N322US

Part: CONTROL VALVE — FAILED (NLG STEERING) · airframe 80,462 hrs · 36,611 cycles

EMERGENCY DECLARED FOR A NOSE WHEEL STEERING FAULT. REPLACED THE NOSE WHEEL STEERING SERVO CONTROL VALVE AND CONNECTOR 6GC IAW AMM. OPS AND LEAK CHECKED GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 80,308 hrs · 36,534 cycles

PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOWER FUSELAGE FRAME 72 TO FRAME 73, STR 24L TO 25L PER PRI 570056-14. COMPLIED WITH PRI/ERA 5700556-14 REV O.

Part: DAMPER — UNSERVICEABLE (CREW DOOR) · airframe 80,308 hrs · 36,534 cycles

CREW DOOR DAMPER 842, AFT GALLEY AREA, DOESN'T PASS CHECK. REMOVED AND REPLACED DOOR DAMPER AND EMERGENCY CYLINDER. CHECKS GOOD.

Part: SLIDE — DEFORMED (DOOR) · airframe 80,308 hrs · 36,534 cycles

SLIDE DEFORMATION PASSENGER CREW DOOR 832, AFT GALLEY AREA. REMOVED AND REPLACED SLIDE. CHECKS GOOD.

Part: ROD END — CORRODED (YAW DAMPER) · airframe 80,308 hrs · 36,534 cycles

CORROSION ON TRAILING EDGE ROD END OF YAW DAMPER. REMOVED, REPLACED AND FUNCTIONAL CHECK.

Part: WIRE — CUT (EVAC SLIDE) · airframe 80,195 hrs · 36,467 cycles

FOUND L2 SLIDE WIRES CUT. REMOVED AND REPLACED L2 DOOR SLIDE ASSEMBLY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 78,053 hrs · 35,475 cycles

EMERGENCY LIGHT FAILED, INT LOADS AFTL, EXT LOADS AFTL & BATTERY AFTL ILLUMINATED. REPLACED THE EPSU 13WL AND SLIDE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,196 hrs · 35,016 cycles

DURING A SERVICE CHECK, FOUND THE AFT LT BATTERY PACK FOR EMERGENCY LIGHTS INOPERATIVE, REPLACED THE BATTERY PACK.

Part: SKIN — NOT REPORTED (FUSELAGE) · airframe 82,899 hrs · 37,830 cycles

FUSELAGE SKIN AT GOGO WI-FI FWD ATG4 ANTENNA, FR 25 TO FR 26, S-43L TO S-42R; SECTION II PERMANENT REPAIR II PER ER/A 539169-14AD REV.B.

Part: VENT — CORRODED (FRAMES 69-70) · airframe 76,293 hrs · 34,621 cycles

LAVATORY VENT HAS CORROSION AND CRACK ON SKIN BETWEEN FR69 AND FR70, S31R AND S32R. SEE NR FOR ADDITIONAL INFORMATION 001-0001:2000-2001/001 00008 SEALED AND PAINTED AND CLOSED RT AFT BULKHEAD PANEL. REPAIRED IAW SRM 53-41-11.

Part: FITTING — DAMAGED · airframe 74,821 hrs · 33,898 cycles

DAMAGE ON RIGHT CRUCIFORM, REPAIRED IAW ER/A 548323-14AD REV A FOR WING CENTER CRUCIFORM FITTING.

Part: FRAME — DAMAGED (FRM 24) · airframe 74,821 hrs · 33,898 cycles

DAMAGE ON FRAME 24, STRINGER 6R ON THE AFT SIDE OF THE FRAME. CUTOUT DAMAGE AND REPAIRED IAW ERA 548700-14.

Part: BOX BEAM — NOT REPORTED (FRAME 43) · airframe 74,821 hrs · 33,898 cycles

CENTER FUSELAGE RT SIDE BOX BEAM AT FRAME 43 AND Y1650. COMPLY WITH ERA 548164-14AD.

Part: BOX BEAM — NOT REPORTED (FRAME 43) · airframe 74,821 hrs · 33,898 cycles

CENTER FUSELAGE LT SIDE BOX BEAM AT FRAME 43 AND Y1650. COMPLY WITH ERA 548129-14AD.

Part: FRAME — CRACKED (FRM 16) · airframe 74,821 hrs · 33,898 cycles

CRACK INDICATIONS AT FRAME 16. COMPLIED WITH FINAL ERA 548219-14AD REV ORIGINAL.

Part: STRINGER — CORRODED (FRAMES 33-37) · airframe 75,756 hrs · 34,392 cycles

CORROSION WAS FOUND ON STRINGER 43L BETWEEN FRAMES 33 AND 34. CORROSION WAS CUTOUT AND REPAIRED IAW SRM.

Part: STRINGER — CORRODED (FRAMES 33-34) · airframe 75,756 hrs · 34,392 cycles

CORROSION WAS FOUND ON STRINGER 43L BETWEEN FRAMES 33 AND 34. CORROSION WAS CUTOUT AND REPAIRED IAW SRM.

Part: SKIN — DAMAGED (FRAME 64) · airframe 74,821 hrs · 33,898 cycles

SKIN MISDRILLED THRU STRINGER FRAME 64 STRINGER 10L. REPAIRED THE SKIN IAW SRM 53-00-11 FIG. 239, PARA 4.W. AND REPAIRED STRINGER IAW SRM 53-00-13 FIG 203 PAR 4.A

Part: SKIN — DAMAGED (FRAMES 25-26) · airframe 72,550 hrs · 32,799 cycles

EVIDENCE OF DAMAGE TO LOWER FWD SKIN BETWEEN FRAMES 25-26 AND STRINGERS 44-43R PRI/ERA ISSUED 539169-14 REV 0 REV 1 REV 2 REV 3. C/W PRI/ERA 539169-14 REV 0,1,2 AND 3.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 70,492 hrs · 31,803 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT AT SEAT 6C INOPERATIVE. FOUND BOTH WIRES PULLED OUT OF LIGHT ASSY IN SEAT. REPAIRED BROKEN WIRES AND FUNCTIONAL CHECKED NORMAL.

Part: LIGHT — MISSING (ROW 20) · airframe 69,593 hrs · 31,379 cycles

DURING INSPECTION, FOUND EMERGENCY EXIT ROW LIGHT AT 20 RT MISSING AT SEAT. MAINTENANCE REPLACED SEAT EMEGENCY LIGHT ASSY AND REPAIRED WIRING. FUNCTIONAL CHECKED NORMAL.

Part: STRINGER SPLICE — CORRODED (FRAMES 28-31) · airframe 69,337 hrs · 31,256 cycles

CORROSION ON STRINGER SPLICE 42R IN FWD CARGO BAY BETWEEN FRAMES 28 - 31. REPLACED STRINGER SPLICE IAW SRM 51-42-11, 51-72-11, DWG D53231248200, ERA 528125-14, ORIGINAL REVISION AND PRI 528125-14 REV 0.

Part: DOOR SILL — CORRODED (L1) · airframe 69,337 hrs · 31,256 cycles

CORROSION ON LOWER L1 DOOR SILL BETWEEN FRAMES 16 - 20. REPLACED LOWER L1 DOOR SILL IAW SRM 51-72-11 AND DWG D53110339.

Part: STRINGER — CORRODED (FRAMES 65-66) · airframe 69,337 hrs · 31,256 cycles

CORROSION ON STRINGER 33L BETWEEN FRAMES 65 - 66. REPAIRED STRINGER IAW SRM 53-00-13 PARAGRAPH 4A, FIG 201, SHEET 2, 3, 4 AND 5, PAGES 202-218.

Part: PLATE — CORRODED (FRAME 20) · airframe 69,337 hrs · 31,256 cycles

AFTER REMOVING LOWER CORNER FITTING PERFORMED VISUAL INSPECTION AND FOUND CORROSION ON REINFORCEMENT PLATE FRAME 20 STRINGER 23L. REPLACED LOWER REINFORCEMENT PLATE AND FASTENER IAW SRM 51-72-11 AND ENGINEERING REPAIR AUTHORIZATION, 527501-14, REV ORIGINAL AND PRI NR 527501-14, REV 0.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 69,337 hrs · 31,256 cycles

DURING M2-CHECK, A CRACK WAS FOUND ON THE FRAME SECTION AT LT SLIDING WINDOW IAW ALI 53-11-35-PB6. REPAIRED IAW ER/A 527498-14AD, REV ORIGINAL.

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-20) · airframe 69,337 hrs · 31,256 cycles

CORROSION ON FLOOR SUPPORT BETWEEN FRAME 16 AND 20 Y-254. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND ENGINEERING REPAIR , AUTHORIZATION N 527502-14, REV: ORIGINAL.

Part: FRAME — CORRODED (FR 20) · airframe 69,337 hrs · 31,256 cycles

CORROSION ON FWD FACE LATERAL FRAME 20 STRINGER 23R. PERFORMED TIME LIMITED REPAIR ON FWD FACE LATERAL FRAME 20 LOCATED FWD PASSENGER ENTRY DOOR LEVEL STR 23 RT INTERNAL STRUCTURE IAW ER/A 527494-14, REVISION ORIGINAL AND PRELIMINARY REPAIR INSTRUCTIONS 527494-14, REVISION O; SECTION II.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · airframe 69,337 hrs · 31,256 cycles

CORROSION ON LOWER SILL IN AFT PAX CABIN LOCATED BETWEEN FRAMES 66 AND 68 AT STRINGER 23R. REPLACED LOWER SILL IN AFT PAX CABIN LOCATED BETWEEN FR 66-FR 68 AT LEVEL STR 23R IAW SRM 51-72-11 AND DWG D53480019; JOB COMPLETE.

Part: FITTING — CORRODED (FRAMES 16-20) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING, FWD OF LEFT PASSENGER ENTRY DOOR, BETWEEN FRAMES 16 - 20. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG D53112109.

Part: FITTING — CORRODED (FRAME 16) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER CORNER ON FWD LEFT PASSENGER DOOR AT FRAME 16, STINGER 23. REPLACED LOWER CORNER IAW SRM 51-72-11 AND DWG D53112109;

Part: STRUCTURE — CORRODED (FRAME 20) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER CORNER LOCATED FWD OF LEFT PASSENGER ENTRY DOOR AT FRAME 20, STRINGER 23L. REPLACED LOWER CORNER STRUCTURE IAW SRM 51-72-11 AND DWG 53112109.

Part: SEAT TRACK — CORRODED (FRAMES 64-66) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y-1292, BETWEEN FRAMES 64 - 66+5". REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (BS 66-67) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-67) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CRACK ON FWD LOAD TRANSMITTING ANGLE LOCATION INTERNAL AREA EMERGENCY DOOR 844. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522 79010.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CRACK ON FWD LOAD TRANSMITTING ANGLE LOCATION INTERNAL AREA EMERGENCY DOOR 834. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D52279010.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CRACK ON AFT LOAD TRANSMITTING ANGLE LOCATED INTERNAL AREA EMERGENCY DOOR 844. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522-79010.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-67) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-464.5 LOCATED BETWEEN FRAMES 64 - 67+10. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534 72305.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CRACK ON FWD LOAD TRANSMITTING ANGLE INTERNAL AREA EMERGENCY DOOR 843. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522 79010.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CRACK ON AFT LOAD TRANSMITTING PROFILE LOCATED INTERNAL AREA EMERGENCY DOOR 833. REPLACED SEGMENT ANGLE LOCATED ON INTERNAL AREA EMERGENCY DOOR AFT POSITION IAW SRM 51-72-11 AND DWG D522 79010.

Part: STRINGER — CORRODED (FRAMES 33-34) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 42L IN FWD CARGO BAY BETWEEN FRAMES 33 - 34. REPLACED STRINGER IAW SRM 51-72-11 AND DWG D53231212.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CRACK ON AFT LOAD TRANSMITTING ANGLE INTERNAL AREA EMERGENCY DOOR 843. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522-79010.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-70) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y512 BETWEEN FRAMES 64 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: STRINGER — CORRODED (BS 32-34) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 43L IN FWD CARGO BAY BETWEEN FRAMES 32 - 34. REPLACED THE STRINGER IAW SRM 51-72-11 AND DWG D53231626.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1162 BETWEEN FRAMES 67+15 - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CRACK ON FWD LOAD TRANSMITTING ANGLE LOCATED INTERNAL AREA EMERGENCY EXIT DOOR 833. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522-79010.

Part: CLEAT — CORRODED (FRAME 33) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT AT FRAME 33 AND BETWEEN STR 40L TO STR 41L MEASURES APPROXIMATELY L=0.110", W=0.105", D=0.002" SSI 532180. REPLACED CLEAT AND FASTENERS LOCATED IN FWD CARGO COMPARTMENT AT FR 33 AND BETWEEN STR 40L TO STR 41L IAW SRM A320 51-72-11 AND DWG D532 30337; D532 31212.

Part: SEAT TRACK — CORRODED (FRAMES 64-66) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y-765 BETWEEN FRAMES 64 - 66. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-765 BETWEEN FRAMES 66 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DG D53472000.

Part: CLEAT — CORRODED (FWD CARGO) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT LOG AT FR 34 AND BETWEEN STR 43L TO STR 44 REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231212.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-70) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-464.5 BETWEEN FRAMES 67+10 - 70 . REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472400.

Part: CLEAT — CORRODED (FRAME 30) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT AT FR 30 AND BETWEEN STR 40R TO STR 41R MEASURES 532180. REPLACED CLEAT IN FWD CARGO COMPARTMENT AT FRAME 30 AND BETWEEN STR 40R TO STR 41R IAW SRM A320 51-72-11 AND DWG D53231582.

Part: CARGO TRACK — CORRODED (FRAME 33) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT AT FR 33 AND BETWEEN STRG 41L TO STRG 42L REPLACED CLEAF IN FWD IAW SRM 51-72-11 AND DWG D53231212, D53230337.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER CORNER LOCATED FWD PASSENGER ENTRY DOOR RT AT FRAME 20 STR 23 INTERNAL STRUCTURE. REPLACED LOWER CORNER OF FWD PASSENGER ENTRY DOOR IAW SRM 51-72-11 AND DWG NRD53112109.

Part: STRUCTURE — CORRODED (DOOR FRAME) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON AFT PAX DOOR CUTOUT LOWER CORNER BETWEEN, STRINGERS 22 - 23L FRAME 68. REPLACED DOOR CUTOUT LOWER CONER IAW SRM 51-72-11 AND DWG D53480505.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-70) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-160.5, BETWEEN FRAMES 68 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: FITTING — CORRODED (FRAMES 66-68) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FRAMES 66 - 68 AND STRINGER 23R. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG D53480505.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER CORNER LOCATED FWD PASSENGER ENTRY DOOR RT AT FRAME 16, LEVEL STR23, INTERNAL STRUCTURE WITH MEASUREMENT OF L=0.500", W=0.238" AND D=0.003" APPROXIMATELY, SSI 531163. REPLACED LOWER CORNER LOCATED FWD PASSENGER ENTRY DOOR RT AT FRAME 16, LEVEL STR 23 INTERNAL STRUCTURE IAW SRM 51-72-11 AND DWG NR D53112109.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER CORNER LOCATED FWD PASSENGER ENTRY DOOR RT AT FRAME 16, LEVEL STR23, INTERNAL STRUCTURE WITH MEASUREMENT OF L=0.500", W= 0.238" AND D=0.003" APPROXIMATELY, SSI 531163. REPLACED LOWER CORNER LOCATED FWD PASSENGER ENTRY DOOR RT AT FRAME 16, LEVEL STR 23 INTERNAL STRUCTURE IAW SRM 51-72-11 AND DWG NR D53112109.

Part: SEAT TRACK — CORRODED (FRAMES 64-66) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y765 LOCATED BETWEEN FRAME 64 - 66. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG NR D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT AT FRAME 20, Y-1292 . REPLACED FLOOR SUPPORT FRAMES 12 - 24 IAW SRM 51-72-11 AND DWG D53112812.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT FRAME 20, Y-765. REPLACED FLOOR SUPPORT BETWEEN FRAMES 12 - 24 IAW SRM 51-72-11 AND DWG D53112812.

Part: STRINGER — CORRODED (FRAMES 33-34) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 43L BETWEEN FRAMES 33 - 34. REPLACED STRINGER.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1162 LOCATED BETWEEN FRAMES 67+17 - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 67) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON UPPER SPLICE INBD SIDE Y1162 AT FRAME 67+17. REPLACED UPPER SPLICE IAW SRM 51-72-11 AND DWG D53472000.

Part: STRINGER — CORRODED (FRAMES 32-33) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 43L BETWEEN FRAMES 32 - 33. REPLACED STRINGER.

Part: FLOOR SUPPORT — CORRODED (FRAMES 20-23) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 20 - 23 Y-189. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112834.

Part: COVER — CORRODED (FRAME 14) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON JOINT COVER IN FWD PAX CABIN AT FRAME 14 Y-1.234. REPLACED JOINT COVER IAW SRM 51-72-11, DWG D53112619, D53110984 AND D53112829.

Part: CLEAT — CORRODED (FRAME 30) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY FRAME 30 BETWEEN STRINGERS 41 - 42R. REPLACED CLEAT IAW SRM 51-72-11, DWGS D532-31582 AND S532-30320.

Part: CLEAT — CORRODED (FRAME 29) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY AT FRAME 29 BETWEEN STRINGERS 42-43L. REPLACED CLEAT IAW 51-72-11, DWGS D532 31212 AND D532 30319.

Part: CLEAT — CORRODED (FRAME 33) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY AT FRAME 33 AND BETWEEN STRINGERS 43-44R. REPLACED THE CLEAT IAW SRM 51-72-11, DWG D532 31212 AND D532 30337.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y765 BETWEEN FRAMES 66 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534 72000.

Part: CLEAT — CORRODED (FRAME 32) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY AT FRAME 32 BETWEEN STRINGERS 42-43R. REPLACED THE CLEAT IAW SRM 51-72-11, DWGS D532 31212 AND D532 31486.

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-21) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 16 - 21 Y254. REPLACED FLOOR SUPPORT IAW SRM 51-72-11, DWGS D53112816 , D53110422 , & D53110984.

Part: WEB — CORRODED (FRAMES 69-70) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON WEB BETWEEN FRAMES 69-70 STR 23R IN AFT PAX CABIN. REPLACED WEB IAW SRM 51-72-11 AND DWG D534 70100.

Part: WEB — CORRODED (FRAMES 69-70) · airframe 69,337 hrs · 31,256 cycles

DURING INSPECTION, FOUND CORROSION ON WEB LOCATED BETWEEN FRAMES 69-70 STR 23L IN AFT PAX CABIN. REPLACED WEB IAW SRM 51-72-11 AND DWG D53470100.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 64,787 hrs · 28,945 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY POWER SUPPLY 11WL BATTERY FAULTED. MX REPLACED BATTERY PACK AT 11WL AND FUNCTIONAL CHECK WAS NORMAL.

Part: EPSU — INOPERATIVE (CABIN) · airframe 5,278 hrs · 2,297 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT TEST FAILED ON TEST. MAINTENANCE REPLACED EPSU AT 11WL AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: EPSU — FAILED (CABIN) · airframe 60,589 hrs · 26,949 cycles

DURING NON ROUTINE CHECK, FOUND THE EMERGENCY EPSU AT AFT LEFT FAILED TEST. MAINTENANCE REPLACED EPSU AND UNIT TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,955 hrs · 25,794 cycles

DURING L-CHECK FOUND CORROSION ON SKIN BETWEEN FR 20 - FR 21 STRINGER 44. REPAIRED PER ERA 4844923-14.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,956 hrs · 25,794 cycles

FUSELAGE LOWER SKIN FR 20/21 STR 44 CORROSION REPAIR PER ERA484923-14 REPAIR PER SECTION I IS TIME LIMITED FOR DAMAGE TOLERANCE ANLYSIS. ASSOCIATED ER/A 13-484923 ADDED FOR AC 3222 ERA 484923-14 HAS BEEN REVISED TO REV A. SECTION II HAS BEEN DELETED. SECTION I IS A PERMANENT REPAIR. CLOSED LOG REMOVED MONITORS. PER S/O 01APR11 LOG COMMENTS ABOVE VIS: Y LRU: 32-2000-9-0001 SER: 03222 MON, 32 REP, COMPLETED 28FEB11 LAX MON, 32 L/L, 0277278; VIS; DTA; ERA484923II; FSLG; 3222 20-0553-8-3581 03222

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 57,955 hrs · 25,794 cycles

DURING L-CHECK FOUND AFT CARGO FLOOR PANEL 151 DF HAD UPPER SURFACE EXPOSED HONEYCOMB. REPLACED FLOOR PANEL IAW DWG 3D25-37705 & AMM 53-42-14-400-001.

Part: FLOOR PANEL — DEFORMED (CARGO BAY) · airframe 57,955 hrs · 25,794 cycles

DURING L-CHECK FOUND FWD CARGO FLOOR PANEL 131EF DEFORMED, PUNCTURED AND PREVIOUS REPAIR. REPLACED FLOOR PANEL IAW AMM 52-22-14-000-001 & DWG 3D25-37705.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 57,955 hrs · 25,794 cycles

DURING L-CHECK FOUND DELAMINATION ON FORWARD CARGO FLOOR PANEL 131AF. REPLACED FLOOR PANEL PER DWG 3D2537705 & AMM 53-22-14-400-001.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 57,955 hrs · 25,794 cycles

DURING L-CHECK FOUND DELAMINATION ON FORWARD CARGO FLOOR PANEL 131HF. REPLACED FLOOR PANEL PER DWG 3D2577705 & AMM 53-22-14-400-001.

Part: A/C PACK — MALFUNCTIONED (NR 2) · airframe 57,689 hrs · 25,683 cycles

ENROUTE, CREW RECEIVED AN ECAM "AIR PACK 2 FAULT" WITH PACK 1 ALREADY ON MEL, FOLLOWED QRH PROCEDURES DONNED MASK AND DECLARED AN EMERGENCY FOR RAPID DESCENT TO 10,000 FT. DURING DESCENT PACK 2 RECOVERED & CABIN ALTITUDE HAD REACHED 7,000, PASSENGER MASKS DID NOT DEPLOY. ACFT DIVERTED AND LANDING WAS UNEVENTFUL. PACK 2 HAD COMPRESSOR OVERHEAT TEMPERATURE SENSOR REPLACED AND PACK 1 HAD THE FLOW CONTROL VALVE REPLACED AND TESTS OK.

Part: DOOR — MISSING (MLG) · airframe 56,925 hrs · 25,357 cycles

DURING GROUND INSPECTION FOUND MLG RIGHT SECONDARY HINGED AND FIXED DOOR MISSING. REPLACED SECONDARY DOOR PER SRM 32-12-13 AND FIXED DOOR PER SRM 32-12-14 PAGE 401.

Part: CONTROL UNIT — MALFUNCTIONED (NR 1 & 2) · airframe 45,189 hrs · 20,008 cycles

AT LIFT-OFF, NOSE LOUD & VIBRATING AS GEAR WAS RAISED. ALL GEAR THEN INDICATED UP & LOCKED. ABOUT 1 MINUTE LATER NOSE GEAR HAD AN UNCOMMANDED EXTENSION AT 8300 FT, 220 KNOTS. CYCLED LANDING GEAR PER COM PROCEDURE, WITH LANDING GEAR INDICATING 3 DOWN-AND-LOCKED, FOLLOWED BY 3 UP-AND-LOCKED. -L/G SYS DISAGREE- FAULT REMAINED ON ECAM. PRIOR TO LANDING CREW DECLARED EMERGENCY, WITH UNEVENTFUL LANDING AND TAXI TO GATE. DISCREPANCY CORRECTED BY CHECK OF RIGGING OF NOSE GEAR DOOR UPLOCK AND NOSE GEAR UPLOCK. REPLACED LGCIU NR 1 AND NR 2 AND REMOVED LARGE AMOUNTS OF GREASE FROM UPLOCK TARGETS. SEVERAL EXTENSION/RETRACTION CYCLES PERFORMED, SYSTEM CHECKED GOOD. LGCIUS 32-3266-9-0001, S/N 11588, 02417 REMOVED.

Part: HOSE — RUPTURED (LEFT MLG DOOR) · airframe 28,812 hrs · 12,648 cycles

DURING CLIMB AFTER LANDING GEAR AND FLAP RETRACITON, RECEIVED HYD G RSVR LO LVL MESSAGE. PER COM PROCEDURES, SHUT OFF THE GREEN HYDRAULIC SYSTEM PUMPS, GRAVITY EXTENDED LANDING GEAR ON APPROACH TO FINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RUPTURED LEFT MAIN GEAR DOOR ACTUATOR FLEX HOSE. OPERATIONAL CHECK OK.

Part: BATTERY — DISCHARGED (CABIN)

DURING LINE MAINTENANCE TEST OF THE EMERGENCY LIGHTING SYSTEM, RECEIVED EPSU COMM EMER LIGHT AND EPSU BATT EMER LIGHT MESSAGES. REPLACED BATTERY PACK AT DOOR 1L, OPERATIONAL CHECK OK.

Part: BATTERY PACK — DUSCHARGED (CABIN)

DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS FAILED THE SYSTEM TEST. REPLACED EPSU AND BATTERY PACK, OPERATIONAL CHECK OK.

Part: LGCIU — INOPERATIVE (COCKPIT)

DURING CLIMBOUT, THE LANDING GEAR WOULD NOT RETRACT ACCOMPANIED BY LGCIU 1 FAULT AND WHEEL NOSE WHEEL STEERING FAULT. CYCLED LANDING GEAR HANDLE, GEAR RETRACTED NORMALLY. CYCLED ANTI-SKID SWITCH AND NOSE WHEEL STEERING FAULT EXTINGUISHED. LGCIU 1 FAULT REMAINED. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 LGCIU, OPERATIONAL CHECK OK.

Part: LGCIU — MALFUNCTION (COCKPIT)

DURING CLIMBOUT, RECEIVED L/G LGCIU 1 FAULT WHILE ATTEMPTING TO RETRACT LANDING GEAR. CYCLED LANDING GEAR HANDLE TO RETRACT LANDING GEAR. ALL INDICAITONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT AT ORIGINAL DESTINATION. MAINTENANCE REPLACED THE NR 1 LGCIU, OPERATIONAL CHECK OK.

Part: FLOORBEAM — CORRODED (BS 8077)

DURING 1L CHECK, FOUND CORROSION ON THE FRAME 20 FLOORBEAM AT RBL 1640. REPAIRED BEAM (P/N D53112785201) PER EA 32-106167.

Part: POWER SUPPLY — DISCHARGED (CABIN)

DURING LINE MAINTENANCE, THE CABIN INTERCOMMUNICATION DATA SYSTEM FAULTED THE LEFT AFT EMERGENCY POWER SUPPLY UNIT. REPLACED EPSU. OPERATIONAL CHECK OK.

Part: ROD ENDS — WORN (ELEVATOR SERVO)

CLIMBING THROUGH 15,000 FEET AT 290 KNOTS, EXPERIENCED AIRFRAME VIBRATION MOST NOTICEABLEY IN THE AFT CABIN. REDUCING SPEED REDUCED VIBTATION. AIRCRAFT RETURNED TO MSP UNDER DIRECTION OF MAINTENANCE CONTROL AND DISPATCH AND ACCOMPLISHED AN UNEVENTFUL LANDING. MAINTENANCE REPLACED FOUR ELEVATOR SERVO CONTROL ROD ENDS.

Part: FLUSH CONTL UNIT — MALFUNCTIONED (FWD LAV)

DURING CRUISE, THE FORWARD LAVATORY TOILET OVERFLOWED SPILLING FLUID INTO THE FIRST CLASS CABIN. AIRCRAFT DIVERTED TO DFW AND LANDED WITHOUT INCIDENT. THE FORWARD LAV WAS PLACED ON MEL AND THE FLUSH CONTROL UNIT LATER WAS REPLACED, OPERATIONAL CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS BATTERY TEST FAILED EMER L AND EMER R POSITIONS. REPLACED THE BATTERY PACKS AT FORWARD LEFT AND MIDDLE LEFT POSITIONS. OPERATIONAL CHECK OK.

Part: FLAP INDICATION — MALFUNCTIONED (TE FLAPS)

DURING APPROACH INTO LAS, RECEIVED 'F/CTL FLAPS LOCKED' ALIGNMENT FAULT, WHEN SELECTING FLAPS 2 POSITION. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES. AIRCRAFT OK FOR SERVICE.