N203UW

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,242 hrs · 17,390 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED L1 DOOR EXTERIOR EMERGENCY LIGHT PER AMM 33-51-06.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,242 hrs · 17,390 cycles

AIRCRAFT WAS NOT GROUNDED: L2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED L2 DOOR EXTERIOR EMERGENCY LIGHT PER AMM 33-51-06.

Part: SLIDE RAFT — LOW PRESSURE (R1 DOOR) · airframe 60,432 hrs · 17,148 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS R1 DOOR SLIDE/RAFT LOW PRESS. REMOVED AND REPLACED R1 DOOR SLIDE/RAFT IAW JOB CARD 19L80025002.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,139 hrs · 17,086 cycles

AIRCRAFT NOT GROUNDED: FLOOR PHOTOLUMINESCENT LIGHT STRIP INOPERATIVE AT ROW 2-3 RIGHT. INSTALLED NEW PHOTOLUMINESCENT LIGHT STRIP IAW AMM 33-50-00. OK FOR SERVICE.

Part: SLIDE — LOW PRESSURE (L3 DOOR) · airframe 59,643 hrs · 16,972 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS L3 DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED L3 DOOR EVACUATION SLIDE IAW JOB CARD 19L83525001.

Part: SKIN — DELAMINATED (VERTICAL STAB) · airframe 59,389 hrs · 16,916 cycles

AIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILIZER RIGHT HAND SIDE FORWARD SKIN PANEL HAS DELAMINATION BETWEEN FIN STATION 113 AND 150. REPLACED SKIN PANEL PER EA 272864A.

Part: LINE — DISCONNECTED (CREW OXYGEN) · airframe 59,135 hrs · 16,859 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS FLIGHT DIVERTIED TO HNL ON ACCOUNT COCKPIT OXYGEN LEVEL DEPLEATED. AIRCRAFT WAS OVERWEIGHT FOR LANDING. AN EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE OXYGEN HOSE BLEW OFF CONNECTION CAUSING THE COMPLETE LOSS OF CREW OXYGEN. SECURED O2 SUPPLY LINE. LEAK CHECK GOOD.

Part: SPRING — BROKEN (R4 GIRT BAR) · airframe 58,983 hrs · 16,824 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS THE R4 DOOR SLIDE GIRT BAR FORWARD LEAF SPRING BROKEN. REPLACED R4 DOOR GIRT BAR IAW JOB CARD 19L80025002.

Part: GOVERNOR — LOW PRESSURE (NR 1 ENGINE) · airframe 58,310 hrs · 16,647 cycles

THE AIRCRAFT WAS GROUNDED. JUST BEGAN TO SPOOL ENGINES FOR TAKEOFF, IMMEDIATE MC FOR HYDRAULIC PUMP, GENERATOR AND ENGINE SYSTEMS. EGT RISING RAPIDLY AND LOW E1 OIL PRESSURE. ACCOMPLISHED ENGINE LIMIT/SURGE/STALL CHECKLIST, INSPECTED BY ARFF, GATE RETURN. ACCOMPLISHED FIM 71-05-00-815-807. REPLACED E1 FUEL FLOW GOVERNOR PER JOB CARDS 19L40073003 AND 19L40073002. OPERATIONS AND LEAK CHECK GOOD.

Part: WINDOW — CRACKED (SEAT 37A) · airframe 57,911 hrs · 16,556 cycles

INNER WINDOW PANE WAS FOUND CRACKED AT SEAT 37A. REPLACED THE WINDOW PANE IAW AMM 56-21-02.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 57,904 hrs · 16,555 cycles

L4 DOOR SLIDE INFLATION CYLINDER HAD LOW PRESSURE. MAINTENANCE REPLACEDTHE DOOR SLIDE IAW TC 19L80025002.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 55,907 hrs · 16,097 cycles

R2 DOOR EMERGENCY LIGHT LENS LOOSE. SECURED AND PERFORMED A SATISFACTORY OPERATIONAL CHECK WITH NO FURTHER DEFECTS NOTED.

Part: WIRE — BROKEN (ZONE 100) · airframe 55,096 hrs · 15,924 cycles

THE AIRCRAFT WAS GROUNDED. THIRTY MINUTES AFTER DEPARTING PHX, RECEIVED EICAS MESSAGE NOSE A/G DISAGREE. THE FLIGHT RETURNED TO PHX AND DECLARED AN EMERGENCY. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. FOUND BROKEN WIRES FROM D40388J TO D41650P. REF NON ROUTINES REPLACED TWISTED PAIR PER SWPM 20-30-12. SYSTEM TESTS GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

AIRCRAFT WAS IN BASE MAINTENANCE. EXTERIOR EMERGENCY EXIT LIGHT BY THE L3 DOOR IS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY PER AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: SKIN — CHAFED (RT WING SLAT) · airframe 54,617 hrs · 15,817 cycles

RIGHT WING NR 8 SLAT TRAILING EDGE 34 INCHES FROM INBOARD END, HAS 3 DEEP CHAFES RUBBING WITH UPPER SURFACE OF LEADING EDGE WING DURING OPERATION. REPAIRED WITH DOUBLER IAW SRM 51-70-10-2R.

Part: SKIN — CHAFED (LT WING SLAT) · airframe 54,617 hrs · 15,817 cycles

LEFT WING NR 3 SLAT TRAILING EDGE, 34 INCHES FROM INBOARD END UNDERNEATH HAS 3 DEEP CHAFES FROM RUBBING WITH UPPER SURFACE OF LEADING EDGE WING DURING OPERATION. REPAIRED IAW SRM 51-70-10-2R.

Part: STIFFENER — CRACKED (BS 1320) · airframe 54,617 hrs · 15,817 cycles

A CRACK WAS FOUND ON THE CABIN FLOOR SUPPORT STIFFENER AT FUSELAGE BS 1320 AND RBL 45.50. REMOVED AND REPLACED SUPPORT STIFFENER IAW SRM 51-40-02.

Part: FITTING — CORRODED (BS 365-377) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

CORROSION ON CABIN LAVATORY MOUNT FITTING BETWEEN BS 365.25 AND 377.7, RBL 13. REMOVED AND REPLACED THE FITTING ASSEMBLY IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MAIN DECK FLOOR SUPPORT CHANNEL AT RBL 24.75 BETWEEN STATION 1300 AND 1320. REPLACED CHANNEL PER SRM 53-00-51, SRM 51-40-02, AND SRM 51-40-05.

Part: MOUNT — CORRODED (ZONE 100) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MAIN CABIN LAVATORY MOUNT BLOCK JUST FORWARD OF STATION 333.45 AND RBL 2.0. REPLACED LAVATORY MOUNT BLOCK PER SRM 51-40-02.

Part: MOUNT — CORRODED (ZONE 100) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON BELLY FAIRING MOUNT AT STATION 900 AND RBL 30. REPAIRED BELLY FAIRING MOUNT PER SRM 51-70-12-0G.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON DOOR 4L LOWER SILL FLOOR SUPPORT ANGLE ATTACHED TO CHANNEL AT STATION 1676 AND LBL 53. REPLACED SUPPORT ANGLE PER SRM 51-40-02.

Part: STIFFENER — CRACKED (BS 1320) · airframe 54,617 hrs · 15,817 cycles

A CRACK WAS FOUND ON THE CABIN FLOOR SUPPORT STIFFENER AT BS 1320 AND RBL 24.75. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MAIN DECK AFT SHEAR WEB TOP SURFACE MOUNTED LEFT HAND FORWARD GALLEY FITTING AT STATION 1687 AND LBL 53. REMOVED AND REPLACED FITTING ASSEMBLY PER SRM 53-00-51-1A -1 AND SRM 51-40-02.

Part: STRAP — CRACKED (BS 560) · airframe 54,617 hrs · 15,817 cycles

CRACKED MAIN DECK FLOORBEAM STABILIZATION STRAP AT BS 560 AND LBL 45. REPAIRED THE STRAP IAW SRM 53-10-51-2R-1, FIGURE 201, AND SRM 51-40-02.

Part: BRACKET — CRACKED (FLOORBEAM) · airframe 54,617 hrs · 15,817 cycles

CRACKED MAIN DECK FLOORBEAM BRACKET AT LBL 24.75 AND BS 1320. REPLACED THE BRACKET IAW SRM 51-40-02, AND SRM 51-40-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED MAIN DECK FLOOR STRUCTURE INTERCOSTAL UPPER CHORD AT RBL 12 BETWEEN STATION 480 AND 500. REPLACED INTERCOSTAL PER SRM 51-40-02 AND SRM 51-40-05.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED FLOORBEAM BRACKET AT LBL 45.5 AND STATION 1320. REPLACED FLOORBEAM BRACKET PER SRM 51-40-02 AND SRM 51-40-05.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MAIN DECK FLOOR CHANNEL AT BL 0, BETWEEN STATION 1661 AND 1682. REPLACED FLOOR CHANNEL PER SRM 51-40-02 AND SRM 51-40-05.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM BETWEEN BL 0 AND LBL 24.75 AT STATION 345. REPAIRED FLOORBEAM PER SRM 53-00-51-1A-1, SRM 53-00-51-2R-10 AND SRM51-40-02.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MAIN CABIN FLOOR SUPPORT PLATE (CABLE GUIDE) AT LBL 26.5 BETWEEN STATION 324 AND 345. REPLACED FLOOR SUPPORT WEB PER SRM 53-00-51-1A -1 AND SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED FLOOR SUPPORT ANGLE LBL 40 BETWEEN STATION 480 AND 500. REMOVED AND INSTALLED UPPER CHORD ANGLE PER SRM 51-40-02 AND SRM 51-40-05.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MAIN DECK AFT SHEAR WEB TOP SURFACE MOUNTED RIGHT HAND AFT GALLEY FITTING AT STATION 1710 AND RBL 53. REPLACED FITTING ASSEMBLY PER SRM 53-00-51-1A -1 AND 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED UPPER CHORD ANGLE AT BL 0 BETWEEN STATION 1320 AND 1340. REPAIRED CHORD ANGLE PER SRM 51-40-02 AND SRM 51-40-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MAIN DECK FLOOR SUPPORT BETWEEN STATION 1300 AND 1320 AT RBL 21.75. REPLACED FLOOR SUPPORT (CHANNEL) PER SRM 51-40-02.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MAIN CABIN FLOOR SUPPORT CHANNEL AT RBL 59 BETWEEN STATION 365 AND 377. REPAIRED SUPPORT CHANNEL PER SRM 51-40-02 AND SRM 51-40-05.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION AND SCRATCH ON MAIN DECK FLOOR CHANNEL AT BL 0 BETWEEN STATION 1640 AND 1661. REPLACED SUPPORT CHANNEL PER SRM 53-00-51-1A -1 AND 51-40-02.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON DOOR 4L LOWER SILL INTERIOR TOP SURFACE, FLOOR SUPPORT FITTING AT LBL 60 AND STATION 1659. REPAIRED FLOOR SUPPORT FITTING (STIFFENER) PER SRM 53-00-51-1A -1 AND SRM 51-40-02.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON DOOR 4R LOWER SILL FLOOR SUPPORT CHANNEL AT RBL 55, BETWEEN STATION 1640 AND 1661. REPLACED FLOOR SUPPORT CHANNEL PER SRM 53-00-51-1A -1 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MAIN CABIN FLOOR SUPPORT CHANNEL AT LBL 20 BETWEEN STATION 324 AND STA 345. REPLACED SUPPORT CHANNEL PER SRM 53-00-51-1A -1 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MAIN DECK FLOOR STRUCTURE SUPPORT FRAME AT RBL 60.5 BETWEEN STATION 720 AND 740. REPLACED FLOOR SUPPORT PER SRM 53-00-51-1A -1 AND 51-40-02.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MAIN CABIN CHANNEL SUPPORT BETWEEN STATION 324 AND 345 AT LBL 32. REPLACED SUPPORT CHANNEL PER SRM 53-00-51-1A -1 AND 51-40-02.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON DOOR 4R LOWER SILL INTERIOR TOP SURFACE SUPPORT CHANNEL AT STATION 1672 AND RBL 60. REPLACED SUPPORT CHANNEL PER SRM 53-00-51-1A -1 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MAIN CABIN BETWEEN FLOOR SUPPORT CHANNEL BETWEEN STATION 324 AND 345 AT LBL 27. REPLACED FLOOR SUPPORT PER SRM 53-00-51-1A -1 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1640-1661) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

CORROSION ON THE L4 DOOR LOWER SILL FLOOR SUPPORT CHANNEL AT LBL 55 BETWEEN STATION 1640 AND 1661 LBL 55. REPLACED THE FLOOR SUPPORT IAW SRM 53-00-51-1A -1, AND 51-40-02.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON DOOR 4L FLOOR SUPPORT CHANNEL AT LBL 55 BETWEEN STATION 1661 AND 1682. REPLACED SUPPORT CHANNEL PER SRM 53-00-51-1A -1 AND 51-40-02.

Part: WEB — CORRODED (BS 1716) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

CORROSION WAS FOUND ON THE DECK PLATE WEB AT BS 1716 BETWEEN BL 0 AND RBL 12. REPAIRED PRESSURE DECK PLATE IAW SRM 53-60-51-2R-2 FIG 201.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON DOOR 4L LOWER SILL INTERIOR TOP SURFACE SUPPORT CHANNEL AT STATION 1656 AND LBL 60. REPLACED SUPPORT CHANNEL PER SRM 53-00-51-1A -1 AND 51-40-02.

Part: CHANNEL — CORRODED (BS 1672) · corrosion level 2 · airframe 54,617 hrs · 15,817 cycles

CORROSION ON THE L4 DOOR SILL INTERIOR TOP SURFACE HAT CHANNEL AT BS 1672 AND LBL 60. REPLACED SUPPORT CHANNEL IAW SRM 53-00-51-1A -1, AND 51-40-02.

Part: BOTTLE — LOW PRESSURE (L4 DOOR SLIDE) · airframe 54,455 hrs · 15,779 cycles

L4 DOOR EMERGENCY EVACUATION SLIDE RESERVOIR\ PRESSURE IS LOW. REMOVED AND REPLACED SLIDE ASSEMBLY IAW JOB CARD 19L80025002. OPERATIONAL CHECKED GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 54,138 hrs · 15,712 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH FLOOR LIGHTS AT ROWS 18 AND 19 ARE COMING UP. RESECURED CARPET AND FLOOR TRACK. OPERATIONAL CHECK GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (CABIN DOOR) · airframe 52,569 hrs · 15,378 cycles

AIRCRAFT WAS NOT GROUNDED. AT APPROXIMATELY 80KTS FLIGHT CREW REJECTED TAKEOFF FOR LEFT AFT CABIN DOOR OPEN LIGHT. MAINTENANCE ADJUSTED PROXIMITY SENSOR, S10097, ON L4 DOOR PER AMM 52-71-00-735-053.

Part: SLIDE — LOW PRESSURE (L4 DOOR SLIDE) · airframe 52,533 hrs · 15,370 cycles

L4 DOOR SLIDE PRESSURE LOW. REPLACED L4 DOOR SLIDE IAW TASK CARD 19L80025002.

Part: ENGINE — ODOR (NR 1) · airframe 52,190 hrs · 15,290 cycles

AIRCRAFT WAS GROUNDED: ON INITIAL DESCENT AS POWER REDUCED TO IDLE DEPARTING FL360, STRONG ODOR NOTICED ON FLIGHT DECK AND REPORTED BY F/A`S IN CABIN. AT INTERMEDIATE LEVEL OFF WITH POWER ABOVE IDLE ODOR DISSIPATED SOMEWHAT-EVERY TIME POWER REDUCED ODOR RETURNED. BOTH PACKS AUTO ENGINE BLEEDS ON APU OFF APU BLEED OFF. CATEGORY A DIRTY SOCK, RANCID CHEESE ODOR-NO IRRITATION TO EYES OR NOSE. REPLACED NR 1 ENGINE IAW TASK CARD 19L40071001.

Part: LIGHT — DETACHED (CABIN) · airframe 51,618 hrs · 15,161 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT OVER DOOR 1R COMING APART. REATTACHED EMERGENCY EXIT LIGHT OVER DOOR 1R IAW AMM 33-10-00.

Part: PUMP — INOPERATIVE (FUEL SYSTEM) · airframe 51,238 hrs · 15,087 cycles

RETURNED TO DEPARTURE; AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED RECEIVING A RT FORWARD FUEL PUMP INOPERATIVE, LOW PRESSURE INDICATION DURING CLIMB OUT. THE AIRCRAFT RETURNED TO DEPARTURE, WHERE THE AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RT FORWARD BOOST PUMP AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 28-22-03.

Part: PRESSURE SWITCH — FAULTY (FUEL SYSTEM) · airframe 51,152 hrs · 15,065 cycles

RETURNED & ACFT WAS GNDED. FLIGHT CREW REPORTED AN EICAS FAULT MSG FOR THE RT FWD FUEL PUMP ALONG WITH A LOW PRESS LIGHT FOR THE SAME FUEL PUMP DURING CLIMB OUT. THE ACFT RETURNED WHERE MX REPLACED THE PRESS SWITCH AT THE RT FWD FUEL BOOST PUMP IAW AMM 28-42-01-004-001 & 28-42-01-424-040. A SATISFACTORY LEAK & OPERATIONAL CHECK WAS PERFORMED.

Part: CONTROLLER — FAULTY (COCKPIT) · airframe 51,089 hrs · 15,052 cycles

AIRCRAFT WAS GNDED. DURING FLIGHT THE CAPTAIN'S NR 1 WINDOW SHATTERED. R & R WINDOW IAW AMM 56-11-01 & NR 1 WINDOW HEAT CONTROLLER IAW AMM 30-41-0. SEE ALSO AALA 201605269001.

Part: WINDOW — CRACKED (COCKPIT) · airframe 51,089 hrs · 15,052 cycles

AIRCRAFT WAS GNDED. DURING FLIGHT THE CAPTAIN'S NR 1 WINDOW CRACKED. R & R WINDOW IAW AMM 56-11-01 & NR 1 WINDOW HEAT CONTROLLER IAW AMM 30-41-01. SEE ALSO AALA 201605269013.

Part: LENS — MISSING (EXIT SIGN)

AIRCRAFT WAS IN BASE MX. EXIT SIGN AT LAVATORY C MISSING LENS. INSTALLED LENS ON EXIT SIGN. PERFORMED SATISFACTORY OPERATIONAL CHECK IAW GPM 17-11-3U.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,978 hrs · 15,024 cycles

AIRCRAFT IN BASE MX. CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL, BETWEEN BS 1320 - 1380 & RBL 19 - 25. REPLACED TRANSITION PANEL IAW SRM 53-00-53-1A-1 DET IV, SRM 51-40-02-0G.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,978 hrs · 15,024 cycles

AIRCRAFT IN BASE MX. CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL, BETWEEN BS 1240 - 1300, AT RBL 19. REPLACED TRANSITION PANEL IAW SRM 53-00-53-1A-1 DET IV, SRM 51-40-02-0G.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,978 hrs · 15,024 cycles

AIRCRAFT IN BASE MX. CORROSION ON AFT CARGO COMPARTMENT FLOOR SIDE PANEL ABOVE DOOR SILL, BETWEEN BS 1380 - 1440, AT RBL 19. REPLACED SIDE PANEL IAW SRM 53-00-53-1A-1 DET IV SRM 51-40-02-0G.

Part: RESERVOIR — LEAKING (L4 DOOR) · airframe 50,978 hrs · 15,024 cycles

AIRCRAFT IN BASE MX. L4 DOOR EMER POWER RESERVOIR IS LEAKING FROM RELIEF PORT. REPLACED RESERVOIR IAW 19C83652003.

Part: HARNESS — WORN (EVAC SLIDE) · airframe 50,978 hrs · 15,024 cycles

AIRCRAFT IN BASE MX. R1 DOOR SLIDE HARNESS IS WORN. REPLACED R1 DOOR SLIDE HARNESS IAW TASK CARD 19C84125005.

Part: HARNESS — WORN (EVAC SLIDE) · airframe 50,978 hrs · 15,024 cycles

AIRCRAFT IN BASE MX. R4 DOOR SLIDE HARNESS IS WORN. REPLACED R4 DOOR SLIDE HARNESS IAW TASK CARD 19C83625005.

Part: HARNESS — WORN (EVAC SLIDE) · airframe 50,978 hrs · 15,024 cycles

AIRCRAFT IN BASE MX. R2 DOOR SLIDE HARNESS IS WORN. REPLACED R2 DOOR SLIDE HARNESS IAW TASK CARD 19C84225005.

Part: PROXIMITY SWITCH — OBSTRUCTED (R4 DOOR) · airframe 50,834 hrs · 14,981 cycles

AIRCRAFT WAS NOT GNDED. 4R DOOR SLIDE LIGHT INOPERATIVE. REMOVED DEBRIS FROM DOOR PROXIMITY SWITCH & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: COUPLER — DEFECTIVE (HF COMM) · airframe 50,735 hrs · 14,950 cycles

DIVERTED, ACFT WAS GNDED. 150 MILES BEFORE ETOP, THE FLIGHT CREW TRIED TO CONTACT SFO & BOTH HR RADIOS WERE INOPERATIVE. ACFT DIVERTED, WHERE IT LANDED SAFELY WITH NO FURTHER INCIDENT. NO EMER WAS DECLARED BY THE CREW. REMOVED & INSTALLED THE LT & RT HF COUPLERS IAW AMM 23-11-01. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LENS — UNSECURE (CABIN) · airframe 50,439 hrs · 14,880 cycles

AIRCRAFT WAS NOT GNDED. EXIT LIGHT LENS COVER 3L FELL OFF BRACKET IS BROKEN. SECURED 3L EXIT LIGHT LENS.

Part: SIGN — UNSECURE (CABIN)

EXIT SIGN FROM DOOR 2R FELL OFF. ADJUSTED & INSTALLED EXIT SIGN ON DOOR 2R IAW AMM 2510.

Part: LATCH — DEFECTIVE (ZONE 800) · airframe 48,631 hrs · 14,428 cycles

R4 DOOR SLIDE LATCH ASSEMBLY DAMAGED, ROLL PINS COMING OUT. R & R R4 DOOR SLIDE LATCH ASSEMBLY IAW CARD 19L80025002.

Part: SPRING — BROKEN (ZONE 800) · airframe 47,046 hrs · 14,034 cycles

L3 DOOR AFT GIRT BAR FITTING SPRING BROKEN. R & R THE L3 DOOR AFT GIRT BAR FITTING SPRING. DOOR & GIRT BAR OPERATIONS CHECKED GOOD.

Part: MECHANISM — OUT OF ADJUST (R1 DOOR) · airframe 47,019 hrs · 14,022 cycles

MULTIPLE ATTEMPTS TO ARM R1 DOOR, VERY DIFFICULT. ADJUSTED THE SLIDE ARM & DISARM MECHANISIM.

Part: OXYGEN MASK — DEPLOYED (CABIN) · airframe 46,202 hrs · 13,777 cycles

PASSENGER OVERHEAD O2 MASKS DEPLOYED ROW 16EF. RE STOWED MASKS.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 46,202 hrs · 13,777 cycles

FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R FWD FLIGHT ATTENDANT FLASHLIGHT.

Part: DOOR — MISSING (NR 2 COWLING) · airframe 45,420 hrs · 13,494 cycles

OIL ACCESS DOOR NR 2 ENG MISSING. REPLACED NR 2 ENG OIL SERVICE DOOR IAW AMM 71-11-04-308-075.

Part: LENS — MISSING (EXIT SIGN) · airframe 43,751 hrs · 13,050 cycles

CLT EXIT SIGN OVER 2R DOOR MISSING. INSTALLED LENS COVER EMERGENCY LIGHT AT 1L DOOR.

Part: LENS — MISSING (CABIN) · airframe 43,744 hrs · 13,048 cycles

CLT EMERGENCY LIGHT COVER OVER 1L MISSING. INSTALLED LENS COVER EMERGENCY LIGHT AT 1L DOOR.

Part: FAN — ODOR (CABIN) · airframe 43,327 hrs · 12,895 cycles

FLIGHT 866 EN-ROUTE SXM TO CLT. LT RECIRCULATING FAN INOPERATIVE WITH BURNING ODOR IN CABIN. R & R LT RECIRCULATING FAN. PRIMARY CAUSE OF FAILURE DUE TO HEAVY CONTAMINATION & SECONDARY DUE TO BEARING FAILURE. UNIT WAS REPAIRED.

Part: LIGHT — UNSECURE (ZONE 200) · airframe 42,205 hrs · 12,561 cycles

EMERGENCY LIGHT IS LOOSE BETWEEN ROWS 11,12,13,14. SECURED STRIP EMERGENCY LIGHT OKAY FOR SERVICE.

Part: LIGHT — LOOSE (ZONE 200) · airframe 42,087 hrs · 12,525 cycles

EMERGENCY STRIP FLOOR LIGHTING LOOSE ON AC LT. SECURED EMERGENCY FLOOR STRIP ACFT LEFT.

Part: LIGHT — UNSECURE (CABIN) · airframe 42,003 hrs · 12,498 cycles

FLOOR LEVEL EXIT LIGHTING STRIPS LOCATED AT 12C ARE BUCKLED AND A TRIPPING HAZARD. MX REMOVED DEBRIS FROM TRACK AND RESECURED LIGHTING STRIP.

Part: LIGHT — UNSECURE (CABIN) · airframe 41,957 hrs · 12,482 cycles

ROW 11 LEFT SIDE FLOOR LIGHTING IS COMING UP. RE-INSTALLED FLOOR PATH CAP AT ROW 11, LT SIDE.

Part: BEAM — LOOSE (CABIN) · airframe 41,871 hrs · 12,460 cycles

EMERGENCY FLOOR LIGHT TRACK BEAM IS LOOSE NEEDS REPOSITIONED. RESECURED, CKS OK.

Part: LIGHT — UNSECURE (CABIN) · airframe 41,769 hrs · 12,437 cycles

EXIT PATH LIGHTING IS PULLED UP AT ROW 11A-12A. RESECURED EXIT PATH LIGHTING AT ROW 11A -12A.

Part: FLAP — WORN (RT WING) · airframe 41,288 hrs · 12,305 cycles

C1 CHECK - WEAR ON RIGHT WING OUTBOARD MAIN FLAP LEADING EDGE, IN CONTACT WITH LOWER WING SURFACE WHEN RETRACTED AT WBL 556. REPLACED RIGHT WING OUTBOARD MAIN FLAP IAW JOB CARD 19L56027001.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 41,288 hrs · 12,305 cycles

C1 CHECK - DELAMINATION ON NR 7 SLAT TRAILING EDGE WEDGE LOWER SURFACE 3 INCHES FROM INBOARD END. REPAIRED NR 7 SLAT TRAILING EDGE WEDGE IAW B757 SRM 51-70-10.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 41,288 hrs · 12,305 cycles

C1 CHECK - DELAMINATION ON LEFT WING NR 4 SLAT TRAILING EDGE WEDGE LOWER SURFACE AT AFT INBOARD END. REPAIRED NR 4 SLAT TRAILING EDGE WEDGE LOWER SURFACE IAW B757 SRM 51-70-10.

Part: STRIP — LOOSE (CABIN) · airframe 40,946 hrs · 12,200 cycles

CLT - 6 INCH SECTION OF FLUORESCENT STRIP THAT RUNS ALONG THE FLOOR IS LOOSE ACROSS FROM MID-ENTRY DOOR. SECURED EMERGENCY PATH STRIP.

Part: LANYARD — UNSECURE (SLIDE RAFT) · airframe 40,930 hrs · 12,195 cycles

CLT - 1R DOOR WILL NOT ARM EMERGENCY SLIDE. FOUND RAFT LANYARD UNDER GIRT BAR. STOWED LANYARD. 1 DOOR SLIDE ARMS OK CHECKS OK.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 40,811 hrs · 12,154 cycles

PHL - FLT 1206 EN ROUTE SXM TO PHL. ON DESCENT, NOTICED ARCING ON THE CAPT WINDSCREEN IN JUST THE UPPER LEFT CORNER. REMOVED AND REPLACED CAPTS NR 1 WINDSHIELD. ALSO REMOVED AND REPLACED CAPT WINDOW HEAT CONTROL AS A PRECAUTION.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 39,986 hrs · 11,859 cycles

CLT - FLT 874 EN ROUTE CLT TO AUA. FLIGHT HAD F/O FORWARD WINDSHIELD OVERHEAT. F/O'S WINDSHIELD CRACKED. THE DECISION WAS MADE TO RETURN TO CLT. THE FLIGHT DECLARED AN EMERGENCY INBOUND TO CLT, AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED F/O'S WINDSHIELD.

Part: COVER — MISSING (R4 DOOR) · airframe 39,953 hrs · 11,852 cycles

PHX - EMERGENCY EXIT LIGHT COVER MISSING AT R4 DOOR LOWER. INSTALLED NEW EMERGENCY EXIT ASSEMBLY. OP'S NORMAL.

Part: LANYARD — OUT OF POSITION (R1 DOOR) · airframe 39,530 hrs · 11,733 cycles

PHL - RIGHT FORWARD ENTRY DOOR WILL NOT ARM. RE- ROUTED R1 SLIDE LANYARD WHICH WAS TANGLED BELOW THE DOOR. OP'S CHECK GOOD FOR DOOR SLIDE & MECHANISM.

Part: LENS — MISSING (CABIN)

PHL - L-4 DOOR EMERGENCY EXIT LENS MISSING. REPLACED LENS.

Part: OVEN — ODOR (GALLEY) · airframe 38,347 hrs · 11,402 cycles

BRU - OVEN 206 (ENVOY), LEFT SIDE SMELLS ELECTRICAL AND TOXIC ACCORDING TO F/A'S. REMOVED AND REPLACED OVEN 206 (ENVOY). OPS CHECK OK.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 37,619 hrs · 11,171 cycles

PHL - EMERGENCY LIGHTING INOP AT L4 DOOR. REMOVED AND REPLACED M 737 BATTERY PACK & CHARGER ASSY.

Part: BEARING — BINDING (AILERON SYS) · airframe 36,852 hrs · 10,899 cycles

PHL FLT 806 EN ROUTE CUN TO PHL. "SPOILER" ADVISORY ON EICAS AFTER STIFF AILERON CONDITION "BROKE FREE" DURING TURN. THE CREW DECLARED AN EMERGENCY COMING IN TO PHL. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LATERAL CONTROL OVERRIDE AND FEEL/TRIM MECHANISM CENTERING BEARINGS. PERFORMED SATISFACTORY OPERATIONAL CHECK OF AILERON AND TRIM SYSTEM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 36,679 hrs · 10,843 cycles

BRU - DURING CABIN CHECK, FOUND A 3 INCH STG STRIP MISSING AT SEATS 19ABC AND A 4 INCH STG STRIP AT 18 DEF. INSTALLED MISSING PHOTOLUMINESCENT PART.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 36,322 hrs · 10,741 cycles

CLT FLT 1761 DFW TO CLT. FWD LAV LT & ALARM GOING OFF FOR SMOKE. MAINTENANCE REMOVED AND REPLACED FWD LAV SMOKE DETECTOR. OPS CHECK GOOD, OK FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,307 hrs · 10,734 cycles

C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOOR SUPPORT BETWEEN BS 365.5 TO BS 332, RBL 61. REPLACED FLOOR SUPPORT BETWEEN BS 365.5 TO BS 332, RBL 61 IAW B757 SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,307 hrs · 10,734 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT BETWEEN BS 1661 TO BS 1701, RBL 54. REPLACED SUPPORT BETWEEN BS 1661 TO BS 1701, RBL 54 IAW B757 SRM 51-40-02 FIG 3, 6, 7, 8 & 12.

Part: CHANNEL — BROKEN (FUSELAGE) · airframe 36,307 hrs · 10,734 cycles

C4 CHECK - FLOORBEAM STABILIZER CHANNEL BROKEN BS 377.7, LBL 45.5. REPLACED FLOORBEAM STABILIZER CHANNEL IAW B757 SRM 53-10-51.

Part: TRUNNION PIN — CORRODED (LT MLG) · airframe 36,307 hrs · 10,734 cycles

C4 CHECK - CORROSION ON THUR BOLT HOLES ON LEFT MAIN LANDING GEAR TRUNNION LINK AFT PIN. REPLACED LEFT MAIN LANDING GEAR TRUNNION LINK AFT PIN IAW B757-200 AMM 32-11-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,307 hrs · 10,734 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT BS 405 BETWEEN RBL 46 TO RBL 56. REPLACED FLOOR SUPPORT AT BS 405 BETWEEN RBL 46 TO RBL 56 IAW B757 SRM 51-40-02 & 53-00-51.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,307 hrs · 10,734 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN BS 1661 TO BS 1701 LBL 54. REPLACED FLOOR SUPPORT BETWEEN BS 1661 TO BS 1701 LBL 54 IAW B757 SRM 51-10-02, 53-00-51 & 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,307 hrs · 10,734 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT BS 1640, LBL 55. REPLACED FLOORBEAM AT BS 1640, LBL 55 IAW B757 SRM 53-00-51 & 53-00-51.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,307 hrs · 10,734 cycles

C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SUPPORT BETWEEN BS 1640 TO BS 1661, LBL 56. REPLACED SUPPORT BETWEEN BS 1640 TO BS 1661, LBL 56 IAW B757-200 SRM 51-40-02 PAR 4 FIG 3 & 4, 53-00-51.

Part: DOUBLER — DAMAGED (VERTICAL STAB) · airframe 36,307 hrs · 10,734 cycles

C4 CHECK - PART OF BONDED REPAIR DOUBLER MISSING ON LEFT SIDE OF VERTICAL STABILIZER AT FSS195. REPLACED REPAIR DOUBLER WITH NEW ON LEFT SIDE OF FORWARD LOWER TORQUE BOX PANEL ASSY FSS195 IAW EA141709 & EA141711.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,307 hrs · 10,734 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON UPPER SURFACE OF R1 DOOR LOWER SILL INBOARD ANGLE BETWEEN BS 332 TO BS 367, WL 208.2. REPLACED R1 DOOR LOWER SILL INBOARD ANGLE IAW B757 SRM 53-00-51 & 51-40-02.

Part: LIGHT — INOPERATIVE (CABIN)

CLT - NUMEROUS CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS. OPS CHECK GOOD.

Part: ACTUATOR — INOPERATIVE (LE FLAP) · airframe 69,394 hrs · 47,675 cycles

FLT 203 - BUR TO PHX - EMERGENCY LANDING - IN ROUTE CREW RECEIVED A NR 4 KRUEGER FLAP DISAGREE INDICATION. THE CREW DECLARED AN EMERGENCY AND PERFORMED A ZERO FLAP LANDING IN PHX. EMERGENCY EQUIPMENT WAS DISPATCHED. THE AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. REPLACED NR 4 L/E FLAP ACTUATOR IAW TC R3M27018.

Part: CABLE — DISCONNECTED (EVAC SLIDE) · airframe 31,037 hrs · 9,226 cycles

CLT - C3 - EES - L-3 DOOR SLIDE PACK RELEASE CABLE DISCONNECTED. REPLACED L-3 DOOR SLIDE IAW JOB CARD 19C83525005.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,538 hrs · 30,548 cycles

BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN FLOORBEAM, BS 365, RBL 5 - RBL 15, WL 208. REPAIRED CABIN FLOORBEAM, BS 365, RBL 5 - RBL 15, WL 208 IAW B757 SRM 53-00-51.