N484DA

Part: SKIN — CRACKED (FUSELAGE)

FOUND ON E1 LETTER CK, 2 CRACKS AT L-4 WINDOW CUTOUT LOWER INBD FASTENER HOLES. REPAIRED PER SRM 53-30-3.

Part: SKIN — CRACKED (BS 360-480)

LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 13 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 366912-14AD, REV A.

Part: SKIN — CRACKED (BS 681-740)

CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS ALONG THE PANEL. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 366914-14AD, REV A.

Part: SKIN — CRACKED (BS 360-480)

LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 6 CRACKS ALONG THE PANEL. THE SKIN LAP WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366911-14AD, REV A.

Part: SKIN — CORRODED (BS 720-740)

THE LOWER FUSELAGE SKIN OF THE STRINGER 26L SKIN LAP SPLICE WAS FOUND CORRODED BETWEEN FS 720 +17 AND FS 740 NEAR AN A/C DUCT CUTOUT. THE DAMAGED SECTION OF SKIN WAS CUT AWAY AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 366954-14, REV A.

Part: SWITCH — LOOSE (AIRSTAIR)

YELLOW AFT AIRSTAIR LIGHT CAME ON DURING TAKEOFF ROLL. FOUND SWITCH (P/N AN3167-1) LOOSE IN BRACKET (P/N 69-20985-6), REFERENCE IPC 52-70-00-49, ITEM 15 AND 20. TIGHTENED SWITCH, ADJUSTED SWITCH, CHECKS NORMAL.

Part: STRINGER — CRACKED (VERT STAB)

VERT FIN STR 9L CRACKED FIN STA 110.400. REPAIRED PER MM 55-30-0.

Part: SKIN — CRACKED (NR 2 ENGINE)

FOUR CRACKS AT FASTENER HOLES FWD OF PNL 9501 RT SIDE. REPAIRED PER MM 54-30-0.

Part: FRAME — CRACKED (PAX DOORWAY)

FOUND AT D-2 LETTER CHECK, .5 INCH VISIBLE CRACK AT RT FRAME AFT ENTRYWAY APPROX 6 INCHES BELOW UPPER STOP. REPAIRED PER SRM 53-10-9.

Part: BRACKET — CRACKED (NR 2 LE FLAP)

LTR CHK D-2 1/6/99, CRACK IN UPPER O/B RADIUS NR 2 L/E FLAP ACTUATOR MOUNT BRACKET. REPAIRED PER MM 57-20-21.

Part: FRAME — CRACKED (R-1 DOOR)

FOUND ON D2 LETTER CK, .75 INCH CRACK IN R-1 DOOR AFT LOWER FRAME. REPAIRED PER MM 52-12-0.

Part: SKIN — CORRODED (BS 560)

CORROSION WAS FOUND IN THE SKIN AT THE STRINGER 26L LAP SPLICE. THE CORRODED AREA WAS TRIMMED OUT AND AN EXTERNAL ALUMINUM REPAIR DOUBLER WAS INSTALLED. THE SKIN LAP WAS SEPARATED AND INSPECTED FWD AND AFT OF THE DAMAGED AREA AND WAS RESTORED WITH PROTRUDING HEAD OVERSIZE RIVETS PER THE B727 SRM. THE REPAIR WAS ACCOMPLISHED PER ER/A 365312-14 REV C.

Part: SKIN — CORRODED (BS 660)

THE FUSELAGE SKIN WAS FOUND CORRODED AT THE STRINGER 26L LAPSPLICE. THE CORRODED AREA WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 365330-14, REV B.

Part: BRACKET — CRACKED (NR 2 LE FLAP)

A .5 INCH CRACK NR 2 L/E FLAP ACT ATTACH BRACKET, LOWER FWD END. FOUND ON D1 LTR CHECK. INSTALLED DOUBLER PER M/M 57-20-21.

Part: CASTING — CRACKED (NR 13 SPOILER)

NR 13 SPOILER ACT I/B AND O/B ATTACH CASTINGS ARE BROKEN. REPLACED PER M/M 57-42-0.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHT ABOVE ROW 26 INOP. REPLACED LIGHT ASSY.

Part: DOOR FRAME — CRACKED (L2 DOOR)

A .75 IN CRACK L2 DOOR FRAME CUTOUT NEXT TO UPPER FWD STOP CASTING. INSTALLED REPAIR PER MM 53-10-0 PG 808.

Part: BEAM — CRACKED (BS 1273)

A CRACK WAS FOUND IN THE UPPER FWD TRANSVERSE BEAM ANGLE AND GUSSET AT FS 1273. THE DAMAGED PARTS ARE LOCATED IN THE TORQUE BOX WHICH IS THE SUBJECT OF THE AD 94-07-08 AND REQUIRES INSP. PER S/B 53-0129 -CO. REPLACE PART, 1273 UPPER FWD TRANSVERSE BEAM ANGLE WITH 69-67881-1 PER DWG 65C13874. REPLACE FS 1273 FWD GUSSET ANGLE WITH 65-17518-6 PER DWG 65C13874. THIS DOES NOT TERMINATE INSPECTIONS.

Part: SEAT TRACK — BROKEN (BS 344)

LT I/B SEAT TRACK BROKEN AT CORNER AROUND BOLT HOLE STA 344. REPAIRED PER SRM 53-10-5 FIG 7 SHEET 4.

Part: LIGHTING — INOPERATIVE (CABIN)

EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE ROW 25 AND AFT. REPAIRED AFT SECTION OF INTERIOR EMERGENCY TRACK LIGHTING SYS. OPS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY FLOOR LIGHTS OUT FROM ROW 27 TO REAR OF CABIN. REPLACED POWER SUPPLY, CHECKS NORMAL.

Part: PROX SENSOR — MALFUNCTIONED (LT MLG)

ON T/O WITH GEAR RETRACTED, HANDLE IN UP POSITION, GOT LT MAIN GEAR RED UNSAFE LIGHT. REPLACED LT MAIN GEAR UP PROX SENSOR. ALSO, AS A PRECAUTIONARY REPLACED LDG MOD.

Part: STIFFENER — CRACKED (WING)

FOUND ON B1 LETTER CHECK, 2 INCH CRACK IN WING L/E SPAR STIFFENER AT NR 6 SLAT INBD TRACK. REPLACED STIFFENER PER MM 57-20-21.

Part: ANGLE — CRACKED (SPAR)

FOUND ON B-1 LETTER CHECK, TWO L/E SPAR STIFFENERS CRACKED .50 INCH, ONE AT NR 3 SLAT INBD TRACK, THE OTHER AT NR 2 SLAT OUTBD TRACK. REPLACED ANGLES PER MM 57-20-21.

Part: ANGLE — CRACKED (NR 7 SPOILER)

FOUND ON B1 LETTER CHECK, NR 7 SPOILER ATTACH CASTING CRACKED AT LOWER WING ATTACH. REPAIRED PER MM 57-20-22.

Part: SKIN — PUNCTURED (RT ELEVATOR)

DURING A SHOP INSPECTION FOUND PUNCTURE DAMAGE TO RT ELEVATOR SKIN AT AT THE OUTBOARD END. REPAIR WAS INSTALLED PER SRM 55-20-3.

Part: ELEVATOR — DAMAGED (RIGHT)

DURING SHOP INSPECTION, RT ELEVATOR WAS RESTORED PER SRM 55-20-3.

Part: BATTERY — DISCHARGED (CABIN)

CENTER AISLE OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES, CKS NORMAL.

Part: SKIN — CORROSION (BS 259.5-312)

CORROSION AT AN EXISTING EXTERNAL REPAIR DOUBLER ON THE LOWER FUSELAGE SKIN PANEL, BETWEEN BS 259.5 AND BS312, AT STRINGER 20R. REMOVAL OF THE DOUBLER REVEALED EXTENSIVE CORROSION DAMAGE. THE SKIN WAS TRIMMED TO REMOVE CORROSION DAMAGE BELOW THE FORWARD LAVATORY SERVICE DOOR. A NEW EXTERNAL REPAIR DOUBLER WILL BE INSTALLED PER DL ERA 302687-14.

Part: ANGLE — CRACKED (FS 1263)

CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND THE AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. REPAIRED PER ERA 302109-14AD.

Part: SKIN — CRACKED (NR 3 LE SLAT)

FOUND DURING A-2 LETTER CHECK, CRACK IN LWR COVE SKIN SUPPORT ANGLE, BELOW TAI DUCT ON NR 3 SLAT. REPAIRED PER SRM 57-54-0.

Part: SKIN — CRACKED (NR 6 LE SLAT)

FOUND DURING A-2 LETTER CHECK, NR 6 SLAT COVE SKIN ANGLE, UNDER TAI DUCT CRACKED. REPAIRED PER SRM 57-54-0.

Part: RIBS — CRACKED (NR 3 LE SLAT)

DURING SHOP INSPECTION, LEFT WING NR 3 LEADING EDGE SLAT WAS FOUND WITH INTERNAL SUPPORT RIBS NR 7 AND NR 9 CRACKED. REPAIRED PER SRM 57-54-0.

Part: STIFFENERS — CRACKED (FS 1263/1273)

DURING INSPECTION AT LETTER CHECK, THE RT TORQUE BOX HAD STIFFENERS/BEAMS CRACKED AT BOTH FS 1263 AND FS 1273. THE DAMAGED PART WILL BE REPLACED IN ACCORDANCE WITH B727 S/B 53-0129, REV 4.

Part: STIFFENER ANGLE — CRACKED (LEFT WING)

DURING LETTER CHECK, A 3 INCH CRACK WAS FOUND IN THE VERTICAL STIFFENER ANGLE ON THE WING FRONT SPAR ON THE OUTBOARD SIDE OF NR 3 SLAT OUTBOARD TRACK ROLLER FITTING. REPAIRED PER MM 57-20-21 PG. 813.

Part: SKIN — CRACKED (RT SIDE S DUCT)

DURING LETTER CHECK, THE NR 2 ENGINE S DUCT HOUSING RIGHT SIDE OUTER SKIN WAS FOUND WITH A 1.25 INCH CRACK EXTENDING UP FROM ACCESS PANEL 9524. REPAIRED PER MM 54-30-0 PG 803.

Part: SLAT RIB — CRACKED (LEFT WING NR 4)

DURING LETTER CHECK, FOUND LEFT WING NR 4 LEADING EDGE SLAT WITH A .5 INCH CRACK IN THE NOSE RIB JUST OUTBOARD OF ACTUATOR ROD ATTACH FITTING. REPAIRED PER MM 57-54-0.

Part: SLAT — CRACKED (LEFT WING)

DURING LETTER CHECK, LEFT WING NR 4 LEADING EDGE SLAT WAS FOUND WITH TWO .5 INCH CRACKS ON THE LOWER SKIN IN THE RADIUS OF THE INBOARD SLAT TRACK FAIRING. REPAIRED PER MM 57-54-0.