N204UW

Part: APU — LEAKING (OIL SYSTEM) · airframe 59,733 hrs · 16,776 cycles

AIRCRAFT WAS GROUNDED: FLIGHT DIVERTED TO HNL ON ACCOUNT OF APU SHUTDOWN DURING CLIMB-OUT. EMERGENCY DECLARED. MAINTENANCE FOUND ZERO OIL QUANTITY WITH NO EVIDENCE OF EXTERNAL OIL LEAKS. AN APU CHANGE HAS BEEN DECLARED. MAINTENANCE REMOVED AND REPLACED THE APU IAW JOB CARD 19L30049001. OPS CHECK & LEAK CHECK GOOD.

Part: RECEPTACLE — ARCED (FIRE WALL) · airframe 59,327 hrs · 16,688 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS DURING INSPECTION, FOUND #2 ENGINE FIREWALL DISCONNECT CONNECTOR PLUG AND RECEPTACLE D1216J/9 HAS EVIDENCE OF SEVERE ARCING ON PINS 'B' AND 'C'. MAINTENANCE REMOVED & REPLACED RH IDG FEEDER CABLES IAW SWPM 20-10-11, 20-10 -12, 20-10-13, AND AMM 24-11-01. IDG SYS OPS CHECK GOOD IAW AMM 24-11-00.

Part: CONNECTOR — DISCONNECTED (NR 2 ENGINE) · airframe 59,326 hrs · 16,687 cycles

AIRCRAFT WAS GROUNDED: PILOT DIVERTED ON ACCOUNT OF MULTIPLE FLIGHT INSTRUMENT FAULTS/ELECTRONIC DISPLAY ISSUES. EMERGENCY WAS DECLARED. DURING INSPECTION, FOUND #2 ENGINE FIREWALL DISCONNECT CONNECTOR PLUG AND RECEPTACLE D1216J/9 HAS EVIDENCE OF SEVERE ARCING ON PINS 'B' AND 'C'. MAINTENANCE REMOVED & REPLACED RH IDG FEEDER CABLES IAW SWPM 20-10-11, 20-10 -12, 20-10-13, AND AMM 24-11-01. IDG SYS OPS CHECK GOOD IAW AMM 24-11-00.

Part: STRAP — CORRODED (BS 1787.45) · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE VISIT: STRAP AT BS 1787.45, RBL 25 HAS 6"X2.5"X0.063" CORRODED AREA.(GENERATED BY NON-CPCP W/C). FABRICATED AND REPLACED FUSELAGE SKIN STRAP ON APU AIR INLET DOOR FWD CUTOUT IAW SRM 51-40-02.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE BISIT: MAINTENANCE REPORTS FLIGHT DECK WINDOW R1 IS DELAMINATED. REMOVED AND REPLACED FLIGHT DECK WINDOW R1 IAW AMM 56-11-01-004-001 AND 56-1-01-424-015. OPS CHECK GOOD IAW AMM 30-41-00-715-001.

Part: ELEVATOR — SEPARATED (RT ELEVATOR) · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR UPPER SURFACE TRAILING EDGE SKIN IS SEPERATED AT THE AFT TRAILING EDGE AREA 18 INCHES INBOARD OF OUTBOARD AFT CORNER. REPAIRED ELEVATOR PER SRM 51-70-10-2R-1.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: FIRST OFFICERS R3 WINDOW DELAMINATED. REPLACED WINDOW PER AMM 56-11-10.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED BRACKET IN THE LEFT HAND MAIN LANDING GEAR WHEEL WELL ON THE FORWARD END OUTBOARD SIDE. REPLACED BRACKET PER SRM 51-40-02-OG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR WHEEL WELL AFT INBOARD CHANNEL CRACKED. REPLACED CHANNEL PER SRM 51-40-02.

Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA FLOOR DECK PLATE AT BS 1681 AND LBL 15. REPAIRED DECK PLATE PER SRM 53-60-51-2R-10.

Part: MOUNT FITTING — CORRODED (FUSELAGE) · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND SIDE GALLEY MOUNT FITTING AT BS 1720. REPLACED FITTING PER SRM 51-10-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR FITTING BETWEEN BS 395 AND BS 418 AT RBL 55. REPLACED FITTING PER SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR FITTING BETWEEN BS 345 AND BS 345 AT LBL 15.40. REPLACED FITTING PER SRM 51-40-02.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOORBEAM STRAP AT BS 348 AND BL 0. REPLACED STRAP PER SRM 53-00-51-2R-13.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK BETWEEN BS 1540 AND BS 1640 AT LBL 45.50. REPLACED SEAT TRACK PER SRM 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR SUPPORT CHANNEL BETWEEN BS 310.5 AND BS 324 AT RBL 45.50. REPLACED FLOOR SUPPORT CHANNEL PER SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK BETWEEN BS 1540 AND BS 1640 AT LBL 24.75. REPLACED SEAT TRACK PER SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FITTING AT BS 330 AND RBL 45.50. REPLACED FITTING PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR SUPPORT AT BS 400 AND RBL 50. REPLACED FLOOR SUPPORT PER SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL BETWEEN BS 1660 AND BS 1681 AT RBL 10. REPLACED INTERCOSTAL PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR SUPPORT AT BS 410 AND RBL 46. REPLACED FLOOR SUPPORT PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR SUPPORT BETWEEN BS 365 AND 377 AT RBL 50. REPLACED FLOOR SUPPORT PER SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FITTING AT BS 330 AT BL 0. REPLACED FITTING PER SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FITTING BS 370 AND RBL 30. REPLACED FITTING PER SRM 51-40-02.

Part: PANEL — INOPERATIVE (ZONE 200) · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE FOUND EMERGENCY LIGHT/PASS OXY PANEL LIGHT PLATE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT/PASS ON PANEL LIGHT PLATE AND TEST IS GOOD IAW AMM 33-13-01-404-006.

Part: FITTING — CORRODED (FUSELAGE) · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: CORRROSION ON FITTING AT BS 396 AND RBL 14.5. REPLACED FITTING PER SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,322 hrs · 16,685 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FITTING AT BS 297 AND RBL 45.50. REPLACED FITTING PER SRM 51-40-02.

Part: LAMP — BURNED OUT (ARMED INDICATOR) · airframe 57,650 hrs · 16,253 cycles

ARM LIGHT AT THE L4 DOOR WAS BURNED OUT. MAINTENANCE REPLACED THE LAMP AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: GUARD — BROKEN (LIGHT SWITCH) · airframe 56,790 hrs · 16,076 cycles

EMERGENCY LIGHT SWITCH GUARD BROKEN. MAINTENANCE REPLACED LIGHT SWITCH GUARD AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LANYARD — UNSECURE (EVAC SLIDE) · airframe 55,829 hrs · 15,863 cycles

THE AIRCRAFT WAS NOT GROUNDED. DOOR 4L WILL NOT ARM. SECURED SLIDE LANYARD. OPERATIONS CHECK OF 4L DOOR ARM/DISARM GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,630 hrs · 15,817 cycles

AIRCRAFT WAS NOT GROUNDED. EXIT EMERGENCY LIGHT DOOR 4L INOPERABLE. REPLACED EMERGENCY EXIT LIGHT AT DOOR 4L. OPERATIONS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHT, AT THE R2 DOOR INOPERATIVE. REPLACED THE EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: CONTROL ROD — OUT OF ADJUST (L2 DOOR) · airframe 55,512 hrs · 15,791 cycles

AIRCRAFT WAS NOT GROUNDED. L2 DOOR WILL NOT FULLY ALLOW ARMING OF SLIDE (ARMING LEVER STICKS HALFWAY). ADJUSTED MODE SELECTOR LEVER CONTROL ROD PER AMM 52-11-20-825-001.

Part: DOOR — OUT OF ADJUST (L2) · airframe 55,512 hrs · 15,791 cycles

AIRCRAFT NOT GROUNDED. PHOENIX MAINTENANCE FOUND L2 DOOR DIFFICULT TO MOVE TO THE CLOSED POSITION PRIOR TO DEPARTURE. ACCOMPLISH DOOR RIGGING AND ADJUST AS REQUIRED PER AMM 52-11-00.

Part: LENS — MISSING (CABIN) · airframe 55,282 hrs · 15,738 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT BY THE L4 DOOR HAS A MISSING LENS COVER. INSTALLED LENS COVER. OPERATIONAL CHECK GOOD.

Part: CONTROLLER — FAILED (BLEED AIR SYS) · airframe 55,271 hrs · 15,736 cycles

THE AIRCRAFT WAS GROUNDED.. AT FL 360 CABIN ALTITUDE REACHED APPROXIMATELY 10,000 FEET. THE CABIN ALTITUDE WARNING HORN SOUNDED. THE COCKPIT CREW DONNED THEIR OXYGEN MASKS AND STARTED A DESCENT TO 10, 000 FEET. DURING DESCENT CABIN ALTITUDE WAS AT 10,000 FT. LEFT AND RIGHT DUCT PRESSURE WAS FLUCTUATING BETWEEN 20 PSI AND 60 PSI. THE FLIGHT DECLARED AN EMERGENCY AND DIVERTED TO HNL. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. PERFORMED FIM 36-11-00-815-805. FOUND L DUCT PRESS LAGGING BEHIND R DUCT PRESSURE. ALSO L RFCC FAILED OPS TEST IAW AMM 36-11-18-710-806-001. REPLACED L RFCC IAW AMM 36-11-18 OPS CHK OK. BITE CHECK BOTH PRESS CONTROLLERS IAW AMM 21-31-00. NO FAULTS FOUND.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS)

EMERGENCY EXIT LIGHTS OVER THE R2 DOOR, BESIDE THE L2 DOOR, AND AT THE BULLNOSE OVER ROW 13 RIGHT ARE INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK (AALA201706239030) IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS OVER THE R2 DOOR, BESIDE THE L2 DOOR, AND AT THE BULLNOSE OVER ROW 13 RIGHT ARE INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK IAW AMM 33-51-07. OPERATIONAL CHECKED GOOD.

Part: COVER — CRACKED (GIRT BAR)

L4 DOOR GIRT BAR AFT FITTING HAS A CRACKED COVER. REMOVED AND REPLACED THE COVER IAW SRM 51-40-02-0G. OPERATIONAL CHECKED GOOD.

Part: LIGHT — UNSECURE (ROW 18) · airframe 54,067 hrs · 15,458 cycles

EMERGENCY LIGHT STRIP AT ROW 18 DELAMINATING FROM FLOOR. MAINTENANCE SECURED EMERGENCY LIGHT STRIP AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: COVER — DAMAGED (L1 DOOR SLIDE)

L1 DOOR EMERGENCY EVACUATION SLIDE COVER IS DAMAGED. REPAIRED SMALL AREA OF DAMAGE IAW AMM 25-00-00-300-801. OPS CHECKED GOOD.

Part: LINER — OUT OF POSITION (R1 DOOR) · airframe 54,012 hrs · 15,438 cycles

AIRCRAFT WAS NOT GROUNDED. R1 DOOR KNUCKLE BUSTER WILL NOT EXTEND WHEN ARMING DOOR. REPOSITIONED DOOR LOWER LINING IAW AMM 52-11-04. OPERATIONAL CHECK GOOD.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 53,357 hrs · 15,290 cycles

EMERGENCY SLIDE AND ARM MECHANISM WILL NOT ARM R1 DOOR. MAINTENANCE INSPECTED ARM/DISARM AT GIRT BAR BRACKETS AND CLEARED DEBRIS FROM BRACKETS. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: TRACK — OBSTRUCTED (L4 DOOR) · airframe 53,194 hrs · 15,251 cycles

L4 DOOR ARMING LEVER STUCK. MAINTENANCE INSPECTED THE DOOR AND FOUND DEBRIS IN THE TRACK. REMOVED DEBRIS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 52,684 hrs · 15,148 cycles

FLASHLIGHT BATTERY DISCHARGED AT THE L2 DOOR FLIGHT ATTENDANT SEAT. REPLACED THE BATTERY PACK IAW AMM 25-64-00-202-023.

Part: GIRT BAR — OBSTRUCTED (R4 DOOR) · airframe 51,591 hrs · 14,915 cycles

R4 DOOR ARM LIGHT DOES NOT ILLUMIANTE WHEN IN ARM POSITION. INSPECTED SLIDE AND FOUND THE GIRT BAR OBSTRUCTED. OBSTRUCTION WAS REMOVED AND A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED IAW AMM 25-66-00. AIRCRAFT GROUNDED.

Part: HF COMM — INOPERATIVE (COCKPIT) · airframe 50,523 hrs · 14,685 cycles

AIRCRAFT WAS GNDED. BOTH HF RADIOS INOPERATIVE. UNABLE TO COMMUNICATE ON ALL FREQUENCY. TRIED TWO NEW HF TRANSCEIVERS, UNABLE TO TRANSMIT OR RECEIVE ON FREQUENCIES 6.640 & 11.342 MHZ, NYC & SFO STATIONS. INSPECTED FEED LINE INSIDE VERTICAL STABILIZER WITH NO DEFECTS NOTED IAW AMM 23-11-03 & 23-11-01, NO HELP. FURTHER TROUBLESHOOTING NEEDED. CONTINUED THE TROUBLESHOOTING BY ACCOMPLISHING SYS BITE WITH NO PROBLEMS NOTED IAW FIM 23-11-00-815-804 & PERFORMED A RADIO CHECK WITH SFO WITH NO PROBLEMS.

Part: LANYARD — UNSECURE (R4 DOOR) · airframe 50,339 hrs · 14,640 cycles

AIRCRAFT WAS NOT GNDED. SLIDE AT 4R SEEMS TO BE HANGING DOWN. RE-STOWED 4R SLIDE LANYARD, NO ADDITIONAL FAULTS NOTED.

Part: LIGHT — DETACHED (CABIN) · airframe 50,254 hrs · 14,623 cycles

AIRCRAFT WAS NOT GNDED. FLOOR EXIT PATH LIGHT STRIP COVER AFT LT IN BACK LOOSE. RE-ATTACHED FLOOR EXIT PATH LIGHT STRIP COVER TO FLOOR.

Part: COVER — LOOSE (CABIN) · airframe 50,094 hrs · 14,582 cycles

AIRCRAFT WAS NOT GNDED. FLOOR LEVEL EMER LIGHTING STRIP, BETWEEN ROWS 34 & 37 LOOSE. SECURED EMER LIGHT STRIP COVER, BETWEEN ROWS 34 - 37.

Part: SWITCH — INOPERATIVE (ZONE 200) · airframe 50,055 hrs · 14,568 cycles

AIRCRAFT IN BASE MX. DOOR L3 EMER LIGHT TEST SWITCH INOPERATIVE. R & R EMER LIGHT TEST SWITCH PUSH BUTTON IAW 03-51-14. PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00 PNB 501.

Part: SPRING — BENT (R4 DOOR) · airframe 50,055 hrs · 14,568 cycles

AIRCRAFT IN BASE MX. R4 DOOR GIRT BAR LEAF SPRINGS BENT. R & R SPRINGS IAW SRM 51-40-02-0G.

Part: WIRE — DAMAGED (ZONE 500) · airframe 49,713 hrs · 14,487 cycles

AIRCRAFT WAS GNDED. LT FUEL SPAR VLV EICAS MSG ON INITIAL CLIMB. REPLACED WIRE BETWEEN CONNECTOR D40902J & CONNECTOR D2142 ON LT SPAR FUEL SOV.

Part: ENGINE — FAILED (LEFT) · airframe 49,640 hrs · 14,463 cycles

INFLIGHT ENG SHUTDOWN. FLIGHT DIVERTED DUE TO A LT ENG FAILURE. AN EMER WAS DECLARED & THE ACFT LANDED SAFELY WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE PER TASK CARD 19L40071001.

Part: SIGN — BROKEN (CABIN) · airframe 48,987 hrs · 14,298 cycles

DOOR 4L EMER EXIT SIGN BROKEN OFF. R & R DOOR 4L EMER EXIT SIGN IPC 33-52-20-07, PN 702409-1001 IAW AMM 33-51-10. OPERATIONS CHECKED SATISFACTORY.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 48,763 hrs · 14,240 cycles

EMERGENCY LIGHTS RT SIDE OF FIRST CLASS CABIN INOPERATIVE. R & R POWER SUPPLY & BATTERY PACK IAW AMM 33-51-07. OPERATIONS CHECKED OK.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 46,380 hrs · 13,641 cycles

MEGA PHONE ABOVE SEAT 1AC DOES NOT PRODUCE ANY NOISE. R & R MEGA PHONE ABOVE SEAT 1AC.

Part: TRIM SWITCH — FAILED (COCKPIT) · airframe 45,763 hrs · 13,433 cycles

PRIOR TO COAST OUT WHILE TRIMMING RUDDER NOSE LT, TRIM WAS MOVING VERY SLOW. TRIMMED NOSE RT & TRIM SPEED WAS NORMAL. WHEN ATTEMPTED NOSE LT AGAIN, RUDDER TRIM WOULD NOT WORK, STILL WILL TRIM NOSE RT. MAINTENANCE R&R THE AILERON / RUDDER TRIM CONTROL MODULE. VENDOR SHOP FINDINGS: UNIT FAILED PRELIMINARY FUNCTIONAL TESTING. VERIFIED CUSTOMER REASON FOR UNIT REMOVAL FROM AIRCRAFT. FOUND THE RUDDER TRIM SWITCH DEFECTIVE. REPLACED THE RUDDER TRIM SWITCH.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 42,623 hrs · 12,562 cycles

CREW REPORTS EMERGENCY FLASHLIGHT AT L2 DOOR, BATTERY LOW. REPLACED FLASHLIGHT BATTERY, OPS CHECKED NORMAL.

Part: LIGHT — UNSECURE (CABIN) · airframe 41,910 hrs · 12,364 cycles

EMERGENCY LIGHTS AT ROW 11 HAS LIFTED UP. SECURED EMERGENCY TRACK LIGHTING AT ROW11. OPS CHECKED GOOD.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 41,685 hrs · 12,304 cycles

PLASTIC EXIT SIGN FROM AFT REAR DOOR DETACHED. REPLACED EXIT SIGN COVER LOCATED JUST AFT OF L-4 DOOR.

Part: LIGHT — LOOSE (CABIN) · airframe 41,349 hrs · 12,208 cycles

EMER EXIT LIGHTING STRIP LOOSE BY ROW 12. RE-SECURED STRIP AT ROW 12, CKS GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 41,333 hrs · 12,200 cycles

EMER LIGHTING STRIP ON FLOOR, ACFT RIGHT IS LOOSE BETWEEN SEATS 11AND 12. RE-SECURED EMER LIGHTING FLOOR STRIP AT SEATS 11 AND 12.

Part: STRIP — BUCKLED (CABIN) · airframe 41,196 hrs · 12,170 cycles

EXIT PATH LIGHTING BUCKLING AT ROW 11/12, ACFT RT. RE-SECURED EXIT PATH LIGHTING STRIP AT ABOVE INDICATED LOCATION.

Part: LIGHT — LOOSE (CABIN) · airframe 41,100 hrs · 12,147 cycles

EMERGENCY FLOOR LIGHTS STRIP IS LOOSE AT ROW 11, SEAT D. REINSTALLED FLOOR STRIP.

Part: LIGHT — LOOSE (CABIN) · airframe 40,965 hrs · 12,119 cycles

EMERGENCY LIGHT STRIP AT ROW 11 (RT) IS BUCKLED. FOUND STRIP LOOSE AT ROW 11. APPLIED DOUBLE SIDED TAPE AND REFITTED STRIP, CHECK OK.

Part: GLOWSTRIP — UNSECURE (EMERGENCY EXIT) · airframe 40,900 hrs · 12,101 cycles

FLOOR MOUNTED EMERGENCY EXIT GLOW STRIP, AROUND ROW 11 ACFT RT, ARE NOT ATTACHED PROPERLY. SECURED FLOOR LEVEL EMERGENCY GLOW STRIP.

Part: DOOR — LACK OF LUBE (L1) · airframe 40,877 hrs · 12,094 cycles

L1 DOOR DIFFICULT TO CLOSE. CHECK AND LUBRICATED L1 DOOR. OPS CHECKED GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 40,754 hrs · 12,050 cycles

PHX - EMERGENCY PATH STRIP PEELING UP NEAR ROW 11-1. RE-SECURED EMERGENCY PATH LIGHTING STRIP AT ROW 11-12.

Part: LIGHT — UNSECURE (CABIN) · airframe 40,579 hrs · 11,985 cycles

PHL - EMERGENCY PATH LIGHTS NOT SECURED TO FLOOR ROW 11. SECURED PATH LIGHTING STRIP. OK FOR SERVICE.

Part: GLOWSTRIP — UNSECURE (CABIN) · airframe 40,488 hrs · 11,971 cycles

PHX - EMERGENCY LIGHTS ROW 9-10-11 STRIP NEEDS SECURING. SECURED EMERGENCY PHOTO LUMINESCENT ESCAPE PATH LIGHTS IN CENTER AISLE BETWEEN ROW 9- 10- 11. OPS CHECK GOOD.

Part: STRIP — UNSECURE (CABIN) · airframe 40,161 hrs · 11,854 cycles

CLT - EMERGENCY FLOOR LIGHTING STRIPS BOTH SIDES ARE NOT FLUSH WITH FLOOR AT ROW 11. SECURED COVER.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,138 hrs · 11,846 cycles

C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOOR SUPPORT BETWEEN BS 1640 TO BS 1660, BL 0. REPLACED FLOOR SUPPORT BETWEEN BS 1640 TO BS 1660, BL 0 IAW B757 SRM 51-40-02 & AIRBUS DRAWING 146N5242.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,138 hrs · 11,846 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL FLOOR SUPPORT BETWEEN BS 1620 TO BS 1681, RBL 50. REPLACED INTERCOSTAL FLOOR SUPPORT BETWEEN BS 1620 TO BS 1681, RBL 50 IAW B757 SRM 51-40-02 & AIRBUS DRAWING 146N6104.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,138 hrs · 11,846 cycles

C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON INTERCOSTAL FLOOR SUPPORT AT BS 335, RBL 38. REPLACED INTERCOSTAL FLOOR SUPPORT AT BS 335, RBL 38 IAW B757 SRM 51-10-02, 53-00-01 & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,138 hrs · 11,846 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL FLOOR SUPPORT BETWEEN BS 1620 TO BS 1681, RBL 50. REPLACED INTERCOSTAL FLOOR SUPPORT BETWEEN BS 1620 TO BS 1681, RBL 50 IAW B757 SRM 51-40-02 & AIRBUS DRAWING 146N6104.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 40,138 hrs · 11,846 cycles

C4 CHECK - CRACK IN FORWARD CARGO DOOR INNER SKIN. REPAIRED CRACKED AREA AT FORWARD CARGO DOOR INNER SKIN IAW B757 SRM 51-70-13.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,138 hrs · 11,846 cycles

C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOOR SUPPORT AT BS 335 BETWEEN RBL 5 TO RBL 23. REPLACED FLOOR SUPPORT AT BS 335 BETWEEN RBL 5 TO RBL 23 IAW B757 SRM 51-40-02 & AIRBUS DRAWING 141N5160.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,138 hrs · 11,846 cycles

C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOOR SUPPORT BETWEEN BS 335 TO BS 345, RBL 19. REPLACED FLOOR SUPPORT BETWEEN BS 335 TO BS 345, RBL 19 IAW B757 SRM 51-40-02, 51-10-02 & 53-00-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,138 hrs · 11,846 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,138 hrs · 11,846 cycles

C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOOR SUPPORT BETWEEN BS 335 TO BS 345, RBL 2. REPLACED FLOOR SUPPORT BETWEEN BS 335 TO BS 345, RBL 2 IAW B757 SRM 51-40-02, 51-10-02 & 53-00-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,138 hrs · 11,846 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT AT BS 370, RBL 25. REPLACED FLOOR SUPPORT AT BS 370, RBL 25 IAW B757 SRM 51-10-02, 53-00-51-1A & 51-40-02.

Part: LENS — BROKEN (EXIT SIGN) · airframe 39,970 hrs · 11,787 cycles

PHX - 4R DOOR EXIT SIGN COVER BROKEN. INSTALLED NEW EXIT LENS, OPS CHECK GOOD.

Part: TRACK — LOOSE (CABIN) · airframe 38,315 hrs · 11,297 cycles

PHL - SEAT 12D TRACK MOUNTED EXIT INDICATORS ARE NOT SECURED TO FLOOR. SECURED TRACK.

Part: BRACKET — UNSECURE (CABIN) · airframe 38,236 hrs · 11,279 cycles

AMS - ROW 12 EMERGENCY LIGHTING COMING OUT OF FLOOR BRACKET. FASTENED BRACKET.

Part: LENS — LOOSE (CABIN) · airframe 38,125 hrs · 11,251 cycles

PHL - LUMINESCENT LIGHT STRIP IS LOOSE AT ROW 11 AIRCRAFT RIGHT. SECURED LUMINESCENT LIGHT STRIP LENS.

Part: COVER — UNSECURE (CABIN) · airframe 38,079 hrs · 11,241 cycles

DUB - EMERGENCY LIGHTS: WITH OVHD PANEL SWITCH ON, EMERGENCY AISLE LIGHTS AT ROW 12 COVER STRIP LIFTED. ALL OTHER LIGHT AND INDICATIONS NORMAL. ROW 12 EMERGENCY LIGHT COVER RE-FITTED.

Part: TRACK — LOOSE (CABIN) · airframe 37,982 hrs · 11,216 cycles

PHL - EMERGENCY FLOOR TRACK LIGHTS ROW 12 A/C RIGHT LOOSE. RE-SECURED AS REQUIRED, OK FOR SERVICE.

Part: STRIP — BUCKLED (CABIN) · airframe 37,754 hrs · 11,152 cycles

PHL - FLOOR MOUNTED TRACK EMERGENCY LIGHTING STRIP BUCKLED AT SEAT 12D. REMOVED DEBRIS UNDER TRACK/STRIP. CONTOUR TO FLOOR PANEL NOW.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 37,686 hrs · 11,130 cycles

EMERGENCY EXIT LIGHT COVER OVER 1L DOOR MISSING. REPLACED EXIT LIGHT LENS 1L DOOR.

Part: LIGHT — BUCKLED (CABIN) · airframe 37,661 hrs · 11,120 cycles

EMERGENCY LIGHT AT ROW 12, IS BUCKLED AND CAUSES PAX AND F/A TO TRIP. SECURED EMERGENCY LIGHT COVER. CHECKED OK.

Part: COVER — DETACHED (CABIN) · airframe 37,304 hrs · 11,008 cycles

CLT - 12 DEF FLOOR LIGHTING STRIP PULLED UP. RE-ATTACHED COVER STRIP OVER SECTION OF LIGHTING STRIP. OK FOR SERVICE.

Part: LIGHT — UNSECURE (CABIN) · airframe 37,030 hrs · 10,911 cycles

CLT - EMERGENCY LIGHT STRIP ON FLOOR ABEAM ROW 10 RT SIDE BROKEN AND NOT SECURED. SECURED EMERGENCY LIGHT STRIP.

Part: HANDLE — LACK OF LUBE (R1 DOOR) · airframe 37,014 hrs · 10,905 cycles

CLT - 1R DOOR DIFFICULT TO OPEN/CLOSE AND ARM AND DISARM. FOUND BUTTERFLY HANDLE OUTSIDE PARTIALLY OPENED. CYCLED DOOR OPERATION & LUBED EXTERIOR HANDLE. OPS CHECKED GOOD.

Part: CABLE — OUT OF POSITION (R1 DOOR) · airframe 36,967 hrs · 10,888 cycles

SXM - DOOR 1R WILL NOT ARM AND CLOSE PROPERLY. ARMING LEVER BINDING. FOUND CABLE TO GIRT BAR OUT OF POSITION. REPOSITIONED CABLE AND SYS CK'D. SYSTEM CHECKS GOOD.

Part: SLIDE — LOW PRESSURE (R4 DOOR) · airframe 36,830 hrs · 10,841 cycles

PHL - R4 DOOR EMERGENCY BOTTLE PRESSURE INDICATION IN THE RED. REMOVED AND REPLACED R4 DOOR SLIDE.

Part: COVER — OUT OF ADJUST (R1 DOOR) · airframe 36,775 hrs · 10,826 cycles

PHL - 1R DOOR WILL NOT ARM. THE 1R DOOR ANTI LATCH OPEN BLOCKER ADJUSTED ON DOOR COVER. DOOR ARMS AND DISARMS NORMAL.

Part: SOCKET — BROKEN (EXTERIOR) · airframe 36,642 hrs · 10,787 cycles

DUB - L3 DOOR EXTERIOR EMERGENCY LIGHT INOP. REPLACED LIGHT SOCKET ASSY.

Part: TRACK — UNSECURE (CABIN) · airframe 36,625 hrs · 10,784 cycles

PHL - EMERGENCY FLOOR TRACK LIGHTING NEEDS TO BE RE-ATTACHED AT 11D. SECURED TRACK.

Part: LIGHT — LOOSE (CABIN) · airframe 36,617 hrs · 10,782 cycles

PHL - EMERGENCY PATH LIGHT A/C RIGHT BETWEEN ROW 11-12 IS LOOSE. RE-SECURED EMERGENCY PATH LIGHT A/C RIGHT BETWEEN ROW 11-12 AS REQUIRED.

Part: COVER — UNSECURE (CABIN) · airframe 36,126 hrs · 10,645 cycles

PHL - EMERGENCY PATH TRACK LIGHTING STRIP ROW 11/12 RT COMING UP. RE-SECURED EMERGENCY PATH TRACK LIGHTING STRIP COVER, CHECKS GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 36,054 hrs · 10,630 cycles

PHL - FLOOR EMERGENCY LIGHTING STRIP BETWEEN ROWS 11 AND 12 A/C RIGHT HAS COME LOOSE FROM FLOOR FASTENERS. RE-SECURED AS REQUIRED.

Part: LINER — INTERFERENCE (R1 DOOR) · airframe 35,977 hrs · 10,612 cycles

CLT - DOOR 1R - THE ARMING KNUCKLE DOES NOT POP OUT WHEN ARMED. FOUND DOOR LINER INTERFERING WITH RETRACTIBLE DOOR OPERATION. TRIMMED CUTOUT AND OPERATIONAL CHECKED ARM/DISARM OK.

Part: LIGHT — LOOSE (CABIN) · airframe 35,854 hrs · 10,581 cycles

BRU - EMERGENCY STRIP LIGHTING SECTION LOOSE AT ROW 11 (DEF). REINSTALLED. OPS OK.

Part: SIGN — LOOSE (CABIN) · airframe 35,672 hrs · 10,522 cycles

PHL - WITH ATTND PNL SW ON, TRACK MOUNTED EXIT INDICATORS AT MID CABIN (ROW 12 ACFT L) AREA NEED TO BE SECURED. MAINTENANCE RE-SECURED SIGN ON ROW 12. CHECKS OK.

Part: COVER — OUT OF POSITION (CABIN) · airframe 35,247 hrs · 10,396 cycles

SJU - EMERGENCY FLOOR LIGHTS COVER OFF OVER ROW 11 - PASSENGER CUT FOOT ON PLASTIC COVER. RE-INSTALLED EMERGENCY FLOOR LIGHT COVER OVER ROW 11 AS REQ.

Part: LIGHT — LOOSE (CABIN) · airframe 35,118 hrs · 10,360 cycles

SJU - FLOOR MOUNTED TRACK LIGHTING AT ROW 11 & 12 RGT LOOSE AND TRIPPING HAZARD. INSTALLED AND SECURED EMERGENCY TRACK LIGHTING AT ROWS 11 & 12 AS REQUIRED.

Part: SLIDE RAFT — UNWANTED DEPLOY (R4 DOOR)

CLT FLT 876 CLT TO AUA. R4 DOOR SHOWED MECHANICAL PROBLEMS. SLIDE WOULD NOT ARM. PLACED IN DISARMED POSITION, CRACKED DOOR OPEN, AND THE SLIDE DEPLOYED. MAINTENANCE REMOVED AND REPLACED THE R4 DOOR SLIDE/RAFT. ALSO REMOVED AND REPLACED THE R4 DOOR EMERGENCY POWER RESERVOIR DUE TO BEING DISCHARGED WHEN THE SLIDE DEPLOYED.

Part: LIGHT — UNSECURE (CABIN)

PHL - ROW 11 ON FLOOR EMERGENCY TRACK FLOOR LIGHTING NEEDS TO BE SNAPPED DOWN OR SECURED DOWN - BUCKLING UP SLIGHTLY. SECURED FLOOR EMERGENCY TRACK LIGHTING AT 10/14.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

PHL - FLASHLIGHT NEEDS NEW BATTERY. REPLACED BATTERY ON FORWARD LEFT FLASHLIGHT. OPERATIONALLY CHECKS GOOD.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,753 hrs · 10,255 cycles

LEVEL 2 GALVANIC CORROSION ON CLIP (ANGLE) AT BS 1420, RBL 19.10. REPLACED CLIP (ANGLE) AT BS 1420, RBL 19.10 IAW B757 SRM 53-00-53 & BOEING DRAWING 146N5393.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,753 hrs · 10,255 cycles

CRACKS IN INTERCOSTAL ANGLE BETWEEN BS 1205 TO BS 1215, BL 0. REPLACED INTERCOSTAL ANGLE BETWEEN BS 1205 TO BS 1215, BL 0 IAW B757 SRM 51-40-02.

Part: ATTACH FITTING — CRACKED (BS 1337) · airframe 34,753 hrs · 10,255 cycles

A 1.25 INCH CRACK IN CLIP AT BS 1337, BL 0. REMOVE AND REPLACED INTERCOSTAL CLIP IAW SRM 51-40-02 PAR 4 FIGS 3, 4, 6, 7 & 8.

Part: BATTERY — DISCHARGED (MEGAPHONE)

FLL - THE FORWARD MEGAPHONE WAS INOPERATIVE. MAINTENANCE REPLACED THE MEGAPHONE BATTERIES.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

SEA - THE FLIGHT ATTENDANT FLASHLIGHT BEHIND LAV "D" IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY.

Part: FUSE — BLOWN (CABIN)

PHX - THE L3 DOOR EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE FUSE ON AFT LEFT EMERGENCY POWER SUPPLY.

Part: BLOCK — CORRODED (L4 DOOR)

PHL - AFT LEFT DOOR ESCAPE SLIDE GIRT BAR CENTERING BLOCK HAS CORROSION. REPLACED L4 DOOR ESCAPE SLIDE CENTERING BLOCK.

Part: BOTTLE — EMPTY (R4 DOOR)

PHX - THE R4 DOOR ASSIST BOTTLE READS 0 PSI. REPLACED THE R4 DOOR ASSIST BOTTLE.

Part: FAN — OVERHEATED (E&E BAY)

PHL - FLT 731 LGW TO PHL. THE EQUIPMENT COOLING OVERHEAT LIGHT CAME ON IN FLIGHT, SIMULTANEOUS WITH ODOR IN CABIN AND COCKPIT. THE ODOR WENT AWAY WHEN CREW WENT TO ALTN ON ALTN EQUIPMENT COOLING SWITCH, FOLLOWING THE QRH PROCEDURE. REMOVED AND REPLACED EQUIPMENT COOLING FAN NR 1.

Part: SLIDE — LOOSE (L2 DOOR)

PHL - THE L2 DOOR HANDLE WAS JAMMED. THE CREW COULD NOT DETERMINE IF THE EMERGENCY EVACUATION SLIDE WAS ARMED. THE SLIDE PACK WAS TIGHTENED TO THE DOOR. THE DOOR WAS CYCLED SEVERAL TIMES. NO DEFECTS WERE NOTED.

Part: SLIDE — STUCK (L2 DOOR)

CLT - THE L2 DOOR HANDLE WAS JAMMED. THE CREW COULD NOT DETERMINE IF THE EMERGENCY ESCAPE SLIDE WAS ARMED. THE FORWARD SLIDER WAS STUCK ON THE FITTING. THE SLIDER WAS RELEASED FROM THE FITTING. THE DOOR WAS CYCLED SEVERAL TIMES. THE DOOR OPERATIONALLY CHECKS OK.

Part: LIGHT — FAULTY (CABIN)

PHL - FLT 1746 MCO TO PHL. THE FLIGHT ATTENDANT REPORTED A STRONG ELECTRICAL ODOR FROM THE AFT GALLEY. THE COFFEEMAKERS WERE TURNED OFF, CIRCUIT BREAKERS WERE PULLED, AND THE AFT GALLEY LIGHTING WAS TURNED OFF. THE ODOR THEN WENT AWAY. THE FLIGHT ARRIVED IN PHL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED A SIDEWALL BULB AROUND SEAT ROW 28DEF. OPERATIONALLY CHECKS OK.

Part: LIGHT — INOPERATIVE (EVAC SLIDE)

PHL - THE SLIDE ARMED LIGHT ABOVE THE R1 DOOR WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BULBS AS REQUIRED. OPERATIONALLY CHECKS GOOD.

Part: STRAP — CRACKED (FUSELAGE) · airframe 23,830 hrs · 30,886 cycles

BFM - MAJOR REPAIR - C1 CHECK - CRACKED FLOOR SUPPORT STABILIZATION STRAP, BS 365.25 - BS 377.7, LBL 40. REPAIRED FLOOR SUPPORT STABILIZATION STRAP, BS 365.25 - BS.377.7, LBL 40 IAW USAIRWAYS TYPICAL REPAIR 53-35-01.

Part: GASKET — LEAKING (RUDDER ACTUATOR)

CUN FLT 803 PHL-CUN DURING LANDING GEAR EXTENSION, LEFT HYD SYSTEM QTY DROPPED TO .48 RF. MAINTENANCE FOUND RUDDER RATIO ACTUATOR SOLENOID GASKET LEAKING. REPLACED GASKET.

Part: PROBE — INTERMITTENT (FUEL QTY) · airframe 21,003 hrs · 6,908 cycles

FLIGHT 724, PHL-SNN: AFTER TAKEOFF, CREW REPORTED THAT THE RIGHT FUEL QUANTITY GAUGE WAS INOPERATIVE AND RECEIVED AN INTERMITTANT FUEL QUANTITY STATUS MESSAGE. FLIGHT RETURNED TO PHL. MAINTENANCE FOUND THE RIGHT FUEL COMPENSATOR PROBE INTERMITTANT. REPLACED PROBE. NO FURTHER FAULTS.