N943FR

Part: TIP CAP — DAMAGED (RT WING) · airframe 54,830 hrs · 23,689 cycles

03/05/2020 SUPPLEMENT: REMOVED DAMAGED R/H WING TIP AND INSTALLED SERVICEABLE R/H WINGTIP IAW AMM 57-31-21-PB401. REMOVED PN D5735052101951A, SN 13572. REMOVED AND REPLACED R/H WINGTIP FENCH IAW AMM 57-31-22-PB401, PN D5735120000300A. SIGNIFICANT DAMAGE TO RH WING TIP & LEADING EDGE.  LOCAL MX SEPARATING AND MOVING OFF GATE TO BEGIN DAMAGE EVALUATION.  SETTING UP FIELD TRIP WITH DEN INSP, ENGINEER, AND AOG BUYER WITH 1133 ETA 2/16 SIGNIFICANT DAMAGE TO RH WING TIP & LEADING EDGE.  LOCAL MX SEPARATING AND MOVING OFF GATE TO BEGIN DAMAGE EVALUATION.  SETTING UP FIELD TRIP WITH DEN INSP, ENGINEER, AND AOG BUYER WITH 1133 ETA 2/16

Part: FITTING — CRACKED (FRM 16) · airframe 54,655 hrs · 23,583 cycles

LOWER AFT FASTENER HOLE ON L/H FRAME 16 UPPER DOUBLE JOGGLE SHOWS CRACK INDICATIONS. REPAIRED L1 DOOR FRAME 16 UPPER DOUBLER JOGGLE HOLE 'D' IAW REPAIR DRAWING R53113041 (ISSUE E). REPAIR INSPECTION THRESHOLD 6800 FC WITH INTERVALS OF 4129 FC PER RDAS.

Part: PIPE — CRACKED (NR 1 ENGINE) · airframe 53,629 hrs · 23,021 cycles

DISCREPENCY: PIPE P/N D2621012400400, CRACKED FIRE BOTTLE DISCHARGE LINE, NUMBER 1 ENGINE PYLON. REFERENCE IPC 26-21-06-01D ITEM 310. CORRECTIVE ACTION: REMOVED AND REPLACED PIPE NUMBER 1 ENGINE FIRE BOTTLE TUBE. PERFORMED LEAK CHECK AMM 26-21-49-400-002-A. GUAGE #F9TAB6174C DUE 07/20.

Part: GENERATOR — LEAKING (APU) · airframe 50,596 hrs · 21,518 cycles

DISCREPANCY: REFERENCE LOG PAGE LP1090541 ITEM 1, IMMEDIATELY UPON TURNING ON APU BLEEN AND PACKS 1 AND 2, WE NOTICED AN OILY MUSTY SMELL ON FLIGHT DECK. ONE MINUTE LATER FLIGHT ATTENDANTS IN BACK CALLED TO INFORM US OF ODOR IN BACK OF AIRCRAFT, TRIED TO ISOLATE WHICH PACK, COULD NOT TELL. CORRECTIVE ACTION: REFERENCE LOG PAGE LP 1090541 ITEM 1, PLACED APU ON MEL 49-10-01A. CONTROL # 1144098. DEAD DATE 11/05/18. COMPLIED WITH MEL PROCEDURES. APU IS DEACTIVATED. AMM 49-10-00-040-008-A. REFERENCE LOG PAGE LP1090541 ITEM 2, PERFORMED BSI OF APU S/N P-4745 LOAD COMPRESSOR DIFFUSER AND LOAD COMPRESSOR IMPELLER TRAILING EDGES, NO OIL WETTING IN THESE AREAS REFERENCE STEPS 4.A. AND 4.B. AMM 49-20-00-200-003-A. REFERENCE LOG PAGE LP1090543 ITEM 2, REFERENCE TECH SERVICES WORK SCOPE DATED 10/17/2018. REMOVED AND REPLACED APU GENERATOR DUE TO EVIDENCE OF OIL LEAKING FROM AROUND GENERATOR PERFORMED OPS/LEAK CHECK OF APU GENERATOR, OPS/LEAK CHECK GOOD. AMM 49-42-51 PB401. REFERENCE LOG PAGE LP1090543 ITEM 3, TECH WORK SCOPE NOT REQUIRED DUE TO APU REPLACEMENT. SEE LP 1090544 ITEM 2, DUE TO EVIDENCE OF APU LEAKING INTERNAL. REFERENCE LOG PAGE LP1090544 ITEM 2, REFERENCE MDDR 1144098. REMOVED AND REPLACED APU IAW WORK TASK CARD MP49111-01 AND MP49111-02, OPS AND LEAK CHECKED OK. TORQUE WRENCHES F9TAB2956C 10/18, F9TAB2944C 5/19. NO ODORS NOTED./END/

Part: POWER SUPPLY — FAILED (CABIN) · airframe 49,429 hrs · 20,954 cycles

EPSU 10WL FAILED EPSU TEST. REMOVED AND REPLACED EPSU ASSEMBLY 10WL IAW AMM 33-51-38 PAGE BLOCK 401. OPERATIONAL CHECK GOOD.

Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 47,976 hrs · 20,294 cycles

CORROSION ON FLOORBEAM -Y765 AT FRAME 66. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14-283-002. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, 51-72-11-911-001, AND 51-44-11.

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 47,976 hrs · 20,294 cycles

CORROSION ON FLOORBEAM -Y1162 BY FRAME 68. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11, SRM 53-00-14, AND SRM 51-44-11.

Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 47,976 hrs · 20,294 cycles

TWO AREAS OF CORROSION ON THE FLOORBEAM -Y1292 BY FRAME 66. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11, SRM 53-00-14, AND SRM 51-44-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,976 hrs · 20,294 cycles

2 AREAS OF CORROSION ON FLOORBEAM -Y765 BETWEEN FR66 AND FR68. REMOVED AND REPLACED FLOORBEAM AT -Y765 BETWEEN FR66 AND FR68 IAW SRM 51-42-11, 53-00-14-283-002, 51-72-911-001 AND 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 47,976 hrs · 20,294 cycles

THREE AREAS OF CORROSION ON THE FLOOR SUPPORT Y765 BETWEEN FRAMES 66 AND 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, 51-72-11-911-001, 53-00-14-283-002, AND 51-44-11.

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 47,976 hrs · 20,294 cycles

FLOORBEAM Y1292 HAS CORROSION AT FRAME 68. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14-283-002. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11-911-001, 51-42-11, AND 51-44-11.

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 47,976 hrs · 20,294 cycles

CORROSION ON THE FLOORBEAM Y1162, FRAME 68. THE FLOORBEAM WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14-283-002. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11, 51-44-11, AND 51-72-11-911-001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,976 hrs · 20,294 cycles

FLOORBEAM Y512 HAS CORROSION AT FR66. REFERENCE NR 1832N291, REMOVED AND REPLACED FLOORBEAM Y512 FR67-64 IAW SRM 51-72-11-911-001, 53-00-14-283-002 AND 51-44-11.

Part: SLIDE — FAILED (L1 DOOR) · airframe 40,370 hrs · 17,034 cycles

EMERGENCY POWER SUPPLY UNIT TEST FAILED FOR L1 DOOR SLIDE. R & R L1 DOOR SLIDE IAW AMM 25-62-44-000-012A & AMM 25-62-44-400-007A. OPERATIONAL CHECKED GOOD.

Part: SEAL — DAMAGED (NR 2 ENGINE) · airframe 40,187 hrs · 16,961 cycles

LOSS OF OIL QTY ON NR 2 ENG. QTY LESS THAN 2 PSI AT CRUISE. OIL PSI 0 ON APPROACH & LAND. OIL TEMP & PRESS WITH NR 2 ENG AT IDLE 28 PSI & 80 DEGREE C. TROUBLE SHOT, LEAK FOUND HYD PUMP PAD SEAL LEAKING. R & R SEAL ON THE HYD PUMP SHAFT IAW AMM 72-63-00-300-802A. INSTALLED HYD PUMP IAW AMM 29-31-51 PB401 CONF 6. OPERATIONS CHECK & LEAK CHECKED GOOD. TORQUE WRENCH F9TAB1100C DATE 10 16. REFERENCE LOG PAGE 962709.

Part: EPSU — FAILED (CABIN) · airframe 39,987 hrs · 16,880 cycles

EMERGENCY POWER SUPPLY UNIT SYS TEST FAILED, CODE 10WL FWD LT. R & R EPSU 10WL. OPERATIONS TESTED GOOD IAW AMM 33-51-38 PB 401. REFERENCE LP 967286.

Part: BATTERY — DISCHARGED (CABIN) · airframe 37,101 hrs · 15,583 cycles

EMERGENCY PATH LIGHTING BATTERY OF EPSU 10WL FAILED TEST DURING HEAVY SERVICE CHECK. R & R BATTERY OF EPSU 10WL. OPERATIONS CHECKED GOOD IAW AMM 33-51-38-000-002 & 33-51-38-400-002 LP 925756.

Part: APU — LEAKING (APU BAY) · airframe 50,596 hrs · 21,518 cycles

DISCREPANCY: REFERENCE LOG PAGE LP1090541 ITEM 1, IMMEDIATELY UPON TURNING ON APU BLEEN AND PACKS 1 AND 2, WE NOTICED AN OILY MUSTY SMELL ON FLIGHT DECK. ONE MINUTE LATER FLIGHT ATTENDANTS IN BACK CALLED TO INFORM US OF ODOR IN BACK OF AIRCRAFT, TRIED TO ISOLATE WHICH PACK, COULD NOT TELL. CORRECTIVE ACTION: REFERENCE LOG PAGE LP 1090541 ITEM 1, PLACED APU ON MEL 49-10-01A. CONTROL # 1144098. DEAD DATE 11/05/18. COMPLIED WITH MEL PROCEDURES. APU IS DEACTIVATED. AMM 49-10-00-040-008-A. REFERENCE LOG PAGE LP1090541 ITEM 2, PERFORMED BSI OF APU S/N P-4745 LOAD COMPRESSOR DIFFUSER AND LOAD COMPRESSOR IMPELLER TRAILING EDGES, NO OIL WETTING IN THESE AREAS REFERENCE STEPS 4.A. AND 4.B. AMM 49-20-00-200-003-A. REFERENCE LOG PAGE LP1090543 ITEM 2, REFERENCE TECH SERVICES WORK SCOPE DATED 10/17/2018. REMOVED AND REPLACED APU GENERATOR DUE TO EVIDENCE OF OIL LEAKING FROM AROUND GENERATOR PERFORMED OPS/LEAK CHECK OF APU GENERATOR, OPS/LEAK CHECK GOOD. AMM 49-42-51 PB401. REFERENCE LOG PAGE LP1090543 ITEM 3, TECH WORK SCOPE NOT REQUIRED DUE TO APU REPLACEMENT. SEE LP 1090544 ITEM 2, DUE TO EVIDENCE OF APU LEAKING INTERNAL. REFERENCE LOG PAGE LP1090544 ITEM 2, REFERENCE MDDR 1144098. REMOVED AND REPLACED APU IAW WORK TASK CARD MP49111-01 AND MP49111-02, OPS AND LEAK CHECKED OK. TORQUE WRENCHES F9TAB2956C 10/18, F9TAB2944C 5/19. NO ODORS NOTED./END/

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,035 hrs · 14,627 cycles

AIRCRAFT DUE C 6 INSPECTION. DISCREPANCY, MAIN CABIN FLOORBEAM FRAME 68 Y1292 CORRODED TO 50% OF MATERIAL THICKNESS. R & R MAIN CABIN FLOORBEAM FRAME 68 Y1292 IAW SRM 51-42-11 PAR 5, 6 & 7 & SRM 51-49-00 TABLE 9. ACFT DUE OUT OF C CHECK SEPTEMBER 2, 2014.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 33,540 hrs · 13,982 cycles

WINDSHIELD CRACKED AT FL390, SEEMS TO BE OUTER PANE ONLY, NO FLUCTUATIONS IN PRESSURIZATION NOTED. R & R FIRST OFFICER`S WINDSHIELD IAW AMM 56-11-11-000-001 & AMM 56-11-11-400-001, OPERATIONS CHECKED GOOD. REPLACED WINDOW HEAT CONTROLLER SEE LOG PAGE 827954 ITEM 2.

Part: COMPUTER — MALFUNCTIONED (ZONE 200) · airframe 26,591 hrs · 10,959 cycles

ECAM ON DESCENT: CIDS 1 AND 2 FAULT WITH UNCOMMANDED EMERGENCY LIGHTS FLICKERING CABIN LIGHTS LOSS OF CABIN COMMUNICATIONS. THIS WAS INTERMITTENT FOR ONLY A FEW MINUTES THEN WENT BACK TO NORMAL. TROUBLESHOT REPLACED CIDS DIRECTOR IAW AMM 23-73·34PB 401. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 3,622 hrs · 1,575 cycles

AT 4000 FT AGL, F/A REPORTED A BURNING ODOR COMING FROM THE AFT LT LAV. TROUBLESHOT IAW TSM 24-00-00-810-823. NO DEFECTS NOTED. INSPECTED THE FOLLOWING AREAS, LAVATORY HOT WATER HEATERS, COFFEEMAKERS IN AFT GALLEY INCLUDING WIRING, LIVE TV COMPONENTS WHILE RUNNING APU AND ENGINES WITH PACKS AND WING ANTI-ICE VALVES ON.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,171 hrs · 9,470 cycles

C-CHECK: NON ROUTINE NR 33820; CABIN FLOOR SUPPORT FRAME 67-69, -Y1292 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-00-14, FIG 102 ALSO SRM 51-42-11 PARA 5 A, D AND 6 B 1-8.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,171 hrs · 9,470 cycles

C-CHECK: MAIN CABIN FRAME 66 -Y1500, AFT PASSENGER DOOR SILL BEAM HAS SURFACE CORROSION. REPARED DOOR SILL BEAM IAW SRM 53-41-14, FIG 201.

Part: SHEAR PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,171 hrs · 9,470 cycles

C-CHECK: NON ROUTINE NR 33802; LT SHEAR PLATE AT FRAME 69-70 HAS CORROSION ON THE UPPER SURFACE. REMOVED AND REPLACED AHEAR PLATE IAW EO A0-53EO-31434 AND SRM 51-42-11.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,171 hrs · 9,470 cycles

C-CHECK: CABIN FLOORBEAM AT FRAME 68, Y1292 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-00-14, FIG 102 ALSO SRM 51-42-11, PARA 5.

Part: SHEAR PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,171 hrs · 9,470 cycles

C-CHECK: NON ROUTINE NR 33801; RT SHEAR PLATE AT FRAME 69 - 70 HAS UPPER SURFACE CORROSION. REMOVED AND REPLACED SHEAR PLATE IAW EO A0-53EO-31-434 AND SRM 51-42-11.

Part: SILL — CORRODED (ZONE 200) · airframe 17,169 hrs · 7,064 cycles

REFERENCE NON ROUTINE C074186. DURING DEN C3 C-CHECK, INSPECTION NOTED CORROSION ON THE L2 DOOR SILL AT FRAME 66 IN FWD SPLICE AREA. MX PERFORMED MAJOR REPAIR IAW SRM 53-41-14, SRM 51-44-00, SRM 51-21-00 AND SRM 51-75-00.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 17,169 hrs · 7,064 cycles

REFERENCE NON ROUTINE C073981. DURING DEN C3 C-CHECK, INSP, NOTED CORROSION IN THE AFT CABIN AREA ON THE FLOOR SUPPORT Y1292 BETWEEN FRAME 66 AND FRAME 68. MX REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-14, SRM 51-42-11 AND SRM 51-44-11.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 17,169 hrs · 7,064 cycles

DURING DEN C3 C-CHECK, INSP NOTED CORROSION ON THE FLOORBEAM Y1162.5 AT FRAME 68. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 53-00-14, SRM 51-42-11, SRM 51-11-13, AND EA A9-53R-31489.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 17,169 hrs · 7,064 cycles

DURING DEN C3 C-CHECK, INSP NOTED CORROSION ON THE FLOOR SUPPORT Y1292 BETWEEN FRAME 64 AND FRAME 66. MX REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-14, SRM 51-42-11, SRM 51-11-13, SRM 51-44-11 AND AMM 20-28-00 PB 501.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 17,169 hrs · 7,064 cycles

REFERENCE NON ROUTINE C073982. DURING DEN C3 C-CHECK, INSP NOTED CORROSION ON FLOORBEAM LOCATED AT -Y1292 BETWEEN FRAME 67 AND FRAME 68. MX REPAIRED THE FLOORBEAM IAW SRM 51-73-11, SRM 51-44-11 AND EA A9-53R-31491.

Part: SAFETY VALVE — LEAKING (LANDING GEAR) · airframe 13,571 hrs · 5,580 cycles

PILOT RETURNED TO BLOCK DUE TO LOSS OF GREEN SYSTEM HYDRAULIC PRESSURE. MAINTENANCE REMOVED AND REPLACED LANDING GEAR SAFETY VALVE AND PERFORMED OPERATIONAL CHECK IAW A319 AMM 32-31-17 PB401 AND 32-31-00-710-005.

Part: TORSION BAR — OUT OF ADJUST (R2 DOOR) · airframe 11,969 hrs · 4,934 cycles

DURING C-CHECK, INSP NOTED THE R2 DOOR WOULD NOT ARM WITH DOOR CLOSED AND LOCKED. THIS OCCURRED DURING OPERATION OF THE DOOR WHILE PERFORMING TASK CARD C528002-2. MAINT ADJUSTED TORSION BAR AND PERFORMED OPS CHECK IAW AMM 52-11-21-400-001 AND TASK CARD C528002-2. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: HOOK — OUT OF ADJUST (R2 DOOR) · airframe 11,969 hrs · 4,934 cycles

DURING C-CHECK INSP, NOTED THE R2 DOOR INSIDE HANDLE CAN BE OPERATED WHILE DOOR IS NOT CLOSED. MAINT ADJUSTED THE R2 DOOR HOOK IAW AMM 52-11-21-400-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 11,969 hrs · 4,934 cycles

DURING C2 C-CHECK, INSPECTION NOTED THE TOP LAYER DELAMINATED ON FLOOR PANEL 251NF. MAINTENANCE REMOVED DELAMINATED LAYER AND APPLIED MYLAR PATCH IN ACCORDANCE WITH A319 SRM 53-02-00.

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 11,969 hrs · 4,934 cycles

DURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151DE WAS PUNCTURED. MAINTENANCE REPAIRED DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 11,969 hrs · 4,934 cycles

DURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151FE WAS PUNCTURED. MAINTENANCE REPAIRED DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 11,969 hrs · 4,934 cycles

DURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 161UG WAS PUNCTURED. MAINTENANCE RECORDED THAT THIS NON ROUTINE HAS THE PANEL NUMBER INCORRECTLY INDICATED. THE DAMAGED PANEL IS 151UG. MAINTENANCE REPAIRED DAMAGE TO PANEL 151UG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 11,969 hrs · 4,934 cycles

DURING C2 C-CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151BE WAS PUNCTURED. MAINTENANCE REPAIRED THE DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 11,969 hrs · 4,934 cycles

DURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151UG WAS PUNCTURED. MAINTENANCE RECORDED THAT THIS IS EITHER A DUPLICATE WRITE-UP (161UG- NON ROUTINE C047467) OR SHOULD HAVE BEEN WRITTEN AS 152UG, WHICH HAD DAMAGE ALSO. THE DAMAGE REPAIR FOR 152UG WAS PERFORMED IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 11,969 hrs · 4,934 cycles

DURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151AE WAS PUNCTURED. MAINTENANCE REPAIRED THE DAMAGE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)