N935UW

Part: LEVER — OBSTRUCTED (L4 DOOR) · airframe 72,284 hrs · 27,239 cycles

AIRCRAFT WAS GROUNDED. ARMING LEVER AT DOOR 4L DIFFICULT TO OPERATE. MAINTENANCE FOUND L4 DOOR, RETRACTABLE DOOR DECAL FOLDED IN HALF. REMOVED AND REPLACED DECAL; ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: LANYARD — UNSECURE (R1 DOOR SLIDE) · airframe 72,028 hrs · 27,167 cycles

LANYARD HANGING OUT OF SLIDE DOOR 1R. PACKED THE GIRT BAR LANYARD IAW AMM 25-66-00-001.

Part: GIRT BAR — OBSTRUCTED (L4 DOOR) · airframe 70,818 hrs · 26,875 cycles

AIRCRAFT WAS NOT GROUNDED, 4L DOOR KNUCKLE WILL NOT MOVE DURING ARMING OF DOOR. CLEANED DEBRIS FROM GIRT BAR AND ACCOMPLISHED A SATISFACTORY OPS CHECK.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 70,532 hrs · 26,801 cycles

AIRCRAFT WAS NOT GNDED. 4R DOOR WILL NOT ARM. REMOVED DEBRIS FROM GIRT BAR.

Part: LATCH — OBSTRUCTED (ENTRY DOOR) · airframe 70,408 hrs · 26,769 cycles

AIRCRAFT WAS NOT GNDED. EICAS, RT AFT ENTRY DOOR WHILE DOOR IS CLOSED. TUCKED SLIDE LANYARD BACK INTO RAFT AREA. REMOVED LOOSE HARDWARE FOUND IN SLIDE GIRT BAR LATCH. OPERATIONAL CHECK OF DOOR INDICATIONS GOOD. ACFT OK FOR SERVICE. SEE AALA 201605069006 FOR ADDITIONAL PART.

Part: MECHANISM — OBSTRUCTED (ZONE 800) · airframe 70,408 hrs · 26,769 cycles

AIRCRAFT WAS NOT GNDED. RT AFT SLIDE WILL NOT ARM, ECAS MSG. CLEANED DEBRIS FROM ARM & DISARM MECHANISM & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 52-71-00.

Part: LANYARD — MISROUTED (EVAC SLIDE) · airframe 70,408 hrs · 26,769 cycles

AIRCRAFT WAS NOT GNDED. EICAS, RT AFT ENTRY DOOR WHILE DOOR IS CLOSED. TUCKED SLIDE LANYARD BACK INTO RAFT AREA. REMOVED LOOSE HARDWARE FOUND IN SLIDE GIRT BAR LATCH. OPERATIONAL CHECK OF DOOR INDICATIONS GOOD. ACFT OK FOR SERVICE. SEE AALA 201605069007 FOR ADDITIONAL PART.

Part: RESERVOIR — LOW (L1 DOOR) · airframe 70,374 hrs · 26,757 cycles

AIRCRAFT WAS NOT GNDED. L1 DOOR EMER POWER RESERVOIR PRESS LOW. REPLACED 1L DOOR EMER POWER RESERVOIR IAW AMM 52-11-30-401.

Part: FASTENER — WRONG PART (L1 DOOR) · airframe 70,286 hrs · 26,733 cycles

AIRCRAFT WAS NOT GNDED. FLIGHT ATTENDANT ADVISED 1L DOOR VERY HARD TO ARM. FOUND INCORRECT HARDWARE INSTALLED ON DISARM INDICATOR FLAP CAUSING INTERFERENCE WITH LEVER. INSTALLED CORRECT HARDWARE & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 52-11-00.

Part: ROD — OUT OF ADJUST (R1 DOOR) · airframe 70,282 hrs · 26,730 cycles

AIRCRAFT IN BASE MX. R1 DOOR DISARM HANDLE DOES NOT TRAVEL ALL THE WAY TO DISARM POSITION, WHEN DOOR IS OPEN WITH EXTERNAL HANDLE. ADJUSTED HANDLE INDICATOR ROD & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 52-11-02-41.

Part: ADAPTER — CRACKED (RT WING) · airframe 70,282 hrs · 26,730 cycles

AIRCRAFT IN BASE MX. RT WING WINGLET ADAPTER AT WBL 740, UPPER LE CRACKED NEAR RIVET HOLES. REPAIRED ADAPTER IAW EA 259332.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 70,282 hrs · 26,730 cycles

AIRCRAFT IN BASE MX. CORROSION ON MAIN CABIN FLOOR CHANNEL, BETWEEN BS 1300 & 1320 AT LBL 22. REPLACED FLOOR CHANNEL IAW SRM 51-40-02 & DWG 46N5281.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 70,282 hrs · 26,730 cycles

AIRCRAFT IN BASE MX. CORROSION ON CABIN FLOOR SEAT TRACK, BETWEEN BS 1320 & 1350 AT LBL 24.75. REPAIRED SEAT TRACK IAW SRM 53-00-52-2R PROCEDURE 1 & SRM 51-40-02.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 69,517 hrs · 26,532 cycles

AIRCRAFT WAS NOT GNDED. L3 DOOR FLIGHT ATTENDANT SEAT EMER FLASHLIGHT LED LIGHT INOPERATIVE. REPLACED FLASHLIGHT & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LENS — DETACHED (CABIN) · airframe 68,612 hrs · 26,263 cycles

2R DOOR EMER LIGHT LENS DETACHED. ADJUSTED EMER LIGHT COVER LOCKING TABS OVER 2R DOOR. OPERATIONS CHECKED OK.

Part: SIGN — UNSECURE (CABIN) · airframe 68,610 hrs · 26,261 cycles

EMERGENCY EXIT SIGN AT 2R FELL FROM DOOR. RE-ATTACHED R2 DOOR EXIT SIGN LENS.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 68,338 hrs · 26,193 cycles

2L DOOR OUTBOARD FLASHLIGHT WON’T TEST. R & R BATTERY PACK 2L DOOR FLASHLIGHT. OPERATIONS CHECKED GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 67,920 hrs · 26,092 cycles

LEFT EMER LIGHT STRIP AT ROW 11 IS LIFTED UP. SECURED EMER LIGHTING STRIP AT ROW 11.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 67,862 hrs · 26,075 cycles

FLIGHT 1752 EN-ROUTE, DURING TAXI OUT, SINGLE ENG FLIGHT ATTENDANT REPORTED EMER EXIT LIGHTS CYCLING ON & OFF, LT & RT SIDE ALTERNATING, FLASHING. THE FLIGHT RETURNED TO GATE. REPLACED THE EMER POWER SUPPLY M730.

Part: RECEPTACLE — SHORTED (EMERGENCY LIGHT) · airframe 66,459 hrs · 25,689 cycles

FORWARD RT SIDE EMERGENCY LIGHTS INOPERATIVE AT ROWS 2DF & 3DF BULLNOSE. MAINTENANCE FOUND SHORTED LIGHT RECEPTACLE, FWD RIGHT. REPLACED LIGHT ASSY.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 66,242 hrs · 25,619 cycles

PLEASE INSPECT FIRST OFFICERS FWD WINDOW FOR DELAMINATION. REMOVED FIRST OFFICERS WINDSHIELD IAW AMM 56-11-01-004-001. INSTALLED WINDSHIELD IAW AMM 56-11-01-424-015.

Part: COVER — MISSING (EXIT SIGN) · airframe 66,003 hrs · 25,535 cycles

EMERGENCY EXIT SIGN COVER MISSING AT BOTTOM CORNER AT DOOR 1R. INSTALLED NEW EMER EXIT SIGN COVER AT DOOR 1R.

Part: SLIDE — UNSECURE (L2 DOOR) · airframe 65,697 hrs · 25,458 cycles

WHILE OPENING A DISARMED L2 DOOR THE SLIDE FELL OFF ONTO THE JET WAY WITH GIRT BAR STILL ATTACHED. REPLACED L2 DOOR ESCAPE SLIDE. THE L2 RESERVOIR ASSIST BOTTLE WAS ALSO REPLACED DUE TO DISCHARGING.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 65,131 hrs · 25,328 cycles

C1 CHECK DELAMINATION ON LT WING NR 5 SLAT TE WEDGE AT APPROX 48 INCHES FROM OTBD END. REPLACED NR 5 SLAT IAW JOB CARD 19L51027001 SLAT 5.

Part: SKIN PANEL — DELAMINATED (RT ELEVATOR) · airframe 65,131 hrs · 25,328 cycles

C1 CHECK DELAMINATION ON RT ELEVATOR UPPER SKIN PANEL AT APPROX 2 INCHES INBD OF STAB STATION 113.068. REPAIRED RT ELEVATOR UPPER SKIN PANEL IAW SRM 51-70-17 & EA 106064.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,131 hrs · 25,328 cycles

C1 CHECK LEVEL 2 EXFOLIATION CORROSION ON SUPPORT BRACKET AT BS 740 BETWEEN STRINGER 26R & 27R. REPLACED SUPPORT BRACKET AT BS 740 BETWEEN STRINGER 26R & 27R IAW SRM 51-20-01 & DWG 453N1853.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 65,131 hrs · 25,328 cycles

C1 CHECK DELAMINATION ON LT WING INBD FLAP TE WEDGE AT APPROX 64.5 INCHES FROM OTBD END & 5.875 INCHES FWD OF TE. REPAIRED LT WING INBD FLAP TE IAW SRM 57-53-01-2R-1 & 51-70-10.

Part: LIFE RAFT — CHAFED (CABIN) · airframe 65,131 hrs · 25,328 cycles

C1 CHECK LIFE RAFT BETWEEN DOORS 3L & 3R LACING IS CHAFED. REPLACED LIFE RAFT ON JOB CARD 19C2502100100.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 65,131 hrs · 25,328 cycles

C1 CHECK DELAMINATION ON RT VERTICAL STABILIZER LOWER TORQUE BOX PANEL AT FSS 220 APPROX 4 INCHES FROM LE OF PANEL. REPLACED RT VERTICAL STABILIZER LOWER TORQUE BOX PANEL AT FSS 220 IAW DWG 175N2001.

Part: SEAL — OUT OF POSITION (LT ENGINE)

CLT FLT 706 EN-ROUTE MCO TO CLT. DURING CLIMB OUT, THE LT ENG N1 EICAS VIBRATION WAS HIGH, READING 2.8. ENG INDICATIONS WERE NORMAL. VIBRATION RETURNED BELOW 2.5 WITH THRUST LEVER RETARDED TO IDLE, ENG WAS NOT SHUT DOWN. THERE WAS NO VIBRATION FELT AT CRUISE POWER & NO AIRFRAME VIBRATION IN CLIMB OR CRUISE. UPON ARRIVAL INTO CLT, THE CREW REQUESTED EMERGENCY EQUIPMENT TO BE CALLED OUT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. FOUND SEVERAL ANNULUS FILLER SEALS OUT OF POSITION. ENSURED ALL SEALS IN CORRECT POSITION. RAN ENG & HAD A MAX OF 1.4 UNITS N1 VIBRATION.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 63,143 hrs · 24,753 cycles

CLT NR 1 PAX DOOR, DOOR 1L HANDLE DIFFICULT TO MOVE TO CLOSE. ACCOMPLISHED ADJUSTMENT OF GUIDE ARM, OPERATIONS CHECKED GOOD.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 62,841 hrs · 24,672 cycles

R, DOOR EMERGENCY LIGHT COVER BROKEN. SECURED COVER. SYS OK FOR SERVICE.

Part: LINE — CRACKED (RT ENG OIL SYS) · airframe 62,762 hrs · 24,646 cycles

RT ENGINE, SLOW OIL LEAK, AT 2 QUARTS DID PRECAUTIONARY SHUTDOWN OF ENGINE. MAINTENANCE REPLACED OIL RETURN LINE GOING TO GEARBOX.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 62,744 hrs · 24,642 cycles

EMERGENCY FLOOR TRACK LIGHTING COVER MISSING ROW 9L. REPLACED CLEAR TRACK COVER.

Part: LIGHT — UNSECURE (CABIN) · airframe 61,995 hrs · 24,446 cycles

EMERGENCY LIGHTS ROW 11, 12, ACFT LEFT NOT SECURED TO FLOOR. TRIP HAZARD. SECURED TO FLOOR TRACK AS REQUIRED.

Part: PNEUMATIC SYSTEM — CONTAMINATED (ZONE 400) · airframe 61,376 hrs · 24,293 cycles

EN-ROUTE, AN OIL SMELL WAS PRESENT IN THE CABIN, ON TAKEOFF AND DESCENT, DURING THE FERRY FLIGHT. THE RT ENGINE HIGH SPEED GEARBOX RADIAL DRIVE SHAFT OIL SEAL HAD BEEN REPLACED PRIOR TO DEPARTURE. AFTER ARRIVAL, MX INSPECTED THE RT ENGINE AND FOUND NO OIL LEAKAGE. ACCOMPLISHED CABIN ODOR T/S, NO FAULTS FOUND. ACCOMPLISHED REMOVAL OF OIL CONTAMINATION FROM AIR CONDITIONING AND PNEUMATIC SYS. ACCOMPLISHED HIGH POWER RUN, NO CABIN ODOR NOTED.

Part: GROUND WIRE — LOOSE (CABIN) · airframe 61,119 hrs · 24,214 cycles

PHL - EMERGENCY LIGHT INOP ON BULLNOSE AT 21 LEFT INTERIOR EMERGENCY LIGHT AT ROW 21 LEFT, LOOSE GROUND. FOUND GROUND TIGHTENED AS REQUIRED, OPS CHECK NORMAL.

Part: WIRE — MISROUTED (EVAC SLIDE) · airframe 60,911 hrs · 24,146 cycles

GIRT BAR CIRCUIT BREAKER ON P-11 PANEL TRIPS. TROUBLESHOT SYSTEM AND FOUND R1 DOOR SLIDE LIGHT WIRING POSITIONED INCORRECTLY. REPOSITIONED AND SECURED WIRES ON R-1 DOOR SLIDE LIGHT IAW B757 AMM 25-66-01. SYSTEM CHECKED NORMAL IAW B757 AMM 25-66-00.

Part: CONNECTOR — UNSECURE (CASBIN) · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - SEAT ROW 11DEF & 19DEF EMERGENCY LIGHT NOT WORKING. SECURED PLUG AT SEAT ROW 11 EMERGENCY LIGHT, REPLACED LIGHT ASSEMBLY HOUSING AT SEAT ROW 19 EMERGENCY LIGHT. PERFORMED OPS CHECK FOUND NORMAL IAW B757 AMM 33-51-05 & 33-51-00.

Part: SUPPORT FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FAIRING SUPPORT FRAME AT BS 800, S28L. REPAIRED FAIRING SUPPORT FRAME AT BS800, S28L IAW B757 SRM 51-10-02, 53-00-71-1A & 51-70-11.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FUSELAGE SKIN BETWEEN BS 747 TO BS 755 & BETWEEN S20L TO S22L. REPAIRED FUSELAGE SKIN BETWEEN BS 747 TO BS 755 & BETWEEN S20L TO S22L IAW EA 505208.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT BS 740, RBL 61. REPAIRED FLOORBEAM AT BS 740, RBL 61 IAW B757 SRM 53-00-51 & EA 502595.

Part: SKIN — CRACKED (TE FLAP) · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - CRACK ON RIGHT INBOARD AFT FLAP UPPER SKIN AT WBL 95. REPAIRED RIGHT INBOARD AFT FLAP UPPER SKIN AT WBL 95 IAW B757 SRM 57-53-01-0I & 51-70-04-0G.

Part: SUPPORT FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FAIRING SUPPORT FRAME AT BS 780, S27L. REPAIRED FAIRING SUPPORT FRAME AT BS780, S27L IAW B757 SRM 51-10-02, 53-00-71-1A, 51-20-01, 51-70-11.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - EMERGENCY ESCAPE PATH LIGHTS AT AFT GALLEY INOPERATIVE. REPLACED EXIT LIGHT LENS ASSEMBLY IAW B757 MM 33-51-10 ON BOTH LEFT & RIGHT AFT GALLEYS. PERFORMED TEST & FOUND NORMAL.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR STRUCTURE CHORD AT BS 1260, LBL 54.9. REPAIRED FLOOR STRUCTURE CHORD AT BS 1260, LBL 54.9 IAW B757 SRM 51-10-02, 53-00-51 & 51-70-12.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON STRINGER 21L AT BS 750. REPAIRED STRINGER 21L AT BS 750 IAW B757 SRM 53-00-03-2R & EA 505208.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FUSELAGE SKIN PANEL BETWEEN BS 766 TO BS 780 & BETWEEN S18L TO S19L. REPAIRED FUSELAGE SKIN PANEL BETWEEN BS 766 TO BS 780 & BETWEEN S18L TO S19L IAW B757 SRM 51-10-02, 53-00-01-1A & EA 505210.

Part: SLAT — DELAMINATED (RT WING) · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - DELAMINATION ON NR 7 SLAT AT WS 313.50. REPAIRED NR 7 SLAT AT WS 313.50 IAW B757 SRM 51-70-10.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON STRINGER 20L AT BS 757. REPAIRED STRINGER 20L AT BS 757 IAW B757 SRM 53-00-03-2R & EA 505208.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON STRINGER 22L AT BS 748. REPAIRED STRINGER 22L AT BS748 IAW B757 SRM 53-00-03-2R & EA 505208.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM UPPER FLANGE AT BS 345, RBL 35. REPAIRED FLOORBEAM AT BS 345 BETWEEN LBL 10 TO RBL 53 IAW B757 SRM 51-10-02, 53-00-51 & 53-00-51, 2R.

Part: WEB — CRACKED (FUSELAGE) · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - CRACK ON WEB BETWEEN BS 860 TO BS 880, LBL 45.5. REPAIRED WEB BETWEEN BS 860 TO BS 880, LBL 45.5 IAW B757 SRM 51-70-11-06.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FUSELAGE SKIN PANEL BETWEEN BS 752 TO BS 760 & BETWEEN S24L TO S25L. REPAIRED FUSELAGE SKIN PANEL BETWEEN BS 752 TO BS 760 & BETWEEN S24L TO S25L IAW B757 SRM 53-00-01-2R & EA 505208.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL BETWEEN BS 324 TO BS 345, RBL 62. REPLACED INTERCOSTAL BETWEEN BS 324 TO BS 345, RBL 62 IAW B757 SRM 51-10-02, 53-00-51 & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN BS 720 TO BS 740, RBL 62. REPLACED FLOOR SUPPORT BETWEEN BS 720 TO BS 740, RBL 62 IAW B757 SRM 51-40-02, 51-10-02 & 53-00-51.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON CHANNEL BETWEEN BS 1300 TO BS 1320, LBL 24.75. REPLACED CHANNEL BETWEEN BS 1300 TO BS 1320, LBL 24.75 IAW B757 SRM 51-10-02, 53-00-51 & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN BS 720 TO BS 740, LBL 62. REPLACED FLOOR SUPPORT BETWEEN BS 720 TO BS 740, LBL 62 IAW B757 SRM 51-10-02, 53-00-51, 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN BS 660 TO BS 680, LBL 62. REPLACED FLOOR SUPPORT BETWEEN BS 660 TO BS 680, LBL 62 IAW B757 SRM 51-40-02, 51-10-02 & 53-00-51.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL BETWEEN BS 700 TO BS 720, LBL 62. REPLACED INTERCOSTAL BETWEEN BS 700 TO BS 720, LBL 62 IAW B757 SRM 51-10-02, 53-00-51 & 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM UPPER FLANGE AT BS 345, BL 0. REPAIRED FLOORBEAM AT BS 345 BETWEEN LBL 10 TO RBL 53 IAW B757 SRM 51-10-02, 53-00-51 & 53-00-51, 2R.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL BETWEEN BS 680 TO BS 700, LBL 52.22. REPLACED INTERCOSTAL BETWEEN BS 680 TO BS 700, LBL 52.22 IAW B757 SRM 51-10-02, 53-00-04 & 51-40-02.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SUPPORT ANGLE AT BS 320, RBL 62. REPLACED SUPPORT ANGLE AT BS 320, RBL 62 IAW B757 SRM 51-10-02, 53-00-51 & 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL BETWEEN BS 680 TO BS 700, LBL 62. REPLACED INTERCOSTAL BETWEEN BS 680 TO BS 700, LBL 62 IAW B757 SRM 51-10-02, 53-00-51 & BOEING DRAWING 143N5413.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL BETWEEN BS 310 TO BS 324, RBL 41. REPLACED INTERCOSTAL BETWEEN BS 310 TO BS 324, RBL 41 IAW B757 SRM 51-10-02, 53-00-51 & 51-40-02.

Part: SLIDE — DAMAGED (R3 DOOR) · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - DURING INSTALLATION OF THE R-3 EMERGENCY EXIT DOOR ESCAPE SLIDE, FOUND ESCAPE SLIDE LIGHTING SYSTEM POWER UNIT DAMAGED. REPLACED R3 DOOR EMERGENCY SIDE IAW B757 AMM 25-66-03. REPLACED LIGHT TEST SWITCH IAW B757 WIRING DIAGRAM 33-51-14.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON MAIN DECK PLATE AT BS 1682, BL 0. REPLACED MAIN DECK PLATE AT BS 1682, BL 0 IAW B757 SRM 51-40-02, 51-10-02 & BOEING DRAWING 146N5230.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT AT BS 365, BL 0. REPLACED FLOOR SUPPORT BETWEEN BS 660 TO BS 680, LBL 62 IAW B757 SRM 51-10-02, 51-00-51-1A, 51-40-02 & BOEING DRAWING 141N5190.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SUPPORT BRACKET STIFFENER AT BS 1670, LBL 62. REPLACED SUPPORT BRACKET STIFFENER AT BS 1670, LBL 62 IAW B757 SRM 51-10-02, 53-60-15-1A, 51-40-02 & BOEING DRAWING 146N8016.

Part: GIRT BAR — DEFECTIVE (R1 DOOR) · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - R-1 DOOR SLIDE GIRT BAR LEAF SPRING FAILED THE INSPECTION CHECK PER TASK CARD 19T80052003, STEP 2, MINIMUM ENGAGEMENT LESS THAN .037 INCHES. REPLACED R-1 DOOR SLIDE GIRT BAR IAW B757 MM 25-66-10-402. OPS CHECK GOOD.

Part: GIRT BAR — DEFECTIVE (R2 DOOR) · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - R-2 DOOR SLIDE GIRT BAR LEAF SPRING FAILED THE INSPECTION CHECK PER US AIRWAYS TASK CARD 19T80052003, STEP 2, MINIMUM ENGAGEMENT LESS THAN .037 INCHES. REPLACED R-2 DOOR SLIDE GIRT BAR IAW B757 MM 25-66-10-402. OPS CHECK GOOD.

Part: GIRT BAR — DEFECTIVE (R4 DOOR) · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - R-4 DOOR SLIDE GIRT BAR LEAF SPRING FAILED THE INSPECTION CHECK PER TASK CARD 19T80052003 STEP 2 MINIMUM ENGAGEMENT LESS THAN .037 INCHES. REPLACED R-4 DOOR SLIDE GIRT BAR IAW B757 MM 25-66-10-402. OPS CHECK GOOD.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON (CHORD) FLOOR STRUCTURE AT BS 1260, RBL 54.5. REPAIRED (CHORD) FLOOR STRUCTURE AT BS 1260, RBL 54.5 IAW B757 SRM 51-10-02, 53-00-51 & 51-70-12.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT AT BS 391, RBL 62. REPAIRED FLOOR SUPPORT AT BS 391, RBL 62 IAW B757 SRM 51-10-02, 53-00-51 & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN BS 1300 TO BS 1320, RBL 24.75. REPLACED FLOOR SUPPORT BETWEEN BS 1300 TO BS 1320, RBL 24.75 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON (CHORD) FLOOR SUPPORT BETWEEN BS740 TO BS 760 RBL 62. REPAIRED (CHORD) FLOOR SUPPORT BETWEEN BS 740 TO BS 760 RBL 62 IAW B757 SRM 51-10-02, 53-00-51 & 51-70-12.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FAIRING SUPPORT BETWEEN BS 780 TO BS 800, BL 0. REPLACED FAIRING SUPPORT BETWEEN BS 780 TO BS 800, BL 0 IAW B757 SRM 51-10-02, 51-40-05, 51-20-01 & 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM UPPER SURFACE AT BS 1640, LBL 52. REPAIRED FLOORBEAM UPPER "T" SECTION AT BS 1640, LBL 52 IAW B757 SRM 51-10-02, 53-00-51-1A & EA 502596.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL BETWEEN BS 1660 TO BS 1682, LBL 62. REPLACED INTERCOSTAL BETWEEN BS 1660 TO BS 1682, LBL 62 IAW B757 SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL BETWEEN BS 1640 TO BS 1660, LBL 62. REPLACED INTERCOSTAL BETWEEN BS 1640 TO BS 1660, LBL 62 IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN BS 680 TO BS 700, RBL 62. REPLACED FLOOR SUPPORT BETWEEN BS 680 TO BS 700, RBL 62 IAW B757 SRM 51-10-02, 53-00-04, 51-20-01 & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN BS 1660 TO BS 1680, BL 0. REPLACED FLOOR SUPPORT BETWEEN BS 680 TO BS 700, RBL 62 IAW B757 SRM 51-10-2, 53-00-51 & 51-40-02.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - CRACK ON FAIRING SUPPORT BRACKET AT BS 1300, S26L. REPLACED FAIRING SUPPORT BRACKET AT BS 1300, S26L IAW B757 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,911 hrs · 24,146 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT BS 355, RBL 62. REPLACED FLOOR SUPPORT AT BS 355, RBL 62 IAW B757 SRM 51-10-02, 53-00-51 & 51-40-02.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 60,217 hrs · 23,917 cycles

SEA - 9L EMERGENCY EXIT BULLNOSE LIGHT INOP. MAINTENANCE R&R BATTERY CHARGER.

Part: OXYGEN GEN — DISCHARGED (CABIN) · airframe 59,518 hrs · 23,679 cycles

PHL - DURING WORK ON PREVIOUSLY DEFERRED MAINTENANCE, FOUND DISCHARGED OXYGEN GENERATOR AT SEAT 9DEF. REMOVED AND REPLACED O2 GENERATOR AT SEAT 9DEF. OK FOR SERVICE.

Part: BALLAST — SHORTED (LAVATORY) · airframe 59,395 hrs · 23,650 cycles

CLT FLT 725 EN ROUTE DUB TO CLT. ODOR AROUND AFT LEFT LAV ELECTICAL SMELL FROM MIRROR LIGHT BALLAST. REMOVED AND REPLACED AFT LEFT LAV LIGHT BALLAST.

Part: STRAP — OUT OF POSITION (R2 DOOR) · airframe 58,669 hrs · 23,446 cycles

PHX - NR 2 PASSENGER DOOR 2R EVACUATION SLIDE HANDLE DIFFICULT TO ENGAGE IN ENGAGE POSITION. FOUND D-RING STRAP HINDERING GIRT BAR. RELOCATED STRAP. DOOR CHECKS GOOD.

Part: COVER — MISSING (CABIN) · airframe 58,627 hrs · 23,434 cycles

PHL - FORWARD ENTRY AREA EXIT LIGHT COVER IS MISSING. INSTALLED FWD ENTRY AREA EXIT LIGHT COVER LIGHT ALL CHECK GOOD. OK FOR SERVICE.

Part: STRAP — OUT OF POSITION (EVAC SLIDE) · airframe 57,804 hrs · 23,179 cycles

PHL - 4L DOOR EVACUATION SLIDE ARMING LEVER DIFFICULT TO POSITION TO ENGAGE POSITION. REPOSITIONED STRAP AS REQ. OPS CHECK OK.

Part: FUEL TANK — LEAKING (CENTER)

FLT 803. EN-ROUTE, CREW EXPERIENCED A RAW FUEL ODOR AFTER ENGINE START. REPAIRED FUEL LEAKS IN CENTER TANK NEAR KEEL BEAM, BY RIGHT HAND PACK BAY.

Part: TANK — LEAKING (FUEL SYSTEM)

PHX FLT 702 EN ROUTE PHX TO PHL. STRONG KEROSENE ODOR OBSERVED IN COCKPIT AND CABIN AFTER ENGINE START. BOTH PACKS ON. BOTH BLEEDS ON. ISOLATION VALVE CLOSED. MX CLEANED AND RESEALED THE LT WING STRINGER TIE FITTING AT THE BULKHEAD SEPARATING THE LEFT AND CENTER TANKS LOWER SHIN, REPLACED THE RT ENGINE P&D VALVE, REPLACED THE RT ENGINE TFU, INSPECTED AND BLEW OUT THE DRAIN CAN TO TFU AND P&D VAVLE, AND BORESCOPED RT ENGINE COMBUSTER SECTION AS DIRECTED. NO LEAKS, BLOCKAGES, OR PROBLEMS WERE FOUND. MX ALSO PERFORMED THE CABIN AIR QUALITY TROUBLESHOOTING STEPS FOR THE CABIN AND ENGINES. THE ENGINES WERE RAN AND THE HEPA AIR RECIRCULATION FILTERS WERE REPLACED. NO PROBLEMS OR ODORS WERE FOUND. SUBSEQUENT EVENTS: REPLACED LT ENGINE P&D VALVE. REPLACED RT ENGINE FUEL FLOW GOVERNOR AND TRANSIENT FUEL VALVE. FUEL LEAK DETECTED; REPAIRED CENTER FUEL TANK. REPAIRED FUEL TANK LEAKS. REPAIRED CENTER FUEL TANK. REPAIRED FUEL TANK LEAKS, AND REPLACED LT FUEL FLOW GOVERNOR.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 57,492 hrs · 23,068 cycles

MCO - 3 GAPS IN PHOTO LUMINESCENT STRIP AT ROWS 11,13,15 ABC. INSTALLED NEW GLOW STRIPES AT ROWS 11,13,15 ABC.

Part: TANK — LEAKING (FUEL SYSTEM)

CLT - FLT 1079 EN ROUTE CLT TO STT. AFTER ENG START AND APU SHUT-DOWN VERY STRONG KEROSENE SMELL THROUGHOUT CABIN AND COCKPIT (STRONGEST IN COCKPIT). FOUND CENTER TANK LEAK IN RT PACK BAY. CENTER TANK LEAK WAS LOCATED, ISOLATED, REPAIRED AND LEAK CHECKED. RAN APU AND PACKS, NO KEROSENE SMELL NOTED.

Part: PLACARD — MISSING (R1 DOOR) · airframe 56,650 hrs · 22,817 cycles

PHX - R1 DOOR MISSING "ATTACH SURVIVAL KIT HERE" PLACARD ON LOWER LT SLIDE COVER. INSTALLED "ATTACH SURVIVAL KIT HERE" PLACARD ON R-1 DOOR LOWER LT SIDE OF SLIDE COVER.

Part: STRAP — BINDING (EVAC SLIDE) · airframe 56,650 hrs · 22,817 cycles

PHX - 1R DOOR EVACUATION SIDE ARMING LEVER DIFFICULT TO POSITION TO ENGAGE POSITION. FOUND SLIDE STRAP BINDING IN GIRT BAR. RE-ADJUSTED STRAP. DOOR NOW ARMS AND DISARMS NORMALLY.

Part: INSULATION — OUT OF POSITION (L4 DOOR)

PHL - PORTAL AT DOOR 4L INSULATION OBSTRUCTING VIEW. MAINTENANCE SECURED INSULATION. PORTAL VIEW CLEAR.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 56,381 hrs · 22,749 cycles

PHL - L-1 SLIDE PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED L1 SLIDE AS PER JOB CARD 19L80025002.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 56,316 hrs · 22,726 cycles

C3 CHECK - EMERGENCY LIGHTS OUT AT SEAT ROW 1, 3 AND 22 RIGHT SIDE. RE-INSTALLED DISPLACED EMERGENCY AISLE LIGHT SOCKET AT ROW 22, REPLACED FUSE M730 EMERGENCY LIGHTING POWER SUPPLY, ALL LIGHTS OPERATE NORMALLY IAW B757-200 AMM 33-51-07-962-071.

Part: SKIN — DEBONDED (VERTICAL STAB) · airframe 56,316 hrs · 22,726 cycles

C3 CHECK - DISBONDED INNER SKIN ON VERTICAL STAB, RIGHT FORWARD LOWER PANEL ASSEMBLY BETWEEN FSS149.765 TO FSS162.890. REPAIRED INNER SKIN ON VERTICAL STAB, RIGHT FORWARD LOWER PANEL ASSEMBLY BETWEEN FSS149.765 TO FSS162.890 IAW EA 130616.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,316 hrs · 22,726 cycles

C3 CHECK - LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL BETWEEN BS 1415 TO BS 1418, STR 4R. REPLACED INTERCOSTAL BETWEEN BS 1415 TO BS 1418, STR 4R IAW B757-200 SRM 53-00-04 FIG 101 SRM 51-40-02 PAR 4.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,316 hrs · 22,726 cycles

C3 CHECK - LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL BETWEEN BS 1500 TO BS 1520, STR 3L. REPLACED INTERCOSTAL BETWEEN BS 1500 TO BS 1520, STR 3L IAW B757-200 SRM 51-10-02, SRM 53-00-04 FIG 101 SRM 51-40-05 FIG 2.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,316 hrs · 22,726 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL BETWEEN BS 1418 TO BS 1420, STR 16L. REPLACED INTERCOSTAL BETWEEN BS 1418 TO BS 1420, STR 16L IAW B757-200 SRM 51-40-02 PAR 4 & 7, SRM 53-00-04 FIG 101.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,316 hrs · 22,726 cycles

C3 CHECK - LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL BETWEEN BS 1500 TO BS 1510, STR 3R. REPLACED INTERCOSTAL BETWEEN BS 1500 TO BS 1510, STR 3R IAW B757-200 SRM 51-40-05 FIG 2, SRM 51-40-02 PAR 4.

Part: TARGET — MISSING (R4 DOOR)

CLT - FOUND THE R4 DOOR EVACUATION SLIDE ARMING LEVER BINDING, AND THE SLIDE ARM LIGHT INOPERATIVE. MAINTENANCE REPLACED A MISSING PROXIMITY SWITCH ACTUATOR (TARGET), AND ADJUSTED THE GIRT BAR AND TARGET AS REQUIRED.

Part: GIRT BAR — LOOSE (R4 DOOR)

CLT - AN R4 DOOR GIRT BAR FITTING WAS FOUND TO BE LOOSE. MAINTENANCE RE-ATTACHED THE R4 DOOR GIRT BAR FITTING.

Part: WINDSHIELD — CRACKED (COCKPIT)

PHL FLT 722 EN ROUTE PHL TO DUB. THE RIGHT WINDOW (F/O) HEAT WAS INOPERATIVE WITH THE SWITCH ON, AND NO INOP ILLUMINATED ON THE SWITCH. ABOUT HALF WAY BETWEEN THE LAST TWO CONNECTORS ON THE LEFT SIDE OF THE WINDOW, A SMALL ARCING COULD BE SEEN. THE RIGHT WINDOW DEVELOPED CRACKS AS A RESULT OF THE ARCING. THE FLIGHT COULD NOT CONTINUE INTO ICING CONDITIONS THAT WERE EXPECTED EN ROUTE TO DUB, SO THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT WINDOW HEAT CONTROLLER (AS A PRECAUTION), AND THE FIRST OFFICER'S WINDSHIELD.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 55,222 hrs · 22,464 cycles

PHX - WEEKLY - MAJOR REPAIR - DISBONDING ON NR 9 LEADING EDGE SLAT TRAILING EDGE WEDGE JUST OUTBOARD OF PREVIOUS REPAIR 30 INCHES FROM OUTBOARD END. REPLACED NR 9 LEADING EDGE SLAT TRAILING EDGE WEDGE IAW JOB CARD 19L52027002.

Part: HANDLE — LACK OF LUBE (L1 DOOR)

CLT - L1 DOOR DIFFICULT TO OPEN. FOUND OUTSIDE HANDLES NOT SNAPPING BACK DURING OPENING. LUBED DOOR HANDLE MECHANISM.

Part: AIR DATA MODULE — MALFUNCTIONED (ZONE 100)

FLT 1041- INDICATED AIRSPEED DROPPED ON BOTH CAPTAIN'S & 1ST OFFICER'S PANELS, WITH EICAS MESSAGES "RUDDER RATIO" & "MACH SPEED TRIM". INDICATED AIRSPEED DROPPED TO 140 KTS. ACFT CONTROL MAINTAINED WITH MANUAL PITCH & THRUST. MOMENTARY ELECTRICAL SMOKE ODOR. INDICATED AIRSPEED FLUCTUATED SHARPLY & RETURNED TO NORMAL. APPROX 1 MINUTE LATER, "MACH SPEED TRIM" MESSAGE DISAPPEARED, RUDDER RATIO MESSAGE REMAINED. SMOKE ODOR DISSIPATED. NORMAL INDICATED AIRSPEED RETURNED. LANDED WITHOUT FURTHER INCIDENT. MX ACCOMPLISHED BITE CHECK OF SAMS SYS, FUNCTIONAL CHECK OF PITOT STATIC SYS, PITOT STATIC HEAT, CSEU POWER SUPPLIES, AUTOLAND SYSTEM 40, & BPCU BITE CHECK. NO FAULTS FOUND. ACCOMPLISHED OPS TEST OF AC ELEC POWER SYS. NO FAULTS FOUND. REPLACED TAT PROBE, LT ADC, & RT DATA COMPUTER. ALL CHECKS OK. VENDOR FOUND NO FAULTS. (ORIGINAL SUBMISSION DATE: 10/07/2010)

Part: FAN — FAULTY (CABIN)

FLT 863- DURING TAKEOFF AND INITIAL CLIMB, A ROTTEN ODOR BECAME APPARENT IN COCKPIT. CREW TURNED OFF THE LT BLEED & LT PACK. ODOR DISSIPATED. AT 5,000 FT, TURNED THEM BACK ON & ODOR RETURNED. CREW TURNED THEM BACK OFF AGAIN. TRIED AGAIN AT 20,000 FEET AND NO ODOR. THE LT BLEED & PACK WERE LEFT ON. NO ODOR NOTED FOR REMAINDER OF FLT. ACFT PLACED ON MEL FOR LT BLEED SYSTEM. PERFORMED INSPECTIONS PER MM & FIM INSTRUCTIONS. REPLACED HEPA FILTERS. REPLACED RT RECIRCULATION FAN. NO ODORS NOTED. REMOVED MEL FOR BLEED SYSTEM. TEST PER LATEST ATP SPECIFICATION, NO ODOR PERCEIVED DURING TIME OF TESTING. NO REASON FOR REJECTION.

Part: SKIN — DELAMINATED (NR 5 SLAT)

DELAMINATION ON NR 5 SLAT. REPLACED NR 5 SLAT IAW JOB CARD 19C51227001 & PERFORMED RIGGING PER AMM 27-61-00. REPAIR COMPLETED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 37,158 hrs · 21,211 cycles

BFM - C2 - MAJOR REPAIR - CORROSION ON FUSELAGE SKIN BETWEEN BS 680 TO BS 700, S2R. REPAIRED FUSELAGE SKIN BETWEEN BS 680 TO BS 700, S2R IAW EA 134126.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,158 hrs · 21,211 cycles

BFM - C2 - MAJOR REPAIR - CORROSION ON PREVIOUS REPAIR OF FLOORBEAM FRAME CAP AT BS 350, BL 0. REMOVED PREVIOUS REPAIR, FABRICATED AND INSTALLED NEW FLOORBEAM IAW B757 SRM 53-00-51, 51-40-02, & US AIRWAYS TYPICAL REPAIR 53-15-01.

Part: LANYARD — OUT OF POSITION (EVAC SLIDE)

MCO - THE GIRT BAR ENGAGEMENT LIGHT EXTINGUISHED WITH THE EVACUATION SLIDE ARMING LEVER IN THE ARMED POSITION AT THE ENTRY/SERVICE DOOR L2. MAINTENANCE STOWED THE L2 DOOR SLIDE LANYARD.

Part: FAN — FAILED (APU)

MCO FLT 816 EN-ROUTE CUN TO CLT. CREW RECEIVED NUMEROUS LAVATORY SMOKE DETECTOR WARNINGS, AND AN ODOR OF SMOKE IN BOTH THE COCKPIT AND CABIN. ALSO RECEIVED AN APU OVERHEAT MESSAGE. THE FLIGHT DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE APU ON MEL. THE APU WAS REPLACED DUE TO AN OIL COOLER FAN CAME APART.

Part: APU — MALFUNCTIONED

MCO FLT 816 EN ROUTE CUN TO CLT. CREW RECEIVED NUMEROUS LAVATORY SMOKE DETECTOR WARNINGS, AND AN ODOR OF SMOKE IN BOTH THE COCKPIT AND CABIN. ALSO RECEIVED AN APU OVERHEAT MESSAGE. THE FLIGHT DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE APU ON MEL. (S)

Part: BATTERY — DISCHARGED (FLASHLIGHT)

CLT - EMERGENCY FLASHLIGHT AT DOOR 3R IS NOT FLASHING. MAINTENANCE REPLACED BATTERY IN FLASHLIGHT AT DOOR 3R. OPERATIONALLY CHECKS OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

BDL - MAINTENANCE REPORTED THE AFT SECTION OF EMERGENCY LIGHTS ARE DIM. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK AT POSITION M736. OPERATIONAL CHECK GOOD.