N57734

Part: WIRE — DAMAGED (AUTOPILOT SYS) · airframe 23,506 hrs · 30,888 cycles

A/P FAILED DURING FLIGHT. A/P FAIL ON MAP AND MASTER WARNING. FOLLOWED QRH. A/P WOULD NOT TRANSFER. REPAIRED WIRE ON CAPTAIN'S TRANSFER SWITCH IAW 22-10-11. OPS CHECKS GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAP) · airframe 23,376 hrs · 30,742 cycles

CAPTAIN REPORTS CONTROL FAULT INDICATION ON FLAP WARNING PANEL. REPLACED LT NACELLE FLAP ACTUATOR PER AMM 27-50-08. OPS AND LEAK CHECKS GOOD.

Part: SERVO — MALFUNCTIONED (STICK SHAKER) · airframe 23,341 hrs · 30,705 cycles

CAPTAINS STICK SHAKER INOP. REMOVED AND REPLACED CAPTAIN'S STICK SHAKER. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN)

IAH- MAINTENANCE, WHILE INSPECTING THE ARICRAFT THE MECHANIC NOTED THAT THE LOWER CENTER EMERGENCY LIGHTS FAILED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AMD REPLACED THE #2 (TWO) EMERGENCY BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTIBG SYSTEM,NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — INOPERATIVE (COCKPIT)

IAH- DURING TAXI, FLIGHT 3585, THE EMERGENCY LIGHT (NOT ARMED LIGHT ON THE MAP)CAME ON WHEN THE SWITCH IS IN THE ARMED POSITION. IAH- MAINTENANCE REMOVED AND REPLACED RELAY K201, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TANK — ODOR (APU)

IAH- AT THE GATE THE CREW NOTED THAT A GAS FUME SMELL IN THE CABIN WITH THE APU RUNNING. MAINTENANCE DRAINED THE APU EPA TANK, PERFORMED A OPERATIONAL CHECK OR THE APU, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

IAH- MAINTENANCE, WHILE PERFORMING A SERVICE CHECK THE MECHANIC NOTED THAT THE MIDDLE CABIN EMERGENCY LIGHTS FAILED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND MIDDLE EMERGENCY BATTERY PACK, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE

Part: O-RING — LEAKING (BLEED AIR SYS)

IAH- DURING FLIGHT 3633 THE CREW NOTED DUCT LEAK ON NUMBER 1 ENGINE IN FLIGHT. SHUT DOWN ENGINE AND DECLARED EMERGENCY, LANDED AT IAH WITHOUT INCIDENT. IAH- MAINTENANCE REPOSITIONED THE WATER SEPARATOR SPRAY NOZZLES AND REMOVED AND REPLACED ALL O-RINGS IN THE NUMBER ONE MAIN AIR DISTRIBUTION SYSTEM FROM ENGINE TO CROSSBLEED VALVE. PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. REINSTALLED INBOARD LEADING EDGE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

IAH- DURING POST FLIGHT THE CREW NOTED THAT THE EMERGENCY ISLE PATH LIGHTS DID NOT ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE #2 EMERGENCY BATTERY PACK,PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED,AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN)

IAH- DURING PREFLIGHT THE CREW NOTED THAT FOUR EMERGENCY LIGHTS ON THE FLOOR FAILED TO ILLUMINATE. IAH- MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CRACKED (RT WING) · airframe 21,294 hrs · 28,245 cycles

SJK - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, STRINGER 8 ON THE RIGHT WING WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE CRACKED STRINGER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (CABIN)

SHV - DURING MAINTENMANCE INSPECTION, THE EMERGENCY EXIT SIGN AT SEAT 10-C WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE EMERGENCY LIGHT SYSTEM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

IAH - DURING MAINTENANCE INSPECTION, THE RIGHT HAND OUTBOARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (LT & RT NACELLE) · airframe 21,294 hrs · 28,245 cycles

SJK - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FRAME 1 ON THE LEFT HAND AND RIGHT HAND NACELLES WERE FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAMES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: A/C PACK — FAILED (NR 2)

CLL - FLIGHT 3463, THE CREW REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED, THE OXYGEN MASKS DEPLOYED, AND THE AIRCRAFT RETURNED TO CLL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE NUMBER TWO PACK HAD FAILED. THE NUMBER TWO PACK WAS PLACED ON MEL 21-50-02 CONTROL NUMBER 004810, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE, THE AIRCRAFT WENT TO SHV ON 01/18/01 WHERE MAINTENANCE PERFORMED EXTENDED OPERATIONAL CHECKS OF HTE NR 2 PACK SYSTEM WITH NO DEFECTS NOTED, REMOVED MEL 21-50-02 CONTROL 004810, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (COCKPIT)

IAH - FLT 3474 - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED A BURNING SMELL IN THE COCKPIT. MAINTENANCE FOUND A LOOSE CONNECTOR ON THE FIRST OFFICER'S SIDE GENERATOR CONTROL UNIT. MAINTENANCE RESECURED THE CONNECTOR AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SENSOR — FAILED (RT MLG)

CLE - FLT 3186 - AFTER TAKEOFF, THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN A LOCK SENSOR HARNESS. OPERATIONAL CHECKS WERE GOOD IAW EMBRAER MM 32-30-00. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CABIN)

CLE - FLT 3147 - ON TAKEOFF ROLL, CREW RECEIVED A SMOKE ALARM INDICATION. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RELEASED IAW MEL 21-51-2. (X)

Part: SWITCH — DIRTY (POWER LEVER)

CLE - FLT 3102 - THE CREW REPORTED AN AURAL WARNING AT 90 KNOTS ON TAKEOFF. THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. (X)

Part: FRAME — CRACKED (LT NACELLE)

DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT REAR NACELLE FRAME CRACKED ABOVE REAR SPAR. FABRICATED AND INSTALLED REPAIR DOBLERS IAW SRM 51-70-05 AND 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: FIRE WALL — CRACKED (APU COMPT)

DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND APU FIRE WALL CRACKED AT FIRE BOTTLE DISCHARGE TUBE. FABRICATED REPAIR DOUBLER AND INSTALLED IAW EC5330-01102. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: BATTERY — DISCHARGED (ROW 8)

DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND EMERGENCY LIGHTING INOPERATAIVE FROM ROW 8 TO AFT. REPLACED BATTERY PACK IN AFT EMERGENCY LIGHTING POWER UNIT IAW AMM 33-50-02 AND CMM 33-51-04. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FRAME 32-39)

DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT INBOARD SEAT TRACK CORRODED FROM FRAME 32 TO 39. REPLACED SEAT TRACK IAW EC25-10-01016. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: SKIN — GOUGED (FUSELAGE)

DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND FUSELAGE SKIN GOUGED FOUR PLACES UNDER PANEL NR 198. BLENDED GOUGES AND INSTALLED RIVETS IAW EC5330-01042 AND DER REPORT NR 99-045. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: BEAM — CORRODED (FRAME 40)

DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND FRAME 40 CROSSBEAMS CORRODED. REMOVED CORROSION FROM LEFT BEAMS. REMOVED AND INSTALLED NEW RIGHT BEAMS IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: SWITCH — CONTAMINATED (RT MLG)

IAH - FLT 3786 - PILOT REPORTED THE RIGHT GEAR DID NOT RETRACT. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED MOISTURE FROM THE RIGHT GEAR UPLOCK PROXIMITY SWITCHES. THE GEAR OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: HYD LINE — CRACKED (LT MLG WW)

CLE - FLT 3182 - CREW REPORTED THAT THEY RECEIVED A LOW LEVEL AND LOW PRESSURE INDICATION ON TEH LEFT GREEN HYDRAULIC SYSTEM. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE LEFT HYDRAULIC PUMP SUCTION LINE IAW EMB-120 MM 20-10-03 AND EMB-120 IPC 29-30-00. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: SUPPORT RIB — CRACKED (GEAR DOOR)

IAH - DURING C-CHECK INSPECTION, FOUND LEFT INBOARD MAIN LANDING GEAR DOOR ACTUATOR ATTACHMENT FORWARD RIB CRACKED AT TOP. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW EMB 120 MM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (CABIN)

IAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE VERTICAL FLOOR ATTACH ANGLE CRACKED AT FRAME NR 13. MAINTENANCE REMOVED AND REPLACED THE ATTACH ANGLE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SKIN — CRACKED (GEAR DOOR)

IAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT NOSE GEAR DOOR INNER SKIN CRACKED AT ACTUATING ROD ATTACHMENT. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW EC NR 5280-01012. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: PROFILE — CRACKED (PAX DOOR)

IAH - DURING C-CHECK INSPECTION, FOUND PASSENGER DOOR CENTER AFT PROFILE ON DOOR STRUCTURE CRACKED. MAINTENANCE REMOVED AND REPLACED THE PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, FOUND LEFT FORWARD SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-10-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SKIN — CRACKED (GEAR DOOR)

IAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT NOSE GEAR DOOR INNER SKIN CRACKED AT ACTUATING ROD ATTACHMENT. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW EC NR 5280-01012. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (CABIN)

IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE VETICAL FLOOR ATTACH ANGLE CRACKED AT FRAME NR 13. MAINTENANCE REMOVED AND REPLACED THE ATTACH ANGLE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SUPPORT — CRACKED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, FOUND FORWARD FUSELAGE SKIN SUPPORT CRACKED AT FRAME NR 9 ON RIGHT SIDE BELOW WINDSHIELD. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: HALF FRAME — CRACKED (LT NACELLE)

IAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE HALF FRAME CRACKED AT OUTBOARD AFT GEAR DOOR FORWARD HINGE POINT. MAINTENANCE REMOVED AND REPLACED THE HALF FRAME IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BRACKET — CRACKED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, FOUND AFT PASSENGER DOOR ACTUATOR FUSELAGE SIDE ATTACHMENT BRACKET CRACKED AT FRAME NR 15. MAINTENANCE REMOVED AND REPLACED THE BRACKET IAW EMB-120 SRM 53-10-10 AND 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, FOND LEFT LOWER ATTACHMENT ANGLE FOR WING TO FUSELAGE FAIRING PANEL 193 CRACKED ON AFT END. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW EMB120 SRM 51-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, FOUND RIGHT FORWARD SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FUSE — BLOWN (CABIN)

IAH - FLT 3952 - LOG PAGE NR 422265 - POST-FLIGHT INSPECTION FOUND LEFT AND RIGHT OVERWING EMERGENCY EXIT EXTERIOR AFT LIGHTS INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHTING FUSE AT FUSELAGE STATION NR 80897, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: CONTROL HANDLE — FAILED (COCKPIT)

IAH - FLT 3993 - PILOT REPORTED THAT AFTER TAKEOFF, THE GEAR 'A' SYSTEM RED POSITION INDICATION LIGHT REMAINED ON AFTER GEAR RETRACTION. THE AIRCRAFT LANDED AT IAH WITHOUT FURTHER INCIDENT, WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE. THE AIRCRAFT OPERATIONALLY CHECKED GOOD AND WAS RETURNED TO SERVICE. (M)

Part: PROP ACTUATOR — SEIZED (RT PROP)

IAH - FLT 3830 - DURING TAKEOFF ROLL, THE NR 2 ENGINE PRODUCED ONLY 22 PERCENT TORQUE. AIRCRAFT RETURNED, MX FOUND THE RIGHT PROPELLER ACTUATOR PITCH CHANGE MECHANISM SEIZED. THE RIGHT PROPELLER ACTUATOR WAS REMOVED AND REPLACED GROUND OPERATIONAL, LEAK CHECKS GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: CHANNEL — CRACKED (RT NACELLE)

IAH - DURING C-CHECK INSPECTION, FOUND RIGHT MAIN LANDING INBOARD LOWER NACELLE CHANNEL DEFORMED AND CRACKED BETWEEN NACELLE FRAME 14 AND FRAME 15. MAINTENANCE REMOVED AND REPLACED NACELLE CHANNEL. (M)

Part: BUTTSTRAP — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, FOUND FRAME 37 TO FRAME 41.5 RIGHT INBOARD BUTTSTRAP TO HAVE CORROSION BEYOND LIMITS. MX REMOVED AND REPLACED RT INBOARD BUTTSTRAP FRAME 37 TO FRAME 41.5. (M)

Part: T-CAP — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, FOUND RIGHT INBOARD T-CAP FRAME 38 TO HAVE CORROSION BEYOND LIMITS. MX REMOVED AND REPLACED RT INBOARD T-CAP FRAME 38. (M)

Part: T-CAP — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, FOUND FRAME 38 LEFT AND RIGHT OUTBOARD T-CAPS TO HAVE CORROSION BEYOND LIMITS. MX REMOVED AND REPLACED LEFT AND RIGHT OUTBOARD T-CAPS FRAME 38. (M)

Part: SEAT TRACK — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, FOUND PASSENGER LEFT AND RIGHT SEAT TRACKS TO HAVE CORROSION BEYOND LIMITS. MX REMOVED AND REPLACED SEAT TRACKS, FRAME 29 TO FRAME 39. (M)

Part: BUTTSTRAP — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, FOUND FUSELAGE CENTER BUTTSTRAP FRAME 39 TO FRAME 44 TO HAVE CORROSION BEYOND LIMITS. MX REMOVED AND REPLACED CENTER BUTTSTRAP FROM FRAME 37 TO FRAME 44. (M)

Part: T-CAP — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, FOUND FRAME 36 LEFT OUTBOARD T-CAP TO HAVE CORROSION BEYOND LIMITS. MX REMOVED AND REPLACED FRAME 36 LEFT OUTBOARD T-CAP. (M)

Part: PIN — BENT (LT MLG)

IAH - FLT NR 2582 - DURING APPROACH TO IAH, WHEN LANDING GEAR WAS SELECTED DOWN, LEFT MLG FORWARD DOOR REMAINED OPEN. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AND FOUND GEAR DOOR MAINTENANCE SAFETY LATCH NOT SECURED. PROBLEM WAS CAUSED BY A BENT CATCH PIN FOR SAFETY LATCH. MAINTENANCE REPLACED CATCH PIN AND PERFORMED OPERATIONAL CHECK. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: WASHER — BROKEN (LT MLG DOOR)

SHV - FLT 2519 - DURING A PREFLIGHT INSPECTION, THE PILOT NOTICED THAT THE LEFT MAIN GEAR AFT OUTBOARD DOOR HAD COME LOOSE AT THE ACTUATING ROD. THE GEAR DOOR WAS REMOVED AND THE AIRCRAFT WAS FERRIED TO IAH, WHERE MAINTENANCE REMOVED AND REPLACED A BROKEN SAFETY TANG WASHER ON THE ACTUATING ROD. THE MAIN GEAR AFT DOOR WAS REINSTALLED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: EEL BULB — INOPERATIVE (EXTERNAL FUS)

IAH - DURING PREFLIGHT CHECK, FOUND AFT EXTERNAL EMERGENCY LIGHTS OUT. MAINTENANCE REMOVED AND REPLACED THE BULBS, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (W)

Part: ANGLE — CRACKED (FIN TO FUSELAGE)

IAH - DURING C-CHECK INSPECTION, FOUND RT FIN TO FUSELAGE ATTACH (DRAG) ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED RT ATTACH ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT - 8,443.7. CYCLES - 12,794. (X)

Part: BLADE — CRACKED (NR 1 PROP)

IAH - DURING C-CHECK INSPECTION, THE NR 1 PROPELLER, NR 1 BLADE WAS FOUND TO HAVE A LIFTING AND TORN EROSION SHEATH. UPON REMOVAL OF THE SHEATH. THE BLADE LEADING EDGE BELOW THE SHEATH, WAS FOUND CRACKED THROUGH THE RESIN INTO THE HEATING ELEMENT IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLADE AND THE AIRCRAFT RETURNED TO SERVICE. A/C TT 8443.7. CYCLES 12,794. (X)