N751RA

Part: LINE — CRACKED (HYDRAULIC SYS) · airframe 38,624 hrs · 26,407 cycles

AIRCRAFT PERFORMED AN UNSCHEDULED LANDING, HYDRAULIC LEAK ON RT SYSTEM. DURING MAINTENANCE REVISION, HYDRAULIC LEAK WAS DETECTED ON REAR CARGO COMPARTMENT AND HYDRAULIC FLEXIBLE LINE WAS INSTALLED TO THE RUDDER CONTROL SHUTOFF VALVE IAW MM 20-12-04, TEST CORRECT. DURING OVERNIGHT SERVICE, HYDRAULIC FLEXIBLE LINE WAS REPLACED AND SYSTEM WAS TESTED IAW MM 27-20-09, ALL CORRECT.

Part: SWITCH — DAMAGED · airframe 38,444 hrs · 26,274 cycles

AIRCRAFT RETURNED TO PLATFORM, DURING TAXING TAKE OFF ALARM WAS ON COULD NOT CANCEL IT. TECHNICAL PERSONNEL PERFORMED TAKE OFF CONFIGURATION TEST AND CHECK SLAT, FLAPS, AND SPOILERS, PARKING BRAKES, STABILIZER AND AURAL WARNING WERE CHECK BUT FAIL CONTINUED. DURING ELECTRICAL CHECK SWITCH S1-491 WAS DETECTED DAMAGED. IT WAS REPLACED IAW WDM 27-52-00 AND TESTED IAW MM 27-00-00, ALL CORRECT.

Part: CSD — MALFUNCTIONED (RT GENERATOR) · airframe 37,983 hrs · 25,941 cycles

CAPTAIN REPORTED, DURING CLIMB CSD TEMPERATURE INCREASED UNTIL INDICATOR RED SECTION, INCREASING RISE TEMPERATURE, SHUTTING OFF CSD. REPORT WAS DEFERRED IAW MEL 24-1-1 CAT B. ENGINES RUN TEST WAS PERFORMED AT TAKEOFF THRUST (1.7 OF EPR'S) DURING 10 MINUTES, REACHING 115 DEGREES (C) AND TEMP RISE 5, SYSTEM AND WIRING WERE CHECKED BEING CORRECT. CSD HARNESS WAS DETECTED WITH DAMAGES AND A CONNECTOR WAS LOOSENED. CSD HARNESS WAS REPLACED IAW MM 24-11-1, TESTS WERE CORRECT. AFTER TAKEOFF CAPTAIN REPORTED CSD SHUTOFF IAW HIGH TEMPERATURE. DURING OVERNIGHT SERVICE, RIGHT CSD AND HEAT EXCHANGER AIR/OIL WERE REPLACED IAW MM, A HOST WAS DETECTED WITH DAMAGES, SO IT WAS REPLACED AND ALL TESTS WERE CORRECT.

Part: CSD — FAILED (RT) · airframe 37,974 hrs · 25,935 cycles

CAPTAIN REPORTED THAT DURING CLIMB RT CSD REACH 180 DEGREES (C), BEING NOT POSSIBLE TO SHUTOFF AND R CSD OIL PRESS LOW LIGHT TURNED ON. ADDITIONALLY, DURING DESCEND WHEN THE APU WAS STARTED THE CSD TEMPERATURE COOL DOWN. TECHNICAL PERSONNEL PERFORMED CSD SHUTOFF TESTS CONFIRMING THE FAILURE. CSD AND RADIATOR WERE REPLACED IAW MM 24-10-01 AND 24-10-03 RESPECTIVELY, TESTS WERE CORRECT.

Part: AHRS — FAILED (LT SIDE) · airframe 37,901 hrs · 25,887 cycles

AIRCRAFT RETURNED TO PLATFORM, AHRU NR 1. AIRCRAFT WAS SENT TO THE HANGAR AND DURING CHECK WERE DETECTED RT RMI FLAGS. AHRU NR 1 WAS REPLACED AND DURING WORKS THE SAME FAILURE APPEARED ON RT SIDE. AHUR NR 2 AND FLUX VALVE WERE REPLACED IAW 34-21-10 AND 34-21-06. AHRU NR 1 WIRING WAS CHECKED WDM 34-22-01.

Part: CONTROL VALVE — DAMAGED (LE FLAPS) · airframe 37,893 hrs · 25,878 cycles

AIRCRAFT WAS SENT TO THE HANGAR TO ATTEND FLAPS DIFFERENCE INDICATIONS AND FLAPS DID NOT RETRACT COMPLETELY. FLAPS CONTROL VALVE AND INTERIOR FLAPS ACTUATORS WERE REPLACED IAW MM 27-50-01 AND 27-50-02, BUT FAIL CONTINUES. FLAPS CONTROL VALVE WAS REPLACED AGAIN AND FAIL WAS CORRECTED. DUE TO TESTS PERFORMING AUXILIARY HYDRAULIC PUMP WAS OVERHEATED. IT WAS REPLACED IAW 29-10-06, ALL TESTS WERE CORRECT.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 37,708 hrs · 25,750 cycles

CAPTAIN REPORTED REVERSE INOPERATIVE DUE TO -LT REVERSE ACCUMULATOR LOW- LIGHT ILLUMINATED. DURING CHECK HYDRAULIC LEAK WAS DETECTED IN ACCUMULATOR LINE. HYDRAULIC LINE WAS REPLACED IAW MM 78-31-04, ALL CORRECT. DURING REVERSE TEST, ACCUMULATOR PRESSURE INDICATED 3000 PSI AND DURING RETRACTED PRESSURE DROPPED TO INITIAL PRESSURE. REVERSE WAS DEFERRED IAW MEL 78-1.

Part: ACTUATOR — DAMAGED (RUDDER) · airframe 37,662 hrs · 25,718 cycles

DURING OVERNIGHT SERVICE, WHEN RUDDER TEST WAS PERFORMED, RUDDER PEDALS WERE HARD DURING OPERATION. RUDDER HYDRAULIC PACKAGE AND RUDDER SHUTOFF VALVE WERE REPLACED IAW MM 27-20-08 AND 27-20-05, TESTS CORRECT.

Part: TRANSMITTER — FAILED (EPR) · airframe 37,176 hrs · 25,383 cycles

AIRCRAFT SUSPENDED TAKE OFF AND RETURNED TO PLATFORM AS A CONSEQUENCE OF LOW TAKE OFF POWER ON RT ENGINE AND DURING TAXING RT ENGINE WITH STALLS. CAPTAIN REPORTED THAT PERFORMED TWO TAKE OFF INTENTS AND RT ENGINE DID NOT RESPOND. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE EPR TRANSMITTER WAS REPLACED IAW MM 77-11-02, TEST CORRECT. BOROSCOPE INSPECTION WAS PERFORMED ON 6A AND 7A STAGES OF HIGH COMPRESSOR, 1A AND 4A STAGES OF TURBINE SECTION AND IGV´S IAW MM 72-00-00, ALL CORRECT. REJECTED TAKE OFF INSPECTION WAS PERFORMED IAW MM 05-57-00 AND OPERATIONAL TESTS IN BOTH ENGINES WERE PERFORMED IAW MM 71-00-00, ALL CORRECT.

Part: WIRE — DAMAGED (SENSOR) · airframe 37,111 hrs · 25,338 cycles

CAPTAIN REPORTED THAT DURING DESCENT WITH ENGINES ON IDLE, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT TURNED ON. PROCEDURE WAS ACCOMPLISHED TURNING OFF THE LIGHT, BUT WITH AIR CONDITIONING SYSTEM ON, HP BLEED OF FLOW LIGHT TURNED ON AND AT 5000 FEET, AIRCRAFT WAS DEPRESSURIZED. DURING TEST ON GROUND BOTH PACKAGES WERE OUT OF SERVICE WITH DUCTS COVERS BROKEN AND WITH THE WIRING SENSOR TEMP HIGH LOOSEN DUE TO A PNEUMATIC LEAKAGE. DUCT WAS CORRECTLY INSTALLED AND WIRING WAS REPAIRED, TESTS WERE PERFORMED IN ACCORDANCE WITH MM 30-10-00 AND 21-00-00, ALL CORRECT.

Part: COOLING FAN — DAMAGED (CABIN) · airframe 36,829 hrs · 25,153 cycles

DURING OVERNIGHT SERVICE THE FAN CIRCUIT BREAKER WAS OFF. FANS WERE REPLACED IN ACCORDANCE WITH MM 21-50-03 AND SMOKE ODOR WAS DETECTED ON PASSENGER CABIN. AIRCRAFT WAS VENTILED AND WATER SEPARATOR COVERS WERE REPLACED. AFTER, AIR CONDITIONING SYSTEM WAS WORKING CORRECT.

Part: ENGINE — BIRD INGESTION

AIRCRAFT RETURNED TO GATE, AIRCRAFT WAS STRUCK BY BIRDS, AND THE CAPTAIN REPORTED THAT THE RIGHT ENGINE LIGHT OF 'STRAINER FILTER CLOGGING' CAME ON. AT GATE, AIRCRAFT WAS VISUALLY INSPECTED FOR DAMAGES IN NLG, SLATS, FLAPS, ENGINES. STABILIZER AND RADOME, ALL CORRECT. BOTH NLG BEAM LIGHTS WERE REPLACED IAW MM 33-41-00, THE ENGINE CHIPS DETECTORS AND THE ENGINE PARAMETERS WERE VERIFIED IAW MM 77-00-00, ALL CORRECT. (M)

Part: PUMP — FAILED (HYD PRESS)

FLT 136 - MEX-AGU - AIRCRAFT RETURNED TO PLATFORM DUE TO DURING ENGINE STARTING HYDRAULIC PRESSURE DROPPED TO ZERO. HYDRAULIC PRESSURE PUMP WAS REPLACED IAW MM 29-10-05, ALL CORRECT. (M0

Part: STRAINER — CLOGGED (RT ENGINE)

AIRCRAFT RETURNED TO GATE DUE TO THE 'RT OIL STRAINER CLOGGING' CAME ON. STRAINER ASSY RESTRICTOR UNITS LPG AND LP5 AND THE OIL FILTER DIFFERENTIAL SWITCH WERE REPLACED AND THE ENGINE WAS TESTED IAW MM 79-35-01, 79-36-01 AND 79-20-06, ALL CORRECT. (M)

Part: RECEIVER — FAILED (VOR SYSTEM)

AIRCRAFT RETURNED TO PLATFORM, DURING TAXING. VOR FLAGS ON RDMI INSIGHT IN BOTH INSTRUMENTS. TX RX VOR/ILS WAS REPLACED BUT FAIL CONTINUED. RETURN TO SERVICE TEST WAS PERFORMED SHOWING 375 FAILURE CODE (VOR/DFGC FAILURE). AIRCRAFT WAS SENT TO THE HANGAR WHERE BOTH TX RX VOR/ILS WERE REPLACED IAW MM 34-32-02.(K)

Part: ENGINE — DAMAGED (NR 1)

AIRCRAFT ARRIVED WITH ONE BLADE OF LEFT ENGINE C1 DISK WITH DAMAGES OUT OF LIMITS. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE THE LEFT ENGINE WAS REPLACED IAW MM 71-00-00, TESTS CORRECT.(K)

Part: INDICATOR — MALFUNCTIONED (COCKPIT)

FLT 419 - IAH-MEX - AIRTURN BACK, LOST NAVIGATION INSTRUMENTS INDICATIONS. REFUEL WAS PERFORMED AND AIRCRAFT TAKEOFF WITHIN PROBLEMS. DURING OVERNIGHT SERVICE, ALL CORRECT. (M)

Part: CONNECTOR — LOOSE (ANTI-SKID SYS)

MEX-MTY - FLT 920 - AIRCRAFT RETURNED TO PLATFORM, BOTH ANTI-SKID LIGHTS CAME ON. DURING REVISION, DETECTED THE INTERIOR LEFT CONNECTOR VALVE LOOSE. THE WIRING WAS CHECKED AND CONNECTOR WAS CLEANED AND RECONNECTED IAW 32-43-00, ALL TESTS CORRECT. (M)

Part: CONTROL VALVE — FAILED (ANTI-SKID SYS)

FLT 263 - REX-MEX - RETURNED TO PLATFORM. DURING TAXI, ANTI-SKID LIGHTS CAME ON, BREAKERS WERE RESEATED IN-CORRECTLY. DURING REVISION ON CONNECTOR, DETECTED FAILURE OF DUAL PRESS CONTROL VALVE. THE CONNECTOR WAS CLEANED IAW 32-43-02, ALL TESTS CORRECT. DURING OVERNIGHT SERVICE, THE DUAL PRESSURE CONTROL VALVE AT LEFT EXTERIOR SIDE WAS REPLACED IAW 32-43-02, ALL TESTS CORRECT. (M)

Part: FAIRING — DAMAGED (RT WING)

AFTER MAKING HIS ROUTINE CHECK-UP TO BE IN POOR CONDTIONS, RIGHT WING NR 4 INBOARD FLAP ACCESS FAIRING, CANOE, DEEP SCRATCHES, PAINT CHIPPED, HAD A SMALL AIR BUBBLE ON THE SURFACE AND IN NUMEROUS PLACES THE WAS CHIPPED OFF. IN ATTENTION TO THE REPORTS THE FAIRING AND RADOME WERE REPAIRED IAW SRM 51-10-3B AND THE ACTUATOR FLAP WAS REWORKED IAW 53-10-01, ALL CORRECT. (M)

Part: CONTROL VALVE — FAILED (ANTI-SKID SYS)

FLT 464 - CUL-HMO - AIRCRAFT RETURNED TO PLATFORM, DURING TAXI ANTI-SKID LIGHTS CAME ON. DURING REVISION, DETECTED FAILURE OF DUAL PRESS CONTROL VALVE. THE DUAL PRESSURE CONTROL VALVE AT LEFT INTERIOR SIDE WAS REPLACED IAW MM 32-43-02, ALL TESTS CORRECT. (M)

Part: RELAY — FAILED (SPOILERS)

AIRCRAFT ABORTED TAKEOFF AND RETURNED TO PLATFORM DUE TO WARNING LIGHT (SPOILER DEPLOYED) ON. AT PLATFORM TECH VERIFIED SENSORS AND SPOILER PANELS, ALL WERE OK. THERE WAS PERFORMED A BITE TO THE PSU AND NO FAULT CODE APPEARS. AIRCRAFT WAS DISPATCHED BY MEL. THE RELAY (PN R2-241 WAS REPLACED IAW WDM, SPOILERS WERE TESTED IAW MM.

Part: COVER — MISSING (RT ENGINE) · airframe 39,505 hrs · 27,000 cycles

DURING TRANSIT CHECK WAS DETECTED RIGHT ENGINE WITH COVER MISSING IN SECONDARY FLOW FAIRING. THE COVER WAS REMOVED AND THE RIGHT ENGINE WAS CHECKED BEING ON OPERATION AT LIMITS IAW P&W MM 72-00-00, INSPECTION CHECK 01 PAGE 649 ITEM 2. THE COVER WAS INSTALLED, ALL CORRECT.

Part: CONTROLLER — FAILED (CABIN PRESSURE)

MEX-IAH - FLT 418 - AT ARRIVING CAPTAIN INFORMED A REPETITIVE REPORT RELATED WITH PRESSURIZATION, DFW TECHNICIAN INFORMED TO FAA AUTHORITIES. IT WAS PERFORMED A BITE TO BOTH PRESSURE CONTROLS, GIVING AS A RESULT AN ACTUATOR FAIL, IT WAS CHANGED DURING TRANSIT CHECK. AT MEX RON, ELECTRONIC PERSONNEL CONFIRMED AIRCRAFT WITHOUT REPORTS AFTER CHANGE. TESTS OK IAW MM 21-32-5. (M)

Part: SLIDE — DISLODGED (PAX DOOR)

RNO - DOOR L-1 SLIDE CAME OFF DOOR. REMOVED AND REPLACED L1 SLIDE PER MM, P/N D29982-113 S/N OFF 1823, S/N ON 0472. (M)

Part: CONNECTOR — DAMAGED (MLG TRANSDUCER)

WHEEL NOT TURNING LIGHT ILLUMINATED VERY EARLY IN THE TAKEOFF ROLL. RETURNED TO GATE. FOUND AND REPAIRED BROKEN PIN ON TRANSDUCER CANNON PLUG (PIN A). SYSTEM OPS CHECK NORMAL IAW MM. (X)

Part: POWER SUPPLY — FAILED (CABIN)

RNO - EMERGENCY EXIT LIGHTS ON RIGHT SIDE BY EMERGENCY EXIT SIGNS OUT. REMOVED AND REPLACED EMERGENCY LIGHT PACK AT AFT RIGHT EXIT ROW. OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (EMPENNAGE)

RNO - EMERGENCY LIGHT IN EMPENNAGE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT PACK, OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SJC - EMPENNAGE 'E' PATH LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M)

Part: FUEL CONTROL — OUT OF ADJUST (NR 2 ENGINE)

RNO - RETURN TO GATE ABORTED TAKEOFF AT ABOUT 30 KNOTS RIGHT ENGINE SLOW TO SPOOL. T/S PER 72-00-04 FIG 114, FOUND BOTH ENGINE IDLES LOW. RETRIM BOTH ENGINE PER 72-00-00. OPS CHECK NORMAL. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SEVERAL EMERGENCY LIGHTS OUT IN AFT CABIN. CHANGED POWER SUPPLY 33-53-00. OPS CHECK NORMAL.

Part: POWER SUPPLY — INOPERABLE (CABIN)

RNO - SEVERAL EMERGENCY LIGHTS OUT IN AFT CABIN. CHANGED POWER SUPPLY 33-53-00. OPS CHECK GOOD. (X)

Part: BATTERIES — DISCHARGED (CABIN)

AT RNO, SEVERAL CABIN EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED BATTERIES. OPS CHECK GOOD. (M)

Part: SIGN — FAILED (CABIN)

AT PHX, LEFT DIVIDER WALL (EXTERNAL), FIRST CLASS AND COACH EMERGENCY EXIT SIGN FAILED LUMINOSITY CHECK. REMOVED AND REPLACED LEFT DIVIDER WALL AT FIRST CLASS AND COACH EMERGENCY EXIT SIGN PER MM 11-00-01. SIGN REPLACED AND RETESTED, INSPECTION APPROVED. (M)

Part: BATTERY PACK — DISCHARGED (ROWS 9-26)

AT PHOENIX, FLOOR PROXIMITY LIGHTING IS OUT FROM SECTINOS 9-26, IN NEED OF TROUBLESHOOTING AND REPAIR. REMOVED AND REPLACED BATTERIES IN BATTERY PACKS. ALL SEAT LIGHTING WORKS WELL AS PER MM 33-53-00. (M)

Part: BATTERY PACK — DISCHARGED (TAIL CONE)

AT SJC, TAIL CONE LIGHTS (ESCAPE) INOPERABLE. RELAMPED BATTERY PACK EMERGENCY ESCAPE LIGHTS. OPS CHECK GOOD. (M)

Part: ACTUATOR — MALFUNCTIONED (TE FLAP)

AT SEATTLE, GATE RETURN, FLAPS DROPPED TO ABOUT 20 DEGREES WHILE AT GATES, AFTER ENGINE START WITH HYD AUS AND TRANS FOR PUMP ON AND ENGINE PUMPS BOTH ON HIGH, FLAPS WOULD NOT MOVE (STILL 20-25 DEGREES) WITH FLAP HANDLE UP/RET. AFTER SEVERAL ATTEMPTS (10 TO 20 CYCLES) FLAPS FINALLY RETRACTED TO UP/RET. REMOVED AND REPLACED BOTH FLAP 2-SPEED CONTROL VALVES AND RT NR 3 FLAP ACTUATOR PER MM. LEAK AND OPS CHECK GOOD. PERFORMED FLAP OPS CHECK PER 27-52-03. FLAPS OPERATE WITHIN LIMITS. OK FOR CONTINUED SERVICE. (M)

Part: VALVE — MALFUNCTIONED (TE FLAP)

AT SEATTLE, GATE RETURN, FLAPS DROPPED TO ABOUT 20 DEGREES WHILE AT GATES, AFTER ENGINE START WITH HYD AUS AND TRANS FOR PUMP ON AND ENGINE PUMPS BOTH ON HIGH, FLAPS WOULD NOT MOVE (STILL 20-25 DEGREES) WITH FLAP HANDLE UP/RET. AFTER SEVERAL ATTEMPTS (10 TO 20 CYCLES) FLAPS FINALLY RETRACTED TO UP/RET. REMOVED AND REPLACED BOTH FLAP 2-SPEED CONTROL VALVES AND RT NR 3 FLAP ACTUATOR PER MM. LEAK AND OPS CHECK GOOD. PERFORMED FLAP OPS CHECK PER 27-52-03. FLAPS OPERATE WITHIN LIMITS. OK FOR CONTINUED SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

AT SJC, EMERGENCY LIGHTS INOPERATIVE, ROWS 20-23. REMOVED AND REPLACED R/A AG BATTERY PACK/CHARGER. OPS CHECK GOOD. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

TAILCONE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED VENTRAL STAIR BATTERY PACK. OPS CHECK GOOD. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED OVERWING EMERGENCY LIGHTS POWER SUPPLY. OPS CEHCK GOOD PER MM. (M)

Part: ANGLE — CORRODED (FWD LAVATORY)

LEVEL 2 CORROSION, FOUND AT FWD LAVATORY, FWD LAVATORY WALL TO FLOOR ANGLE. INSTALLED NEW ANGLE IAW EA 13-25-EA 009. (M)

Part: ANGLE — CORRODED (CARGO COMPT)

LEVEL 2 CORROSION, FOUND MID PIT FLOOR SUPPORT ANGLE AT DOOR OPENING. FABRICATED DOUBLERS IAW MD80 SRM 53-01 FIG 2. INSTALLED DOUBLERS IAW 51-70-2 AND 51-30-5. (M)

Part: ANGLES — CORRODED (CARGO COMPT)

LEVEL 2 CORROSION, FOUND ON FWD PIT DOOR SEAL DEPRESSOR, LOWER DOOR OPENING, FWD AND AFT SPLICE DOUBLERS. FABRICATED AND INSTALLED NEW ANGLES IAW SRM 51-10-2. (M)

Part: WEB — CORRODED (CARGO DOOR)

LEVEL 2 CORROSION, FOUND AT SURFACE ON WEB FORWARD OF AFT PIT DOOR 24-27L. REMOVED LIGHT CORROSION (LESS THAN .004 MATERIAL REMOVED) ON WEB FORWARD OF AFT PIT DOOR IAW DC9 SRM 51-10-3. TREATED AND PRIMED IAW DC9 SRM 51-10-3. (M)

Part: GUSSETT — CORRODED (BS 1155-1212)

LEVEL 2 CORROSION, FOUND ON WEB STATION 1155-1212 AFT CARGO DOOR CUTOUT. REMOVED AND REPLACED GUSSET IAW DC9 SRM 51-10-2. (M)

Part: WASHERS — CORRODED (BS 1212)

LEVEL 2 CORROSION, FOUND ON HI-LOCK WASHERS AFT OF BS 1212. REMOVED AND REPLACED CORRODED WASHERS IAW DC9 SRM 51-30-1. (M)

Part: STRAP — CORRODED (CABIN DOORWAY)

LEVEL 2 CORROSION, FOUND ON FORE TO AFT STRAP AT INBOARD EDGE OF L1 DOOR THRESHOLD. REMOVED STRAP, FABRICATED NEW ONE IAW DC9 SRM 51-10-2. TREATED PRIMED AND INSTALLED IAW DC9 SRM 51-30-1 AND 51-30-1. (M)

Part: ANGLE — CORRODED (CABIN)

LEVEL 2 CORROSION, FOUND G2 GALLEY UNDER TOP SHELF OF TABLE. REMOVED CORROSION FROM UNDERSIDE OF TOP SHELF AND FABRICATED NEW 'A' ANGLE AND INSTALLED IAW DC9 SRM 51-00, 51-30-1, AND 51-10-03. (M)

Part: WIRE — BROKEN (CABIN)

FIRST THREE FLOOR TRACK EMERGENCY LIGHTS INOP. RE-SPLICED WIRE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS AT FORWARD OVERWING EXIT DOORS OUT. INSTALLED NEW NICAD IN BATTERY PACK. OPS CHECK GOOD. (X)

Part: BULB — MISSING (CABIN)

EMERGENCY LIGHT LENS AND BULB MISSING AT ROWS 1 AND 21. INSTALLED BULB AND LENSES AT ROW 1 AND 21. (M)

Part: BATTERY — DISCHARGED (CABIN)

AFT EMERGENCY OVERWING EXIT LIGHTS INOPERABLE. REPLACED BATTERIES FOR AFT OVERWING EXIT LIGHTS.

Part: LIGHT — BROKEN (CABIN)

EMERGENCY FLOOR EGRESS LIGHT BROKEN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IN ROW 7. OPS CHECK GOOD. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY AISLE LIGHTS WILL NOT LIGHT WITH SWITCH IN 'ON' POSITION. REMOVED AND REPLACED AFT EMERGENCY LIGHT POWER SUPPLY. AISLE LIGHTS OPS NORMAL. (M)

Part: BATTERIES — DISCHARGED (CABIN)

AFT OVERHEAD EMERGENCY LIGHT IN EMPANNAGE INOP. INSTALLED NEW BATTERIES. OPS CHECKS NORMAL. (M)

Part: LENS — MISSING (CABIN)

THREE FLOOR EMERGENCY TRACK LIGHT LENSES MISSING. REPLACED MISSING LENSES IN FLOOR EMERGENCY LIGHTS. (X)

Part: LENS — MISSING (CABIN)

'E' PATH LAMP AT ROW 26 MISSING A LENS. INSTALLED A NEW LENS FOR 'E' PATH LAMP AT ROW 26. (X)

Part: BATTERY — DISCHARGED (EMPENNAGE)

EMPENNAGE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY. OPS CHECKS GOOD. (X)

Part: EEL BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS, ON THE FORWARD OVER THE WING EXIT LIGHTS, DO NOT ILLUMINATE WITH EMERGENCY POWER ON. REMOVED AND REPLACED EMERGENCY BATTERIES. OPS CHECK GOOD. (M)

Part: START VALVE — FAILED (NR 2 ENGINE)

RIGHT START VALVE OPEN LIGHT ON IN FLIGHT. RETURNED TO SJC. REMOVED AND REPLACED NR 2 ENGINE START VALVE. OPS AND LEAK CHECK GOOD PER MM 80-10-01. (M)

Part: FLASHLIGHT — INOP (FWD EMERG)

FOUND INBD FWD EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY, OPS CHECKED GOOD. (X)