N87551

Part: ANNUNCIATOR — DEFECTIVE (COCKPIT) · airframe 31,971 hrs · 37,391 cycles

FLIGHT: 3983 TPA/PNS NOSE GEAR ANNUNCIATOR FLICKERS WITH THE LANDING GEAR IN THE DOWN POSITION. REPLACED THE LANDING GEAR ANNUNCIATOR ASSEMBLY OPERATIONAL CHECK GOOD.

Part: POSITION SWITCH — OUT OF ADJUST (RT MLG) · airframe 31,734 hrs · 37,112 cycles

FLIGHT:3967 GNV/MCO PILOT REPORTED UNSAFE RED GEAR HANDLE LIGHT INFLIGHT. ADJUSTED RIGHT UP POSITION SWITCH, OPERATIONAL CHECK GOOD.

Part: POSITION SWITCH — OUT OF ADJUST (RT MLG) · airframe 31,734 hrs · 37,112 cycles

FLIGHT:3967 GNV/MCO PILOT REPORTED UNSAFE RED GEAR HANDLE LIGHT INFLIGHT. ADJUSTED RIGHT UP POSITION SWITCH, OPERATIONAL CHECK GOOD.

Part: PRESSURE SWITCH — BROKEN (LANDING GEAR) · airframe 31,486 hrs · 36,814 cycles

FLIGHT: 3981 TPA/PNS PILOT REPORTED LANDING GEAR CONTROL 2 AMP BREAKER POPPED IN FLIGHT. REPLACED POWER PACK PRESSURE SWITCH. LANDING GEAR OPERATIONAL CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,128 hrs · 36,389 cycles

DURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED 1.0 INCH CRACK THROUGH FASTENER AT APPROXIMATELY FS 294 RBL 30 EXTERNAL. REMOVED DAMAGE SKIN AND INSTALLED A 4.5 X 9.5 INCH EXTERNAL DOUBLER REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 31,098 hrs · 36,352 cycles

REPORT: DURING SCHEDULED ROUTINE INSPECTION FOUND TWO SPOTS OF CORROSION OUT OF LIMITS ON AIRCRAFT BELLY NEXT TO NUMBER 3 FLAP. REMOVED CORROSION AND INSTALLED FILLER AND AN EXTERNAL DOUBLER REPAIR.

Part: TORQUE TUBE — CORRODED (RT ELEVATOR) · airframe 30,919 hrs · 36,153 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT ELEVATOR TORQUE TUBE HAS CORROSION. REPLACED RIGHT ELEVATOR TORQUE TUBE.

Part: ATTACH BRACKET — CORRODED (HORIZ STAB) · airframe 30,919 hrs · 36,153 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT STABILIZER INBOARD ATTACH BRACKET FOR ELEVATOR SHOWING CORROSION. REPLACED RIGHT STABILIZER INBOARD ATTACH BRACKET.

Part: ATTACH BRACKET — CORRODED (HORIZ STAB) · airframe 30,919 hrs · 36,153 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT STABILIZER INBOARD ATTACH BRACKET FOR ELEVATOR SHOWING CORROSION. REPLACED RIGHT STABILIZER INBOARD ATTACH BRACKET.

Part: HANDLE — LOOSE (AIRSTAIR DOOR) · airframe 30,836 hrs · 36,053 cycles

FLIGHT: 3978 FPO/FLL PILOT REPORTS AIRSTAIR DOOR HANDLE INTERIOR CABLE BROKE. AFTER VISUAL INSPECTION FOUND AIRSTAIR DOOR HANDLE CABLE NOT BROKEN AND SERVICEABLE RESECURED AIRSTAIR DOOR HANDLE ARM ASSEMBLY CABLE TENSIONS CHECKED GOOD. OPERATIONAL CHECK GOOD.

Part: LINKAGE — BINDING (EMERGENCY EXIT) · airframe 30,405 hrs · 35,566 cycles

DURING SCHEDULED ROUTINE STRUCTURAL INSP, DISCOVERED LT EMERGENCY DOOR LINKAGE OPEN AND CLOSE STIFF AND NOT WORKING CORRECTLY. CLEANED AND LUBRICATED LT EMERGENCY DOOR LOCKING MECHANISM, OPS CHECK GOOD.

Part: HANDLE — STICKING (EMERGENCY EXIT) · airframe 29,912 hrs · 34,997 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED LT EMERGENCY EXIT HANDLES STICKING. LUBRICATED LT EMERGENCY EXIT HANDLES, OPS CHECK NORMAL.

Part: SKIN — CORRODED (RT WING) · airframe 29,777 hrs · 34,827 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT WING UPPER SKIN T/E CORROSION AND DEBOND BETWEEN WING STATIONS 127.00 THROUGH 174.00 JUST FWD OF NR4 FLAP. REMOVED DAMAGE AND INSTALLED AN EXTERNAL DOUBLER REPAIR.

Part: SCREW — MISSING (PAX DOOR) · airframe 29,735 hrs · 34,781 cycles

PILOT REPORTED CABIN DOOR HARD TO OPEN. INSTALLED MISSING SCREWS ON AIRSTAIR DOOR PLASTIC COVER, CABIN DOOR OPENS AND CLOSES NORMALLY.

Part: LATCH — LACK OF LUBE (EMERGENCY EXIT) · airframe 29,604 hrs · 34,618 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT OUTER HANDLE WILL NOT SPRING OPEN. CLEANED AND LUBRICATED LATCH MECHANISM.

Part: LIGHT — LOOSE (MLG INDICATOR) · airframe 29,017 hrs · 33,958 cycles

DURING FLIGHT, LANDING GEAR "H" GREEN LIGHTS LOOSE AND FLICKERED ON AND OFF WHEN LANDING GEAR DOWN OR PRESS TO TEST. RESECURED LANDING GEAR "H" GREEN LIGHTS, OPS CHECK NORMAL.

Part: CABLE — KINKED (AIRSTAIR DOOR) · airframe 28,792 hrs · 33,719 cycles

DURING SCHEDULED STRUCTURAL INSP DISCOVERED TOP FWD AND BOTTOM FWD AIRSTAIR DOOR CABLES KINKED. REPLACED TOP FWD AND BOTTOM FWD AIRSTAIR DOOR CABLES. NOTE: ACFT DOWN FOR STRUCTURAL INSP.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,792 hrs · 33,719 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED LT WING TO FUSELAGE CLOSING ANGLE CRACKED 1.65 INCHES. STOP DRILLED END OF CRACK AND INSTALLED REPAIR ANGLE. NOTE: ATA CODE UPDATED TO 5300.

Part: ANGLE — CRACKED (LT WING) · airframe 28,792 hrs · 33,719 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED LT WING TO FUSELAGE CLOSING ANGLE CRACKED 1.65 INCHES. STOP DRILLED END OF CRACK AND INSTALLED REPAIR ANGLE.

Part: ANGLE — CRACKED (BS 150 S9A-4L) · airframe 28,792 hrs · 33,719 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED AIRSTAIR DOOR ANGLE CRACKED AT TOP AND BOTTOM, SNUBBER BRACKET ATTACH POINTS APPROX FS 150 STRINGERS 9AL AND 4L. REMOVED DAMAGED SECTION AND INSTALLED REPAIR ANGLE.

Part: SKIN — DELAMINATED (WING) · airframe 27,436 hrs · 32,269 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED WING SKIN DELAMINATED AROUND FUEL ACCESS PANEL 632 AT. REMOVED INTERNAL RING CLEAN AREA AND INSTALLED EXTERNAL REPAIR DOUBLER AROUND FUEL ACCESS PANEL.

Part: UPLOCK SWITCH — INTERMITTENT (MLG) · airframe 27,176 hrs · 31,981 cycles

AFTER TAKEOFF LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED FOR FIVE MINUTES AFTER GEAR RETRACTED. REPLACED RT MAIN LANDING GEAR UPLOCK SWITCH. OPS CHECK NORMAL.

Part: HINGE BRACKET — CORRODED (RT ELEVATOR) · airframe 26,849 hrs · 31,643 cycles

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

Part: LIGHT — INOPERATIVE (ANNUNCIATOR) · airframe 26,530 hrs · 31,303 cycles

DURING APPROACH AFTER SELECTING LANDING GEAR DOWN, GEAR GREEN "H" LIGHTS DID NOT ILLUMINATE. RESEATED ANNUNCIATOR "H" LIGHTS. OPS CHECK GOOD.

Part: ANNUNCIATOR — INOPERATIVE (MLG) · airframe 26,497 hrs · 31,272 cycles

DURING APPROACH, LANDING GEAR "H" ANNUNCIATOR INOPERATIVE. RESET AND SECURED LANDING GEAR "H" ANNUNCIATOR MODULE OPS CHECK GOOD.

Part: DOOR — STIFF (AIRSTAIR) · airframe 26,305 hrs · 31,076 cycles

FLIGHT: 9245, PILOT REPORTED AIRSTAIR DOOR DIFFICULT TO CLOSE. PERFORMED AIRSTAIR DOOR RIGGING OPS CHECK, OK.

Part: STRINGER — CORRODED (RT WING) · airframe 25,952 hrs · 30,711 cycles

DURING SCHEDULED INSP DISCOVERED RT WING CORROSION INSIDE COLLECTOR TANK ON J STRINGER AFT FLANGE BETWEEN WS 114.25 TO 124.25. CLEANED CORROSION AND INSTALLED EXTERNAL STRAP ON RIGHT WING J STRINGER.

Part: SPAR — CORRODED (RT WING) · airframe 25,952 hrs · 30,711 cycles

DURING SCHEDULED INSP DISCOVERED CORROSION ON RT WING INSIDE COLLECTOR TANK FWD SPAR AFT FLANGE AND K STRINGER FWD FLANGE BETWEEN WS 114.25 TO 124.25. CLEANED CORROSION AT RIGHT FORWARD AFT FLANGE MATERIAL LOSS IS STILL ABOVE DESIGN MINIMUM STRENGTH.CLEANED CORROSION AT RIGHT K STRINGER AND INSTALLED DOUBLER REPAIR.

Part: STRINGER — CORRODED (RT WING) · airframe 25,952 hrs · 30,711 cycles

DURING SCHEDULED INSP DISCOVERED CORROSION ON LT WING INSIDE COLLECTOR TANK ON K STRINGER FWD FLANGE BETWEEN WS 114.25 TO 124.25. INSTALLED EXTERNAL STRAP ON K STRINGER ON LT WING.

Part: SPAR — CORRODED (RT WING) · airframe 25,952 hrs · 30,711 cycles

DURING SCHEDULED INSP, DISCOVERED CORROSION ON RT WING J STRINGER FWD FLANGE AND RT FWD SPAR, FD FLANGE BETWEEN WS 124.58 TO 135.86. CLEANED CORROSION SPOT ALLOWABLE DAMAGE WITHIN LIMITS ALSO CLEANED AND TREATED AND PRIMED SURFACE AREA AT RIGHT WING J STRINGER BETWEEN WS 124.58 TO 135.86.

Part: SPAR — CORRODED (LT WING) · airframe 25,952 hrs · 30,711 cycles

DURING SCHEDULED INSP DISCOVERED CORROSION ON LT WING INSIDE COLLECTOR TANK FWD SPAR AFT FLANGE AND J STRINGER AFT FLANGE BETWEEN WS 114.25 TO 124.25. REMOVED CORROSION INSTALLED INTERNAL STRAP ON LEFT FORWARD SPAR FLANGE AND EXTERNAL STRAP ON J STRINGER.

Part: SPAR — CORRODED (LT WING) · airframe 25,952 hrs · 30,711 cycles

DURING SCHEDULED INSP DISCOVERED CORROSION ON LT WING FWD SPAR FWD FLANGE AND J STRINGER FWD FLANGE BETWEEN WS 124.58 TO 135.86. REMOVED CORROSION AND INSTALLED FILLER AND REPAIR DOUBLER ON LEFT FORWARD SPAR FORWARD FLANGE AND INSTALLED EXTERNAL STRAP ON J STRINGER.

Part: CABLE — FRAYED (AIRSTAIR DOOR) · airframe 25,847 hrs · 30,600 cycles

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

Part: CABLE — FRAYED (AIRSTAIR DOOR) · airframe 25,847 hrs · 30,600 cycles

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

Part: HANDLE — WORN (AIRSTAIR DOOR) · airframe 25,847 hrs · 30,600 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED AIRSTAIR DOOR OUTER HANDLE SHOWING SIGNS OF WEAR. REPLACED AIRSTAIR DOOR OUTER HANDLE.

Part: CABLE — FRAYED (AIRSTAIR DOOR) · airframe 25,847 hrs · 30,600 cycles

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

Part: DOOR — LACK OF LUBE (EMERGENCY EXIT) · airframe 25,532 hrs · 30,231 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED EMERGENCY DOOR AT SEAT 6F STIFF TO OPEN. LUBRICATED EMERGENCY DOOR. OPERATIONAL CHECK NORMAL.

Part: DOOR — LACK OF LUBE (EMERGENCY EXIT)

DURING SCHEDULED ROUTINE MAINT DISCOVERED SEAT 6F EMERGENCY EXIT HARD TO OPEN. LUBED EMERGENCY EXIT. OPS CHECK GOOD. (K)

Part: WIRE — OUT OF POSITION (LANDING LIGHT)

AFTER TAKEOFF UPON TURNING BOTH LANDING LIGHTS SWITCHES OFF THERE WAS A SPARK COMING OUT OF THE SWITCH. SPLICED AND REPOSITIONED WIRE AT LT LANDING LIGHT SWITCH. OPS CHECK GOOD. (K)

Part: HINGE BRACKET — CORRODED (LT ELEVATOR) · airframe 24,897 hrs · 29,448 cycles

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

Part: HINGE BRACKET — CORRODED (ELEVATOR) · airframe 24,897 hrs · 29,448 cycles

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

Part: ACTUATOR — LEAKING (NLG) · airframe 23,373 hrs · 27,712 cycles

FLIGHT: 9179, DURING FLIGHT RT MAIN LANDING GEAR EXTENDED ON ITS OWN WITH NOSE AND LT STILL RETRACTED. ATTEMPTED TO EXTEND LANDING GEAR, AND WAS UNABLE. PERFORMED MANUAL GEAR EXTENSION,GEAR EXTENDED AND LOCKED WITH (3) GREEN LIGHTS. RETURNED TO FLL LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR ACTUATOR OPERATIONAL CHECK NORMAL.

Part: ROD — BENT (MLG ACTUATOR) · airframe 23,174 hrs · 27,473 cycles

FLIGHT: 5407, DURING APPROACH NOSE LANDING GEAR WOULD NOT COME DOWN ON THE FIRST TRY RECYCLED, LANDING GEAR EXTENDED NORMALLY. REPLACED NOSE LANDING GEAR ACTUATOR, OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY.

Part: DOWNLOCK SWITCH — DAMAGED (NLG) · airframe 23,173 hrs · 27,471 cycles

FLIGHT: 9244 FLL/GGT DURING APPROACH THE LANDING GEAR IN TRANSIT LIGHT REMAINED ILLUMINATED WITH THE GEAR HANDLE IN THE DOWN POSITION. NOSE GEAR INDICATED UNSAFE CONDITION. RECYCLED LANDING GEAR OBTAINED GOOD INDICATIONS. REPLACED NOSE GEAR DOWNLOCK SWITCH AND ADJUSTED. OPERATIONAL CHECK NORMAL.

Part: BRACKET — BENT (DOWNLOCK) · airframe 23,168 hrs · 27,466 cycles

FLIGHT: 9224, DURING FINAL APPROACH NOSE GEAR DID NOT INDICATE DOWN AND LOCK UNTIL FIVE TO TEN SECONDS AFTER SELECTED DOWN POSITION. REPLACED NOSE LANDING GEAR DOWNLOCK BRACKET. OPERATIONAL CHECK NORMAL.

Part: HANDLE — FAILED (MLG) · airframe 23,164 hrs · 27,461 cycles

FLIGHT: 9128, DURING APPROACH NOSE GEAR DID NOT IMMEDIATELY SAFE INDICATION AFTER APPROXIMATELY 5 SECONDS NOSE GEAR SHOWED DOWN AND LOCKED WITH AN ASSOCIATED POPPED CIRCUIT BREAKER. REPLACED LANDING GEAR CONTOL HANDLE. OPERATIONAL CHECK NORMAL.

Part: SKIN — CORRODED (BS 250) · airframe 22,969 hrs · 27,231 cycles

AT SCHEDULED INSPECTION DISCOVERED BELLY SKIN CORROSION AT FS 250.00 AT STRINGER 14L. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 51-70-06.

Part: BUSHING — FROZEN (EMERGENCY EXIT) · airframe 22,670 hrs · 27,231 cycles

AT SCHEDULED FLEET CAMPAIGN INSPECTION: LEFT EMERGENCY EXIT DOOR INTERNAL BEARING BUSHING AT HANDLE FROZEN. REPLACED BUSHING.

Part: CONTROL HANDLE — FAILED (MLG) · airframe 22,951 hrs · 27,207 cycles

FLIGHT: 9181 PNS/FLL - DURING APPROACH, NOSE GEAR WOULD NOT EXTEND AND CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER NOSE GEAR EXTENDED BUT CIRCUIT BREAKER POPPED AGAIN. REPLACED LANDING GEAR CONTROL HANDLE. OPERATIONAL CHECK NORMAL.

Part: BOLT — LOOSE (BELLCRANK) · airframe 22,905 hrs · 27,155 cycles

FLIGHT: 9184 MIA/GNV - DURING APPROACH WHEN EXTENDING THE LANDING GEAR NOSE GEAR LIGHT DID NOT COME ON THE INTRANSIT LIGHT STAYED ON. RECYCLED THE LANDING GEAR HEARD A LOUD NOISE WHILE GEAR COMING UP. EXTENED LANDING GEAR AGAIN EVERYTHING WAS NORMAL. TIGHTENED NOSE LANDING GEAR BELLCRANK BOLT. LANDING GEAR OPERATIONAL CHECK NORMAL.

Part: CABLE ASSY — BROKEN (AIRSTAIR DOOR) · airframe 22,748 hrs · 26,968 cycles

CAMS ON FWD PASSENGER DOOR WILL NOT TURN. REPLACED AIRSTAIR DOOR FORWARD LOWER CABLE ASSEMBLY.

Part: BLEED VALVE — MALFUNCTIONED (LT ENGINE) · airframe 22,037 hrs · 26,118 cycles

FLIGHT: 9165, DURING FLIGHT LT ITT INDICATED ABOVE 900 DEGREES SHUTDOWN ENGINE IN FLIGHT ALL OTHER PARAMETERS NORMAL. COMPLETED RESTART ALL OPERATIONS RESUMED NORMAL. MAINTENANCE FERRY. PERFORMED ITT SYSTEM CHECK,TORQUE CALIBRATION CHECK AND PRECOOLER CHECK REPLACED ENGINE BLEED VALVE PERFORMED POWER ASSURANCE RUNS ALL PARAMETERS WITHIN LIMITS.

Part: ODOR — DETECTED (CABIN)

FLIGHT: 9196 GGT/FLL DURING FLT INTERMITTENT OIL ODOR VENTING THROUGH THE ENVIRONMENTAL SYSTEM WITH THE LT OR RT BLEED ON. RAN ENGINES WITH BLEEDS ON TOGETHER AND INDEPENDENTLY, NO DEFECTS NOTED. OPERATIONAL CHECK GOOD.

Part: SKIN — DAMAGED (BS 513-544)

AT SCHEDULED ROUTINE MAINTENANCE LEFT FUSELAGE HAS CREASED SKIN LOCATED 3 INCHES AFT OF CARGO DOOR BETWEEN FUSELAGE STATIONS 513.00 THRU 544.250 AT STRINGER 9L AND 10L. INSTALLED REINFORCEMENT DOUBLER OF 2024-T3 .050 IN DIMENSION 19.0 IN X 7.0 IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED IN THE RAYTHEON STRUCTURAL REPAIR MANUAL SECTION 51-70-06.

Part: HINGE BRACKET — CORRODED (VERTICAL STAB)

AT SCHEDULED ROUTINE MAINTENANCE, VERTICAL FIN UPPER HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED UPPER HINGE BRACKET.

Part: PITOT TUBE — OVERHEATED (FUSELAGE)

DURING APPROACH, FO ALTIMETER, FLT DIRECTOR AND YAW DAMP BECAME INOPERATIVE FOLLOWED BY SMOKE IN THE COCKPIT THROUGH THE FO INSTRUMENT PANEL. DETERMINED THAT THE RT PITOT TUBE OVERHEATED CAUSINGTHE RT PITOT HOSES TO BURN FROM THE INSIDE OUT PRODUCING SMOKE, AND CAUSING A STATIC LEAK IN THE ALTIMETER AND FLIGHT DIRECTOR/ YAW DAMPER SYSTEMS. REPLACED PNEUMATIC HOSES (PN 36001-5-0080 (2 EA) AND PITOT TUBE ASSEMBLY. (K)

Part: HINGE BRACKET — CORRODED (RT ELEVATOR)

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

Part: BRACKET — CORRODED (RT ELEVATOR)

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

Part: BRAKE ASSY — MALFUNCTIONED (MLG)

FLT 9281 - MIA/MCO - WHEN LEFT BRAKE APPLIED, AIRCRAFT WILL NOT STOP. RETURNED TO GATE. PERFORMED BRAKE SYSTEM BLEEDING. OPS CHECK NORMAL. (M)

Part: HOSE — LEAKING (LEFT ENGINE)

UNIDENTIFIABLE ODOR IN THE CABIN WHEN BLEEDS ARE ON. REMOVED AND REPLACED LEFT ENGINE FUEL PURGE PNEUMATIC HOSE. LEAK CHECK GOOD. (M)

Part: CONNECTOR — DIRTY (FIRE LOOP)

ON PREFLIGHT, THE FIREWALL SHUT OFF HANDLE ILLUMINATES WHEN LEFT FIRE LOOP IS TESTED. CLEANED LEFT FORWARD FIRE LOOP CONNECTOR OPERATIONAL CHECK NORMAL.

Part: PRINTED CKT BOARD — DEFECTIVE (FIRE DETECTION)

CLE FLT 3001 THE CREW REPORTED NR 2 ENGINE FIRE LOOP WILL NOT TEST. MAINTENANCE REPLACED ANNUNCIATOR FAULT DETECTION SYSTEM PRINTED CIRCUIT BOARD. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: PCU — OUT OF ADJUST (NR 1 & NR 2 ENG)

CLE - FLT 3023 - THE CREW REPORTED THE PROPS ONLY REACHED 1,650 RPM AT FULL POWER. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE NR 1 AND NR 2 ENGINE HIGH PROP RPM IAW BEECH 1900D MM 61-20-00 AND PERFORMED OPERATIONAL CHECKS IAW BEECH 1900D MM 61-00-00, NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (X)

Part: PROP CONTROL — MALFUNCTIONED (E/E COMPT)

CLE - FLT 3154 - THE CREW REPORTED ON TAKEOFF ROLL, THE NR 1 PROPELLER ONLY WENT TO 1,650 RPM AND THE NR 2 PROPELLER ONLY WENT TO 1,670 RPM. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED GROUND OPERATIONAL CHECKS IAW BEECHCRAFT MM 61-20-00, ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. (X)

Part: COMPRESSOR — DAMAGED (LT ENGINE)

CLE - DURING A SCHEDULED INSPECTION, THE LEFT ENGINE COMPRESSOR BLADES WERE FOUND TO BE DAMAGED BEYOND MANUFACTURES LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW B1900 MM 71-00-00, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY IAW B1900 MM 71-10-00 AND CONTINENTAL EXPRESS TASK CARD NR 4361001. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: AIR DISTRIBUTION — ODOR (COCKPIT)

CLE - FLT 3165 - CREW REPORTED A VERY STRONG BURNING SMELL/SULPHUR SMELL IMMEDIATELY AFTER GEAR UP, AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AIRCRAFT, ALSO OPERATIONAL CHECKS WERE PERFORMED WITH ENGINES RUNNING AT DIFFERENT POWER SETTINGS AND ENVIROMENTALS ON USING DIFFERENT SETTINGS AND LOADS WITH NO DEFECTS NOTED ON ANY SYSTEM. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: TRUSS — CRACKED (LT ENGINE)

CLE - DURING A SCHEDULED INSPECTION, THE LEFT ENGINE TRUSS MOUNT WAS FOUND TO BE CRACKED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE TRUSS MOUNT IAW B1900 MM 71-20-00. (M)

Part: TRUSS — CRACKED (RT ENGINE)

CLE - DURING A SCHEDULED INSPECTION, THE RIGHT ENGINE TRUSS MOUNT WAS FOUND TO BE CRACKED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE TRUSS MOUNT IAW B1900 MM 71-20-00. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: BLOWER — FAILED (COCKPIT)

FLT 3013 - CREW REPORTED A STRONG SMELL OF SMOKE IN THE COCKPIT AND CABIN, GREY SMOKE WAS ALSO VISIBLY OBSERVED. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE FORWARD VENT BLOWER IAW B1900D MM 21-10-01. OPERATIONAL CHECKS WERE GOOD, AIRCRAFT RETURNED TO SERVICE. ACFT TT: 1,005.9 HOURS. ACFT TC: 1,196.