N207UW

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,381 hrs · 11,396 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS PHOTOLUMINESCENT EMERGENCY STRIP INOP AT ROWS 1 THUR 11 RT/H. REPLACED PHOTOLUMINSCENT STRIPS FROM ROW 1 RT TO 11 RT. IAW ACFT DRAWING #DBE2285. OPS CHECK GOOD AND AMM 33-51-15-201.

Part: STARTER — FAILED (APU) · airframe 46,960 hrs · 11,074 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS AFTER APU OIL SERVICING ON ARRIVAL, APU WOULD NOT START-FAILED. SMOKE EVIDENT. APU WAS SHUTDOWN FROM NLG POSITION. MAINTENANCE REMOVED AND REPLACED APU STARTER IAW AMM 49-41-01. ON 3RD START ATTEMPT ON THE NEW STARTER, THERMAL RUNAWAY WAS EXPERIENCED AND THE STARTER OVERHEATED AND CAUGHT FIRE. DRY CHEMICAL EXTINGUISHER WAS APPLIED INTO APU COMPARMTENT. INSPECTED APU IAW AMM 49-11-00-206-021. APU EXTERNAL DAMAGE FOUND AND APU BATT BUS TRIPPED. MAINTENANCE IS CURRENTLY TROUBLESHOOTING THE ROOT CAUSE. MAINTENANCE REMOVED AND REPLACED APU STARTER IAW AMM 49-41-01. ON 3RD START ATTEMPT ON THE NEW STARTER, THERMAL RUNAWAY WAS EXPERIENCED AND THE STARTER OVERHEATED AND CAUGHT FIRE. DRY CHEMICAL EXTINGUISHER WAS APPLIED INTO APU COMPARMTENT. INSPECTED APU IAW AMM 49-11-00-206-021. APU EXTERNAL DAMAGE FOUND AND APU BATT BUS TRIPPED. MAINTENANCE REMOVED AND REPLACED THE APU ASSEMBLY IAW CARD 19L30049001.

Part: AUTOPILOT SYS — MALFUNCTIONED (RIGHT) · airframe 46,777 hrs · 11,027 cycles

THE PILOT REPORTED THAT THE RT AUTOPILOT UNCOMMANDEDLY DISCONNECTED. MAINTENANCE PERFORMED AN FCC TEST THROUGH MCDP. NO FAULTS. ENGAGED THE RT AUTOPILOT AND MOVED FLIGHT CONTROLS. DID NOT DISCONNECT. NO FAULTS CAN BE DUPLICATED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 46,526 hrs · 10,967 cycles

FLIGHT ATTENDANT FLASHLIGHT AT THE L2 DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT IAW 25-64-00.

Part: BOTTLE — LOW PRESSURE (L1 DOOR SLIDE) · airframe 45,889 hrs · 10,827 cycles

THE L1 DOOR HAD LOW BOTTLE PRESSURE. MAINTENANCE REPLACED THE L1 DOOR SLIDE IAW JC 19L80025002, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 45,397 hrs · 10,716 cycles

THE AIRCRAFT WAS NOT GROUNDED. R1 DOOR SLIDE BELOW PRESSURE LIMITS. REPLACED SLIDE PER JOB CARD 19L80025002.

Part: SLIDE — BINDING (R1 DOOR) · airframe 44,120 hrs · 10,445 cycles

AIRCRAFT IN BASE MAINTENANCE. R1 SLIDE GIRT FOLD SEEMS TO MAKE DOOR A BIT DIFFICULT TO OPEN. REPLACED R1 ESCAPE SLIDE.

Part: WINDOW — DELAMINATED (L1) · airframe 44,127 hrs · 10,447 cycles

CAPTAIN`S L1 WINDOW BUBBLING AND DELAMINATED ALONG UPPER EDGE. REMOVED AND REPLACED THE L1 WINDOW IAW MM 56-11-00-206-068.

Part: SLIDE — LOW PRESSURE (L4 DOOR)

L4 DOOR SLIDE PRESSURE LOW. MAINTENANCE REPLACED L4 DOOR SLIDE IAW 19L80025002 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: PROXIMITY SENSOR — INOPERATIVE (R1 DOOR) · airframe 42,865 hrs · 10,161 cycles

R1 DOOR ARMED LIGHT IS INOPERATIVE WHEN THE DOOR IS CLOSED AND ARMED. REMOVED AND REPLACED PROXIMITY SENSOR S10216 SLIDE ENGAGEMENT LIGHT. OPS CHECKED GOOD.

Part: CONTROL VALVE — FAULTY (AC BAY)

PHX FLT 663 PHX - KOA. THE AIRCRAFT WAS GROUNDED. ON T/O RT PACK AND BLEED SHOWED OFF. ON CLIMB DUCT PSI VARIED 40-50 PSI. AS POWER IS PULLED TO IDLE RT PACK SHOWS OFF. REMOVED & REPLACED RT PACK FLOW CONTROL VALVE LEAK & OP CHECKED GOOD REF AMM 21-51-01-402.

Part: ACTUATOR — DAMAGED (LT AILERON) · airframe 41,332 hrs · 9,808 cycles

DURING APPROACH THE CREW REPORTED UNCOMMANDED RIGHT AILERON ROLL WHEN THE CONTROL WHEEL WAS RELEASED ON ROLL OUT. CREW WAS ABLE TO CORRECT AND LANDING WAS UNEVENTFUL. MAINTENANCE FOUND DAMAGED TRAILING EDGE FAIRING AT THE LEFT AILERON. PERFORMED DFDR DOWNLOAD PER TSI PER JOB CARD 19T21031001. AIRCRAFT WAS GROUNDED. FOREIGN OBJECT DAMAGE TO AILERON POWER CONTROL ACTUATOR AND SKIN ON AILERON LOWER PANEL LEADING EDGE. REMOVED AND REPLACED POWER CONTROL ACTUATOR UNIT IAW AMM 27-11-20-422-018. REPAIRED LOWER AILERON IAW EA 270036.

Part: SKIN — DAMAGED (LT AILERON)

DURING APPROACH, THE CREW REPORTED AN UNCOMMANDED RIGHT AILERON ROLL WHEN THE CONTROL WHEEL WAS RELEASED ON ROLL OUT. CREW WAS ABLE TO CORRECT AND LANDING WAS UNEVENTFUL. MAINTENANCE FOUND DAMAGED TRAILING EDGE FAIRING AT THE LEFT AILERON. FOREIGN OBJECT DAMAGE TO AILERON POWER CONTROL ACTUATOR AND SKIN ON AILERON LOWER PANEL LEADING EDGE. REMOVED AND REPLACED POWER CONTROL ACTUATOR UNIT IAW AMM 27-11-20-422-018. REPAIRED LOWER AILERON IAW EA 270036. AIRCRAFT WAS GROUNDED.

Part: COVER — DAMAGED (L1 DOOR) · airframe 41,041 hrs · 9,739 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR EMERGENCY EVACUATION SLIDE COVER IS DAMAGED. SLIDE COVER REPAIRED AND REINSTALLED. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — DEFECTIVE (EMERGENCY LIGHT) · airframe 40,386 hrs · 9,602 cycles

EMERGENCY EXIT LIGHTS CONNECTOR D42694J WILL NOT STAY CONNECTED TO D42694P AT BS 1635. REPLACED THE CONNECTOR IAW SWPM 20-61-28, WDM 33-51-22 AND AMM 33-51-00-715-039.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 39,876 hrs · 9,479 cycles

AIRCRAFT IN BASE MAINTENANCE. WHEN L1 DOOR GIRT BAR SLIDE IS ARMED, LIGHT IS INOPERATIVE. REPLACED SLIDE LIGHT ASSEMBLY AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 34-21-02-962-001.

Part: SEAT TRACK — DAMAGED (BS 460) · airframe 40,104 hrs · 9,528 cycles

ELONGATED HOLE ON MAIN DECK SEAT TRACK LBL 45, BS 460. REPAIRED THE SEAT TRACK IAW EA 256388.

Part: CONNECTOR — BROKEN (R2 DOOR SLIDE) · airframe 39,876 hrs · 9,479 cycles

R2 DOOR SLIDE ARMED LIGHT CONNECTOR IS BROKEN. REPLACED INDICATOR IAW AMM 33-51-06 AND ACCOMPLISHED SATISFACTORY. OPERATIONAL CHECK IAW AMM 25-66-11.

Part: FLOORBEAM — DAMAGED (BS 1540) · airframe 40,104 hrs · 9,528 cycles

FLOOR BEAM HAS AN ELONGATED HOLE. CUT OUT DAMAGE AREA, FABRICATED A REPAIR AND INSTALLED IAW SRM 53-00-51-SR-5 REPAIR 5.

Part: CHANNEL — CORRODED (BS 1640-1680) · corrosion level 2 · airframe 40,104 hrs · 9,528 cycles

CHANNEL CORRODED. REPLACED THE CHANNEL IAW SRM 51-40-02, AND SRM 51-40-05.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,104 hrs · 9,528 cycles

AIRCRAFT IN BASE MAINTENANCE, CORROSION ON FITTING AT BS 1682 AND RBL 45. REPLACED FITTING PER SRM 51-40-02.

Part: ANGLE — CRACKED (BS 1420-1440) · airframe 40,104 hrs · 9,528 cycles

CRACK ON MAIN DECK FLOOR WEB UPPER FLANGE ANGLE BETWEEN BS 1420 AND 1440 AT BUTTLINE 0. REPLACED THE ANGLE IAW SRM 51-40-02, 51-40-05.

Part: SEAT TRACK — CORRODED (BS 1620-1640) · corrosion level 2 · airframe 40,104 hrs · 9,528 cycles

CORROSION ON MAIN DECK SEAT TRACK BETWEEN BS 1620 AND 1640 AT RBL 24.75. REPAIRED THE SEAT TRACK IAW SRM 51-40-02, 51-40-05 AND 51-20-01.

Part: SEAT TRACK — CORRODED (BS 1620-1640) · corrosion level 2 · airframe 40,104 hrs · 9,528 cycles

CORROSION ON MAIN DECK SEAT TRACK ON AND AROUND CROWN AREA BETWEEN BS 1620 AND 1640 AT RBL 45.50 REPAIRED THE SEAT TRACK IAW SRM 51-40-02, 51-40-05 AND 51-20-01.

Part: FLOOR SUPPORT — CORRODED (BS 780-879) · corrosion level 2 · airframe 40,104 hrs · 9,528 cycles

CORROSION ON MAIN DECK FLOOR SUPPORT BETWEEN BS 780 AND 879 AT RBL 64. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: SLIDE — LOW PRESSURE (L4 DOOR) · airframe 39,925 hrs · 9,491 cycles

L4 DOOR SLIDE, LOW PRESSURE. R & R L4 DOOR SLIDE IAW 19L80025002.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,884 hrs · 9,481 cycles

RIGHT EMERGENCY LIGHT STRIP IN FIRST CLASS DOES NOT ILLUMINATE. AIRCRAFT WAS GROUNDED. INSTALLED A NEW LIGHT IAW AMM 33-51-15.

Part: LIGHT — LOOSE (CABIN) · airframe 39,104 hrs · 9,304 cycles

EMERGENCY LIGHT LOOSE AT ROWS 14-16 LEFT. SECURED THE EMERGENCY LIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 38,524 hrs · 9,179 cycles

AIRCRAFT WAS GNDED. AFT CABIN FLASHLIGHT INOPERATIVE. REPLACED BATTERY IN AFT CABIN FLASHLIGHT.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 38,451 hrs · 9,161 cycles

AIRCRAFT WAS NOT GNDED. FLASHLIGHT AT L4 DOOR POSITION IS INOPERATIVE. R & R FLASHLIGHT.

Part: LIGHT — LOOSE (CABIN) · airframe 37,765 hrs · 9,010 cycles

AIRCRAFT WAS NOT GNDED. EMER FLOOR LIGHTING COMING LOOSE AT ROW 14 ON ACFT RT. R & R ADHESIVE TAPE FOR EMER LIGHTING AT ROW 14 IAW AMM 33-51-11.

Part: LIGHT — LOOSE (CABIN) · airframe 37,700 hrs · 8,999 cycles

EMERGENCY FLOOR LIGHT STRIP COMING OUT AT SEAM, ROW 14 & 15. SECURED EMER FLOOR LIGHT STRIP BY SEAT ROW 14 & 15 IAW AMM 33-51-15.

Part: RADIO — INOPERATIVE (HF COMM) · airframe 36,847 hrs · 8,819 cycles

FLIGHT RETURNED DUE TO BOTH HF RADIOS BEING INOPERATIVE, NO TUNE OR TRANSMIT. AN EMER WAS DECLARED & THE ACFT LANDED WITHOUT INCIDENT & THE ACFT WAS TAKEN OUT OF SERVICE. CONTACTED SFO BY PHONE TO CONFIRM FREQUENCIES TO BE USED. ESTABLISHED NORMAL CONTACT USING BOTH HF SYSTEMS SEVERAL TIMES & RETURNED TO ACFT TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,650 hrs · 8,778 cycles

NUMBER 3R EMER EXIT DOOR LIGHT DOES NOT OPERATE. REPLACED R3 DOOR EXIT LIGHT BATTERY & CHARGER. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-01-401. SEE AALA201511099004 FOR ADDITIONAL INFORMATION.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 36,650 hrs · 8,778 cycles

NUMBER 3R EMER EXIT DOOR LIGHT DOES NOT OPERATE. REPLACED R3 DOOR EXIT LIGHT BATTERY & CHARGER. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-01-401. SEE AALA201511089001 FOR ADDITIONAL INFORMATION.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,427 hrs · 8,735 cycles

C3 CHECK, CORROSION ON L3 EMER EXIT CUT OUT LOWER SILL BOTTOM SURFACE AT BS 1350 & LBL 63. REPLACED SILL WEB IAW SRM 53-60-15-1A-1 DET V & SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 36,427 hrs · 8,735 cycles

C3 CHECK, CRACKED FLOOR SUPPORT ANGLE IN THE AFT CARGO COMPARTMENT AT BS 1330 & BL 0. REPLACED IAW SRM 51-40-02 & DWG 146N5180.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,427 hrs · 8,735 cycles

C3 CHECK, CORROSION ON AFT CARGO SIDE PANEL, BETWEEN BS 1310 - 1410, LBL 19 - 26. REPLACED SIDE PANEL IAW SRM 53-00-53-1A-1 DET V & 51-40-02.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,427 hrs · 8,735 cycles

C3 CHECK, CORROSION ON AFT CARGO COMPARTMENT FWD LOWER SUPPORT ANGLE AT BS 1200 & LBL 15. REPLACED ANGLE IAW SRM 53-00-53-1A-1 DET V & SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,427 hrs · 8,735 cycles

C3 CHECK, CORROSION ON AFT CARGO FLOOR STRINGER AT BS 1510 & RBL 7.55. REPAIRED STRINGER IAW AARD 757 53-10-00-1 REPAIR 1 PART C.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,427 hrs · 8,735 cycles

C3 CHECK, CORROSION ON AFT CARGO COMPARTMENT FLOOR STRINGER AT BS 1510 & RBL 2.90. REPAIRED FLOOR STRINGER IAW AARD 757 53-10-00-1 REPAIR 1 PART C.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,427 hrs · 8,735 cycles

C3 CHECK, CORROSION ON AFT CARGO COMPARTMENT FLOOR STRINGER AT BS 1510 & RB 11.40. REPAIRED FLOOR STRINGER IAW AARD 757 53-10-00-1 REPAIR 1 PART C.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,427 hrs · 8,735 cycles

C3 CHECK, CORROSION ON AFT CARGO COMPARTMENT FLOOR STRINGER AT BS 1510 & LBL 2.90. REPAIRED FLOOR STRINGER IAW AARD 757 53-10-00-1 REPAIR 1 PART C.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,427 hrs · 8,735 cycles

C3 CHECK, CORROSION ON AFT CARGO COMPARTMENT SIDE PANEL, BETWEEN BS 1200 - 1310, LBL 19 - LBL 26. REPLACED SIDE PANEL IAW SRM 53-00-53-1A-1 DET V & SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,427 hrs · 8,735 cycles

C3 CHECK, CORROSION ON AFT CARGO COMPARTMENT FLOOR STRINGER, BETWEEN STATION 1314 & 1344 AT RBL 7.55. REPLACED FLOOR STRINGER IAW AARD 53-10-00-1 REPAIR 1 ESO 90928 & SRM 53-00-53-1A.

Part: WINDOW — SCRATCHED (L3 DOOR) · airframe 36,427 hrs · 8,735 cycles

C3 CHECK, L3 PAX ENTRY DOOR WINDOW, OUTER PANE EXTERIOR, HAS SCRATCHES ON GLASS. REPLACED WINDOW IAW AMM 56-31-02-401.

Part: CABLE — OUT OF ADJUST (R1 DOOR) · airframe 36,427 hrs · 8,735 cycles

C3 CHECK, R1 DOOR EMER BOTTLE ASSIST CABLE REQUIRES ADJUSTMENT. ADJUSTED R1 DOOR ASSIST BOTTLE CABLE & TRAVEL IAW AMM 52-11-32-404-010. OPERATIONS CHECKED GOOD.

Part: LIGHT — UNSECURE (CABIN)

ROW 15 ACFT LT EMER LIGHT STRIP NEEDS TO BE REATTACHED TO FLOOR. SECURED EMER LIGHT STRIP AT ROW 1, ACFT LT IAW AMM 33-51-11.

Part: O-RING — WORN (R3 DOOR SLIDE) · airframe 32,975 hrs · 8,045 cycles

R3 DOOR SLIDE PRESSURE GAUGE IS IN THE RED. R & R THE ESCAPE SLIDE ASSEMBLY. FOUND O-RING WORN. REPLACED THE O-RING & OVERHAULED SLIDE ASSEMBLY.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 31,529 hrs · 7,764 cycles

C2 CHECK FLIGHT COMPARTMENT L3 WINDOW IS DELAMINATED AT FWD LOWER CORNER & DISCOLORED AROUND OUTER EDGE. REPLACED L3 WINDOW IAW AMM 56-11-10-424.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 31,522 hrs · 7,762 cycles

C2 CHECK, CRACK ON INTERCOSTAL SUPPORT WEB AT BS 1321, LBL 46.5. REPAIRED INTERCOSTAL SUPPORT WEB AT BS 1321, LBL 46.5 IAW SRM 51-40-02, 51-10-02 & DWG 140N2506.

Part: COVER — BROKEN (CABIN) · airframe 31,062 hrs · 7,681 cycles

PHX DOOR 3L & R PLASTIC COVER BROKEN ON THE EMERGENCY EXIT FLOOR STRIP. MX REPLACED 3L & R PLASTIC COVERS ON THE EMERGENCY EXIT FLOOR STRIP.

Part: SPRING — DAMAGED (L2 GIRT BAR)

L2 DOOR SLIDE GIRT BAR SPRINGS ARE DAMAGED. R & R L2 DOOR SLIDE GIRT BAR LEAF SPRINGS.

Part: WINDOW — CRAZED (L1 DOOR) · airframe 29,543 hrs · 7,375 cycles

PASSENGER ENTRY DOOR FWD WINDOW CRAZED AND CRACKED. R & R L1 DOOR WINDOW.

Part: CONTROLLER — INOPERATIVE (CABIN) · airframe 28,640 hrs · 7,181 cycles

L3 DOOR EXTERIOR EMERGENCY LIGHT INOP. R & R EMERGENCY LIGHT CONTROLLER L 3 DOOR.

Part: GIRT BAR — WORN (R1 DOOR) · airframe 27,610 hrs · 6,990 cycles

PHX - R1 DOOR GIRT BAR LEAF SPRING WORN. REMOVED AND REPLACED GIRT BAR ASSY.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 27,036 hrs · 6,889 cycles

PHX - CAPTAIN'S NR 1 WINDSHIELD DELAMINATING & ARCING. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S NR 1 WINDSHIELD.

Part: STRIP — UNSECURE (CABIN) · airframe 26,658 hrs · 6,813 cycles

PHX - EMERGENCY LIGHTING FLOOR STRIP BY ROW 13C LIFTING UP FROM FLOOR. REFASTENED FLOOR STRIP BY ROW 13.

Part: MEGAPHONE — INTERMITTENT (CABIN) · airframe 26,502 hrs · 6,785 cycles

PHX - FORWARD CABIN MEGAPHONE IS INTERMITTANT. PUSH TO TALK LEVER IS BAD. REPLACED THE FORWARD CABIN MEGAPHONE.

Part: SLAT — DELAMINATED (LT WING) · airframe 26,496 hrs · 6,782 cycles

C1 CHECK. NR 4 LEADING EDGE SLAT DELAMINATED 59 INCHES OUTBOARD OF INBOARD END AND 8 INCHES FORWARD OF TRAILING EDGE. REPAIRED SLAT IAW B527 SRM 57-43-01-01-1 AND 51-70-10.

Part: LENS — OUT OF POSITION (CABIN)

PHX - EMERGENCY EXIT LIGHT COVER MISSING AT DOOR R4. FOUND LENS IN GALLEY, RE-SECURED. OPS GOOD.

Part: GLOWSTRIP — UNSECURE (CABIN) · airframe 25,590 hrs · 6,605 cycles

PHX - EMERGENCY LIGHTING BY ROW 13C IS LOOSE AND STICKING UP. SECURED PHOTO LUMINESCENT STRIP.

Part: CABLE — DISLODGED (EVAC SLIDE) · airframe 24,621 hrs · 6,424 cycles

PHX - DOOR SLIDE 2R WILL NOT ARM. SECURED CHORD INTO SLIDE. OPS CHECKS GOOD.

Part: COVER — BROKEN (CABIN) · airframe 24,147 hrs · 6,335 cycles

PHX - DOOR 4L EMERGENCY EXIT LIGHT COVER BROKEN OFF. REPLACED 4L EMERGENCY LT. OPERATIONAL TEST NORMAL.

Part: COVER — OUT OF POSITION (CABIN) · airframe 22,471 hrs · 5,982 cycles

PHX FLT 601 EN ROUTE LAS TO PHX. EMER EXIT PLACARD ON DOOR 4R FELL OFF DURING TAXI. RE-INSTALLED EMERGENCY EXIT DOOR LIGHT COVER ON 4R DOOR. OPS NORMAL.

Part: LIGHT — LOOSE (CABIN)

PHX - FLOOR LIGHTING ROW 13, ACFT RIGHT, COMING UP. DISLODGED, RE-SECURED TRIM STRIP AT ROW 13 RIGHT.

Part: GLOWSTRIP — UNSECURE (CABIN)

LIH - FLOOR EXIT PATH STRIP UNSECURED AT 14D. SECURED FLOOR EXIT PATH STRIP.

Part: BOTTLE — IMPROPER PART (L1 DOOR)

PHX - AS DIRECTED, INSPECTED DOOR ASSIST BOTTLE AT THE L1 DOOR POSITION FOR PROPER PART NUMBER INSTALLATION. FOUND THE INCORRECT PART INSTALLED. MAINTENANCE REPLACED THE L1 DOOR ASSIST BOTTLE WITH THE CORRECT PART.

Part: MEGAPHONE — DEFECTIVE (CABIN)

PHX - THE FORWARD MEGAPHONE VOLUME KNOB IS MISSING. MAINTENANCE REPLACED THE FORWARD MEGAPHONE.

Part: WEB — CRACKED (FUSELAGE) · airframe 21,023 hrs · 5,700 cycles

BFM - C4 - MAJOR REPAIR - CRACK IN SUPPORT WEB AT BS 301, WL 197, RBL 22. REPLACED SUPPORT WEB AT BS 301, WL 197, RBL 22 IAW B757 SRM 51-40-02 & 51-40-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 21,123 hrs · 5,700 cycles

BFM - MAJOR REPAIR - C4 CHECK - CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT AT BS 1320, BL 0. REPLACED AFT CARGO COMPARTMENT FLOOR SUPPORT AT BS 1320, BL 0 IAW B757 SRM 51-45-05, 51-40-02, 53-00-53.