N405DA

Part: STIFFENER — CRACKED (LE SLAT)

I/B SPAR STIFFENER CRACKED NR 7 SLAT I/B TRACK. REPAIRED PER M/M 57-20-21 P 813.

Part: LIGHT — DAMAGED (R1 DOOR)

R1 DOOR EMERGENCY EXIT LIGHT DAMAGED. REPLACED EMERGENCY LIGHT ASSY.

Part: SKIN — CRACKED (BS 580)

LFEC INSPECTIONS PER SI 4-74176-12AD, REV J ON S26L LAP JOINT FROM BS 481-681 YIELDED SEVERAL CRACK INDICATIONS. ACCOMPLISHMENT OF THE HFEC CONFIRMED 4 CRACKS IN THE LOWER LAP ROW IN THE OVERLAPPED (LWR) SKIN. REPAIRED PER ERA 367594-14AD, REV A.

Part: WEB — CRACKED (BS 1249&1236)

RT INBOARD VERT TORQUE BOX WEB CRACKED AT UPPER FASTENER STA 1248 AND 1236. REPAIRED PER MM 53-11-0.

Part: BATTERY PACK — DISCHARGED (EMER EXIT)

FOUND ON PREFLIGHT, LT OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, OPS CKS NORMAL.

Part: RIB — CRACKED (WS 171.5)

UPPER CHORD OF THE LT WING RIB AT WS 171.5 WAS FOUND W/CRACKS. THE CRACKS WERE LOCATED EMANATING FROM FASTENER HOLES ON THE HORIZ FLANGE OF THE CHORD ANGLE UNDER WING STRINGERS 17 AND 20. REPAIRED PER ERA 332081-14.

Part: CHORD — CRACKED (BS 761)

DURING ACCOMPLISHMENT OF 4-58560-3AD, A CRACK WAS FOUND IN THE VERT FLANGE OF THE WING TO FUSELAGE UPPER ATTACH CHORD. CRACK PROPAGATES FROM THE EDGE OF THE CHORD ABOVE THE TWO FWD MOST FASTENER HOLES AND TRAVELS DOWN. REPAIRED PER ERA 332062-14AD.

Part: CHORD — CRACKED (WS 171.5)

UPPER CHORD ANGLE OF THE RT WING AT WS 171.5 WAS FOUND WITH TWO CRACKS. THE CRACKS WERE LOCATED AT FASTENER HOLES ON THE HORIZ FLANGE OF THE CHORD ANGLE UNDER STRINGERS 16 AND 19. ALSO, THE S18 TAB WAS CRACKED. REPAIRED PER ERA 332040-14.

Part: RIB — CRACKED (BS 760)

DURING ACCOMPLISHMENT OF 4-58560-3AD, A CRACK WAS FOUND IN THE VERTICAL FLANGE OF THE WING TO FUSELAGE UPPER ATTACH CHORD. THE CRACK PROPAGATES FROM THE EDGE OF THE CHORD ABOVE THE 2 FWD MOST FASTENER HOLES AND TRAVELS DOWN, THRU THE ENTIRE THICKNESS OF THE HORIZ FLANGE. REPAIRED PER ERA 332037-14AD.

Part: FITTING — CORRODED (LT WING)

LEFT WING FWD WING FITTING BORE HAS CORROSION AND SCORING, FOUND WHEN BUSHING REMOVED. REMOVED BTL PIN ON R/C 59, OPN 5508AD AND REMOVED FWD BUSHING PER M/M 57-41-11. FOUND CORROSION TO BE WITHIN .15 OF INNER EDGE OF TERMINAL FITTING AT 10 AND 11 O'CLOCK POSITION FACING AFT. MACHINE BORE TO 3500 PER SRM 53-40-01 PG 13. CORR REMOVAL COMPLETE, OK TO TREAT BORE. TREATED BORE, TURNED AND TREATED BUSHING, INSTALLED BUSHING.

Part: RIB — CRACKED (NR 1 TE MIDFLAP)

DURING SHOP INSPECTION, THE I/B AFT CLOSEOUT RIB WAS FOUND CRACKED AT LOWER AFT CORNER. THE RIB WAS REPAIRED PER 727 MM 57-52-0, FIG 808 BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER AND FILLER.

Part: SPAR — DAMAGED (RT TE FLAP)

AFT SPAR RAIL CRACKED 37 INCHES FROM I/B END OF FLAP. REPAIRED ON SO 529555 PER MM 57-52-0 FIG 802.

Part: ANGLE — REPAIRED (LT TE MIDFLAP)

DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 30 INCHES FROM O/B END OF FLAP. THE CRACK WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0 FIG 802.

Part: SKIN — CRACKED (NR 2 TE MIDFLAP)

DURING SHOP INSPECTION, THE AFT LOWER COVE SKIN WAS FOUND CRACKED IN THE CORNERS OF THE CUTOUT FOR I/B DRIVE ROD. THE CRACKS WERE ROUTED OUT AND A DOUBLER INSTALLED PER 727 MM 57-52-0 FIG 809.

Part: RIB — CRACKED (NR 6 LE SLAT)

AT HMV FOUND, RIBS CRACKED I/B AND O/B OF GUIDE TRACK NR 6 SLAT I/B GUIDE TRACK. REMOVED ARM, FABRICATED DOUBLER MM 57-54-00 PG 813A, INSTALLED DOUBLER PER SAME.

Part: ANGLE — CRACKED (NR 2 TE MIDFLAP)

DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 32 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 BY INSTALLING A DOUBLER.

Part: BULKHEAD WEB — CRACKED (BS 1303)

STA 1303 INSIDE OF VERT LOWER LT CORNER OF BULKHEAD WEB CRACKED. REMOVED EXISTING FASTENERS, STOP DRILLED CRACK, FAB AND DRILLED REPAIR DOUBLER PER SRM 53-10-4 FIG 17. REPAIRED PER SRM 53-10-4 FIG 17.

Part: BULKHEAD WEB — CRACKED (BS 1303)

STA 1303 INSIDE OF VERT RT SIDE CTR OF BULKHEAD WEB CRACKED AT CUTOUT FOR STR. REMOVED SECTION OF ANTI-ICE DUCT FOR ACCESS, REMOVED HORT SUPPORT BRACE FOR ACCESS, REMOVED EXISTING FASTENER AND DOUBLER. STOP DRILLED CRACK, FAB AND DRILLED REPAIR DOUBLER PER SRM 53-10-4 FIG 17. REPAIRED PER SRM 53-10-4 FIG 17. REINSTALLED ANTI-ICE DUCT AND HORT SUPPORT BRACE.

Part: FITTING — CRACKED (FUSELAGE)

FOUND AT A2 LETTER CH, 1.5 INCH CRACK LT INBD TENSION TIE BOLT CASTING. REPLACED FIITING PER DRAWING 65-17509 REV M AND COLD WORK AND SPOT FACE PER DRAWING 65-16350.

Part: BATTERY — DISCHARGED (CABIN)

AFT AIRSTAIR EMER LIGHT INOP. REPL BATT, OPS CK OK.

Part: LIGHT — INOPERATIVE (CABIN)

L1 DOOR EXIT SIGN EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY.

Part: BATTERY CHARGER — INOPERATIVE (CABIN)

E-PATH LIGHT INOP ROWS 12 TO 19. REPLACED BATTERY CHARGER.

Part: BULB — FAILED (CABIN)

1R DOOR EXT EMER LIGHT AND C2 AFT LIGHT INOP. REPLACED BULBS.

Part: BATTERY — DISCHARGED (AFT AIRSTAIRS)

AFT AIRSTAIRS EMERGENCY LIGHT INOP. REPLACED BATTERY, OPS GOOD.

Part: WEB — CRACKED (BS 1248/1228)

FOUR EACH CRACKS IN LT AND RT LOWER TORQUE BOXES AT VERTICAL WEB AT LIGHTENING HOLES STA 1238 RT, STA 1228 LT, STA 1248 LT. ALL CRACKS .25 INCH. ROUTED PER M/M 53-11-0-NR 15.

Part: ANGLE — CRACKED (NR 8 LE FLAP)

FOUND ON F2 LETTER CHECK, NR 8 SLAT CRACKED AT THE LOWER COVE SKIN ATTACH ANGLE AT THE OUTBOARD STOP. REPAIRED PER MM 57-54-0.

Part: LIGHT — CRACKED (R1 DOOR)

R1 DOOR SLIDE LIGHT INOP. REPLACED REFLECTOR LIGHT ASSEM.

Part: LIGHT — INOPERATIVE (CABIN)

L-1 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OP CKS GOOD.

Part: SKIN — CORRODED (FS 720)

DURING INSPECTION, CORROSION WAS FOUND ON THE BELLY SKIN ABOVE THE RAM AIR INLET. THE DAMAGE CUTOUT MEASURES 12 INCHES FWD AND AFT BY 10 INCHES INBD AND OUTBD AT FS 720C. IN ACCORDANCE WITH 8110-3 DATED 1/26/96, AN EXTERNAL DOUBLER AND TRIPLER WERE INSTALLED AROUND THE CUTOUT. AN PREEXISTING TI DOUBLER WAS REPLACED BY THIS REPAIR.

Part: SKIN — DENTED (C-3 CARGO DOOR)

DURING INSPECTION, C-3 CARGO DOOR OUTER SKIN WAS FOUND WITH THREE DENTS BEYOND ALLOWBLE LIMITS. REPAIRED SKIN PER SRM 52-30-1 FIG 9.

Part: ANGLE — CRACKED (NR 2 LE SLAT)

FOUND DURING E-2 LETTER CHECK, NR 2 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT. REPAIRED PER M/M 57-54-0 FIG 805.

Part: ANGLE — CRACKED (NR 7 LE SLAT)

FOUND DURING E-2 LETTER CHECK, NR 7 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED .375 INCH BELOW TAI DUCT. REPAIRED PER M/M 57-54-0 FIG 805.

Part: SOLENOID — FAILED (GEAR SELECTOR)

IRR - ON TAKEOFF, GEAR HANDLE WOULD NOT RAISE PAST THE OFF POSITION. PUT GEAR HANDLE BACK DOWN. DIVERTED TO DEN DUE TO GEAR HANDLE. CORRECTIVE ACTION - REPLACED LANDING GEAR HANDLE LATCH LEVER SOLENOID PER DELTA M/M 32-31-16. CYCLED GEAR SEVERAL TIMES, ALL NORMAL.

Part: ANGLE — CRACKED (FS 1263)

1.0 CRACK IN ANGLE OF FWD BEAM OF THE RT TORQUE BOX, FS 1263. REPAIRED PER DL ERA 301959-14.

Part: STIFFENER — CRACKED (RT WING)

FOUND DURING E-1 LETTER CHECK, WING SPAR STIFFENER AT NR 6 LE SLAT I/B TRACK O/B SIDE HAS 1 INCH CRACK FROM BOTTOM. REPAIRED PER M/M 57-20-21.