N441AA

Part: COVER — BROKEN (EMERGENCY LIGHTS) · airframe 64,699 hrs · 34,209 cycles

EMERGENCY EVACUATION DOOR LIGHT LENS COVER BROKEN. REPLACED LENS COVER.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 64,699 hrs · 34,209 cycles

AFT STAIRWAY EMERGENCY EXIT SIGN BROKEN. REPLACED EMERGENCY LIGHT SIGN IN AFT STAIRWAY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,699 hrs · 34,209 cycles

EMERGENCY LIGHT IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK IN FORWARD CABIN.

Part: LENS — MISSING (CABIN) · airframe 64,614 hrs · 34,159 cycles

CEILING MOUNTED EMERGENCY LIGHT LENS MISSING AT ROW 11. REPLACED LENS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,484 hrs

LGA - EMERGENCY BATTERY AT FORWARD POSITION INOPERATIVE. REPLACED BATTERY AT FORWARD POSITION.

Part: STIFFENER — CRACKED (RT WING) · airframe 62,916 hrs · 33,241 cycles

FORWARD END OF RIGHT FOD PANEL ABOVE RIGHT MAIN LANDING GEAR, INBOARD END VERTICAL STIFFENER CRACKED. INSTALLED NEW VERTICAL STIFFENER PER SRM 51-10-01.

Part: ATTACH FITTING — CRACKED (FLAP ACTUATOR) · airframe 69,916 hrs · 33,241 cycles

INBOARD LEFT FLAP ACTUATOR ATTACH FITTING CRACKED AT LOWER WEB. INSTALLED DOUBLERS ON FLAP MECHANISM SUPPORT FITTING PER AARD 57-10-00-2.

Part: CASTING — CRACKED (SPOILER) · airframe 62,916 hrs · 33,241 cycles

RIGHT GROUND SPOILER CASTING CRACKED. INSTALLED NEW GROUND SPOILER CASTING PER SRM 51-10.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,480 hrs

LGA- FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS EMERGENCY LIGHTS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,480 hrs

LGA- FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS EMERGENCY LIGHTS.

Part: OIL SYSTEM — LOW PRESSURE (NR 1 ENGINE) · airframe 61,750 hrs

PHL INFLIGHT JFK TO DFW - DURING CLIMB NUMBER ONE ENGINE OIL PRESSURE LOW LIGHT ILLUMINATED. OIL PRESSURE DROPPED TO ZERO ON GAUGE AND OIL TEMPERATURE DROPPED. CREW SHUT DOWN ENGINE AS PRECAUTION. LANDED PHL WITHOUT INCIDENT. SINGLE ENGINE TIME 15 MINUTES. FOUND METAL IN FILTER. REPLACED NUMBER ONE ENGINE ON 13 OCT AT PHL DUE TO OIL PRESSURE OUT OF LIMITS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — DAMAGED (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT ROW 21 HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — DAMAGED (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT ROW 12 HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — DAMAGED (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT ROW 23 HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 23. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHTS IN CEILING FROM SEAT ROWS 23 TO 27 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CEILING FROM SET ROWS 23 TO 27. SYSTEM ROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHTS AT SEAT ROW 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROW 26. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISLODGED (EMERGENCY LIGHTS)

LGA - EMERGENCY LIGHTS AT OVERHEAD TAIL CATWALK INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHTS A OVERHEAD TAIL CATWALK. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - EMERGENCY LIGHTS AT TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (CABIN)

DFW - EMERGENCY LIGHTS AT SEATS 16D, 17D, AND 28D HAVE MISSING LENS. SEAT 27D HAS WRONG LENS. REPLACED EMERGENCY LIGHT LENS AT 16D, 17D, AND 28D AND REPLACED CORRECT LENS FOR SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

ORD - OVERWING EMERGENCY EVACUATION LIGHT INOPERATIVE DURING TEST. REPLACED BATTERY PACK FOR OUTSIDE OVERWING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: O-RING — DAMAGED (RT ENGINE)

STL - LOST RIGHT HAND OIL QUANTITY AND PRESSURE. OIL PRESSURE STEADY AT 40 DEGREES C. N2 58 TO 68 PERCENT. IDLE POWER FROM 1540 TO 1617, LANDED STL WITHOUT INCIDENT. FOUND OIL LEAK FROM OIL FILTER HOUSING. O-RINGS FOUND DAMAGED. REPLACED NUMBER TWO ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

ALL OVERHEAD EMERGENCY LIGHT IN AFT TAIL CONE ARE INOPERATIVE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY EXIT LIGHTS AT FORWARD ENTRY CEILING INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD ENTRY CEILING EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - LEFT AND RIGHT EMERGENCY EXIT LIGHTS AT ROW 21 ARE INOPERATIVE. RESEATED BATTERY PACKS AT B5105 FOR EMERGENCY EXIT LIGHTS AT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (CABIN)

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

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DEN - OVERHEAD EMERGENCY LIGHT AT SEAT 4 AND 5B INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHT AT SEAT 4 AND 5B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (A/C BAY)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE ON CATWALK. SECURED LOOSE CONNECTOR ON FORWARD CATWALK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BEAM — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON BEAM AROUND 2 FITTINGS AT CARGO DORO CUT OUT LOWER SIDE. REMOVED AND REPLACED CARGO DOOR BEAM PER SRM 51-30-00. (M)

Part: BEAM — CORRODED (FUSELAGE)

TUL - FOUND STATION 1212-1216 TOP OF DOOR BEAM L28R, DOOR FRAME WEB CORRODED AT TWO NUTPLATES. REMVOED AND REPLACED DOOR FRAME WEB PER SRM 51-30-00. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN CRACKED BETWEEN TWO RIVETS, STATION 1380 BELOW LONGERON 13L. CUT OUT DAMAGE, FABRICATED FILLER AND INSTALLED EXTERNAL DOUBLER PER SRM 53-01 FIG 4. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN FUSELAGE SKIN AT STATION 1437 BETWEEN L3R AND L4R. CUT OUT DAMAGE INSTALLED FILLER AND EXTERNAL DOUBLER PER SRM 53-01. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND TEMP REPAIR DOUBLER ON NLG JAMB SKIN JUST AFT OF LEFT STRUT DR AFT HINGE, DUE TO CRACK ON SKIN. REMOVED AND INSTALLED NEW SECTINO OF SKIN AND INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

TUL - FOUND STATION 1332 SIDE OF VAULT DOOR FRAME. STOP DRILLED CRACK, INSTALLED DOUBLER PER SRM 53-01 FIG 2. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN CUSP STATION 240 RBL 47-49. REMOVED DAMAGED AREA. INSTALLED DOUBLER REPAIR PER AARD 53-00-00-02 PAGE 1. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN CUSP WEB AT STATION 248 RBL 55 AND CORROSION AT STATION 245/240 RBL 55. REMOVED CRACK AND CORROSION AND INSTALLED REPAIR DOUBLER PER 53-00-00-02 PAGE 1. (M)

Part: SCAVENGE PUMP — FAILED (LT ENGINE)

DFW - FLT 1456 - EN ROUTE DEN-DFW - UPON DESCENT DETECTED LEFT ENGINE OIL PRESSURE LOW CAUTION LIGHT ILLUMINATE. LEFT OIL QUANTITY DECREASED TO ZERO AND LEFT ENGINE WIND MILLED UNTIL TOUCH DOWN. LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE ENGINE. THE NR 4 AND 5 SCAVENGER PUMPS FAILED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TUBE — LEAKING (APU)

DFW - FLT 2437 - EN ROUTE DFW-LAX, SHORTLY AFTER TAKEOFF DETECTED LIGHT SMOKE AND FUMES AT COCKPIT. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED OIL FILL SCUPPER ASSEMBLY AT APU. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT AT AFT DOOR INOPERATIVE. RECONNECTED WIRES BEHIND LEFT AFT LAVATORY MIRROR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (PAX DOOR)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGH AT R1 DOOR INOPERATIVE. REPAIRED CONNECTOR AT R1 DOOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (TAIL CONE)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN TAIL COMPARTMENT INOPERATIVE. SECURED LOOSE CONNECTION TO EMERGENCY LIGHT IN TAIL CONE. SYSTEM GROUNC CHECK NORMAL OPERATION. (M)

Part: LINK — BROKEN (NLG DOOR)

DFW - FLT 1038 - AFTER TAKEOFF, LOUD VIBRATION FROM NOSE DOOR AREA. RECYCLED GEAR, NO HELP. RETURNED AND LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED NOSE GEAR DOOR LINK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HYD LINE — LEAKING (TAIL COMPARTMENT)

DFW - FLT 2374 - AFTER TAKEOFF DFW TO ORD, NOTED HYDRAULIC FLUID ODOR THROUGHOUT CABIN AND LEFT HYDRAULIC FLUID QTY DECREASING. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPAIRED LEAKING HYDRAULIC FLUID LINE CONNECTED TO HYDRAULIC FLUID TRANSFER PUMP. ACCOMPLISHED AIR CONDITIONING PACK BURN OUT AND REPLACED SEPARATOR BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PAN — CORRODED (PAX DOORWAY)

TUL - FOUND CORROSION ON DOOR PAN. REPLACED SPLICED SECTION OF NEW PAN PER SRM 53-05 FIG 44. (M)

Part: MOUNT — CORRODED (BS 210)

TUL - INBOARD FORWARD NR 2 GALLEY MOUNT CORRODED. INSTALLED NEW GALLEY MOUNT PER STANDARD PRACTICE 51-00. (M)

Part: SUPPORT — CORRODED (BS 218)

TUL - FOUND INBOARD AFT NR 2 GALLEY MOUNT CORRODED. INSTALLED NEW INBOARD AFT UPPER G2 GALLEY MOUNT PER STANDARD PRACTICE 51-00. (M)

Part: TRACK — CORRODED (BS 1155-1221)

TUL - FOUND CORROSION AROUND T/O TRACK MOUNT HOLES. REPLACED SECTION OF SEAT TRACK PER STANDARD PRACTICE 51-00. (M)

Part: FUEL PUMP — DEFECTIVE (NR 1 ENGINE)

DFW - FLT 1389 - DURING TAKEOFF DFW, LT ENGINE SLOW TO SPOOL. AT LEVEL FLIGHT 22,000 FEET, LT EPR, N1 AND N2 STARTED FLUCTUATING. ENGINE WENT TO IDLE FOR A FEW SECONDS AND THEN STARTED OPERATING NORMALLY. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE FUEL PUMP AND FUEL CONTROL. LEAK CHECKED WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)