N316US

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 77,772 hrs · 35,319 cycles

MULTIPLE BULBS INOP IN MOST LARGE EMERGENCY EXIT SIGNS, RE-LAMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,808 hrs · 34,777 cycles

EMERGENCY EXIT PATH LIGHT AT SEAT ROW 23 ABC INOPERATIVE, INSTALLED NEW LIGHT ASSY.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 75,246 hrs · 34,029 cycles

SEAT ROW 24 EMERGENCY LIGHT INOPERATIVE. RECONNECTED LIGHT ASSY.

Part: STRINGER SPLICE — CORRODED (FRAMES 56-57) · airframe 75,246 hrs · 34,029 cycles

CORROSION ON STR 43L SPLICE REPAIR COUPLING BETWEEN FRAMES 56 AND 57. REPLACED STR 43L SPLICE IAW SRM 53-00-13, FIG 201.

Part: STRINGER — CORRODED (FRAMES 56-57) · airframe 75,246 hrs · 34,029 cycles

CORROSION ON STR 42L BETWEEN FRAMES 56 AND 57. REPLACED STR SPLICE 42L IAW SRM 53-00-13, FIG 201.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,341 hrs · 33,552 cycles

DURING SERVICE CHECK, INTERNAL LOADS EMERGENCY LIGHT FAULTED ON CIDS PANEL ON EMERGENCY LIGHT SYSTEM CHECK. REPAIRED LIGHT AND ALL TESTS OK.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 72,403 hrs · 32,614 cycles

DURING NON ROUTINE CHECK, FOUND SEAT ROW 9 LT EMERGENCY LIGHT INOPERATIVE. REPLACED SPLICE AT SEAT 9D EMERGENCY LIGHT AND FUNCTIONAL CHECK WAS NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 72,132 hrs · 32,492 cycles

DURING NON-ROUTINE CHECK, FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 18ABC. SECURED ELECTRICAL CONNECTOR AT 18ABC AND FUNCTIONAL CHECKED NORMAL.

Part: WIRE — UNSECURE (EMERGENCY LIGHT) · airframe 70,321 hrs · 31,552 cycles

DURING NON-ROUTINE CHECK, FOUND EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE AT SEAT 4C. MAINTENANCE SECURED WIRE AND FUNCTIONAL CHECKED NORMAL.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 68,389 hrs · 30,597 cycles

DURING NON-ROUTINE CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHT AT ROW 18 ABC INOPERATIVE. MX FOUND SEAT HARNESS WIRE PULLED FROM CONNECTOR. INSTALLED NEW CONNECTOR AND FUNCTIONAL CHECK WAS NORMAL.

Part: LIGHT — DAMAGED (CABIN) · airframe 68,217 hrs · 30,493 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY SEAT MOUNTED LIGHT DAMAGED AND INOPERATIVE. MX REPLACED LIGHT ASSY AND FUNCTIONAL CHECK WAS NORMAL.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CRACK ON LT AND RT LOAD TRANSMITING PROFILE LOCATED AT INTERNAL STRUCTURE OF RT FWD EMERGENCY EXIT. REPLACED LT AND RT LOAD TRANSMITTING PROFILE INTERNAL STRUCTURE OF RT FWD EMERGENCY EXIT IAW SRM 51-72-11.

Part: PROFILE — CRACKED (FUSELAGE) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CRACK ON LT AND RT LOAD TRANSMITTING PROFILE LOCATED INTERNAL STRUCTURE OF RT AFT EMERGENCY EXIT 844 MEASURES ARE LT L=1" RT L=3" APPROX. REPLACED LT AND RT LOAD TRANSMITTING PROFILE LOC. INTERNAL STRUCTURE OF RT AFT EMERGENCY EXIT 844 IAW SRM 51-72-11 AND DWG D52279040.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 44 IN BULK CARGO COMPARTMENT BETWEEN FR 66 AND FR 67. REPAIRED IAW SRM 53-00-13.

Part: SEAL BRACKET — CORRODED (FUSELAGE) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON SEAL LOCATED UNDER INTERNAL STRUCTURE OF CUT OUT DOOR LOCKING FITTING AREA FWD CARGO. REPLACED SEAL LOCATED UNDER INTERNAL STRUCTURE OF CUT OUT DOOR LOCKING FITTING AREA FWD CARGO IAW SRM 51-72-11 AND DWG D53231668.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT LOCATED BETWEEN STGR 40-41R AT FR 31. REPLACED CLEAT IN FWD CARGO COMPARTMENT LOCATED BETWEEN STR 40R AND STR 41R AT FR 31 IAW SRM 51-72-11 AND DWG D53232747.

Part: CROSSBEAM — BENT (CARGO BAY) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND BEND ON CROSSBEAM LOCATED IN FWD CARGO BAY FR 32 BETWEEN STR 37L TO STR 37R. REPLACED CROSSBEAM IAW SRM 51-72-11 AND DWG.

Part: CLEAT — CORRODED (CARGO BAY) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT STR 41-42R FR 32 FWD CARGO BAY. REPLACED CLEAT IAW SRM 51-72-11 AND DRAWING D53231582.

Part: CLEAT — CORRODED (CARGO BAY) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY BETWEEN STRINGER 43 - 44L FR 32. REPLACED CLEAT AND FASTENER FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D53231212.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT LOCATED BETWEEN STGR 43L AND STGR 44 AT FR 32. REPLACED CLEAT IAW 51-72-11.

Part: FLOORBEAM — BROKEN (CABIN) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND BROKEN UPPER FLANGE OF FLOORBEAM FR 33+16" AND -Y254. PERFORMED PERMANENT REPAIR ON UPPER FLANGE OF FLOORBEAM IAW SRM 53-00-14, PARA 4.D, FIG 204 (SHEET 1).

Part: FLOORBEAM — BROKEN (CABIN) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND BROKEN UPPER FLANGE OF FLOORBEAM FR32+4" AND Y254 FWD PAX CABIN. PERFORMED PERMANENT REPAIR ON UPPER FLANGE OF FLOORBEAM IAW SRM 53-00-14, FIG 204 (SHEET 1) PARA 4D.

Part: FLOORBEAM — BROKEN (CABIN) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND BROKEN UPPER FLANGE OF FLOORBEAM. PERFORMED PERMANENT REPAIR ON UPPER FLANGE OF FLOORBEAM IAW SRM 53-00-14, PARA 4.D FIG 204 (SHEET 1) PAGE 225/226.

Part: FLOORBEAM — BROKEN (CABIN) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND BROKEN UPPER FLANGE OF FLOORBEAM FR.32+13" AND -Y254 FWD PAX CABIN. PERFORMED PERMANENT REPAIR ON UPPER FLANGE OF FLOORBEAM IAW SRM 53-00-14. FIG 204 (SHEET 1) PARA 4D, PAGES 225-226.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION FOUND CORROSION ON CLEAT LOCATED BETWEEN STR 41R AND STR 42R AT LEVEL FR 31 FWD CARGO COMP. L=0.50", W=0.20", D=0.001" APROX. REPLACED CLEAT LOCATED BETWEEN STR 41R AND STR 42R AT LEVEL FR 31 FWD CARGO COMPARTMENT, IAW SRM 51-72-11 AND DWG D53231582.

Part: CLEAT — CORRODED · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT LOCATED AT FR 32 BETWEEN STGR 40L AND STGR 41LIN FWD CARGO COMPARTMENT L=0.800", W=0.500", D=0.001" APPROX. REPLACED CLEAT LOCATED FR 32 BETWEEN STR 40L AND STR 41L IN FWD CARGO COMPARTMENT, IAW SRM 51-72-11 AND DWG.

Part: THRESHOLD — CORRODED · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON THRESHOLD SHEET LOCATED BETWEEN FR 52A AND FR 56 AND BETWEEN STR 38R AND STR 39R INTERNAL STRUCTURE OF AFT CARGO COMPARTMENT SSI 534107, L=0.400, W=0.260, D=0.002 APPROX. REPLACED TRESHOLD SHEET LOCATED BETWEEN FR 52A AND FR 56 AND BETWEEN STR 38R AND STR 39R INTERNAL STRUCTURE OF AFT CARGO COMPARTMENT, AND FASTENER IAW SRM 51-72-11 AND DWG D53475500.

Part: SPLICE — CORRODED · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON SPLICE IN BULK CARGO COMPARTMENT AT FR 67 AT LEVEL STR 30R. REPLACED SPLICE LOCATED IN BULK CARGO COMPARTMENT AT FR.67 AT LEVEL STR 30R IAW SRM 51-72-11 AND DWG D53480009.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK, FWD PAX CABIN BETWEEN FR 20 TO FR 24 AND -Y1292 L=3.00", W=0.500",D=0.005" APPROX, REPLACED SEAT TRACK FWD PAX CABIN BETWEEN FR 12 TO FR 24 AND -Y1292 AND FASTENERS IAW SRM 51-72-11 AND DWG D53112812.

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON UPPER SHEET METAL LOCATED BETWEEN FR 24A AND FR 28, S39-41R IN FWD CARGO COMPARTMENT. MEASURES L=1.5" W=0.300", D=0.002 APPROX. MAJOR DIMENSION. REPLACED UPPER SHEET METAL LOCATED BETWEEN FR 24A AND FR 28, STR 39R AND STR 41R IN FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D53230315.

Part: SPLICE — CORRODED · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON SPLICE IN BULK CARGO COMPARTMENT AT STR 30L AND AT LEVEL FR 67. REPLACED SPLICE LOCATED IN BULK CARGO COMPARTMENT AT STR 30L AND AT LEVEL FR 67 IAW SRM 51-72-11 AND DWG D53480009.

Part: SPLICE — CORRODED · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON SPLICE IN BULK CARGO COMPARTMENT AT STR 29L AND AT LEVEL FR 67. REPLACED SPLICE LOCATED IN BULK CARGO COMPARTMENT AT STR 29L AT LEVEL FR.67 IAW SRM 51-72-11 AND DWG D53480009.

Part: FLOOR SUPPORT — CORRODED · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER SILL LOCATED BETWEEN FR 66 AND FR 68 LT SIDE L=1", W=0.500", D=0.002" APROX. REPLACED LOWER SILL AND FASTENERS LOCATED BETWEEN FR 66 AND FR 68 LT SIDE IAW SRM 51-72-11 AND DWGS D53480020 AND D53480505.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM STRUCTURE, FR 66 LEVEL Y-1292. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG D53472230.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT STRUCTURE, LOCATED AFT PAX CABIN, AT FR 68 LEVEL Y-1162. REPLACED FLOOR SUPPORT IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER SILL LOCATED BETWEEN FR 66 AND FR 68 RT SIDE L=0.500", W=0.250", D=0.001" APPROX. REPLACED LOWER SILL LOCATED BETWEEN FR 66 AND FR 68 RT SIDE IAW SRM 51-72-11 AND DWG D53480020, D53480505.

Part: FITTING — CORRODED · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FR 16 AND FR 20 AT LEVEL STR 23 RT L=0.500" W=0.250" D=0.001" APPROX. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG D53112198.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM STRUCTURE, LOCATED AFT PAX CABIN AT FR 67+13", LEVEL Y-1162. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG NR D53472000.

Part: FLOOR SUPPORT — CORRODED (MAIN CABIN) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON SUPPORT LOCATED AT FR.68 AT LEVEL OF S24R IN AFT PAX CABIN. REPLACED SUPPORT SECTION IAW SRM 51-72-11 AND DWG D53470150.

Part: FITTING — CORRODED · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON CORNER FITTING LOCATED FR 68 AT LEVEL STR 23 RT L=0.500" W=0.250" D=0.001" APPROX. REPLACED CORNER FITTING LOCATED FR 68 AT LEVEL STR 23 RT IAW SRM A320 51-72-11 AND DWG D53480505.

Part: FLOORBOARD — CORRODED (CABIN) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON OTBD UPPER FLOORBOARD SPLICE LOCATED AFT PAX CABIN AT FR.64, LEVEL Y-765, SSI 534147. L=1", W=0.5", D=0.003" APPROX. REPLACED OTBD UPPER FLOORBOARD SPLICE IAW SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON CORNER FITTING AND FASTENERS LOCATED FR 68 AT STR 23. REPLACED CORNER FITTING AND FASTENERS IAW SRM 51-72-11 AND DWG NR D53480019.

Part: WEB — CORRODED (CABIN) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON WEB BETWEEN FR20 TO FR21 AND AT LEVEL -Y1680 FWD PAX CABIN. REPLACED WEB IAW SRM 51-72-11 AND DWG D53112783.

Part: FITTING — CORRODED (FUSELAGE) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON FITTING LOCATED INTERNAL STRUCTURE OF CUT OUT DOOR LOCKING FITTING AREA AND BETWEEN FR 26 AND FR 27 FWD CARGO. REPLACED FITTING AND FASTENER LOCATED INTERNAL STRUCTURE OF CUT OUT DOOR LOCKING FITTING AREA AND BETWEEN FR 26 AND FR 27 FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D53231668.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND DENT ON EXTERNAL SKIN LOCATED AT FR 80+2" AFT UPPER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BETWEEN FR 80 AND FR 81 AFT UPPER FUSELAGE IAW SRM 53-51-11, PARA 5.B, FIG 203 (SHEET 1).

Part: SKIN — DENTED (FUSELAGE) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND DENT ON EXTERNAL FUSELAGE SKIN LOCATED FR 24+7" AND BETWEEN STR 41L AND STR 42L. PERFORMED PERMANENT REPAIR ON EXTERNAL FUSELAGE SKIN BETWEEN FR 24 AND FR 25 AND BETWEEN STR 41L AND STR 43L IAW SRM 53-21-11, PARA 5K, FIG 214, MUST BE INSPECTED FIRST INSP AFTER REPAIR EMBODIMENT AT 60000 FC/FH NOT RELEVANT IAW SRI 53-21-11-2-003-00, PARA 3.C, TABLE 204.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM STRUCTURE LOCATED AFT PAX CABIN AT FR 66, LEVEL Y-765. REPLACED FLOORBEAM STRUCTURE LOCATED AFT PAX CABIN AT FR 66, LEVEL Y-765 IAW SRM 51-72-11.

Part: FLOOR SUPPORT — DAMAGED (CABIN) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND ELONGATED HOLES ON FLOOR SUPPORT STRUCTURE LOCATED AFT PAX CABIN BETWEEN FR 66+5" AND FR 67+17" LEVEL Y1162 REPLACED FLOOR SUPPORT LOCATED AFT PAX CABIN BETWEEN FR 66+5" ANDFR 67+17" Y1162 IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT STRUCTURE LOCATED AFT PAX CABIN BETWEEN FR 68 AND FR 69, LEVEL Y1162. REPLACED FLOOR SUPPORT LOCATED AFT PAX CABIN BETWEEN FR 68 AND FR 69 Y1162 IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOORBEAM — CORRODED · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM STRUCTURE LOCATED AFT PAX CABIN AT FR 68+5" LEVEL Y-765; REPLACED FLOORBEAM LOCATED AFT PAX CABIN AT FR 68+5" LEVEL -Y765 IAW SRM 51-72-11 AND DWG D53472000.

Part: FITTING — CORRODED (FUSELAGE) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FR 66 AND FR 68 AT LEVEL STR 23 RT L=0.500" W=0.250" D=0.001" APROX SSI 534132. REPLACED CENTER FITTING LOCATED BETWEEN FR 66 AND FR 68 AT LEVEL STR 23 RT IAW SRM 51-72-11 AND DWG D53480020.

Part: FITTING — CORRODED (FUSELAGE) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FR 66 AND FR 68 AT LEVEL STR 23 LT L=0.500", W=0.250", D=0.001" APPROX. REPLACED CENTER FITTING LOCATED BETWEEN FR 66 TO FR 68 AT LEVEL STR 23 LT IAW SRM 51-72-11 AND DWG D53480020.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 67,893 hrs · 30,324 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM STRUCTURE LOCATED AFT PAX CABIN AT FR 66 LEVEL -Y465. REPLACED FLOORBEAM AND FASTENERS IAW SRM 51-72-11 AND DWG D53472000.

Part: DAMPER — FAILED (LT DOOR) · airframe 61,882 hrs · 27,461 cycles

DURING L CHECK AFT LEFT DOOR DAMPER FAILED OPERATIONAL CHECK. REMOVED AND REPLACED DOOR DAMPER PER AMM 52-13-14. OPERATIONAL CHECK GOOD PER AMM 52-13-14.

Part: DAMPER — FAILED (LT DOOR) · airframe 61,882 hrs · 27,461 cycles

DURING L CHECK FORWARD LEFT DOOR DAMPER FAILED OPERATIONAL CHECK. REPLACED DAMPER PER AMM 52-13-14. OPERATIONAL CHECK GOOD PER AMM 52-13-14.

Part: DAMPER — FAILED (RT DOOR) · airframe 61,882 hrs · 27,461 cycles

DURING L CHECK FORWARD RIGHT DOOR DAMPER FAILED. OPERATIONAL CHECK. REPLACED DAMPER PER A320 AMM 52-13-14. ACCOMPLISHED OPERATIONAL CHECK OF DAMPER WITH SLIDE AND PANELS INSTALLED PER AMM 52-13-14, CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,073 hrs · 27,133 cycles

DURING EMERGENCY LIGHT TEST FOUND ROW 13 PATH LIGHT INOP. REPLACED LIGHT ASSEMBLY AND TESTS OK.

Part: LIGHT — BROKEN (SEAT 8C) · airframe 60,785 hrs · 27,012 cycles

UPON ARRIVAL FOUND SEAT 8C ARM REST AND EMERGENCY PATH LIGHT BROKEN. PATH LIGHT LENS AND LIGHT WERE REPLACED AND TESTS OK.

Part: SLIDE — NO TEST (L1 DOOR) · airframe 57,518 hrs · 25,634 cycles

DURING A NON ROUTINE CHECK, FOUND DOOR 1L EXTERNAL LOAD FAULT ON CIDS. MX REPLACED DOOR 1L SLIDE AND FUNCTIONAL CHECK WAS NORMAL. ACFT OK FOR SERVICE.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 53,685 hrs · 23,985 cycles

GREEN RESERVOIR LO LEVEL OCCURRED IN CRUISE. COMPLIED WITH COM, LG GRAVITY EXTENDED PRIOR TO LANDING. ACFT LANDED UNEVENTFULLY AND WAS TOWED TO GATE. REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP. CHECKS OK.

Part: EPSU — DISCHARGED (CABIN) · airframe 53,655 hrs · 23,937 cycles

EMERGENCY EGRESS PATH LIGHTING INOP BETWEEN ROWS 1 AND 8. REPLACED EPSU 10WL, CHECKS OK.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,321 hrs · 22,892 cycles

DURING "M" CHECK, FOUND CORROSION ON BUTT STRAP AT FR 64 BETWEEN S43R-S44R. REPAIRED PER EA 32-211424.

Part: TRANSDUCER — MALFUNCTIONED (FLT CONTROLS) · airframe 48,579 hrs · 21,589 cycles

FLIGHT CONTROL STABILIZER JAMB, DIVERTED, LANDING UNEVENTFULLY. CORRECTED BY REPLACING BOTH PITCH TRIM POSITION TRANSDUCER UNITS, PERFORMED THS MECHANICAL CONTROL ADJUSTMENT (L/P 3842667, 3842664), REPLACED ELAC 2 (L/P 3842666), REPLACED THS MONITORING TRANSDUCER (L/P 2596067).

Part: CHECK VALVE — MALFUNCTIONED (HYD SYSTEM) · airframe 48,579 hrs · 21,589 cycles

IN CRUISE, HYDRAULIC YELLOW RESERVOIR LOW LEVEL, FLIGHT LANDED UNEVENTFULLY. CORRECTED BY REPLACING PTU MANIFOLD CHECK VALVE.

Part: TRANSDUCER — MALFUNCTIONED (PITCH TRIM) · airframe 48,579 hrs · 21,589 cycles

FLIGHT CONTROL STABILIZER JAMB, DIVERTED TO CMH, LANDING UNEVENTFULLY. CORRECTED BY REPLACING BOTH PITCH TRIM POSITION TRANSDUCER UNITS, PERFORMED THS MECHANICAL CONTROL ADJUSTMENT (L/P 3842667, 3842664). REPLACED ELAC 2 (L/P 3842666). REPLACED THS MONITORING TRANSDUCER (L/P 2596067).

Part: ACTUATOR — MALFUNCTIONED (HORIZ STAB) · airframe 47,023 hrs · 20,867 cycles

LOST BOTH AUTOPILOTS ON DESCENT, ECAM MESSAGE FLT STABILIZER JAM ANNUNCIATED, MANUAL TRIM OK. UNEVENTFUL NORMAL LANDING IN DIRECT LAW. INSPECTED PITCH TRIM CONTROL WHEEL, INSPECTED AND LUBED CABLES, CHECKED FOR FREEDOM OF MOVEMENT. PRECAUTIONARY REPLACEMENT OF THS ACTUATOR. AIRCRAFT PREPARED FOR TEST FLIGHT. Â

Part: HYDRAULIC LINE — LOOSE (HYDRAULIC SYS) · airframe 46,897 hrs · 20,813 cycles

DURING CLIMBOUT, LOST GREEN HYDRAULIC SYSTEM FLUID. TURNED PTU AND GREEN ENGINE 1 PUMP OFF PER COM. ON ARRIVAL MEM, GRAVITY EXTENDED LANDING GEAR PER COM, EMERGENCY LANDING DECLARED. LANDED UNEVENTFULLY, LANDING GEAR PINNED AND AIRCRAFT TOWED TO GATE. FLUID LOSS DUE TO LOOSE HYDRAULIC LINE AT PYLON. INSPECTED AND SECURED LINE, LEAK CHECKED GOOD. ENGINE DRIVEN HYDRAULIC PUMP REPLACED, PERFORMED GREEN SYSTEM BLEEDING PROCEDURE, PERFORMED OPERATIONAL CHECK OF THRUST REVERSER, AND RESET GRAVITY GEAR EXTENSION HANDLE.

Part: REGULATOR — LEAKING (AVIONICS COMPT)

DURING CRUISE, THE CREW NOTED THAT THE OXYGEN PRESSURE HAD DROPPED TO 300 PSI. FLIGHT DEPARTED WITH A PRESSURE OF 700 PSI. AIRCRAFT DIVERTED TO MIA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE CREW OXYGEN BOTTLE AND REGULATOR, LEAK AND OPERATIONAL CHECK OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING INTERMEDIATE LAYOVER VISIT, THE RIGHT EMERGENCY LIGHTS POWER SUPPLY FAILED SYSTEM TEST. REPLACED EPSU, OPERATIONAL CHECK OK.

Part: LONGERON — CORRODED (FS 13767-14300)

DURING IL CHECK, FOUND CORROSION ON STR 42R BETWEEN FRAMES 32 - 33. REPAIRED STRINGER PER EA 32-106870.

Part: LONGERON — CORRODED (FS 14300-14834)

DURING IL CHECK, FOUND CORROSION ON STR 41R BETWEEN FRAMES 33 - 34. REPAIRED STRINGER PER EA 32-106869.

Part: WEB — CRACKED (FUSELAGE)

DURING PERIODIC CHECK, THE TRIANGLE WEB PANEL AFT OF FRAME 68, NEAR THE FUSELAGE SKIN WAS FOUND CRACKED. STOP DRILLED CRACK AND SEALED PER EA 32-106827.

Part: BUSHING — WORN (RAM AIR DOOR)

DURING CLIMBOUT AT 22,000 FEET AND 315 KNOTS, AIRCRAFT BEGAN VIBRATING. VIBRATION WAS FELT THROUGHOUT THE CABIN. ENGINE VIBRATION MONITORS WERE NORMAL. AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT FORWARD END RAM AIR INLET DOOR ACTUATOR BUSHING. OPERATIONAL CHECK OK.