N82539

Part: CONTACT — DIRTY (ANNUCIATOR) · airframe 32,557 hrs · 41,946 cycles

FLIGHT: 4008 PNS/TPA PILOT REPORTED LEFT "L" LETTER GEAR INDICATOR ANNUNCIATOR LAMP IS INOPERATIVE. CLEAN CONTACT ON GEAR INDICATOR ANNUNCIATOR OPERATIONAL CHECK OK.

Part: PRINTED CKT BOARD — FAULTY (COCKPIT) · airframe 32,540 hrs · 41,927 cycles

FLIGHT: 9385 TLH/TPA PILOT REPORTED UNABLE TO SILENCE GEAR WARNING HORN WHEN POWER IS REDUCED AND FLAPS AT O. REPLACED PCB A119 AND CB1 OPERATIONAL CHECK NORMAL COULD NOT DUPLICATE.

Part: BUTTON — MALFUNCTIONED (WARNING SYSTEM) · airframe 32,572 hrs · 41,908 cycles

FLIGHT: 5200 EYW/FLL PILOT REPORTED LANDING GEAR WARNING HORN SILENCE BUTTON DOES NOT SILENCE THE LANDING GEAR WARNING HORN. PERFORMED LANDING GEAR EXTENSION AND RETRACTION INSPECTION COULD NOT DUPLICATE, OPERATIONAL CHECK GOOD.

Part: SKIN — CORRODED (RT WING) · airframe 32,514 hrs · 41,894 cycles

DURING SCHEDULED ROUTINE C-1 INSPECTION DISCOVERED RIGHT WING TRAILING EDGE SKIN OUTBOARD OF NACELLE SPOT OF CORROSION. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER REPAIR.

Part: CONTROL SWITCH — FAULTY (COCKPIT) · airframe 32,436 hrs · 41,762 cycles

FLIGHT: 4057 PNS/TPA PILOT REPORTED GEAR WARNING HORN BUTTON DOES NOT SILENCE HORN WITH GEAR UP FLAPS UP AND POWER RETARDED. REPLACED LANDING GEAR CONTROL SWITCH ASSEMBLY.

Part: WARNING HORN — FAULTY (COCKPIT) · airframe 32,417 hrs · 41,741 cycles

FLGHT: 4025 EYW/FLL PILOT REPORTED UNABLE TO SILENCE GEAR WARNING HORN. INSPECTED LANDING GEAR SYSTEM OPERATIONAL CHECK NORMAL COULD NOT DUPLICATE.

Part: SWITCH — INOPERATIVE (COCKPIT) · airframe 32,391 hrs · 41,719 cycles

FLIGHT: 4042 FPO/FLL PILOT REPORTED LANDING GEAR WARNING HORN WILL NOT SILENCE WHEN BUTTON IS PRESSED. REPLACED LANDING GEAR HORN SILENCE SWITCH OPERATIONAL CHECK GOOD.

Part: PRINTED CKT BOARD — DEFECTIVE (WARNING SYS) · airframe 32,340 hrs · 41,643 cycles

FLIGHT 9254 PNS/TPA PILOT REPORTED LANDING GEAR WARNING HORN WILL NOT SILENCE WHEN WARNING HORN SILENCE BUTTON PRESSED. REPLACED PCB A119 OPERATIONAL CHECK NORMAL TEST FLIGHT SATISFACTORY.

Part: HANDLE — INOPERATIVE (EMERGENCY EXIT) · airframe 32,178 hrs · 41,447 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT OUTER HANDLE DOES NOT SPRING OPEN WHEN BUTTON IS DEPRESSED. LUBRICATED LT EMERGENCY EXIT OUTER HANDLE.

Part: ACCESS PANEL — DELAMINATED (RT WING) · airframe 32,084 hrs · 41,336 cycles

DURING SCHEDULED ROUTINE MX, DISCOVERED FUEL LEAKING AT RT WING LOWER FUEL ACCESS PANEL 631CB. FOUND SKIN AROUND RT WING LOWER FUEL ACCESS PANEL 631CB DELAMINATED CLEANED AREA AND INSTALLED EXTERNAL DOUBLER REPAIR.

Part: VALVE — FAILED (MLG) · airframe 31,958 hrs · 41,197 cycles

ON TAKEOFF, UNABLE TO RETRACT LANDING GEAR, RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR SERVICE VALVE, OPS CHECK OK.

Part: WARNING HORN — OUT OF ADJUST (MLG) · airframe 31,635 hrs · 40,812 cycles

FLIGHT: 9191, PILOT REPORTED INSPECT LANDING GEAR HORN AS IT COMES ON 82.9% N1 ON NUMBER ONE ENGINE AND 84.0% N1 ON NUMBER TWO ENGINE. ADJUSTED LEFT AND RIGHT LANDING GEAR WARNING HORN PEDESTAL SWITCHES. TEST FLIGHT SATISFACTORY.

Part: VANE — CRACKED (ENGINE ICE) · airframe 31,544 hrs · 40,714 cycles

DURING MAGNETIC PARTICLE INSP DISCOVERED RT FWD ICE VANE ATTACH POINT WELD AREA CRACK. PERFORMED WELD REPAIR TO ENGINE TRUSS ICE VANE ATTACH POINT WELD AREA.

Part: STRINGER — CORRODED (BS 288) · airframe 31,601 hrs · 40,781 cycles

DURING SCHEDULED ROUTINE STRUCTURAL INSP, DISCOVERED CORROSION ON STRINGER 15L AT FS 288. REMOVED CORRODED AREA OF STRINGER AND INSTALLED STRINGER REPAIR.

Part: STRINGER — CORRODED (BS 288) · airframe 31,601 hrs · 40,781 cycles

DURING SCHEDULED ROUTINE STRUCTURAL INSPECTION, DISCOVERED CORROSION ON STRINGER 16 AFT OF FS 288. REMOVED CORRODED AREA OF STRINGER AND INSTALLED STRINGER REPAIR AND AN EXTERNAL DOUBLER REPAIR.

Part: STRINGER — CORRODED (BS 288 S16) · airframe 31,601 hrs · 40,781 cycles

DURING SCHEDULED ROUTINE STRUCTURAL INSP, DISCOVERED CORROSION ON STRINGER 16 AFT OF FS 288. (OPEN)

Part: STRINGER — DEBONDED (BS 385-406 S15R) · airframe 31,601 hrs · 40,781 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED STRINGER 15R DEBONDED AT FS 385-406 21 INCHES. REPAIRED STRINGER 15R INSTALLED 1.0 X 26 INCH EXTERNAL DOUBLER REPAIR.

Part: DOOR FRAME — CRACKED (BS 150) · airframe 31,601 hrs · 40,781 cycles

DURING SCHEDULED ROUTINE STRUCTURAL INSP, DISCOVERED ASD FRAME ANGLE CRACKED AT FS 150. FUTHER INSP FOUND ASD FRAME ANGLE REPAIR INSTALLED.

Part: STRINGER — DEBONDED (BS 400-405.5 S15) · airframe 31,601 hrs · 40,781 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED STRINGER 15L DEBONDED AT FS 400-405 5 INCHES AND FS 396-285 11 INCHES. REPAIRED STRINGER 15L INSTALLED 1.0 X 26 INCH EXTERNAL DOUBLER REPAIR.

Part: ANNUNCIATOR — LOOSE (MLG) · airframe 31,516 hrs · 40,680 cycles

PILOT REPORTED WHEN LANDING GEAR CONTROL LOWERED NOSE GEAR GREEN ANNUNCIATOR DOES NOT ILLUMINATE UNLESS YOU TAP ON THE ANNUCIATOR. RESECURED NOSE GEAR ANNUNCIATOR.

Part: HANDLE — STICKING (EMERGENCY EXIT) · airframe 31,056 hrs · 40,148 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT OUTER HANDLE STICKING. CLEANED AND LUBRICATED LT EMERGENCY EXIT OUTER HANDLE.

Part: ANNUNCIATOR — MALFUNCTIONED (NLG) · airframe 31,006 hrs · 40,093 cycles

PILOT REPORTED GREEN "NOSE" ANNUNCIATOR FOR LANDING GEAR FLICKERS. NO DEFECTS NOTED COULD NOT DUPLICATE. OPS CHECKS GOOD .

Part: HANDLE — BINDING (EMERGENCY EXIT) · airframe 30,873 hrs · 39,933 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT AFT EMERGENCY EXIT INNER AND OUTER HANDLE BINDING. LUBRICATED RT AFT EMERGENCY EXIT OPS CHECK GOOD.

Part: HANDLE — BINDING (EMERGENCY EXIT) · airframe 30,873 hrs · 39,933 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT FWD EMERGENCY EXIT OUTER HANDLE BINDING. LUBRICATED RT FWD EMERGENCY EXIT HANDLE, OPS CHECK GOOD.

Part: TRANSFER TUBE — LEAKING (FUEL SYSTEM) · airframe 30,786 hrs · 39,830 cycles

DURING CLIMBOUT, PASSENGERS REPORTED SMOKE AFTER OPENING BLEED VALVES. SMOKE DISSIPATED WITH VALVES SWITCH TO ENVIRO OFF. FOUND FUEL NOZZLE TRANSFER TUBE LEAKING AT (3) O`CLOCK POSITION, REPLACED TRANSFER TUBE, LEAK CHECK, OK, NO SMOKE NOTED.

Part: SKIN — DEBONDED (WING) · airframe 30,597 hrs · 39,619 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED FUEL PANELS 542DB, 542CB AND 532FB HAD SEVERE DEBONDING OF DOUBLER RING ACCESS HOLES AT WING SKIN. FABRICATED AND INSTALLED REPAIR DOUBLERS FOR FUEL PANEL ACCESS HOLES.

Part: LANDING GEAR — MALFUNCTIONED · airframe 30,480 hrs · 39,475 cycles

AFTER TAKEOFF HAD TO USE DOWNLOCK TO RAISE LANDING GEAR. CHECKED RT SAFETY SWITCH AND LANDING GEAR CONNECTOR FOR SECURITY NO DEFECTS NOTED OPS CK NORMAL.

Part: INDICATION SYS — MALFUNCTIONED (MLG) · airframe 30,480 hrs · 39,475 cycles

DURING APPROACH, UPON LANDING, GEAR SELECTED. GEAR DOWN RT GEAR ANNUNCIATOR DID NOT ILLUMINATE, AFTER CYCLING GEAR THE A SECOND TIME THE RT GEAR ANNUNCIATOR ILLUMINATED. PERFORMED RT LANDING GEAR DOWNLOCK. OPS CHECK AND PERFORMED LANDING GEAR OPS CHECK COULD NOT DUPLICATE DISCREPANCY.

Part: FIRE LOOP — CHAFED (RT NACELLE) · airframe 30,448 hrs · 39,440 cycles

DURING CLIMB, RT FIRE HANDLE ILLUMINATED. SECURED THE ENG RETURNED TO AIRPORT, LANDED WITHOUT INCIDENT. REPLACED RT ENG FWD FIRE LOOP CABLE. OPS CHECK GOOD.

Part: LANDING GEAR — MALFUNCTIONED · airframe 30,409 hrs · 39,394 cycles

AFTER TAKEOFF, LANDING GEAR WOULD NOT COME UP, TRIED DOWN LOCK RELEASE BUT STILL WOULD NOT COME UP FLEW FLIGHT AT LESS THAN 180 KTS. PERFORMED SEVERAL LANDING GEAR EXTENSIONS AND RETRACTIONS COULD NOT DUPLICATE PROBLEM. TEST FLIGHT SATISFACTORY.

Part: FIRE BOTTLE — CONTAMINATED · airframe 30,308 hrs · 39,291 cycles

DURING FLIGHT, RT FIRE ANNUNCIATOR ILLUMINATED FOR 3 TO 5 SECONDS. SHUT DOWN ENGINE AS PRECAUTION NO SECONDARY FIRE INDICATIONS DID NOT DISCHARGE BOTTLE. DIVERTED, LANDED WITHOUT INCIDENT. INSPECTED RT FIRE DETECTION SYS NO DEFECTS NOTED, INSPECTED FIRE BOTTLE FOUND MOISTURE IN ELECTRICAL BOOT, CLEANED MOISTURE. OPS CHECK OK.

Part: DOOR — BINDING (EMERGENCY EXIT) · airframe 29,976 hrs · 38,947 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT AFT EMERGENCY EXIT DOOR HARD TO OPEN. LUBED RT AFT EMERGENCY EXIT.

Part: SKIN — CORRODED (RT WING) · airframe 29,976 hrs · 38,947 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT WING T/E TOP SURFACE HAS CORROSION AT WS 223.48. CUT OUT CORRODED SECTION OF RT WING T/E AT WS 223.48 AND INSTALLED EXTERNAL DOUBLER REPAIR.

Part: BRACKET — CRACKED (NACELLE) · airframe 29,872 hrs · 38,837 cycles

DURING MAGNETIC PATICLE INSP, DISCOVERED ENGINE TRUSS COWL BRACKET WELD AREA CRACKS. PERFORMED WELD REPAIR TO ENGINE TRUSS COWL BRACKET WELD AREA CRACKS. NOTE: FOUND DURING MAGNETIC PARTICLE INSP.

Part: SPAR — DAMAGED (WING) · airframe 29,872 hrs · 38,837 cycles

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

Part: SOCKET — LOOSE (MLG INDICATOR) · airframe 29,696 hrs · 38,649 cycles

DURING FINAL APPROACH, RT MLG "R" INDICATION INOPERATIVE. RESECURED RT GEAR INDICATION SOCKET. OPS CHECK GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 29,622 hrs · 38,567 cycles

AFTER TAKEOFF BLACK SMOKE CAME FROM UNDER FLOORBOARDS OF ROWS 2 AND 3, ACRID AS IF ELECTRICAL. TURNED THE BLEEDS OFF AND THE SMOKE STOPPED. THE ELECTRICAL ODOR STILL VERY STRONG DECLARED EMERGENCY. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. PERFORMED VISUAL INSP OF FLOOR COMPONENTS. PERFORMED OPS CHECK, UNABLE TO DUPLICATE. TEST FLIGHT SATISFACTORY.

Part: HOSE — LEAKING (MLG ACTUATOR) · airframe 29,289 hrs · 38,189 cycles

DURING CRUISE FLIGHT LANDING GEAR LIGHT ILLUMINATED AND GEAR CIRCUIT BREAKER POPPED. DIVERTED, MANUALLY EXTENDED LANDING GEAR, LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR ACTUATOR HOSES, OPS CHECK GOOD.

Part: SKIN — DELAMINATED (LT WING) · airframe 29,191 hrs · 38,086 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED LT WING SKIN DELAMINATED AROUND FUEL PANEL 532 EB. OPEN

Part: SKIN — DELAMINATED (LT WING) · airframe 29,191 hrs · 38,086 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT WING LOWER SKIN DELAMINATED AROUND FUEL PANEL 531DB. REPAIRED LEFT WING LOWER SKIN AROUND FUEL ACCESS PANEL 531DB.

Part: SKIN — DELAMINATED (RT WING) · airframe 29,191 hrs · 38,086 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT WING LOWER SKIN DELAMINATED AROUND FUEL PANEL 631DB. REPAIRED RIGHT WING LOWER SKIN AROUND FUEL ACCESS PANEL 631DB.

Part: TUBE — BROKEN (BLEED AIR SYS) · airframe 29,136 hrs · 38,028 cycles

DURING APPROACH, UPON EXTENDING LANDING GEAR THERE WERE EXTREMELY LOUD GEAR GRINDING NOISES, IT TOOK APPROX 15 SECONDS FOR THE GEAR TO FULLY EXTEND. THE GEAR MOTOR SEEMED TO BE RUNNING IN INTERMITTENT SEGMENTS, THE RT MAIN EXTENDED FIRST FOLLOWED BY THE LT MAIN AND NOSE. FOUND SUPPLY BLEED AIR TUBE BROKEN AT AIR FILTER CHECK VALVE. REPLACED TUBE ASSY. OPS CHECK GOOD.

Part: CONNECTOR — CORRODED (MLG VALVE) · airframe 29,130 hrs · 38,024 cycles

DURING APPROACH, LANDING GEAR DOWN, NO INDICATION OF GEAR DOWN. MANUALLY EXTENDED LANDING GEAR, GOT 3 GREEN DOWN AND LOCKED INDICATION. LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR SERVICE VALVE. OPS CHECK NORMAL. TEST FLIGHT SATISFACTORY.

Part: CONTROL HANDLE — NO INDICATION (MLG) · airframe 29,129 hrs · 38,022 cycles

FLIGHT: 9202, DURING APPROACH WHEN SELECTED LANDING GEAR CONTROL DOWN GOT NO INDICATION OF THREE GREEN OR THE RED LIGHT LIGHT ON THE GEAR HANDLE. RECYCED GEAR HANDLE TWO TIMES WITH THE SAME RESULT ON THIRD CYCLE GOT THE THREE GREEN DOWN AND LOCKED INDICATION.LANDING WITHOUT INCIDENT. REPLACED LANDING GEAR CONTROL HANDLE AND LANDING GEAR RELAY. OPERATIONAL CHECKS GOOD.

Part: LANDING GEAR — UNKNOWN · airframe 29,058 hrs · 37,947 cycles

FLIGHT: 9192, DURING DESCENT UNABLE TO LOWER LANDING GEAR PERFORMED MANUAL LANDING GEAR EXTENSION, OBTAINED THREE GREEN GEAR DOWN AND LOCKED INDICATION. LANDED WITHOUT INCIDENT. INSPECTED LANDING GEAR SYSTEM COMPONENTS NO DEFECTS FOUND. CYCLED LANDING GEAR SIX TIMES OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY.

Part: SKIN — CORRODED (RT WING) · airframe 28,580 hrs · 37,439 cycles

DURING MX DISCOVERED RT FUEL LEAK AT RT WING ACCESS PANEL 632AT. REPAIRED SKIN .

Part: SKIN — CORRODED (FUSELAGE SKIN) · airframe 28,388 hrs · 37,231 cycles

DURING SCHEDULED ROUTINE INSP LT AND RT SIDE FUSELAGE BELLY REQUIRES SURFACE CORROSION CLEANING FROM FS 243.250 TO FS 327.630. REMOVED SURFACE CORROSION AND DISCOVERED SKIN EXFOLIATION LWR CTR AFT SPAR. REMOVED SECTION OF EXFOLIATED SKIN AND FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR BETWEEN FS 243.250 TO FS 327.630.

Part: SPAR — CORRODED (WING) · airframe 28,388 hrs · 37,231 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED CORROSION AT RT FWD SPAR FLANGE JUST BEHIND DRAIN PLUG WS 126.5. BLENDED OUT CORROSION AT RT FWD MAIN SPAR FLANGE JUST BEHIND DRAIN PLUG.

Part: STRINGER — CORRODED (LT WING) · airframe 28,388 hrs · 37,231 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED SMALL AREA OF CORROSION AT LT COLLECTOR TANK STRINGER J WS 118.50. REMOVED CORROSION AT LEFT COLLECTOR TANK STRINGER J WS 118.50 AND INSTALLED REPAIR DOUBLER STRAP.

Part: SPAR — CORRODED (LT WING) · airframe 28,388 hrs · 37,231 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED SMALL AREA OF CORROSION AT LT WING FWD SPAR FLANGE WS 125.25. REMOVED SURFACE CORROSION AT LEFT WING FORWARD SPAR WS 125.25 AND INSTALLED REPAIR DOUBLER STRAP.

Part: STRINGER — CORRODED (LT WING) · airframe 28,388 hrs · 37,231 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED SMALL AREA OF CORROSION AT LT WING COLLECTOR TANK STRINGER J WS 119.00. REMOVED CORROSION AT LEFT WING COLLECTOR TANK STRINGER J AND INSTALLED EXTERNAL DOUBLER REPAIR.

Part: SKIN — CORRODED (BS 213) · airframe 28,388 hrs · 37,231 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED .5 INCH CRACK ON RT FUSELAGE BELLY AT FS 213.250. CLEANED AREA OF SUSPECT CRACK DYE PENETRANT INSPECTION PERFORMED NO CRACKS FOUND.

Part: SKIN — CORRODED (BS 327) · airframe 28,388 hrs · 37,231 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT FUSEALGE BELLY EXFOLIATED AT FS 327.630. REMOVED CORRODED SECTION OF FUSELAGE SKIN CUT STRINGER 15R AND STRINGER 16 INSTALLED REINFORCEMENT STRAP,STRINGER AND REPAIR PATCH.

Part: SKIN — CORRODED (BS 423) · airframe 28,388 hrs · 37,231 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT FUSEALGE BELLY EXFOLIATED AT FS 423.250. REMOVED CORRODED SECTION OF SKIN AND SECTION OF STRINGER 16 AT FS 423.250 BETWEEN FS 415.250 AND 430.250 REPAIRED STRINGER AND INSTALLED EXTERNAL REPAIR PATCH AND DOUBLER.

Part: SKIN — CORRODED (BS 243) · airframe 28,388 hrs · 37,231 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT FUSELAGE BELLY EXFOLIATED AT FS 243.250. REMOVED CORRODED SECTION OF SKIN AT FS 243.250 AND DAMAGED SECTION OF STRINGER 15R REPAIRED STRINGER 15R,FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR FROM FS 228.250 TO 243.250.

Part: DOOR — STIFF (EMERGENCY EXIT) · airframe 27,506 hrs · 36,315 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED LT EMERGENCY EXIT INTERIOR AND EXTERIOR HANDLES HARD TO OPERATE. LUBRICATED LT EMERGENCY EXIT LATCH PINS AND GUIDES. OPS CHECK OK.

Part: DOOR — STIFF (EMERGENCY EXIT) · airframe 27,506 hrs · 36,315 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED RT AFT EMERGENCY EXIT INTERIOR AND EXTERIOR HANDLES HARD TO OPERATE. LUBRICATED RT AFT EMERGENCY EXIT HANDLES. OPS CHECK GOOD.

Part: ANNUNCIATOR — LOOSE (COCKPIT) · airframe 27,035 hrs · 35,848 cycles

FLIGHT - 9236 - EYW/TPA - PILOT REPORTED "H H" LANDING GEAR POSITION INDICATORS INTERMITTENT. RESET AND RE-SECURED H H ANNUNCIATOR SOCKET ASSEMBLIES.

Part: HINGE BRACKET — CORRODED (RT ELEVATOR) · airframe 26,050 hrs · 34,755 cycles

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

Part: UPLOCK SWITCH — OUT OF ADJUST (MLG) · airframe 25,443 hrs · 34,058 cycles

AFTER TAKEOFF, LANDING GEAR UNSAFE LIGHT ON WHEN GEAR HANDLE PLACED IN THE UP POSITION. DIVERTED AND LANDED WITHOUT INCIDENT. ADJUSTED NOSE LANDING GEAR UPLOCK SWITCH.

Part: RELAY — SHORTED (MLG WARNING) · airframe 24,194 hrs · 32,579 cycles

FLIGHT: 9151 PNS/TPA DURING APPROACH LANDING GEAR WARNING HORN SILENCE BUTTON CAUSES GEAR WARNING LIGHTS TO EXTINGUISH. REPLACED NUMBER 8 RELAY CARD MODULE. LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK NORMAL.

Part: HINGE BRACKET — CORRODED (ELEVATOR) · airframe 24,042 hrs · 32,408 cycles

REPORT: AT SCHEDULED ROUTINE MAINTENANCE LEFT OUTBOARD ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED LEFT OUTBOARD ELEVATOR HINGE BRACKET.

Part: HYDRAULIC SYSTEM — LEAKING · airframe 23,997 hrs · 32,351 cycles

FLIGHT: 9264 MHH/FLL - UPON LANDING, NO RIGHT BRAKE PRESSURE BRAKING INOPERATIVE POST FLIGHT REVEALED HYDRAULIC FLUID LEAK. SECURED RIGHT BRAKES FRONT BLEEDING PORTS. OPERATIONAL CHECK NORMAL.

Part: SKIN — CORRODED (BS 327) · airframe 23,946 hrs · 32,285 cycles

SCHEDULED INSPECTION DISCOVERED BELLY SKIN CORROSION AT FS 327.830 BETWEEN STRINGER 15R THRU 14R. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW STRUCTURAL REPAIR MANUAL 51-70-06.

Part: HINGE BRACKET — CORRODED (RT ELEVATOR)

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

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 3 · airframe 21,880 hrs · 29,881 cycles

AT SCHEDULED STRUCTURAL C-CHECK DISCOVERED CORROSION AT FS 423.25, STR 16 THRU 14R. REMOVED DAMAGED MATERIAL, AND INSTALLED EXTERNAL DOUBLER IAW SRM SECTION 51-70-06.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 21,880 hrs · 29,881 cycles

AT SCHEDULED STRUCTURAL C-CHECK DISCOVERED CORROSION IN BELLY SKIN AT FS408.25, STR 16 TRU 14R. REMOVED DAMAGED MATERIAL AND INSTALLED EXTERNAL DOUBLER IAW SRM 51-70-06.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 21,880 hrs · 29,881 cycles

AT SCHEDULED STRUCTURAL C-CHECK DISCOVERED BELLY SKIN CORROSION AT FS 393.25, STR 16 THRU 14R. REMOVED DAMAGED MATERIAL AND INSTALLED EXTERNAL DOUBLER IAW SRM SECTION 51-70-06.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 21,880 hrs · 29,881 cycles

AT SCHEDULED STRUCTURAL C-CHECK DISCOVERED BELLY SKIN CORROSION AT FS 348.25, STR 16 THRU 14R. REMOVED DAMAGED MATERIAL AND INSTALLED EXTERNAL DOUBLER IAW SRM SECTION 51-70-06.

Part: MASTER CYLINDER — INOPERATIVE (BRAKES)

DURING TAXI, LT PEDAL WENT FLAT. RETURNED TO GATE. REPLACED FO LT MASTER CYLINDER. (K)

Part: PACKING — LEAKING (LT BRAKE)

LT BRAKE INOPERATIVE. PEDAL GOES TO FLOOR. REPLACED LT BRAKE INTERCONNECT PACKINGS. BLED BRAKE SYS. (K)

Part: RESERVOIR — LOW (LT BRAKE)

LT BRAKE INOPERATIVE. FOUND BRAKE RESERVOIR LOW. SERVICED RESERVOIR. BLED LT BRAKE ASSEMBLY. (K)

Part: BRAKE — FAILED (MLG)

CAPTAIN`S SIDE LT BRAKE PEDAL WOULD NOT BRAKE. SERVICED BRAKE SYSTEM. NO LEAK NOTED. (K)

Part: CONNECTING ROD — OUT OF ADJ (LT ENGINE)

FLT 9137 - FLL - DURING FLIGHT, LEFT ENGINE SURGES THREE TIMES AT DIFFERENT POWER SETTINGS. ENGINE SHUTDOWN AND SECURED. ADJUSTED GOVERNOR INTERCONNECT ROD. OPERATIONAL CHECK NORMAL. (M)

Part: SKIN — FAILED (RT WING)

AZO - DURING A 3RD 200 HOUR INSPECTION, A 1.5 INCH CRACK WAS FOUND ON THE EXTERIOR SKIN ON THE RIGHT WING ROOT INBOARD JUST FORWARD OF WING SPAR. MAINTENANCE REMOVED THE INTERIOR FOR INSPECTION OF THE SPAR AND SURROUNDING AREAS AND FOUND NO OTHER DAMAGE. THE SKIN WAS REPAIRED AT FS 303 BY STOP DRILLING CRACK AND WITH A DOUBLER PATCH IAW FAA/DER APPROVED DWG NR DA0007-51S DATED JULY 19, 2000. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: SWITCH — WIRE BROKEN (COCKPIT)

CLE - FLT 3251 - CREW REPORTED THAT THE LEFT GENERATOR VOLTAGE SELECT INDICATOR READS 'O' VOLTS WHEN GENERATOR IS ON LINE. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT AND THEN REPAIRED A BROKEN WIRE ON THE MAIN VOLTAGE SWITCH IAW B1900 MM 31-10-00. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: DEICE BOOT — DEBONDED (NR 1 PROP)

TYL - FLT 9447 - PILOT REPORTED DURING A POST-FLIGHT WALKAROUND INSPECTION, FOUND LT PROPELLER HAD ONE DEICE BOOT DEBONDED FROM BLADE. THE DEICE BOOT REMOVED AND ACFT FERRIED TO IAH WHERE MAINTENANCE INSTALLED A DEICE BOOT ON PROPELLER. ACFT WAS THEN APPROVED FOR RETURN TO SERVICE. (X)