N942FR

Part: HOSE — RUPTURED (ZONE 700) · airframe 22,703 hrs · 10,866 cycles

ON DEPARTURE, GREEN SYS FAILURE (FLUID LOSS) R & R LT MLG SWIVEL JOINT REF AMM 32-31-38-000, PB401. R & R FLEX HOSE ASSY REF AMM 32-31-39-000, PB 401. OPS LEAK CHECKED NORMAL, SERVICED GREEN HYD SYS 12-12-29-611-001, OK.

Part: CONNECTOR — MISINSTALLED (EMERGENCY LIGHTS) · airframe 22,148 hrs · 10,592 cycles

EXTERIOR OVERWING EMERGENCY LIGHTS INOP". "FOUND BOTH EXTERNAL OVERWING EMERGENCY LIGHTS ON THE RT SIDE WERE NOT CONNECTED TO ACFT WIRING. RECONNECTED CONNECTORS TO LIGHT ASSY. SYS OPS CHECKS NORMAL REF AMM 33-S1-1 S PB401. NOTE: THERE WERE NO DEFECTIVE PARTS. NO DEFECTIVE SYS. SYS WAS NOT CONNECTED. DIFFICULTY WAS MOST LIKELY INDUCED BY TECH.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,834 hrs · 10,439 cycles

C-CHECK: NON ROUTINE NR 38830; R-2 DOOR SILL AT FR66 Y-1500 HAS CORROSION OUT OF LIMITS. REPAIRED R-2 DOOR SILL AT FR66 IAW SRM 53-41-14, FIG 201, REPAIR PRINCIPLE 6.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,834 hrs · 10,439 cycles

C-CHECK: L-2 DOOR SILL AT FR66 HAS CORROSION. REPAIRED L-2 DOOR SILL AT FR66 IAW 53-41-14, FIG 201, REPAIR PRINCIPLE 6.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 21,636 hrs · 10,343 cycles

PILOT REPORT YELLOW HYDRAULIC LOW RESERVOIR LEVEL. REMOVED AND REPLACED ENGINED NR2 HYDRAULIC PUMP DRIVER IAW AMM 29-13-51, PB 401, OPS CHECKS GOOD. FOUND SEVERAL LEAK YELLOW SYSTEM LINE TO PRESSURE SWITCH. REMOVED AND REPLACED LINE IAW AMM 28-23-11 LEAKED CHECK GOOD. NO FURTHER LEAKS NOTED.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 20,955 hrs · 10,034 cycles

EPSU BATTERY 13WL FAILED OPS TEST IAW REPLACED BATTERY PACK 13WL IAW AMM 33-51-38-400-002.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 20,392 hrs · 9,769 cycles

DURING CLIM, AFTER RETRACTING THE LANDING GEAR, VISUAL GREEN HYD LOW PRESSURE MESSAGE. MANUAL GEAR EXTENTION PERFORMED. AIR TURN BACK, REPLACED RT MLG AFT HYD HOSE ASSY IAW AMM 32-31-39, PB 401. SERVICED GREEN HYD SYS IAW AMM 12-12-29-611-001. STOWED GRAVITY GEAR EXTEND HANDLE AND PERFORM OPS TEST OF THE MAIN LANDING GEAR DOORS. IAW AMM 32-31-00-710-002. OPS CHECK GOOD.

Part: PROXIMITY SWITCH — MALFUNCTIONED (OVERWING DOOR) · airframe 16,919 hrs · 8,129 cycles

DURING C3 C CHECK INSP NOTED EXIT OVERWING EMERGENCY EXTERIOR LIGHTS ON THE RT SIDE DO NOT COME ON WHEN DISARMING OVER WING EXIT DOOR. MX REMOVED AND REPLACED PROXIMITY SWITCH IAW AMM 52-73-11-400-004A AND AMM 52-73-00-710-002.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,919 hrs · 8,129 cycles

REFERENCE NON ROUTINE C078794. DURING C3 C CHECK INSP NOTED THE OPS TEST OF THE EMERGENCY LIGHTS WITH THE MCDU FAULTING. MX REPAIRED IAW AMM 33-51-38-000-001, AMM 33-51-38-400-001, AMM 25-62-44-000-002 AND AMM 33-51-00-710-001.

Part: BLANKING PLATE — CORRODED (ZONE 100) · airframe 16,919 hrs · 8,129 cycles

DURING C3 C CHECK INSPECTION NOTED BLANKING PLATE CORRODED ON AFT PLATE R2 DOOR. MX REMOVED AND REPLACED PLATE IAW AMM 52-13-31-400-007.

Part: FLOORBOARD — CORRODED (ZONE 100) · airframe 16,919 hrs · 8,129 cycles

DURING C3 C CHECK INSPECTION NOTED FLOOR PANEL 261FF WAS CORRODED. MX REMOVED AND REPLACED FLOOR PANEL 261FF IAW AMM 53-42-12-400-002.

Part: BLANKING PLATE — CORRODED (ZONE 100) · airframe 16,919 hrs · 8,129 cycles

DURING C3 C CHECK INSPECTION NOTED BLANKING PLATE CORRODED FORWARD R2 DOOR. MX REMOVED AND REPLACED PLATE IAW AMM 52-13-31-400-007.

Part: BLANKING PLATE — CORRODED (ZONE 100) · airframe 16,919 hrs · 8,129 cycles

DURING C3 C CHECK INSPECTION NOTED BLANKING PLATE CORRODED AFT PLATE L2 DOOR. MX REMOVED AND REPLACED PLATE IAW AMM 52-13-31-400-007.

Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 16,919 hrs · 8,129 cycles

DURING C3 C CHECK INSP NOTED FLOOR PANEL 262FF WAS CORRODED. MX REMOVED AND REPLACED FLOOR PANEL 262FF IAW TASK CARD C534103-02.

Part: BLANKING PLATE — CORRODED (ZONE 100) · airframe 16,919 hrs · 8,129 cycles

DURING C3 C CHECK INSPECTION NOTED BLANKING PLATE CORRODED FORWARD PLATE L2 DOOR. MX REMOVED AND REPLACED PLATE IAW AMM 52-13-400-007.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 16,919 hrs · 8,129 cycles

DURING C3 C-CHECK INSP NOTED THE LT FRAME SUPPORT AT FRAME 70 HAS CORROSION ON THE BOTTOM SIDE AT NUTPLATE HOLES. MX REMOVED AND REPLACED SUPPORT FRAME IAW SRM 51-42-11.

Part: PLATE — CORRODED (ZONE 100) · airframe 16,919 hrs · 8,129 cycles

DURING C3 C CHECK INSP NOTED LT SHEAR PLATE AT FRAME 70 HAS SURFACE CORROSION AND APPEARS TO BE COMING FROM UNDER GALLEY FLOORBOARD. MX REMOVED AND REPLACED SHEAR PLATED IAW SRM 51-57-12.

Part: SILL — CORRODED (ZONE 100) · airframe 16,919 hrs · 8,129 cycles

DURING C3 C-CHECK INSP NOTED L2 DOOR SILL FASTENER HOLE AFT OF AFT GIRT BAR MOUNT FITTING HAS CORROSION. MX REPAIRED IAW EA A9-53R-31638, SRM 51-74-00, SRM 53-41-14, NTM 51-10-01-250-802-A-01, NTM 51-10-04-270-801-A-01 AND NTM 51-10-08-250-803-A-01.

Part: PLATE — CORRODED (ZONE 100) · airframe 16,919 hrs · 8,129 cycles

DURING C3 C CHECK INSP NOTED PLATE BETWEEN Y1292 AND L2 THRESHOLD AT FRAME 66 IS CORRODED. MX REMOVED AND REPLACED PLATE IAW SRM 51-74-00, SRM 51-75-12 AND DWG D53670670.

Part: PLATE — CORRODED (ZONE 100) · airframe 16,919 hrs · 8,129 cycles

DURING C3 C-CHECK INSP NOTED THE RT SHEAR PLATE AT FRAME 70 HAS SURFACE CORROSION AND APPEARS TO BE COMING FROM UNDER GALLEY FLOORBOARD. MX REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11 AND SRM 51-44-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 16,919 hrs · 8,129 cycles

DURING C3 C CHECK INSP NOTED Y1292 FROM FRAME 60 TO FRAME 68 ALL SCREW HOLES ARE CORRODED ON UPPER AND LOWER AREAS. MX REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11 PAGE 6.

Part: SILL — CORRODED (ZONE 100) · airframe 16,919 hrs · 8,129 cycles

DURING C3 C CHECK INSPECTION NOTED L2 DOOR FASTENER HOLES INBD OF AFT GIRT BAR MOUNT FITTING HAS CORROSION. MX REPAIRED IAW EA A9-53R-31638, SRM 53-41-14, NTM 51-10-01, NTM 51-10-01-250-802-A-01 AND NTM 51-10-08-250-803-A-01.

Part: SILL — CORRODED (ZONE 100) · airframe 16,919 hrs · 8,129 cycles

DURING C3 C-CHECK INSP NOTED THE L2 DOOR SILL INBD FLANGE FASTENER HOLE CORRODED. MX REPAIRED IAW SRM 53-41-14, SRM 51-23-11 AND SRM 51-42-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 16,919 hrs · 8,129 cycles

DURING C3 C CHECK INSP NOTED Y1292 JUST AFT OF FRAME 68 HAS A LARGE AREA OF CORROSION ON TOP SIDE WHICH EXTENDS UNDER GALLEY FLOORBOARD. MX REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11 PAGE 6.

Part: PLATE — CORRODED (ZONE 100) · airframe 16,919 hrs · 8,129 cycles

DURING C3 C-CHECK INSP NOTED THE RT SHEAR PLATE AT FRAME 70 HAS SURFACE CORROSION AND APPEARS TO BE COMING FROM UNDER GALLEY FLOORBOARD. MX REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11 AND SRM 51-44-11.

Part: SENSOR — FAILED (TAT) · airframe 14,856 hrs · 7,207 cycles

FLIGHT CREW DIVERTED. PILOT REPORTED LOST TOTAL AIR TEMPERATURE AND STATIC AIR TEMPERATURE INDICATIONS. MX REMOVED AND REPLACED THE NR 1 TOTAL AIR TEMPERATURE SENSOR AT POSITION 11FP1 AND PERFORMED OPERATIONAL TEST, REF AMM 34-11-18 PB 401. DURING THE SAME EVENT, PILOT REPORTED MULTIPLE INDICATIONS ON THE ELECTRONIC CENTRALIZED ACFT MONITORING SYS INCLUDING AUTO PILOT OFF, AUTO THRUST OFF, RUDDER TRAVEL LIMITER 1 AND ENGINE 1 THRUST REVERSER INOPERATIVE. MX PERFORMED AUTO FLIGHT SYS TEST, REF AMM 22-96-00-710-001. MX PERFORMED RUDDER TRAVEL LIMITER OPS CHECK, REF AMM 22-61-00-710-001. MX PERFORMED OPS CHECK OF THE NR 1 ENGINE THRUST REVERSER SYS, REF AMM 78-31-00-710-042. NO FURTHER DEFECTS WERE NOTED.

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 11,484 hrs · 5,613 cycles

DURING C-CHECK, INSP NOTED THE AFT CARGO PIT CENTER LT UPPER TRANSITION PANEL 151FE WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 151FE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 11,484 hrs · 5,613 cycles

DURING C-CHECK, INSP NOTED THE AFT CARGO PIT AFT LT UPPER TRANSITION PANEL 161CF WAS PUNCTURED IN THE CENTER, COVERED WITH TAPE. MAINT REPAIRED TRANSITION PANEL 161CF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — GOUGED (FUSELAGE) · airframe 11,484 hrs · 5,613 cycles

DURING C-CHECK, INSP NOTED THE AFT CARGO PIT AFT RT LOWER TRANSITION PANEL 162BF WAS GOUGED AND A PREVIOUS REPAIR WAS PEELING UP. MAINT REPAIRED TRANSITION PANEL 162BF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 11,484 hrs · 5,613 cycles

DURING C-CHECK, INSP NOTED THE AFT CARGO PIT AFT LT LOWER TRANSITION PANEL 161BF WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 161BF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — GOUGED (FUSELAGE) · airframe 11,484 hrs · 5,613 cycles

DURING C-CHECK, INSP NOTED THE AFT CARGO PIT FORWARD LT LOWER TRANSITION PANEL 151AE WAS GOUGED IN THE CENTER OF THE PANEL. MAINT REPAIRED TRANSITION PANEL 151AE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 11,484 hrs · 5,613 cycles

DURING C-CHECK, INSP NOTED THE AFT CARGO PIT CENTER LT LOWER TRANSITION PANEL 151DE WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 151DE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 11,484 hrs · 5,613 cycles

DURING C2 C-CHECK, INSP NOTED THE AFT CARGO PIT FWD RT LOWER TRANSITION PANEL 152WG WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 152WG IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 11,484 hrs · 5,613 cycles

DURING C2 C-CHECK, INSP NOTED THE AFT CARGO PIT FWD LT UPPER TRANSITION PANEL 151BE WAS PUNCTURED. MAINT REPAIRED TRANSITION PANEL 151BE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 11,484 hrs · 5,613 cycles

DURING C-CHECK, INSP NOTED THE PREVIOUS REPAIRS PEELING LOOSE ON THE AFT CARGO PIT FWD LT UPPER TRANSITION PANEL 151UG. MAINT REPAIRED TRANSITION PANEL 151UG IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 11,484 hrs · 5,613 cycles

DURING C-CHECK, INSP NOTED THE AFT CARGO PIT FLOOR PANEL 161NF WAS PUNCTURED SEVERAL TIMES. MAINT REPAIRED FLOOR PANEL 161NF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.(A)

Part: GUST LOCK — INOPERATIVE (L1 DOOR) · airframe 4,634 hrs · 2,287 cycles

FOUND GUST LOCK 1L INOP. ADJUSTED BUFFER PER AMM 52-11-12-820. RII INSPECTION ACCOMPLISHED. AIRCRAFT RELEASED FOR SERVICE.

Part: ODOR — DETECTED (ENTERTAIN SYS) · airframe 1,463 hrs · 709 cycles

FLIGHT CREW RECEIVED LIVE TV SMOKE INDICATION. FLIGHT ATTENDANT REPORTED AN ELECTRIC ODOR IN AFT GALLEY. DECLARED AM EMERGENCY AND LANDED WITHOUT INCIDENT IN DEN. PERFORMED INSPECTION PER AMM 24-00-00-810-873. VERIFIED LIVE TV EXHAUST COOLING FAN FAILED. PLACARDED LIVE TV SYSTEM INOPERATIVE PER MEL 44-20-01AA, CONTROL NR 1019880. AN ADDENDUM WILL BE SUBMITTED UPON REMOVAL OF PLACARD. REPLACED AFT RACK COOLING FAN ASSY. PER LIVE TV AMM 44-25-00, PAGE 4772.