N262AT

Part: GEAR SHAFT — SHEARED (ENGINE)

AFTER DEPARTING FROM ANGUILLA ISLAND AND DURING THE CLIMBING STAGE THE ENGINE SURGED APPROXIMATELY 40-50 PERCENT TORQUE. ENGINE WAS SHUT DOWN AND AIRCRAFT DIVERTED AND LANDED IN ST MARTEEN ISLAND. FURTHER INVESTIGATION REVEALED THAT THE ENGINE TOWER SHAFT WAS SHEARED CAUSING THE ENGINE SURGE. ENGINE WAS REMOVED AND REPLACED. (M)

Part: GEAR SHAFT — SHEARED (ENGINE)

AFTER DEPARTING FROM ANGUILLA ISLAND AND DURING THE CLIMBING STAGE THE ENGINE SURGED APPROXIMATELY 40-50 PERCENT TORQUE. ENGINE WAS SHUTDOWN AND AIRCRAFT DIVERTED AND LANDED IN ST MARTEEN ISLAND. FURTHER INVESTIGATION REVEALED THAT THE ENGINE TOWER SHAFT WAS SHEARED CAUSING THE ENGINE SURGE. ENGINE WAS REMOVED AND REPLACED. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY BATTERY LOW VOLTAGE AT STATION 10WL, 10WL, 15WL, AND 29WL. REMOVED AND REPLACED BATTERY PACK 10WL, 18WL, 15WL AND 29WL AS PER MM 33-50-00. (M)

Part: THRESHOLD — CORRODED (LAVATORY)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED THE LAVATORY THRESHOLD CORRODED OUT OF LIMITS AT FRAME 39. MAINTENANCE REMOVED AND REPLACED THRESHOLD IAW SRM 51-25-02. AC WS RETURNED TO SERVICE. (M)

Part: FLOOR BEAM — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED FLOOR BEAMS 36, 38, 39, AND 40 CORRODED OUT OF LIMITS. MAINTENANCE REMOVED, FABARICATED AND INSTALLED NEW FLOOR BEAMS AT LOCATIONS 36, 38, 39, AND 40. MAINTENANCE SPLICED FLOOR BEAM 40 IAW SRM 53-00-00, FIG 429. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NRS 97ZZZX69, 97ZZZX70, AND 97ZZZX71. (X)

Part: FLOOR BEAM — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED FLOOR BEAMS 36, 38, 39, AND 40 CORRODED OUT OF LIMITS. MAINTENANCE REMOVED, FABARICATED AND INSTALLED NEW FLOOR BEAMS AT LOCATIONS 36, 38, 39, AND 40. MAINTENANCE SPLICED FLOOR BEAM 40 IAW SRM 53-00-00, FIG 429. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NRS SIMA97349-2, 97ZZZX70, AND 97ZZZX71.

Part: FLOOR BEAM — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED FLOOR BEAMS 36, 38, 39, AND 40 CORRODED OUT OF LIMITS. MAINTENANCE REMOVED, FABARICATED AND INSTALLED NEW FLOOR BEAMS AT LOCATIONS 36, 38, 39, AND 40. MAINTENANCE SPLICED FLOOR BEAM 40 IAW SRM 53-00-00, FIG 429. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NRS SIMA97349-2, 97ZZZX69, AND 97ZZZX70.

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED THE LEFT AFT OUTBOARD, LEFT CENTER INBOARD, RIGHT AFT OUTBOARD AND RIGHT AFT INBOARD SEAT TRACKS CORRODED OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED ALL FOUR SEAT TRACKS IAW SRM 51-25-04. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NRS SIMA97349-1, 97ZZZX72, AND 97ZZZX74.

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED FLOOR BEAMS 36, 38, 39, AND 40 CORRODED OUT OF LIMITS. MAINTENANCE REMOVED, FABARICATED AND INSTALLED NEW FLOOR BEAMS AT LOCATIONS 36, 38, 39, AND 40. MAINTENANCE SPLICED FLOOR BEAM 40 IAW SRM 53-00-00, FIG 429. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NRS SIMA97349-2, 97ZZZX71, AND 97ZZZX72.

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED THE LEFT AFT OUTBOARD, LEFT CENTER INBOARD, RIGHT AFT OUTBOARD AND RIGHT AFT INBOARD SEAT TRACKS CORRODED OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED ALL FOUR SEAT TRACKS IAW SRM 51-25-04. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NRS SIMA97349-1, 97ZZZX72, AND 97ZZZX73.

Part: SKIN — CORRODED (PASSENGER DOOR)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED THE PASSENGER CREW DOOR INNER SKIN CORRODED AT BOTTOM SIDE. MAINTENANCE REPAIRED THE INNER SKIN IAW SRM 51-25-03. AIRCRAFT RETURNED TO SERVICE. (X)

Part: ZEE MEMBER — CORRODED (FUSELAGE)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED THE RIGHT AFT ZEE MEMBER BETWEEN FRAME 39 AND FRAME 41 CORRODED OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED NEW ZEE MEMBER IAW SRM 51-25-02. AICRAFT REURNED TO SERVICE. (X)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED THE LEFT AFT OUTBOARD, LEFT CENTER INBOARD, RIGHT AFT OUTBOARD AND RIGHT AFT INBOARD SEAT TRACKS CORRODED OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED ALL FOUR SEAT TRACKS IAW SRM 51-25-04. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NRS 97ZZZX72, 97ZZZX73, AND 97ZZZX74. (X)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, MAINTENANCE DISCOVERED THE LEFT AFT OUTBOARD, LEFT CENTER INBOARD, RIGHT AFT OUTBOARD AND RIGHT AFT INBOARD SEAT TRACKS CORRODED OUT OF LIMITS. MAINTENANCE REMOVED AND INSTALLED ALL FOUR SEAT TRACKS IAW SRM 51-25-04. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NRS SIMA97349-1, 97ZZZX73, AND 97ZZZX74.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ORD - FLT 4341 - FORWARD FLOOR EMERGENCY LIGHT INOP. RAI'D EMERGENCY POWER SUPPLY AND BATTERY PACK OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BULB — LOOSE (CABIN)

MSN - FLT 4046 - FORWARD NR 1 FLOOR PROXIMITY LIGHT INOPERABLE. ITEM MEL'D PER 33-22 AND AIRCRAFT RETURNED TO SERVICE. ON OVERNIGHT VISIT, FOUND LIGHT BULB LOOSE IN SOCKET. RE-INSTALLED LIGHT BULB IAW STANDARD MAINTENANCE PRACTICES. PERFORMED OPS CHECK SATISFACTORILY AND RETURNED AIRCRAFT TO SERVICE. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - FLT 4034 - REMOVED AND REPLACED BATTERY PACK AT 10W1. PERFORMED SYSTEM OPS CHECK AND RETURNED AIRCRAFT TO SERVICE. (X)

Part: LIGHTS — INOPERATIVE (CABIN)

PIA - FLT 4144 - EMERGENCY FLOOR LIGHT ROW 2, 3, AND 5 INOP. CHECK EMERGENCY FLOOR LIGHTING, DEFERRED PER SIMMONS MEL 33-22. AIRCRAFT WAS RETURNED TO SERVICE. MAINTENANCE PEFORMED OPS CHECK OF EMERGENCY LIGHT SYSTEM WITH NO DEFECTS NOTED. CLEARED MEL AND RETURNED AIRCRAFT TO SERVICE. (M)

Part: POWER SUPPLY — FAILED (CABIN)

ORD - FLT 4147 - FORWARD EMERGENCY EXIT SIGNS ARE INOP. REPLACED FORWARD EMERGENCY LIGHT POWER SUPPLY. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PRESS SWITCH — FAILED (BLEED AIR SYST)

ORD - FLT 4171 - CREW REPORTED AN AIRFRAME/AIRBLEED FAULT FOLLOWED BY A HYDRAULIC LOW PRESSURE AND AN ACRIC SMELL IN THE COCKPIT. RAI'D AIRFRAME AIRBLEED PRESSURE SWITCH AND RESET CB FOR HYD SYSTEM. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BOLT — BROKEN (LT MLG ACT)

MQT - MAINTENANCE PERFORMING AN IMBV INSPECTION, FOUND THE LEFT MAIN LANDING GEAR ACTUATOR BRACKET FORWARD LOWER BOLT BROKEN OFF. MAINTENANCE REMOVED AND REPLACED BOLT IAW EO E15300-208. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: TRUNNION LEG — FAILED INSP (RIGHT)

ORD - RIGHT LANDING GEAR FAILED ULTRASOUND INSPECTION OF TRUNNION LEG AS PER MESSIER DOWTY TECHNIQUE A/VT NR 20317/96 (FCD E9-32-002). REPLACED GEAR ASSEMBLY IAW ATR 42 JIC 32-11-00. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: EEL — INOPERATIVE (RT FWD FUS)

RFD - DURING PS-2 CHECK, MAINTENANCE DISCOVERED THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY IAW JIC 33512-0. PERFORMED OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONTROL ROD — CORRODED (RUDDER TAB)

MQT - DURING BRIDGE INSPECTION, MAINTENANCE FOUND THE RUDDER TAB CONTROL ROD APPEARED TO BE CORRODED ON INTERNAL ROD. THE ROD WAS REMOVED AND CLEANED OF CORROSION IAW SRM SECTION 51. AFTER ROD INSTALLATION, OPERATIONAL CHECKS OF THE RUDDER TAB WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (W)

Part: BELL CRANK — CORRODED (RT AILERON)

MQT - MAINTENANCE REPORTED THE RIGHT AILERON BELL CRANK JUST OUTBOARD OF FLAP, AFT BEARING CORRODED. THE BELL CRANK WAS REMOVED AND REPLACED AND OPS TEST GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (W)