N206UW

Part: FAN — FAILED (RECIRCULATION) · airframe 80,228 hrs · 27,137 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS RIGHT RECIC R FAN MSG WITH BURNING SMELL IN CABIN. FAN TURNED OFF, SMELL DISSAPATED. MAINTENANCE REMOVED AND REPLACED RH RECIRCULATION FAN IAW AMM 21-25-01-404. OPS CHECK GOOD.

Part: SLIDE — LOW PRESSURE (R4 DOOR) · airframe 79,789 hrs · 27,037 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS R4 DOOR SLIDE PRESSURE IS IN THE RED BAND. REMOVED AND REPLACED R4 DOOR EVAC SLIDE IAW JOB CARD 19L80025002.

Part: WINDSHIELD — FAILED (OUTER PANE) · airframe 76,881 hrs · 26,329 cycles

FIRST OFFICER`S WINDSHIELD OUTER PANE SHATTERED. QRH CHECKLIST PERFORMED. AIRCRAFT PRESSURIZATION AND OTHER SYSTEMS WERE NORMAL AND FLIGHT CONTINUED TO DESTINATION. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE WINDSHIELD IAW STANDARD PRACTICES AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: COVER — OUT OF ADJUST (R2 DOOR) · airframe 76,881 hrs · 26,329 cycles

THE AIRCRAFT WAS NOT GROUNDED. 2R SLIDE ARMED INDICATOR DOES NOT POP OUT. ADJUSTED 2R DOOR COVER PANEL, SLIDE ARMED INDICATOR KNUCKLE BUSTER. OPERATIONS CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 76,277 hrs · 26,197 cycles

AIRCRAFT WAS NOT GROUNDED. 1 LT JUMPSEAT FLASHLIGHT NEEDS REPLACING. REPLACED FORWARD JUMPSEAT FLASHLIGHT BATTERY AND RESECURED WITH SEAL. OK FOR SERVICE.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 76,137 hrs · 26,168 cycles

AIRCRAFT WAS NOT GROUNDED. L3 WINDOW UPPER FORWARD CORNER DELAMINATED. REPLACED LEFT HAND NR 3 COCKPIT WINDOW PER MM 56-11-10.

Part: BULKHEAD — CRACKED (ZONE 400 - NAC/P) · airframe 75,654 hrs · 26,058 cycles

NR 2 NACELLE OUTBOARD MID BULKHEAD IS CRACKED. REPAIRED THE BULKHEAD IAW EA 278458

Part: INTERCOSTAL — CORRODED (BS 1320-1340) · airframe 75,654 hrs · 26,058 cycles

CORROSION ON THE AFT CARGO INTERCOSTAL, STRINGER 28L BETWEEN BS 1320 TO 1340, LBL 10.45. REMOVED RIVETS, REMOVED CORROSION, TREATED AREAS, AND REINSTALLED THE INTERCOSTAL IAW SRM 51-40-02, AND SRM 53-00-04.

Part: FLOOR SUPPORT — CRACKED (BS 1214-1218) · airframe 75,654 hrs · 26,058 cycles

CRACKED INDICATED ON THE FLOOR SUPPORT, BS 1214 - 1218. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02, AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1320-1340) · corrosion level 2 · airframe 75,654 hrs · 26,058 cycles

CORROSION FOUND ON THE CARGO FLOOR SUPPORT, BS 1320 - 1340, LBL 16.1. CUT OUT CORRODED AREA AND INSTALLED A REPAIR ANGLE IAW 53-10-00, REPAIR 1.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 75,445 hrs · 26,013 cycles

R1 DOOR SLIDE PRESSURE IN THE RED. R & R THE DOOR SLIDE IAW J/C 19L80025002.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 74,944 hrs · 25,897 cycles

AIRCRAFT WAS NOT GROUNDED. AFT GALLEY ENTRY & R4 DOOR EMERGENCY LIGHT WILL NOT STAY ON PAST 5 SEC. REPLACED POWER SUPPLY PER AMM 33-51-07.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 74,752 hrs · 25,859 cycles

FLIGHT ATTENDANT FLASHLIGHT AT THE L2 DOOR, RIGHT JUMPSEAT IS INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT BATTERY. OPS CHECKED GOOD.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 74,752 hrs · 25,859 cycles

FLIGHT ATTENDANT FLASHLIGHT AT THE L2 DOOR LEFT JUMPSEAT IS INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT BATTERY. OPS CHECKED GOOD.

Part: SLIDE — LOW PRESSURE (L3 DOOR) · airframe 73,872 hrs · 25,657 cycles

AIRCRAFT WAS GROUNDED. L3 DOOR SLIDE PRESSURE, LOW. REPLACED SLIDE PER JOB CARD 19L83525001. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 73,858 hrs · 25,655 cycles

L3 DOOR EMERGENCY EXIT SIGN COVER LOOSE. SECURED THE EMERGENCY SIGN COVER AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BOLT — LOOSE (L1 DOOR SLIDE) · airframe 73,816 hrs · 25,643 cycles

L1 DOOR SLIDE PACK WAS JAMMED IN DOOR WHEN CLOSING FOR DEPARTURE.DUE TO LOOSE GUIDE ARM BOLTS. TORQUED THE BOLTS AND ACCOMPLISHED ADJUSTMENT OF GUIDE ARM IAW AMM 52-11-04-822-056. OPS CHECKED GOOD.

Part: SIGN — MISSING (CABIN) · airframe 73,673 hrs · 25,608 cycles

EMERGENCY EXIT SIGN BY THE L2 DOOR IS MISSING. REPLACED THE EXIT SIGN IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 73,662 hrs · 25,605 cycles

EMERGENCY EXIT SIGN AT THE L2 DOOR HAS A DETACHED LENS. SECURED THE LENS. OPS CHECKED GOOD.

Part: WINDSHIELD — FAILED (COCKPIT)

CAPTAIN`S WINDSHIELD BEGAN ARCING IN UPPER RT, SHUT OFF WINDOW HEAT. SEVERAL MINUTES LATER OUTER PANE CRACKED AT FL 370. REPLACED THE WINDSHIELD IAW AMM 56-11-01. THE AIRCRAFT WAS GROUNDED.

Part: CAM — INTERFERENCE (R1 DOOR) · airframe 73,304 hrs · 25,519 cycles

R1 DOOR DIFFICULT TO CLOSE DUE TO UPPER AFT LATCH ROLLER INTERFERING WITH LATCH CAM. REMOVED AND REPLACED UPPER AFT LATCH CAM AND ADJUSTED GUIDE ARM IAW AMM 52-11-04-822-056. OPERATIONAL CHECK GOOD.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 73,247 hrs · 25,507 cycles

EMERGENCY EXIT SIGN BY THE L2 DOOR, THE LENS DETACH DURING FLIGHT. SECURED THE LENS IAW AMM 33-51-01. OPS CHECKED GOOD.

Part: INDICATOR — FAULTY (FUEL SYS) · airframe 72,628 hrs · 25,333 cycles

LEFT CENTER TANK FUEL PUMP EICAS MESSAGE AND OVERHEAD SWITCH. REMOVED AND REPLACED UNIVERSAL FAULT INDICATOR AND RELAY ADAPTER MODULE IAW TDG SUPPLEMENT 28-22-00. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: RELAY — FAULTY (FUEL SYS) · airframe 72,628 hrs · 25,333 cycles

LEFT CENTER TANK FUEL PUMP EICAS MESSAGE AND OVERHEAD SWITCH. REMOVED AND REPLACED UNIVERSAL FAULT INDICATOR AND RELAY ADAPTER MODULE IAW TDG SUPPLEMENT 28-22-00. OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.

Part: WARNING MESSAGE — ACTIVATED (CONFIGURATION) · airframe 72,484 hrs · 25,274 cycles

AT 120KTS, CONFIGURATION WARNING & M/W. ABORTED TAKEOFF, BELIEVE TRIM WAS INADVERTENTLY ACTIVATED DURING THE TAKEOFF ROLL. THRUST REVERSERS USED. BRAKING NORMAL. MAINTENANCE ACCOMPLISHED SATISFACTORY OPERATIONAL CHECKS IAW AMM 05-51-14 AND AMM 27-41-00. AIRCRAFT WAS GROUNDED.

Part: RESERVOIR — LOW PRESSURE (R4 DOOR ASSIST) · airframe 72,212 hrs · 25,197 cycles

R4 DOOR ASSIT BOTTLE HAS LOW PRESSURE INDICATION. REPLACED EMERGENCY POWER RESERVOIR FOR R4 DOOR IAW AMM 52-11-30.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 72,212 hrs · 25,197 cycles

R1 DOOR SLIDE HAS LOW PRESSURE INDICATION. REPLACED R1 DOOR SLIDE IAW 19L80025002. AIRCRAFT WAS GROUNDED.

Part: LIGHT — DIRTY (R1 DOOR SLIDE) · airframe 72,207 hrs · 25,196 cycles

R1 DOOR SLIDE LIGHT INOPERATIVE. MAINTENANCE REMOVED DEBRIS FROM SLIDE LIGHT AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LANYARD — BROKEN (ESCAPE SLIDE) · airframe 70,770 hrs · 24,817 cycles

LEFT EMERGENCY EXIT DOOR ESCAPE SLIDE, AFT QUICK RELEASE CABLE PARACHUTE PIN HAS A BROKEN NYLON CORD. REPLACED BROKEN NYLON CHORD IAW CMM 25-66-03.

Part: PUSHROD — OUT OF ADJUST (R2 GIRT BAR) · airframe 70,770 hrs · 24,817 cycles

R2 DOOR AFT GIRT BAR CRANK, TOUCHING THE GIRT BAR LIFTER WHEN DOOR IS IN DISARMED POSITION. ADJUSTED R2 DOOR AFT GIRT BAR PUSH ROD IAW AMM 52-11-25-825-001 AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 52-11-25-735-024.

Part: STRAP — CRACKED (RT WING) · airframe 70,770 hrs · 24,817 cycles

RIGHT WING LOWER STRINGER REINFORCMENT STRAP CRACKED AT WS 520 AND STRINGER 6. REPLACED THE STRAP IAW SRM 51-40-02-OG AND DWG 757-3440 TR 10986.

Part: STRAP — CRACKED (LT WING) · airframe 70,770 hrs · 24,817 cycles

LEFT WING LOWER STRINGER REINFORCMENT STRAP CRACKED AT WS 415 AND STRINGER 8. REPLACED THE STRAP IAW SRM 51-40-02-OG AND DWG 757-3440 TR 10986.

Part: STIFFENER — CRACKED (BS 1320) · airframe 70,770 hrs · 24,817 cycles

CABIN FLOORBEAM SUPPORT STIFFENER CRACKED AT BS 1320 AND LBL 45.50. REPLACED SUPPORT STIFFENER IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (BS 1337) · airframe 70,770 hrs · 24,817 cycles

CABIN FLOOR SUPPORT ANGLE CRACKED AT BS 1337 AND BL 0. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02.

Part: GIMBAL JOINT — WORN (L2 DOOR) · airframe 70,770 hrs · 24,817 cycles

L2 DOOR GIRT BAR MECHANISM HAS EXCESSIVE PLAY (FORE AND AFT). REPLACED L2 DOOR GIRT BAR MECHANISM GIMBAL PER CMM 52-11-15 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BUSHING — DAMAGED (GIRT BAR) · airframe 70,770 hrs · 24,817 cycles

R2 DOOR AFT GIRT BAR MECHANISM LINK HAS A DAMAGED SPACER ON TORSION SPRING ASSEMBLY. REPLACED SPRING ASSEMBLY AND ADJUSTED GIRT BAR MECHANISM LINK PER AMM 20-11-00-912 AND TASK CARD 19C84252007.

Part: ATTACH BOLT — LOOSE (ZONE 800) · airframe 70,770 hrs · 24,817 cycles

AIRCRAFT IN BASE MAINTENANCE: L1 ENTRY DOOR GIRT BAR MECHANISM FORWARD GIRT BAR LOCKING CAM ATTACH BOLT LOOSE. SECURED BOLT IAW AMM 20-11-00-201.

Part: SUPPORT BRACKET — OUT OF POSITION (L1 DOOR) · airframe 70,528 hrs · 24,738 cycles

AIRCRAFT WAS GROUNDED: L1 DOOR OUT OF SEQUENCE AND WILL NOT CLOSE. MAINTENANCE FOUND LOWER GUIDE ARM SUPPORT BRACKET IN WRONG POSITION. ADJUSTED POSITION OF BRACKET TO DOOR IAW AMM 52-11-04-822-056 AND ACCOMPLISHED A SATISFACTORY OPS CHECK.

Part: FITTING — WORN (R1 DOOR) · airframe 68,685 hrs · 24,240 cycles

1R DOOR DIFFICULT TO LATCH, NOTICED SCARRING OF UPPER RT DOOR FRAME LATCH ASSEMBLY. CHECKED FOR WEAR ON DOOR HINGES & REPLACED AFT UPPER LATCH FITTING IAW 52-11-37-404-038.

Part: GOVERNOR — DEFECTIVE (LT ENGINE) · airframe 68,576 hrs · 24,212 cycles

WHEN SHUTTING DOWN LT ENG, THE LT FUEL CONTROL WOULD NOT WORK IN THE CUT OFF POSITION. PULLING THE LT FIRE SWITCH DID SHUT DOWN THE ENG. LT ENG FIRE SWITCH HAS RESET TO THE DOWN OR CLOSED POSITION. REPLACED NR 1 ENG FUEL FLOW GOVERNOR & ACCOMPLISHED A SATISFACTORY LEAK & OPERATIONAL CHECK IAW 19L40073002 & 19L40073003.

Part: SOLENOID VALVE — FAULTY (FUEL SYSTEM) · airframe 68,176 hrs · 24,063 cycles

FLIGHT 803 CANNOT SHUTDOWN LT ENG WITH FUEL CUT OFF SWITCH. R & R FUEL FLOW GOVERNOR SOLENOID VLV IAW AMM 73-21-15. OPERATIONAL & LEAK CHECKED OK.

Part: LENS — DETACHED (EMERGENCY LIGHTS) · airframe 67,472 hrs · 23,898 cycles

EXIT SIGN OVER DOOR 2L FELL OFF. R & R EXIT SIGN COVER OVER 2L DOOR.

Part: ACTUATOR — FAILED (RT MLG) · airframe 67,462 hrs · 23,893 cycles

FLIGHT 1796 EN-ROUTE, EICAS, GEAR DISAGREE, WITH DOORS LIGHT & RT GEAR DOOR DOWN. FOLLOWED QRH & USED ALTERNATE GEAR EXTENSION ALL GEAR DOWN. GEAR DISAGREE WAS WITH GEAR HANDLE UP & OFF. THE FLIGHT RETURNED TO FIELD & LANDED WITHOUT FURTHER INCIDENT. R & R RT GEAR TILT ACTUATOR IAW AMM 32-32-15. LEAK CHECK, OPERATIONS CHECKED GOOD. GEAR SWUNG SEVERAL TIMES, OPERATIONS CHECKED GOOD IAW 32-33-00.

Part: LENS — MISSING (CABIN) · airframe 67,453 hrs · 23,889 cycles

ON DAILY CHECK FOUND L4 DOOR EXIT LIGHT LENS MISSING. REPLACED EMER LIGHT ASSEMBLY IAW AMM 33-51-10-002-045. OPERATIONS CHECKED OK.

Part: GATE — CORRODED (L1 DOOR) · airframe 66,320 hrs · 23,606 cycles

C1 CHECK, CORROSION ON L1 DOOR LOWER GATE. R & R L1 DOOR LOWER GATE IAW AMM 52-11-38-004-01 & 52-11-38-404-009.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,320 hrs · 23,606 cycles

C1 CHECK, CORROSION ON STRINGER AT STATION 655, RBL 16.10 IN FWD CARGO COMPARTMENT. REPLACED STRINGER IAW SRM 53-00-53-1A & SRM 53-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,320 hrs · 23,606 cycles

C1 CHECK, CORROSION ON STRINGER AT STATION 748, RBL 7.55 IN THE FWD CARGO COMPARTMENT. REPAIRED STRINGER IAW TR757-5310-12-0665 PART A.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,320 hrs · 23,606 cycles

C1 CHECK, CORROSION ON FWD CARGO INTERCOSTAL LOWER ANGLE BETWEEN STATION 740 & 760 AT RBL 16.10. R & R INTERCOSTAL IAW SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,320 hrs · 23,606 cycles

C1 CHECK, FWD CARGO INTERCOSTAL WEB HAS CORROSION ON LOWER ANGLE 5-031. BLENDED OUT & REMOVED CORROSION BUT FOUND TO BE OUT OF LIMITS. REPLACED INTERCOSTAL WEB IAW SRM 51-30-01, 51-40-05 & 51-40-02. TOP COATED FASTENERS IAW AMM 51-12-15.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,320 hrs · 23,606 cycles

C1 CHECK, FWD CARGO FLOOR STRINGER & NUTPLATE HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A. REPLACED FLOOR STRINGER IAW SRM 51-40-02.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,320 hrs · 23,606 cycles

C1 CHECK, FWD CARGO FLOOR STRINGER HAS CORROSION ON THE STRINGER & NUTPLATE. REMOVED CORROSION IAW SRM 51-10-02 & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A. REPLACED FLOOR STRINGER IAW SRM 51-40-02.

Part: HOSE — LEAKING (SLIDE RAFT)

SLIDE FELL OUT OF DOOR ON OPENING, DID NOT DEPLOY. THE ACFT WAS MX FERRIED FOR REPAIRS. DURING REPLACEMENT OF THE L1 DOOR SLIDE & AFT, FOUND THE DOOR EMER POWER RESERVOIR PRESS AT 0 PSI. REPLACED THE L1 DOOR SLIDE, RAFT & THE L1 DOOR EMER POWER RESERVOIR.

Part: PLATE — DEBONDED (LE SLAT) · airframe 65,571 hrs · 23,361 cycles

RON LT WING NR 4 SLAT AFT INBD CORNER, AFT FACE, STIFFENER PLATE DISBONDED. R & R LT NR 4 SLAT IAW JOB CARD 19L52027002.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 65,035 hrs · 23,240 cycles

3L DOOR EMER FLASHLIGHT INOPERATIVE. REPLACED 3L DOOR FLASHLIGHT. OPERATIONS CHECKED OK.

Part: LIGHT — BROKEN (COCKPIT) · airframe 64,760 hrs · 23,180 cycles

ON APPROACH, THE RT MLG LIGHTS FAILED TO ILLUMINATE WITH LG HANDLE SELECTED DOWN. QRH PROCEDURES WERE ACCOMPLISHED & AN EMER WAS DECLARED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE RT MLG KORRY LIGHT ASSEMBLY BROKEN. REPLACED KORRY LIGHT DRAWER ASSEMBLY & RELAMPED. OPERATIONS CHECKED GOOD.

Part: EEC — FAULTY (RT ENGINE) · airframe 64,060 hrs · 23,031 cycles

CLT FLT 1857 EN-ROUTE CLT TO MCO. DURING TAKEOFF RT ENG WOULD NOT DEVELOP TAKEOFF THRUST, RT ENG EEC LIGHT ON, REJECTED TAKEOFF APPROXIMATELY 80KTS. REPLACED RT ENG EEC. VENDOR SHOP FINDINGS, THIS EEC WAS EXCHANGED FOR ANOTHER AT THE VENDOR.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

PHL - AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY, OPERATIONS CHECKED GOOD.

Part: STOP FITTING — BROKEN (CARGO DOOR) · airframe 61,765 hrs · 22,292 cycles

AFT CARGO DOOR UPPER FWD DOOR STOP BROKEN. REPLACED AFT CARGO DOOR UPPER FWD DOOR STOP AT BS 1420, STRINGER 19R IAW B757 AMM 52-34-02.

Part: SWITCH — FAILED (CONTROL PANEL) · airframe 62,599 hrs · 22,553 cycles

PHX WITH EMERGENCY LIGHT SWITCH IN OFF POSITION, EMERGENCY LIGHTS REMAIN ON. REPLACED EMERGENCY LIGHT PAX OXY CONTROL PANEL, SYS OPS CHECKED GOOD. UNIT FAILED PRELIMINARY FUNCTIONAL TESTING DUE TO THE EMERGENCY SWITCH INTERMITTENTLY MEASURED OPEN AT THE OFF POSITION. INOPERATIVE LAMP AT THE UNARMED INDICATION. LIGHT PLATE BACKLIGHTING IS DIM. REPLACED THE EMERGENCY SWITCH, THE UNARMED INDICATION LAMPS & THE LIGHT PLATE BACKLIGHTING LAMPS. UNIT PASSED ALL FUNCTIONAL TESTS & IS OK FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,344 hrs · 22,190 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON UPPER T-CAP OF FLOORBEAM AT BS1682, LBL56. REPAIRED FLOORBEAM UPPER T-CAP AT BS1682, LBL56 IAW EA 104864.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,344 hrs · 22,190 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR PAN BETWEEN BS1581 TO BS1720 & BETWEEN RBL50 TO LBL50. REPLACED FLOOR PAN BETWEEN BS1581 TO BS1720 & BETWEEN RBL50 TO LBL50 IAW EA 104864.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,344 hrs · 22,190 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SILL SUPPORT CHANNEL BETWEEN BS1661 TO BS1680, LBL58. REPAIRED SILL SUPPORT CHANNEL BETWEEN BS1661 TO BS1680, LBL58 IAW DWG 146N5230 & SRM 51-40-02.

Part: SKIN PANEL — DEBONDED (VERTICAL STAB) · airframe 61,344 hrs · 22,190 cycles

C4 CHECK - AREA OF DISBOND ON LT SIDE OF VERTICAL STABILIZER FWD TORQUE BOX PANEL AT FIN STA 220, 4" AFT OF PANEL L/E. INSTALLED SERVICEABLE LT VERTICAL STABILIZER FWD TORQUE BOX PANEL IAW BOEING DWG 175N2001 & SRM 51-40-02.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,344 hrs · 22,190 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON STIFFENER AT BS1715 BETWEEN LBL33 TO LBL39. REPAIRED STIFFENER AT BS1715 BETWEEN LBL33 TO LBL39 IAW SRM 51-40-02.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,344 hrs · 22,190 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON STIFFENER AT BS1715 BETWEEN RBL33 TO RBL39. REPAIRED STIFFENER AT BS1715 BETWEEN RBL33 TO RBL39 IAW SRM 51-40-02.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,344 hrs · 22,190 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CREASE BEAM BETWEEN BS1254.5 TO BS1282, RBL54.9. REPAIRED CREASE BEAM BETWEEN BS1254.5 TO BS1282, RBL54.9 IAW EA 104901 & 104902.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,344 hrs · 22,190 cycles

C4 CHECK - CORROSION ON FLOORBEAM AT BS 1640, LBL 58. REPAIRED FLOORBEAM IAW SRM 53-00-51-2R & EA 68897.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,344 hrs · 22,190 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON R1 DRAIN PAN FLOOR SUPPORT BETWEEN BS324 TO BS345, S31R. REPLACED R1 DRAIN PAN FLOOR SUPPORT BETWEEN BS324 TO BS345, S31R IAW SRM 51-40-02.

Part: SIGN — BROKEN (CABIN)

CLT - EMERGENCY EXIT LIGHTED SIGN AT THE L4 DOOR BROKE. REMOVED AND REPLACED EMERGENCY EXIT LIGHTED SIGN AT THE L4 DOOR.

Part: SIGN — DAMAGED (CABIN) · airframe 60,016 hrs · 21,774 cycles

PHX - ACFT R4 DOOR LOWER EXIT SIGN DAMAGED AFT DOOR. REPLACED LOWER EXIT SIGN ASSY, OPS CHECK GOOD. R4 DOOR.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 59,394 hrs · 21,583 cycles

PHX - ACFT R4 EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY (M736). OPS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 58,921 hrs · 21,452 cycles

GLA - DOOR L4 EMERGENCY LIGHT LENS MISSING. REPLACED THE EMERGENCY LIGHT LENSE OF THE L4 DOOR.

Part: LENS — MISSING (CABIN) · airframe 58,921 hrs · 21,452 cycles

GLA - DOOR L4 EMERGENCY EXIT LENS MISSING. REPLACED THE L4 (LOWER) EMERGENCY EXIT LIGHT ASSEMBLY, AND BATTERY CHARGER M737.

Part: CABLE — OUT OF POSITION (GIRT BAR) · airframe 57,679 hrs · 21,116 cycles

PHX - 4R EMERGENCY DOOR WON'T ARM. REPOSITIONED GIRT BAR CABLE. OPS CHECK NORMAL. CABLE CLEARED FROM OBSTRUCTION.

Part: ACTUATOR — DAMAGED (LE FLAPS) · airframe 57,320 hrs · 20,994 cycles

FLT 1033, DEPARTING, BOTH FLAP POINTERS ON 1/2 WITH THE FLAP LEVER UP. L/E SLAT DISAGREE DISPLAYED. THE CREW WAS ABLE TO GET THE LIGHT TO EXTINGUISH, AND CONTINUED TO CLT. UPON ARRIVAL TO CLT, AN EMERGENCY WAS DECLARED AND A NO FLAPS LANDING WAS MADE. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. FOUND NR 5 SLAT INBD ACTUATOR AT FAULT (MAKING GRINDING NOISES WHEN TURNED). REPLACED INBD NR 5 SLAT ROTARY ACTUATOR. L/E SLAT SYSTEM TESTED GOOD. FAILED AS RECEIVED TEST DUE TO LOW EFFICIENCY & LOCK OUT AT START-UP. 1 PLANETARY PIN, 3 WASHERS & 160 NEEDLE BEARINGS CORRODED REQUIRING REPLACMENT. PLANETARY CAGE REQUIRES RE-WORK, TORQUE LIMITER REQUIRES RESHIMMING.

Part: ACTUATOR — NOISY (SLATS) · airframe 57,320 hrs · 20,994 cycles

FLT 1033 , BOTH FLAP POINTERS ON 1/2 WITH THE FLAP LEVER UP. L/E SLAT DISAGREE DISPLAYED. CREW WAS ABLE TO GET THE LIGHT TO EXTINGUISH, AND CONTINUED TO DESTINATION. ON ARRIVAL, AN EMERGENCY WAS DECLARED AND A NO FLAPS LANDING WAS MADE. LANDED WITHOUT FURTHER INCIDENT. FOUND NR 5 SLAT OTBD ACTUATOR AT FAULT (MAKING GRINDING NOISES WHEN TURNED). REPLACED OTBD NR 5 SLAT ROTARY ACTUATOR. L/E SLAT SYSTEM TESTED GOOD. DAMAGED ACTUATOR FUNCTIONED WITHIN MFG SPECS AS RECEIVED. ALL COMPONENTS IN SERVICEABLE CONDITION. RE-SHIMMED TORQUE LIMITER AS PRECAUTIONARY MEASURE.

Part: TRANSMITTER — FAULTY (LE SLAT) · airframe 57,313 hrs · 20,991 cycles

CLT FLT 1032 EN-ROUTE CLT TO SJU. ON DEPARTURE, BOTH FLAP POINTERS ON 1/2 WITH THE FLAP LEVER UP. L/E SLAT DISAGREE DISPLAYED. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO FIELD CLT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED L/E SLAT PDU POSITION TRANSMITTER TS5048. OPERATIONALLY CHECKED OK. VENDOR SHOP FINDINGS: FAILS INSULATION TEST. UNIT RECEIVED WITHOUT WINDOW (P/T). UNIT HAS HUMIDITY INSIDE. VACUUM BAKED UNIT TO ELIMINATE THE HUMIDITY. REPLACED THE WINDOW. F/T'D.

Part: BOLT — LOOSE (LT ENGINE) · airframe 57,192 hrs · 20,945 cycles

CLT FLT 885 EN ROUTE CLT TO CUN. LEFT ENGINE LO OIL PRESS LIGHT. LEFT ENGINE OIL QUANTITY 0. COMPLIED WITH QRH PROCEDURE TO SHUT DOWN LEFT ENGINE. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE. ALL ENGINE OIL EXITED THROUGH SCAVENGE TUBE BEHIND RADIAL DRIVESHAFT THAT SEPARATED FROM FLANGE. THE TUBE SEPARATED DUE TO FLANGE BOLTS THAT VIBRATED LOOSE.

Part: APU — FAILED (APU BAY)

PHL FLT 1199 AT GATE, PRIOR TO PHL - PHX FLIGHT. APU AUTO SHUTDOWN FAULT LIGHT ILLUM, EICAS MSG FAULT DISPLAYED. HAZE & SMELL THROUGHOUT CABIN PRIOR TO SHUTDOWN. MAINTENANCE FOUND THAT APU HAD MAJOR FAIL. REPLACED THE APU ASSY.

Part: PUSHROD — OUT OF ADJUST (EMERGENCY DOOR) · airframe 56,501 hrs · 20,711 cycles

PHL FLT 751 EN-ROUTE BRU TO PHL. EICAS MESSAGE EMERGENCY DOOR DISPLAYED STEADY AND EMER DOOR OPEN LIGHT ILLUM STEADY WITH DOOR CLOSED. LIGHT WENT OUT DURING DESCENT THROUGH FL180. ADJUSTED ARMING ROD. DOOR ARMS NORMALLY.

Part: COUPLING — OUT OF POSITION (AC PACK)

CLT FLT 806 EN ROUTE CUN TO PHL. THE FLIGHT DEPARTED CUN WITH THE LEFT AIR CONDITIONING PACK ON MEL. DURING CRUISE, THE CREW STATES: "COULD NOT HOLD PRESSURIZATION IN AUTO, WENT TO MANUAL. ALSO COULD NOT CONTROL UNTIL FL 7000. L&R DUCT PRESSURE 40-50 PSI." THE FLIGHT DECLARED AN EMERGENCY, DESCENDED QUICKLY TO FL 170, AND THEN DIVERTED INTO CLT. MAINTENANCE FOUND DUCT COUPLING OFF RT PACK. REPLACED COUPLING & CLAMPS. LEAK CHECKED, NO LEAKS NOTED. ACCOMPLISHED EXCESSIVE CABIN PRESSURE LEAK TEST. CHECK'S GOOD. OK FOR SERVICE.

Part: LOCK — UNSECURE (GIRT BAR) · airframe 56,137 hrs · 20,607 cycles

SJU - CATERING CREW REPORTED GIRT BAR DOOR 1R LOOSE FROM CASE. FOUND THE GIRT BAR END CAP FELL OFF. RE-INSTALLED END CAP. VERIFIED SLIDE 1R OPERATION NORMAL.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - CORROSION ON UPPER CHORD OF CREASE BEAM AT BS 640, LBL 64.4. REPLACED UPPER CHORD OF CREASE BEAM AT BS 640, LBL 64.4 IAW B757 53-30-13 DETAIL VIII, 51-40-02 FIG 12.

Part: WEB — CORRODED (FUSELAGE) · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - CORROSION WEB TOP AT BS 1420, RBL 18 IN AFT PIT. REPLACED WEB TOP AT BS 1420 RBL 18 IAW B757 SRM 51-40-02 FIG 8.

Part: STRUCTURE — CRACKED (NR 1 PYLON) · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - NR 1 PYLON, INBOARD MID CHORD, LOWER FASTENER HOLE CRACKED. REPAIRED NR 1 PYLON INBOARD LOWER FASTENER HOLE OF MID CHORD FITTING IAW EO 5496R042.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - LEVEL 2 GALVANIC CORROSION ON UPPER CHORD OF INTERCOSTAL BETWEEN BS1361 TO BS 1377, RBL 425. REPLACED UPPER CHORD OF INTERCOSTAL BETWEEN BS 1361 TO BS 1377, RBL 425 IAW B757 SRM SRM 51-40-02-0G.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - CRACK ON FLOOR PANEL INTERCOSTAL ATTACH ANGLE BETWEEN BS 1320 TO BS 1340, BL 0. REPLACED FLOOR PANEL INTERCOSTAL ATTACH ANGLE BETWEEN BS 1320 TO BS 1340, BL 0 IAW B757 SRM 51-10-02 PAR 4 FIG 7 & 8.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - CRACK ON FLOOR PANEL ATTACH ANGLE BETWEEN BS 1620 TO BS 1640, BL 0. REPLACED FLOOR PANEL ATTACH ANGLE BETWEEN BS 1620 TO BS 1640, BL 0 IAW B757 SRM 51-40-02 FIG 5.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL ATTACH ANGLE CHORD BETWEEN BS 1280 TO BS 1310, RBL 25. REPLACED INTERCOSTAL ATTACH ANGLE CHORD BETWEEN BS 1280 TO BS 1310, RBL 25 B757 SRM 51-40-02.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - CORROSION ON FLOOR PANEL ATTACH ANGLE AT BS 729 BETWEEN LBL 65 TO LBL 69. REPLACED FLOOR PANEL ATTACH ANGLE AT BS 729 BETWEEN LBL 65 TO LBL 69 IAW B757 SRM 51-40-02-0G PARA 9.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - CORROSION ON FLOOR PANEL ATTACH ANGLE AT BS 690.40 BETWEEN LBL 65 TO LBL 69. REPLACED FLOOR PANEL ATTACH ANGLE AT BS 690.40 BETWEEN LBL 65 TO LBL 69 IAW B757 SRM 51-40-02-0G PARA 9.

Part: SILL — CORRODED (FUSELAGE) · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - CORROSION AT L-2 DOOR CUTOUT LOWER MAIN SILL ON CHORD BETWEEN BS 686 TO BS 729, WL 208, LBL 64. REPLACED L-2 DOOR CUTOUT LOWER MAIN SILL ON CHORD IAW B757 SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - CORROSION ON INTERCOSTAL SUPPORT BETWEEN BS 680 TO BS 700, LBL 58.22. REPLACED INTERCOSTAL SUPPORT BETWEEN BS 680 TO BS 700, LBL 58.22 IAW B757 SRM 51-40-02 FIG 12.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - CORROSION ON FLOORBEAM AT BS 740 BETWEEN LBL 45 TO LBL 58. REPAIRED FLOORBEAM AT BS 740 BETWEEN LBL 45 TO LBL 58 IAW B757 SRM 53-00-51-2R-3 & 53-00-51 DETAIL III.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - CORROSION ON FLOORBEAM AT BS 700, LBL 45.5 TO LBL 58.2. REPAIRED FLOORBEAM AT BS 700, LBL 45.5 TO LBL 58.2 IAW B757 SRM 53-00-51-1A-1.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - DELAMINATION ON LEFT FORWARD VERTICAL STABILIZER PANEL BETWEEN FSS 120-129 & FSS 155-175 APPROX 7 INCHES FROM LEADING EDGE OF PANEL. PANEL REMOVED SENT TO OUTSIDE VENDOR FOR REPAIR & REINSTALLED IAW B757 SRM 51-40-02-0G PAR 4 & 7 FIG 3, 6, 7, 8 & 12.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - CORROSION ON INTERCOSTAL SUPPORT BETWEEN BS 720 TO BS 740, LBL 64. REPLACED INTERCOSTAL SUPPORT BETWEEN BS 720 TO BS 740, LBL 64 IAW B757 SRM 51-40-02 FIG 12.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - CORROSION ON INTERCOSTAL SUPPORT AT BS 683 BETWEEN LBL 45.5 TO LBL 58.22. REPLACED INTERCOSTAL SUPPORT AT BS 683 BETWEEN LBL 45.5 TO LBL 58.22 IAW B757 SRM 51-40-02 FIG 12.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - CORROSION ON INTERCOSTAL SUPPORT BETWEEN BS 720 TO BS 740, LBL 64. REPLACED INTERCOSTAL SUPPORT BETWEEN BS 720 TO BS 740, LBL 64 IAW B757 SRM 51-40-02 FIG 12.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - CORROSION ON INTERCOSTAL SUPPORT BETWEEN BS 680 TO BS 700, LBL 58.22. REPLACED INTERCOSTAL SUPPORT BETWEEN BS 680 TO BS 700, LBL 58.22 IAW B757 SRM 51-40-02 FIG 12.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - CORROSION ON INTERCOSTAL SUPPORT BETWEEN BS 700 TO BS 720, LBL 61. REPLACED INTERCOSTAL SUPPORT BETWEEN BS 700 TO BS 720, LBL 61 IAW B757 SRM 51-40-02 FIG 12 & 51-10-02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,078 hrs · 20,592 cycles

C3 CHECK - CORROSION ON INTERCOSTAL SUPPORT BETWEEN BS 700 TO BS 720, LBL 61. REPLACED INTERCOSTAL SUPPORT BETWEEN BS 700 TO BS 720, LBL 61 IAW B757 SRM 51-40-02 FIG 12 & 51-10-02.

Part: SLIDING WINDOW — OVERHEATED (COCKPIT)

PHL - THE LEFT SLIDING WINDOW HAD BUBBLES FORMING IN THE LOWER CENTER SECTION. IT WAS ALSO NOTED THAT THE LOWER LEFT CORNER OF THE SLIDING WINDOW WAS EXTREMELY HOT. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND, NUMBER TWO SLIDING WINDOW.

Part: CLAMP — LOOSE (RT A/C PACK)

PHL FLT 1528 - EN ROUTE CLT TO PHL. DURING CLIMB, THE FLIGHT DECK CREW COMPLAINED OF EXCESS NOISE IN THE COCKPIT. THE LEFT PACK WAS TURNED OFF. THEN THE AIRCRAFT INDICATED EXCESS CABIN ALTITUDE. THE FLIGHT WENT TO 13,000 FEET AND DECLARED AN EMERGENCY WITH ATC. THE FLIGHT CONTINUED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. FOUND BOOT AND CLAMP LOOSE ON RT PACK OUTPUT DUCT, JUST AFT OF CHECK VALVE ASSEMBLY IN PACK BAY. RESECURED BOOT AND CLAMP.

Part: PANEL — WARPED (SPOILER) · airframe 51,500 hrs · 19,375 cycles

CLT - C2 - MAJOR REPAIR - NR 5 SPOILER PANEL IS WARPED. REPLACED NR 5 SPOILER IAW JOB CARD 19L55027003.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 51,500 hrs · 19,375 cycles

CLT - C2 - MAJOR REPAIR - CABIN SEAT TRACK DAMAGED BETWEEN BS 850 TO BS 882, RBL 45. REPAIRED CABIN SEAT TRACK BETWEEN BS 850 TO BS 882, RBL 45 IAW B757 SRM 53-00-25 REPAIR 3 & EA 101868.

Part: LIGHT — INOPERATIVE (EVAC SLIDE)

BRU - THE 2R SLIDE ARMED LIGHT NOT ILLUMINATED WITH GIRT BAR IN PLACE. MAINTENANCE RELAMPED. CHECKS SATISFACTORY.

Part: SLIDE — LOW PRESSURE (L1 DOOR)

THE L1 DOOR EMERGENCY ESCAPE SLIDE PRESSURE WAS FOUND OUT OF THE GREEN BAND. MX REPLACED THE L1 DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE.

Part: MODULE — MALFUNCTIONED (SPOILER) · airframe 27,808 hrs

CLT FLT 811, ENROUTE PHL TO CUN. WHILE IN CRUISE FLT, THE SPOILER LIGHT ILLUMINATED, ALONG WITH EICAS MESSAGE "SPOILER". THE SPOILERS WERE SELECTED DOWN AT THE TIME. AFTER DISCUSSIONS WITH OPERATIONS, THE DECISION WAS MADE TO DIVERT TO CLT. THE FLT LANDED IN CLT WITHOUT FURTHER INCIDENT. MX REPLACED THE SPOILER CONTROL MODULE M532. OPS CHECK OK.

Part: INDICATOR — INOPERATIVE (COCKPIT)

PHL FLT 798 ENROUTE PHL TO AMS. THE STANDBY ALTITUDE INDICATOR FAILED ABOUT 45 MINUTES AFTER DEPARTURE. THE DECISION WAS MADE TO RETURN TO PHL. THE FLIGHT RETURNED WITHOUT FURTHER INCIDENT. MX REPLACED THE STANDBY ALTITUDE INDICATOR. OPS CHECKS OK.

Part: INVERTER — INOPERATIVE (COCKPIT)

PHL FLT 798 ENROUTE PHL TO AMS. THE STANDBY ATTITUDE INDICATOR FAILED ABOUT 45 MINUTES AFTER DEPARTURE. THE DECISION WAS MADE TO RETURN TO PHL. THE FLIGHT RETURNED WITHOUT FURTHER INCIDENT. MX REPLACED THE STANDBY HORIZON INVERTER. OPS CHECKS OK.

Part: CONNECTOR — DAMAGED (GOVERNOR)

PHL FLT 1209 PHL TO SXM - DURING TAKEOFF ROLL, TNE NR 2 ENG WOULD NOT DEVELOP TAKEOFF POWER. THE CREW ABORTED THE TAKEOFF AT 60 KNOTS AND RETURNED TO THE GATE. MAINTENANCE REPAIRED THE CONNECTOR ON THE FUEL FLOW GOVERNOR SOLENOID. OPERATIONALLY CHECKS OK. (S)

Part: CIRCUIT BREAKER — MALFUNCTIONED (ELECTRICAL SYS)

FLL FLT 811 EN ROUTE PHL TO CUN. DURING CRUISE, RECEIVED A LT UTILITY BUS OFF MESSAGE. ATTEMPTS TO RESET WERE UNSUCCESSFUL. THE CREW DECIDED TO STOP IN FLL TO HAVE MAINTENANCE REPAIR THE ACFT. THE FLIGHT DIVERTED TO FLL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LFT DC BUSS, SECTION 1 CIRCUIT BREAKER. OPERATIONALLY CHECKED OK. (S)

Part: ACTUATOR — FAILED (NLG DOOR) · airframe 43,098 hrs · 17,376 cycles

FERRY FLIGHT 9243, MCN-PHL: AFTER TAKEOFF, CREW RECEIVED EICAS MESSAGE GEAR DISAGREE AND GEAR DOORS. RETURNED TO MCN. MAINTENANCE REPLACED THE NLG DOOR ACTUATOR. NO FURTHER FAULTS.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 297, RBL 5 - RBL 16, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 297, RBL 5 - RBL 16, WL 208 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 310 - BS 324, LBL 19.75, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 310 - BS 324, LBL 19.75, WL 208 IAW B757 SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR STRUCTURE ANGLE, BS 1640, LBL 58.22, WL 208. REPLACED CABIN FLOOR STRUCTURE ANGLE, BS 1640, LBL 58.22, WL 208 IAW B757 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOORBEAM UPPER CHORD, BS 324, LBL 10 - RBL 42, WL 208. REPAIRED CABIN FLOORBEAM UPPER CHORD, BS 324, LBL 10 - RBL 42, WL 208 IAW B757 SRM 51-70-12.

Part: FLOOR SUPPORT — CORRODED (ZONE 200 - FUSEL) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 365.25 - BS 377.7, LBL 61, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 365.25 - BS 377.7, LBL 61, WL 208 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR ANGLE, BS 310.5 - BS 365.20, RBL 65, WL 208. REPLACED CABIN FLOOR ANGLE, BS 310.5 - BS 365.20, RBL 65, WL 208 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR ANGLE, BS 1661 - BS 1681, RBL 9.2, WL 208. REPLACED CABIN FLOOR FLOOR ANGLE, BS 1661 - BS 1681, RBL 9.2, WL 208, WL 208 IAW B757 SRM 51-40-02.

Part: STRAP — CRACKED (ZONE 200) · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - CRACKED CABIN FLOOR STABILIZATION STRAP, BS 1681, RBL 24.75, WL 204. REPAIRED CABIN FLOOR STABILIZATION STRAP, BS 1681, RBL 24.75, WL 204 IAW USAIRWAYS TR 53-.35-01.

Part: CHANNEL — CORRODED (ZONE 200 - FUSEL) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR INTERCOSTAL CHANNEL, BS 310.5 - BS 324, BL 0, WL 208. REPLACED CABIN FLOOR INTERCOSTAL CHANNEL, BS 310.5 - BS 324, BL 0, WL 208 IAW B757 SRM 51-40-02.

Part: STRAP — CRACKED (ZONE 200) · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - CRACKED CABIN FLOOR STABILIZATION STRAP, BS 1661, LBL 24.75, WL 204. REPAIRED CABIN FLOOR STABILIZATION STRAP, BS 1661, LBL 24.75, WL 204 IAW USAIRWAYS TR 53-.35-01.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN INTERCOSTAL FILLER, BS 295 - BS 310.5, RBL 2, WL 208. REPLACED CABIN INTERCOSTAL FILLER, BS 295 - BS 310.5, RBL 2, WL 208 IAW BOEING DRAWING 141N5160.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN INTERCOSTAL WEB, BS 1661 - BS 1681, RBL 9.2, WL 208. REPLACED CABIN INTERCOSTAL WEB, BS 1661 - BS 1681, RBL 9.2, WL 208 IAW B757 SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN SUPPORT ANGLE, BS 1676, LBL 58.22. REPLACED CABIN SUPPORT ANGLE, BS 1676, LBL 58.22 IAW B757 SRM 51-40-02.

Part: SKIN — CORRODED (BS 750-780) · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON FUSELAGE SKIN, BS 750 - BS 780, S18L - S21L. REPAIRED FUSELAGE SKIN, BS 750 - BS 780, S18L - S21L IAW B757 SRM 53-00-01 FIGURE 201.

Part: SUPPORT ANGLE — CORRODED (ZONE 200) · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON THE R4 DOOR CUT LOWER SILL THRESHOLD FORWARD SUPPORT ANGLE CHANNEL CLIP, BS 1640, RBL 58.22. REPLACED THE R4 DOOR CUT LOWER SILL THRESHOLD FORWARD SUPPORT ANGLE CHANNEL CLIP, BS 1640, RBL 58.22 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 345 - BS 360.25, RBL 58.22, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 345 - BS 360.25, RBL 58.22, WL 208 IAW B757 SRM 51-40-02.

Part: SUPPORT FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON GALLEY SUPPORT FITTING, BS 324 - BS 345, RBL 1.0, WL 208. REPLACED GALLEY SUPPORT FITTING, BS 324 - BS 345, RBL 1.0, WL 208 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 345 - BS 377.7, BL 0, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 345 - BS 377.7, BL 0, WL 208 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 324 - BS 345, RBL 58.22, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 324 - BS 345, RBL 58.22, WL 208 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 324 - BS 345.5, LBL 19.75, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 324 - BS 345.5, LBL 19.75, WL 208 IAW B757 SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (ZONE 200) · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON THE R4 DOOR CUT LOWER SILL THRESHOLD MID SUPPORT ANGLE, BS 1671, RBL 58.22. REPLACED THE R4 DOOR CUT LOWER SILL THRESHOLD MID SUPPORT ANGLE, BS 1671, RBL 58.22 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 324 - BS 345, LBL 33, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 324 - BS 345, LBL 33, WL 208 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL UPPER TEE FITTING, BS 297, RBL 20, WL 208. REPLACED INTERCOSTAL UPPER TEE FITTING, BS 297, RBL 20, WL 208 IAW B757 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOORBEAM, BS 377.7, LBL 48.0, WL 208. REPAIRED CABIN FLOORBEAM, BS 377.7, LBL 48.0, WL 208 IAW USAIRWAYS TYPICAL REPAIR 53-15-01 AND EA 98947.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOORBEAM, BS 365.25, RBL 10 - RBL 65, WL 208. REPAIRED CABIN FLOORBEAM, BS 365.25, RBL 10 - RBL 65, WL 208 IAW USAIRWAYS TYPICAL REPAIR 53-15-01 AND EA 98947.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON FLOORBEAM, BS 310.5, LBL 19 - RBL 42, WL 208. REPAIRED FLOORBEAM, BS 310.5, LBL 19 - RBL 42, WL 208 IAW B757 SRM 51-70-12.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 338, LBL 33 - LBL 38, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 338, LBL 33 - LBL 38, WL 208 IAW B757 SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (ZONE 200) · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - CORROSION ON THE L4 DOOR CUT LOWER SILL SUPPORT ANGLE, BS 1640 - BS 1676, LBL 58.22. REPLACED THE L4 DOOR CUT LOWER SILL SUPPORT ANGLE, BS 1640 - BS 1676, LBL 58.22 IAW B757 SRM 51-40-02.

Part: CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR STRUCTURE CHANNEL, BS 310 - BS 324, RBL 42, WL 208. REPLACED CABIN FLOOR STRUCTURE CHANNEL, BS 310 - BS 324, RBL 42, WL 208 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 377.7 - BS 395, RBL 58.22, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 377.7 - BS 395, RBL 58.22, WL 208 IAW B757 SRM 51-40-02.

Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON FITTING, BS 365.25 - BS 377.7, RBL 15.0, WL 208. REPLACED FITTING, BS 365.25 - BS 377.7, RBL 15.0, WL 208 IAW B757 SRM 51-10-02, 51-40-05 AND 51-40-02.

Part: PANEL — CRACKED (NR 1 SLAT) · airframe 43,098 hrs · 17,375 cycles

MCN - MAJOR REPAIR - C4 CHECK - LEFT WING NR 1 SLAT COVE PANEL CRACKED, WS 736. REPLACED LEFT WING NR 1 SLAT COVE PANEL, WS 736 IAW B757 SRM 51-40-02.

Part: PROBE — FAILED (TAT) · airframe 42,834 hrs · 17,307 cycles

FLIGHT 724, PHL-SNN: TAT PROBE HEAT FAILED. RETURNED TO PHL. MAINTENANCE REPLACED THE TAT PROBE. NO FURTHER FAULTS.

Part: COMPUTER — FAILED (EICAS) · airframe 42,795 hrs · 17,298 cycles

FLIGHT 739, LIS-PHL: AFTER TAKEOFF, BOTH EICAS COMPUTERS FAILED. RETURNED TO LIS. MAINTENANCE REPLACED BOTH EICAS COMPUTERS.

Part: FILTER — DETERIORATED (CABIN) · airframe 42,644 hrs · 17,274 cycles

FLIGHT 725, SNN-PHL: AFTER TAKEOFF, FLIGHT ATTENDANTS REPORTED INSULATION LIKE MATERIAL COMING FROM OVERHEAD VENTS. FLIGHT RETURNED TO SNN. MAINTENANCE FOUND THAT THE LEFT RECIRC FILTER HAD BROKEN DOWN, ALLOWING MATERIAL FROM FILTER INTO THE DUCT SYSTEM. THE FILTER WAS REPLACED AND THE DUCT SYSTEM CLEARED OF EXCESS DEBRIS.

Part: SUPPORT — CORRODED (BS 720-740) · airframe 41,864 hrs · 41,864 cycles

BS 720 - 740 RBL 62.45 HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-30-15, 51-10-02, 51-40-02, DEFECT SIZE: 6 X 1 INCH.

Part: ANGLE — CORRODED (BS 719-745) · airframe 41,864 hrs · 41,864 cycles

BS 719.6 - 745.6 RBL 62.45 ANGLE HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-30-15, 51-10-02, 51-40-02, DEFECT SIZE: 6 X 1 INCHES.

Part: SUPPORT — CORRODED (BS 680-700) · airframe 41,864 hrs · 41,864 cycles

BS 680-700, RBL 62.45, GUTTER SUPPORT ASSEMBLY HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-30-15, 51-10-02; 51-40-02, DEFECT SIZE: 4 X 1 INCH.

Part: APU — FAILED (APU BAY) · airframe 41,250 hrs · 16,857 cycles

FLIGHT 1026, TPA-CLT: ON TAXI OUT, CABIN BEGAN TO FILL WITH SMOKE AND THE LAV SMOKE DETECTORS BEGAN TO SOUND. FLIGHT RETURNED TO GATE. MAINTENANCE FOUND THE APU HAD CONTAMINATED THE A/C SYSTEM WITH OIL. ACCOMPLISHED DE-CONTAMINATION OF AIR DISTRIBUTION SYSTEM. NO FURTHER FAULTS.