ASN Wikibase Occurrence # 379087
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information.
If you feel this information is incomplete or incorrect, you can
submit corrected information.
Date: | Saturday 30 June 1984 |
Time: | 14:32 LT |
Type: | Cessna 421B |
Owner/operator: | Silverline Industries, Inc. |
Registration: | N554 |
MSN: | 42180938 |
Engine model: | Continental GTSIO-520-H |
Fatalities: | Fatalities: 0 / Occupants: 8 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | El Paso, TX -
United States of America
|
Phase: | Landing |
Nature: | Executive |
Departure airport: | Greenville, TX (KGVT) |
Destination airport: | El Paso, TX (KELP) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:FIRST EVIDENCE OF LANDING GEAR TIRE MARKS WERE FOUND APRX 4,000 FT DOWN THE RWY, RIGHT OF CENTERLINE AND CONTINUED UNTIL THE ACFT ROLLED OFF THE RIGHT SIDE OF THE RWY. ALL 3 LANDING GEAR COLLAPSED IN THE SOFT DIRT AND GRAVEL. ACCORDING TO THE PLT, WHEN THE AUTO-PILOT WAS DISENGAGED ON FINAL APPROACH, 3 MILES OUT, THE ACFT YAWED RIGHT. POWER AND RUDDER WERE USED TO MAINTAIN CONTROL. AT TOUCHDOWN POWER WAS REDUCED AND SHORTLY THEREAFTER THE ACFT DRIFTED RIGHT DESPITE THE APPLICATION OF LEFT RUDDER AND BRAKE. EXAM OF THE WRECKAGE REVEALED NO MECHANICAL MALFUNCTIONS IN THE AUTO-PILOT, WHEEL BRAKES, FLIGHT CONTROLS, AND TRIM SYSTEMS. THE CAUSE OF THE DIRECTIONAL CONTROL LOSS WAS NOT DETERMINED.
Probable Cause:
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | FTW84FA296 |
Status: | Investigation completed |
Duration: | |
Download report: | Final report |
|
Sources:
NTSB FTW84FA296
Revision history:
Date/time | Contributor | Updates |
31-Mar-2024 15:36 |
ASN Update Bot |
Added |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation