N205UW

Part: SLAT — MISREPAIRED (LT WING) · airframe 60,034 hrs · 16,607 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: MAJOR REPAIR ACCOMPLISHED ON LEFT WING LEADING EDGE #1 SLAT WEDGE AS A RESULT OF DETERMINING THE TYPE OF WEDGE INSTALLED AS REQUIRED PER AD 2017-22-12, SB 757-57-0066 AND TASK CARD 19C50057010.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 56,843 hrs · 15,843 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR SLIDE PRESS LOW. REPLACED L1 DOOR SLIDE ASSEMBLY PER JOB CARD 19L80025002.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 56,745 hrs · 15,819 cycles

L4 DOOR ASSIST BOTTLE SHOWS ZERO PRESSURE. REPLACED THE DOOR ASSIST BOTTLE IAW AMM 52-11-30.

Part: DOOR — UNKNOWN (L4) · airframe 56,551 hrs · 15,774 cycles

L4 DOOR DIFFICULT TO CLOSE. MAINTENANCE CHECKED THE RIG OF THE L4 DOOR IAW AMM 52-11-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 56,491 hrs · 15,762 cycles

L2 AND L3 EMERGENCY LIGHTS FAILED TO TEST. MAINTENANCE REPLACED THE L2 EMERGENCY LIGHT TEST SWITCH, PINNED THE L3 SWITCH, AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00-715-003.

Part: GIRT BAR — OUT OF ADJUST (R4 DOOR) · airframe 56,119 hrs · 15,670 cycles

R4 DOOR LT GIRT BAR ATTACHED SHOWS RED WHEN ARMED. ADJUSTED GIRT BAR, OPS CHECKED GOOD IAW AMM 52-11-25-825-001.

Part: SKIN — CORRODED (TE FLAP) · airframe 56,119 hrs · 15,670 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. LEFT HAND WING MAIN INBOARD FLAP UPPER SKIN CORRODED AT INBOARD SIDE. REPLACED LEFT HAND WING INBOARD MAIN FLAP PER AMM 27-51-02.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 56,119 hrs · 15,670 cycles

AFT SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPAIRED THE WIRE W3534-0038-22 IAW SWPM 20-30-15, PERFORMED AN OPS CHECK IAW AMM 33-51-00-715-039, SATISFACTORY.

Part: DOOR FRAME — CORRODED (BS 1380) · airframe 56,119 hrs · 15,670 cycles

CORROSION FOUND ON THE AFT CARGO DOOR FRAME INNER ANGLE AT BS 1380, BETWEEN STRINGERS 26R AND 27R. REPAIRED THE DOOR FRAME IAW EA 281351.

Part: CREASE BEAM — CORRODED (BS 580) · corrosion level 2 · airframe 56,119 hrs · 15,670 cycles

CORROSION WAS FOUND ON THE ANGLE OF THE OUTBOARD CREASE BEAM AT BS 580, STRINGER 17R. REPAIRED THE ANGLE IAW EA 281167.

Part: LIGHT — DAMAGED (CABIN) · airframe 56,119 hrs · 15,670 cycles

CABIN EMERGENCY LIGHT DAMAGED. REPLACED THE EMERGENCY LIGHT IAW DWG 19P33D1283.

Part: DOUBLER — CORRODED (BS 420-440) · corrosion level 2 · airframe 56,119 hrs · 15,670 cycles

CORROSION FOUND ON THE DOUBLER BETWEEN BS 420 - 440, STRINGERS 28L - 29L. REPLACED FORWARD LAVATORY PAN DOUBLER IAW SRM 51-40-02.

Part: WINDOW — DELAMINATED (COCKPIT R3) · airframe 56,119 hrs · 15,670 cycles

R3 COCKPIT WINDOW HAD INTERNAL DELAMINATION IN THE LOWER SECTION. REPLACED THE R3 WINDOW IAW AMM 56-11-10.

Part: FLOOR SUPPORT — CORRODED (BS 365-377) · corrosion level 2 · airframe 56,119 hrs · 15,670 cycles

CORROSION FOUND ON THE CABIN FLOOR SUPPORT BETWEEN BS 365.25 - 377.7, RBL 24.75. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 56,119 hrs · 15,670 cycles

CORROSION FOUND ON THE FORWARD CABIN FLOOR GALLEY MOUNT FITTING. REPLACED THE GALLEY MOUNT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,119 hrs · 15,670 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION FOUND ON LONGERON LOCATED BETWEEN BS 1620-1640, AND RBL 45.50. REPAIRED FLOOR SUPPORT LONGERON PER SRM 51-40-02 & 51-40-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,119 hrs · 15,670 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION FOUND ON SEAT TRACK SUPPORT LOCATED BS 365.5 & 418, RBL 24.75. REPAIRED SEAT TRACK SUPPORT PER SRM 53-00-51-1A FIG 101 DET IV AND SRM 51-40-02.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,119 hrs · 15,670 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION FOUND ON CHANNEL LOCATED AT BS 1280-1300, AND RBL 45.50. REPLACED CHANNEL PER SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,119 hrs · 15,670 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION FOUND ON GUTTER SUPPORT (L2 DOOR) LOCATED AT BS 740 AND LBL 62. REPLACED GUTTER SUPPORT PER SRM 51-40-02 & 51-40-05.

Part: FITTING — CORRODED (BS 1280-1320) · corrosion level 2 · airframe 56,119 hrs · 15,670 cycles

CORRODED FITTINGS, BETWEEN BS 1280 - 1320, RBL 24.75 AND RBL 45.50. REPLACED THE FITTINGS IAW SRM 51-40-02.

Part: FITTING — CORRODED (BS 1280-1320) · corrosion level 2 · airframe 56,119 hrs · 15,670 cycles

CORROSION TO FITTINGS BETWEEN BS 1280 - 1320, LBL 24.75 TO LBL 45.50. REPLACED THE FITTINGS IAW SRM 51-40-02.

Part: FITTING — CORRODED (BS 1685) · corrosion level 2 · airframe 56,119 hrs · 15,670 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION TO FITTING AT BS 1685, BL 0. REPLACED FITTING IAW SRM 51-40-02.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 56,119 hrs · 15,670 cycles

L1 DOOR FLIGHT ATTENDANT SEAT FLASHLIGHTS INOPERATIVE AND L2 DOOR FLIGHT ATTENDANT SEAT. INSTALLED NEW BATTERIES IAW DRAWING 19P25D0060. OPS CHECKED GOOD.

Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 56,119 hrs · 15,670 cycles

L1 DOOR FLIGHT ATTENDANT SEAT FLASHLIGHT INOPERATIVE AND L2 DOOR. INSTALLED NEW BATTERIES IAW DRAWING 19P25D0060. OPS CHECKED GOOD.

Part: SEAT TRACK — BROKEN (BS 1320-1540) · airframe 56,119 hrs · 15,670 cycles

SEAT TRACK, BS 1320 - 1540, LBL 45 HAD 2 BROKEN LUGS. REPLACED THE SEAT TRACK IAW SRM 53-60-52-01, FIG 1, AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 365.25-377) · corrosion level 2 · airframe 56,119 hrs · 15,670 cycles

CORROSION WAS FOUND ON THE FLOOR SUPPORT, BETWEEN BS 365.25 - 377, RBL 45.55. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: CREASE BEAM — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 56,119 hrs · 15,670 cycles

CORROSION FOUND ON CREASE BEAM LOCATED AT BS 365.25, RBL 0-24.75. BLENDED CORROSION FOUND OUT OF LIMITS, FABRICATED REPAIR PART AND INSTALLED CORRECTED CREASE BEAM PER SRM 53-00-51-1A FIG 101 DET IV AND SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (BS 1664-1681) · corrosion level 2 · airframe 56,119 hrs · 15,670 cycles

CORROSION FOUND ON THE SUPPORT ANGLE, BS 1664 - 1681, RBL 10. REPLACED THE SUPPORT ANGLE IAW 51-40-02.

Part: WINDOW — DELAMINATED (L3) · airframe 55,792 hrs · 15,599 cycles

FLIGHT COMPARTMENT L3 WINDOW DELAMINATED LEFT LOWER CORNER. REPLACED THE L3 WINDOW IAW AMM 56-11-10. AIRCRAFT WAS GROUNDED.

Part: SLIDE — UNSERVICEABLE (L2 DOOR) · airframe 55,771 hrs · 15,593 cycles

AIRCRAFT WAS GROUNDED. 2L DOOR SLIDE BOTTLE PRESSURE IN RED ARC. REPLACE L2 DOOR SLIDE ASSEMBLY PER JOB CARD 19L80025002.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 55,673 hrs · 15,573 cycles

L2 DOOR SLIDE PRESSURE LOW. MAINTENANCE REPLACED THE SLIDE IAW 19L80025002 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FMC — FAULTY (LEFT)

THE FLIGHT DIVERTED DUE TO FMC LT OUTPUT LOSS. THE FLIGHT DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED FIM 34-61-00-815-820. REPLACED THE LEFT FMC IAW AMM 34-61-01. OPS CHECKED OK. THE AIRCRAFT WAS GROUNDED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 54,816 hrs · 15,388 cycles

AIRCRAFT NOT GROUNDED. FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED BATTERY IN FORWARD FLIGHT ATTENDANT FLASHLIGHT AS REQUIRED.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 53,815 hrs · 15,159 cycles

R1 DOOR ESCAPE SLIDE ARMED LIGHT INOPERATIVE. REMOVED DEBRIS FROM THE GIRT BAR. ARMED INDICATION OPS CHECKED NORMAL.

Part: RADAR — MALFUNCTIONED · airframe 53,481 hrs · 15,089 cycles

DURING TAKE OFF ROLL, THE WINDSHEAR TEST MODE ACTIVATED AND RADAR ON TERRAIN ANNUNCIATED. TAKE OFF ABORTED. FLIGHT CREW DEACTIVATED RADAR, PERFORMED RADAR TEST AND SYSTEM RETURNED TO NORMAL OPERATION. SUBSEQUENT TAKE OFF UNEVENTFUL

Part: RESERVOIR — LOW PRESSURE (R1 DOOR) · airframe 51,942 hrs · 14,756 cycles

DURING INSPECTION, FOUND THE L1 DOOR EMERGENCY POWER RESERVOIR PRESSURE UNSATISFACTORY. REPLACED L1 DOOR EMERGENCY POWER RESERVOIR IAW AMM 52-11-30.

Part: GIRT BAR — OBSTRUCTED (L1 DOOR) · airframe 51,919 hrs · 14,752 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR L1 OPENED, SLIDE DID NOT DEPLOY WHEN ARMED. INSPECTED GIRT BAR MOUNTS AND CLEANED DEBRIS FROM MOUNTS PER AMM 25-66-10.

Part: ACCESS DOOR — DAMAGED (ZONE 800) · airframe 51,618 hrs · 14,689 cycles

AIRCRAFT WAS NOT GROUNDED. ON ARRIVAL, FOUND RAM AIR ACTUATOR ACCESS PANEL FOR LEFT HAND PACK OPEN AND HINGES DAMAGED. MAINTENANCE REPLACED DOOR ASSEMBLY PER AMM 52-40-02. (SEE ALSO AALA201612229012 AND AALA201703089025).

Part: HINGE — DAMAGED (ZONE 800) · airframe 51,618 hrs · 14,689 cycles

AIRCRAFT WAS NOT GROUNDED. ON ARRIVAL, FOUND RAM AIR ACTUATOR ACCESS PANEL FOR LEFT HAND PACK OPEN AND HINGES DAMAGED. MAINTENANCE REPLACED HINGE PER AMM 52-40-02. (SEE ALSO AALA201612229012 AND AALA201703089026).

Part: HINGE — DAMAGED (ACCESS PANEL) · airframe 51,618 hrs · 14,689 cycles

ON ARRIVAL, FOUND RAM AIR ACTUATOR ACCESS PANEL FOR LEFT PACK OPEN AND HINGES DAMAGED. REPLACED IAW HINGE IAW AMM 52-40-02.

Part: GIRT BAR — LACK OF LUBE (R1 DOOR) · airframe 51,152 hrs · 14,592 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 1R SLIDE LIGHT NOT ILLUMINATED WITH SLIDE ARMED. CLEANED AND LUBRICATED 1R DOOR SLIDE GIRT BAR PER MM 25-66-01 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: FLOOR SUPPORT — CORRODED (BS 1510) · corrosion level 2 · airframe 50,758 hrs · 14,509 cycles

CORROSION ON AFT CARGO BAY FLOOR SUPPORT LBL 2.9 UPPER AND LOWER SURFACES AT BS 1510. REPAIRED FLOOR SUPPORT IAW ESO 90928 PART C STEPS A-J AND EA 263438A.

Part: FLOORBEAM — CORRODED (BS 1510) · corrosion level 2 · airframe 50,758 hrs · 14,509 cycles

CORROSION ON AFT CARGO BAY FLOORBEAM RBL 2.90 UPPER AND LOWER SURFACES AT BS 1510. REPAIRED THE FLOORBEAM IAW ESO 90928 PART C STEPS A-J AND EA 263438A.

Part: FLOORBEAM — CORRODED (BS 1510) · corrosion level 2 · airframe 50,758 hrs · 14,509 cycles

CORROSION ON AFT CARGO BAY FLOORBEAM LBL 11.40 UPPER AND LOWER SURFACES AT BS 1510. REPAIRED THE FLOORBEAM ESO 90928 AND EA 263438A STEPS A-J PART C AND SECTION A.

Part: FLOORBEAM — CORRODED (BS 1510) · corrosion level 2 · airframe 50,758 hrs · 14,509 cycles

CORROSION ON AFT CARGO BAY FLOOR SUPPORT RBL 7.55 UPPER AND LOWER SURFACES AT BS 1510. REPAIRED STRINGER PER ESO 90928 PART C STEPS A-J AND EA 263438A.

Part: FLOORBEAM — CORRODED (BS 1510) · corrosion level 2 · airframe 50,758 hrs · 14,509 cycles

CORROSION ON AFT CARGO BAY FLOORBEAM LBL 7.55 UPPER AND LOWER SURFACES AT BS 1510. REPAIRED THE FLOORBEAM IAW ESO 90928 STEPS A-J PART C AND SECTION A OF EA 263438A.

Part: FLOORBEAM — CORRODED (BS 1470) · corrosion level 2 · airframe 50,758 hrs · 14,509 cycles

CORROSION ON AFT CARGO BAY FLOORBEAM RBL 7.55 UPPER AND LOWER SURFACES AT BS 1470. REPLACED THE FLOORBEAM IAW SRM 51-40-02-OG, AND SRM 51-20-01.

Part: FLOORBEAM — CORRODED (BS 1470) · corrosion level 2 · airframe 50,758 hrs · 14,509 cycles

CORROSION ON AFT CARGO BAY FLOORBEAM RBL 10.45 LOWER SURFACE AT BS 1470. REPLACED THE FLOORBEAM IAW SRM 51-40-02-0G, AND SRM 51-20-01.

Part: FLOORBEAM — CORRODED (BS 1470) · corrosion level 2 · airframe 50,758 hrs · 14,509 cycles

CORROSION ON AFT CARGO BAY FLOORBEAM RBL 2.90 LOWER SURFACE AT BS 1470. REMOVED AND REPLACED THE FLOORBEAM SRM 51-40-02-OG, SRM 51-20-01.

Part: FLOORBEAM — CORRODED (BS 1330) · corrosion level 2 · airframe 50,758 hrs · 14,509 cycles

CORROSION ON AFT CARGO BAY FLOORBEAM AT RBL 16.10 UPPER AND LOWER SURFACES AT BS 1330. REPLACED FLOORBEAM SEGMENT IAW ESO 90928 AND 53-10-00-1 REPAIR 1.

Part: FLOORBEAM — CORRODED (BS 1470) · corrosion level 2 · airframe 50,758 hrs · 14,509 cycles

CORROSION ON AFT CARGO BAY FLOORBEAM RBL 16.10 BS 1470. REMOVED DAMAGED AREA IAW SRM 51-10-02-OG. REPLACED IAW SRM 51-40-02-0G, AND SRM 51-20-01.

Part: FLOORBEAM — CORRODED (BS 1330) · corrosion level 2 · airframe 50,758 hrs · 14,509 cycles

CORROSION ON AFT CARGO BAY FLOORBEAM RBL 2.90 UPPER AND LOWER SURFACES AT BS 1330. REPLACED THE FLOORBEAM SEGMENT IAW ESO 90928 AND 53-10-00-1 REPAIR 1.

Part: FLOOR PANEL — CORRODED (BS 1445-1530) · corrosion level 2 · airframe 50,758 hrs · 14,509 cycles

CORROSION ON AFT CARGO BAY RIGHT FLOOR PANEL UPPER AND LOWER SURFACES BETWEEN BS 1445 AND 1530 AT RBL 20. REPLACED THE FLOOR PANEL IAW SRM 51-40-02-0G, AND SRM 51-40-05-0G.

Part: FLOORBEAM — CORRODED (BS 1330) · corrosion level 2 · airframe 50,758 hrs · 14,509 cycles

CORROSION ON AFT CARGO BAY FLOORBEAM RBL 7.55 UPPER AND LOWER SURFACES AT BS 1330. REPLACED THE FLOORBEAM SEGMENT IAW ESO 90928, AND 53-10-00-1 REPAIR 1

Part: FLOORBEAM — CORRODED (BS 1330) · corrosion level 2 · airframe 50,758 hrs · 14,509 cycles

CORROSION ON AFT CARGO BAY FLOORBEAM RBL 10.45 UPPER AND LOWER SURFACES AT BS 1330. REPLACED FLOORBEAM SEGMENT IAW ESO 90928 AND 53-10-00-1 REPAIR 1.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 50,758 hrs · 14,509 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR SUPPORT ANGLE CRACKED BETWEEN BS 1320 AND BS 1340 AT BUTT LINE 0. REPLACED ANGLE IAW SRM 51-40-02 AND SRM 51-40-05.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 50,081 hrs · 14,361 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY FLASHLIGHT LOCATED UNDER THE JUMPSEAT AT THE L2 DOOR HAS A DEAD BATTERY. REPLACED EMERGENCY FLASHLIGHT BATTERY AND ACCOMPLISHED A SATISFACTORY OPS CHECK.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 50,058 hrs · 14,357 cycles

AIRCRAFT WAS NOT GROUNDED: RT FLOOR MOUNTED PHOTOLUMINESCENT STRIP INOPERATIVE FROM FORWARD GALLEY THRESHOLD TO R2 DOOR, BS 377.25 - BS 683. REPLACED FLOOR MOUNTED PHOTOLUMINESCENT STRIP AND ACCOMPLISHED A SATISFACTORY OPS CHECK.

Part: COVER — UNSECURE (CABIN) · airframe 49,832 hrs · 14,311 cycles

AIRCRAFT WAS NOT GNDED. PLASTIC COVER OVER FLOOR LIGHTING IS COMING OFF IN CABIN AT ROWS 18 - 21. SECURED CABIN FLOOR PLASTIC COVER STRIP, BETWEEN ROW 18 - 21 IAW AMM 33-51-15.

Part: DOUBLER — DEBONDED (LE SLAT) · airframe 49,527 hrs · 14,244 cycles

AIRCRAFT WAS GNDED. DISBOND ON LE LT NR 4 SLAT WEDGE, LOWER SURFACE EXTERNAL DOUBLER. REPAIRED SLAT IAW EA 259776.

Part: DOUBLER — DEBONDED (LE SLAT) · airframe 49,527 hrs · 14,244 cycles

AIRCRAFT WAS GNDED. DISBOND ON LE RT NR 7 SLAT WEDGE, LOWER SURFACE EXTERNAL DOUBLER. REPAIRED SLAT IAW EA 259773.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 48,907 hrs · 14,109 cycles

AIRCRAFT WAS GNDED. L2 DOOR SLIDE PRESS OUT OF LIMITS. REPLACED L2 DOOR SLIDE IAW TASK CARD 19L80025002.

Part: LIGHT — LOOSE (CABIN) · airframe 48,807 hrs · 14,088 cycles

AIRCRAFT WAS NOT GNDED. ROW 14 RT EMER LIGHT STRIP LOOSE FROM FLOOR. SECURED LIGHT STRIP AT ROW 14 RT.

Part: GIRT BAR — DEFECTIVE (R1 DOOR) · airframe 48,709 hrs · 14,069 cycles

AIRCRAFT WAS GNDED. DOOR 1R WILL NOT ARM. REPLACED 1R DOOR GIRT BAR. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 25-66-10.

Part: SLIDE RAFT — LOW PRESSURE (L4 DOOR) · airframe 48,540 hrs · 14,032 cycles

AIRCRAFT WAS NOT GNDED. L4 DOOR SLIDE & RAFT INDICATING BELOW GREEN AREA. REPLACED L4 DOOR SLIDE IAW 19L80025002.

Part: REFLECTOR — FAULTY (EXTERIOR LIGHT) · airframe 48,321 hrs · 13,987 cycles

AIRCRAFT WAS NOT GNDED. L4 DOOR EXTERIOR EMER LIGHT INOPERATIVE. R & R REFLECTOR ON L4 DOOR. OPERATIONS CHECKED GOOD.

Part: STRIP — LOOSE (CABIN) · airframe 48,307 hrs · 13,982 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT STRIP AT ROW 38 POPPING UP. SECURED STRIP TO FLOOR.

Part: D-RING — UNSECURE (R1 DOOR) · airframe 48,188 hrs · 13,953 cycles

FOUND R1 DOOR SLIDE STATIC LINE & D RING IMPROPERLY SECURED. PROPERLY SECURED D RING & STATIC LINE ON THE R1 DOOR IAW AMM 25-66-01-404-044.

Part: LIGHT — UNSECURE (CABIN) · airframe 48,070 hrs · 13,918 cycles

EMERGENCY LIGHT STRIP NEAR ROW 12 NOT SECURE TO FLOOR. SECURED EMER LIGHT STRIP.

Part: LENS — BUCKLED (CABIN) · airframe 48,070 hrs · 13,918 cycles

EMERGENCY FLOOR LIGHTING, BETWEEN ROW 11 - 12 BUCKLED. RESEATED EMER FLOOR LIGHTING COVER LENS.

Part: LIGHT — DETACHED (CABIN) · airframe 48,039 hrs · 13,907 cycles

FLOOR LEVEL EMER LIGHTING LIFTED, ROW 11. SECURED EMER LIGHT AS REQUIRED.

Part: LENS — DETACHED (CABIN) · airframe 48,029 hrs · 13,904 cycles

EMERGENCY LIGHT LENS AT ROW 11 DETACHED FROM FLOOR. SECURED LENS.

Part: LIGHT — LOOSE (CABIN) · airframe 48,007 hrs · 13,901 cycles

EMERGENCY LIGHT STRIP ON FLOOR AT 11D COMING UP. REPLACED COVER STRIP ON FLOOR AT ROW 11. CHECKED OK IAW AMM 25-27-31.

Part: LIGHT — LOOSE (CABIN) · airframe 47,938 hrs · 13,888 cycles

FLIGHT 750 EMERGENCY LIGHT STRIP AROUND ROW 11 IS LOOSE. APPLIED DOUBLE SIDED TAPE & RE-FITTED EMER LIGHT STRIP.

Part: LIGHT — BUCKLED (CABIN) · airframe 47,865 hrs · 13,867 cycles

FLIGHT 774, EMER STRIP LIGHTS ROW 11, BUCKLED & TRIP HAZARD. SECURED EMER STRIP LIGHT AT ROW 11. OPERATIONAL CHECKED GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 47,790 hrs · 13,843 cycles

EMERGENCY FLOOR STRIP LIGHTING RISING OFF FLOOR BETWEEN ROWS 11 & 12 ACFT LT. LIGHTING STRIP SECURED.

Part: LIGHT — BUCKLED (CABIN) · airframe 47,766 hrs · 13,838 cycles

ILLUMINATE STRIP IS BUCKLING UP BY SEAT 11D ON FLOOR. REMOVED BOTTLE CAP FROM UNDERNEATH ILLUMINATE STRIP & RESEATED STRIP AT ROW 11D.

Part: CHARGER — DEFECTIVE (CABIN) · airframe 47,747 hrs · 13,835 cycles

EMERGENCY EXIT LIGHT FLICKER ON & OFF FROM ROW 26 TO AFT GALLEY. REPLACED R4 DOOR BATTERY CHARGER & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-07.

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 47,740 hrs · 13,833 cycles

EMERGENCY LIGHTS FLICKER AGAIN IN CABIN AFT ZONE, OCCURRED AFTER LIFTOFF. REPLACED EMER POWER LIGHT SUPPLY & OPERATIONAL CHECKED GOOD IAW AMM 33-51-07-0222-020.

Part: LENS — LOOSE (CABIN) · airframe 47,490 hrs · 13,762 cycles

EMERGENCY EXIT PATH LIGHTING FLOOR STRIP IS LOOSE NEAR ROW 11. INSTALLED NEW PLASTIC LENS COVER.

Part: LIGHT — LOOSE (CABIN) · airframe 47,457 hrs · 13,756 cycles

FLOOR EXIT LIGHTING STRIP NEAR ROW 11 LOOSE. SECURED FLOOR LIGHTING STRIP AT ROW 11. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-15.

Part: GATE — CORRODED (L2 DOOR) · airframe 47,127 hrs · 13,682 cycles

C2 CHECK, L2 PAX DOOR LOWER GATE HAS CORROSION. R & R L2 DOOR LOWER GATE IAW SRM 51-40-02-0G, MM 52-11-38-404-009 & MM 52-11-00-501.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 47,127 hrs · 13,682 cycles

C2 CHECK, SEVERAL EMER EXIT SIGN LIGHTS ARE INOPERATIVE AT L4. REPLACED AFT LT EMER EXIT LIGHT POWER SUPPLY. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-07.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 47,127 hrs · 13,682 cycles

C2 CHECK, SEVERAL EMER EXIT SIGN LIGHTS ARE INOPERATIVE AT R3 & R4. REPLACED AFT RT EMER EXIT LIGHT POWER SUPPLY. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-07.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 47,127 hrs · 13,682 cycles

C2 CHECK, R1 DOOR RESERVOIR BOTTLE HAS LOW PRESS. REPLACED R1 DOOR RESERVOIR BOTTLE IAW AMM 52-11-30-401.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 45,637 hrs · 13,261 cycles

L1 SLIDE LOW PRESS. R & R THE L1 SLIDE.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 41,386 hrs · 12,021 cycles

PHOTOLUMINESCENT STRIP MISSING AT ROW 10, INSTALLED MISSING SECTION. OK FOR SERVICE.

Part: COVER — MISSING (CABIN) · airframe 40,786 hrs · 11,851 cycles

ESCAPE PATH MARKING AT ROW 9-11 LT SIDE COVER MISSING. INSTALLED NEW COVER ON ESCAPE PATH MARKING AT ROWS 9-11 LT SIDE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 40,358 hrs · 11,748 cycles

FWD RT F/A STATION FLASHLIGHT IS INOP. R & R FWD RT FLASHLIGHT LIGHT BATTERY AS REQUIRED.

Part: INDICATOR — LOOSE (CABIN) · airframe 39,389 hrs · 11,469 cycles

PHL - TRACK MOUNT EXIT INDICATOR COMING LOOSE AT ROW 11 ON A/C RIGHT, WITH THE FLOOR TRACK LIGHTING COVER CRACKED. REMOVED AND REPLACED CRACKED TOP OF E-LIGHTING STRIP AT ROW 11, RE-SECURED TO CABIN FLOOR.

Part: LIGHT — LOOSE (CABIN) · airframe 39,034 hrs · 11,372 cycles

FLL - EMERGENCY LIGHTS, EMERGENCY LIGHT FLOOR STRIP IS LOOSE AND LIFTING UP OFF THE FLOOR. SECURED PATH LIGHTING STRIP.

Part: LENS — MISSING (CABIN) · airframe 38,689 hrs · 11,260 cycles

SEA - R-4 DOORWAY EMERGENCY EXIT SIGN LENS COVER MISSING. INSTALLED LENS COVER ON EMERGENCY EXIT LIGHT AT R-4 DOOR.

Part: STRIP — UNSECURE (CABIN) · airframe 38,505 hrs · 11,199 cycles

PHL - EMERGENCY EXIT FLOOR STRIP LIGHTING COMING UP, ROW 11 ACFT RIGHT. SECURED STRIP AS REQUIRED.

Part: COVER — BROKEN (CABIN) · airframe 38,380 hrs · 11,157 cycles

CLT - PLASTIC COVER ON FLOOR FLUORESCENT EMERGENCY EXIT STRIP BROKEN. COVER LOCATED AIRCRAFT LEFT, RUNS 9 THROUGH 11. RE-INSTALLED FLOOR TRACK. OPS NORMAL.

Part: LIGHT — SHORTED (CABIN) · airframe 38,330 hrs · 11,136 cycles

CLT - EXIT PATH LIGHTING, ROW 9 AIRCRAFT LEFT, PLASTIC COVER UNFASTENED. REMOVED AND REPLACED R-2 DOOR SLIDE LIGHT ASSY. OP CHECKS GOOD.

Part: COVER — UNSECURE (CABIN) · airframe 38,050 hrs · 11,042 cycles

CLT - EMERGENCY EXIT COVER FROM ROW 10 DISLODGED. RE-SECURED EXIT COVER FROM ROW 10.

Part: TRACK — BUCKLED (CABIN) · airframe 37,859 hrs · 10,990 cycles

PHL - EMERGENCY TRACK LIGHTS (ROW 11) BUCKLED CAUSING PEOPLE TO TRIP. TRIMMED TO FIT & REMOVED DEBRIS.

Part: STRIP — UNSECURE (CABIN) · airframe 37,756 hrs · 10,965 cycles

PHL - LOW LEVEL EMERGENCY LIGHTING STRIP IS LOOSE AT ROW 11 DEF. RE-SECURED EMERGENCY LIGHT STRIP.

Part: STRIP — UNSECURE (CABIN) · airframe 37,752 hrs · 10,964 cycles

PHX - EMERGENCY IN FLOOR LIGHT STRIP ROW 12 PLASTIC COVER COMING OFF. RE-ATTACHED LIGHT STRIP TO FLOOR AS REQUIRED.

Part: LIGHT — UNSECURE (CABIN) · airframe 37,721 hrs · 10,954 cycles

PHL - EMERGENCY LIGHT; WITH ATTND PANEL SWITCH ON TRACK MOUNTED EXIT INDICATORS AS MAIN CABIN AREA OFF (TRACK LIGHTING LOOSE AT ROW 11). SECURED PHOTOLUMINESCENT TRACK LIGHTING AT ROW 11 AS REQUIRED, OK FOR SERVICE.

Part: TRACK — UNSECURE (CABIN) · airframe 37,541 hrs · 10,909 cycles

CLT - EMERGENCY PATH LIGHTING-TRACK, AFT ROW 12 A/C RT UN-ATTATCHED & BOWED CAUSING A TRIPPING HAZARD. SECURED EMERGENCY TRACK LIGHTING ROW 12, CHECK'S GOOD.

Part: COVER — UNSECURE (CABIN) · airframe 37,291 hrs · 10,838 cycles

EMERGENCY EXIT TRACK LIGHTING IS LIFTED (TRIP THREAT) AT ROWS 11-12. MAINTENANCE RE-SECURED EMERGENCY EXIT TRACK COVER. OK FOR SERVICE.

Part: LENS — UNSECURE (CABIN) · airframe 37,236 hrs · 10,823 cycles

FLOOR EMERGENCY EXIT LIGHTING PLASTIC COVER NEEDS RE-ATTACHING. MAINTENANCE RE-ATTACHED AND SECURED EMERGENCY EXIT LIGHTING PLASTIC COVER RIGHT SIDE FROM ROW 7 TO ROW 10.

Part: LIGHT — UNSECURE (CABIN) · airframe 37,213 hrs · 10,816 cycles

PHL - EMERGENCY FLOOR LIGHTING STRIP NEAR ROW 2 DISMOUNTED FROM TRACK ON BOTH SIDES OF AISLE. RE-SECURED EMERGENCY FLOOR LIGHTING AS REQUIRED.

Part: LIGHT — UNSECURE (CABIN) · airframe 37,206 hrs · 10,815 cycles

PHX - EMERGENCY FLOOR LIGHTING STRIP NEAR ROW 11 DISMOUNTED FROM TRACK. RE-ATTACHED FLOOR LIGHTING STRIP COVER TO BASE AS REQUIRED.

Part: TRACK — UNSECURE (CABIN) · airframe 37,192 hrs · 10,810 cycles

PHL - FLOOR EMERGENCY PATH LIGHTING LOOSE FROM FLOOR NEAR SEAT 11C. INSTALLED MISSING CLEAR FLUSH TOP TRACK & RE-SECURED IT BACK TO A/C.

Part: STRIP — UNSECURE (CABIN) · airframe 36,974 hrs · 10,749 cycles

PHL - CLEAR PLASTIC STRIP THAT COVERS CABIN FLOOR EMERGENCY LIGHTS HAS COME OFF. STRIP NOW LOCATED IN COCKPIT. RE-SECURED PLASTIC STRIP.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 36,964 hrs · 10,746 cycles

AMS - EMER/ LIGHTS ROWS 11 LEFT AND 13 RIGHT EXTENDED UP FROM FLOOR. STOWED IN CORRECT POSITION NOW.

Part: LIGHT — UNSECURE (CABIN) · airframe 36,948 hrs · 10,742 cycles

PHL - EMERGENCY LIGHT: FLOOR TRACK EMERGENCY LIGHTS COMING UP OFF FLOOR ROW 11 LEFT AND ROW 13 R. SECURED EMERGENCY LIGHTING TRACKS AR ROWS 11L AND 13R.

Part: LIGHT — DAMAGED (CABIN) · airframe 36,933 hrs · 10,739 cycles

DUB - EMERGENCY TRACK LIGHTS PULLED UP ROW 10/11 AIRCRAFT LEFT. MAINTENANCE RE-SECTIONED THE AFFECTED ROWS WITH ENOUGH MATERIAL TO COMPLY WITH THE MEL DEFERRAL PROCEDURES. MAINTENANCE COMPLETED THE MEL DEFERRAL PROCEDURES AND RELEASED THE AIRCRAFT FOR FLIGHT. MAINTENANCE REPLACED FLOOR PATH COVERING AS REQUIRED. OK FOR SERVICE. REMOVED THE MEL DEFERRAL.

Part: COVER — OUT OF POSITION (CABIN) · airframe 36,895 hrs · 10,727 cycles

CLT - EMERGENCY LIGHTS MID FWD, WITH ATTND PANELS ON TRACK MOUNTED EXIT INDICATORS AT MAIN CABIN AREA OFF. ALL OTHER LIGHTS NORMAL. INSTALLED EMERGENCY LIGHT TRACK COVER.

Part: COVER — UNSECURE (CABIN) · airframe 36,855 hrs · 10,709 cycles

CLT - WHITE TAPE HOLDING DOWN EMERGENCY EXIT LIGHTING ON CENTER AISLE FROM ROW 9 TO ROW 11 IS NOT HOLDING DOWN EMERGENCY LIGHT STRIP. WHEN A/C PRESSURIZES. STRIP RAISES ABOUT 2 INCHES OFF FLOOR. RE-SECURED PLASTIC COVER OVER EMERGENCY LIGHTS, OPS CHECK GOOD.

Part: BEARING SUPPORT — BROKEN (RT GOVERNOR) · airframe 36,810 hrs · 10,690 cycles

YQX FLT 725 EN ROUTE DUB TO CLT. R ENGINE EXCEEDED LIMITS/OVERSPEED (AT CRUISE ALTITUDE). PERFORMED QRH PROCEDURES. R ENG TEMP REMAINED HIGH (AT RED) WHEN THRUST LEVER RETARDED. R ENGINE WAS SHUT DOWN. THE FLIGHT DIVERTED TO YQX AND LANDED WITHOUT FURTHER INCIDENT. SINGLE ENGINE TIME WAS 90 MINUTES. ACCOMPLISHED FIM TASKS FOR "NO RESPONSE TO THRUST MOVEMENT", AND "N1 OVERSPEED FAULT" ON THE RIGHT ENGINE. ALSO ACCOMPLISHED A RIGHT ENGINE LP TURBINE BORESCOPE. NO DISCREPANCIES WERE NOTED. ACCOMPLISHED TASKS LED TO FFG REPLACEMENT. REPLACED THE RIGHT ENGINE FUEL FLOW GOVERNOR. RIGHT ENG OPERATES NORMAL. ALL PARAMETERS ARE NORMAL. LPV BEARING SEAT BROKEN. REPLACED LPV BEARING SEAT.

Part: SILL — CORRODED (FUSELAGE) · airframe 36,787 hrs · 10,682 cycles

C4 CHECK - CORROSION ON FLOOR SILL WEB BETWEEN BS 1320 TO BS 1360, S17R. REPAIRED FLOOR SILL WEB BETWEEN BS 1320 TO BS 1360, S17R IAW B757 SRM 51-10-02 SEC 9 & BOEING DRAWING 146N8326.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,787 hrs · 10,682 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT BS 1640, BBL 0 TO RBL 55. REPAIRED SEAT TRACK AT BS 1640, BBL 0 TO RBL 55 IAW B757 SRM 53-00-51 & BOEING DRAWING 146N5089.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,787 hrs · 10,682 cycles

C4 CHECK - EXFOLIATION CORROSION ON FLOORBEAM AT BS 365, RBL 12. REPAIRED FLOORBEAM AT BS 365, RBL 12 IAW B757 SRM 53-00-51 R2.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,787 hrs · 10,682 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON R-4 DOOR SUPPORT CHANNEL AT BS 1660, S17R. REPAIRED R-4 DOOR SUPPORT CHANNEL AT BS 1660, S17R IAW B757 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,787 hrs · 10,682 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT BS 1640, RBL 58. REPAIRED FLOORBEAM AT BS 1640, RBL 58 IAW EA 103876.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,787 hrs · 10,682 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON THRESHOLD SUPPORT CHANNEL BETWEEN BS 1660 TO BS 1680 AT R4 DOOR OPENING. REPAIRED THRESHOLD SUPPORT CHANNEL BETWEEN BS 1660 TO BS 1680 AT R4 DOOR OPENING IAW B757 SRM 51-10-02.

Part: CAP — BROKEN (CABIN) · airframe 35,492 hrs · 10,251 cycles

CLT - OVERHEAD 'EMERGENCY DOOR' ANNUNCIATOR CAP BROKEN OFF. INSTALLED CAP.

Part: GIRT BAR — LACK OF LUBE (R2 DOOR) · airframe 35,459 hrs · 10,238 cycles

CLT - 2R EVACUTION SLIDE BINDING WHEN ARMING. LUBRICATED GIRT BAR MECHANISM & ENGAGEMENT PLATES.

Part: PLACARD — OUT OF POSITION (R1 DOOR) · airframe 34,599 hrs · 10,026 cycles

CLT - EVACUATION SLIDE ARMING LEVER BINDING AT DOOR 1R. ADJUSTED "DISARMED" PLACARD, OPS NORMAL.

Part: LATCH — FAILED (OXYGEN MASK) · airframe 34,229 hrs · 9,916 cycles

FLIGHT 798: F/A REPORTED THAT DURING CABIN ALTITUDE EVENT WHEN THE CABIN OXYGEN SYSTEM WAS MANUALLY TURNED ON SEVERAL OXYGEN MASK DID NOT DEPLOY. FOUND OXYGEN CANISTERS INTERFERING WITH DOOR DROP HINGE REPOSITIONED OXYGEN CANISTERS PERFORMED DOOR LATCH MECHANISM TEST PER TASK 35-21-00-705-076 OPS CHECKS NORMAL. ALSO REPLACED 2 O2 MASK THAT WERE FOUND TORN.

Part: CONTROLLER — UNRELIABLE (CABIN PRESSURE)

PHL FLT 798 EN ROUTE PHL TO AMS. UNABLE TO CONTROL CABIN PRESSURE IN ANY MODE. AN EMERGENCY DESCENT WAS PERFORMED AND THE OXYGEN MASKS WERE MANUALLY DEPLOYED. THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NUMBER ONE PRESSURE CONTROLLER AND RECONNECTED THE RUBBER BOOT ON THE RIGHT PACK OUTFLOW DUCT FLANGE. ALSO REPLACED THE CABIN PRESSURE SELECTOR PANEL AND NUMBER TWO CABIN PRESSURE CONTROLLER AS A PRECAUTION.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

MCO - THE AFT FLIGHT ATTENDANT FLASHLIGHT WAS INOPERATIVE. REPLACED BATTERY IN THE AFT FLIGHT ATTENDANT FLASHLIGHT.

Part: SLIDE RAFT — LOW PRESSURE (PAX DOOR)

PHL - THE AFT PASSENGER, NUMBER FOUR DOOR RIGHT SLIDE HAS LOW PRESSURE IN SLIDE/RAFT INFLATION BOTTLE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR RIGHT PASSENGER DOOR SLIDE/RAFT ASSEMBLY.

Part: OIL CAP — MISINSTALLED (OIL TANK)

PHX FLT 1540 EN-ROUTE PHX TO CLT. AT CRUISE ALTITUDE, THE CREW NOTICED THAT THE LEFT ENGINE OIL QUANTITY WAS DROPPING. THE OIL TEMP AND PRESSURE, AS WELL AS ENGINE VIBRATION LEVELS WERE NORMAL. THE FLIGHT WAS ADVISED TO RETURN TO PHX. THE CREW DECLARED AN EMERGENCY AND RETURNED TO PHX WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE NUMBER ONE ENGINE AND FOUND THE OIL TANK CAP NOT INSTALLED. THE CAP WAS INSPECTED AND INSTALLED BACK ONTO THE OIL TANK. MAINTENANCE RAN THE NUMBER ONE ENGINE. NO LEAKS WERE FOUND.

Part: WARNING SWITCH — MALFUNCTIONED (CABIN PRESSURE)

FLL FLT 921 EN-ROUTE AUA TO PHL. DURING CRUISE, THE COCKPIT CREW OBSERVED A CABIN ALTITUDE WARNING. THE FLIGHT DESCENDED DOWN TO 10,000 FEET AND DIVERTED TO FLL. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED A CABIN ALTITUDE WARNING SWITCH.

Part: LEAF SPRING — BROKEN (EVAC SLIDE)

PHX - THE L1 DOOR SLIDE GIRT BAR LEAF SPRING IS BROKEN. MAINTENANCE REMOVED AND REPLACED BROKEN SPRING.

Part: INVERTER — DEFECTIVE (ZONE 100)

PHX FLT 813 EN ROUTE CUN TO PHX. THE CREW REPORTS: STANDBY ATTITUDE INDICATOR GYRO FLAG IN VIEW. SAI TUMBLED, AND ACCOMPLISHED IMMEDIATE ACTION ITEMS SMOKE FIRE FUMES PROCEDURE IN QRH. SHUT OFF LIGHTS IN CABIN - UTILITY BUSS SWITCHES OFF: ELECTRICAL SMELL WENT AWAY. F/A NOTED HEAVY ELECTRICAL SMELL AT ROW 17. MAINTENANCE FINDINGS: FOUND INVERTER PROCESSOR FOR STANDBY ATTITUDE INDICATOR BURNED, AND STANDBY ATTITUDE INDICATOR FAILED DUE TO POWER SUPPLY FAILURE IN INVERTER PROCESSOR. POWER SUPPLY BURNED UP. REMOVED AND REPLACED SAI AND INVERTER PROCESSOR.

Part: SENSOR — FAILED (CABIN)

HNL FLT 807 EN-ROUTE HNL TO PHX. THE AIRCRAFT EXPERIENCED AN "OVBD EX/OPEN" STATUS DISPLAY, FOLLOWED BY A CLIMB IN CABIN ALTITUDE. THE FLIGHT DESCENDED TO FL 270 WHERE THE CABIN ALTITUDE STABILIZED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD HNL. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED AN ACP BITE ON CABIN PRESSURE CONTROLLER AUTO 1 AND 2. NO FAULTS WERE NOTED. PERFORMED OVERBOARD EXHAUST VALVE OPERATIONAL CHECK. AN "EQPT CLG SENSOR" MESSAGE DISPLAYED. THE AIRCRAFT HAD THE EQUIPMENT COOLING AIRFLOW DETECTION SYSTEM PLACED ON MEL. IT WAS LATER FIXED BY REPLACING THE FORWARD SUPPLY LOW FLOW SENSOR. OPERATIONALLY CHECKS OK.

Part: LOCK PLATE — DETACHED (RT ENGINE)

FLT 1556 EN ROUTE AT 26,000 FT, CAPTAIN FELT A YAW & HEARD A COMPRESSOR STALL COMING FROM RT ENGINE. ENGINE READINGS NORMAL. HOWEVER, A PASSENGER SAW FIRE COMING FROM RT ENGINE DURING STALL. CAPTAIN DECLARED AN EMERGENCY & FLT DIVERTED. DURING TAXI TO GATE, RT ENGINE OIL PRESSURE DROPPED & OIL TEMP CLIMBED TO RED. CREW SHUTDOWN RT ENGINE & TAXIED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED RT ENGINE. REPAIR SHOP REPORTED THE COMBINATION OF HEAVY SPALLING OF ATTRITION LINING OF HPC CASES & IOD OF HPC BLADES CAUSED REPORTED HPC SURGE. IOD CAUSED BY THE LIBERATION OF STAGE 2 LOCK PLATE.

Part: TRANSMITTER — MALFUNCTIONED (ENGINE EPR)

FLT 1071. LEFT ENGINE INDICATIONS (ALL) FLUCTUATING, ENGINE SURGING. THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS PLACED ON MEL. REMOVED AND REPLACED LEFT ENGINE EPR TRANSMITTER. RAN ENGINE AND BITE CHECKED EEC. NO DEFECTS NOTED.

Part: SEAL — MISSING (LIFE RAFT)

AFT RAFT MISSING SEAL. REMOVED AND REPLACED THE SLIDE/RAFT ASSEMBLY.

Part: SLIDE — LOW PRESSURE (L2 DOOR)

PHL - THE 2L DOOR SLIDE PRESSURE WAS FOUND LOW (RED). MAINTENANCE REPLACED 2L DOOR SLIDE.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

PHL - THE FLASHLIGHT AT MID-CABIN WAS INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT ASSEMBLY.

Part: PRESSURE SWITCH — FAILED (ENGINE)

ORF PHL-MCO FLT NR 1727 20 MINUTES AFTER TAKEOFF CREW RECEIVED A FUEL FILTER STATUS MESSAGE FOR NR 2 ENGINE. FLIGHT DIVERTED TO ORF PER QRH. MAINTENANCE REPLACED THE LOW PRESSURE FUEL FILTER ON NR 2 ENGINE. NO FAULT FOUND. REPLACED NR 2 ENGINE DIF PRESSURE SWITCH. LEAK AND OPS CHECKS OK.

Part: CONNECTOR — UNSECURE (RT GENERATOR) · airframe 22,167 hrs · 6,931 cycles

FLIGHT 752, SEA-PHL: AFTER TAKEOFF, RIGHT GENERATOR OFF LIGHT ILLUMINATED FOLLOWED BY APU GENERATOR OFF LIGHT. FLIGHT RETURNED TO FIELD. MAINTENANCE RE-SEATED THE ENGINE FIREWALL CONNECT PLUG AS2080N010. NO FURTHER FAULTS.

Part: CHECK VALVE — CHATTERING (APU) · airframe 21,175 hrs · 6,714 cycles

FLIGHT 728, PHL-GLA: CREW REPORTED A RHYTHMIC KNOCKING SOUND IN THE AREA OF SEAT 13A. FLIGHT RETURNED TO PHL. MAINTENANCE REPLACED THE APU CHECK VALVE.