ASN Wikibase Occurrence # 379137
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Date: | Monday 25 June 1984 |
Time: | 13:20 LT |
Type: | Bell 212 |
Owner/operator: | Pumpkin Air Inc. |
Registration: | N2180J |
MSN: | 31207 |
Year of manufacture: | 1981 |
Total airframe hrs: | 1177 hours |
Engine model: | P&W PT6T-3B-TPAC |
Fatalities: | Fatalities: 0 / Occupants: 10 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Galveston, TX -
United States of America
|
Phase: | Initial climb |
Nature: | Unknown |
Departure airport: | Galveston, TX |
Destination airport: | High Isl 474, GM |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:DURING TAKEOFF, THE HELICOPTER LIFTED OFF IN AN 80% POWER CHECK & THE PLT BEGAN A NORTHERLY DEPARTURE. BEFORE ACHIEVING TRANSLATIONAL LIFT, THE ROTOR RPM DROPPED TO APRX 85%. THE TORQUE METER INDICATED A SPLIT WITH THE #1 ENG INDICATING ABOUT 55% & THE #2 ENG INDICATING AS LOW AS 39%. THE LOW ROTOR RPM AUDIO & WARNING LIGHT ACTIVATED & THE HELICOPTER BEGAN TO SINK. THE PLT HAD INSUFFICIENT ALT TO RECOVER RPM. HE LANDED THE HELICOPTER IN A CLEAR AREA IN A NOSE HIGH ATTITUDE & WITH FORWARD SPEED. DURING THE LANDING, THE SKIDS WERE DAMAGED (SPREAD), THE HELICOPTER ROCKED FORWARD, THE RADOME WAS DAMAGED & THE TAIL BOOM WAS SEVERED. AN INVESTIGATION REVEALED THAT THE #2 ENG, MAIN FUEL CONTROL, PN3244736-8 HAD AN AIR LEAK AT THE P3-TP-PG REGULATOR AIR DIAPHRAM WJERE A RETAINING SCREW WAS LOOSE. THE SCREW HAD BEEN SAFETY WIRED & SEALED BY THE MANUFACTURER BUT WOULD TURN SLIGHTLY WITHIN THE LIMITS OF THE WIRE. WHEN TIGHTENED, WITHIN THE LIMITS, THE AIR LEAK STOPPED.
Probable Cause:
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | FTW84FA287 |
Status: | Investigation completed |
Duration: | |
Download report: | Final report |
|
Sources:
NTSB FTW84FA287
Location
Revision history:
Date/time | Contributor | Updates |
31-Mar-2024 16:08 |
ASN Update Bot |
Added |
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