N115DA

Part: WEDGE — DEBONDED (LT WING SLAT TE) · airframe 57,583 hrs · 27,575 cycles

LEFT WING OUTBOARD SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 418205-14.

Part: WEDGE — DEBONDED (RT WING SLAT TE) · airframe 57,583 hrs · 27,575 cycles

RIGHT WING OUTBOARD SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 418206-14.

Part: SMOKE — DETECTED (CABIN) · airframe 56,995 hrs · 27,258 cycles

ON TAKEOFF ROLL, SMOKE AND FUMES THROUGHOUT CABIN. PERFORMED DUCT BURN OUT FOR BOTH PACKS AND BOTH ENGINES. NO EVIDENCE OF FUMES FROM PNEU SYS AFTER DUCT BURN OUT. CONTINUE TO MONITOR AIRCRAFT.

Part: BATTERY — DISCHARGED (MID CABIN) · airframe 56,808 hrs · 27,156 cycles

MID LEFT AND RIGHT OVERHEAD EMERGENCY LIGHTS INOP REPLACED_BATTERY PACKS

Part: WIRE — SHORTED (CONTROL PANEL) · airframe 53,386 hrs · 25,538 cycles

AFTER FINDING CONDENSATION DRIPPING FROM COCKPIT OVERHEAD PANEL AT THE TOP OF C/B PANEL FOUND NUMEROUS BURNT WIRES ON P6-15 PANEL. REPAIRED WIRES PER MM CHAP 20.

Part: FITTING — DAMAGED (LT WING) · airframe 52,635 hrs · 25,201 cycles

THE O/B HOLE IN THE I/B SIDE OF THE LT KICKLOAD FITTING FOUND DAMAGED. THE HOLE WAS SLIGHTLY ELONGATED AND WORN UNDER THE NUT. THE HOLE WAS OVERSIZED AND SPOTFACED TO REMOVE DAMAGE. ER/A 334858-14AD.

Part: BULKHEAD — DAMAGED (NR 1 & 2 PYLON) · airframe 52,635 hrs · 25,201 cycles

WEAR DAMAGE FOUND ON THE I/B FLANGES OF BOTH THE NR 1 AND NR 2 PYLON AFT ENGINE MOUNT BULKHEADS. THIS DAMAGE IN CONJUNCTION WITH MULTIPLE NUT PLATE ATTACH RIVETS ON THE NR 1 PYLON GSE ATTACH HOLE REQURED THE HOLE TO BE ENLARGED TO INCORPORATE NEAREST ATTACH RIVET LOCATIONS. THE NR 2 PYLON AFT ENGINE MOUNT BULKHEAD WAS WORK IN THE LOCATIONS SHOWN IN FIGURE 2. 334780-14.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,635 hrs · 25,201 cycles

FUSELAGE SKIN FOUND CORRODED AND CRACKED AT STA 445 - 470, S-34R AND STA 466 AT S-33R S-34R. ER/A 334816-14.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,635 hrs · 25,201 cycles

EXISTING SKIN REPAIR FOUND CORRODED AT STA 1373 STR 34L. DAMAGE FOUND IN SAME AREA AT THE TEAR STRAP AND STRINGER. TWO LARGE DENTS FOUND IN THE SKIN AT STA 1329 AND 1351 AT STR 34L. ER/A 334806-14 REV A.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 52,635 hrs · 25,201 cycles

AFT PRESSURE BULKHEAD OIL CANNED AT BL 0 AND LBL 7 AT LOWER END. ER/A 334742-14.

Part: STRAP — CORRODED (FUSELAGE FRAME) · airframe 52,635 hrs · 25,201 cycles

C-1 DOOR FWD FRAME FAIL-SAFE STRAP AT STA 539.5 BETWEEN S-25R AND 32R WAS FOUND WITH CORROSION DAMAGE. DURING CORROSION REMOVAL SEVERAL FASTENER HOLES WERE DAMAGED. 334775-14.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 52,589 hrs · 25,179 cycles

EMERGENCY LIGHTS IN FIRST CLASS INOP. FOUND PINS 11 AND 12 WITH NO OUTPUT. REMOVED AND REPLACED BATTERY PACK POWER SUPPLY. LIGHT OPN CHECKED GOOD.

Part: LIGHT — INOPERATIVE (OVERWING) · airframe 51,848 hrs · 24,859 cycles

ON LAYOVER, FOUND 3 OVERWING EMERGENCY LIGHTS INOP. RELAMPED, CHECKS NORMAL.

Part: ENGINE — FAILED (RIGHT)

ON TAKOFF ROLL, RT ENG COMPRESSOR STALL AND EGT WENT TO 1081 DEG CELSIUS. ICING CONDITIONS PRESENT, ANTI ICE ON. ENGINE HAD METAL IN TAILPIPE ON GATE RETURN. REPLACED ENGINE.

Part: CHECK VALVE — FAILED (NR 2 ENGINE)

RIGHT GEN DRIVE LIGHT ILLUMINATED AFTER TAKEOFF. REPLACED PRESSURE SERVICE CHECK VALVE, LEAK CHECK GOOD.

Part: BOLT — LOOSE (NR 2 ENG MOUNT)

NR 2 ENGINE FWD MOUNT BOLTS LOOSE. RT FWD, 50 INCH/POUNDS. RT AFT, 500 INCH/POUNDS. LT FWD, 500 INCH/POUNDS. LT AFT, 2,000 INC/POUNDS. WHICH IS THE NORMAL TORQUE. NO GAP EXISTS BETWEEN THE MATING SURFACE OF THE FWD ENGINE MOUNTS. BOLTS REPLACED AND TORQUED PER ERA 360634-14.