N314US

Part: SKIN — DENTED (FUSELAGE) · airframe 78,685 hrs · 35,837 cycles

DENT ON EXTERNAL SKIN LOC AT FR 79 BTW STR 4L TO STR 5L ON UPPER FUSELAGE, PERFORMED REPAIR ON EXTERNAL SKIN LOCATED AT FR 79 BTW STRINGER 4L TO 5L ON UPPER FUSELAGE AS PER SRM 53-51-11 PARAGRAPH 5B FIGURE 203.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 78,685 hrs · 35,837 cycles

CRACK INDICATION IN AFT HOLE OF SIDE BOX BEAM UPPER FLANGE, ON FRAME 43 LT SIDE. CRACK DIRECTION: FWD ON CENTER WING BOX, REPLACED PRESSURE PLATE LOC ON FR 43 LT SIDE AS PER SRM 51-72-11 AND JOB CARD 5310-014-50-02-DE

Part: BOX BEAM — CRACKED (FRAME 43) · airframe 78,680 hrs · 35,836 cycles

CRACK INDICATION IN CENTER HOLE OF SIDE BOX BEAM UPPER FLANGE, ON FRAME 43 L/H SIDE. CRACK DIRECTION: AFT. ON CENTER WING BOX, REPAIR PER AMDS 5310-01450-02 IN ACCORDANCE WITH SB A320-53-1251 REV 1

Part: BOX BEAM — CRACKED (FRAME 43) · airframe 78,680 hrs · 35,836 cycles

CRACK INDICATION IN CENTER HOLE OF SIDE BOX BEAM UPPER FLANGE, ON FRAME 43. THE BOX BEAM WAS REPAIRED IAW SB A320-53-1251 REV 1.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,470 hrs · 35,175 cycles

LEFT EMERGENCY LIGHT BATTERY FAILED. REPLACED THE BATTERY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,585 hrs · 34,250 cycles

INTERIOR AFT LEFT BATTERY, DURING SERVICE CHECK ON F/A PANEL, REPLACED EPSU 13WL BATTERY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,057 hrs · 32,971 cycles

DURING NON-ROUTINE CHECK, FOUND SEAT 18 ABC EMERGENCY LIGHT INOPERATIVE. SECURED, REPLACED THE LAMP AND FUNCTIONAL CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,491 hrs · 32,719 cycles

DURING NON ROUTINE CHECK, FOUND LT EPSU AND THE EMERGENCY LIGHT, EXTERIOR, UNDER AFT LT EMERGENCY DOOR INOPERATIVE. MAINTENANCE REPLACED LT EPSU AND BATTERY PACK; OPS CHECK WAS NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 72,473 hrs · 32,711 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE AT ROWS 19 & 20. REPAIRED BROKEN WIRE AND FUNCTIONAL CHECKED NORMAL.

Part: B-NUT — LEAKING (HYD SYSTEM) · airframe 71,792 hrs · 32,380 cycles

AFTER LANDING, THE CREW CONTACTED MAINTENANCE AND ADVISED THAT THEY HAD DONNED THEIR OXYGEN MASKS DUE TO AN OIL ODOR. REPORTED PASSENGERS WERE GETTING SICK DUE TO THE ODOR. MAINTENANCE FOUND HYDRUALIC FLUID IN INTAKE DUCT AND PLENUM OF APU. ALSO FOUND LT GEAR B-NUT ON ACTUATOR LOOSE; SECURED AND SAFTIED B-NUT. REPLACED CATALITIC CONVERTOR, APU OIL COOLER AND FUNCTIONAL CHECK WAS NORMAL.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT FUSELAGE, UNDERFLOOR FR66 AT STR26R AREA HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED DIMENSIONS L=0.90" W=0.450" D=0.20". NO ALLOWABLE DAMAGE LIMITS IN SRM. ACCOMPLISHED REPAIR IAW ER/A 510352-14, REV ORIGINAL SECTION I PERMANENT REPAIR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO COMPT AT FR33 BET STR 40R AND STR 41R SHEAR TIE HAS CORROSION. REPLACED SHEAR TIE IN FWD CARGO COMPT AT FR33 BETWEEN STR 40R & 41R IAW SRM 51-42-11. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=0.90" W=0.30" D=0.009" NO ALLOWABLE LIMITS IN SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO COMPT AT FR312 BET STR 41R AND STR 40R, SHEAR TIE HAS CORROSION. REPLACED SHEAR TIE AT FR31 BETWEEN STR 41R-40R IAW SRM 51-42-11. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=1.30" W=0.35" D=0.008" NO ALLOWABLE DAMAGE LIMITS IN SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO COMPT AT FR32 BET STR 41R AND STR 42R SHEAR TIE HAS CORROSION. REPLACED SHEAR TIE IN FWD CARGO COMPT AT FR32 BETWEEN STR 41R & STR 42R IAW SRM 51-42-11. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=0.50" W=0.40" D=0.010" NO ALLOWABLE DAMAGE LIMITS IN SRM.

Part: SHEAR TIE — CORRODED · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO BAY AT FR31 BETWEEN STR 43R AND STR 42R, SHEAR TIE HAS CORROSION. BLENDED CORROSION ON SHEAR TIE AT FR31 BTW STR 43R AND 42R, FOUND TO BE OUT OF LIMITS IAW SRM 51-74-00 L=.960" W=.670" D=.007". FABRICATED NEW SHEAR TIE ON TRAVELER T13/982442 2024-T42 .063" BATCH NR 758572, LOCATED AND DRILLED SHEAR TIE IAW SRN 51-44-11, TREATED AND PRIMED NEW SHEAR TIE IAW SRM 51-21-11 AND TOP COATED IAW SRM 51-75-12. INSTALLED NEW SHEAR TIE IAW SRM 51-42-11, PRIMED AND TOPCOATED FASTENERS IAW SRM 51-21-11 AND 51-75-12.

Part: PLATE — CHAFED (PAX DOOR) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND RT AFT PASSENGER DOOR UPPER SIDE, FWD EDGE OF CLOSING PLATE HAS CHAFE MARK. DAMAGE DIMENSION L=3.5" W=.50" D=0.006" NO ALLOWABLE LIMIT IN THIS AREA IAW SRM 52-10-00, TABLE 101. REPLACED PLATE COVER IAW DWG 5211475 & AMM 52-13-18. RESTORED FINISH IAW SRM 51-21-11 & SRM 51-75-12.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO COMPT AT FR32 BET STR 40R AND STR 41R SHEAR TIE HAS CORROSION. REPLACED SHEAR TIE AT FR32 BETWEEN STR 40R-41R IAW SRM 51-42-11. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=1.0" W=0.30" D=0.006" NO ALLOWABLE DAMAGE LIMITS IN SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO COMPT AT FR 31 BET STR 43R AND STR 42R, SHEAR TIE HAS CORRSIOON. RII: BLENDED CORROSION ON SHEAR TIE AT FR 31 BET STR 43R AND 42R IAW SRM 51-74-00,L=.960"W=.670"D=.007" NO ESTABLISHED LIMITS ON SRM. FABRICATED NEW SHEAR TIE ON TR NR T13/982442 MAT.2024.D .063C BATCH NR 0001942024. LOCATED AND DRILLED SHEAR TIE IAW SRM 51-44-11. TREATED AND PRIMED NEW SHEAR TIE IAW SRM 51-21-11. APPLIED TOP COAT TO NEW SHEAR TIE IAW SRM 51-75-11. INSTALLED NEW SHEAR TIE IAW SRM 51-42-11. PRIMED FASTENERS IAW 51-21-11 APPLIED TOP COAT TO FASTENERS IAW 51-75-12.

Part: SHEAR TIE — CORRODED · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO BAY AT FR32 BETWEEN CENTER LINE AND STR 43R, SHEAR TIE HAS CORROSION. R & R SHEAR TIE IAW SRM 51-42-11 DAMAGE DIM; L=1.5" W=1.020" D=.020". NO ALLOWABLE LIMITS ESTABLISHED IN SRM.

Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND MCD FLOOR PANEL 241EF DELAMINATED AT AFT END. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D2537498. (DAMAGE DIM. L=12.0" W=8.0").

Part: SHEAR TIE — CORRODED (FWD CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO AT FR 31 BETWEEN CENTERLINE AND STR 43R, SHEAR TIE HAS CORROSION. CHECKED LIMITS L=1.00" W=1.00" D=0.010" NO ALLOWABLE DAMAGE IAW SRM 53-21-12. INSTALLED FABRICATED SHEAR TIE ON STAM TRAVELER T13/982826 MAT 2024-0 .063C BATCH 1942022 HEAT TREATED TO T4 IAW AMS 27705 IAW SRM 53-21-12 AND SRM 51-42-11.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO BAY BET FR28 AND FR29, STR 43L AND STR 43R, PORTABLE WATER DOUBLER HAS CORROSION. REPLACED STAMPING P/N D532309352000 BATCH 2385934 IAW SRM A320 51-42-11, 51-44-11 AND DWG D53230935.

Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT UTILITY RT DOOR SILL AFT GIRT BAR ATTACH HOLES, 3EA HAVE CORROSION. REMOVED CORROSION IAW SRM 51-74-00, FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 101 ORIG MAT .236" MAT LOSS 100 PERCENT OF THICKNESS. REPLACED DOOR SILL PN D5348004320701, BATCH 1820031, IAW SRM 51-42-11 & 51-44-11.

Part: FLOOR SUPPORT — CORRODED · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT FUSELAGE UNDERFLOOR BET FR66 AND FR67, STR 26R HAS CORROSION. REPLACED STRINGER, PN D5348004720201, BATCH: 0002384124 IAW SRM 51-42-11 AND DWG D53480024. FABRICATED NEW CLEAT CLIP ON STAM TRAVELER T13/979626, MAT 2024-0 .071C BATCH 0001942001, FABRICATED NEW CONNECTING SECTION ON STAM TRAVELER T13/979625, MAT 2024--T351/3X3. BATCH 0002185878. STRINGER DAMAGE DIMENSION L=18" W=1.0" D=0.040" NO ALLOWABLE DAMAGE LIMITS ESTABLISHED.

Part: SHEAR TIE — CORRODED (FWD CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO AT FR32 BET STR 42R AND STR 43R SHEAR TIE HAS CORROSION. REPLACED 1EA SHEAR TIE IAW SRM 51-42-11. DAMAGE DIMENSION L=1 W=.800 D=0.070 NO ESTABLISHED LIMITS ON SRM.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND RT AFT EMERGENCY EXIT DOOR, FWD LOAD TRANSMITTING PROFILE HAS CRACKED. RM 51-44-11, INSTALLED NEW PROFILE IAW SRM 51-42-11, TOUCHED UP PAINT ON FASTENER HEADS COMMON TO EXTERIOR SKIN IAW SRM 51-21-11.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CARGO REAR DOOR ACTUATOR FWD FRAME MOUNT BRACKET HAS CRACK. REPLACED BRACKET IAW SRM 51-42-11. CRACKED LENGTH = 1". P/N D5347212720600.

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND RT AFT FUSELAGE LAV VENT HAS CORROSION ON SKIN SURFACE. PERFORMED REPAIR IAW SRM 53-41-11 FIG 205. BLENDED AREA IAW SRM 51-74-00. CHECKED LIMITS DEPTH: 0.011" MAX ALLOW 0.06" FOUND TO BE OUT OF LIMITS IAW SRM 53-41-11, DIAGRAM 102 SHEET 1, CUT OUT DAMAGE SKIN IAW SRM 53-41-11, STEP 2E; FABRICATED REPAIR PARTS 1EA DOUBLER MAT 2024-T3. .071C BATCH 000213529 AND 2 EA FILLER MAT 2024-T3 .063C BATCH 0002339436 IAW SRM 53-41-11; INSTALLED REPAIR PARTS IAW SRM 51-42-11 & SRM 53-41-11 DIMENSION OF CUT OUT L; 2" W; 1".

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151PF DAMAGED 12" X 24". FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: PANEL — DELAMINATED (AFT CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151MF DELAMINATED 6" X 4". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT PIT FLOOR PANEL 151GF DAMAGED 1" X 2" AND HAS DAMAGED INSERT. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: PANEL — CRACKED (FWD CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FORWARD CARGO SLOPE PANEL 131JF CRACKED 6.0" LONG. FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: PANEL — DAMAGED (AFT CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 152CF, DAMAGED 12" X 12". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: PANEL — DAMAGED (AFT CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151EF DAMAGED 12" X 12". FABRICATED SLOPE PANEL 151EF ON STAM TRAVELER T13/979335. MATERIAL A402AB-60X144, BATCH 2335662, DWG 3D25-37705.

Part: PANEL — DAMAGED (AFT CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 152QF DAMAGED 6" X 4". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: PANEL — DAMAGED (AFT CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 152EF DAMAGED 12"X36". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131 EF DELAMINATED 40"X3.5". FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: PANEL — DAMAGED (FWD CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 131FF DAMAGE AT TDP. FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: PANEL — DAMAGED (AFT CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151FF DAMAGED 12" X 6". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: PANEL — PUNCTURED (FWD CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 131KF PUNCTURED 2.0" X 1.0". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: PANEL — DELAMINATED (AFT CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151 HF DELAMINATED 8" X 4". FABRICATED SLOPE PANEL 151 HF ON STAM TRAVELER T13/979331. MATERIAL A402AB-60X144, BATCH 2335662, DWG 3D25-37705.

Part: PANEL — DAMAGED (AFT CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151RF DAMAGED 4" X 4". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131AF DAMAGED TDP. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: PANEL — DAMAGED (FWD CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 131CF DAMAGED AT TDP. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: PANEL — CRACKED (FWD CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 132GF CRACKED 1.0". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: PANEL — DAMAGED (FWD CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 132KF DAMAGED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: PANEL — DELAMINATED (AFT CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151 NF DELAMINATED 4" X 4". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: PANEL — DAMAGED (FWD CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO SLOPE PANEL 132JF HAS DAMAGE AT TDP. FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: PANEL — DAMAGED (AFT CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151CF DAMAGED 12" X 12". FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 132 FF, DAMAGED 2.0"X2.0". FABRICATED FLOOR PANEL IAW DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 221PF DAMAGED/DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CABIN FLOOR PANEL 262AB DAMAGED & DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.

Part: SHACKLE — GOUGED (NR 2 PYLON) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND NR 2 ENG PYLON AFT SHACKLE 1EA SIDE HAS GOUGED MARK AROUND THE BUSHING HOLE. BLENDED DAMAGE IAW SRM 51-73-00, CHECKED LIMIT DIMENSION DEPTH=.010" MAX ALLOW .006". FOUND TO BE OUT OF LIMIT IAW ER/A 507720-14MA. RECEIVED NEW SHACKLE INSTALLED ON JIC 5450-6010-RT.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CABIN FLOOR PANEL 261PF DAMAGED & DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CABIN FLOOR PANEL 261EF DAMAGED/DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CABIN FLOOR PANEL 262EF DAMAGED & DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CABIN FLOOR PANEL 261DF DAMAGED/DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND MAIN CABIN FLOOR PANEL 231BF DELAMINATED 4.0" X 6.0". FABRICATED NEW FLOOR PANEL 231BF ON STAM TRAVELER NR T13/981225 IAW SRM 53-02-00, FIG 209. DAMAGE DIMENSION LENGHT=6" WIDTH 4" & DWG NR 3D25-37498.

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 221EF DELAMINATED 4" X 6". FABRICATED NEW FLOOR PANEL 221EF ON STAM TRAVELER NR T13/981226 IAW SRM 53-02-00, FIG 209. DAMAGE DIMENSION LENGTH=6", WIDTH 4" & DWG NR 3D25-37498.

Part: FLOORBOARD — DELAMINATED (AFT CABIN) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CABIN FLOORBOARD 252GF DELAMINATED ON UNDERSIDE AROUND FASTENER HOLE. FABRICATED NEW FLOORBOARD IAW SRM 53-02-00, FIG. 209.

Part: FLOOR SUPPORT — CRACKED · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND COCKPIT AREA AT FR11+Y765, FLOOR SUPPORT WEB CRACKED. CHECK LIMITS ON CRACK AND LENGTH .815" IS OUT OF LIMITS. REMOVED FLOOR WEB SUPPORT, LOCATED, DRILLED AND INSTALLED NEW SUPPORT WEB AT FR1 1 +Y765 IAW SRM 53-11-14, 51-42-11 AND 51-44-11 AT FR11 +Y76 5.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND COCKPIT AREA AT FR11 FLOOR SUPPORT WEB CRACKED AT -Y765. CHECK LIMITS ON CRACK LENGTH .57" AND OUT OF LIMITS. REMOVED FLOOR WEB SUPPORT, DRILLED AND INSTALLED NEW FLOOR WEB SUPPORT IAW SRM 53-11-14,51-42-11 AND 51-44-11 AT FR11 +Y765. RETAIN.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT UTILITY FLOOR SUPPORT -Y1292 BETWEEN FR 66 AND FR 68 HAS CORROSION AROUND FASTENERS AND HOLES AT FR 68 SPLICE. REMOVED CORROSION IAW SRM 51-74-00. CHECK LIMIT L=3.0"W=2.0" D=0.030" FOUND OUT OF LIMIT IAW 53-00-14, FIG 102. REPLACED FLOOR BEAM P/N D5347217220300, BATCH 0001786216 IAW SRM 51-42-11 & DWG NR 17D53472000.

Part: FLOOR SUPPORT — CORRODED (UTILITY AREA) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT UTILITY FLOOR SUPPORT -Y1292 BETWEEN FR 68 AND FR 70 HAS CORROSION ON BEAM AROUND FASTENERS HOLES AND UPPER FLANGE ABOVE SPL ICE. REMOVED CORROSION IAW SRM 51-74-00. CHECK LIMIT L=4.0"W=2.5" D=0.030"FOUND OUT OF LIMIT IAW A320 53-00-14, FIG 102. REPLACED FLOORBEAM IAW SRM 51-42-11 & DWG NR 17D53472000.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT UTILITY FLOOR SUPPORT -Y1292 BETWEEN FR 64 AND FR 66 HAS CORROSION AND MISDRILLED HOLE AT FR 66. REMOVED CORROSION IAW SRM 51-74-00. CHECK LIMIT L=5"W=2.0"D=0.035" FOUND OUT OF LIMIT IAW 53-00-14, FIG 102. R & R FLOORBEAM PN D5347219020590 BATCH 0002384156 IAW SRM 51-42-11 & DWG NR 17D53472000.

Part: HINGE — DAMAGED (RT AILERON) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND RT AILERON, HINGE BOLT NR 3, SCORED. SCORED BEYOND LIMITS IAW AMM 27-14-41, PB 601. RECEIVED NEW BOLT TO BE INSTALLED ON JIC 5760-1010S-RT. DIMENSIONS: L=.8750"X W=.7500".

Part: BOLT — SCORED (RT AILERON) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND RT AILERON, HINGE BOLT NR 2 SCORED. SCORED IS BEYOND LIMITS IAW AMM 27-14-41 PB 601. RECEIVED NEW BOLT TO BE INSTALLED ON JIC 5760-1010S-RT. DIMENSIONS L=.8750" X W=.7500".

Part: SPAR — CORRODED (NR 2 PYLON) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND NR 2 ENG PYLON UPPER SPAR, SPIGOT FITTING BORE PITTED. MAX DIA OF SPIGOT FITTING IS 4.335", AFTER REWORK DIA IS 4.337 " FOUND TO BE OUT OF LIMITS IAW SRM 54-51-12, FIG 101, SH. 2. REPLACED SPIGOT FITTING IAW SRM 54-51-41-400-001- A.

Part: BOLT — SCORED (RT WING) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND RT AILERON, HINGE BOLT NR 1 SCORED. SCORED IS BEYOND LIMITS IAW AMM 27-14-41, PB 601. RECEIVED NEW BOLT TO BE INSTALLED ON JIC 5760-1010S-RT. DIMENSION L=.8750"X W=.7500".

Part: TRAY — CRACKED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT UTILITY RT SIDE TRAY AT S23R AFT OF FR 68 IS CRACKED. REPLACED RT SIDE TRAY AT STR 23R AFT OF FR68 IAW SRM 51-42-11, NEW SIDE TRAY FABRICATED FROM 2024T3.063 BATCH 0002344339 IAW SRM 53-41-14.

Part: TRAY — CRACKED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT UTILITY RT SIDE TRAY AT S23R AFT OF FR68 IS CRACKED. REPLACED RT SIDE TRAY AT STR 23R AFT OF FR68 IAW SRM 51-42-11, NEW SIDE TRAY FABRICATED FROM 2024T3.063 BATCH 0002344339 IAW SRM 53-41-14.

Part: BOLT — SCORED (RT AILERON) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND RT AILERON, HINGE BOLT NR 4, SCORED. SCORED IS BEYOND LIMITS IAW AMM 27-14-41, PB 601. RECEIVED NEW BOLT TO BE INSTALLED ON JIC 5760-1010S-RT. DIMENSIONS L=.8750" X W=.7500".

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND RT AFT DOOR CUT OUT FR 68 FWD FACE HAS CORROSION APPROX 1" ABOVE DOOR SILL. REMOVED CORROSION IAW SRM 51-74-00, CHECKED LIMITS, L=1.5"X W =1"X D=.021" FOUND OUT OF LIMITS IAW SRM 53-41-12. REPAIRED IAW SRM 53-41-12, FIG 201. PRINCIPLE I, REPAIR PART FAB ON TRAVELER T13/979197 IAW SRM 53-41-12. REQUIRES FIRST INSPECTION AFTER A/C DELIVERY AT 64000 FC IAW SRI 53-41-12-2-001-00, PG 203- 204.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT UTILITY FLOOR SUPPORT -Y1732 HAS CORROSION AT FASTENER HOLE SEVEN INCHES FWD OF FR66. REPLACED FLOOR SUPPORT IAW SRM 51-42-11, TOP COAT PAINTED FASTENERS IAW SRM 51-75-12. REMOVED CORROSION IAW SRM 51-74-00 FOUND TO BE OUT OF LIMITS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT UTILITY FLOOR SUPPORT Y1292 FWD OF FR68 BETWEEN FR66 AND FR68 HAS CORROSION AROUND AND UNDER FASTENERS AT SPLICES. BLENDED CORROSION IAW SRM 53-00-14 FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REPLACED FLOOR SUPPORT IAW SRM 51-42-11 IAW TRM 53-21-01.

Part: SILL — CORRODED · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND RT AFT DOOR CUTOUT FR66 AFT FACE APPROX 1" ABOVE DOOR SILL HAS CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-41-12. REPAIR IAW SRM 53-41-12, FIG 201, REPAIR PART FAB ON TRAVELER T13/979196 IAW SRM 51-41-12. REQUIRES INSPECTION, FIRST INSP AFTER ACFT DELIVERY AT 64000FC IAW SRI 53-41-12, PG 203/204.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152KF CORRODED. REPLACED FLOOR PANEL IAW SRM 51-72-11.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FORWARD CABIN FLOOR PANEL 222FF DAMAGE AND PUNCTURED. DAMAGED DIM: L=3" W=2" D=.020" NO ESTABLISH LIMIT ON SRM. REPLACED FLOOR PANEL, IAW SRM 5 1-72-11.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 132DF CORRODED. REPLACED IAW SRM 51-72-11.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT CABIN FLOOR PANEL 262FF DAMAGED AND CORRODED. DAMAGE DIMENSIONS: L=4" W=2" D=0.015" NO ALLOWABLE LIMIT ESTABLISHED ON SRM. REPLACED FLOOR PANEL IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND AFT UTILITY FLOOR SUPPORT -Y765 BETWEEN FR66 AND FR70 HAS SIX AREAS OF CORROSION. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND TO BE OUT OF LIMITS. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FWD UTILITY AREA FRAME 20, RT WEB CORRODED. REPLACED RT WEB IN FWD UTILITY AREA WITH PN D53112 78520301 IAW SRM 51-42-11. NO ALLOWABLE DAMAGE FOUND IN SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,439 hrs · 30,165 cycles

DURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR16 TO FR21, Y1292 UPPER FLANGE HAS CORROSION. BLENDED CORROSION ON Y1292 FLOOR SUPPORT IAW SRM 51-74-00 DIM ON CROWN AT SEAT TRACK IS L=2.0 W=.375 D=.053 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15, FIG 102. REPLACED FWD CABIN FLOOR SUPPORT IAW SRM 51-42-11.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,360 hrs · 2,826 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHT AT 24C INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY AND OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 61,496 hrs · 27,364 cycles

LEFT FWD OVERWING EMERGENCY EXIT DOOR FWD LOWER VERTICAL FRAME IS CRACKED. REMOVED FWD LOWER VERTICAL FRAME IAW SRM 51-42-11. NEW VERTICAL FRAME TREATED AND PRIMED IAW SRM 51-21-11. INSTALLED NEW VERTICAL FRAME IAW SRM 51-42-11.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 61,496 hrs · 27,364 cycles

LT FWD OVERWING EMERGENCY EXIT DOOR RT PROFILE HAS CRACKS AROUND RIVETS AS MARKED. REMOVED DAMAGED PROFILE IAW SRM 51-42-11. RECEIVED AND INSTALLED NEW PROFILE IAW SRM 51-42-11.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 61,496 hrs · 27,364 cycles

(MZAR) RT AFT OVERWING EMERGENCY EXIT DOOR RT LOAD TRANSMITTING PROFILE CRACKED. REMOVED RT PROFILE IAW SRM 51-42-11. LOCATED AND DRILLED NEW ANGLE. INSTALLED NEW PROFILE ANGLE IAW SRM 51-42-11.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 61,496 hrs · 27,364 cycles

AFT CARGO FLOOR PANEL 151DF DAMAGED. REMOVED AFT CARGO FLOOR PANEL 151DF IAW SRM 51-42-11. FABRICATED NEW PANEL ON TRAVELER T11/867721 IAW NWD 3D25-37705. INSTALLED PANEL151DF IAW AMM 53-42-12-400-001.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 61,496 hrs · 27,364 cycles

AFT CARGO FLOOR PANEL 151AF DAMAGED. REMOVED AFT CARGO FLOOR PANEL 151AF IAW SRM 51-42-11. FABRICATED NEW PANEL ON TRAVELER T11/867710 IAW NWD 3D25-37705. INSTALLED PANEL.

Part: PROFILE — CRACKED (OVERWING EXIT) · airframe 61,496 hrs · 27,364 cycles

(MZAR) LT AFT OVERWING EMERGENCY EXIT DOOR RT PROFILE HAS CRACKS AROUND RIVETS AS MARKED. R & R LOAD TRANSMITTING PROFILE IAW SRM 51-42-11 PN D5227902620300 BATCH-0001982356.

Part: PROFILE — CRACKED (RT OVERWING EXIT) · airframe 61,496 hrs · 27,364 cycles

(MZAR) FWD OVERWING EMERGENCY EXIT DOOR, RT LOAD TRANSMITTING PROFILE CRACKED. R & R LOAD TRANSMITTING PROFILE IAW SRM 51-42-11, PN-D5227902620300, BATCH-0001982358. RETAIN FOR RECORDS.

Part: PROFILE — CRACKED (OVERWING EXIT) · airframe 61,496 hrs · 27,364 cycles

(MZAR) LT AFT OVERWING EXIT DOOR LT PROFILE HAS CRACKS AROUND RIVETS AS MARKED. REMOVED ANGLE IAW SRM 51-42-11, LOCATED AND DRILLED NEW ANGLE IAW SRM 51-21-11, INSTALLED NEW ANGLE IAW SRM 51-42-11. DAMAGE DIM: L=.100 RETAIN FOR RECORDS.

Part: LIGHT — MISSING (CABIN) · airframe 60,252 hrs · 26,819 cycles

EMERGENCY ESCAPE PATH LIGHT MISSING AT SEAT 12C, REPLACED LIGHT AND TESTED OK.

Part: EPSU — FAILED (CABIN) · airframe 56,812 hrs · 25,419 cycles

EMERGENCY EGRESS LIGHT TEST FUNCTION INOP. PLACED PTP (TEST PANEL) ON MEL. NEXT DDG, EMER R, EMERGENCY EXIT RT SUPPLY FAILED. REPLACED RT EPSU, CHECKS GOOD.

Part: SKIN — GOUGED (FUSELAGE) · airframe 55,781 hrs · 24,960 cycles

RT AFT FUSELAGE AFT OF R2 PASSENGER DOOR, FUSELAGE HAS GOUGES BETWEEN FR69 & FR70 AND STR 20R - STR 21R BLENDED GOUGES AT AREA IAW SRM 51-73-00 OUT OF LIMITS IAW SRM 53-41-11. FABRICATED & INSTALLED REPAIR DOUBLER IAW SRM 53-00-11 FIG 227. DURING LCK AT BFM, JAN2011. SECTION II-TO BE ACCOMP AT EVERY 1000FC AFTER SECT.I. SECTION III- TO BE ACCOMP WITHIN 3000FC AFTER SECT.I (AFTER L-CK, JAN2011).

Part: UNKNOWN — ODOR (UNKNOWN) · airframe 50,167 hrs · 22,276 cycles

CRUISE FLIGHT 380, FLIGHT CREW DETECTED FOUL ODOR, NOTICED FWD AND AFT CARGO FIRE EXTINGUISHING DISCHARGE LIGHTS BOTH ILLUMINATED, WITH NO ASSOCIATED INDICATIONS. NO SMOKE WAS DETECTED IN CABIN, ODOR WAS REPORTED BY FLIGHT ATTENDANT. FLIGHT DIVERTED INTO TLH, LANDING UNEVENTFULLY. REPLACED ELECTRICAL CONNECTORS 1154VCA AND 1156VCA, REPLACED LAVATORY EXTRACT FAN 32-2120-9-0021 AND CABIN RECIRCULATION FAN 32-2120-9-0021 (L/P 3976012, 3976018).

Part: LIGHT — DEFECTIVE (CABIN) · airframe 36,939 hrs · 16,170 cycles

EN ROUTE TO SPOKANE, THE LEAD FLIGHT ATTENDANT NOTICED AN ELECTRICAL ODOR FROM THE AREA OF ROW 10DEF. FLIGHT CONTINUED AND LANDED WITHOUT INCIDENT. RELAMPED AND INSPECTED AREA. NO ODOR PRESENT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,916 hrs · 13,055 cycles

DURING 1C-CHECK, FOUND CRACK ON FRAME NR 54 AT AFT CARGO DOOR. REPAIRED PER EA 32-175984.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

CREW OBSERVED CABIN LIGHTING CIRCUIT BREAKER POPPED. FURTHER INVESTIGATION REVEALED EMERGENCY EXIT LIGHTS AFT OF ROW 9 INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AND BATTERY 13WL AND 11WL.

Part: T12 SENSOR — MALFUNCTIONED (NR 2 ENGINE)

DURING CLIMB, NR 2 ENGINE N1, FUEL FLOW, AND EGT BEGAN TO FLUCTUATE. FLUCTUATION CONTINUED DESPITE VARIOUS POWER SETTINGS OR IN A CONSTANT POWER SETTING. FLIGHT CREW RETURNED TO DEPARTURE AIRPORT. MAINTENANCE REPLACED THE FUEL FILTER, FUEL PUMP, HMU, AND T12 SENSOR. ENGINE HAD A BORESCOPE INSPECTION AND WAS FOUND OK. AIRCRAFT GROUND RUN AND LEAK CHECK OK.

Part: SUPPORT — CORRODED (BS 32571)

DURING IL CHECK, FOUND CORROSION IN THE FS 68 FLOOR BEAM SUPPORT AT THE LEFT DOOR SILL. REPAIRED SUPPORT (P/N D53480043) PER EA 32-109588.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST SHOWED UNIT EMER L. EPSU 11WL FAILED SELF-TEST. REPLACED POWER SUPPLY UNIT. OPERATIONAL CHECK OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING LINE MAINTENANCE, FOUND THE CENTER EMERGENCY EXIT LIGHT AND LEFT OVERWING EXIT LIGHT INOPERATIVE. REPLACED POWER SUPPLY UNIT. OPERATIONAL CHECK OK.

Part: INTERFACE UNIT — MALFUNCTIONED (LANDING GEAR)

DURING CLIMBOUT AFTER PLACING THE LANDING GEAR HANDLE IN THE UP POSITION, ALL GEAR REMAINED EXTENDED. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 LANDING GEAR CONTROL INTERFACE UNIT, OPERATIONAL CHECK OK.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG WW)

DURING CLIMBOUT AFTER PLACING THE LANDING GEAR HANDLE IN THE UP POSITION, THE LANDING GEAR DID NOT RETRACT WHILE THE GEAR DOORS INDICATED OPEN. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 LANDING GEAR CONTROL INTERFACE UNIT AND THE LANDING GEAR SELECTOR VALVE, OPERATIONAL CHECK OK.

Part: PROX SENSOR — MALFUNCTIONED (RT MLG DOOR)

DURING CLIMBOUT AFTER LANDING RETRACTION, RECEIVED L/G GEAR NOT UPLOCKED AND L/G DOORS NOT CLOSED MESSAGES. ALL DOORS INDICATIONS WERE ILLUMINATED AMBER INTRANSIT AND ALL GEAR INDICATION TRIANGLES WERE ILLUMINATED RED. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED ALL GEAR DOOR OPEN PROXIMITY SENSORS AND REPLACED THE RIGHT MAIN LANDING GEAR DOOR PROXIMITY SENSOR, OPERATIONAL CHECK OK.

Part: LONGERON — CORRODED (FS 14300-14834)

DURING 1C1 CHECK, FOUND CORROSION ON FUSELAGE STRINGERS 41R, 43R AND 44 EACH BETWEEN FRAMES 33 TO 34. REPAIRED STRINGERS PER EA 32-105085, -105086 AND -105087.

Part: OIL TEMP WIRE — CHAFED (NR 1 ENGINE)

DURING CLIMB, THE NR 1 ENGINE OIL TEMPERATURE GAUGE INDICATED HIGH. ENGINE WAS SHUTDOWN AND THE AIRCRAFT WAS DIVERTED TO CLE AND LANDED WITHOUT INCIDENT. CHAFED WIRES IN THE PYLON SECTION WERE FOUND AND REPAIRED. ENGINE WAS RUN AND LEAK CHECKED OK. AIRCRAFT DEEMED OK FOR SERVICE.

Part: TRANSMITTER — MALFUNCTIONED (NLG STEERING)

AFTER TAKEOFF, THRUST WAS APPLIED, THE AIRCRAFT DRIFTED SLIGHTLY TO THE RIGHT, FULL LEFT RUDDER WAS APPLIED WITH NO RESPONSE. FULL LEFT TILLER WAS APPLIED WITH NO RESPONSE. THE TAKEOFF WAS ABORTED AT 40 KNOTS. AIRCRAFT RETURNED SAFELY TO THE GATE. MAINTENANCE REPLACED BOTH THE LEFT AND RIGHT NOSE STEERING TRANSMITTERS, 1GC AND 2GC. OPERATIONAL CHECK OK.

Part: CONNECTOR — LOOSE (NR 1 OIL QTY IND)

DURING CRUISE, THE NR 1 OIL QUANTITY INDICATION DROPPED TO 1.5. THE CIRCUIT BREAKER WAS RESET, BUT INDICATION STAYED THE SAME. THE PRESSURE PROCEEDED TO FLUCTUATE AND THE ENGINE WAS SHUTDOWN. THE AIRCRAFT DIVERTED TO ORD WHERE AN UNEVENTFUL LANDING WAS MADE. THE OIL QUANTITY CANNON CONNECTOR PLUG WAS CLEANED AND SECURED AND NO ADDITIONAL PRESSURE FLUCTUATION WAS NOTED.

Part: HYD DOOR — LOOSE (AFT FUSELAGE)

DURING CLIMB-OUT FROM DTW, EXPERIENCED MEDIUM FREQUENCY AIRFRAME VIBRATION AT 310 KNOTS. LEVELED OFF AT FL230 AND REDUCED SPEED TO 290 KNOTS AND VIBRATION STOPPED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED YELLOW HYDRAULIC SYSTEM ACCESS DOOR WITH SLIGHT AMOUNT OF LOOSENESS. REPOSITIONED LATCH, OPS CHECKED OK.

Part: DMC — FAILED (NR 1 SYST)

DURING TAKEOFF ROLL, THE CAPTAIN'S PRIMARY FLIGHT DISPLAY, NAVIGATION DISPLAY AND UPPER ENGINE DISPLAY FAILED. THE TAKEOFF WAS ABORTED AT 60 KNOTS. ECAM FAULTED EIS DMC NR 1. PLACED NR 1 DISPLAY MANAGEMENT COMPUTER ON MEL 31-63-01 AND LATER REPLACED. OPS CHECKED OK.

Part: FLAP DRIVE — OUT OF RIG (LT TE FLAP)

DURING APPROACH INTO SNA RECEIVED 'F/CTL FLAPS LOCKED' ALIGNMENT FAULT WHEN SELECTING FLAPS 3. THE FLAPS WERE LOCKED AT ZERO. AN EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. MAINTENANCE RIGGED THE NR 1, 2, 3, AND 4 LEFT WING FLAP ACTUATORS. OPERATIONAL CHECK OK.

Part: RETRACT MECH — MALFUNCTIONED (TE FLAPS)

DURING APPROACH INTO PHX RECEIVED 'F/CTL FLAPS LOCKED' ALIGNMENT FAULT. ACCOMPLISHED A FLAPS LESS THAN ONE LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTION OF THE FLAP DRIVE MECHANISM REVEALED NO DISCREPANCY. OPERATIONAL CHECK OK.