N524DA

Part: DOOR — MALFUNCTIONED (RT MLG) · airframe 60,625 hrs · 47,346 cycles

AFTER TAKE-OFF, WHEN GEAR LEVER WAS MOVED TO -OFF- POSITION RT MAIN GEAR DOOR RE-OPENED. LEVER WAS MOVED TO -UP- AND DOOR CLOSED. RETURNED LEVER TO -OFF- AND DOOR STAYED CLOSED. VISUALLY INSPECTED DOOR AND OPERATING MECHANISM. NO PROBLEMS FOUND. OPERATED GEAR DOORS AND FOUND NORMAL.

Part: SIGN — INOPERATIVE (CABIN) · airframe 60,487 hrs · 47,163 cycles

L2 SVC DOOR OVERHEAD EMERGENCY EXIT SIGN INOP. REPLACED LIGHT RACK.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 60,369 hrs · 47,010 cycles

THE FS 1183 BULKHEAD WAS FOUND WITH A 1.5 INCH LONG TYPICAL CRACK IN THE WEB JUST BELOW THE LBL & RBL 8 STIFFENERS AT WL 182. THE CRACKS ARE TYPICAL OF BAC S/B 727-53-0175. THE CRACKS WERE CUT OUT OF THE WEB AND REPAIRED WITH TITANIUM DOUBLERS PER ER/A 377201-14.

Part: STIFFENER — CRACKED (NR 3 SLAT) · airframe 60,366 hrs · 47,008 cycles

A 2 INCH CRACK IN NR 3 SLAT O/B TRACK O/B SPAR STIFFENER. REPLACED STIFFENER PER M/M 57-20-21.

Part: WEB — CRACKED (TORQUE BOX) · airframe 60,366 hrs · 47,008 cycles

FOUND ON B1 LETTER CK, .5 INCH CRACK AT RT TORQUE BOX VERTICAL WEB UPPER LIGHTENING HOLE STA 1323. REPAIRED PER MM 53-11-0.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,128 hrs · 46,696 cycles

EMERGENCY LIGHT INOP AT R2 DOOR DURING SVC CHECK. REPLACED BATT PACK, OPS CKS OK.

Part: BATTERY — DISCHARGED (L1 DOOR)

L1 EMERGENCY EXIT DOOR LIGHT BATTERY WOULD NOT TEST. REPLACED BATTERY.

Part: SKIN — CRACKED (BS 680-740)

LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 4 CRACKS IN CONSECUTIVE FRAME BAYS. THE ENTIRE SKIN LAP WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367316-14AD.

Part: SKIN — CRACKED (BS 481-681)

LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER PANEL. INTERNAL HFEC INSPECTION CONFIRMED 14 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367317-14AD.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHT IN BETWEEN OVERWING EXITS INOP. REPLACED LIGHT ASSY.

Part: SLIDE — DISLODGED (L1 DOOR)

DURING TAKEOFF ROLL, L1 SLIDE PACK DISLODGED FROM DOOR. ACFT RETURNED TO BLOCK. RESECURED SLIDE PACK, CKS NORMAL.

Part: SKIN — DAMAGED (NR 2 TE MIDFLAP)

DURING SHOP INSPECTION, A HOLE WAS FOUND IN COVE SKIN PANEL AT 2ND FROM I/B AFT FLAP TRACK. THE SKIN WAS REPAIRED PER MM 57-52-0, FIG 809.

Part: STRINGER — DAMAGED (BS 1018)

S7L WAS GOUGED DURING INSTALLATION OF NEW GALLEY, DAMAGE IS IN INNER RADIUS AT BS 1018. REPAIRED PER ERA 332697-14.

Part: BULKHEAD RING — DAMAGED (BS 1183)

DURING INITIAL INSPECTION, A FASTENER AFT OF BS 1183 AT RBL 24 WAS FOUND LOOSE. DURING REMOVAL OF THE FASTENER, TOOLING DAMAGE WAS DONE TO THE TENSION FITTING AND THE SKIN AND ATTACH RING OF THE BS 1183 BLKHD. THE FITTING WAS REPLACED. REPAIRED PER ERA 332717-14.

Part: SKIN — DAMAGED (BS 990)

EXISTING TRIM OUTS AND ADDITIONAL GROUND DAMAGE WAS FOUND IN THE SKIN AT THE AFT EDGE OF THE C2 DOOR CUTOUT AT BS 990. THE DAMAGED AREAS ARE NEAR S24R. REPAIRED PER ERA 332684-14.

Part: SKIN — DAMAGED (NR 2 TE MIDFLAP)

DURING SHOP INSPECTION, THE AFT COVE SKIN WAS FOUND WITH TOOL DAMAGE 60 FROM O/B END. THE SKIN WAS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0 PAGE 819.

Part: SKIN — CRACKED (RT TE MIDFLAP)

DURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED AT 35 FROM THE I/B END. THE COVE SKIN WAS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0 FIG 809.

Part: SKIN — WORN (NR 2 TE MIDFLAP)

DURING SHOP INSPECTION, THE COVE SKIN WAS FOUND WORN 35 FROM O/B END OF FLAP. A REPAIR DOUBLER WAS INSTALLED PER MM 57-52-0, FIG 809.

Part: SKIN — DAMAGED (NR 2 TE MIDFLAP)

DURING SHOP INSPECTION THE COVE SKIN WAS FOUND TO HAVE A TEMPORARY REPAIR INSTALLED 34 FROM I/B END OF FLAP. THE SKIN WAS REPAIRED BY INSTALLING A PERMANENT REPAIR DOUBLER PER MM 57-52-0, FIG 809.

Part: SKIN — CRACKED (NR 2 TE MIDFLAP)

DURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED 31 INCHES FROM I/B END. A REPAIR DOUBLER WAS INSTALLED PER MM 57-52-0, FIG 809.

Part: BLKHD STIFFENER — CRACKED (BS 1183)

A CRACK WAS FOUND IN THE LBL 36.83 VERT STIFFENER ON THE FWD SIDE OF THE BS 1183 BLKHD. CRACK IS LOCATED APPROX AT WL 238 AND IS APPROX 2 IN LENGTH. REPAIRED PER ERA 332664-14.

Part: SPAR — CRACKED (RT TE FLAP)

CRACKS AT AFT SPAR RAIL AT 18, 32 & 61 FROM I/B END OF FLAP. REPAIRED ON N/R'S 010525, 010526 & 010527. REPAIRS WERE PERFORMED PER M/M 57-52-0 FIG 802 . ON SHOP ORDER 655739.

Part: SKIN — WORN (LT TE MIDFLAP)

DURING SHOP INSPECTION, THE LEADING EDGE WAS FOUND WORN AT THE O/B END OF FLAP. THE DAMAGE WAS REMOVED AND A DOUBLER AND FILLER INSTALLED PER MM 57-52-0, FIG 803.

Part: WEB — CRACKED (BS 1285)

FOUND AT A-1 LETTER CHECK, VERT TORQUE BOX WEB CRACKED .625 AT UPPER LIGHTENING HOLE STA 1285 RT. REPAIRED PER M/M 53-11-0.

Part: CHORD — CRACKED (VERT STAB)

FOUND ON F-2 LETTER CK, LT ATTACH CHORD CRACKED .75 INCH AT VERTICAL STAB S-7L. REPAIRED PER MM 55-30-0.

Part: WEB — CRACKED (BS 1303)

FOUND ON F2 LETTER CK, .75 INCH CRACK LOWER RT CORNER OF WEB STA 1303 ABOVE NR 2 ENGINE S-DUCT. REPAIRED PER SRM 53-10-4.

Part: ACTUATOR — LEAKING (NR 3 LE FLAP)

AFTER T/O AT 5,000 FT, A-SYS HYD QTY WENT TO ZERO. REPLACED NR 3 L/E FLAP ACTUATOR.

Part: LIGHT — INOPERATIVE (1L DOOR)

OVERHEAD EMERGENCY LIGHT AT 1L DOOR INOP. REPLACED EMERGENCY LIGHT ASSY AT 1L DOOR, CKS OK. FOUND ON L/O CK.

Part: SKIN — DAMAGED (L-1 DOORWAY)

THE L-1 DOOR HINGE CUT-OUTS WERE FOUND TO HAVE EXISTING DOUBLER REPAIRS INSTALLED. THE DOUBLERS WERE INSPECTED AND IDENTIFIED AS PERMANENT PER BACO S/B 727-53-0198.

Part: FLOORBEAM — CORRODED (BS 344)

FLOO BEAM CAP CORRODED STA 344 AT RBL 6. REPAIRED PER SRM 53-10-8 FIG 11.

Part: BULKHEAD SUPPORT — WORN (BS 720)

FOUND DURING MV2 F1 - STA 720D VERTICAL BULKHEAD SUPPORTS WORN AT UPPER ATTACH POINTS LT ABOVE STRINGER 26 LT AND RT ABOVE STR 26 RT. INSTALLED REPAIR PER SRM 53-10-9 FIG. 9.

Part: MOUNT BRACKET — CRACKED (NR 5 LE FLAP ACT)

FOUND DURING MV2F1, TOP I/B CORNER CRACKED ON NR 5 L/E FLAP ACTUATOR MOUNT BRACKET. FABRICATED REPAIR PER M/M 57-20-21 AND LEAK CHECKED.

Part: CLOSING MECH — BROKEN (PAX DOOR)

ON ARRIVAL AT GATE, THE FWD LT ENTRY DOOR WOULD NOT OPEN. FOUND SEVERAL BROKEN PARTS JAMMING UPPER HINGE AND LOWER CAM PLATE, UPPER HINGE WAS LOOSE IN AT FUSELAGE. REPLACED BROKEN SNAP RING AND TIGHTENED CAM PLATE, OPERATION NORMAL.

Part: BATTERIES — DISCHARGED (CABIN)

AFT AISLE EMERGENCY FLOOD LIGHT INOP. REPLACED BATTERIES IN AFT AISLE EMERGENCY FLOOD LIGHT, CHECKS NORMAL.

Part: NOSE RIB — CRACKED (NR 4 LE SLAT)

FOUND DURING D-2 LETTER CHECK, NR 4 L/E SLAT ACT ATTACH RIB CRACKED 1.75 INCH I/B SIDE. REPAIRED PER MM 57-54-0.

Part: RIBS — CRACKED (NR 3 SLAT)

DURING SHOP INSPECTION, LEFT WING NR 3 SLAT WAS FOUND WITH NR 3, NR 7, NR 9 AND NR 10 RIBS CRACKED. REPAIRED PER SRM 57-50-3 AND SRM 57-54-0 FIG 804.