N203FR

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 52,088 hrs · 21,253 cycles

FOUND THE CAPTAIN'S WINDSHIELD SHATTERED. REPLACED THE WINDSHIELD IAW AMM 56-11-11 PB 401. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 51,648 hrs · 21,078 cycles

FLOOR SUPPORT Y1292 FROM FRAMES 64 - 66 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-70) · corrosion level 2 · airframe 51,648 hrs · 21,078 cycles

FLOOR SUPPORT -Y254 BETWEEN FRAMES 68 - 70 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND 51-72-11-911-001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,648 hrs · 21,078 cycles

FLOORBEAM Y254 BETWEEN FR66-FR67 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED NEW FLOORBEAM Y254 BETWEEN FR66-FR67 IAW SRM 51-72-11, 51-42-11 AND 53-41-14.

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 51,648 hrs · 21,078 cycles

FLOORBEAM -Y1292 AT FRAME 68 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND 51-72-11-911-001.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-68) · corrosion level 2 · airframe 51,648 hrs · 21,078 cycles

FLOOR SUPPORT -Y765, FRAMES 67 - 68 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND 51-72-11-911-001.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-68) · corrosion level 2 · airframe 51,648 hrs · 21,078 cycles

FLOOR SUPPORT Y765 BETWEEN FRAMES 67 AND 68 HAS CORROSION ON UPPER SERVICE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001.

Part: FLOORBEAM — CORRODED (FRAME 67) · corrosion level 2 · airframe 51,648 hrs · 21,078 cycles

FLOORBEAM Y1292 AT FRAME 67 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11-911-001.

Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 51,648 hrs · 21,078 cycles

FLOORBEAM -Y765 AT FRAME 66 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW 51-42-11, AND 51-72-11-911-001.

Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 51,648 hrs · 21,078 cycles

FLOORBEAM Y1292 AT FR68 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND 51-72-11-911-001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,648 hrs · 21,078 cycles

FLOORBEAM -Y1292 AT FR 66 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED, NEW FLOORBEAM -Y1292 AT FR66 IAW SRM A320-51-42-11 AND 51-72-911-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,648 hrs · 21,078 cycles

FLOORBEAM Y765 AT FR66 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION ON FLOORBEAM Y765 AT FR66 FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAM Y765 AT FR66 REPLACE WITH NEW FLOORBEAM Y765 IAW SRM A320-51-72-11.

Part: FLOORBEAM — CORRODED (FRAME 67) · corrosion level 2 · airframe 51,648 hrs · 21,078 cycles

FLOORBEAM -Y1292 AT FRAME 67 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND 51-72-11-911-001.

Part: COFFEEMAKER — ODOR (GALLEY)

F/A SMELLED ODOR COMING FROM AFT CABIN DESCRIBED AS POSSIBLY POPCORN, BURNING RUBBER, OF BURNED COFFEE. POSSIBLY COMING FROM HIGHER IN THE CABIN PERFORMED TROUBLESHOOTING IAW TSM 05-50-00-810-831A. IDENTIFIED THE MOST PROBABLE CAUSE OF THE ODOR TO BE COMING FROM THE AFT GALLEY COFFEEMAKER WITH DRIED COFFEE RESIDUE ON THE HOT PLATE. CLEAN ENTIRE AREA AND PERFORMED OPS TEST OF THE AFT GALLEY COFFEEMAKER.

Part: COFFEEMAKER — DIRTY (GALLEY) · airframe 47,774 hrs · 19,562 cycles

REFERENCE LOG PAGE 989574, DURING CRUISE THE CREW NOTED AN ODOR COMING FROM THE AFT CABIN & THE ACFT DIVERTED. MX IDENTIFIED THE CAUSE OF THE ODOR TO BE THE AFT GALLEY COFFEE MAKER & FOUND BURNT DRIED COFFEE RESIDUE ON AFT GALLEY COFFEE MAKER. MX CLEANED & INSPECTED COFFEE MAKER INSPECTED ALL OTHER GALLEY CABIN ITEMS & NO DEFECTS NOTED IAW AMM 25-35-15 PB 401, AMM 25-35-00-710-003, OPERATIONAL CHECKED GOOD.

Part: SAFETY VALVE — INOPERATIVE (ZONE 700) · airframe 45,728 hrs · 18,770 cycles

DISCREPANCY ITEM 1, SPOILERS 1 & 2 FAULT INFLIGHT. DISCREPANCY ITEM NR 2 NOSE WHEEL STEERING FAULT INFLIGHT. RESET SEC 1 & 2. OPERATIONS CHECKED OK IAW AMM 27-94-00-710-001 & -002. NR 2 R & R NLG ELECTRONIC BOX 5GC IAW AMM 32-51-12-000-001 & 32-51-12-400-001. TW F9TAB3948C DUE 10 16. AIR DATA TESTER F9TAB2181C DUE 10 16. R & R SAFETY VLV 496A IAW AMM 32-31-17 PB 401. PERFORMED NOSE GEAR SWING & TAXI, OPERATIONS CHECKED OK IAW AMM 32-31-00-720-003A. REFERENCE LOG PAGES 957951 & 957953.

Part: LINE — CHAFED (HYD SYSTEM) · airframe 308 hrs · 128 cycles

HYD RESERVOIR LOW LEVLE, DURING CRUISE FLIGHT. DECLARED AN EMERGENCY. MX FOUND A HOLE IN THE RETURN LINE FOR THE NR 2 ENG THRUST REVERSER HYDRAULIC LINE. THE LINE WAS REPLACED IAW AMM 78-31-49 & HYD SYS SERVICED IAW AMM 29-13-00-710003-A.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 45,357 hrs · 18,617 cycles

EMERGENCY SLIDE LIGHT AT DOOR 1 RT INOPERATIVE. PLACED ON MEL CONTROL NR 1116039. REPLACED L1 DOOR SLIDE AMM 25-62-44-000-002-A & 25-62-44-400-006-A. OPERATIONAL CHECKED GOOD, LIGHTS OPERATE NORMAL & PLACARD REMOVED.

Part: WIRE — DAMAGED (CABIN) · airframe 43,008 hrs · 17,674 cycles

DISCREPANCY, EMER EXIT LIGHTS INOPERATIVE AT L1, L2, R1 & R2. RETERMINATED WIRING AT ALL 4 EPSUS AS REQUIRED, COMPLIED WITH EA A2-33R-33040. EMER LIGHTS OPERATIONS CHECKED GOOD. PN INVOLVED, 10WL 3351-5408, 11WL 3351-1917, 12WL 3351-1779 & 13WL 3351-1927.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 38,208 hrs · 15,606 cycles

DURING C8/S2 CHECK. SEAT TRACK Y1292 HAS CORROSION AT FRAME 16. SEAT TRACK CORROSION EVALUATED AND FOUND OUT OF LIMITS. REMOVED DAMAGED TRACK AND INSTALLED NEW SEAT TRACK, IAW SRM 51-42-11, SECT 5.A THRU C.6 AND SECT 7.B3 A-D.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 38,208 hrs · 15,606 cycles

DURING C8/S2 CHECK. THERMOGRAPHIC INSPECTION OF LT ELEVATOR REVEALED INDICATIONS ON UPPER PANEL IRREGULAR IN SHAPE AND BLACK IN COLOR. REPAIRED IAW SRM 55-20-00, PB201, PARA 2.A.-B, PARA. 2.B, 2.B(1)(A)2, SRM 55-21-11, PB201, C1 PARA.5.E.(2)(A)(B), FIGURE 205 SHEET 3, PARA. 5.E. (2)(B)(L)(2),PARA. 5.E.(2)(B)2, PARA. 5.E.(2)(F)1-5, PARA. 2(G) AND CMM 55-21-15-200-801-G01, SUB TASK 55-21-15-210-010-G01, SECT. A(1-5)(6)(A),(7-8),(9)(C).

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,208 hrs · 15,606 cycles

DURING C8/S2 CHECK. FORWARD CARGO LOWER SILL UPPER SURFACE HAS CORROSION BETWEEN FRAMES 26 AND 27. REPAIRED IAW SRM 51-74-00 PARA 6.A - 6.B(2}(5), SRM 51-75-12, SRM 51-21-11 AND SRM 51-23-11.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,208 hrs · 15,606 cycles

DURING C8/S2 CHECK. FORWARD CARGO DOOR SILL LOWER SKIN HAS SURFACE CORROSION ON UPPER SURFACE AT FRAMES 24 TO 25. REPAIRED IAW SRM 5L-74-00 PARA 6.A-6.B.

Part: SHEAR TIE — CORRODED (FRAME 70) · corrosion level 2 · airframe 15,606 hrs

DURING C8/S2 CHECK, LT LATERAL SHEAR PLATE HAS CORROSION AT FRAME 70, STRINGER 24. REMOVED AND REPLACED IAW SRM 51-42-11, PARAGRAPH 6.B., 1 THROUGH 8.

Part: SHEAR TIE — CORRODED (FRAME 70) · corrosion level 2 · airframe 38,208 hrs · 15,606 cycles

DURING C8/S2 CHECK. RT LATERAL SHEAR PLATE HAS CORROSION AT FRAME 70, STRINGER 24. R & R IAW SRM 51-42-11, PARA 6.B., 1 THROUGH 8.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,462 hrs · 13,668 cycles

SEAT ROW 24 EMERGENCY LIGHT INOPERATIVE. R & R BULBS, IAW AMM 33-41-11-400-002A, 33--41-11-000-002A. OPS CHECKED OK.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,462 hrs · 13,668 cycles

SEAT ROW 25 EMERGENCY LIGHT INOPERATIVE. R & R BULBS IAW AMM 33-51-18-400-002A. OPS CHECKED OK.

Part: ELECTRICAL BOX — FAILED (ENTERTAIN SYS) · airframe 32,560 hrs · 13,316 cycles

ODOR OF ELETRICITY BETWEEN ROW 3 AND 4. NO VISIBLE SMOKE. TURNED OFF LIVE TV AND ODOR CLEARED. PERFORMED ELETRICAL ODOR SYS INTEGRITY CHECK IAW LTV AMM 44-25-00. NO DISCREPANCIES NOTED. CHANGED SEB IAW LTV AMM 44-25-00. OPS CHECKED GOOD.

Part: FEEL UNIT — BINDING (RUDDER) · airframe 30,967 hrs · 12,661 cycles

REFERENCE PILOT REPORT LOG PAGE 615630 ITEM 1, UPON TOUCHDOWN PILOT NEEDED RIGHT RUDDER TO STRAIGHTEN NOSE BUT RUDDER FELT LOCKED IN CENTERED POSITION. AFTER APPLYING MORE PRESSURE PEDAL UNLOCKED AND APPEARED TO WORK NORMALLY. REMOVED AND REPLACED ARTIFICIAL FEEL AND TRIM UNIT. REFERENCE AMM 27-23-41 PAGE BLOCK 401. OPERATIONAL CHECK GOOD.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 28,379 hrs · 11,679 cycles

C-CHECK: NON ROUTINE N0401; FLOORBOARD UNDER LAV E IS DELAMINATED. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701 REV G.

Part: TRANSITION PANEL — DELAMINATED (ZONE 100) · airframe 28,379 hrs · 11,679 cycles

C-CHECK: NON ROUTINE N0289; FWD CARGO TRANSITION PANEL 132GF UPPER SURFACE IS DELAMINATED IN 2 PLACES, 2 SQUARE IN, 4 SQUARE IN. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701, REV G.

Part: COVER — GOUGED (DOOR SEAL) · airframe 28,379 hrs · 11,679 cycles

C-CHECK: NON ROUTINE N0138; FWD CARGO DOOR INTERNAL SIDE HAS 2.5 INCHES ABOVE THE LOWER DOOR SEAL AND 26.5 INCHES FWD AFT DOOR SEAL IS GOUGED, THAT MEASURES 1/8 INCH WIDE BY 3/4 INCH LONG BY .008 INCH DEEP. REPAIRED IAW A320SRM 52-31-00 PARAGRAPH (O).

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,379 hrs · 11,679 cycles

C-CHECK: NON ROUTINE N0566; MAIN CABIN FLOORBEAM RT SIDE NR4 BETWEEN FRAME 67-69, CORROSION ON BOTTOM SIDE OF FLOORBEAM AT FASTENER HOLE. R & R FLOORBEAM IAW SRM 51-72-11, PAGE 1 AND 2.

Part: TRANSITION PANEL — DEBONDED (ZONE 100) · airframe 28,379 hrs · 11,679 cycles

C-CHECK: NON ROUTINE N0291; FWD CARGO TRANSITION PANEL 132FF UPPER SURFACE DEBONDED 6 SQ IN. FABRICATED REPLACEMENT PANEL IAW MCG IRM 9701, REV G.

Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,379 hrs · 11,679 cycles

C-CHECK: NON ROUTINE N0561; AFT GALLEY UNDERFLOOR STRUCTURE RT LATERAL SHEAR PLATE BETWEEN FRAME 69 AND 70, HAS CORROSION AT 8 IN AFT OF FRAME 69 (ABOUT 2 SQUARE INCHES). R & R SHEARPLATE IAW SRM 51-42-11.

Part: SEAL — GOUGED (CARGO DOOR) · airframe 28,379 hrs · 11,679 cycles

C-CHECK: NON ROUTINE N0134; AFT CARGO DOOR INTERNAL SIDE HAS 2 IN ABOVE THE LOWER SEAL AND 25 INCHES OF FWD SEAL IS GOUGED THAT MEASURES .3750 IN WIDE X .7500 IN LONG X 0018 INCH DEEP. REPAIRED IAW SRM 52-31-00, PARAGRAPH (O)

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,379 hrs · 11,679 cycles

C-CHECK: NON ROUTINE N0558; MAIN CABIN FLOOR AT FRAME 68L FLOOR SUPPORT HAS CORROSION APPROX 25 SQ IN AT THE FASTENER HOLES. CORROSION ON FLOOR SILL. REMOVED CORROSION ON L-2 DOOR SILL AT FRAME 68 IAW SRM 51-74-00 BLEND OUT FOUND TO BE OUT OF LIMITS, REPAIRED IAW SRM 53-41-14, FIG 201 REPAIR PRINCIPLE NR 5.

Part: PANEL — GOUGED (CARGO DOOR) · airframe 28,379 hrs · 11,679 cycles

C-CHECK: NON ROUTINE N0132; AFT CARGO DOOR INTERNAL SIDE HAS A 2.5 INCHES ABOVE THE LOWER DOOR SEAL AND 27 INCHES FWD OF AFT SEAL IS A GOUGE THAT MEASURES .7500 IN WIDE BY 1 IN LONG BY .090 IN DEEP. REPAIRED IAW SRM 52-30-00, PARAGRAPH (O).

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,379 hrs · 11,679 cycles

C-CHECK: NON ROUTINE N0557; MAIN CABIN FLOORBEAM, NR 4 LT BETWEEN FRAME 67-68 HAS APPROX 2 SQ IN OF CORROSION AT THE FASTENER HOLES. R & R FLOORBEAM IAW SRM 51-44-11, SRM 51-42-11.

Part: FLOOR PANEL — PUNCTURED (ZONE 100) · airframe 28,379 hrs · 11,679 cycles

C-CHECK: NON ROUTINE N0286; FWD CARGO TRANSITION FLOOR PANEL 131BF HAS A 1 SQUARE IN PUNCTURE. FABRICATED REPLACEMENT PANEL IAW MCG 9701, REV G.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 28,379 hrs · 11,679 cycles

C-CHECK: FWD CARGO PIT TRANSITION FLOOR PANEL 131BF UPPER SURFACE AFT END DISBOUNDED 8 SQUARE INCHES. FABRICATED TRANSITION PANEL IAW MCW IRM 9701 REV G.

Part: MODULE — LOOSE (EMERGENCY LIGHTS) · airframe 28,379 hrs · 11,679 cycles

C-CHECK: NON ROUTINE N0694; EMERGENCY EXIT LIGHTS ON SEAT ROWS 16 AND 24 ARE INOP. RETERMINATED PINS ON EMERGENCY EXIT LIGHT CONNECTORS AT SEATS 16 LT AND 24 LT IAW AMM 33-51-19-020-051, STEP 4A1C AND AMM 33-51-19-420-051 STEP 4B1B. OPS CHECK GOOD IAW AMM 33-51-00710-001, SUBTASK 33-51-00-710-050.

Part: BLEED VALVE — FAULTED (NR 1 ENGINE) · airframe 27,326 hrs · 11,291 cycles

AIR TURNBACK DUE TO ENGINE NUMBER 1 CONTROL VALVE FAULT. REMOVED AND REPLACED TRANSIENT BLEED VALVE REFERENCE AMM 75-26-10-000-001 AND AMM 75-26-10-400-001. OPERATIONAL CHECK GOOD.

Part: RELAY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,150 hrs · 10,529 cycles

REF LOG PAGE 492624. FLIGHT CREW MAD A BLOCK TURN BACK DUE TO THE F/A CIDS PANEL EMERGENCY LIGHTS ON AND COULD NOT BE RESTORED AND TURNED OFF. MX REMOVED AND REPLACED RELAY 8WL IAW AMM 33-31-00-710-004.

Part: OXYGEN MASK — NO TEST (ZONE 900) · airframe 23,096 hrs · 9,783 cycles

DURING AIRCRAFT INDUCTION CHECK, THE FORWARD LAVATORY OXYGEN MASK WOULD NOT DROP DURING THE MANUAL MASK DROP TEST. MAINTENANCE REPACKED THE OXYGEN MASK AND PERFORMED SATISFACTORY DROP TEST, REFERENCE AMM 35-23-00-550-053.