N879RA

Part: WIRE — LOOSE (COCKPIT)

PDX - DURING DESCENT INTO PDX, ONE LARGE SPARK WITH ASSOCIATED SOUND CAME FROM ABOVE CAPTAINS HEAD. A BURNING EMBER FROM THIS SPARK DROPPED FROM OVERHEAD ONTO FLOOR JUT BEHIND CAPTAINS KIT BAG STORAGE. SPARK APPEARED TO ORIGINATE NEAR CIRCUIT BREAKER LIGHT OVER CAPTAINS HEAD. FOUND LEFT CIRCUIT PANEL LIGHT SOCKET INTERMITTENTLY FLASHING ON AND OFF. REPLACED BULB, NO HELP. REMOVED LIGHT ASSEMBLY FROM CEILING AND INSPECTED INSULATION. NO SIGN OF OVERHEAT. FOUND CENTER TERMINAL LOOSE, TIGHTENED. SOME LIGHT STAYS ON STEADY. INSPECTED ALL OTHERS ADJACENT PANEL LIGHTS AND INSUALTION FOR OVERHEAT. ALL FOUND NORMAL. (M)

Part: WIRE — DISCONNECTED (ROW 8)

FOUND ROW 8 SEAT EMERGENCY LIGHT INOPERATIVE. REPLACED BULBS AND RECONNECTED WIRES AT ROW 8 EMERGENCY SEAT LIGHT, CHECKS GOOD. (M)

Part: BATTERY — INOPERATIVE (AFT LAVATORY)

FOUND EMERGENCY LIGHTS, SEVERAL FLOOD LIGHTS IN EMPANAGE, ARE OUT. REPLACE NICAD BATTERIES IN LEFT AFT LAVATORY CHARGERS. ALL CHECK GOOD. (M)

Part: SEPARATOR — FAILED (ACM BAY)

AFTER TAKEOFF, CABIN FILLED WITH SMOKE. IT LOOKED WHITE AND SMELLED LIKE MUSTY A/C. IT DISSIPATED AFTER A FEW MINUTES. THE SMELL CONTINUED THROUGH THE FLT. SEEMED TO INCREASE ON DESCENT. REPLACED WATER SEPARATOR BAGS PER MM. ACCOMPLISHED PACK BURN PER MM 21-20-01. NO FAULTS NOTED. A/C REQS FCF. REINSPECTED A/C FOLLOWING FCF FOR SMOKE IN CABIN. NO SMOKE NOTED. OK FOR SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (ROW 2 - 14)

RNO - SEVERAL OVERHEAD EMERGENCY LIGHTS ARE OUT BETWEEN ROWS 2 TO 14. REPLACED EMERGENCY BATTERY PACK BATTERIES. OPS NORMAL. (M)

Part: COALESCER — CONTAMINATED (AC BAY)

APPROXIMATELY ONE MINUTE AFTER TAKEOFF, F/A'S REPORTED SMELLING STRONG SMOLDERING LIKE SMELL IN CABIN. ALSO, SMELLED IN COCKPIT. EMERGENCY DECLARED. AIRCRAFT LANDED AT 132,000 POUNDS. INSPECTED AIRCRAFT AND FOUND OIL SMELL COMING FROM BOTH AIR CONNDITIONING PACKS. REPLACED BOTH COALESCER BAGS. NO OIL WAS FOUND IN BAGS. PERFORMED BURN-OUT PROCEDURE DUE TO STRONG SMELL REPORTS. RAN AIR CONDITION PACK FULL HOT AND COLD AT POWER. NO SMELL OR FUMES NOTED. INSPECTED RECIRCULATING FANS AND ACM. BOTH ARE NORMAL. LANDING WEIGHT IS WITHIN LIMITS. (X0

Part: MANIFOLD — FAILED (LT MLG WW)

RNO - THE RIGHT HYDRAULIC BRAKE PRESSURE INDICATOR DROPS TO 1500 PSI WITH ENGINE HYD PUMP IN LOW AND AUXILIAR PUMP OFF. REMOVED AND REPLACED RT ABS LANDING MANIFOLD IAW MM 32-44-03, OPS CHECK GOOD. (M)

Part: FLIGHT DIRECTOR — FAILED (LT/RT)

SJC - FLT 241 - RETURNED TO GATE, FLIGHT DIRECTORS ON BOTH SIDES INOPERATIVE, WHEN TAKEOFF/GO AROUND SWITCHES ENGAGED. PLACING BOTH FLIGHT DIRECTORS ON DMI AS PER 34-16 THIS AIRCRAFT IS NOT CATII DMI NR 16374 19552 LED. (M)

Part: BATTERIES — DISCHARGED (EMPENNAGE)

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

Part: WIRE — DISCONNECTED (ROWS 8-9)

SJC - EMERGENCY EXIT LIGHT OUT AT ROWS 8-9. RECONNECTED WIRING. OPS CHECK GOOD. (X)

Part: LIGHT — INOPERATIVE (CABIN)

ROWS 8-11 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT TRACK RIGHT FORWARD. (M)

Part: JAMB — CORRODED (CARGO DOOR)

NUMEROUS AREAS OF CORROSION AT AFT CARGO LOWER DOOR JAMB. AREAS OF CORROSION WERE REMOVED. AREAS OUT OF LIMITS WERE REPAIRED BY FABRICATING DOUBLER AND STRAP. PARTS WERE INSTALLED. ALL WORK PERFORMED IAW SRM 53-05, PAGES 173-174. (M)

Part: RELIEF VALVE — INOPERATIVE (LT ENG)

DURING TAXI, LEFT ENGINE OIL PRESSURE DROPPED BELOW 40 PSI. SHUT DOWN ENGINE, RETURNED TO GATE. REPLACED LEFT ENGINE OIL PRESSURE RELIEF VLV IAW WITH MM 79-20-03. OPS CHECK GOOD. (M)

Part: PRESS RELIEF VLV — FAILED (LT ENG)

DURING TAXI, LEFT ENGINE OIL PRESSURE DROPPED BELOW 40 PSI. SHUT DOWN ENGINE, RETURNED TO GATE. REPLACED LEFT ENGINE OIL PRESSURE RELIEF VALVE IAW MAINTENANCE MANUAL 79-20-03. OPS CHECK GOOD. (M)

Part: ATTACH BOLT — SHEARED (LT MLG ACT)

LEFT LANDING ACTUATOR LOWER LINK ATTACH BOLT SHEARED. REMOVED AND REPLACED LEFT MLG ACTUATOR LOWER LINK LOWER ATTACH BOLT. PART TOTAL CYCLES, 3,685.(X)

Part: WHEEL ASSEMBLY — BROKEN (NR 3 MLG)

ON WALK AROUND, FOUND BROKEN THROUGH BOLT ON NR 3 MAIN WHEEL. REPLACED NR 3 MAIN IN AW MM CHAPTER 32. (M)

Part: BOLT — BROKEN (NR 4 MAIN WHEEL)

NR 4 MAIN TIRE HAS BROKEN THROUGH-BOLT. REMOVED AND REPLACED NR 4 MAIN TIRE FOR BROKEN THROUGH-BOLT PER MM 32. (X)

Part: SKIN — CORRODED (FUSELAGE)

SURFACE CORROSION ON PRODUCTION SKIN SPLICE 3 FRAMES AFT OF L-1 DOOR CUT OUT BETWEEN 4TH AND 5TH STRINGERS BELOW CUSP. CLEANED AND TREATED AREA. IAW MD-80 SRM 51-10-3. (X)

Part: DISH — CORRODED (RADAR)

MINOR SURFACE CORROSION ON AFT FACE OF RADAR DISH. REMOVED MINOR CORROSION AND TREATED WITH ALODINE. REF SRM 51-10-3. (X)

Part: EEL BATT PACK — DISCHARGED (CABIN)

AFT OVER THE WING DOOR EXITS EMERGENCY LAMPS INOP. REMOVED AND REPLACED BATTERIES. OPS CHECK OK. (X)