N972EA

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 22,578 hrs · 34,590 cycles

LEFT PROP GAUGE INOPERATIVE ON TAKEOFF ROLL. R & R PROP INDICATOR, OPERATIONS CHECKED GOOD IAW MM 31-10-00.

Part: SPAR WEB — CHAFED (RT WING) · airframe 21,351 hrs · 32,248 cycles

RIGHT WING REAR SPAR HAS DEEP CHAFE SPOT CAUSED BY SPLIT FLAP SWITCH WIRE WS120.98 AND WS121.73. REPAIRED (BLENDED)CHAFING RT WING AFT SPAR WEB, WS 120 IAW FIELD REPAIR FR-CO-100695.

Part: SEALANT — DEFECTIVE (FUSELAGE) · airframe 21,126 hrs · 31,829 cycles

"CABIN ALT.HIGH" LIGHT ON AT 20,000FT CONTINUED LOSS OF DIFF PRESSURE. AIR LEAK FOUND ALONG LOWER EDGE OF AIRSTAIR DOOR. SEALED ALONG EDGE OF FUSELAGE SKIN AT BOTTOM OF AIRSTAIR DOOR IAW BE1900D MAINTENANCE MANUAL 20-10-00 AND PRESSURE CHECKS GOOD ON GROUND IAW BE19000D MAINTENANCE MANUAL 21-30-00.

Part: GAUGE — INOPERATIVE (COCKPIT) · airframe 20,783 hrs · 31,276 cycles

RIGHT ITT BECAME INOPERATIVE IN FLIGHT. REMOVED AND REPLACED RIGHT ENGINE ITT GAUGE, RAN ENGINE, OPS CHECK GOOD. OK FOR SERVICE.

Part: ACTUATOR — DEFECTIVE (LT MLG) · airframe 20,356 hrs · 30,581 cycles

LEFT MAIN GEAR LIGHT FAILED TO ILLUMINATE. REMOVED AND REPLACED LT MLG ACTUATOR AND RIGGED IAW B1900D MAINTENANCE MANUAL 32-30-10 AND 32-30-09. BLED IAW 32-30-00 GEAR SWING COMPLIED WITH SYSTEM OP CHECKS GOOD.

Part: CONTROLLER — INOPERATIVE (TCAS) · airframe 18,201 hrs · 27,040 cycles

TCAS CONTROLLER AND TRANSPONDER CONTROLLER DISPLAY WENT BLANK ON SHORT FINAL INTO ANC. REPLACED CONTROLLER AND SYSTEM OPERATES OK.

Part: ACTUATOR — CRACKED (LT MLG) · airframe 16,868 hrs · 24,997 cycles

AFTER LANDING FLIGHT CREW NOTED HYDRAULIC FLUID LEAKING FROM LEFT MAIN LANDING GEAR. MAINTENANCE FOUND LMLG ACTUATOR END CAP CRACKED AND LEAKING. REPLACED ACTUATOR WITH OVERHAULED. FAILED UNIT SUBJECT TO 1200 CYCLE REPETITIVE ULTRASONIC INSPECTION OF THE END CAP IAW AD 2009-23-01. LAST ULTRASONIC INSPECTION WAS COMPLETED 410 CYCLES PRIOR TO FAILURE WITH NO FAULT FOUND.

Part: HANDLE — SEPARATED (ZONE 800) · airframe 15,251 hrs · 22,387 cycles

CARGO DOOR HANDLE FELL OFF. REMOVED DOOR HANDLE, REPLACED SNAP RING AND REINSTALLED DOOR HANDLE IAW HB1900D MM 52-30-00.

Part: TRANSDUCER — SHORTED (RT ENGINE) · airframe 13,588 hrs · 19,790 cycles

FAI - UPON CLIMBOUT FROM FAI FOUND OIL PRESSURE WENT TO "0" ON RIGHT ENGINE. SHUT DOWN RIGHT ENGINE AND RETURNED TO FAI. REPLACED ENGINE OIL PRESSURE XDCR S/N 4518-1-247 WITH S/N 7651-6-137. RAN ENGINE, OPERATED NORMALLY.

Part: FITTING — CRACKED (AILERON) · airframe 11,713 hrs · 17,416 cycles

WHILE INSPECTING IAW SB27-3928, FLIGHT CONTROLS- AILERON BALANCE WEIGHT CLIP INSPECTION; FOUND ONE CLIP CRACKED ON THE RT AILERON.

Part: FITTING — CRACKED (AILERONS) · airframe 11,713 hrs · 17,416 cycles

WHILE INSPECTING IAW SB27-3928 FLIGHT CONTROLS- AILERON BALANCE WEIGHT CLIP INSPECTION; FOUND ONE CLIP CRACKED ON LT AILERON.

Part: UNKNOWN — ODOR (CABIN) · airframe 9,306 hrs · 12,620 cycles

STRONG BURNING SMELL AT FL190 AND LIGHT SMOKE OBSERVED BY CREW & PAX. RETURNED TO ANC. VISUALLY INSPECTED WIRING & CONNECTIONS AT WINDSHIELD PANELS, CB PANELS, OVERHEAD SWITCH PANELS. NO DEFECTS NOTED. UNABLE TO DUPLICATE DISCREPANCY AT EXTENSIVE GROUND RUN SIMULATING FLIGHT CONDITIONS. A/C DISPATCHED FOR OPERATIONAL TEST FLT ONLY.