N175AN

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,137 hrs · 16,372 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL PETWEEN BS 1410 AND BS 1530 AT LBL 30. REPLACED TRANSITION PANEL PER SRM 51-70-00. SUPPLEMENTAL REPORT TO UPDATE SECTION 7 CORROSION LEVEL TO REFLECT 2.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · airframe 57,137 hrs · 16,372 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT LEFT HAND TRANSITION PANEL BETWEEN BS 1310 AND BS 1410. REPLACED TRANSITION PANEL PER SRM 53-00-51-1A.

Part: SKIN — CRACKED (RT WING) · airframe 57,137 hrs · 16,372 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING UPPER SURFACE SKIN DRAG FITTING MOUNTING AREA FASTENER HOLE#12 CRACKED. REPAIRED SKIN PER EA 300899.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,137 hrs · 16,372 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO DOOR CUT OUT LOWER SILL PLATE BETWEEN BS 1380 AND BS 1440 AT S27R. REPLACED SILL PLATE PER SRM 51-70-00 AND 51-00-05-1.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,137 hrs · 16,372 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 1200 AND BS 1310 AT RBL 45. REPLACED TRANSITION PANEL PER SRM 53-00-51-1A.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,137 hrs · 16,372 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 1200 AND BS 1310 AT S27L. REPLACED TRANSITION PANEL PER SRM 51-70-00.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,137 hrs · 16,372 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 1530 AND BS 1640 AT LBL 30. REPLACED TRANSITION PANEL PER SRM 51-70-00. SUPPLEMENTAL REPORT TO UPDATE SECTION 7 CORROSION LEVEL TO REFLECT 2.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,137 hrs · 16,372 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 1310 AND BS 1380 AT S27R. REPLACED TRANSITION PANEL PER SRM 51-70-00.

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,137 hrs · 16,372 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT RIGHT HAND SIDE TRANSITION PANEL BETWEEN BS 1440 AND BS 1530. SUPPLEMENTAL REPORT: REPLACED TRANSITION PANEL PER SRM 51-70-00. (CLOSED)

Part: TRANSITION PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,137 hrs · 16,372 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL BETWEEN BS 1530 AND BS 1640 AT S27R. REPLACED TRANISTION PANEL PER SRM 51-70-00.

Part: DECK PLATE — CORRODED (BS 1680) · corrosion level 2 · airframe 57,137 hrs · 16,372 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA FLOOR DECK PLATE AT BS 1680 AND RBL 53. REPLACED DECK PLATE.PER AARD 51-00-05-1.

Part: MOUNT — CORRODED (LAVATORY) · corrosion level 2 · airframe 57,137 hrs · 16,372 cycles

AIRCRAFT IN BASE VISIT: LH AFT LAV MOUNT HAS CORROSION AT STA1638, LBL24. REPLACED LH LAV MOUNT IAW AARD 51-00-05-1.

Part: MOUNT — CORRODED (BS 1638) · corrosion level 2 · airframe 57,137 hrs · 16,372 cycles

AIRCRAFT IN BASE VISIT: LAV MOUNT HAS CORROSION AT STA1638, LBL45. REPLACED LAV MOUNT IAW AARD 51-00-05-1.

Part: OVEN — SMOKE (GALLEY) · airframe 56,226 hrs · 16,094 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS SMOKE IN THE CABIN AT THE GATE. MAINTENANCE FOUND OVEN IN FWD GALLEY TO BE THE SOURCE. REMOVED AND REPLACED FWD OVEN IAW AMM 25-31-05. NO FURTHER SMOKE NOTED.

Part: CONTROL PANEL — FAILED (COCKPIT) · airframe 56,206 hrs · 16,089 cycles

AIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO JFK ON ACCOUNT OF RADIO ISSUE. COMPLETE VHF COMM FAILURE AFTER DEPARTURE. EMERGENCY DECLARED. MAINTENANCE TROUBLESHOT AND FOUND LEFT AUDIO CONTROL PANEL CAUSING ALL VHFS NOT TO OPERATE. REPLACED LEFT AUDIO CONTROL PANEL AS IAW AMM 23-51-01, ALL VHFS OPS CHECK NORMAL IAW AMM 23-51-01.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 55,068 hrs · 15,750 cycles

MAINTENANCE FOUND SEAT 3E AFT EMERGENCY LIGHT INOPERATIVE. SECURED A LOOSE CONNECTOR UNDER THE SEAT, OPS CHECKED OK IAW AMM 33-51-00.

Part: UNKNOWN — VIBRATION (AIRFRAME) · airframe 53,512 hrs · 15,287 cycles

DURING CLIMB AT 37000 FT, HEARD AND FELT LOW RUMBLING IN THE AIRFRAME. POSSIBLELY A LT ENGINE COMPRESSOR STALL. LEFT ENGINE EXHAUST GAS TEMPERATURE ROSE. AMBER LIGHT ON ENGINE GAS TERMPERATURE INDICATOR. ODOR OF ACRID FUMES NOTICED IN THE COCKPIT AND A REPORT FROM FLIGHT ATTENDANTS IN THE CABIN. NO VISIBLE SMOKE. RETURN TO LAND. TORN OFF LEFT ENGINE BLEED WHILE DESCENDING. ENGINE INDICATIONS REMAINED NORMAL, FUMES DISSIPATED. AIRCRAFT TAKEN OUT OF SERVICE. ACCOMPLISHED MCM 72-92-12, COMPRESSOR SURGE, NO FAULTS NOTED SIC 05-96-70, SMOKE ODOR FUMES, NO ODOR NOTED.MCM 72-92-12, LEFT ENGINE OIL FILTER CHANGE. SIC 4919, LEFT ENGINE OIL SYSTEM CHIP DETECTORS CHECK, AND SERVICED, ALL OK. OK FOR SERVICE.

Part: MEGAPHONE — DAMAGED (CABIN) · airframe 52,221 hrs · 14,975 cycles

FIRST CLASS MEGAPHONE BATTERY TRAY CORRODED. REPLACED THE MEGAPHONE IAW AMM 25-64-00.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 51,832 hrs · 14,858 cycles

AFT R3 DOOR EXIT SIGN LENS BROKEN. REPLACED THE LENS IAW MM 33-51-10.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 51,832 hrs · 14,858 cycles

AFT EXIT SIGN EMERGENCY LIGHT AT THE R3 DOOR, THE LENS WAS FOUND BROKEN. REPLACED THE LENS IAW MM 33-51-10. OPS CHECKED GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 51,550 hrs · 14,763 cycles

BROKEN EMERGENCY LIGHT AT SEAT 3E. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY AND PERFORMED SUCCESSFUL OPERATIONAL CHECK IAW WDM 33-51-21. AIRCRAFT WAS GROUNDED

Part: LENS — MISSING (CABIN) · airframe 51,098 hrs · 14,620 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EVACUATION SLIDE ARMED LIGHT ABOVE THE L2 DOOR HAS A MISSING LENS COVER. REPLACED LENS COVER PER AMM 33-13-00. OPERATIONAL CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 50,879 hrs · 14,572 cycles

FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT THE L2 JUMPSEAT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW AMM 25-64-00. OPS CHECKED GOOD.

Part: BUSTLE — CRACKED (EVAC SLIDE) · airframe 50,691 hrs · 14,524 cycles

AIRCRAFT WAS NOT GROUNDED. R4 DOOR ESCAPE SLIDE BUSTLE HAS A SMALL CRACK IN THE UPPER LEFT HAND CORNER. REMOVED AND REPLACED SLIDE BUSTLE PER AMM 52-11-02. OPERATIONAL CHECK GOOD. (CLOSED)

Part: GIRT BAR — OBSTRUCTED (R4 DOOR SLIDE) · airframe 50,553 hrs · 14,497 cycles

ON ARRIVAL, FLIGHT ATTENDANT WAS UNABLE TO FULLY DISARM THE R4 DOOR. CLEARED DEBRIS FROM THE GIRT BAR AREA. OPS CHECKED GOOD IAW AMM 52-11-00.

Part: CONNECTOR — LOOSE (CABIN) · airframe 50,448 hrs · 14,473 cycles

AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 12D IS INOPERATIVE. RESEATED LOOSE CONNECTOR ON MODULE IAW AMM 33-51-11. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,116 hrs · 14,116 cycles

AIRCRAFT NOT GROUNDED. SEAT MOUNTED ESCAPE PATH LIGHTS IN FIRST CLASS ARE VERY DIM. REMOVED AND REPLACED BATTERY PACK AT L1 DOOR IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: TACH GENERATOR — FAULTY (RT ENGINE) · airframe 48,996 hrs · 14,085 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. MIA-LPB FLIGHT DIVERTED TO PTY ACCOUNT RIGHT ENGINE N3 TACHOMETER AND PRESSURIZATION. LANDING UNEVENTFUL. REMOVED AND REPLACED HIGH PRESSURE N3 TACHOMETER GENERATOR IAW AMM 77-12-02. OPERATIONAL CHECK GOOD.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 48,690 hrs · 14,026 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. PREVIOUS CORROSION BLEND OUT ON FLOORBEAM 365.25 AT RBL 12 FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM IAW SRM 53-00-51-2R-5.

Part: CONNECTOR — NOT SEATED (EVAC SLIDE) · airframe 48,614 hrs · 14,013 cycles

AIRCRAFT NOT GROUNDED. LEFT OFF-WING EMERGENCY ESCAPE SLIDE PRESSURE BOTTLE SQUIB FAILED TEST. RESEATED LEFT SQUIB CONNECTOR IAW AMM 25-65-00. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — NOT SEATED (EVAC SLIDE) · airframe 48,614 hrs · 14,013 cycles

AIRCRAFT NOT GROUNDED. RIGHT OFF-WING EMERGENCY ESCAPE SLIDE PRESSURE BOTTLE SQUIB FAILED TEST. RESEATED RIGHT SQUIB CONNECTOR IAW AMM 25-65-00. OPERATIONAL CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 46,832 hrs · 13,546 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHTS BETWEEN ROWS 9 & 15 RT INOPERATIVE. R & R POWER SUPPLY & BATTERY PACK IAW AMM 33-51-07. SYS CHECKED NORMAL. SEE ALSO AALA 20160420006.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,832 hrs · 13,546 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHTS BETWEEN ROWS 9 & 15 RT ARE INOPERATIVE. R & R POWER SUPPLY & BATTERY PACK IAW AMM 33-51-07. SYS CHECKED NORMAL. SEE ALSO AALA 20160420004.

Part: BATTERY — DISCHARGED (CABIN) · airframe 46,771 hrs · 13,533 cycles

AIRCRAFT WAS NOT GNDED. L1 DOOR EXTERIOR EMER LIGHT IS INOPERATIVE. R & R M731 CHARGER & BATTERY IAW AMM 33-51-07. ACCOMPLISHED OPERATIONAL TEST IAW AMM 33-51-00. SYS TESTED NORMAL. SEE ALSO AALA 20160413001.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 46,771 hrs · 13,533 cycles

AIRCRAFT WAS NOT GNDED. L1 DOOR EXTERIOR EMER LIGHT IS INOPERATIVE. R & R M731 CHARGER & BATTERY IAW AMM 33-51-07. ACCOMPLISHED OPERATIONAL TEST IAW AMM 33-51-00. SYS TESTED NORMAL. SEE ALSO AALA 20160413002.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 45,090 hrs · 13,141 cycles

UPON ARRIVAL, THE RT RAM AIR ACTUATOR DOOR WAS FOUND TO BE OPEN & TO HAVE CREATED A HOLE IN THE WING TO BODY PANEL, AFT OF THE DOOR. REPAIRED THE PANEL IAW SRM 53-00-72-2R.

Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 45,060 hrs · 13,132 cycles

WEATHER RADAR FAILED DURING FLIGHT. AN EMER WAS DECLARED & THE FLIGHT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. R & R WEATHER RADAR TRANSCEIVER IAW MM 34-43-01. OPERATIONALLY CHECKED OK.

Part: TACH GENERATOR — FAULTY (RT ENGINE) · airframe 44,058 hrs · 12,911 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB RT ENG N3 INDICATION FLUCTUATED WIDELY. R & R RT ENG N3 TACH GEN IAW AMM 77-12-02. ACCOMPLISHED HIGH POWER ASSURANCE RUN IAW AMM 71-00-00 WITH ALL INDICATIONS NORMAL. SYS CHECKED NORMAL.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 43,341 hrs · 12,742 cycles

SEAT MOUNTED EMER LIGHT AT 2E IS INOPERATIVE. R & R DAMAGED CONNECTOR IAW SWPM 20-64-17. PERFORMED OPERATIONAL TEST IAW AMM 33-51-11. SYS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,891 hrs · 12,638 cycles

ROW 33 EMER LIGHT INOPERATIVE. R & R LAMP IN EMER LIGHT. PERFORMED OPERATIONAL CHECK IAW AMM 33-51-01. SYS CHECKED NORMAL.

Part: TRANSMITTER — FAILED (WX RADAR SYS) · airframe 42,548 hrs · 12,562 cycles

DURING CLIMB WEATHER RADAR FAILED, EMERGENCY WAS DECLARED. LANDING UNEVENTFUL. R & R WEATHER RADAR TRANSMITTER IAW AMM 34-43-01 401. OPERATIONAL TEST PERFORMED IAW AMM 34-43-00-715-139-001. SYS CHECKED NORMAL.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 42,217 hrs · 12,484 cycles

EMERGENCY ESCAPE PATH LIGHTS AT SEAT 1EF INOPERATIVE. R & R EXTENSION HARNESS IAW AMM 33-51-00. SYS CHECKED NORMAL.

Part: COVER — MISSING (EXIT SIGN) · airframe 41,630 hrs · 12,338 cycles

LEFT NR 1 DOOR AFT EMER EXIT SIGN COVER MISSING. REPLACED AFT EMER EXIT SIGN COVER. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,431 hrs · 12,285 cycles

EMERGENCY LIGHT OVER SEAT 15D INOPERATIVE. REPLACED LAMP FOR EMER LIGHT OVER SEAT 15D. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,431 hrs · 12,285 cycles

RIGHT NR 2 EXTERIOR EMER LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 2 EXTERIOR EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: FLEX LINE — LEAKING (HYDRAULIC SYS) · airframe 41,067 hrs · 12,187 cycles

RIGHT HYD SYS FLUID LOSS ON CLIMB OUT. EMER DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND RT UPPER RUDDER PCA FLEX LINE LEAKING. REPLACED FLEX LINE. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,952 hrs · 12,160 cycles

LEFT NR 2 DOOR EXTERIOR EMER LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 2 DOOR EXTERIOR EMER LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,952 hrs · 12,160 cycles

LEFT SIDE EMER EXIT ROW EMER LIGHT INOPERATIVE. REPLACED LAMPS FOR LT SIDE EMER EXIT ROW LIGHT. OPERATIONS CHECKED NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 38,832 hrs · 11,644 cycles

FIRST CLASS GALLEY EMERGENCY FLOOD LIGHT INOPERATIVE. FOUND BROKEN WIRE AT CONNECTOR D9896. REPAIRED WIRING AT CONNECTOR. OPERATIONS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,721 hrs · 11,620 cycles

FIRST CLASS EMERGENCY LIGHTS ARE INOPERATIVE & COACH EMERGENCY LIGHTS WORK INTERMITTENTLY. REPLACED BATTERY PACK & MODULE AT RT NR 2 DOOR.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 11,600 cycles

APU INLET SUPPORT STRUCTURE, LOWER SUPPORT ANGLE IS CORRODED AT STRINGER 6 RT FROM BS 1815 TO 1825. REMOVED CORRODED ANGLE & INSTALLED NEW ANGLE IAW SRM 51-40-02.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,652 hrs · 11,600 cycles

AUXILIARY POWER UNIT INLET SUPPORT STRUCTURE, FORWARD STRAP IS CORRODED AT STATION 1787.45 & STRINGER 5 TO 6 RT. REMOVED CORRODED STRAP & INSTALLED NEW STRAP IAW SRM 51-40-02 & SRM 51-10-02 PARAGRAPH 9.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,652 hrs · 11,600 cycles

AFT PIT LT FRAME AT BS 1480 HAS A DENT. ACCOMPLISHED REPAIR TO FRAME, BS 1480 LT IAW B757-200 SRM 5300-07-2R-5 FIGURE 201, DETAIL III & DRAWING 140N2063 IAW B757-200 SRM 53-00-07-2R-5 FIG 201, TABLE I.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,652 hrs · 11,600 cycles

AFT PIT LT FRAME AT STATION 1440 HAS A DENT. ACCOMPLISHED REPAIR TO FRAME IAW B757-200 SRM 53-00-07-2R-5 FIGURE 201 DETAIL I.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 36,490 hrs · 11,078 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT OVERWING EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: SIGN — DAMAGED (CABIN) · airframe 36,195 hrs · 10,995 cycles

RIGHT AFT GALLEY RIGHT NUMBER 4 DOOR EMERGENCY EXIT SIGN MISSING LENS AND DAMAGED. REPLACED RIGHT AFT GALLEY EXIT SIGN. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,307 hrs · 10,773 cycles

LEFT NUMBER 1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 DOOR EXTERIOR EMERGENCY EXIT LIGHT. OPS CHECK NORMAL.

Part: WIRE HARNESS — DISCONNECTED (CABIN) · airframe 35,307 hrs · 10,773 cycles

EMERGENCY EXIT LIGHT AT SEAT 20D INOPERATIVE. FOUND HARNESS DISCONNECTED. RESECURED HARNESS FOR SEAT 20D EMERGENCY EXIT LIGHT. OPS CHECK NORMAL.

Part: SKIN — DENTED (TE FLAP) · airframe 34,349 hrs · 10,571 cycles

NUMEROUS DENTS IN MIDDLE OF FLAP ON UPPER SKIN. REMOVED DAMAGED SKIN AND CORE FROM DENTED AREA. INSTALLED NEW CORE AND PERMANENT ALUMINUM HOT BONDED DOUBLER REPAIR AS PER SRM 51-70-10-2R.

Part: IDG — MALFUNCTIONED (RT ENGINE) · airframe 33,846 hrs · 10,467 cycles

BOS - CREW REPORTED RIGHT GENERATOR DRIVE LIGHT CAME ON DURING CLIMBOUT. AIRCRAFT REMOVED FROM SERVICE. INSPECTED RIGHT INTEGRATED DRIVE GENERATOR AND FOUND DELTA "P" FILTER POPPED. REPLACED RIGHT IDG. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 32,698 hrs · 10,228 cycles

RIGHT NUMBER 1 DOOR SLIDE INADVERTENTLY UNSUCCESSFULLY DEPLOYED WHEN DOOR OPENED FROM INSIDE. PACK FELL FROM HOUSING AND WAS RESTING ON CATERING TRUCK. SLIDE DID NOT INFLATE. REPLACED RIGHT NUMBER 1 ESCAPE SLIDE.

Part: GENERATOR — FAILED (LT ENGINE) · airframe 32,479 hrs · 10,181 cycles

CREW REPORTED ON SHORT FINAL THE LEFT GENERATOR FAILED. "L" GEN LIGHT, "L" BUS LIGHT, AND "L" BUS TIE ISOLATION LIGHT ALL ILLUMINATED. ACCOMPLISHED GO AROUND, STARTED THE APU AND FOLLOWED THE QRH PROCEDURES. REGAINED THE LEFT BUS WHEN THE "L" BUS ISOLATION SWITCH WAS RESET. EMERGENCY DECLARED FLIGHT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: PANEL — BROKEN (COCKPIT) · airframe 27,756 hrs · 9,220 cycles

EMERGENCY ARM SWITCH IN COCKPIT METAL ARM TAB BROKEN. REPLACED EMERGENCY ARM PANEL. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,867 hrs · 8,798 cycles

EMERGENCY PATH LIGHTS AT FORWARD COACH CLASS INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER TWO DOOR.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 25,159 hrs · 8,608 cycles

EMERGENCY SEAT LIGHTS INOPERATIVE AT SEAT ROWS 6 TO 15. REPLACED BATTERY PACK.

Part: CONNECTOR — BROKEN (CABIN) · airframe 24,122 hrs

SFO - EMERGENCY EXIT LIGHT AT SEAT 28D INOPERATIVE. INSTALLED CONNECTOR AT SEAT 28D.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,863 hrs

DFW - EMERGENCY EXIT LIGHTS ABOVE RIGHT NUMBER 3 DOOR INOPERATIVE. REPLACED LAMPS FOR EMERGENCY EXIT LIGHTS ABOVE RIGHT NUMBER 3 DOOR.

Part: LIGHT — MISINSTALLED (CABIN) · airframe 23,863 hrs

DFW - CEILING EMERGENCY LIGHTS BETWEEN LEFT AND RIGHT NUMBER 2 DOORS INOPERATIVE. LIGHT ASSEMBLY INCORRECTLY CONNECTED. PROPERLY CONNECTED.

Part: MODULE — INOPERATIVE (CABIN) · airframe 23,774 hrs

BOS - EMERGENCY LIGHTS ON AIRCRAFT INOPERATIVE. REPLACED FIVE 5537 MODULES FOR EMERGENCY LIGHTS ON AIRCRAFT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,774 hrs

BOS - EMERGENCY LIGHTS ON AIRCRAFT INOPERATIVE. REPLACED BATTERY PACK.

Part: SHROUD — BROKEN (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 20D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT AT SEAT 16D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: SHROUD — BROKEN (EMERGENCY LIGHTS)

DFW - EMERGENCY LIGHT AT SEAT 16D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,558 hrs

LGA - EMERGENCY LIGHTS AT SEAT ROW 16 INOPERATIVE. REPLACED CONTROL MODULE FOR EMERGENCY LIGHTS AT SEAT ROW 16. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHTS AT FLOOR SEAT ROWS 14D TO 25D INOPERATIVE. REPLACED BATTERY PACK AT M10953 FOR EMERGENCY LIGHTS AT FLOOR SEAT ROWS 14D TO 25D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHTS AT MID COACH INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID COACH. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SFO - EMERGENCY LIGHTS FROM SEAT ROWS 16DEF TO 25DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SEAT ROWS 16DEF TO 25DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA - EMERGENCY LIGHT AT SEAT 17F INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 17F. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

DFW - EMERGENCY LIGHT AT SEAT 16D MISSING LENS AND INOPERATIVE. REPLACED LENS AND BULB FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SJU - EMERGENCY LIGHTS FROM ROWS 16 TO 27 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM ROWS 16 TO 27. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - SEAT MOUNTED LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PIN — LOOSE (CONNECTOR)

SFO - AISLE EMERGENCY LIGHTS BOTH INOPERATIVE AT 16D. RESECURED PIN IN CONNECTOR AT SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SPRING — DAMAGED (GIRT BAR)

DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, TWO GIRT BAR SPRINGS NEEDING REPLACED. REPLACED TWO GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)