N615AM

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,430 hrs · 26,114 cycles

13ABC BULL NOSE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR BULL NOSE EMERGENCY LIGHT. OPERATION CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 74,430 hrs · 26,114 cycles

LT NR 2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 2 DOOR EXTERIOR LIGHT. OPERATION CHECKED NORMAL.

Part: LENS — MISSING (EXTERIOR) · airframe 74,430 hrs · 26,114 cycles

LT NR 4 DOOR EXTERIOR EMERGENCY LIGHT LENS MISSING. REPLACED LT EXTERIOR LIGHT LENS. OPERATION CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 74,430 hrs · 26,114 cycles

LT 4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT EXTERIOR LIGHT. OPERATION CHECKED NORMAL.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 70,541 hrs · 24,697 cycles

EMERGENCY LIGHT BATTERY PACK M10798 CONNECTOR DAMAGED. REPLACED CONNECTOR, OPS CHECK NORMAL.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 70,541 hrs · 24,697 cycles

EMERGENCY LIGHTS AT LEFT AND RIGHT NUMBER 1 DOORS, LOWER END OF WALL BETWEEN FORWARD GALLEY AND FIRST CLASS SEATS, AND SEAT MOUNTED LIGHTS IN FIRST CLASS DID NOT TEST. REPLACED CONNECTOR, OPS CHECK NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,984 hrs · 24,491 cycles

UPPER FUSELAGE DAMAGED AT STATION 600 AND STRINGER 2 LEFT. INSTALLED DOUBLER PER EA B757-53-022291.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,984 hrs · 24,491 cycles

LIGHTNING STRIKE TO STATIONS 1140 TO 1160 AND STRINGERS 6 TO 7 RIGHT. INSTALLED DOUBLER PER SRM 53-00-01-2R.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,984 hrs · 24,491 cycles

LIGHTNING STRIKES TO FUSELAGE SKIN STATIONS 1380 TO 1400 AND BETWEEN STRINGERS 6 AND 7 RIGHT. INSTALLED DOUBLER PER SRM 53-00-01-2R AND EA 757-53-022347.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,795 hrs · 23,682 cycles

T-FITTING CORRODED AT STATION 1720 RIGHT BODY LINE 60, WATER LINE 208.1. INSTALLED T-FITTING, BATHTUB FITTINGS AND FASTENERS PER AARD 51-10-05-1.

Part: PLACARD — MISSING (CABIN) · airframe 66,968 hrs · 23,383 cycles

LEFT OVERWING SIDEWALL ARROW AT FORWARD POSITION MISSING. INSTALLED LEFT OVERWING ARROW AT FORWARD POSITION.

Part: PLACARD — MISSING (CABIN) · airframe 66,968 hrs · 23,383 cycles

LEFT OVERWING SIDEWALL ARROW AT AFT POSITION MISSING. INSTALLED LEFT OVERWING ARROW AT AFT POSITION. OPS CHECK NORMAL.

Part: PLACARD — MISSING (CABIN) · airframe 66,968 hrs · 23,383 cycles

RIGHT OVERWING SIDEWALL ARROW AT AFT POSITION MISSING. INSTALLED RIGHT OVERWING ARROW AT AFT POSITION. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 66,461 hrs · 23,191 cycles

LEFT NUMBER 4 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 4 DOOR EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: SUPPORT — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 65,968 hrs · 23,022 cycles

FORWARD CARGO DOOR LOWER TEE SUPPORT CORRODED. REPLACED TEE SUPPORT PER SRM 51-10-02-0G.

Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 65,968 hrs · 23,022 cycles

FORWARD CARGO DOOR 6TH FROM FORWARD WEB CORRODED. REPLACED WEB PER SRM 51-10-02-0G.

Part: BEAM — DAMAGED (CARGO DOOR) · airframe 65,968 hrs · 23,022 cycles

FORWARD CARGO DOOR LOWER EDGE SEAL DAMAGED. LOWER SEAL EDGE BEAM REPLACED PER SRM 51-10-02-0G.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 65,968 hrs · 23,022 cycles

AFT CARGO DOOR UPPER FORWARD DOOR STOP CUTOUT CRACKED. REPLACED DOOR STOP PER SRM 51-10-02-0G.

Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 65,968 hrs · 23,022 cycles

FORWARD CARGO DOOR 6TH FROM LOWER WEB CORRODED. INSTALLED NEW WEB PER SRM 51-10-02-0G.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 65,968 hrs · 23,022 cycles

STOP FITTING CRACKED AFT CARGO DOOR. REPLACED STOP FITTING PER SRM 51-10-02-0G.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,968 hrs · 23,022 cycles

FUSELAGE SKIN HAS HEAVY CORROSION AT SKIN LAP JUST ABOVE LEFT HAND AUXILIARY POWER UNIT DOOR STATION 1885.20. INSTALLED DOUBLER PER SRM 51-70-13-OG AND EA B757-53-013305.

Part: STRAP — CRACKED (FUSELAGE) · airframe 65,968 hrs · 23,022 cycles

FLOORBEAM STABILIZER STRAP CRACKED AT STATION 397.7 LEFT BUTTLINE 24. INSTALLED DOUBLER TO FLOORBEAM STABILIZER STRAP PER AARD 53-30-51-1.

Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 65,968 hrs · 23,022 cycles

FORWARD CARGO DOOR 5TH FROM FORWARD LOWER WEB CORRODED. INSTALLED NUMBER 5 WEB AND ANGLE PER SRM 51-10-02-0G.

Part: SUPPORT — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 65,968 hrs · 23,022 cycles

LOWER SUPPORT TEE CORRODED. REPLACED TEE PER SRM 51-10-02-0G.

Part: FLANGE — CORRODED (APU BAY) · corrosion level 2 · airframe 65,968 hrs · 23,022 cycles

CORROSION ON FORWARD FLANGE OF AXILIARY POWER UNIT INLET BOX FRAME. INSTALLED NEW FORWARD FLANGE.

Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 65,968 hrs · 23,022 cycles

FORWARD CARGO DOOR 4TH FROM FORWARD LOWER WEB CORRODED. INSTALLED NUMBER 4 WEB AND ANGLE PER SRM 51-10-02-0G.

Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 65,968 hrs · 23,022 cycles

FORWARD CARGO DOOR 3RD FROM FORWARD LOWER WEB CORRODED. INSTALLED NUMBER 3 WEB AND ANGLE PER SRM 51-10-02-0G.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,968 hrs · 23,022 cycles

CORROSION ON LOWER MOUNTING ANGLE FOR AUXULIARY POWER UNIT INLET DOOR ASSEMBLY. INSTALLED NEW ANGLE PER SRM 51-70-00-06.

Part: FLANGE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,968 hrs · 23,022 cycles

AFT MOUNTING FLANGE FOR AUXILIARY POWER UNIT INLET DOOR ASSEMBLY HAS CORROSION AROUND ATTACH FASTENER HOLES ON UPPER SURFACE AT STATION 1825. INSTALLED REPAIR DOUBLER PER EA B757-53-013232 AND BOEING DRAWING LOR5L53011.

Part: FLANGE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,968 hrs · 23,022 cycles

AFT MOUNTING FLANGE FOR AUXILIARY POWER UNIT INLET DOOR ASSEMBLY HAS CORROSION AROUND ATTACH FASTENER HOLES ON LOWER SURFACE AT STATION 1825. INSTALLED REPAIR PER BOEING DRAWING LOR5L53011 AND EA B757-53-013232.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 65,968 hrs · 23,022 cycles

CRACK BETWEEN UPPER BEAM CORD AND BEAM WEB OF THE EXTRUSION AT FLOOR BEAMS STATIONS 660 TO 700. FLANGE STATION 660 REPAIRED PER AARD 53-30-51-02 AND SRM 53-00-51-2R REPAIR 3. FLANGE STATION 700 FLOORBEAM REPAIRED PER SECTION 12 PATTERN CARD 53-98-01. MINOR DEVIATIONS TO REPAIR GUIDE LINES PER B757 SRM 53-00-51-2 R 3, AND AARD B 757 53-30-51-2, PROVIDED BY EA B757 53-013218.

Part: SUPPORT — SHEARED (WING FAIRING) · airframe 65,385 hrs · 22,802 cycles

VVI - CREW REPORTED AIRFRAME VIBRATIONS ORIGINATING FROM AFT FUSELAGE. EMERGENCY DECLARED FLIGHT RETURNED VVI LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND WING FAIRING INBOARD OF NUMBER 8 SPOILER WITH TWO HOLD DOWN SUPPORT RODS SHEARED OFF. REPLACED SUPPORT RODS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — MISSING (CABIN) · airframe 64,719 hrs · 22,592 cycles

LEFT NUMBER 4 DOOR AFT EXIT LIGHT LENS MISSING. REPLACED LENS FOR LEFT NUMBER 4 AFT DOOR EXIT LIGHT. OPS CHECKED NORMAL.

Part: PLACARD — DAMAGED (CABIN) · airframe 64,719 hrs · 22,592 cycles

RIGHT FRONT OVERWING EXIT PLACARD DAMAGED. INSTALLED SERVICEABLE EXIT PLACARD. OPS CHECKED NORMAL.

Part: PLACARD — DAMAGED (CABIN) · airframe 64,719 hrs · 22,592 cycles

LEFT NUMBER 4 DOOR FORWARD EXIT PLACARD DAMAGED. INSTALLED SERVICEABLE EXIT PLACARD. OPS CHECKED NORMAL.

Part: PLACARD — DAMAGED (CABIN) · airframe 64,719 hrs · 22,592 cycles

RIGHT AFT OVERWING EXIT PLACARD DAMAGED. INSTALLED SERVICEABLE EXIT PLACARD. OPS CHECKED NORMAL.

Part: LENS — LOOSE (CABIN) · airframe 64,719 hrs · 22,592 cycles

RIGHT NUMBER 2 DOOR AFT EXIT LIGHT LENS LOOSE. REPLACED LENS FOR RIGHT NUMBER 2 DOOR AFT EXIT LIGHT. OPS CHECKED NORMAL.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 63,899 hrs · 22,290 cycles

EMERGENCY LIGHT AT SEAT 13DEF INOPERATIVE. RESEATED EMERGENCY LIGHT CONNECTOR.

Part: GOVERNOR — FAILED (LT ENGINE) · airframe 63,090 hrs · 22,018 cycles

LEFT ENGINE FAILED AT 1500 FEET ON FINAL APPROACH. ENGINE FLAMED OUT. DID RESTART BUT ENGINE GAS TEMPERATURE WAS CLIMBING, SO ELECTED TO SHUT DOWN ENGINE. LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME LESS THAN ONE MINUTE. REPLACED FUEL FLOW GOVERNOR.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 62,307 hrs · 21,761 cycles

FLOORBEAM CRACKED REPAIRED IAW EA B757-53-005762 DATED 26 MAR 09.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,307 hrs · 21,761 cycles

FLOORBEAM CRACKED. REPAIRED IAW EA B757-53-005762 DATED 26 MAR 09.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,310 hrs · 21,762 cycles

FLOORBEAM CRACKED. REPAIRED IAW EA B757-53-005762.

Part: PRESSURE PANEL — CORRODED (MLG WW) · corrosion level 2 · airframe 62,307 hrs · 21,761 cycles

WHEEL WELL PRESSURE DECK CORRODED. REPAIRED IAW EA B757-53-005785 DATED 03/25/09 SRM 53-40-14B01.

Part: PRESSURE PANEL — CORRODED (MLG WW) · corrosion level 2 · airframe 62,320 hrs · 21,766 cycles

WHEEL WELL PRESSURE DECK CORRODED. REPAIRED IAW SRM 53-40-14 BD1, EA B757-53-005785 ESO 26-534014-5579.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,315 hrs · 21,403 cycles

INTERCOSTAL CRACKED. REPAIRED IAW SRM 53-00-51.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 61,315 hrs · 21,408 cycles

VERTICAL STIFFENER CRACKED. REPAIRED IAW SRM 53-00-51.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 61,315 hrs · 21,408 cycles

LEFT WING REAR SPAR CORRODED. REPAIRED IAW EA B757-57-005721.

Part: PLACARD — DAMAGED (CABIN)

DFW EMERGENCY LIGHT ARROW IDENTIFIER AT LT NR 2 EXIT NOT READABLE. REPLACED PLACARD FOR EMERGENCY LIGHT ARROW IDENTIFIER AT LT NR 2 EXIT. SYSTEM GROUND CHECKED NORMAL OPS.

Part: PLACARD — DAMAGED (CABIN)

DFW EMERGENCY LIGHT PLACARD AT LT AFT OVERWING EXIT SIGN COMING OFF. REPLACED PLACARD FOR EMERGENCY LIGHT AT LT AFT OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPS.

Part: PLACARD — DAMAGED (CABIN)

DFW EMERGENCY LIGHT PLACARD AT LT FORWARD OVERWING EXIT SIGN COMING OFF. REPLACED PLACARD FOR EMERGENCY LIGHT AT LT FORWARD OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LENS — LOOSE (CABIN)

DFW EMERGENCY LIGHT LENS AT OVERHEAD SEAT 17A LOOSE. SECURED LENS FOR EMERGENCY LIGHT AT OVERHEAD SEAT 17A. SYSTEM GROUND CHECKED NORMAL OPS.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,315 hrs · 21,408 cycles

INTERCOSTAL CORRODED. REPAIRED IAW SRM53-60-51-01 1.

Part: PRESSURE PANEL — CORRODED (MLG WW) · airframe 61,315 hrs · 21,408 cycles

WHEEL WELL PRESSURE DECK CORRODED. REPAIRED IAW SRM 53-40-14 BD1 EA B757-53-005785 ESO 26-534014-5579.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAS - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. FOUND LEFT NUMBER ONE DOOR FLIGHT ATTENDANT EMERGENCY LIGHT CONSOLE SWITCH LEFT ON. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

LAS - EMERGENCY LIGHTS AT AFT COACH CABIN INOPERATIVE. FOUND LEFT NUMBER ONE DOOR FLIGHT ATTENDANT EMERGENCY LIGHT CONSOLE SWITCH LEFT ON. REPLACED BATTERY PACK AT AFT SEAT ROW 32 FOR EMERGENCY LIGHTS AT AFT COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAS - EMERGENCY LIGHTS AT MID COACH CLASS CABIN INOPERATIVE. FOUND LEFT NUMBER ONE DOOR FLIGHT ATTENDANT EMERGENCY LIGHT CONSOLE SWITCH LEFT ON. REPLACED BATTERY PACK AT AFT SEAT ROW 19 FOR EMERGENCY LIGHTS AT MID COACH CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAS EMERGENCY LIGHTS AT FORWARD COACH CLASS CABIN INOPERATIVE. FOUND LEFT NUMBER ONE DOOR FLIGHT ATTENDANT EMERGENCY LIGHT CONSOLE SWITCH LEFT ON. REPLACED BATTERY PACK AT FORWARD SEAT ROW 9 FOR EMERGENCY LIGHTS AT FORWARD COACH CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ENGINE — FAILED (LEFT)

SJU - AT 1000 FEET LEFT ENGINE LIMITER FAILED APPROXIMATELY 700 TO 600 FEET LEFT ENGINE FAILED. LEFT OIL PRESSURE IN RED. SHUT ENGINE OFF. LANDED WITHOUT INCIDENT. REPLACED TRANSIENT PRESSURE UNIT, BLEED VALVE CONTROL UNIT, AND GENERATOR CONTROL UNIT AND REPLACED BOTH OIL FILTERS FOR LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SPRING — OUT OF ADJUST (GIRT BAR)

DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, FOUR GIRT BAR SPRINGS OUT OF ADJUSTMENT AND TWO NEEDING REPLACED. ADJUSTED FOUR GIRT BAR SPRINGS AND REPLACED TWO. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTROL PANEL — DEFECTIVE (COCKPIT)

KIN - FLT 924 - EN ROUTE MDE-MIA, UNCOMMANDED CLIMB OF CABIN BY BOTH AUTO CONTROLLERS. CABIN ALTITUDE ALERT SOUNDED AND EMERGENCY DESCENT INITIATED AND OXYGEN MASKS DEPLOYED. LANDED AT KIN WITHOUT FURTHER INCIDENT. FOUND OVERHEAD CABIN PRESSURE SELECTOR PANEL INOPERATIVE. REPLACED PANEL AND NR 1 CABIN PRESSURE CONTROLLER. PERFORMED PRESSURIZATION CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: INSULATION — BURNED (CABIN)

TUL - INSULATIONS SHOWS EVIDENCE OF BEING BURNED AT 860 STRINGER 29R AND AT 880 STRINGER 29R. INSPECT THE AREA FOUND NO STRUCTURAL HEAT DAMAGE. MODIFIED AND SECURED INSULATION BLANKET TO PROVIDE CLEARANCE BETWEEN HEAT SOURCE AND BLANKET, OK FOR CONTINUED SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

TUL - FOUND TOP OF FRAME 1640 FROM LEFT SIDE TO RIGHT HAS NUMEROUS AREAS OF HEAVY CORROSION UNDER NUT CLIPS. INSTALLED FABRICATED FLOORBEAM CAP AND ASSOCIATED PARTS PER SRM 51-10-010. (M)

Part: CONTACTOR — DIRTY (EMERGENCY EXIT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT LEFT WING SLIDE INOPERATIVE. CLEANED EMERGENCY EXIT CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR TRACK LIGHT AT SEAT 6E INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR TRACK LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PANEL — FAILED (COCKPIT)

CUN - FLT 2112 - AFTER TAKEOFF, CREW REPORTED SMOKE FROM ANTI-COLLISION PANEL. RETURNED AND LANDED CUN WITHOUT INCIDENT. REPLACED ANTI-COLLISION LIGHTING PANEL ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — BROKEN (4L DOOR)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTS IN AFT COACH CABIN WERE INOPERATIVE. REPAIRED EMERGENCY EXIT PATH LIGHT JUMPER WIRE NEAR THE 4L DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — DEFECTIVE (CABIN)

LHR - DURING MAINTENANCE, L1 DOOR EMERGENCY ESCAPE BI-DIRECTIONAL ARROW FAILED TO ILLUMINATE. REPLACED L1 DOOR BASE LIGHT EMERGENCY ESCAPE ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: BUSHINGS — ROTATED (LT/RT MLG)

AFW - FOUND LEFT AND RIGHT MAIN GEAR INNER SHOCK STRUT BUSHINGS AT TRACK ATTACH POINT HAS CRACKED SEALANT, POSSIBLE BUSHING ROTATION. REQUEST TO CLEAN SEALANT CHECK FOR CORROSION, RESEAL AND APPLY TORQUE STRIPE FOR FURTHER INSPECTION. PER MRB 757-789. (M)

Part: BUSHING — ROTATED (NLG)

AFW - NOSE GEAR SHOCK STRUT BUSHINGS AT DRAG STRUT ATTACH POINT HAS CRACKED SEALANT, POSSIBLE BUSHING ROTATION, REQUEST TO CLEAN SEALANT CHECK FOR CORROSION, RESEAL AND APPLY TORQUE STRIPE FOR FURTHER INSPECTION. PER MRB 757-790. (M)