N392CA
Registered owner: INTERNATIONAL AIR SERVICES INC TRUSTEE, NV (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| UNIVERSAL AIR SERVICE, LLC (UVRA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
DURING INSPECTION FOUND CORROSION IN AFT CARGO DOOR. REMOVED CORROSION DAMAGED PANELS. FABRICATED & INSTALLED TWO REPAIR PANELS. ALL REPAIRS PERFORMED IAW SRM.
DURING 1200 HR FALSE SPAR RECURRING INSPECTION, & AD INSPECTION AD 98-12-28. FOUND CRACKS IN THE PROFILE OF FALSE SPAR LOCATED IN THE RT WING. REMOVED RT WING AUXILIARY SPAR PROFILE ANGLE. INSTALLED REINFORCED RT WING AUXILIARY SPAR PROFILE ANGLE. ALL REMOVAL AND REPLACEMENT OF PARTS WAS ACCOMPLISHED IAW CASA C-212 SERVICE BULLETIN SB-212-57-30.
DURING 1200 HR FALSE SPAR RECURRING AD INSPECTION, IAW AD 98-12-28. FOUND CRACKS IN THE PROFILE OF FALSE SPAR LOCATED IN THE LT WING. REMOVED LT WING AUXILIARY SPAR PROFILE ANGLE, WS 5700. INSTALLED REINFORCED LT WING AUXILIARY SPAR PROFILE ANGLE. ALL REMOVAL AND REPLACEMENT OF PARTS ACCOMPLISHED IAW EADS CASA C-212 SERVICE BULLETIN SB-212-57-30 REV.1.
DURING FLIGHT LT WINDOW HEAT SHORTED.
LEVEL 2 CORROSION ON MAIN LEFT LANDING GEAR FWD INTERIOR SUPPORT FITTING AT FS 5744.3 BELOW FLOOR.
LEFT WING OUTBOARD FLAP, AND INBOARD ACTUATOR BELL CRANK BOTTOM SUPPORT ARE CORRODED (OUTBOARD SIDE OF BEARING CUP)(LEVEL 2).
LEFT WING, CENTER SECTION, AREAS OF TRAILING EDGE OVER FLAP REMOVED, WS 1963-2200 AND WS 3296-3497, SAME AREAS HAVE SEVERE CORROSION (LEVEL 2).
RIGHT WING UPPER INBOARD ENGINE MOUNT ON FWD SIDE OF FRONT SPAR IS DELAMINATED
LEFT WING, UPPER INBOARD ENGINE MOUNT ON FWD SIDE OF FRONT SPAR IS DELAMINATED
LEFT WING UPPER OUTBOARD ENGINE MOUNT FITTING HAS START OF DELAMINATION, FWD SIDE OF FRONT SPAR.
CORROSION ON RIGHT ELEVATOR TOP SKIN PANEL AT THE SKIN PANEL JOINTS LOCATED 44 INCHES I/B FROM O/B EDGE.
LEFT AND RIGHT RUDDER SERVO CABLE QUADRANT BLOCKS MOUNTED ON LOWER SURFACE RUDDER CABLE QUADRANT HAVE CORROSION.
RIGHT FWD UPPER HSS (FUSE SIDE) HAS LEVEL 3 CORROSION ON FITTING AT FS 13268.
LEVEL 1 CORROSION ON LEFT AFT HSS FWD UPPER (FUSE SIDE) UNDER BUSHINGS AT FS 13268.
LEVEL 1 CORROSION ON THE HSS LEFT FWD LOWER (FUSE SIDE) FITTING AROUND THE BUSHINGS.
LEVEL 1 CORROSION ON THE LEFT AFT HSS LOWER FITTING (FUSE SIDE) IN FWD RIGHT AFT RADIUS OF THE FITTING AT FS 13845.
VERTICAL STABILIZER RIGHT FITTING (FUSE SIDE) AT FS 13845 HAS LEVEL 2 CORROSION.
VERTICAL STABILIZER LEFT AFT FITTING (FUSE SIDE) AT FS 13845 HAS LEVEL 3 CORROSION.
VERTICAL STABILIZER LEFT FWD FITTING (FUSE SIDE) AT FS 13268 HAS LEVEL 3 CORROSION.
HORIZONTAL STABILIZER LEFT AFT UPPER (FUSE SIDE) AT FS 13845 HAS LEVEL 3 CORROSION.
HORIZONTAL STABILIZER RIGHT LOWER FITTING (FUSE SIDE) AT FS 13268 HAS LEVEL 1 CORROSION.
HORIZONTAL STABILIZER RIGHT ATTACH FITTINGS (HSS SIDE) FWD AND AFT FITTINGS HAVE LEVEL 2 CORROSION.
VERTICAL STABILIZER AFT FITTING (VERT STAB SIDE) HAS LEVEL 3 CORROSION ON THE AFT LEFT SIDE OF THE FITTING.
HORIZONTAL STABILIZER LEFT (STAB SIDE) FWD ATTACH FITTING HAS LEVEL 3 CORROSION.
RIGHT AFT HSS HAS LEVEL 3 CORROSION ON FITTING AT FS 13845.
RIGHT WING, REAR SPAR WEB HAS CORROSION, WS 5940 AFT SIDE AT BOTTOM SPAR CAP (MARKED).
RIGHT OUTER FLAP INBOARD ACTUATOR BELLCRANK BOTTOM SUPPORT IS CORRODED ON INBOARD FWD CORNER.
LEVEL 3 CORROSION ON CHINE PLATE LEFT SIDE BETWEEN FS 5390 AND FS 5744.3.
RIGHT FLOOR SEAT TRACK IS CORRODED FROM FS 3950 TO FS 7332.
RIGHT CENTER WING AILERON CONTROL QUADRANT IS CORRODED ON UPPER SURFACE FS 6735 (LEVEL 3).
CORROSION ON UPPER SURFACE OF AILERON QUADRANT CONTROL RODS CENTER WING FS 6735.
RIGHT SIDE SEAT TRACK RAIL IS CORRODED IN SEVERAL PLACES: FS 3950, FS 4310, AND FROM FS 5744 TO FS 8950.
RIGHT BRAKE DRAGGING AND LOCKING UP. THIS WOULD ONLY HAPPEN WHEN COPILOT RIGHT BRAKE WAS USED. WOULD NOT DRAG OR LOCK WHEN PILOT''S BRAKES WERE USED. AFTER TROUBLESHOOTING, CHANGED PILOT''S RIGHT MASTER CYLINDER WHICH TOOK CARE OF PROBLEM. (X)
PRE-FLIGHT INSPECTION FOUND 5.50 INCH BY 4 INCH PIECE OF EXHAUST NOZZLE MISSING FROM AFT END OF NOZZLE. EXHAUST DUCT WAS DAMAGED AS PART DEPARTED AIRCRAFT. BOTH PARTS REPLACED.