N722CK

Part: ACTUATOR VALVE — INOPERATIVE (ZONE 100) · airframe 59,141 hrs · 37,779 cycles

AFTER TAKEOFF, ACFT WOULD NOT PRESSURIZE IN AUTO OR MANUAL.

Part: SUPPORT ANGLE — CRACKED (BS 950) · airframe 59,106 hrs · 37,756 cycles

CRACKED LOWER SUPPORT ANGLE BS 950 AFT SIDE RT LOWER

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,105 hrs · 37,755 cycles

LOWER CHORD HAS EVIDENCE OF CORROSION AT STA 950, STR 29R.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,105 hrs · 37,755 cycles

LEFT WW STA 950, LBL 67, AFT OTBD CORNER OF WHEEL WELL PRESSURE DECK SUPPORT CORRODED.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,105 hrs · 37,755 cycles

LT WW PRESSURE DECK SUPPORT ANGLE STA 950, LBL 67.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,105 hrs · 37,755 cycles

FRAME SHEAR TIE CORROSION AT STA 720D, STR 27-26L.

Part: BULKHEAD WEB — CORRODED · corrosion level 2 · airframe 59,106 hrs · 37,756 cycles

CORROSION AT FWD BULKHEAD UNDER RAY DOME

Part: STIFFENER — CORRODED (BS 918) · corrosion level 2 · airframe 59,106 hrs · 37,756 cycles

VERTICAL STIFFNER CORRODED BS 918 LT MLG WW APU INLET FWD SUPPORT LOWER END.

Part: TORQUE TUBE — DETACHED (TE FLAPS) · airframe 58,839 hrs · 37,606 cycles

OTBD T/E FLAPS WENT ASYMMETRIC, FOUND LT T/E OTBD DRIVESHAFT TORQUE TUBE COUPLING CAME OFF. RESECURED TORQUE TUBE, SAFETY WIRED, PERFORMED ADJUSTMENT AND TEST. NO DEFECTS NOTED AT THIS TIME.

Part: SHEAR TIE — CORRODED (BS 320) · corrosion level 2 · airframe 58,692 hrs · 37,527 cycles

SHEAR TIE CORRODED.

Part: BEAM — CORRODED (BS 296) · corrosion level 2 · airframe 58,692 hrs · 37,527 cycles

BEAM CHORD CORROSION, RT SIDE OF WALKWAY.

Part: SKIN — WORN (ZONE 400) · airframe 58,016 hrs · 37,180 cycles

NR 3 NOSE COWL AT 6 O'CLOCK POSITION, EXTERIOR SKIN WORN.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 58,016 hrs · 37,180 cycles

STRINGER 26L CORRODED AT BS 720F+15".

Part: MOUNT — CORRODED (NR 2 ENGINE AFT) · corrosion level 2 · airframe 58,016 hrs · 37,180 cycles

NR 2 AFT ENGINE MOUNT SHOWS EVIDENCE OF CORROSION.

Part: GASKET — BLOWN (BLEED AIR SYS) · airframe 5,745 hrs · 36,854 cycles

AFTER TAKEOFF FROM MCI AT APPROX 1500 FT, NR 1 ENGINE FIRE WARNING LIGHT. COMPLETED ENGINE FIRE CHECKLIST AND NOTIFIED TOWER, DECLARED EMERGENCY. REQUESTED TO RETURN RETURN TO MCI FOR LANDING, PROCEEDED TO DUMP FUEL AREA, DUMPED FUEL TO LANDING WEIGHT, FIRE DETECTION LIGHT DID EXTINGUISH DURING CHECKLIST PROCEDURES. NO FIRE BOTTLE WAS DISCHARGED. AIRPORT EMERGENCY CREW ADVISED NO INDICATION OF FIRE, TAXIED TO RAMP AND SHUTDOWN. INSPECTED AND FOUND 8TH STAGE AND 13TH STAGE BLEED AIR MANIFOLD GASKETS BLOWN AND A CRACK IN THE 13TH STAGE SUPPLY DUCT. REPLACED GASKETS AND SUPPLY DUCT. PERFORMED ENGINE RUN AND AIR LEAK CHECK'S WITH NO OTHER DEFECTS NOTED IAW PRATT MM AND BOEING AMM.

Part: SKIN — CHAFED (FUSELAGE) · airframe 57,441 hrs · 36,848 cycles

SKIN CHAFED 1 X 1 INCH.

Part: STRINGER FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,441 hrs · 36,848 cycles

STRINGER END FITTING HAS CORROSION 1 X 1 INCH.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,152 hrs · 36,663 cycles

STRINGER CORROSION, LOWER SIDE OF EXTERNAL POWER RECEPTICAL 1X3 INCHES.

Part: STIFFENER — CORRODED (LT WING) · corrosion level 2 · airframe 56,426 hrs · 32,775 cycles

L/W FRONT SPAR STIFFENER CORROSION, 1X4 INCHES.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,426 hrs · 32,775 cycles

AFT PIT STRINGER CORROSION, 1X6 INCHES.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,426 hrs · 32,775 cycles

AFT PIT STRINGER CORROSION, 1X8 INCHES.

Part: SUPPORT FITTING — CRACKED (SPOILER) · airframe 57,152 hrs · 36,663 cycles

SPOILER ACTUATOR I/B SUPPORT FITTING CRACKED, 1X3 INCHES.

Part: STIFFENER — CORRODED (LT WING) · corrosion level 2 · airframe 57,152 hrs · 36,663 cycles

WING FRONT SPAR STIFFENER CORROSION, 1X3 INCHES.

Part: STIFFENER — CORRODED (LT WING) · corrosion level 2 · airframe 57,152 hrs · 36,663 cycles

WING FRONT SPAR STIFFENER CORROSION, 1X4 INCHES AND .5X1 INCHES.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,152 hrs · 36,663 cycles

STRINGER END FITTING CORROSION, 1X1 INCHES.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,152 hrs · 36,663 cycles

STRINGER END FITTING CORROSION, 1X1 INCHES.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,122 hrs · 36,645 cycles

DURING AD INSPECTION FOUND FRAME 1148 CRACKED IN 2 AREAS BETWEEN STRINGERS 30L AND 28L.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

STRINGER CORROSION.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,799 hrs · 36,457 cycles

FRAME CRACKED ABOVE R1 DOOR.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

VERT STIFFENER CORRODED 5 INCHES.

Part: SILL — CRACKED (FUSELAGE) · airframe 56,799 hrs · 36,457 cycles

L2 DOOR LOWER SILL HAS 1 INCH CRACK.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

AFT ENTRY DOOR FRAME CORRODED UPPER DOOR FRAME (20 INCHES).

Part: FRAME — DENTED (FUSELAGE) · airframe 56,799 hrs · 36,457 cycles

FRAME DAMAGE (2 INCH DENT).

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

INTERCOSTAL DAMAGED 24 INCHES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

SEAT TRACK CORROSION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

SEAT TRACK CORROSION.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

SHEAR WEB CORROSION, CORROSION 10 INCHES.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

FRAME WEB CORROSION AT RT HORIZONTAL WALKWAY.

Part: STRINGER — CORRODED (BS 1177 S17L) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

STRINGER HAS CORROSION, 12 INCHES.

Part: WEB — CORRODED (BS 1172) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

WEB HAS HOLE CORRODED THRU ENTIRE WEB, 6 INCHES.

Part: TANK — CORRODED (FUEL SYSTEM) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

UPPER SURFACE CENTER TANK CORROSION (CORROSION 1 X 2 INCHES).

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

FLOORBEAM UPPER CHORD CORROSION 10 INCHES.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,799 hrs · 36,457 cycles

STRINGER CRACKED.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

AFT ENTRY DOOR CUROUT AFT SIDE CORRODED DOUBLER STRAP (40 INCHES).

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

AFT ENTRY DOOR CUTOUT FRAME CORROSION RIGHT SIDE (20 INCHES OF CORROSION).

Part: SPAR — CRACKED (CENTER WING) · airframe 56,799 hrs · 36,457 cycles

WING CTR SECTION REAR SPAR WEB, UPPER HAS CRACK IND IN WEB RADIUS, 1 INCH.

Part: STRUCTURE — CORRODED (BS 1177) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

REINFORCEMENT CHORD HAS CORROSION, 20 INCHES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

SEAT TRACK CORROSION 20 INCHES.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

FLOORBOARD SUPPORT CORROSION 10 INCHES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

SEAT TRACK CORROSION 77 INCHES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

FLOORBEAM UPPER CHORD CORROSION 5 INCHES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

SEAT TRACK CORROSION 90 INCHES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

SEAT TRACK CORROSION 90 INCHES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

FLOORBEAM CORROSION 50 INCHES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

FLOORBEAM CORROSION 57 INCHES.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

MAIN CABIN CORROSION, 5 INCHES.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

STRINGER CORROSION 20 INCHES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

SEAT TRACK CORROSION 80 INCHES.

Part: SEAT TRACK — CORRODED (BS 930) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

SEAT TRACK CORROSION 20 INCHES.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

STRINGER CORROSION 5 INCHES.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

STRINGER 4 CORROSION 10 INCHES.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

MAIN CABIN CORROSION.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

C1 DOOR FWD FRAME CORROSION 2 INCHES.

Part: STRUCTURE — CRACKED (L1 DOOR) · airframe 56,499 hrs · 36,457 cycles

L1 DOOR TOP HINGE POINT .5 INCH CRACK.

Part: STRAP — CORRODED (NLG WW) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

CORROSION ON SIDE WALL STRAP, NOSE WHEEL WELL LEFT SIDE 21 INCHES FROM TOP. 5 INCHES OF STRAP.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

FLOOR SUPPORT CORRODED.

Part: FLOOR SUPPORT — CORRODED (BS 1125) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

FLOOR SUPPORT CORRODED 18 INCHES.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,799 hrs · 36,457 cycles

S-DUCT EXTERIOR WEB CRACKED (CRACK 2 INCH).

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,779 hrs · 36,457 cycles

SKIN CORROSION (CORROSION 11 INCHES).

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

CORROSION ON O/B LOWER FLANGE OF OVERWING LONGERON (2 INCHES).

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,799 hrs · 36,457 cycles

SEAT TRACK CORROSION - 20 INCHES (DISCARD SDR NUMBER K11A2010007107220).

Part: HOUSING — CORRODED (TRUNNION) · airframe 56,226 hrs · 36,201 cycles

AFT TRUNNION BRG HSG CORRODED.

Part: SLEEVE — CORRODED (TRUNNION) · airframe 56,226 hrs · 36,201 cycles

RT MAIN LANDING GEAR TRUNNION SLEEVE IN RT MLG SUPPORT BEAM CORRODED.

Part: CASE — DAMAGED (NR 3 ENGINE) · airframe 56,221 hrs · 36,198 cycles

NO EMERGENCY PROCEDURES USED, PER DIRECTOR OF OPERATIONS INSPECT NR 3 ENGINE DUE THROTTLE STAGGER, UPON INSPECTING NR 3 ENGINE FOUND QUARTER SIZE HOLE AT 10 O'CLOCK POSITION IN INTERMEDIATE CASE.

Part: WEB — CORRODED (BS 312-340) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

E AND E BAY WALKWAY WEB CORRODED AT STA 312 TO 340 AND LBL 38. CORROSION 4 BY 6 INCHES.

Part: STIFFENER — CRACKED (NLG) · airframe 55,922 hrs · 36,042 cycles

LT FORWARD EDGE ON NLG TRUNNION SUPPORT VERTICAL STIFFENER IS CRACKED 3 INCHES STA 320, LBL 16, WL 149.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

CORROSION ON BS 1110 FUSELAGE FRAME BETWEEN STR 17R AND STR 18R. CORROSION 2 X 2 INCHES.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 55,922 hrs · 36,042 cycles

AFT AIRSTAIRS LT WING BS 1250 APPROX WL 190 CRACKED AT LIGHTENING HOLE .5 INCH CRACK.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 55,922 hrs · 36,042 cycles

LOWER TEE CHORD FLANGE CORRODED, VIEWED THRU ACCESS HOLE ON NLG WHEEL WELL.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

INTERCOSTAL CORROSION UNDER F/S SEAT TRACK (CORROSION OUT OF LIMITS).

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,922 hrs · 36,042 cycles

CRACKED FUSELAGE STRINGER (NOSE WHEEL WELL) AT STA 270.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,922 hrs · 36,042 cycles

FRAME 1110 LT SIDE AT LBL 30 CRACKED AND DENTED.

Part: PANEL — CORRODED (NLG WW) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

NOSE WHEEL WELL PANEL 1104 HAS CORROSION ON ATTACH UNDER NUT PLATES.

Part: WEB — CORRODED (NLG WW) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

NLG WHEEL WELL WEB INNER SURFACE HAS CORROSION AT STA 292, LBL 148-153. CORROSION 1 X 1 INCH.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

STA 312 FRAME UPPER CHORD ASSY UPPER AND LOWER SURFACE CORRODED WHERE NLG STEERING CABLE PULLEY BRACKET ATTACHES AT LBL 32. CORROSION 2 X 2 INCHES.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

FRAME WEB HAS CORROSION ON AFT SIDE ABOVE STRINGER 24L AT STA 303.9 LBL 37. CORROSION 2 X 2 INCHES.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

LOWER TEE CHORD OTBD FLANGE UPPER SURFACE CORRODED BETWEEN FRAME WEBS AT STA 302-312, LBL 16, WL 149. CORROSION 1 BY 2 INCHES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

FLOORBEAM HAS CORROSION ON UPPER CHORD, UPPER SURFACE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

MAIN DECK, CORROSION ON BS 1110 FLOORBEAM UPPER CHORD AT RBL 62. CORROSION 2 X 1 INCHES.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,215 hrs · 35,695 cycles

AFT LAV SERVICE PANEL SKIN DOUBLER CORRODED ON INSIDE LOWER CORNER.

Part: MOUNT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

APU INLET SCREEN DRAIN ASSY HORIZONTAL MOUNT BRACKET (CHORD) CORRODED ON INSIDE OF KEEL BEAM.

Part: FLOOR SUPPORT — CORRODED (COCKPIT) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

SURFACE CORROSION FOUND ON COCKPIT FLOOR PANEL SUPPORT RAIL TO BE OUT OF LIMITS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

COCKPIT FLOOR PANEL SUPPORT RAIL HAS SURFACE CORROSION TO BE OUT OF LIMITS.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

FRAME SHEAR TIE 2 INCHES BY 2 INCHES CORROSION STA 950D, BETWEEN STR 26L AND 27L FRAME SHEAR TIE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,922 hrs · 36,042 cycles

CORROSION AROUND FASTENER HOLE ON FLOORBEAM BOTTOM CHORD.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

FRAME TIE CORRODED, 9 INCHES IN LENGTH.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

UPPER WEB FRAME BELOW SUB FLOOR CORROSION (WHERE CABLES PASS THRU).

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

UPPER CHORD OF FRAME CORRODED BELOW SUB FLOOR AT STA 304, ABOVE STR 24L, LBL 38. CORROSION 2 X 1 INCHES.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

STRINGER ANGLE CORROSION OUT OF LIMITS.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 55,922 hrs · 36,042 cycles

FLOORBEAM STA 380, RBL 45 HAS GOUGES ON BOTH SIDES ON LOWER SURFACE OF UPPER CHORD AND ON UPPER WEB.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,922 hrs · 36,042 cycles

FLOORBEAM ON THE LOWER SURFACE OF THE UPPER CHORD AT WEB HAS GRINDING MARKS AND CORROSION BEYOND LIMITS.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,922 hrs · 36,042 cycles

EVIDENCE OF CORROSION ON LOWER WEB OF SUB FLOOR FRAME ON AFT SIDE BETWEEN STRINGERS 26L AND 27L BY NOSE GEAR WELL BULKHEAD AT STA 304, LBL 16, WL 146.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 55,215 hrs · 35,695 cycles

THE E-H WINDOW POST CRACKED 4 INCHES ABOVE LOWER CORNER.

Part: SKIN — DAMAGED (CARGO DOOR) · corrosion level 2 · airframe 55,215 hrs · 35,965 cycles

C-3 BULKPIT DOOR EXTERIOR SURFACE WIDE ARRAY OF DAMAGE, INCLUDING CORROSION, DING/DENTS AND EDGE DAMAGE.

Part: SPAR — CORRODED (ELEVATOR) · corrosion level 2 · airframe 55,215 hrs · 35,695 cycles

ELEVATOR REAR SPAR CORRODED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,215 hrs · 35,695 cycles

PREVIOUSLY BLENDED AREA IN SKIN WITH QUESTIONABLE LIMITS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,215 hrs · 35,695 cycles

APPROX STA 300 STR 18R SKIN DAMAGE AT LAV SERVICE CUTOUT FWD UPPER CORNER.

Part: ANGLE — CORRODED (NLG WW) · corrosion level 2 · airframe 55,215 hrs · 35,695 cycles

CORROSION IN THE NOSE LANDING GEAR WHEEL WELL, LT ANGLE.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 55,215 hrs · 35,965 cycles

RT STAB TOP SKIN HAS SURFACE CORROSION AT THE 3 OTBD ELEVATOR HINGE POINT. ( RT STAB STA 168 )

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,215 hrs · 35,695 cycles

SEAT TRACK HAS AREAS OF CORROSION.

Part: SKIN — DAMAGED (AILERON) · airframe 55,215 hrs · 35,695 cycles

DAMAGED SKIN RT OUTBOARD AILERON.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,215 hrs · 35,695 cycles

SEAT TRACK HAS AREAS OF CORROSION.

Part: STRUCTURE — CRACKED (AIRSTAIRS) · airframe 55,215 hrs · 35,695 cycles

LIGHTENING HOLE CRACK, LT SIDE OF AIRSTAIRS.

Part: SKIN — DENTED (FUSELAGE) · airframe 55,215 hrs · 35,695 cycles

SKIN DENTED.

Part: LAP JOINT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,215 hrs · 35,965 cycles

CORROSION BENEATH LAP SEAM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,215 hrs · 35,695 cycles

SEAT TRACK HAS AREAS OF CORROSION.

Part: TEAR STRAP — DAMAGED (FUSELAGE) · airframe 55,215 hrs · 35,695 cycles

TEAR STRAP DAMAGED.

Part: LAP JOINT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,215 hrs · 35,965 cycles

CORROSION BENEATH LAP SEAM.

Part: LAP JOINT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,215 hrs · 35,965 cycles

CORROSION BENEATH LAP SEAM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,215 hrs · 35,695 cycles

SEAT TRACK HAS AREAS OF CORROSION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,215 hrs · 35,695 cycles

APPROX STA 310 STR 23 R SKIN DAMAGE.

Part: ATTACH ANGLE — CRACKED (WING) · airframe 55,215 hrs · 35,695 cycles

FWD SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACK

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 55,215 hrs · 35,695 cycles

FEW SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACK.

Part: BEAM — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 55,215 hrs · 35,695 cycles

UPPER BEAM HAS SEVERAL AREAS OF CORROSION (RT STAB T/E).

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,215 hrs · 35,965 cycles

FWD BULKHEAD BENEATH RADOME EDGE OF STIFFNER CORRODED.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,215 hrs · 35,695 cycles

BELOW AFT ENTRY DOOR SURFACE CORROSION.

Part: STATIC WICK — SEPARATED (RT ELEVATOR) · corrosion level 2 · airframe 55,215 hrs · 35,965 cycles

RT ELEVATOR T/E OTBD EDGE NEXT TO STATIC WICK BASE SKIN IS SEPARATING.

Part: ANGLE — CRACKED (HORIZ STAB) · airframe 55,215 hrs · 35,695 cycles

ANGLE HAS 2 INCH CRACK FWD OF JACKSCREW, STAB STA 32, RBL 14.

Part: SKIN — CORRODED (ELEVATOR) · corrosion level 2 · airframe 55,215 hrs · 35,965 cycles

CORROSION ON LT ELEVATOR UPPER SURFACE, FWD OF T/E. ( ELEVATOR STA 199 3.5 INCHES)

Part: WEB — CRACKED (STABILIZER) · airframe 55,215 hrs · 35,695 cycles

VERTICAL WEB HAS 4 INCH CRACK FWD OF JACKSCREW, STAB STA 32, RBL 14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,215 hrs · 35,695 cycles

APPROX STA 480 STR 22 R TO 23 R HAS NUMEROUS AREAS OF SKIN DAMAGE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,215 hrs · 35,965 cycles

STA 1090, STR 22 R VICINITY CORROSION ALONG FWD EDGE OF C-3 DOOR CUT OUT.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 55,215 hrs · 35,965 cycles

FWD SPAR ATTACH ANGLE CRACKED ( RT WING ).

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 55,215 hrs · 35,695 cycles

FWD SPAR ATTACH ANGLE CRACKED ( RT WING).

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 55,215 hrs · 35,965 cycles

FWD SPAR ATTACH ANGLE CRACKED ( RT WING ).

Part: RUB STRIP — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 55,215 hrs · 35,695 cycles

RUB PADS HAVE CORROSION AROUND ADJUSTMENT SCREWS, LT HORIZONTAL STABILIZER STAB T/E 2ND AND 3RD FROM O/B ELEVATOR.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 55,215 hrs · 35,965 cycles

FWD SPAR ATTACH ANGLE CRACKED. ( RT WING )

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 55,215 hrs · 35,965 cycles

FWD SPAR ATTACH ANGLE CRACKED. ( RT WING )

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 55,215 hrs · 35,965 cycles

FWD SPAR ATTACH ANGLE CRACKED. ( RT WING )

Part: SKIN — DENTED (RT WING) · airframe 55,215 hrs · 35,695 cycles

SEVERAL DENTS, RIGHT WING L/E BL 70.59 - 130.59.

Part: SKIN — DENTED (RT WING) · airframe 55,215 hrs · 35,695 cycles

SEVERAL DENTS ALONG LEADING EDGE, RT WING ABOVE KRUEGER FLAPS.

Part: SKIN — DENTED (LT WING) · airframe 55,215 hrs · 35,695 cycles

SEVERAL DENTS, LEFT WING L/E BL 70.59 - 130.59.

Part: SKIN — DENTED (LT WING) · airframe 55,215 hrs · 35,695 cycles

SEVERAL DENTS ALONG LEADING EDGE, LT WING ABOVE KRUEGER FLAPS.

Part: STIFFENER — CORRODED (WING) · corrosion level 2 · airframe 55,215 hrs · 35,695 cycles

VERTICAL STIFFNER HAS AREA OF CORROSION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,215 hrs · 35,695 cycles

EXTERIOR SKIN HAS AREA OF DAMAGE, 720D + 10 INCHES STRINGER 19L.

Part: STIFFENER — CORRODED (L1 DOOR) · corrosion level 2 · airframe 55,215 hrs · 35,695 cycles

HORIZONTAL STIFFENER CORRODED L1 DOOR 12 INCH FWD OF DOOR WINDOW.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,215 hrs · 35,695 cycles

ABOVE NR 2 ENGINE 2 INCH AREA OF CORROSION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,215 hrs · 35,695 cycles

APPROX STA 328 STR 23 R SKIN DAMAGED.

Part: SKIN — DENTED (FUSELAGE) · airframe 55,215 hrs · 35,695 cycles

FUSELAGE SKIN DAMAGED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,215 hrs · 35,695 cycles

APPROX STA 200 STR 23 R SKIN DAMAGE.

Part: SKIN — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 55,215 hrs · 35,965 cycles

APPROX STA 1020- 1060 STR 26 R LAP SEAM HAS NUMEROUS FASTNERS W/ SKIN PILLOWING AROUND HEADS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,215 hrs · 35,965 cycles

APPROX STA 1263 STR 26 R SKIN DAMAGE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,215 hrs · 35,695 cycles

APPROX STA 385 25 L SKIN DAMAGE.

Part: STIFFENER — CORRODED (LT MLG WW) · corrosion level 2 · airframe 55,215 hrs · 35,965 cycles

CORROSION ON BACK SIDE OF STIFFNER, (LT WHEEL WELL).

Part: STIFFENER — CORRODED (WING) · corrosion level 2 · airframe 55,215 hrs · 35,695 cycles

REAR SPAR VERTICAL STIFFNER HAS AREA OF A COOROSION.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,215 hrs · 35,965 cycles

CORROSION ON BACK SIDE OF STIFFNERS.

Part: STIFFENER — CORRODED (LT WING) · corrosion level 2 · airframe 55,215 hrs · 35,695 cycles

REAR SPAR VERTICAL STIFFNER HAS AREA OF CORROSION.

Part: STIFFENER — CORRODED (RT WING) · corrosion level 2 · airframe 55,215 hrs · 35,695 cycles

VERTICAL STIFFENER CORRODED WS 198.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,215 hrs · 35,695 cycles

APPROX STA 380 STR 17 L SKIN DAMAGE.

Part: SKIN — DENTED (FUSELAGE) · airframe 55,215 hrs · 35,695 cycles

DENT IN SKIN, BELOW STR 19L STA 1015.

Part: LAP JOINT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,215 hrs · 35,695 cycles

APPROX STA 720A STR 19 R HAS CORROSION DIRECTLY BENEATH LAP SEAM.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,215 hrs · 35,695 cycles

APPROX STA 740 STR 19 L CORROSION ON SKIN JUST BENEATH LAP SEAM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,215 hrs · 35,695 cycles

APPROX STA 710 STR 24 L SKIN DAMAGE.

Part: SKIN — DENTED (FUSELAGE) · airframe 55,215 hrs · 35,695 cycles

SKIN DENTED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,215 hrs · 35,965 cycles

APPROX STA 1230 STR 23 L SKIN DAMAGED.

Part: ATTACH ANGLE — CRACKED · airframe 55,215 hrs · 35,695 cycles

FWD SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACK.

Part: ATTACH ANGLE — CRACKED · airframe 55,215 hrs · 35,695 cycles

FWD SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACK.

Part: ATTACH ANGLE — CRACKED · airframe 55,215 hrs · 35,695 cycles

FORWARD SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACK.

Part: ATTACH ANGLE — CRACKED · airframe 55,215 hrs · 35,695 cycles

FORWARD SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACK

Part: ATTACH ANGLE — CRACKED · airframe 55,215 hrs · 35,695 cycles

FORWARD SPAR VERTICAL ATTACH ANGLE HAS EVIDENCE OF A CRACK.

Part: BULKHEAD WEB — CRACKED (BS 740)

DURING ROUTINE CPCP CHECK INSPECTION, FOUND 0.5 CRACK AT FS 740 NR 2 FUEL TANK CENTER SECTION BULKHEAD WEB LOWER SECTION AT LBL 48. INSTALLED DOUBLER REPAIR IAW EA B2-57-008 DTD 12 AUG 97 AND IAW SKETCH NO AIA/E/2608 REV A DTD 11 AUG 97 IAW FAA FORM 8110-3 DTD 8/12/97. CORROSION TASK CARD NUMBER C57-174-01 PART 01 OF 01. NON-ROUTINE TASK CARD NUMBER 000425.

Part: CHORD — CORRODED (BS 740)

DURING ROUTINE CPCP CHECK INSPECTION, FOUND INTERGRANULAR CORROSION ON LOWER CHORD LBL 48, FS 740 FUEL TANK CENTER SECTION. INSTALLED DOUBLER REPAIR IAW EA B2-57-008 DTD 12 AUG 97 AND IAW SKETCH NR AIA/E/2608 REV A DTD 11 AUG 97. CORROSION TASK CARD NUMBER C57-174-01. NON-ROUTINE TASK CARD NUMBER 000426.

Part: SKIN — GOUGED (CARGO DOOR)

AFT LOWER CARGO DOOR GOUGED. REPLACED C-3 DOOR OUTER SKIN IAW ENGINEERING DEVIATION REQUEST B2-05454 AND B727 SRM 51-10-2. NON-ROUTINE TASK CARD NUMBER 000252.

Part: SKIN — HOLE (BS 950)

DURING ROUTINE CPCP CHECK INSPECTION, FOUND AFT LOWER BODY OUTER SKIN HAS SMALL HOLE AT STA 950.0C S-26 RT SIDE FWD OF NR 2 CARGO DOOR. REPAIRED HOLES IAW B727 SRM 51-40-9 PAGE 31 FIGURE 3. CORROSION TASK CARD NUMBER C-53-113-02. NON-ROUTINE TASK CARD NUMBER 000395.

Part: BULKHEAD — CRACKED (BS 740)

DURING ROUTINE CPCP CHECK INSPECTION, FOUND 2 CRACKS 1.5 APART FS 740 NR 2 FUEL TANK CENTER SECTION LEFT SIDE FOWARD BULKHEAD 5-6.5 FROM TOP LEFT 3.5-6 DOWN. INSTALLED DOUBLER REPAIR IAW EA B2-57-007 DTD 12 AUG 97 AND IAW SKETCH NR AIA/E/2607 REV B DTD 11 AUG 97. CORROSION TASK CARD NUMBER C57-174-01. NON-ROUTINE TASK CARD NUMBER 000394.

Part: BRAKES — OVERHEATED (LT/RT MLG)

WHEEL WELL FIRE INDICATED DURING CLIMBOUT. PROCEDURE IN FLIGHT MANUAL ACCOMPLISHED. LIGHT WENT OUT AS SOON AS GEAR WAS EXTENDED. INSPECTED LEFT AND RIGHT MAIN GEAR WELLS FOR FIRE DAMAGE, NO DAMAGE FOUND. CREW REPORTED HEAVY DUE TO SHORT FIELD LANDING REQUIREMENTS AND INSUFFICIENT TIME ON GROUND FOR NORMAL COOLING CYCLE. INSPECTED TIRES AND BRAKES FOR THERMAL DAMAGE, NONE NOTED. INSPECTION PERFORMED PER BAC727 MM 5-5-0 PAGE 206, ITEM 10.

Part: FIRE LIGHT — ILLUMINATED (WHEEL WELL)

WHEEL WELL FIRE WARNING LIGHT CAME ON. ACCOMPLISHED PROCEDURE IN FLIGHT MANUAL AND LIGHT WENT OUT, LIGHT WAS ON APPROXIMATELY 5 SECONDS. CHECKED BRAKES FOR OVERHEATING AND DRAGGING, FOUND BRAKE TEMPERATURE NORMAL ON ARRIVAL. INSPECTED WHEEL WELL FIRE LOOPS FOR CONDITION AND SECURITY, FOUND OK. WHEEL WELL LOOPS TEST NORMALLY.