N242AA

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · 70,678 cycles

LGA EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 18 TO 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 18 TO 26. SYSTEM GROUND CHECKED NORMAL OPS.

Part: APU — LEAKING

CREW REPORTED SMOKE IN CABIN. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. FOUND AUXILIARY POWER UNIT (APU) OIL LEAKAGE WITH POSITIVE INDICATIONS OF INGESTION INTO APU INTAKE. REPLACED APU AND PERFORMED PACK BURN. SYS GROUND CHECKED NORMAL OPERATION. (K)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,911 hrs

LGA - EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 14 TO 19 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 14DEF FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 14 TO 19. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

LGA - EMERGENCY LIGHTS THROUGHOUT CABIN INOPERATIVE. REPLACED BATTERY PACKS AT B27, B28, B5104 AND B5107 FOR EMERGENCY LIGHTS THROUGHOUT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HYDRAULIC SYSTEM — LOW (RIGHT)

PHX - RIGHT HYDRAULIC PRESSURE DROPPED TO 0 AND HYDRAULIC QUANTITY DROPPED TO 4 QUARTS. EMERGENCY GEAR EXTENSION PROCEDURES USED. LANDED PHX WITHOUT INCIDENT. SERVICED RIGHT HYDRAULIC SYSTEM TO FULL. INSPECTED ALL RIGHT SYSTEM HYDRAULIC COMPONENTS AND OPERATED ALL RIGHT HYDRAULIC SYSTEMS. NO LEAKS NOTED. RELEASED AIRCRAFT FOR FLIGHT CHECK PER SPOTTING MESSAGE 12 044. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: RUDDER — MALFUNCTIONED (TAIL)

DFW T497/30 ON LANDING DFW, RUDDER TRAVEL UNRESTRICTED, LIGHT DID NOT ILLUMINATE. SPEED WENT BELOW 140 KTS AND STILL NO LIGHT. GO-AROUND WAS ACCOMPLISHED DUE TO CROW-WIND LIMITATIONS OF 12 KTS. ON SECOND APPROACH LANDING LIGHT ILLUMINATED. MAINTENANCE INSPECTED AREA DOWN RUDDER MECHANISM FOR CONDITION AND SECURITY. SYSTEM GROUND CHECKED NORMAL OPERATION. UNABLE TO DUPLICATE.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, AFT STAIRWAY TAIL HANDLE EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED AFT STAIRWAY TAIL HANDLE EMERGENCY EXIT LIGHTS SPLICES. SYSTEM GROUND CHCKED NORMAL OPERATION. (M)

Part: GASKET — FAILED (TEMP SENSOR)

EN ROUTE MIA-ORD, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. PERFORMED PROCEDURE, LIGHT DID NOT EXTINGUISH AFTER 2 MINUTES. RETURNED AND LANDED MIA WITHOUT INCIDENT. REPLACED LEFT PNEUMATIC SUPPLY TEMPERATURE SENSOR GASKET BROKEN. PRESSURIZED PNEUMATIC DUCTS, NO FURTHER LEAKS NOTED. NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND SEVERAL SMALL SPOTS OF CORROSION ON WEB ALONG LOWER DOOR JAMB STATION 1155 TO STATION 1212. INSTALLED NEW DOOR AREA WEB FROM STATION 1155-AFT TO STATION 1212 PER AARD 53-10-00-3. (M)

Part: BEAM — CORRODED (FUSELAGE)

TUL - FOUND HEAVY CORROSION ON BEAM FACE AND LOWER LEG FROM STATION 1155 AFT TO STATION 1212. INSTALLED FULL LENGTH BEAM DOUBLER PER AARD 53-10-00-3 FIG 1 SHEETS 1-13. (M)

Part: FITTING — CORRODED (CARGO DOORWAY)

TUL - FOUND CORROSION ON T-FITTING AT LOWER AFT CORNER OF MID CARGO DOOR JAMB. INSTALLED NEW T-FITTING PER SRM 51-30 E58-4A NR 0210772. (M)

Part: PAN — CORRODED (PAX DOORWAY)

TUL - FOUND FORWARD DOOR PAN IS CORRODED IN FRONT, BACK AND BOTTOM INSTALLED PAN SPLICE REPAIR PER SRM 53-05 PT 1. (M)

Part: FLOORBEAM — WORN (FUSELAGE)

TUL - FOUND DEEP WORN AREA IN BOTTOM OF CABIN FLOORBEAM AT STATION 389 BL 0. REMOVED DAMAGED AREA. INSTALLED ANGLE DOUBLER FILLER AND WEAR STRIP, CLEANED AND TREATED AND PRIMED PER AARD 53-20-00-21. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CRACKED FASTENER HOLES UNDER NR 2 SEAT TRACK ON CUSP AT STATION'S 1211-1213-1219. INSTALLED ONE DOUBLER STATION 1209-1215 AND ONE DOUBLER STATION 1225-1229, PER AARD 53-00-00-02. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON FUSELAGE SKIN AROUND FORWARD ANTENNA 1 INCH HOLE STATION 380. BLENDED CORRODED FROM SKIN AND TREATED DAMAGE IS ACCEPTABLE AS IS PER SRM 53-01 FIG 1, SHEET 3, PAGE 6. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE CEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 25 THROUGH 26 INOPERATIVE. REPLACED CEILING MOUNTED EMERGENCY EXIT LIGHT BATTERY PACK. SYTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

BOS - DURING OVERNIGHT INSPECTION, EMERGENCY EXIT LIGHT CONNECTOR PIN NOT SEATED. REINSTALLED EMERGENCY EXIT LIGHT CONNECTOR PIN AT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SEAL — DEFECTIVE (RT WING)

MCO - FLT 1125 - AFTER TAKEOFF FROM MCO, FLIGHT CREW NOTED FUEL LEAK FROM RIGHT WING 10 FEET FROM WING ROOT. RETURNED AND LANDED MCO WITHOUT INCIDENT. TIGHTENED SCREW ON BOOST PUMP. SYSTEM GROUND CHECK NORMAL OPERATION. REPEATED ON TRIP 0712 SAME DAY PIREP NR 57, LANDED LGA WITHOUT INCIDENT. REPLACED SEAL ON RIGHT WING UPPER PLATE ISOLATION PROBE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: APU — LEAKING (AFT FUSELAGE)

SLC - FLT 1464 - AT 3,000 FEET, AFL CABIN FILLED WITH SMOKE. REPLACED AUXILIARY POWER UNIT. LEAKING OIL. REPLACED COELESCER BAGS AND ACCOMPLISHED PACK BURN-OUT. SYSTEM GROUND CHECK , NORMAL OPERATION. (X)

Part: WIRE — BURNED (TAIL COMPARTMENT)

DFW - DURING OVERNIGHT MAINTENANCE, TAIL COMPARTMENT EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRE TO TAIL COMPARTMENT EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: INDICATOR — DEFECTIVE (COCKPIT)

LAX - FLT 896 - EN ROUTE SJC-DFW - CENTER TANK BOOST PUMP CIRCUIT BREAKERS POPPED WHEN TURNED ON. AIRCRAFT AIR INTERRUPTED AND LANDED LAX WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND FUEL QTY INDICATION SYSTEM AT FAULT. MAINTENANCE REPLACED COCKPIT FUEL QTY INDICATOR. AS A PRECAUTIONARY, BOTH CENTER BOOST PUMPS WERE REPLACED. REQUIRED FUEL QTY AND TRANSFER CHECKS WERE ACCOMPLISHED WITH NO FAULTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — DEFECTIVE (RT MLG DOOR)

DFW - FLT T1911 - AFTER TAKEOFF, THE RIGHT MAIN GEAR OPEN LIGHT STAYED ILLUMINATED AFTER RAISING THE GEAR HANDLE. CREW RAN CHECK LIST PROCEDURES AND THE RIGHT MAIN GEAR DOOR LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT MAIN GEAR DOOR SENSOR, CYCLED LANDING GEAR SEVERAL TIMES. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: HARNESS — FAILED (TAIL CONE)

DFW - DURING OVERNIGHT CHECK, EMERGENCY LIGHT IN TAIL CONE INOPERATIVE. REPLACED UPPER POWER HARNESS ASSY. SYSTEM GROUND CHECKED, NORMAL OPERATION.

Part: LOCK LINK ASSY — CRACKED (NLG)

LGA - DURING OVERNIGHT CHECK WHILE ACCOMPLISHING FCD KFD KFO405A TO CHECK NOSE LANDING GEAR UPPER AND LOWER LOCK LINK ASSEMBLY, UPPER AND LOWER LOCK LINKS FOUND CRACKED. REPLACED UPPER AND LOWER LOCK LINK ASSEMBLY. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRIP — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY FOUND INOPERATIVE. REPLACED EMERGENCY LIGHT STRIP BY FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)