N587NK

Part: OIL SYSTEM — LEAKING (NR 2 ENGINE) · airframe 39,319 hrs · 16,824 cycles

DURING FLIGHT, NR 2 ENGINE OIL QUANTITY DECREASED. FLASHING ADVISORY BEGAN AT 5.0 LOWEST LEVEL NOTED WAS 3.5 QTS ON APPROACH NR 2 PSI AND TEMP WERE NORMAL. AFTER ENGINE SHUTDOWN OIL QTY WAS AT 10QTS. SERVICED THE OIL QTY WITH 12 QTS OF OIL IAW AMM 12-13-79 PB301.A. EXAMINE ENGINE, NO LEAKS NOTED. INSPECTED FCOC, NO DEFECTS NOTED IAW AMM 79-21-43-200-010-B. R & R OIL SCAVENGE PUMP IAW AMM 79-22-41. LEAK CHECKED GOOD IAW AMM 71-00-00-710-012. REMOVED & REPLACED NR 2 ENG DEOILER BREATHER SEAL ASSY IAW AMM 72-60-31 PB401. REMOVED & REPLACED NR 4 BEARING SCAVENGE VALVE IAW AMM 79-23-51 PB401. PERFORMED BORESCOPE INSPECTION OF NR 2 ENG HP COMPRESSOR IAW 72-00-00-200-016B. NO DEFECTS NOTED. PERFORMED BORESCOPE INSPECTION OF STAGE 1 HPT BLADES, DUCT SEGMENTS STAGE 2 HPT BLADES, DUCT SEGMENTS INSIDE COMBUSTION CHAMBER, & HP TURBINE STAGE 1 VANES IAW AMM 72-00-00-00-200-013/ 014, 015, NO DEFECTS NOTED. ACCOMPLISHED HIGH POWER ASSURANCE TEST IAW AMM 71-00-00-710-013-C, TESTED OK. PERFORM ENGINE RUN AT FLIGHT IDLE FOR 45 MINUTES IAW AMM 71-00-00, TESTED OK. OIL COMBUSION WAS 0.5 OIL QTS FOR 1 HOUR OF ENG RUNNING. FLIGHT TESTED SATISFACTORY.

Part: BOTTLE — LOW PRESSURE (DOORS) · airframe 39,319 hrs · 16,824 cycles

R1, L2, R4 SERVICE DOOR REQUIRES SERVICING DOOR ASSIST BOTTLE LOW PRESSURE.. SERVICED R1, L2, R4 DOORS IAW 52-10-00-614-001-A. SERVICED TO PROPER PRESSURE"

Part: UNKNOWN — ODOR (CABIN) · airframe 38,843 hrs · 16,618 cycles

F/A REPORTED SMELLY SOCKS ROW 24 AFT. LATE ON APPROACH 5000 FEET IDEL POWER BOTHE PACKS RUNNING. PERFORMED TSM 05-50-00-810-831-A. ISOLATED PACKS, ENGINES. PERFORMED ENGINE IDLE RUN IAW AMM 71-00-00-860-823-A. NO DIRTY SOCK SMELL OR ODORS DETECTED. A/C OK FOR SERVICE.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 38,482 hrs · 16,464 cycles

CAPTAIN`S O2 MASK LEAKS. R & R O2 CAPTAIN`S MASK IAW AMM 35-12-41, ALL CHECKS OK.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 37,046 hrs · 15,837 cycles

L-2 DOOR DAMPING CYLINDER LOW. SERVICED L-2 DOOR DAMPING CYLANDER IAW AMM 52-10-00. OPS CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 36,132 hrs · 15,416 cycles

L2 DOOR DAMPER CYLINDER LOW IN CHARGE. SERVICED L-2 DOOR DAMPER CYLINDER WITH NITROGEN IAW AMM 52-10-00-614-001-A.

Part: BOTTLE — LOW PRESSURE (L4 DOOR) · airframe 35,615 hrs · 15,183 cycles

L4 DOOR ASSIST BOTTLE IS LOW. SERVICED L4 DOOR ASSIST BOTTLE IAW AMM 52-10-00.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 12 ABC) · airframe 35,516 hrs · 15,143 cycles

O2 MASKS IN CABIN ROW 12ABC COLLAPSED, PASSENGER OXYGEN STORAGE MODULES. PERFORMED REPACKED OF O2 MASK IN ROW 12 ABC IAW AMM 35-21-43, AND PERFORMED OPS CHECK OF MANUAL MASK RELEASED IAW AMM 35-23-00, ALL CHECKS NORMAL, NO DEFECTS NOTED, THIS CLEARS DMI 5817514, MOC NOTIFIED, PLACARD REMOVED.

Part: SKIN — CORRODED (RT WING) · airframe 350,919 hrs · 15,140 cycles

CORROSION FOUND ON UPPPER SURFACE OF BOTTOM SKIN PANEL 3. INSPECT BETWEEN REAR SPAR AND + BETWEEN RIB 5 + THE MLG GEAR SUPPORT RIB ON THE RT WING. EO 5721-1518, REV 0, DATED 23 NOV 2015 CORROSION REPAIR ON RT WING BOTTOM SKIN PANEL 3 ACCOMPLISHED MWI 5780409 OPENED FOR 180 DAYS IAW STEP 5 OF THIS EO.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 32,357 hrs · 13,818 cycles

FWD F/A NR 1 POSITION EMERGENCY FLASHLIGHT WILL NOT TEST OR ILLUMINATE. R & R THE FLASHLIGHT IAW CMM 25-60-02. OPS CHECKED GOOD.

Part: DIAPHRAGM — RUPTURED (ASSIST BOTTLE) · airframe 31,353 hrs · 13,402 cycles

R1 PAX DOOR ASSIST BOTTLE DIAPHRAM RUPTURED. R & R R1 DOOR ASSIST BOTTLE DIAPHRAM IAW AMM 52-11-14, PB 401. BOTTLE CHARGED TO 1740 PSI AT 20' C. NO LEAKS NOTED.

Part: OXYGEN MASK — DISLODGED (ROW 26 ABC) · airframe 31,162 hrs · 13,318 cycles

PAX OXYGEN MASK ABOVE ROW 26ABC FELL DOWN IN FLIGHT. PERFORMED OPS TEST OF THE PASSENGER EMERGENCY OXYGEN SYS IAW AMM 35-23-00-710-050-A. OPS CHECK GOOD. NO DEFECTS NOTED. ALL MASKS RESTOWED AS REQUIRED IAW AMM 35-21-43-550-801-A.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 30,741 hrs · 13,137 cycles

F/A REPORTED L4 DOOR MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-65-51.

Part: CROSSBEAM — CRACKED (FRAME 48) · corrosion level 2 · airframe 30,735 hrs · 13,134 cycles

DURING REMOVAL OF RIGHT ROLLER TRACK FOUND CROSSBEAM SECTION OF FRAME 48 FLANGE CRACKED. REPAIRED IAW EO 5341-1405, REV-00.

Part: STOWAGE BOX — INOPERATIVE (OXYGEN MASK) · airframe 29,934 hrs · 12,803 cycles

NR 2 OBSERVER OXYGEN MASK INOPERATIVE. R & R NR 2 OBSERVER OXYGEN MASK IAW AMM. NO HELP. R & R NR 2 OBSERVER OXYGEN MASK STOWAGE BOX IAW AMM. OPS & LEAK CK GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEATS 9&14 ABC) · airframe 29,924 hrs · 12,799 cycles

OXYGEN MASKS DROPPED ON LANDING, SEATS 9ABC AND 14. PERFORMED MANUAL DROP CHECK OF PAX OXYGEN MASK IAW AMM 35-23-00-710-001. ALL CHECKS GOOD.

Part: KNOB — MISSING (MEGAPHONE) · airframe 29,915 hrs · 12,795 cycles

FWD MEGAPHONE VOLUME KNOB MISSING. R & R MEGAPHONE KNOB IAW CMM. OPS CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (R1 DOOR ASSIST) · airframe 29,659 hrs · 12,691 cycles

R1 DOOR ASSIST ACCUMULATOR BOTTLE LOW. SERVICED BOTTLE IAW AMM.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 29,651 hrs · 12,688 cycles

R1 DOOR ASSIST ACCUMULATOR BOTTLE LOW. SERVICED THE R1 DOOR ASSIST ACCUMULATOR IAW AMM.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 28,854 hrs · 12,356 cycles

F/A MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 2565-51-920-001.

Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 28,490 hrs · 12,193 cycles

F/O OXYGEN MASK HEADBAND BROKEN. R & R MASK ASSY IAW MM 35-12-40-000-002-A & 35-12-41-400-002-A. OPS CHECKED GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 27,991 hrs · 11,981 cycles

EPSU 11WL, BATTERY FAILED, OPS CHECK. R & R EPSU BATTERY AT 11WL IAW ACFT MM. OP’S CHECKED GOOD.

Part: LEVER — LOOSE (R3 DOOR) · airframe 27,822 hrs · 11,910 cycles

R3 DOOR ARMING LEVER IS LOOSE. SECURED ARMING LEVER IAW ACFT MM, OK FOR SERVICE.

Part: BUTTON — BROKEN (MEGAPHONE) · airframe 27,747 hrs · 11,878 cycles

DURING PREFLIGHT F/A FOUND FRONT MEGAPHONE VOLUME BUTTON MISSING. INSTALLED NEW VOLUME BUTTOM ON THE FRONT MEGAPHONE.

Part: DIAPHRAGM — RUPTURED (EMERGENCY EXIT) · airframe 26,716 hrs · 11,443 cycles

BOTH AFT EMERGENCY EXIT DOOR OPEN ASSIST ACTUATORS DIAPHRAGM RUPTURED. R & R DIAPHRAGMS IN BOTH AFT EMERGENCY EXIT DOORS ASSIST ACTUATORS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,161 hrs · 11,204 cycles

FLOOR LIGHT BY ROW 16 RT INOPERATIVE. SECURED LIGHT IAW AMM 33-51-21-400-001-A.

Part: CYLINDER — LOW PRESSURE · airframe 25,925 hrs · 11,099 cycles

FOUND R4 DOOR ASSIST PRESSURE LOW. SERVICED R4 DOOR ASSIST IAW AMM 52-10-00-614-001-A LEAK CHECK GOOD.

Part: DOOR — INOPERATIVE (R3) · airframe 25,759 hrs · 11,027 cycles

R3 DOOR WILL NOT LATCH. REMOVED AND REINSTALLED DOOR PIN ON R3 OPS CHECK GOOD IAW AMM 52-10-00, PB 201 SECTION 4/2(A).

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 25,634 hrs · 10,973 cycles

R4 DOOR PASSENGER DOOR ASSIST CYLINDER PSI 1000. SERVICED RT DOOR WITH NITROGEN TO REQUIRED LEVEL IAW AMM 52-10-00-614-001-A LEAK CHECKED OK AT THIS TIME.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 24,514 hrs · 10,499 cycles

L2 DOOR EMERGENCY ACCUMULATOR PRESSURE LOW. SERVICED DOOR EMERGENCY ACCUMULATOR IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (PAX DOOR) · airframe 24,514 hrs · 10,499 cycles

R4 DOOR EMERGENCY ACCUMLUATOR PRESSURE LOW. SERVICED DOOR EMERGENCY ACCUMULATOR IAW AMM 52-10-00-614-001.

Part: ACCUMULATOR — LOW PRESSURE (L2 DOOR) · airframe 23,931 hrs · 10,225 cycles

L2 DOOR ASSIST ACCUMULATOR HAS LOW PRESSURE. SERVICED L2 DOOR PRESSURE IAW AMM 52-10-00-614-001.

Part: RESERVOIR — LOW PRESSURE (R3 DOOR SLIDE) · airframe 23,931 hrs · 10,225 cycles

FOUND R3 DOOR SLIDE INFLATION RESERVOIR BELOW PROPER PRESSURE. R & R R3 DOOR SLIDE RESERVOIR REF AMM 25-62-49-400-001A. OPS CHECKED OK.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 23,677 hrs · 10,106 cycles

R & R EPSU 15WL BATTERY OPS CHECKED OK REF AMM 33-51-38-400-002A.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 23,677 hrs · 10,106 cycles

L4 EXIT SIGN LENS BROKEN. REINTALLED EXIT SING LENS AT L4 DOOR REF 33-51-13-400-001.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 23,613 hrs · 10,076 cycles

L2 DOOR ACCUMULATOR PRESSURE REQUIRE SERVICE. SERVICED L2 DOOR ACCUMULATOR PRESSURE IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 23,503 hrs · 10,023 cycles

R4 DOOR ACTUATOR PRESSURE LOW. SERVICED R4 DOOR ACTUATOR TO PROPER PRESSURE IAW AMM 52-10-00-614-001.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 19,759 hrs · 8,316 cycles

BATTERY/EPSU (14WC) MID R CLASS I MESSAGE. R & R EPSU BATTERY PACK (14WL) IAW AMM 33-51-000-002-A AND 33-51-38-400-002-A. EPSU SYS TESTED OK.

Part: CYLINDER — LOW PRESSURE (PAX DOOR) · airframe 21,967 hrs · 9,301 cycles

PAX DOOR RT AFT LOW ON PRESSURE. SERVICED PAX DOOR RT AFT TO PROPER PRESSURE IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (L2 DOOR ASSIST) · airframe 21,829 hrs · 9,231 cycles

L2 DOOR ASSIST BOTTLE LOW. SERVICED L2 DOOR PRESSURE IAW AMM 52-10-00-614-001.

Part: SUPPORT ANGLE — CRACKED (NR 1 NACELLE) · airframe 20,902 hrs · 8,762 cycles

ENGINE NR 1, PYLON UPPER SIDE (AT PRECOOLER AREA RT SIDE) BETWEEN PYLON STA 537/RIB07 AND STA 608/RIB08, SUPPORT ANGLE WITH CRACK. NOTE: THE SUPPORT ANGLE CRACK REQUIRES A MAJOR REPAIR.

Part: FAIRING — CRACKED (NR 1 PYLON) · airframe 20,902 hrs · 8,762 cycles

ENGINE NR 1, AFT PYLON SECTION LOWER AFT FIXED FAIRING WITH CRACK. MAJOR REPAIR.

Part: PANEL — CRACKED (ZONE 600) · airframe 20,902 hrs · 8,762 cycles

RT WING, RIB 16 L/E PANEL, LOWER SURFACE WITH CRACK. MAJOR REPAIR.

Part: PANEL — CRACKED (ZONE 500) · airframe 20,902 hrs · 8,762 cycles

LT WING, RIB 16 L/E PANEL, LOWER SURFACE WITH CRACK. MAJOR REPAIR.

Part: SUPPORT ANGLE — CRACKED (ZONE 400) · airframe 20,902 hrs · 8,762 cycles

ENGINE NR 2, PYLON UPPER SIDE (AT PRECOOLER AREA LT SIDE) BETWEEN PYLON STA 537 AND STA 608, SUPPORT ANGLE WITH CRACK. NOTE: THE SUPPORT ANGLE CRACK REQUIRES A MAJOR REPAIR.

Part: BUMPER — WORN (THRUST REVERSER) · airframe 20,902 hrs · 8,762 cycles

ENG NR1, INBD/RT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE WEAR REQUIRES A MAJOR REPAIR.

Part: SKIN — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 20,902 hrs · 8,762 cycles

ENGINE NR1, PYLON AFT FIXED FAIRING, OTBD AND INBD LATERAL SKIN PANEL WITH CORROSION. NOTE: THE PANELS' CORROSION REQUIRES A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,902 hrs · 8,762 cycles

PAX CABIN, UPPER REAR FUSELAGE, AFT SERVICE AREA FR66+3" -Y52 FLOORBEAM WITH CORROSION. NOTE: THE BEAM CORROSION REQUIRES A MAJOR REPAIR.

Part: BUMPER — WORN (THRUST REVERSER) · airframe 20,902 hrs · 8,762 cycles

ENGINE NR 2, OTBD/RT THRUST REVERSER C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE BUMPER WEAR REQUIRES A MAJOR REPAIR.

Part: ATTACH FITTING — CORRODED (ZONE 600) · corrosion level 2 · airframe 20,902 hrs · 8,762 cycles

RT WING, MLG ATTACHMENTS, RETRACTION JACK ANCHORAGE FITTING BORE WITH CORROSION. IT IS LOCATED ON INNER REAR SPAR BETWEEN RIB 2 AND RIB 3. NOTE: THE ANCHORAGE FITTING'S REWORK (PN 57259162001) REQUIRES A MAJOR REPAIR.

Part: ATTACH FITTING — CORRODED (ZONE 500) · corrosion level 2 · airframe 20,902 hrs · 8,762 cycles

LT WING, MLG ATTACMENTS, RETRACTION JACK ANCHORAGE FITTING BORE WITH CORROSION. IT IS LOCATED ON INNER REAR SPAR BETWEEN RIB 2 AND RIB 3. NOTE: THE ANCHORAGE FITTING'S REWORK (PN D57259162000) REQUIRES MAJOR REPAIR IAW ACFT INSTRUCTIONS.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,902 hrs · 8,762 cycles

PAX CABIN, UPPER REAR FUSELAGE, AFT SERVICE AREA BETWEEN FR68 AND FR69 -Y52 FLOORBEAM WITH CORROSION. NOTE: THE BEAM CORROSION REQUIRES A MAJOR REPAIR.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 20,902 hrs · 8,762 cycles

RT WING, WX1835.15 FALSE REAR SPAR AND GEAR RIB LEVEL, BETWEEN RIB 3 AND RIB 4, TOP SKIN CORRODED. NOTE: THE TOP SKIN CORROSION REWORKS REQUIRE MAJOR REPAIR IAW MM INSTRUCTIONS.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,902 hrs · 8,762 cycles

PAX CABIN, UPPER REAR FUSELAGE, AFT SERVICE AREA BETWEEN FR67 AND FR68 -Y52 FLOORBEAM WITH CORROSION. NOTE: THE FLOORBEAM CORROSION REQUIRES A MAJOR REPAIR.

Part: BUMPER — WORN (THRUST REVERSER) · airframe 20,902 hrs · 8,762 cycles

ENGINE NR 1, OTBD/ LT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE WEAR REQUIRES A MAJOR REPAIR.

Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 20,902 hrs · 8,762 cycles

ENG NR 2, PYLON AFT FIXED FAIRING , INBD AND OTD LATERAL SKIN PANEL WITH CORROSION. NOTE: THE PANELS' CORROSION REQUIRES A MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 20,902 hrs · 8,762 cycles

PAX CABIN, UPPER REAR FUSELAGE, RT AFT PASSENGER DOOR LOWER SILL STA 3848 -Y59 FR66 FLOORBEAM WITH CORROSION. NOTE: THE FLOORBEAM CORROSION REQUIRES A MAJOR REPAIR IAW MM INSTRUCTIONS.

Part: BUMPER — WORN (THRUST REVERSER) · airframe 20,902 hrs · 8,762 cycles

ENGINE NR 2, INBD/LT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE BUMPER WEAR REQUIRES A MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,922 hrs · 6,571 cycles

FLOOR SUPPORT CORROSION AT -Y1292 BETWEEN FR68 AND FR69 / REMOVED AND REPLACED FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,922 hrs · 6,571 cycles

RT FLOOR SUPORT AT -Y1292 BETWEEN FR66 AND FR68 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT.

Part: SHEAR PLATE — CRACKED (ZONE 200) · airframe 15,922 hrs · 6,571 cycles

LT SHEAR PLATE AT APPROX Y1400 BETWEEN FR69 AND FR70 CRACKED/ REMOVED AND REPLACED SHEAR PLATE.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,922 hrs · 6,571 cycles

FLOOR SUPPORT AT -Y765 BETWEEN FR66 AND FR70 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 15,922 hrs · 6,571 cycles

RT SHEAR PLATE AT APPROX -Y1400 BETWEEN FR69 AND FR70 CRACKED/REMOVED AND REPLACED SHEAR PLATE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 9,985 hrs · 4,146 cycles

FRAME 69 LT AND RT HAVE EVIDENCE OF CORROSION. REMOVED AND REPLACED SHEAR PLATES. (K)

Part: SLEEVE — CRACKED (MLG) · airframe 1,469 hrs · 623 cycles

FOUND NR 4 MAIN TIRE WORN TO LIMITS, WHEN TIRE WAS REMOVED FOUND NR4 MLG AXLE SLEEVE CRACKED. DAMAGED LENGTH MEASUREMENT IS NOT BEYOND .238 INCH, ACCOMPLISHED NDT INSPECTION OF NR4 AXLE SLEEVE, NO CRACK PROPAGATION BEYOND VISIBLE MEASUREMENT OF .238 INCH. (K)

Part: PROXIMITY SWITCH — OUT OF ADJUST (R1 DOOR)

R1 DOOR NOT SHOWING CLOSED INFLIGHT ON ECAM. RECYCLED EMERGENCY LIGHT TEST SWITCH ON FAP AND DOOR LIGHTS WORKED NORMALLY. PERFORMED ADJUSTMENT OF R1 DOOR PROX SWITCH PER AMM. SYSTEM OPS CHECK GOOD, LP NR 179708-3. (M)