N663AM

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,075 hrs · 21,833 cycles

EMERGENCY LIGHT AT SEAT 17F FORWARD OVERWING LAMPS INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 17F FORWARD OVERWING. OPS CHECK NORMAL.

Part: PANEL — INOPERATIVE (CABIN) · airframe 63,075 hrs · 21,833 cycles

EMERGENCY LIGHTS DO NOT TEST AT FORWARD FLIGHT ATTENDANTS PANEL. INSTALLED NEW PANEL, OPS CHECK NORMAL.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 62,806 hrs · 21,725 cycles

LEFT WING OUTBOARD SLAT NUMBER 3 SUSPECT CORRODED ON OUTER LEADING EDGE SKIN AT INBOARD RIB FASTENER ROW. INSTALLED DOUBLER PER SRM 51-40-02 AND 57-43-01-2R.

Part: FIREWALL — WORN (FUSELAGE) · airframe 62,809 hrs · 21,726 cycles

AUXILIARY POWER UNIT COMPARTMENT FIREWALL AFT FACE CHAFED FROM RIGHT DOOR HOLD OPEN HOOD BODY STATION 1787, RIGHT BUTTLINE 10. INSTALLED DOUBLER PER SRM 53-80-08-2R.

Part: DOOR — CRACKED (R2) · airframe 62,809 hrs · 21,726 cycles

RIGHT NUMBER 2 DOOR UPPER HINGE ARM CUTOUT IS CRACKED AND GOUGED. INSTALLED DOUBLER PER SRM 52-10-02-2R1.

Part: RIB — CORRODED (LE SLAT) · corrosion level 2 · airframe 62,741 hrs · 21,707 cycles

RIGHT WING NUMBER 9 SLAT MOST INBOARD RIB HAS 2 EACH AREAS OF CORROSION ON LEADING EDGE SKIN. INSTALLED DOUBLER PER SRM 51-40-02.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 62,741 hrs · 21,707 cycles

NUMBER 3 SLAT LOWER LEADING EDGE SKIN 2 FEET FROM THE INBOARD END IS CORRODED. INSTALLED DOUBLER PER SRM 57-43-A1-2 AND AARD 57-43-00A1.

Part: SKIN — DAMAGED (LE SLAT) · airframe 62,741 hrs · 21,707 cycles

RIGHT WING NUMBER 9 SLAT LEADING EDGE SKIN (OUTBOARD RIB) PREVIOUS BLENDOUT HAS 2 EACH FASTENER HEADS BLENDED. REMOVED DAMAGE PER AARD 57-43-00-1 AND SRM 57-43-2R2. INSTALLED DOUBLER PER SRM 51-40-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 62,183 hrs · 21,489 cycles

SCRIBE LINE FOUND AT LAP SEAM BODY STATION 1344, STRINGER 14 LEFT APPROXIMATELY 1 INCH IN LENGTH. INSTALLED DOUBLER REPAIR PER EA B757-53-021569.

Part: FITTING — DAMAGED (LT PYLON) · airframe 62,183 hrs · 21,489 cycles

TWO LOOSE FASTENERS FOUND ON THE VERTICAL FLANGE OF THE DIAGONAL BRACE FITTING. ACCOMPLISHED INTERIM REPAIR TO LEFT PYLON VERTICAL FLANGE DIAGONAL BRACE FITTING PER EA B757-54-015408.

Part: PAN — GOUGED (R4 DOOR) · airframe 62,183 hrs · 21,489 cycles

RIGHT NUMBER 4 DOOR HANDLE PAN HAS A .015 INCH GOUGE THAT HAS INTERIM REPAIR ACCOMPLISHED. REMOVED AND REPLACED HANDLE PAN PER SRM 51-40-02 AND BAC DRAWING 146N6100, REVISION C.

Part: STRUCTURE — CRACKED (R1 DOOR) · airframe 62,183 hrs · 21,489 cycles

RIGHT NUMBER 1 DOOR HANDLE BOX HAS CRACKS AT INSERTS AND LIGHT PITTING. REMOVED HANDLE BOX AND INSTALLED NEW BOX PER B757-200 CMM 52-11-09 AND AMM 52-11-13-2.

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 62,183 hrs · 21,489 cycles

RIGHT NUMBER 2 DOOR FORWARD FRAME UPPER HINGE CUTOUT IS CRACKED. INSTALLED REPAIR DOUBLER PER SRM 52-10-02-2R.

Part: DOOR FRAME — CRACKED (L2 DOOR) · airframe 62,183 hrs · 21,489 cycles

LEFT NUMBER 2 DOOR FORWARD FRAME UPPER HINGE CUTOUT IS CRACKED. INSTALLED REPAIR DOUBLER PER SRM 52-10-02-2R.

Part: TRANS PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,183 hrs · 21,489 cycles

FORWARD CARGO DOOR SILL, FLOOR SUPPORT CHANNEL CORRODED THROUGHOUT BODY STATIONS 560 TO 620. REMOVED AND REPLACED TRANSITION PANEL PER SRM 51-40-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 62,183 hrs · 21,489 cycles

FUSELAGE INTERNAL STRINGER NUMBER 13 AT STATION 680 RIGHT IS CRACKED. REMOVED AND REPLACED STRINGER NUMBER 13 PER SRM 51-40-02 AND BAC DRAWING 143N8334.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,183 hrs · 21,489 cycles

LEFT NUMBER 4 DOOR CUTOUT FORWARD FRAME WEB AT APPROXIMATLEY STATION 1640 AT FLOOR LEVEL IS CORRODED. REMOVED AND REPLACED WEB PER SRM 51-40-02 AND BOEING DRAWING 146N8713.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,183 hrs · 21,489 cycles

BETWEEN STATIONS 1680 TO 1701 STRINGER 21 LEFT EXFOLIATED CORROSION. ACCOMPLISHED NESTED REPAIR ANGLE PER SRM 53-00-03-R1.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 62,183 hrs · 21,489 cycles

LEFT WING OUTBOARD SLAT NUMBER 3 UPPER SKIN CORRODED. INSTALLED REPAIR PLATE AND DOUBLERS PER SRM 57-43-01-2R1 FIGURE 201 SHEET NUMBER 3.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,183 hrs · 21,489 cycles

AFT CARGO STATION 1300 BETWEEN STRINGERS 20 AND 21 LEFT SHEAR TIE CRACKED. REPLACED CRACKED SHEAR TIE IN AFT CARGO STATION 1300 BETWEEN STRINGERS 20 AND 21 LEFT PER BAC DWG 140N2002 AND SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,183 hrs · 21,489 cycles

MAIN CABIN FLOOR SHEAR WEB BULGED AT FLOORBEAM UPPER CHORD AND CORRODED UPPER SIDE BODY STATION 1681, LEFT BUTTLINES 11 TO 14. ACCOMPLISHED NESTED ANGLE REPAIR PER EA B757-53-021379.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 62,183 hrs · 21,489 cycles

LEFT WING OUTBOARD SLAT NUMBER 2 UPPER SKIN SURFACE IS CORRODED. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER B757 AARD 57-43-00-1, FIGURE/REPAIR 3.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,183 hrs · 21,489 cycles

MAIN CABIN FLOOR SHEAR WEB DOUBLER CORRODED UPPER SIDE BODY STATIONS 1680 TO 1683 LEFT BUTTLINE AS 19 TO 38. REPLACED AFT PRESSURE DECK WEB PER B757 SRM 51-40-02 AND BAC DWG 146N5300.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 62,183 hrs · 21,489 cycles

LEFT AFT WING TO BODY AREA, FAIRING PANEL 195DL SUPPORT ANGLE CRACKED AT BODY STATION 1300, STRINGER 21 LEFT. REPLACED SUPPORT ANGLE ON LEFT AFT WING TO BODY FAIRING PANEL 195DL AT BS 1300 STR 21L IAW B757 SRM 53-60-71-2R1.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,183 hrs · 21,489 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL CORRODED STATION 1440 AND RIGHT BUTTLINE 12 UNDER NUT PLATE. ACCOMPLISHED NESTED ANGLE REPAIR PER SRM 51-40-02 AND SRM 51-40-05.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 62,183 hrs · 21,489 cycles

LEFT WING OUTBOARD SLAT NUMBER 1 UPPER SKIN SURFACE IS CORRODED. INSTALLED DOUBLER AND FILLER PER B757 SRM 57-43-01.

Part: SKIN — GOUGED (FUSELAGE) · airframe 62,183 hrs · 21,489 cycles

AUXILIARY POWER UNIT COMPARTMENT FORWARD LOWER SKIN GOUGED BY DOOR LATCH. FABRICATED AND INSTALLED DOUBLER PER SRM 53-80-08-2R.

Part: CHANNEL — CRACKED (LT MLG WW) · airframe 62,183 hrs · 21,489 cycles

LEFT MAIN WHEEL WELL AFT BULKHEAD ATTACH CHANNEL CRACKED 4 INCHES OUTBOARD OF KEEL BEAM. REMOVED CRACKED CHANNEL PER SRM 51-40-02. INSTALLED NEW CHANNEL PER SRM 51-40-02 AND BAC DWG NUMBER 144N2503 REVISION BM.

Part: CHANNEL — CRACKED (RT MLG WW) · airframe 62,183 hrs · 21,489 cycles

RIGHT MAIN WHEEL WELL AFT BULKHEAD ATTACH CHANNEL CRACKED 4 INCHES OUTBOARD OF KEEL BEAM. REMOVED CRACKED CHANNEL PER SRM 51-40-02. INSTALLED NEW CHANNEL SRM 51-40-02 AND BAC DWG NUMBER 144N2503 REVISION BM.

Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 62,183 hrs · 21,489 cycles

CORROSION ON LOWER LEADING EDGE SKIN 39.0 INCHES FROM INBOARD END NUMBER 1 SLAT. CORROSION REMOVED AND HFEC DETERMINED NO CRACKS ON REMAINING .052. INSTALLED REPAIR FILLER DOUBLER SHIM PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,183 hrs · 21,489 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL CORRODED AT STATION 1420 AND APPROXIMATELY RIGHT BUTTLINE 6 UNDER NUT PLATE. REMOVED CORROSION AND ACCOMPLISHED SPLICE REPAIR PER SRM 51-40-02.

Part: TRANS PANEL — GOUGED (FUSELAGE) · airframe 62,183 hrs · 21,489 cycles

FORWARD CARGO COMPARTMENT, BODY STATION 845, LEFT TRANSITION PANEL GOUGED. REMOVED DAMAGE AND FABRICATED REPAIR PER B757 SRM 51-70-13. INSTALLED PANEL PER SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,183 hrs · 21,489 cycles

MAIN CABIN FLOOR SUPPORT ANGLE CORRODED UPPER AND LOWER SIDES BODY STATIONS 1660 TO 1680, LEFT BUTTLINE 56. REPLACED INTERCOSTAL PER DRAWING 146N5246 AND SRM 51-40-02.

Part: RETAINER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,183 hrs · 21,489 cycles

MAIN CABIN FLOOR GALLEY RETAINER CORRODED AT BODY STATIONS 1681 TO 1720, BUTTLINE 0. INSTALLED NEW HAT CHANNEL GALLEY RETAINER PER B757 51-40-05 AND 51-40-02.

Part: GATE — GOUGED (R4 DOOR) · airframe 62,183 hrs · 21,489 cycles

RIGHT NUMBER 4 DOOR LOWER GATE IS GOUGED ON LOWER OUTER EDGE. INSTALLED NEW GATE ASSEMBLY PER CMM 52-11-25 AND ESO 90108.

Part: SKIN — DENTED (LE SLAT) · airframe 62,183 hrs · 21,489 cycles

LEFT WING NUMBER 2 SLAT UPPER SKIN DENTED OUT OF LIMITS. ACCOMPLISHED DOUBLER REPAIR PER SRM 57-43-02 AND 51-70-10 REPAIR 4 FIGURE 201.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 62,183 hrs · 21,489 cycles

FUSELAGE INTERNAL STRINGER NUMBER 14 AT STATION 680 RIGHT SIDE IS CRACKED. INSTALLED NEW WEB PER SRM 51-40-02 AND DRAWING 143N8334.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,183 hrs · 21,489 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT CHANNEL CORRODED AT STATION 1420 AND RIGHT BUTTLINE 16 UNDER NUT PLATE FRAME STATION 1420 AND RIGHT BUTTLINE 12. INSTALLED NEW FLOOR SUPPORT PER SRM 51-40-05.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 62,183 hrs · 21,489 cycles

FUSELAGE INTERNAL STRINGER NUMBER 14 AT STATION 680 LEFT SIDE IS CRACKED. INSTALLED WEB PER B757 SRM 51-40-02.

Part: SKIN — DENTED (LE SLAT) · airframe 62,183 hrs · 21,489 cycles

LEFT WING NUMBER 1 SLAT UPPER SKIN DENTED OUT OF LIMITS. ACCOMPLISHED DOUBLER REPAIR PER SRM 57-43-02 AND 51-70-10 REPAIR NUMBER 4 FIGURE 201.

Part: SKIN — DENTED (LE SLAT) · airframe 62,183 hrs · 21,489 cycles

LEFT WING NUMBER 5 SLAT INBOARD END UPPER SKIN DENTED OUT OF LIMITS. ACCOMPLISHED DOUBLER REPAIR PER SRM 51-70-10-2R AND 57-43-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,183 hrs · 21,489 cycles

MAIN CABIN FLOOR SUPPORT ANGLE CORRODED UPPER SIDE BODY STATIONS 1645 TO 1647, LEFT BUTTLINE 56. INSTALLED FLOOR SUPPORT AND NUT PLATES PER SRM 51-40-02.

Part: SKIN — DENTED (LE SLAT) · airframe 62,183 hrs · 21,489 cycles

RIGHT WING NUMBER 10 SLAT, TRAILING EDGE WEDGE SKIN DENTED. REMOVED DAMAGE APPROXIMATELY 8 INCHES LENGTH 4 INCHES WIDE OVAL PER SRM 57-43-02. ACCOMPLISHED REPAIR PER SRM 57-43-02 AND 51-70-10.

Part: WEDGE — DENTED (LE SLAT) · airframe 62,183 hrs · 21,489 cycles

RIGHT WING NUMBER 9 SLAT, TRAILING EDGE WEDGE SKIN DENTED. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 57-43-02 AND 51-70-10.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,862 hrs · 21,039 cycles

SEAT 17D EMERGENCY LIGHT HAS ONE LAMP INOPERATIVE. REPLACED LAMP FOR SEAT 17D EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,437 hrs · 20,516 cycles

EMERGENCY LIGHT AT 16C BULLNOSE IS BURNT OUT. REPLACED LAMP FOR 16C EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,437 hrs · 20,516 cycles

EMERGENCY LIGHTS AT SEAT 36D DO NOT LIGHT UP. REPLACED LAMP FOR EMERGENCY LIGHTS AT SEAT 36D. OPS CHECKS NORMAL.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,333 hrs · 20,472 cycles

CORROSION ON RIGHT PRESSURE DECK STATION 1073 RIGHT BUTTLINE 54. ACCOMPLISHED DOUBLER REPAIR PER EA 010523.

Part: FRAME — CRACKED (PYLON) · airframe 58,005 hrs · 20,028 cycles

NUMBER 1 PYLON MID FRAME BULKHEAD INBOARD LOWER FORWARD ATTACH TO LOWER SPAR HAD SHIM MIGRATION. INSTALLED NEW SHIM. ALSO EDDY CURRENT INSPECTION SHOWED CRACK INDICATION AT INBOARD FORWARD LOWER HOLE. REAMED FORWARD OUTBOARD HOLE TO .498 NO CRACK INDICATED. INSTALLED NEW FASTENER PER AARD 54-50-02-3.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,005 hrs · 20,028 cycles

WEB CORRODED AT STATIONS 1440 TO 1460 STRINGER 27 RIGHT. REMOVED AND REPLACED WEB PER 51-10-02-G8.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 58,005 hrs · 20,028 cycles

FLOORBEAM STATION 700 LEFT BUTTLINE 24 CRACKED. REPAIRED FLOORBEAM WITH SPLICED T-CAP AND DOUBLER PER TASK CARD 53-98-01 AND SRM 53-00-51-2R REPAIR NUMBER 3.

Part: SLAT TRACK — CORRODED (LE SLAT) · corrosion level 2 · airframe 58,005 hrs · 20,028 cycles

NUMBER 9 SLAT UPPER SURFACE AT OUTBOARD SLAT TRACK CORRODED AROUND 2 EACH RIVETS. REMOVED DAMAGED AREA AND INSTALLED A FLUSH DOUBLER PER AARD 57-43-00-1.

Part: PLACARD — DAMAGED (OVERWING EXIT) · airframe 56,052 hrs · 19,345 cycles

RIGHT AFT OVERWING EXIT PLACARD DAMAGED. INSTALLED PLACARD AT RIGHT AFT OVERWING EXIT, OPS OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,052 hrs · 19,345 cycles

BULL NOSE EMERGENCY LIGHT AT 3AB INOPERATIVE. RELAMPED BULL NOSE EMERGENCY LIGHT AT 3AB, OPS OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,980 hrs · 19,319 cycles

THE 16D THRU 25D SEAT EMERGENCY LIGHT DIM. REMOVED AND REPLACED 16D THRU 25D EMERGENCY LIGHT BATTERY PACK.

Part: SLAT — DEBONDED (RT WING) · airframe 55,912 hrs · 19,297 cycles

LAX - INFLIGHT SAN-DFW. CREW REPORTED PASSENGER ADVISED FLIGHT ATTENDANT SOMETHING HAD COME OFF WING DURING TAKEOFF. EMERGENCY DECLARED, LANDED AT LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RIGHT INBOARD SLAT TRAILING EDGE DISBONDED. REPLACED RIGHT INBOARD SLAT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,392 hrs · 18,349 cycles

G1-B GALLEY MOUNT SUPPORT CORRODED. REPLACED IAW SRB 53-10-5.

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,392 hrs · 18,349 cycles

RIGHT NR 4 DOOR DRAIN GUSSET CORRODED. REPAIRED AND REPLACED IAW SRM 51-21-03.

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,392 hrs · 18,349 cycles

RIGHT NR 4 DOOR DRAIN GUSSET CORRODED. REPAIRED IAW SRM 51-21-03.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,392 hrs · 18,349 cycles

HAT CHANNEL CORRODED. REPLACED HAT CHANNEL IAW SRM 51-21-03-7.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 53,392 hrs · 18,349 cycles

HAT CHANNEL CORRODED. REPLACED HAT CHANNEL IAW SRM 51-21-03-7.

Part: TEE FITTING — CORRODED (BS 1720) · corrosion level 2 · airframe 53,392 hrs · 18,349 cycles

TEE FITTING CORRODED AFT RT CORNER OF DECK PLATE. REPLACED TEE FITTING IAW SRM 53-60-51.

Part: STRAP — CRACKED (ZONE 100) · airframe 53,392 hrs · 18,349 cycles

STRAP ATTACHED TO BOTTOM OF FLOORBEAM FORWARD OF NR 2 SEAT TRACK CRACKED. REPAIR DOUBLER INSTALLED IAW SRM 53-10-51-2R.

Part: FAN — INOPERATIVE (AIR CONDITIONING)

MKE INFLIGHT T164/18JUL LAX TO EWR - THREE HOURS INTO FLIGHT CREW HEARD LOUD BANG ACCOMPANIED BY VIBRATIONS AND STRONG ELECTRIC SMOKE ODOR. FLIGHT ATTENDANTS REPORTED HAZE IN THE AFT CABIN. SMOKE DISSAPATED BEFORE LANDING. LANDED MKE WITHOUT INCIDENT. REPLACED RIGHT RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 36D INOPERATIVE. REPLACED HARNESS FOR EMERGENCY LIGHT AT SEAT 36D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HOSE — FAILED (HYD SYSTEM)

JFK INFLIGHT T1853/26APR LGA TO MIA LANDED JFK DUE TO LOSS OF LEFT HYDRAULIC SYSTEM FAILED. PERFORMED MANUAL GEAR AND FLAP PROCEDURES. LANDED JFK OVERWEIGHT WITHOUT INCIDENT. FOUND HYDRAULIC LINE TO LEFT GEAR UNLOCK ACTUATOR FAILED. REPLACED HOSE ASSEMBLY FOR LEFT GEAR UNLOCK ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT ROWS 9 TO 15 INOPERATIVE. REPLACED BATTERY PACK AT ZONE 2 FOR EMERGENCY LIGHTS AT ROWS 9 TO 15. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: KEELBEAM — CORRODED (BS 1176)

TUL - KEEL BEAM WEB HAS HEAVY CORROSION INSIDE LEFT WHEEL WELL AT STATION 1176. REMOVED DAMAGED AREAS AND FABRICATED DOUBLER, FILLERS, AND SPLICES. REPAIRED PER 757AARD AND ESO 90309 DATED 11-29-2005.

Part: LINE — LEAKING (HYDRAULIC SYS)

RIGHT MAIN GEAR UNDER INDICATION AND LOCKED GEAR DISAGREE EICAS MESSAGE WITH HANDLE UP. RETURNED TO BDA AND LANDED WITHOUT INCIDENT. FOUND RIGHT MAIN GEAR TILT ACTUATOR HYDRAULIC LINE LEAKING. REPLACED HYDRAULIC LINE WITH A FLEX LINE AND NOTIFIED TECH SERVICES FOR FLEX LINE REPLACEMENT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WINDOW — DELAMINATED (CABIN)

SAN - THIRD WINDOW AFT OF L2 DOOR, AT SEAT 11A, FOUND BROKEN BY FLEET SERVICE CLERK AT DEPARTURE TIME. APPEARS TO BE DELAMINATED. CAUSE UNKNOWN. REPLACED WINDOW AT SEAT 11A AND REINSTALLED INNER WINDOW. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FAN — FAILED (RECIRCULATION)

ON LANDING RT RECIRCULATION FAN FAILED AT TOUCHDOWN AND ON TAXI IN SMOKE IN CABIN AND UNABLE TO CLEAR. FOUND EVIDENCE OF A FIRE IN THE CENTER EQUIPMENT BAY THAT BURNED THE INSULATION BLANKETS IN THE BAY. REPLACED THE RT RECIRCULATION FAN, AND THE BURNED INSULATION BLANKETS. REPLACED THE RT RECIRCULATION FAN CIRCUIT BREAKER AND FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: SLIDE — FAILED (R1 DOOR)

UPON ARRIVAL R1 SLIDE FELL FROM COVER ASSEMBLY WHEN DOOR OPENED BY SKYCHEF CATERING. DOOR ASSIST BOTTLE DEPLETED. SLIDE DID NOT DEPLOY. REPLACED R1 SLIDE AND DOOR ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ACTUATOR — FAILED (L/E SLAT)

MIA - FLT 971 - EN ROUTE DFW-MIA, ON APPROACH TO MIA, RECEIVED LEADING SLAT ASYMMETRY EICAS MESSAGE WHEN EXTENDING FLAPS FROM 1 DEGREE. DECLARED EMERGENCY AND LANDED AT MIA WITHOUT INCIDENT. TROUBLESHOT AND REPLACED NR 7 SLAT OUTBOARD ROTARY SLAT ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFW - FLOORBEAM AT STATION 1640 RBL 58 HAD CORROSION BLENDED BEYOND SRM LIMITS. INSTALLED REPAIR STRAP AS SHOWN IN ATTACHED FIGURE. FABRICATE REPAIR STRAP FROM 301 1/2H STAINLESS STEEL .050 THICK. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDS AND REPAIR PARTS WITH TWO COATS BMS 10-11 PRIMER. FILL BLENDS WITH BMS 5-92. INSTALL STRAPS WET WMM BMS5-95. SEALANT PROSEAL 870. FASTENER LOCATIONSNAND SHAPE OF REPAIR STRAP MAY VARY. (M)

Part: STRAP — CORRODED (FUSELAGE)

AFW - FUSELAGE STRAP AT STATION 1825 JUST BELOW 53R HAD INTERGRANNULAR CORROSION AT 2 NUT PLATES. REMOVED CORROSION PER REF/01. FABRICATE REPAIR DOUBLER FROM .125 INCH 7075-T6. FABRICATE FILLER AND SHIM FROM 7075-T6 THICKNESS AS REQUIRED. FINISH DOUBLER FILLER AND SHIM PER REF/D/. INSTALL REPAIR PARTS WET WITH BMS5-95 SEALANT, REFER TO FIGURE. USE BACB30NW6 HI-LOCKS OR EQUIVALENT. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

AFW - FOUND LOWER MAIN SILL NR 2 CX DOOR CUTOUT INNER CHORD HAS CORROSION REMOVAL AS SHOWN ON SKETCH. MATERIAL REMAINING IS 002 INCH BEYOND SRM LIMITS. REQUEST ENG APPROVAL TO CONT IN SERVICE. REMOVED CORROSION PER REF/C/. VERIFY CORROSION COMPLETELY REMOVED. APPLY ALODINE AND 2 COATS PRIMER TO BLEND AREAS. FILL BLENDS ON UPPER SURFACE W/BMS-95. APPLY CORROSION INHIBITING COMPOUND TO ENTIRE SILL AREA. (M)

Part: UNKNOWN — ODOR (CABIN)

DFW - FLT 2497 - DURING FINAL PORTION OF CLIMB-OUT, FLIGHT ATTENDANT REPORTED ACRID SMELL COMING FROM AFT LAVATORY AREA. RETURNED AND LANDED DFW WITHOUT INCIDENT. AFTER LANDING SMELL DISSIPATED. (M)

Part: LIGHT — INOPERATIVE (ROWS 9-17)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT ROWS 9-17 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP BETWEEN ROWS 9-17. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, L1 AND R1 AND RIGHT FORWARD SECTION EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED WIRING AT L-25. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOOR BEAM — CORRODED (BS 1640)

AFW - FOUND FLOOR BEAM AT 1640 HAS CORROSION. PER MRB 757-966. (M)

Part: ENGINE — FLAMED OUT (RIGHT)

LGA - FLT 732 - DURING DESCENT INTO LGA AT APPROXIMATELY 7000 FEET WITH POWER LEVERS AT IDLE, RIGHT ENGINE FLAMED OUT. ATTEMPTED RE-START SUCCESSFUL AND AIRCRAFT LANDED LGA WITHOUT INCIDENT. REPLACED RT ENGINE BVCU, TPU, IPG SOLENOID AND PLA TRANSDUCER. ACCOMPLISHED SYSTEM LEAK AND GROUND ENGINE RUN CHECKS WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT ROW 3 FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT ROW 3. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: EEL STRIP — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTS AT FORWARD PART OF FIRST CLASS CABIN INOPERATIVE. REPLACED EMERGENCY LIGHT STRIP AT FORWARD PART OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)