N945FR

Part: CONTROL UNIT — INOPERATIVE (APU GENERATOR) · airframe 23,537 hrs · 11,146 cycles

AIRCRAFT BEING POWERED BY APU. ALL DROPPED OFF WITH APU STILL INDICATING AVAILABLE - STRONG ODOR OF ELECTRICAL SMOKE IN COCKPIT. R & R GAPCU-(GROUND AUX POWER CTRL UNIT) IAW AMM 24-41-34-400-001-B. CHECKED GOOD IAW AMM 24-41-00-740-002-B.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,405 hrs · 10,065 cycles

C-CHECK: FWD CARGO EIGHT INCHES AFT OF FRAME 27 DOOR SILL WEB HAS LIGHT SURFACE CORROSION. BLENDED AREA AND FOUND TO BE WITHIN LIMITS IAW SRM 51-73-00, PAR 5.F AND FIG 001.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,405 hrs · 10,065 cycles

C-CHECK: MAIN CABIN FLOORBEAM AT FRAME 68 -Y1292 AFT OF SPLICE HAS LIGHT SURFACE CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,405 hrs · 10,065 cycles

C-CHECK: MAIN CABIN FRAME 66 AT L2 DOOR, DOOR SILL BEAM HAS CORROSION AT FASTENER HOLE. REPAIRED IAW SRM 53-41 -14 PB201 .

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,405 hrs · 10,065 cycles

C-CHECK: MAIN CABIN FLOORBEAM AT FRAME 68 Y765 HAS CORROSION. R & R FLOORBEAM IAW SRM 51-42-11 PARA 5.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,405 hrs · 10,065 cycles

C-CHECK: MAIN CABIN FLOORBEAM AT FRAME 68 -Y1292 FWD OF SPLICE HAS LIGHT SURFACE CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARAGRAPH 5.

Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,008 hrs · 7,965 cycles

C-CHECK: NON ROUTINE N0596; FR69-70 SHEAR WEB PLATE HAS CORROSION AROUND FASTNER HOLES AND IS OLD CONFIGURATION. FOUND TO BE OUT OF LIMITS. REPLACED SHEAR WEB PLATE WITH NEW CONFIGURATION IAW EO AO-53EO-31434.

Part: SPLICE — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,008 hrs · 7,965 cycles

C-CHECK: NON ROUTINE N0438; LT FLOORBEAM, Y1292 SPLICE COUPLING AT FRAME 66L HAS 2 INCHES OF CORROSION. CORROSION IS OUT OF LIMITS. REPLACED SPLICE COUPLING AT FRAME 66L IAW SRM 53-72-11, PARA 6.

Part: FLOOR PANEL — CHAFED (ZONE 100) · airframe 17,008 hrs · 7,965 cycles

C-CHECK: NON ROUTINE N0399; AFT CARGO PANEL 151VG AFT EDGE IS WORN THROUGH TOP PLY. AREA IS 10 SQ INCHES. DAMAGE IS OUT OF LIMITS. FABRICATED REPLACEMENT PANEL 151VG IAW MCG IRM 9701 REV G.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,008 hrs · 7,965 cycles

C-CHECK: NON ROUTINE N0484; R2 DOOR SILL HAS 3 SQ INCHES OF CORROSION AROUND AFT GIRT BAR FITTING. FOUND TO BE OUT OF LIMITS. REPLACED THE R2 DOOR SILL IAW SRM 51-74-00 & CHECK LIMITS IAW SRM 53-41-14.

Part: SHEAR TIE — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,008 hrs · 7,965 cycles

C-CHECK: NON ROUTINE N0595; LT MAIN CABIN SHEAR PLATE HAS CORRORION AROUND FASTENER HOLES. SHEAR PLATE IS UNMODIFIELD TYPE ACFT IS IN C-CHECK. REPLACED THE SHEAR, FRAME FR69L TO FR70L IAW SRM 51-42-11 AND FRONTIER E) 53EO-31434.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,008 hrs · 7,965 cycles

C-CHECK: NON ROUTINE N0436; LT FLOORBEAM, Y1292 AT FRAME 68L HAS A 2 SQ. INCHES OF CORROSION ON THE UPPER AND LOWER SIDERS. CORROSION IS OUT OF LIMITS. REPLACED FLOORBEAM, Y1292 BETWEEN FRAMES 68LT AND 69LT IAW SRM 51-72-11, PARA 6.

Part: THERMOSTAT — DEFECTIVE (CABIN AIR) · airframe 16,696 hrs · 7,816 cycles

LOST BLEED NR1 AT 36,000 CAUSING CABIN PRESSURE EXCESS CABIN ALTITUDE. EMERGENCY WAS DECLARE AND DECENTED TO 10,000. FOUND THERMOSTAT DEFECTIVE, R & R THE THERMOSTAT IAW AMM 36-11-43-PB401. OPS CHECK GOOD.

Part: UNKNOWN — ARCED (COCKPIT) · airframe 15,452 hrs · 7,227 cycles

UPON ENGINE SHUTDOWN BRIGHT ARCHING FROM AFT CIRCUIT BREAKER PANEL WITH LOUD BANG FROM WITHIN CIRCUIT BREAKER PANEL. ALSO PUFF OF SMOKE. PERFORMED TSM PROCESS REFERENCE TSM 24-00-00-810-823. NO CIRCUIT BREAKERS TRIPPED. NO ECAM WARNINGS. INSPECTED CIRCUIT BREAKERS AND CONTACTORS BEHIND 121VU AND 122VU PANELS. NO EVIDENCE OF ARCHING OR ODORS. OBSERVED TRANSFORMER RECTIFIERS AND CONTACTORS WHILE SIMULATING POWER TRANSFERS AND LOSS WITH ENGINES AND APU RUNNING. NO ABNORMALITIES NOTED.

Part: SERVO CONTROL — FAULTED (ELEVATOR) · airframe 11,387 hrs · 5,353 cycles

IN DEN, AIRCRAFT RETURNED TO BLOCK DUE TO NR 1 ELEVATOR AILERON COMPUTER PITCH FAULT DURING FLIGHT CONTROL CHECK. MAINTENANCE REMOVED AND REPLACED THE LEFT OUTBOARD ELEVATOR SERVO (BLUE SYSTEM, POSITION 34CE3) AND MADE ADJUSTMENTS PER AMM 27-34-51-000-001, 27-34-51-400-001 AND 27-34-00-820-002. MAINTENANCE PERFORMED SATISFACTORY OPERATIONAL AND LEAK TEST.

Part: LANYARD — MISSING (ESCAPE SLIDE) · airframe 5,553 hrs · 2,726 cycles

DURING C-1 CHECK, INSPECTION REPORTED LT OVERWING EMERGENCY ESCAPE SLIDE LOWER ACTUATING CABLE WAS MISSING THE LOWER END PIECE TO ATTACH TO THE SLIDE RELEASE BOTTLE/TEST FIXTURE. REMOVED, REPLACED AND OPS CHECKED LT OVERWING EMERGENCY ESCAPE SLIDE LOWER ACTUATING CABLE IAW AMM 25-62-43-000-001, 25-62-43-400-001, 52-21-00, PB 501, AND TASK CARD 528001-11.

Part: LANYARD — MISSING (ESCAPE SLIDE) · airframe 5,553 hrs · 2,726 cycles

DURING C-1 CHECK, INSPECTION REPORTED RT OVERWING EMERGENCY ESCAPE SLIDE RELEASE CABLE FAILED TO RETRACT DURING MANUAL RELEASE TEST. REMOVED AND REPLACED PULL CABLE AND OPS CHECKED RT OVERWING EXIT SLIDE RELEASE CABLE IAW AMM 52-21-00, PB501, AND TASK CARD C522101-3.

Part: BUSHING — OUT OF ADJUST (R1 DOOR) · airframe 2,758 hrs · 1,384 cycles

R1 DOOR WOULD NOT LATCH IN OPEN POSITION. RESEATED BUSHING UNDER PUSHBUTTON. PERFORMED OPS CHECK IAW AMM 52-10-00, PAGE 201. CHECKED GOOD. INSPECTED R1 DOOR GUST LOCK. OPERATED PROPERLY.