N754RA

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 44,049 hrs · 30,610 cycles

DURING TRANSIT CHECK, A HYD LEAK ON THE LT WHEEL WELL LANDING GEAR WAS DETECTED. MX REPLACED AND TESTED THE HYDRAULIC LINE IAW AMM 20-50-00, ALL CORRECT.

Part: FAN BLADE — NICKED (RT ENGINE) · airframe 43,824 hrs · 30,427 cycles

DURING OVERNIGHT CHECK, FOUND A NICK OF 0.005 INCHES DEPTH ON THE LEADING EDGE OF ONE FAN BLADE AT .4375 INCHES FROM THE ROOT, AND A NICK OF 0.0035 INCHES OUT OF LIMITS ON THE LEADING EDGE OF THE OTHER FAN BLADE AT .7500 INCHES FROM THE ROOT. RT ENG WAS REPLACED AND OPERATIONAL TEST WAS PERFORMED IAW MM 71-00-02 AND CM 71-00-01, ALL CORRECT.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 42,328 hrs · 29,277 cycles

CAPTAIN REPORTED LT HYDRAULIC PUMP WITH FAILURE. MAINTENANCE CHECKED THE LT SYSTEM AND DETECTED A HYDRAULIC LEAK IN THE REVERSE CONTROL VALVE LINE. THE HYDRAULIC LINE WAS REPLACED BY A FLEXIBLE LINE IAW MM 12-13-01 AND HYDRAULIC PUMP WAS REPLACED IAW MM 29-11-11, TESTED CORRECT. DURING OVERNIGHT CHECK, THE LT FLEXIBLE LINE, FILTER AND WATER SEPARATORS WERE REPLACED AND PNEUMATIC SYSTEM DUCTS WERE CLEANED, TESTED CORRECT IAW MM 29-10-05 AND 29-01-02.

Part: CONTROL CABLE — BROKEN (NLG) · airframe 41,972 hrs · 28,998 cycles

DURING TAXING, CAPTAIN REPORTED STEERING FAILURE. MAINT CHECKED THE STEERING BY-PASS, FINDING ALL CORRECT; THEN, THE STEERING VALVE WAS CHECKED, DETECTING THE STEERING CONTROL CABLE BROKEN, AC WAS SENT TO THE HANGAR AND THE CONTROL CABLE WAS REPLACED AND ADJUSTED IAW MM 32-50-00 AND 32-50-01, TESTED CORRECT.

Part: LINK — LOOSE (NLG) · airframe 41,868 hrs · 28,925 cycles

AC RETURNED TO DEPARTURE DURING TAKEOFF, NOISE AND VIBRATION IN THE NOSE LANDING GEAR WERE DETECTED AND CONTINUED WITH FLAPS AT 40 DEGREES. ABNORMAL PROCEDURE SECTION 5-10 WAS PERFORMED. AT PLATFORM, MAINT DETECTED THE NOSE LANDING GEAR DOOR OPEN AND UNLOCKED, AC WAS SENT TO THE HANGAR AND A LINK WAS DETECTED LOOSE. THE LINK WAS REPLACED IAW MM 32-22-01, TESTED CORRECT. THE OVERWEIGHT INSP WAS NOT NECESSARY DUE TO THE LANDING WEIGHT WAS 110,500 POUNDS AND THE MAXIMUM IS 128,000 POUNDS.

Part: PLATE — BROKEN (SPIRAL DRIVE) · airframe 40,731 hrs · 28,073 cycles

CAPTAIN REPORTED THAT DURING CRUISE THE AILERON GOT STUCK WHEN THE COMPENSATOR KNOB IS TURNED TO THE RT SIDE. DURING CHECK, A SCREW WAS DAMAGED AND PLATE SPIRAL DRIVE BROKEN. THEY WERE REPLACED AND TRIM WAS PERFORMED TO CONTROL MECHANISM IAW MM 27-10-07, TESTED CORRECT.

Part: DISPLAY — DAMAGED (LT SIDE) · airframe 40,510 hrs · 27,932 cycles

CAPTAIN REPORTED LT NAVIGATION DISPLAY OUT OF SERVICE AND SMOKE ODOR IN CABIN. DURING MAINTENANCE CHECK, IT WAS DETECTED THAT THE ODOR WAS ORIGINATED BY THE DISPLAY UNIT, WHICH WAS REPLACED IAW MM 34-22-06, TESTED CORRECT.

Part: TRANSCEIVER — FAILED (WX RADAR SYS) · airframe 40,158 hrs · 27,720 cycles

AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, DUE TO THE WEATHER RADAR FAILED IN FLIGHT. MAINTENANCE PERSONNEL REPLACED THE RADAR TRANSCEIVER IAW MM 34-41-04 TESTED CORRECT.

Part: TRANSCEIVER — FAILED (WX RADAR) · airframe 40,158 hrs · 27,720 cycles

AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, WEATHER RADAR FAILED IN FLIGHT. MAINTENANCE PERSONNEL REPLACED THE RADAR TRANSCEIVER IAW MM 34-41-04 TESTED CORRECT.

Part: PRESSURE VALVE — FAILED (OIL SYSTEM) · airframe 39,881 hrs · 27,539 cycles

AIRCRAFT RETURNED, DUE TO HIGH OIL PRESSURE (57 PSI) AND TEMPERATURE (157 DEGREES C) INDICATIONS OF RT ENGINE WERE SHOWN. DURING MAINTENANCE CHECK, A BOROSCOPIC INSPECTION WAS PERFORMED AND CHIP DETECTOR WAS CHECKED, ALL CORRECT. AS PRECAUTIONARY ACTION OIL, FILTER AND OIL PRESSURE REGULATOR VALVE WERE REPLACED AND ADJUSTED IAW MM 79-20-03, TESTED CORRECT.

Part: PROXIMITY SWITCH — FAILED (MLG) · airframe 39,391 hrs · 27,232 cycles

CAPTAIN REPORTED THAT 3 RED LANDING GEARS LIGHTS TURNED ON DURING CLIMB AND CRUISE. PROXIMITY SWITCH COMPUTER WAS TESTED, CIRCUIT BREAKER WAS RESEATED, LANDING UP SENSORS AND CONNECTORS WERE CHECKED, ALL CORRECT. DURING TRANSIT CHECK AT GDL, THE PROXIMITY SWITCH COMPUTER WAS REPLACED IAW MM 32-60-04, TESTED CORRECT. DURING OVERNIGHT CHECK, THE FAILURE CONTINUED, THEREFORE THE RT THROTTLE SWITCH UNIT WAS REPLACED IAW MM 76-10-03 AND LANDING GEAR TEST WAS PERFORMED IAW MM 32-60-00, ALL CORRECT.

Part: RELAY — FAILED (AHRS) · airframe 39,178 hrs · 27,090 cycles

CAPTAIN REPORTED AHRS 1, 2 AND 3 BASIC MODE LIGHTS TURNED ON. AHRS 1, 2 AND 3 BREAKERS WERE RESEATED AND AHRS 1 AND 2 WORKED CORRECT BUT AHRS NR 3 FAILED, SO IT WAS DEFERRED IAW MEL 34-38. AIRCRAFT WAS DISPATCHED BUT RETURNED TO PLATFORM DUE TO THE SAME FAILURE. THE FLIGHT DIRECTOR BARS WERE CHECKED BEING CORRECT AND AIRCRAFT WAS DISPATCHED WITH THE 1, 2 AND 3 AHRS´S IN BASIC MODE. DURING OVERNIGHT CHECK, WIRING WAS CHECKED, BREAKER B10-407 AND RELAYS R20-92 AND R20-91 WERE REPLACED IAW WDM 34-24-01 AND TESTED IAW MM 34-24-00, ALL CORRECT.

Part: CADC — MALFUNCTIONED (NR 2) · airframe 38,475 hrs · 26,614 cycles

AIRCRAFT RETURNED TO PLATFORM DUE TO (F/S FAIL) AND (TRI FAIL) FLAGS WERE SHOWN IN THE LT FLIGHT DIRECTOR. CADC NR 1 WAS RESEATED, BUT FAILURE CONTINUED, THE CADC NR 2 WAS RESEATED, ALL CORRECT. CADC NR 1 WAS REPLACED IAW MM 34-16-01, BUT (MACH) AND (LT ALTIMETER) FLAGS WERE SHOWN. CADC NR 1 WAS REMOVED, CONNECTORS WERE CLEANED AND COMPUTER WAS INSTALLED AGAIN, TESTED CORRECT. DURING OVERNIGHT CHECK, SYSTEM WAS TESTED IAW MM 34-16-01, ALL CORRECT.

Part: BLADE — BROKEN (LT ENGINE) · airframe 38,151 hrs · 26,405 cycles

DURING THE BOROSCOPIC INSPECTION RELATED TO THE EO 987211 R4 PERFORMED DURING OVERNIGHT CHECK, WERE DETECTED SEVERAL BLADES WITH DENTS OUT OF LIMITS AND ONE BLADE BROKEN IN T2 SECTION. LT ENGINE WAS REPLACED AND TESTED IAW MM 71-00-02 AND 71-00-01, ALL CORRECT.

Part: CADC — FAILED (LT SIDE) · airframe 37,744 hrs · 26,150 cycles

AIRCRAFT RETURNED TO PLATFORM, CADC FAIL WINDSHEAR INOP AND F/D FAIL LIGHTS TURNED ON. DURING MAINTENANCE REVISION, WHEN BOTH AIR DATA SYSTEMS WERE SELECTED TO CADC NR 1 POSITION, THE FAIL DISAPPEARED, BUT WHEN SYSTEMS RETURNED TO NORMAL POSITION, FAILURE APPEARED AGAIN. CADC NR 2 WAS REPLACED, BUT FAIL CONTINUED, THEREFORE, CADC NR 1 WAS REPLACED TOO IAW MM 34-16-01 AND TESTS WERE PERFORMED IAW MM 34-11-00, ALL CORRECT.

Part: PRESSURE SWITCH — FAILED (CABIN PRESSURE) · airframe 37,742 hrs · 26,148 cycles

CAPTAIN REPORTED THAT DURING DESCENT AT 10,000 FEET, BOTH LT AND RT AIR CONDITIONING SYS SHUTDOWN WITHOUT APPARENTLY CAUSE, AIRCRAFT WAS DEPRESSURIZED, BUT OXYGEN MASKS DID NOT ACTIVATE. BOTH PRESSURE CONTROLLERS WERE RESEATED, AIR CONDITIONING SYSTEMS WERE CHECKED BY LEAKS, AND ENGINES WERE RUN, PRESSURIZING AT 7 POUNDS OF DIFFERENTIAL PRESSURE. AIRCRAFT WAS REFUELED AND DISPATCHED AT FL 250. DURING OVERNIGHT CHECK AT MEX, BOTH AIR CONDITIONING SYSTEMS, REGULATOR VALVE, FLOW CONTROL VALVE, COOLING TURBINES, CHIP DETECTORS AND TEMPERATURE CONTROL VALVE WERE CHECKED, DETECTING A PNEUMATIC LEAK IN SENSOR LINE NR 1, SO BOTH SECOND SEGMENT SWITCHES WERE REPLACED AND TESTED IAW MM 21-31-09, NO LEAKS WERE FOUND.

Part: ACTUATOR — LEAKING (MLG) · airframe 37,021 hrs · 25,699 cycles

DURING TRANSIT CHECK IT WAS DETECTED A HYDRAULIC LEAK IN THE RIGHT MAIN LANDING GEAR ACTUATOR. THE ACTUATOR WAS REPLACED AND THE SYSTEM TESTED IAW M/M 32-32-00, BEING ALL CORRECT.

Part: CSD — FAILED (LEFT) · airframe 36,230 hrs · 25,177 cycles

AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING LT ENGINE STARTING, THE LT CSD TEMPERATURE INCREASED AND WENT OUT OF RANGE AND LOAD AC WITH 7. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK, THE LT CSD AND HEAT EXCHANGER AIR/OIL ASSY WERE REPLACED IAW MM 24-10-01, TESTED CORRECT.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 34,772 hrs · 24,162 cycles

DURING TRANSIT CHECK WAS DETECTED HYDRAULIC LEAK IN RIGHT WING. DURING REVISION IN RIGHT INBOARD SPOILER ACTUATOR LINE WAS DETECTED LEAKED, HYDRAULIC TUBE WAS REMOVED AND HYDRAULIC HOSE WAS INSTALLED IAW MM 20-12-04, TESTED CORRECT. DURING OVERNIGHT SERVICE, THE HYDRAULIC HOSE WAS REPLACED PER RIGHT PIPING ASSY HYDRAULIC GROUND SPOILER DOWN RIGHT SIDE IAW MM 27-61-07, TESTED CORRECT.

Part: PTU — FAILED (HYD SYSTEM) · airframe 34,310 hrs · 23,880 cycles

AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXING, RIGHT HYDRAULIC SYSTEM WAS FAILED. DURING REVISION, RIGHT HYDRAULIC PUMP CONTINUED INDICATING PRESSURE WHEN IT WAS SHUTOFF AND HYDRAULIC POWER TRANSFER UNIT (PTU) WAS DETECTED WITH FAIL. THE PTU WAS REPLACED IAW MM 29-10-08, TESTED CORRECT.

Part: TRANSMITTER — FAILED (LT ENGINE EPR) · airframe 34,159 hrs · 23,784 cycles

AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF LEFT ENGINE EPR'S WERE IN 1.2. EPR INDICATOR EGG WERE REPLACED IAW MM 77-11-01 AND 77-11-02 RESPECTIVELY, TESTED CORRECT. ENGINE WAS TESTED IAW MM 71-00-00, ALL CORRECT.

Part: START VALVE — INOPERATIVE (RT ENGINE) · airframe 33,000 hrs · 23,002 cycles

AIRCRAFT RETURNED TO PLATFORM, RT ENGINE DID NOT START. TECHNICAL PERSONNEL OPENED MANUALLY THE VALVE. AT GDL, PNEUMATIC LINE OF START VALVE WAS REPLACED IAW MM 80-10-01, ALL CORRECT.

Part: PITOT TUBE — DAMAGED (LT SIDE) · airframe 32,606 hrs · 22,716 cycles

AIRCRAFT RETURNED TO PLATFORM, (PITOT STALL HEAT OFF) LIGHT TURNED ON. DURING MAINTENANCE REVISION, CAPTAIN PITOT TUBE WAS DETECTED WITH DAMAGE, IT WAS REPLACED IAW MM 34-11-02, TEST CORRECT.

Part: RELAY — FAILED (GLIDE SLOPE) · airframe 31,802 hrs · 22,170 cycles

AIRCRAFT RETURNED TO PLATFORM DURING ENGINE START, VHF NAV NR 1 FAILED. VHF NR 1 CONTROL PANEL, DFGC AND VOR RECEPTOR WERE REPLACED AND FAIL CONTINUE. ENGINE WAS SHUTDOWN AND HIGH FREQUENCY ON LT GENERATOR WAS DETECTED. LT GENERATOR WAS INOPERATIVE AND AIRCRAFT WAS SENT TO THE HANGAR. DURING OVERNIGHT SERVICE, RELAY R2-47 WAS REPLACED IAW WDM 24-23-00 AND TEST WAS PERFORMED IAW MM 34-32-00, ALL CORRECT.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 31,096 hrs · 21,733 cycles

AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF HYDRAULIC PRESSURE ON LEFT ENGINE REACHED 4000 PSI AND DROPPED TO ZERO. THE HYDRAULIC PUMP WAS REPLACED IAW MM 29-10-05, TEST CORRECT.

Part: EXCITER — FAILED (LT ENGINE) · airframe 33,891 hrs · 23,608 cycles

WITH LEFT IGNITION SYSTEM IN OVERRIDE, THE LEFT ENGINE DID NOT START. THE CIRCUIT BREAKER C/B U42 WAS REESTABLISHED BUT FAILURE CONTINUED. THE LEFT IGNITION C/B WAS DEFERRED IAW MEL 74-A BUT DURING PUSH BACK, THE LEFT ENGINE IGNITION WAS OUT SERVICE AGAIN. THE LEFT SIDE EXCITER IGNITION WAS REPLACED IAW MM 74-10-01, TESTED CORRECT. DURING OVERNIGHT SERVICE, IGNITION SYSTEM WAS TESTED IAW MM 74-10-01, ALL CORRECT.

Part: STRUT — LEAKING (RT MLG)

DURING THE AIRCRAFT DISPATCH AT GDL STATION, THE TECHNICAL PERSONNEL SAW A LITTLE LEAK IN THE STRUT OF THE RT MLG. AT STATION , PERFORMED A VERIFICATION OF THIS LEAK. THE STRUT SEALS WERE CHANGED AND THE MLG WAS TESTED IAW MM, ALL CORRECT.

Part: STRAINER — FAILED (LT ENGINE)

AIRCRAFT RETURN TO PLATFORM DU TO FILTER OBSTRUCTED LT ENGINE LIGHT CAME ON. THE FILTER AND ALARM WERE REPLACED AND ALARM WAS CHECKED IAW MM 79-35-00/01 AND 71-00-01 RESPECTIVELY, ALL TESTS CORRECT.

Part: LINE — BROKEN (POTABLE WATER)

DURING TRANSIT CHECK WAS DETECTED POTABLE WATER LEAK, DRAINING TO THE ELECTRIC/ELECTRONIC COMPARTMENT. TCAS AND FDAU WERE WET. AIRCRAFT WAS SENT TO THE HANGAR. DURING REVISION WAS DETECTED NIPPLE AND SUPPLY LINE BROKEN THE 218 STATION. THE NIPPLE AND SUPPLY LINE WERE REPLACED, ALL TESTS CORRECT.

Part: ENGINE — FAILED (LEFT)

DURING CLIMB-OUT, NOTED LEFT ENGINE OIL PRESSURE WENT TO ZERO, TEMP WAS 58, QUANTITY WAS 16 QUARTS, TEMPERATURE SLOWLY DECREASED TO 40, HAD NO VIBRATIONS OR OTHER ABNORMAL INDICATIONS. ABOUT 10 MINUTES LATER LEFT ENGINE STARTED TO VIBRATE, IMMEDIATELY SHUT ENGINE DOWN, SHUTDOWN WAS NORMAL. ENGINE IS SCHEDULED FOR REMOVAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

CCI-LAX - MID CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED FUSE IN AFT OVERWING EXIT SIGN. OPS CHECK OK. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

CCI-LAX - ROW 17, 18, 19 AND 20 EMERGENCY AISLE LIGHTS INOPERATIVE. REPLACED BATTERY PACK LOCATED AFT RIGHT OVERWING EXIT ROW. OPS NORMAL. (M)

Part: POWER SUPPLY (CABIN)

CCI - RIGHT AFT OVERWING EMERGENCY EXIT IGHT BATTERY SUPPLY INOPERATIVE. REPLACED BATTERY SUPPLY. OPS CHECK GOOD. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

CCI-LAX - FOUND ROW 21, 22, 23, 24 EMERGENCY AISLE LIGHT INOPERATIVE. REPLACED LEFT BATERY PACK AT 19A, OPS NORMAL. (M)

Part: FUSE — BLOWN (CABIN)

CCI-SNA - EMERGENCY LIGHTING INOPERATIVE, RIGHT OVERWING SEAT LIGHTING. REPLACED FUSE IN BATTERY PACK. OPS CHECK GOOD. (M)

Part: CHARGER — INOPERATIVE (CABIN)

CCI-SNA - FOUND SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE ON SEATS 17D, 18D, 19D AND 20D. REPLACED SEGMENT BATTERY AND CHARGER, OPS CHECK OK. REF AALA016051. (M)

Part: BATTERY — INOPERATIVE

CCI-SNA - FOUND SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE ON SEATS 17D, 18D, 19D AND 20D. REPLACED SEGMENT BATTERY AND CHARGER, OPS CHECK OK. (M)

Part: BATTERY PACK — DISCHARGED (ROWS 17-20)

CCI-LAX - SEAT MOUNTED EMERGENCY EXIT LIGHTS AT ROWS 17, 18, 19 AND 20 NOT WORKING. INSTALLED NEW BATTERY PACK, ALL EMERGENCY LIGHTS WORK OK. (M)

Part: WIRE — BROKEN (AFT AIRSTAIR)

CCI-RNO - FOUND FORWARD OVERHEAD EMERGENCY LIGHT IN AFT STAIRWELL INOPERATIVE. REPAIRED BROKEN WIRE AT LIGHT ASSEMBLY. OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

CCI-LAX - RED EMERGENCY SEAT LIGHTS INOPERATIVE. REPLACED BATTERIES, OPS CHECK NORMAL. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

CCI-ROWS 13D-16D SEAT EMERGENCY LIGHTS OUT AND EMERGENCY LIGHT EXIT SIGN FWD OF THE LT FWD EMERGENCY EXIT DOOR INOPERATIVE.SECURED LOOSE CONNECTOR FOR SEAT 16D AND REPLACED BATTERY PACK, OPS CK OK

Part: CONNECTOR — UNSERVICEABLE (PATH LIGHTS)

CCI - FOUND SEAT 10D EMERGENCY LIGHT ON SEAT INOPERATIVE. FOUND LOOSE CONNECTION, RECONNECTED AS REQUIRED. OPS CHECK NORMAL. (M)

Part: WIRE — PINCHED (EXIT LIGHT)

LAX - EMERGENCY LIGHTS AT SEATS 13-16 AND EMERGENCY EXIT LIGHT AT SEAT 18AB INOPERATIVE. EMERGENCY EXIT LIGHT ASSY BLOWS FUSE. CONNECTORS AT SEATS 13 THROUGH 16 CHECKED OK FOR SECURITY. FOUND PINCHED WIRE. REPAIRED PER STD PRACTICES. EMERGENCY LIGHTS OPS CHECK NORMAL. (M)

Part: CONNECTOR — DAMAGED (EMPENNAGE)

RNO-CCI - E LIGHTS IN EMPENNAGE INOPERATIVE. REPLACED BAD CONNECTOR AND REWIRED PER BRUCE PATHFINDER MANUAL 400-079. OPS NORMAL. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

SJC-CCI - FORWARD SERVICE DOOR EMERGENCY PACK INOPERATIVE. REMOVED AND REPLACED FORWARD SERVICE DOOR BATTERY. OPS CHECK GOOD. (M)

Part: WIRE — DAMAGED (SEAT 12)

LAX - EMERGENCY LIGHT IN RIGHT SEAT 12 INOPERATIVE. REPAIRED WIRING, OPS CHECKED GOOD. (M)

Part: WIRE — BROKEN (ROW 25)

RNO - CCI EMERGENCY LIGHT AT 25 INOPERATIVE. REPAIRED BROKEN WIRE. OPS NORMAL. (M)

Part: WIRE — BROKEN (ROW 25)

RNO-CCI - EMERGENCY LEFT AT ROW 25 DEF INOPERATIVE. RESPLICED BROKE WIRE, OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

RNO - LT AFT OVERWING DOOR EMERGENCY LIGHT BATTERY PACK INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AS REQUIRED, OPS GOOD. (M)

Part: LIGHT — INOPERATIVE (TAIL)

RNO - TWO UPPER TAIL SLIDE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED CHARGER (AFT RT LAV, AFT CHARGER), OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (ROW 23-26)

EMERGENCY LIGHTS ROW 23 THROUGH 26 ILLUMINATED DURING FLIGHT, COULD NOT TURN THEM OFF WITH ANY SWITCH POSITION. REMOVED AND REPLACED EMERGENCY POWER PACK FOR ROWS 23 THROUGH 26 AS REQUIRED, OPS CHECKED GOOD. (M)

Part: BATTERY PACK — DISCHARGED (ROWS 22-26)

RNO - ROW 22-26 EMERGENCY LIGHTS INOPERATIVE. REPLACED LEFT AFT EXIT BATTERY PACK PER MM, OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (ROW 9-12)

EMERGENCY LIGHTS RT SIDE ROW 9, 10, 11, 12 CAME ON. REMOVED AND REPLACED BATTERY PACK IN EMERGENCY ROW 20, OPS CHECK GOOD AT THIS TIME PER MM 33-00-00. (M)

Part: BATTERY PACK — DISCHARGED (ROW 9-15)

EMERGENCY LIGHTS FOR ROWS 9-15 CAME ON IN FLIGHT, EXTINGUISHED PRIOR TO LANDING, NO LONGER WORKING. REMOVED AND REPLACED BATTERIES FOR BATTERY PACK OF EMERGENCY EXIT LIGHT OF RT EMERGENCY EXIT IAW 35-00. OPS CHECK GOOD. (M)

Part: POWER PACK — INOPERATIVE (ROWS 19-22)

E-LIGHTS INOPERABLE, ROWS 19-22. REMOVED AND REPLACED E-POWER PACK FOR ROWS 19-22. OPS CHECK GOOD. (X)

Part: POWER SUPPLY — INOPERATIVE (ROWS 27-29)

EMERGENCY LIGHTS AT ROWS 27-29 ON IN-FLIGHT. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS POWER SUPPLY AT LEFT EMERGENCY EXIT PER MM 25-50-04. OPS CHECK GOOD. (X)

Part: POWER SUPPLY — FAILED (OVERWING)

OKC - THE FOLLOWING EMERGENCY LIGHTS ARE INOPERATIVE, ROWS 10-18, LT FORWARD OVERWING, RT FORWARD OVERWING, LT OVERHEAD VERTICAL STAIRS. REMOVED AND REPLACED OVERWING POWER SUPPLY IAW MD-80 MM 33-53-00. OPS CHECK GOOD IAW MD80 MM 33-53-00. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

OKC - EMERGENCY LIGHTS INOPERATIVE AT ROW 27-29. REMOVED AND REPLACED BATTERY PACK FOR AFT CABIN DOOR EXIT ID. OPS CHECK GOOD IAW MD-80 MM 33-53-00. (M)

Part: BATTERY CHARGER — INOPERATIVE (CABIN)

AT LAX, REAR ROW EMERGENCY LIGHTS CAME ON AND STAYED ON DURING FLIGHT. REMOVED AND REPLACED LEFT AFT EMERGENCY LIGHT BATTERY CHARGER PER MM 33-00-00. (M)

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

AT LAX, EMERGENCY LIGHTS CAME ON DURING DESCENT AISLE ROW 15 THROUGH 18. REPLACED LEFT OVERWING BATTERY PACK ASSY. OPS CHECK NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

AT SJC, FIRST EMERGENCY EXIT LIGHTS ON. REMOVED AND REPLACED BATTERY PACK FROM FORWARD GALLEY. OPS CHECK GOOD AS PER 33-53-00. (M)

Part: BATTERY CHARGER — FAILED (ROW 8D)

AT RNO, EMERGENCY LIGHTS AT SEAT 8D INOPERATIVE, SEAT AND CEILING. RELAMPED CEILING LAMPS AND REPLACED FORWARD GALLEY EXIT EMERGENCY LIGHT CHARGER. OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (ROW 1-9)

AT SJC, AT SEATS AT ROWS 1 THROUGH 9 EMERGENCY EXIT LIGHTS NOPERATIVE. REMOVED AND REPLACED EMERGENCY PACK, LOCATED IN FORWARD GALLEY AS PER MM 33-24-00. OPS CHECK GOOD. (M)

Part: LIGHT — INOPERABLE (CABIN)

AT SJC, EMERGENCY LIGHTING LAST ROW FLOOR LAMP INOPERABLE. REPAIRED EMERGENCY LIGHTING AT LAST ROW SEAT LIGHT IAW MM 20-50-04. OPS CHECK GOOD. (M)

Part: POWER SUPPLY — INOPERATIVE (ROW 18)

AT SJC, EMERGENCY SEAT LIGHTING IS OFF AT 18 DEF. REMOVED AND REPLACED POWER SUPPLY ASSEMBLY IAW MM 33. OPS CHECK GOOD. (M)

Part: POWER PACK — INOPERATIVE (ROW 18 DEF)

AT SJC, EMERGENCY SEAT LIGHTING IS OFF AT 18 DEF. REMOVED AND REPLACED POWER SUPPLY ASSEMBLY IAW MM 33, OPS CHECK GOOD. (M)

Part: BATTERY PACK — INOPERATIVE (ROW 25-28)

AT LAX, EMERGENCY EXI TLIGHTS ON AT ROWS 25, 26, 27, 28. REPLACED BATTERY PACK WITH SPARE IN AFT STAIRWELL. OPS CHECK OK. (M)

Part: BATTERY CHARGER — INOPERATIVE (ROW 19-26)

AT LAX, EMERGENCY LIGHTS AT ROWS 19-26 OUT. REMOVED AND REPLACED 3 BATTERY CHARGERS AT 21A, 20A AND 21F. SYSTEM OPS CHECK GOOD. (M)

Part: BATTERY CHARGER — INOPERATIVE (ROW 19-26)

AT LAX, EMERGENCY LIGHTS AT ROWS 19-26 OUT. REMOVED AND REPLACED 3 EACH, BATTERY CHARGERS AT 21A, 20A AND 21F. SYSTEM OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (ROW 23-26)

AT LAX, EMERGENCY LIGHTS REMAIN ON AT ROWS 23-26. CAME ON AT 10,000 IN DESCENT. REMOVED AND REPLACED LEFT BATTERY PACK. SYSTEM OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (ROWS 22-26)

AT RNO, INFLIGHT EMERGENCY LIGHTS CAME ON AT ROWS 22-26. REPLACED LEFT AFT O/W EXIT SIGN BATTERY PACK ASSY. OPS CHECK OK. (M)

Part: WIRE — FAILED (ROW 29)

AT SJC, EMERGENCY LIGHT OUT AT SEAT 1, ROW 29. REWIRED EMERGENCY LIGHT. OPS CHECK GOOD. (M)

Part: WIRE — BROKEN (ROWS 28/29)

AT RNO, EMERGENCY LIGHTS INOPERABLE AT SEATS 28 AND 29 D-F. REWIRED CONNECTIONS. OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (ROWS 19-22)

AT SJC, EMERGENCY LIGHTS INOPERABLE AT ROWS 19 TO 22. REPAIRED CHAFED WIRINGS. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. (M)

Part: CHARGER — INOPERATIVE (SEAT 19)

AT SJC, ROWS 17-20 ESCAPE LIGHTS ARE INOPERABLE. FOUND AND REPAIRED SHORTED WIRE ON SEAT 19. INSTALLED NEW CHARGER. OPS CHECK GOOD. (M)

Part: BATTERY CHARGER — INOPERATIVE (ROW 17-20)

AT SJC, ROWS 17-20 ESCAPE LIGHTS INOPERABLE. FOUND AND REPAIRED SHORTED WIRE ON SEAT 19. INSTALLED NEW CHARGER. OPS CHECKS GOOD. (M)

Part: WIRE — BROKEN (ROW 12)

SJC - BROKEN WIRE TO EMERGENCY LIGHTS AT SEAT 12F. REPAIRED BROKEN WIRE AT SEAT 12F. OPS CHECK GOOD. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

AT SJC, AFT OVERWING EXIT LIGHTS WOULD NOT GO OFF. REMOVED AND REPLACED RIGHT AFT OVERWING EXIT BATTERY PACK. OPS CHECKS GOOD. (M)

Part: LIGHT — INOPERATIVE (ROW 2)

AT SJC, EMERGENCY LIGHT INOPERABLE AT ROW 2. REPLACED EMERGENCY LIGHT CABLE ASSEMBLY AT 2 DF. OPS CHECKS GOOD. (M)

Part: BATTERY PACK — DISCHARGED (ROW 21)

AT SEA, EMERGENCY LIGHTS WERE ON AT ROW 21 DEF. REPLACED BATTERY PACK AT 21D. OPS NORMAL. BAD BATTERY PACKS IN E/E. (M)

Part: BATTERY PACK — DISCHARGED (ROWS 19-22)

AT SJC, EMERGENCY LIGHTS AT ROWS 19, 20, 21, 22 INOPERABLE. REMOVED AND REPLACED BATTERY PACK ON RIGHT EXIT SIGN. (M)

Part: BATTERY — DISCHARGED (ROWS 16-20)

AT RENO, OVERHEAD EMERGENCY LIGHTS INOPERABLE FROM ROW 16 TO ROW 20. REMOVED AND REPLACED BATTERIES. (M)

Part: HARNESS — FAILED (ROW 23 DEF)

IN SJC, EMERGENCY LIGHTING ON SEAT 23 DEF INOPERATIVE. REMOVED AND REPLACED WIRING HARNESS, OPS CHECK OK. (M)

Part: CHARGER — FAILED (ROWS 20/21)

AT LAS, FLIGHT ATTENDANT REPORTED THAT EMERGENCY EXIT LIGHTS AT ROWS 20 AND 21 CAME ON IN FLIGHT AND COULD NOT BE TURNED OFF. REPLACED BATTERY CHARGER AT RIGHT AFT O/W EXIT. OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (ROWS 19-22)

AT RENO, CABIN EVACUATION LIGHTS AT ROWS 19-22 ILLUMINATED DURING FLIGHT. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT RIGHT AFT OVERWING DOOR. ALSO, CHECKED POWER TO BATTERY PACK, POWER OK. REPAIRED WIRES AT ROWS 21 AND 22. EMERGENCY LIGHT SYSTEM OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (ROWS 19-21)

AT LAS, RED EMERGENCY LIGHTS WILL NOT EXTINGUISH AT 19D, 20D AND 21D. INSTALLED NEW BATTERY PACK ON FORWARD RIGHT OVERWING EXIT. OPS CHECK NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (ROWS 19-22)

AT SJC, EMERGENCY LIGHTS INOPERABLE AT ROWS 19-22. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (SEATS 19/20/21)

AT LAS, TRACK LIGHTS WILL NOT EXTINGUISH AT 19D, 20D AND 21D. REMOVED AND REPLACED BATTERY PACK AT ROW 20. ALL EMERGENCY TRACK LIGHTS, OPS CHECK NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (ROW 23-26)

EMERGENCY LIGHTS INOPERABLE AT ROW 23-26, OCCURING AT RENO. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (ROW 19-22)

AT SJU, EMERGENCY LIGHTS ON ROWS 19, 20, 21, 22 FOUND INOPERATIVE. FOUND PACK TO BE BAD. REMOVED AND REPLACED WITH NEW PACK, ROW DEF. OPS CHECKS GOOD. (M)

Part: POWER PACK — INOPERATIVE (TAIL COMP)

AT SJC, REAR TAIL EMERGENCY LIGHT NO OPERATING. REPLACED BATTERIES AND ONE POWER PACK. EMERGENCY EXIT LIGHTS, TAIL STAIRWAY. REPAIRED ONE LIGHT HANGING LOOSE. OPS CHECK OK. (M)

Part: BATTERY — DISCHARGED (TAIL COMP)

AT SJC, REAR TAIL EMERGENCY LIGHT NO OPERATING. REPLACED BATTERIES AND ONE POWER PACK. EMERGENCY EXIT LIGHTS, TAIL STAIRWAY. REPAIRED ONE LIGHT HANGING LOOSE. OPS CHECK OK. (M)

Part: BATTERY — DISCHARGED (CABIN)

AT LAS VEGAS, RIGHT OVERWING EMERGENCY LIGHTS CAME ON DURING DESCENT AND WOULD NOT GO OUT. REPLACED RIGHT OVERWING EXIT EMERENCY LIGHTS BATTERIES WITH NEW. OPS CHECK NORMAL. (M)

Part: POWER SUPPLY — INOPERATIVE (ROW 23-26)

AT SJC, EMERGENCY EXIT LIGHTS AT ROWS 23-26 CAME ON, COULD NOT EXTINGUISH. INSTALLED NEW BATTERY ASSEMBLY. OPS CHECK GOOD AT ROWS 23-26. (M)

Part: BATTERY CHARGER — FAILED (CABIN)

AT SJC, FLOOR EMERGENCY EGRESS LIGHTS ILLUMINATED WITH SWITCH IN ARMED POSITION AT SEATS, 19, 20, 21 AND 22. REPLACED BATTERY CHARGER AND BATTERY PACK AT ROWS 19, 20, 21 AND 22. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SJC - EMERGENCY LIGHTS AT ROW 21 ILLUMINATE AT ALL TIMES. REMOVED BATTERY PACK RIGHT AFT EMERGENCY DOOR, OPS CHECK NORMAL. (M)

Part: CHARGER — FAILED (CABIN)

EMERGENCY FLOOR PATH, ROWS 19-21, AIRCRAFT RIGHT, CAME ON IN FLIGHT. STAYED ON 30 MINUTES AND WENT OUT. LIGHTS DO NOT TEST ON GROUND AT ORD. REPLACED BATTERY/CHARGER PACK FOR EMERGENCY FLOOR PATH LIGHTS AT RENO 21, SEAT F IAW BRUCE INDUSTRIES MM400-079. OPS CHECKED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS INOPERABLE AT ROWS 9-14 AND 21-25. REMOVED AND REPLACED EMERGENCY BATTERIES. OPS CHECK OK. (M)

Part: BATTERIES — DISCHARGED (CABIN)

LAST THREE ROWS AND AFT DOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERIES IN CHARGER. OPS CHECK GOOD. (M)

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS AT ROWS 11, 12, 13 - STAY ON. REPLACED BATTERY PACK FOR ROWS 11, 12, AND 13. OPS CHECK GOOD. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS IN ROWS 15-18 REMAIN ON WHEN EMERGENCY LIGHT SWITCH IS SELECTED TO OFF. REPLACED BATTERIES IN BATTERY PACK FOR ROW 15-18. OPS CHECK NORMAL. (M)

Part: CONNECTOR — FAILED (CABIN)

SEAT 26D (AISLE SEAT) EMERGENCY LIGHT INOPERATIVE. REPAIRED CONNECTOR ON BOTTOM OF SEAT. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

PRE-FLIGHT RNO, LEFT FORWARD OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED LEFT FORWARD OVERWING BATTERY PACK ASSY, OPS CHECK OK. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

RETURNED TO GATE DURING PUSH BACK EMERGENCY LIGHTING AT ROWS 16, 17, 18, 19 CAME ON COULD NOT BE EXTINGUISHED ALSO EMERGENCY EXIT LIGHT AT ROW 20 A/C LEFT CAME ON AND COULD NOT BE EXTINGUISHED. REPLACED LEFT FORWARD EMERGENCY EXIT SIGN BATTERY PACK ASSY AND REPAIRED SHORTED WIRING AT SEAT O/B LEGS AT ROW 17-19 RIGHT SIDE, OPS CHECK NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

OVERWING FORWARD LEFT EMERGENCY FLOOR LIGHTS POWER SUPPLY WON'T SHUT OFF EMERGENCY LIGHTS REMAIN ON UNTIL BATTERY EXHAUSTION. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECK GOOD AT THIS TIME. (M)

Part: BATTERY CHARGER — INOPERATIVE (CABIN)

ROWS 15-18 AIRCRAFT RIGHT EMERGENCY LIGHTS STAY ON IN ARMED POSITION 18, REST OF THE SYSTEM WORKS NORMALLY. REMOVED AND REPLACED BATTERY CHARGER AT SEAT 18A, SYSTEM OPS CHECK NORMAL. (M)

Part: COMPRESSOR — STALLED (NR 1 ENGINE)

LEFT ENGINE COMPRESSOR STALLED DURING TAKEOFF RUN SUSPECT ICE INGESTION DUE TO SEVERE WINTER CONDITIONS. INSPECTED NR 1 ENGINE INLET FAN AND EXHAUST AREAS, NO DAMAGED NOTED RAN NR 1 ENGINE TO TAKEOFF POWER AND PERFORMED ACCELERATION AND POWER ASSURANCE RUN NR 1 ENGINE PARAMETERS ARE NORMAL PER MM 71-00-00. (M)

Part: CHARGER — FAILED (CABIN)

EMERGENCY ESCAPE PATH LIGHTS IN ROWS 19, 20, 21, AND 22 ILLUMINATED WOULD NOT SHUT OFF UNTIL BATTERY PACK WAS DISCHARGED. INSTALLED NEW EMERGENCY PATH LIGHT BATTERY PACK CHARGER ROWS 19-22. OPS CHECK NORMAL IAW MM 33-00-00. (M)

Part: WIRE — BROKEN (CABIN)

EMERGENCY LIGHT AT SEAT 10 OUT. REPAIRED BROKEN WIRE ON EMERGENCY LIGHT, OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHT OUT IN ROW 14-18. REPLACED FUSE IN BATTERY PACK, OPS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

RIGHT FORWARD EMERGENCY EXIT LIGHT INOP. REPLACED RIGHT FORWARD EMERGENCY LIGHT ASSEMBLY. OPS CHECK NORMAL. (M)

Part: PUMP — FAILED (NR 2 ENGINE)

DURING CLIMB-OUT OF SJC, NOTED RT ENGINE HYD PUMP FAILURE. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYD PUMP PER MM 29-10-05. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FUSE — FAILED (CABIN)

FIRST PORTION OF COACH, EMERGENCY LIGHTS OUT. REPLACED FUSE AT RT FORWARD O/W EXIT SIGN. OPS NORMAL. AIRCRAFT RETURNED TO SERVICE. (X)

Part: WIRE — BROKEN (CABIN)

EMERGENCY LIGHT AT ROW 23 INOPERABLE. REPAIRED BROKEN WIRE AT SEAT 23 F. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BATTERIES — DISCHARGED (CABIN)

THREE EMERGENCY CEILING LIGHTS INOP AT REAR Y CABIN. REMOVED AND REPLACED BATTERIES IN BATTERY PACK IN CEILING OF THE AFT RIGHT LAVATORY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: WIRE — BROKEN (CABIN)

EMERGENCY LIGHTS AT ROWS 11, 23 AND 25 INOP. FOUND WIRE TO CONNECTOR BROKEN REPAIRED PER MM 33-50-01. ALL LIGHTS OPS CHECK OK. (M)

Part: CONNECTOR — LOOSE (CABIN)

SEAT 2D OR ROW 2, EMERGENCY LIGHT INOPERABLE. FOUND LOOSE CONNECTOR; RE-SNAPPED. OPS CHECK GOOD. (X)

Part: BURN BARRIER — INOPERATIVE (NR 1 ENGINE)

NR 1 ENGINE 'B' LOOP LIGHT ILLUMINATED, OPENED DMI 9187. CLEARED DMI NR 9187 ON 3/26/97. REMOVED AND REPLACED LOWER BURN THROUGH BARRIER ON 'B' LOOP, NR 1 ENGINE. (M)

Part: CONNECTOR — DAMAGED (NR 1 ENGINE)

NR 1 ENGINE 'B' LOOP COMES INTERMITTENTLY. CLEARED DMI NR 9166 ON 3/24/97. FOUND CANNON PLUG AT AMP DAMAGED. REMOVED AND REPLACED CANNON PLUG. OPS NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

NR-EMERGENCY LIGHTS OUT ON LEFT SIDE OF STAIRWAY. TROUBLESHOT SYSTEM IAW BRUCE IND DWG BR2013-R-870P. RESEATED ARM AND GROUND WIRES AT AFT VENTRAL FLOOD LIGHTS/POWER SUPPLY SYSTEM. OPS CHECK GOOD IAW BRUCE IND CHECK OUT MANUAL 400-082. (M)

Part: WIRE — BROKEN (CABIN)

EMERGENCY LIGHTS INOP AT ROW 26 DEF AND AT ROW 20 DEF. REATTACHED BROKEN WIRE AT LOWER FLOOR/SEAT ATTACH POINT. OPS CHECK NORMAL. (M)

Part: OIL FILTER — CLOGGED (RT ENGINE)

RETURNED TO GATE FOR LEFT OIL STRAINER CLOGGING LIGHT. REMOVED AND REPLACED RIGHT (NR2) ENGINE OIL AND OIL FILTER. LEAKS AND OPS CHECK NORMAL AT THIS TIME. (M)

Part: BATTERY — DISCHARGED (CABIN)

REMOVED LEFT FORWARD EMERGENCY EXIT LIGHT BATTERY PACK. INSTALLED LEFT FORWARD EMERGENCY EXIT LIGHT BATTERY PACK. (M)

Part: TIE BOLT — BROKEN (NR 4 MLG WHEEL)

REMOVED AND REPLACED NR 4 MAIN WHEEL ASSY (PN 26088911). REMOVED AND REPLACED NR 4 MAIN WHEEL ASSY DUE TO BROKEN TIE BOLT IAW MM 32. (X)

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY CEILING LIGHTING IN 1ST CLASS INOP. REPLACED BATTERY PACK AND OPS CHECKED GOOD. (X)