ASN Wikibase Occurrence # 363404
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: | Friday 26 June 1992 |
| Time: | 16:53 LT |
| Type: | Smith, Ted Aerostar AEROSTAR 601 |
| Owner/operator: | Private |
| Registration: | N601DE |
| MSN: | 61-0007 |
| Total airframe hrs: | 2589 hours |
| Engine model: | LYCOMING IO-540-P1A5 |
| Fatalities: | Fatalities: 0 / Occupants: 1 |
| Aircraft damage: | Substantial |
| Category: | Accident |
| Location: | Prescott, AZ -
 United States of America
|
| Phase: | Initial climb |
| Nature: | Ferry/positioning |
| Departure airport: | (KPRC) |
| Big Bear City, CA (L35) | |
| Investigating agency: | NTSB |
| Confidence Rating: |  Accident investigation report completed and information captured |
BFR FLT, THE OWNER/PLT RCVD A SPECIAL AIRWORTHINESS CERTIFICATE, ALLOWING HIM TO MAKE A FERRY FLT FM COLORADO TO CALIFORNIA FOR MAINT. A COND FOR THE FAA'S ISSUANCE OF THE PERMIT WAS THAT AN A & P MECHANIC MUST CERTIFY THE ACFT WAS 'SAFE FOR THE FLIGHT.' THE PLT WAS AN A & P MECHANIC & PROVIDED THE REQUISITE CERTIFICATION. AN ACDNT OCCURRED DRG TAKEOFF FM AN EN ROUTE STOP. A WITNESS TO THE TAKEOFF RPRTD THE ACFT USED 5500 FT OF RWY BEFORE BECOMING AIRBORNE. THE ACFT FAILED TO CLIMB HIGHER THAN 200 FT AGL BEFORE COLLIDING WITH ROUGH TRRN ABOUT 2 MI FM THE ARPT. AT THE TIME OF THE MISHAP, THE COMPUTED DENSITY ALT WAS APRX 7760 FT. PERSONNEL, WHO RESPONDED TO THE CRASH SITE, OBSERVED THAT DUCT TAPE HAD BEEN USED TO SECURE AN ANGLE IRON ONTO A LANDING GEAR LEG (FOR THE PURPOSE OF PROVIDING A STIFF LEG COND). DUCT TAPE HAD ALSO BEEN USED ON THE DETERIORATED WING TIPS (TO KEEP THEM STREAMLINED). TWO HORNET NESTS WERE FND IN AIRFRAME AIR INLETS. THE PLT RPRTD THAT NO MECH FAILURE OR MALFUNCTION OCCURRED DRG TAKEOFF.
Probable Cause: THE AIRPLANE'S FAILURE TO ACHIEVE AN ADEQUATE RATE OF CLIMB BECAUSE OF DEGRADED AERODYNAMIC PERFORMANCE AND THE PILOT'S INTENTIONAL OPERATION OF THE AIRCRAFT WITH KNOWN DEFICIENCIES. A FACTOR IN THE ACCIDENT WAS THE HIGH DENSITY ALTITUDE CONDITION.
Accident investigation:
 |
|
Sources:
NTSB LAX92LA263
Location
Revision history:
| Date/time | Contributor | Updates |
|---|---|---|
| 18-Mar-2024 16:56 | ASN Update Bot | Added |
Corrections or additions? ... Edit this accident description
The Aviation Safety Network is an exclusive service provided by:
Quick Links:
| ASN Home | Send Correction / Feedback |
| FSF Home | Disclaimer | Copyright |
| Contact Us | Privacy Policy |
| Press / Media |
CONNECT WITH US:
©2024 Flight Safety Foundation