N218AA

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT FIRST CLASS GALLEY OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS GALLEY OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: GEARBOX — INOPERATIVE (RIGHT ENGINE)

AFTER TAKEOFF FLIGHT ATTENDANT REPORTED HEARING LOUD POP FOLLOWED BY A MODERATE VIBRATION. ALL INSTRUMENTS APPEARED NORMAL. AT FLIGHT LEVEL 290 RIGHT ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED. CREW SHUT DOWN RIGHT ENGINE AND LANDED DFW WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE AT DFW ON 24 MARCH 2007 DUE TO METAL IN OIL FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: INDICATION SYS — INOPERATIVE (COCKPIT)

RIGHT ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED AT FLIGHT LEVEL 370. LIGHT STAYED ON AT IDLE. CREW SHUT DOWN RIGHT HAND ENGINE. ENGINE WINDMILLED FOR 27 MINUTES WITH NORMAL OIL PRESSURE AND QUANTITY. RETURNED TO TPA AND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE OIL FILTER. FILTER CHECKED CLEAN. PLACARDED RIGHT ENGINE OIL STRAINER INDICATION INOPERATIVE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

BOS - EMERGENCY LIGHTS IN CEILING FROM ROWS 22 TO 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CEILING FROM ROWS 22 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MOTOR — INOPERATIVE (STAB TRIM)

ORD - EN ROUTE ORD-DCA LEVELING OFF AT 5000 FEET WITH AUTOPILOT ON, AUTOPILOT TRIM LIGHT CAME ON WITH NOSE UP PITCH. DISCONNECTED AUTOPILOT AND RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ALT STABILIZER TRIM MOTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

MIA - EMERGENCY LIGHT IN COCKPIT OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT IN COCKPIT OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

AUS - FORWARD AUXILIARY OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD AUXILIARY OVERWING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGNECY LIGHT)

AUS - OVERHEAD EMERGENCY LIGHT AT SEAT ROW 9DEF INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT ROW 9DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

RDU - CEILING EMERGENCY LIGHTS BETWEEN ROWS 18 AND 21 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS BETWEEN ROWS 18 AND 21. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 17 THROUGH 29 INOPERATIVE. REPLACED BATTERY PACKS FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 17 THROUGH 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

AUS EMERGENCY CEILING LIGHTS OVER SEATS 28DEF THROUGH 31DEF INOPERATIVE. REPLACED EMERGENCY CEILING LIGHT BATTERY PACK IN OVERHEAD BIN AT SEAT 28DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, CEILING EMERGENCY EXIT LIGHT AT ROW 18-21 INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

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

BOS - FLT 1201 - EN ROUTE BOS-DFW, DURING CLIMB-OUT, RIGHT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED. RIGHT HYDRAULIC SYSTEM HAD TOTAL LOSS OF FLUID, UNABLE TO RETRACT LANDING GEAR. RETURNED BOS AND LANDED WITHOUT INCIDENT. REPLACED ANTI-SKID CONTROL VALVE. REPLACED RIGHT ENGINE DRIVEN HYDRAULIC PUMP AND ELECT HYDRAULIC PUMP AS PRECAUTIONARY. REPLACED RIGHT ENGINE AND RIGHT HYDRAULIC SYSTEM FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CRACKED (FUSELAGE)

FOUND TWO CRACKS AT FASTENERS THROUGH FUSELAGE SKIN STATION 1380, LONGERON 14 RT. .25 INCH STOP DRILLED END OF TWO CRACKS AT STATION 1380 RIGHT DYE CHECK. END OF STOP DRILLED VERIFIED BY QA, 006, INSTALLED DOUBLER PER SRM CH 53-01-00 FIG 2 SHEET 3 AND AARD 53-30-00-2. (M)

Part: SKIN — CRACKED (FUSELAGE)

FOUND CRACK IN FUSELAGE SKIN STATION 138 LONGERON 13L. STOP DRILLED END OF CRACK AND APPLIED NON-PRESSURIZED DOUBLER PATCH PER SRM 53-01-00 FIG 2 SHEET 3, SRM 53-34-00 PAGE 17 FIG 4 SHEET 2, PAGE 16 FIG 4 SHEET 1, SRM 51-01-00 PAGE 1, AND AARD 53-30-00-02 PAGE 1. (M)

Part: BATTERY PACK — INOPERATIVE (AFT ACCESSORY)

TPA - DURING OVERNIGHT MAINTENANCE, TWO EMERGENCY LIGHTS ABOVE TAIL CONE ESCAPE SLIDE INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: O-RING — LEAKING (APU)

DFW - FLT 2090 - EN ROUTE SAN-DFW - SHORTLY AFTER TAKEOFF, DETECTED HAZE IN CABIN. LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED MAGNETIC DRAIN PLUG O-RING AT APU. PERFORMED LEAK CHECK. NO LEAKS NOTED. PERFORMED PACK BURNOUT PER THE MM. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SAT - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD SECTION INOPERATIVE. REINSTALLED EMERGENCY EXIT LIGHT CONNECTOR AT FORWARD BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SENSOR — DEFECTIVE (MLG)

IAH - FLT 2011 - WHILE ON RUNWAY, BRAKE OVERHEAT LIGHT ILLUMINATED, NR 1 INDICATED 400 DEGREES AFTER CLEARING RUNWAY. FIRE DEPARTMENT CHECKED BRAKE, LIGHT WENT OUT, TEMPERATURE BACK TO NORMAL. RETURNED TO GATE AND LIGHT EXTINGUISHED AND TEMPERATURE WAS NORMAL. REPLACED NR 1 BRAKE TEMPERATURE SENSOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: STATOR VANE — FAILED (NR 2 ENGINE)

PHL - FLT 317 - DURING CLIMB-OUT AT 33,000 FT, FLT CREW HEARD A LOUD NOISE FROM NR 2 ENG WITH THE EGT PEGGED AT 800 DEGREES.FLT CREW DECLARED AN EMERGENCY, SECURED NR 2 ENG AND DIVERTED TO PHL. A/C LANDED PHL WITHOUT FURTHER INCIDENT. MX FOUND THE NR 2 ENG TURBINE FAILED. REPLACEDNR 2 ENG, PERFORMED ENG RUN UP. SYSTEM GROUND CHECKED NORMAL OPS. THE 8TH STAGE STATOR VANE WAS BROKEN AND LIBERATED. THE LIBERATED VANE CAUSED THE DAMAGE TOTHE REST OF THE HPC AND ALL STAGES OF THE TURBINE. FATIGUE MARKS WERE NOTED ON THE 8TH STAGE STATOR FRACTURE SURFACE BUT DUE TO THE SECONDARY DAMAGE, AN IMPACTINITIATION SITE COULD NOT BE DETERMINED. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: INDICATOR — MALFUNCTIONED (COCKPIT)

ORD - FLT 756 - DURING CRUISE, EN ROUTE TUL-ORD RED GEAR UNSAFE LIGHTS ILLUMINATED WITH NO ADVERSE YAW OR EXCESS NOISE. NO ASSOCIATED ORAL WARNING WITH GEAR UNSAFE LIGHTS. LANDED ORD WITHOUT INCIDENT. CYCLED GEAR WITH NO DEFECTS INDICATED. COULD NOT DUPLICATE. PRECAUTIONARY REPLACED PROXIMITY CONTROL BOX AND TESTED ACCORDING TO MM. NO DEFECTS INDICATED. CYCLED GEAR AGAIN NUMEROUS TIMES COULD NOT DUPLICATE. AIRCRAFT HAS NO HISTORY OR RED GEAR UNSAFE LIGHTS ILLUMINATING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FITTING — CORRODED (BS 215)

TUL - G2 GALLEY TIE DOWN FITTING IS CORRODED AT STATION 215. REMOVED AND REPLACED WITH NEW TIE DOWN FITTING AT STATION 215, G2 GALLEY. (M)

Part: PAN — CORRODED (BS 150)

TUL - FOUND CORROSION ON G1 GALLEY WATER CONNECTION FLOOR PAN AND CUSP. REMOVED CORRODED CUSP AND ASSOCIATED CORRODED AREAS INSTALL DOUBLER, TREATED, PRIMED AND PAINTED PER SRM CHAPT 51. (M)

Part: SUPPORT — CORRODED (BS 162-198)

TUL - FLOORBOARD SUPPORT JUST INBOARD OF FORWARD ENTRY DOOR SILL WAS CORRODED. REMOVED AND REPLACED AFFECTED SUPPORT PER SRM CHAP 51. (M)

Part: ANGLE — CORRODED (BS 1322)

TUL - LOWER J-ANGLE CORRODED. REMOVED AFFECTED AREA OF J-ANGLE. INSTALLED NEW SECTION OF FRAME AND DOUBLERS PER SRM 53-03, FIGURE 2A, SHEET 1, PAGE 4A AND ESO 80559, DATED 3-13-96. TST: 39,427. CYCLES: 22,544. (X)

Part: CUSP — CORRODED (BS 1136-1155)

TUL - CUSP CORRODED LT SIDE, STA 1136 TO STA 1155. INSTALLED DOUBLER REPAIR PER CHAPTER 53 AND ESO 80559. TST: 39,429.01. CYCLES: 22,544. (X)

Part: ANGLE — CORRODED (BS 1155)

TUL - FORWARD LOWER CORNER DOOR CUT-OUT, LOWER ANGLE FITTING CORRODED. REMOVED DAMAGED ANGLE FITTING. REPLACED WITH NEW ANGLE FITTING. TST: 39,421. CYCLES: 22,544. (X)