N81533

Part: SKIN — CORRODED (RT WING) · airframe 31,857 hrs · 37,956 cycles

DURING SCHEDULED X-RAY INSP DISCOVERED CORROSION RT WING LOWER SKIN NR 2 STRINGER IN COLLECTOR TANK INBD OF MAIN DRAIN. REMOVED SURFACE CORROSION PERFORMED FLOURESCENT PENETRANT INSPECTION NO FURTHER CORROSION FOUND.

Part: STRINGER — CORRODED (LWS 124.25-114.2) · airframe 31,857 hrs · 37,956 cycles

DURING SCHEDULED X-RAY INSPECTION DISCOVERED MINOR CORROSION ON LEFT WING NR 1 STRINGER IN THE COLLECTOR TANK WS 124.25-114.25. REMOVED CORROSION AND INSTALLED REPAIR STRINGER AND REPAIR DOUBLERS.

Part: SKIN — CORRODED (RT WING) · airframe 31,857 hrs · 37,956 cycles

DURING SCHEDULED X-RAY INSPECTION DISCOVERED CORROSION RIGHT WING LOWER SKIN RIB IN COLLECTOR TANK FORWARD OF MAIN SPAR OUTBOARD WS 125.25. REMOVED SURFACE CORROSION PERFORMED FLOURESCENT PENETRANT INSPECTION NO FURTHER CORROSION FOUND.

Part: TRUSS — CRACKED (ENGINE) · airframe 31,853 hrs · 37,955 cycles

DURING MAG PARTICLE INSP, DISCOVERED ENGINE TRUSS TUBE WELD AREA CRACK. (OPEN)

Part: LONGERON — CRACKED (BS 107) · airframe 31,853 hrs · 37,955 cycles

DURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED RIGHT LONGERON CRACKED APPROXIMATELY 2.0 INCHES AND FORMER DAMAGE AT APPROXIMATELY FS 107 DIRECTLY BELOW FIRST OFFICERS STORM WINDOW. REMOVED DAMAGED SECTION OF LONGERON AND INSTALLED REPAIR REINFORCEMENT ANGLE AND FORMER REPAIR STRAP.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 31,853 hrs · 37,955 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED 7.0 INCH CRACK ALLTHE WAY THROUGH THE CARGO FRAME FROM ONE END TO THE OTHER AT FS 509.5 STRINGER 15L. REMOVED DAMAGED SECTION OF CRACKED FRAME AND INSTALLED ANGLE REINFORCEMENT STRAIGHT "L" ANGLE REPAIR.

Part: FRAME — CRACKED (BS 509.5) · airframe 31,853 hrs · 37,955 cycles

REPORT: DURING SCHEDULED ROUTINE INSPECTION DISCOVERED 2.5 INCH CRACK IN THE CARGO FRAME INNER SKIN FROM THE LIGHTNING HOLE TO EDGE AT FS 509.5 STRINGER 11L. REMOVED DAMAGED SECTION OF CRACKED FRAME AND INSTALLED INSERTION PATCH AND COVER PATCH.

Part: ANGLE — CRACKED (BS 288) · airframe 31,853 hrs · 37,955 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED LT WING FUSELAGE CLOSING ANGLE CRACKED 1.0 INCH AT FS 288.0. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE.

Part: ANGLE — CRACKED (BS 150) · airframe 31,853 hrs · 37,955 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED CRACK FWD ANGLE AT FS 150 TOP STRUT ASSY SUPPORT BRACKET NUTPLATE. REMOVED DAMAGED ANGLE AND INSTALLED FILLER ANGLE AND REPAIR SPLICES.

Part: ANNUNCIATOR — WORN (MLG) · airframe 31,620 hrs · 37,712 cycles

PILOT REPORTED WHEN GEAR IS LOWERED YOU MUST TAP ON THE "NOSE" ANNUNCIATOR FOR IT TO ILLUMINATE. REPLACED NOSE ANNUNCIATOR ASSY OPS CHECK GOOD.

Part: ANNUNCIATOR — LOOSE (NLG INDICATOR) · airframe 31,584 hrs · 37,665 cycles

NOSE GEAR INDICATION LOOSE. RESECURED NOSE GEAR ANNUNICATOR.

Part: LAMP — LOOSE (NLG INDICATOR) · airframe 31,583 hrs · 37,664 cycles

NOSE GEAR INDICATION LOOSE. RESECURED NOSE GEAR INDICATION LAMP.

Part: DOOR — LACK OF LUBE (EMERGENCY EXIT) · airframe 31,054 hrs · 37,078 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED LT EMERGENCY EXIT DOOR IS HARD TO LOCK. LUBRICATED LT EMERGENCY DOOR OPS CHECK NORMAL.

Part: WIRE — LOOSE (MLG) · airframe 31,054 hrs · 37,078 cycles

DURING APPROACH, LANDING GEAR DOWN, NO 3 GREEN LIGHT INDICATION. RECONNECTED LOOSE WIRE AT LIGHT SENSOR ASSY. OPS CHECK GOOD.

Part: DOOR — BINDING (EMERGENCY EXIT) · airframe 30,875 hrs · 36,891 cycles

DURING SCHEDULED ROUTINE MX, DISCOVERED LT EMERGENCY EXIT HARD TO CLOSE. MADE ADJUSTMENTS TO UPPER PIN GUIDES, OPS CHECK GOOD.

Part: DOOR — BINDING (EMERGENCY EXIT) · airframe 30,875 hrs · 36,891 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED RT AFT EMERGENCY EXIT HARD TO OPEN. LUBRICATED RT AFT EMERGENCY EXIT OPS CHECK GOOD.

Part: DOOR LATCH — INOPERATIVE (EMERGENCY EXIT) · airframe 30,816 hrs · 36,831 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT AFT EMERGENCY EXIT HARD TO OPEN. LUBRICATED RT AFT EMERGENCY EXIT DOOR LATCH MECHANISM. OPS CHECK GOOD.

Part: AOA — MALFUNCTIONED (STALL WARNING) · airframe 30,788 hrs · 36,794 cycles

UPON TAKEOFF AFTER LANDING GEAR UP STALL WARNING CAME ON AND SOUNDED UP TO 500 FEET ON AND OFF. SECURED AND CLEANED STALL WARNING VANE. TEST FLIGHT SATISFACTORY.

Part: TRANSDUCER — FLUCTUATES (TORQUE GAUGE) · airframe 30,788 hrs · 36,794 cycles

DURING TEST FLIGHT, LT TORQUE GAUGE WENT TO 5,000 THEN STARTED TO FLUCTUATE TO ZERO. REPLACED LT TORQUE TRANSDUCER, OPERATIONAL CHECK OK. TEST FLIGHT SATISFACTORY.

Part: PROXIMITY SWITCH — OUT OF ADJUST (MLG) · airframe 30,769 hrs · 36,770 cycles

AFTER TAKEOFF LANDING GEAR UNSAFE LIGHTS IN THE GEAR HANDLE REMAIN ILLUMINATED AFTER GEAR RETRACTION. ADJUSTED LT MAIN GEAR UP POSITION SWITCH. OPS CHECK NORMAL TEST FLIGHT SATISFACTORY.

Part: SKIN — DENTED (RT WING) · airframe 30,769 hrs · 36,769 cycles

DURING INSPECTION FOUND SKIN DENTS ON SEVERAL AREAS OF RIGHT WING UPPER SKIN BETWEEN WS 236.62 AND WS 249.75. CUT OUT DAMAGED AREAS AND INSTALLED AN INSERTION PATCH AND REPAIR DOUBLERS.

Part: CONTROL HANDLE — INTERMITTENT (MLG) · airframe 30,755 hrs · 36,759 cycles

FLIGHT 9200, DURING APPROACH WHEN LANDING GEAR IS EXTENDED THE IN TRANSIT LIGHTS IN THE GEAR HANDLE DO NOT ILLUMINATE. REPLACED LANDING GEAR SWITCH CONTROL HANDLE, OPERATIONAL CHECK GOOD.

Part: WIRE HARNESS — INOPERATIVE (SQUAT SWITCH) · airframe 30,734 hrs · 36,737 cycles

PILOT REPORTED UPON DEPARTURE, LANDING GEAR J HOOK WOULD NOT MOVE TO THE LT TO PRESS DOWN LOCK RELEASE TO RETRACT GEAR. REPLACED LT SQUAT SWITCH AND HARNESS, OPS CK NORMAL.

Part: DOOR — BINDING (EMERGENCY EXIT) · airframe 30,540 hrs · 36,513 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT AFT EMERGENCY EXIT HARD TO OPEN. CLEANED AND LUBRICATED LATCH SYS.

Part: CONNECTOR — LOOSE (MLG HANDLE) · airframe 30,502 hrs · 36,468 cycles

FLIGHT 9316 FLL/FPO AFTER TAKEOFF LEFT MAIN LANDING GEAR DID NOT RETRACT, GEAR HANDLE ILLUMINATED RED. WHEN LANDING GEAR DOWN THREE GREEN GEAR HANDLE INDICATED SAFE. RETURNED TO FLL LANDED WITHOUT INCIDENT. RE-SECURED CONNECTOR P200 AT LANDING GEAR HANDLE. OPERATIONAL CHECK OK.

Part: HINGE BRACKET — CORRODED (LT ELEVATOR) · airframe 30,199 hrs · 36,127 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED LT ELEVATOR OTBD SUPPORT HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR OTBD HINGE BRACKET.

Part: SPAR — DAMAGED (WING) · airframe 30,199 hrs · 36,127 cycles

COMPLIED WITH COLD EXPANSION OF FASTENER HOLES IN THE WING REAR SPAR LOWER CAP IAW FAA APPROVED DATA CONTAINED IN THE ACFT COMPANY KIT 118-4014-0003.

Part: CIRCUIT BREAKER — TRIPPED (MLG) · airframe 30,196 hrs · 36,122 cycles

FLIGHT: 9174 MIA/TPA PILOT REPORTED LANDING GEAR RELAY CIRCUIT BREAKER POPPED. TROUBLESHOT SYSTEM CHECKED LANDING GEAR RELAY CIRCUIT BREAKER COULD NOT DUPLICATE. TEST FLIGHT SATISFACTORY.

Part: ACCESS PANEL — DEBONDED (RT WING) · airframe 30,152 hrs · 36,078 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RIGHT WING FUEL ACCESS PANEL 632 AT INNER RING DEBONDED. FABRICATED AND INSTALLED RING DOUBLER REPAIR AT ACCESS PANEL 632AT.

Part: ACCESS PANEL — DEBONDED (LT WING) · airframe 30,152 hrs · 36,078 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT WING FUEL ACCESS PANEL 531DB INTERNAL RING DEBONDED. FABRICATED AND INSTALLED RING DOUBLERS AT WING FUEL ACCESS PANEL 531DB.

Part: DOOR — INOPERATIVE (MAIN PAX) · airframe 30,121 hrs · 36,043 cycles

FLIGHT: 9167 MCO/PNS PILOT REPORTED AIRSTAIR DOOR WILL NOT OPEN. REPOSITIONED AIRSTAIR DOOR HANDRAIL CABLE OPERATIONAL CHECK GOOD.

Part: CAM — DIRTY (PAX DOOR) · airframe 29,986 hrs · 35,919 cycles

PILOT REPORTED CABIN DOOR HARD TO CLOSE. CLEANED CABIN DOOR CAMS, OPS CHECK GOOD.

Part: VALVE — STICKING (MLG)

AFTER TAKEOFF, WHEN SELECTING GEARS UP NOTHING HAPPENED BECAUSE OF TRIPPED CIRCUIT BREAKER. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR SERVICE VALVE. TEST FLIGHT SATISFACTORY.

Part: SWITCH — BROKEN (MLG HANDLE) · airframe 29,965 hrs · 35,890 cycles

AFTER TAKEOFF, TRIED TO PUT THE LANDING GEAR UP HAD TO USE THE DOWN LOCK RELEASE BUTTON TO GET HANDLE UP, GEAR CIRCUIT BREAKER POPPED. RAN QRH RETURNED GEAR HANDLE TO THE DOWN POSITION. RETURNED TO DEPARTURE LANDED WITHOUT INCIDENT. TROUBLESHOT LANDING GEAR WIRING FOR RETRACTION AND EXTENSION SYS. REPLACED LANDING GEAR HANDLE. OPS CHECK GOOD.

Part: DOOR — OBSTRUCTED (PAX DOOR) · airframe 29,899 hrs · 35,815 cycles

PILOT REPORTED PLASTIC INTERIOR OF CABIN DOOR GETS STUCK ON DOOR JAMB WHEN OPENING. REPLACED WELL NUTS AND RESECURED AIRSTAIR DOOR FWD COVER, OPS CHECK GOOD.

Part: SKIN — CORRODED (AIRSTAIR DOOR) · airframe 29,859 hrs · 35,765 cycles

DURING SCHEDULED ROUTINE MX, DISCOVERED AIRSTAIR DOOR LOWER FWD SKIN EXFOLIATED AND CRACKED AND LOWER AFT AREA DEBONDED. OPEN

Part: SWITCH — OUT OF ADJUST (MLG WARNING HORN) · airframe 29,373 hrs · 35,247 cycles

DURING FLIGHT GEAR WARNING HORN SOUNDS ON 2300 LBS OF TORQUE. RIGGED RT LANDING GEAR WARNING HORN SWITCHES. OPS CHECK NORMAL. TEST FLIGHT SATISFACTORY.

Part: BRACKET — FAILED (MLG) · airframe 29,237 hrs · 35,107 cycles

FLT: 9274. PILOT REPORTED LANDING GEAR HORN COMES ON AROUND 8O PERCENT N1. REPLACED RIGHT LANDING GEAR SWITCH BRACKET ASSEMBLY AND RIGGED LANDING GEAR SWITCHES AND AUTOFEATHER SWITCHES.OPERATIONAL CHECK NORMAL ON THE GROUND.TEST FLIGHT SATISFACTORY.

Part: ACCESS PANEL — LEAKING (RT WING) · airframe 29,193 hrs · 35,066 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED FUEL LEAK AT RT WING LWR PANELS FOUND FUEL PANEL 631DB DELAMINATED AND WING SKIN DELAMINATED. FABRICATED AND INSTALLED INNER DOUBLER RING REPAIR AND OUTER DOUBLER REPAIR AT RT WING LWR SKIN FUEL PANEL 631DB.

Part: SKIN — DAMAGED (BS 258-273) · airframe 29,023 hrs · 34,876 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED HOLE AT RIGHT SIDE OF AIRCRAFT BELLY BETWEEN FS 258.25 AND 273.25. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR BETWEEN FS 258.25 AND 273.25.

Part: FUEL TANK — LEAKING (RT AUX) · airframe 29,023 hrs · 34,876 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT AUX TANK HAS A LEAK AT AUX PUMP MOUNT RING. REBONDED AROUND BOOST PUMP RING AND INSTALLED REPAIR DOUBLER.

Part: HINGE BRACKET — CORRODED (LT ELEVATOR) · airframe 28,456 hrs · 34,308 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED LT ELEVATOR CENTER HINGE BRACKET CORRODED. REPLACED LT ELEVATOR CTR HINGE BRACKET.

Part: SKIN — CORRODED (RT WING) · airframe 28,456 hrs · 34,308 cycles

DURING FURTHER INSP OF RT WING UPPER SKIN SURFACE CORROSION DISCOVERED DEBOND BETWEEN WS 146.00 THROUGH 171.00. REMOVED DAMAGED OF RIGHT WING UPPER SKIN FROM WS 126.50 TO 196.06 AND INSTALLED EXTERNAL DOUBLER REPAIR.

Part: HINGE BRACKET — CORRODED (RT ELEVATOR) · airframe 28,456 hrs · 34,308 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT ELEVATOR OTBD HINGE BRACKET CORRODED. REPLACED RT ELEVATOR OTBD HINGE BRACKET.

Part: DOOR — STIFF (EMERGENCY EXIT) · airframe 28,079 hrs · 33,923 cycles

DURING SCHEDULED ROUTINE MX, DISCOVERED RT FWD EMERGENCY EXIT HARD TO OPEN. LUBRICATED RT FWD EMERGENCY EXIT DOOR OUTSIDE HANDLE. OPS CHECK OK.

Part: BRAKE — INOPERATIVE (MLG) · airframe 27,885 hrs · 33,703 cycles

FLIGHT NR 9246 MHH/FLL AFTER LANDING RT BRAKE INOPERATIVE. BOTH CAPTAIN AND FIRST OFFICER RT BRAKE HAS NO RESISTANCE. PEDAL GOES STRAIGHT TO THE FLOOR. PERFORMED BRAKE BLEEDING. OPS CHECK GOOD.

Part: BRAKE SYS — CONTAMINATED (RIGHT) · airframe 27,704 hrs · 33,514 cycles

FLIGHT 9207 PNS/TPA - PILOT REPORTED RIGHT BRAKE INOPERATIVE THE PEDAL GOES ALL THE WAY DOWN BLED RIGHT BRAKES. OPERATIONAL CHECK NORMAL.

Part: BRAKE SYS — CONTAMINATED (RIGHT) · airframe 27,704 hrs · 33,514 cycles

FLIGHT 9207PNS/TPA - PILOT REPORTED RIGHT BRAKE INOPERATIVE, THE PEDAL GOES ALL THE WAY DOWN. BLED RIGHT BRAKES. OPERATIONAL CHECK NORMAL.

Part: BRAKE SYS — CONTAMINATED (RIGHT) · airframe 27,705 hrs · 33,515 cycles

FLIGHT 9158 TPA/EYW - PILOT REPORTED RIGHT BRAKE INOPERATIVE RIGHT PEDAL GOES ALL THE WAY DOWN. BLED RIGHT BRAKE. OPERATIONAL CHECK NORMAL.

Part: BRAKE SYS — CONTAMINATED (RIGHT) · airframe 27,700 hrs · 33,511 cycles

FLIGHT 9272 EYW/FLL - PILOT REPORTED RIGHT BRAKE INOPERATIVE. PERFORMED BRAKE BLEEDING ON RIGHT BRAKE ASSEMBLY. OPERATIONAL CHECK NORMAL.

Part: BRAKE ASSY — MALFUNCTIONED (MLG)

PILOT REPORTED NO BRAKES AND NO STEERING AT THE END OF LANDING ROLL. PERFORMED PRESSURE POT BLEEDING OF BRAKE SYSTEM. OPERATIONAL CHECK OF BRAKES AND STEERING NORMAL. (K)

Part: ACM — ODOR

FLIGHT 9128 VPS/TPA. DURING DESCENT ACM BLOWS BURNING ODOR OUT OF FLOOR WHEN HEAT IS DECREASED IN MANUAL MODE. RAN ENGS AND PERFORMED OPERATIONAL CHECK OF ACM SYSTEM IN MANUAL AND AUTO MODES. NO ODOR NOTED. (S)

Part: BRAKE — WEAK (MLG)

FLIGHT 9232 TPA/EYW - PILOT REPORTED, CAPTAIN`S RT BRAKE PEDAL GOES TO THE FLOOR. NO BRAKING ACTION AT ALL. FIRST OFFICER`S BRAKES WORK MINIMALLY. BLED RT BRAKE. OPERATIONAL CHECK GOOD. (S)

Part: HINGE BRACKET — CORRODED (UPPER RUDDER) · airframe 26,380 hrs · 32,015 cycles

DURING SCHEDULED ROUTINE MAINT, DISCOVERED UPPER RUDDER HINGE BRACKET EXFOLIATED. REPLACED UPPER RUDDER HINGE BRACKET.

Part: HINGE BRACKET — CORRODED (LT ELEVATOR) · airframe 26,380 hrs · 32,015 cycles

DURING SCHEDULED ROUTINE MAINT, DISCOVERED LT OB ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED LT OB ELEVATOR HINGE ASSY.

Part: UPLOCK SWITCH — SHORTED (NLG) · airframe 26,163 hrs · 31,766 cycles

FLIGHT: 9201, DURING FLIGHT, LANDING GEAR HANDLE LIGHT ILLUMINATED WITH LANDING GEAR RETRACTED. INSTALLED UPLOCK SWITCH AND RIGGED UP AND DOWNLOCK SWITCHES FOR THE NOSE LANDING GEAR.

Part: DOOR — UNSECURE (EMERGENCY EXIT) · airframe 25,957 hrs · 31,527 cycles

FLIGHT: 9179, PILOT REPORTED: DISCOVERED LT EMERGENCY EXIT DOOR APPEARS UNSECURE. RIGGED LT EMERGENCY EXIT DOOR.

Part: SKIN — CRACKED (BS 281) · airframe 25,877 hrs · 31,430 cycles

AT SCHEDULED INSPECTION, DISCOVERED (2) CRACKS IN FUSELAGE BELLY SKIN AT FS 281, ONE WAS A (2) INCH LATERAL CRACK, AND THE OTHER A ONE INCH LONGITUDINAL CRACK, STOP DRILLED CRACKS AND INSTALLED ONE EXTERNAL DOUBLER OVER BOTH CRACKED AREA. REFERENCE SRM 53-90-18.

Part: MASTER CYLINDER — MALFUNCTIONED (RT BRAKES) · airframe 25,443 hrs · 30,942 cycles

FLIGHT:9250, AFTER LANDING DISCOVERED RT BRAKE NOT HOLDING. REPLACED CAPTAIN RT BRAKE MASTER CYLINDER. OPERATIONAL CHECK GOOD.

Part: SWITCH — OUT OF ADJUST (MLG) · airframe 23,685 hrs · 28,904 cycles

FLIGHT:9227 DURING FLIGHT LANDING GEAR WARNING HORN SOUNDS BETWEEN 90-91 PERCENT, N1 WITH 2300-2500 POUNDS OF TORQUE. ADJUSTED LANDING GEAR WARNING HORN PEDESTAL SWITCHES. TEST FLIGHT SATISFACTORY.

Part: TURBINE BLADES — FAILED (RIGHT ENGINE)

MCO/LEE DURING TAKEOFF ROLL RIGHT ENGINE FAILED, ABORTED TAKEOFF. REPLACED RIGHT ENGINE, OPERATIONAL CHECK NORMAL. SUSPECT 2ND STAGE PT BLADE FATIGUE CRACKING.

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: SEAT TRACK — BROKEN (FUSELAGE) · airframe 19,947 hrs · 24,478 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED RT SEAT TRACK FLOOR BOARD ATTACH TAB BROKEN AT FS 238. REPAIRED BROKEN RT SEAT TRACK FLOOR SUPPORT TAB AT FS 238.

Part: BRACKET — CORRODED (ELEVATOR)

AT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB ELEVATOR HINGE BRACKET.

Part: BRACKET — CORRODED (RT ELEVATOR)

AT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB ELEVATOR HINGE BRACKET.

Part: TRANSDUCER — FAILED (LT ENGINE)

FLT 9134 - FLL - AFTER TAKEOFF, LEFT ENGINE OIL PRESSURE DROPPED TO ZERO WITH NO ANNUNCIATOR INDICATION. REMOVED AND REPLACED NR 1 ENGINE OIL PRESSURE TRANSDUCER. OPS AND LEAK CHECKS NORMAL. (M)

Part: INDICATOR — WORN (COCKPIT)

FLT 9389 - MIA/FLL - DURING FLIGHT, ELEVATOR TRIM WHEEL POSITION INDEX MARKER DOES NOT CORRESPOND TO TRIM SETTINGS. REMOVED AND REPLACED ELEVATOR TRIM DIAL INDICATOR ASSEMBLY AND INDEXED. OPERATIONAL CHECK NORMAL. (M)

Part: ACTUATOR — MALFUNCTIONED (LT W/W)

FLT 9330 - TPA-JAX - DURING APPROACH, WITH LANDING GEAR DOWN, LEFT SIDE GREEN ANNUNCIATOR WILL NOT ILLUMINATE. NO UNSAFE LIGHT OR HORN. REMOVED AND REPLACED LEFT LANDING GEAR ACTUATOR. OPERATIONAL CHECK NORMAL. (M)

Part: TRIM TAB — MALFUNCTIONED (ELEVATOR)

CLE - FLT 3036 - AFTER TAKEOFF FROM CLEVELAND, THE CREW REPORTED THEIR ELEVATOR PITCH TRIM WHEEL WAS DIFFICULT TO OPERATE. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPOSITIONED ELEVATOR TRIM TAB CONTROL WHEEL AND INDICATOR IAW BEECHCRAFT MM 27-30-08 AND VERIFIED ELEVATOR TRIM TAB DEFLECTION AND TRAVEL IAW BEECHCRAFT MM 27-30-05. PERFORMED OPERATIONAL CHECKS OF ELEVATOR TRIM TAB SYSTEM IAW BEECHCRAFT MM 27-00-00. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ACTUATOR — FAILED (RT MLG)

LAN - THE CREW REPORTED THAT THE RIGHT MAIN GEAR LIGHT DID NOT ILLUMINATE WITH THE GEAR SELECTED DOWN. THE AIRCRAFT LANDED IN LAN WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN GEAR ACTUATOR AND PERFORMED OPERATIONAL CHECK IAW B1900D MM 32-30-10, NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: MOTOR — FAILED (TE FLAP)

CLE - FLT 3101 - CREW REPORTED THAT THE FLAPS WOULD NOT RETRACT AND THEY RECEIVED A STRONG SMELL IN CABIN AFTER TAKEOFF. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE FLAP DRIVE MOTOR IAW B1900 MM 27-50-03, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: SAFETY SWITCH — FAILED (TE FLAPS)

CLE - FLT 3080 - CREW REPORTED AFTER TAKEOFF AND DURING CLIMB, THE FLAPS WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE LEFT HAND FLAP SAFETY SWITCH IAW B1900D MM 27-50-00, ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RELEASED FOR SERVICE. ACFT TT, 3,426.8 HOURS. ACFT TOTAL CYCLES, 4,135. (X)

Part: RELAY BOARD — FAILED (CABIN)

CLE - FLT 3019 - CREW REPORTED THE LEFT SIDE AUTOFEATHER DISARMED ONCE AIRBORNE. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED AUTOFEATHER RELAY BOARD, P/N 129-364079-7, IAW B1900D MM 61-21-00. MAINTENANCE ALSO REMOVED AND REPLACED THE ANNUNCIATOR POWER SOURCE CIRCUIT BOARD IAW B1900D MM 31-50-00 FOR PREVENTATIVE MEASURES. AIRCRAFT RELEASED FOR SERVICE. ACFT TT, 3,421.1 HOURS. ACFT TOTAL CYCLES, 4,129. (X)