N373CM

Part: ACTUATOR — BINDING (ZONE 600) · airframe 100,809 hrs · 35,187 cycles

ON FLAP RETRACTION, AFTER LANDING, LEADING EDGE SLAT ASSY WARNING. AFTER INSPECTION FOUND DAMAGE TO SLATS 11, ROTARY ACTUATOR AND OFFSET GEARBOX

Part: SKIN — CRACKED (RT WING SLAT) · airframe 91,837 hrs · 32,333 cycles

NR 9 SLAT SKIN LOWER TRAILING EDGE HAD A MISSING FILLER.

Part: SKIN — CORRODED (RT WING TE) · corrosion level 2 · airframe 91,837 hrs · 32,333 cycles

RT WING OUTBOARD TRAILING EDGE CORRODED.

Part: SUPPORT BEAM — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 91,837 hrs · 32,333 cycles

LEFT WING NR 2 FLAP SUPPORT 1-2-3 BEAM HAD CORROSION IN 5 CODE C FASTENER HOLES.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 91,837 hrs · 32,333 cycles

LEFT WING LOWER SPAR WAS CORRODED AROUND A HOLE.

Part: STRUCTURE — CORRODED (RT WING) · corrosion level 2 · airframe 88,060 hrs · 30,450 cycles

RT WING LEADING EDGE UPPER CHORD CORRODED.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 91,837 hrs · 32,333 cycles

LEFT WING LOWER SPAR CHORD CORRODED.

Part: SPLICE PLATE — CRACKED (LT WING) · airframe 91,837 hrs · 32,333 cycles

LEFT WING LOWER SPLICE PLATE CHORD WAS DAMAGED BY SLAT CONTROL ROD.

Part: BEAM — CRACKED (NR 2 NACELLE) · airframe 91,837 hrs · 32,333 cycles

UPPER FWD PYLON TRANSVERSE BEAM CRACKED ON OUTBOARD SIDE OF THE NR 2 PYLON.

Part: WEB — CORRODED (LT WING) · corrosion level 2 · airframe 9,183,658 hrs · 32,333 cycles

LEFT WING T/E LOWER SPAR WEB CORRODED

Part: BEAM — CORRODED (HYD BAY) · airframe 9,183,658 hrs · 32,333 cycles

HYD BAY LOWER FRAME BEAM CRACKED

Part: STRUCTURE — CORRODED (RT WING) · corrosion level 2 · airframe 9,183,658 hrs · 32,333 cycles

RIGHT WING UPPER CHORD CORRODED WS 446.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 9,183,658 hrs · 32,333 cycles

LEFT WING T/E LOWER SKIN CORRODED.

Part: WEB — CORRODED (LT WING) · corrosion level 2 · airframe 9,183,658 hrs · 32,333 cycles

LEFT WING AFT LOWER SPAR WEB CORRODED

Part: STRUCTURE — CORRODED (RT WING LE) · corrosion level 2 · airframe 9,183,658 hrs · 32,333 cycles

RIGHT WING LEADING EDGE CHORD CORRODED

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 9,183,658 hrs · 32,333 cycles

LEFT WING LOWER SKIN PANEL IS CORRODED

Part: STIFFENER — CRACKED (NR 1 NACELLE) · airframe 9,183,658 hrs · 32,333 cycles

NR 1 PYLON LOWER SKIRT FAIRING STIFFENER CRACKED

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 9,183,658 hrs · 32,333 cycles

RIGHT WING LOWER SPAR CHORD UPPER SURFACE CORRODED

Part: RIB — CRACKED (RT WING LE) · airframe 9,183,658 hrs · 32,333 cycles

RIGHT LEADING EDGE RIB CRACKED

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 9,183,658 hrs · 32,333 cycles

RIGHT WING LEADING EDGE RIB AT THE NR 11 SLAT CORRODED.

Part: BEAR STRAP — CORRODED (BS 871-883) · corrosion level 2 · airframe 9,183,658 hrs · 32,333 cycles

CORROSION FOUND ON BEAR STRAP FLIGHT STATION 871.5 TO 883.5

Part: BEAM — CRACKED (L2 DOOR) · airframe 9,183,658 hrs · 32,333 cycles

L2 DOOR LOWER BEAM CRACKED

Part: BEAM — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 9,183,658 hrs · 32,333 cycles

#2 FLAP 1-2-3 BEAM CODE C HOLES CORRODED

Part: SKIN — CRACKED (NR 9 SLAT) · airframe 9,183,658 hrs · 32,333 cycles

#9 SLAT T/E SKIN CRACKED

Part: RIB — CRACKED (RT WING) · airframe 9,183,658 hrs · 32,333 cycles

RT WING AIR LOAD RIB CRACKED

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 9,183,658 hrs · 32,333 cycles

LEFT HORIZ STAB UPPER O/B SKIN CORRODED AT HSBL 314.214

Part: DOUBLER — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 9,183,658 hrs · 32,333 cycles

#1 PYLON CORRODED STA 204

Part: SKIN — CRACKED (BS 1654) · airframe 9,183,658 hrs · 32,333 cycles

LT AFT FUSELAGE SKIN CRACKED AT STATION 1654.5

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 9,183,658 hrs · 32,333 cycles

RT WING LOWER SKIN CORRODED

Part: SPLICE PLATE — CORRODED (LT WING) · corrosion level 2 · airframe 9,183,658 hrs · 32,333 cycles

LEFT WING FLIGHT STATION 871.5 TO 883.5 LOWER SPAR SPLICE PLATE CORRODED

Part: SPLICE PLATE — CORRODED (LT WING) · corrosion level 2 · airframe 9,183,658 hrs · 32,333 cycles

LT WING AT LES 370 SPLICE PLATE FASTENER HOLE CORRODED.

Part: SKIN — CRACKED (BS 1720) · airframe 9,183,658 hrs · 32,333 cycles

LEFT AFT FUSELAGE SKIN CRACKED AT STATION 1720

Part: NOT REPORTED — LEAKING (HYDRAULIC SYS) · airframe 88,505 hrs · 30,673 cycles

MAIN RIGHT HYDRAULIC SYSTEM PRESS AND QUANTITY ZERO AND CENTER HYDRAULIC QUANTITY 1.34.

Part: FLOORBEAM — CRACKED (BS 346) · airframe 88,060 hrs · 30,450 cycles

FORWARD ACCESSORY, BS 346, RBL 58, FLOORBEAM WEB IS CRACKED ON FORWARD SIDE. REPAIRED THE FLOORBEAM IAW REA 47316REA11.

Part: STRINGER — DAMAGED (BS 434) · airframe 88,060 hrs · 30,450 cycles

OUT OF ROUND AND ELONGATED HOLES IN THE END OF STRINGER 2L, FORWARD OF BS 434. REPLACED DAMAGED THE STRINGER SECTION, FROM BS 390 TO 434 IAW REA 47316REA09, REV A.

Part: STRINGER — DAMAGED (BS 434) · airframe 88,060 hrs · 30,450 cycles

OUT OF ROUND AND ELONGATED HOLES IN THE END OF STRINGER 3L FORWARD OF BS 434. REPLACED THE STRINGER SECTION 3L BETWEEN BS 390 TO 434 IAW REA 47316REA09, REV A.

Part: STRINGER — DAMAGED (BS 434) · airframe 88,060 hrs · 30,450 cycles

OUT OF ROUND AND ELONGATED HOLES ON THE END OF STRINGER 1L, FORWARD OF BS 434. REPLACED THE STRINGER SECTION, BS 390 TO 434 IAW REA 47316REA09, REV A.

Part: STRINGER — CRACKED (BS 434) · airframe 88,060 hrs · 30,450 cycles

BS 434, STRINGER 4L IS CRACKED ON FORWARD SIDE OF CIRCUMFERENTIAL SKIN SPLICE. REMOVED AND REPLACED THE DAMAGED SECTION OF STRINGER 4L, FROM BS 400 TO 434 IAW REA 47316REA09.

Part: SKIN — CORRODED (LT WING LOWER) · corrosion level 2 · airframe 88,060 hrs · 30,450 cycles

LEFT WING LOWER SKIN CORRODED AT WS 924, L6. REPAIRED LEFT WING LOWER SKIN AT WS 924, L6 IAW REA 47316REA05.

Part: STRINGER — DAMAGED (BS 434) · airframe 88,060 hrs · 30,450 cycles

OUT OF ROUND AND ELONGATED HOLES IN THE END OF STRINGER 6L FORWARD OF BS 434. REPLACED THE STRINGER SECTION IAW REA 47316REA09, REV A.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 88,060 hrs · 30,450 cycles

LEFT WING LOWER SKIN CORRODED AT LES 495. REMOVED CORROSION AND REPAIRED IAW REA 47316REA04

Part: STRINGER — DAMAGED (BS 434) · airframe 88,060 hrs · 30,450 cycles

OUT OF ROUND AND ELONGATED HOLES IN THE END OF STRINGER 5L, FORWARD OF BS 434. REPLACED THE STRINGER SECTION, FROM BS 412 TO 434 IAW REA 47316REA09, REV A.

Part: STRINGER — DAMAGED (BS 434) · airframe 88,060 hrs · 30,450 cycles

OUT OF ROUND AND ELONGATED HOLES IN THE END OF STRINGER 7L FORWARD OF BS 434. REPLACED THE STRINGER SECTION FROM BS 390 TO 434 IAW REA 47316REA09, REV A.

Part: STRINGER — DAMAGED (BS 434) · airframe 88,060 hrs · 30,450 cycles

OUT OF ROUND AND ELONGATED HOLES IN THE END STRINGER 1R FORWARD OF BS 434. REMOVED THE DAMAGE SECTION OF THE STRINGER, BS 390 TO 434 IAW REA 47316REA09.

Part: SKIN — CRACKED (BS 1725) · airframe 88,060 hrs · 30,450 cycles

RIGHT FUSELAGE EXTERNAL SKIN IS CRACKED AT BS 1725.5, STRINGER 7R.

Part: SKIN — CORRODED (RT WING LOWER) · corrosion level 2 · airframe 88,060 hrs · 30,450 cycles

RIGHT WING LOWER SKIN AT REAR SPAR RWS 1053 HAS CORROSION. BLENDED AND FOUND OUT OF LIMITS. REPAIRED THE SKIN IAW REA 47316REA07.

Part: SKIN — CORRODED (RT WING) · airframe 88,060 hrs · 30,450 cycles

RIGHT WING LOWER SKIN AT REAR SPAR RWS 810 TO 850 WAS CORRODED. BLENDED THE CORROSION AND FOUND OUT OF LIMITS. REPAIRED SKIN IAW 47316REA10.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 88,060 hrs · 30,450 cycles

RIGHT WING LOWER SKIN AT L6 SPAR RWS 800 WAS CORRODED. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED SKIN IAW REA 47316REA12.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 88,060 hrs · 30,450 cycles

LEFT WING LES 458, CORRODED ON THE AFT END OF UPPER AIR LOAD RIB OTBD SIDE

Part: SKIN — CORRODED (RT WING LOWER) · corrosion level 2 · airframe 88,060 hrs · 30,450 cycles

RIGHT WING LOWER SKIN AT RWS 968, AT L6 SPAR WAS CORRODED. BLENDED AND FOUND OUT OF LIMITS IAW SRM 57-20-01, PG 104, DETAIL1, TABLE 2. REPAIRED IAW REA 47316REA08.

Part: SKIN — CORRODED (RT WING LOWER) · corrosion level 2 · airframe 88,060 hrs · 30,450 cycles

RIGHT WING LOWER SKIN AT REAR SPAR RWS 930 IS CORRODED. REPAIRED THE SKIN IAW REA 47316REA06.

Part: SKIN — CORRODED (RT WING LOWER) · corrosion level 2 · airframe 88,060 hrs

RIGHT WING LOWER SKIN AT L10 SPAR RWS 785 WAS CORRODED OUT OF LIMITS. REPAIRED THE SKIN IAW REA 47316REA14.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 88,060 hrs · 30,450 cycles

LEFT HORIZONTAL STAB TRAILING EDGE UPPER OUTBOARD SURFACE HAS EVIDENCE OF CORROSION AT A REPAIR DOUBLER. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 55-10-01. REMOVED AND REPLACED THE REPAIR DOUBLER IAW REA 47316REA03.

Part: SPLICE PLATE — CORRODED (LT WING) · corrosion level 2 · airframe 88,060 hrs · 30,450 cycles

LEFT WING LEADING EDGE WS 675, LOWER SPLICE PLATE CORRODED. REMOVED DAMAGED IAW REA 47316REA01.

Part: BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 88,060 hrs · 30,450 cycles

RT WING LEADING EDGE FORWARD WEB AT LES 884 CORRODED AT LOWER ANGLE AND FACE OF WEB. REMOVED AND REPLACED NOSE BEAM ASSEMBLY IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 903) · airframe 88,060 hrs · 30,450 cycles

LEFT LOWER STUB FRAME INNER STRUCTURE WAS FOUND CRACKED AT BS 903.5, LBL 89. TRIMMED OUT THE DAMAGE AND REPAIRED IAW SB 76753A0209, REV2, FIG 17.