N478DA

Part: WIRE — BROKEN (CABIN)

EMERGENCY EXIT FLOOR LIGHTS DO NOT WORK FROM ROW 28 BACK. REPAIRED BROKEN WIRES AT END OF TRACK.

Part: WEB — CRACKED (BS 1275)

RT VERTICAL TORQUE BOX WEB CRACKED .25 INCH PAST ROUTE OUT AT LIGHTNING HOLE STA 1275 RT UPPER HOLE. REPAIRED PER M/M 53-11-0 FIG 819.

Part: PANEL — CRACKED (LT ELEVATOR)

NR 2 LT BALANCE BOARD CLOSE OUT PANEL HAS A 2 INCH CRACK AT O/B END. REPAIRED PER SRM 55-20-3.

Part: SUPPORT — CRACKED (NR 8 SLAT ACT)

NR 8 SLAT ACTUATOR SUPPORT CRACKED I/B SIDE. REPAIRED PER MM 57-20-21.

Part: OVEN — FAILED (CABIN)

ELECTRICAL ODOR IN F/C REPORTED BY F/A. REPLACED FIRST CLASS OVEN.

Part: MEGAPHONE — INOPERATIVE (CABIN)

FOUNDED FWD MEGA PHONE INOP. REPLACED SAME, CKS OK.

Part: TORQUE BOX — CRACKED (BS 1263)

THE FS 1263 BEAM AND CHANNEL ON THE RT TORQUE BOX OF THE AFT VENTRAL STAIRWAY WERE FOUND WITH TYPICAL CRACKS PER S/B 53-0129. THE CRACKED PARTS WERE REPLACED PER THE S/B INSTRUCTIONS AND DOCUMENTED PER ER/A 363704-14AD.

Part: SKIN — DELAMINATED (NR 3 SPOILER)

FOUND ON F-2 LETTER CHECK, NR 3 SPOILER TOP SKIN DELAMINATED O/B END 23 X 9. MADE FIBERGLASS REPAIR PER SRM 57-50-6 FIG 1.

Part: WEB — CRACKED (BS 1273)

FOUND DURING F-2 LETTER CHECK, .0625 INCH CRACK AT UPPER EDGE OF TORQUE BOX LIGHTENING HOLE LT SIDE STA 1273. ROUTED OUT PER M/M 53-11-0.

Part: ANGLE — CRACKED (NR 7 SLAT)

FOUND DURING F-2 LETTER CHECK, NR 7 SLAT COVE SKIN ANGLE CRACKED O/B OF I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0.

Part: SKIN — CORROSION (BS 535)

THE FUSELAGE SKIN HAS A 2.3 BY 2.6 CUTOUT FOR A CORROSION REPAIR AT STA 535 BETWEEN STR 26R AND 27R. THE CUTOUT IS NEXT TO STR 27R BELOW THE LAP JOINT. THE REPAIR WAS APPROVED PER FAA/DER FORM 8110-3, DER DESIGNATION SO-831, DTD 6-5-97.

Part: SKIN — LOOSE RIVETS (RT AILERON)

RT O/B AILERON SKIN HAD LOOSE RIVETS ON UPPER SKIN. INSTALLED NEW SKIN SECTION REPAIR PER SRM 57-50-5.

Part: SPAR — WORN (RT AILERON)

RT O/B AILERON REAR O/B SPAR WORN. INSTALLED REPAIR DOUBLER PER SRM 51-40-03.

Part: VERTICAL WEB — CRACKED (BS 1303)

FOUND VERTICAL WEB CRACKED AT STA 1303 ON LT SIDE OF S-DUCT VIEWED FROM 48 SECTION. REMOVED CROSS SECTION REPAIRED PER SRM 58-10-4, FIG 17.

Part: SLIDE — LOOSE (R1 DOOR)

EMERGENCY ESCAPE SLIDE IN FORWARD GALLEY DOOR, FELL OUT OF ITS CONTAINER IN FLIGHT. SECURED SLIDE OK FOR SERVICE.

Part: PANEL — BROKEN (HORIZ STABILIZER)

ON WALK AROUND ON GROUND GEG, FOUND PANEL 9216 PARTIALLY MISSING FROM BOTTOM OF HORIZONTAL STABILIZER. ONE QUARTER OF PANEL WAS MISSING. REPLACED PANEL MFG P/N 65-20657-26.

Part: LIGHTS — INOPERATIVE (CABIN)

AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTS INOP. REPLACED SPLICE IN AFT SECTION, OPERATION NOW NORMAL.

Part: LOCK SWITCH — FAILED (NLG)

NOSE GEAR RED INTRANSIT LIGHT DID NOT ILLUMINATE WHEN GEAR RAISED. LIGHT TESTS GOOD, WORKED WELL WHEN GEAR LOWERED/CA. REPLACED NOSE GEAR LOCK SW, PERFORMED NLG RETRACTION ALL INDICATIONS NORMAL.

Part: BRACKET — CRACKED (LT WING)

FOUND DURING E-1 LETTER CHECK, NR 1 SLAT ACTUATOR SUPPORT BRACKET CRACKED I/B SIDE. REPAIRED PER MM 57-20-21 PG 812.

Part: BRACKET — CRACKED (NR 1 SLAT)

FOUND ON E1 LETTER CHECK, NR 1 SLAT ACTUATOR MOUNT BRACKET CRACKED ON O/B SIDE. REPAIRED PER M/M 57-20-21.

Part: WEB — CRACKED (FUSELAGE)

FOUND DURING E-1 LETTER CHECK, LIGHTENING HOLE AT RT FWD TORQUE BOX WEB CRACKED .1875 INCH. REPAIRED PER MM 53-11-0.

Part: SKIN — CRACKED (NR 4 LE FLAP)

FOUND ON E1 LETTER CHECK, 2 CRACKS IN OUTBD SURFACE OF NR 4 L/E FLAP, 1.5 INCH AND 2 INCH. REPAIRED AND REPLACED L/E FLAP.

Part: RIB — CRACKED (NR 4 LE SLAT)

DURING INSPECTION, NR 4 L/E SLAT INTERNAL SUPPORT RIB NR 5 AND NR 17 WERE FOUND CRACKED. REPAIRED PER MM 57-54-0.

Part: SKIN — CRACKED (NR 4 LE SLAT)

DURING INSPECTION, NR 4 L/E SLAT UPPER SKIN WAS FOUND CRACKED SEVERAL PLACES UNDER THE WING FENCE. REPAIRED SKIN PER MM 57-54-0.

Part: FUEL PUMP — FAILED (NR 2 ENGINE)

ON TAKEOFF ROLL WITH ALT POWER SET, NR 2 ENG ROLLED BACK AND SHUTDOWN ACCOMPANIED BY AUTO PACK TRIP. TAKEOFF ABORTED AND RETURNED TO GATE. INSPECTED NR 2 ENG INLET AND EXH FOR VISIBLE DAMAGE, NONE FOUND. REPLACED ENG DRIVEN FUEL PUMP, LEAK CKS GOOD. PERFORMED TAKEOFF PWR AND ENG RUN UP PER PFHB, ALL CKS GOOD.

Part: SKIN — CRACKED (BS 344)

DURING INSPECTION, FOUND FUSELAGE SKIN CRACKED BETWEEN 3 RIVET HOLES AT FS 344 BETWEEN STRINGERS 22L AND 23L. REPAIRED PER SRM 53-30-3 FIG 1.