N409UA

Part: MODULE — DAMAGED (NR 2 ENGINE) · airframe 88,231 hrs · 34,154 cycles

*EMERGENCY DECLARED* BIRDSTRIKE ENG 2 ENGINE #2 SN V10989 HAD BIRDSTRIKE ON TAKEOFF. ONLY PARAMETERS CHANGE WAS VIBRATION. ENGINE WAS NOT SHUTDOWN, BROUGHT BACK TO IDLE UNTIL LANDING. TRANSFERRED TO OFF #2 ENG SN V10989 AC 8802 LP3191823. ONLY PARAMETERS CHANGE WAS VIBRATION. ENGINE WAS NOT SHUTDOWN, BROUGHT BACK TO IDLE UNTIL LANDING. FAN MODULE REPLACED WITH LVL 3.0

Part: NONE — MISSING (NLG) · airframe 86,390 hrs · 33,258 cycles

PDA 3 NLG TOWING ELECT BOX LEVER MISSING SPRING CLIP -- SEE PHOTO PHOTO ADDED INSTALLED NEW SPRING CLIP ON NLG ELECT BOX LEVER..REF IPC 32-51-12-01E.

Part: RIB — CRACKED (RT WING) · airframe 84,624 hrs · 32,432 cycles

A3NB-57-4-6049 RIGHT WING O/B TRAILING EDGE CAVITY AT APPROX. WI NG RIB 26, T/E RIBLET CRACKED AT AFT UPPER FASTENER HOLE. REF BY PEMCO NR.11035.0240. REMOVED AND REPLACED WING RIB 26 ON R/H WING O/B TRAILING EDGE C AVITY AT APPROX WING RIB 26 IAW A320 SRM 51-72-11-911-001.

Part: BRACE — CRACKED (EMERGENCY EXIT) · airframe 84,624 hrs · 32,432 cycles

RH FWD OVERWING EMERGENCY EXIT DOOR HAS CRACK IN INTERIOR AFT SUPPORT BRACE. REF N/R 11035.0333 REMOVED AND REPLACED NEW SEGMENT AT RH FWD OVERWING EMERGENCY EXIT DOOR INTERIOR AFT SUPPORT BRACE IAW A320 SRM 51-42-11/001.

Part: SEAT TRACK — CRACKED (FRAME 20) · airframe 84,624 hrs · 32,432 cycles

A3NB-25-3-611. CORROSION ON O/B SEAT TRACK UNDER R/H WINDSCREEN. REF BY PEMCO NR.11035.0385. ACCOMPLISHED SPLICE REPAIR ON SEAT TRACK AT FR20 ON Y-1292 IAW A 320 SRM 53-11-15-300-008. ACCOMPLISHED SPLICE REPAIR ON SEAT TRACK AT FR20 ON Y-1292 IAW A 320 SRM 53-11-15-300-008.

Part: SUPPORT BRACKET — CRACKED (EMERGENCY EXIT) · airframe 84,624 hrs · 32,432 cycles

RH FWD OVERWING EMERGENCY EXIT DOOR HAS CRACK IN INTERRIOR FWD SUPPORT BRACE. REF N/R 11035.0334 REMOVED AND REPLACED NEW SEGMENT P/N D5227902620451 AT R/H FWD OVERWING EMERGENCY EXIT DOOR INTERIOR FWD SUPPORT IAW A3 20 SRM 51-42-11/001 COMPLETED BY V062325 INP BY Q930 ENTERED BY V933103 COMPLETED BY V062325 INP BY Q930 ENTERED BY V933103. RE-INSP BY Q966.

Part: FRAME — CRACKED (EMER EXIT DOOR) · airframe 84,624 hrs · 32,432 cycles

RH FWD OVERWING EMERGENCY EXIT DOOR HAS CRACK IN INTERIOR AFT SUPPORT BRACE. REF N/R 11035.0333

Part: FRAME — CRACKED (EMER EXIT DR) · airframe 84,624 hrs · 32,432 cycles

RH FWD OVERWING EMERGENCY EXIT DOOR HAS CRACK IN INTERRIOR FWD SUPPORT BRACE. REF N/R 11035.0334

Part: SKIN — DAMAGED (FRMS 72-76 S24R) · airframe 84,621 hrs · 32,431 cycles

SUPPORT TASK: FOUND AIRCRAFT DAMAGE AFT OF R2 DOOR ON SKIN (UNPR ESSURIZED AREA). REPAIRED SKIN BETWEEN FR72-73 STQR 24RHIAW EA 210070AND EC/RA NO 5351-01181. WORK ACCOMPLISHED ON AAR NR 99897653 BY TECH V920656 AND AAR QC V895387. RII INSPECTION PERFORMED BY AAR QC V895387, ESFR#1025654.

Part: PANEL — CRACKED (FRAMES 35-36) · airframe 81,368 hrs · 30,958 cycles

RESULTS OF ROTO HOLE SCAN AT RH FR35-36, FOUND 12 EA HOLES IB OF CUT-OUT AREA WITH CRACK INDICATIONS. CONTACT ENGINEERING FOR RE PAIR INSTRUCTIONS & REPAIR BEFORE NEXT FLIGHT ON HAECO LCQ REF 9 292517 AD RELATED AD2018-06-04. REPAIRED DISCREPANT HOLE S FR35-36 R/H PRESSURE PANEL IAW ECRA 5331-02343.

Part: RESERVOIR — DAMAGED (EVAC SLIDE) · airframe 81,368 hrs · 30,958 cycles

DATA TRANSFER DURING SETUP FOR RT OVER WING EMER EXIT OPS CHK, FOUND NIPPLE ON CABLE CONNECTOR FROM INFLATION RESERVOIR SHEARED OFF AND NOT CO NNECTED, A3NB-52-3-6028, PER NR 9292025. RMVD & RPLCD RT OVER WING SLIDE INFLATION RESERVOIR IAW AMM 25-62-46-000-001-A & 25-62-46-400-001-A. S/N: A-1684, DUE 21 AUG 19, INSP PERFORMED, N078625 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1324189 SN OFF 5889 IPC REFERENCE # 2560-02442 BOTTLE, AY-OFFW OFF 31-2560-9-9001 5889 ON 31-2560-9-9001 8231.

Part: PRESSURE PANEL — CRACKED (FRAME 36) · airframe 81,368 hrs · 30,958 cycles

AD RELATED AD 2018-06-04, RESULTS OF ROTO-TEST ON TC 14332, FOUND 3RD & 4TH HOLES FROM LH OB END ALONG FR36 CRACK IND IN PRESSUR E PLATE LAYER "CONTACT ENG FOR REPAIR INSTRUCTIONS & REPAIR BEFO RE NEXT FLIGHT" PER HAECO LCQ NR 9292516, GEN. BY MECH V892444 HAECO TECHNICIAN V061616 AND INSP LC 10 REPAIRED DISCREPANT HOLE S IAW ECRA 5331-02342 REV A. DTA LOGPAGE READS ACCOMPLISH THE PE RMANENT REPAIR AT FUSELAGE FR35-36 LH PRESSURE PANEL HOLES PER P ADD EMP:V061616 PART 3 OF ECRA 5331-02342 ON OR BEFORE 28-SEP-2019. PLANNING TO CONTACT ENGINEERING AFTER 28-JUL-2019 BUT BEFORE 28-AUG-2019 FOR PERMANENT REPAIR. REPAIR AT FUSELAGE FR35-36 LH PRESSURE PANEL HOLES PER PART 3 OF ECRA 5331-02342 ON OR BEFORE 28-SEP-2019. PLANNING TO CONTACT ENGINEERING AFTER 28-JUL-2019 BUT BEFORE 28-AUG-2019 FOR PERMANENT REPAIR. DIP APPROVED PER ECRA 5331-02342 REV A ACCOMPLISH THE PERMANENT TOMC-APPROVAL FROM SC1ELBYC COMMENT Q/C REVIEWED. Q/C REVIEWED. INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 81,368 hrs · 30,958 cycles

EEPL LIGHTS AT SEAT ROW 11L IS INOP, A3NB-33-3-6014, PER NR 9292546, RMVD AND RPLCD CONNECTOR FOR EEPL AT SEAT ROW 11L AND OP CHECKS GOOD IAW NAT DRAWING WIRING DIAGRAM 430NWD02 33-51-06 AND AMM 33-51-00-710-009-D.

Part: SEAL — DAMAGED (FAIRING) · airframe 80,294 hrs · 30,466 cycles

HUMMING NOISE AND VIBRATION IN CABIN AT ROW 21. NO SPECIFIC LOCATION NOTED. REPLACED WING TO BODY FAIRING SEALS PANEL 192DT REF AMM 53-35-11. VERIFIED SAFETY AND SECURITY OF PANEL INSTALLATION. OP CK OF EEL LIGHTING NORMAL. WING ROOT PANEL HAS EMERGENCY LIGHTING FOR OVER WING EXITS INSTALLED.

Part: ALTIMETER — READS HIGH (STANDBY) · airframe 76,323 hrs · 28,657 cycles

STANDBY ALTIMETER INDICATION ERRONEOUS, STANDBY ALTIMETER READ 500 FT HIGH THROUGH CLIMBOUT. REPLACED THE STANDBY ALTIMETER IAW AMM 34-21-22. OPS CHECKED OK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,131 hrs · 28,574 cycles

LT FUSELAGE SKIN AT FRAME 35 AT STRINGER 30 HOLE 2 CRACKED (DOWNWARD/AFT) IN SIDE SHELL. ACP REPAIR OF FR 35L STR 30 AS PER ECRA 5320-02797 PART 1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,131 hrs · 28,574 cycles

RT FUSELAGE SKIN AT FRAME 35 AT STRINGER 30 HOLE 2 CRACKED IN SIDE SHELL (DOWNWARD AND AFT). ACP REPAIR OF FR 35R STR 30 AS PER ECRA 5320-02797 PART 1.

Part: FITTING — CRACKED (AFT PAX DOOR) · airframe 76,131 hrs · 28,574 cycles

LEFT AFT PASSENGER DOOR, FRAME 68, SECOND STOP FITTING UP FROM FLOOR LOWER INBOARD HOLE IS CRACKED IN FRAME LAYER AT 5 POSITION. EVALUATED AND REPAIRED NR 2 STOP FITTING ON LT FRAME 68 IAW SRM 53-41-12-300-011. REQUIRES INSPECTION AT 17,100FC, 34,200FH AND INTERVALS OF 5200FC,10,400FH FROM REPAIR EMBODIMENT.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 76,131 hrs · 28,574 cycles

R2 DOOR SILL FROM FR65 TO FR68 HAS CORROSION. REMOVED CORROSION R2 DOOR SILL AT FR68 FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14 FAB REPAIR ANGLE AND INSTALLED IAW SRM 53-41-14 REV 118. THIS REPAIR IS CONSIDERED PERMANENT WITH NO SRI REQUIRED IAW SRM 53-41-14-300-001 REV 118.

Part: PLATE — CORRODED (FRAMES 52A-56) · airframe 76,131 hrs · 28,574 cycles

AFT CARGO BAY COVER PLATE HAS CORROSION BETWEEN FRAMES 52A - 56, STRINGERS 39-41R. REMOVED AND REPLACED COVER PLATE IAW SRM 51-42-11.

Part: COVER — CORRODED (FUSELAGE) · airframe 76,131 hrs · 28,574 cycles

FWD CARGO COMPARTMENT, POTABLE WATER DRAIN COVER CORROSION FR28-29 STR 43L. REMOVED AND REPLACED POTABLE WATER DRAIN COVER IAW SRM 51-4 2-11 REV 118.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 76,131 hrs · 28,574 cycles

FWD PIT AT FR31 CLEAT BETWEEN STR42 -41 HAS CORROSION. REMOVED AND REPLACED CLEAT IN FWD CARGO PIT FR 31RT BETWEEN STR42 -41 IAW SRM 51-42-11 PG6 REV 118.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 76,131 hrs · 28,574 cycles

FWD CARGO AT FR28RT CLEAT BETWEEN S TR43-42 HAS CORROSION. REMOVED AND REPLACED CLEAT AT FR28 BETWEEN STR43-42RT IAW SRM 51-42-11 PG6 REV 118.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,131 hrs · 28,574 cycles

FWD CARGO COMPARTMENT, CORROSION IN 41R BETWEEN FR30-34 MULTIPLE LOCATIONS. REMOVED AND REPLACED STR41R FR31-34 IAW SRM 51-42-11 PG6 REV 118.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 76,131 hrs · 28,574 cycles

FWD CARGO COMPARTMENT, CORROSION ON STR 40R BETWEEN FR 31-34 MULTIPLE LOCATIONS. REMOVED DAMAGED PORTION OF STR 40R & INSTALLED 2EA SPLICES REF SRM 53-00-13-300-001 FIG 20101.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 76,131 hrs · 28,574 cycles

FWD CARGO COMPARTMENT, CORROSION IN CLEAT FR29 STR44-43L. REMOVED AND REPLACED CLEAT FR29 BETWEEN STR44-43L IAW SRM 5 1-42-11 P6 REV 118.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 76,131 hrs · 28,574 cycles

AFT CARGO PIT BETWEEN FR58-59 STR38 L SHEAR PLATE HAS CORROSION. REMOVED AND REPLACED SHEAR PLATE IN AFT CARGO PIT AT STR 38L BETWEEN FR 58-59 IAW SRM 51-42-11 PG1 REV 118.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 76,131 hrs · 28,574 cycles

FWD PIT AT FR28 AT STR41-42RT HAS CORROSION (CLEAT). REMOVED AND REPLACED CLEAT IN FWD CARGO PIT FR28 AT STR41-42RT IAW SRM 51-42-11 PG6 REV 118.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 76,131 hrs · 28,574 cycles

FWD CARGO BAY HAS CORROSION ON THE SHEAR TIE AT FRAME 28, STRINGER 44. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-42-11, PAGE 1, REV 118.

Part: INTERCOSTAL — CORRODED (FRAMES 50-51) · airframe 76,131 hrs · 28,574 cycles

AFT CARGO BAY, BETWEEN FRAMES 50 AND 51, STRINGER 38L, INTERCOASTAL HAS CORROSION AROUND FASTENER HOLE AND SURROUNDING AREA. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-11, PARA 2F, REV 118.

Part: PLATE — CORRODED (EXHAUST VENT) · airframe 76,131 hrs · 28,574 cycles

LAVATORY EXHAUST VENT OUTLET REINFORCEMENT PLATE CORRODED. BLENDED IAW SRM 57-74-00, REV 118. FOUND TO BE OUT OF LIMITS IAW SRM 57-73-11, REV 118. REMOVED AND REPLACED EXHAUST VENT OUTLET REINFORCEMENT PLATE IAW SRM 51-72-11-911-001.

Part: STRINGER — CORRODED (FRAMES 54-60) · airframe 76,131 hrs · 28,574 cycles

AFT CARGO BAY STRINGER CORRODED BETWEEN FRAMES 54 - 60. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-11-001, PG 6, REV 118 AND PG 2, REV 118.

Part: SHEAR PLATE — CORRODED (FRAMES 56-57) · airframe 76,131 hrs · 28,574 cycles

AFT CARGO BAY SHEAR PLATE BETWEEN FRAMES 56 - 57 HAS CORROSION. REMOVED AND REPLACED THE SHEAR PLATE IAW SRM 51-42-11, PG 1, FIG 0013, REV 118.

Part: DOOR SILL — CORRODED (FRAME 68) · airframe 76,131 hrs · 28,574 cycles

AFT ENTRANCE DOOR LT SILL PLATE HAS CORROSION AT GIRT BAR FITTING BRACKET, FRAME 68. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 101, AND INSTALLED A NEW DOOR SILL IAW SRM 51-72-11

Part: STRINGER — CORRODED (FRAMES 67-68) · airframe 76,131 hrs · 28,574 cycles

MAIN CABIN AFT WET AREA STRINGER 25L HAS CORROSION BETWEEN FRAMES 67 - 68. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-44-11-001, FABRICATED A NEW STRINGER IAW DWG D53480046, AND INSTALLED IAW SRM 51-4 2-11

Part: STRINGER — CORRODED (FRAMES 53-60) · airframe 76,131 hrs · 28,574 cycles

AFT CARGO BAY STRINGER 42L CORRODED BETWEEN FRAMES 53 - 60. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-11, P.2, REV 118.

Part: STRINGER — CORRODED (FRAMES 58-59) · airframe 76,131 hrs · 28,574 cycles

AFT CARGO BAY STRINGER 39R BETWEEN FRAMES 58 - 59 HAS CORROSION. R & R THE SECTION OF THE STRINGER AND INSTALLED A REPAIR SPLICE IAW SRM 53-00-13-300-001, REV 118.

Part: STRINGER SPLICE — CORRODED (FRAMES 30-31) · airframe 76,131 hrs · 28,574 cycles

FWD CARGO BAY, CORROSION ON STRINGER SPLICE 42L BETWEEN FRAMES 30-31. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-11, P 10, REV 118.

Part: SHEAR TIE — CORRODED (FRAME 27) · airframe 76,131 hrs · 28,574 cycles

CORROSION ON THE SHEAR TIE OF FRAME 27, STRINGER 43R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-42-11.

Part: STRINGER SPLICE — CORRODED (FRAMES 30-21) · airframe 76,131 hrs · 28,574 cycles

FWD CARGO BAY CORROSION ON STRINGER SPLICE 43L BETWEEN FRAMES 30 - 31. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-11, P 10, PARE, REV 118.

Part: ANGLE — GOUGED (FRAME 60) · airframe 76,131 hrs · 28,574 cycles

LEFT AFT CARGO BAY FRAME 60 WEB TO STRINGER 37L FORWARD OUTBOARD FLANGE HAS GOUGES AROUND FASTENER HOLE. REMOVED, FABRICATED & INSTALLED A NEW ANGLE IAW SRM 51-73-11, SRM 51-26-11, & SRM 51-42-11

Part: BATTERY — FAILED (CABIN) · airframe 75,241 hrs · 28,186 cycles

EEL BATTERY PACK 11WL FAILS BATTERY CAPACITY TEST REF AMM 33-51-00-710-003. REPLACED BATTERY REF AMM 33-51-38-000-002A AND 38-51-38-000-002A . OPS CHECKED OK

Part: UPLOCK — OUT OF POSITION (NLG) · airframe 74,744 hrs · 27,953 cycles

VERY LOUD WIND RUSH, WITH COCKPIT FLOOR VIBRATION, DOES NOT CHANGE WITH SPEED DEREASED. WITH ALT INCREASE. WIND NOISE AND VIBRATION AT ROW 1, ALL NORMAL AFT OF ROW2. ALL GEAR DOORS SHOWED CLOSED AFTER TAKE OFF. NLD INDICATION IS NOW XX. ALSO, AFTER LANDING MLG DISAGREE ECAM. ACCOMPLISHED VISUAL INSPECTION, NO DEFECTS NOTED. ACCOMPLISHED LG BACK TO NORMAL AFTER FREE FALL TEST IAW AMM32-00-00-860-003, TESTED GOOD. FOUND DOORS NOT FULL Y CLOSING HYDRAULICALLY. DOOR UPLOCK HOOK OUT OF POSITION. REPLACED NLG UPLOCK ASSY AND SWUNG NOSE GEAR, DOOR OPERATION AND INDICATION NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,023 hrs · 27,626 cycles

EMERGENCY LIGHTS INOPERATIVE AT ROWS 11, 12, 20 A ND 21. REPLACED THE POWER SUPPLY UNIT 12WL IAW AMM 33-51-39 PG 401, OPS CHECKED NORMAL.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 73,904 hrs · 27,579 cycles

RIGHT WING EMERGENCY LIGHT CAME ON DURING LANDING RESET CIDS, LIGHTS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 73,822 hrs · 27,549 cycles

ON 2 SERVICE CHECKS, EMERGENCY LIGHTS TEST FAIL WITH FOLLOWING MSG, EXT LOADS EMERGENCY RT BATTERY, EMERGENCY RT AND UNIT EMERGENCY LT. REPLACED DOOR 2L LIGHT POWER SUPPLY AND BATTERY OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 73,822 hrs · 27,549 cycles

WITH EMERGENCY LIGHT SWITCH IN ARMED MODE AND LOSS OF ACFT POWER, EMERGENCY LIGHTS DO NOT COME ON IN THE CABIN AND OVERWING. REPLACED EMERGENCY POWER SUPPLY AND BATTERY AT DOOR 1L. OPS CK GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 73,822 hrs · 27,549 cycles

EMERG LIGHTS MESSAGE. EXT LOADS EMER R, BATT EMER R, EMER L REPLACED RIGHT OVERWING EPSU & BATTERY

Part: BRACE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,561 hrs · 26,570 cycles

AT FRAME 66, STRINGER 25 BRACE, FROM FRAME TO STRINGER CORRODED. R & R SECTION OF STRINGER 25R & INSTALLED BETWEEN FRAME 66.5 - 67.5 IAW SRM 53-00-13. ACCOMPLISHED AT LCQ C4.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,561 hrs · 26,570 cycles

FUSELAGE STRUCTURE, BENEATH OUTFLOW VLV, FRAME 66, STRINGER 31R, CORROSION. R & R STRINGER 31R, FROM FRAME 64 - 66 IAW SRM 51-42-11 PGS 25 - 26.

Part: BEAM — CRACKED (FUSELAGE) · airframe 71,561 hrs · 26,570 cycles

LEFT SIDE BOX BEAM, UPPER FLANGE AT FRAME 43, HAS CRACK INDICATION AT AFT HOLE NR 9, FWD & AFT SIDES OF HOLE, 6 O'CLOCK & 12 O'CLOCK, FROM TOP SURFACE OF FLANGE TO A DEPTH OF .230". REPAIRED ON EA 5331-01704 OPS 3 - 12.

Part: BEAM — CRACKED (FUSELAGE) · airframe 71,561 hrs · 26,570 cycles

LEFT SIDE BOX BEAM, UPPER FLANGE AT FRAME 43, HAS CRACK INDICATION AT HOLE NR 10, AFT SIDE OF HOLE, 6 O'CLOCK, FROM TOP SURFACE OF FLANGE TO A DEPTH OF .110". REPAIRED ON EA 5331-01704 OPS 3 - 12.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,561 hrs · 26,570 cycles

STRINGER 26R FWD & AFT OF FRAME 66 HAS CORROSION. R & R STRINGER IAW SRM 51-42-11 PGS 25 - 27.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,561 hrs · 26,570 cycles

AT FRAME 66, STRINGER 32R CORRODED UNDER & BEHIND FRAME. R & R STRINGER 32R AT FRAME 66 IAW SRM 51-42-11 PARA 7.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 71,561 hrs · 26,570 cycles

AT FRAME 66, STRINGER 28R CLEAT, AFT OF FRAME CORRODED. R & R CLEAT IAW SRM 51-42-11 PG 25 PARAGRAPH 7.

Part: CLEAT — DAMAGED (FUSELAGE) · airframe 71,561 hrs · 26,570 cycles

TWO EACH ENLARGED LOCK FASTENER HOLES ON CLEAT, BY FRAME 65 & STRINGER 31R. R & R CLEAT IAW GPM 07-35-0 & SRM 51-42-11 PARA 6 & 7.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,561 hrs · 26,570 cycles

R2 DOOR SILL HAS CORROSION IN MULTIPLE LOCATIONS & CORROSION MIGRATING GIRT BAR PLATES. R & R R2 DOOR SILL IAW SRM 51-72-11.

Part: UNKNOWN — SMOKE (CARGO BAY) · airframe 66,892 hrs · 24,724 cycles

AFT CARGO SMOKE DISPLAYED ON UPPER ECAM. RAMP REPORTS SMOKE COMING FROM AFT CARGO.

Part: UNKNOWN — MALFUNCTIONED (FLIGHT CONTROL) · airframe 66,845 hrs · 24,705 cycles

ALTERNATE LAW PROT LOST DISPLAYED ON UPPER ECAM SCREEN, FLIGHT CONTROL. CYCLED BREAKERS B 3 & 4. PERFORMED AFS TEST IAW MM22-96-00, CHECKED GOOD.

Part: YAW DAMPER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 66,845 hrs · 24,705 cycles

YAW DAMPER 1 INOPERATIVE AUTO FLT. CYCLED BREAKERS B 3 & 4, RESET FAC1. PERFORMED AFS TEST IAW MM22-96-00, CHECKED GOOD.

Part: A/C PACK — FAULTED (AC BAY) · airframe 66,845 hrs · 24,705 cycles

PACK 2 FAULT DISPLAYED ON UPPER ECAM SCREEN, AIR. RESTARTED ENGS AT THE GATE. PACK 2 OPERATED NORMAL, NO FAULTS.

Part: STRUT — DEFECTIVE (TE FLAP) · airframe 66,390 hrs · 24,531 cycles

FLAPS LOCKED ALIGNMENT FAULT DISPLAYED ON UPPER ECAM SCREEN. ECAM AFTER LANDING WHEN FLAPS SELECTED UP, WAS ABLE TO DUPLICATE FLAP LOCKOUT PROBLEM. HAD FLIGHT CONTROL FLAPS LOCKED ECAM MESSAGE WITH AMBER INDICATION ON FLAPS. IAW TSM 27-51-00-810-818 SUSPECT BAD FLAP INTERCONNECTING STRUT, PART IS BEING SOURCED.

Part: WINDSHIELD — DAMAGED (COCKPIT) · airframe 66,195 hrs · 24,458 cycles

CAPTAIN'S WINDSHIELD VISIBILITY IS IMPAIRED. EVIDENCE OF ARCING. CRACKED AREA IS DISCOLORED & APPEARS TO BE LOCATED ON THE MIDDLE PANE. FAR LOWER LT CORNER OF WINDSHIELD APPEARS TO BE CRACKING AT THE OUTER PANE. WILL REQUIRE REPLACEMENT IAW AMM. REPLACED CAPT WINDSHIELD IAW MM 56-11-11, OPERATIONS CHECKED IAW MM 30-42-00, OPERATIONS CHECKED GOOD

Part: AUDIO PANEL — FAULTY (COCKPIT) · airframe 65,769 hrs · 24,294 cycles

THIRD OBSERVERS AUDIO CONTROL PANEL SELECTOR LIGHTS DO NOT WORK IN NORMAL OR TEST MODE. BACKGROUND LIGHTS WORK NO SELECT LIGHTS WORK. TRIED NEW ACP & CONTROLLER. ORIGINAL EQUIPMENT BACK IN PLACE, IAW MEL. REPLACED IAW ASM 33-14-08 ACP BAD CAUSING 37LP XFMR FUSE T TO BLOW. REPLACED FUSE IAW MM 33-14-51. R&R THIRD OBSERVERS ACP MM 23-51-12 OPERATIONS CHECKED GOOD.

Part: SEAT — DEFECTIVE (COCKPIT) · airframe 65,641 hrs · 24,248 cycles

FIRST OFFICER SEAT MANUAL ADJUSTMENT, RECLINE DEFECTIVE. SEATBACK WILL NOT RETURN TO UPRIGHT ON ITS OWN. REPLACED SEAT PER AMM.

Part: WIRE — SHORTED (SWITCH) · airframe 65,495 hrs · 24,191 cycles

RAMP REPORTED FWD CARGO NESTING SYS NOT WORKING. FOUND THAT THE LIGHT SWITCH WAS SMOKING IN THE DOOR OPENING PANEL. SUSPECT SWITCH IS SHORTING OUT. FOUND 9MJ FWD DOOR OPEN AND LOCKED LIGHT SWITCH WIRE 5037 AND 5030 CHAFED AND SHORTING TO EACH OTHER, REPAIRED WIRING IAW SWP20-10-13, ALSO REPLACED 9MJ AS PRECAUTIONARY IAW AWM 52-35-01. OPS CK GOOD.

Part: ENGINE — LEAKING (NR 1) · airframe 65,389 hrs · 24,153 cycles

AFTER ENG 1 START, LIQUID LEAKING OUT OF ENG 1. SMELLED LIKE FUEL.

Part: LINER — MISSING (NR 2 NACELLE) · airframe 64,995 hrs · 24,006 cycles

NR 2 ENGINE ACOUSTIC MATERIAL AT THE 6 O'CLOCK POSITION MISSING. REPAIRED IAW MT 72-017.

Part: SKIN — DAMAGED (RT NLG DOOR) · airframe 64,958 hrs · 23,992 cycles

RT NOSE GEAR DOOR HAS 2 LIGHTNING BURNS. PERFORMED INTERIM REPAIR, REF SRM 52-82-11 FIG 103.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 64,921 hrs · 23,980 cycles

EMERGENCY LIGHT BITE FAILS LT EPSU AND AFT BATTERY. REPLACED LT EPSU AND BATTERY AND AFT BATTERY. CHECKS OK.

Part: PAINT — PEELING (RADOME) · airframe 64,883 hrs · 23,963 cycles

NOSE RADOME HAS PAINT PEELING ON FRONT MIDDLE PORTION.

Part: UNKNOWN — ODOR (CABIN) · airframe 64,853 hrs · 23,952 cycles

ELECTRICAL ODOR IN ACFT, NO DISCERNABLE LOCATION. AFTER EXTENSIVE TROUBLESHOOTING OF ACFT SYSTEMS, NO FAULTS FOUND. ODOR WENT AWAY. THERE ARE NO FAULTS FOUND ON THE ACFT SYS AND AFTER USING APU AND PACKS ODOR WENT AWAY AND HASN'T RETURNED IAW TSM.

Part: ENGINE — STALLED (NR 2) · airframe 64,850 hrs · 23,950 cycles

NR 2 ENG STALL, FLT DIVERTED.

Part: VALVE — LEAKING (CARGO DOOR) · airframe 64,734 hrs · 23,902 cycles

LONG TERM HYDRAULIC LEAK FROM DRAIN HOLES AFT OF FWD CARGO DOOR ACTUATOR. INSTALLED CARGO BAY DOOR SELECTOR VALVE ON FWD DOOR. LEAK CHECKED, OKAY.

Part: HANDLE — FAULTY (LANDING GEAR) · airframe 64,422 hrs · 23,788 cycles

LANDING GEAR NR 1 LGCIU FAULT ECAM ON GEAR DOWN ON APPROACH. REMOVED AND REPLACED LANDING GEAR HANDLE PER AMM, OPS NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 63,970 hrs · 23,606 cycles

FWD EMERGENCY LIGHT ON THE SIDE OF SEAT 1B LENS MISSING. REPLACED LIGHT ASSY, TESTED OK.

Part: STRUCTURE — DAMAGED (NR 1 INLET) · airframe 63,892 hrs · 23,573 cycles

NR 1 ENG INLET SOUNDPROOFING MATERIAL 12 O'CLOCK POSITION HAS APPROX ONE INCH HOLE. REPAIRED DAMAGE PER MT 72-017.

Part: COVER — UNSECURE (R2 DOOR SLIDE) · airframe 63,839 hrs · 23,550 cycles

DOOR 2R SLIDE PACK COVER UNSECURE. ATTACHED AND SECURED R2 SLIDE COVER, OK TO CONTINUE.

Part: MONITOR — MALFUNCTIONED (CASBIN) · airframe 63,426 hrs · 23,390 cycles

ACRID SMELL IN AFT CABIN FOLLOWED BY 3 MONITORS GOING OUT. CYCLED ALL MONITORS AND PLAYED VIDEO NO SMELL NOTED AT ANY TIME, ALL OP CHECK GOOD.

Part: SEALANT — DETERIORATED (RT WING) · airframe 62,795 hrs · 23,141 cycles

FUEL DRIPPING FROM RIGHT WING OUTBOAR FLAP CANOE. FOUND DETERIORATED SEALANT O/B SIDE OF CASTING THAT HOLDS FLAP TRACK FAIRING. CLEANED AFFECTED AREA AND RESEALED. ALSO RESEALED ENTIRE CASTING AREA AND CAP SEALED FASTENERS AS PRECAUTIONARY.

Part: LIGHT — INOPERATIVE (EXTERNAL POWER) · airframe 62,557 hrs · 23,040 cycles

EXTERNAL POWER NOT IN USE LIGHT AT PLUG-IN IS INOPERATIVE. RELAMPED NOT IN USE LIGHT AT EXTERNAL POWER PANEL, OPS CHECK GOOD.

Part: POWER SUPPLY — FAULTY (SMOKE DETECTOR) · airframe 62,423 hrs · 22,992 cycles

SMOKE LAV+CRG DET FAULT DISPLAYED ON ECAM. REPLACED SMOKE DETECTOR PWR SUPPLY UNIT PER AMM, OPS GOOD.

Part: LINER — DAMAGED (NR 1 ENGINE) · airframe 62,109 hrs · 22,876 cycles

NR 1 ENGINE ACOUSTICAL LINER HAS SOME DAMAGE. REF MT78-010 FOR ALLOWABLE DAMAGE. DAMAGED AREA IS ON THRUST REVERSE R SLEEVE INNER WALL. AREA IS APPROXIMATELY 7 INCHES WIDE BY 31. 5 LONG. LOOSE MATERIAL TRIMMED AND INTERIM REPAIR ACCOMPLISHED BY APPLYING SPEED TAPE PER MT 78-010. ACCOMPLISHED REPAIR, IAW MT 78-010.

Part: BULB — BURNED OUT (TAIL) · airframe 61,667 hrs · 22,726 cycles

TAIL LIGHT BURNED OUT IN NR 1 POSITION. CLEANED CENTER CONTACT ON LIGHT ASSEMBLY POSITION 2. REPLACED BULB PER AMM 33-41-15 PG 401, OPS CHECKED GOOD.

Part: ACTUATOR — LEAKING (THRUST REVERSER) · airframe 61,379 hrs · 22,610 cycles

NR 2 OTBD THRUST REVERSER COWL OPEN ACTUATOR LEAKING. REPLACED ACTUATOR.

Part: GIRT BAR — DAMAGED (FUSELAGE) · airframe 61,379 hrs · 22,610 cycles

FWD RT ENTRY DOOR SLIDE IS BROKEN. LACED GIRT BAR ONTO NEW SLIDE.

Part: SEAL — LEAKING (COMPRESSOR) · airframe 61,279 hrs · 22,578 cycles

OIL LEAKING FROM BACK OF NR 1 ENGINE 1ST STAGE COMPRESSOR BLADES BEHIND SPINNER CONE AT 6 O'CLOCK POSITION. REPLACED BOTH SEALS IN THE LOW PRESS TURBINE SHAFT BLIND CAP COMPARTMENT. ALSO COMPLIED WITH COMPARTMENT OIL RETURN LINE COKING INSPECTION. NO COKING RAN ENG AT FLX MAX & CLIMB PWR FOR 2 MINUTES AND INDL FOR 20 MINUTES NO MORE OIL LEAK AT FRONT OR BACK OF ENGINE.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 61,249 hrs · 22,566 cycles

SEAT 21C & 26C EMERGENCY FLOOR LIGHTS ARE INOP. NO TIME. FOUND LOOSE CONNECTION ON SEAT 26C. SECURED CONNECTOR UNDER SEAT 26C, OPS CKS NORMAL. SEAT 21C STILL INOPERATIVE. REPLACED HARNESS AT 21C. OPS GOOD.

Part: STRAP — EXPOSED (L2 DOOR SLIDE) · airframe 61,074 hrs · 22,505 cycles

2L DOOR YELLOW RELEASE STRAP HAS EXCESS STRAP STICKING OUT OF GIRT ASSEMBLY. REF AMM. ACCOMPLISHED ROUTING OF YELLOW RELEASE STRAP REF AMM, OPS CHECKED GOOD.

Part: ACTUATOR — FAULTY (ELEVATOR) · airframe 61,028 hrs · 22,486 cycles

NEED TO REPLACE L/G ELEV SERVO ACT. REMOVED L/G ELEV SERVO ACT PER MM. INSTALLED L/G ELEV SERVO ACT. NEED TO INSTALL COTTER PIN 25, 20, AND LOCKING CAP 19 PER 27 34-51 PG 428. THEN CONT 27-34-51 PG 431 STEP D TIL END. MR27350 DASH OFF 421 DASH ON 69. ACCOMPLISHED FROM 27-34-51 PG 431 STEP 'D' TO COMPLETION. INSTALLED COTTER PINS AND LOCKING CAP.

Part: COMPUTER — FAULTY (NR 2) · airframe 61,028 hrs · 22,486 cycles

INSTALLED NEW ELAC 2 STILL HAVE A HARD FAULT. MR27935-280 INSTALLED. OLD ELAC IS MR27935-232. ACCMP'D AFS LAND TEST. GROUND OPS CHECK GOOD.

Part: INDICATOR — FAULTY (FUEL SYSTEM) · airframe 61,025 hrs · 22,485 cycles

CB L26 (FQI 1&2) FOUND OPEN, ELECTRICAL ODOR WAS NOTED. FOR AMT TROUBLESHOOTING. FOUND RFL-DFL PANEL HOT TO TOUCH AND INOPERATIVE, CB L26 CB FOR FQIC 1 AND 2 WOULD OPEN ON ITS OWN WITH S=ELEC ODOR BUT NO SMOKE IN CABIN, EFS REQUESTED. SHUT DOWN AIRCRAFT SYSTEMS UNTIL EFS ARRIVES. REPLACED INDICATOR, OP CHECKS NORMAL. ALSO REPLACED PRESELECTOR PER AMM. INSPECTED WIRING NO FAULTS FOUND.

Part: VALVE — FAULTY (COCKPIT) · airframe 61,007 hrs · 22,478 cycles

CREW REPORT: UNABLE 2 CONTROL TEMPS COCKPIT SET FULL HOT TEMP-68-FWD CABIN SET FULL COLD TEMP-74. SAMC TEXT: AFT FULL HOT TEMP-70. SECURED HOT AIR PRV CLOSED.

Part: SERVO CONTROL — MALFUNCTIONED (NLG STEERING) · airframe 60,602 hrs · 22,342 cycles

N-W STEERING FAULT SHORT FINAL. WENT AROUND & LANDED NEXT APPROACH. NO N-W STEERING. RESET NOSE WHEEL SERVO CONTROL PER MM. ACCOMPLISHED FUNCTIONAL TEST. OPS TEST NORMAL NO FAULTS.

Part: VALVE — FAULTY (AC SYSTEM) · airframe 60,535 hrs · 22,321 cycles

VENT SKIN VLV FAULT, RTFL.

Part: VALVE — OUT OF SEQUENCE (CABIN PRESSURE) · airframe 60,507 hrs · 22,308 cycles

SKIN AIR OUTLET VLV FAULT, RTFL DISPLAYED ON UPPER ECAM. OVERWEIGHT LANDING SPEED 142 KNOTS, 300 FPM DESCENT. LANDING WEIGHT 152000 LBS. BASED ON THE INFORMATION AND PER MM, NO INSPECTION IS REQUIRED. SKIN AIR OUTLET VALVE WAS OUT OF SEQUENCE WITH INLET VALVE. RESET OUTLET VALVE AND TESTED AEVC TEST FOUR TIMES,TESTED OK EACH TIME WITH NO FAULTS.

Part: LIGHT — FALSE INDICATION (CABIN) · airframe 60,094 hrs · 22,166 cycles

DURING TEST OF EMERGENCY EXIT LIGHTS, RECEIVED MESSAGE FOR LT AFT BATTERY. REPEATED TEST SEVERAL TIMES WITH SAME RESULT. ACCOMPLISHED SUCCESSFUL SYSTEM TEST OF EMERGENCY LIGHTS, TEST OK DISPLAYED, NO FAULTS. OBSERVED AFT EMERGENCY LIGHTS ILLUMINATE.

Part: LANYARD — FAULTY (L1 DOOR) · airframe 59,896 hrs · 22,086 cycles

DOOR 1L IS HARD TO ARM. FOUND LANYARD HANGING DOWN 2" RESTRICTING GIRT BAR. REPACKED LANYARD PER AMM.

Part: OXYGEN MASK — DEPLOYED (CABIN) · airframe 59,564 hrs · 21,937 cycles

SEAT 2A AND 2B OXYGEN MASK DEPLOYED. MASKS RESTOWED AS PER MT 35-003, O2 SYSTEM REQ DROP CHECK AS PER MT 35-003.

Part: OXYGEN MASK — MISSING (PORTABLE O2) · airframe 59,473 hrs · 21,894 cycles

O2 MASK MISSING FOR PORTABLE O2 BOTTLE AT DOOR 1L. REPLACED MASK.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 59,378 hrs · 21,851 cycles

EMERGENCY LIGHTS OUT AT ROW 28-30, AND ROW 22-24. RESEATED CONNECTORS AT SEAT BOX LOCATIONS AT ROWS 28-30 AND 22-24. OPS CHECK GOOD. ACPD ON WU Y 1056H.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 59,066 hrs · 21,715 cycles

2L DOOR ASSIST BOTTLE LOW. DOOR BOTTLE WAS 1600 LBS, SERVICED TO 1750.

Part: PANEL — MISSING (THRUST REVERSER) · airframe 58,864 hrs · 21,635 cycles

NR 2 ENGINE ISLAND PANEL MISSING FROM TRANSLATING COWL. PART ON AOG 5186. ISLAND ASSY 222-1349. REPLACED THE ISLAND ASSY (222-1349) IAW AMM.

Part: SLIDE — UNSERVICEABLE (CABIN) · airframe 58,864 hrs · 21,635 cycles

FOUND LT OFF WING SLIDE WITH PAINT IN ALL 3 BALL LOCK PINS. FOUND PER EG5371 AND MM PAGE 420. LT OVERWING SLIDE IS PCN 649-9000. REPLACED LT OVERWING SLIDE ASSY PER MM.

Part: SWITCH — FAULTY (CABIN) · airframe 58,323 hrs · 21,446 cycles

EMERGENCY LIGHTS COME ON. HISTORY OF EMERGENCY LIGHTS COMING ON WITH SWITCH IN "ARM" POS. FOLLOW TSM AND REPLACE SWITCH 4WL (565-2161). REPLACED EMERGENCY LIGHT SWITCH (4WL). OPERATION CHECK EMERGENCY LIGHT SYSTEM. LIGHTS OP CHECKS OKAY. PERFORMED CIDS EMERGENCY LIGHT CHECK OKAY.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 58,314 hrs · 21,442 cycles

OVERHEAD EMERGENCY LIGHT(S) INOP. CREW COMMENTS: CABIN EMERGENCY EXIT LIGHTS CAME ON IN FLIGHT. WILL EXTINGUISH WITH EMERGENCY LIGHT SWITCH IN OFF. REPLACED EMERGENCY POWER SUPPLY 11WL AND 12WL PER AMM. EMERGENCY LIGHT TEST CHECK WAS NORMAL.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 58,253 hrs · 21,414 cycles

SMOKE IN COCKPIT, RTFL

Part: TRU — MALFUNCTIONED (NR 1) · airframe 57,958 hrs · 21,306 cycles

BURNING ODOR OCCURED AT THE SAME TIME AS TRANSFORMER RECTIFIER 1 FAULT. FOUND FAULTY TRANSFORMER. REPLACED NR 1 TRANSFORMER RECTIFIER, OPS NORMAL.

Part: SEAL — FAILED (EMERGENCY EXIT) · airframe 57,372 hrs · 21,065 cycles

LOUD HISS-SQUEAL FROM FWD RIGHT OVERWING EMERGENCY EXT DISSIPATES AT HIGH PSI. REMOVED FWD RT EMERGENCY WING EXIT DOOR. REPLACED DOOR SEAL PER MM. INSTALLED DOOR. ARMED DOOR AND STOWED PINS RT OFF-WING ESCAPE SLIDE PER MM.

Part: REGULATOR — LEAKING (CREW O2) · airframe 56,764 hrs · 20,783 cycles

CREW O2 LOW, (1200). REPLACED OXYGEN PRESSURE REGULATOR & TRANSMITTER. REPLACED DUE TO OXYGEN LEAKING.

Part: UNKNOWN — ODOR (CABIN) · airframe 56,744 hrs · 20,774 cycles

AVIONICS SMOKE ECAM, RTFL. REVIEWED CFDS: NO FAULT MESSAGES. PERFORMED AEVC TEST: NO FAILURES. SDCU TEST HAS NO FAULTS. INSPECTED - SNIFFED E & E AREA: NO EVIDENCE OF SMOKE. VENT EXHAUST FAN HAS NO SMOKE ODOR. --WET WOOD BOXES IN FWD CARGO HAVE A WOODEN ODOR, NOT SMOKE. DUE TO RTFL, PERFORMED WALK AROUND TO VERIFY NO OTHER FAULTS (E.G. RAT DEPLOY) EXIST.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,460 hrs · 20,630 cycles

AFT FUSELAGE STRINGER JUST BELOW CABIN OUTFLOW VALVE IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REMOVED CORRODED STRINGER. INSTALLED NEW REPLACEMENT STRINGER & REPAIR SPLICE ANGLES. WORK ACP BY STAM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 56,460 hrs · 20,630 cycles

AFT PIT BILGE STR 43L CORRODED BETWEEN FR 57 AND 58. MAJOR REPAIR ACCOMPLISHED: STRINGER 43L CORRODED BETWEEN FR57 AND FR58. REMOVED CORROSION AND INSTALLED ANGLE REPAIR.

Part: PROXIMITY SWITCH — FAULTY (DOOR 2R) · airframe 56,244 hrs · 20,546 cycles

CREW REPORTED DOOR 2R WILL NOT ARM. CONFIRMED DR 2R SLIDE ARMS NORMALLY, NO ARMED ECAM IN FLT DECK. SEE PREVIOUS HISTORY. MEL 2560R APPLIED. REPLACED SLIDE ARM HANDLE PROXIMITY SWITCH 7WN2 IAW AMM. PRESSURIZED PLANE TO 5000', SLIDE MESSAGE STAYED. ACP INSTALLATION INSP OF PROX SWITCH IAW MM.

Part: SLIDING WINDOW — DELAMINATED (COCKPIT) · airframe 55,731 hrs · 20,336 cycles

CAPTAIN'S SLIDING WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS. NEED TO EVALUATE CONDITION. CREW COMMENTS: CAP SLIDING WINDOW, VERYHOT, MANY DELAMINATION BUBBLES OBSCURING VISIBILITY. REPLACED LT SLIDING WINDOW.

Part: SMOKE WARNING — FALSE ACTIVATION (E/E BAY) · airframe 55,661 hrs · 20,299 cycles

AVIONICS SMOKE ECAM. INSPECTED AVIONICS COMPARTMENT AND NO SMOKE PRESENT. REMOVED SMOKE DETECTOR, AIRFLOW THRU TUBES NORMAL. REINSTALLED SMOKE DETECTOR. CYCLED CB'S TO RESET THE AEVC AND FWC'S. RAN BITE TEST OF AEVC AND ALL NORMAL. NO ECAM MSG'S PRESENT.

Part: ACTUATOR — FAULTY (TE FLAP) · airframe 54,857 hrs · 19,963 cycles

REPLACE RIGHT WING NR 3 FLAP ACTUATOR ON ACCT OF CHRONIC LOCKED FLAPS. INSTALLED NR 3 RT WING FLAP ACTUATOR PER MM. NEED LONGER BOLTS FOR NEW STYLE ACTUATOR. TEMPORARILY INSTALLED WITH SHORTER BOLTS, WILL NEED CORRECT LENGTH BOLTS. ON AOG T1408 & S1381. INSTALLED ALL BUT 1 CORRECT LENGTH BOLT. INSTALLED BOLT AND COMPLETED INSTALLATION AND ADJUSTMENT OF NR 3 RT FLAP ACTUATOR.

Part: ACTUATOR — FAULTED (TE FLAPS) · airframe 54,857 hrs · 19,963 cycles

FLAPS LOCKED - ALIGNMENT FAULT DISPLAYED ON UPPER EC AM SCREEN, - F-CTL. REMOVED RT WING NR 1 FLAP ACTUATOR, INSTALLED NR 1 RT WING FLAP ACTUATOR (PN 791C0000-02, SN (N985). NEED LONGER BOLTS FOR NEW STYLE ACTUATOR. INSTALLED CORRECT LENGTH BOLTS. INSTALLED NR 2 RT WING FLAP ACTUATOR (PN 792D0000-02 SN(N991). NEED LONGER BOLTS FOR NEW STYLE ACTUATOR. INSTALLED CORRECT LENGTH BOLTS. INSTALLED NR 3 RT WING FLAP ACTUATOR. NEED LONGER BOLTS FOR NEW STYLE ACTUATOR. TEMPORARILY INSTALLED WITH SHORTER BOLTS, WILL NEED CORRECT LENGTH BOLTS. INSTALLED ALL BUT 1 CORRECT LENGTH BOLT. INSTALLED BOLT AND COMPLETED INSTALLATION AND ADJUSTMENT OF NR 3 RT FLAP ACTUATOR. REPLACED RT WING NR 4 FLAP TRACK ACTUATOR.

Part: ACTUATOR — FAULTY (TE FLAP) · airframe 54,857 hrs · 19,963 cycles

REPLACE RIGHT WING NR 4 FLAP ACTUATOR ON ACCT OF CHRONIC LOCKED FLAPS. REPLACED RIGHT WING NR 4 FLAP TRACK ACTUATOR.

Part: ACTUATOR — MALFUNCTIONED (TE FLAP) · airframe 54,857 hrs · 19,963 cycles

REPLACE RIGHT WING NR 3 FLAP ACTUATOR ON ACCT OF CHRONIC LOCKED FLAPS PER CH8644. INSTALLED NR 3 RT WING FLAP ACTUATOR PER MM. INSTALLED BOLTS AND COMPLETED INSTALLATION AND ADJUSTMENT OF NR 3 RT FLAP ACTUATOR.

Part: BOLT — WRONG PART (TE FLAP ACTUATOR) · airframe 54,857 hrs · 19,963 cycles

REPLACE RIGHT WING NR 2 FLAP ACTUATOR ON ACCT OF CHRONIC LOCKED FLAPS PER CH8644. INSTALLED NR 2 RT WING FLAP ACTUATOR FROM STEP C (3) OF MM. INSTALLED CORRECT LENGTH BOLTS.

Part: BOLT — WRONG PART (TE FLAP ACTUATOR) · airframe 54,857 hrs · 19,963 cycles

REPLACE RIGHT WING NR 1 FLAP ACTUATOR ON ACCT OF CHRONIC LOCKED FLAPS. REMOVED RIGHT WING NR 1 FLAP ACTUATOR. INSTALLED 1 RT WING FLAP ACTUATOR. INSTALLED CORRECT LENGTH BOLTS.

Part: PICKUP — OUT OF ADJUST (FLAPS) · airframe 54,792 hrs · 19,935 cycles

F/CTL FLAPS LOCKED ECAM. FLT CONT FLAP LOCKED. FOUND ASSY POSITION PICKUP UNIT OUT OF ADJUSTMENT AND REPLACED. TOLERANCE IS NOW WITHIN 0.1 AT ALL FLAP SETTINGS. LIMIT IS 0.9 AT ZERO FLAPS AND 1.3 AT FLAP SETTINGS 1, 2 AND 3.

Part: BOTTLE — LOW (ESCAPE SLIDE) · airframe 54,783 hrs · 19,929 cycles

F/A REPORTED SLIDE BOTTLES LOW AT DOOR 1L & 2R. SERVICED DOOR ASSIST BOTTLES TO NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,755 hrs · 19,916 cycles

FUSELAGE SKIN CREASED APPROX 38 INCHES FWD OF L2 DOOR AT STRINGER 21L (FRAME 64-65). REPAIRED IAW SRM AND MARKED REPAIR.

Part: LANYARD — OUT OF ADJUST (R2 DOOR SLIDE) · airframe 54,246 hrs · 19,710 cycles

DOOR 2R SLIDE ARMING LEVER HARD TO OPERATE. REPOSITIONED YELLOW LANYARD, ARMING LEVER OPERATES NORMAL.

Part: D-RING — OUT OF POSITION (SURVIVAL PACK) · airframe 53,585 hrs · 19,364 cycles

ALL 4 DOOR SURVIVAL PACK D-RINGS ARE NOT ACCESSIBLE. D-RING LANYARDS ARE NOT ACCESSIBLE. D-RINGS LOCATED AND ACCESSIBLE.

Part: SPRING — BROKEN (GIRT BAR FITTING) · airframe 52,495 hrs · 18,902 cycles

DOOR 2L AFT GIRT BAR FITTING HAS A BROKEN SPRING MAKING DOOR HARD TO ARM. INSTALLED NEW SPRING IN GIRT BAR FITTING. ACCOMPLISHED INSTALLATION INSPECTION AS REQUIRED.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 52,132 hrs · 18,751 cycles

AFT LEFT BATTERY HAS FAULTED. REPLACED BATTERY, EMERGENCY SYSTEM TEST PASS.

Part: VALVE — FAILED (CABIN) · airframe 51,948 hrs · 18,674 cycles

CABIN TEMPERATURE PROBLEM. RTFL. REVIEWED POST FLIGHT REP, FAILURE MSG TRIM AIR PRESS VALVE OR PRESS SWITCH. REPLACED TRIM AIR PRESS REG VALVE 14HK. RAN BOTH PACKS FROM BOTH ENGINES TO VERIFY NO FURTHER FAULTS. NO DEFECTS OBSERVED.

Part: STRUCTURE — DAMAGED (RT WING TE FLAP) · airframe 51,928 hrs · 18,665 cycles

RT OUTBOARD TRAILING EDGE FLAP DAMAGED BY BIRD STRIKE. FOUND RT MOST OUTBOARD LEADING EDGE FLAP WITH ONE QTR IN. PUNCTURE ABOVE 4 IN. CRACK FOLLOWED BY A 2 AND A HALF INCH LONG CRACK. BOTH CRACKS ARE WITHIN HALF AN INCH APART. REMOVED RT O/B FLAP LEADING EDGE. ACP SURVEILLANCE INSP. REPAIR IAW SRM 57-53-00. RESTORED FINISH. RE-INSTALLED LEADING EDGE.

Part: LANYARD — LOOSE (EVAC SLIDE) · airframe 51,311 hrs · 18,434 cycles

LANYARD LOOSE AT DOOR 1R. SECURED LANYARD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 50,804 hrs · 18,235 cycles

GEAR NOT UPLOCKED DISPLAYED ON UPPER ECAM SCREEN - L-G.

Part: COMPUTER — FAULTY (ELAC 2) · airframe 48,117 hrs · 17,245 cycles

ELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. ELAC 2 FAILURE, CIRCUIT BOARD FAILURE. BOTH ELAC 1 AND ELAC 2 WERE REPLACED ON THE A/C FOR PRECAUTION. ALL SYSTEM TEST ACCOMPLISHED AND NO FAULTS NOTED. THE ELAC UNIT WAS SENT TO THALES AND SEVERAL COMPONENTS (INTERNAL) WERE REPLACED, MN61, MN13, ,M73, MN173, MN71, MN121 ONBOARD MDG.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 47,135 hrs · 16,928 cycles

AFT OF L1 DOOR BETWEEN FRAMES 23 & 24, S22-23L. A LARGE DENT MEASURING 3.5 INCHES BY 2 INCHES AND .250 INCHES DEEP. PATCH ON FWD EDGE IS ALSO DENTED.

Part: UNKNOWN — ODOR (COCKPIT/CABIN) · airframe 47,073 hrs · 16,900 cycles

DURING INITIAL CLIMBOUT STRONG ELECTRICAL ODOR IN CABIN AND COCKPIT, ODOR DISSIPATED SHORTLY. 11-01-07 FOUND F/O MAP LIGHT SHORTING. REPLACED THE F/O MAP LIGHT ON THE F/O WINDOW.

Part: WINDOW — OUT OF ADJUST (COCKPIT) · airframe 47,062 hrs · 16,895 cycles

LOUD SQUEAL F/O SLIDING WINDOW FL260 CABIN ALT 4250. STOPPED FL130 CABIN ALTITUDE 2650. PROBLEMS RECURRED ON FLT 166-19 CAUSING DIVERSION TO DEN. FOUND AFT ROLLER OF FO WINDOW OUT OF ADJUSTMENT. ADJUSTED FO WINDOW AFT ROLLER PRESSURIZED A/C WITH NO NOTED PROBLEMS. NO REPEATS SINCE ORIGINAL.

Part: TARGET — LOOSE (EMERGENCY EXIT) · airframe 46,335 hrs · 16,619 cycles

L AFT EMER EXIT DISPLAYED ON UPPER ECAM SCREEN, DOOR. FOUND PROX TARGET LOOSE UPON INSPECTION, RE-SECURED TARGET.

Part: LIGHT — NO TEST (ROWS 9 & 18) · airframe 46,190 hrs · 16,569 cycles

EMERGENCY AISLE LIGHTS AT SEAT ROWS 9&18 NOT ILLUMINATING ON TEST. DISCONNECTED CONNECTOR UNDER SEAT 9A. SECURED CONNECTOR AND RELAMPED THE LIGHT FIXTURE.

Part: GIRT BAR — DIRTY (AFT LT DOOR) · airframe 45,265 hrs · 16,235 cycles

AFT LEFT DOOR WILL NOT ARM. [06-26-07] CLEANED DEBRIS FROM GIRT BAR AREA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,182 hrs · 16,205 cycles

SEATS 11C & 22C EEL LIGHTS HAVE 1 LAMP INOPERATIVE. [SUP 05-16-07] REPLACED LAMP. OPS GOOD.

Part: COVER — BROKEN (CABIN) · airframe 45,182 hrs · 16,205 cycles

SEAT 3C FWD EEL LAMP COVER BROKEN OFF. [SUP 05-16-07] REPLACED EEL LIGHT ASSY CRUSHED BY FOOD CARTS SUSPECTED, OPS GOOD.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 45,182 hrs · 16,205 cycles

2 RT DOOR UPPER EMERGENCY EXIT SIGN HAS 5 INOP LAMPS. [SUP 05-16-07] REPLACED LAMP.

Part: LIGHTER — INOPERATIVE (CABIN) · airframe 44,749 hrs · 16,028 cycles

THE 2L EXIT SIGN HAS 1 BULB, 2R EXIT SIGN HAS 4 BULBS & RIGHT OVERWING EXIT SIGN HAS 1 BULB INOPERATIVE. [5-1-07] REPLACED LAMPS OPS GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,749 hrs · 16,028 cycles

MIDSHIP OVERHEAD EXIT SIGN FWD SIDE HAS 1 BULB, AFT FACE HAS 3 BULBS & AFT BULKHEAD OVERHEAD EXIT SIGN HAS 1 BULB INOPERATIVE. [5-1-07] REPLACED LAMPS OPS GOOD.

Part: SEAL — MISINSTALLED (CARGO DOOR) · airframe 44,309 hrs · 15,859 cycles

FLIGHT DIVERTED DUE TO PRESSURIZATION PROBLEM. FOUND AFT CARGO DOOR SEAL INSTALLED INCORRECTLY. HOLES IN SEAL ARE NOT IN A POSITION TO LET THE AIR GET INTO THE SEAL. CORRECTLY INSTALLED AFT CARGO DOOR SEAL.

Part: ENGINE — SHUTDOWN (NR 2) · airframe 43,657 hrs · 15,648 cycles

RTBL WITH NR 2 ENGINE WOULD NOT STAY RUNNING. CREW REPORTED ENGINE SHUT DOWN TWICE. FOUND 10 STAGE VALVE FAILED OPERATIONAL CHECK. REPLACED 10TH STAGE BLEED VALVE. OPS CHECKS GOOD.

Part: ENGINE — FIRE (NR 1) · airframe 42,590 hrs · 15,258 cycles

ON SHUTDOWN NR 1 ENG HAD A TAILPIPE FIRE AROUND THE INNER TURBINE EXHAUST AREA.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 42,041 hrs · 15,064 cycles

EMERGENCY LIGHT TEST FAILED. REPLACED LEFT MID EMERGENCY BATTERY, OF THE EPSU. OPS CHECK GOOD.

Part: B-NUT — LEAKING (PARKING BREAKS) · airframe 39,402 hrs · 14,135 cycles

YELLOW HYDRAULIC SYSTEM PROBLEM IAD MM FOUND FLUID LEAKING AT BRAKE SHUTOFF VALVE 2579GM LOWER B-NUT FITTING. IAD MM REPLACED PARKING BRAKE SHUTOFF VALVE FIN 2579GM PER MM 32-45-14. NO LEAKS NOTED. SERVICED YELLOW HYD SYSTEM TO FULL.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 38,857 hrs · 13,951 cycles

ON CLIMB-OUT, NR 2 ENGINE COMPRESSOR STALLED. SHUT DOWN NR 2 ENGINE.

Part: SLIDE — FAILED (DOOR 2L) · airframe 38,681 hrs · 13,898 cycles

DURING SLIDE TEST DEPLOYMENT DOOR 2LH SLIDE INFLATION WAS NOT COMPLETE, SIDE WALLS WERE NOT FULL AND 5 OUT OF 6 POSTS DID NOT INFLATE. EVERYTIME A SLIDE DEFECT IS FOUND DURING THE MAINTENANCE OF SLIDE IN THE SHOP, A SHOP SDR IS ISSUED. HOWEVER DURING THE OVERHUAL OF THIS UNIT AFTER THIS SDR INCIDENT, THERE WAS NO SHOP SDR REPORTED TO SHOW ABNORMAL CONDITION OF THE SLIDE/RAFT. SEVERAL PROBABLE CAUSES COULD RESULT IN UNDER INFLATION. IT COULD BE DUE TO LOW BOTTLE PRESSURE BEFORE DEPLOYMENT OR PERHAPS THE ASPIRATOR MALFUNCTIONED OR MAYBE ASPIRATOR WAS PARTIALLY BLOCKED BY A FOREIGN OBJECT ON THE AIRCRAFT. NOT ENOUGH DATA TO PINPOINT THE PROBABLE CAUSE.

Part: LIGHT — INOPERATIVE (ROWS 12,13,14,18) · airframe 38,473 hrs · 13,826 cycles

CABIN EMERGENCY LIGHTS IN ROW 12-13-14 AND ROWS 18-19 AND 20 INOP.

Part: HOSE — OUT OF POSITION (ESCAPE SLIDE)

SLIDE HOSE WAS PACKED INTO ONE FOLD ON THE RIGHT FRONT CORNER. SLIDE ASSEMBLY PREVIOUSLY PACKED INCORRECTLY. REPACKED SLIDE TO SPECIFICATIONS.

Part: HYDRAULIC SYSTEM — INOPERATIVE (BLUE SYSTEM) · airframe 35,177 hrs · 12,748 cycles

RETURNED TO FIELD DUE TO LOSS OF BLUE SYSTEM HYDRAULICS. FOUND BLUE HYDRAULIC SYSTEM ELECTRIC PUMP PRESSURE FLEX LINE CHAFED. REPLACED CHAFED LINE AE707414-2. OPERATIONS CHECK NORMAL.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,300 hrs · 12,085 cycles

STRINGER 43L CORRODED BETWEEN FRAMES 56 AND 57. MAJOR REPAIR ACCOMPLISHED. REMOVED CORRODED STRINGER SECTION. FABRICATED & INSTALLED NESTED STRINGER SPLICE REPAIR PER SRM 53-0013 FIG 201.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 32,650 hrs · 11,854 cycles

RETURN TO FIELD DUE FWD CARGO SMOKE ECAM MESSAGE. REPLACED FORWARD CARGO DETECTOR AS FAULTED BY CENTRALIZED SMOKE DETECTOR CONTROL UNIT. OPERATIONS CHECK NORMAL.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 27,303 hrs · 9,738 cycles

RETURNED TO FIELD DUE TO CABIN PRESSURIZATION PROBLEM. UNABLE TO MAINTAIN CABIN PRESSURE IN AUTO OR MANUAL MODE. SKIN AIR OUTLET VALVE WAS DEACTIVATED AND SUBSEQUENTLY REPLACED.

Part: HARNESS — CHAFED (NR 2 ENGINE) · airframe 24,755 hrs · 8,796 cycles

NR 2 ENGINE EXHAUST GAS TEMPERATURE OVERTEMP INDICATION. SUPPLEMENTAL DATA UPDATE EXHAUST GAS TEMPERATURE (EGT) HARNESS EXHIBITED UNUSUAL PHYSICAL CHAFING. REPLACED THE EGT HARNESS.

Part: PAN — CRACKED (CABIN)

DURING FIRST HEAVY MAINT VISIT (HMV-1), ALL COACH SEATS IN PAX CABIN WERE FOUND WITH CRACKED SEAT PANS AT FWD ATTACH HOLES FOR SEAT PAN. THESE ARE RECARO 720 SERIES SEATS INSTALLED IN A320232. SEAT MFG DESIGNATES THE SEAT PAN AS PRIMARY STRUCTURE FOR SEAT. SEAT PANS ARE BEING REPLACED WITH NEW SEAT PANS WITH SAME DESIGN. THESE SEAT PANS WILL CRACK IN SAME PLACES DURING THEIR SERVICE LIFE. SUBMITTER STATED AD SHOULD BE ISSUED TO INSPECT THESE SEAT PANS FOR CRACKS EACH 90 DAYS, AND FOR REMOVAL FROM SERVICE OF ANY SEAT PANS THAT ARE CRACKED. THERE ARE 132 OF THESE SEAT PANS ON ACFT. THIS IS 8TH CONSECUTIVE A320232 THAT HAS EXHIBITED A 100 PERCENT FAILURE RATE OF THESE SEAT PANS THAT EQUALS 1,056 FAILURES.

Part: TUBE — FAILED (SLIDE/RAFT)

MR25612-016 SLIDE/RAFT TOP TUBE SEAM FAILED DURING PROOF TEST. MECHANIC WAS LOWERING PRESSURE IN TOP TUBE FROM 4.4 PSI TO 2.2 PSI. SEAM SEPARATED (6 FT) AT APPROXIMATELY 2.8 PSI.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO COMPT)

FORWARD CARGO SMOKE INDICATION ON UPPER ECAM FLASHED INTERMITTENTL, THEN CAME ON CONTINUOUSLY. DISCHARGED AGENT. RETURNED TO FIELD. *S/D* DEFECTIVE SMOKE DETECTOR COUPLED WITH OPEN GROUND 1999UT TERMINAL BLOCK. REPLACED SMOKE DETECTOR CONTROL UNIT AND SMOKE DETECTORS. CHECKED WIRING AND TEST FLEW A/C.

Part: SEAL — DAMAGED (NLG STRUT)

NOSE LANDING GEAR FAILED TO RETRACT. *S/D* NLG SHOCK ABSORBER WAS UNDER SERVICED RESULTING IN A PARTIAL COMPRESSION NEAR END OF RETRACTION CYCLE. THIS ACTION CAUSED THE S/A EXTENDED PROXIMITY SENSORS TO MOVE OUT OF POSITION RESULTING IN THE LGCIU COMMANDING THE NOSE GEAR TO EXTEND. REPLACED SHOCK ABSORBER AND FOUND DYNAMIC SEAL DAMAGED FOLLOWING DISASSEMBLY.

Part: SMOKE DET CONTL — MALFUNCTIONED (CARGO COMPT)

RECEIVED INTERMITTENT FORWARD CARGO PIT SMOKE ALARM. DISCHARGED AGENT 1 BOTTLE INTO FORWARD PIT. DIVERTED TO LAS UNDER AMBER ALERT. FOUND NO SMOKE OR FIRE IN CARGO PIT. *S/D* NORMAL DISCHARGE NOTED. CONFIRMED NO INDICATIONS OF FIRE OR SMOKE. NO LIVESTOCK OR FRUIT CARRIED IN PIT. FWD CARGO SMOKE WARNING, SMOKE DETECTOR CONTROL UNIT REPLACED. SMOKE DETECTOR CONTROL UNIT SENT TO VENDOR FOR ANALYSIS.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO COMPT)

FWD CARGO COMPARTMENT NR 1 FIRE BOTTLE DISCHARGED DURING FLIGHT DUE TO FALSE FIRE WARNING INDICATION. DIVERTED TO SYR AND ACCOMPLISHED A PRECAUTIONARY LANDING. *S/D* NORMAL DISCHARGE NOTED. CONFIRMED NO INDICATIONS OF FIRE OR SMOKE AND NO LIVESTOCK OR FRUIT. FWD CARGO SMOKE WARNING, SMOKE DETECTOR CONTROL UNIT REPLACED. SMOKE DETECTOR CONTROL UNIT SENT TO VENDOR FOR ANALYSIS.

Part: SMOKE DETECTOR — MALFUNCTIONED (E/E COMPT)

RECEIVED FWD CARGO SMOKE WARNING IN FLIGHT. DISCHARGED FWD FIRE BOTTLE. DIVERTED TO DEN AND ACCOMPLISHED A PRECAUTIONARY LANDING. *S/D* NORMAL DISCHARGE NOTED. CONFIRMED NO INDICATIONS OF FIRE OR SMOKE. FWD CARGO SMOKE WARNING, SMOKE DETECTOR CONTROL UNIT REPLACED. SMOKE DETECTOR CONTROL UNIT SENT TO VENDOR FOR ANALYSIS.

Part: CIRCUIT BREAKER — TRIPPED (CABIN)

EMERGENCY LIGHTS FAILED SYSTEM TEST. RESET CIRCUIT BREAKERS AND SYSTEM OPERATED NORMALLY.

Part: ACTUATOR — LEAKING (LT AILERON)

GREEN HYD SYSTEM QTY INDICATION APPROACHED YELLOW BAND, FLIGHT DIVERTED TO DEN. GEAR EXTENDED MANUALLY, LANDED WITHOUT INCIDENT. REPORTED LT INBOARD AILERON ACTUATOR HAD PIN HOLE HYD LEAK ON TOP OF ACTUATOR. REPLACED ACTUATOR.