N530NK

Part: MEGAPHONE — INOPERATIVE (ZONE 900) · airframe 58,349 hrs · 26,770 cycles

DURING SERVICE CHECK FOUND L1 DOOR MEGAPHONE NOT WORKING PROPERLY.FWD-R/R L1 DOOR MEGAPHONE IAW AMM 25-65-00 NO DEFECTS NOTED FWD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,834 hrs · 26,520 cycles

MID TO AFT CABIN EMITTING A STRONG ODOR. F/A COMPLAINED ABOUT VERY STRONG SMELL-PERFORMED TSM 05-50-00-810-831. PACK #2 BURN OUT . ALL CHECKS OK. AEROTRACER WAS USED AROUND CABIN, NO SIGNS OF SMELL. A/C OK FOR SERVICE. REF. AMM 49-00-00.

Part: OIL COOLER — UNKNOWN (RH ENGINE) · airframe 57,607 hrs · 26,410 cycles

LOW OIL ADV. FOLLOWED BY A LOSS OF ABOUT .5 QTS EVERY 7 MIN DIVERTED TO MCI AND QUANTITY SHOWED ZERO ON SHORT FINAL. OIL SETTLED AT 1.5 JUST BEFORE ENGINE SHUTDOWN.--

Part: NONE — NONE · airframe 56,059 hrs · 25,671 cycles

DURING DESCENT CABIN SMELLED LIKE DIRTY SOCKS-PERFORMED TSM IAW 05-50-00-810-831. COULD NOT DUPLICATE AT THIS TIME.

Part: NONE — NONE · airframe 55,436 hrs · 25,362 cycles

"LG LGCIU 1 FAULT IN FLIGHT-PERFORMED OPS CHECK OF LGCIU 1 + 2 FAULT CLEARED IAW AMM 32-69-00 AIRCRAFT OKAY TO CONTINUE SERVICE"

Part: UNKNOWN — ODOR (CABIN) · airframe 52,362 hrs · 24,052 cycles

MUSTY / OIL SMELL ON DESCENT @ 15,000 ISULATED PACK 1 SMELL DISIPATED ( PACKS A319 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - AT OR BELOW FL 310 )--

Part: ENGINE — SURGES (NR 1) · airframe 52,299 hrs · 24,027 cycles

ENGINE 1 SURGING IN BOTH AUTO & MAN THRUST. N2 FLUCTUATING +/- 2 PERCENT. AIR RETURN LANDING WEIGHT 135.5-ACCOMPLISHED FAULT ISOLATION FOR EPR SURGING IAW TSM 71-00-00-810-832 PRESSURE CHECKED SENSE LINES TO PRV NO FAULTS NOTED IAW AMM 36-11-00-810-900. REMOVED & REPLACED PRV (4001HA) ON #1 ENG LEAK & OPERATIONAL TEST SATISFACTORY IAW AMM 36-11-52 PB401

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 50,403 hrs · 23,253 cycles

FWD MEGAPHONE HORN INOP-R&R FWD MEGAPHONE IAW SPIRIT AIRLINES A319 EMERGENCY EQUIPMENT LAYOUT DRAWING. OPS CHECK GOOD

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 48,405 hrs · 22,391 cycles

AFT CABIN MEGAPHONE INOP HAS FLASHING YELLOW LIGHT. R&R MEGAPHONE PER AMM 25-65-51 OPS CHECK GOOD.

Part: ADIRU — MALFUNCTIONED · airframe 45,077 hrs · 20,987 cycles

CAPTAIN & FIRST OFFICER FMA AND AIRSPEED INDICATIONS DISAPPEARED AT 100 KTS DURING TAKEOFF AND APPEARED. AFTER LIFTOFF, FDS & AUTOTHRUST STOPPED FUNTIONING AND AIRCRAFT REVERTED TO ALTERNATE LAW. ECAM NAV STDBY AOA FAULT APPREARED ON ENG SHUTDOWN. R & R ADIRU, R & R THE AOA SENSOR. IAW AMM 34-12-34, AND AMM 34-11-19

Part: UNKNOWN — ODOR (COCKPIT) · airframe 45,066 hrs · 20,981 cycles

ACRID SMELL (LIKE PLASTIC BURNING/HOT WIRING) DETECTED IN COCKPIT WHEN ENG A/ICE TURNED ON. SMELL DISSPATED WHEN PACK ONE WAS TURNED OFF AND ENG A/ICE TURNED OFF. -INSPECTED BOTH ENGINES NO SIGNS OF INGETSTION FOUND. PERFORMED ENG. RUN WITH BOTH ENGINES. IAW AMM 71-00-00 PERFORM OPS CHECK OF ENG. ANTI-ICE IN BOTH ENGINES WITH BOTH PACKS RUNNING IAW AMM 30-21-00 AND 36-11-00 NO BURNING OR PLASTIC SMELLS NOTED. A/C OK FOR SERVICE.

Part: FILTER — FUMES (AC BAY) · airframe 44,723 hrs · 20,829 cycles

FUME EVENT ON DESCENT THROUGH 12000' AT OR BELOW FL 370. R&R OZONE FILTER IAW AMM 21-51-41, R&R RECIRCULATION FILTER IAW AMM 21-21-41. OPS CHECK/LEAK CHECK GOOD. NO ODOR DETECTED FROM PACK 1.

Part: UNKNOWN — ODOR (CABIN) · airframe 43,494 hrs · 20,284 cycles

STRONG MUSTY SUCK ODOR NOTED BY CABIN CREW & PASSENGERS FROM 10K & BELOW. COCKPIT DID NOT SMELL ANYTHING, PERFORMED ENGINE IDLE RUNS ON ENG NR 1 & 2 IAW AMM 71-00-00. RAN PACKS 1 & 2 WHILE ENGINE RAN AND ISOLATED THEM TO DETERMINE SMELL IAW AMM 36-11-00. COULDN’T DUPLICATE SMELL. . A/C IS OK FOR CONTINUED SERVICE

Part: LINE — LEAKING (GUIDE VANE) · airframe 43,193 hrs · 20,158 cycles

FUEL ODOR IN THE CABIN, ACCOMPLISHED DECONTAMINATION OF THE ENVIROMENTAL CONTROL SYSTEM IAW AMM 21-00-00-615-002, NO ODOR IN CABIN. FOUND THE SOURCE OF THE ODOR TO BE A LEAKING LINE ON INLET GUIDE VANE ACTUATOR . SECURED THE LINE IAW AMM 49-23-51. OPS & LEAK CHECKED GOOD.

Part: SEAL — LEAKING (DEOILER) · airframe 43,048 hrs · 20,100 cycles

MUSTY ODOR DURING DESCENT, REMOVED AND REPLACED THE NR 1 PACK OZONE FILTER IAW AMM 21-51-41 PB 401, NO LEAKS NOTED. REMOVED AND REPLACED THE NR 2 PACK OZONE FILTER IAW AMM 21-51-41 PB401, LEAK CHECKED SATISFACTORY. ACCOMPLISHED TSM 71-00-00-810-801-A. FOUND OIL ACCUMULATION AT THE DEOILER EXHAUST DUCTS. REMOVED & REPLACED THE DEOILER MATING RING ASSY IAW AMM 76-60-29 PB 401, IDLE LEAK CHECKED SATISFACTORY. PERFORMED ECS DECONTAMINATION IAW AMM 21-00-00-615-004-A. NO FURTHER ODORS NOTED.

Part: APU — LEAKING (APU BAY) · airframe 43,048 hrs · 20,100 cycles

DIRTY SOCK, MUSTY ODOR PRESENT AFTER EXTERNAL AIR START. FOUND THE APU WITH AN INTERNAL OIL LEAK, REMOVED AND REPLACED THE APU IAW AMM 49-11-11, AND OPS CHECK OK, NO DEFECTS NOTED, LEAK CHECKED OK.

Part: ELBOW — CONTAMINATED (APU) · airframe 43,046 hrs · 20,099 cycles

FUME EVENT AFTER EXTERNAL AIR START. ON INSPECTION OF APU, FOUND THE ELBOW TO HAVE A SMALL EVICENCE OF OIL IAW AMM 49-16-00. PERFORMED A PACK BURN OUT PROCEDURE IAW 71-00-00-810-801-A. APU REMAINS ON DMI FOUND NO EVIDENCE OF ODOR IN CABIN AT THIS TIME

Part: UNKNOWN — ODOR (CABIN) · airframe 42,652 hrs · 19,929 cycles

FUME EVENT IN CRUISE DESCENT, INSPECTED THE NR 1 AND 2 ENGINES FOR OIL LEAKS, NO LEAKS NOTED, PERFORMED A NR 1 AND 2 IDLE RUN, OPS CHECKED THE NR 1 & 2 PACKS. CHECKED FWD AND AFT GALLEY EQUIPMENT, OPS CHECKED OF CABIN LIGHTS IAW TSM 05-50-00-810-834-A, NO ODOR PRESENT. ACFT OK TO RETURN TO SERVICE.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 41,138 hrs · 19,284 cycles

AFT F/A MEGAPHONE INOPERATIVE. REMOVED AND REPLACED THE MEGAPHONE IAW AMM 25-60-00. OPS CHECKED OK. ACFT OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 41,105 hrs · 19,269 cycles

CAPTAIN`S SIDE EMERGENCY FLASHLIGHT INOPERATIVE. R & R THE FLASHLIGHT IAW CMM 25-60-02. OPS TESTED GOOD,

Part: SEAL — OBSTRUCTED (EMERGENCY EXIT) · airframe 39,991 hrs · 18,774 cycles

OVERWING EXIT AT SEAT 11A LEAKING AIR. REMOVED EMERGENCY EXIT DOOR IAW AMM 52-21-11-000-001-A. PERFORMED A DETAIL INSPECTION IAW AMM 52-21-00-220-801-A. REMOVED DEBRIS FROM DOOR SEAL. INSTALLED THE EMERGENCY EXIT DOOR IAW AMM 52-21-11-400-001-A. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: FAN — FAILED (E&E BAY) · airframe 38,768 hrs · 18,247 cycles

VENT EXTRACT FAN FAILURE SMELLED ELECTRICAL SMOKE SEVERAL TIMES DIVERTED TO KMTJ. LANDED UNDER MOW, NORMAL LANDING. R&R AVIONICS EXTRACT FAN IAW AMM 21-26-51 OPS CHECK GOOD.

Part: SEAL — LEAKING (NR 2 ENGINE) · airframe 38,640 hrs · 18,195 cycles

DURING CRUISE, F/A REPORTED AN ODOR IN AFT CABIN. NR 2 PACK IAW OB-17-04. ODOR DISSAPATED AFTER (7) SEVEN MINUTES.PERFORMED TSM IAW TSM 05-50-00-810-831/71-00-00-810-801. CHANGED THE NR 2 ENGINE OILER SEAL IAW AMM 72-60-31. PERFORMED THE DECONTAMINATION OF THE ECS IAW AMM 21-00-00. NO FURTHER DEFECTS NOTED.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 37,751 hrs · 17,802 cycles

FOUND FROM ROW 10 AND BACK NO EMERGENCY LIGHTS ARE WORKING IAW CIDS TEST, BATTERY PACKS 13WL AND 12WL ARE FOUND BAD. R & R THE BATTERY PACKS IAW AMM 3-51-38 PB 401. ALL CHECKED GOOD.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 36,286 hrs · 17,114 cycles

AFT MEGAPHONE INOPERATIVE. R & R AFT MEGA PHONE IAW AMM 25-65-51. OPS CHECK GOOD.

Part: SKIN — CORRODED (LT WING) · airframe 42,821 hrs · 17,070 cycles

DURING INSPECTION FOUND CORROSION LT WING TOP SKIN PANEL 2, T/E OVERHANG BETWEEN RIB 10-11. 60 MM OTBD OF RIB10, 170MML X 20MMW X 1MMD.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 42,821 hrs · 17,070 cycles

DURING INSPECTION FOUND CORROSION ON LT WING TOP SKIN, PANEL 2 T/E OVERHAND BETWEEN RIB 14-15. 110MML X 50MMW X 3.8MMD.

Part: SKIN — DENTED (FRAMES 4-5) · airframe 42,821 hrs · 17,070 cycles

DURING INSPECTION FOUND RT NOSE FUSELAGE DENTED BETWEEN FRAME 4 AND 5. - 0.95 MML X 100 MMW X 3.2 MMD-REF RAF 818768-02.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 42,821 hrs · 17,070 cycles

DURING INSPECTION FOUND CORROSION LT WING, TOP SKIN PANEL 2 T/E OVERHANG AT RIB 14. - 60 MML X 20 MMW X 4.67D.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 42,821 hrs · 17,070 cycles

DURING INSPECTION FOUND CORROSION RT WING TOP SKIN, PANEL 2 T/E BETWEEN RIB 16-17. 130 MML X 35 MMW X 4.6 MMD.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 42,821 hrs · 17,070 cycles

DURING INSPECTION FOUND CORROSION RT WING TOP SKIN PANEL 2, T/E OVERHANG BETWEEN RIB 15-16. 50MML X 30MMW X 0.39MMD.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 52,821 hrs · 17,070 cycles

DURING INSPECTION FOUND CORROSION ON LT WING TOP SKIN PANEL 2 AFT REAR SPAR AT RIB 6A - 7B. 85MML X 55MMW X 051MMD. RAF 210277202

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 42,821 hrs · 17,070 cycles

DURING INSPECTION, FOUND CORROSION LT WING TOP SKIN PANEL 2, T/E OVERHANG BETWEEN RIB 10-11. 300MM OTBD OF RIB 10, 120MML X 50MMW X 3MMD.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 42,821 hrs · 17,070 cycles

DURING INSPECTION FOUND CORROSION LT WING TOP SKIN PANEL 2, T/E OVERHANG BETWEEN RIB 8-9. - 200MML X 58MMW X 4.95MMD

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 42,821 hrs · 17,070 cycles

DURING INSPECTION FOUND CORROSION ON RT WING, TOP SKIN PANEL 2, T/E BETWEEN RIB 14-15. 105 MML X 50 MML X 3.72 MMD.

Part: SKIN — LEAKING (LT WING) · corrosion level 2 · airframe 42,821 hrs · 17,070 cycles

DURING INSPECTON, FOUND CORROSION LT WING, BOTTOM SKIN PANEL NR 1 BETWEEN RIBS 7-8 FWD OF SPAR. AREAS 1 =110 MML X 70MMW X 8.87 WWD, AREAS 2 = 60 MML X 65 MML X 8.87 MMD.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 42,821 hrs · 17,070 cycles

DURING INSPECTION FOUND CORROSION ON LT WING TOP SKIN PANEL 2 T/E OVERHAND AT RIB 1. 100ML X 47 MMW X 0.49 MMD.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 35,174 hrs · 16,607 cycles

MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW SPIRIT DWG NK319-132-EQ. OPS CHECKED GOOD.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 35,174 hrs · 16,607 cycles

FWD MEGAPHONE GREEN LIGHT NOT FLASHING. R & R FWD MEGAPHONE GREEN LIGHT TESTS GOOD IAW AMM 25-65-51.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 34,702 hrs · 16,406 cycles

SECONDARY MASK INOPERATIVE. R & R SECONDARY MASK IAW AMM 35-12-41. OP'S CHECK GOOD, THIS DMI IS CLEAR PLACARD REMOVED MOC CONTACTED.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 34,087 hrs · 16,127 cycles

UPON INSPECTION, FOUND AFT MEGAPHONE HAS STRIPPED SET SCREWS. R & R AFT MEGAPHONE IAW AMM 25-65-51. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,837 hrs · 15,548 cycles

FWD EPSU INOPERATIVE BATTERY TEST FAILURE. R & R EPSU BATTERY IAW AMM 33-51-38. OPS CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 30,650 hrs · 14,575 cycles

R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER LOW PRESSURE SERVICED R-1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER WITH NITROGEN TO THE CORRECT PRESSURE IAW AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 29,706 hrs · 14,119 cycles

DOOR ASSIST BOTTLE PRESSURE LOW ON R2 DOOR. SERVICED DOOR ASSIST BOTTLE IAW AMM 52-10-00.

Part: LINE — FAILED (HYD SYSTEM) · airframe 29,402 hrs · 13,974 cycles

LOST ALL HYD G FLUID AFTER GEAR RETRACTION AFTER TAKEOFF. REPLACED LT MAIN GEAR DOWNLOCK ACTUATOR LINES DUE TO OTBD LINE LEAKING, IAW AMM 52-11-22-400-004A. NO LEAKS NOTED. DUE TO LOSS OF GREEN SYS REMOVE AND INSPECTED NR 1 ENGINE CASE DRAIN FILTER. REMOVED AND INSPECTED NR 1 ENGINE CASE DRAIN FILTER, NO DEBRIS OR CONTAMINATION NOTED, REPLACED FILTER IAW AMM 29-11-43-610-010 LEAK CHECKED GOOD. PERFORMED FUNCTIONAL CHECK OF THE LT MLG MAINSTAY ACTUATOR CYLINDER IAW AMM 32-31-00-720-007A, OPS CHECKED NORMAL.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 28,230 hrs · 13,421 cycles

R1 DOOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED R1 DOOR ASSIST BOTTLE IAW AMM 52-10-00.

Part: ACCUMULATOR — LOW PRESSURE (R1 DOOR) · airframe 27,700 hrs · 13,194 cycles

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

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 26,919 hrs · 12,865 cycles

R2 DOOR DAMPENER HAS LOW PRESSURE. SERVICED IAW AMM.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 26,588 hrs · 12,722 cycles

FOUND R2 DOOR CYLINDER PRESSURE LOW. SERVICED R2 DOOR CYLINDER IAW AMM.

Part: BOTTLE — LOW PRESSURE (R1 DOOR ASSIST) · airframe 26,070 hrs · 12,510 cycles

R1 DOOR ASSIST PRESSURE LOW. SERVICED R1 DOOR ASSIST BOTTLE TO PROPER PRESSURE IAW AMM 52-10-00-614-001.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 25,734 hrs · 12,352 cycles

R1 DOOR ASSIST CYLINDER PRESSURE IS LOW. SERVICED CYLINDER IAW AMM.

Part: MEGAPHONE — DAMAGED (CABIN) · airframe 25,271 hrs · 12,134 cycles

FWD GALLEY MEGAPHONE IS DAMAGED. R & R FWD GALLEY MEGAPHONE IAW ACFT MM. OPS CHECKED GOOD.

Part: RELEASE MECH — FAILED (EMERGENCY EXIT) · airframe 22,602 hrs · 10,825 cycles

RT EMERGENCY EXIT HATCH SLIDE RELEASE MECHANISM FAILED OPS CHECK. WORK ACCOMPISHED AND FAILURE CLEARED ON NON-ROUTINE 6865N00605.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 23,786 hrs · 11,410 cycles

CHECK OF THE DOOR SWITCH POWER SUPPLY AND DOOR FAILED SUBTASK 33-51-00-720-050A, STEP 9 & 10 (10WL-A) FWD RT DOOR. ALSO, FAILED 11&12 (13WL-A) AFT RT PAX DOOR. R & R PROXIMITY SENSOR IAW AMM 52-71-11-400-001-A. ADJUSTED AND OPS TESTED ORIGINAL SENSOR IAW AMM 51-71-00-850-002-A 01 AND 52-73-0-710-001-A. CHECKED GOOD IAW FORMED CHECK OF DOOR SWITCH POWER SUPPLY FROM EMERGENCY LIGHT SYS ON FWD RT AND AFT RT PAX CREW DOORS IAW 33-51-00-720-050-A.

Part: FITTING — CORRODED (ZONE 700) · airframe 23,786 hrs · 11,410 cycles

RT MLG ACTUATOR JACK FITTING HAS CORROSION LOWER SIDE. REPLACED RT WING MLG RETRACTION JACK FITTING.

Part: FITTING — CORRODED (ZONE 700) · airframe 23,786 hrs · 11,410 cycles

LEFT MLG ACTUATOR JACK FITTING HAS CORROSION LOWER SIDE. REPLACED LT WING MLG RETRACTION JACK ANCHORAGE FITTING.

Part: PROXIMITY SENSOR — DAMAGED (PAX DOOR) · airframe 23,786 hrs · 11,410 cycles

CHECK OF DOOR POWER SUPPLY FROM THE EMEGENCY LIGHT SYS & DOOR FAILED SUBTASK 35-51-06-720 STEP 9 + 10. FWD RT DOOR ALSO FAILED STEP 11+ 12 (13WL-A). R & R WITH SERVICEABLE PROXIMITY SENSOR. ADJUSTED AN OPS TESTED C/W 1 + 2 PROX SENSOR IAW AMM 52-71-00-820-002-A01 AND 52-73-00-710-001A. OPS CHECKS GOOD. PERFORMED CHECK OF DOOR SWITCH POWER SUPPLY FROM EMERGENCY LIGHT SYS ON FWD RT AND AFT RT DOORS. CHECK GOOD ON STEPS 5,9,10,11,12. ITEM CLEARED.

Part: CYLINDER — LOW PRESSURE (DOOR ASSIST) · airframe 22,123 hrs · 10,588 cycles

R1 DOOR ASSIST ACCUMULATOR PRESSURE LOW. SERVICED R1 OVER ASSIST R1 ACCUMULATOR PRESSURE IAW AMM 52-10-00-614-001.

Part: DOOR — OBSTRUCTED (R1) · airframe 21,650 hrs · 10,336 cycles

RT AFT CABIN AMBER ECAM INFLT RT AFT CABIN DOOR OPENED LOST PRESSURE AT 3000-4000 FT. RETRIEVED IAW FAULT MESSAGE RECOR "52-00" DOOR RT AFT CABIN INSPECTED DOOR AND FOUND SECURITY DOOR STRAP JAMMED (BUNCHED UP) APPLIED TSM 52-13-00-810-804-A. ALL INDICATIONS & DOOR OPS NORMAL AT THIS TIME.

Part: CYLINDER — LOW PRESSURE (PAX DOOR) · airframe 20,044 hrs · 9,559 cycles

R1 DOOR ASSIST BOTTLE HAS LOW PRESSURE. SERVICED R1 DOOR ASSIST BOTTLE TO PROPER PRESSURE IAW AMM 52-10-00-614-001.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 19,976 hrs · 9,523 cycles

ON GEAR RETRACTION, EMERGENCY EXIT LIGHTS IN MAIN CABIN REMAINED ON THROUGHOUT FLT. AFTER LANDING EMERGENCY EXITS WILL NOT EXTINGUISH WITH SWITCH IN OFF POSITION. PERFORMED OPS CHECK OF EMERGENCY LIGHT SYS IAW AMM 33-51-00-710-001. OPS CHECKED GOOD.

Part: ACCUMULATOR — LOW PRESSURE (R2 DOOR) · airframe 19,623 hrs · 9,351 cycles

R-2 DOOR EMERGENCY ACCUMULATOR PRESSURE LOW. SERVICED DOOR EMERGENCY ACCUMULATOR AS REQ IAW AMM 52-10-00-614-001. NO FURTHER DEFECTS NOTED.

Part: CYLINDER — LOW PRESSURE (SERVICE DOOR) · airframe 19,311 hrs · 9,188 cycles

R1 SERVICE DOOR CYLINDER REQUIRES SERVICE. CORRECTIVE ACTION: SERVICED R1 SERVICE DOOR CYLINDER IAW AMM 52-10-00 PB 301 EXCLUDING SUBTASK 52-10-00-614-051-A & SUB TASK 52-10-00-610-001-A.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,499 hrs · 8,770 cycles

UPPER FUSELAGE PAX CABIN FROM STA 2801 TO STA 2869 +Y 1292 FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT IAW SRM 51-72-11, PARAGRAPH 4 AND 6.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,499 hrs · 8,770 cycles

UPPER FUSELAGE PAX CABIN STA 2791 +Y 1292 FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT TRACK IAW SRM 51-72-11, PARAGRAPH 4 AND 6.

Part: SKIN — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 18,499 hrs · 8,770 cycles

ENGINE NR 2 PYLON SECTION INBD AND OTBD AFT FIXED PANELS WITH CORROSION. REPLACED ENGINE NR 2 PYLON AFT FIXED FAIRING SECTION INBD AND OTBD SKIN PANELS FROM STA 829 TO STA 1005 IAW SRM 51-72-11, PARAGRAPH 4 AND 6.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,499 hrs · 8,770 cycles

UPPER FUSELAGE PAX CABIN STA 2884 +Y 1162 FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT IAW SRM 51-72-11, PARAGRAPH 4 AND 6.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,499 hrs · 8,770 cycles

UPPER FUSELAGE PAX CABIN AFT ENTRANCE AREA FROM STA 2884 TO STA 2992, +Y 16, FLOOR SUPPORT WITH CORROSION. REPLACED FLOOR SUPPORT IAW SRM 51-72-11, PARAGRAPH 4 AND 6.

Part: SKIN — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 18,499 hrs · 8,770 cycles

ENGINE NR 1 PYLON SECTION INBD AND OTBD AFT FIXED PANELS WITH CORROSION. REPLACED ENGINE NR 1 PYLON AFT FAIRING SECTION INBD AND OTBD SKIN PANEL IAW SRM 51-72-11 PARAGRAPH 4 AND 6.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,499 hrs · 8,770 cycles

UPPER FUSELAGE PAX CABIN FROM STA 2801 TO 2869 -Y 1292 FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 PARAGRAPH 4 AND 6.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,499 hrs · 8,770 cycles

UPPER FUSELAGE PAX CABIN STA 2884 -Y 1162 FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT IAW SRM 51-72-11, PARAGRAPH 4 AND 6.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 18,408 hrs · 8,723 cycles

R-1 DOOR EMER ASSIT BOTTLE PRESSURE LOW. SERVICED R-1 DOOR EMERGENCY ASSIST BOTTLE WITH NITROGEN IAW AMM TASK 52-10-00-614-001.

Part: DAMPER — LOW PRESSURE (R1 DOOR) · airframe 18,076 hrs · 8,553 cycles

R-1 DOOR ASSIST DAMPER PRESSURE LOW. SERVICED R-1 DOOR ASSIST DAMPER TO PROPER PRESSURE IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (R1 DOOR ASSIST) · airframe 17,559 hrs · 8,307 cycles

R1 DOOR CYLINDER PRESSURE LOW. SERVICE PASSENGER R1 DOOR ASSIST TO PROPER LIMIT IAW 52-10-00-614-001.