CARIBBEAN SUN AIRLINES INC

Operated by Caribbean Sun Airlines Inc (per NTSB report)

DURING PREFLIGHT INSPECTION, FLIGHT CREW REPORTED THAT THE TAIL CONE LIGHT WAS INOPERATIVE. ADDITIONALLY, WHEN THE EMERGENCY LIGHTING SYSTEM WAS ACTIVATED, MULTIPLE CEILING LIGHTS DID NOT ILLUMINATE AS REQUIRED. THE EMERGENCY EXIT LIGHT AT THE L2 DOOR WAS ALSO FOUND INOPERATIVE. THE DISCREPANCIES WERE IDENTIFIED ON THE GROUND AND RECORDED IN THE AIRCRAFT MAINTENANCE LOG. MAINTENANCE PERFORMED TROUBLESHOOTING AND CORRECTIVE ACTIONS IN ACCORDANCE WITH APPLICABLE PROCEDURES, AND THE SYSTEM WAS RETURNED TO SERVICE AFTER SATISFACTORY OPERATIONAL CHECKS.

DURING PRE-FLIGHT CHECK FOUND L1 DOOR EMERGENCY EXIT PORTABLE LIGHT INOPERATIVE.

DURING SERVICE CHECK FOUND DOOR R1 LIGHT EXIT LENS COVER IS CRACKED. REMOVED & REPLACED LENS IAW WITH AMM 33-60-98. LENS IS A CONSUMABLE ITEM.

BURNING SMELL REPORTED AFTER FLIGHT BY FLT ATTENDANTS SUSPECTED FROM LEFT PACK PER THEM. PERFORMED INSPECTION WITH L/H AND R/H A/C PACKS AND NO DISCREPANCY FOUND AS PER MD80 AMM 21-00-00: PERFORMED INSPECTION LEFT AND RIGHT ELECTRIC SYSTEMS NO DISCREPANCY FOUND AS PER MD80 AMM 24-20-00

LEFT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AT UPPER EDGE, ALL THRU THE LENGHT ALSO THE HARWARE OF LOWER EDGE IS RUSTY AND HAS CORROSION AROUND THE FASTENER HEAD. REPAIRED LEADING EDGE PER E.O.'S WAA-250220, WAA-250221, WAA-250222, WAA-250223, WAA-250224, WAA 250225 AND E.O. WAA-250615.

RIGHT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AT UPPER CENTER EDGE AREA AND LOWER SECTION. REPAIRED RIGHT HORIZONTAL STABILIZER LEADING EDGE PER E.O.'S WAA-250319, WAA-250623, AND E.O. WAA-250620.

MAIN CABIN AFT R/H LAVATORY HAS CORROSION ALL AROUND THE FLOOR BASE AND INCORRECT HOSE INSTALL. ACCOMPLISHED AFT R/H LAVATORY STRUCTURAL REPAIR IAW E.O. WAA-250503.

FWD LAVATORY L/H SIDE HAS CORROSION ALL AROUND THE FLOOR BASE. ACCOMPLISH FWD LAVATORY L/H SIDE STRUCTURAL REPAIR IAW E.O. WAA-250303

MAIN CABIN L/H SIDE LAVATORY HAS CORROSION ALL AROUND FLOOR BASE ATTACHMENT AREA. ACCOMPLISH L/H SIDE LAVATORY STRUCTURAL REPAIR IAW E.O. WAA 250403.

MULTIPLES INTERNAL AND EXTERNAL EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS AND EMERGENCY LIGHTSPER MD-80 AMM 33-53-00 OPS CKECK OK.

MAIN CABIN LEFT SIDE WINDOW CUT OUT HAS SEVERAL CORROSION 4, 5, 13, 29, 43, 51. ACCOMPLISHED CORROSION REMOVAL AT MAIN CABIN LEFT SIDE WINDOW CUT OUT NBR 4,13, 29, 43, 51, FOUND WITHIN LIMITS AND REPAIR WINDOW AT # 5 POSITION PER E.O. WAA-250227, MD-80 SRM 53-05 FIG 111, SRM 51-10-3, 51-10-4 AND 51-30-01.

MAIN CABIN RIGHT SIDE WINDOW # 21 HAS CORROSION AROUND CUT OUT. ACCOMPLISHED REPAIR AT WINDOW # 21 R/H SIDE OF FUSELAGE BETWEEN BS 616 AND BS 636 PER E.O. WAA-250219

LEFT HORIZONTAL STABILIZER LEADING EDGE HAS CORROSION AT UPPER EDGE, ALL THRU THE LENGHT ALSO THE HARDWARE OF LOWER EDGE IS RUSTY AND HAS CORROSION AROUND THE FASTENER HEAD. REPAIR DONE BY E.O. WAA-250220, 250221, 250222, 250223, 25024, 250225, 250615.

LOW LEVEL EMERGENCY LIGHTS ON SEATS ROWS 21-32 BURNED OUT

LH ENGINE FAILURE AFTER TAKEOFF

AFTER TAKEOFF AND RISING LANDING GEAR, THE LANDING GEAR'S RED NOSE LIGHT WAS NOT EXTINGUISHED.

EMERGENCY LIGHTS AT CABIN AFT DOOR INOP

EMERGENCY LIGHTSAT L1 AND L2DOORS ARE INOP (NOT TESTING)

EMERGENCY LIGHTS AT INBOARD OVERWING EXIT DOORS L/H AND R/H ARE INOP

EMERGENCY EXIT LIGHT INOP

CENTER FUEL TANK NOT CONSUMING FUEL. REMAINED IN 14.3, DECLARED EMERGENCY DIVERTED TO KMIA.

DURING ADVERSE WEATHER LOST MULTIPLE NAV GUIDANCE INSTRUMENTS, AUTO THROTLE AND AUTO PILOT, DECLARED EMERGENCY DIVERTED TO KIAH. UPON LANDING EVERTHING RETORNED TO NORMAL.

FWD FLIGHT ATTENDANT EMERGENCY EXIT LIGHT WILL NOT HOLD A CHARGE. REMOVED AND REPLACED FWD FLIGHT ATTENDANT EMERGENCY LIGHT IAW MD80 AMM 33-53-00. OPS CHECK NORMAL.

LT ENGINE LOOP A AND FIRE HANDLE INTERMITTENT ILLUMINATION DURING APPROACH WITHOUT FIRE BELL FOR THE ENGINE FIRE AND NO CAWS ALERT. OPS CHECK LT ENGINE FIRE DETECTION LOOP A FOUND TO BE NORMAL IAW AMM 26-10-00. DURING APPROACH, THE LT ENGINE DETECTION LOOP A ND LT FIRE HANDLE INTERMITTENT ILLUMINATION. WHEN TESTING LOOP A IAW QRH, ONLY TWO LOOP LIGHTS CAME ON INSTEAD OF THREE. RT ENGINE AND APU ILLUMINATED, THE LT ENGINE FIRE LOOP A LIGHT AND FIRE HANDLE LIGHT DID NOT ILLUMINATE, FIRE WARNING WAS NOT ACTIVATED IN LT ENGINE, NO CAWS, NO FIRE BELL. TEST WAS NOT SATISFACTORY. PERFORMED TROUBLESHOOTING OF THE NR 1 ENGINE FIRE DETECTION SYSTEM IAW AMM 26-10-00 WDM 26-26-31-01, 26-11-00. FOUND A BROKEN WIRE AT LOOP B OF THE LOWER PYLON DETECTOR ELEMENT THAT WAS CORRECTED. ALSO FOUND SWAPPED ELEMENT WIRES AT UPPER PYLON ELEMENT SENSOR SECURED PER WDM 26-11-00. PERFORMED OPS CHECK. OPS CHECK NORMAL IAW AMM MD-80 26-10-00. NO FAULTS NOTED.

DURING WALK-AROUND, DISCOVERED PASSENGER CABIN WINDOW AT ROW 11 R/H WAS DAMAGED AND ENTERED THE #2 ENGINE. R/R PASSENGER CABIN WINDOW AT ROW 11 RH IAW MD-80 AMM 56-20-00

1. RIGHT ENGINE FAILURE DURING CRUISE, FOLLOWED QRH PROCEDURES AND DIVERTED TO BRO, DECLAIRED EMERGENCY UNEVENTFUL LANDING. 2. DURING WALK-AROUND, DISCOVERED PASSENGER CABIN WINDOW AT ROW 11 R/H WAS DAMAGED. 1. DURING T/S FOUND #2 ENGINE HAD CONSIDERABLE FOD DAMAGE. R/R # 2 ENG IAW W.O. #4863, TC 71-900-01-01. PERFORMED ADJUSTMENT/TEST ENG GROUND RUN-UP ENG CHANGE IAW TC 71-900-02-01. ITEMS S,A,B, +C, SYNCHRONIZATION SYSTEM TEST 6, ELECTRICAL SYSTEM CHK + ITEM, ENGINE GENERATOR FIELD DISCONNECT + OPERATIONAL CHECK COULD NOT BE ACCOMPLISHED DUE TO R/H GENERATOR FAILURE TO COME ONLINE. ADJUSTED PART POWER TRIM AND ENG LOW IDLE TRIM IAW MD80 AMM 71-00-00. ALL PARAMETERS WITHIN LIMITS. C/W BOEING TC 76-021-01-02, ENG EMERGENCY SHUTDOWN SYSTEM. OPS CHK IS SATISFACTORY. 2. R/R PASSGENER CABIN WINDOW AT ROW 11 R/H IAW MD80 AMM 56-20-00.

SMOKE COMING FROM OVERHEAD BIN #3 A/C RH. R/R CABIN SIDEWALL LIGHTING BALLAST IAW MD-80 AMM 33-21-03. OPS CHECK NORMAL.

DURING CRUISE FWD CENTER PUMP STOPPED WORKING. DIVERSION TO MMUN. PERFORMED AIRCRAFT FUEL SUMP IAW MD-80 AMM 12-11-08. FUEL NORMAL. PERFORMED OPS CHK OF FUEL BOOST PUMP IAW MD-80 AMM 28-20-07 OPS CHK NORMAL. COULD NOT DUPLICATE ON GROUND. THIS ACTION CLEARS DMI 4725. PLACARD REMOVED.

AT TOP OF CLIMB LH ENGINE STUCK IN CLIMB SETTING NO THROTTLE RESPONSE BE IT FULL OR IDLE. COMPLETED QRH IDLE 12.2.5 AND 12.2.10 ENGINE. NORMAL SHUTDOWN. LANDING WEIGHT 122.2. DURING T/S DISCOVERED LH THROTTLE PUSH PULL CABLE ROD HAD COME LOOSE FROM FCU. POWER LEVER CRANK. SECURED THROTTLE PUSH-PULL TO FUEL CONTROL UNIT POWER LEVER CRANK IAW M80 76-11-00. FUNCTIONAL CHECK NORMAL.

FWD CABIN EMERGENCY LIGHT BATTERY PACK INOP. R/R FWD CABIN EMERGENCY LIGHT BATTERY PACK IAW AMM 33-53-00.

DURING APPROACH LT ENGINE FIRE INDICATION INTERMITTENT AND THEN WENT OFF. MTX T/S ENGINE FIRE DETECTION STSYEM. FOUND LT FIRE LOOP "A" TEST SYSTEM FAILED. TRANSFERRED TO DMI 4568. IN REFRENCE TO DMI 4568: RERACKED LT ENGINE FIRE DETECTOR CONTROL UNIT AS PER AMM 26-10-03. OPS CHECK NORMAL AS PER AMM 26-10-00. THIS ACTION CLEARED DMI 4568.

FOUND BOTH RIGHT SIDE LOWER EMERGENCY EXIT LIGHT INOP.

DURING ATTEMPTED TAKE OFF AS THRUST LEVERS WERE BEING ADVANCED TO T/O THRUST SETTINGS "L OIL FILTER CLOGGING" WARNING LIGHT ILLUMINATED. THRUST LEVERS WERE RETARDED TO IDLE POSITION AND ABOVE WARNING LIGHT EXTINGUISHED. ANOTHER T/O THRUST SETTING WAS ATTEMPTED WITH SAME "L OIL FILTER CLOGGING" WARNING LIGHT ILLUMINATED. ABORTED TAKE OFF WAS ACCOMPLISHED. A/C RETURNED TO GATE. MT FOUND LT ENGINE MAIN OIL FILTER CONTAMINATED. FILTER WAS R/R. PERFORMED LEAK CHECK AND ENGINE RUN UP. OPS CHECK NORMAL NO LEAKS NOTED. ITEM WAS PLACED ON DMI TO ACCOMPLISH REPETITIVE INSPECTION OF OIL FILTER IN 50 FH.

AFTER TAKE OFF RED "TAIL COMPARTMENT TEMP HIGH" AND "MASTER WARNING" LIGHT ILLUMINATED. INSPECTED TAIL COMPARTMENT FOUND AIR LEAK AT LT PACK PNEUMATIC DUCT. PERFORMED INSPECTION AND CHECK OF LT SECONDARY HEAT EXCHANGER AND FOUND CRACKED. R&R LT SECONDARY HEAT EXCHANGER. OPS CHECK NORMAL. NO LEAKS NOTED.

PRIMARY TRIM COMPENSATOR DID NOT WORK AFTER TAKE OFF AND DURING CLIMB. LT TRIM HANDLE NO CABLE TENSION. T/S FOUND PRIMARY LONGITUDINAL TRIM MANUAL OVERRIDE AND SHUTOFF CONTROL SYSTEM DETENT ROLLER SPRING LOOSE. SECURED ROLLER SPRING. OPS CHECK NORMAL ON GROUND CHECK.

ON TAKE OFF RT ENGINE APPROACHED CAUTION ZONE EGT. AFTER TAKE OFF RT ENGINE EGT 75 DEGREES CELSIUS HIGHER THAN LT ENGINE 560 DEGREES CELSIUS OIL TEMP EXCEEDED 130 DEGREES CELSIUS. FUEL FLOW RT ENGINE 1000 PPH HIGHER THAN LT ENGINE

DURING CLIMB THRU FL270 TAIL COMPARTMENT TEMP HIGH ANNUNCIATOR LIGHT ON. FOUND PRIMARY HEAT EXCHANGER DUCT LEAKING. R&R PRIMARY HEAT EXCHANGER DUCT. NO LEAKS NOTED. OPS CHECK NORMAL.

FUEL NOT PUMPING OUT OF CENTER TANK.

AFT CENTER FUEL PUMP IS NOT PASSING TEST DURING PREFLIGHT.

SMOKE REPORTED IN CABIN. FOUND ROW 2AB SIDEWALL UPPER LIGHT WALL SOCKET HAD AN ELECTRICAL ODOR AND SMOKE. REMOVED A BURNED OUT BULB AT SECTION 2AB IAW 33-21-03. SMOKE WAS CLEARED AND NO ODOR.

RT ENGINE OIL PRESSURE LIGHT ILLUMINATED. RT ENGINE OIL QTY INDICATE "0" PERFORMED QRH.

AT 25,000 FT NOTICED RT ENGINE OIL/FUEL TEMP HIGH PERFORMED QRH AND SHUT DOWN RT ENGINE RETURNED TO KBRO SINGLE ENGINE LANDING.

AIR RETURN TO MGGT. AIRCRAFT WILL NOT PRESSURIZE WITH BOTH PACKS ON AND INDICATING NORMAL.

FWD & AFT CENTER FUEL TANK BOOST PUMP CIRCUIT BREAKER TRIPPED DURING FLIGHT. TROUBLESHOT THE FUEL PUMP CONTINUITY AND RESISTANCE, CHECKED UNSATISFACTORY IAW AMM 28-20-07. REMOVED AND REPLACED THE FUEL BOOST PUMPS FWD AND AFT IAW AMM 28-20-07. OPS CHECKED THE BOOST PUMPS AND FOUND NORMAL IAW AMM 28-20-07.

FWD & AFT CENTER FUEL BOOST PUMP CIRCUIT BREAKER TRIPPED DURING FLIGHT. TROUBLESHOT THE FUEL PUMPS CONTINUITY AND RESISTANCE CHECKED UNSATISFACTORY IAW AMM 28-20-07. REMOVED AND REPLACED THE FUEL BOOST PUMPS FWD AND AFT IAW AMM 28-20-07. OPS CHECKED NORMAL IAW AMM 28-20-07.

RIGHT MAIN LANDING GEAR COLLAPSED AFTER LANDING.

L1 DOOR ESCAPE SLIDE FAILED TO INFLATE DURING DEPLOYMENT PROCESS.

ON LANDING, WHITE SMOKE IN THE CABIN. SUSPECTED AND INSPECTED APU, FOUND APU OIL ENTERING APU AIR INLET.

AFTER LANDING AIRCRAFT WITH APU RUNNING AND 1 PACK ONLINE (RIGHT), SMOKE WAS PRESENT IN CABIN. APU TEMPERATURE RED LINE. REMOVED AND REPLACED APU IAW AMM 49-10-00. OPS CHECK NORMAL.

TAIL COMPARTMENT TEMP HIGH WARNING LIGHT CAME ON DURING CLIMB. DURING TROUBLESHOOTING, FOUND THE RT COOLING TURBINE OUTLET DUCT CLAMP LOOSE. REPOSITIONED THE PNEUMATIC DUCT AND SECURED THE CLAMP. PERFORMED AN OPS & LEAK CHECK, NO LEAKS NOTED IAW AMM 21-51-01. PERFORMED OPS CHECK OF THE TAIL COMPARTMENT OVERHEAT SENSORS AND ALERTS AND FOUND SATISFACTORY IAW AMM 36-20-02.