N415DA

Part: ACCESSORY UNIT — MALFUNCITONED (NLG)

AFTER GEAR EXT, NOSE GEAR GREEN DOWN AND LOCK FAILED TO ILLUM. DIVERTED INTO JFK. REPLACED LANDING GEAR ACCESSORY UNIT.

Part: SEAL — LEAKING (NR 2 ENGINE)

DURING CRUISE AT FL290, NR 2 ENG OIL QNTY DECREASED TO ZERO GAL. OIL PRESS LOW LIGHT ILLUMINATED OIL TEMP RAISE TO 130 OIL PRESS 17 PSI ENG SHUTDOWN PER CHECKLIST WINDMILLED FOR 22 MINS. PRIOR TO SHUTDOWN OTHER INSTRUMENTS NORMAL. MAINTENANCE T/S FOUND FUEL PUMP/GEAR BOX CARBON SEAL LEAKING. MTC IN WORK REPLACING SEAL PER M/M.

Part: BATTERY PACK — DISCHARGED (RT EMER EXIT)

ON L/O, FOUND RT OVERWING EXIT EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. OPS NML.

Part: LIGHT — FAILED (COCKPIT)

COCKPIT OVER DOOR EMERGENCY LIGHT FAILED TO TEST. REPLACED, OPS NORMAL.

Part: BATTERY PACK — DISCHARGED (BS 800)

AFT OVERHEAD EMERGENCY EXIT SIGN WOULD NOT ILLUM WHEN TESTED. REPLACED BATTERY CARTRIDGE AND RACK ASSY CKS NORMAL.

Part: ANGLE — CRACKED (BS 1273)

FOUND ON C1 LETTER CK, HORIZONTAL TORQUE BOX ANGLE CRACKED AT STA 1273 RT LOWER TORQUE BOX. REPAIRED PER SRM 53-10-10.

Part: BATTERY — DISCHARGED (CABIN)

LFT AFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY, OPS OK.

Part: STRINGER — CORRODED (BS 950)

STG 28R WAS FOUND WITH CORROSION FROM FS 950F+10 AFT. THE STG WAS CUT AT FS 950E+10 AND WILL BE REPLACED AFT TO THE FACTORY SPLICE AT FS 1010. REPAIRED PER ERA 331405-14.

Part: SKIN — CRACKED (L1 DOORWAY)

A TIME LIMITED REPAIR AT THE L1 DOOR UPPER HINGE CUTOUT WAS REMOVED AND THE SKIN AND INTERNAL STRUCTURE WAS INSPECTED. THE STRAP WAS FOUND CRACKED AS WELL AS 4 OTHER HOLE LOCATIONS IN THE SKIN ASSY. REPAIRED PER ERA 331410-14.

Part: SEAL RING — WORN (NR 2 ENGINE COWL)

MV-2, FOUND NR 2 ENG FIREWALL COWLING SEAL RING 9 O'CLOCK POSITION WORN THRU. REMOVED DAMAGE PER MM 53-11-00 PG 801, FABD REPAIR INSTALLED PER AND PAINTED.

Part: BRACKET — CRACKED (RT LE FLAP ACT)

BRACKETS CRACKED RT WING L/E ATTACH BRACKETS FOR THE NR 5 KRUEGER FLAP ACTUATOR ARE CRACKED, O/B BRACKET LOWER CORNER AND I/B BRACKET UPPER CORNER. STOP DRILLED CRACKS. STOP DRILLS OK. OK TO INSTALL REPAIRS PREVIOUS REPAIR PER MM 57-20-21 FIG 807 ALREADY EXISTS. FABRICATED REPAIR DOUBLER PER MM 57-20-21 FIG 807. REPLACED O/B BRACKET PER SRM 51-00. REMOVED AND REINSTALLED NR 5 KRUEGER FLAP ACTUATOR, REPLACED PER M/M 57-20-21 CONT NR 944.

Part: SKIN — CRACKED (S DUCT HOUSING)

FOUND DURING B-2 LETTER CHECK, 1 INCH CRACK S-DUCT HOUSING 10 FT AFT NR 2 ENG INLET BELOW ACCESS PANEL. REPAIRED PER M/M 54-30-0.

Part: SKIN — CRACKED (NR 2 ENG INLET)

FOUND DURING B-2 LETTER CHECK, 3 EA .75 INCH CRACKS IN OUTER SKIN OF NR 2 ENG INLET AT 3 O'CLOCK POSITION. REPAIRED PER M/M 54-30-0.

Part: BULB — BROKEN (CABIN)

EMERGENCY PATH LIGHT AT ROW 1 HAS A BROKEN LIGHT ELEMENT. RELAMPED, OPS NML.

Part: WEB — CRACKED (BS 1303)

FOUND TWO 1.5 INCH CRACKS AT LOWER LT AND RT CORNERS OF VERTICLE WEB AT STA 1303 ABOVE THE 'S' DUCT. REPAIRED PER SRM 53-10-4, FIG 17.

Part: RIB — CRACKED (NR 4 SLAT)

FOUND ON MV1 CHECK, REFERENCE EO 04-05512-12 OPN 0304, WHILE BORESCOPING SLAT TRACK BOLT HOLES, FOUND .75 INCH CRACK IN L/E RIB NR 4 SLAT AT I/B TRACK I/B RIB. REPAIR: REPAIRED PER M/M 57-54-00, FIG 813A.

Part: FRAME — CRACKED (L 2 DOOR)

FOUND ON MV1 CHK L-2 DOOR S/N 1097 HAS .50 INCH CRACK AT FWD FRAME UPPER HINGE CUTOUT. REPAIR: REPAIRED PER SRM 52-40-2, FIG 4.

Part: SKIN — CRACKED (NR 2 INTAKE)

A 6 INCH BY .25 INCH CRACKS FROM RIVETS ON LT VERT SPAR SKIN, JUST FWD AND BELOW BOTTOM CORNER OF SADDLE PANEL 9501. ALSO, 2 INCH BY .25 INCH CRACKS ON RT SIDE SAME LOCATION AS ITEM 1 ABOVE, AT NR 2 INTAKE STRUCTURE. REPAIRED PER MM 54-30-0.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

DURING LAYOVER, R-2 DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK OPERATION NORMAL.