N822RA

Part: WIRE — DAMAGED (TAIL)

CCI - THREE EMERGENCY LIGHTS INOPERATIVE IN TAIL. REPAIRED BROKEN WIRES, BATTERY PACK IN TAIL. (M)

Part: BATTERY PACK — INOPERATIVE (OVERWING)

RNO-CCI - EXTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR EXTERIOR OVERWING EMERGENCY LIGHT CHECKED OK. (M)

Part: WIRE — BROKEN (CHARGER)

RNO-CCI - EMERGENCY LIGHT IN TAIL CATWALK INOPERATIVE. REPAIRED BROKEN WIRE AT CHARGER. OPS CHECK GOOD. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

LAX-CCI - FIRST CLASS EMERGENCY LIGHTS DIM TO TEST. REPLACED BATTERY PACK. (M)

Part: HARNESS — DAMAGED (ROW 25)

RNO - FA REPORTS EMERGENCY LIGHTS ON ROWS 26, 27 AND 28 WITH SWITCH IN ARM. FOUND SHORTED WIRE. REPLACED BAD HARNESS AT ROW 25 DEF. SYSTEM OPS CHECKS GOOD. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

LAX-CCI - INSEAT EMERGENCY LIGHTS IN SEATS 25 THROUGH 28 INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK NORMAL. (M)

Part: SLIDE — DISLODGED (GALLEY)

RNO - AFT GALLEY EVAC SLIDE PACK FALLS OUT OF DOOR. REMOVED AND REPLACED AFT GALLEY SLIDE PER MM. (M)

Part: BATTERY CHARGER — INOPERATIVE (ROW 12/14/15/17)

SJC - EMERGENCY PATH LIGHTS OUT IN ROWS 12, 14, 15 AND 17. CHANGED BATTERY PACK FOR EMERGENCY PATH LIGHTS. OPS CHECK GOOD. (M)

Part: BATTERY — DISCHARGED (CABIN)

RECHARGE LIGHTS ON FLIGHT ATTENDANT EMERGENCY FLASHLIGHTS NOT BLINKING. REMOVED AND REPLACED BATTERY ASSY. ALL FLIGHT ATTENDANTS FLASHLIGHTS OPS CHECK OK. (X)

Part: ENGINE — FIRE (NR 1 ENGINE)

RNO - STARTED NR 1 ENGINE DURING PUSH BACK INFORMED BY GROUND NR 1 ENGINE ON FIRE, CUT FUEL AND IGNITION, MOTORED AND DISCHARGED NR 1 BOTTLE. INSPECTED ENGINE PER MM 70-00-00 PAGE 263. ENGINE NR 1 HAD A TAILPIPE FIRE, FOUND EXHAUST ACOUSTIC PANEL DAMAGED 21 INCH BY 14 INCH. REMOVED LOOSE DEBRIS, PERFORMED TAKEOFF POWER ASSURANCE CHECK. BOTH NR 1 AND NR 2 ENGINES OPS CHECK NORMAL PER MM 71-00-00 PAGE 533. ENGINE CHANGED IN RENO. (M)

Part: POWER SUPPLY — INOPERATIVE (FUSELAGE)

RNO - EXTERIOR LEFT AND RIGHT EMERGENCY LIGHTS NOT WORKING. REMOVED AND REPLACED OVERWING 'E' LIGHTS POWER SUPPLY, OPS CHECK GOOD. (M)

Part: OVERHEAT LOOP — MALFUNCTIONED (TAIL COMPT)

FROM RENO, AIR TURNBACK TO RENO, TAIL COMPT TEMP HIGH LIGHT CAME ON AFTER TAKEOFF. STAYED ON FOR 3 MINUTES. WENT OUT ON FIRST POWER REDUCTION. RAN ENGINES NR 1 AND NR 2 AND APU AT TAKEOFF POWER 3 TIMES. COULD NOT DUPLICATE TAIL TEMP HIGH LIGHT AT THIS TIME. SYSTEM OPS CHECKS NORMAL, AND NO LEAKS NOTED. (M)

Part: BATTERIES — DISCHARGED (CABIN)

RNO - O/H EMERGENCY LIGHTS INOP BETWEEN ROWS 18A-21AC, LEFT SIDE. REMOVED AND REPLACED BATTERIES, OPS CHECK OK. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SJC - LEFT AND RIGHT AFT EMERGENCY EXI TLIGHTS INOP, UPPER. REMOVED AND REPLACED AFT EMERGENCY BATTERY PACK, OPS CHECK NORMAL. (M)

Part: DETECTOR — MALFUNCTIONED (TAIL COMP)

RETURN TO RENO, TAIL COMPT TEMP HI LIGHT CAME ON FOR 2 MINUTES AFTER TAKEOFF. OPERATING WITH LEFT THROTTLE RETARDED FOR 2 MINUTES, LIGHT WENT OUT. RESTORED THROTTLE AND TURNED LT PACK OFF. LIGHT CAME ON, THEN WENT OUT. PERFORMED MAINTENANCE ENGINE RUN PER MM 36-10-00, MODE 1, WITH LT PACK DISCONNECT FOR 5 MINUTES. RECONNECTED LT PACK, RAN FOR 5 MINUTES AT HIGH POWER. DID NOT GET LIGHT AT ANYTIME. SUSPECT WHEN PILOT WANTED GROUND START CART HOOKED UP TO AUGMENT APU AIR TO COOL A/C THAT IT OVERTEMPED TAIL COMPARTMENT. (M)

Part: DUCT — CRACKED (A/C MACHINE)

AIR TURN BACK DUE TO TAIL COMPARTMENT TEMP HIGH LIGHT CAME ON DURING CLIMB. COMPLIED WITH EMERGENCY PROCEDURES. COULD EXTINGUISH LIGHT WITH POWER REDUCTION ONLY AND SO RETURNED FOR PRECAUTIONARY LANDING. FOUND CRACKED DUCT ABOVE A/C MACHINE AFT SIDE RT, ASSIGNED TO DMI 13988 PER MEL 21-1. A/C IS SINGLE PACK OPERATION. REMOVED AND REPLACED RT ACM, DMI 13988 CLOSED. (M)

Part: FUEL CONTROL — MALFUNCTIONED (RT ENGINE)

ENGINE SHUT DOWN DUE TO THE FACT THAT THE RIGHT ENIGNE WOULD NOT IDLE BELOW 68 PERCENT N2. ENTERED DMI NR 13546. (M)

Part: WINDSHIELD — FAILED (CTR COCKPIT)

AIR RETURN TO LAS, CLIMBING THROUGH 12,000 MSL CENTER WINDSHIELD POPPED AND STARTED LEAKING AT SEAMS. REMOVED AND REPLACED WINDSHIELD IAW MM 56-10-01 PRESSURED A/C TO 7 PSI AND NO LEAKS NOTED, ANTI-ICE AND ANIT-FOG OPS CHECK GOOD. (M)

Part: LIGHT — FAILED (CABIN)

EMERGENCY LIGHTS (4 TOTAL, 2 RED, AND 2 WHITE) DO NOT TEST AT SEATS 17-20 A/C RT. REMOVED AND REPLACED EMERGENCY AISLE PATH AFT RT EMERGENCY EXIT IAW MM. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER PACK — INOPERATIVE (CABIN)

PAX - EMERGENCY LIGHTS ROW 8 THROUGH 11 INOP. REMOVED AND REPLACED POWER PACK. OPS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FUEL CONTROL — MALFUNCTIONED (NR 1 ENGINE)

NR 1 ENGINE SURGING PLUS OR MINUS .03 EPR (INDICATING ALL ENGINE PARAMETERS). F/A REPORTS UNUSUAL VIBRATIONS AND NOISES. BORESCOPED ENGINE PER MM 72-00-04, ALL OK. REMOVED AND REPLACED FUEL CONTROL NR 2 ENGINE IAW MM 73-20-01 AND TRIMMED ENGINE IAW MM SYSTEM. ALL OPS CHECKS NORMAL, ALL ENGINE PARAMETERS IAW MM 71-00-00. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SENSE LINE — DIRTY (NR 1 ENGINE)

NR 1 ENGINE SURGING PLUS OR MINUS .03 EPR ON CLIMB-OUT. ENGINE ANTI-ICE, NO AFFECT. ENGINE STABILIZED AT 1.6 EPR, RETURNED TO GPT. CLEANED OUT FUEL CONTROL MOISTURE TRAP SENSE LINE IAW MM 73-20-03. SYSTEM OPS CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. (X)

Part: FUEL FLOW TRANS — FAILED (RT ENGINE)

DURING TAKEOFF FLASHING EGT 500 DEGREES RIGHT ENGINE. DISCONTINUED TAKEOFF AT 80 KNOTS WHEN RT FUEL FLOW FLASHED AT 500 DEGREES CELSIUS. MAINTENANCE NOTED NO FUEL FLOW TRANSMITTER, LEAKS ON RUN UP. (M)

Part: SEAT TRACK — CORRODED (BS 1145-1160)

SEAT TRACK NR X22L CORRODED FROM BS 1145 TO 1160. FABRICATED AND DRILLED PARTS, TREATED PRIMED AND PAINTED. INSTALLED IAW SRM'S 53-05, 51-10. (M)

Part: BATTERY — DISCHARGED (CABIN)

OVERHEAD EMEGENCY EXIT LIGHTS INOP ROW 27. REPLACED BATTERIES IN CHARGER, OPS NORMAL. (M)

Part: LOCK RING — CRACKED (C1 BLADE)

FOUND C-1 BLADE LOCK RING BROKEN AT PULL HOLE APPROXIMATELY 2 INCHES FROM END. REPLACED C-1 BLADE LOCK RING. PART TOTAL CYCLES, 11,904. (X)

Part: BATTERY — DISCHARGED (CABIN)

AFT SECTION OF E-LIGHT FLOOR PATH INOP. REMOVED AND REPLACED APPLICABLE BATTERIES FOR AFT SECTION. E-PATH LIGHTING OPS CHECKS GOOD. (M)

Part: BATTERIES — DISCHARGED (CABIN)

CEILING EMERGENCY LIGHTS ROW 11-16 WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERIES FOR ROWS 11-16. OPS CHECK NORMAL. (M)

Part: BATTERIES — DISCHARGED (CABIN)

AFT GALLEY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. INSTALLED NEW BATTERIES IN CHARGER. OPS CHECK NORMAL. (X)

Part: BOLT — BROKEN (NR 2 WHEEL ASSY)

NR 2 WHEEL THROUGH-BOLT SHEARED. REPLACED NR 4 WHEEL ASSY. (X)

Part: ENGINE — FAILED (RIGHT)

IRW - RIGHT ENGINE OIL QUANTITY DECREASED TO 12 QUARTS. TEMPERATURE INCREASED TO 140 DEGREES. REMOVED AND REPLACED 'R' ENGINE PER MD-80 MM 71-00. OPS CHECK GOOD. (X)

Part: EEL BATTERY — DISCHARGED (CABIN)

AFT SECTION OF FLOOR TRACK INOP (EMERGENCY). INSTALLED NEW EMERGENCY FLOOR TRACK LIGHTING SUPPLY POWER PACK. OPS TESTS NORMAL. (X)

Part: EEL BATTERY — DISCHARGED (CABIN)

SECTION 15 THROUGH SECTION 20, RIGHT SIDE EMERGENCY FLOOR LIGHTS OUT. REPLACED POWER PACK BATTERY ON SECTION 15. OPS GOOD. (X)

Part: CONTROLLERS — MALFUNCTIONED (NR 1/2)

AT 26,000 FEET, NOTED CABIN ALTITUDE INCREASING, WHILE STILL CLIMBING TO ASSIGNED ALTITUDE. AIRCRAFT LEVELED AND DESCENT REQUESTED. RED CABIN LIGHT CAME ON AT 11M. CABIN ALTITUDE PRESSURE CONTROLLERS SWITCH, CABIN ALTITUDE KEPT INCREASING AND OXYGEN MASK DEPLOYED. AIRCRAFT WAS DESCENDED TO 11M. FLIGHT ATTENDANT REPORTED FUMES AND HAZE IN CABIN. REMOVED AND REPLACED NR 1 AND NR 2 PRESSURE CONTROLLERS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: EEL — INOPERATIVE (CABIN)

EMERGENCY FLOOR LIGHTS INOP AT 6 AND 7 DEF. REPLAMPED AND RESECURED FLOOR TRACK LIGHTING. OPS CHECK OKAY. (X)