N412SN

Part: NONE — NONE · airframe 75,358 hrs · 15,426 cycles

LVL 2 HYDRAULIC 2 FAIL.

Part: WARNING MESSAGE — ILLUMINATED (OIL FILTER) · airframe 74,239 hrs · 15,213 cycles

AIR RETURN DUE TO LEVEL 2 ENGINE 2 OIL FILTER ALERT. SHUTDOWN ENGINE IN FLIGHT PER CHECKLIST.

Part: WARNING MESSAGE — ILLUMINATED (CARGO DOOR) · airframe 74,217 hrs · 15,198 cycles

AIR RETURN CARGO DOOR WARNING "UPPER B".

Part: MANIFOLD — FAILED (WING DE ICE) · airframe 74,130 hrs · 15,151 cycles

IN ICING CONDITIONS WING A-ICE DISAGREE WITH WING ANTI-ICE. WITH WING ANTI-ICE ON LEVEL 1 AIR SYSTEM FAIL MANIFOLD ILLUMINATION ON OVERHEAD PANEL.

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 73,807 hrs · 15,081 cycles

CABIN PRESSURE UNCONTROLLABLE, CPC FAULT.

Part: ELECTRICAL SYS — SHORTED · airframe 70,787 hrs · 14,326 cycles

DURING CLIMB OUT, EXPERIENCED LEVEL 3 CABIN ALERT, PRIMARY FLIGHT DISPLAYS LOST ALL INSTRUMENTATION, BOTH PFDS NO CONTROL OF GCP. CONTINUOUS EGPWS WARNINGS. CAPTAINS WINDOW BLEW A SEAL ON FINAL. NO CONTROL OF AUTOTHROTTLE, COULD NOT DISENGAGE UNTIL AFTER LANDING. AIRCRAFT SYSTEMS BEING TROUBLESHOT. WATER FOUND IN CENTER ELECTRICAL COMPARTMENT. MORE TO FOLLOW.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 70,480 hrs · 14,244 cycles

TAILCONE AFT BODY BULKHEAD RH ALIGNMENT PIN FITTING HAS ELONGATED HOLE. ACCOMPLISHED REPAIR ON FUSELAGE AFT BODY BULKHEAD RT ALIGNMENT PIN FITTING AT Y=2163.35 AND L-35 PER EA 011-5360-52-A7438 I/R AND DWG AJC7880-1.

Part: FILLET — CRACKED (ZONE 500) · airframe 70,480 hrs · 14,244 cycles

LT PERFORMANCE FILLET IS CRACKED AT OTBD UPPER ATTACH FITTING. ACCOMPLISHED REPAIR ON LT OTBD UPPER ATTACH FITTING SKIN PER SRM 57-40--71 REPAIR 1 REV 64 REF NRC3 A044628.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,480 hrs · 14,244 cycles

FWD AVIONICS COMP FRAME AT STA 455 LBL 35 HAS CORROSION. ACCOMPLISHED REPAIR AT FWD AVIONICS COMPARTMENT FRAME AT STA 455 LBL 35 PER SRM 53-00-07 REPAIR 2 FIG 201 REF NRC A043591.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,480 hrs · 14,244 cycles

FWD AVIONICS COMPARTMENT AFT PRESSURE BULKHEAD SUPPORT STRUCTURE IS CORRODED AT STA 475 LBL17 TO RBL 29. REMOVED, FABRICATED AND INSTALLED FWD AVIONICS COMPARTMENT AFT PRESSURE BULKHEAD FRAME STIFFENER AT STA 475 LBL 10 TO RBL 10 PER SRM 51-31-01 PG 1 AND DWG NCA6042-117 REF NRC A042921.

Part: SPAR CAP — CORRODED (RT WING) · corrosion level 2 · airframe 70,480 hrs · 14,244 cycles

RIGHT WING REAR SPAR UPPER CAP AT XORS 975 TO XORS 1051 HAD CORROSION. ACCOMPLISHED A REPAIR IAW EA 011-5720-52-A7392, I/R.

Part: FRAME — CRACKED (TAILCONE) · airframe 70,480 hrs · 14,244 cycles

TAILCONE FRAME BS 2257 RH SIDE UPPER CORNER IS CRACKED. ACCOMPLISHED REPAIR ON TAILCONE FRAME RH SIDE AT STA 2257 PER MD-11 SRM 53-80-07 REPAIR 4 .

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 70,480 hrs · 14,244 cycles

RIGHT INBD FLAP VANE OUTER SKIN WAS DELAMINATED AROUND PANEL 643CT. ACCOMPLISHED A REPAIR IAW EA 011-5750-52-A7381 I/R.

Part: PIN — GOUGED (TAILCONE) · airframe 70,480 hrs · 14,244 cycles

FWD TAIL CONE MID LT GUIDE PIN WAS LOOSE. ACCOMPLISHED A REPAIR IAW SRM 53-80-07, REPAIR 1, REV 64.

Part: SKIN — CORRODED (BS 2120) · corrosion level 2 · airframe 70,480 hrs · 14,244 cycles

AFT FUSELAGE, RT SIDE EXTERNAL SKIN HAD CORROSION AT BS 2120. ACCOMPLISHED A REPAIR BETWEEN BS 2120 AND 2164, STRINGER 32R AND 35R IAW EA 011-5370-52-A7383, I/R.

Part: SKIN — DENTED (TAILCONE) · airframe 70,480 hrs · 14,244 cycles

FUSELAGE TAIL CONE HAS A DENT ON LH SIDE STA 2205. ACCOMPLISHED SKIN REPAIR ON LH AFT SIDE OF EXTENDED TAIL CONE BETWEEN STA 2199 AND STA 2204 Z=5.0 PER VT SAA EA#011-5310-52-A7322 I/R REF VT SAA NRC# A042789.

Part: SKIN — GOUGED (LT WING SLAT) · airframe 70,480 hrs · 14,244 cycles

LH WING #8 SLAT HAS CHAFFE DAMAGE ON INBD SIDE

Part: SKIN — CORRODED (BS 2128-2164) · corrosion level 2 · airframe 70,480 hrs · 14,244 cycles

LH AFT FUSELAGE SKIN BETWEEN STA 2128 TO STA 2164 BETWEEN STGR 32L AND STGR 35L HAS CORROSION. ACCOMPLISHED REPAIR ON LH AFT FUSELAGE SKIN BETWEEN STA 2128 AND STA 2164 AT STGR 32L TO STGR 35L PER VT SAA EA#011-5370-52-A7375 I/R REF VT SAA NRC# A043610.

Part: SKIN — CHAFED (TAILCONE) · airframe 70,480 hrs

TAILCONE RT INNER SKIN WAS CHAFED. ACCOMPLISHED A REPAIR IAW EA011-5380-52-A7369 I/R.

Part: DOOR — CRACKED (TAILCONE) · airframe 70,480 hrs · 14,244 cycles

FWD TAILCONE UPPER RT AFT DOOR WAS CRACKED. REPAIRED IAW EA 011-5246-52-A7329 I/R.

Part: SKIN — CRACKED (TAILCONE) · airframe 70,480 hrs · 14,244 cycles

FWD TAILCONE UPPER LT PATIO DOOR WAS CRACKED AND GOUGED ON EXTERNAL SKIN. ACCOMPLISHED A REPAIR ON THE TAILCONE EXTERNAL SKIN IAW EA 011-5246-52-A7328, I/R.

Part: SKIN — CHAFED (TAILCONE) · airframe 70,480 hrs · 14,244 cycles

EXTENDED TAILCONE LT SIDE BS 2163 TO 2165 SKIN WAS CHAFED. ACCOMPLISHED A REPAIR ON THE TAILCONE SKIN IAW EA 011-5380-52-A7368, I/R.

Part: BEAM — GOUGED (TAILCONE) · airframe 70,480 hrs · 14,244 cycles

STRUCTURE IS GOUGED INSIDE FWD TAILCONE ABOVE LADDER. REMOVED AND REPLACED FWD TAILCONE BEAM, SUPPRT FITTING AND UPPER LATCH FITTING PER MD-11 SRM 51-31-01 AND SRM 53-00-00 FIG 210 REF VT SAA NRC# A042754.

Part: PIN — WORN (TAILCONE) · airframe 70,480 hrs · 14,244 cycles

FWD TAILCONE MID RH GUIDE PIN WORN THROUGH SURROUNDING STRUCTURE. ACCOMPLISHED REPAIR AT FWD TAILCONE IAW SRM 53-80-07 REPAIR 1.

Part: SKIN — CORRODED (RUDDER) · corrosion level 2 · airframe 70,480 hrs · 14,244 cycles

UPPER FWD RUDDER HAD CORROSION ON THE LOWER RT SIDE. REPAIRED IAW SRM 55-40-01, REPAIR 1, FIG 201.

Part: STIFFENER — CORRODED (E/E DOOR FRAME) · corrosion level 2 · airframe 70,480 hrs · 14,244 cycles

LEFT VERTICAL STIFFENER IN THE AVIONICS BAY DOOR CUTOUT WAS CORRODED. ACCOMPLISHED A REPAIR IAW SRM 51-33-01, PARA 8B.

Part: BULKHEAD — CRACKED (NR 1 NACELLE) · airframe 70,480 hrs · 14,244 cycles

NR 1 PYLON CENTER STRUCTURE BULKHEAD, INBD SIDE WAS CRACKED AT YN 307. ACCOMPLISHED A REPAIR ON THE PYLON BULKHEAD IAW EA 011-5450-52-A7385, I/R.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 70,480 hrs · 14,244 cycles

LEFT PRIMARY AND SECONDARY STATIC PORT PLATES, INTERIOR SIDE, HAD CORROSION. ACCOMPLISHED A BLEND OUT REPAIR ON THE LT PRIMARY AND SECONDARY STATIC PORT PLATES IAW EA 011-3411-52-A7389, I/R.

Part: TRUNNION — GOUGED (NLG) · airframe 70,480 hrs · 14,244 cycles

NLG TRUNION FITTING, LT SIDE WAS GOUGED. ACCOMPLISHED A BLEND OUT REPAIR IAW EA 011-5310-52-A7326, IR.

Part: BEAM — CORRODED (LT WING) · corrosion level 2 · airframe 70,480 hrs · 14,244 cycles

LEFT WING T/E BEAM ASSY, UPPER CAP HAD CORROSION AT XW 265. ACCOMPLISHED A REPAIR IAW EA 011-5710-52-A7320 I/R.

Part: SLAT — GOUGED (LT WING SLAT) · airframe 70,480 hrs · 14,244 cycles

LEFT WING NR 5 SLAT T/E HAD A GOUGE. ACCOMPLISHED A BLENDOUT REPAIR ON THE NR 5 SLAT T/E SKIN IAW EA 011-5750-52-A7350 I/R.

Part: LANDING — CORRODED (LT WING) · corrosion level 2 · airframe 70,480 hrs · 14,244 cycles

LEFT WING T/E ACCESS PANEL LANDING HAD CORROSION AT XORS 402. ACCOMPLISHED A BLEND OUT REPAIR IAW EA 011-5750-52-A7390, I/R.

Part: VANE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 70,480 hrs · 14,244 cycles

FOUND HEAVY CORROSION AND DEEP PITTING ON THE RT INBD FLAP VANE AT THE INNER AND OUTER ATTACH POINT INNER RIBS. REMOVED AND REPLACED THE FLAP VANE IAW AMM 27-50-22.

Part: PIN — CRACKED (TAILCONE GUIDE) · airframe 70,480 hrs · 14,244 cycles

FWD TAILCONE LT GUIDE PIN WAS LOOSE. ACCOMPLISHED A REPAIR ON FWD TAILCONE IAW SRM 53-80-07, REPAIR 1.

Part: FRAME — CHAFED (THRUST REVERSER) · airframe 70,480 hrs · 14,244 cycles

NR 2 ENG LT TR FWD FRAME LOWER SURFACE HAS SEVERAL CHAFING MARKS. INSTALLED REPAIR DOUBLERS ON NR 2 LT TR FWD FRAME OUTER RING PER CMM 78-32-02 REPAIR 32.

Part: RIB — CRACKED (LE SLAT) · airframe 70,480 hrs · 14,244 cycles

RT WING NR 3 SLAT INNER RIB IS CRACKED. REMOVED, FABRICATED AND INSTALLED RT WING NR 3 SLAT INNER RIB PER SRM 51-35-01 REV 64 REF NRC A043716.

Part: SKIN — GOUGED (LE SLAT) · airframe 70,480 hrs · 14,244 cycles

NR 3 SLAT AFT INNER SKIN IS GOUGED FWD OF NR 6 SLAT TRACK. ACCOMPLISHED REPAIR ON NR 3 SLAT INNER SKIN BETWEEN XOS 455 AND XOS 497 PER SRM 57-40-01 REPAIR 3 FIG 201 REF NRC A043464.

Part: HOUSING — CHAFED (THRUST REVERSER) · airframe 70,480 hrs · 14,244 cycles

NR 2 LT TR FWD FRAME ACTUATOR HOUSING SUPPORT BRACKET IS CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER ON NR 2 LT TR FWD FRAME LOWER BALLSCREW ACTUATOR HOUSING PER CMM 78-32-02 REPAIR 16.

Part: HOUSING — CRACKED (THRUST REVERSER) · airframe 70,480 hrs · 14,244 cycles

NR 2 ENG RT TR FWD FRAME LOWER BALLSCREW ACTUATOR HOUSING SUPPORT BRACKET IS CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER ON NR 2 RT TR FWD LOWER FRAME HOUSING PER CMM 78-32-02 REPAIR 16.

Part: DOUBLER — GOUGED (TAILCONE) · airframe 70,480 hrs · 14,244 cycles

AFT TAILCONE FWD LH SIDE OF FRAME DOUBLER IS GOUGED. REMOVED, FABRICATED AND INSTALLED NEW ANGLE REPAIR PER SRM 53-00-00 FIG 210.

Part: DOUBLER — CHAFED (TAILCONE) · airframe 70,480 hrs · 14,244 cycles

FWD TAIL CONE IS CHAFED ON DOUBLER AT AFT TAI CONE. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER AT FWD TAIL CONE PER SRM 53-00-00 FIG 204.

Part: WEB — CRACKED (TAILCONE) · airframe 70,480 hrs · 14,244 cycles

AFT TAILCONE LT FWD FLOOR FRAME WEB IS CRACKED. REMOVED DAMAGED, FABRICATED AND INSTALLED REPAIR DOUBLER ON AFT TAILCONE LT FWD FLOOR FRAME WEB PER SRM 53-80-02 AND DWG AKC7602.

Part: DOUBLER — CRACKED (LT WING) · corrosion level 2 · airframe 70,480 hrs · 14,244 cycles

LT WING L/E BEADED DOUBLER IS CRACKED IN 2 PLACES AT XOS 695. ACCOMPLISHED REPAIR AT LT WING L/E BEADED DOUBLER AT STA XOS 695 PER SRM 57040-02 REPAIR 15 REF NRC A042990.

Part: DOUBLER — CRACKED (RT WING) · airframe 70,480 hrs · 14,244 cycles

RT WING L/E BEADED DOUBLER IS CRACKED AT XOS 610. ACCOMPLISHED REPAIR ON RT WING L/E BEADED DOUBLER AT XOS 610 PER SRM 57-40-02 REPAIR 15 FIG 205 REF NRC A042951.

Part: STATIC PORT — OBSTRUCTED (PITOT/STATIC SYS) · airframe 70,480 hrs · 14,244 cycles

AVIONICS FAN OVER RIDE ON DESCENT INTERMTTANTLY. REVIEWED FAULT HISTORY FROM ESC, "NO FAULTS STORED" INSPECTED LEFT ALTERNATE STATIC PORT, FOUND OBSTRUCTION INSIDE STATIC PORT. CLEANED AND INSPECTED LEFT AND RIGHT STATIC PORTS. PERFORMED PURGE OF THE PITOT AND STATIC SYSTEM PER AMM 34-11-00. LEAK CHECK GOOD.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 69,214 hrs · 13,803 cycles

EMERGENCY LIGHTS FAIL TO ILLUMINATE WITH EMERGENCY LIGHT SWITCH ON. REPAIRED A SHORTED WIRE.

Part: HINGE FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

LEFT OUTBOARD FLAP, OUTBOARD FORWARD HINGE FITTING, SIDE FITTING BORES HAVE CORROSION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,214 hrs · 13,803 cycles

EMERGENCY LIGHTS DO NOT ILLUMINATE WITH SWITCH SET TO ON.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CENTER E & E BAY LONGERON 51R AT STATION 1140 HAS CORROSION UNDER THE JUNCTION BOX.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CENTER E & E BAY SPLICE FITTING AT STATION 1145 LONGERON 50R IS CORRODED.

Part: BEAM — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

MAIN CARGO DOOR UPPER JAMB BEAM HAS CORROSION AT THE FORWARD END THAT EXTENDS UNDER THE FIRST LOCK ROLLER

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

LEFT WING UPPER SKIN IS CORRODED AT THE AFT SPAR AT XORS 388 TO 423

Part: LONGERON — CORRODED (BS 1140) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CENTER E & E BAY LONGERON 51R AT BS 1140 HAS CORROSION UNDER THE JUNCTION BOX.

Part: BRACE — CORRODED (RT MLG) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

RIGHT MLG LOWER SIDE BRACE NUT HAS CORROSION IN THREADS

Part: SKIN — CRACKED (RT WING LE) · airframe 69,214 hrs · 13,803 cycles

CRACK IN THE LEADING EDGE SKIN OF THE RIGHT WING LOWER SURFACE TRAILING EDGE AT STATION XORS 803

Part: NUT — CORRODED (MLG) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

LEFT MAIN LANDING GEAR SIDE BRACE NUT IS CORRODED IN THE THREADS.

Part: DOUBLER — CRACKED (RT WING) · airframe 69,214 hrs · 13,803 cycles

CRACK IN THE STRINGER DOUBLER OF THE LEADING EDGE SKIN OF THE RIGHT WING LOWER SURFACE AT STATION XORS 815.

Part: PIN — CORRODED (RT MLG) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

RIGHT MAIN LANDING GEAR FORWARD TRUNION PIN NUT AND PIN HAVE CORROSION IN THE THREADS.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CENTER E & E BAY LONGERON 50R AT BS 6-80 HAD CORROSION.

Part: STRAP — CORRODED (ZONE 600) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

RIGHT WING STRAP ON THE AFT SPAR IS CORRODED AT WING STATION 412 TO WING STATION 480

Part: ATTACH FITTING — WORN (RT WING TE FLAP) · airframe 69,214 hrs · 13,803 cycles

RIGHT OUTBOARD FLAP OUTBOARD ACTUATOR ATTACH POINT LUG BORES ARE WORN.

Part: DOOR SILL — CORRODED (CENTER CARGO) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CENTER CARGO DOOR SILL PLATE IS CORRODED AT THE AFT MOST DOOR LOCK.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,214 hrs · 13,803 cycles

MAIN CARGO DOOR LOCK ROLLER LOWER FITTING IS CRACKED FROM HOLES TO FASTENERS AT NR 7 LOCK ROLLER.

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CENTER E & E BAY CORROSION ON LONGERON 50R AT STATION 6-75.

Part: LONGERON — CORRODED (E/E BAY) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CENTER E & E BAY STATION 6-73.5 LONGERON 49R IS CORRODED

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CORROSION ON THE LEFT WING REAR SPAR STRAP AT XORS 446 TO 485

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

LEFT WING AFT SPAR UPPER IS CORRODED AT XORS 412 TO 420.

Part: FITTING — CRACKED (CARGO DOOR LOCK) · airframe 69,214 hrs · 13,803 cycles

MAIN CARGO DOOR LOCK ROLLER LOWER HATCH SPOOL BACKUP FITTING HAS EVIDENCE OF CRACKS FROM HOLES TO FASTENER NR 6 LOCK ROLLER

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

RIGHT WING UPPER SKIN IS CORRODED AT XORS 392 AT STRINGER 5R.

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

RIGHT WING AFT SPAR IS CORRODED AT XORS 480

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

RIGHT WING AFT SPAR UPPER CHORD IS CORRODED AT XORS -412 TO -418

Part: STRAP — CORRODED (RT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

RIGHT WING STRAP ON AFT SPAR RWS 412 TO 480 HAS CORROSION

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

LEFT WING REAR SPAR IS CORRODED AT XORS 981

Part: SEAT TRACK — CORRODED (BS 459-525) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CORROSION ON SEAT TRACK AT LAVATORY INBOARD FORWARD ATTACH POINT. BS 459 TO 525, LBL 56.

Part: INLET — CORRODED (NR 2 ENGINE) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

NR 2 ENGINE INLET DUCT PLATING IS CORRODED AT YID 279.443, ZID -44.00, XID 0.00 TO 9.5, POSITION 6 O'CLOCK.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

LEFT WING UPPER SKIN IS CORRODED AT XORS 446 STRINGER 6

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

RIGHT WING UPPER SKIN IS CORRODED AT XORS 455 TO 493 AT STRINGERS 6-9R

Part: FLOORBEAM — CORRODED (BS 457) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CORROSION ON TRANSVERSE FLOORBEAM AT BS 457 BL 0 TO RBL 12.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

RIGHT WING UPPER SKIN IS CORRODED AT XORS 899 AT THE AFT SPAR.

Part: FITTING — CRACKED (BS 1145) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CENTER E & E BAY SPLICE FITTING HAS CRACK INDICATIONS AT BS 1145 STRINGER 50R AND CORROSION

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

OUTBOARD SEAT TRACK AFT LAVATORY ATTACH POINT IS CORRODED

Part: SKIN — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

LEFT WING OUTBOARD FLAP PANEL UPPER SURFACE IS CORRODED AT THE AFT SPAR.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

LEFT WING UPPER SKIN IS CORRODED AT XORS 693.0 AT THE REAR SPAR.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

LEFT WING UPPER SKIN AND AFT SPAR UPPER CHORD ARE BOTH CORRODED AT XORS 1047

Part: SKIN — CORRODED (BS 1259) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CENTER SKIN IS CORRODED AT BS 1259, RBL 107, STRINGER 11R.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

LEFT WING UPPER SKIN IS CORRODED AT XORS 287.0 STRINGER 5.

Part: SEAT TRACK — CORRODED (BS 517) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CORROSION ON SEAT TRACK AT BS 517 AT RBL 55.

Part: SEAT TRACK — CORRODED (BS 505) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CORROSION ON SEAT TRACK AT BS 505 AT RBL 55.

Part: SKIN — CORRODED (BS 1210) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

BS 1210 RBL 5 STRINGER 17R HAS CORROSION ON THE SKIN.

Part: SKIN — CORRODED (BS 1227) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

BS 1227, LBL 108, STRINGER 15L SKIN HAS CORROSION

Part: SEAT TRACK — CORRODED (BS 522) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CORROSION ON SEAT TRACK AT BS 522 AT RBL 55.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

LEFT WING UPPER SKIN AND AFT SPAR UPPER CHORD CORRODED AT XORS 1047.

Part: SEAT TRACK — CORRODED (BS 459-525) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

SEAT TRACK CORRODED FROM BS 459 TO 525 AT LBL 56

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

LEFT WING UPPER SKIN IS CORRODED AT XORS 738.0 STRINGER 6.

Part: FLOORBEAM — CORRODED (BS 465) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CORROSION ON TRANSVERSE FLOORBEAM AT STATION 465 AS IT RUNS ACROSS THE FRONT OF THE LAV

Part: SEAT TRACK — CORRODED (BS 541) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CORROSION ON SEAT TRACK AT BS 541 AT RBL 55

Part: SKIN — CORRODED (BS 1227) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

BS 1227, RBL 60, STRINGER 15R SKIN HAS CORROSION.

Part: SKIN — CORRODED (BS 1264) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CORROSION ON THE SKIN AT BS 1264 AT LBL 107 STRINGER 10L.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

LEFT WING UPPER SKIN IS CORRODED AT XORS 243.0 STRINGER 10

Part: LONGERON — CORRODED (BS 1140) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CENTER E & E BAY LONGERON 51L AT BS 1140 HAS CORROSION

Part: DOOR SILL — CRACKED (CARGO DOOR) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

MAIN CARGO DOOR SILL PLATE NR 7 DOOR LOCK ROLLER BOLT HOLES HAVE EVIDENCE OF CORROSION AND CRACKS

Part: SKIN — CORRODED (BS 1224) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

BS 1224 LBL 70 STRINGER 15L SKIN HAS CORROSION

Part: SKIN — CORRODED (BS 1239) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CORROSION ON THE SKIN BS 1239, LBL 106, STRINGER 13L.

Part: PLATE — CORRODED (CARGO DOOR SILL) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

MAIN CARGO DOOR SILL PLATE NR 7 DOOR LOCK ROLLER HAS SEVERE CORROSION.

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 69,214 hrs · 13,803 cycles

CENTER FUSELAGE DOOR FRAME FORWARD UPPER CORNER INNER STRUCTURE HAS A TWO INCH CRACK JUST ABOVE THE MOST UPPER LIGHTING HOLE.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

RIGHT WING UPPER SKIN IS CORRODED AT XORS 553 TO 575 STRINGER 9 TO 11.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

LEFT WING UPPER SKIN IS CORRODED AT XORS 590.0 STRINGER 9.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

RIGHT WING UPPER SKIN IS CORRODED AT XORS 640.0 STRINGER 9.

Part: FLOORBEAM — CORRODED (BS 501) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CORROSION ON TRANSVERSE FLOORBEAM AT BS 501 UNDER THE LAVATORY HAS SEVERAL AREAS OF CORROSION THE ENTIRE LENGTH IT RUNS UNDER THE LAVATORY

Part: SKIN — CORRODED (BS 1250) · corrosion level 2 · airframe 69,214 hrs · 13,803 cycles

CORROSION ON SKIN AT BS 1250 AT LBL 107 STRINGER 12

Part: DOWNLOCK TARGET — OUT OF POSITION (LT MLG) · airframe 68,236 hrs · 13,516 cycles

DURING EXTENSION OF THE LG, UNSAFE INDICATION OF LT MAIN BOTH PRIMARY & ALTERNATE INDICATIONS. CYCLED GEAR, ALERTS REMAINED. PERFORMED ALTERNATE EXTENSION & ALERTS STILL REMAINED UNSAFE. VERIFIED GEAR VISUALLY & LANDED WITH LT MAIN GEAR STILL UNSAFE INDICATED. FOUND LEFT MLG PROXIMITY SENSOR TARGET OUT OF POSITION. SECURED TARGET & ADJUSTED TARGET IAW AMM 32-61-15. ALL INDICATIONS NORMAL. PERFORMED GEAR RTS TEST IAW AMM TASK 32-61-15 741-802. RTS NORMAL NO FAULTS NOTED OK FOR SERVICE.

Part: MANIFOLD — FAILED (BLEED AIR SYS) · airframe 67,979 hrs · 13,444 cycles

AT FL 350, NOTICED BURNING SMELL, FEW MINUTES LATER, LEVEL 3 AIR MANIFOLD 2 FAILED, FOLLOWED QRH & RETURNED.