N316CM

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 103,756 hrs · 29,948 cycles

CORRODED

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 1,037,560 hrs · 29,948 cycles

CORRODED

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 103,756 hrs · 29,948 cycles

CORRODED

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 103,756 hrs · 29,948 cycles

CORRODED

Part: SPLICE PLATE — CORRODED (WING) · corrosion level 2 · airframe 103,756 hrs · 29,948 cycles

CORRODED

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 1,037,560 hrs · 29,948 cycles

CORRODED

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 109,756 hrs · 29,948 cycles

CORROSION

Part: STRINGER — CRACKED (FUSELAGE) · airframe 103,756 hrs · 29,948 cycles

CRACKED

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 1,037,560 hrs · 29,948 cycles

CORRODED

Part: SKIN PANEL — CORRODED (WING) · corrosion level 2 · airframe 103,756 hrs · 29,948 cycles

CORROSION

Part: STRINGER — CRACKED (FUSELAGE) · airframe 103,756 hrs · 29,948 cycles

CRACKED

Part: STRINGER — CRACKED (FUSELAGE) · airframe 103,756 hrs · 29,948 cycles

CRACKED

Part: BEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 103,756 hrs · 29,948 cycles

CORRODED

Part: STRUCTURE — CORRODED (WING) · corrosion level 2 · airframe 103,756 hrs · 29,948 cycles

CORRODED

Part: BEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 103,756 hrs · 29,948 cycles

CORRODED

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,142,934 hrs · 43,909 cycles

CORNER OF PICKLE CORRODED.

Part: SKIN — CORRODED (RT WING) · corrosion level 3 · airframe 103,238 hrs · 29,679 cycles

LEVEL 3 CORROSION FOUND AT RH WING LOWER SKIN - WS 826 TO WS 835

Part: FORMER — CRACKED (RT WING) · airframe 99,657 hrs · 27,866 cycles

NOSE FORMER AT ILES 482.00 BROKEN (CRACKED).

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 99,657 hrs · 27,866 cycles

UPPER CARGO FLOOR BEAM SUPPORT FITTING CRACKED AT STA 1065 LBL 12.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 99,657 hrs · 27,866 cycles

UPPER CARGO FLOOR BEAM SUPPORT FITTING STA 1021 LBL 56 CRACKED.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 99,657 hrs · 27,866 cycles

UPPER CARGO FLOOR BEAM SUPPORT FITTING STA 1043, LBL 12 CRACKED.

Part: FORMER — CRACKED (RT WING) · airframe 99,657 hrs · 27,866 cycles

NOSE FORMER CRACKED AT RT WING STA 436.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,657 hrs · 27,866 cycles

ANGLE IS CORRODED IN THE LWW KEEL AREA, ON FWD SIDE OF STA 1021 AT BOTTOM OF FRAME.

Part: SUPPORT FITTING — CRACKED (BS 1043) · airframe 99,657 hrs · 27,866 cycles

UPPER CARGO FLOORBEAM SUPPORT FITTING BS 1043, LBL 56 FOUND CRACKED

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,657 hrs · 27,866 cycles

BULK CARGO DOOR CUTOUT, AFT EDGE FRAME HAS CORROSION ON WEB AT NUTPLATES.

Part: FITTING — CORRODED (CARGO BAY) · corrosion level 2 · airframe 99,657 hrs · 27,866 cycles

CARGO LOADING SYSTEM ATTACHMENT POINT CORRODED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,657 hrs · 27,866 cycles

O/B SIDE OF STR 39R STA 655-658 CORROSION.

Part: CARGO TRACK — CORRODED (BS 1120-1610) · airframe 99,657 hrs · 27,866 cycles

UPPER CARGO RBL 54 CARGO TRACK CORRODED FROM BS 1120 - 1610.

Part: CARGO TRACK — CORRODED (BS 1120-1610) · corrosion level 2 · airframe 99,657 hrs · 27,866 cycles

UPPER CARGO, RBL 33 CARGO TRACK CORRODED FROM BS 1120 - 1610.

Part: CARGO TRACK — CORRODED (BS 1120-1610) · corrosion level 2 · airframe 99,657 hrs · 27,866 cycles

UPPER CARGO, RBL 11 CARGO TRACK CORRODED FROM BS 1120 - 1610.

Part: CARGO TRACK — CORRODED (BS 1120-1610) · corrosion level 2 · airframe 99,657 hrs · 27,866 cycles

UPPER CARGO, LBL 54 CARGO TRACK CORRODED FROM BS 1120 - 1610.

Part: CARGO TRACK — CORRODED (BS 1120-1520) · corrosion level 2 · airframe 99,657 hrs · 27,866 cycles

UPPER CARGO, LBL 77 CARGO TRACK CORRODED FROM BS 1120 - 1520.

Part: CARGO TRACK — CORRODED (BS 1120-1610) · corrosion level 2 · airframe 99,657 hrs · 27,866 cycles

UPPER CARGO, LBL11 CARGO TRACK CORRODED BS 1120 - 1610.

Part: FLOOR SUPPORT — CORRODED (BS 1480-1610) · corrosion level 2 · airframe 99,657 hrs · 27,866 cycles

UPPER CARGO OTBD FLOOR SUPPORT LBL 77, CORRODED FROM BS 1480 - 1610.

Part: CHANNEL — CORRODED (BS 867) · corrosion level 2 · airframe 99,657 hrs · 27,866 cycles

FLOOR DRAIN CHANNEL CORRODED, LBL 33 - RBL 77, BS 687

Part: FLOORBEAM — CRACKED (BS 1021) · airframe 99,657 hrs · 27,866 cycles

UPPER CARGO FLOORBEAM FITTING CRACKED AT LBL 12, BS 1021.

Part: CARGO TRACK — CORRODED (BS 1120-1610) · corrosion level 2 · airframe 99,657 hrs · 27,866 cycles

UPPER CARGO, LBL 33 CARGO TRACK CORRODED FROM BS 1120 - 1610.

Part: SEAT TRACK — CORRODED (BS 1120-1520) · corrosion level 2 · airframe 99,657 hrs · 27,866 cycles

SEAT TRACK CORRODED FROM BS 1120 - 1520, RBL 77. BLENDED WITHIN LIMITS.

Part: CARGO TRACK — CORRODED (BS 1120-1610) · corrosion level 2 · airframe 99,657 hrs · 27,866 cycles

UPPER CARGO, RBL 11 CARGO TRACK CORRODED FROM BS 1120 - 1610.

Part: CHANNEL — CRACKED (NR 1 NACELLE) · airframe 99,657 hrs · 27,866 cycles

NR 1 ENGINE INBD CORE COWL LATCH RETAINER CHANNEL CRACKED.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 999,657 hrs

LEFT WING LOWER SURFACE CORRODED AT SURGE TANK.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 999,657 hrs · 27,866 cycles

LEFT WING LOWER L/E LOWER SKIN CORRODED AT WS 655 TO 695.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 999,657 hrs · 27,866 cycles

CORROSION ON RIGHT WING LOWER SURFACE WS 1045

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 999,657 hrs · 27,866 cycles

THE NR 2 NACELLE INBD CORE COWL SKIN CRACKED AT LOWER IN THIRD ALIGNMENT PIN.

Part: STRINGER — CRACKED (BS 903) · airframe 999,657 hrs

BS 903.5 STRINGER CRACKED.

Part: CHANNEL — CORRODED (BS 624) · corrosion level 2 · airframe 999,657 hrs

CHANNEL CORRODED BS 624, RBL.38.

Part: FLOORBEAM — CRACKED (BS 785) · airframe 999,657 hrs

BS 785, RBL 90 UPPER CARGO FLOORBEAM CRACKED.

Part: ANGLE — CORRODED (BS 1413-1540) · corrosion level 2 · airframe 999,657 hrs

BULK CARGO SIDE WALL ANGLE CORRODED AT BS 1413 TO 1540.

Part: FLOORBEAM — CORRODED (BS 742) · corrosion level 2 · airframe 999,657 hrs

BS 742 FLOORBEAM UPPER TEE CORRODED.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 999,657 hrs

LEFT WING LOWER SURFACE AT WS 810 TO 815 CORRODED

Part: SUPPORT — CORRODED (BS 1351-1540) · corrosion level 2 · airframe 999,657 hrs

BULK CARGO CEILING SUPPORTS CORRODED BS 1351 TO 1540.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 999,657 hrs · 27,866 cycles

NR 2 NACELLE INBD CORE COWL SKIN CRACKED.

Part: ANGLE — CORRODED (BS 1461-1480) · corrosion level 2 · airframe 999,657 hrs · 27,866 cycles

BULK CARGO, ANGLE CORRODED AT BS 1461 TO 1480.

Part: STRINGER — CRACKED (BS 654) · airframe 999,657 hrs

STRINGER 25L CRACKED AT BS 654+22.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 999,657 hrs · 27,866 cycles

RIGHT WING LOWER SURFACE CORRODED AT WS 1040

Part: FLOOR SUPPORT — CORRODED (BS 504) · corrosion level 2 · airframe 999,657 hrs · 27,866 cycles

FLOOR SUPPORT CORRODED AT BS 504. RBL 39

Part: FLOORBEAM — CORRODED (BS 654) · corrosion level 2 · airframe 999,657 hrs · 27,866 cycles

FLOOR BEAM CORRODED AT BS 654+94 TO 654+44.

Part: WEB — CORRODED (BS 654) · corrosion level 2 · airframe 999,657 hrs

PRESSURE DECK WEB CORRODED AT BS 654, RBL 38

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 999,657 hrs

LEFT WING LOWER SURFACE AT WS 866, CORRODED.

Part: SKIN — CRACKED (NACELLE) · airframe 999,657 hrs · 27,866 cycles

NR1 ENGINE INBD CORE COWL REPAIR DOULBER CRACKED AT CTR LATCH.

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 999,657 hrs

BULK CARGO DOOR FRAME WEB CORRODED.

Part: STRUCTURE — CRACKED (BS 883-903) · airframe 999,657 hrs

STRUCTURE CRACKED AT BS 883.5 TO 903.5 RIGHT.

Part: SUPPORT BEAM — CRACKED (BS 785) · airframe 999,657 hrs

BS 785, LBL 90 UPPER CARGO SUPPORT BEAM CRACKED.

Part: FRAME — CRACKED (BS 883) · airframe 999,657 hrs · 27,866 cycles

FRAME BS 883.5, LBL 88 CRACKED.

Part: SKIN — CORRODED (RT WING LE) · corrosion level 2 · airframe 999,657 hrs · 27,866 cycles

CORROSION ON RIGHT WING LE RWS 710

Part: ACTUATOR — SHEARED (RT MLG) · airframe 96,362 hrs · 26,081 cycles

FRM CODE 32 30 19 02. RT GEAR DOWN LIGHT FAILED TO GO OFF WITH GEAR HANDLE UP. EICAS MSG GEAR DISAGREE DISPLAYED. DOORS AMBER LIGHT & GEAR AMBER LIGHTS ON. RT MAIN GEAR VISUALLY VERIFIED TO BE EXTENDED BY TOWER FLY BY.

Part: STRUCTURE — CRACKED (BS 620) · airframe 96,043 hrs · 25,915 cycles

LOWER FUSELAGE FWD CARGO COMPARTMENT OUTER CHORD WITH CRACK STRINGERS 30 - 31R, BS 620.

Part: SUPPORT BEAM — CORRODED (LT WING) · corrosion level 2 · airframe 92,350 hrs · 24,103 cycles

LEFT WING T/E UPPER PANEL SUPPORT BEAM CORRODED WS 235. REPAIRED IAW SRM.

Part: SUPPORT — CORRODED (ZONE 600) · corrosion level 2 · airframe 92,350 hrs · 24,103 cycles

RIGHT OTBD FLAP NR 7 SUPPORT OTBD FLANGE HOLE HAS DEFECT INDICATION WITH EDY CURRENT. REPAIRED IAW REA.

Part: STRINGER — CRACKED (BS 654) · airframe 92,350 hrs · 24,103 cycles

BS 654+22, STR 17L CRACKED. REPAIRED STRINGER IAW SRM.

Part: STRINGER — CRACKED (BS 654) · airframe 92,350 hrs · 24,103 cycles

BS 654+22, STR 11L CRACKED. R & R STRINGER SECTION IAW SRM.

Part: SUPPORT — CORRODED (ZONE 500) · corrosion level 2 · airframe 92,350 hrs · 24,103 cycles

LEFT OTBD FLAP NR 1 SUPPORT OTBD FLANGE HOLE HAS DEFECT INDICATION WITH EDDY CURRENT. REPAIRED IAW REA.

Part: SUPPORT — DAMAGED (TE FLAP) · airframe 92,360 hrs · 24,103 cycles

RIGHT OTBD FLAP NR 7 SUPPORT OUTBOUND FLANGE HOLD AT 2 O'CLOCK HAS DEFECT INDICATION WITH ROTARY SCAN. POSSIBLE CORROSION OR PITTING. REPAIRED FLANGE AT 2 O'CLOCK POSITION TO .480. FREEZE PLUG INSTALLED & DRILLED TO NOMINAL LIMITS IAW REA 47100REA01.

Part: SUPPORT — DAMAGED (TE FLAP) · corrosion level 2 · airframe 92,360 hrs · 24,103 cycles

LEFT OTBD FLAP NR 1 SUPPORT OTBD FLANGE HOLE AT 12 O'CLOCK HAS DEFECT INDICATION WITH ROTARY SCAN. POSSIBLE CORROSION OR PITTING. REPAIRED FLANGE AT 12'O CLOCK POSITION TO FINAL OF .480. FREEZE PLUG INSTALLED & DRILLED TO NOMINAL LIMITS IAW REA 47100REA01.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 92,360 hrs · 24,103 cycles

STATION 654+22 STRINGER 17L CRACKED 5 INCHES. REPAIRED STRINGER 17L AT STATION 654+22 IAW SRM 53-00-03.

Part: THRUST REVERSER — CRACKED (ZONE 400) · airframe 90,847 hrs · 23,593 cycles

NR 2 ENGINE OTBD THRUST REVERSER HAS A .5" CRACK AT THE OPENING ACTUATOR BOTTOM END BRACKET. R & R THE NR 2 ENGINE OTBD THRUST REVERSER IAW AMM 78-31-01. ADJUSTED LATCH RING IAW AMM 78-31-02. OPS CHECK GOOD IAW AMM 78-31-00.

Part: SUPPORT — BROKEN (RT MLG ACTUATOR) · airframe 90,847 hrs · 23,593 cycles

RT MLG MAIN DOOR ACTUATOR AFT SUPPORT LINK LOWER END BROKEN AT ATTACH POINT. REPLACED RT MLG DOOR ACTUATOR AFT SUPPORT LINK IAW AMM 32-32-12 3F(1-3,6).

Part: ANGLE — CRACKED (NR 8 SLAT) · airframe 90,847 hrs · 23,596 cycles

LOWER ANGLE CRACKED THRU LOCK FASTENER HOLE ON UPPER RIB STRUT AFT OF NR 8 SLAT AT L/E STA 512 ADJACENT TO FRONT SPAR. STOP DRILLED CRACK IAW SRM 57-41-09. REPAIR 4 ITEM 2 AND PERFORMED HFEC INSPECTION IAW NDT MANUAL 51-00-19, PART 6. NO DEFECTS NOTED. INSTALLED REPAIR DOUBLER ON RT WING L/E STATION 512 IAW SRM 57-41-09, REPAIR 4, DETAIL II.

Part: FITTING — CRACKED (NR 2 NACELLE) · airframe 90,847 hrs · 23,593 cycles

NR 2 PYLON FAN COWL SUPPORT BEAM FITTING ASSY CRACKED AT OTBD ATTACHING LUG. R & R SUPPORT BEAM FITTING ASSY FOR FAN COWL IAW DWG 311T2210 AND SRM 51-40-02.

Part: SKIN — DENTED (NR 7 SLAT) · airframe 90,847 hrs · 23,593 cycles

NR 7 SLAT L/E SKIN DENTED (6.0" X 2.0" X 0.75") AND CRACKED (0.5" IN LENGTH) ON INBD END. INBD RIB DAMAGE 0.5" CRACK. PERFORMED TRIMOUT AT THE CRACKED AREA IAW SRM 57-43-01, FIG 201. COMPLIED WITH HFEC INSP OF TRIMOUT AREA IAW NDT MANUAL 51-00-19. REPAIRED NR 7 SLAT SKIN DAMAGE IAW SRM 51-10-02 AND 51-10-01.

Part: ANGLE — CRACKED (NR 9 SLAT) · airframe 90,847 hrs · 23,593 cycles

LOWER ANGLE CRACKED THRU LOCK FASTENER HOLE ON UPPER RIB STRUT AFT OF NR 9 SLAT AT L/E STA 531 ADJACENT TO FRONT SPAR. STOP DRILLED CRACK IAW SRM 57-41-09. REPAIR 4 ITEM 2 AND PERFORMED HFEC INSPECTION IAW NDT MANUAL 51-00-19, PART 6. NO DEFECTS NOTED. INSTALLED REPAIR DOUBLER ON RT WING L/E STATION 531 IAW SRM 57-41-09, REPAIR 4, DETAIL II.

Part: SKIN — CORRODED (LT WING) · airframe 90,847 hrs · 23,593 cycles

CORROSION WAS FOUND AT FIVE LOCATIONS ON THE LOWER LT WING SKIN AT LOCATIONS 872, 889, 896, 951 AND 957 AT FASTENER LOCATIONS. FASTENERS WERE REMOVED AND CORROSION BLENDED IAW SRM 51-10-02. FASTENERS WERE REPLACED IAW SRM 51-40-02.

Part: STRUCTURE — CRACKED (LT WING TE FLAP) · airframe 86,973 hrs · 22,730 cycles

DURING PRE DEPARTURE CHECK FOUND LT INBD T/E FLAP CRACKED. FABRICATED AND INSTALLED REPAIR IAW SRM 57-33-01, FIG 201. ACFT RETURNED TO SERVICE.