N472DA

Part: BATTERY PACK — DISCHARGED (CABIN)

RT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN)

FWD OVERWING EXTERNAL EMERG LIGHT INOP LT SIDE. REPLACED BATT PACK M654, OPS CHKS GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN)

LT OVRWING EXIT IDENT EMERG LIGHTS INOP. REPLACED BATT PACK M1090, OPS CHKS GOOD.

Part: POSITION IND — FAILED (TE FLAPS)

TRAILING EDGE DEVICES (OUTBOARD) SPLIT BETWEEN 0 DEG AND 2 DEG. ACCOMPLISHED TRAILING EDGE FLAP ABNORMAL CHECKLIST AND DIVERTED TO JFK. REPLACED OUTBOARD FLAP POSITION IND.

Part: STRINGER — CRACKED (BS 940)

SEVERAL OF THE FASTENER HOLES ON THE S18A STRINGER AT FS 940 OF BOTH RT AND LT SIDES WERE FOUND TO HAVE CRACKS AND OR CORROSION IN THEM. REPAIRED PER ERA 331316-14.

Part: BULKHEAD WEB — CRACKED (BS 870)

ON MV2, FOUND AT STA 870 BLKHD WEB IS CRACKED AT LWR END JUST LEFT OF DELTA BEAM. REMOVED DAMAGED SECTION OF WEB, FABD NEW REPAIR PER SRM 53-10-9 FIG 4, INSTALLED DOUBLER PER SAME.

Part: LIP — GOUGED (NR 2 PYLON)

AT MV2, FOUND DEEP GOUGE IN NR 2 PYLON LIP 5 O'CLOCK POSITION. FABRICATED REPAIR DOUBLER/FILLER PER MM 53-11-00 PG 801.

Part: STRINGER — CRACKED (VERT STAB)

AT MV2, FOUND STRINGER CRACKED FIN ATA 110.4 STR 10 LT STRINGER IS CRACKED INSIDE VERT STAB. FABRICATED REPAIR DOUBLER PER MM 55-30-00 FIG 803.

Part: COWL RING — WORN (NR 2 ENGINE)

AT MV2, FOUND COWL LANDING RING WORN SEVERAL PLACES AND TEMP REP AIR AT 6 CLOCK POS. INSTALLED NEW REPAIR PER MM 53-11-0 PG 801.

Part: ACTUATOR MOUNT — CRACKED (NR 2 LE FLAP)

AT MV2, FOUND CRACK NR 2 FLAP O/B MOUNT CORRODED. FABRICATED REP AIR DOUBLER PER MM 57-20-21 FIG 807. INSTALLED REPAIRED ACTUATOR MOUNT ON A/C.

Part: FLAP TRACK SHIM — MIGRATED (RT INBD TRACK)

DURING INSPECTION PER DAL SI 4-58662-12AD (AD 90-07-05), THE LAMINATED SHIM OF THE RT INBD FLAP TRACK WAS FOUND MIGRATED BEYOND THE .25 ALLOWED LIMIT. THE MIGRATED SHIM WAS REINSTALLED PER AD REQUIREMENTS AND ACCOMPLISHED PER ER/A 363668-14AD.

Part: LIGHT — INOPERATIVE (CABIN)

ON L/O, FOUND LT FWD ENTRY DOOR EXTERIOR EMERGENCY LIGHT OUT. REPLACED LIGHT ASSY, OPS CK GOOD.

Part: WEB — CRACKED (BS 1293)

A 1.375 INCH CRACK UPPER LT TORQUE BOX WEB LIGHTENING HOLE STA 1293. REPAIRED PER MM 53-11-0 PG 828.

Part: SKIN — CRACKED (VERT STAB)

A 1 INCH CRACK VERT STAB SKIN BELOW ROUND ACCESS PANEL 9523. REPAIRED PER MM 54-30-0 PG 803.

Part: WEB — CRACKED (BS 1293)

A .25 INCH CRACK PAST ROUTE OUT AT RT VERT TORQUE BOX WEB STA 1283. REPAIRED PER MM 53-11-0.

Part: SKIN — CRACKED (VERT STAB)

A 1 INCH CRACK AT VERT STAB SKIN BELOW ROUND ACCESS PANEL 9524. REPAIRED PER MM 54-30-0 PG 803.

Part: ANGLE — CRACKED (RT TE MIDFLAP)

NR 3 MIDFLAP LOWER AFT CHORD WAS FOUND CRACKED. THIS CHORD ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0.

Part: SKIN — CRACKED (RT LE FLAPS)

LOWER SKIN CRACKED AT O/B END. REPAIRED SKIN PER M/M 57-54-00 FIG 801.

Part: BATTERY PACK — DISCHARGED (CABIN)

LT AND RT FWD EMERGENCY SLIDE ILLUM LIGHTS INOP. REPLACED BATT PACK-CKS NML.

Part: FLOORBEAM — CORRODED (BS 344)

FOUND ON MV1 CHECK, CORROSION SEVERAL PLACES FLOORBEAM STA 344. REPAIRED PER SRM 53-10-8 FIG 11.

Part: BLKHD STIFFENER — CRACKED (FS 1183)

FOUND ON MV1 1183 BULKHEAD VERTICAL STIFFENER CRACKED 1 INCH AT LOWER END, BL 8L WL 185. REPAIR: REPAIRED PER M/M 55-11-0, PAR 9.

Part: WEB — CRACKED (FUSELAGE)

FOUND DURING A-2 LETTER CHECK, 2 CRACKS TORQUE BOX WEB UPPER ROW OF RIVETS FWD SIDE RT. REPAIRED PER MM 53-11-0 PAR 19.

Part: ANGLE — CRACKED (NR 4 LE SLAT)

FOUND DURING A-2 LETTER CHECK, NR 4 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT O/B END. REPAIRED PER MM 57-54-0 PAR 5A.

Part: SKIN — CRACKED (NR 2 LE SLAT)

FOUND DURING A-2 LETTER CHECK, NR 2 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT O/B END. REPAIRED PER MM 57-54-0 PAR 5A.

Part: ANGLE — CRACKED (FS 910)

FOUND DURING A-2 LETTER CHECK, ANGLE AT STA 910 CRACKED. REPAIRED PER M/M 53-11-0 PAR 20.

Part: SKIN — CRACKED (NR 1 LE SLAT)

FOUND DURING A-2 LETTER CHECK, NR 1 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0 PG 12.

Part: EEL RACK — FAILED (CABIN)

ON LAYOVER, FOUND RT OVERWING EMERGENCY EXIT SIGN INOP DURING TEST. REPLACED RACK ASSEMBLY OPERATION NORMAL.