N172GA

Part: BOLT — BROKEN (MLG DRAG BRACE) · airframe 41,851 hrs · 55,463 cycles

RIGHT MAIN LANDING DRAG BRACE DISCONNECTED FROM WING ATTACH POINT. LANDING GEAR STRUT RETRACED THE AFT CONTACTING WING STRUCTURE. INVESTIGATION FOUND DRAG BRACE ATTACH BOLT BROKEN AT GREASE GALLEY.

Part: SWITCH — FAILED (CARGO DOOR) · airframe 41,171 hrs · 54,846 cycles

DURING TAKEOFF ROLL BAGGAGE DOOR ANNUNCIATION ILLUMINATED. PILOT ABORTED TAKEOFF. INSPECTION REVEALED THE NOSE BAGGAGE DOOR SWITCH HAD FAILED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 3 · airframe 40,537 hrs · 54,109 cycles

DURING MX, THE RT SIDE SEAT RAIL WAS FOUND TO BE CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 3 · airframe 40,537 hrs · 54,109 cycles

DURING MX INSPECTION, THE LT SIDE SEAT RAIL WAS FOUND TO BE CORRODED.

Part: SPAR CAP — CORRODED (LT WING) · airframe 39,846 hrs · 53,367 cycles

INSPECTION REVEALED CORROSION DEVELOPING ON THE LT UPPER MAIN SPAR CAP UNDER THE VORTEX GENERATORS.

Part: SKIN — DEBONDED (LT WING) · airframe 39,846 hrs · 53,367 cycles

LEFT WING DEBOND. UPPER SKIN OF BONDED PANEL IN AREA AROUND FUEL BAY ACCESS OVAL PANEL DEBONDED FROM FUEL ACCESS DISH & HONEYCOMB CORE.

Part: SKIN — CRACKED (LT WING) · airframe 39,846 hrs · 53,367 cycles

SEVERAL CRACKS DEVELOPED IN THE SKIN OTBD OF THE LT NACELLE & AFT OF THE MAIN SPAR ORIGINATING FROM VARIOUS RIVETS.

Part: SKIN — DEBONDED (RT WING) · airframe 39,846 hrs · 53,367 cycles

RIGHT WING DEBOND. UPPER SKIN OF BONDED PANEL IN AREA AROUND FUEL BAY ACCESS OVAL PANEL DEBONDED FROM FUEL ACCESS DISH & HONEYCOMB CORE.

Part: RIB — CRACKED (ZONE 300) · airframe 39,432 hrs · 52,912 cycles

TWO CRACKS WERE DISCOVERED IN THE VERTICAL STABILIZER RIB AT CSS 69. REPAIRED IAW SRM 51-10-21.

Part: DOUBLER — CRACKED (HORIZONTAL STAB) · airframe 39,432 hrs · 52,912 cycles

A CRACK WAS DISCOVERED IN THE LT HORIZONTAL STABILIZER FWD SPAR DOUBLER. THE LT HORIZONTAL STABILIZER FORWARD SPAR DOUBLER WAS REPLACED WITH A NEW PART.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 39,432 hrs · 52,912 cycles

A CRACK WAS DISCOVERED IN THE LT FWD SPAR CAP OF THE VERTICAL STABILIZER ABOVE CSS 61. REPAIRED IAW FR-CO-02599, REV 1.

Part: TEE FITTING — CRACKED (HORIZONTAL STAB) · airframe 39,431 hrs · 52,911 cycles

DURING AN INSPECTION, A CRACK IN THE LT HORIZONTAL STABILIZER LOWER TEE EXTRUSION WAS DISCOVERED. REPAIRED THE CRACKED TEE EXTRUSION BY SPLICING IN A NEW SECTION IAW REPAIR FR-CO-02598. TWO REPAIR ANGLES WERE FABRICATED USING A SECTION OF A NEW TEE.

Part: ACTUATOR — CRACKED (MLG) · airframe 37,255 hrs · 50,500 cycles

MAIN LANDING GEAR ACTUATOR ROD END CAP FOUND CRACKED DURING NDT INSPECTION TO C/W AD 2009-23-01.

Part: SKIN — CORRODED (FUSELAGE)

WHILE CLEANING LITE CORROSION ON SURFACE OF BELLY AFT OF WINGS, NOTICED SOME APPARENT BLISTERING OF THE SKIN. INVESTIGATION REVEALED THERE WAS CORROSION BETWEEN THE SKIN AND THE FUSELAGE FRAME. AFFECTED SKIN WAS CUT OUT AND REPLACED AS A COVER PATCH IN ACCORDANCE WITH BEECH STRUCTURAL REPAIR MANUAL.

Part: FIRE LOOP — BROKEN (RT NACELLE)

PILOT EXPERIENCED A FIRE WARNING ANNUNCIATION DURING TAKEOFF ROLL. PILOT ABORTED TAKEOFF. MAINTENANCE FOUND THAT ONE FIRELOOP HAD FAILED AND CAUSED THE FALSE FIRE INDICATION. (K)

Part: SKIN — CRACKED (HORIZ STAB)

LEADING EDGE OF STABILIZER DISBONDED ON LOWER SIDE AND A CRACK FORMED JUST OFF THE END CAP AND COMPOSITE JOINT. (CONTROL NR 74)

Part: ANGLE — BROKEN (NACELLE)

ANGLE LOCATED ABOVE THE ICE DOOR HINGE. THIS ANGLE HOLDS THE LOWER FIRE SEAL BULK HEAD WHEN THIS ANGLE CRACKS, IT ALLOWS THE OUTSIDE COWL RIVETS TO WORK LOOSE, AND THIS CAUSES THE COWL SIDE SKIN TO CRACK.

Part: BOLT — CORRODED (NOSE STRUT)

BOLT PN 908200115, CONNECTING NOSE GEAR DRAG BRACE TO NOSE STRUT, AND BOLT PN 908200111 CONNECTING THE TWO DRAG BRACE HALVES WAS FOUND WITH PITTING TYPE CORROSION.

Part: CABLE — BROKEN (AIRSTAIR DOOR)

AIRSTAIR DOOR CABLE BROKE, ALLOWING ONE SIDE OF THE DOOR TO REMAIN UNLOCKED.

Part: WIRE — BROKEN (COCKPIT)

THE ICE VANE CONTROL WIRE NUMBER 20A20 BROKE AT THE TERMINAL END UNDER THE PANEL AT INST ZONE 245 CAUSING A SHORT WHICH CAUSED SMOKE IN THE COCKPIT.

Part: SHAFT — DEFECTIVE (T/E FLAP)

INSPECTION OF FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE RIGHT OUTBOARD FLAP CABLE DEFECTIVE. THE INNER SHAFT RETAINER WAS NOT ATTACHED TO THE FERRULE AS REQUIRED. (M)

Part: B-NUT — LOOSE (OIL SYSTEM)

OIL LINE TO THE TORQUE MANIFOLD, B-NUT CAME LOOSE, OIL PRESSURE FLUCTUATED AND ENGINE SHUT DOWN. AIRCRAFT LANDED. ENGINE WAS INSPECTED AS PER MM, LOW OIL PRESSURE PROCEDURE. NO DAMAGE FOUND - OIL SERVICED AND ENGINE TEST RUN PER P/W CHECK.

Part: B-NUT — LOOSE (TORQUE MANIFOLD)

OIL LINE TO THE TORQUE MANIFOLD B-NUT CAME LOOSE. OIL PRESSURE FLUCTUATED AND ENGINE SHUT DOWN. AIRCRAFT LANDED. ENGINE WAS INSPECTED AS PER PWA MM. LOW OIL PRESSURE PROCEDURE, NO DAMAGE FOUND. OIL SERVICED AND ENGINE TEST RUN, PER PWA CHECK.

Part: TRIM TAB — CORRODED (LT AILERON)

LEFT AILERON TRIM TAB HORN CORRODED.

Part: CAP — CORRODED (LT STABILIZER)

LOWER CAP LEFT STABILIZER OUTER 6 IS CORRODED.

Part: SPAR CAP — CORRODED (HORZ STAB)

FOUND THE OUTBOARD 6 INCHES LOWER RIGHT REAR SPAR CAP EXTRUSION CORRODED. CORROSION WAS FOUND WHILE REPLACING A CORRODED OUTBOARD ELEVATOR HINGE BRACKET.

Part: INTERCOSTAL — CRACKED (FUSELAGE)

P43 INSPECTION FOUND A .8 INCH CRACK IN THE OUTDBOARD FLANGE RADIUS OF THE INTERCOSTAL AT THE UPPER CARGO DOOR FRAME AT FS 494.

Part: HINGE BRACKET — CORRODED (ELEVATOR)

DURING INSPECTION, THE RIGHT OUTBOARD AND THE RIGHT MIDDLE ELEVATOR HINGE BRACKET WERE FOUND TO BE CORRODED.

Part: BLOCK — WORN (BETA SYSTEM)

FLT 9410 - MIA/EYW - AFTER ROTATION, RIGHT PROP RPM DROPPED TO APPROXIMATELY 1200 RPM. RETURNED TO MIA. DETERMINED RIGHT BETA BLOCK TO BE WORN. REPLACED RIGHT BETA BLOCK AND RIGGED. (M)

Part: NOZZLE — LOOSE (LT ENGINE)

FLT 9209 - ON CLIMB-OUT FROM TAMPA, RIGHT T-HANDLE FIRE WARNING ILLUMINATED. PILOT SHUT DOWN ENGINE, DECLARED EMERGENCY AND RETURNED TO TAMPA. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED RIGHT ENGINE. NO EVIDENCE OF FIRE. DETERMINED TO BE HOT AIR LEAKING FROM LOOSE INLET HEAT BLAST TUBE. SECURED BLAST TUBE CLAMP. (M)