REDDING AERO ENTERPRISES, INC.
Also recorded as: CORPAC, LLC, REDDING AERO ENTERPRISES, INC., REDDING JET CENTER, Redding Aero Enterprises Inc, Redding Aero Enterprises, Inc.
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.
9 reports on file.
WHILE PERFORMING A FLEET CAMPAIGN DIRECTIVE CREATED TO INSPECT THE HORIZONTAL STABILIZER MOUNT BOLTS, IT WAS FOUND THAT ALL FOUR OF THEM WERE CORRODED.
DURING ANNUAL INSPECTION, FOUND SIGNIFICANT CORROSION ON FLAP TRACKS. R & R FLAP TRACKS.
DURING ANNUAL INSPECTION, FOUND SIGNIFICANT EXFOLIATION CORROSION ON 4 OF 6 FLAP TRACKS. R & R FLAP TRACKS WITH NEW.
DURING ANNUAL INSPECTION, FOUND SIGNIFICANT EXFOLIATION CORROSION OF 4 OF 6 FLAP TRACKS. R & R FLAP TRACKS WITH NEW.
DURING ANNUAL INSPECTION, FOUND SIGNIFICANT CORROSION FLAP TRACKS. R & R FLAP TRACKS.
PILOT REPORTED HIS GENERATOR FAILED. MX FOUND THAT THE INPUT SHAFT HAS EITHER SHEERED INTERNAL OF THE UNIT OR BECAME DISCONNECTED. UNIT HAS NOT BEEN OPENED UP FOR INSP AT THIS TIME. A VIDEO SHOWING THIS CONDITION IS ACCOMPANYING THIS REPORT. UNIT WILL BE SENT FOR REPAIR AND A TEAR DOWN REPORT WILL BE REQUESTED. (K)
THE PILOT REPORTED HIS TAIL BEACON INOPERATIVE. MX TECHS TROUBLESHOT THE WIRING AND FOUND THAT THE WIRING BUNDLE THAT CONTAINS THE POWER WIRE FOR THE TAIL BEACON WHERE IT ROUTES OVER THE GLOVE BOX HAD CHAFED ON THE GLOVE BOX. THE CHAFING CAUSED THE WIRE TO BURN THROUGH THE GLOVE BOX. (K)
PILOT OBSERVED SMOKE IN AND UPON SCANNING INSTRUMENTS, NOTICED LOWER THAN NORMAL OIL PRESSURE AND HIGHER THAN NORMAL OIL TEMP. ENGINE WAS SHUT DOWN. PILOT ALSO REPORTED FACE OF INSTRUMENT GLOWING AS CABIN FILLED WITH SMOKE. PILOT DONNED O2 MASK AS SMOKE THICKENED. MASTER POWER WAS NEVER SHUTDOWN AND 5 AMP BREAKER NEVER OPENED AUTOMATICALLY NOR WAS IT PULLED. AFTER LANDING AND SECURING THE MASTER SWITCH THE SMOKE CLEARED. ALL DAMAGE APPEARED TO BE CONTAINED INTERNALLY AND SMOKE MOST LIKELY EXITED INSTRUMENT THRU THE VENT FITTING.
ENGINE FAILED IN FLIGHT DUE TO SHEARED FUEL PUMP DRIVE, AIRCRAFT LANDED SAFELY IN FARMERS FIELD. NO AIRCRAFT DAMAGE. SUGGEST MANDATORY DRIVE REPLACEMENT AT EACH OVERHAUL.
Linked aircraft
| N-number | Make / model | Year | Status | Link basis |
|---|---|---|---|---|
| N106VE | CESSNA 208B | 1999 | Valid Registration | Matched by certificate designator |
| N121HA | CESSNA 208B | 1988 | Valid Registration | Matched by certificate designator |
| N208PG | CESSNA 208B | 1999 | Valid Registration | Matched by certificate designator |
| N208TM | CESSNA 208B | 1994 | Valid Registration | Matched by certificate designator |
| N24MG | — | — | Operator named in NTSB report | |
| N36908 | CESSNA 402C | 1980 | Valid Registration | Matched by certificate designator |
| N40NE | CESSNA 208B | 2000 | Valid Registration | Matched by certificate designator |
| N4662B | CESSNA 208B | — | Valid Registration | Matched by certificate designator |
| N5849C | — | — | Operator named in NTSB report | |
| N681RC | CESSNA 402C | — | Valid Registration | Matched by certificate designator |
| N68379 | CESSNA 402C | 1981 | Valid Registration | Matched by certificate designator |
| N90GL | CESSNA 208B | 1990 | Valid Registration | Matched by certificate designator |
| N932C | CESSNA 208B | 1987 | Valid Registration | Matched by certificate designator |
| N9623B | CESSNA 208B | 1988 | Valid Registration | Matched by certificate designator |
| N9766B | CESSNA 208B | 1988 | Valid Registration | Matched by certificate designator |