N947FR

Part: BATTERY — FAILED (CABIN) · airframe 39,599 hrs · 19,508 cycles

REFERENCE LOG PAGE 9029000 ITEM 2, EPSU BATTERY CAPACITY CHECK FAILED TEST AT 12WL. REMOVED AND REPLACED BATTERY AT 12WL IN REFERENCE TO AMM 33-38-000-002-A AND 33-51-38-400-002-A. OPS CHECK GOOD.

Part: DOOR SILL — CORRODED (FRAME 66) · corrosion level 2 · airframe 37,481 hrs · 18,510 cycles

R2 DOOR SILL HAS EVIDENCE OF CORROSION AROUND FASTNER HOLES. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-72-11-911-001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,481 hrs · 18,510 cycles

AFT FLOOR SUPPORT Y-1292 FR68-69 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM Y-1292 FRAME 68-69 IAW SRM 53-00-14 AND 51-72-11.

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 37,481 hrs · 18,510 cycles

LEFT AFT PASSENGER DOOR SILL HAS CORROSION. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 37,481 hrs · 18,510 cycles

AFT FLOOR SUPPORT Y-1292, FRAMES 66 TO 68 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-14 AND 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,481 hrs · 15,810 cycles

AFT FLOORBEAM Y765 FR66 TO FR69 CORROSION. REMOVED AND REPLACED FLOORBEAM Y765 AT FR66 TO FR69 IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,481 hrs · 18,510 cycles

CORROSION AT Y1292 FR 66-68. REMOVED AND REPLACED FLOORBEAM Y1292 FRAME 66-68 IAW SRM 53-00-14 AND 51-72-11.

Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 37,481 hrs · 15,810 cycles

AFT FLOORBEAM Y765 FR66 CORRODED. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-69) · corrosion level 2 · airframe 37,481 hrs · 18,510 cycles

AFT FLOOR SUPPORT Y765 FRAMES 66 TO 69 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 31,116 hrs · 15,520 cycles

AIRCRAFT DUE C6 CHECK, AFT CABIN RT LATERAL SHEAR PLATE CRACKED AT FRAME 69 - 70. R & R SHEAR PLATE IAW SRM 51-42-1. ACFT DUE OUT OF C6 CHECK ON 5 25 2015.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 31,116 hrs · 15,520 cycles

AIRCRAFT DUE C6 CHECK, AFT CABIN LT LATERAL SHEAR PLATE CRACKED FRAME 69 - 70. R & R SHEAR PLATE IAW SRM 51-42-11. ACFT DUE OUT OF C6 CHECK ON 5 25 2015.

Part: LIGHT — CRACKED (ZONE 200) · airframe 25,276 hrs · 12,469 cycles

DURING C5 CHECK. R1 DOOR LOWER EXIT LIGHT LENS FRAME CRACKED. R & R IAW AMM 33-51-13-020-050-C, STEP 4 A1 A-F AND AMM 33-51-13-420-050-C, STEP 4.A. 1-4. OPS CHECK GOOD IAW AMM 33-51-13-710-050-A.

Part: UNKNOWN — ODOR (COCKPIT/CABIN) · airframe 20,242 hrs · 9,901 cycles

UNIDENTIFIABLE ODOR NOTICED ON CLIMB OUT, WENT AWAY DURING CLIMB OUT OF CLOUDS. CAME BACK AT CRUISE. ODOR WORSE UP FRONT (FWD GALLEY / COCKPIT). ODOR HAD A TASTE. NO SMOKE WAS NOTICED. ODOR COULD NOT BE DESCRIBED. TSM 21-00-00-810-820A UNSATISFACTORY CABIN AIR QUALITY REFERS TO SIL 1-132 INSPECTION OF APU DE-ICING FLUID TABLE 4. FOUND ODOR TO REOCCUR WHEN SELECTING APU BLEED WITH PACKS ON. CLEANED APU INLET AND RAN PACKS REF AMM 21-61-00-710-001A.

Part: SHEAR PLATE — CRACKED (ZONE 200) · airframe 19,881 hrs · 9,721 cycles

C-CHECK: RIGHT SHEAR PLATE AT FRAME 69-70 IS CRACKED AT FASTENER HOLE. R & R SHEAR PLATE IAW SRM 53-42-00.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 19,881 hrs · 9,721 cycles

C-CHECK: CABIN DOOR SILL BEAM R-2 FR66 -Y1732 HAS CORROSION AROUND FASTENER HOLE IS OUT OF LIMITS. REPAIRED DOOR SILL IAW SRM 53-41-14.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 19,881 hrs · 9,721 cycles

C-CHECK: MAIN CABIN FRAME 66 -Y1500, AFT PASSENGER L-2 DOOR SILL BEAM CORROSION. REPAIRED DOOR SILL BEAM IAW SRM 53-41-14.

Part: SHEAR PLATE — CRACKED (ZONE 200) · airframe 19,881 hrs · 9,721 cycles

C-CHECK: LEFT SHEAR PLATE AT FRAME 69·70 IS CRACKED AT FASTENER HOLE. R & R SHEAR PLATE IAW SRM 53-42-00.

Part: SHEAR PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 16,846 hrs · 8,221 cycles

C-CHECK: NON ROUTINE N0286; LT AFT FUSELAGE SHEAR PLATE BETWEEN FRAMES 69L AND 70L HAS 4 SQ INCHES OF CORROSION. IAW EO AO-53EO-31434 SHEAR PLATE NEEDS TO BE REPLACED WITH NEW CONFIGURATION. REPLACED RT SHEAR PLATE BETWEEN FRAMES 69L AND 70L WITH NEW CONFIGURATION.

Part: SHEAR PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 16,846 hrs · 8,221 cycles

C-CHECK: NON ROUTINE N0284; RT AFT FUSELAGE SHEAR PLATE BETWEEN FRAMES 69R AND 70R HAS 4 SQUARE INCHES OF CORROSION. EO AO-53EO-31434 SHEAR PLATE NEEDS TO BE REPLACED WITH NEW CONFIGURATION. REPLACED RT SHEAR PLATE BETWEEN FRAMES 69R AND 70R WITH NEW CONFIGURATION.

Part: ACCELEROMETER — FAILED (ZONE 200) · airframe 16,846 hrs · 8,221 cycles

C-CHECK: NON ROUTINE N0299; DFDRS TEST SHOW CLASS 2 FAULT FOR ACCELEROMETER (6TU0. REPLACED ACCELEROMETER (6TU), OPS CHECKED NORMAL.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 16,846 hrs · 8,221 cycles

C-CHECK: NON ROUTINE N0232; MAIN CABIN LT SIDE LONGTUDINAL BEAM Y1292 FRAME 67 HAS 2 SQUARE INCHES OF CORROSION. R & R BEAM Y1292 LT AT FRAME 67 IAW SRM 51-42-11, PARA 5 AND 7 AND SRM 51-72-11 PARA 5.A-B AND 6.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,323 hrs · 7,972 cycles

EMERGENCY EXIT LIGHT INOP AT SEAT 17C (LP 564000 ITEM M2)AND 16C (LP 576001 M1). REPLACED LIGHT ASSY (PN BR9644-24) AT SEAT 17C, OPS CHECKED NORMAL. RELAMPED (PN BR9644-22) EMERGENCY LIGHT SEAT 16C, OPS CHECKED NORMAL.

Part: CIRCUIT BREAKER — OPEN (OIL PRESSURE) · airframe 14,884 hrs · 7,217 cycles

REFERENCE PILOT WRITE-UP LOG PAGE 541210 07/07/2010. AIR TURNBACK. LEFT ENGINE OIL PRESSURE GAUGE INOP. FOUND LEFT ENGINE OIL PRESSURE CIRCUIT BREAKER RELEASED. RESET LEFT ENGINE OIL PRESSURE CIRCUIT BREAKER AND PERFORMED LEFT ENGINE IDLE RUN. LEFT ENGINE OIL PRESSURE INDICATION NORMAL. NO PARTS FOUND TO BE DEFECTIVE.

Part: HOSE — BLISTERED (NR 1 ENG FUEL) · airframe 11,136 hrs · 5,504 cycles

REF NON-ROUTINE C062832. DURING DEN C2 C-CHECK, INSP NOTED A FUEL LEAK FROM THE NR 1 ENGINE HYDROMECHANICAL UNIT, COMING FROM A BLISTER ON A FUEL LINE. MX REMOVED AND REPLACED THE FLEXIBLE LINE IAW AMM 73-21-10-420-054 AND PERFORMED LEAK CHECK IAW AMM 73-21-10-400-002.

Part: STRUCTURE — DAMAGED (TE FLAP) · airframe 11,136 hrs · 5,504 cycles

REF NON ROUTINE C062722, C062723, C062724, C062725. DURING DEN C2 C-CHECK, INSP NOTED THAT THE RT INBD FLAP HAD 4 AREAS OF LIGHTNING STRIKE DAMAGE LOCATED ON CTR RUB STRIP. MX REMOVED RUBSTRIP AND PERFORMED MAJOR REPAIR TO THE FLAP BY SANDING DAMAGED AREA, CLEANING AND FILLING WITH RESIN IAW SRM 57-52-00 PARAGRAPH 8E AND INSTALLED NEW RUBSTRIP IAW SRM 57-52-11 PB 201.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,887 hrs · 2,888 cycles

DURING RON MAINTENANCE, ROW 4, SEATS ABC AISLE MOUNTED EMERGENCY LIGHT FAILED ITS OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE ROW 4, SEATS ABC AISLE MOUNTED EMERGENCY LIGHT IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-19 PB 401. UPON COMPLETION OF THE INSTALLATION AND INSPECTION, THE LIGHT WAS TESTED AND FOUND TO BE ACCEPTABLE.

Part: SKIN — DENTED (FUSELAGE) · airframe 4,871 hrs · 2,407 cycles

BIRD STRIKE TO FWD LT SIDE OF FUSELAGE. LT SKIN PANEL DENTED AT FR 4, 11.5" ABOVE STBY STATIC PORT, 2.5" ABOVE SIDE STR 3" BY 4" BY .067. LT SKIN PANEL DENTED AT FR 5 15.5" FROM STBY STATIC PORT, 2.5" ABOVE LT SIDE STR 3.8" BY 2.8"BY .037. INSPECTED AREA PER EA A9-53R-12191. NO ADDITIONAL DAMAGE FOUND. INITIATED TDI 0000682 FOR PERMANENT REPAIR, TO BE DETERMINED BY ENGINEERING WITHIN 50 FLIGHT CYCLES. PERFORMED HFEC AND DVI INSPECTIONS OF AREAS TO BE REPAIRED IAW NTM 51-10-08 AND 51-90-00 NORTEC 2000S AND S/N F9TAB2309C, CAL DUE DATE 08/2008. REWORKED DAMAGED SKIN AREA FR 4 AND FR 5 TO WITHIN LIMITS IAW SRM 51-73-00 FIG 5 AND EA A9-53R-12191. REMOVED SAID FASTENERS IN FR 4 AND FR 5 PER EA A9-53R-12191 AND SRM 51-42-11. ROTO PROBE TESTED FASTENER HOLES IAW NTM 51-10-01, PART 6, PROCEDURE A, NORTEC 2000ST, S/N F9TAB0511C, CAL DUE 10/07. HFEC INSP SURFACE OF REWORKED DENTS IAW NTM 51-10-08, PART 6, NORTEC 2000ST, S/N F9TAB2309C, CAL DUE DATE 08-2008. PERFORMED DVI OF REWORKED AREA IAW NTM 51-90-00, PART 9. NO DEFECTS NOTED. INSTALLED FASTENERS FR 4 AND FR 5 IAW EA A9-53R-12191 AND SRM 51-42-11. PAINTED AREA AS REQUIRED IAW SRM 51-23-11. NO FURTHER ACTION REQUIRED.