N815AF

ATA 5753

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 8,827 hrs · 8,291 cycles

LEFT FLAP BOTTOM SKIN IS CRACKED BETWEEN TWO RIVETS ON FORWARD LAP JOINT BETWEEN FORWARD AND AFT FLAP SPARS, BETWEEN FLAP RIBS FIVE AND SIX. REMOVED DAMAGE AND INSTALLED DOUBLER AND FILLER IAW SRM 12-A-57-50-00-00A-664B-A.

ATA 5524

Part: MOUNT — DAMAGED (LT ELEVATOR) · airframe 7,252 hrs · 6,904 cycles

THIS ACFT WAS UNDERGOING REPAINT & SOME DAMAGE OCCURRED TO THE LT ELEVATOR AT THE INBD STATIC WICK MOUNT. THE DAMAGE WAS REPAIRED USING ENGINEERING REPAIR RM-12-000844 WITH ASSOCIATED STATEMENT OF APPROVED DESIGN DATA, SADD-12-0761. A FORM 337 WAS SUBMITTED FOR THIS REPAIR.

ATA 3421

Part: DISPLAY — FAULTY (EADI) · airframe 3,845 hrs · 3,725 cycles

DURING ROUTINE MX THE PILOTS EADI WAS FOUND TO BE FUZZY. THE EADI DISPLAY PN 066-03125-2500 WAS R & R WITH A SERVICEABLE UNIT OF THE SAME PN IAW MM 12-A-34-26-03-00A-920A-A, AND OPS CHECKED GOOD IAW 12-A-34-26-00-00A-903A-A.

ATA 3421

Part: EFIS — DEFECTIVE (ZONE 200) · airframe 3,454 hrs · 3,388 cycles

PILOT REPORTED COPILOTS EADI IS INOP. REMOVED ED462, PN 066-03125-2500, INSTALLED SERVICEABLE EXCHANGE ED462 UNIT OF THE SAME PN, SYS OPS CHECK GOOD IAW AMM CH 12-A-34-26-03-00A-920A-A.

ATA 2432

Part: SENSOR — FAULTY (ZONE 100) · airframe 3,454 hrs · 3,388 cycles

PILOT REPORTS THAT BATTERY NR1 INDICATES CONTINUOUS 457 AMP DISCHARGE WITH NO DEPLEATION OF VOLTAGE. THE BATTERY NR 1 CURRENT SENSOR PN 524.52.12.720 WAS R & R IAW AMM 12-A-24-30-08-00A-920A-A.

ATA 5751

Part: BALANCE WEIGHT — CORRODED (AILERON) · airframe 3,064 hrs · 2,931 cycles

DURNG ANNUAL INSP FOUND RT AILERON BALANCE WEIGHT TO HAVE CORROSION ON THE INBD END. INSTALLED NEW AILERON BALANCE WEIGHT AND BALANCED AILERON.

ATA 3240

Part: BRAKE DISC — BROKEN (MLG) · airframe 1,879 hrs · 1,735 cycles

DURING A 100 HOUR INSPECTION THE LEFT MAIN LANDING GEAR BRAKE OUTBOARD DISC WAS DISCOVERED TO BE CRACKED. REMOVED AND REPLACED THE BRAKE ASSEMBLY.