N724CK

Part: BULKHEAD — CORRODED (ZONE 200) · corrosion level 2 · airframe 63,736 hrs · 48,791 cycles

RT AFT A/C BAY HAS EVIDENCE OF CORROSION ON AFT BULKHEAD.

Part: LUG — CORRODED (BONDING WIRE) · corrosion level 2 · airframe 63,736 hrs · 48,791 cycles

NR 2 KRUEGER FLAP OUTBOARD BONDING WIRE ATTACH POINT HAS CORROSION.

Part: STRUCTURE — CORRODED (RT WING LE) · corrosion level 2 · airframe 63,736 hrs · 48,791 cycles

RT WING LEADING EDGE NR 4 INTERNAL SIDE HAS CORROSION AT ATTACHMENT POINT OUTBOARD LOWER BONDING STRAP.

Part: STRUCTURE — CORRODED (RT WING LE FLAP) · corrosion level 2 · airframe 63,736 hrs · 48,791 cycles

RT WING #5 LEADING EDGE FLAP HAS CORROSION AT ATTACH POINT FOR INBOARD LOWER BONDING WIRE.

Part: SUPPORT ANGLE — CORRODED (LT WING) · corrosion level 2 · airframe 63,736 hrs · 48,791 cycles

LT WING LEADING EDGE BULLNOSE SUPPORT ANGLE HAS CORROSION AT FWD EDGE AT WS 328.

Part: LUG — CORRODED (BONDING WIRE) · corrosion level 2 · airframe 63,736 hrs · 48,791 cycles

RT WING LEADING EDGE FLAP NR 6 INTERNAL SIDE HAS CORROSION AT BOTH ATTACHMENT POINT INBOARD LOWER BONDING WIRE ON FLAP SIDE.

Part: LUG — CORRODED (BONDING WIRE) · corrosion level 2 · airframe 63,736 hrs · 48,791 cycles

NR 3 KRUEGAER FLAP OUTBOARD LOWER BONDING WIRE ATTACH POINT HAS CORROSION.

Part: SUPPORT ANGLE — CORRODED (LT WING LE) · corrosion level 2 · airframe 63,736 hrs · 48,791 cycles

LT WING LEADING EDGE BULLNOSE SUPPORT ANGLE HAS CORROSION AT FWD EDGE AT WS 237.

Part: SEAT TRACK — CORRODED (BS 720A-740) · corrosion level 2 · airframe 63,736 hrs · 48,791 cycles

MAIN DECK SEAT TRACK CORROSION

Part: CONTROL VALVE — FAILED (CABIN PRESSURE) · airframe 63,732 hrs · 48,789 cycles

AIRCRAFT WILL NOT PRESSURIZE, CABIN ALTITUDE WARNING WENT OFF PASSING THROUGH 10000 AFL WITH AIRCRAFT AT 10000 CABIN ALTITUDE DESCENDED TO 9500. DUCT PRESSURE 38 PSI – R 32 PSI – L, MANUAL PNEUMATIC CONTROLLER APPEARED TO OPERATE NORMAL. R & R NR 3 ENGINE SHUTOFF VALVE, IAW B727 AMM 36-10-10. OPS CHECK GOOD. R & R RT FLOW CONTROL VALVE. OPS AND LEAK CHECK GOOD, IAW B727 AMM 36-12-61. REPAIRED WIRES TO RT PACK, IAW SWPM 20-20-10 & 20-60-07.

Part: FLOW MULTIPLIER — FAILED (AC BAY) · airframe 63,672 hrs · 48,757 cycles

ON CLIMB OUT RIGHT PACK TRIP OFF LIGHT ILLUMINATED, AFTER RESET THE RT PACK WILL NOT RETURN TO OPERATE. IN WORK TO REPLACE THE FLOW MULTIPLIER

Part: FLOW MULTIPLIER — FAILED (RT A/C PACK) · airframe 63,672 hrs · 48,757 cycles

ON CLIMB OUT RIGHT PACK TRIP OFF LIGHT ILLUMINATED, AFTER RESET THE RT PACK WILL NOT RETURN TO OPERATE.

Part: ISOLATION VALVE — DEFECTIVE (CABIN PRESSURE) · airframe 63,667 hrs · 48,752 cycles

PRESSURIZATION SYSTEM FAILED TO PRESSURIZE DURING CLIMB OUT. AIRCRAFT RETURNED TO KCVG FOR UNSCHEDULED LANDING.

Part: FLOORBEAM — CORRODED (BS 620) · corrosion level 2 · airframe 63,550 hrs · 48,673 cycles

CORROSION ON LOWER CHORD OF FLOORBEAM STA 620 LBL 13

Part: FLOORBEAM — CORRODED (BS 620) · corrosion level 2 · airframe 63,550 hrs · 48,673 cycles

CORROSION ON MAIN DECK FLOORBEAM LOWER CHORD @ STA 620 LBL 6

Part: FLOORBEAM — CORRODED (BS 620) · corrosion level 2 · airframe 63,550 hrs · 48,673 cycles

CORROSION ON MAIN DECK FLOORBEAM LOWER CHORD @ STA 620 RBL 32

Part: FLOORBEAM — CORRODED (BS 620) · corrosion level 2 · airframe 63,550 hrs · 48,673 cycles

CORROSION ON LOWER CHORD OF FLOORBEAM STA 620 RBL 32

Part: FLOORBEAM — CORRODED (BS 620) · corrosion level 2 · airframe 63,550 hrs · 48,673 cycles

CORROSION ON LOWER SURFACE OF UPPER CHORD OF FLOORBEAM STA 620 LBL 2

Part: SEAT TRACK — CORRODED (BS 650-690) · corrosion level 2 · airframe 63,550 hrs · 48,673 cycles

CORROSION ON MAIN DECK SEAT TRACK STA 650 - 690 LBL 24

Part: SEAT TRACK — CORRODED (BS 620-660) · corrosion level 2 · airframe 63,550 hrs · 48,673 cycles

CORROSION ON MAIN DECK SEAT TRACK @ 620 - 660 RBL 24

Part: SEAT TRACK — CORRODED (BS 620-720A) · corrosion level 2 · airframe 63,550 hrs · 48,673 cycles

CORROSION ON MAIN DECK SEAT TRACK @ STA 620-720A BL0.

Part: FLOORBEAM — CORRODED (BS 620) · corrosion level 2 · airframe 63,550 hrs · 48,673 cycles

CORROSION ON MAIN DECK FLOORBEAM UPPER CHORD STA 620 LBL 2

Part: SEAT TRACK — CORRODED (BS 500) · corrosion level 2 · airframe 63,550 hrs · 48,673 cycles

CORROSION ON MAIN DECK STA 500 BL 0

Part: FLOORBEAM — CORRODED (BS 500) · corrosion level 2 · airframe 63,550 hrs · 48,673 cycles

CORROSION ON MAIN DECK FLOORBEAM @ STA 500 LBL 10 TO RBL 10

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,343 hrs · 48,501 cycles

INTERCOSTAL CRACKED @ STA 850-870 INBETWEEN STR 8 & 9R.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,343 hrs · 48,501 cycles

EVIDENCE OF CORROSION ON FUSELAGE SKIN @ STA 869 BETWEEN STR 8 & 9R.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,343 hrs · 48,501 cycles

@ STA 1161, LAP SEAM STR 20L, EXTERNAL SKIN HAS AREA OF PULLING FASTENERS & PILLOWING SKIN.

Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 63,343 hrs · 48,501 cycles

ULTRASONIC INDICATIONS FOUND @ STA 870 FRAMESPLICE @ STR 9L IN CENTER OF TERMINAL FITTING O/B FLANGE.

Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 63,343 hrs · 48,501 cycles

ULTRASONIC CRACK INDICATION FOUND @ STA 870 FRAME SPLICE @ STR 9R IN CENTER OF TERMINAL FITTING O/B FLANGE.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,343 hrs · 48,501 cycles

RT SIDE OF AIRSTAIRS LIGHTNING HOLE CRACKED @ STA 1293 RBL 20.5.

Part: CLAMP — LOOSE (AC BAY) · airframe 62,873 hrs · 48,293 cycles

DURING THE CLIMB PHASE OF FLIGHT CABIN ALTITUDE CLIMBED AT 1500’/MIN AFTER CLIMBING THROUGH 20000 FEET CABIN PRESSURIZATION COULD NOT BE CONTROLLED, DECENT BELOW 10000 REQUIRED AND RETURNED TO KYIP. CORRECTIVE ACTION: UPON INVESTIGATION FOUND RT MOISTURE SEPARATOR CLAMP LOOSE, R&R O-RINGS AND RE SECURED CLAMPS IAW AMM 21-55-41, OPS CHECK GOOD IAW AMM 21-31-00, LEAK CHECK GOOD IAW AMM 21-55-41.

Part: PITOT LINE — CLOGGED · airframe 62,776 hrs · 48,234 cycles

DURING THE CLIMB PHASE OF FLIGHT (THROUGH FL250) THE ELEVATOR FEEL DIFFERENTIAL PRESSURE LIGHT ILLUMINATED. NO OTHER INDICATIONS OCCURRED. PILOT CALLED FOR AND COMPLIED WITH CHECKLIST. PILOT THEN COORDINATED WITH OPS TO DIVERT TO KLRD CORRECTIVE ACTION: FOUND DEBRIS IN L/H ELEVATOR FEEL PITOT LINE CLEARED LINE OF DEBRIS PER B727AMM 27-30-00 TROUBLE SHOOTING CHART FIG 101, LEAK & OPS CHECK GOOD IAW B727 AMM 27-30-81, NO FURTHER DEFECTS NOTED

Part: STRINGER — CRACKED (BS 294.5) · airframe 62,774 hrs · 48,233 cycles

STRINGER CRACKED AT STA 294.5 STR 14L @ UPPER & LOWER FASTENER HOLES COMMON TO FRAME

Part: STRINGER — CRACKED (BS 294.5) · airframe 62,774 hrs · 48,233 cycles

STRINGER CRACKED AT STA 294.5 STR 15L @ UPPER & LOWER FASTENER HOLES COMMON TO FRAME

Part: BEAM — CRACKED (VERTICAL STAB) · airframe 62,774 hrs · 48,233 cycles

VERTICAL STAB KICK LOAD BEAM WEB POST CRACKED.

Part: STRUCTURE — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 62,774 hrs · 48,233 cycles

INNER CHORD ABOVE #2 ENGINE

Part: STRUCTURE — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 62,774 hrs · 48,233 cycles

INNER CHORD ABOVE #2 ENGINE RIGHT SIDE HAS AREAS OF CORROSION.

Part: STRUCTURE — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 62,774 hrs · 48,233 cycles

OUTER CHORD ABOVE #2 ENGINE HAS CORROSION

Part: SUPPORT RIB — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 62,774 hrs · 48,233 cycles

FUSELAGE SKIN SUPPORT RIB ABOVE #2 ENGINE HAS CORROSION ON RIGHT SIDE.

Part: SKIN — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 62,774 hrs · 48,233 cycles

FUSELAGE EXTERIOR CORROSION. #2 ENGINE RIGHT SIDE ABOVE COWLING.

Part: SKIN — CRACKED (BS 1095) · airframe 62,774 hrs · 48,233 cycles

FUSELAGE SKIN, 1 INCH CRACK. UNDER ENGINE INLET FWD END OF CAVITY THROUGH ACCESS PANELS 9521 AND 9522, ON FUSELAGE.

Part: SHEAR TIE — CRACKED (BS 1350) · airframe 62,774 hrs · 48,233 cycles

SHEAR TIE CRACK ON KICKLOAD BEAM

Part: FLOORBEAM — CORRODED (BS 312) · corrosion level 2 · airframe 62,774 hrs · 48,233 cycles

FLOOR BEAM CORROSION

Part: FLOORBEAM — CORRODED (BS 328) · corrosion level 2 · airframe 62,774 hrs · 48,233 cycles

FLOOR BEAM CORROSION

Part: SKIN — CRACKED (ZONE 200) · airframe 62,774 hrs · 48,233 cycles

CRACK IN EXTERIOR SKIN ABOVE LEFT AFT EMERGENCY EXIT HATCH, ABOVE HANDLE.

Part: WEB — CRACKED (BS 1350) · airframe 62,774 hrs · 48,233 cycles

WEB CRACK ON KICKLOAD BEAM

Part: SUPPORT ANGLE — CRACKED (RT MLG WW) · airframe 62,774 hrs · 48,233 cycles

SUPPORT ANGLE CRACKED IN RIGHT WHEEL WELL

Part: WARNING SYSTEM — FALSE ACTIVATION (FIRE DETECTION) · airframe 62,717 hrs · 47,793 cycles

CARGO FIRE BELL AND LIGHT ACTIVATED AT APPROXIMATELY 20,000 FT. DURING CLIMB OUT. WARNINGS CEASED AFTER APPROXIMATELY ONE MINUTE. ACCOMPLISHED EMERGENCY PROCEDURES AND RETURNED TO DEPARTURE. PERFORMED AN OPS CHECK OF THE CARGO SMOKE DETECTION SYSTEM. OPS CHECKED GOOD IAW AMM 26-15-00-7. NO DEFECTS NOTED.

Part: NOT REPORTED — MALFUNCTIONED (CABIN PRESSURE) · airframe 62,352 hrs · 47,877 cycles

AIRCRAFT WOULD NOT PRESSURIZE.

Part: SHEAR TIE — CORRODED (BS 720A) · corrosion level 2 · airframe 61,962 hrs · 47,607 cycles

SHEAR TIE CORRODED BS 720A BETWEEN STRINGERS 27 - 28R.

Part: DRIVE UNIT — DEFECTIVE (TE FLAP) · airframe 61,935 hrs · 47,589 cycles

OTBD FLAPS RETRACTED FROM 25 DEGREES TO 0 ON FINAL APPROACH UNCOMMANDED. LEADING EDGE DEVICES ALSO RETRACTED. REPLACED OUTBOARD FLAP DRIVE POWER UNIT.

Part: SWITCH — FAILED (MLG HANDLE) · airframe 61,873 hrs · 47,550 cycles

GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. REPLACED CONTROL LEVER POSITION SWITCH, OP'S CHECKED GOOD IAW AMM 32-61-12.

Part: SPAR — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 61,780 hrs · 47,489 cycles

VERTICAL STABILIZER INTERIOR REAR SPAR CORROSION BS 1342, RBL 5.

Part: MOUNT — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 61,780 hrs · 47,489 cycles

NR 1 PYLON LOWER SIDE OF FWD MOUNT FITTING HAS CORROSION ON AND AROUND FASTENERS.

Part: TRUNNION — CORRODED (NLG) · corrosion level 2 · airframe 61,780 hrs · 47,489 cycles

RIGHT UPPER NLG TRUNNION CAP EVIDENCE OF CORROSION ON OTBD FACE.

Part: SKIN — CORRODED (BS 1101) · corrosion level 2 · airframe 61,780 hrs · 47,489 cycles

LAP SEAM AREA OF CORROSION BS 1101, STR 10L.

Part: FRAME — CRACKED (BS 1303) · airframe 61,780 hrs · 47,489 cycles

FRAME WEB CRACKED BS 1303 OTBD END.

Part: TRUNNION — CORRODED (NLG) · corrosion level 2 · airframe 61,780 hrs · 47,489 cycles

NLG LT UPPER TRUNNION CAP EVIDENCE OF CORROSION ON OTBD FACE.

Part: TRUNNION — CORRODED (NLG) · corrosion level 2 · airframe 61,780 hrs · 47,489 cycles

TRUNNION CAP EVIDENCE OF CORROSION BOTH INBD AND OTBD FACE, NLG.

Part: FITTING — CORRODED (FIRE WALL) · corrosion level 2 · airframe 61,780 hrs · 47,489 cycles

SEVERAL CORRODED FASTENERS ON RIGHT SIDE OF S-DUCT FIREWALL FITTING.

Part: WARNING LIGHT — ILLUMINATED (NR 2 ENG FILTER) · airframe 61,706 hrs · 47,443 cycles

NR 2 ENGINE FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. PERFORMED PRECAUTIONARY SHUTDOWN IAW ABNORMAL PROCEDURES AND RETURNED TO DEPARTURE.

Part: PUMP — INOPERATIVE (HYDRAULIC SYS) · airframe 60,958 hrs · 47,026 cycles

AFTER TAKEOFF, LOST (B) SYSTEM HYDRAULICS, REPLACED RT (B) SYSTEM HYDRAULIC PUMP IAW AMM 29-12-11, SERVICED HYD IAW AMM 12-12-01, PERFORMED SYSTEM TEST IAW AMM 29-12-11, OPS CHECK GOOD, NO LEAKS NOTED.

Part: GYRO — DEFECTIVE (ZONE 200) · airframe 60,687 hrs · 46,876 cycles

F/O'S HSI COMPASS CARD FAILED, RETURNED TO HOME BASE, NO EMERGENCY PROCEDURES TAKEN. PART RETURNED FROM VENDOR WITH THE FOLLOWING FINDINGS, HOUSING LOOSE, FOUND OPEN LAMPS, BACKPLATE LOOSE, BOTH POINTERS STICKING, MOTOR AND GEARS DIRTY. THIS REPORT IS A FOLLOW UP TO THE ORIGINAL SUBMITTED ON 11/29/2012.

Part: TRU — MALFUNCTIONED (E&E BAY) · airframe 60,493 hrs · 46,758 cycles

NR 2 GEN RT SYNC LIGHT REMAINED ILLUMINATED AFTER SYNCHRONIZING GEN WITH STANDARD BLEED CONFIGURATION AT 35,000 VISIBLE SMOKE IN COCKPIT CAME FROM AROUND PILOTS FEET, PACKS WERE FULL COLD COOLING DOOR HALF OPEN, 1 PACK TEMP IND RIGHT TEMP 50 DEGREES RAN A/C SMOKE CHECKLIST. TURNED OFF GASPER FAN, SMOKE CLEARED OUT 5 MIN LATER, SMELL GONE GASPER REMAINED OFF.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,931 hrs · 46,409 cycles

STRINGER CORROSION, 10 INCHES.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,931 hrs · 46,409 cycles

SHEAR TIE CLIP CORROSION, 6 INCHES, STA 1130 STRINGER 20 TO 21 LEFT.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 59,931 hrs · 46,409 cycles

NOSE WHEEL PRESSURE WEB CRACK.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,931 hrs · 46,409 cycles

STRINGER CORROSION, STA 950E PLUS 16 INCHES TO = 20 INCHES STRINGER 30, 20 INCH CORROSION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,931 hrs · 46,409 cycles

FLOORBEAM CORROSION AT STA 1130 LBL 28 AND 43.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,931 hrs · 46,409 cycles

FRAME CORROSION, 3 INCHES AT STA 620 RBL 24.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,931 hrs · 46,409 cycles

SKIN CORROSION, STA 720B PLUS 8 INCHES STRINGER 28R, 2 X 3 INCHES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,931 hrs · 46,409 cycles

FLOORBEAM CORROSION AT STA 1130 LBL 11 AND 18. 2 INCH IN EACH POSITION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,931 hrs · 46,409 cycles

SEAT TRACK CORROSION, 60 INCHES, STA 1010 TO 1070 LBL 46.

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

FRAME SHEAR TIE CORROSION 5 INCHES.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,441 hrs · 46,146 cycles

EVIDENCE OF SKIN CORROSION 12 X 12 INCH.

Part: NUT — LOOSE (OXYGEN SYSTEM) · airframe 59,351 hrs · 46,098 cycles

ON CLIMBOUT NOTED OXYGEN HAD DEPLETED FROM 1750 LBS TO 1000 LBS VERIFIED ALL REGULATORS / VALVES IN NORMAL FLIGHT POSITIONS ATTEMPTED TO TEST SYSTEM AND AFTER SEVERAL SHORT BREATHS OXYGEN SYSTEM DROP TO 0 PSI AND NO FLOW. UPON INSPECTION FOUND REGULATOR NUT LOOSE, SERVICED IAW B727 MM 12-15-11, OP'S CHECK GOOD AND NO OTHER DEFECTS NOTED.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,182 hrs · 45,998 cycles

SKIN DENTED 1 X 1 INCH.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,182 hrs · 45,998 cycles

SKIN DENTED 1.3 X 1.5 INCHES.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,182 hrs · 45,998 cycles

SKIN DENTED 1 X 1 INCH.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,182 hrs · 45,998 cycles

SKIN HAS DENT 1 X 2 INCHES.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,182 hrs · 45,998 cycles

SKIN DENTED 1 X 1 INCH.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,182 hrs · 45,998 cycles

SKIN DENT.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,182 hrs · 45,998 cycles

SKIN HAS DENT 1 X 1 INCH.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,182 hrs · 45,998 cycles

SKIN HAS DENT.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,182 hrs · 45,998 cycles

SKIN DENTED .5 X .5 INCH.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,182 hrs · 45,998 cycles

SKIN HAS DENT 1 X 1 INCH.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,182 hrs · 45,998 cycles

SKIN HAS DENT, 1 X 1 INCH.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,182 hrs · 45,998 cycles

SKIN DENTED 1 X 1 INCH.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,182 hrs · 45,998 cycles

SKIN DENTED 2 X 2 INCHES.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,182 hrs · 45,998 cycles

SKIN HAS DENT AND CREASE 1 X 4 INCHES.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 59,182 hrs · 45,998 cycles

SEAT TRACK HAS CORROSION ON TOP SIDE.

Part: STIFFENER — CORRODED (VERTICAL STAB) · corrosion level 3 · airframe 59,182 hrs · 45,998 cycles

REAR SPARS STIFFENER CORROSION ON WEB.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 3 · airframe 59,182 hrs · 45,998 cycles

SEAT TRACK HAS CORROSION ON TOP SIDE.

Part: SPAR — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 58,817 hrs · 45,763 cycles

HORIZONTAL STABILIZER CORROSION ON LOWER CHORD RT HORIZONTAL REAR SPAR.

Part: WEB — CRACKED (BS 1223) · airframe 58,594 hrs · 45,631 cycles

VERTICAL WEB CRACKED AT LIGHTNING HOLE.

Part: BEAM — DAMAGED · airframe 58,594 hrs · 45,631 cycles

TRANSVERSE LOWER CHORD BEAM DAMAGED.

Part: WEB — CRACKED (BS 1223) · airframe 58,594 hrs · 45,631 cycles

VERTICAL WEB CRACKED AT LIGHTING HOLE.

Part: WEB — CRACKED (DOOR) · airframe 58,594 hrs · 45,631 cycles

VERTICAL WEB FWD OF AIRSTAIRS HAS 6 INCH CRACK IN WEB.

Part: WEB — PUNCTURED (FUSELAGE) · airframe 58,594 hrs · 45,631 cycles

VERTICAL WEB JUST FORWARD OF AIRSTAIRS HAS 1 INCH PUNCTURE.

Part: STOP FITTING — CRACKED (PAX DOOR) · airframe 58,151 hrs · 45,299 cycles

A 5 INCH CRACK IN DOOR STOP FITTING.

Part: WEB — CORRODED · airframe 58,151 hrs · 45,299 cycles

A 3 X 1 INCH AREA OF CORROSION ON WEB.

Part: ATTACH ANGLE — CORRODED · airframe 58,151 hrs · 45,299 cycles

A .5 X .5 INCH AREA OF CORROSION ON ATTACH ANGLE.

Part: STOP FITTING — CRACKED · airframe 58,151 hrs · 45,299 cycles

A 5 INCH CRACK IN DOOR STOP FITTING.

Part: STRINGER CLIP — CRACKED · airframe 58,151 hrs · 45,299 cycles

A .5 INCH CRACK IN STRINGER CLIP.

Part: FITTING — CRACKED · airframe 58,151 hrs · 45,299 cycles

A .5 INCH CRACK IN FITTING.

Part: STRINGER CLIP — CRACKED · airframe 58,151 hrs · 45,299 cycles

A 1 INCH CRACK IN STRINGER CLIP.

Part: SKIN — CORRODED · airframe 58,151 hrs · 45,299 cycles

THREE 2 INCH DIAMETER AREAS OF CORROSION ON INNER SKIN.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 58,151 hrs · 45,299 cycles

SEVERAL AREAS OF CORROSION ON NOSE T-CHORD.

Part: WEB — CORRODED (FUSELAGE) · airframe 58,151 hrs · 45,299 cycles

A 2 X 10 INCH AREA OF CORROSION ON WEB.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,151 hrs · 45,299 cycles

CRACK IN STRINGER SPLICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 58,151 hrs · 45,299 cycles

CRACK IN ANGLE.

Part: BRACE — CRACKED (FUSLEAGE) · airframe 58,151 hrs · 45,299 cycles

CRACK IN BRACE.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 58,151 hrs · 45,299 cycles

CRACK IN LOWER CHORD.

Part: DOUBLER — NICKED (FUSELAGE) · airframe 58,151 hrs · 45,299 cycles

NICK IN DOUBLER.

Part: DOUBLER — NICKED (FUSELAGE) · airframe 58,151 hrs · 45,299 cycles

NICK IN DOUBLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 58,151 hrs · 45,299 cycles

DENT ON FUSELAGE FRAME FLANGE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,151 hrs · 45,299 cycles

CRACKS ON STRINGER RIB FLANGE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,151 hrs · 45,299 cycles

CRACKS ON STRINGER RIB ATTACHMENT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,151 hrs · 45,299 cycles

CRACK IN FUSELAGE FRAME SUPPORT.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,151 hrs · 45,299 cycles

CRACKS ON STRINGER RIB ATTACHMENT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,151 hrs · 45,299 cycles

A 1 INCH CRACK ON FUSELAGE FRAME.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 58,181 hrs · 45,299 cycles

CORROSION ON DOOR OPENING REINFORCEMENT.

Part: SEAT TRACK — CORRODED (FUSELAGE)

1 X 1 AREA OF CORROSION SEAT TRACK.

Part: FRAME — CRACKED (FUSELAGE)

2 INCH CRACK ON FUSE FRAME CHORD REPLACEMENT

Part: FRAME — CRACKED (FUSELAGE)

1 INCH CRACK ON FRAME REPLACEMENT