N836NK

Part: PA SYSTEM — NOISY (CABIN) · airframe 44,357 hrs · 30,772 cycles

L2 PA ATT ALERT SQUEALS WHEN PRESSED.

Part: MICROPHONE — FAULTY (PA SYSTEM) · airframe 44,314 hrs · 30,748 cycles

PASSENGER ADDRESS SYS FROM COCKPIT ON HANDSET OR AUDIO PANEL, CAPTAIN & FLIGHT OFFICER, INOPERATIVE. R & R PA MIC PREAMP ASSEMBLY SYS, OPERATIONS CHECKED GOOD.

Part: GAUGE — BROKEN (EVAC SLIDE)

EVACUATION SLIDE AT L1, MAIN ENTRY DOOR HAD BROKEN PRESS GAUGE AT TIME OF C CHECK INSPECTION.

Part: TORQUE TUBE — WORN (RUDDER)

UPON REMOVAL OF RUDDER ASSEMBLY, THE TORQUE TUBE ASSEMBLY WAS FOUND TO HAVE PITTING CORROSION & WEAR DAMAGE BEYOND ALLOWABLE LIMITS.

Part: SUPPORT FITTING — CORRODED (TE FLAP) · corrosion level 2

LEFT HAND OTBD TE FLAP SUPPORT FITTING ASSEMBLY & MOUNTING STUDS HAD PITTING CORROSION DAMAGE AT C CHECK INSPECTION BEYOND ALLOWABLE LIMITS.

Part: DOOR FRAME — CRACKED (CARGO DOOR)

DOOR FRAME CRACKED AT AFT DOOR LATCH LOCATION ON LOWER, MID CARGO COMPARTMENT DOOR BEHIND EXISTING REPAIR.

Part: UNKNOWN — UNKNOWN (PA SYSTEM) · airframe 44,296 hrs · 30,737 cycles

CRACKING & STATIC NOISES FROME PA. OPS CHECKED PA IAW AMM 23-20-00, NO CRACKING OR STATIC NOISE, NOTED OPS CHECKED GOOD.

Part: WARNING LIGHT — ILLUMINATED (RT GENERATOR) · airframe 44,196 hrs · 30,681 cycles

RT GENERATOR INOPERATIVE LIGHT CAME ON DURING FLT. COMPLETED QRH STARTED APU TO POWER RT BUSS.

Part: JACKSCREW — WORN (HORIZONTAL STAB) · airframe 43,899 hrs · 30,526 cycles

APPARENT WEAR SPOTS ON HORIZONTAL STAB JACKSCREW ABOVE MID SPAN SUPPORT LT SIDE.

Part: INTERPHONE — MALFUNCTIONED (CABIN) · airframe 43,704 hrs · 30,393 cycles

INTERCOM HARD TO HEAR AT STATIONS R1, RC, R2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,704 hrs · 30,393 cycles

EMERGENECY LIGHT INOPERATIVE, R1 DOOR. REPLACED BATTERIES, OPS CHECK GOOD IAW AMM 33-53-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,704 hrs · 30,393 cycles

EMERGENECY LIGHT INOPERATIVE, R1 DOOR. REPLACED BATTERIES, OPS CHECK GOOD IAW AMM 33-53-01.

Part: AMPLIFIER — INOPERATIVE (PA SYSTEM) · airframe 43,654 hrs · 30,361 cycles

PA SYSTEM INOPERATIVE. R & R PA AMPLIFIER, SYS OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (HYD PUMP) · airframe 43,654 hrs · 30,361 cycles

RIGHT AUXILLARY HYD PUMP CIRCUIT BREAKER OUT UNABLE A/B RESET. CLEANED CONNECTOR ON AUX PUMP RESET BREAKER OPS CHECK GOOD MM 29-00-00. CAPT RMI HEADING FLAG DISPLAYED. CYCLED POWER RMI CAME UP OPS CHECK GOOD MM 34-00-00.

Part: PA SYSTEM — MALFUNCTIONED (CABIN) · airframe 43,654 hrs · 30,361 cycles

WHEN IN FLIGHT, PA EMITS A LOUD SCREECHING NOISE.

Part: HANDSET — MALFUNCTIONED (PA SYSTEM) · airframe 43,637 hrs · 30,352 cycles

PA STATIC/FEEDBACK WHEN USING FWD ATTENDANT HANDSET.

Part: WARNING HORN — MALFUNCTIONED (MLG) · airframe 43,637 hrs · 30,352 cycles

UNABLE TO SILENCE GEAR HORN DURING APPROACH.

Part: PA SYSTEM — INTERMITTENT (CABIN) · airframe 43,592 hrs · 30,328 cycles

INTERFERENCE COMING THROUGH P/A SPEAKER INTERMITTENLY. FEEDBACK THROUGH OUT SPEAKERS IN CABIN.

Part: PA SYSTEM — INOPERATIVE · airframe 43,405 hrs · 30,202 cycles

P/A ADDRESS SYSTEM OVER CABIN SPEAKERS INOP.

Part: CALL CHIME — INOPERATIVE (CABIN) · airframe 43,405 hrs · 30,202 cycles

FWD F/A CALL CHIME TO LOW.

Part: PA SYSTEM — MALFUNCTIONED · airframe 43,405 hrs · 30,202 cycles

FWD F/A CALL CHIME TOO LOW.

Part: PA SYSTEM — INOPERATIVE · airframe 43,405 hrs · 30,302 cycles

P/A ADDRESS SYSTEM OVER CABIN SPEAKERS INOPERATIVE.

Part: PA SYSTEM — INOPERATIVE (CABIN) · airframe 43,371 hrs · 30,185 cycles

PA CHIME SYS FORWARD CABIN INOPERATIVE.

Part: PA SYSTEM — INOPERATIVE (CABIN) · airframe 43,371 hrs · 30,185 cycles

PA CHIME SYS FORWARD CABIN INOPERATIVE.

Part: PA SYSTEM — MALFUNCTIONED · airframe 43,340 hrs · 30,160 cycles

L1, L2 AND RC PA'S NOT WORKING IN AIR. PERFORMED PA CHECK IN ALL STATIONS L1, L2 AND RC DURING FLIGHT AND ON GROUND OPERATIONS WITH SENIOR F/A. OPS CHECKED GOOD FOR CONTINUED SERVICE AMM 23-30-00.

Part: PA SYSTEM — INOPERATIVE (L1 DOOR) · airframe 43,289 hrs · 30,122 cycles

L1 PA NOT WORKING IN THE AIR, PAX COULD NOT HEAR ANNOUNCEMENTS IN CABIN.

Part: PA SYSTEM — INOPERATIVE (L1 DOOR) · airframe 43,289 hrs · 30,122 cycles

L1 DOOR PA NOT WORKING IN THE AIR, PAX COULD NOT HEAR ANNOUNCEMENTS IN CABIN.

Part: PA SYSTEM — INOPERATIVE (CABIN) · airframe 43,277 hrs · 30,111 cycles

L1 F/A PANEL PA NOT WORKING PROPERLY. PAX NOT ABLE TO HEAR ANNOUNCEMENTS DURING FLT.

Part: A/C PACK — OVERHEATED (LEFT) · airframe 43,206 hrs · 30,063 cycles

IMMEDIATELY AFTER TAKE OFF, CABIN TEMP WENT TO FULL HOT LT PACK, SMOKE FILLED CABIN WITH SMOKE DETECTORS ACTIVE.

Part: PA SYSTEM — INOPERATIVE (CABIN) · airframe 43,206 hrs · 30,063 cycles

PA LOW DURING FLIGHT, PAX CAN'T HEAR F/A ANNOUNCEMENTS.

Part: PA SYSTEM — INOPERATIVE (CABIN) · airframe 43,206 hrs · 30,063 cycles

PA LOW DURING FLT, PAX CAN'T HEAR ANNOUNCEMENTS.

Part: LIGHT — BURNED OUT (GALLEY) · airframe 43,154 hrs · 30,029 cycles

EMERGENCY LIGHT OUT IN L1 GALLEY.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 43,122 hrs · 30,008 cycles

DURING SERVICE CHECK, FOUND ROW 23 OVERWING EXIT LIGHTS INOPERATIVE. REPLACED BLOWN FUSE ON LIGHT ASSY AT AFT OVERWING EXIT. OPS CHECKED GOOD MM 33-53-00.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 43,122 hrs · 30,008 cycles

DURING SERVICE CHECK, FOUND ROW 23 OVER WING EXIT LIGHTS INOPERATIVE. REPLACED BLOWN FUSE ON LIGHT ASSY AT AFT OVERWING EXIT OPS CHECKED GOOD IAW AMM 33-53-00.

Part: PA SYSTEM — INOPERATIVE (CABIN) · airframe 43,106 hrs · 29,998 cycles

FWD PA SPEAKER IN GALLEY NOT AUDIBLE.

Part: PA SYSTEM — INOPERATIVE · airframe 43,106 hrs · 29,998 cycles

FWD PA IN GALLEY NOT AUDIABLE:

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 43,078 hrs · 29,980 cycles

CABIN ALTITUDE CLIMBED UNCONTROLLED, DECENDED QRH COMPLETED, CABIN ALT EXCEEDED 12,000 FT, CABIN O2.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 43,078 hrs · 29,980 cycles

CABIN ALTITUDE CLIMBED UNCONTROLLED. DECESENDED, QRH COMPLETED. CABIN ALTITUDE EXCEEDED 12,000 FT CABIN 02 DEPLOYED.

Part: UNKNOWN — LEAKING (FUEL SYSTEM) · airframe 43,037 hrs · 29,950 cycles

WHEN OPENING AFT STAIRS, A PUDDLE OF FUEL ON GROUND, SUSPECT APU LEAK.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,037 hrs · 29,950 cycles

WHEN OPENING AFT STAIRS A PUDDLE OF FUEL ON THE GROUND.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR) · airframe 42,965 hrs · 29,880 cycles

FWD CARGO DOOR LIGHT CAME ON DURING TAKE OFF ROLL.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR) · airframe 42,965 hrs · 29,880 cycles

FWD CARGO DOOR LIGHT CAME ON DURING TAKE OFF ROLL.

Part: PA SYSTEM — INOPERATIVE (CABIN) · airframe 42,949 hrs · 29,865 cycles

PA INOPERATIVE IN FLIGHT.

Part: PA SYSTEM — WEAK (CABIN) · airframe 42,926 hrs · 29,842 cycles

PA NOT WORKING IN FLIGHT, NOT LOUD ENOUGH.

Part: PA SYSTEM — INOPERATIVE · airframe 42,926 hrs · 29,842 cycles

PA NOT WORKIN IN FLIGHT,NOT LOUD ENOUGH.

Part: PA SYSTEM — OUT OF ADJUST · airframe 42,926 hrs · 29,842 cycles

PA SYSTEM IN CABIN NOT LOUD ENOUGH FOR F/A'S AND PAX TO HEAR.

Part: PA SYSTEM — WEAK (CABIN) · airframe 42,926 hrs · 29,842 cycles

PA SYSTEM IN CABIN NOT LOUD ENOUGH FOR F/A'S & PAX TO HEAR.

Part: PA SYSTEM — INOPERATIVE · airframe 42,865 hrs · 29,791 cycles

L-1 PA NOT LOUD ENOUGH IN CABIN WHEN APU IS ON.

Part: PA SYSTEM — WEAK (CABIN) · airframe 42,865 hrs · 29,791 cycles

L1 P/A NOT LOUD ENOUGH IN CABIN WHEN APU IS ON.

Part: PA SYSTEM — INOPERATIVE (CABIN) · airframe 42,865 hrs · 29,791 cycles

L1 PA CABIN NOT ABLE TO HEAR ANNOUNCEMENTS.

Part: CABIN PRESSURE — FAILED (CABIN) · airframe 42,865 hrs · 29,791 cycles

UNABLE TO GET PRESSURIZATION STABILIZED IN CRUISE, CABIN WOULD CLIMB ON DESCENT & OR- 500PM IN MANUAL. CAUSED 1 PILOT TO BE COMPLETELY DEVOTED TO CONTROLLING THE PRESS CABIN WAS ALMOST TOTALLY UNCONTROLLABLE DURING DESCENT.

Part: CABIN PRESSURE — UNSTABLE · airframe 42,865 hrs · 29,791 cycles

UNABLE TO GET PRESSURE STABILIZED IN CRUISE. CABIN WOULD CLIMB OR DESCEND ON OR -500 FPM IN MANUAL CAUSES 1 PILOT TO BE COMPLETELY DEVOTED TO CONTROLLING THE PRESSURE CABIN WAS ALMOST TOTALLY UNCONTROLLABLE DURING DESCENT.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHTS) · airframe 42,857 hrs · 29,788 cycles

EMERGENCY LIGHTS INOPERTIVE FROM ROWS 9 THROUGH 12, AFT OVERWING EXIT IDENTIFIERS AND TAIL ACCESSORY COMPARTMENT. TROUBLESHOT EMERGENCY LIGHTS AND FOUND WEAK BATTERIES . REPLACED BATTERIES IAW MM 33-53-00.

Part: ENGINE — BIRD INGESTION (LEFT) · airframe 42,857 hrs · 29,786 cycles

ON TAKEOFF, HEARD A LOUD NOISE, UPON LANDING, DISCOVERED NOSE OF ACFT ENCOUNTERED BIRD STRIKE. LT ENGINE INGESTED BIRD CAUSING DAMAGE TO N1 COMPRESSOR BLADES.

Part: COMPRESSOR — DAMAGED (LT ENGINE) · airframe 42,857 hrs · 29,786 cycles

AFTER TAKEOFF, HEARD A LOUD POP. ON LANDING DISCOVERED NOSE OF ACFT ENCOUNTERED BIRD STRIKE. LEFT ENGINE INGESTED BIRD CAUSING DAMAGE TO 3 N1 COMPRESSOR BLADES.

Part: UNKNOWN — UNKNOWN (CABIN PRESSURE) · airframe 42,842 hrs · 29,779 cycles

CABIN PRESSURE LOST AT FL330, CABIN WOULD NOT MAINTAIN PRESSURE INIATED EMERGENCY DESCENT.

Part: PA SYSTEM — INOPERATIVE (L1 DOOR) · airframe 42,813 hrs · 29,767 cycles

L1 PA AUDIO NOT LOUD ENOUGH.

Part: PA SYSTEM — WEAK (CABIN)

L1 PA AUDIO NOT LOUD ENOUGH.

Part: PA SYSTEM — WEAK (CABIN) · airframe 42,813 hrs · 29,767 cycles

L1 PA AUDIO NOT LOUD ENOUGH.

Part: HANDSET — INOPERATIVE (CABIN) · airframe 42,813 hrs · 29,767 cycles

FWD F/A HANDSET DOES RESET WHEN RETURNED TO CRADDLE CALL AURAL ALERT DOES NOT WORK.

Part: HANDSET — MALFUNCTIONED · airframe 42,813 hrs · 29,767 cycles

FWD F/A HAND SET DOES NOT RESET WHEN RETURNED TO CRADDLE, CALL AURAL ALERT DOES NOT WORK.

Part: WARNING HORN — MALFUNCTIONED (CABIN) · airframe 42,794 hrs · 29,755 cycles

F/A CALL AURAL ALERT VERY FAINT IN FLIGHT UNABLE TO HEAR. LIGHT OPS NORMAL.

Part: PA SYSTEM — INTERMITTENT (CABIN) · airframe 42,794 hrs · 29,755 cycles

F/A'S PA INTERMITTENT.

Part: PA SYSTEM — INTERMITTENT (CABIN) · airframe 42,794 hrs · 29,755 cycles

F/A'S PA INTERMITTENT.

Part: PA SYSTEM — INTERMITTENT (CABIN) · airframe 42,794 hrs · 29,755 cycles

F/A'S PA INTERMITTENT.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 42,794 hrs · 29,755 cycles

EMERGENCY DESCENT FROM FL340 DUE TO RISING CABIN ALTITUDE OF ABOVE 10K FLOW LIGHT AND CABIN ALT MASTER WARNING ON. CREW COMPLIED WITH MEMORY/QRH ITEMS, RESUMED FLIGHT IN MANUAL.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 42,794 hrs · 29,755 cycles

EMERGENCY DESCENT FROM FL 340 DUE TO RISING CABIN ALTITUDE OF ABOVE 10K, FLOW LIGHT AND CABIN ALT MASTER WARNING ON. CREW COMPLIED WITH MEMORY/QRM ITEMS, RESUMED FLIGHT IN MANUAL.

Part: PA SYSTEM — MALFUNCTIONED (CABIN) · airframe 42,640 hrs · 29,654 cycles

AFT F/A PA CHIMES FLIGHT DECK INTERMITTENTLLY.

Part: HANDSET — INTERMITTENT (CABIN) · airframe 42,616 hrs · 29,632 cycles

F/A HANDSET WORKS INTERMITTENTLY AT L2 AND RC HANDSETS F/A TO F/A AND F/A TO PILOTS WORK.

Part: INTERPHONE — INTERMITTENT (CABIN) · airframe 42,626 hrs · 29,642 cycles

INTERPHONE BETWEEN FLIGHT DECK AND CABIN IS INTERMITTENT.

Part: INTERPHONE — INTERMITTENT (CABIN) · airframe 42,626 hrs · 29,642 cycles

INTERPHONE BETWEEN FLIGHT DECK AND CABIN IS INTERMITTENT.

Part: PA SYSTEM — INTERMITTENT (CABIN) · airframe 42,616 hrs · 29,632 cycles

P/A WORKS INTERMITTENTLY AT L-2 AND RC HANDSETS F/A TO F/A AND F/A TO FLT CREW.

Part: HANDSET — INOPERATIVE (CABIN) · airframe 42,526 hrs · 29,570 cycles

L2 HAND SET INOPERATIVE,

Part: HANDSET — INOPERATIVE · airframe 42,526 hrs · 29,570 cycles

L2 HAND SET INOPERATIVE.

Part: INTERPHONE — INOPERATIVE (CABIN) · airframe 42,371 hrs · 29,462 cycles

L2 INTERPHONE NOT WORKING WHEN TRYING TO CALL L-I F/A.

Part: INTERPHONE — INOPERATIVE (CABIN) · airframe 42,371 hrs · 29,462 cycles

L2 INTERPHONE NOT WORKING WHEN TRYING TO CALL L1 F/A.

Part: OIL SYSTEM — EMPTY (LT ENGINE) · airframe 42,371 hrs · 29,462 cycles

DESCENDING THROUGH 10,00 FT THE LT ENGINE LOW PRESSURE LIGHT ILLUMINATED, THE LT ENGINE OIL QTY SHOWED ZERO QUARTS. SHUTDOWN THE ENGINE IAW OUR CHECK LIST.

Part: OIL SYSTEM — EMPTY (LT ENGINE) · airframe 42,371 hrs · 29,462 cycles

DESCENDING THROUGH 10,000 FT, LEFT ENGINE OIL PRESSURE LOW LIGHT ILLUMINATED. THE LT ENGINE OIL QTY SHOWED ZERO QUARTS. SHUTDOWN THE LT ENGINE IAW THE CHECK LIST.

Part: SELECTOR PANEL — WRONG PART (OBSERVER AUDIO) · airframe 42,371 hrs · 29,462 cycles

WITH INT SELECTED WITH HOT MIKE FWD F/A CALL ON HANDSET CAN TALK WITHOUT USING COCKPIT HANDSET. FOUND OBSERVER AUDIO SELECT PANEL NOT TO BE EFFECTIVE FOR ACFT. R & R OBSERVERS AUDIO SELECT PANEL AND OPS CHECKED GOOD IAW MM 23-50-02.

Part: PA SYSTEM — INTERMITTENT (CABIN)

ACFT ARRIVED WITH TWO LOG ITEMS BOTH AFT PA INTERMITTENT, FORWARD INTERCOM TO FLIGHT DECK IS INTERMITTENT.

Part: PA SYSTEM — INTERMITTENT

ACFT ARRIVED WITH 2 LOG ITEMS BOTH AFT PA INTERMITTENT, FORWARD INTERCOM TO FLIGHT DECK IS INTERMITTENT.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 42,253 hrs · 29,365 cycles

LOST CABIN AT FL 320 LOCKED OUTFLOW VALVE AND MANAGED TO CABIN FROM EXCEEDING 10,000 FT. ACCOMPLISHED EMERGENCY DESCENT.

Part: BATTERY — FAILED (ZONE 100) · airframe 42,227 hrs · 29,344 cycles

DURING WALK AROUND, FOUND SMOKE COMING OUT OF BATTERY VENT PORTS. MX R & R BOTH SHIPS BATTERIES, BATTERY CHARGER AND THERMAL SENSORS IAW AMM 24-30-01,02,00.

Part: WARNING BELL — WEAK · airframe 42,166 hrs · 29,301 cycles

COCKPIT TO CABIN CALL BELL VERY WEAK IN FLIGHT CANNOT HEAR. TURNING SEAT BELT SIGN ON IN FLIGHT, VERY WEAK CANNOT HEAR.

Part: EXTINGUISHER — EMPTY · airframe 42,166 hrs · 29,301 cycles

ON TAXI OUT F/A REPORTED THE HALON FIRE EXTINGUISHER WAS EMPTY, ACFT RETURNED TO THE BLOCK WHERE MX ENTERED THE DISCREPANCY ON DMI IAW MEL 26-9 CAT "D" AC WAS DISPATCHED FOR FLIGHT.

Part: WARNING LIGHT — ILLUMINATED (CSD) · airframe 42,153 hrs · 29,290 cycles

RIGHT CSD LOW OIL LIGHT ON POWER APPLICATION FOR TAKEOFF, ABORTED, RETURN TO RAMP.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 42,153 hrs · 29,290 cycles

DURING TEST OF THE EMERGENCY LIGHTS THE COCKPIT FLOOD LIGHTS DID NOT ILLUMINATE.

Part: PA SYSTEM — MALFUNCTIONED · airframe 41,607 hrs · 28,946 cycles

F/A CALL BUTTON IN COCKPIT INOPERATIVE, CALL BUTTON FROM F/A STATION TO COCKPIT OPS NORMAL. CABIN P/A INOPERATIVE, COCKPIT P/A NORMAL. ATTENDANT TO ATTENDANT CALL BUTTON INOPERATIVE, LIGHT WORKS NORMAL.

Part: PA SYSTEM — INOPERATIVE (CABIN) · airframe 41,607 hrs · 28,946 cycles

CABIN PA SYSTEM INOPERATIVE, COCKPIT PA OPS NORMAL.

Part: CABIN PRESSURE — MALFUNCTIONED

DURING DESENT AT APPROX 3,000 AGL, ACFT DEPRESSURISED STANDBY, LOCKOUT LIGHT ILLUMINATED.

Part: AMPLIFIER — MALFUNCTIONED (PA SYSTEM) · airframe 41,541 hrs · 28,910 cycles

BOTH AUDIO PANELS HAVE BLED OVER WHEN P/A IS USED BY F/A. R & R P/A AMPLIFIER IAW AMM 23-30-01.

Part: EPR SYSTEM — INOPERATIVE (ENGINE) · airframe 41,448 hrs · 28,842 cycles

LEFT EPR WILL NOT GO ABOVE 1.63 ON TAKEOFF.

Part: ENGINE — OVERTEMP (NR 1) · airframe 41,378 hrs · 28,803 cycles

ON TAKEOFF, NR 1 ENGINE TEMP AT 660 DEGRESS C, IN CLIMB TEMPERATURE AT 635 DEGREES C. ACFT RETURNED TO AIRPORT OF ORIGIN WHERE A ENGINE REPLACEMENT WAS ACCOMPLISHED AND THE ACFT WAS RETURNED TO SERVICE.

Part: INDICATOR — FALSE INDICATION (EPR) · airframe 41,307 hrs · 28,746 cycles

NR1 EPR AND NR2 EPR HAVE ERRONEOUS READING, NR1 1.47, NR2 2.09 IN CRUISE AT 23.0' NOTE:A/T INOP AC RADIO INTO DISPATCH AND REPORTED THE DISCREPANCY; MOC AND DISPATCH DEVERTED THE AC BACK TO DEPARTURE, WHERE MX CAN BE PERFORMED.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 41,305 hrs · 28,743 cycles

DURING CLIMB OUT OF 20K, RT ENG WITH EPR GAGE MATCHED, NR1, EGT, N2 & FUEL FLOW LOW. WHEN NR1 IS MATCHED EPR GAGE PEGGED OUT. ACFT DEVERTED WHERE MX IS IN PROCESS OF TROUBLESHOOTING RT ENGINE EPR SYS.

Part: PRESSURE SWITCH — DEFECTIVE (RT ENGINE) · airframe 41,270 hrs · 28,721 cycles

AFTER TAKEOFF AND CLIMBOUT FROM SAL RT ENGINE FILTER CLOGGED LIGHT ILLUMINATED, AC DIVERTED TO GUATEMALA. UPON PARKING MAINTENANCE REMOVED THE MAIN OIL FILTER ASSY AND INSPECTED FOR FOD, NONE WAS FOUND. MAINTENANCE REPLACED THE RT ENG MAIN OIL FILTER PER MD 80 AMM 79-20-06 AND 79-35-01 AND DETERMINED THE ENGINE DIFFERENTIAL OIL PRESSURE INDICATION SYSTEM WAS AT FAULT. MOC ISSUED DMI M79JN-4632 AC WAS RELEASED PER MEL 79-5. AC 836RA REPOSITIONED TO IWA, UPON ARRIVAL RT ENGINE DIFFERENTIAL OIL PRESS SWITCH WAS REPLACED PER MD 80 AMM 79-35-01 DMI WAS CLEARED. AC OPERATIONS WERE CONDUCTED 6/29/2011 NO FURTHER CREW REPORTS WERE RECEIVED AT THIS TIME.

Part: SHAFT — FAILED (HYD PUMP)

AFTER TAKEOFF, NR 1 ENG HYD PRESSURE LOW; ACFT RETURNED TO DEPARTURE, MX TROUBLESHOT TO LT ENGINE HYD PUMP SHAFT FAILED. R & R LEFT HYD PUMP AND CASE DRAIN FILTER IAW AMM 29-10-05 AND 29-10-14.

Part: PA SYSTEM — INTERMITTENT (CABIN) · airframe 40,716 hrs · 28,352 cycles

L-1 PA SYS-CAN NOT HEAR, INTERMITTENT FROM ALL STA SYS DEFERED AND ACFT WAS RELEASED UNDER MEL 23-6-1.

Part: BUTTON — BROKEN (F/A CALL)

COCKPIT F/A CALL BUTTON BROKEN.

Part: PA SYSTEM — WEAK (FLT ATTENDANT)

AFT F/A POSITION PA WEAK.

Part: PA SYSTEM — INOPERATIVE

COCKPIT TO CABIN PA INOP.

Part: PA SYSTEM — INTERMITTENT (CABIN) · airframe 40,165 hrs · 28,043 cycles

COCKPIT PA CUTS OUT WHEN IN USE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 39,651 hrs · 27,813 cycles

AFTER TAKEOFF, F/A REPORTED SMOKE IN THE AFT CABIN. RETURNING TO DEPARTURE UPON LANDING THE ACFT WEIGHTED 150,000 LBS MAKING IT AN OVERWEIGHT LANDING.

Part: PA SYSTEM — INOPERATIVE (CABIN) · airframe 39,553 hrs · 27,722 cycles

P.A. INOPERATIVE ALL STATIONS.

Part: PA SYSTEM — INOPERATIVE · airframe 39,553 hrs · 27,722 cycles

PA WAS INOP IN ALL STATIONS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,452 hrs · 27,676 cycles

EXTERIOR EMERGENCY LIGHTS WILL NOT COME ON.

Part: INTERPHONE — INOPERATIVE · airframe 39,452 hrs · 27,676 cycles

INTERPHONE BETWEEN COCKPIT AND CABIN INOPERATIVE AND BETWEEN FRONT AND REAR CABIN.

Part: PA SYSTEM — INOPERATIVE · airframe 39,405 hrs · 27,655 cycles

PA SYSTEM INOPERATIVE.

Part: INTERPHONE — INTERMITTENT

COCKPIT TO CABIN INTERPHONE INTERMITTENT.

Part: PA SYSTEM — MALFUNCTIONED (ZONE 100)

CAPTAIN P/A INAUDIBLE IN FLIGHT.

Part: PA SYSTEM — INOPERATIVE · airframe 39,385 hrs · 27,647 cycles

F/A PA SYS IS NOT WORKING IN FLIGHT.

Part: PA SYSTEM — INOPERATIVE · airframe 39,304 hrs · 27,610 cycles

PA NOT WORKING PROPERLY IN FLIGHT BUT WORKING ON THE GROUND. UNABLE TO MAKE ANNOUNCEMENTS, VOLUME TOO LOW IN ALL HANDSETS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,111 hrs · 27,532 cycles

POSTFLIGHT FOUND EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,869 hrs · 27,442 cycles

EMERGENCY EXIT LIGHT AT FWD EXITS DID NOT ILLUMINATE WHEN TESTED. ALSO, SOME POSITIONS WITHIN THE CABIN DID NOT ILLUMINATE.

Part: WINDOW — STUCK (COCKPIT) · airframe 38,430 hrs · 27,293 cycles

UNABLE TO OPEN CAPTAIN'S WINDOW.

Part: LINE — LEAKING (RT ENGINE) · airframe 38,381 hrs · 27,279 cycles

DURING CRUISE , RT ENGINE OIL QUANTITY DROPPED TO ZERO , SHORTLY AFTER THE RIGHT OIL PRESSURE DROPPED BELLOW 35 PSI AND OIL TEMPERATURE ROSE , INFLIGHT RIGHT ENGINE WAS SHUTDOWN BY CREW. AIRCRAFT LANDED SAFELY , MAINTENANCE FOUND AN OIL LINE LEAKING FROM RIGHT ENGINE OIL PRESSURE TRANSMITTER INDICATOR TO LOW OIL PRESSURE WARNING SWITCH.

Part: SENSOR — DIRTY (ZONE 200) · airframe 38,173 hrs · 27,210 cycles

DURING CLIMB , TAIL COMPARTMENT HIGH LIGHT ILLUMINATED.

Part: UNKNOWN — UNKNOWN (CABIN PRESSURE) · airframe 37,350 hrs · 26,896 cycles

UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF.

Part: LINE — CLOGGED (PT2)

DURING TAKEOFF ROLL, AFTER 1.4 EPR CHECK & AUTOTHROTTLE ENGAGEMENT ENGINE NR 2 EPR INDICATION WENT TO 1.75 AND REMAINED FIXED. AUTOTHROTTLE DISENGAGED AND WOULD NOT RE-ENGAGED. ABORTED T/O AT 65 KIAS & RETURNED TO GATE. FOUND PT2 LINE CLOGGED. CLEANED PT2 LINE AND REPLACED ENGINE FUEL FILTERS. SYSTEM TESTED NORMAL DURING TEST FLIGHT.

Part: COMPUTER — OUT OF ADJUST

ABORTED TAKEOFF DUE TAKEOFF WARNING. FOUND TAKEOFF CONDITION COMPUTER SETTING NOT SET CORRECTLY.

Part: CSD — OVERTEMP (RT ENGINE)

AT TOC RIGHT CSD TEMP RISE INCREASED TO RED ARC.

Part: FCU — LEAKING (APU)

AFTER ENGINE STARTING AND DURING TAXI A STRONG ODOR OF FUEL IN THE AIRCRAFT CABIN WAS DETECTED FOR THESE REASON THE AIRCRAFT RETURNED TO THE BLOCK. LOG PAGE 38680 - MIA LINE MTX INSPECTED THE AIRCRAFT AND FOUND THAT THERE WAS FUEL LEAKING OUT OF THE APU FUEL DRAIN, SHUT DOWN THE APU AND ASSIGNED TO DMI M49JL27-3661. LOG PAGE 38687 - MIA LINE MTX REMOVED AND REPLACED THE APU FUEL CONTROL, OPS CHECKED NORMAL.

Part: DISPLAY — MALFUNCTIONED (ENGINE)

DTW - ABORTED TAKEOFF, LEFT ENGINE EPR STUCK AT 1.71 DURING TAKEOFF, CAPTAIN CALLED FOR SET FLEX POWER, F/O PUSHED THROTTLES UP EPR STAYED AT 1.71, N2 FLASHING AT 010 OR 001 ABORTED TAKEOFF AT 70 KNOTS, AIRCRAFT TAIL SWAP WITH N811NK. REMOVED AND REPLACED ENGINE DISPLAY PANEL, OPS CHECK GOOD. (M)

Part: PUSH-PULL ROD — DISCONNECTED (NR 1 THOTTLE)

AFTER INITIAL LEVEL OFF, THE NR 1 ENGINE AT NEAR CLIMB POWER STOPPED RESPONDING TO AUTO-THROTTLE POWER REDUCTION, THROTTLES BECAME SPLIT AND A/T DISCONNECTED. FULL THROTTLE GAVE NO INCREASE IN POWER AND FULL IDLE WOULD DROP NO LOWER THAN 1.64 EPR, ENGINE WAS SHUT-DOWN ON APPROACH WITH EPR AT 1.53 AND ABOUT 9000 FEET. FOUND NR 1 ENGINE THROTTLE PUSH-PULL CONTROL ROD DISCONNECTED AT AFT CONTROL SECTOR, RE-CONNECTED AS REQUIRED AND RIGGED THROTTLE SYSTEM NR 1. BOTH ENGINE PART POWR STOPS WERE INSTALLED AND THEN STOWED, RUN-UP AND TRIM AS REQUIRED. GROUND CHECKS GOOD. (M)

Part: SMOKE — DETECTED (CABIN)

DURING TAXI, AFT FLIGHT ATTENDANT REPORTED SMOKE IN THE AFT CABIN, ENTIRE AIRCRAFT SMELLED LIKE AN OVERHEATED PACK, GATE RETURN. OPS CHECKED RT AUTO-TEMP. NO DEFECTS NOTED, OPS CHECKED GOOD. (K)

Part: LANYARD — MISROUTED (ESCAPE SLIDE)

R1 SLIDE GIRT BAR SLIDE PACK LANYARD NOT ROUTED PROPERLY. RE-ROUTED R1 SLIDE GIRT BAR LANYARD.

Part: A/C PACK — MALFUNCTIONED (RIGHT)

CABIN FILLED WITH SMOKE WHEN APU AIR WAS TURNED ON. FOUND RT PACK, DID AN AUTO SHUTDOWN. WHEN RT PACK COOLED DOWN, RAN LT AND RT PACK FOR 90 MINUTES. NO SMOKE AT THIS TIME. CHANGED LT AND RT COALESCER SOCKS FOR COMPANY CONV. WORK DOWN IAW MM 21-20-02. OPS AND LEAK CHECK GOOD AT THIS TIME.

Part: PROXIMITY SWITCH — FAILED (NLG)

MCO - FLT 1862 - FOUND NOSE GEAR RED LIGHT ILLUMINATED SEVERAL TIMES DURING FLIGHT. DUE TO PROXIMITY SWITCH ELECTRONIC UNIT FAILURE, REMOVED AND REPLACED PSEU. (M)

Part: RHEOSTAT — BURNED OUT (MAP LIGHT)

ORD - FLT 1108 - AFTER LEVELING OFF AT 330, SMELLED SMOKE. NOTICED IT IN THE OVERHEAD MAP LIGHT. I WENT TO TURN THE LIGHT UP AND THE REOSTAT WAS VERY HOT TO THE TOUCH, PULLED THE C/B. REMOVED AND REPLACED CAPTAINS OVERHEAD LIGHT RHEOSTAT. (M)

Part: SLIDE — DEPLOYED (L2 DOOR)

L2 DOOR SLIDE PACK CABLE FOR AUTO/MANUAL DEPLOY NOT HOOKED UP. REMOVED COVER AND REINSTALLED CABLE OT LANYARD AND REINSTALLED COVER. (M)

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 30,285 hrs · 23,913 cycles

R1 SLIDE FELL OFF DOOR WHEN OPENED BY CATERING. REINSTALLED SLIDE.

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FTW - FOUND MAIN C/B STATION 389 TO STATION 465 LBL 24 INCHES TO 44 INCHES FLOOR PANEL HAS CRACKED ON EDGES/SEVERAL INSERTS DAMAGED. FABRICATED FLOOR PANEL. (M)

Part: FLASHLIGHT — MISSING (AFT LAVATORY) · airframe 30,186 hrs · 23,873 cycles

RT AFT LAV AFT SIDE MISSING 2 EA EMERGENCY LIGHTS. RT AFT LAV EMERGENCY FLASHLIGHTS ARE INSTALLED.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 30,186 hrs · 23,873 cycles

MAIN CB STA 446 TO 466 RT SIDE MID FLOOR PANEL HAS CRACKED/DAMAGE ON EDGE.

Part: LIGHT — MISSING (CABIN) · airframe 30,186 hrs · 23,873 cycles

SEVERAL EMERGENCY EXIT IDENTIFIERS LIGHTS MISSING. INSTALLED 4 EA NEW EMERGENCY EXIT IDENTIFIERS.

Part: FLOOR PANEL — CRACKED (FUSELAGE)

MAIN CB STA 1079 TO STA1136, LBL 24 INCH TO 44 INCHES FLOOR PANEL HAS CRACKED ON EDGE/ SEVERAL INSERTS CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND RIGHT INBOARD SEAT TRACK STATION 836-1036 CORRODED AND GOUGED. REMOVED TRACK RIGHT INBOARD STATION 836-1036. LOCATED AND DRILLED NEW TRACK. LOCATED AND DRILLED SPLICES. INSTALLED NEW TRACKS AND THREE SPLICES. (M)

Part: FLOOR PANEL — DEBONDED (FUSELAGE)

FTW - FOUND MAIN CABIN FLOOR PANEL LEFT OUTBOARD FS 1250-1309 HAT CHANNEL ON BOTTOM IS DISBONDED ON FORWARD END AND CRACKED AT BOTH ENDS. REPAIRED DAMAGED HAT CHANNEL. BONDED FORWARD END OF HAT CHANNEL. (M)

Part: ACOUSTIC LINER — BOWED (THRUST REVERSER) · airframe 30,186 hrs · 23,873 cycles

NR 2 T/R, SN 49785 ACOUSTIC LINER BOWED. REMOVED NR 2 T/R INSTALLED NR 2 T/R.

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD STATON 826-864 RIGHT CENTER AFT INBOARD CORNER IS CRACKED ON LOWER SURFACE. FABRICATED FLOORBOARD. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

FTW - FOUND CABIN CENTER FLOORBOARD STATION 579-617 HAS PEELING FIBERGLASS. FABRICATED CABIN CENTER FLOORBOARD. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

FTW - FOUND CABIN CENTER FLOORBOARD STATION 541-579 HAS PEELING FIBERGLASS. DAMAGED INSERTS. FABRICATED NEW FLOORBOARD. (M)

Part: FLOORBOARD — PUNCTURED (FUSELAGE)

FTW - FOUND CENTER CABIN FLOORBOARD STATION 256-313, CREASED ALONG UPPER SKIN, PUNCTURED. FABRICATED NEW FLOORBOARD. (M)

Part: FLOOR PANEL — DEBONDED (FUSELAGE)

FTW - FOUND MAIN C/B METALLIC PANEL RIGHT SIDE OUTBOARD HAS DISBONDED AT HATS CHANNEL, RUB STRIP, BARE METAL AT HAT SECTON STATON 1079-1117, 541-617, 826-927. BONDED RIGHT SIDE OUTBOARD AT HAT CHANNEL. (M)

Part: FLOORBEAM — CRACKED (FUSELAGE)

FTW - FOUND FLOOR SUPPORT CRACKED AT FS 905 36 INCHES LBL. REMOVED CRACKED FLOOR SUPPORT. LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FTW - FOUND FORWARD CABIN STATION 200 TO 160 LBL 55 INCH SUPPORT FLOOR CORRODED. REMOVED FLOOR SUPPORT. FABRICATED AND LOCATED HOLES. INSTALLED FLOOR SUPPORT. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

FTW - FOUND CABIN RBL 55, SUBFLOOR WEB FROM STA 1136 TO 1212 IS CORRODED. FOUND STATION 1150, 1185, AND 1205 TO BE OUT OF LIMITS. FABRICATED TWO SECTION CUSP WEBS. INSTALLED CUSP WEB STATION 1098-1250. (M)

Part: SPLASH GUARD — BENT (NOSE WHEEL)

FOUND NOSE WHEEL SPLASH GUARD RIGHT BENT AND SEPARATING AT RUBBER SEAL LEFT BENT AND RUST ON RUB PLATE. REMOVED RUB PLATES. FABRICATE NEW NOSE WHEEL RUB PLATES. INSTALLED NOSE WHEEL RUB PLATES. (M)

Part: FLOORBOARD — DEBONDED (FS)

FTW - FOUND CABIN FLOORBOARD STATION 769-826 RIGHT OUTBOARD HAT CHANNEL DEBONDED. BONDED THE DISBONDED HAT CHANNEL. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FTW - FOUND MAIN C/B STATION 1250 TO STATION 1309 LBL 24 TO 44 INCHES FLOOR PANEL HAS SOFT/MUSHEY SEVERAL INSERTS CORRODED. FABRICATED FLOORBOARD. (M)

Part: FLOORBOARD — DEBONDED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD STATION 1174-1250 RIGHT OUTBOARD STRIPS DEBONDED. REBONDED STRIPS ON CABIN FLOORBOARD. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FTW - FOUND MAIN C/B STATION 1155 TO STATION 1250 LBL 24 INCHES TO 44 INCHES FLOOR PANEL HAS BROKEN HALF/SEVERAL INSERTS CORRODED. FABRICATED NEW FLOORBOARD. (M)

Part: FLOOR PANEL — DEBONDED (FUSELAGE)

FTW - FOUND MAIN C/B LEFT SIDE OUTBOARD METALLIC PANEL HAS DISBONDED AT HAT CHANNELS/RUB STRIPS, BARE METAL AT HAT CHANNEL, STATION 256-313, 313-398, 826-923, 923-1003, 1003-1079. REBONDED HAT CHANNEL. (M)

Part: FLOORBOARD — DETERIORATED (FUSELAGE)

FTW - FOUND MAIN C/B STATION 674 TO 693 MID RIGHT SIDE HAS DETERIORTATED ON TOP PANEL EDGE FILLER. FABRICATED FLOORBOARD. (M0

Part: CHANNEL — CRACKED (FLOORBOARD)

FTW - FOUND CABIN FLOORBOARD STATION 389-465 LEFT OUTBOARD HAT CHANNEL CRACKED AND STRIP DEBONDED. REMOVED DAMAGE ON HAT CHANNEL. FABRICATED SPLICE AND HAT CHANNEL. INSTALLED NEW PIECES. (M)

Part: FLOOR PANEL — DEBONDED (FUSLAGE)

FTW - FOUND MAIN C/B STATION 1155 TO 1250 METALLIC PANEL LEFT SIDE OUTBOARD HAS DISBONDED AT RUB STRIP/HAT CHANNEL. REBONDED RUBSTRIP HAT CHANNEL. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - FOUND MAIN C/B STATION 256 TO STATION 313 LBL 24 INCHES TO 44 INCHES FLOOR PANEL HAS CRACKED/DAMAGED ON EDGE. FABRICATED FLOORBOARD. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FOUND MAIN C/B STATION 1174 TO STATION 1193 RIGHT SIDE MID HAS CRACKS AND DAMAGED ON EDGE. FABRICATED FLOORBOARD. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD STATION 160-200 LEFT INBOARD NO EDGE FILLER AND COVERING SPLINTERED. FABRICTED NEW CABIN FLOORBOARD. (M)

Part: FLOORBOARD — TORN (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD STATION 150-160 RIGHT OUTBOARD COVERING TORN. FABRICATED NEW CABIN FLOORBOARD. (M)

Part: FLOORBOARD — DEBONDED (FUSELAGE)

FOUND CABIN FLOORBOARD STATION 693-769 RIGHT OUTBOARD STRIPS DEBONDED. REBONDED STRIPS ON CABIN FLOORBOARD. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD STATION 160-200 CENTER EDGE BROKE. COVER TORN CORE EXPOSED AND CORROSION ON INSERTS. FABRICATED FLOORBOARD. (M)

Part: FLOORBOARD — PEELING (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD STATION 150-160 LEFT OUTBOARD COVERING PEELING. FABRICATED NEW CABIN FLOORBOARD. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FOUND MAIN C/B STATION 1079 TO STATION 1117 RIGHT SIDE MID FLOOR PANEL HAS CRACKED/DAMAGED CORNER AND EDGE. FABRICATED FLOOR PANEL. (M)

Part: FLOORBOARD — DENTED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD STATION 160-200 LEFT OUTBOARD DENTED, PUNCTURED, CORE CRUSHED, BROKEN INSERTS, COVERING PEELING AND DELAMINATED. FABRICATED FLOORBOARD. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FTW - FOUND MAIN C/B STATION 693 TO STATION 769 LEFT SIDE OUTBOARD METALLIC PANEL CRACKED AT HAT SECTION, DISBONDED AT RUB STRIPS. RE-BONDED RUB STRIP. REMOVED HAT CHANNEL. INSTALLED HAT CHANNEL. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD STATION 617-693 RIGHT OUTBOARD STRIPS DEBONDED, HAT CHANNEL DEBONDED, FLOORBOARD CRACKED. FABRICATED NEW BOARD. (M)

Part: FLOOR PANEL — DEBONDED (FUSELAGE)

FOUND MAIN C/B LEFT SIDE OUTBOARD METALLIC PANEL BARE METAL AT HAT CHANNEL DISBONDED AT RUB STRIPS ONE MISSING RUB STRIP STATION 617-693. FABRICATED NEW FLOOR PANEL. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FTW - FUOND MAIN C/B CENTER FLOOR PANEL STATOIN 886-946 TWO RIVETS PULL THROUGH, CRACKED AT EXPANSION CHANNEL BOTH SIDES AND PUNCTURE HOLE. FABRICATED FLOOR PANEL. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - FOUND MAIN C/B STATION 617 TO STATION 541 LBL 24 INCHES TO 44 INCHES FLOOR PANEL HAS CRACKED/DAMAGED FORWARD AND AFT EDGE. FABRICATED NEW FLOORBOARD. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FTW - FOUND MAIN C/B LEFT SIDE OUTBOARD METALLIC PANEL STATION 541 TO 617 HAS CRACKED AND DAMAGED AT HAT CHANNEL TWO RUB STRIP MISSING ONE DISBONDED. REMOVED HAT CHANNEL. INSTALLED HAT CHANNEL. (M)

Part: FLOORBOARD — CRACKED (FUSELAGE)

FTW - FOUND MAIN C/B STATON 1079 TO STATOIN 1155 LEFT SIDE O/B METALLIC PANEL HAS CRACKED/DISBONDED AT HAT CHANNEL. REPAIRED MAIN CABIN FLOORBOARD. (M)

Part: FLOORBOARD — CORRODED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD STATION 160-180 RIGHT INBOARD NO EDGE FILLER AND INSERTS CORRODED. FABRICATED FLOORBOARD. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FOUND CABIN FLOORBOARD STATION 150-160 CENTER INSERT BROKEN AND CORE DAMAGED. FABRICATED NEW CABIN FLOORBOARD. (M)

Part: FLOORBOARD — DAMAGED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD STATION 160-200 RIGHT OUTBOARD NO EDGE FILLER, MISSING INSERT AND COVERING TORN. FABRICATED NEW CABIN FLOORBOARD. (M)

Part: FLOORBOARD — DELAMINATED (FUSELAGE)

FTW - FOUND CABIN FLOORBOARD STATION 218-237 LT OUTBOARD COVER TORN, EXPOSED CORE. COVER DELAMINATED AND BLUE WATER STAINS IN CORE. FABRICATED NEW CABIN FLOORBOARD. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FTW - FOUND MAIN C/B STATION 1309 TO STATION 1250 RIGHT SIDE OUTBOARD METALLIC PANEL HAS CRACKED AT HAT CHANNEL. REPAIRED DAMAGE. (M)

Part: FLOOR PANEL — CRACKED (FUSELAGE)

FTW - FOUND MAIN STATION 541 TO 465 LBL 24 ICHES TO 44 INCHES FLOOR PANEL HAS CRACKED, DAMAGED ON EDGE. FABRICATED NEW FLOOR PANEL. (M)

Part: WEB — CORRODED (FUSELAGE)

FOUND LEFT MAIN CABIN CUSP WEB STATION 612, 625, 630, 664, CORRODED, STATION 645 HAS BARE METAL, STATION 668 IS PUNCTURED. REMOVED CORRODED WEB. FABRICATED NEW WEB. INSTALLED NEW WEB. (M)

Part: WEB — CORRODED (FUSELAGE)

FOUND LEFT MAIN CABIN CUSP WEB STATION 515, STATION 520, STATION 525, STATION 550, STATION 570, STATION 572, STATION 565 AND STATION 580 HAS CORROSION. REMOVED CORRODED WEB. FABRICATED NEW WEB. INSTALLED WEB. (M)

Part: BULKHEAD — CRACKED (FUSELAGE)

FTW - FOUND FORWARD CARGO FORWARD BULKHEAD FS 218 L27L-L28L LOWER BRACKET AND B/H SKIN, BOTH HAVE CRACK. CUT OUT DAMAGED/CRACKED AREA ON B/H SKIN. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR DOUBLER AND FILLER. (M)

Part: RIB — CORRODED (VERTICAL STAB)

FTW - FOUND VERTICAL STAB LOWER DORSAL FIN ACCESS PANEL SUPPORT MATING SURFACES CORRODED, SEVERAL NUTPLATES CORRODED AND MISSING. AFTER FURTHER EVALUATION, FOUND RIB CRACKED. DORSAL FIN PANEL SUPPORT FOUND TO BE OUT OF LIMITS. FABRICATED NEW PANEL SUPPORT. INSTALLED NEW PANEL SUPPORT. REMOVED AND REPLACED FORMER. (M)

Part: CUSP WEB — CORRODED (FUSELAGE)

FTW - FOUND LEFT MAIN CABIN CUSP WEB STATION 780, STATION 800, STATION 836, STATION 874, STATION 894 IS CORRODED. WEB AT STATOIN 836 TO 894 IS OUT OF LIMITS. REMOVED WEB. FABRICATED TWO SECTION CUSPS FROM STATION 807-845 AND 845-905. INSTALLED LEFT MAIN CABIN CUSP WEB. (M)

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 30,186 hrs · 23,873 cycles

LT MAIN CABIN CUSP WEB STA 229 IS CRACKED. REMOVED CUSP WEB SECTION. FABRICATED NEW CUSP WEB. INSTALLED CUSP WEB.

Part: WEB — CORRODED (FUSELAGE)

FTW - PASSENGER CABIN STATION 712-731 STRINGER 18R WEB CORRODED. REMOVED DAMAGED SECTION OF WEB. FABRICATED REPAIR CUSP WEB. INSTALLED REPAIR AND REPAIR SPLICE. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

FTW - FOUND FORWARD CARGO DOOR LATCH SUPPORT ATTACHMENT ANGLE IS CRACKED. REMOVED CRACKED ANGLE. FABRICATED NEW ANGLE. INSTALLED NEW ANGLE. (M)

Part: LIGHT — MISSING (R1 DOOR) · airframe 30,186 hrs · 23,873 cycles

FWD RT GALLEY SERVICE DOOR LINER EXIT LIGHT ASSY MISSING. INSTALLED NEW LIGHT ASSY.

Part: ANGLE — CRACKED (FUSELAGE)

FTW - FOUND AFT CARGO DOOR LATCH SUPPORT HOOK HAS CRACKED ANGLE AT AFT END. REMOVED CRACKED ANGLE. FABRICATED NEW ANGLE. INSTALLED NEW ANGLE. (M)

Part: SKIN — LIGHTNING STRIKE (RT TE FLAP)

FOUND RIGHT OUTBOARD FLAP INBOARD NR 2 TRAILING EDGE HAS LIGHTING STRIKE SEVERAL PLACES AT LOWER INBOARD SURFACE. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. INSTALLED NEW SKIN. (M)

Part: WEB — CRACKED (FUSELAGE)

FTW - FOUND L1 DOOR TORQUE BOX WEB CRACKED AT STATION 207 LONGERON 15L. CUTOUT CRACKED AREA. FABRICATED FILLER AND DOUBLER. INSTALLED FILLER AND DOUBLER. (M)

Part: FLOOR PANEL — CRACKED (COCKPIT)

FTW - FOUND LEFT COCKPIT FLOOR PANEL NR 1144 WOOD CRACKED, NO NONSKID. REPAIRED CRACKED WOOD. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND LEFT MID SEAT TRACK STATION 1136-1309 CORRODED AND GOUGED. REMOVED OUT OF LIMITS SEAT TRACK FROM FS 1126-1309. FABRICATED NEW SEAT TRACK. INSTALLED SEAT TRACK. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND LEFT INBOARD SEAT TRACK 1136-1309 CORRODED AND GOUGED. REMOVED DAMAGED TRACK STATION 1136-1309. LOCATED AND DRILLED SEAT TRACK. LOCATED AND DRILLED SPLICES. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND LEFT INBOARD SEAT TRACK STATION 1176-1309 CORRODED AND GOUGED. REMOVED DAMAGED SEAT TRACK AT STATION 1176-1309. FABRICATED SEAT TRACK. FABRICATED SPLICES. INSTALLED SEAT TRACKS AND SPLICES. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND RIGHT INBOARD SEAT TRACK STATION 200-256 CORRODED AND GOUGED. REMOVED DAMAGED SEAT TRACK. LOCATED AND DRILLED NEW TRACK. LOCATED AND DRILLED SEAT TRACK SPLICES. INSTALLED NEW TRACKS AND SPLICES. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND LEFT INBOARD SEAT TRACK STATION 200-256 CORRODED, GOUGED. REMOVED DAMAGED SECTION OF TRACK STATION 200-256. LOCATED AND DRILLED NEW SEAT TRACK. LOCATED AND DRILLED SPLICES. INSTALLED SEAT TRACK AND SPLICES. (M)

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 30,186 hrs · 23,873 cycles

LT ELEVATOR ANTI FLOAT TAB DELAMINATED, 2 EA. REMOVED LT ELEVATOR ANTI FLOAT TAB. INSTALLED SERVICEABLE ANTI FLOAT TAB.

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND RIGHT OUTBOARD SEAT TRACK STATION 1036-1309 CORRODED AND GOUGED. REMOVED OUT OF LIMITS SEAT TRACK RIGHT OUTBOARD STATION 1036-1309. FABRICATED SEAT TRACK. FABRICATED SPLICES. INSTALLED SEAT TRACK. INSTALLED SPLICES. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND LEFT OUTBOARD SEAT TRACK STATION 436-636 CORRODED AND GOUGED. SEAT TRACK STATION 436-570 IS OUT OF LIMITS. REMOVED SEAT TRACK. FABRICATED SEAT TRACK. INSTALLED SEAT TRACK AND SPLICES. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND LEFT OUTBOARD SEAT TRACK STATION 1036-1136 CORRODED AND GOUGED. REMOVED SEAT TRACK LEFT OUTBOARD STATION 1036-1136. FABRICATED SEAT TRACKS. FABRICATED SPLICES. INSTALLED LEFT OUTBOARD SEAT RACKS AND SPLICES. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND RIGHT INBOARD SEAT TRACK STATION 636-836 CORRODED AND GOUGED. REMOVED DAMAGED SEAT TRACK INBOARD RIGHT STATION 636-836. LOCATED AND DRILLED NEW TRACK. LOCATED AND DRILLED TRACK SPLICES. INSTALLED NEW TRACKS AND THREE SPLICES. INSTALLED NEW TRACKS AND THREE SPLICES. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND RIGHT INBOARD SEAT TRACK STATION 436-636 CORRODED AND GOUGED. REMOVED DAMAGED SEAT TRACK RIGHT INBOARD STATION 436-636. LOCATED AND DRILLED NEW TRACK. LOCATED AND DRILLED SPLICES. INSTALLED NEW TRACKS AND THREE SPLICES. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND LEFT INBOARD SEAT TRACK STATION 656-856 CORRODED AND GOUGED. REMOVED DAMAGED SECTION OF TRACK STATION 656-856. LOCATED AND DRILLED SEAT TRACK. LOCATED AND DRILLED. INSTALLED LEFT INBOARD SEAT TRACK AND SPLICES. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND LEFT INBOARD SEAT TRACK STATION 856-1056 CORRODED AND GOUGED. REMOVED DAMAGED TRACK STATION 856-1056. LOCATED AND DRILLED SEAT TRACK. LOCATED AND DRILLED SPLICES. INSTALLED LEFT INBOARD SEAT TRACK AND SPLICES. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND RIGHT INBOARD SEAT TRACK CORRODED AND GOUGED FS 1036-1309. REMOVED DAMAGED TRACK RIGHT INBOARD STATION 1036-1309. LOCATED AND DRILLED NEW TRACK. LOCATED AND DRILLED TRACK SPLICES. INSTALLED NEW TRACKS AND THREE SPLICES. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND RIGHT OUTBOARD SEAT TRACK STATION 636-836 CORRODED AND GOUGED. REMOVED LEFT OUTBOARD SEAT TRACK STATION 636-836. FABRICATED SEAT TRACK, INSTALLED SEAT TRACK AND SPLICES. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND RIGHT OUTBOARD SEAT TRACK STATION 436-636 CORRODED AND GOUGED. FOUND STATION 480-636 TO BE OUT OF LIMITS. REMOVED SEAT TRACK. FABRICATE SEAT TRACK. FABRICATED SPLICES. INSTALLED SEAT TRACK. INSTALLED SPLICES. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND LEFT INBOARD SEAT TRACK STATION 456-656 CORRODED AND GOUGED. REMOVED DAMAGED TRACK STATION 456-656. LOCATED AND DRILLED SEAT TRACK. LOCATED AND DRILLED SPLICES. INSTALLED LEFT INBOARD SEAT TRACK. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND LEFT INBOARD SEAT TRACK STATION 256-456 CORRODED AND GOUGED. REMOVED DAMAGED TRACK STATION 256-456. LOCATED AND DRILLED HOLES ON SEAT TRACK. LOCATED AND DRILLED SPLICES. INSTALLED LEFT INBOARD SEAT TRACK AND SPLICES. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND LEFT INBOARD SEAT TRACK STATION 1056-1136 CORRODED AND GOUGED. REMOVED DAMAGED TRACK STATION 1056-1136. LOCATED AND DRILLED SEAT TRACKS. LOCATED AND DRILLED SPLICES. INSTALLED LEFT INBOARD SEAT TRACKS AND SPLICES. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FTW - FOUND RIGHT OUTBOARD SEAT TRACK STATION 836-1030 CORRODED AND GOUGED. REMOVED OUT OF LIMITS SEAT TRACK RIGHT OUTBOARD STATION 836-1036. FABRICATE SEAT TRACK. FABRICATED SPLICES. INSTALLED SEAT TRACK. INSTALLED SPLICES. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

FTW - FOUND MID CARGO DOOR SUPPORT ATTACHMENT ANGLE IS CRACKED. REMOVED SUPPORT ANGLE. FORMED NEW ANGLE. INSTALLED NEW SUPPORT ANGLE. (M)

Part: BULKHEAD — DENTED (FUSELAGE)

FTW - FOUND FORWARD PIT STATION 218 FORWARD BULKHEAD HAS CRACKED SUPPORT CHANNEL AND DENT LBL 7 INCHES. CUT OUT DAMAGED AREA ON WEB. FABRICATED DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER. LOCATED AND DRILLED UPPER SUPPORT. INSTALLED UPPER SUPPORT. (M)