N934AX

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 54,403 hrs · 48,858 cycles

EMERGENCY LIGHTS WILL ARM BUT WOULD NOT ILLUMINATE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY IAW DC9 MM 33-53-00-8.

Part: WINDOW — OUT OF ADJUST (COCKPIT) · airframe 54,322 hrs · 48,768 cycles

CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED CAPTAIN'S CLEARVIEW WINDOW IAW DC9 MM 56-10-03-5.

Part: LINKAGE — LACK OF LUBE (COCKPIT WINDOW) · airframe 53,558 hrs · 48,217 cycles

CAPTAIN'S SLIDING WINDOW (EMERGENCY EXIT) WOULD NOT OPEN. LUBED CAPTAIN'S SLIDING WINDOW LINKAGE AS REQUIRED. OPERATIONAL CHECK GOOD IAW MM 56-10-03-5-0002.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 53,511 hrs · 48,187 cycles

LEFT WHEEL WELL AFT CORNER ANGLE WAS CRACKED. REMOVED AND REPLACED MAIN FRAME AT FS 756 LEFT IAW DACO DC9 DWG 9919649.

Part: FRAME — CRACKED (BS 756) · airframe 53,511 hrs · 48,187 cycles

LEFT WHEEL WELL, LEFT AFT CORNER ANGLE WAS CRACKED. REMOVED AND REPLACED MAIN FRAME AT FS 756 LEFT IAW DACO DC9 DWG 9919649.

Part: ROD END — BROKEN (SLAT ACTUATOR) · airframe 52,929 hrs · 47,743 cycles

UPON SLAT EXTENSION, AIRCRAFT ROLLED TO THE RIGHT AND SLAT DISAGREEMENT LIGHT ILLUMINATED AND THE SLAT EXTEND LIGHT DID NOT ILLUMINATE AFTER RECYCLING SLATS, NORMAL INDICATIONS WERE OBTAINED. FOUND BROKEN ROD END ON LEFT WING INBOARD SLAT ACTUATOR. REMOVED AND REPLACED BROKEN SLAT ACTUATOR CYLINDER ASSEMBLY IAW DC9 MM. OPS CHECKED GOOD.

Part: CONTACT — WORN (COCKPIT) · airframe 52,134 hrs · 47,073 cycles

UPON LOWERING THE LANDING GEAR, NO NOSE GEAR SAFE LIGHT. TESTED IN BRIGHT AND DIM. AFTER INITIATING A GO-AROUND, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED (APPROXIMATELY 30 SECONDS). FOUND BULB CONTACTS TO BE WORN. RELAMPED, OPS CHECKED GOOD.

Part: WINDOW — STUCK (COCKPIT) · airframe 51,938 hrs · 46,913 cycles

CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. OPENED WINDOW AND APPLIED LUBRICANT TO WINDOW MECHANISM, WINDOW OPERATES NORMAL.

Part: BEARING — CRACKED (HORIZONTAL STAB) · airframe 51,932 hrs · 46,908 cycles

RIGHT HORIZONTAL STAB PIVOT BEARING FOUND CRACKED IN HALF. REPLACED BEARING ON NR 0131 IAW DC-9 SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,932 hrs · 46,908 cycles

RIGHT FORWARD MAIN FRAME FS 699 CRACKED AT FORWARD FLANGE POINTS F & E AND AFT FLANGE POINTS H & I. REMOVED AND REPLACED FRAME AT STA 699 IAW EA 53400322-001-3.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,932 hrs · 46,908 cycles

MAIN ENTRY DOOR UPPER AFT STOP HAD CRACKED SURFACE SKIN. REPAIRED MAIN ENTRY DOOR UPPER AFT CORNER IAW JOB CARD EA 53100126-001, SERVICE REPAIR DRAWING SR09530252-7001 AND DC-9 SRM 53-05.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,932 hrs · 46,908 cycles

LOWER AFT CORNER OF FORWARD LOWER CARGO DOOR CUTOUT HAD 2 EACH CRACKS. REPAIRED IAW DC-9 SRM 53-05 AND REA D953-51052MR.

Part: SKIN PANEL — CRACKED (AFT FUSELAGE) · airframe 51,932 hrs · 46,908 cycles

TWO CRACKS IN FUSELAGE SKIN FS 1143, APPROXIMATELY LONGERON 14 RIGHT. REPAIRED FUSELAGE SKIN IAW DC-9 SRM 53-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,932 hrs · 46,908 cycles

AFT ASSY CANTED FRAME 1121 CRACKED BETWEEN LONGERON 16 LEFT AND LONGERON 17 LEFT. REPAIRED IAW DC-9 SSRM K05159.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 51,932 hrs · 46,908 cycles

LONGERON 30 CRACKED FORWARD AND AFT AT SPLICE FS 380. REMOVED AND REPLACED LONGERON 30 FROM STA 355 TO 415.

Part: FRAME — CRACKED (FUSELAGE) · airframe 51,932 hrs · 46,908 cycles

FRAME CRACKED FS 357 AT LONGERON 30. REPAIRED FRAME STA 357 AT LONGERON 30 IAW DC-9 SRM 53-03.

Part: SWITCH — MALFUNCTIONED (NLG) · airframe 51,351 hrs · 46,402 cycles

AFTER GEAR HANDLE SELECTED DOWN, NOSE GEAR LIGHT DID NOT ILLUMINATE. RECYCLED GEAR WITH SAME RESULT. CHECKED GEAR DOWN VISUAL (PEEP HOLE) AND NOSE LIGHT ILLUMINATED AT 500 FT AGL ON FINAL. FOUND WIRING HARNESS KINKED BEHIND DOWNLOCK SWITCH CANNON PLUG. RE-ROUTED HARNESS TO PROVIDE CLEARANCE. NO DEFECTS ON WIRES OR PLUG. REPLACED DOWNLOCK SWITCH AS PRECAUTION.

Part: SKIN — DELAMINATED (RT WING SPOILER) · airframe 50,597 hrs · 45,765 cycles

LARGE AREA OF DELAMINATION ON UPPER AND LOWER SURFACE OF THE RIGHT WING INBOARD SPOILER PANEL. REPLACED SPOILER IAW DC-9 MM 27-61-01-4-0001.

Part: OUTFLOW VALVE — LACK OF LUBE (CABIN PRESSURE) · airframe 50,403 hrs · 45,610 cycles

AIRCRAFT WOULD NOT AUTO PRESSURIZE ON CLIMBOUT. MANUAL PRESSURIZATION ATTEMPTED, BUT OUTFLOW CONTROL WHEEL WOULD NOT MOVE. INSPECTED AND CLEANED OUTFLOW VALVE AS REQUIRED. NO DEFECTS NOTED. REMOVED CIRCUIT BREAKER COLLARS FROM CABIN PRESS CONTROL. OPS CHECKED GOOD. CLEANED VALVE AND LUBRICATED IAW DC-9 AMM 21-32-05 AND INSPECTED, OPS CHECKED IAW DC-9 AMM 21-32-00.

Part: ACTUATOR — FAILED (RUDDER CONTROL) · airframe 50,203 hrs · 45,447 cycles

RUDDER PEDALS WERE STIFF DURING CONTROL CHECK, ON CLIMB OUT OF ICT. CLIMBING TO FL 350, AIRCRAFT STARTED TO YAW AND DUTCH ROLL. DISCONNECTED AUTO PILOT. TURNING OFF YAW DAMPER AND GOING TO MANUAL RUDDER DID NOT STOP YAW/DUTCH ROLL. AIRCRAFT SLOWED AND DESCENDED TO 280 FOR REMAINDER OF FLIGHT. FOUND RUDDER POWER CONTROL ACTUATOR ASSEMBLY BY-PASSING HYDRAULIC FLUID. REPLACED THE CONTROL ACTUATOR ASSEMBLY IAW DC-9 AMM 27-20-06-4-0002.

Part: CONTROL CABLE — BROKEN (NLG) · airframe 50,090 hrs · 45,359 cycles

ON INITIAL CLIMB OUT, EXCESSIVE NOISE AND VIBRATION IN VICINITY OF NOSE GEAR. WHEN GEAR LOWERED, NOISE, VIBRATION STOPPED. FOUND RIGHT FORWARD NOSE GEAR DOOR OPEN, AND DOOR STOP CABLE BROKEN. REPLACED LEFT AND RIGHT NOSE GEAR DOOR STOP CABLES IAW DC-9 MM 32-22-01-2-0004. OPS CHECKED GOOD.

Part: FITTING — CORRODED (LEFT WING) · airframe 49,340 hrs · 44,654 cycles

LEFT SLANT PANEL, OUTBOARD ATTACH FITTING WAS CORRODED. REPLACED FITTING IAW DC-9 SRM 51-30-5.

Part: PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 49,340 hrs · 44,654 cycles

LEFT SLANT PANEL WAS CORRODED AROUND THE LOWER NUTPLATES. LEVEL II CORROSION. INSTALLED NEW SLANT PANEL IAW DC-9 SRM 51-30-1.

Part: PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 49,340 hrs · 44,654 cycles

RIGHT SLANT PANEL WAS CORRODED AROUND NUTPLATES ON THE LOWER EDGE OF PANEL. LEVEL II CORROSION. INSTALLED NEW SLANT PANEL IAW DC-9 SRM.

Part: BATTERY PACK — DISCHARGED (COCKPIT) · airframe 49,239 hrs · 44,571 cycles

COCKPIT EMERGENCY LIGHTING WAS FOUND TO BE INOPERATIVE AT RFD. MAINTENANCE INSPECTED AND RE-SEATED THE EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. IN ILN AS A PRECAUTION, MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW DC-9 MM 33-5-02.

Part: SWITCH — INTERMITTENT (COCKPIT) · airframe 49,101 hrs · 44,461 cycles

THE EMERGENCY EVACUATION LIGHT SWITCH WAS REPORTED AS INTERMITTENT. MAINTENANCE INSPECTED AND REPLACED THE COCKPIT EMERGENCY LIGHT CONTROL SWITCH, AND RELAMPED THE EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 48,472 hrs · 44,043 cycles

DURING PRE-DEPARTURE CHECK, NOTED COCKPIT EMERGENCY LIGHTS INOP. REPLACED COCKPIT EMERGENCY LIGHT BATTERIES IAW DC9 MM 33-51-0-2. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,447 hrs · 44,021 cycles

DURING PREFLIGHT INSPECTION, FOUND THE EMERGENCY LIGHTS INOPERATIVE. RESECURED WIRING TO OVERHEAD LIGHT SOCKET.

Part: BATTERY — DISCHARGED (CABIN)

DURING COCKPIT CHECK, EMERGENCY EVAC LIGHT FOUND NOT WORKING WHEN SWITCH WAS IN THE ON POSITION. REPLACED EMERGENCY LIGHT BATTERY SUPPLY IAW DC9 SMM 33-53-00. OPS CHECKED GOOD.

Part: PANEL — CRACKED (SPOILER)

DURING C-CHECK, FOUND THE LEFT INBOARD SPOILER CRACKED AT THE UPPER SURFACE CUT-OUT. REPLACED SPOILER PANEL IAW DC9 SMM 27-61-01..

Part: WEB — CORRODED (BULKHEAD)

DURING C-CHECK, FOUND THE AFT LOWER CARGO COMPARTMENT AFT BULKHEAD WEB EXFOLIATED AND RIVET HEADS POPPED JUST ABOVE LONGERON 30 ON BOTH SIDES OF BULKHEAD CENTER SUPPORT. REPLACED WEB IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FITTING — CRACKED (BS 579)

DURING C-CHECK, FOUND THE FLOORBEAM FITTING AT STATION 579 JUST BELOW CUSP WEB RIGHT SIDE CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: WEB — CORRODED (BS 579)

DURING C-CHECK, FOUND THE CUSP WEB CORRODED AND CRACKED AT STATION 579 ON RIGHT SIDE. REPLACED CUSP WEB IAW DC9 SRM 53-01.

Part: FLOORBEAM — CORRODED (BS 996)

DURING C-CHECK, FOUND THE FLOORBEAM AT STATION 996 CORRODED AT THE RIGHT OUTBOARD END. REPAIRED IAW ABX REA D95334863 MR.

Part: FLOORBEAM — CORRODED (BS 965)

DURING C-CHECK, FOUND FLOORBEAM AT STATION 965 AND RBL 8 CORRODED. REPAIRED FLOORBEAM IAW ABX REA D95334885 MR.

Part: SPAR — CORRODED (CENTER WING)

DURING C-CHECK, FOUND THE FORWARD SIDE OF THE LOWER T-CAP OF THE FRONT SPAR CORRODED AT LBL 5 TO RBL 12 (CENTER WING). REPLACED FINGER DOUBLER IAW DC9 SRM 51-30-2.

Part: FRAME — CRACKED (BS 579)

DURING C-CHECK, FOUND THE FUSELAGE FRAME FOOT FITTING AT STATION 579 RIGHT CRACKED AT BOLT HOLE. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: SWITCH — INTERMITTENT (NLG)

FIRST ATTEMPT ON FINAL, NO NOSE GEAR DOWN AND LOCKED GREEN LIGHT. RECYCLED GEAR OBTAINED ALL THREE GEAR GREEN LIGHTS. REPLACED NOSE GEAR DOWNLOCK POSITION SWITCH.

Part: FLOORBEAM — CORRODED (BS 370-427)

DURING C-CHECK, FOUND LONGITUDINAL FLOORBEAM EXFOLIATED AT STATION 370-371 AND 426-427, RBL 42 ABOVE THE FLC DOOR CUTOUT. REPLACED FLOORBEAM IAW DC9 SRM 51-30-1 AND 51-30-2.

Part: FITTING — CRACKED (PAX DOORWAY)

DURING C-CHECK, FOUND FITTING CRACKED IN AFT ENTRY DOOR, RIGHT JAMB, FWD SIDE, 36 ABOVE FLOOR LINE. REPLACED FITTING IAW DC9 SRM 51-30-22 AND 51-30-5.

Part: SHEAR TIE — CRACKED (BS 945)

DURING C-CHECK, FOUND SHEAR-TIE CRACKED AT STATION 945 BELOW LONGERONS 14L AND 15L. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: LATCH — FAILED (COCKPIT DOOR)

COCKPIT DOOR LATCH INOPERATIVE FROM CABIN SIDE. REPAIRED COCKPIT DOOR LATCH AS NECESSARY.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY BATTERIES, OPS CHECKED IAW DC9 MM 33-53-0.

Part: BEAM — CRACKED (DOOR)

FOUNR FWD SERVICE DOOR LOWER BEAM CRACKED AND SECOND BEAM FROM BOTTOM CRACKED. REPAIRED LOWER BEAM (P/N 9911582-3) AND SECOND BEAM (P/N 9911581-3) IAW DC9 SRM 52-05.

Part: FLOORBEAM — DAMAGED (BS 917)

DURING C-CHECK, THE AFT FLANGE OF THE FLOORBEAM AT STA 917 WAS FOUND TO BE GOUGED AND WORN. REPAIRED IAW REA D953-16470-MR.

Part: INTERCOSTAL — CRACKED (BS 897-889)

DURING C-CHECK, AN INTERCOSTAL WAS FOUND CRACKED BETWEEN STATION 897 TO 889 LONGERONS 30 AND 29 RIGHT. REPLACED IAW DC-9 SRM 53-30-2.

Part: SKIN — DAMAGED (BS 975)

DURING C-CHECK, AN EXISTING CLASS TWO REPAIR WAS REMOVED FROM THE FUSELAGE SKIN AT STA 975 LONG 20 AND 21 RIGHT. REPAIRED IAW REA D953-16442-MR.

Part: TAB — DELAMINATED (ELEVATOR)

DURING C-CHECK, AN ELEVATOR CONTROL TAB WAS FOUND DELAMINATED. REPLACED IAW DC-9 MM 27-30-3.

Part: ENGINE MOUNT — CORRODED (RT ENGINE)

DURING C-CHECK, THE RIGHT HAND FORWARD ENGINE MOUNTS, BEAVERTAIL, WERE FOUND TO BE CORRODED. REPAIRED IAW REA D953-16454-MR.

Part: FITTING — CORRODED (FUSELAGE)

DURING C-CHECK, AN END FITTING WAS FOUND TO BE ELONGATED AND CORRODED. REPAIRED IAW REA D953-16455-MR.

Part: FRAME — CORRODED (FUSELAGE)

DURING C-CHECK, CORROSION WAS FOUND ON FUSELAGE FRAME 351 UPPER CAP AT LONGERON 24 LEFT. REPAIRED IAW REA D953-16412-MR.

Part: TAB — DELAMINATED (LT AILERON)

DURING C-CHECK, AN AILERON TRIM TAB WAS FOUND DELAMINATED. REPLACED IAW DC-9 MM 27-10-5.

Part: TAB — DELAMINATED (LT ELEVATOR)

THE LEFT ELEVATOR TAB WAS DELAMINATED ON THE INBOARD TRAILING EDGE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.

Part: TAB — DENTED (RUDDER)

THE RUDDER TAB HAD 2 LARGE DENTS TO THE OUTER SURFACE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.

Part: LIGHT SOCKET — DEFECTIVE (RT MLG)

ON GEAR UPLATCH CHECK, RIGHT LANDING GEAR GREEN LIGHT CAME ON BRIGHT. GEAR RECYCLING WAS NORMAL EXCEPT LIGHT STAYED ON BRIGHT ALL THROUGH RECYCLING. REPLACED THE RIGHT MAIN LANDING GEAR DOWN LIGHT SOCKET.

Part: HINGE — WORN (LT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07, ASB 32-244 R2, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR ARTICULATING DOOR HINGE WORN. REPLACED HINGE IAW DC-9 SRM 51-30-2.

Part: HINGE — WORN (LT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07, ASB 32-244 R2, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGE WORN. REBUSHED HINGE IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: BUSHING — WORN (RT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07, ASB 32-244 R2, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR HINGE WORN. REBUSHED HINGE HALF IAW DC-9 OVERHAUL MANUAL 32-10-16.

Part: HYD LINE — BROKEN (RT MLG WW)

RIGHT HYDRAULIC SYSTEM FLUID LOSS FAILURE ON CLIMBOUT. CREW PERFORMED ABNORMALS AND CAME TO A FULL STOP ON RUNWAY. MAINTENANCE SECURED THE GEAR AND STOWED MLG DOORS PRIOR TO TAXI. FOUND ALTERNATE PUMP HYDRAULIC LINE BROKEN IN THE RIGHT WHEEL WELL, REPLACED WITH FLEX LINE AND DEFERRED. ALSO, FOUND GEAR PRESSURE RETURN LINE (7912697-932) IN LEFT WHEEL WELL RUPTURED, REPLACED LINE. REPLACED RIGHT MLG INBD DOOR, BOTH RETURN FILTERS, NR 2 ENGINE DRIVEN HYDRAULIC PUMP AND CASE DRAIN FILTER, LEAK CHECKED AND SERVICED IAW DC9 MM.

Part: DNLOCK SWITCH — DEFECTIVE (NLG)

DURING APPROACH WHEN LANDING GEAR HANDLE WAS PLACED DOWN, NO GREEN NOSE GEAR DOWN LIGHT ILLUMINATED. RECYCLED GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. REPLACED NOSE GEAR DOWNLOCK AND UPLIMIT SWITCHES PER DC-9 M.M.

Part: ENGINE — FAILED (LEFT)

ON TAKEOFF ROLL, HEARD A LOUD EXPLOSION, FOLLOWED BY A VIBRATION AND A LOSS OF POWER ON THE LEFT ENGINE. EGT REACHED 680 DEGREES. REPLACED THE NR 1 ENGINE IAW ABX JOB CARD J7001. OPS CHECKED GOOD, NO LEAKS NOTED AT THIS TIME.

Part: DOUBLER — CRACKED (BS 130)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 90-18-03; S.B. 56-11, REV. 3, FOUND SMALL CRACKS AROUND FASTENERS ON DOUBLER. REPLACED DOUBLER IAW DC-9 SRM 51-30-2 AND 51-30-1.

Part: SKIN — DENTED (BS 209)

DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED AT LONGERON 19R AT STA 207. REPAIRED IAW ABX REA D953-11089-MR.

Part: FRAME — DAMAGED (BS 756)

DURING C-CHECK INSPECTION, FOUND DRILL HOLE IN FUSELAGE FRAME STA 756 BETWEEN LONGERONS 7L AND 8L. REPAIRED IAW ABX REA D953-11085-MR.

Part: INTERCOSTAL — CORRODED (BS 415)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 94-03-01, FOUND CORROSION ON UPPER DOOR JAMB AT AFT CORNER. REMOVED CORROSION, TREATED AND PRIMED AREA IAW DC-9 SRM 51-10-3.

Part: FRAME — CRACKED (BS 699)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 78-07-05, S.B. 53-131 FOUND FRAME STA 699 RIGHT, CRACKED ON THE FORWARD LOWER FLANGE. CRACK IS WITHIN LIMITS OF DC-9 S.B. 53-131.

Part: BLKHD JAMB — CRACKED (BS 996)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 85-01-02, S.B. 53-137 FOUND THE AFT PRESSURE BULKHEAD UPPER DOOR JAMB LEFT AND RIGHT CORNERS HAVE BEND RADIUS CRACKS IN THE FORWARD FLANGE WHICH EXTEND BEYOND THE STOP DRILLS. REPAIRS ARE ACCEPTABLE AS IS PER SERVICE REWORK DRAWING J060097, GENERAL NOTE NR 28. CRACKS UNDER REPAIR ANGLE ARE STILL ACCEPTABLE PER GENERAL NOTE NR 34 OF SERVICE REWORK DRAWING J060097.

Part: SPAR CAP — CORRODED (XRS 563)

DURING C-CHECK INSPECTION, FOUND RIGHT WING REAR SPAR LOWER T-CAP HAD LEVEL II CORROSION AT WING TIP. REPAIRED IAW ABX REA D957-11076-MR.