N723CK

Part: FIRE LOOP — DEFECTIVE (NR 1 ENGINE) · airframe 60,827 hrs · 39,716 cycles

NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED, FOLLOWED EMERGENCY PROCEDURES SHUTTING DOWN NR 1 ENGINE AND DISCHARGING FIRE BOTTLES NR 1 AND NR 2. FIRE WARNING LIGHT REMAINED ILLUMINATED APPROX 5 MIN AFTER SECOND BOTTLE DISCHARGE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,603 hrs · 19,751 cycles

LT STA 540 MAIN DECK EMERGENCY LIGHT INOP.

Part: DUCT — CRACKED (AC PACK) · airframe 59,814 hrs · 39,154 cycles

AIRCRAFT DEPRESSURIZED ON 1 PACK (RIGHT) ONLY.

Part: CONTROL VALVE — CLOSED (BLEED AIR SYS) · airframe 59,814 hrs · 39,153 cycles

PRESSURIZATION WOULD NOT HOLD CABIN ALTITUDE ON ONE PACK AT 10,000 MSL.

Part: SKIN — CORRODED (RUDDER) · corrosion level 3 · airframe 59,369 hrs · 38,883 cycles

LOWER RUDDER, RT SKIN NEAR L/E CORRODED 19 INCHES UP FROM BOTTOM EDGE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 59,369 hrs · 38,883 cycles

CORROSION ON LEFT ANGLE BELOW FRAME AT STA 1090 BETWEEN STR 27R AND 28R AFT SIDE OF FRAME 2 X 2 INCHES.

Part: DOUBLER — CRACKED (LT WING) · airframe 59,369 hrs · 38,883 cycles

RIB LOWER REPAIR ANGLE CRACKED LEFT WING INTERNAL WS 656.5 STRINGER 6.

Part: RIB — CRACKED (RT WING) · airframe 59,369 hrs · 38,883 cycles

RT WING INTERNAL WS 629.0 RIB CRACKED AT S-6.

Part: RIB — CRACKED (LT WING) · airframe 59,369 hrs · 38,883 cycles

LT WING WS 629.0 UPPER S-14 RIB ATTACH TANG CRACKED INTERNAL WING.

Part: RIB — CRACKED (RT WING) · airframe 59,369 hrs · 38,883 cycles

LOWER RIB REPAIR ANGLE CRACKED AT RIGHT WING INTERNAL WS 686.5 STR 11, 1 INCH CRACK.

Part: WEB — CRACKED (FUSELAGE) · airframe 59,369 hrs · 38,883 cycles

CRACK IN WEB, LT TORQUE BOX IN STAIRWELL BS 1213 LBL 22 (1 INCH).

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,369 hrs · 38,883 cycles

SKIN DAMAGE AT STA 1313 STRINGER 19R-20R 10 X 10 INCHES.

Part: LAP JOINT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 59,369 hrs · 38,883 cycles

LITE CORROSION AT LAP SEAM, CORROSION 1 X 5 INCHES.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 3 · airframe 59,369 hrs · 38,883 cycles

LOWER NOSE W/W T-CHORD BELOW STRINGER HAS AREAS OF CORROSION, 2X2 INCH CORROSION.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 59,369 hrs · 38,883 cycles

INSIDE NOSE WHEEL WELL AND ON EXTERNAL SKIN HAS SIGNS OF CORROSION AT STA 285 STR 26L AND 27L.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 3 · airframe 59,369 hrs · 38,883 cycles

SEAT TRACK CROWN CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 3 · airframe 59,369 hrs · 38,883 cycles

SEAT TRACK CROWN CORRODED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 3 · airframe 59,369 hrs · 38,883 cycles

SEAT TRACK CROWN CORRODED.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 59,369 hrs · 38,883 cycles

INSIDE NOSE W/W AND ON EXTERNAL SKIN HAS SIGNS OF CORROSION 1 X 1 INCHES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 3 · airframe 59,369 hrs · 38,883 cycles

SEAT TRACK CROWN CORRODED.

Part: SKIN — BULGED (FUSELAGE) · corrosion level 3 · airframe 59,369 hrs · 38,883 cycles

FUSELAGE SKIN BULGING, CORROSION 1X1 INCH.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

SHEAR TIE CRACKED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 3 · airframe 58,494 hrs · 38,327 cycles

STRINGER CORROSION.

Part: SKIN — DENTED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

DENT IN FUSELAGE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 3 · airframe 58,494 hrs · 38,327 cycles

STRINGER HAS CORROSION.

Part: SKIN — CORRODED (BS 1362) · corrosion level 2 · airframe 59,029 hrs · 38,708 cycles

SKIN CORROSION, 4 INCHES ABOVE NR 2 ENG RT SIDE.

Part: FRAME — CORRODED (BS 227) · corrosion level 2 · airframe 59,029 hrs · 38,708 cycles

FRAME, CORROSION OUT OF LIMITS STA 227R 16 INCHES OFF CABIN FLOOR.

Part: SKIN — DAMAGED (L1 DOOR) · airframe 58,494 hrs · 38,327 cycles

L1 DOOR HAS INTERIOR SKIN DAMAGE.

Part: FRAME — CORRODED (BS 211) · corrosion level 2 · airframe 59,029 hrs · 38,708 cycles

FRAME, CORROSION TO BE OUT OF LIMITS STA 211 APPROX 19 INCH FROM CABIN FLOOR.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 3 · airframe 58,494 hrs · 38,327 cycles

STRINGER CORROSION.

Part: SUPPORT FRAME — CORRODED (COCKPIT WINDOW) · corrosion level 3 · airframe 58,494 hrs · 38,327 cycles

COCKPIT SLIDING WINDOW SUPPORT FRAME HAS AREA OF CORROSION.

Part: FITTING — CORRODED (DOOR) · corrosion level 3 · airframe 58,494 hrs · 38,327 cycles

DOOR BACK UP FITTING CORRODED.

Part: SKIN — GOUGED (FUSELAGE) · airframe 59,029 hrs · 38,708 cycles

EXTERNAL FUSELAGE SKIN, SKIN GOUGED OUT OF LIMITS.

Part: FASTENER — LOOSE (C3 DOOR) · airframe 58,494 hrs · 38,327 cycles

C-3 DOOR HAS LOOSE FASTENERS.

Part: FRAME — DAMAGED (L1 DOOR) · corrosion level 3 · airframe 58,494 hrs · 38,327 cycles

HOLES IN FRAME ELONGATED, L 1 DOOR.

Part: BEAM — CORRODED (LT MLG) · corrosion level 3 · airframe 58,494 hrs · 38,327 cycles

LT MLG BEAM LOWER SURFACE CORROSION HAS CORROSION IN AND AROUND FASTENER HOLES.

Part: SLAT — MALFUNCTIONED (WING) · airframe 58,538 hrs · 38,369 cycles

AFTER DEPARTURE AND DURING FLAP RETRACTION ^3 LED FAILED TO RETRACT AT FLAPS 2 POSITION. ATTEMPTED TO TURN OFF ENGINE HEAT AND PERFORMED ABNORMAL PROCEDURES WITH NO RESULTS. INSPECTED SLATS PER AMM 27-81-00. SLATS AND LIGHTS OP'S CHECKS OK. OK FOR SERVICE.

Part: FLOORBEAM — CORRODED (BS 400) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

MAIN DECK FLOORBEAM UPPER CHORD HAS CORROSION.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON SKIN, AFT PIT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON FLOORBEAM UPPER CHORD AFT SURFACE.

Part: SKIN — CORRODED (BS 870) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON FUSELAGE SKIN.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

FLOORBEAM HAS CRACK.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

STRINGER CLIP CORRODED AT AFT SIDE OF FRAME.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON OVERWING FRAME.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON INTERCOSTAL, AFT PIT.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

FRAME HAS CORROSION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

FRAME CRACKED.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 58,494 hrs · 38,327 cycles

GOUGE AND CORROSION ON SKIN.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

HORIZONTAL WEB STIFFENER CORRODED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

CRACK ON ANGLE BOTTOM SIDE OF DOOR INNER SKIN, NR 2 CARGO DOOR 12 INCHES AFT OF THE FWD EDGE.

Part: GUSSET — CORRODED (CARGO DOOR) · airframe 58,494 hrs · 38,327 cycles

CORROSION ON GUSSET ANGLE BOTTOM EDGE OF DOOR, C-1 DOOR 28 INCHES AFT OF LEADING EDGE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

FRAME HAS CORROSION.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

DOOR CUTOUT WEB AND ANGLE CORRODED.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

FWD SIDE OF DOOR CUTOUT HAS AREAS OF CORROSION.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 58,494 hrs · 38,327 cycles

INNER SKIN PANEL CRACKED AT CUTOUT, NR 2 CARGO DOOR 18 INCHES OF THE FWD EDGE 25 INCHES DOWN FROM THE TOP.

Part: SKIN — CORRODED (CENTER TANK) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CENTER TANK LOWER SKIN HAS SEVERAL AREAS OF CORROSION.

Part: SKIN — CORRODED (CENTER TANK) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CENTER TANK LOWER SKIN HAS SEVERAL AREAS OF CORROSION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

FRAME CRACKED.

Part: SKIN — CORRODED (CENTER TANK) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CENTER TANK LOWER SKIN HAS SEVERAL AREAS OF CORROSION.

Part: SKIN — DENTED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

SMALL DENT IN SKIN.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

SKIN INNER DOUBLER CORRODED.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

KEEL BEAM LONGERON CORRODED ON BOTTOM WEB ATTACHING LEG.

Part: BEAM — CORRODED (NLG WW) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

I-BEAM ON TOP OF NOSE W/W CORRODED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON INTERCOSTAL, AFT PIT.

Part: SKIN — CORRODED (BS 720C-720D) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

SKIN HAS AREA OF CORROSION.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

SKIN HAS AREA OF CORROSION.

Part: SKIN — CORRODED (BS 720A-720C) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

SKIN HAS AREA OF CORROSION.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

LOWER WEB UPPER SURFACE HAS CORROSION ALONG FWD EDGE OF LIGHTENING HOLE.

Part: STRINGER — CORRODED (BS 400-420) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

STRINGER HAS CORROSION.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON STRINGER, AFT PIT.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

INTERNAL SKIN DOUBLER FOUND TO BE OUT OF LIMITS AFTER CORROSION REMOVAL, FWD E&E.

Part: SKIN — CORRODED (NLG WW) · airframe 58,494 hrs · 38,327 cycles

CRACK UNDER DOUBLER ON SKIN, NOSE W/W.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON STRINGER, AFT PIT.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

VERTICAL STIFFENER HAS CORROSION.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

KEEL BEAM INTERIOR HAS CORROSION ALONG WEB STIFFENER.

Part: FLOORBEAM — CORRODED (BS 620) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

FLOORBEAM HAS CORROSION AROUND UPPER CLIP NUT.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

VERTICAL STIFFENER HAS CORROSION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

FRAME CRACKED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

STRINGER HAS CORROSION.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

STRINGER HAS CORROSION.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

FRAME HAS CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

SEAT TRACK HAS SEVERAL AREAS OF CORROSION.

Part: STRINGER — CORRODED (BS 1030) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON STRINGER.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON LOWER SURFACE OF BULKHEAD STIFFENER.

Part: SPAR — CORRODED (WING) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

REAR SPAR LOWER CHORD VERTICAL FLANGE HAS CORROSION.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON SHEAR TIE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

FLOORBEAM HAS AREAS OF CORROSION.

Part: FRAME — DENTED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

FRAME HAS A DENT.

Part: RAIL — CRACKED (EXTERNAL POWER) · airframe 58,494 hrs · 38,327 cycles

EXTERNAL POWER RECEPTICAL ACCESS CUTOUT LOWER RAIL CRACKED.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

SKIN HAS AREA OF CORROSION.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

HORIZONTAL WEB STIFFENER CORRODED.

Part: STIFFENER — CORRODED (KEELBEAM) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON KEEL BEAM VERTICAL STIFFENER.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

FRAME CORRODED.

Part: FRAME — DENTED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

FRAME HAS A DENT.

Part: FRAME — CRACKED (BS 680) · airframe 58,494 hrs · 38,327 cycles

FRAME WEB HAS EVIDENCE OF A CRACK.

Part: SKIN — DENTED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

DENT ON SKIN.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION SHEAR TIE, AFT PIT.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

SKIN CORROSION BELOW LAP SEAM.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

KEEL BEAM INTERIOR WEB LOWER STIFFENER CORRODED.

Part: SKIN — DENTED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

EXTERIOR FUSELAGE SKIN DENT.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

SKIN DAMAGE.

Part: STRUCTURE — CRACKED (DOOR) · airframe 58,494 hrs · 38,327 cycles

CRACK ON FWD EDGE OF DOOR AT CABLE BRACKET, 24 INCHES UP FROM BOTTOM.

Part: STIFFENER — CORRODED (BS 740) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

FRAME VERTICAL STIFFENER HAS AREA OF CORROSION.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

FRAME CRACKED AT AFT HINGE AATACJ POINT, C-3 DOOR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

FRAME CRACKED AT FWD HINGE ATTACH POINT.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON BULKHEAD VERTICAL STIFFENER.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

STRINGER CLIP CORRODED ON AFT SIDE OF FRAME.

Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

INNER SKIN PANEL CORROSION, NR 3 CARGO DOOR SKIN REPLACEMENT.

Part: STRINGER CLIP — CORRODED (BS 1050) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON STRINGER CLIP.

Part: SKIN — CORRODED (BS 725A) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

SKIN HAS AREA OF CORROSION.

Part: STRINGER — CORRODED (BS 720D-720E) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

STRINGER HAS AREA OF CORROSION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

SKIN DAMAGED.

Part: SKIN — DENTED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

SMALL DENT IN SKIN.

Part: SKIN — DENTED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

SMALL DENT IN SKIN.

Part: STRINGER — CORRODED (BS 740) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

STRINGER END FITTING HAS AREA OF CORROSION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON FLOORBEAM UPPER CHORD LOWER SURFACE, AFT PIT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

CORROSION ON FLOORBEAM UPPER CHORD LOWER SURFACE, AFT PIT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON FLOORBEAM UPPER CHORD LOWER SURFACE, AFT PIT.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

SEAT TRACK HAS SEVERAL AREAS OF CORROSION.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

STRINGER HAS AREA OF CORROSION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 58,494 hrs · 38,327 cycles

SKIN DAMAGE.

Part: SKIN — BULGED (FUSELAGE) · corrosion level 3 · airframe 58,494 hrs · 38,327 cycles

SKIN BULGING AROUND FASTENERS.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

STRINGER CORRODED AT NUT PLATE HOLES.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON INTERCOSTAL.

Part: SPLICE — CORRODED (SEAT TRACK) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON SEAT TRACK SPLICE, AFT PIT.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON STRINGER, AFT PIT.

Part: SPLICE — CORRODED (SEAT TRACK) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON SEAT TRACK SPLICE, AFT PIT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON FLOOR SUPPORT, AFT PIT.

Part: SPLICE — CORRODED (SEAT TRACK) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON SEAT TRACK SPLICE, AFT PIT.

Part: STRINGER — CORRODED (BS 740) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

STRINGER HAS AREA OF CORROSION.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON STRINGER, AFT PIT.

Part: STRINGER — CORRODED (BS 720F-740) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

STRINGER HAS AREA OF CORROSION.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON STRINGER, AFT PIT.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON STRINGER, AFT PIT.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON STRINGER, AFT PIT.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON STRINGER, AFT PIT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON FLOORBEAM LOWER CHORD, AFT PIT.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 58,494 hrs · 38,327 cycles

SEVERAL SMALL AREAS OF CORROSION AROUND FASTENERS ON SKIN.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

STRINGER HAS AREA OF CORROSION.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

FRAME HAS AREA OF CORROSION.

Part: STRINGER CLIP — CORRODED (BS 1030) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON STRINGER CLIP.

Part: RIB — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

UPPER CLOSURE RIB HAS CORROSION ON BOTTOM OF HORIZONTAL FLANGE, VERTICAL STAB STA 297.

Part: WARNING LIGHT — ILLUMINATED (NR 1 FIRE)

FIRE WARNING LIGHT ILLUMINATED IN FLIGHT NR 1 ENG. FIRE PULLED, ENGINE FIRE SWITCH. RETURNED TO DAY.

Part: ANGLE — CORRODED (BULKHEAD) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON BULKHEAD LOWER CHORD ANGLE.

Part: STRINGER — CORRODED (BS 875 S5L) · corrosion level 2 · airframe 58,494 hrs · 38,327 cycles

CORROSION ON STRINGER 5L.

Part: VALVE — FAILED (FUEL HEAT)

NR 2 ENGINE OIL TEMPERATURE IN HIGH RANGE FOR 15 MINUTES WITH NR 2 FUEL HEAT VALVE ALREADY DEFERRED. ABNORMAL PROCEDURE GUIDELINES IN AOM REQUIRED PRECAUTIONARY ENGINE SHUT DOWN. AIRCRAFT RETURNED TO TUS.

Part: TEE FITTING — CORRODED (FUSELAGE)

CORROSION ON T-ANGLE.

Part: FRAME — CORRODED (FUSELAGE)

A 2 X 2 INCH AREA OF CORROSION ON FRAME.

Part: STRINGER — CORRODED (FUSELAGE)

A 1 X 14 INCH AREA OF CORROSION ON STRINGER.

Part: STRINGER — CORRODED (FUSELAGE)

CORROSION ON STRINGER ANGLE.

Part: STIFFENER — CORRODED (FUSELAGE)

6 X 3 AREA OF CORROSION ON STIFFENER

Part: FLOORBEAM — CORRODED (FUSELAGE)

A 1 X 8 INCH AREA OF CORROSION ON FLOORBEAM.

Part: SHEAR TIE — CORRODED (FUSELAGE)

A 4 X 1 INCH AREA OF CORROSION ON SHEAR TIE.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

CORROSION ON INTERCOSTAL REPLACEMENT.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 6 X 1 INCH AREA OF CORROSION.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 3 X 2 INCH AREA OF CORROSION.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 1 X 1 INCH AREA OF CORROSION.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 10 X 1 INCH AREA OF CORROSION.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 1 X 1 INCH AREA OF CORROSION.

Part: FRAME — CORRODED (BULKHEAD)

A 1 X 2 INCH AREA OF CORROSION ON BULKHEAD FRAME.

Part: SHEAR TIE — CRACKED (FUSELAGE)

A 1 INCH CRACK ON SHEAR TIE.

Part: SHEAR TIE — CRACKED (FUSELAGE)

A 2.5 INCH CRACK ON SHEAR TIE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 1 X 2 INCH AREA OF CORROSION.

Part: FRAME — CORRODED (FUSELAEG) · airframe 57,862 hrs · 37,872 cycles

A 1 X 1 INCH AREA OF CORROSION ON FRAME.

Part: STRINGER — CORRODED (FUSELAGE)

A 8 X 3 INCH AREA OF CORROSION ON STRINGER.

Part: STRINGER — CRACKED (FUSELAGE)

.5 INCH CRACK BETWEEN FASTENER HOLES IN STRINGER.

Part: FITTING — CRACKED (STRINGER) · airframe 57,862 hrs · 37,872 cycles

.5 INCH CRACK ON STRINGER END FITTING.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,862 hrs

SEVERAL AREAS OF CORROSION ON STRINGER.

Part: STRINGER — CORRODED (FUSELAGE)

A 1 X 6 INCH AREA OF CORROSION ON STRINGER.

Part: STRINGER — CORRODED (FUSELAGE)

A 8 X 2 INCH AREA OF CORROSION ON STRINGER.

Part: SHEAR TIE — CORRODED (FUSLEAGE) · airframe 57,862 hrs

A .75 X .75 INCH AREA OF CORROSION ON BOTTOM OF SHEAR TIE.

Part: FITTING — CRACKED (STRINGER) · airframe 57,862 hrs · 37,872 cycles

A 1 INCH CRACK ON STRINGER FITTING.

Part: STRINGER — CORRODED (FUSELAGE)

A 20 X 3 INCH AREA OF CORROSION ON STRINGER.

Part: STRINGER — CORRODED (FUSELAGE)

A .75 X .5 INCH AREA OF CORROSION ON STRINGER.

Part: STRINGER — CORRODED (FUSELAGE)

1 INCH BY 4 INCH AREA OF CORROSION ON BOTTOM OF STRINGER.

Part: STRINGER — CORRODED (FUSELAGE)

8 INCH BY 3 INCH AREA OF CORROSION ON STRINGER.

Part: FITTING — CORRODED (FUSELAEG) · airframe 57,862 hrs · 37,872 cycles

A 1 X 1.5 INCH AREA OF CORROSION ON FITTING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

3 INCH BY .75 INCH AREA OF CORROSION ON FLOORBEAM UPPER CHORD.

Part: STRINGER — CORRODED (FUSELAGE)

A 2 X 2 INCH AREA OF CORROSION ON STRINGER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 1 X 2 INCH AREA OF CORROSION ON STRINGER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 10.5 X 25 INCH AREA OF CORROSION ON SKIN INTERIOR.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 6 X 3 INCH AREA OF CORROSION ON STRINGER.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

DAMAGED FASTENER HOLES IN UPPER CHORD.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A .5 INCH CRACK COMING FROM HOLE TO OUTER EDGE OF STRINGER FLANGE.

Part: FITTING — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 1 X 1 INCH AREA OF CORROSION ON STRINGER END FITTING.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 4 X 1 INCH AREA OF CORROSION ON FRAME WEB.

Part: STRINGER — CORRODED (FUSELAGE)

A 1 X 2 INCH AREA OF CORROSION ON STRINGER.

Part: FRAME — CRACKED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 INCH CRACK ON FRAME VERTICAL WEB BY FASTENER LOCATION.

Part: SHEAR TIE — DAMAGED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A .25 X .25 INCH AREA OF DAMAGE ON VERTICAL FLANGE OF SHEAR TIE.

Part: FRAME — CRACKED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A .75 INCH CRACK ON LOWER FRAME ATTACH FLANGE OF WEB.

Part: SHEAR TIE — DAMAGED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A .25 X .25 INCH AREA OF DAMAGE ON LOWER LEG OF SHEAR TIE.

Part: STRINGER — GOUGED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

APPROX .25 X .5 INCH GOUGE IN STRINGER.

Part: SHEAR TIE — DAMAGED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A .25 X .25 INCH AREA OF DAMAGE ON VERTICAL PORTION OF SHEAR TIE.

Part: STRINGER CLIP — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 1.5 INCH AREA OF CORROSION ON STRINGER CLIP.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 1 INCH AREA OF CORROSION ON BOTTOM OF SHEAR TIE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

APPROX 5 INCH CRACK IN STRINGER.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 1 INCH AREA OF CORROSION ON LOWER LEG OF SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 3 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 6 X 1 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 20 X 3 INCH AREA OF CORROSION ON ENTIRE STRINGER FROM STA 460 TO STA 480.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 20 X 3 INCH AREA OF CORROSION ON ENTIRE STRINGER FROM STA 500 TO STA 520.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 20 X 3 INCH AREA OF CORROSION ON ENTIRE STRINGER FROM STA 460 TO STA 480.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 4 X 1 INCH AREA OF CORROSION ON STRINGER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

AREAS OF CORROSION: 5 X 2 INCH FROM STA 480 TO STA 485, 2 X 1 INCH FROM STA 560 TO STA 562, 10 X 2 INCH FROM STA 600 TO STA 610, 5 X 1 INCH FROM STA 655 TO STA 660.

Part: LAP JOINT — CORRODED (FUSELAGE)

3 X 200 INCH AREA OF CORROSION ON LAP SEAM

Part: FRAME — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 16 INCH AREA OF CORROSION ON CHORD.

Part: FRAME — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 5 INCH AREA OF CORROSION ON CHORD.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A .75 X 6 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 4 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A .5 X 1 INCH AREA OF CORROSION ON BOTTOM OF SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 2 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 3 X 1 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SKIN — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

THREE AREAS OF CORROSION ON BOTTOM OF SPLICE APPROX 4 X 2 INCH, 6 X 2 INCH AND 6 X 2 INCH.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 1 X 1 INCH AREA OF CORROSION ON BOTTOM OF STRINGER.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 3 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A .5 X .75 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 4 X 1 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X .5 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 3 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A .75 X 4 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 3 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (FUSELAGE)

A 1 X 1 AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A .75 X 2.5 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 3 X 1 INCH AREA OF CORROSION ON BOTTOM OF SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 3 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A .5 INCH X .5 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SKIN — CORRODED

10 X 5 INCH AREA OF CORROSION ON SKIN SPLICE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (FUSELAGE)

A 1 X 3 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 6 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 2 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 2 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 4 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 2 INCH AREA OF CORROSION ON SHEAR TIE.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 57,862 hrs

A .5 X .75 INCH AREA OF CORROSION ON STRINGER CLIP.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 1 X 2 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 2 INCH AREA OF CORROSION ON SHEAR TIE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 1 X 8 INCH AREA OF CORROSION ON STRINGER BOTTOM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 5 INCH AREA OF CORROSION ON BOTTOM OF STRINGER.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1.5 X 18 INCH AREA OF CORROSION ON STRINGER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 1 X 35 INCH AREA OF CORROSION ON FLOORBEAM FLANGE.

Part: STRINGER CLIP — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1.5 INCH BY 2 INCH AREA OF CORROSION ON STRINGER CLIP.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

SEVERAL AREAS OF CORROSION ON FRAME.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

1.500 INCH BY 3 INCH AREA OF CORROSION ON STRINGER.

Part: THRESHOLD — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

SEVERAL AREAS OF CORROSION ON BOTTOM SIDE OF SERVICE DOOR THRESHOLD WEB WITHIN A 7 INCH BY 50 INCH AREA.

Part: STRINGER CLIP — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 3 INCH AREA OF CORROSION ON STRINGER CLIP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 1 X 1 INCH AREA OF CORROSION ON FLOORBEAM UPPER CHORD.

Part: CREASE BEAM — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

SEVERAL AREAS OF CORROSION ON BOTTOM SIDE OF WEB WITHIN A 7 INCH BY 40 INCH AREA.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CORROSION ON SEAT TRACK.

Part: SHEAR WEB — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

SEVERAL AREAS OF CORROSION ON BOTTOM OF SHEAR WEB.

Part: SHEAR WEB — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

SEVERAL AREAS OF CORROSION ON BOTTOM OF SHEAR WEB.

Part: SHEAR WEB — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

SEVERAL AREAS OF CORROSION ON BOTTOM OF SHEAR WEB.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

3 INCH BY 16 INCH AREA OF CORROSION ON SKIN AT LAP SEAM.

Part: FRAME — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1.5 X 24 INCH AREA OF CORROSION ON FRAME FLANGE AND WEB.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 4 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

APPROX 1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE.

Part: STRINGER CLIP — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

APPROX 2 INCH BY 2 INCH AREA OF CORROSION ON CLIP.

Part: STRINGER CLIP — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

APPROX 1 INCH BY 2 INCH AREA OF CORROSION ON STRINGER SLIP.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

.75 INCH BY 1.5 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CRACKED (FUSELAGE)

.5 INCH CRACK IN SHEAR TIE RADIUS.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

.75 INCH CRACK IN SHEAR TIE LOWER RADIUS.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1.25 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE.

Part: ANGLE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

2.5 INCH BY 4 INCH AREA OF CORROSION ON CLOSE OUT ANGLE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,862 hrs

A .75 X 2 INCH AREA OF CORROSION ON BOTTOM OF SHEAR TIE.

Part: ANGLE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

APPROX 3 INCH BY 7 INCH AREA OF CORROSION ON CLOSE OUT ANGLE.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

APPROX 1 INCH CRACK IN SHEAR TIE RADIUS.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE.

Part: FRAME — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

APPROX 2 INCH BY 3 INCH AREA OF CORROSION ON FRAME.

Part: SHEAR TIE — DAMAGED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

LOWER FLANGE OF SHEAR TIE HAS DAMAGED FASTENER HOLES.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

SEVERAL SMALL AREAS OF CORROSION ON BOTTOM OF STRINGER.

Part: FRAME — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 3 INCH AREA OF CORROSION ON LOWER FRAME ANGLE.

Part: ANGLE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 29 INCH AREA OF CORROSION ON ANGLE.

Part: ANGLE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 3 INCH AREA OF CORROSION ON REINFORCEMENT ANGLE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

CORROSION ON STRINGER 27R.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

SEVERAL SMALL AREAS OF CORROSION ON BOTTOM OF STRINGER

Part: SHEAR TIE — DAMAGED (FUSLEAGE) · airframe 57,862 hrs · 37,872 cycles

LOWER FLANGE OF SHEAR TIE HAS DAMAGED FASTENER HOLES.

Part: SHEAR TIE — GOUGED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

APPROX (3) .1875 INCH GOUGES IN SHEAR TIE FLANGE.

Part: SHEAR TIE — GOUGED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

.1875 INCH DIAMETER GOUGE ON LOWER FLANGE OF SHEAR TIE.

Part: SHEAR TIE — DAMAGED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

LOWER FLANGE OF SHEAR TIE HAS DAMAGED FASTENER HOLES.

Part: SHEAR TIE — GOUGED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

.9375 GOUGE AT SIDE OF FASTENER HOLE ON LOWER FLANGE OF SHEAR TIE.

Part: STIFFENER — CORRODED (FUSELAEG)

A 2 X 3 INCH AREA OF CORROSION ON STIFFENER.

Part: SKIN — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

SEVERAL AREAS OF CORROSION ON LOWER FUSELAGE SKIN.

Part: STRINGER — CORRODED (FUSELAGE)

A 2 X 1 INCH AREA OF CORROSION ON STRINGER.

Part: FITTING — CORRODED (FUSELAGE)

A 3 X 1 INCH AREA OF CORROSION ON FITTING.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

SEVERAL AREAS OF CORROSION ON STRINGER.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

CORROSION ON STRINGER BETWEEN BS 600-660.

Part: BULKHEAD — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1.5 INCH BY 1.5 INCH AREA OF CORROSION ON WEB.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

SMALL AREAS OF CORROSION ON STRINGER.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCY BY 3 INCH AREA OF CORROSION ON STRINGER.

Part: DOOR FRAME — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

3 INCH BY 5 INCH AREA OF CORROSION ON FUSELAGE DOOR FRAME.

Part: FRAME — CORRODED (FUSELAGE)

1 INCH BY 1 INCH AREA OF CORROSION ON LOWER CHORD.

Part: FRAME — CORRODED (FUSELAGE)

1 INCH BY 9 INCH AREA OF CORROSION ON LOWER CHORD.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

TWO 1 X 1 INCH AREAS OF CORROSION ON FLOORBEAM CHORD.

Part: FITTING — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

CORROSION ON END FITTING APPROX 2.5 INCH BY 6 INCH BY 4 INCH.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 1 INCH AREA OF CORROSION ON STRINGER.

Part: FRAME — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

3 INCH BY 5 INCH AREA OF CORROSION ON FRAME WEB.

Part: SPAR — CORRODED (WING) · airframe 57,862 hrs · 37,872 cycles

A 3 X 3 INCH AREA OF CORROSION ON SPAR CHORD VERT FLANGE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

2 INCH BY 3 INCH AREA OF CORROSION ON FRAME WEB.

Part: FRAME — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

2 INCH BY 8 INCH AREA OF CORROSION ON FRAME.

Part: KEELBEAM — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1.5 INCH BY 2.5 INCH AREA OF CORROSION ON BOTH SIDES OF KEEL BEAM EXTENSION.

Part: KEELBEAM — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

2 INCH BY 2.5 INCH AREA OF CORROSION ON BOTH SIDES OF KEEL BEAM EXTENSION.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 8 INCH AREA OF CORROSION ON STRINGER.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

CORROSION ON SHEAR TIE.

Part: SKIN — CORRODED (ANTENNA DOUBLER) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 1 INCH AREA OF CORROSION ON SKIN DOUBLER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

TWO 3 X 3 INCH AREAS OF CORROSION.

Part: STRINGER — CORRODED (FUSLEAGE) · airframe 57,862 hrs · 37,872 cycles

CORROSION ON STRINGER BETWEEM BS 670 AND 720.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

.5 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CRACKED (FUSELAGE)

CRACK IN SHEAR TIE RADIUS.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 2.5 INCH AREA OF CORROSION ON SHEAR TIE.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

.5 INCH BY 1 INCH AREA OF CORROSION IN CENTER OF S-26R.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

2 INCH CRACK IN SHEAR TIE RADIUS.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 10 INCH AREA OF CORROSION ON BOTTOM OF STRINGER

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH CRACK IN PREVIOUS SHEAR TIE REPAIR ANGLE RADIUS.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 4 INCH AREA OF CORROSION ON SHEAR TIE.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 5 X 2 INCH AREA OF CORROSION ON STRINGER.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1.25 INCH BY 3 INCH AREA OF CORROSION ON BOTTOM OF SHEAR TIE.

Part: FRAME — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 1 INCH AREA OF CORROSION ON FRAME.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

.75 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE.

Part: ATTACH FITTING — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

CORROSION IN BORE OF RT STAB HINGE BEARING LUG.

Part: FRAME — CRACKED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

CRACKED FRAME UPPER FLANGE 1 INCH IN LENGTH.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

APPROX 1 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

CORROSION ON BOTTOM OF S-24 LT.

Part: ATTACH FITTING — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

CORROSION IN BORE OF LT STAB HINGE BEARING LUG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 1 X 2 INCH AREA OF CORROSION ON STRINGER BOTTOM.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

A 1 X 2 INCH AREA OF CORROSION ON STRINGER.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

2 INCH BY 4 INCH AREA OF CORROSION ON BOTTOM OF STRINGER.

Part: SKIN — CORRODED (FUSELAGE)

A 3 X 5 INCH AREA OF CORROSION ON SKIN.

Part: FITTING — CORRODED (FUSELAGE)

A 1 X 1 INCH AREA OF CORROSION OF FITTING.

Part: STIFFENER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

2 INCH BY .5 INCH AREA OF CORROSION ON STIFFENER.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE.

Part: STRINGER — CORRODED (FUSLEAGE) · airframe 57,862 hrs · 37,872 cycles

SEVERAL AREAS OF CORROSION ON BOTTOM OF STRINGER.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH AREA OF CORROSION ON S-26R.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 1.5 X 5 INCH AREA OF CORROSION ON STRINGER BOTTOM.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

SEVERAL AREAS OF CORROSION ON STRINGER.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

2 INCH BY 2 INCH AREA OF CORROSION ON FRAME WEB.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

A 3 X 6 INCH AREA OF CORROSION ON FRAME WEB.

Part: THRESHOLD — CORRODED (FUSELAGE)

CORROSION ON DOOR THRESHOLD ATTACHMENT ANGLES, WEB STIFFENERS, WEB REPLACEMENT.

Part: REINFORCEMENT — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 1 INCH AREA OF CORROSION ON REINFORCEMENT CHORD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

3 INCH BY 12 INCH AREA OF CORROSION ON STRINGER.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 1.5 INCH AREA OF CORROSION ON CHORD.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 16 INCH AREA OF CORROSION ON BOTTOM OF STRINGER

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,862 hrs

A 1 X 2 INCH AREA OF CORROSION ON BOTTOM OF STRINGER END FITTING.

Part: SKIN — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

APPROX 2 INCH BY 2 INCH AREA OF CORROSION AROUND ANTENNA MOUNT ON FUSE SKIN.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

3 INCH BY 16 INCH AREA OF CORROSION ON STRINGER.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 13 INCH AREA OF CORROSION ON BOTTOM OF STRINGER

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

STRINGER FLANGE CORRODED 20 INCH IN LENGTH.

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 15 INCH AREA OF CORROSION ON BOTTOM OF STRINGER

Part: STRINGER — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

2.5 INCH BY 5 INCH AREA OF CORROSION ON STRINGER.

Part: SKIN — CORRODED (DOOR)

CORROSION ON INTERIOR DOOR SKIN.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

.5 INCH BY 1 INCH AREA OF CORROSION ON SHEAR TIE

Part: SKIN — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

SEVERAL AREAS OF CORROSION ON INTERIOR OF SKIN.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 1.5 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1.5 INCH BY 2 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 3 INCH AREA OF CORROSION ON SHEAR TIE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 57,862 hrs · 37,872 cycles

1 INCH BY 4 INCH AREA OF CORROSION ON SHEAR TIE.

Part: FLANGE — CRACKED (FUSELAGE)

A 1 INCH CRACK IN UPPER FLANGE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,862 hrs · 37,872 cycles

SEVERAL AREAS OF CORROSION ON BOTTOM OF STRINGER.

Part: SKIN — CORRODED (BS 1183-1148)

DURING CPCP CHECK INSPECTION, FOUND CORROSION ON INTERIOR SKIN AT LAP SPLICE ABOVE S20LT FROM BS 1183 TO BS 1148. REPAIRED LAP SPLICE INTERIOR SKIN ABOVE S20LT BS1183-BS1148 IAW B727 SRM 53-30-03 FIG 13. CORROSION TASK CARD NUMBER C53-113-01 PART 2 OF 2. NON-ROUTINE TASK CARD NUMBER 110962.

Part: FITTING — CRACKED (BS 950)

DURING CPCP CHECK INSPECTION FOUND, AFT PIT STA 950A ABOVE STRINGER 28R FLOOR FITTING IS CRACKED. REPLACED FLOOR FITTING STR 28R AFT PIT STA 950A IAW B727 SRM 51-10-01. CORROSION TASK CARD NUMBER C53-113-01 PART 02 OF 02. NON-ROUTINE TASK CARD NUMBER 110587.

Part: SHEAR TIE — CORRODED (BS 950)

DURING CPCP CHECK INSPECTION FOUND LEVEL 2 CORROSION, AFT PIT STA 950F SHEAR-TIE CORRODED BETWEEN STR'S 28 AND 29L. REPAIRED SHEAR TIE AFT PIT STA 950F BETWEEN STR 28 AND 29L IAW B727 SRM 53-10-4. CORROSION TASK CARD NUMBER C53-113-01 PART 02 OF 02. NON-ROUTINE TASK CARD NUMBER 110595.

Part: STRINGER — CRACKED (WS 629)

DURING ACCOMPLISHMENT OF AD 88-17-06, FOUND CRACK ON LT WING STRINGER S11 AT RIB ATTACHMENT WS 629. REPAIRED STR 11 LT WING AT RIB ATTACHMENT WS 629 IAW SB 727-57-A159. NON-ROUTINE TASK CARD NUMBER 110067.

Part: INTERCOSTAL — CRACKED (BS 740)

DURING CPCP CHECK INSPECTION, FOUND FLOORBEAM INTERCOSTAL WEB AT STA 740 LBL 20 HAS CRACK ON UPPER SURFACE AT RIVET. REPAIRED INTERCOSTAL WEB AT STA 740 LBL20 IAW B727 SRM 51-40-2 FIG 1. CORROSION TASK CARD NUMBER C57-174-01 PART 1 OF 1. NON-ROUTINE TASK CARD NUMBER 110106.

Part: RIB — CRACKED (WS 546.5)

DURING ACCOMPLISHMENT OF AD 94-07-08, FOUND CRACKED RIB WS 546.5 AT STRINGER 15. INSTALLED DOUBLER REPAIR IAW AIA EA B2-57-001 REV ORIG DTD 07/09/97. NON-ROUTINE TASK CARD NUMBER 106760.

Part: ANGLE — CORRODED (LT TE FLAP)

DURING CPCP CHECK INSPECTION, FOUND LEFT WING I/B FLAP O/B TRACK TO FALSE SPAR HAS BOTH ATTACH BOLTS BROKEN ATTACH ANGLE CORRODED. REMOVED AND REPLACED ATTACH ANGLE DUE TO EXCESSIVE CORROSION IAW B727 SRM 51-10-1 AND 51-30-2 AND 57-20-2. CORROSION TASK CARD NUMBER C57-500-02 PART 1 OF 2. NON-ROUTINE TASK CARD NUMBER 110072.

Part: DOOR LOCK — MISSING (AFT AIRSTAIR)

DURING CPCP CHECK INSPECTION, FOUND AFT AIRSTAIR IN FLIGHT DOOR LOCK (DB COOPER) MISSING. REMOVED AFT AIRSTAIR IN FLIGHT DOOR LOCK IAW S/B 727-52-110 PG 15 AND IAW ENGINEERING ORDER NR 727-52-001 DTD 07/24/97 AND EDR NO B205440. CORROSION TASK CARD NUMBER C53-111-02 PART 02 OF 02. NON-ROUTINE TASK CARD NUMBER 110079.

Part: SHEAR TIE — CRACKED (VERT STAB)

DURING CPCP CHECK INSPECTION, FOUND INTERNAL VERTICAL STAB RIB NR 3 SHEAR TIE HAS SMALL CRACK AT STRINGER NR 8. REMOVED AND REPLACED SHEAR TIE IAW B727 SRM 51-10-1 AND 51-30-2. CORROSION TASK CARD NUMBER C55-395-10 PART 01 OF 01. NON-ROUTINE TASK CARD NUMBER 110634.

Part: CONNECTOR — FAILED (NR 2 ENGINE)

KHUF - FLT 73729 - AT CRUISE, ENGINE FIRE WARNING BELL CAME ON VERY WEAK WITHOUT ANY FIRE WARNING LIGHTS. SILENCED THE BELL AND TESTED FIRE WARNING SYSTEM. TESTED OK, BUT WHEN ATTEMPTED RE-TEST, NR 2 FIRE LIGHT WOULD NOT TEST. AFTER SEVERAL ATTEMPTS, NR 2 FIRE LIGHT TESTED OK. POSSIBLE SHORT. REPAIRED NR 2 ENGINE FIREWALL FIRE WARNING CONNECTOR, SYSTEM OPS CHECK GOOD IAW MM 26-11-03. (X)