N1275N

CESSNA 208B No injuries Part 135 — Hageland Aviation Services, Inc.

Operated by HAGELAND AVIATION SERVICES INC (per NTSB report)

ATA 5520

Part: HINGE — CORRODED (ELEVATOR) · airframe 18,944 hrs

DURING SCHEDULE INSPECTION IT WAS NOTED THAT ELEVATOR HINGE PART NUMBER 2632055-1 HAD EXFOLIATED CORROSION TO THE EXTENT THAT THE PART HAD TO BE REPLACED.

ATA 5751

Part: STRUCTURE — CRACKED (LT AILERON) · airframe 13,998 hrs · 30,661 cycles

LEFT AILERON L/E SKIN CRACKED AT OTBD BALANCE WEIGHT ATTACH POINT. REPLACED AILERON ASSEMBLE WITH SERVICEABLE UNIT.

ATA 7110

Part: ANGLE — CRACKED (NOSE CAP)

FORWARD ANGLE ON LEFT NOSE CAP FOR INDUCTION AIR PLENUM ATTACHMENT CRACKED. (X)

ATA 2752

Part: ACTUATOR — SHEARED (TE FLAPS)

STANDBY FLAP MOTOR INOPERATIVE. ACTUATOR SHAFT ROLL PIN SHEARED. JACKSCREW CONTAMINATED WITH METAL PARTICLES, MOTOR INOPERATIVE. UPON REPLACEMENT OF TRANSMISSION ASSY, ALSO DISCOVERED ELECTRICAL PIN IN PRIMARY FLAP MOTOR POWER CONNECTOR PARTIALLY DISENGAGED CAUSED BY PIN LOCKING TABS NOT EXTENDED. (X)

ATA 7532

Part: BLEED VALVE — FAILED (ENGINE)

MANUFACTURER RECALLED THIS SPECIFIC COMPRESSOR BLEED VALVE FOR TESTING OF INTERNAL PACKING FOR DEFECTS. BLEED VALVE SERIAL NUMBER FELL OUTSIDE OF ANY AD OR SB. (X)

ATA 2842

Part: TRANSMITTER — SHORTED (LEFT WING)

LEFT FUEL QUANTITY INDICATOR INACCURATE AND ERRATIC. REPLACED DEFECTIVE CENTER OUTBOARD FUEL SENDING UNIT. (X)

ATA 7261

Part: O-RING — CUT (ENGINE OIL)

DURING A POST-FLIGHT INSPECTION, THE PILOT NOTED EXCESSIVE OIL ON THE LOWER COWL AND DOWN THE LEFT SIDE OF THE AIRCRAFT. UPON FURTHER INSPECTION, DETERMINED A NR 2 BEARING OIL SCAVENGETUBE COUPLING O-RING LOCATED AT C-FLANGE WAS LEAKING. UPON REMOVAL OF THE O-RING, IT WAS FOUND TO BE 75 PERCENT CUT IN HALF. THE O-RING WAS REPLACED. (X)