana.

PROBABLE CAUSE: "Structural failure of the left wing resulting from forces generated by undampened propeller whirl mode."

Accident investigation:
cover
  
Investigating agency: CAB
Report number: 1-0060
Status: Investigation completed
Duration: 1 year and 7 months
Download report: Final report

Sources:

ICAO Circular 64-AN/58 (51-61)
Northwest Flight 710 accident, 17 March 1960

Location

Revision history:

Date/timeContributorUpdates

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org