N306FL

Part: ROLLER — WORN (GUIDE ARM) · airframe 24,272 hrs · 11,795 cycles

MAINTENANCE REPORTED R1 DOOR HARD TO CLOSE. REPLACED GUIDE ARM ROLLER PER MM 52-61-20. ADJUSTED R1 DOOR PER MM 52-41-00. REMOVED AND REINSTALLED R1 DOOR SLIDE PER MM 25-61-35. REMOVED AND REINSTALLED R1 DOOR LINER PER MM 52-41-31. REMOVED AND REINSTALLED R1 DOOR PER MM 52-41-00.

Part: SKIN — DENTED (FUSELAGE) · airframe 21,103 hrs · 9,980 cycles

DURING C-7 CHECK, INSPECTION REPORTED CREASED DENT IN EXTERNAL FUSELAGE SKIN AT STA 368, 4 IN BELOW STR 18R. REPAIRED PER SRM 53-00-01 FIG 202.

Part: ACTUATOR — INOPERATIVE (NR 3 SLAT) · airframe 21,103 hrs · 9,980 cycles

DURING C-7 CHECK, INSPECTION REPORTED NR 3 SLAT ACTUATOR FAILED LOCK PIN TEST. REPLACED NR 3 SLAT ACTUATOR IAW MM 27-81-41 AND ACCOMPLISHED LE SLAT ACTUATOR LOCK PIN TEST AND LE SLAT ALTERNATE SYSTEM TESTS IAW TASK CARD 5-2710 AND MM 27-81-00.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 21,103 hrs · 9,980 cycles

DURING C-7 CHECK, INSPECTION REPORTED MAIN DECK FLOOR INTERCOSTAL CRACKED BETWEEN STA 294 AND STA 312 AT RBL 32. REPLACED DAMAGED UPPER CHORD OF FLOOR INTERCOSTAL PER SRM 51-40-2.

Part: OXYGEN BOTTLE — DISCHARGED (CABIN) · airframe 21,103 hrs · 9,980 cycles

DURING C-7 CHECK, INSPECTION REPORTED SEAT 7 ABC OXYGEN CANISTER DISCHARGED. REPLACED OXYGEN GENERATOR CANISTER PER MM 35-22-11, PAGE 201, STEPS 1-3 AND MM 35-22-11, PAGE 401, STEPS 1-3.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,103 hrs · 9,980 cycles

DURING C-7 CHECK, INSPECTION REPORTED SHEARTIE IN FWD CARGO COMPARTMENT CORRODED AT STA 500B, BETWEEN STR 27R AND 28R. REPAIRED IAW SRM 53-00-07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,103 hrs · 9,980 cycles

DURING C-7 CHECK, INSPECTION REPORTED SHEAR TIE IN FWD CARGO COMPARTMENT CORRODED AT STA 500B, BETWEEN STR 28L AND 28R. REPAIRED PER SRM 53-00-07.

Part: MODULE — FAULTY (FIRE DETECTION) · airframe 21,103 hrs · 9,980 cycles

DURING C-7 CHECK, INSPECTION REPORTED FIRE WARN LIGHT ON P-7, ENG 1/2 OVERHEAT LIGHTS ON P-8 AND CONTROL CABIN ALARM BELL DID NOT OPERATE IN STEPS 1 G-3 AND 1 G-7 OF FIRE WARNING SYSTEM TEST. TEST 1 G-10 PASSED. REPLACED FIRE DETECTION MODULE PER MM 26-10-01. PERFORMED ENGINE FIRE DETECTION OPERATIONAL TEST PER MM 26-11-00 AND CHECKED GOOD. PERFORMED APU FIRE DETECTION OPERATIONAL TEST PER MM 26-15-00 AND CHECKED GOOD.

Part: FLAP TRACK — CORRODED (T/E FLAP) · corrosion level 2 · airframe 21,103 hrs · 9,980 cycles

DURING C-7 CHECK, INSPECTION REPORTED CORROSION ON NR 7 OTBD FLAP TRACK ASSY. REMOVED EXISTING BUSHINGS TO EXPOSE ALL SURFACES TO INSPECTION. INSPECTED FLAP TRACK PER OHM 57-53-15. MACHINED THE HOLE FORWARD OF BUSHING NR 60 PER SOPM 20-10-01 AND SOPM 20-10-02 TO REMOVE CORROSION. PERFORMED ALL POST MACHINING REQUIREMENTS PER SOPM 20-10-02. PERFORMED MAGNETIC PARTICLE INSPECTION OF TRACK PER SOPM 20-20-01. SHOT AND/OR FLAP PEENED THE REWORKED BORE PER SOPM 20-10-03. STYLUS CADMIUM PLATED THE BORE PER SOPM 20-42-10. REFINISHED PER OHN 57-53-15.

Part: BATTERY PACK — FAILED (EVAC SLIDE) · airframe 21,103 hrs · 9,980 cycles

DURING C-7 CHECK, INSPECTION REPORTED FWD GALLEY DOOR ESCAPE SLIDE BATTERY PACK FAILED VOLTAGE TEST. REPLACED FWD GALLEY DOOR ESCAPE SLIDE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 21,103 hrs · 9,980 cycles

DURING C-7 CHECK, INSPECTION REPORTED FRAME CRACKED AT BIN RAIL ATTACH BRACKET HOLE, STA 907, BETWEEN STR 8L AND 9L. REPAIRED PER SRM 53-00-07 FIG 202, STEPS 1-10.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,117 hrs · 8,212 cycles

DURING C-6 CHECK, INSPECTION REPORTED FILLER/STRAP CORRODED BETWEEN STA 787 AND 807, RBL 20 ABOVE STR 25-R. REPLACED FILLER/STRAP PER SRM 51-40-02 AND 51-10-02.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,117 hrs · 8,212 cycles

DURING C-6 CHECK, INSPECTION REPORTED WEB BETWEEN STA 794.3 AND 847, STR 25-R, CORRODED AROUND SEVERAL NUT PLATE HOLES. REPLACED AND INSTALLED WEB PER SRM 51-40-02 AND 51-10-02.

Part: STRAP — CORRODED (STA. 774 - 858) · corrosion level 2 · airframe 18,117 hrs · 8,212 cycles

DURING C-6 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO DOOR LOWER SILL STRAP, STA. 774 TO 858, RBL 20. REPLACED SILL STRAP PER SRM 51-40-07 AND 51-10-02.

Part: SUPPORT ANGLE — GOUGED (APU DOOR) · airframe 18,117 hrs · 8,212 cycles

DURING C-6 CHECK, INSPECTION REPORTED SUPPORT ANGLE ON AFT SIDE OF AFT DOOR LATCH CUTOUT GOUGED ON APU DOOR. FABRICATED NEW SUPPORT ANGLE PER SRM 52-40-02 AND 51-70-11. ALODINED AND PRIMED PER MM 51-21-41 AND SOPM 20-41-02. INSTALLED NEW ANGLE PER SRM 52-40-02 AND 51-70-11.

Part: COWL DOOR — CHAFED · airframe 18,117 hrs · 8,212 cycles

DURING C-6 CHECK, INSPECTION REPORTED PREVIOUS REPAIR ON LT. SECTION OF APU COWL DOOR CHAFFED/GROOVED. REMOVED ADDITIONAL DAMAGE FOUND AT EDGE OF PREVIOUS REPAIR. FABRICATED NEW DOUBLER TO ENCOMPASS NEW CUTOUT IN SKIN PER SRM 52-40-02, 52-40-01, MM 51-21-41 AND SOPM 20-41-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,117 hrs · 8,212 cycles

DURING C-6 CHECK, INSPECTION REPORTED CORROSION ON L-ANGLE IN FWD CARGO COMPARTMENT, STA 500D, LBL 29 TO RBL 21. REPAIRED ANGLE PER SRM 51-40-02, 51-40-05 AND 51-10-02.

Part: SHUTOFF VALVE — FAILED (NR 2 ENGINE) · airframe 17,260 hrs · 7,785 cycles

AIR TURNBACK. FLIGHT CREW REPORTED WING/BODY OVERHEAT ILLUMINATED IN FLIGHT. COMPLIED WITH CHECKLIST AND LIGHT REMAINED ILLUMINATED. PRESSURE IN RT DUCT 10 PSI, WHICH DECREASED TO 5 PSI WHEN THRUST LEVER REDUCED IN POWER. SHUT DOWN NR 2 ENGINE AND MONITORED OIL PRESSURE. REPLACED M237 MODULE AND NR 2 ENGINE PRSOV. PERFORMED OVERWEIGHT LANDING INSPECTION PER MM 05-51-74, PHASE I. NO DAMAGE NOTED. PERFORMED OPERATIONAL TESTS AND CHECKED OKAY.

Part: WIRE — BROKEN (CABIN) · airframe 14,746 hrs · 6,565 cycles

PRIOR TO DEPARTURE, FLIGHT CREW REPORTED EMERGENCY EXIT FLOOR PATH WIRING EXPOSED AT ROW 15. SPLICED BROKEN WIRE PER STANDARD PRACTICES 20-30-12, PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM AND CHECKED OKAY.

Part: FITTING — CORRODED (AFT LAVATORY) · corrosion level 2 · airframe 11,771 hrs · 5,139 cycles

DURING C-4 CHECK, INSPECTION REPORTED CORROSION AROUND RT. AFT LAVATORY OTBD AFT FLOOR MOUNT. MAINTENANCE FABRICATED AND REPLACED NEW FITTING PER EA 25-737-108.

Part: BATTERY — DISCHARGED (R2 DOOR SLIDE)

DEN - DURING C-CHECK INSPECTION REPORTED R-2 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOLTAGE TEST. REPLACED R-2 EMERGENCY ESCAPE SLIDE. CYCLES: 2,635. (X)

Part: BATTERY — DISCHARGED (L1 DOOR SLIDE)

DEN - DURING C-CHECK INSPECTION REPORTED L-1 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOLTAGE TEST. REPLACED L-1 EMERGENCY ESCAPE SLIDE. CYCLES: 2,635. (X)

Part: BATTERY — DISCHARGED (L2 DOOR SLIDE)

DEN - DURING C-CHECK INSPECTION REPORTED L-2 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOLTAGE TEST. REPLACED L-2 EMERGENCY ESCAPE SLIDE. CYCLES: 2,660. (X)

Part: WIRE — LOOSE (CABIN)

DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED WIRES DISCONNECTED FROM FLOOR PROXIMITY LIGHTING AT ROW 13. MAINTENANCE RECONNECTED WIRES AND SYSTEM CHECKED OKAY. (X)