N882RA

Part: CHARGER — INOPERATIVE (CABIN)

SJC-CCI - FORWARD ENTRY E LIGHT BATTERY CHARGER INOPERATIVE. REMOVED AND REPLACED FORWARD ENTRY BATTERY CHARGER, OPS CHECK NORMAL. (M)

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

RNO-CCI - FORWARD EMERGENCY EXIT LIGHT NEON LAMP WON''T ILLUMINATE. REMOVED AND REPLACED LIGHT ASSEMBLY. (M)

Part: CHARGER — INOPERATIVE (FWD GALLEY)

RNO-CCI - FORWARD GALLEY EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED CHARGER, OPS CHECK GOOD. (M)

Part: POWER SUPPLY — INOPERATIVE (GALLEY)

ORD - TWENTY-FIVE MINUTES PRIOR TO LANDING FIRST ROW OF EMERGENCY LIGHTS ILLUMINATED IN CABIN NOW BURNED OUT, GALLEY TO ROW 15 A/C RT, ROW 5 WORKS. REPLACED FORWARD ENTRY DOOR POWER PACK EMERGENCY LIGHTS. OPS CHECKED NORMAL. (M)

Part: BATTERY — DISCHARGED (TAILCONE)

1 TAIL CONE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERIES IN CHARGER AS REQ. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS IN 1ST CLASS 1-4 INOPERATIVE, COACH 6-10 INOPERATIVE. REMOVED AND REPLACED L-1 POWER SUPPLY AND BATTERIES. SYSTEM OPS CHECKS NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SJC - BATTERY PACK AT RIGHT AFT 'E' EXIT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FROM AFT AUX CHARGER PACK, OPS CHECK GOOD. (M)

Part: BATTERY — DISCHARGED (FWD/AFT GALLEY)

SJC - EMERGENCY BATTERY PACKS ON FORWARD GALLEY AND AFT GALLEY INOPERATIVE. REMOVED AND REPLACED BATTERY PACKS ON FORWARD GALLEY AND AFT GALLEY. OPS CHECK GOOD. (M)

Part: POWER SUPPLY — UNSERVICEABLE (ROW 10)

SJC - EMERGENCY LIGHTS IN CABIN FROM SEAT ROW 10 ALL THE WAY FORWARD ARE ON. WE CANNOT EXTINGUISH THEM. REPLACED FORWARD ENTRY DOOR EMERGENCY LIGHT POWER SUPPLY. SYSTEM GROUND CHECKS NORMAL. (M)

Part: TANK — CRACKED (FWD LAV)

LAS - AFTER TAKEOFF, INCURRED MULITPLE ELECT MALFUNCTIONS. RETURNED IN IMC FOR OVERWEIGHT LANDING. LAV LEAK FORWARD LAV FLUID LEAKING INTO E/E. CLEANED EXCESS FLUID IN E/E FOUND LAV TANK CRACKED. FWD LAV ALREADY ON DMI. REF DMI NR 18672. ACCOMP RTS CU BOTH SIDES. REPLACED NR 1 AND NR 2 ENG GCUS AND BUS CONTROL PANEL RAN ENGINES ELECT SYSTEM. INST AND WARN LIGHTS GROUND ON GOOD. NO OVERWEIGHT LANDING INSPECTION REQUIRED PER MM 05-51-04 PAGE NR 609. A/C REQUIRES A FUNCTIONAL CHECK FLT. FUNCTIONAL CHECK FLT REQUIRED BECAUSE OF MULTIPLE ELECTRICAL MALFUNCTIONS. A/C HAS BEEN INSPECTED AND NO KNOWN CONDITIONS EXISTS THAT WOULD MAKE THIS A/C UNSAFE FOR A FUNCTIONAL CHECK FLT. ACCOMP INSPECTION OF A/C. NO

Part: BATTERIES — DISCHARGED (ROW 5DF)

RNO - FIRST CLASS 5DF AISLE EMERGENCY LIGHTS AND FORWARD GALLEY LIGHTS ARE 'ON' WITH ALL POWER OFF. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES, OPS CHECKED GOOD SEVERAL TIMES. (M)

Part: JAMB — CORRODED (PAX DOORWAY)

OKC - JUST AFT OF FORWARD ENTRANCE DOOR JAM HAS CORROSION. BLENDED OUT OF LIMITS IAW DC-9 SRM 51-01 MAT LOSS .030 FABRICATED NEW THRESHOLD DOOR JAM IAW DC-9 SRM 51-1002. TREATED AND PRIMED IAW DC-9 SRM 51-10-3. (M)

Part: BRAKE — FAILED (NR 1 BRAKE ASSY)

LAS-LAX - FLT 2803 - HEAVY BRAKING REQUIRED DURING TAXI FOR TAKEOFF. NR 1 BRAKE LOCKED UP, AIRCRAFT UNABLE TO TAXI UNDER POWER. AIRCRAFT TOWED TO GATE. REMOVED AND REPLACED NR 1 BRAKE ASSY PER MM 32-42-01. LEAK AND OPS CHECK GOOD. (M)

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

SJC - EMERGENCY LIGHTS INOPERATIVE ROW 21-24. REMOVED AND REPLACED BATTERY PACK LEFT ROW 24 PER MM 33-53-00. OPS CHECK GOOD. (M)

Part: CONNECTOR — LOOSE (ROW 17DEF)

RNO - EMERGENCY SEAT LIGHT AT 17 DEF, INOPERATIVE. FOUND LOOSE CONNECTOR RE-ATTACHED. OPS CHECK GOOD. (M)

Part: CONNECTOR — LOOSE (ROW 2)

RNO - ROW 2 EMERGENCY LIGHT INOPERABLE. RE-CONNECTED CONNECTOR, OPS CHECK GOOD IAW 33-53-01. (X)

Part: BATTERY PACK — DISCHARGED (ROWS 17-21)

LAX - (ON LANDING LAX) A SEGMENT OF EXIT ROW LIGHTING FROM SEATS 17D TO 21D ILLUMINATED. WILL NOT TURN OFF. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT 21F IAW MM 33-53-01. (X)

Part: BATTERY PACK — DISCHARGED (RT EMER EXIT)

IN LAS - EMERGENCY LIGHTS ROW 6-10 ON. REMOVED AND REPLACED EXIT BATTERY PACK AT FORWARD RIGHT O/W EMERGENCY EXIT PER MM 33-53-00 LIGHTS OPS CHECK NORMAL. (M)

Part: BATTERY PACK — DISCHARGED (ROW 6-10)

IN LAS, EMERGENCY LIGHTS ROWS 6-10 ON. REMOVED AND REPLACED EXIT BATTERY PACK AT FORWARD RIGHT O/W EMERGENCY EXIT PER MM 33-53-00. LIGHTS OPS CHECK NORMAL. (M)

Part: BATTERY CHARGER — INOPERATIVE (CABIN)

LAS - LAST SECTINO OF EMERGENCY LIGHTS CAME ON IN CRUISE. REMOVED AND REPLACED LEFT MAIN BATTERY CHARGER, SYSTEM OPS CHECK GOOD. (M)

Part: LIGHT — FAILED (ROW 17-20)

ORD - EMERGENCY LIGHTS ON RIGH SEATS ROWS 17-20 WOULD NOT GO OUT. REPLACED LIGHT MODULE AT LEFT EXIT LIGHT, ACCOMPLISHED CHECK, NO FAULTS. (M)

Part: BATTERY PACK — DISCHARGED (ROW 29-32)

RNO - EMERGENCY LIGHTS ROW 29 THROUGH 32 ILLUMINATED AND WILL NOT SHUT OFF. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK FOR ROW 29-32 IAW MM 33-00. OPS CHECK NORMAL, OK FOR SERVICE. (M)

Part: CHARGER — INOPERATIVE (ROW 29-32)

RNO - EMERGENCY EXIT LIGHTS AT ROWS 29, 30, 31 AND 32 INOP. REPLACED AFT BATTERY PACK CHARGER, OPS CHECK GOOD. (M)

Part: PIN — UNSECURED (ROW 23)

RNO - EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 23. RESECURED PIN IN WIRE TO LIGHT CONNECTION, OPS CHECK GOOD. (M)

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

RNO - ON DESCENT, EMERGENCY EXIT ROW LIGHTS CAME ON SECTION OF ROWS 17-20. REPLACED EMERGENCY BATTERY PACK LEFT AFT POSITIVE, OPS CHECK GOOD. (M)

Part: BATTERIES — DISCHARGED (CABIN)

TWO EMERGENCY LIGHTS OUT, ILLUMINATE TAIL CONE. REMOVED AND REPLACED BATTERIES IN BATTERY PACK. OPS CHECK GOOD. (M)

Part: WIRE — BROKEN (CABIN)

EMERGENCY SEAT TRACK LIGHT INOP AT 15 DEF. REMOVED AND REPLACED LAMP AND REPAIRED WIRING, OPS CHECK GOOD. (M)

Part: OIL SYSTEM — REQ'D SERVICE (LT ENGINE)

GATE RETURN FOR LEFT ENGINE OIL QTY LEFT OIL QUANTITY PRIOR TO START 9 QUARTS AFTER START 6 QUARTS. SERVICED LEFT ENGINE OIL QUANTITY TO APPROXIMATELY 8 QUARTS ENGINE OIL. (M)

Part: PROX SENSORS — OUT OF ADJUST (MLG)

GEAR DOOR OPEN LIGHT ILLUMINATED IN-FLIGHT. ENGINE HYDRAULIC PUMPS IN LO. RETURNED TO RENO. ADJUSTED MAIN LANDING GEAR DOOR PROXIMITY SENSORS PER MM 32-60-05. OPS CHECK NORMAL ON GROUND. AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — FAILED (NR 2)

LAS - NR 2 ENGINE WAS SHUT DOWN INFLIGHT DUE TO DECREASING OIL QTY AND PRESSURE. A/C LANDED AT LAS WITHOUT FURTHER INCIDENT. PRIOR TO ENGINE SHUT DOWN, OIL QTY WAS '0' AND OIL PRESSURE WAS 38 PSI. NR 2 ENGINE WAS AT IDLE FOR 3 MINUTES WITH ALL OTHER PARAMETERS NORMAL. NR 2 ENGINE WAS AT IDLE FOR 3 MINS WITH ALL OTHER PARAMETERS NORMAL. NR 2 ENGINE WINDMILLED FOR 10 MINS. MX INSPECTED NR 2 ENG UPON ARRIVAL AND DISCOVERED EXCESSIVE OIL WETTING IN THE TAILPIPE. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE. AIRCRAFT WAS RETURNED BACK TO SERVICE. (M)

Part: LPT SHAFT — TWISTED (NR 2 ENGINE)

NR 2 ENG WAS SHUT DOWN IN FLT DUE TO DECREASING OIL QTY AND PRESSURE. LANDED AT LAS W/O INCIDENT. PRIOR TO ENG SHUT DOWN, OIL QTY WAS '0' AND OIL PRESSURE WAS 38 PSI. NR 2 ENG WAS IDLE FOR 3 MINS WITH ALL OTHER PARAMETERS NORMAL. NR 2 ENG WINDMILLED FOR 10 MINS. MX INSPECTED NR 2 ENG UPON ARRIVAL AND DISCOVERED EXCESSIVE OIL WETTING IN THE TAILPIPE. MX REMOVED AND REPLACED NR 2 ENG. OIL QTY LOSS WAS RELATED TO A TWISTED LPT SHAFT FOUND DURING ENG DISASSEMBLY. ALL INDICATIONS ARE THAT THE LPT SHAFT RUBBED ON THE N2 CENTER TUBE WHICH CREATED EXCESSIVE FRICTION HEAT WITHIN THE SHAFT, SOFTENING THE MATERIAL WHICH EVENTUALLY TWISTED FROM TORSIONAL LOADS. (M)

Part: CIRCUIT BREAKER — DEFECTIVE (FORWARD GALLEY)

LARGE AMOUNT OF SMOKE APPEARED OUT OF WALL BEHIND FIRST OFFICER'S SEAT ON LANDING. INSPECTED PASSENGER OXYGEN MASK DROP SWITCH WIRING AND F/O'S ANTI-FOG WIRING, NO DEFECTS NOTED. INSEPCTED FORWARD GALLEY CIRCUIT BREAKER PANEL, FOUND WORK LIGHT CIRCUIT BREAKER DEFECTIVE. DISCONNECTED WIRING AND STOWED. ENTERED IN LOG AS DMI NR 9638 MEL 33-2, PER STANDARD PRACTICES. (X)

Part: SENSOR — OUT OF ADJUST (NLG)

NOSE GEAR UNSAFE LIGHT CAME ON AFTER LEVEL OFF AT 330. LIGHT STAYED ON FOR REMAINDER OF FLIGHT. WHEN GEAR WAS EXTENDED, 3 GREEN AND NORMAL EXTENSION. ONCE AIRCRAFT WAS TAXIED TO GATE AND A/C POWER WAS SWITCHED TO EXTERNAL POWER, THE RED UNSAFE NOSE GEAR LIGHT CAME BACK AND REMAINED ON. REVIEW OF PSEU SHOWS NOSE GEAR LOCKED SENSOR D1-32 AT FAULT. CLEANED AND ADJUSTED SENSOR SYSTEM. GROUND CHECKS NORMAL. NO FAULTS ON POWER SWITCH OUT. (M)

Part: SLIDE — LOW PRESSURE (PASSENGER DOOR)

REMOVE AND REPLACE PASSENGER DOOR EVACUATION SLIDE DUE TO LOW BOTTLE PRESSURE. REMOVED AND REPLACED PASSENGER DOOR EVACUATION SLIDE DUE TO LOW BOTTLE PRESSURE. (X)

Part: LOCK RING — CRACKED (C-1 BLADE)

FOUND C-1 BLADE LOCK RING BROKEN AT PULL HOLE APPROXIMATELY TWO INCHES FROM END. REPLACED C-1 BLADE LOCK RING. (M)