TOWARDS AIR, LLC

Part: INTAKE DUCT — CORRODED (NR 2 ENGINE) · airframe 78,574 hrs · 50,641 cycles

NR 2 ENGINE S-DUCT INTERNAL SKIN BULGING AT RIB 22 AT 6 O'CLOCK POSITION.

Part: FLOOR SUPPORT — CORRODED (BS 1177) · airframe 78,574 hrs · 50,641 cycles

MAIN DECK FLOOR SUPPORT AT BS 1177, RBL 3, HAS AREA OF CORROSION.

Part: SKIN — CORRODED (BS 1160-1180) · airframe 78,574 hrs · 50,641 cycles

EVIDENCE OF CORROSION AT SKIN DOUBLER AT STRINGER 26L BETWEEN BS 1160 AND 1180.

Part: SHEAR TIE — CORRODED (BS 1010) · airframe 78,574 hrs · 50,641 cycles

SHEAR TIE CORRODED AT BS 1010 BETWEEN STRINGERS 29-30L.

Part: STRINGER — CORRODED (BS 1000) · airframe 78,574 hrs · 50,641 cycles

STRINGER 29R CORRODED AT BS 1000.

Part: STRINGER — CORRODED (BS 970-990) · airframe 78,574 hrs · 50,641 cycles

STRINGER 29L HAS AREAS OF CORROSION BETWEEN BS 970 AND 990.

Part: SHEAR TIE — CORRODED (BS 985) · airframe 78,574 hrs · 50,641 cycles

SHEAR TIE CORRODED AT BS 985 STUB FRAME BETWEEN STRINGER 28-29R.

Part: STRINGER — CORRODED (BS 950E-950F) · airframe 78,574 hrs · 50,641 cycles

STRINGER 29L HAS AREAS OF CORROSION BETWEEN BS 950E AND 950F.

Part: STRINGER — CORRODED (BS 950D-950E) · airframe 78,574 hrs · 50,641 cycles

STRINGER 29L HAS CORROSION BETWEEN BS 950D AND 950E.

Part: STRINGER — CORRODED (BS 950D-950E) · airframe 78,574 hrs · 50,641 cycles

STRINGER 29R HAS CORROSION BETWEEN BS 950D AND 950E.

Part: STRINGER — CORRODED (BS 950A-950C) · airframe 78,574 hrs · 50,641 cycles

STRINGER 30L HAS AREAS OF CORROSION BETWEEN BS 950A AND 950C.

Part: INTAKE DUCT — CORRODED (NR 2 ENGINE) · airframe 78,574 hrs · 50,641 cycles

NR 2 ENGINE S-DUCT HAS CORROSION ON INTERNAL SKIN BETWEEN RIB 16-17 AT 6 O'CLOCK POSITION.

Part: STRINGER — CORRODED (BS 735) · airframe 78,574 hrs · 50,641 cycles

STRINGER 24L HAS CORROSION AT BS 735.

Part: STRINGER — CRACKED (BS 1000) · airframe 78,574 hrs · 50,641 cycles

STRINGER 29R AT BS 1000 UPPER FLANGE CRACKED.

Part: INTAKE DUCT — DAMAGED (NR 2 ENGINE) · airframe 78,574 hrs · 50,641 cycles

AT PRODUCTION BREAK SPLICE IN S-DUCT AT BS 1243 BOTTOM SIDE BETWEEN RIB 16 AND 17 SPLICE REPAIR DAMAGED.

Part: ATTACH ANGLE — CORRODED (BS 299) · airframe 78,574 hrs · 50,641 cycles

HORIZONTAL WEB INBD ATTACH ANGLE AT BS 299, LBL 16 CORRODED.

Part: ATTACH ANGLE — CORRODED (BS 300) · airframe 78,574 hrs · 50,641 cycles

HORIZONTAL WEB INBD ATTACH ANGLE CORRODED AT BS 300, RBL16.

Part: ATTACH ANGLE — CORRODED (BS 348) · airframe 78,574 hrs · 50,641 cycles

HORIZONTAL WEB INBD ATTACH ANGLE CORRODED AT BS 348, RBL16.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

INTERCOSTAL CORRODED AT STA 1060 STRINGER 20 LEFT.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

EVIDENCE OF CORROSION BETWEEN STA 950E AND 950E, STRINGER 15L.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

SEAT TRACK CORRODED BETWEEN STA 800 TO 815, LEFT BUTTLINE 25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

LEFT BUTTLINE 56, STA 344 SEAT TRACK CORRODED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

TOP CORD OF FLOORBEAM CORRODED ON FLOORBEAM AT STA 1110, LEFT BUTTLINE 24 TO 52.

Part: WEB — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

CORROSION AROUND EDGE OF WALL AND FLOOR WEB AT STA 1148, RIGHT BUTTLINE 63.

Part: WEB — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

CORROSION AROUND PINS IN FLOOR WEB AT STA 1146 BETWEEN RIGHT BUTTLINE 54 AND 58.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

LEFT BUTTLINE 55 SEAT TRACK HAS SEVERAL AREAS OF CORROSION BETWEEN STA 991 TO 1030.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

SEAT TRACK SUPPORT CORRODED AT LEFT BUTTLINE 45.5, STA 1090 TO 1110.

Part: MOUNT — CORRODED (NR 2 ENGINE) · airframe 42,419 hrs · 26,696 cycles

NR 2 ENGINE, UPPER FORWARD MOUNT ASSY CORRODED.

Part: INTERCOSTAL — CORRODED (BS 360-380) · airframe 78,574 hrs · 50,641 cycles

INTERCOSTAL AT STRINGER 20R HAS CORROSION HAS CORROSION AT BS 360 - 380.

Part: PIN — CORRODED (RT WING) · airframe 42,419 hrs · 26,696 cycles

RIGHT WING AFT BOTTLE PIN CUP HAS EVIDENCE OF CORROSION UNDER PIN CUP.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

INTERCOSTAL AT STA 1060, LEFT BUTTLINE 26 AREA OF CORROSION.

Part: SKIN — CORRODED (RUDDER) · airframe 42,419 hrs · 26,696 cycles

CORROSION ON LEFT SIDE OF UPPER RUDDER TRAILING EDGE BETWEEN RS 220 AND 242.

Part: STRUCTURE — CRACKED (NR 1 PYLON) · airframe 42,419 hrs · 26,696 cycles

CRACK ON TOP OF NR 1 PYLON OUTBD FASTENER HOLE"P" OF S/B 727-54A0010R6, FROM HOLE TO OTBD EDGE OF LOWER ANGLE.

Part: STRUCTURE — CORRODED (RUDDER) · airframe 42,419 hrs · 26,696 cycles

CORROSION ON LEFT SIDE OF UPPER RUDDER BETWEEN STA 212 AND 220.

Part: SKIN — DAMAGED (RUDDER) · airframe 42,419 hrs · 26,696 cycles

UPPER RUDDER SKIN CORRODED RIGHT SIDE TRAILING EDGE BETWEEN STA 220-247.

Part: SKIN — DAMAGED (RUDDER) · airframe 42,419 hrs · 26,696 cycles

SKIN DAMAGED ON LOWER RUDDER LEFT SIDE BETWEEN STA 113-118.

Part: SKIN — CORRODED (RUDDER) · airframe 42,419 hrs · 26,696 cycles

CORROSION ON RIGHT SIDE OF UPPER RUDDER TRAILING EDGE AT RS 175.

Part: FRAME — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

FRAME AT STA 1148 CORRODED AT STR 26R.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

SHEAR TIE CORRODED AT STA 1130 BETWEEN STR 27 AND 28 RIGHT.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

SHEAR TIE CORRODED AT STATION 1130 BETWEEN STR 27 AND 28 LEFT.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

SHEAR TIE CORRODED AT STA 1130 BETWEEN STR 29 AND 30 LEFT.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

SHEAR TIE CORRODED AT STA 1110, BETWEEN STR 28 AND 29 LEFT.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

SHEAR TIE CORRODED STA 1166 BETWEEN STR 29 AND 30 LEFT.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

FLOOR TO SKIN WEB CRACKED, .25' AT EDGE OF LIGHTENING HOLE AT STA 490, RIGHT BUTTLINE 72.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

FLOORBEAM CORRODED STA 1110 LEFT BUTTLINE 12 TO LEFT BUTTLINE 24 TOP AND BOTTTOM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

FLOORBEAM CORRODED ON UPPER AND LOWER SURFACE AT STA 1110 LEFT BUTTLINE 1 TO RIGHT BUTTLINE 12.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

SUPPORT WEB CRACKED LEFT BUTTLINE 25 FROM STA 1130 TO 1110.

Part: PANEL — DELAMINATED (RUDDER) · airframe 42,419 hrs · 26,696 cycles

LEFT UPPER RUDDER PANEL BETWEEN STA 212 AND 220 HAS ONE AREA OF DELAMINATION.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

FRAME DAMAGED AT STA 1130 BETWEEN STR 27 AND 28 RIGHT.

Part: DOOR FRAME — DAMAGED (BS 950E) · airframe 42,419 hrs · 26,696 cycles

OTBD STRUCTURE AT DOOR FRAME, BS 950E DAMAGED AT STR 27R.