N2809W

Part: SKIN — CRACKED (BS 351)

THE UPPER FUSE SKIN AT BS 351 ON THE UPPER ROW OF THE S24R LAP SPLICE WAS FOUND CRACKED. THE CRACK EXTENDED THRU THREE CONSECUTIVE FASTENERS WITH A TOTAL LENGTH OF 3. REPAIRED PER ERA 366371-14.

Part: LIGHT — INOP (COCKPIT)

COCKPIT OVERHEAD EMERGENCY LIGHT PACK INOP ON TEST. REPLACED BATTERIES, CKS OK.

Part: LIGHT — ILLUMINATED (NLG WARN)

AFTER GEAR EXTENSION THE NOSE GEAR UNSAFE LIGHT ILLUMINATED WITH NO GREEN NOSE GEAR LIGHT. POM PROCEDURES COMPLIED WITH AND A SAFE INDICATION OBTAINED AFTER MANUAL EXTENSION PROCEDURES ACCOMPLISHED.

Part: SEQUENCE VALVE — CRACKED (RT MLG)

DURING CLIMBOUT, LOST 'A' SYSTEM HYDRAULIC PRESSURE AND FLUID QTY. FOUND RIGHT MLG DOOR SEQUENCING VALVE CRACKED. REPLACED VALVE. LEAK CHECK AND GEAR SWING GOOD.

Part: BATTERY RACK — DISCHARGED (ROW 18 ABCDEF)

SEAT ROW 18 ABCDEF OVERHEAD EMER LIGHT INOP. REPLACED BATTERY RACK OPS NOW NML.

Part: STRINGER — CORRODED (BS 950)

STRINGER 29L WAS FOUND CORRODED. THE STRINGER WAS TRIMMED AT STA 950D+10 AND THE AFT PORTION REMOVED. REPAIRED PER ERA 331787-14.

Part: STRINGER — CORRODED (BS 950)

FUSELAGE STRINGER 29R WAS FOUND WITH CORROSION AT FS 950E PLUS 10. A NEW SECTION OF STRINGER IS SPLICED IN. REPAIRED PER ERA 331848-14.

Part: SKIN — CRACKED (BS 700)

FUSELAGE BELLY SKIN WAS FOUND WITH CRACKS AND CORROSION AT STA 700 AND STR 28L - 28R. BELLY SKIN WILL BE REPLACED DUE TO NUMEROUS EXISTING REPAIRS. REPAIRED PER ERA 303637-14.

Part: SKIN — GOUGED (L1 DOORWAY)

FUSELAGE SKIN WAS GOUGED FWD OF THE L1 DOOR AT S10L LAP SPLICE. REPAIRED PER ERA 331851-14.

Part: SPAR CHORD — CRACKED (WS 340)

FRONT SPAR UPPER CHORD WAS FOUND WITH A CRACK IN THE FORWARD FLANGE AT A FASTENER HOLE AT APPROX WL340. REPAIRED PER ERA 331817-14.

Part: FRAME — CRACKED (BS 784)

FS 784 FRAME ON THE LT SIDE HAD TWO CRACKS AT THE SECOND HOLE UP FROM THE FLOOR LINE. REPAIRED PER ERA 331783-14AD.

Part: ACTUATOR — LOOSE (NR 13 SPOILER)

NR 13 SPOILER ACTUATOR MOUNT LOWER INBD AND OUTBD BOLTS ARE LOOSE. REPAIRED MOUNT HOLES IAW MM 57-42-0.

Part: TRUNNION — CRACKED (BS 940)

RT MLG TRUNNION BEAM SUPPORT FITTING AT FS 940 FOUND WITH 1.5 INCH FATIGUE CRACK ON INBRD SURFACE, WL 190. REPAIRED WITH FABRICATED DOUBLER PER ER/A 373040-14. CRACK FOUND DURING MID VISIT INSPECTION.

Part: FLOORBEAM — CORRODED (BS 344)

REMOVED EXISTING T-CAP REPAIR, FWD AND AFT SPLICE ANGLES, 1 VERTICAL STIFFENER AND 1 FLOORBOARD SUPPORT. REMOVED EXISTING T-CAP FROM C/L TO RBL 52. BEGAN DRILLING NEW T-CAP. COMPLETED FABRICATION OF REPAIR PER SRM 53-10-8 PG 56-57. INSTALLED T-CAP BEAM SPLICE REPAIR PER SRM 53-10-8 PG 56-57.

Part: ENGINE — BIRD STRIKE (NR 1/2)

AIRCRAFT FLEW THROUGH FLOCK OF GEESE. NR 1 AND 2 ENGINES WILL BE REPLACED. NR 3 WILL BE BORESCOPED. NR 6 SLAT WILL BE REPLACED. RADOME AND RADAR ANTENNA WILL BE REPLACED.

Part: TRUNNION FTG — CORROSION (RT MLG)

THE TRUNNION ATTACH FITTING OUTBOARD CLEVIS AND MATING TEE ATTACH FLANGE HAD CORROSION IN THE BORE. IN ADDITION, THE COUTER SINK THROUGH THE ATTACH FITTING LUG WAS FOUND TO EXTEND ALMOST COMPLETELY THROUGH THE LUG FLANGE. THIS DAMAGE WAS REMOVED BY OVERSIZED HOLE TO .847 DIA.

Part: SPAR CAP — DAMAGED (WS 770)

THE SUBJECT AIRCRAFT EXPERIENCED A COLLAPSE OF THE RT MAIN LANDING GEAR DURING LANDING ROLLOUT. THIS RESULTED IN DAMAGE TO THE RT WING FRONT SPAR LOWER CAP ON THE OUTBOARD END. THE EXTENT OF THE DAMAGE REQUIRED THAT THE LOWER CAP TO BE CUT AT APPROX FS 770 AND THE OUTBOARD SECTION REMOVED AND A NEW SECTION SPLICED IN. THIS REPAIR WAS APPROVED PER FAA/DER FORM 8110-3, DER DESGINATION SO-831, DATED 7-23-97.

Part: LIGHT — INOPERATIVE (CABIN)

AFT STAIRS EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, CHECKS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT FWD OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, CHECKS OK.

Part: SKIN — CRACKED (RT ELEVATOR)

FOUND A 1.5 IN CRACK RT ELEV LOWER SKIN FWD OF TAB. REPAIRED PER SRM 55-20-3.

Part: SKIN — CRACKED (BS 700)

SKIN CORROSION AND CRACK JUST FWD OF STA 700 BETWEEN STRINGERS 28L AND 28R NEAR BL 0. CUTOUT MEASURED 7.5 BY 3.75 INCH. REPAIRED PER DAL ER/A 303637-14, REV A.

Part: SKIN — CRACKED (BS 700)

THE SKIN JUST FWD OF STA 700 BETWEEN STR 28L AND 28R NEAR BL 0 WAS FOUND CRACKED AND CORRODED. REPAIRED WITH A DOUBLER AND TRIPLER PER FAA/DER FORM 8110-3, DER DESIGNATION SO-9-57.

Part: SKIN — CORRODED (BS 720)

SKIN CORROSION AT STA 720F AT STRINGER 27R. DAMAGE REMOVAL RESULTED IN A 1.75 BY 5 INCH CUTOUT JUST FWD OF AN EXISTING REPAIR AT STA 730, ERA 213172. EXISTING REPAIR REQUIRED THE REMOVAL OF THE CORNER OF THE LWR SKIN AT STA 740 AND STRINGER 26R. REPAIRED PER DAL ER/A 303611-14, REV A.

Part: SKIN — CORROSION (BS 720)

SKIN CORROSION AT FS 720F AT STR 27R. REMOVED A 1.75 INCH BY 5 INCH CUTOUT JUST FWD OF AN EXISTING REPAIR AT STA 730. ERA WILL INCORPORATE BOTH REPAIRS INTO ONE REPAIR.

Part: FLOOR BEAM — CORRODED (BS 1070)

FOUND ON MV1 CK, CORROSION/RIVETS SHEARD AT CABIN FLOOR BEAM STA 1070 AT RT O/B GALLEY FLOOR TRACK. REPAIRED PER M/M 53-20-11 FIG 804.

Part: FLOOR BEAM — CORRODED (BS 400)

FOUND CORROSION ON FLOOR BEAM UPPER ANGLE STA 400 RBL 55. REPAIRED PER M/M 53-20-11 PG 811 B.

Part: LIGHT — INOPERATIVE (L1 DOOR)

EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. REPLACED LIGHT ASSY AND BATTERIES.

Part: RIB — CRACKED (NR 6 LE SLAT)

DURING INSPECTION, NR 6 L/E SLAT WAS FOUND WITH INTERNAL SUPPORT RIB NR 11 CRACKED. REPAIRED PER MM 57-54-0.

Part: SKIN — CRACKED (NR 6 LE SLAT)

INNER SKIN CRACKED AT NUTPLATES, RIBS 10, 11, 12 AND 13. REPAIRED PER M/M 57-54-0, FOR NR 6 L/E SLAT.

Part: RIB — CRACKED (NR 6 LE SLAT)

DURING INSPECTION, FOUND NR 6 L/E SLAT WITH INTERNAL SUPPORT RIB NR 10 CRACKED. REPAIRED PER MM 57-54-0.

Part: ATTACH FITTING — BROKEN (LT MLG DR ACT)

LT MAIN LANDING GEAR DOOR OPENED IN FLIGHT. FOUND LANDING GEAR DOOR ACTUATOR ATTACH FITTING BROKEN, IPC 32-10-4 FIG 2 ITEM 250.

Part: SKIN — WORN (LT AILERON)

DURING INSPECTION, LEFT WING AILERON LOWER OUTBOARD SKIN HAD SEVERAL OVERSIZED AND WORN FASTENER HOLES DUE TO FATIGUE. SPLICED IN NEW SECTION OF SKIN PER MM 57-51-00, FIG 801.

Part: WEB — CRACKED (FS 294.5)

DURING INSPECTION, THE LT SIDEWALL WEB OF THE NOSE WHEEL WELL HAD A 1.25 INCH CRACK AT STA 294.5, APPROXIMATELY AT WL 170. THE DAMAGED PORTION WAS TRIMMED OUT AND A REPAIR DOUBLER AND STRAPS WAS INSTALLED IN ACCORDANCE WITH B727-53-145.

Part: ANGLE — CRACKED (NR 7 SLAT)

SLAT ANGLE CRACKED UNDER NR 7 SLAT I/B STOP PAD AREA. FOUND DURING LETTER CHECK, NR 7 L/E SLAT. INSTALLED REPAIR PER MM 57-54-0.

Part: STRINGER — CRACKED (BS 850)

A 1 INCH CRACK THROUGH HORIZ LEG OF STR 18A AND STA 950. REPAIRED PER MM 53-12-0, FOUND AT LETTER CHECK.

Part: BRACKET — CRACKED (NR 6 LE FLAP ACT)

FOUND AT LETTER CHECK, NR 6 L/E FLAP ACTUATOR MOUNT BOX CRACKED, I/B SIDE UPPER AND LWR CORNERS. REPAIRED PER MM 57-20-21.

Part: ANGLE — CRACKED (NR 1 SLAT ACT)

A 1.5 INCH CRACK AT NR 1 SLAT ACTUATOR O/B ATTACH ANGLE. REPAIRED PER MM 57 20-21.

Part: ANGLE — CRACKED (FS 1263)

CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT STA 1263. REPAIRED PER DL ERA302097-14AD.

Part: SKIN — GOUGED (NOSE)

DURING INSPECTION, FOUND TOOLING DAMAGE TO RT FUSELAGE NOSE AT FS 243.7, APPROXIMATELY HALFWAY UP THE SKIN PANEL. REPAIRED PER SRM 53-30-3 FIG 3.

Part: BULKHEAD — MISMFG (FS 178)

DURING INSPECTION, FS 178 RT BULKHEAD HAD AN ACCESS HOLE. INSTALLED PER SRM 53-10-0 FIG 3.

Part: RIB — CRACKED (NR 3 LE SLAT)

DURING SHOP INSPECTION, NR 3 SLAT PANEL WAS FOUND WITH L/E RIB NR 17 CRACKED. REPAIRED PER MM 57-54-00 FIG 809.

Part: BULKHEAD — MISMFG (NOSE)

DURING INSPECTION, LT FS 178 BULKHEAD HAD ACCESS HOLE. INSTALLED PER SRM 53-10-9 FIG 3.

Part: RIB — CRACKED (NR 3 SLAT)

DURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH SUPPORT RIB NR 9 CRACKED. REPAIRED PER SRM 57-54-0 FIG 805.