N47542

Part: FUEL CAP — MISSING (RT WING) · airframe 30,958 hrs · 40,111 cycles

FLIGHT 4031 FLL/FLL AFTER TAKEOFF RIGHT FUEL CAP LOST FLIGHT. INSTALLED FUEL CAP ON RIGHT WING.

Part: CABLE — INOPERATIVE (AIRSTAIRS) · airframe 30,654 hrs · 39,692 cycles

FLIGHT: 4066 EYW/GNV PILOT REPORTED AIRSTAIR IS NOT CLOSING, INOPERATIVE. REPLACED AIRSTAIR DOOR LOWER FORWARD DOOR CABLE OPERATIONAL CHECK GOOD.

Part: HANDLE — STIFF (EMERGENCY EXIT) · airframe 300,098 hrs · 39,012 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT EMERGENCY EXIT OUTER HANDLE STIFF TO OPERATE. CLEANED AND LUBRICATED LEFT EMERGENCY EXIT OUTER HANDLE.

Part: STRINGER — CRACKED (VERTICAL STAB) · airframe 29,650 hrs · 38,482 cycles

DURING SCHEDULED C-6 INSPECTION DISCOVERED VERTICAL STABILIZER BAY 331 DL RIGHT OF CANTED RIB 54.026 ONE CRACK AT 29.75 STRINGER AND ONE CRACK AT 49.25 PERCENT CHORD STRINGER. REPAIRED.

Part: STRINGER — CRACKED (VERTICAL STAB) · airframe 29,650 hrs · 38,482 cycles

DURING SCHEDULED C-6 INSPECTION DISCOVERED VERTICAL STABILIZER BAY 331 DL RIGHT OF CANTED RIB 54.026 ONE CRACK AT 39.5% CHORD STRINGER AND ONE CRACK AT VERTICAL STABILIZER BAY 331 CL RIGHT OF CANTED RIB 69.184 AT 49.25% CHORD STRINGER. INSTALLED REPAIRS AT RIGHT SIDE OF CANTED RIB 54.026 AT 39.5% STRINGER AND CANTED RIB 69.184 AT 49.25% CHORD STRINGER.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 29,472 hrs · 38,258 cycles

FLIGHT: 4073 CLE/LWB DURING TAKEOFF ROLL HEARD A LOUD BANG COMING FROM THE LEFT ENGINE A LOSS OF POWER AND A HUMMING NOISE AFTER ENGINE SHUTDOWN AND VISUAL INSPECTION SEVERAL BUMPS ARE FOUND ON THE LEFT ENGINE EXHAUST. REPLACED LEFT ENGINE ASSEMBLY.

Part: UPLOCK SWITCH — FAULTY (MLG) · airframe 29,022 hrs · 37,434 cycles

AFTER RETRACTING THE LANDING GEAR THE RED GEAR HANDLE LIGHT REMAINED ILLUMINATED. RAN QRH AND THE LIGHT STILL REMAINED ILLUMINATED. EXTENDED THE LANDING GEAR AND RETURNED TO OUR DEPARTING STATION. A NORMAL LANDING WAS EXECUTED WITH NAY FURTHER INCIDENT. R & R NLG UPLOCK SWITCH.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,997 hrs · 37,379 cycles

DURING SCHEDULED STRUCTURAL INSP, DISCOVERED LT HEAVY ANGLE CRACKED AT FWD END APPROX 1.7 INCHES. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,997 hrs · 37,379 cycles

DURING SCHEDULED STRUCTURAL INSP, DISCOVERED RT HEAVY ANGLE CRACKED AT FORWARD END, APPROX 2.0 INCHES. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE.

Part: DOOR FRAME — CRACKED (BS 150) · airframe 28,997 hrs · 37,379 cycles

DURING SCHEDULED STRUCTURAL INSP, DISCOVERED AIRSTAIR DOOR FRAME CRACKED AT LOWER COUNTER BALANCE MOUNT. REMOVED DAMAGED PORTION OF ANGLE AND INSTALLED FRAME REPAIR SECTION.

Part: UPLOCK SWITCH — OUT OF ADJUST (NLG) · airframe 28,875 hrs · 37,133 cycles

DURING FLIGHT, LANDING GEAR UNSAFE LIGHT ILLUMINATED WITH GEAR HANDLE IN THE RETRACT POSITION. GEAR EXTENDED NORMALLY UPON LANDING. ADJUSTED NOSE GEAR UPLOCK INDICATOR SWITCH, LANDING GEAR OPS CHECK OK.

Part: UPLOCK SWITCH — DIRTY (NLG) · airframe 28,870 hrs · 37,123 cycles

PILOT REPORTED WHEN LANDING GEAR SELECTED UP THE RED GEAR UNSAFE LIGHTS REMAIN ILLUMINATED. RAN QRH SELECTED GEAR DOWN AND GOT 3 GREEN LIGHTS EXECUTED A NORMAL LANDING. CLEANED NLG UPLOCK SWITCH, OPS CHECKS GOOD.

Part: LATCH — OUT OF ADJUST (PAX DOOR) · airframe 28,738 hrs · 36,870 cycles

PILOT REPORTED AIRSTAIR DOOR CAM LOCKS, DOOR DIFFICULT TO LOCK AND UNLOCK FROM OUTSIDE. ADJUSTED AIRSTAIR DOOR UPPER FWD CAM LATCH, OPS CHECK GOOD.

Part: PROPELLER — MALFUNCTIONED · airframe 28,708 hrs · 36,816 cycles

PILOT REPORTED WHEN PULLING PROPS BACK FROM 1550 RPM ON THE DESCENT TO 1400 RT PROP LAGGED ABOUT A KNOB AND HALF FROM LT SIDE PROPS WERE OUT OF SYNC AND COULD NOT GET INTO SYNC. WHEN PROPS PUSHED FULL FWD LT PROP REACHED ABOUT 1700 RPM WHILE RT PROP INCREASED TO OVER 1800 RPM. BOTH PROPS WERE PULLED TO 1700 RPM BY THE GAUGE AND LANDED WITHOUT INCIDENT. COMPLIED WITH PROPELLER CONTROL RIGGING, OPS CKS NORMAL.

Part: RELAY — INOPERATIVE (MLG) · airframe 28,258 hrs · 35,995 cycles

DURING APPROACH, LANDING GEAR CIRCUIT BREAKER POPPED ON GEAR EXTENSION. RESET BREAKER AND POPPED AGAIN. MANUALLY EXTENDED LANDING GEAR GOT DOWN LOCK INDICATION. DIVERTED AND LANDED WITHOUT INCIDENT. REPLACED 60AMP, LANDING GEAR CIRCUIT BREAKER AND LANDING GEAR MOTOR RELAY. OPS CHECK GOOD.

Part: CIRCUIT BREAKER — POPPED (LANDING GEAR) · airframe 28,045 hrs · 35,606 cycles

DURING APPROACH LANDING GEAR CIRCUIT BREAKER POPPED. INSPECTED HYD POWER PACK AND WIRING NO DEFECTS NOTED COMPLIED WITH LANDING GEAR EXTEND/RETRACT SYS INSP CYCLED LANDING GEAR SEVERAL TIMES COULD NOT DUPLICATE.

Part: SAFETY SWITCH — SHORTED (MLG WARNING) · airframe 27,590 hrs · 34,843 cycles

PILOT REPORTED LANDING GEAR SILENCE BUTTON DOES NOT SILENCE GEAR WARNING. REPLACED AND ADJUSTED RT MLG SAFETY SWITCH LANDING GEAR OPS CHECKS GOOD.

Part: GUIDE — BENT (DOOR CABLE) · airframe 27,319 hrs · 34,386 cycles

FLIGHT: 5200 CLE/DUJ PILOT REPORTED CABIN DOOR VERY DIFFICULT TO CLOSE AND TO EXTINGUISH CABIN DOOR ANNUNCIATOR. REPLACED CABLE GUIDE AND AFT UPPER CAM SWITCH OPERATIONAL AND RIG CHECK GOOD.

Part: DOOR — BROKEN (MLG) · airframe 27,319 hrs · 34,386 cycles

FLIGHT: 9303 LWB/CLE PILOT REPORTED LEFT MAIN GEAR CAM DOOR ASSEMBLY ON INBOARD GEAR DOOR BROKEN. INSTALLED NEW CAM DOOR ASSEMBLY ON LEFT MAIN GEAR INBOARD GEAR DOOR.

Part: ACTUATOR — MALFUNCTIONED (RT MLG) · airframe 27,221 hrs · 34,227 cycles

DURING APPROACH LANDING GEAR MAINS TAKE LONGER 10-15 SECONDS TO LOCK INTO POSITION. REPLACED RT MLG ACTUATOR. OPS CHECK NORMAL.

Part: SPAR — CORRODED (RT WING) · airframe 26,897 hrs · 33,673 cycles

DURING SCHEDULED RT WING X-RAY INSP DISCOVERED INDICATION OF CORROSION ON FWD LWR SPAR ANGLE AT WS 126.5. BLENDED OUT CORROSION AND INSTALLED REINFORCEMENT STRAP.

Part: CIRCUIT BREAKER — FAILED (MLG) · airframe 26,734 hrs · 33,432 cycles

DURING APPROACH, CANNOT SILENCE LANDING GEAR WARNING HORN. REPLACED LANDING GEAR WARNING HORN CIRCUIT BREAKER. OPS CHECK GOOD.

Part: PRESSURE BLKHD — CHAFED (FUSELAGE) · airframe 26,732 hrs · 33,428 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT PRESSURE BULKHEAD CHAFED AT APPROX FS 256. BLENDED AND POLISHED CHAFED AREA AND PERFORMED NDT-DYE PENETRANT INSP TO CHAFE AREA NO DEFECTS NOTED.

Part: SKIN — CHAFED (LT WING) · airframe 26,732 hrs · 33,428 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED SKIN CHAFE AT LT CTR WING L/E AREA APPROXFS 256 TO 265. REPAIRED LEFT CENTER WING SKIN CHAFE INSTALLED REPAIR DOUBLER.

Part: PRESSURE BLKHD — CHAFED (BS 256) · airframe 26,732 hrs · 33,428 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED LT PRESSURE BULKHEAD CHAFED AT APPROXIMATELY FS 256. BLENDED AND POLISHED CHAFED AREA AND PERFORMED NDT-DYE PENETRANT INSP TO CHAFE AREA NO DEFECTS NOTED.

Part: SKIN — CHAFED (RT WING) · airframe 26,732 hrs · 33,428 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED SKIN CHAFE AT RT CTR WING L/E AREA APPROX FS 256 TO 265. REPAIRED BY INSTALLING REPAIR DOUBLER TO CHAFE AREA.

Part: SWITCH — OUT OF ADJUST (MLG) · airframe 26,371 hrs · 32,912 cycles

PILOT REPORTED LANDING GEAR WARNING HORN SOUNDS AT 3000 FT LBS TORQUE AT 91 PERCENT N1. ADJUSTED RT GEAR WARNING HORN SWITCH TEST FLIGHT SATISFACTORY.

Part: MASTER CYLINDER — MALFUNCTIONED (BRAKES) · airframe 26,209 hrs · 32,646 cycles

PILOT REPORTS RT BRAKE PEDAL STILL GOES TO THE GROUND. HAVE TO CONSTANTLY PUMP TO BRAKE. REPLACED NR 4 BRAKE MASTER CYL, BLED BRAKE LINES. OPS CHECK NORMAL.

Part: BRAKE — MALFUNCTIONED (MLG) · airframe 26,203 hrs · 32,638 cycles

PILOT REPORTS RT BRAKE GOES TO THE GROUND. BLED BRAKES. LEAK CHECK AND OPS CHECK NORMAL.

Part: HANDLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 26,075 hrs · 32,433 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED EMERGENCY EXIT DOOR AT SEAT 6F EXTERNAL HANDLE IS TIGHT AND DOES NOT SPRING OUT. LUBRICATED HANDLE, OPS CHECK GOOD.

Part: CABLE — FRAYED (AIRSTAIR DOOR) · airframe 25,841 hrs · 32,092 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED AIRSTAIR DOOR AFT UPPER FORWARD CABLES FRAYED. REPLACED AIRSTAIR DOOR AFT UPPER CABLE.

Part: CABLE — FRAYED (AIRSTAIR DOOR) · airframe 25,841 hrs · 32,092 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED AIRSTAIR DOOR AFT LOWER FORWARD CABLE FRAYED. REPLACED AIRSTAIR DOOR AFT LOWER CABLE.

Part: HINGE BRACKET — CORRODED (ELEVATOR) · airframe 24,750 hrs · 30,655 cycles

DURING SCHEDULED MAINT, DISCOVERED RT OB ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT OB ELEVATOR HINGE BRACKET.

Part: HANDLE — CRACKED (AIRSTAIR DOOR) · airframe 24,388 hrs · 30,241 cycles

DURING SCHEDULED ROUTINE MAINT, DISCOVERED AIRSTAIR DOOR INTERIOR HANDLE CRACKED. REPLACED AIRSTAIR DOOR INTERIOR HANDLE.

Part: CABLE — FAILED (AIRSTAIR) · airframe 24,388 hrs · 30,241 cycles

FLIGHT: 9302, PILOT REPORTED CABIN DOOR EXTREMELY HARD TO OPEN FROM OUTSIDE. REPOSITIONED AIRSTAIR DOOR FWD UPPER HANDRAIL CABLE.

Part: BEARING — FAILED (NR 2 WHEEL) · airframe 23,775 hrs · 29,538 cycles

FLIGHT: 9171, AFTER LANDING ROLL OUT LOST ALL BRAKE PRESSURE ON LT TOE BRAKES. DETERMINED NR TWO MAIN WHEEL ASSEMBLY BEARING FAILED,REPLACED NR ONE AND TWO MAIN WHEEL ASSEMBLIES AND LT MAIN LANDING GEAR ASSEMBLY.

Part: CONNECTOR — LOOSE (MLG) · airframe 23,589 hrs · 29,307 cycles

DURING APPROACH LANDING GEAR FAILED TO EXTEND WHEN GEAR HANDLE PLACED IN THE DOWN POSITION. RETURNED TO DEPARTURE. MANUALLY EXTENDED LANDING GEAR. LANDED WITHOUT INCIDENT. SECURED LOOSE CONNECTOR P200 AT LANDING GEAR CONTROL. OPERATIONAL CHECK NORMAL.

Part: SPAR CAP — CRACKED (LT WING) · airframe 23,445 hrs · 29,132 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT WING REAR SPAR LOWER CAP CRACKED FROM RIVET HOLE TO REAR EDGE AT LWS 117.50. REMOVED DAMAGED SECTION OF LT LOWER AFT SPAR FROM LWS 73 TO LWS 129.86 SPLICED IN NEW SECTION OF SPAR IAW FIELD REPAIR FR-CO-01583 REV 2.

Part: BEARING — FAILED (NOSE WHEEL) · airframe 22,352 hrs · 27,870 cycles

FLIGHT: 9179 FLL/EYW AFTER LANDING IN EYW FELT SOME VIBRATION LOST NOSE WHEEL. REPLACED NOSE GEAR ASSEMBLY AND NOSE WHEEL ASSEMBLY.

Part: SKIN — TORN (FUSELAGE) · airframe 18,840 hrs · 23,737 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED SKIN TEAR AT FS 475.5 RUNNING FROM THE SKIN EDGE AT THE AFT CARGO DOOR LOWER DOOR SILL EXTENDING DOWN 2.5 INCHES. STOP DRILLED TEAR AND INSTALLED EXTERNAL DOUBLER REPAIR.

Part: BRACKET — CORRODED (RT ELEVATOR)

AT SCHEDULED ROUTINE MAINTENANCE, RT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT CENTER ELEVATOR HINGE BRACKET. (K)

Part: FIRE LOOP — BROKEN (RT ENGINE)

AFTER TAKEOFF, FIRE LOOP ENUNCIATOR AND RT T-HANDLE ILLUMINATED. THE RT ENGINE WAS SHUT DOWN AND THE FIRE EXTINGUISHER WAS FIRED. DECLARED AN EMERGENCY RETURN TO FLL. INSPECTED RT ENGINE. NO EVIDENCE OF FIRE OR FLUID LEAKS FOUND. FORWARD FIRE LOOP BROKEN AT FIREWALL CONNECTOR. REMOVED AND REPLACED FORWARD FIRE LOOP. REMOVED AND REPLACED RT ENGINE FIRE EXTINGUISHER BOTTLE. OPERATIONAL CHECK NORMAL.

Part: BRACKET — CORRODED (RT STAB)

AT SCHEDULED ROUTINE MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RIGHT OUTBOARD ELEVATOR HINGE BRACKET. (M)

Part: BOLT — LOOSE (VERTICAL STAB)

(BOLT) AT REDUCED INTERVAL FLEET CAMPAIGN, DISCOVERED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT, UPPER BOLTS REQUIRED RETORQE. RETORQUED VERTICAL STABILIZER FORWARD SPAR LOWER ATTACH POINT UPPER BOLTS IAW MFG MM.

Part: SWITCH — FAULTY (RT ENGINE)

CLE FLIGHT3007 THE CREW REPORTED THAT ON FINAL APPROACH, THOUGHT A PROPELLER HAD AUTOFEATHERED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE AUTOFEATHER LOW PRESSURE SWITCH. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: GOVERNOR — OUT OF ADJ (LEFT ENGINE)

CLE FLIGHT#3240 THE CREW REPORTED THE LEFT ENGINE GOES INTO FEATHER BEFORE THE FEATHER STOP.MAINTENANCE INSPECTED AND ADJUSTED THE #1 ENGINE PROPELLOR GOVERNOR FEATHER PLUNGER.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SWITCH — FAILED (COCKPIT)

CLE FLIGHT# 3375 THE CREW REPORTED AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT WITHOUT USING THE DOWN LOCK RELEASE SWITCH.MAINTENANCE REPLACED THE LANDING GEAR CONTROL SWITCH.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SWITCH — LOOSE (PITCH CONTROL)

ON APPROACH TO CLE CREW REPORTED RIGHT SIDE OF FIRST OFFICER''S CONTROL WHEEL (YOKE) WAS EMITTING SMOKE. A EMERGENCY WAS DECLARED AND A/C LANDED AND TAXIED TO GATE WITHOUT FURTHER INCIDENT. MX INSPECTED AND REASSEMBLED THE FIRT OFFICER''S FLIGHT DIRECTOR SYNC, SWITCH BACK INTO THE YOKE IAW BEECHCRAFT IPC 27-10-00. OPS CHECKS WERE GOOD IAW BEECH 1900 MM 22-10-00. THE A/C WAS RELEASED FOR SERVICE.

Part: TORQUE TUBE — DAMAGED (RT ELEVATOR)

IAH - DURING 200 HOUR INSPECTION, THE RIGHT ELEVATOR WAS FOUND TO HAVE PLAY AT THE TORQUE TUBE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED TORQUE TUBE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: UPLOCK SWITCH — INOPERATIVE (RT MLG)

IAH - DURING FLIGHT 3449, THE CREW REPORTED A GEAR UNSAFE LIGHT DURING EXTENSION AND RETRACTION. THE CREW MANUALLY EXTENDED THE LANDING GEAR AND RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG UPLOCK SWITCH IAW B1900-D MM 32-61-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: POWER PACK — FAILED (LT MLG)

CLE - FLT 3280 - CREW REPORTED THAT AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD WITHOTU FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE HYDRAULIC POWER PACK IAW B1900D MM 32-30-02. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: TORQUE GAUGE — INTERMITTENT (RT ENGINE)

CLE - FLT 3263 - CREW REPORTED THE RIGHT HAND ENGINE TORQUE GAUGE FLUCTUATES FROM 5,000 TO ZERO IN FLIGHT. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGINE TORQUE GAUGE IAW B1900D MM 77-10-00, OPERATION CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X)