N432CV

ATA 2497

Part: TERMINAL — BURNED (NR 2 GENERATOR) · airframe 7,299 hrs · 9,637 cycles

PILOT NOTED AFTER ENGINE START THAT GENERATOR 2 WAS TRIPPED OFF LINE. THE PILOT MEL'D GENERATOR 2 AND RETURNED TO HOME BASE. A TECHNICIAN NOTED UPON AN INSPECTION OF GENERATOR 2 THAT THE RING TERMINAL ATTACHED TO THE GENERATOR OUTPUT POST (B+) WAS SEVERELY HEAT DAMAGE DUE TO HIGH RESISTANCE. THE TECHNICIAN REPLACED THE RING TERMINAL AND, AS A PRECAUTION, REPLACED THE GENERATOR 2. NO FURTHER ACTION WAS REQUIRED. GENERATOR 2 OPERATIONAL CHECK WAS SATISFACTORY.

ATA 2751

Part: TRANSMITTER — FAULTY (RT WING TE FLAP) · airframe 13,177 hrs · 14,183 cycles

PILOT REPORTED A FLAPS FAILED INDICATION. INVESTIGATION DISCLOSED THE RT FLAP POSITION TRANSMITTER WAS FAULTY. INSTALLED A NEW TRANSMITTER. SUBSEQUENT FLAP OPERATIONAL CHECKS WERE SATISFACTORY. NO FURTHER ACTION WAS REQUIRED.

ATA 3100

Part: EADI — BURNED (ZONE 200) · airframe 11,663 hrs · 12,487 cycles

PILOT REPORTED SMOKE IN THE CABIN/COCKPIT FROM THE COPILOTS EADI. PART TOTAL TIME IS UNKNOWN, PROPELLER TOTAL CYCLES ARE UNKNOWN.

ATA 5210

Part: WINDSHIELD — FAILED (ZONE 200) · airframe 4,221 hrs · 3,494 cycles

IN CRUISE FLIGHT AT FL200, IMC, THE PILOT’S WINDSCREEN CRACKED WITH A LOUD BANG. PIC PREFORMED AN EMERGENCY DESCENT AND CHOSE TO DIVERT, 10 MILES IN FRONT OF US. COORDINATED WITH ATC, DECLARED AN EMERGENCY, SET UP ILS, GOT ATIS, ETC. ALSO DE-PRESSURIZED THE ACFT USING THE MANUAL CONTROL VALVE DURING THE DESCENT. PIC PERFORMED THE ILS 13 AT DSM, TOOK OVER CONTROLS AND LANDED FROM THE RT SEAT DUE TO REDUCED VISIBILITY FROM THE LT SEAT. THERE WERE NO CHECKLIST ITEMS ON THE QRH FOR A CRACKED WINDSCREEN SO WE USED OUR BEST JUDGMENT IN DESCENDING, DEPRESSURIZING, AND LANDING ASAP. ALSO DEEMED IT PRUDENT TO DUCK BEHIND THE PANEL IN CASE THE WINDSCREEN WAS TO SHATTER INWARD. AFTER LANDING, THE OUTER LAYER WAS DISCOVERED TO BE CRACKED, THE INNER LAYER WAS INTACT. SOME SORT OF GOGGLES OR EYE/FACE PROTECTION SHOULD BE INCLUDED FOR THE PILOTS IN THE EVENT THIS WAS TO REOCCUR. MECHANICS COMMENT: UPON EXAMINATION OF THE REMOVED WINDSHIELD, IT APPEARS THE GLASS SHATTERED FROM ONE ORIGINAL STRESS RISER, MOST LIKELY DAMAGE RECEIVED FROM A STONE CHIP OR SOMETHING SIMILAR. IT SHOULD ALSO BE NOTED THAT THE WINDSHIELD WAS REMOVED IN ONE PIECE WITH THE INNER PLY MAINTAINING THE INTEGRITY OF THE GLASS. ALTHOUGH THE PILOT REPORTED A CRACKED WINDSHIELD, IT ACTUALLY SHATTERED TO THE POINT OF BEING COMPLETELY OPAQUE.