N621AM

Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 3 · airframe 72,990 hrs · 25,540 cycles

LOWER WING SKIN PANEL LANDING HAS CORROSION ON UPPER SURFACE OF LANDING NEAR THE SERVICE INTERPHONE JACK AT THE INBD END OF THE FUEL PANEL. REMOVED CORROSION & ACCOMPLISHED REPAIR EA B757-57-032464.

Part: BATTERY — FAULTY (MAIN) · airframe 72,459 hrs · 25,343 cycles

STL INFLIGHT BOS-DFW CREW REPORTED "MAIN BATTERY CHARGER" EICAS STATUS MESSAGE ILLUMINATED IN FLIGHT. EMERGENCY DECLARED FLIGHT DIVERTED STL LANDED WITHOUT INCIDENT. REPLACED MAIN BATTERY & MAIN BATTERY CHARGER (MPN S282T002-6). SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: TRANSMISSION — MALFUNCTIONED (TE FLAP) · airframe 70,878 hrs · 24,794 cycles

SFO - (REPEAT ITEM) CREW REPORTED DURING APPROACH TRAILING EDGE FLAP/SLAT DISAGREE INDICATION. EMERGENCY DECLARED FLIGHT LANDED SFO WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND NUMBER FIVE FLAP TRANSMISSION OVERLOAD INDICATOR TRIPPED. RESET AND SERVICED NUMBER FIVE TRANSMISSION. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TRANSMISSION — MALFUNCTIONED (TE FLAP) · airframe 70,878 hrs · 24,794 cycles

SJU - (REPEAT ITEM) CREW REPORTED TRAILING EDGE FLAP DISAGREE MESSAGE. ACCOMPLISHED QRH PROCEDURES AND EXECUTED GO AROUND. EMERGENCY DECLARED FLIGHT LANDED SJU WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT INBOARD FLAP TRANSMISSION. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FSEU — MALFUNCTIONED (TE FLAP) · airframe 70,878 hrs · 24,794 cycles

SJO - CREW REPORTED TRAILING EDGE FLAP ASYMMETRY MESSAGE. GO AROUND AND ACCOMPLISHED QRH PROCEDURES AND GO AROUND. EMERGENCY DECLARED FLIGHT LANDED SJO WITHOUT INCIDENT. RESET FLAP/SLAT ELECTRONICS UNIT CIRCUIT BREAKERS AND PERFORMED FSEU BITE. NO FAULTS FOUND. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,131 hrs · 24,172 cycles

SEAT 35D ESCAPE PATH LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 35D ESCAPE PATH LIGHT. OPS CHECK NORMAL.

Part: SHROUD — MISSING (CABIN) · airframe 69,131 hrs · 24,172 cycles

SHROUD MISSING FROM FORWARD ESCAPE PATH LIGHT ON SEAT 3E. REPLACED SHROUD ON FORWARD ESCAPE PATH LIGHT ON SEAT 3E. OPS CHECK NORMAL.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,938 hrs · 24,105 cycles

CORROSION ON CREASE ANGLE AT STATION 1635. REPAIRED PER AARD 51-00-05.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,938 hrs · 24,105 cycles

CABIN AFT DECK CORROSION AT LONGERON 4 NUMBER 3 THRESHOLD SUPPORT. REPLACED THRESHOLD SUPPORT PER SRM 51-10-02-0G AND AARD 51-00-05-1, REPAIR 1.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,938 hrs · 24,105 cycles

CABIN AFT DECK CORROSION AT LONGERON FOUR NUMBER TWO THRESHOLD SUPPORT. REPLACED NUMBER TWO THRESHOLD SUPPORT PER SRM 51-10-02-0G AND AARD 51-00-05-01, REPAIR 1.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,938 hrs · 24,105 cycles

CABIN AFT DECK CORROSION AT LONGERON 4 NUMBER 5 THRESHOLD SUPPORT. REPLACED THRESHOLD SUPPORT PER SRM 51-10-02-0G AND AARD 51-00-05-1, REPAIR 1.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,938 hrs · 24,105 cycles

CABIN AFT DECK CORROSION AT LONGERON 4 NUMBER 6 THRESHOLD SUPPORT. REPLACED THRESHOLD SUPPORT PER SRM 51-10-02-0G AND AARD 51-00-05-1, REPAIR 1.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,938 hrs · 24,105 cycles

FORWARD GUTTER SUPPORT FROM FRAME STATIONS 324 TO 345 RIGHT BUTTLINE 61 CORRODED. REPLACED FORWARD GUTTER SUPPORT PER SRM 51-10-02-0G, 9 AND AARD 51-00-05-1, REPAIR 1.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,938 hrs · 24,105 cycles

CORROSION ON INTERCOSTAL FROM STATIONS 404 TO 409 RIGHT BUTTLINES 47 TO 59. INSTALLED INTERCOSTAL FRAME STATIONS 404 TO 409 RIGHT BUTTLINES 47 TO 59 PER SRM 51-10-02-0G 9 AND AARD 51-00-05-1 REPAIR 1.

Part: DOUBLER — CRACKED (R2 DOOR) · airframe 68,938 hrs · 24,105 cycles

RIGHT NUMBER 2 DOOR UPPER HINGE CUTOUT CRACKED. INSTALLED DOUBLER PER SRM 52-10-02-2, REPAIR 1.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,938 hrs · 24,105 cycles

THE FORWARD LEFT NUMBER 4 DOOR GUTTER DRAIN SUPPORT IS CORRODED. REPLACED FORWARD GUTTER SUPPORT PER AARD 51-00-05-1 REPAIR 1.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,938 hrs · 24,105 cycles

LEFT NUMBER 4 DOOR AFT GUTTER DRAIN SUPPORT IS CORRODED. REPLACED LEFT NUMBER 4 DOOR AFT GUTTER DRAIN SUPPORT PER SRM 51-10-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,938 hrs · 24,105 cycles

CORROSION ON FLOORBEAM 1640 AT SCREW HOLES. ACCOMPLISHED SPLICE REPAIR PER EA B757-53-024162.

Part: PLACARD — MISSING (ZONE 200) · airframe 68,040 hrs · 23,775 cycles

RIGHT FORWARD EMERGENCY EXIT LIGHT LENS MISSING ARROW DECAL. REPLACED ARROW DECAL. OPS CHECK NORMAL.

Part: PLACARD — MISSING (CABIN) · airframe 68,040 hrs · 23,775 cycles

LEFT FORWARD EMERGENCY EXIT LIGHT LENS MISSING ARROW DECAL. REPLACED ARROW DECAL. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,750 hrs · 22,583 cycles

ROWS 9D TO 19D EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT M100799. OPS CHECK NORMAL.

Part: MODULE — INOPERATIVE (CABIN) · airframe 64,750 hrs · 22,583 cycles

ROWS 9D TO 19D EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY MODULE AT M100799. OPS CHECK NORMAL.

Part: SKIN — CORRODED (TE FLAP) · airframe 64,377 hrs · 22,450 cycles

FLAP INBOARD TOP INBOARD SIDE FORWARD CORRODED. INSTALLED 7075-T6 DOUBLER .016 INCH THICK ON INSIDE SKIN OVER POTTED AREAS CREATED DURING DOUBLER DRILL UP PER SRM 51-70-10-2R 2 FIGURE 203 SHEET 1.

Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 64,377 hrs · 22,450 cycles

FLAP INBOARD TOP INBOARD SIDE FORWARD CORRODED. ALL WORK ACCOMPLISHED PER EA. B757-57-014562.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 64,377 hrs · 22,450 cycles

FORWARD CARGO INTERCOSTAL VERTICAL SUPPORTS CRACKED FROM STATIONS 660 TO 680 LEFT BUTTLINE 45.5. REMOVED AND REPLACED INTERCOSTAL. RE-ATTACHED POTABLE WATER LINE AND DRAIN LINE TO S-LAVATORY PER SRM 51-10-02-0G PARAGRAPH 9.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,377 hrs · 22,450 cycles

CORROSION TOP OF KEEL BEAM LEFT WHEEL WELL AFT LOWER CORNER. REMOVED CORROSION FLAPPER PEENED AREA ON NDT PER EA 014625.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,377 hrs · 22,450 cycles

CORROSION ON TOP OF KEEL BEAM LEFT WHEEL WELL LOWER AFT CORNER. VERTICAL STIFFENER REPLACED PER SRM 51-10-02-0G.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,490 hrs · 21,798 cycles

RIGHT ROW 9 TO 14 EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT ROW 9 TO 14 EMERGENCY LIGHTS. OPS CHECKED NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 60,009 hrs · 20,922 cycles

THE 34D SEAT EMERGENCY LIGHT INOPERATIVE. RE-INSTALLED 34D SEAT EMERGENCY LIGHT SIDEWALL CONNECTOR PLUG, OPS CHECKED NORMAL.

Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,748 hrs · 20,825 cycles

RIGHT AFT LAVATORY: FORWARD INBOARD MOUNT CORRODED. REPAIRED IAW SRM 53-01-51-01 REPLACED MOUNT.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,745 hrs · 20,824 cycles

INTERCOSTAL CORRODED. REPAIRED IAW SRM 51-70-13-0G REPLACED ANGLE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,748 hrs · 20,825 cycles

FLOORBOARD SUPPORT CORRODED. REPAIRED IAW SRM 51-10-02-06.

Part: TORQUE TUBE — CRACKED (L1 DOOR) · airframe 59,135 hrs · 20,598 cycles

LEFT NUMBER ONE PASS DOOR AFT END OF LOWER TORQUE TUBE IS CRACKED. INSTALLED NEW TORQUE TUBE PER ESO 90283

Part: DOOR FRAME — CORRODED (R1 DOOR) · corrosion level 2 · airframe 59,748 hrs · 20,825 cycles

UPPER DOOR FRAME CORNER CORRODED. REPAIRED IAW ESO 90284.

Part: TORQUE BOX — CRACKED (R4 DOOR) · airframe 59,135 hrs · 20,598 cycles

RIGHT NUMBER FOUR DOOR HANDLE TORQUE BOX IS CRACKED AT THE THREE CAM BASKET MOUNT HOLES. INSTALLED TORQUE BOX PER ESO 90108.

Part: PAN — WORN (L4 DOOR) · airframe 59,135 hrs · 20,598 cycles

WORN HANDLE PAN AT PASS DOOR LEFT HAND NUMBER FOUR. REPLACED PASS DOOR HANDLE PAN PER ESO 90108.

Part: TORQUE BOX — CRACKED (FUSELAGE) · airframe 59,135 hrs · 20,598 cycles

TORQUE BOX HAS TWO FASTENER HOLES CRACKED ON OUTER SIDE TO CAM BASKET. INSTALLED NEW TORQUE BOX PER ESO 90108.

Part: GATE — CORRODED (R2 DOOR) · corrosion level 2 · airframe 59,135 hrs · 20,598 cycles

LOWER DOOR GATE AT RIGHT HAND NUMBER TWO HAS CORROSION. INSTALLED NEW LOWER DOOR GATE PER ESO 090282.

Part: PLACARD — DAMAGED (CABIN)

DFW EMERGENCY LIGHT EXIT SIGN DECAL AT RT NR 2 EXIT DOOR DAMAGED. REPLACED DECAL FOR EMERGENCY LIGHT EXIT SIGN AT RT NR 2 DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: PLACARD — DAMAGED (CABIN)

DFW EMERGENCY LIGHT EXIT SIGN DECAL AT RT NR 3 DOOR DAMAGED. REPLACED DECAL FOR EMERGENCY LIGHT EXIT SIGN AT RT NR 3 DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: PLACARD — DAMAGED (CABIN)

DFW EMERGENCY LIGHT EXIT SIGN DECAL AT RT OVERWING EXIT DOOR DAMAGED. REPLACED DECAL FOR EMERGENCY LIGHT EXIT SIGN AT RT OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: PLACARD — DAMAGED (CABIN)

DFW EMERGENCY LIGHT EXIT SIGN DECAL AT RT NR 1 EXIT DOOR DAMAGED. REPLACED DECAL FOR EMERGENCY LIGHT EXIT SIGN AT RT NR 1 EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: SIGN — DAMAGED (CABIN)

DFW EMERGENCY LIGHT EXIT SIGN AT RT FORWARD OVERWING EXIT DOOR DAMAGED. REPLACED SIGN ASSEMBLY FOR EMERGENCY LIGHT EXIT SIGN AT RT FORWARD OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: SIGN — DAMAGED (CABIN)

DFW EMERGENCY LIGHT EXIT SIGN AT LT NR 1 DOOR DAMAGED. REPLACED SIGN ASSEMBLY FOR EMERGENCY LIGHT EXIT SIGN AT LT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: PLACARD — DAMAGED (CABIN)

DFW EMERGENCY LIGHT EXIT SIGN DECAL AT LT OVERWING EXIT DOOR DAMAGED. REPLACED DECAL FOR EMERGENCY LIGHT EXIT SIGN AT LT OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,872 hrs

DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 11D. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHTS AT SEAT ROW 34DEF INOPERATIVE. REPLACED CONNECTOR AND SOCKET 1703663 FOR EMERGENCY LIGHTS AT SEAT ROW 34DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHT)

DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 2E HAS BROKEN SHROUD. REPLACED SHROUD FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 2E. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HOSE — LEAKING (HYD SYSTEM)

ORD INFLIGHT T681/19MAY - ON FIRST APPROACH AUTO SPEEDBRAKE INDICATION WHEN SPOILERS ARMED. RESET NO HELP. WHEN LANDING GEAR EXTENDED RIGHT MAIN LANDING GEAR UNSAFE INDICATION. INITIATED GO AROUND AND LOWERED LANDING GEAR MANUALLY. LANDED ORD WITHOUT INCIDENT. FOUND HYDRAULIC LEAK IN GEAR AREA. AIRCRAFT TAKEN OUT OF SERVICE FOR REPAIR. REPLACED HYDRAULIC LINE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

DFW - EMERGENCY LIGHT IDENTIFIER AT AFT LEFT NUMBER TWO DOOR BROKEN. REPLACED EMERGENCY LIGHT IDENTIFIER ASSEMBLY AT AFT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROL MODULE — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, FOUND ALL KNEE LEVEL AND FLOOR LEVEL EMERGENCY EXIT MARKERS INOPERATIVE. REPLACED CONTROL MODULES AND BATTERY PACKS FOR EQUIPMENT M10798, M10799, M10800 AND M10801 EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SPRING — DAMAGED (GIRT BAR)

DURING ACCOMPLISHMENT OF ENGINEERING REQUEST OT CHEKC GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, SIX GIRT BAR SPRINGS NEED REPLACEMENT. REPLACED SIX GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NROMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

DURNIG OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 27D INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 27D. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

TUL - FOUND TOP OF FLOORBEAM CORRODED AT STATION 1640. REMOVED DAMAGED SECTION OF BEAM. INSTALLED NEW SECTION PER SRM 51-70. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

FOUND TOP OF AFT FLOOR SUPPORT CORRODED CENTER, FS 1640-1660. REMOVED AFT FLOOR SUPPORT. INSTALLED NEW AUX FLOOR SUPPORT PER SRM 51-70. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

TUL - FOUND TOP OF FLOOR SUPPORT CORRODED CTR, FS 1660. REMOVED TOP OF FLOOR SUPPORT FROM STATION 1660 TO 1680 CENTER SUPPORT PER SRM 51-70. INSTALLED NEW SUPPORT. (M)

Part: PRESSURE PANEL — CORRODED (MLG WW)

IN THE LT MAIN LANDING GEAR WHEEL WELL, INBOARD WALL BETWEEN STATION 1100 AND 1120 THERE IS AN AREA OF CORROSION. BLENDED CORROSION PER SRM 53-40-12-1. ALODINED AND PRIMED AND PAINTED. (M)

Part: PIN — NOT SEATED (CONNECTOR)

DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 12D INOPERATIVE. RESEATED PIN AT EMERGENCY EXIT LIGHT SIDEWALL CONNECTOR AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - FOUND EMERGENCY LIGHT AT SEAT 25D IS INOPERATIVE. CLEANED AND RESEATED EMERGENCY LIGHT POWER CONNECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: MODULE — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT SEAT LIGHTS INOPERATIVE. REPLACED MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ROW 27DEF INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT LIGHT AT L2 DOOR DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK AT L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 2EF INOPERATIVE. RE-SECURED EMERGENCY EXIT LIGHT CONNECTOR AT BIN 2EF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 18D INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT ASSEMBLY AT SEAT 18D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 18D INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — DEFECTIVE (CABIN)

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

Part: CONNECTOR — BROKEN (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)