N805FR

Part: BLANKING PLATE — CORRODED (ZONE 200) · airframe 20,693 hrs · 10,824 cycles

DURING DEN C4/S1 C-CHECK, INSP NOTED CORROSION ON THE L2 FWD GIRT BAR FITTING BLANKING PLATES. MX REMOVED AND REPLACED THE GIRT BAR BLANKING PLATES AND INSTALLED IAW WORK CARD C250001-3.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,693 hrs · 10,824 cycles

DURING DEN C4/S1 C-CHECK, INSP NOTED CORROSION ON THE LT PROFILE AT FRAME 56. MX REMOVED AND REPLACED THE PROFILE IAW SRM 51-42-11 AND 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 20,693 hrs · 10,824 cycles

REF NON ROUTINE C075817. DURING DEN C4/S1 C-CHECK, INSP NOTED CORROSION ON THE FLOORBEAM AT -Y1292 AND FRAME 20. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,693 hrs · 10,824 cycles

DURING DEN C4/S1 C-CHECK, INSP NOTED CORROSION IN THE AFT CARGO COMPARTMENT LOCATED AT FRAME 58 AND STRINGER 40R. MX BLENDED THE AREA IAW SRM 51-75-12 AND INSTALLED NEW PROFILE IAW SRM 51-42-11.

Part: SHEAR PLATE — CORRODED (ZONE 200) · airframe 20,693 hrs · 10,824 cycles

REF NON ROUTINE C075822. DURING DEN C4/S1 C-CHECK, INSP NOTED THE SHEAR PLATE LOCATED AT FRAMES 69-70 AND STA -Y1292 HAS CORROSION AROUND THE NUT PLATE HOLES. MX REMOVED AND REPLACED THE SHEAR PLATE IAW SRM 51-42-11 PARAGRAPHS 6 AND 14 AND STEP 4 OF EO A0-53EO-31434.

Part: SHEAR PLATE — CORRODED (ZONE 200) · airframe 20,693 hrs · 10,824 cycles

REF NON ROUTINE C075819. DURING DEN C4/S1 C-CHECK, INSP NOTED THE SHEAR PLATE LOCATED AT FRAMES 69-70 AND STA Y1292 HAS CORROSION AROUND THE NUT PLATE HOLES. MX REMOVED AND REPLACED THE SHEAR PLATE AND SHEAR SUPPORT IAW SRM 51-42-11 PARAGRAPHS 6, 7, 14 AND STEP 4 OF EO A0-53EO-31434.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 20,693 hrs · 10,824 cycles

DURING C4 S1 C-CHECK, INSP NOTED CORROSION ON FLOOR SUPPORT Y1292 FRAME 66 TO FRAME 68. MX REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11, SRM 53-41-14, SRM 51-44-11 AND SRM 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 20,693 hrs · 10,824 cycles

REF NON ROUTINE C075818. DURING DEN C4/S1 C-CHECK, INSP NOTED CORRODED NUT PLATE HOLES ON THE FLOORBEAM LOCATED AT FRAME 68 AND STA Y1292. MX REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, SRM 51-44-11 AND SRM 51-72-11.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 20,693 hrs · 10,824 cycles

REF NON ROUTINE C075806. DURING DEN C4/S1 C-CHECK, INSP NOTED CORROSION ON THE SEAT TRACK LOCATED AT FRAMES 64 TO 66 AND STA Y1292. MX REMOVED AND REPLACED SEAT TRACK IAW SRM 51-42-11, SRM 53-41-14, SRM 51-44-11, SRM 51-21-00, SRM 51-75-00 AND SRM 51-72-11.

Part: SILL — CORRODED (ZONE 200) · airframe 20,693 hrs · 10,824 cycles

DURING DEN C4/S1 C-CHECK, INSP NOTED CORROSION AT THE NUT CLIP HOLE AT FRAME 66 AND STA -Y1732. MX PERFORMED MAJOR REPAIR TO THE DOOR SEAL IAW SRM 53-41-14, SRM 51-75-12 AND SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 20,693 hrs · 10,824 cycles

REF NON ROUTINE C075821. DURING DEN C4/S1 C-CHECK, INSP NOTED CORROSION ON THE FLOOR SUPPORT NUT PLATE HOLES LOCATED AT FRAMES 68 TO 69 AND STA -Y1292. MX REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-44-11, AND SRM 51-23-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 20,693 hrs · 10,824 cycles

DURING C4 S1 C-CHECK, INSP NOTED CORROSION AT NUT PLATE HOLES ON Y1292 LT AT FRAME 68. MX REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, SRM 51-44-11 AND SRM 51-72-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,693 hrs · 10,824 cycles

REF NON ROUTINE C075679. DURING DEN C4/S1 C-CHECK, INSP NOTED CORRODED FASTENERS ON THE FLOORBEAM LOCATED AT FRAME 61 AND STR 40R. MX REMOVED AND REPLACED THE PROFILE IAW SRM 51-42-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,693 hrs · 10,824 cycles

DURING DEN C4/S1 C-CHECK, INSP NOTED CORROSION ON THE FLOORBEAM LOCATED IN THE AFT CARGO COMPARTMENT AT FRAME 60 AND STRINGER 40R. MX PERFORMED REPAIR IAW SRM 51-42-11, SRM 51-44-00, SRM 51-21-11, SRM 51-75-12 AND EA A8-53R-31553.

Part: FITTING — CORRODED (ZONE 100) · airframe 20,693 hrs · 10,824 cycles

REF NON ROUTINE C075703. DURING C4 S1 CHECK, INSP NOTED THE SUPPORT FITTING IN THE AFT CARGO COMPARTMENT AT FRAME 60 STR 43 RT HAS CORROSION AT THE NUT PLATE HOLE. MX REMOVED AND REPLACED THE FITTING IAW SRM 51-74-00, SRM 51-74-00, SRM 51-42-11 AND SRM 51-44-11.

Part: RIB — CORRODED (HORIZONTAL STAB) · airframe 20,693 hrs · 10,824 cycles

DURING C4/S1 C-CHECK, INSP NOTED THE LT SIDE HORIZONTAL STABILIZER OTBD L/E RIB WHERE THE HORIZONTAL STABILIZER SECURES TO, HAS SURFACE CORROSION. MX REPAIRED RIB IAW EA A8-55R-31516 AND IAW SRM 51-74-00, NTM 51-10-04-270-801-A-01, NTM 51-10-08-250-803-A-01, SRM 51-75-12 AND SRM 51-42-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 20,693 hrs · 10,824 cycles

DURING DEN C4/S1 C-CHECK, INSP NOTED THE LT SUPPORT PROFILE AT FRAMES 57-60 IN THE AFT CARGO PIT HAS CORROSION ON THE UPPER SURFACE. MX REMOVED AND REPLACED THE PROFILE IAW SRM 51-42-11 AND SRM 51-44-11.

Part: STRUT — CHAFED (NLG) · airframe 20,693 hrs · 10,824 cycles

DURING DEN C4/S1 C-CHECK, INSP NOTED WIRING CONDUIT CHAFING THE RT SIDE OF THE NLG BARREL. MX PERFORMED MAJOR REPAIR, REFERENCE EA A8-32R-31531, REV A.

Part: SERVO CONTROL — FAULTED (NLG STEERING) · airframe 18,547 hrs · 9,675 cycles

AIR TURN BACK DUE TO NOSE WHEEL STEERING FAULT. MAINTENANCE PERFORMED TROUBLESHOOTING PER TSM 32-51-00-810 FAILURE OF NOSE WHEEL STEERING AND FOUND STEERING SERVO VALVE FAULTED PER TROUBLESHOOTING DATA FAULT CODE 745. MAINTENANCE REMOVED AND REPLACED THE NOSE STEERING CONTROL VALVE AND PERFORMED OPERATIONAL TEST PER AMM 32-51-51 PB 401.

Part: SWITCH — MALFUNCTIONED (HYD LOW LEVEL) · airframe 18,490 hrs · 9,646 cycles

AIR TURN BACK DUE TO BLUE HYDRAULIC RESERVOIR LOW INDICATION ON THE ELECTRONIC CENTRALIZED AIRCRAFT MONITORING SYSTEM. MAINTENANCE APPLIED MEL 29-30-04F FOR THE RESERVOIR LOW LEVEL SWITCH, COMPLIED WITH FOLLOW-UP ACTION TO VERIFY THE BLUE HYDRAULIC RESERVOIR LEVEL WAS ADEQUATE IAW WITH MEL REQUIREMENTS AND RETURNED THE AIRCRAFT TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,004 hrs · 8,833 cycles

LINE MAINTENANCE NOTED THAT THE SEAT MOUNTED EMERGENCY EXIT LIGHT AT ROW 5ABC WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED SEAT MOUNTED EMERGENCY EXIT LIGHT AND PERFORMED OPERATIONAL TEST IN ACCORDANCE WITH A318 AMM 33-51-19 PB 401.

Part: GIRT BAR — OUT OF ADJUST · airframe 15,773 hrs · 8,172 cycles

DURING CLIMB OUT THE L2 AND R2 DOOR DISARMED AT 8500 FT AND REARMED DURING DESCENT AT 10000 FT. MAINT ADJUSTED GIRT BAR FITTINGS ON THE L2 AND R2 DOORS AND OPS AND RIG CHECKED GOOD IAW AMM 52-11-00-820-001, AMM 25-62-44-400-006 AND AMM 05-53-00-780-003. UPON COMPLETION OF THE REPAIR THE AC WAS INSPECTED AND WAS FOUND ACCEPTABLE AND THE AC RETURNED TO SERVICE. (B)

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 15,771 hrs · 8,171 cycles

DURING C-CHECK INSP NOTED CORROSION AROUND FAR RT NUTCLIP HOLE ON SHEAR PLATE ALONG FRAME 68 BETWEEN Y765 AND Y1292. MAINT REMOVED SHEAR CONNECTING PLATE, FABRICATED AND INSTALLED SHEAR CONNECTING PLATE IAW DRAWING D53670099 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,771 hrs · 8,171 cycles

DURING C-CHECK INSP NOTED FLOOR BEAM Y1292 HAS CORROSION AT NUTCLIP HOLE AT FRAME 68 OB SIDE JUST FWD OF GALLEY. MAINT BLENDED CORROSION AND OVERSIZED HOLE, INSTALLED FLANGE BUSHING TREATED PRIMED AND PAINTED IAW EA A8-53R-30435 AND SRM 51-75-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,771 hrs · 8,171 cycles

DURING C-CHECK INSP NOTED FLOORBEAM Y1292 HAS CORROSION AT FWD OB NUTCLIP HOLE AT FRAME 66 JUST AFT OF LT LAVATORY. MAINT BLENDED CORROSION AND OVERSIZED HOLE, FABRICATED FLANGE BUSHING AND TREATED PRIMED AND PAINTED IAW EA A8-53R-30435 AND SRM 51-75-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,771 hrs · 8,171 cycles

DURING C-CHECK INSP NOTED FLOOR PANEL 261FF HAS CORROSION ON SURFACE. MAINT REMOVED AND REPLACED FLOOR PANEL 261FF IAW AMM 53-42-12-400-002. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,771 hrs · 8,171 cycles

DURING C-CHECK INSP NOTED FLOORBEAM Y1292 LT HAS CORROSION AT FIRST, SECOND AND THIRD NUTCLIP HOLES. MAINT REMOVED AND REPLACED FLOORBEAM IAW SRM 51-72-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 15,771 hrs · 8,171 cycles

DURING C-CHECK INSP, FLOOR PANEL 262FF HAS CORROSION ON SURFACE. MAINT REMOVED AND REPLACED FLOOR PANEL 262FF IAW AMM 53-42-12-400-002. UPON COMPLETION OF THE REPAIR, INSPECTED AND FOUND ACCEPTABLE. (B)

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,771 hrs · 8,171 cycles

DURING C-CHECK INSP, NOTED CORROSION AROUND FAR RT NUTCLIP HOLE ON SHEAR PLATE ALONG FRAME 68 BETWEEN Y765 AND Y1292. MAINT REMOVED, FABRICATED AND INSTALLED SERVICEABLE SHEAR PLATE AT FRAME 68 BETWEEN Y765 AND Y1292 IAW DRAWING O53670099, SRM 51-21-11, SRM 51-31-00 AND SRM 53-42-12-420-051B. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: PLATE — CORRODED (GIRT BAR COVER) · corrosion level 2 · airframe 15,771 hrs · 8,171 cycles

DURING C-CHECK INSP NOTED GIRT BAR BLANKING PLATE L2 AFT HAS CORROSION. MAINT REMOVED AND REPLACED CORRODED L2 AFT GIRT BAR BLANKING PLATES IAW WORK CARD C250001-03. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: BLANKING PLATE — CORRODED (GIRT BAR) · corrosion level 2 · airframe 15,771 hrs · 8,171 cycles

DURING C-CHECK INSP, NOTED GIRT BAR BLANKING PLATE ON R2 DOOR AFT HAS CORROSION. MAINT REMOVED AND REPLACED R2 DOOR GIRT BAR BLANKING PLATES IAW WORK CARD C250001-03. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: WEB — GOUGED (ZONE 500) · airframe 15,771 hrs · 8,171 cycles

DURING C-3 C-CHECK INSP, NOTED THAT THE LT NR 4 SPOILER ANTI-ROTATION LUG HAS A GOUGE. MX REPAIRED DAMAGED AREA IAW EA A8-57R-30431.

Part: WEB — GOUGED (ZONE 600) · airframe 15,771 hrs · 8,171 cycles

DURING C-3 C-CHECK INSP, NOTED THAT THE RT NR 3 SPOILER ANTI-ROTATION FLAT HAS A GOUGE. MX REPAIRED DAMAGED AREA IAW EA A8-57R-30430.

Part: PANEL — DAMAGED (CARGO BAY) · airframe 15,771 hrs · 8,171 cycles

DURING C-CHECK INSP NOTED FWD CARGO PIT TRANSITION PANEL 131BF IS DAMAGED. MAINT REPAIRED FWD CARGO PIT TRANSITION PANEL 131BF IAW SRM 53-02-00 PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: PANEL — DAMAGED (CARGO BAY) · airframe 15,771 hrs · 8,171 cycles

REFERENCE NON ROUTINE C046424. DURING C-CHECK INSPECTION NOTED FWD CARGO PIT TRANSITION PANEL 132DG IS DAMAGED. MAINT REPAIRED FWD CARGO PIT TRANSITION PANEL 132DG IAW SRM 53-02-00 PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)

Part: EPSU — FAULTED (EMERGENCY LIGHTS) · airframe 13,032 hrs · 6,778 cycles

DURING A-CHECK, INSPECTION REPORTED EPSU (13WL) BATTERY FAULT. REPLACED EPSU BATTERY (13WL) IAW AMM 33-51-38-PB 401. OPS CHECKED GOOD.

Part: FAN — DEFECTIVE (CABIN) · airframe 11,160 hrs · 5,803 cycles

FLIGHT CREW REPORTED TOXIC ODOR IN CABIN DURING FLIGHT. ODOR MORE PREVALENT IN AFT PASSENGER CABIN AREA. INSPECTED AFT GALLEY AREA AND FOUND AFT CARGO VENT FAN DEFECTIVE. REPLACED FAN PER AMM 21-28-54-000-001. RAN PACKS AND ENGINES FOR SEVERAL MINUTES AND NO UNUSUAL ODORS WERE DETECTED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 10,629 hrs · 5,532 cycles

DURING HEAVY CHECK, INSPECTION REPORTED EMERGENCY LIGHT FAILED TEST, 14RU MCDU. REPLACED BATTERY PACK 10WL. OPS CHECKED GOOD. REF AMM 33-51-38-000-002 AND 33-51-38-400-002.

Part: NUT — LOOSE (NR 1 ENGINE) · airframe 9,872 hrs · 5,151 cycles

DURING C-2 CHECK, INSPECTION REPORTED NR 1 ENGINE PYLON AFT UPPER THREADED SLEEVE AT RIB 10 LOCK WASHER NR 103 TANG SLIGHTLY ENGAGED IN NUT, AFT PYLON-TO-WING ATTACH FITTING. ENGAGED TANG ON NUT FOR NR 1 ENGINE PYLON AFT UPPER THREADED SLEEVE AT RIB 10 IAW AMM 54-51-17-400-002, PAGE 3, ITEM 14.

Part: LOCKWASHER — DAMAGED (ENGINE MOUNT) · airframe 9,872 hrs · 5,151 cycles

DURING C-2 CHECK, INSPECTION REPORTED NR 2 ENGINE PYLON AFT UPPER THREADED SLEEVE AT RIB 10 NUT BACKING OFF AND LOCK WASHER NR 103 DAMAGED, AFT PYLON-TO-WING ATTACH FITTING. REMOVED DAMAGED LOCK WASHER IAW AMM 54-51-17, SUBTASK 54-51-17-481-050, AND INSTALLED REPLACEMENT LOCK WASHER IAW AMM 54-51-17-400-002 AND EA A8-54R-1692.

Part: LUG — DAMAGED (LANDING GEAR) · airframe 6,307 hrs · 3,249 cycles

WHILE PERFORMING A BORESCOPE INSPECTION PER EO A0-32EO-20391 (AD 2005-24-06), INSPECTION FOUND DAMAGE TO THE NOSE LANDING GEAR UPPER SUPPORT, THREE ANTI-ROTATIONAL LUGS WERE FOUND TO BE SHEARED AND ONE ANTI-ROTATIONAL LUG WAS FOUND TO BE CRACKED. THE NOSE LANDING GEAR REQUIRES REPLACEMENT. AN ADDENDUM WILL BE SUBMITTED WHEN THE NOSE LANDING GEAR HAS BEEN REPLACED. ADDENDUM: REPLACED THE NOSE LANDING GEAR ASSEMBLY ON 12/27/05.