N508NK

Part: NONE — NONE · airframe 57,461 hrs · 26,504 cycles

DOOR ASSIST BOTTLE L1 LOW PRESSURE-SERVICE DOOR ASSIST BOTTLE L1 IAW AMM 52-10-00

Part: NONE — FAULT MESSAGE (1CC1) · airframe 57,194 hrs · 26,380 cycles

ON DEPT OUT OF PHL HAD A YAW DAMPER 1 FAULT SYSTEM RESET W/MOC PRIOR TO DEPT W/ CB RESET ONCE AIRBORNE STARTED GETTING 2FD2 W/AP DISC THEN GOT CONT WINDSHEAR AURAL WARNINGS AND OCCAL SPEED WARNING NO ECAM. DID FAC 1 RESET W/ NO SUCESS.-PERFORMED A TROUBLESHOOTING IAW TSM 22-63-00-810-801-A AND R * R FLIGHT AUGMENTATION COMPUTER FAC # 1 IAW AMM 22-66-34-000/400-002-A OPS CHECK GOOD.

Part: NONE — NONE · airframe 57,193 hrs · 26,379 cycles

FUME EVENT REPORTED BY FA B/C BELOW 10,000 FT AND ON GROUND-PERFORMED OSILLATION FOR FUME EVENT BY RUNNING PACL 1 FOR 15 MIN THEN PACK 2 15 MIN INDEPENDENTLY/ BOTH HOT/ COLD. THEN RAN ENG 1 AND 2 FOR 10 MIN BY OSCILLATING PACK 1 ND 2, NO SMELL/ FUME NOTED DURING BOTH PROCEDURES. COULDN'T NOT DUPLICATE EVENT. ALL IAW AMM 71-00-00-710-063/ AMM 21-00-00, NO HISTORY FOR PAST MONTH.

Part: IDG — FAILED (ENGINE 2) · airframe 56,099 hrs · 25,885 cycles

GEN 2 LOSS ON DESCENT RESULTING IN EMERGENCY ELECTRICAL CONFIGURATION-PERFORMED TSM 24-20-00-810-951-A. NO FAULTS NOTED. PERFORMED PRECAUTIONARY REMOVAL AND INSTALLATION OF THE #2 IDG IAW AMM 24-21-51. OPS/LEAK CHECK OK

Part: IDG — FAILED (ENGINE 1) · airframe 56,099 hrs · 25,885 cycles

GEN 1 LOSS AFTER CAPTAINS DU'S FLICKERING ON CLIMBOUT AROUND 17,000 FT-T/S PER TSM 24-00-00 R&R #1 ENG IDG IAW AMM 24-21-51 PENDING OPS AND LEAK CK . REF TO LOG PAGE 2863078-2 FOR OPS AMD LEAK CK

Part: NONE — NONE · airframe 54,917 hrs · 25,363 cycles

PASSENGER/CREW DOOR L1 DOOR ASSIST BOTTLE NEEDS SERVICING-SERVICED PASSENGER/CREW DOOR L1 IAW AMM 52-10-00

Part: NONE — NONE · airframe 54,550 hrs · 25,543 cycles

FORWORD MEGAPHONE EMMITTING LOUD SQUEAL -REMOVED AND REPLACED FWD MEGAPHONE IAW AMM 25-65-51. OPS CHECKS GOOD

Part: A/C PACK — ODOR (NR 2) · airframe 54,394 hrs · 25,143 cycles

IN FLIGHT FA,S REPORTED DIRTY SOCK SMELL IN CABIN PERFORMED SUPPLEMENTARY PROCEDURE FOR ELIM OF ODOR FUMES IN THE CABIN FOR PACK 2 ODOR DISSIPATED-PER TSM ISOLATED TO PACK 2 PACK 2 TO BE PLACED ON DMI A/C OK FOR SERVICE PER TSM 05-50-00

Part: PRESSURE SWITCH — LOOSE (APU) · airframe 53,722 hrs · 24,877 cycles

AFT CABIN ENCOUNTERED DIRTY SOCK SMELL ON SHOT FINAL -PERFORMED TSM 05-50-00-810-831 FOUND APU LEAKING FROM PRESSURE SWITCH. RE- TIGHTED PRESSURESWITCH LINE IAW AMM 49-94-14. PERFORMED DECONTAMINATION OF THE ECS IAW AMM 21-00-00. NO SMELL NOTICED. PERFORMED # 1 AND # 2 ENG RUN . NO SMELL NOTICED AT THIS TIME.

Part: UNKNOWN — ODOR (CABIN) · airframe 52,880 hrs · 24,358 cycles

ON APPROACH AFTER FLAPS 1, A STRONG MUSTY ODOR FILLED THE COCKPIT SHUTTING OFF PACK 1 SEEMED TO HELP ODOD DISSIPATED THE SMELL-PERFORMED INSP TSM 05-50-00-810-831-A AND PERFORMED ENGINE RUN IAW AMM 71-00-00 ISOLATED PACK 1 WITH ENG 1 AND 2 AND ISOLATED PACK 2 WITH ENG 1 AND 2 NO DEFECTS NOTED CANNOT DUPLICATE ON GRAND A/C OK FOR SERVICE

Part: ECS — CONTAMINATED · airframe 52,871 hrs · 24,534 cycles

ON APPROACH AT ABOUT 2,000' A STRONG TURPENTINE SMELL WAS IN THE FLIGHT DECK AND CABIN. SHUTTING OFF PACK ONE MADE SMELL STRONGER. SMELL DISAPATED ON ENGINE SHUTDOWN.-ACCOMPLISHED TSM 05-50-00-810-831-A PROCEDURES. PACKS WERE CAUSED OF THE ODOR. PERFORMED DECONTAMINATION OF THE ACS IAW 21-00-00 & 44-00-00 NO DEFECTS NOTED A/C OK FOR SERVICE.

Part: VALVE — LEAKING (HYD SYSTEM) · airframe 52,695 hrs · 24,450 cycles

CRUISE FL 380, AFT CABIN REPORTED PERFUMY/GASSY SMELL. XBLEED SHUT AND PACK 2 OFF AND ODOR DISSIPATED. ( PACKS A319 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - AT OR BELOW FL 370 )-FOUND GREEN HYD DRAIN VALVE LEAK. R/R DRAIN VALVE IAW AMM 29-11-40 PB401. LEAK CHECKED OK. PERFORMED PRE-CONDITIONING IAW AMM 12-33-21 PB201 FOR 20 MINS. NO FUME DETECTED. THIS CLEARS DMI 247247401. PLACARD REMOVED. DMI LOG UPDATED. MOC NOTIFIED.

Part: ECS — CONTAMINATED · airframe 52,574 hrs · 24,392 cycles

FUME EVENT IN CABIN ON DESCENT BELOW 10,000 FT. ( PACKS A319 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - AT OR BELOW FL 370 )-COMPLETED DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM IAW AMM 21-00-00-615-001-A. NO FURTHER EVIDENCE OF VAPORS IN CABIN. THIS CLEARS DMI 249212801. PLACARD REMOVED. MOC NOTIFIED.

Part: A/C PACK — CONTAMINATED (AC BAY) · airframe 51,996 hrs · 24,122 cycles

PACK 1 FUMES ON APU BLEED AND ENGINE BLEED ON APPROACH AND TAXI IN BURNING OIL SMELL. PERFORMED TSM 05-50-00-810-831-A FOUND PACK 1 TO BE CONTAMINATED.

Part: UNKNOWN — ODOR (CABIN) · airframe 51,787 hrs · 24,034 cycles

ON DESCENT SMELL OF DIRRTY SOCKS IN COCKPIT-APPLIED TSM 05-50-00-810-831A TO IDENTIFY ODOR. PERFORMED GVI OF ENGINES AND APU FOR LEAKS NO EVIDENCE OF LEAKS NOTED PERFORMED ENGINES 1 & 2 RUN UP NO ODORS NOTED. AC PACKS BURN, NORMAL PER AMM 21-00-00 AIRCRAFT OK TO CONTINUE OPS

Part: A/C PACK — SMOKE (AC BAY) · airframe 51,328 hrs · 23,813 cycles

COCKPIT FILLED WITH SMOKE AT ABOUT 1000' AFTER DEPARTURE. STRONG BURNING SMELL IN COCKPIT AND BACK OF AIRCRAFT. AIRCRAFT GOT EXTREMELY HOT ESPECIALLY IN THE COCKPIT. TROUBLESHOOTING DONE IAW TSM 05-50-00-810-831-A ISOLATED CABIN ODOR AND SMOKE COMING FROM PACK 1. SEE L/P 251413702 FOR PACK DEFERRAL.

Part: APU — ODOR (APU BAY) · airframe 51,280 hrs · 23,789 cycles

"DIRTY SOCKS SMELL WITH APU RUNNING THE PACKS-FOUND APU TO BE SOURCE OF ODOR IWA TSM 21-00-00. PERFORMED ECS DECONTAMINATION IAW TM 05-50-00 WITH ENGINE # 2. NO ODOR DETECTED ON PACK 1 OR 2. A/C OK FOR CONTINUE SERVICE."

Part: UNKNOWN — ODOR (CABIN) · airframe 51,031 hrs · 23,675 cycles

FA REPORTED SMELLING FUME EVENT IN CABIN ( APU SYSTEM ).

Part: A/C PACK — ODOR (AC BAY) · airframe 50,540 hrs · 23,464 cycles

"NOTICED SMELL CONSISTANT WITH FUME EVENT AT ABOUT 11000 FEET ON ARRIVAL. COMPLETED PROCEDURE FOR FUME ELIMINATION IN QRM WHEN PACK 1 SHUT DOWN SMELL WENT AWAY-IAW TASK 05-50-00-810-831 FOUND PACK ONE TO BE SOURCE OF ODOR CONTINUED ON LOG PAGE 244950002"

Part: A/C PACK — ODOR (NR 1) · airframe 50,215 hrs · 23,328 cycles

FUME EVENT ON ANUAL THROUGH 8,000-ACCOMPLISHED TSM 05-50-00-810-831- PROCEDURES FOUND PACK # 1 TO BE SECURE OF ODOR. PERFORMED DECONTAMINATION ON ECS PACK # 1 IAW AMM 21-00-00 R/R BOTH RECN FILTER IAW AMM 24-21-45. OPS CHECKS GOOD. NO SIGNS OF ODOR NOTED AT THIS TIME OK TO RETURN TO SERVICE

Part: UNKNOWN — FUMES · airframe 50,154 hrs · 23,303 cycles

"FUME EVENT OF DESCENT COS REPORTING SHEET FILLED OUT. PER CREW REPORTING SHEET ENG NR 1 EVALUATED. PERFORMED ENG. RUN IAW AMM 71-00-00, BOTH ENG'S. ENG. BLEED AIR TEST PRODUCED NO EVIDENCE OF ABNORMAL ODOR OR OIL SMELL. FOR ANALYSER SHOWED NO FAULTS. REF TSM 71-00-00-800-801-A. NO EVIDENCE OF FUME. A/C OK FOR SVC."

Part: SEAL — LEAKING (NR 2 DEOILER) · airframe 46,263 hrs · 21,693 cycles

FA REPORTED STRONG FUMES FROM MID TO AFT CABIN FA REPORTED A DIRTY SOCK ODOR. R & R THE NR 2 ENGINE DEOILER SEAL IAW AMM 72-60-31. BOTH RESIRT FILTERS WERE REMOVED AND REPLACED IAW AMM 21-21-41. RAN BOTH ENGINES WITH BOTH PACKS ISOLATED. NO ODORS PRESENT. ACFT OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 45,790 hrs · 21,516 cycles

FA COMPLAINED OF ODOR IN THE CABIN FROM ROW 6 FORWARD, THROUGH OUT THE FLIGHT. PROPANE GAS ODOR. FLIGHT CREW SHUT OFF THE NR 2 PACK, NEVER IDENTIFIED ODOR. DEBRIEFED CREW, ODOR PRESENT ONLY AT ROWS 1 - 6. CLEANED OVERHEAD COMPARTMENTS ROW 1 - 6, NO ODOR PRESENT AT THIS TIME IAW AMM 12-21-12. RAN PACKS 1, & 2, NO ODOR PRESENT IAW AMM 21-51-00.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 44,625 hrs · 21,034 cycles

FIRST OFFICER`S FLASHLIGHT FOUND BROKEN. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 25-65-52, OPS TESTED OK

Part: SKIN — CONTAMINATED (RUDDER) · airframe 44,591 hrs · 21,016 cycles

WATER INGRESS FOUND DURING THERMOGRAPHY INSPECTION OF THE RUDDER LT & RT SIDESHELL RUDDER, LT SIDE SHELL NR 3 HOIST POINT, TOTAL DAMAGE 10100 SQMM. THE RUDDER RTSIDE SHELL NR 3 HOIST POINT TOTAL DAMAGE = 7950 SQMM. PERFORMED A CUT OUT AND LAY UP REPAIR IAW EO 5541-1713.

Part: WINDOW FRAME — CRACKED (FRAMES 3-4) · airframe 44,591 hrs · 21,016 cycles

RIGHT WINDSHIELD POST HAS A CRACK AT FRAMES 3 - 4. REPAIRED IAW EO 5311-1768

Part: UNKNOWN — ODOR (CABIN) · airframe 44,481 hrs · 20,962 cycles

DIRTY SOCKS ODOR ON APPROACH TO LANDING, AND TAXI-IN. APU WAS TURNED OFF. ATTEMPTED TO ISOLATE BY TURNING OFF THE NR 1 BLEED, NO CHANGE ON SHORT TAXI. NR 1 PACK OFF. NR 2 PACK ON. NR 2 PACK OFF. NR 1 ON. PERFORMED NR 1 ENGINE WITH NR 2 PACK OFF. AND BLEED OPEN. PERFORMED NR 2 ENG RUN WITH BLEED OPEN. NR 1 PACK ON, NR 2 PACK OFF, AND NR 1 PACK OFF, NR 2 PACK ON. RAN APU WITH PACK 1 OFF, AND PACK 2 ON. AND PACK 2 OFF AND PACK 1 ON. NO ODOR DETECTED IAW TSM 05-50-00-810-931-A. OK FOR SERVICE.

Part: STRAP — UNSECURE (L1 DOOR) · airframe 44,127 hrs · 20,811 cycles

L1 SEAL BAD MAKE NOISE.TSM 52-11-00-810-A FOUND L1 DOOR SAFETY STRAP NOT FULLY RETRACTED IN DOOR FRAME BY 6'. RE-SECURED STRAP & PERFORMED GV1 OF DOOR SEAL PER AMM 52-10-00-220-006. NO DEFECTS. NOISE SUSPECTED TO BE FROM STRAP PREVENTING DOOR TO FULLY SEAL. A/C OK FOR CONTINUED OPERATION.

Part: UNKNOWN — ODOR (CABIN) · airframe 42,224 hrs · 19,999 cycles

STRONG DIRTY SOCK ODOR IMMEDIATELY AFTER ROTATION. TURNED PACK OFF AND THE ODOR IMMEDIATELY WENT AWAY. TROUBLESHOT IAW TSM 05-50-00-810-831-A. INSPECTED APU FOR EXTERNAL OIL LEAKS, NONE FOUND. OPS CHECKED BOTH PACKS WITH AIR SOURCE. APU, NR 1 ENG, NR 2 ENG. NO CABIN RECIRCULATION FILTERS IAW AMM 21-21-41 PB 401. PERFORMED OPS CHECK AND SYS, OK FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT/CABIN) · airframe 42,221 hrs · 19,997 cycles

STRONG DIRTY SOCK ODOR DURING DECENT, TURNED NR 1 PACK OFF, AND THE ODOR WENT AWAY. OPERATED BOTH PACKS INDIVIDUALLY AND AT THE SAME TIME. COULD NOT DUPLICATE THE ODOR. F/A AND NEW FLIGHT CREW COULD NOT DETECT ANYTHING IRREGULAR. AMM 21-58-00.

Part: UNKNOWN — ODOR · airframe 41,865 hrs · 19,843 cycles

FUMES & ODOR AT START OF TOP OF DESCENT. PACKS & BLEEDS ON, POWER IDLE. ISOLATED ALL ENGINE BLEEDS, PACKS AND RAN BOTH ENGINES AT IDLE AND TESTED OK IAW TSM 05-50-810-831-A. UNABLE TO DUPLICATE ISSUE. ACFT FOUND TO BE OK FOR SERVICE.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 41,243 hrs · 19,567 cycles

CAPTAIN`S OXYGEN MASK LEAKS AROUND HEAD BAND. REMOVED & REPLACED OXYGEN MASK IAW 35-12-21 OPS CHECKED GOOD.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 40,160 hrs · 19,055 cycles

DURING INSPECTION, FOUND CORROSION ON THE LEFT WING SKIN PANEL WS 9235 RIB 17. REPAIRED IAW EO 5721-1640.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 40,160 hrs · 19,055 cycles

DURING INSPECTION, FOUND CORROSION ON THE LT WING SKIN PANEL WS 12870 - 13464, RIBS 24-25. REPAIRED IAW EO 5721-1640.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 40,160 hrs · 19,055 cycles

DURING INSPECTION, FOUND CORROSION ON THE LEFT WING SKIN PANEL WS 3758 RIB 7. REPAIRED IAW EO 5721-1640.

Part: DOOR SEAL — UNSECURE (L1 DOOR) · airframe 40,015 hrs · 18,996 cycles

CLIMBING THROUGH ABOUT 22,000 WE HEARD AND FELT A VIBRATION. THE F/A`S SAID IT WAS VERY LOUD AND THEY COULD FEEL THE VIBRATION IN THE FORWARD GALLEY, DOWN THE AISLE, AND IN THE REAR GALLEY. THE SOUND AND VIBRATION WAS FROM L1 DOOR. THEY ALSO REPORTED AN OIL BURNING ODOR. IAW AMM 52-11-18-401, FOUND SEAL ON UPPER FWD LT CORNER OF L1 RESECURED SEAL, ACFT OK FOR SERVICE. IAW TSM 21-00-00-810-801-A OPERATED PACKS WITH ENGINES AND PACKS NO OIL OR BURNED ODOR NOTED AT THIS TIME. IAW AMM 52-11-18-401 FOUND SEAL ON UPPER FWD LT CORNER OF L1 RESECURED SEAL, ACFT OK FOR SERVICE. IAW TSM 21-00-00-810-801-A OPERATED PACKS WITH ENGINES AND PACKS NO OIL OR BURNED ODOR NOTED AT THIS TIME.

Part: LANYARD — LOOSE (L1 DOOR SLIDE) · airframe 36,673 hrs · 17,442 cycles

F/A IS REPORTING A VERY LOUD WIND NOISE COMING FROM L1 DOOR. FOUND L1 DOOR GIRT BAR LANYARD LOOSE. SECURE LANYARD. IAW AMM 25-62-44 PB401. OK FOR SERVICE.

Part: LATCH — LACK OF LUBE (L1 DOOR) · airframe 34,076 hrs · 16,281 cycles

L1 DOOR HAS ISSUES OPENING FROM THE OUTSIDE. CLEANED AND LUBRICATED THE L1 DOOR HANDLE LATCH ASSY , OPS NORMAL IAW AMM 52-00-00.

Part: STRUCTURE — CORRODED (RT WING) · airframe 28,080 hrs · 13,562 cycles

RIGHT WING CORROSION BETWEEN WS 7792 & 8268. REPAIRED IAW EA 5720-1307.

Part: STRUCTURE — CORRODED (LT WING) · airframe 28,080 hrs · 13,562 cycles

LT WING CORROSION AT WS 5512. REPAIRED IAW EA 5720-1308.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 28,080 hrs · 13,562 cycles

LT & RT O/W EXIT SIGN LENS DAMAGED. R & R LENS IAW AMM NR 7089N00166.

Part: STRUCTURE — CORRODED (RT WING) · airframe 28,080 hrs · 13,562 cycles

RIGHT WING CORROSION AT WS 9704. REPAIRED IAW EA 5720-1307.

Part: STRUCTURE — CORRODED (RT WING) · airframe 28,080 hrs · 13,562 cycles

RIGHT WING CORROSION AT WS 6699. REPAIRED IAW EA 5720-1307.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 27,965 hrs · 13,500 cycles

DURING CRUISE AT FL 370, CAPTAINS WINDSHIELD OUTER PANE SHATTERED. COMPLETED COM PROCEDURE 3.80-12. NO EMERGENCY ACTION TAKEN. AFTER CAPTAIN WINDOW SHATTERING, RECEIVED ANTI-ICE LT WINDSHIELD ECAM. COMPLETED COM PROCEDURE 3.30.14. R & R CAPTAINS WINDSHIELD IAW ACFT MM. R & R WINDOW HEAT COMPUTER 1 IAW ACFT MM. NO FAULTS NOTED. OPS CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 25,019 hrs · 12,040 cycles

RT OVER WING EMERGENCY EXIT SIGN MISSING LENS COVER.

Part: SKIN — CORRODED (THRUST REVERSER) · corrosion level 2 · airframe 21,982 hrs · 10,579 cycles

ENGINE NR 2, LEFT C-DUCT LOWER BIFURCATION OUTER SKIN WITH CORROSION, LOCATED JUST ABOVE THE 740-0420 FAIRING AT 6 O'CLOCK POSITION. NOTE: THE C-DUCT OUTER SKIN REQUIRES A MAJOR REPAIR IAW ENGINEERING GUIDELINES.

Part: ANCHOR FITTING — CORRODED (ZONE 500) · corrosion level 2 · airframe 21,982 hrs · 10,579 cycles

LT WING, INNER SPAR BETWEEN RIB 2 AND RIB 3, MLG RETRACTION JACK ANCHORAGE FITTING'S BORE, LOWER & UPPER SURFACE WITH CORROSION. NOTE: THE FITTING'S CORROSION/REWORKS REQUIRES A MAJOR REPAIR IAW ENGINEERING GUIDELINES.

Part: ANCHOR FITTING — CORRODED (ZONE 600) · corrosion level 2 · airframe 21,982 hrs · 10,579 cycles

RT WING, INNER SPAR BETWEEN RIB 2 AND RIB 3, MLG RETRACTION JACK ANCHORAGE FITTING'S BORE, LOWER & UPPER SURFACE WITH CORROSION. NOTE: THE FITTING'S CORROSION/REWORKS REQUIRES A MAJOR REPAIR IAW ENGINEERING GUIDELINES.

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,982 hrs · 10,579 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE, BETWEEN FR59 TO FR60 AT STRINGER 38LT LEVEL, PROFILE-CORNER WITH CORROSION.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,982 hrs · 10,579 cycles

PAX CABIN FROM FR 66 TO FR 66+5, -Y50 WITH SEAT TRACK CORRODED. THE SEAT TRACK DAMAGED WAS REPLACED IAW SRM 51-72-11.

Part: SKIN — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 21,982 hrs · 10,579 cycles

ENGINE NR1, PYLON AFT FIXED FAIRING, OTBD AND INBD LATERAL SKIN PANEL WITH CORROSION. THE FAIRING SKIN PANEL REQUIRES A MAJOR REPAIR IAW SRM GUIDELINES.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,982 hrs · 10,579 cycles

AFT CARGO COMPARTMENT BETWEEN FR47/51 TO FR55A AT STRINGER 38RT LEVEL, FLOOR STRUCTURE, PROFILE-CORNER WITH CORROSION.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,982 hrs · 10,579 cycles

PAX CABIN, FROM FR 19 TO FR 20, -Y10 WITH FLOOR SUPPORT CORRODED. THE FLOOR SUPPORT DAMAGED WAS REPLACED IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,982 hrs · 10,579 cycles

PAX CABIN, UPPER REAR FUSELAGE BETWEEN FR19 TO FR20 Y-254 FLOOR SUPPORT WITH CORROSION. MAJOR REPAIR.

Part: SKIN — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 21,982 hrs · 10,579 cycles

ENGINE NR 2, PYLON AFT FIXED FAIRING, OTBD AND INBD LATERAL SKIN PANEL WITH CORROSION. THE FAIRING SKIN PANEL REQUIRES A MAJOR REPAIR IAW SRM GUIDELINES.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,983 hrs · 10,579 cycles

UPPER FUSELAGE PAX CABIN, FROM FR66 TO FR66+5, -Y30", SEAT TRACK WITH CORROSION. REPLACED PAX CABIN SEAT TRACK IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,983 hrs · 10,579 cycles

UPPER FUSELAGE PAX CABIN, FROM FR66+5 INCHES TO FR68, -Y50 INCHES FLOOR SUPPORT WITH CORROSION. REPLACED PAX CABIN FLOOR SUPPORT IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,983 hrs · 10,579 cycles

UPPER FUSELAGE PAX CABIN, FROM FR68 TO FR70, +Y6 INCHES FLOOR SUPPORT WITH CORROSION. REPLACED PAX CABIN FLOOR SUPPORT IAW SRM 51-72-11.

Part: DOOR FRAME — CORRODED (ZONE 800)

LIGHT SURFACE CORROSION ON R4 DOOR SILL PLATE INBD OF FWD GIRT BAR FITTING PANEL 262FF.

Part: SHEAR PLATE — CRACKED (ZONE 100)

SHEAR PLATE BETWEEN FRAMES 69 AND 70 LT SIDE IS CRACKED.

Part: SHEAR PLATE — CORRODED (ZONE 100)

LT UPPER SHEAR PLATE HAS 2 AREAS OF CORROSION.

Part: FLOORBEAM — DAMAGED (ZONE 100)

BEAM STATION Y-160.5 JUST AFT OF SPLICE HAS A DRILL MARK

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 3 · airframe 11,070 hrs · 5,399 cycles

FLOORBEAM SEAT TRACK CORRODED AT Y-765 BETWEEN FR 64 AND FR 66.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 3 · airframe 11,070 hrs · 5,399 cycles

FR 65 - FR 70 FLOORBEAM HAS CORROSION AT Y765.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 3 · airframe 11,070 hrs · 5,399 cycles

FR 65-FR 70 FLOORBEAM CORRODED AT STA Y765.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 3 · airframe 11,070 hrs · 5,399 cycles

FR 67.5 - FR 70 STA Y765 FLOORBEAM HAS CORROSION.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 3 · airframe 11,070 hrs · 5,399 cycles

FR 68 - FR 69.5 FLOORBEAM HAS CORROSION AT Y1292.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 3 · airframe 11,070 hrs · 5,399 cycles

FR68 - FR70 FLOORBEAM CORRODED AT Y765.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 3 · airframe 11,070 hrs · 5,399 cycles

RIGHT Z BEAM CORRODED FR 65 - FR 66 AT Y1292.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 33 hrs · 17 cycles

FLIGHT CONTROL FLAP FAULT FOLLOWED BY FLIGHT CONTROL FLAPS LOCKED, COULD NOT GET FLAPS TO EXTEND AFTER ENGINE START PRIOR TO TAXI, TAIL SWAP WITH AIRCRAFT N802NK. FOUND FAULT ON SFCC NR1, RESET THE WING TIP BRAKE AND SYSTEM OPS CHECK GOOD. (K)