CAL-ORE LIFE FLIGHT LLC.
Also recorded as: CAL-ORE LIFE FLIGHT LLC., Cal-Ore Life Flight, Cal-Ore Life Flight LLC.
Accident & enforcement record
Events that happened, regardless of the operator's own reporting. Each links to its public source.
NTSB accidents & incidents
FAA enforcement actions
FAA enforcement records haven't been loaded into GroundCheck yet, so none can be shown — a gap in our data, not evidence of a clean enforcement history.
Maintenance disclosure history
Service Difficulty Reports are self-reported maintenance findings. The NUMBER of reports is not a measure of reliability — diligent operators file more, not fewer. These are shown for transparency, not as a negative signal.
7 reports on file.
DURING INSPECTION, A CRACK WAS FOUND ON THE LOWER LEFT PORTION OF THE CABIN DOOR FRAME AT BS 243.38. THE CRACK ORIGINATES FROM A BEND RELIEF CUTOUT IN A HEAVILY FORMED SECTION OF THE FRAME. THIS IS THE THIRD AIRCRAFT WE FOUND THIS CRACK PRESENT, SAME MAKE AND MODEL. THE REGION OF THE FRAME HAS TO BE DISASSEMBLED AND INSPECTED FOR OTHER SIGNS OF DAMAGE OR DISTRESS. AN ENGINEERED DOUBLER HAS TO BE INSTALLED WITH STRUCTURAL ADHESIVE AND RIVETS.
THE ADJUSTABLE GRIP LATCH FASTENER THAT HOLDS DOWN THE CENTER ISLE FLOORBOARD IN THE CABIN FALLS APART AND CONDUCTIVE PIECES FALL INTO THE ELECTRICAL EQUIPMENT BELOW THE FLOORBOARDS. A PIECE WAS FOUND ON THE FLAP RELAY DURING REGULAR MAINTENANCE.
INSPECTION OF RUDDER AND VERTICAL STABILZIER AREA REVEALED RIVETS WITH POPPED HEADS ON ATTACHMENT FITTING FOR AFT SPAR ON VERTICAL STABILIZER-TO-EMPENNAGE ATTACH POINT. (SIX OUT OF EIGHT RIVETS WERE SHEARED). THOROUGH INSPECTION OF EMPENNAGE REVEALED NO OTHER PROBLEMS.
THE FLAP LEVER ATTACH BRACKET IS CRACKED AT THE FORWARD LOWER BEND RADIUS, ADJACENT TO THE ATTACH POINT TO THE FLOOR.
DURING A MAGNETO 500-HOUR INSPECTION, ONE MOUNTING HOLE FOR THE DISTRIBUTER BLOCK WAS FOUND CRACKED.
DURING MAGNETO 500-HOUR INSPECTION, ONE MOUNTING HOLE OF THE DISTRIBUTOR BLOCK WAS FOUND CRACKED.
THE SHOP HEAD OF THE RIVET ON THE RIGHT SIDE OF THE VERTICAL STABILIZER, JUST ABOVE THE FUSELAGE THAT HOLDS THE AFT INNER CHANNEL TO THE SKIN, WAS BROKEN OFF. THIS MAY HAVE BEEN CAUSED BY VIBRATION. SUBMITTER KNOWS OF SEVERAL INSTANCES OF SAME RIVETS ON BOTH SIDES BREAKING ON FLEET AIRCRAFT.
Linked aircraft
| N-number | Make / model | Year | Status | Link basis |
|---|---|---|---|---|
| N336LA | RAYTHEON AIRCRAFT COMPANY C90GT | — | Valid Registration | Matched by certificate designator |
| N4377X | ROBINSON HELICOPTER COMPANY R44 II | 2009 | Valid Registration | Matched by certificate designator |
| N5431M | RAYTHEON AIRCRAFT COMPANY C90A | 2002 | Valid Registration | Matched by certificate designator |
| N588SA | RAYTHEON AIRCRAFT COMPANY C90A | 2000 | Valid Registration | Matched by certificate designator |
| N661TC | — | — | Operator named in NTSB report | |
| N912MF | — | — | Matched by certificate designator | |
| N982SB | RAYTHEON AIRCRAFT COMPANY C90A | 1998 | Valid Registration | Matched by certificate designator |