N755RA

Part: INDICATOR — BURNED (AHRU) · airframe 35,306 hrs · 23,593 cycles

CAPTAIN REPORTED THAT DURING DESCENT BOTH COMPASS OPENED, AUTO PILOT DEACTIVATED AND HEADING LIGHT AND AUTOMATIC ACCELERATORS SHUTDOWN. AHRU´S WERE CHECKED BY CONDITION AND LT AHRU WAS DETECTED WITHOUT SYNCHRONY AND OPENED MORE THAN 45 DEGREES. AHRU WAS INTERCHANGED AND TESTED CORRECT SO AIRCRAFT WAS DISPATCHED. LATER, CAPTAIN PERFORMED AN UNSCHEDULED LANDING AT GDL DUE TO RIGHT COMPASS FAILED DURING FLIGHT. DURING MAINTENANCE REVISION, AHRU NR 1 WAS DETECTED DAMAGED WITH BURNED ODOR IAW FAILURE OF ITS COOLING FAN. AHRU NR 1 WAS REPLACED IAW MM 34-21-10 AND 34-21-00, TESTED CORRECT.

Part: INDICATION SYS — MALFUNCTIONED (OIL TEMP) · airframe 34,832 hrs · 23,314 cycles

AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF DURING CLIMB RIGHT OIL TEMPERATURE INDICATOR SHOWED 135 GRADES AND INCREASED UP TO 145 IN 5 SECONDS, SO THRUST WAS REDUCED IN ORDER TO PREVENT HIGHER OIL TEMPERATURE. AT PLATFORM, RIGHT ENGINE TEMPERATURE SENSOR AND CHIP DETECTOR WERE VERIFIED BEING CORRECT. OIL TEMPERATURE SENSORS WERE INTERCHANGED AND ENGINE WAS TESTED IAW MM 79-32-01 AND 79-00-00, NO LEAKS WERE FOUND.

Part: CONTROLLER — FAILED (ANTI FOG) · airframe 33,748 hrs · 22,615 cycles

AIRCRAFT RETURNED TO PLATFORM, SMOKE ODOR WAS DETECTED IN THE CABIN FROM THE SEATS 1 AND 2 GRID. THE FORWARD SIDEWALL OF ELECTRICAL / ELECTRONIC COMPARTMENT FROM STATIONS 110 TO 218 WAS OPENED DETECTING THE CAPTAIN FLOOR BURNED AND STRONG SMOKE ODOR IN 3 TEMPERATURE CONTROLLERS. THE WINDOWS AND WINDSHIELDS ANTI-FOG TEMPERATURE CONTROLLERS WERE REPLACED IAW MM 30-41-01 AND WIRING WAS CHECKED IAW WDM 20-50-01, TESTED CORRECT.

Part: PLATE — DAMAGED (CONTROL COLLUMN) · airframe 33,055 hrs · 22,151 cycles

AIRCRAFT REJECTED TAKEOFF AT 60 KTS AND RETURNED TO PLATFORM AS A CONSEQUENCE RUDDER MOVEMENT TO THE RIGHT SIDE WAS VERY HARD, RIGHT PEDAL STOCKS FULLY INSIDE AND THE DIRECTION CONTROL WAS UNABLE WITH PEDALS. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK, THE CONTROL PEDESTAL COVER AND SPIRAL DRIVE PLATE WERE REPLACED IAW MM 27-20-07, ADJUSTMENT AND RUDDER HYDRAULIC POWER PACKAGE TEST WAS PERFORMED IAW MM 27-20-08, BEING CORRECT.

Part: VALVE — LEAKING (COFFEEMAKER) · airframe 32,383 hrs · 21,749 cycles

AIRCRAFT RETURNED TO PLATFORM, WATER LEAK IN THE COFFEE MAKER OF AFT GALLEY. DURING REVISION WAS DETECTED THE FEEDING WATER VALVE LOOSEN. THE FEEDING WATER VALVE WAS REPRESSED IAW MM 20-30-02, ALL CORRECT. DURING OVERNIGHT SERVICE, THE TORQUE IN COFFEE MAKER CONNECTORS OF AFT GALLEY WAS VERIFIED IAW MM 20-30-02, ALL CORRECT.

Part: FIRE LOOP — FAILED (RT ENGINE) · airframe 32,153 hrs · 21,589 cycles

DURING TRANSIT CHECK, FIRE ALARMS IN BOTH ENGINES DID NOT OPERATE AND ONLY LIGHTS TURNED ON. DURING REVISION DETECTED FIRE WARNING AURAL SWITCH OPERATED CORRECTLY. AMPLIFIER CONNECTORS WIRING WAS VERIFIED, SYSTEM CHECKED OKAY. DURING REVISION DETECTED THE RIGHT ENGINE AMPLIFIER WITH FAILURE. AMPLIFIER DETECTOR UNIT A2-6 WAS REPLACED, TESTED CORRECT. REJECTED TAKEOFF AS A CONSEQUENCE OF RIGHT ENGINE DID NOT REACH TAKEOFF EPRS OF 1.98, IT STAYED IN 1.80 EPR INCREASING EGT TEMPERATURE. AIRCRAFT SENT TO HANGAR, PT7 & PT2 LEAK CHECK PERFORMED, PRBC LINES TIGHTENED, ACCELERATION CHAMBER AND ANTI SURGE VALVES WERE LUBRICATED, RUDDER PT2 UNION REPLACED AND REMOTE CONTROL TRIM PERFORMED, TESTED CORRECT.

Part: FCU — FAILED (RT ENGINE) · airframe 32,152 hrs · 21,588 cycles

AIRCRAFT REJECTED TAKEOFF AS A CONSEQUENCE OF RIGHT ENGINE DID NOT ACCELERATE INCREASING TEMPERATURE TO 600 DEGREES AT STATIC TAKEOFF WITH 30 DEGREES AT ATMOSPHERE TEMPERATURE. AT PLATFORM, RIGHT ENGINE WAS STARTED GETTING 580 DEGREES AT 1.20 OF EPR. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, RIGHT FCU AND FUEL PUMP FILTER WERE REPLACED IAW MM 73-20-01 AND 73-12-01 RESPECTIVELY. THE PT2 AND PT7 LEAK CHECK WAS PERFORMED IAW MM 77-11-01, ALL CORRECT. EGT SYSTEM INDICATION CHECK WAS PERFORMED IAW MM 77-21-04, ALL CORRECT. A 500 HOURS BOROSCOPIC INSPECTION WAS PERFORMED IAW MM 72-00-00, NOT DETECTING DAMAGES.

Part: LINE — DAMAGED (PT2) · airframe 32,134 hrs · 21,576 cycles

CAPTAIN REPORTED RIGHT ENGINE REACHED 641°C PER 3 SECONDS. BOROSCOPIC INSPECTION WAS PERFORMED IAW MM 72-00-00, BEING ALL CORRECT. TRIM WAS PERFORMED TO ENGINES, DETECTING A PT2 LINE DAMAGED AND AN INTERNAL LEAK IN TH PT7 LINE. PT2 LINE WAS REPLACED AND PT7 LINE LEAK WAS CORRECTED IAW MM 77-11-00. TRIM WAS CONCLUDED WITH BOTH ACCELERATORS WERE CORRECT.

Part: STARTER — MALFUNCTIONED (RT ENGINE) · airframe 31,915 hrs · 21,439 cycles

AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING RIGHT ENGINE STARTED, THE A AND B IGNITION SYSTEM DID NOT HAVE ROTATION IN N1 AND N2. DURING REVISION, THE RIGHT ENGINE FAN WAS DETECTED JAMMED. THE STARTER WAS DEINSTALLED AND REINSTALLED IAW MM 80-10-01, ALL CORRECT. DURING OVERNIGHT SERVICE, THE RIGHT ENGINE WAS STARTED FOUR TIMES INSPECTING BY FREE ROTATION, BEING ALL CORRECT IAW MPCM 71-00-01. THE STARTER WAS CHECKED AND STARTER DRIVE GEAR SHAFT COUPPLING WAS REPLACED IAW MM 72-61-04 AND THE RIGHT CHIP DETECTORS WERE CHECKED IAW EO 987218, ALL CORRECT.

Part: STARTER — FAILED (RT ENGINE) · airframe 31,910 hrs · 21,436 cycles

AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING RIGHT ENGINE STARTED, THE A AND B IGNITION SYSTEM DID NOT HAVE ROTATION IN N1 AND N2 AND HYDRAULIC PRESSURE DID NOT INCREASE. DURING REVISION, THE RIGHT ENGINE WAS STARTED WITH NEGATIVES RESULTS, STARTER VALVE LIGHT TURNED ON AND OSCILLATION OF PNEUMATIC PRESSURE WITHOUT ROTATION. THE ENGINE AIR TURBINE STARTER WAS REPLACED IAW MM 80-10-01, TESTED CORRECT.

Part: FUEL CONTROL — FAILED (RIGHT ENGINE) · airframe 31,887 hrs · 21,420 cycles

AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING RIGHT ENGINE STARTED, ACCELERATION INCREASED SLOWLY. THE RIGHT ENGINE WAS VERIFIED AND FOUND ALL CORRECT. THE FCU WAS REPLACED IAW MM 73-20-01 AND ACCELERATION CHECK WAS PERFORMED IAW 71-00-00, ALL CORRECT. DUE TO THE TYPE OF FAILURE, RIGHT ENGINE WAS REPLACED IAW 71-00-02, TESTED CORRECT.

Part: COMPRESSOR WHEEL — DAMAGED (LT ENGINE) · airframe 31,226 hrs · 21,012 cycles

DURING TRANSIT CHECK WERE DETECTED 15 BLADES OF LEFT ENGINE DAMAGED BY FOD. ONE BLADE HAD 0.25 DEPTH AND 7.25 FORM THE BLEED ROOT. AIRCRAFT WAS SENT TO THE HANGAR AND BLADES WERE REWORKED IAW MM 72-33-22. BOROSCOPE INSPECTION WAS PERFORMED TO THE SIX AND SEVEN STAGES, BEING ALL CORRECT. DURING OVERNIGHT SERVICE, LEFT ENGINE C1 DISK WAS REPLACED IAW MM 72-33-02, ENGINE RUNNING TEST WAS PERFORMED IAW MM 71-00-00, ALL CORRECT.

Part: LINE — LEAKING (SPOILER ACTUATOR) · airframe 30,708 hrs · 20,640 cycles

AIRCRAFT ARRIVED WITH CAPTAIN REPORT THAT HYDRAULIC LEAK FROM OUTBOARD SPOILER SYSTEM IN RIGHT WING. BOTH LINES SPOILER IN RIGHT WING WERE REPLACED IAW MM 27-60-00, ALL CORRECT.

Part: TURBINE BLADES — DAMAGED (LT ENGINE) · airframe 30,380 hrs · 20,398 cycles

AIRCRAFT RETURNED OF FLIGHT, LT ENGINE FLAME OUT AFTER TAKEOFF AT 400 FT EGT'S WERE 590 DEGREE C. DURING REVISION, TECHNICAL PERSONNEL DETECTED THE LOW TURBINE BLADES WERE DAMAGED. AIRCRAFT WAS SENT TO THE HANGAR AND LT ENGINE WAS REPLACED IAW MM 71-00-00 AND 71-00-02, TESTS WERE CORRECT. FURTHER INFORMATION WILL BE SENT AS A SUPPLEMENT.

Part: FILTER — CLOGGED (FUEL SYSTEM) · airframe 29,784 hrs · 19,995 cycles

AIRCRAFT RETURNED TO PLATFORM, (RT FUEL STRAINER CLOGGING) LIGHT TURNED ON. MAIN FUEL FILTER AND DIFFERENTIAL PRESSURE ALARM WERE REPLACED IAW MM 73-12-01, TEST CORRECT.

Part: ADC — FAILED (COCKPIT) · airframe 29,427 hrs · 19,744 cycles

DURING TRANSIT CHECK, CAPTAIN REPORTED FAST/SLOW FLAGS IN BOTH ADI´S AND DIFFERENCE OF 150 FEET BETWEEN ALTIMETERS. LT ADC WAS REPLACED IAW MM 34-16-01, TEST CORRECT.

Part: BLADE — DAMAGED (LT ENGINE) · airframe 29,051 hrs · 19,481 cycles

DURING OVERNIGHT SERVICE, FOD´S WERE DETECTED ON 15 BLADES OF LT ENGINE. BOROSCOPE INSPECTION WAS PERFORMED ON C6 AND C7 COMPRESSOR STAGE IAW MM 72-00-00 AND NO DAMAGE WAS DETECTED. ON FAN STAGE, 3 BLADES WERE DETECTED WITH DAMAGES AND C1 FAN STAGE WAS REPLACED IAW MM 72-33-02, TEST CORRECT.

Part: FCU — FAILED (NR 1 ENGINE)

AIRCRAFT RETURN TO PLATFORM AS CONSEQUENCE OF ENGINE NR 1 SHOWS N2 46.5 PERCENT AND EGT 430. TRIM WAS ACCOMPLISHED AND PARAMETERS WERE WITHIN LIMITS. DURING OVERNIGHT SERVICE, THE FCU AND PRBC WERE REPLACED IAW MM 73-20-01 AND 75-31-01, RESPECTIVELY. TEST CORRECT IAW MM 71-00-01. (M)

Part: SWITCH — FAILED (ANTI-SKID SYS)

FLT 426 - MEX-IAH - AIRCRAFT ARRIVED WITH CAPTAIN REPORT OF LIGHTS ANTI-SKID COME ON. DURING REVISION, THE SWITCH S1-130 WAS OUT OF SERVICE. THE SWITCH S1-130 WAS REPLACED IAW WDM 32-41-00 AND LIGHTS ANTI-SKID COME OFF. THE CONTROL BOX WAS TESTED IAW MM 32-43-00, ALL TESTS CORRECT. (M)

Part: SWITCH — FAILED (TAIL OVERHEAT)

AFTER TAKEOFF ON CUU STATION TAIL COMP TEMP HIGH LIGHT COMES ON. DURING OVERNIGHT SERVICE, TAIL COMP OVERHEAT SENSORS WERE REPLACED IAW MM 36-20-02 AND WIRING SENSORS WERE VERIFIED IAW WDM 36-23-00, ALL TESTS CORRECT. (M)

Part: WARNING LIGHT — ILLUMINATED (AHRS)

AIRCRAFT CARRIED OUT AN UNSCHEDULED LANDING DUE TO FLIGHT DIRECTOR FAILURE DUE TO AHRS FAILURE MESSAGE ON EFIS DISPLAY. AHRS NR 2 BRAKERS WERE RESETED AND CONNECTORS WERE CLEANED IAW MM 34-20-00. BOTH FLIGHT GUIDANCE WERE TESTED IAW MM 22-01-05, ALL CORRECT.

Part: LINK — FAILED (MLG DOOR)

FLT 929 - MTY-MEX - AIRCRAFT RETURNED TO GATE, AFTER RETRACTING LANDING GEAR, HAD STRONG VIBRATION. AIRCRAFT RETURNED WITH RIGHT NOSE LANDING GEAR DOOR OPEN. FOUND FORWARD DOOR LINK LEVER BYPASS DID NOT WORK, DOOR LINK WAS REPLACED IAW MM 32-22-01, ALL CORRECT.

Part: INDICATOR — OVERHEATED (RAM AIR TURBINE)

FLT 934 - MEX-SAT - AIRCRAFT RETURNED TO PLATFORM DUE RAT AND EPR LIMIT OUR OF SERVICE INDICATIONS. DURING CHECK IT WAS DETECTED THAT THE RAT INDICATOR OVERHEATED. THE R2-5 RAT INDICATOR WAS REPLACED IAW MM 34-10-0, TESTS CORRECT. (M)

Part: FIRE DETECTOR — INOPERATIVE (NR 1 ENGINE)

LEFT ENGINE FIRE DETECTOR LOOP B ILLUMINATED DURING FLIGHT. SWITCHED TO LOOP A AND ACCOMPLISHED A GOOD TEST. LEFT SWITCH IN LOOP A AS PER PROCEDURE. PULLING INTO GATE AT SJC LEFT ENGINE FIRE LIGHT AND BELL ILLUMINATED. SHUT DOWN ENGINE, PULLED FIRE HANDLE, FIRED BOTH BOTTLES. LIGHT REMAINED ILLUMINATED. GROUND CREW REPORTED A SMALL AMOUNT OF SMOKE COMING FROM TOP OF ENGINE AFTER FIRING BOTTLES. UPON INVESTIGATION, MAINTENANCE DETERMINED THERE WAS NO ACTUAL FIRE. MAINTENANCE FOUND UPPER FIRE DETECTOR LOOP A AND B BAD. REPLACED UPPER FIRE DETECTOR LOOP A AND B. PERFORMED FIRE DETECTOR TEST AS REQUIRED. REMOVED AND REPLACED NR 1 AND NR 2 FIRE EXTINGUISHER, INSTALLED SQUIBB, FIRE SYSTEM TEST OK PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

CCI - RIGHT AFT EMERGENCY EXIT LIGHT AND 3 RED PATH LIGHTS INOPERATIVE. REMOVED AND REPLACED RIGHT AFT EMERGENCY EXIT LIGHT PACK. OPS CHECK GOOD ON PATH LIGHT PACK. OPS CHECK GOOD ON PATH LIGHTS AND EXIT LIGHTS. (M)

Part: DOOR — MISINSTALLED (EMERGENCY EXIT)

AFTER TAKEOFF, FLIGHT ATTENDANT ADVISED LOUD NOISE AD FLOW FROM LEFT AFT OVERWING EXIT. RETURNED FOR LANDING. FOUND AFT LEFT OVERWING EMERGENCY EXIT DOOR NOT PROPERLY SEATED. RE-SEATED DOOR AND PRESSURIZED AIRCRAFT TO 6 PSI. DOOR CHECKED GOOD WITH NO LEAKS NOTED, OK FOR SERVICE. (M)

Part: WIRE — DAMAGED (CABIN)

FOUND SEAT MOUNTED EMERGENCY LIGHT AT ROW 21D INOPERATIVE. SPLICED BROKEN SEAT MOUNTED EMERGENCY LIGHT WIRE PER MM. OPS CHECK NORMAL. (M)

Part: WIRE — BROKEN (CABIN)

CCI - FOUND SEAT MOUNTED EMERGENCY LIGHT AT 21D INOPERATIVE. SPLICED BROKEN WIRE PER MM. OPS CHECK OK. (M)

Part: CHARGER — INOPERATIVE (COCKPIT)

LAS - EMERGENCY LIGHT NUDE BULBS IN COCKPIT WILL NOT ILLUMINATE WHEN EMERGENCY LIGHT SWITCH IS ON. REPLACED EMERGENCY LIGHT CHARGING UNIT. SYSTEM TEST NORMAL. (M)

Part: SIGN — INOPERATIVE (CABIN)

OKC - THE FORWARD SERVICE DOOR SELF ILLUMINATING EMERGENCY EXIT SIGN FAILED LUMINESCENT TEST AND HAS SOME DAMAGE TO RED COVER. INSTALLED NEW EMERGENCY EXIT SIGN OVER FORWARD SERVICE DOOR PER MO-80, MM 20-30-01. (M)

Part: SIGN — INOPERATIVE (CABIN)

OKC - THE SELF ILLUMINATING EMERGENCY EXIT SIGN AT THE AFT CABIN DROP CEILING FAILED ILLUMINSCENT TEST. INSTALLED NEW EMERGENCY EXIT SIGN PER MO-80, MM 20-30-01, INTO AFT CABIN DROP CEILING. (M)

Part: CONNECTOR — LOOSE (ROW 25)

RNO-CCI - EMERGENCY LIGHT AT ROW 25 IS OUT. SECURED LOOSE CONNECTOR. LIGHT AT 25 CHECKS OK. (M)

Part: SWITCH — BROKEN (CABIN)

RNO-CCI - L1 DOOR EMERGENCY LIGHT ASSY OFF-ON SWITCH BROKEN. REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT ASSY. OPS CHECK GOOD. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

SJC - EMERGENCY FLOOR LIGHTING INOPERATIVE, STARBOARD SIDE. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK GOOD. (M)

Part: POWER SUPPLY — INOPERATIVE (LT OVERWING)

RNO - LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED POWER PACK. OPS CHECK NORMAL. (M)

Part: CHARGER — INOPERATIVE (BATTERY)

RNO-CCI - EMERGENCY LAMPS INOPERATIVE AT FORWARD OVERWING EXIT NR 1 SIDE. REPLACED CHARGER. OPS CHECK GOOD. (M)

Part: CHARGER — FAILED (BATTERY)

SJC-CCI - LEFT EMERGENCY EXIT BATTERY CHARGER INOPERATIVE 4 ROWS OUT ON EMERGENCY ILGHT CHECK. CHANGED BATTERY CHARGER. E-LIGHTS OPS CHECK GOOD. (M)

Part: BATTERY PACK — INOPERATIVE (ROW 15 - 18)

LAX - EMERGENCY LIGHTS AT ROW 15-19 AT SEATS ARE INOPERATIVE. REPLACED BATTERY PACK AT LEFT OVERWING DOOR. EMERGENCY LIGHTS AT ROWS 15-18. OPS CHECK OK. (M)

Part: BATTERY PACK — INOPERATIVE (ROW 21 - 24)

FLOOR LEVEL EMERGENCY LIGHT AT A/C RIGHT, ROWS 21-24 ARE ILLUMINATED AND WILL NOT EXTINGUISH. REPLACED EMERGENCY EXIT SIGN BATTERY PACK. OPS CHECK OK. (M)

Part: WIRE — BROKEN (ROW 19)

ON TAXI OUT, FLOOR LEVEL LIGHTING AIRCRAFT LEFT ROWS 21-24 CAME ON AGAIN. RETURNED TO GATE. FOUND BROKEN WIRE ON ROW 19 DEF. RESPLICED WIRES. OPS CHECK NORMAL. (M)

Part: FUSE — FAILED (BATTERY PACK)

SJC - AFT EMPENNAGE A/C LEFT E-PATH BATTERY PACK INOPERATIVE. REPLACED FUSE IN E-PATH BATTERY PACK. OPS CHECK GOOD. (X)

Part: SLIDE — DISLODGED (CABIN)

LAS - FORWARD DOOR SLIDE PACK FELL OUT. INSPECTED AND REINSTALLED DOOR SLIDE ON LEFT FORWARD ENTRY DOOR. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

RNO - CHECK EMERGENCY AISLE BATTERY PACK. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT SEAT 20A DUE TO ROWS 15 THROUGH 18 INTERMITTENT, OPS CHECK GOOD AT THIS TIME. (X)

Part: BATTERY PACK — DISCHARGED (AFT AIRSTAIR)

RNO - EMERGENCY LIGHT BATTERY CHARGER BY AFT AIRSTAIR DOOR IS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER 33-53-00. (M)

Part: CONNECTOR — FAILED (ROW 9)

AT SJC, EMERGENCY LIGHT AT ROW 9 INOPERATIVE. REPAIRED CONNECTION ON EMERGENCY LIGHT AT ROW 9. OPS CHECK GOOD AS PER MM 33-53-00. (M)

Part: TAIL PIPE — FIRE (ENGINE)

AT SJC, MAINTENANCE ASKED FLIGHT 101 TO RETURN TO GATE AFTER OBSERVING ABNORMAL START. ENGINE START PARAMETERS DID APPEAR WITHIN NORMAL LIMITS. UPON TAXI OUT SAW EVIDENCE OF A TIAL PIPE FIRE. PERFORMED INSPECTION OF ENGINE PER MM, CHAP 72-00-00, PAGE 813. ALL ENGINE COMPONENTS CHECKED GOOD. DRY MOTORED FOR ONE MINUTE TO BLOW OUT EXCESSIVE FUEL. EGT REPORT FROM CREW WAS 430 ON START PER MM. ONLY VISUAL INSPECTION REQUIRED. THIRD START ATTEMPT NORMAL. OK FOR CONTINUED SERVICE. (M)

Part: WIRE — BROKEN (ROW 24 DEF)

AT SJC, SEAT MOUNTED 'E' PATH LIGHT WIRE BROKEN AT SIDEWALL CONNECTOR AT 24 DEF. REPAIRED WIRE AT SEAT 24 DEF 'E' PATH CONNECTOR LIGHT. OPS CHECKS GOOD. (M)

Part: WIRE — LOOSE (ROW 14)

FLIGHT ATTENDANT REPORTS EXPOSED WIRING ALONG SIDEWALL AT ROW 14. SECURED WIRING AT ROW 14 DEF. EMERGENCY SEAT WIRING. OK FOR CONTINUED SERVICE. (M)

Part: WIRE — DAMAGED (ROW 12)

SJC - FOUND BARE WIRE FOR EMERGENCY LIGHTS. REPAIRED AND SECURED WIRES AT ROW 12 DEF. (X)

Part: WIRE — FAILED (CABIN)

EMERGENCY LIGHTS AT 10W 20D INOPERATIVE. RE-INSTALLED WIRE INTO CONNECTOR. OPS CHECK GOOD. (X)

Part: APU — INOPERATIVE (APU COMPT)

AT PUSH BACK, FOUND APU TO BE INOP RETURNED TO GATE, REF DMI NR 13018. (M)

Part: TRANDUCER PINS — BACKED OUT (MLG)

ON TAKEOFF ROLL, APPROX 60 KNOTS WHEEL NOT TURNING LIGHT ILLUMINATED AFTER RETURNING TO TAXI SPEED THE LIGHT WENT OUT. REMOVED NR 1 WHEEL HUB CAP FOUND TRANSDUCER PINS BACKED OUT. REPLACED PINS BIT CHECK NORMAL OF ANTI-SKID CONTROLLER. (M)

Part: FUSE — FAILED (CABIN)

AFT EMERGENCY LIGHT INOP. REPLACED FUSE PER MM. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ACM — SMOKING (LEFT)

LEFT PACK CAUSED SMOKE IN CABIN. DMI NR 10352. NEEDS ACM, PART ON ORDER. (X)