N412AA

Part: BATTERY — NOT SEATED (ZONE 100) · airframe 68,309 hrs · 36,214 cycles

CEILING EMERGENCY LIGHTS INOPERATIVE FROM ROWS 23 TO 30. RESEATED BATTERY FOR LIGHTS FROM ROWS 23 TO 30. OPS CHECK NORMAL.

Part: BATTERY — NOT SEATED (EMERGENCY LIGHTS) · airframe 68,309 hrs · 36,214 cycles

RIGHT FORWARD OVERWING HATCH LOWER EXIT LIGHT INOPERATIVE. RESEATED BATTERY FOR RIGHT FORWARD OVERWING HATCH LOWER EXIT LIGHT. OPS CHECK NORMAL.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 68,309 hrs · 36,214 cycles

CEILING EMERGENCY LIGHT RIGHT SIDE ABOVE SEAT 6E INOPERATIVE. REPLACED LAMP FOR CEILING EMERGENCY LIGHT. OPS CHECK GOOD.

Part: LAMP — BURNED OUT (ZONE 200) · airframe 68,309 hrs · 36,214 cycles

CEILING EMERGENCY LIGHT RIGHT SIDE ABOVE SEAT 4E INOPERATIVE. REPLACED LAMP FOR CEILING EMERGENCY LIGHT. OPS CHECK OK.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,122 hrs · 35,547 cycles

TWO DENTS FORWARD OF FORWARD ENTRY DOOR JUST ABOVE LONGERON 19L AT STATION 133. INSTALLED DOUBLER PER SRM 53-04-00 AND EA MD80-53-00-5267.

Part: BRACKET — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,122 hrs · 35,547 cycles

GIRT BAR SUPPORT STRUCTURE AFT BRACKET CORRODED. INSTALLED NEW GIRT BAR SUPPORT BRACKET PER SRM 51-01.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 67,122 hrs · 35,547 cycles

SHEAR TIE CRACKED IN AFT ACCESSORY COMPARTMENT BETWEEN STRINGER 1 RIGHT AND STRINGER 2 RIGHT AT STATION 1437. INSTALLED NEW SHEAR TIE PER SRM 51-30.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,122 hrs · 35,547 cycles

CANT FRAME 1463 WEB CRACKED 2 INCHES AT RIGHT SIDE ABOVE ACCUMULATOR LONGERON 17 TO 18 RIGHT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 53-00-00-09 AND SRM 53-01-00 FIGURE 162.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,122 hrs · 35,547 cycles

INTERCOSTAL IS CRACKED AT RIGHT CANT FRAME AT STATION 1485 AT AFT ARC. INSTALLED NEW INTERCOSTAL AT RIGHT CANT FRAME 1485 PER SRM 53-01.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,122 hrs · 35,547 cycles

NUMBER FIVE PLATE LUG BORE CORRODED AND OUT OF LIMITS. INSTALLED SERVICEABLE NUMBER FIVE LUG PLATE IN ACCORDANCE WITH WORK CARD K2988AA.

Part: LUG — CORRODED (ZONE 300) · corrosion level 2 · airframe 67,122 hrs · 35,547 cycles

NUMBER 8 RIGHT OUTBOARD HORIZONTAL STABILIZER PLATE LUG BORE CORRODED AND OUT OF LIMITS. INSTALLED SERVICEABLE NUMBER 8 LUG PLATE PER CARD NR 2988AA.

Part: LUG — CORRODED (ZONE 300) · corrosion level 2 · airframe 67,122 hrs · 35,547 cycles

NUMBER ONE PLATE LUG BORE CORRODED AND OUT OF LIMITS. LT OUTBOARD (TAIL HORIZONTAL STABILIZER). INSTALLED SERVICEABLE NR 1 PLATE LUG IN ACCORDANCE WITH WORK CARD K2988AA.

Part: LUG — CORRODED (ZONE 300) · corrosion level 2 · airframe 67,122 hrs · 35,547 cycles

NR 2 PLATE LUG LEFT OUTBOARD (TAIL HORIZONTAL STABILIZER) CORRODED AND OUT OF LIMITS. INSTALLED SERVICEABLE NR 2 LEFT OUTBOARD LUG PLATE IN ACCORDANCE WITH WORK CARD K2988AA.

Part: LUG — CORRODED (ZONE 300) · corrosion level 2 · airframe 67,122 hrs · 35,547 cycles

NUMBER FOUR PLATE LUG BORE AT LEFT INBOARD CORRODED AND OUT OF LIMITS. INSTALLED SERVICEABLE NUMBER FOUR LEFT INBOARD LUG BORE PLATE IN ACCORDANCE WITH WORK CARD K2988AA.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,122 hrs · 35,547 cycles

NUMBER SIX PLATE LUG BORE CORRODED AND OUT OF LIMITS. INSTALLED SERVICEABLE NUMBER SIX LUG PLATE PER CARD K2988AA.

Part: PLATE — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 67,122 hrs · 35,547 cycles

NUMBER SEVEN LUG PLATE BORE RIGHT OUTBOARD IS CORRODED AND OUT OF LIMITS (HORIZONTAL STABILIZER). INSTALLED NEW SERVICEABLE NUMBER SEVEN LUG PLATE PER CARD K2988AA.

Part: LUG — CORRODED (ZONE 300) · corrosion level 2 · airframe 67,122 hrs · 35,547 cycles

NR 3 LEFT INBOARD LUG PLATE BORE CORRODED (TAIL HORIZONTAL STABILIZER) AND OUT OF LIMITS. INSTALLED SERVICEABLE NR 3 LEFT INBOARD LUG PLATE IN ACCORDANCE WITH WORK CARD K2988AA.

Part: BEAM — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 67,122 hrs · 35,547 cycles

CORROSION ON DOOR BEAM IN MID CARGO AT STATION 636 TO 693. INSTALLED DOUBLER PER AARD 53-10-00-3.

Part: FASTENER — MISSING (ZONE 300) · airframe 67,122 hrs · 35,547 cycles

MISSING FASTENERS IN BOTTOM LEG OF LEFT SKATE ANGLE APPROXIMATELY STATION CANT FRAME 1431 (VERTICAL STABILIZER). INSTALLED DOUBLER WITH CORRECT AMOUNT OF FASTENERS IN BOTTOM LEG OF LEFT SKATE ANGLE IN ACCORDANCE WITH AARD 53-10-00-2.

Part: SEAT TRACK — MISREPAIRED (COCKPIT) · airframe 67,122 hrs · 35,547 cycles

FIRST OFFICER SEAT TRACK REPAIR TEES INCORRECT AT STATION 148 ON FLIGHT DECK. REMOVED AND REPLACED SEAT TRACK TEES PER DRAWING EDK1346.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,122 hrs · 35,547 cycles

CORROSION ON FLOORBEAM AT STATION 1338 RIGHT SIDE (LAVATORY). REPLACED RIGHT OUTBOARD TOP ANGLE AT STATION 1338 ON FLOORBEAM IN ACCORDANCE WITH SRM 53-05-00.

Part: CUSP WEB — CRACKED (ZONE 200) · airframe 67,122 hrs · 35,547 cycles

CUSP CRACKED AT RIGHT CABIN AREA. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BRACKET — BROKEN (ZONE 100) · airframe 67,122 hrs · 35,547 cycles

FLOORBOARD SUPPORT (INTERCOSTAL) TIE BRACKET BROKEN AT STATION 598 BUTTLINE 0. INSTALLED NEW FITTING IN ACCORDANCE WITH SRM 51 30 00.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 67,122 hrs · 35,547 cycles

CRACK IN RIGHT WINDOW FRAME FORWARD OF STATION 1060 UPPER CORNER. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: LUG — CRACKED (LE SLAT) · airframe 67,122 hrs · 35,547 cycles

OUTBOARD ATTACH FITTING (RIB) OF RIGHT NR 5 SLAT HAS A CRACKED LUG. REPLACED ATTACH LUG PER ESO 80117.

Part: WINDOW FRAME — CRACKED (ZONE 100) · airframe 67,122 hrs · 35,547 cycles

CRACK IN RIGHT WINDOW FRAME FORWARD OF STATION 1079 UPPER CORNER. INSTALLED DOUBLER PER AARD53-10-00-25.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 67,122 hrs · 35,547 cycles

NUMBER FOUR SEAT TRACK CORRODED AT STATION 237. REPAIRED BY INSTALLING PLUG AND CHANNEL IN ACCORDANCE WITH AARD 53 20 00 10.

Part: BRACKET — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,122 hrs · 35,547 cycles

GIRT BAR SUPPORT STRUCTURE FORWARD BRACKET CORRODED. INSTALLED NEW GIRT BAR SUPPORT BRACKET PER SRM 51-01.

Part: RIB — CRACKED (LE SLAT) · airframe 67,122 hrs · 35,547 cycles

LEFT NR 5 SLAT OUTBOARD ATTACH RIB CRACKED. REPLACED CRACKED RIB PER ESO 80117.

Part: TEE FITTING — CRACKED (CARGO DOOR) · airframe 67,122 hrs · 35,547 cycles

TEE BRACKET AT CARGO DOOR HAS CRACKED TEE FITTING. INSTALLED NEW TEE ANGLE PER SHOP ESO 80174.

Part: ATTACH FITTING — CRACKED (ZONE 200) · airframe 67,122 hrs · 35,547 cycles

CRACK IN WINDOW FRAME BOTTOM CORNER RIGHT SIDE AT STATION 1022. INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53-10-25.

Part: FRAME — CRACKED (ZONE 200) · airframe 67,122 hrs · 35,547 cycles

CRACK IN RIGHT WINDOW FRAME UPPER CORNER AT STATION 1041. INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53-10-00-25.

Part: MAGNETIC PLUG — LEAKING (APU) · airframe 64,718 hrs

EWR INFLIGHT T1883/13FEB - CREW REPORTED SMOKE IN CABIN AFTER TAKEOFF. RETURNED TO EWR AND LANDED WITHOUT INCIDENT. FOUND AUXILLIARY POWER UNIT (APU) LEAKING OIL AT OIL TANK MAGNETIC PLUG. REPLACED O-RINGS ON MAGNETIC PLUG. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PUMP — INOPERATIVE (RT HYD SYSTEM)

SAN INFLIGHT T1429/19DEC - LOST RIGHT HYDRAULIC SYSTEM FLUID. INDICATION SHOWED FLUID LOSS BUT NO PRESSURE LOSS. LOWERED LANDING GEAR MANUALLY. LANDED SAN WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE DRIVEN PUMP AND FILTERS AND REPLACED ELECTRONIC DRIVEN AUXILIARY PUMP AND RIGHT SYSTEM RETURN LINE FILTERS. SERVICED HYDRAULIC QUANTITY TO FULL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

ATL - EMERGENCY LIGHT AT COCKPIT OVERHEAD PANEL INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT COCKPIT OVERHEAD PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PIPE — CRACKED (FUEL SYSTEM)

LGA - CLIMBING THROUGH 10000 FEET NOTICED UNWANTED FUEL TRANSFER FROM CENTER TANK TO LEFT WING TANK. RETURNED TO LGA AND LANDED WITHOUT INCIDENT. FOUND PIPE CRACKED IN LEFT HAND WING TANK. REPLACED LEFT WING MAIN TANK FUEL SYSTEM PIPE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - CEILING EMERGENCY LIGHTS ABOVE SEAT ROWS 28 THROUGH 31 INOPERATIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS ABOVE SEAT ROWS 28 THROUGH 31. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DTW - EMERGENCY LIGHTS IN AFT AIR STAIR COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT AIR STAIR COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SENSOR — FAULTY (NLG)

ON GEAR RETRACTION AFTER TAKEOFF NOSE LANDING GEAR POSITION INDICATOR REMAINED RED. RECYCLED GEAR. NOSE LANDING GEAR POSITION LIGHT STILL REMAINED RED. NOSE LANDING GEAR INDICATOR PIN ON CENTER CONSOLE. COMPLETELY RETRACTED. ON GEAR EXTENSION, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED. NOSE LANDING GEAR VISUAL INDICATOR PIN ON THE CENTER CONTROL PEDESTAL WAS FULLY EXTENDED INDICATING NOSE GEAR DOWN AND LOCKED. LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR SENSOR D1-32. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW FWD EMERGENCY OVERWING LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD EMERGENCY OVERWING LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW EMERGENCY AUXILLARY LIGHTS AT L2 245 AND L2 246 LEFT AND RIGHT AT STATION 916 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK B5 105 L2 245 L2 246 LEFT AND RIGHT AT STATION 916. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — DISCHARGED (CABIN)

DTW FIRST CLASS OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY FOR FIRST CLASS OVERHEAD EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY CEILING LIGHTS OVER ROWS 8 THROUGH 11 INOPERATIVE. REPAIRED LOOSE BATTERY CONNECTION FOR EMERGENCY CEILING LIGHTS OVER ROWS 8 THROUGH 11. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FRAME — CRACKED (FUSELAGE)

TUL - FOUND CRACK IN CANT FRAME 1485 WEB UPPER LEFT CORNER. DOUBLER INSTALLED PER AARD 53-10-00-32. (M)

Part: FLASHLIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY EMERGENCY PORTABLE FLASHLIGHT INOPERATIVE. REPLACED FORWARD ENTRY EMERGENCY PORTABLE FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

TPA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT SEAT 9 INOPERATIVE. REPAIRED BROKEN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: OVEN — SHORTED (GALLEY)

EWR - FLT 801 - EN ROUTE EWR-ORD, DURING CLIMB TO ALTITUDE DETECTED A BURNING ODOR IN CABIN AND COCKPIT. RETURNED EWR AND LANDED WITHOUT INCIDENT. REPLACED FIRST CLASS GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — FAILED (TAIL)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN AFT HALF OF CABIN INOPERATIVE. REPAIRED SHORTED WIRE IN TAIL COMPARTMENT FOR EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SKIN — CORRODED (BS 712-731)

TUL - FOUND CORROSION ON FUSELAGE SKIN IN MID CARGO BELLY AREA STATION 712 THROUGH 731 LONGERON L30 THROUGH L29RT. SRM 53-04 FIG 12B AND ESO 80559, DATED 12-2-99 RFS GENERATED RFS 225844. (M)

Part: BLADE — BROKEN (NR 2 ENGINE)

SYR - FLT 303 - DURING CRUISE AT 31,000 FEET, FLIGHT CREW HEARD A LOUD NOISE LIKE A COMPRESSOR STALL. CAPTAIN NOTICED NR 1 ENGINE N2 DROPPED TO IDLE POWER. FLIGHT CREW DECLARED AN EMERGENCY, SECURED NR 1 ENGINE AND DIVERTED TO SYR. AIRCRAFT LANDED SYR WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE TURBINE FAILED. REPLACED NR 1 ENGINE, PERFORMEDENGINE RUN UP. SYSTEM GROUND CHECKED NORMAL OPERATION.A 4TH STAGE TURBINE BLADE FAILED JUST ABOVE THE ROOT PLATFORM DUE TO HIGH CYCLE FATIGUE. THE LIBERATION OF THE BLADE CAUSED EXTENSIVE DAMAGE TO THE 3RD AND 4TH STAGE AND SUBSEQUENTLY CA USED COMPRESSOR STALL. (M)

Part: CONNECTOR — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN AFT COACH CABIN INOPERATIVE. MAINTENANCE FOUND A BROKEN CONNECTOR. REPLACED CONNECTOR TO EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SHEAR TIE — CRACKED (BS 1309)

TUL - SHEAR TIE CRACKED AT STA 1309, LONGERON 16L. REPLACED SHEAR TIE PER SRM 53. TST: 33,449.15 HOURS. CYCLES: 18,839. (X)

Part: SEAT TRACK — CORRODED (BS 386)

TUL - SEAT TRACK NR 4, STA 386 - STA 387, HAS CORROSION AT THE CENTER. CUT OUT DAMAGED AREA AND INSTALLED PLUG, PN 7452952-3, PER SRM CHAPTER 53. TST: 33,449.15 HOURS. CYCLES: 18,839. (X)