N986AX

Part: RELAY — INTERMITTENT (LANDING GEAR) · airframe 54,818 hrs · 51,308 cycles

UPON SELECTING GEAR DOWN, NO GREEN NOSE GEAR LIGHT WAS OBSERVED. RECYCLED GEAR, GOT 3 GREEN LIGHTS. CHECKED OPERATION OF NOSE GEAR UP AND DOWN LIMIT SWITCHES. NO FAULT FOUND. VERIFIED INTERMITTENT CONTACT BETWEEN A2 AND A3 OF RELAY R2-25. REPLACED RELAY, OPS CHECK GOOD IAW DC9 AMM 32-60-001.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 54,641 hrs · 51,122 cycles

FITTING ON CANTED STA 1143, RIGHT BUTT LINE 6 WAS CRACKED AT LOWER END. REMOVED AND REPLACED RUDDER BEARING SUPPORT FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: PAN — CRACKED (FUSELAGE) · airframe 54,641 hrs · 51,122 cycles

DOUBLER BULGED AND CRACKED AT CENTER OF FORWARD LOWER CARGO DOOR CUTOUT, STA 394, BETWEEN THRESHOLD AND SCUFF PLATE. REMOVED AND REPLACED NEW DOOR PAN IAW DC9 SRM 51-30-2.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,641 hrs · 51,122 cycles

MAIN ENTRY DOOR INTERCOSTAL CRACKED PAST PREVIOUS STOP DRILL IN UPPER FORWARD CORNER AREA. REMOVED AND REPLACED REPAIR IAW DC9 SRM 51-30-5 AND 51-30-1.

Part: WIRE — BURNED (WINDSHIELD HEAT) · airframe 54,026 hrs · 50,580 cycles

DURING FLIGHT AN ARID ODOR WAS NOTICED IN THE GLARESHIELD AREA SIMILAR TO HOT PLASTIC OR HOT ELECTRICAL INSULATION. CENTER WINDSHIELD WAS TOO HOT TO TOUCH SO CENTER WINDSHIELD ANTI-ICE CIRCUIT BREAKER WAS PULLED. ODOR CEASED AND THEN RETURNED WITH CENTER WINDSHIELD STILL HOT TO THE TOUCH. FOUND WIRE H578B16 BURNED AT S1-193. SPLICED IN NEW WIRE. RAN WINDSHIELD HEAT, NO OVERHEATING OCCURRED.

Part: THERMAL SWITCH — FAILED (WINDSHIELD HEAT) · airframe 54,025 hrs · 50,578 cycles

DURING FLIGHT, SMOKE BEGAN EMINATING FROM CENTER WINDSHIELD RIGHT SIDE. WINDSHIELD HEAT WAS SELECTED OFF AND ANTI-ICE CIRCUIT BREAKER'S WERE PULLED. SMOKING STOPPED, WINDSHIELD WAS HOT TO THE TOUCH. INSPECTED CENTER WINDSHIELD FOR DEFECTS AND OHMED OUT WINDSHIELD & TEMPERATURE SENSOR, NO DEFECTS NOTED. REPLACED ANTI-FOG THERMAL SWITCH AND WINDSHIELD TEMPERATURE SENSOR AS PRECAUTION.

Part: CIRCUIT BREAKER — FAULTY (COCKPIT) · airframe 53,738 hrs · 50,333 cycles

UPON GEAR EXTENSION, NO THREE GEAR GREEN OR RED GEAR UNSAFE LIGHTS. FOLLOWED ABNORMALS (GEAR RECYCLE), CONTACTED MAINTENANCE CONTROL. INSTRUCTED TO PULL AND RESET LANDING GEAR WARNING CIRCUIT BREAKER. ALL INDICATIONS THEN WERE NORMAL FOR LANDING. REMOVED AND REPLACED 5 AMP LANDING GEAR WARNING CIRCUIT BREAKER (B1-187). SYSTEM OPS CHECKED GOOD IAW DC9 AMM 32-60-00-0-0101.

Part: ENGINE — DEFECTIVE (LEFT) · airframe 53,233 hrs · 49,890 cycles

NR 1 ENGINE HIGH OIL TEMP. LEFT ENGINE SHUTDOWN AT FLT LEVEL 310 DUE TO OIL TEMP IN THE RED ZONE. INITIALLY TEMP WAS AT TOP OF YELLOW BAND, THEN WENT TO RED, THEN PEGGED ON SHUTDOWN. REMOVED AND REPLACED LEFT ENGINE IAW ABX JOB CARD 90900010.

Part: FITTING — CRACKED (FUSLEAGE) · airframe 53,102 hrs · 49,762 cycles

NR 4 BEAM FORWARD END FITTING CRACKED ON AFT LOWER CARGO DOOR. REMOVED AND REPLACED FITTING AT NR 4 FORWARD BEAM IAW DC-9 SRM 51-30-5.

Part: FITTING — CRACKED (AFT CARGO DOOR) · airframe 53,102 hrs · 49,762 cycles

NR 2 BEAM AFT END FITTING CRACKED ON AFT LOWER CARGO DOOR. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-5.

Part: WEB — CRACKED (AFT CARGO) · airframe 52,023 hrs · 48,688 cycles

CUSP WEB HAD 5 EACH CRACKS BETWEEN FS 945 AND 965. REMOVED AND REPLACED SECTION OF CUSP WEB IAW DC-9 SRM 51-30-2, 51-30-1 AND 50-01.

Part: STRUCTURE — CORRODED (LT ELEVATOR) · corrosion level 2 · airframe 52,023 hrs · 48,688 cycles

LEFT ELEVATOR OUTBOARD OF GEARED TAB HAD LEVEL II CORROSION WITH DISHED RIVETS AND BULGING SKIN. REPLACED LEFT ELEVATOR ON NON ROUTINE 0518, IAW DC-9 MM.

Part: DOWNLOCK SWITCH — MALFUNCTIONED (NLG) · airframe 51,235 hrs · 47,853 cycles

INITIAL LANDING GEAR EXTENSION, NOSE GEAR GREEN LIGHT EXTINGUISHED. RECYCLED GEAR FOR DOWN AND LOCKED. NOSE GEAR GREEN LIGHT ILLUMINATED AS NORMAL. REPLACED THE NOSE LANDING GEAR DOWNLOCK SWITCH AND THROTTLE TRANSFER RELAY, NO HELP. REPLACED THE NOSE LANDING GEAR DOWNLOCK LIGHT ASSEMBLY. OPS CHECKED GOOD IAW DC-9 MM.

Part: LIGHT — CORRODED (COCKPIT) · airframe 51,228 hrs · 47,848 cycles

UPON GEAR EXTENSION, NOSE LANDING GEAR LIGHT WOULD NOT ILLUMINATE. AFTER GEAR WAS RECYCLED, THE NOSE GEAR LIGHT ILLUMINATED. FOUND MINOR CORROSION ON THE NOSE LANDING GEAR INDICATION LIGHT. REPLACED THE NOSE LANDING GEAR INDICATION LIGHT BULBS. PERFORMED GEAR SWING IAW DC-9 MM 32-60-00. OPS CHECKED GOOD.

Part: PANEL — CORRODED (CABIN) · airframe 50,975 hrs · 47,594 cycles

LEVEL I CORROSION UNDER 8 EACH LOWER FLOATING NUT PLATES ON THE RIGHT SLANT PANEL. REMOVED AND REPLACED THE RIGHT SLANT PANEL IAW DC-9 SRM 51-30-2, 51-30-1 AND 51-20-0.

Part: PANEL — CORRODED (CABIN) · airframe 50,975 hrs · 47,594 cycles

LEVEL I CORROSION UNDER 10 EACH LOWER FLOATING NUT PLATES ON LEFT SLANT PANEL. REMOVED AND REPLACED THE LEFT SLANT PANEL IAW DC-9 SRM 51-30-1.

Part: SKIN — CORRODED (FUSELAGE) · airframe 50,975 hrs · 47,594 cycles

FUSELAGE SKIN FLUSH REPAIR BULGING OUTWARD AND HAD RIVETS INSTALLED INTO RIVETS, STATION 379, BETWEEN LONGERON 2 - 3 RIGHT. REPAIRED AREA IAW DC-9 SRM 53-04.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 50,762 hrs · 47,379 cycles

COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC-9 MM 33-53-0.

Part: SWITCH — INTERMITTENT (NLG) · airframe 50,320 hrs · 46,930 cycles

WHEN THE MAIN LANDING GEAR WAS EXTENDED A NOSE GEAR UNSAFE LIGHT DID NOT ILLUMINATE. THE CREW COMPLETED A GEAR RECYCLE AND ALL INDICATIONS CHECKED NORMAL. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR UP LIMIT SWITCH AND COMPLETED OPERATIONAL CHECKS.

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,741 hrs · 46,392 cycles

EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY.

Part: SHEAR TIE — CRACKED (RT SPAR) · airframe 49,715 hrs · 46,362 cycles

SHEAR CLIP CRACKED AT STATION 111.000 AND REAR SPAR STRINGER 11. REPLACED SHEAR CLIPIAW DC9 SRM 51-30-5.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 49,715 hrs · 46,362 cycles

OUTBOARD FIXED VANE DELAMINATED ON TOP SIDE. REPLACED OUTBOARD FIXED VANE.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 49,715 hrs · 46,362 cycles

LONGERON 14 RIGHT AT STATION 1076 WAS CRACKED UNDER FRAME. REPLACED LONGERON SECTION IAW DC9 SRM 53-02.

Part: STRUCTURE — CRACKED (CARGO DOOR) · airframe 49,715 hrs · 46,362 cycles

FORWARD LOWER CARGO DOOR WAS CRACKED IN 2 PLACES AT NR 2 STOP. REPLACED FORWARD LOWER CARGO DOOR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,715 hrs · 46,362 cycles

FUSELAGE FRAME CRACKED BETWEEN FASTENERS ON FORWARD FLANGE AT STATION 598 BELOW LONGERON 11 LEFT. REPAIRED CRACK IAW ABX REA D953-38087MR.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 49,715 hrs · 46,362 cycles

INTERCOSTAL CRACKED INSIDE ENTRY DOOR FORWARD OF HANDLE. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2.

Part: STRUCTURE — DELAMINATED (MLG DOOR) · airframe 49,715 hrs · 46,362 cycles

LEFT FLYING DOOR (FORWARD HALF) HAD AREA OF DELAMINATION. REPLACED OUTBOARD LEFT MAIN LANDING GEAR DOOR.

Part: PAN — CRACKED (PAX DOOR) · airframe 49,715 hrs · 46,362 cycles

ENTRY DOOR INNER PAN TO SIDE STRUCTURE ATTACH FRAME CRACKED. REPAIRED IAW ABX REA D952-38104.

Part: FITTING — CRACKED (PAX DOOR) · airframe 49,715 hrs · 46,362 cycles

ENTRY DOOR HAS CRACKED BEAM END FITTING ABOVE BAYONET. REPLACED FITTING IAW DC9 SRM 51-30-1.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTING WOULD NOT TEST. REPLACED EMERGENCY LIGHTS BATTERY PACK.

Part: ANGLE — CRACKED (LT PYLON)

DURING C-CHECK, FOUND LEFT PYLON UPPER ATTACH ANGLE CRACKED. REPAIRED ATTACH ANGLE IAW DC9 SRM 54-04.

Part: BULKHEAD WEB — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED. REPAIRED WEB CRACK IAW ABX REA D953-26127MR.

Part: FITTING — CRACKED (HORIZ STAB)

DURING C-CHECK, FOUND CRACKED FITTING ON HORIZONTAL STABILIZER CENTER SECTION AT NUT CHANNEL. REPLACED FITTING IAW DC9 SRM 51-30-01.

Part: SKIN — CORRODED (LT TE FLAP)

DURING C-CHECK, FOUND CORROSION ON UPPER SURFACE OF LEFT FLAP AFT OF MOVEABLE VANE. REPLACED UPPER SKIN ON INBOARD FLAP TRAILING EDGE IAW DC9 SRM 51-30-01.

Part: SHEAR TIE — CRACKED (BS 980)

DURING C-CHECK, FOUND FUSELAGE FRAME SHEAR TIE AT STATION 980 CRACKED AT LONGERON 15 LEFT. REPLACED SHEAR TIE IAW DC9 SRM 51-30-2.

Part: SHEAR TIE — CRACKED (BS 980)

DURING C-CHECK, FOUND FUSELAGE FRAME SHEAR TIE AT STATION 980 CRACKED ABOVE LONGERON 16 RIGHT. REPLACED SHEAR TIE IAW DC9 SRM 51-30-2.

Part: SUPPORT — CRACKED (LT SPOILER)

DURING C-CHECK, FOUND LEFT INBOARD SPOILER TORQUE TUBE INBOARD SUPPORT CRACKED. REPLACED SUPPORT IAW DC9 SRM 51-30-1.

Part: LONGERON — CRACKED (BS 980)

DURING C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT STATION 980. REPLACED LONGERON SECTION IAW DC9 SRM 53-02.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT STATIONS 965 AND 980. REPLACED LONGERON 17 RIGHT SECTION IAW DC9 SRM 53-02.

Part: BULKHEAD FITTING — CRACKED (BS 965)

DURING C-CHECK, FOUND LEFT PYLON BULKHEAD, LOWER FORWARD, SUPPORT FITTING AT STATION 965 CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1.

Part: LONGERON — CRACKED (BS 160)

DURING C-CHECK, FOUND LONGERON 3 LEFT CRACKED AT STATION 160. SPLICED IN NEW SECTION OF LONGERON IAW DC9 SRM 53-02.

Part: BULKHEAD FITTING — CRACKED (BS 965)

DURING C-CHECK, FOUND LEFT PYLON BULKHEAD AT STATION 965, LOWER SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-01.

Part: SOCKET — INOPERATIVE (GEAR DOOR)

THE GEAR DOOR OPEN LIGHT DID NOT ILLUMINATE WHEN THE LANDING GEAR LEVER WAS PUT IN THE DOWN POSITION DURING APPROACH. REPLACED THE GEAR DOOR OPEN LIGHT SOCKET.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS COME ON WHEN AIRCRAFT POWER IS TURNED OFF, WITH LIGHT SWITCH DISARMED OR OFF. REPLACED EMERGENCY BATTERY POWER SUPPLY IAW DC9 MM 33-50-0.

Part: GEARBOX — LEAKING (NR 2 ENGINE)

DURING CLIMB, NR 2 ENGINE OIL PRESSURE LOW LIGHT ILLUMINATED, OIL PRESSURE AND OIL QUANTITY GAUGE DECREASED TO ZERO. SECURED ENGINE. NR 2 ENGINE GEARBOX FOUND TO BE LEAKING. REPLACED GEARBOX IAW PRATT- WHITNEY MM 72-60.

Part: FLOORBEAM — CORRODED (BS 965)

DURING C-CHECK, FOUND THE FLOORBEAM AFT LOWER FLANGE HEAVILY CORRODED AT F/STA 965 AND LBL 10. REPAIRED IAW ABX REA D953-19401-MR.

Part: FRAME — CRACKED (BS 617)

DURING C-CHECK, FOUND LT FUSELAGE FRAME AT F/STA 617, LONGERON 14L CRACKED. REPAIRED FRAME IAW ABX REA D53-19396-MR.

Part: FLOORBEAM — CORRODED (BS 965)

DURING C-CHECK, FOUND THE FLOORBEAM AT F/STA 965, LBL 47 LOWER FLANGE HEAVILY CORRODED. REPAIRED IAW ABX REA D953-19407-MR.

Part: CONTROL CABLE — CORRODED (RT MLG WW)

DURING C-CHECK, FOUND THE EMERGENCY FUEL SHUTOFF CABLE INSIDE THE FORWARD PULLEY JUST BELOW THE PRESSURE FAIRLEAD IN TOP OF RT WHEEL WELL HEAVILY RUSTED. REPLACED CABLE RUN 149C IAW DC9 MM 75-20.

Part: CONTROL CABLE — CORRODED (RT MLG WW)

DURING C-CHECK, FOUND THE LANDING GEAR CONTROL CABLES HEAVY RUSTED INSIDE THE PULLEY JUST ABOVE THE LANDING CONTROL VALVE. REPLACED CABLE RUN 102A IAW DC9 MM 32-31-0.

Part: ANGLE — CRACKED (BS 237)

DURING C-CHECK, FOUND A CRACKED INTERCOSTAL ATTACH ANGLE CRACKED AT F/STA 237 BETWEEN LONGERONS 27R AND 28R. REPLACED CRACKED INTERCOSTAL ATTACH ANGLE IAW DC9 SRM 51-30-5.

Part: HINGE FITTING — CRACKED (AFT ACC COMP)

DURING C-CHECK, FOUND THE LT HINGE FITTING F/STA 1059 FOR AFT VENTRAL DOOR CRACKED. REMOVED AND REPLACED HINGE FITTING IAW DC9 SRM 51-30-1 AND 52-63-00.

Part: CONTROL CABLE — CORRODED (LT MLG WW)

DURING C-CHECK, FOUND THE EMERGENCY FUEL SHUTOFF CABLE INSIDE THE PULLEY JUST BELOW THE PRESSURE FAIRLEAD IN TOP OF LT WHEEL WELL HEAVILY RUSTED. REPLACED CABLE RUN 140C IAW DC9 MM 76-20-0.

Part: SEAT TRACK — CORRODED (BS 200)

DURING C-CHECK, FOUND SEAT TRACK CORRODED AT F/STA 200 RBL 44. REPLACED SEAT TRACK IAW DC9 SRM 51-30-1, 51-30-5, AND 51-30-4.

Part: SKIN — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND THE FUSELAGE SKIN UNDER THE RT STATIC PORT PLATE CORRODED. REMOVED CORROSION AND REPAIRED SKIN IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: ANGLE — CRACKED (NR 1 PYLON)

DURING C-CHECK, FOUND NR 1 PYLON LOWER OUTBOARD ANGLE CRACKED FORWARD OF AFT ENGINE MOUNT. REPAIRED IAW ABX REA D954-19336.

Part: SKIN — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND THE FUSELAGE SKIN UNDER THE LT STATIC PORTED PLATE CORRODED. FABRICATED INTERNAL DOUBLER (P/N 5920419-3) AND REPAIRED IAW ABX REA D953-19365.

Part: ANGLE — CRACKED (NR 1 PYLON)

DURING C-CHECK, FOUND ATTACH ANGLE CRACKED INSIDE OF NR 1 PYLON UPPER OUTBOARD CORNER INSIDE PANEL 8105A. REPLACED ANGLE (P/N 9958154-9) AND FITTING (P/N 4919864-1) IAW DC9 SRM 51-30-1, 51-30-2 AND 51-10-4.

Part: TAB — DELAMINATED (LT ELEVATOR)

DURING C-CHECK, FOUND THE LEFT ELEVATOR GEARED TAB INBOARD LOWER SURFACE DELAMINATED. *S/D* REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.

Part: IDLER LINK — CHAFED (NR 2 ENGINE)

DURING C-CHECK, FOUND NR 2 THRUST REVERSER IDLER LINK CHAFED UPPER T/R DOOR INBOARD SIDE NEAR SMALL END. REPLACED UPPER INBOARD IDLER LINK IAW DC9 78-31-5, IAW DC9 SRM 51-30-1, 51-30-2, 51-30-5 AND 51-10-4.

Part: HAT CHANNEL — CRACKED (LT WING)

DURING C-CHECK, FOUND PANEL NR 2206A HAT CHANNEL CRACKED. REPAIRED HAT CHANNEL IAW ABX SSRM DWG K05159.

Part: FRAME — CRACKED (BS 699)

DURING C-CHECK, FOUND THE LT MAIN FRAME AT F/STA 699 CRACKED IN THE FORWARD INBOARD FLANGE. REPLACED MAIN FRAME IAW DC9 SB 53-131 AND ABX REA D953-19377-MR.

Part: FRAME — CRACKED (BS 699)

DURING C-CHECK, FOUND THE RT MAIN FRAME AT F/STA 699 CRACKED IN THE AFT INBOARD FLANGE. REPLACED MAIN FRAME IAW DC9 SB 53-131 AND ABX REA D953-19377-MR.

Part: IDLER LINK — CHAFED (NR 2 ENGINE)

DURING C-CHECK, FOUND NR 2 THRUST REVERSER IDLER LINK CHAFED UPPER T/R DOOR OUTBOARD SIDE NEAR SMALL END. REPLACED UPPER OUTBOARD IDLER LINK IAW DC9 78-31-5, IAW DC9 SRM 51-30-1, 51-30-2, 51-30-5 AND 51-10-4.

Part: WEB — CRACKED (NR 1 PYLON)

DURING C-CHECK, FOUND NR 1 PYLON OUTBOARD WEB CRACKED AT LOWER ATTACH ANGLE FORWARD OF AFT ENGINE MOUNT. REPLACED WEB (P/N 9958221-3) IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: IDLER LINK — CHAFED (NR 2 ENGINE)

DURING C-CHECK, FOUND NR 2 THRUST REVERSER IDLER LINK CHAFED LOWER T/R DOOR OUTBOARD SIDE NEAR SMALL END. REPLACED LOWER OUTBOARD IDLER LINK IAW DC9 78-31-5, IAW DC9 SRM 51-30-1, 51-30-2, 51-30-5 AND 51-10-4.

Part: SWITCH — DEFECTIVE (NLG)

GREEN NOSE LANDING GEAR INDICATOR INTERMITTENTLY INOPERATIVE. BOTH BULBS. RECYCLED GEAR ON FINAL APPROACH, LIGHT CAME ON, BUT LATER WENT OUT. REPLACED NOSE GEAR DOWNLOCK SWITCH PER DC-9 M.M.

Part: CONNECTOR — CONTAMINATED (NLG)

ON GEAR EXTENSION NOSE GREEN LIGHT DID NOT ILLUMINATE, ALL OTHER RED AND MAIN GREENS NORMAL. RECYCLED AND LIGHTS NORMAL. CLEANED WATER FROM NOSE GEAR DOWNLOCK SWITCH CANNON PLUG. NOSE DOWNLOCK GREEN LIGHT INDICATION NORMAL IAW DC-9 SUPP MM.

Part: BUSHING — WORN (LT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND WING MOUNTED HINGE ON THE LEFT OUTBOARD MAIN LANDING GEAR DOOR HAD EXCESSIVE SIDE PLAY. REPAIRED IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: ANGLE — CRACKED (WS 383)

DURING C-CHECK INSPECTION, FOUND BOTH OUTBOARD FLAP HINGE ATTACH BRACKETS CRACKED INSIDE RIGHT FLAP. REPLACED BRACKETS IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: ANGLE — CRACKED (WS 383)

DURING C-CHECK INSPECTION AND COMPLIANCE OF AD 92-22-08, FOUND BOTH OUTBOARD FLAP HINGE ATTACH BRACKETS CRACKED INSIDE THE RIGHT FLAP. REPLACED BRACKETS IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: ANGLE — CRACKED (WS 383)

DURING C-CHECK INSPECTION, FOUND BOTH OUTBOARD FLAP HINGE ATTACH BRACKETS CRACKED INSIDE THE LEFT FLAP. REPLACED BRACKETS IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: ANGLE — CRACKED (WS 383)

DURING C-CHECK INSPECTION, FOUND BOTH OUTBOARD FLAP HINGE ATTACH BRACKETS CRACKED INSIDE LEFT FLAP. REPLACED BRACKETS IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: CV WINDOW — MALFUNCTIONED (RT COCKPIT)

DURING PREFLIGHT INSPECTION, FOUND FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT CLOSE. OPENED, INSPECTED, CLOSED FIRST OFFICER'S WINDOW. OPS CHECKED GOOD IAW DC9 MM.