N910FR

Part: PUMP — FAILED (NR 2 ENGINE) · airframe 60,953 hrs · 25,968 cycles

ATB, Y HYD ENG 2 PUMP LOW PRESSURE. NO OVERHEAT, Y OR G. REMOVED AND REPLACED NR 2 HYDRAULIC PUMP IAW AMM 29-13-51 PB401. T/W F9T0345C DUE DATE 07/19. T/W F9TAB2956C DUE DATE 06/19. OPS CHECK/LEAK CHECK IS SATISFACTORY.

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 58,468 hrs · 24,767 cycles

L1 DOOR SLIDE NOT ARMING. REMOVED AND REPLACED THE LEFT FORWARD DOOR SLIDE IAW AMM 25-62-44PB401. OPERATIONAL CHECKED GOOD.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 57,683 hrs · 24,422 cycles

FORWARD POWER SUPPLY FAILED TO TEST AT 10WL. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-38, PB401. OPS CHECKED GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,179 hrs · 23,292 cycles

CORROSION ON FLOORBEAM Y254 BETWEEN FR66 AND FR67. REPLACED FLOORBEAM Y254 BETWEEN FR66 AND FR67 IAW SRM 51-72-11-911-001.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-68) · corrosion level 2 · airframe 55,179 hrs · 23,292 cycles

CORROSION ON THE FLOOR SUPPORT Y765 BETWEEN FRAMES 67 AND 68. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW 53-00-14. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 55,179 hrs · 23,292 cycles

CORROSION AT FLOORBEAM - Y765 BETWEEN FR67 AND FR68. REMOVED AND REPLACED - Y765 FLOORBEAM AT FR66 TO FR70 IAW SRM 51-72-11-911-001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,179 hrs · 23,292 cycles

CORROSION AT FLOORBEAM - 1292 JUST FORWARD OF FR68. REPLACED 1292 FR68 FLOORBEAM IAW SRM 51-72-11 AND 51-42-11.

Part: BATTERY PACK — FAILED (CABIN) · airframe 45,505 hrs · 19,052 cycles

EPSU BATTERY 12WL FAILED CAPACITY TEST AT A8 CHECK INTERVAL. R & R THE BATTERY PACK IAW AMM 33-51-39-000-005-A & 33-51-39-400-005A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,505 hrs · 19,052 cycles

SEAT EMER EGRESS LIGHT AT ROW 8 FAILED TO ILLUMINATE DURING TEST AT A8 CHECK INTERVAL. R & R THE LAMP ASSEMBLY IAW AMM 33-51-18-000-002A & 33-51-18-400-002A.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 17,665 hrs

AIRCRAFT OUT OF SERVICE, FOUR C8/S2 CHECK. FLOORBEAM Y1292 HAS CORROSION FWD OF FR 20. REMOVED CORROSION, FLOORBEAM CHECKED OUT OF LIMITS. R & R FLOORBEAM, REF SRM 51-42-11, PARA 7.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,361 hrs · 17,665 cycles

ACFT OUT OF SERVICE FOR C8/S2 CHECK. FWD CABIN FLOOR SUPPORT -Y1292 AT FRAMES 19 - 20, CORRODED OUT OF LIMITS. R & R FLOOR SUPPORT IAW SRM 51-42-11. PARA 5 AND PARA 7.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,361 hrs · 17,665 cycles

ACFT OUT OF SERVICE FOR C8/S2 CHECK. AFT CABIN FLOORBEAM -Y1292 AT FRAME 68, CORRODED OUT OF LIMITS. R & R FLOORBEAM IAW SRM 51-42-11, PARA 7B AND PARA 5.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 42,361 hrs · 17,665 cycles

ACFT OUT OF SERVICE DUE TO C8/52 CHECK. LT ELEVATOR THERMOGHRAPHIC INSPECTION REVEALED INDICATION THAT IS IRREGULAR IN SHAPE AND BLACK IN COLOR, ON UPPER SKIN. SEE NOT REPORT FOR DETAILS. REPAIRED LT ELEVATOR AT 1EA AREA OF LIQUID INGRESS IAW SRM 55-20-00, PB201, PAR 2.A, 1, A-C, 2A, 2,A-J, 2.B, 1, 2.B,2,A)(1-10), 2.B(3)(A-G), 2.D(1)(3-9,11-12,14-15) AND SRM 55-21-11, PB201, C.L, PAR 5.D, 2, D-E, FIG 204 AND CMM 55-21-15-200-801-A02, SUBTASK 55-21-15-210-010-G01, SECTION A1-5, 6,A, 7-8,9, B WITH HOT BONDER.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 42,361 hrs · 17,665 cycles

ACFT OUT OF SERVICE FOR C8/S2 CHECK. RT ELEVATOR THERMOGHRAPHIC INSPECTION REVEALED 2EA INDICATIONS IRREGULAR IN SHAPE AND BLACK IN COLOR, ON UPPER SKIN. SEE NDT REPORT FOR DETAILS. CORRECTIVE ACTION: REPAIRED RT ELEVATOR AT 2EA AREA OF LIQUID IAW SRM 55-20-00, PB201, PAR 2A 2A-C, 2.A2, A-J, 2.B1, 2.B2A,1-10, 2.B3, A-G, 2.D1, 3-9, 11-12, 14-15 AND SRM 55-21-11, PB201, C.1, PAR 5.D2,D-E, FIG204 AND CMM 55-21-15-200-801-A02, SUBTASK 55-21-15-210-010-G01, SECTION A1-5, 6, A, 7-8,9, B WITH HOT BONDER.

Part: ELT — NO TEST (ZONE 200) · airframe 42,361 hrs · 17,665 cycles

ACFT OUT OF SERVICE, FOR C8/S2 CHECK. EMERGENCY LOCATOR TRANSMITTER WILL NOT TURN ON. R & R EMERGENCY LOCATOR TRANSMITTER REF AMM 25-65-35, PAGE BLOCK 401, CONFIGURATION 00. OPS CHECK NORMAL, REF AMM 25-65-00-740-051-G.

Part: SHEAR PLATE — CRACKED (ZONE 200) · airframe 42,361 hrs · 17,665 cycles

ACFT OUT OF SERVICE, FOR C8/S2 CHECK. AFT CABIN LT LATERAL SHEAR PLATE CRACKED. R & R IAW SRM 51-42-11, PARA 6, 7 AND 13.

Part: SHEAR PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,361 hrs · 17,665 cycles

AIRCRAFT OUT OF SERVICE FOR C8/S2 CHECK. AFT CABIN RT LATERAL SHEAR PLATE HAS CORROSION. R & R IAW SRM 51-42-11, PARA 6, 7 AND 13.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,361 hrs · 17,665 cycles

ACFT OUT OF SERVICE FOR C8/S2 CHECK. MAIN CABIN AFT SECTION R2 DOOR SILL HAS CORROSION IN TWO AREAS AT FRAME 68. REPAIRED IAW SRM 53-41-14, FIG 201, SHEET 1 AND FIGURE 201, SHEET 3.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,361 hrs · 17,665 cycles

AIRCRAFT OUT OF SERVICE FOR C8/S2 CHECK. MAIN CABIN FLOORBEAM, Y254 HAS CORROSION AT FRAME 16. REPAIRED FLOORBEAM IAW SRM 53-11-15 PB201.

Part: LOCK — DIRTY (ZONE 800) · airframe 42,361 hrs · 17,665 cycles

DURING C8/S2 CHECK. AFT ENTRY DOOR FAILS OPS TEST OF THE INTERLOCK MECHANISM. DISASSEMBLED, CLEANED AND REASSEMBLED, EMERGENCY CONTROL HANDLE IAW AMM 52-13-22-000-002-A, PARA 4.A.(4), AMM 52-13-22-400-001-A, PARA 4.F (18) THROUGH (21) AND AMM 52-10-00-710-002-A. OPS TESTED GOOD.

Part: CONTROL PANEL — DAMAGED (ELT) · airframe 42,361 hrs · 17,665 cycles

EMERGENCY LOCATOR TRANSMITTER TEST SWITCH IS INOPERATIVE. R & R EMERGENCY LOCATOR TRANSMITTER REMOTE CONTROL PANEL IAW AMM 25-65-18-020-050-A STEP A AND INSTALLED IAW AMM 25-65-18-420-050-C, STEP A. OPS CHECKED GOOD IAW AMM 25-65-00-740-051-G.

Part: CASTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,855 hrs · 16,993 cycles

FORWARD CARGO DOOR OPENING LOWER AFT CORNER FRAME CRACKED AND CORRODED AT FASTENER HOLE. REMOVED DAMAGED CORNER CASTING. MATCH DRILLED AND INSTALLED NEW CORNER CASTING FORWARD CARGO DOOR CUT OUT AFT LOWER CORNER IAW SRM 51-42-11 AND SRM 51-44-11.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 36,302 hrs · 15,056 cycles

C-CHECK: FWD CARGO BETWEEN FRAME 27 AND FRAME 28 DOOR SILL HAS CORROSION. R & R DOOR SILL IAW SRM 51 -42-11, SRM 51 -44-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,209 hrs · 12,987 cycles

C-CHECK: NON ROUTINE N0330 LT SHEAR PLATE AT FRAME 69 TO UPPER CABIN HAS CORROSION. REMOVED AND REPLACED LT SHEAR PLATE IAW FRONTIER E) A0-53EO-31434 REVISION ORIGINAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,209 hrs · 12,987 cycles

C-CHECK: NON ROUTINE N0289; AFT CABIN RIGHT FLOORBEAM - Y1292 FORWARD OF FRAME 68R HAS AN AREA OF CORROSION. AIRCRAFT IS IN C-CHECK AFTER CORROSION REMOVED FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED AND REPLACED FLOORBEAM -Y1292 BETWEEN FRAMES 68R AND 69R IAW A319 SRM 51-42-11 PARA 7.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,209 hrs · 12,987 cycles

C-CHECK: NON ROUTINE N0449; UPON REMOVAL OF AFT CABIN LT SHEAR PLATE AT FRAME 68L TO 69L FOUND SUPPORT CORRODED. A/C IN C-CHECK CORROSION OUT OF LIMITS. REMOVED AND REPLACED SUPPORT IAW A319 SRM 51-72-11 PARA 1-7.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 31,209 hrs · 12,987 cycles

C-CHECK: NON ROUTINE N0434; AT CARGO PIT PANEL 151HE UPPER SURFACE IS DELEMINATED. FABRICATED FLOOR PANEL IAW MC GILL IRM 9701 REVISION G, PARA 3.2 TABLE 1.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,209 hrs · 12,987 cycles

C-CHECK: NON ROUTINE N0331; AFT MAIN CABIN RT SHEAR PLATE AT FRAME 69R TO 70R HAS CORROSION. AIRCRAFT IS IN C-CHECK, SHEAR PLATE ALSO OLD CONFIGURATION. REMOVED AND REPLACED SHEAR PLATE IAW FRONTIER EO A)-53EO-31434 REV ORIGINAL AND A319 SRM 51-42-11.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,209 hrs · 12,987 cycles

C-CHECK: NON ROUTINE N0420; UPON REMOVAL OF SHEAR PLATE AT FRAME 68R TO 69R FOUND SUPPORT CORRODED. AIRCRAFT IS IN C-CHECK AND CORROSION IS OUT OF LIMITS. REMOVED AND REPLACED SUPPORT IAW A319 SRM 51-72-11 PAGE 1 & PAGE 2.

Part: PLENUM — CRACKED (AC BAY) · airframe 31,225 hrs · 12,996 cycles

PILOT REPORT: PACK NR 1 PRODUCING SMOKE AND FUMES AFTER NR 1 ENGINE START. AIRCRAFT RETURNED TO BLOCK, REMOVED AND REPLACED NR 1 PACK PLENUM CHAMBER, IAW AMM 21-52-22 PB 401.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 25,258 hrs · 10,576 cycles

DURING C5 C-CHECK, INSPECTION NOTED THAT THE EMERGENCY POWER SUPPLY UNIT AT POSITION 13WL FAILED THE CAPACITY CHECK. MAINTENANCE REMOVED FAILED BATTERY AND INSTALLED NEW, REFERENCE AMM 33-51-38-400-002. MAINTENANCE PERFORMED SATISFACTORY OPERATIONAL TEST, REFERENCE AMM 33-51-38-710-052.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 23,727 hrs · 9,953 cycles

PILOT REPORTED THAT THE DEICING CREW STARTED DEICING THE AIRCRAFT BEFORE CONTACT WITH THE COCKPIT CREW. SMOKE FILLED COCKPIT AND MID-CABIN. AN ALARM WAS RECEIVED FROM THE PARTICLE SENSORS IN THE AFT AND FORWARD CARGO AREA. PILOT TURNED OFF THE APU BLEED AND ALL PROBLEMS WENT AWAY. MAINTENANCE WAS CALLED TO INSPECT THE AIRCRAFT. MAINTENANCE OPERATED THE PACK SYSTEM AND SMOKE ODOR DISSIPATED. MAINTENANCE RESET CIRCUIT BREAKERS C7 AND S22 FOR CARGO SMOKE DETECTION SYSTEM AND PERFORMED OPERATIONAL TEST OF THE SAME. NO FAULTS NOTED IN ACCORDANCE WITH AMM 26-16-710-003.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 23,275 hrs · 9,758 cycles

LINE MAINTENANCE NOTED THAT MULTIPLE EMERGENCY LIGHTS FAILED TO ILLUMINATE IN CABIN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT AT POSITION 11WL IN ACCORDANCE WITH AMM 33-51-38-400-001. ALL EMERGENCY LIGHTS WORK NORMALLY.

Part: UPLOCK HOOK — DAMAGED (L2 DOOR SLIDE) · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED THAT UPON INSTALLATION OF THE L2 DOOR SLIDE, THE L2 DOOR HANDLE COULD BE MOVED INTO THE CLOSED POSITION BEFORE THE DOOR WAS IN THE HOLE. REMOVED AND REPLACED L2 DOOR UP-LOCK HOOK IAW 52-11-21-400-001, SUBTASK AMM 52-11-21-420-052.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM Y503.2 CORRODED ON UPPER SURFACE BETWEEN FRAMES 14 AND 16. DETERMINED CORROSION ON DUMMY RAIL Y503.2 TO BE OUT OF LIMITS IAW A319 SRM 53-11-14, FIG 106. REMOVED AND INSTALLED DUMMY RAIL Y503.2 IAW 51-42-11, AND 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM Y254 CORRODED ON UPPER SURFACE BETWEEN FRAMES 16 AND 18. FABRICATED AND INSTALLED FLOOR SUPPORT REPAIR PARTS IAW SRM 53-11-14, 51-47-00, 51-23-00, 51-75-12, 51-44-11, EAR 910-4551, AND EA A9-53R-12224.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 262FF CORRODED ON BOTTOM SIDE. REMOVED AND REPLACED FLOOR PANEL 262FF IAW WORK CARD CP753-36 AND AMM 53-42-12-PB401.

Part: NUT PLATE — CORRODED (L2 DOOR SILL) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION IN THE AFT OTBD NUTPLATE HOLE OF THE L2 DOOR SILL FWD GIRT BAR FITTING MOUNT PLATE. PERFORMED ROTO PROBE INSPECTION ON HOLE IAW NTM 51-10-01, PAGES 601-622 AND AND FOUND A CRACK BETWEEN RIVET HOLE AND FASTENER HOLE. REMOVED DAMAGE AND PERFORMED HFEC, NO DEFECTS FOUND. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AND INSTALLED NEW NUTPLATE ON REPAIR DOUBLER. WORK ACCOMPLISHED IAW SRM 53-41-14, 51-74-00, 51-10-01, 51-10-08, 51-11-13, 51-75-12, 51-42-11 AND EA A9-53R-12218.

Part: BLANKING PLATE — CORRODED (L1 GIRT BAR) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON L1 DOOR GIRT BAR FITTING AFT BLANKING PLATE. REMOVED AND REPLACED L1 DOOR AFT GIRT BAR BLANKING PLATE IAW AMM 53-11-31-PB401.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED SUPPORT FRAME AT FR70 CORRODED ON UNDERSIDE AT NUTPLATE CUTOUT, WHICH WAS FOUND AFTER REMOVAL OF THE SHEAR WEB. REMOVED SUPPORT FRAME AT LT SIDE OF FR70 IAW A319 SRM 51-42-11. DETERMINED TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 2. INSTALLED SHEAR PLATE TO NEW SUPPORT FRAME IAW SRM 51-72-11 AND 51-42-11.

Part: BLANKING PLATE — CORRODED (R1 GIRT BAR) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON R1 DOOR GIRT BAR FITTING AFT BLANKING PLATE. REPLACED R1 DOOR AFT GIRT BAR FITTING BLANKING PLATE IAW AMM 53-11-31-PB401.

Part: NUT PLATE — CORRODED (R2 DOOR SILL) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION IN THE AFT OTBD NUTPLATE HOLE OF THE R2 DOOR SILL FWD GIRT BAR FITTING MOUNT PLATE. PERFORMED HFEC ON DAMAGED AREA IAW NTM 51-10-08, PAGES 601-608, AND FOUND NO DEFECTS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-42-11, 53-41-14, 51-74-00, 51-11-13, 51-21-11 AND EA A9-53R-12220.

Part: BLANKING PLATE — CORRODED (L2 GIRT BAR) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON L2 DOOR GIRT BAR FITTING BLANKING PLATE. REMOVED AND REPLACED L2 DOOR BLANKING PLATE IAW AMM 53-11-31-PB401.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR WEB AT FR 70L CORRODED. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11 AND 51-72-11.

Part: SUPPORT — CORRODED (FUSLEAGE) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AT FLOOR WEB NUTPLATE IN FWD CARGO COMPARTMENT, AFT RT CORNER, WHERE TRANSITION PANEL, AFT CARGO WALL AND FLOOR MEET. REMOVED CORRODED TRANSITION STRIP AT AFT BULKHEAD IAW SRM 51-42-11, PARA. 6. INSTALLED NEW TRANSITION STRIP AT AFT BULKHEAD IN FWD CARGO COMPARTMENT IAW SRM 51-42-11, PARA 6 AND 17.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM BETWEEN FRAME 68R AND 69R CORRODED. BLENDED CORRODED AREA AND FOUND FLOORBEAM TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 102. REMOVED AND INSTALLED FLOORBEAM IAW SRM'S 51-42-11, 51-44-00, AND 51-72-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 221FF CORRODED ON LOWER SURFACE, FWD EDGE. REMOVED AND REPLACED FLOOR PANEL 221FF IAW AIRBUS AMM 53-12-12-400-001, 53-12-12-PB401, AND WORK CARD CP753-12.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AT FWD CARGO COMPARTMENT FLOOR WEB NUTPLATES, RT SIDE WHERE TRANSITION PANEL AND FLOOR MEET, BETWEEN FR 28 AND FR 29. REMOVED AND REPLACED CORRODED TRANSITION STRIP IAW SRM 51-42-11 AND 51-44-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM AT FR67R CORRODED IN NUTPLATE HOLES. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, PARA 5, AND 71-72-11.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED SHEAR WEB AND SUPPORT PLATE AT FR70R BLOWN OUT FROM CORROSION. REMOVED AND REPLACED SHEAR PLATE SUPPORT IAW SRM 51-42-11, PARAGRAPHS 6, 7, AND 77, AND DWG D53474180.

Part: SILL — CORRODED (R2 DOOR) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION IN R2 DOOR SILL NUTPLATE HOLE AT FR 66. BLENDED MATERIAL AT FWD END OF R2 DOOR SILL AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG. 101. FABRICATED REPAIR FILLER IAW SRM 53-41-14, FIG. 201, REPAIR PRINCIPLE NR 6 (SHEET 4). FABRICATED REPAIR ANGLES IAW SRM 53-41-14, PAGES 215/216, AND SRM 53-41-14, PAGE 217, FIG 201. REPAIR COMPLETED IAW SRM 53-41-14, FIG. 201, REPAIR PRINCIPAL NR 6 (SHEETS 1 AND 4).

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CABIN FLOORBEAM AT FR 69 RT CORRODED IN NUTPLATE HOLE. REMOVED AND REPLACED FLOORBEAM IAW SRM 53-00-14, FIG. 102, 51-42-11 AND 51-72-11.

Part: THRESHOLD — CORRODED (R1 DOOR) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED R1 DOOR THRESHOLD STRIP CORRODED ON LOWER SURFACE. REMOVED AND REPLACED R1 DOOR THRESHOLD STRIP IAW MM 53-12-12-400-001.

Part: THRESHOLD — CORRODED (L1 DOOR) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED L1 DOOR THRESHOLD STRIP CORRODED ON LOWER SURFACE. REMOVED AND REPLACED L1 DOOR THRESHOLD STRIP IAW AMM 53-12-12-400-001.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION AT FLOOR WEB NUTPLATE IN FWD CARGO COMPARTMENT AT FR 28, 6" INBD OF C1 DOOR CUTOUT. REMOVED AND REPLACED TRANSITION STRIP IAW SRM 51-42-11, 51-72-11 AND 51-21-11.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOOR PANEL 222FF CORRODED ON LOWER SURFACE, FWD EDGE. REMOVED AND REPLACED FLOOR PANEL IAW AMM 53-12-12-PB401 AND WORK CARD CP753-12.

Part: BLANKING PLATE — CORRODED (R2 GIRT BAR) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON R2 DOOR FWD AND AFT GIRT BAR PADS. REMOVED AND REPLACED FWD AND AFT R2 DOOR GIRT BAR BLANKING PLATES IAW AMM 52-13-31-PB401 AND 52-13-31-400-007.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED FLOORBEAM BETWEEN FR 68 AND FR 69 AT Y1292, INBD AND AFT OF L1 DOOR FRAME, CORRODED. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, PARA 7.

Part: WIRE HARNESS — DAMAGED (R1 DOOR SLIDE) · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED R1 DOOR SLIDE ELECTRICAL HARNESS CAME FROM THE FACTORY PINCHED IN THE SLIDE ASSY, AND CANNOT BE ROUTED AS SHOWN IN AMM FIG 25-62-44-911-003, SHEET 404.2/3. REMOVED AND REPLACED DAMAGED R1 DOOR SLIDE IAW AMM 25-62-44-400-007.

Part: SKIN — DENTED (FUSELAGE) · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED A SMALL DENT IN THE LT FUSELAGE AT FR 15, STR30, AFT AND ABOVE 02 SERVICE DOOR. REMOVED PAINT FROM AREA IAW SRM 51-75-11 AND BLENDED AREA IAW SRM 51-73-00. DEPTH OF DENT IS .007, SIZE OF DENT IS .4" WIDE BY .5" LONG, 10" FROM CORNER OF DOOR CUTOUT AREA. PERFORMED HFEC ON BLENDED AREA IAW NTM 51-10-08, PART 6, NO CRACKS NOTED. REMOVED TWO FASTENERS, AND PERFORMED ROTOPROBE TEST OF BOTH HOLES IAW NTM 51-10-01, PAGES 601-622, NO FAULTS FOUND. ACCOMPLISHED IAW EA A9-53R-12213.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,360 hrs · 8,205 cycles

DURING C4/S1 CHECK, INSPECTION REPORTED CORROSION ON UPPER SURFACE OF FLOORBEAM Y254, BETWEEN FRAMES 16 AND 18. BLENDED 3 AREAS ON FLOOR SUPPORT Y254, ALL FOUND TO BE OUT OF LIMITS PER SRM 53-11-14-FIG 104. CUT OUT CORRODED UPPER CAP SECTION OF FLOOR SUPPORT IAW SRM 53-11-14, PARA 5 AND FIG 201. FABRICATED REPAIR PARTS AND INSTALLED FLOOR SUPPORT REPAIR IAW SRM 53-11-14, 51-47-00, 51-23-00, AND EAR 910-4551.

Part: SLIDE — INOPERATIVE (L2 DOOR) · airframe 13,494 hrs · 5,717 cycles

DURING C-3 CHECK, INSPECTION REPORTED LT AFT EPSU INDICATED EXTERNAL FAULT ON PTP DURING OPERATIONAL CHECK OF EMERGENCY LIGHTS AT L2 DOOR/ESCAPE SLIDE. REPLACED SLIDE RAFT ASSY AT L2 DOOR.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 13,494 hrs · 5,717 cycles

DURING C-3 CHECK, INSPECTION REPORTED SURFACE CORROSION ON SUPPORT CHANNEL FOR R-1 THRESHOLD AT ATTACH HOLE. BLENDED CORROSION ON SUPPORT CHANNEL, TREATED, PRIMED AND PAINTED PER EA A9-53R-11365.

Part: SMOKE — DETECTED (CABIN) · airframe 9,852 hrs · 4,222 cycles

FLIGHT ATTENDANTS AND PASSENGERS REPORTED ODOR OF SMOKE ON FLIGHT FROM MZT TO DEN. FLIGHT CREW DECLARED AN EMERGENCY AND DIVERTED TO ELP. AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOT SMOKE IN CABIN PER MM 26-17-00-810-804, LAV SMOKE WARNING, NO DEFECTS NOTED; AND PER MM 12-33-21-618-09-02, PRECONDITIONING CHECK OF APU, NO DEFECTS NOTED; AND PER MM 31-50-00-710-01, GROUND SCANNING OF CENTRAL WARNING SYSTEM, NO DEFECTS NOTED.

Part: FAN BLADE — BENT (NR 2 ENGINE) · airframe 5,247 hrs · 2,280 cycles

DURING CLIMBOUT, FLIGHT CREW REPORTED ABNORMAL NR 2 ENGINE NOISE (NO ABNORMAL ENGINE VIBRATION). FOUND FAN BLADES BENT DUE TO ICE INGESTION. REPLACED NR 2 ENGINE FAN BLADES PER MM 72-21-00-300-028, PERFORMED NR 2 ENGINE TRIM BALANCE PER MM 77-32-34-750-001 AND CHECKED NORMAL.