N952AX

Part: FRAME — CORRODED (BS 579 L30) · airframe 56,591 hrs · 46,491 cycles

FORWARD LOWER CARGO FRAME AT STATION 579 WAS CORRODED AT LONGERON 30. REPAIRED FRAME IN ACCORDANCE WITH DC9 SRM 53-03.

Part: BRACKET — CORRODED (SPOILER CONTROL) · airframe 56,591 hrs · 46,491 cycles

SPOILER CONTROL TORQUE TUBE BRACKET CORRODED. REMOVED AND REPLACED SPOILER TORQUE TUBE BRACKET IN ACCORDANCE WITH DC9 MAINTENANCE MANUAL 20-16-00-2-0001.

Part: ATTACH ANGLE — CRACKED (RT NACELLE) · airframe 56,591 hrs · 46,491 cycles

LOWER PYLON LEADING EDGE ATTACH ANGLE CRACKED. REMOVED AND REPLACED FORWARD SECTION OF PYLON LOWER ATTACH ANGLE IN ACCORDANCE WITH DC9 SRM 54-04.

Part: SEAT TRACK — CORRODED (BS 996-1021) · airframe 56,591 hrs · 46,491 cycles

SEAT TRACK CORRODED AT LEFT BUTT LINE 9.88, STATION 996-1021. REMOVED AND REPLACED TRACK IN ACCORDANCE WITH DC9 SRM 51-30-5 AND 51-30-1.

Part: GUSSET — CRACKED (BS 206 L16L) · airframe 56,591 hrs · 46,491 cycles

FS 206.00, LONGERON 16 LEFT GUSSET CRACKED. REMOVED AND REPLACED GUSSET IN ACCORDANCE WITH DC9 SRM.

Part: LONGERON — CRACKED (BS 1041-1056) · airframe 56,591 hrs · 46,491 cycles

LONGERON 17 LEFT CRACKED AT FRAME ATTACH POINTS AT STATION 1041 AND 1056. REMOVED AND REPLACED LONGERON SECTION IN ACCORDANCE WITH DC9 SRM.

Part: LONGERON — CRACKED (BS 1041 L16R) · airframe 56,591 hrs · 46,491 cycles

LONGERON 16 RIGHT CRACKED AT UPPER FRAME ATTACH HOLE AT STATION 1041. REMOVED AND REPLACED SECTION IN ACCORDANCE WITH DC9 SRM 53-02.

Part: FLOORBEAM — CORRODED (BS 1011) · airframe 56,591 hrs · 46,491 cycles

FLOORBEAM AT STATION 1011 LOWER FORWARD FLANGE CORRODED AT APPROXIMATELY RIGHT BUTT LINE 15 UNDER NUT PLATES. REPAIRED FLOORBEAM IN ACCORDANCE WITH DC9 SSRM K07411.

Part: GUSSET — CRACKED (BS 206) · airframe 56,591 hrs · 46,491 cycles

FS 206.00, APPROXIMATE LONGERON 11 LEFT, GUSSET CRACKED. REMOVED AND REPLACED GUSSET IN ACCORDANCE WITH DC9 SRM.

Part: SUPPORT ANGLE — CRACKED (MLG DOOR) · airframe 56,591 hrs · 46,491 cycles

LEFT MAIN LANDING GEAR DOOR ACTUATOR SUPPORT ANGLE CRACKED FORWARD SIDE. REMOVED AND REPLACED IN ACCORDANCE WITH DC9 SRM.

Part: ATTACH FITTING — CRACKED (LT WING SPOILER) · airframe 56,591 hrs · 46,491 cycles

LEFT WING OUTBOARD SPOILER, OUTBOARD SPOILER ATTACH FITTING CRACKED. REMOVED AND REPLACED FITTING IN ACCORDANCE WITH DC9 SRM.

Part: LONGERON — CRACKED (BS 160) · airframe 56,591 hrs · 46,491 cycles

LONGERON 4 LEFT CRACKED AT FRAME ATTACH POINTS AT STATION 160. SPLICED IN NEW LONGERON IN ACCORDANCE WITH DC9 SRM.

Part: SUPPORT — CRACKED (RT SPOILER) · airframe 56,591 hrs · 46,491 cycles

RIGHT INBOARD SPOILER TORSION BAR CENTER SUPPORT CRACKED IN THREE (3) PLACES. REPLACED SUPPORT ASSEMBLY IN ACCORDANCE WITH DC9 SRM 51-30-5.

Part: FRAME — CORRODED (BS 598 L30)

FORWARD LOWER CARGO AFT SIDE AND LOWER LEG OF FRAME CORRODED FS 598 AT LONGERON 30. BLENDED AREA IN ACCORDANCE WITH DC9 SRM.

Part: COUNTERBALANCE — CORRODED (RIGHT ELEVATOR) · airframe 56,591 hrs · 46,491 cycles

RIGHT ELEVATOR COUNTERBALANCE HEIGHT RUSTY IN SEVERAL AREAS. REPAIRED AREA IN ACCORDANCE WITH REA D955-56583.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 55,978 hrs · 46,073 cycles

EMERGENCY LIGHTS WOULD NOT STAY ON. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW MM 33-53-00.

Part: CONTROL BOX — DEFECTIVE (MLG PROXIMITY) · airframe 55,420 hrs · 45,747 cycles

RT MAIN GEAR UNSAFE LIGHT WITH ASSOCIATED RT LANDING GEAR GREEN LIGHT. ALTERNATE MAIN GEAR INDICATION OPERATES NORMAL. REPLACED PROXIMITY SWITCH CONTROL BOX IAW MM 32-60-01-2.

Part: DUCT — LOOSE (A/C BAY) · airframe 54,689 hrs · 45,285 cycles

WHEN PRESSURIZATION WAS SET AT TOP OF DESCENT AND POWER WAS PULLED BACK (1.3 EPR), THE CABIN BEGAN TO CLIMB AT 300 FPM. CABIN ALTITUDE REACHED 10,000 FT AND CREW TOOK OVER PRESSURIZATION MANUALLY. CREW WENT ON OXYGEN. FOUND COLD AIR DUCT LOOSE AT WATER SEPARATOR-TIGHTENED DUCT AND CLEANED CABIN PRESSURE CONTROL AIR FILTERS. OPERATIONAL CHECKED GOOD.

Part: STOP FITTING — CRACKED (MLG DOOR FRAME) · airframe 54,183 hrs · 45,060 cycles

AFT P DOME DOOR JAMB UPPER RIGHT DOOR STOP FITTING CRACKED. REMOVED AND REPLACED AFT P DOME DOOR JAMB UPPER RIGHT DOOR STOP FITTING IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: KEELBEAM — CRACKED (CENTER WING SECT) · airframe 54,183 hrs · 45,060 cycles

END FITTING SIDE SUPPORT CRACKED ON LEFT SIDE OF KEEL BEAM CENTER SUPPORT LONGERON 30, FS 646 APPROXIMATELY. REMOVED AND REPLACED END FITTING AT STA 646, LONGERON 30 IAW DC-9 SRM 51-30-5.

Part: FITTING — CORRODED (CENTER WING SECT) · airframe 54,183 hrs · 45,060 cycles

END FITTING CORRODED JUST INBOARD OF LONGERON 29 RIGHT IN KEEL BEAM AREA LOWER WING CENTER SECTION FS 649. REMOVED AND REPLACED END FITTING IAW DC-9 SRM 51-30-5.

Part: FITTING — CORRODED (BS 649) · airframe 54,183 hrs · 45,060 cycles

END FITTING CORRODED LONGERON 29 LEFT APPROXIMATELY STA FS 649, LOWER WING CENTER SECTION IN KEEL BEAM AREA. REMOVED AND REPLACED LONGERON END FITTING IAW DC-9 SRM 51-30-5.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 54,183 hrs · 45,060 cycles

ATTACH BRACKET ON AFT SIDE OF PYLON BULKHEAD AT LONGERON 17 RIGHT WAS CRACKED. REMOVED AND REPLACED BRACKET IAW DC9 SRM 51-30-2.

Part: SHEAR TIE — CRACKED (BS 1021) · airframe 54,183 hrs · 45,060 cycles

SHEAR TIE CRACKED AT STA 1021 BETWEEN LONGERON 15 RIGHT AND LONGERON 16 RIGHT. REMOVED AND REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5 AND 51-30-2.

Part: CONTROL BOX — DEFECTIVE (MLG PROXIMITY) · airframe 53,996 hrs · 44,945 cycles

GEAR DOOR OPEN LIGHT ILLUMINATED IN FLIGHT. INSPECTED AIRCRAFT MAIN LANDING GEAR DOOR UPLATCHES AND MECHANISMS IAW DC-9 AMM 32-60-03-2. ALL OKAY, NO DEFECTS NOTED. INSPECTED PROX SENSORS FOR POSITIONING AND ATTACHMENT, NO DEFECTS NOTED. REMOVED AND REPLACED LANDING PROX SWITCH CONTROL BOX IAW DC-9 AMM. OPS CHECKED GOOD. LUBRICATED MAIN LANDING GEAR DOOR UPLATCHES AND ROLLERS. ALL OKAY. (PROBLEM REPORTED OUT OF GEG EN ROUTE TO BIL) DIVERTED AIRCRAFT TO SLC. CREW RECYCLED GEAR INTO SLC, GEAR RECYCLED OKAY.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,673 hrs · 44,014 cycles

FUSELAGE SKIN CRACKED AT LEFT AFT NOSE LANDING GEAR DOOR AFT HINGE. REPAIRED LEFT SKIN CRACK IAW DC-9 SRM 53-05.

Part: SUPPORT — CRACKED (LT SPOILER) · airframe 51,673 hrs · 44,014 cycles

LEFT OUTBOARD SPOILER OUTBOARD SUPPORT TEE WAS CRACKED. REPLACED SUPPORT TEE IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: BRACKET — CORRODED (SEAT TRACK) · corrosion level 2 · airframe 51,673 hrs · 44,014 cycles

LEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 237 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED BRACKET IAW DC-9 SRM 51-30-5.

Part: SUPPORT — CORRODED (SEAT TRACK) · corrosion level 2 · airframe 51,673 hrs · 44,014 cycles

LEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 427 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED ATTACH BRACKET IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: BRACKET — CORRODED (CARGO TRACK) · corrosion level 2 · airframe 51,673 hrs · 44,014 cycles

LEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 541 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED BRACKET IAW DC-9 SRM 51-30-5.

Part: SUPPORT — CORRODED (CARGO TRACK) · corrosion level 2 · airframe 51,673 hrs · 44,014 cycles

LEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 365 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED ATTACH BRACKET IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: BRACKET — CORRODED (CARGO TRACK) · corrosion level 2 · airframe 51,673 hrs · 44,014 cycles

LEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD CARGO AT FS 484 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED BRACKET IAW DC-9 SRM 51-30-5.

Part: BRACKET — CORRODED (CARGO TRACK) · corrosion level 2 · airframe 51,673 hrs · 44,014 cycles

LEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 446 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED BRACKET IAW DC-9 SRM 51-30-5.

Part: SPAR — CORRODED (LT WING) · airframe 51,673 hrs · 44,014 cycles

ANGLE EXFOLIATED AND BULGED UPPER AFT FLANGE OF REAR SPAR UPPER TEE JUST OUTBOARD OF TRUNNION. REPLACED TEE ANGLE XRS 111.00 LEFT WING IAW DC-9 SRM.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,673 hrs · 44,014 cycles

AFT ACCESSORY LONGERON 11 RIGHT END FITTING EXFOLIATED JUST FORWARD OF CANTED FRAME. REPLACED LONGERON 11 RIGHT END FITTING IAW DC-9 SRM 51-30-5.

Part: WINDOW — STIFF (COCKPIT) · airframe 51,250 hrs · 43,847 cycles

CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. MAINTENANCE OPS CHECKED WINDOW ON GROUND. OPS CHECKED GOOD IAW DC9 MM 56-10-03.

Part: BRACKET — BROKEN (RIGHT WING) · airframe 50,179 hrs · 43,385 cycles

SLAT DISAGREEMENT LIGHT ILLUMINATED UPON SLAT EXTENSION. FLIGHT CREW VERIFIED THROUGH FLIGHT CONTROLS THAT THERE WAS AN ASSYMETRY PROBLEM. FLIGHT CREW RETRACTED SLATS AND MADE A NO SLAT LANDING. FOUND AT ILN, #1 AND #2 SLAT PULLEY BRACKETS BROKEN, AND 3 EACH LEADING EDGE RIBS (FORMERS) DAMAGED. THE RIGHT #2 SLAT DRIVE TRACK CABLE PULLEY BRACKET (P/N 3920277-2) WAS BROKEN IN HALF AT BOTH FEET AND CORRODED AT A SMALL CORNER OF THE BROKEN SURFACE. REPLACED PULLEY BRACKET IAW DC-9 MM 20-17-2-001.

Part: SUPPORT — BROKEN (RIGHT WING) · airframe 50,179 hrs · 43,385 cycles

SLAT DISAGREEMENT LIGHT ILLUMINATED UPON SLAT EXTENSION. FLIGHT CREW VERIFIED THROUGH FLIGHT CONTROLS THAT THERE WAS AN ASSYMETRY PROBLEM. FLIGHT CREW RETRACTED SLATS AND MADE A NO SLAT LANDING. FOUND AT ILN, NR 1 AND NR 2 SLAT PULLEY BRACKETS BROKEN AND 3 EACH LEADING EDGE RIBS (FORMERS) DAMAGED. THE RIGHT NR 1 SLAT INBOARD IDLER PULLEY SUPPORT UPPER INBOARD ATTACH BOLT LUG WAS BROKEN IN HALF, CORRODED WITHIN THE BOLT HOLE AND CORRODED ON THE BROKEN SURFACE. THE LOWER INBOARD BOLT LUG WAS ALSO BROKEN BUT NOT CORRODED. REPLACED THE IDLER PULLEY SUPPORT IAW DC-9 MM 20-17-2-001.

Part: CONTROLLER — MALFUNCTIONED (AUTOPILOT) · airframe 49,795 hrs · 43,191 cycles

ELEVATOR OSCILLATES VIOLENTLY WHEN AUTO PILOT WAS ENGAGED. COULD NOT DUPLICATE. REPLACED THE AUTO PILOT CONTROLLER IAW DC9 M.M. 22-10-00-5. AUTO PILOT SYSTEM OPS CHECK GOOD.

Part: ANGLE — CRACKED (EXT. FUSELAGE) · airframe 49,368 hrs · 43,045 cycles

LOWER RIGHT PYLON ATTACH ANGLE WAS CRACKED AT STATION 1072. INSTALLED SECTION OF ATTACH ANGLE IAW DC-9 SRM 54-04.

Part: SPAR — CRACKED (ELEVATOR) · airframe 49,368 hrs · 43,045 cycles

UNREPAIRED CRACKS NOTED ON LEFT ELEVATOR FRONT SPAR .625 INCH LONG AT XE 174.5 AND .75 INCH AT XE 172.5. INSTALLED NEW ELEVATOR IAW DC-9 MM.

Part: BRACKET — CORRODED (SPOILER) · airframe 49,368 hrs · 43,045 cycles

SPOILER - ACTUATOR MIXER BRACKET WAS CORRODED AND PITTED IN NUMEROUS PLACES. REPLACED MIXER BRACKET IAW DC-9 MM.

Part: DOOR — CHAFED (LT MLG) · airframe 49,368 hrs · 43,045 cycles

LEFT MAIN LANDING GEAR OUTBOARD DOOR CHAFED ON INNER FORWARD LIP AND UNDER ARTICULATING DOOR COUNTER BALANCE ARM. REPLACED THE LEFT MAIN LANDING GEAR OUTBOARD DOOR AIW DC-9 MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,628 hrs · 42,767 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED THE EMERGENCY EVACUATION LIGHTS BATTERY PACK IAW DC-9 MM 33-53-02.

Part: BATTERY — DISCHARGED (CABIN) · airframe 48,450 hrs · 42,709 cycles

EMERGENCY LIGHTS FAILED TEST. REPLACED THE EMERGENCY LIGHT BATTERIES IAW DC-9 MM 33-53-02-4-001. OPS CHECKED GOOD IAW DC-9 MM 33-53-00.

Part: FIRE WARNING — MALFUNCTIONED (COCKPIT) · airframe 48,450 hrs · 42,709 cycles

LOOP-A LEFT ENGINE LIGHT ILLUMINATED DURING DESCENT. PERFORMED ABNORMAL CHECKLIST AND REMAINED ON LOOP-B. INSPECTED LOOP FOR DEFECTS, NONE FOUND. CHECKED CONTINUITY OF LOOP, ALL OK. CLEANED CONNECTOR FROM WATER/OIL SOAKAGE. OPS CHECKED GOOD IAW DC-9 AMM CHAPTER 26.

Part: WINDOW — OPEN (COCKPIT) · airframe 47,929 hrs · 42,432 cycles

OUT OF 2500 FT AGL, THE CAPTAIN'S CLEAR VIEW WINDOW OPENED AND DUMPED PRESSURIZATION. CHECKED AND INSPECTED CAPTAIN'S CLEAR VIEW WINDOW PER DC9 AMM 56-10-03. PRESSURIZED AIRCRAFT TO 3 PSI. NO LEAKS NOTED. CHECKED CLEARANCES OF THE LOWER AFT HOOK AND FITTING, AFT LOCK BAR, FORWARD LOCK BAR STOP AND FORWARD LOCK HOOK & FITTING. ALL FOUND WITHIN LIMITS. CHECKED THE WINDOW FRAME AND SEALS. NO DEFECTS FOUND. LUBRICATED THE LOWER AFT LINKAGE ROD IAW DC9 AMM 56-10.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,482 hrs · 42,249 cycles

THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE DURING THE PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERIES IAW DC-9 MM.

Part: STUD — BROKEN (LT TE FLAP) · airframe 47,005 hrs · 42,030 cycles

LEFT FLAP OUTBOARD FLAP HINGE FITTING, OUTBOARD LOWER SPAR ATTACH STUD WAS BROKEN. MAINTENANCE INSPECTED AND REPLACD 4 OUTBD FLAP HINGE STUDS IAW DC-9 MM 57-118, 57-40-01 AND SERVICE SKETCH 2673.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 46,749 hrs · 41,911 cycles

FORWARD UPPER ROTATING BEACON DOUBLER WAS CRACKED AT MOUNTING HOLE. MAINTENANCE REPLACED THE DOUBLER IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: STRAP — CRACKED (RT PYLON) · airframe 46,749 hrs · 41,911 cycles

UPPER RIGHT PYLON TO FUSELAGE ATTACH ANGLE AT STATION 1095 WAS REPORTED TO BE CRACKED. MAINTENANCE REMOVED SPLICE STRAP AND DYE CHECKED THE AREA. NO CRACKS WERE NOTED IAW ABX GMM CHAPTER 3 SECTION 5.01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,749 hrs · 41,911 cycles

RIGHT FUSELAGE FRAME AT STATION 677 WAS CRACKED AT LOWER END BELOW CUSP IN THE RADIOUS. MAINTENANCE INSPECTED AND REPAIRED CRACK IAW DC-9 SRM 53-03 FIG 16.

Part: VANE — CRACKED (LT WING) · airframe 46,749 hrs · 41,911 cycles

LEFT WING TRAILING EDGE INBOARD FIXED VANE WAS CRACKED AND HAD LOOSE RIVETS. MAINTENANCE INSPECTED FABRICATED AND INSTALLED NEW TRAILING EDGE PANEL IAW DC-9 SRM 51-30-2 AND 51-30-8.

Part: FRAME — CRACKED (FUSELAGE) · airframe 46,749 hrs · 41,911 cycles

LEFT FUSELAGE FRAME 677 WAS CRACKED AT LOWER END BELOW CUSP, IN THE RADIOUS. MAINTENANCE REPAIRED CRACKED FRAME IAW DC-9 SRM 53-03 FIG 16.

Part: PAN — CRACKED (FUSELAGE) · airframe 46,749 hrs · 41,911 cycles

OUTER BAG BIN DOOR PAN WAS CRACKED AT THE FORWARD CORNER. MAINTENANCE INSPECTED AND REPLACED THE BAG BIN DOOR IAW DC-9 MM.

Part: CONTROLLER — OUT OF ADJ (CABIN PRESSURE) · airframe 46,396 hrs · 41,741 cycles

THIRTY MIN INTO CRUISE FLIGHT, AIRCRAFT PRESSURIZATION BEGAN 1500 FPM CLIMB, FOLLOWED BY 1500 FPM DESCENT. INITIATED EMERGENCY DESCENT AND DIVERTED TO FSD. FLEW AIRCRAFT TO ILN UNPRESSURIZED. PERFORMED ADJUST/TEST OF CABIN PRESSURE CONTROL IAW DC9 MM 21-32-00. OPS CHECKED GOOD.

Part: CONTROLLER — OUT OF ADJ (CABIN PRESSURE) · airframe 46,396 hrs · 41,741 cycles

AUTO PRESSURIZATION WAS UNCONTROLLABLE. INITIATED EMERGENCY DESCENT AND AIR TURNEDBACK TO BIL. PERFORMED ADJUST/TEST OF CABIN PRESSURE CONTROL IAW DC9 MM 21-32-00.

Part: UPLOCK — FAILED (MLG) · airframe 44,994 hrs · 41,067 cycles

UNSATISFACTORY UPLATCH CHECK. BOTH MAINS UNSAFE LIGHTS ILLUMINATED AND GEAR DOOR OPEN LIGHT ON. RECYCLED GEAR, SECOND UPLATCH CHECK WAS GOOD. FERRIEDAIRCRAFT TO ILN, INSPECTED AND PERFORMED GEAR SWING IAW DC9 MM 32-60-0. NODEFECTS NOTED.

Part: VANE — CRACKED (LT TE FLAP)

DURING C-CHECK, FOUND LEFT FLAP FORWARD MOVEABLE VANE ARM CRACKED. REPLACED LEFT FORWARD FLAP MOVEABLE VANE IAW DC9 MM 27-51-2.

Part: CONTROL TAB — DELAMINATED (LT AILERON)

DURING C-CHECK, FOUND LEFT AILERON CONTROL TAB DELAMINATED. REPLACED LEFT AILERON CONTROL TAB IAW DC9 MM 27-10-2.

Part: PAN — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND AFT CARGO COMPARTMENT DOOR OUTER PAN CRACKED. REPAIRED CRACKED IAW DC9 SRM 52-03.

Part: WEB — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND AFT LOWER CARGO DOOR WEB CRACKED AT AFT HINGE. REPAIRED IAW ABX REA D952-28315.

Part: WEB — CRACKED (BS 910)

DURING C-CHECK, FOUND CUSP WEB AT STATION 910, RBL 54-44 CRACKED. REPLACED CUSP WEB IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: SLANT PANEL — CORRODED (CARGO COMPT)

DURING C-CHECK, FOUND LEFT SLANT PANEL CORRODED. REPLACED LEFT SLANT PANEL IAW DC9 SRM 51-30-01 AND DWG 9923419-29.

Part: FLOORBEAM — CRACKED (BS 180)

DURING C-CHECK, FOUND FLOORBEAM WEB CRACKED AT STATION 180, LBL 22. REPAIRED IAW DC9 SRM 53-01.

Part: PANEL — CORRODED (CENTER WING)

DURING C-CHECK, FOUND RIGHT CENTER WING SLANT PANEL CORRODED. REPLACED SLANT PANEL IAW ABX EA 53200018-301.

Part: SKIN — CRACKED (RT AILERON)

DURING C-CHECK, FOUND RIGHT AILERON SKIN TRAILING EDGE CRACKED. REPLACED RIGHT AILERON SKIN TRAILING EDGE IAW DC9 SRM 51-30-08.

Part: WEB — CRACKED (BS 1021)

DURING C-CHECK, FOUND CUSP WEB CRACKED AT STATION 1021 RIGHT. REPLACED CUSP WEB IAW ABX REA D953-28177 MR.

Part: RIB — CRACKED (WS 232.5)

DURING C-CHECK, FOUND LEFT WING NR 5 TRACK RIB CRACKED AT STATION XOS 232.5. REPLACED INBOARD WING RIB IAW DC9 SRM.

Part: WEB — CRACKED (BS 984-992)

DURING C-CHECK, FOUND CUSP WEB CRACKED STATION 984 TO 992 LEFT SIDE. REPLACED CUSP WEB IAW DC9 SRM 51-30-02.

Part: POWER PACK — INOP (CABIN)

DURING MAINTENANCE, FOUND EMERGENCY LIGHTS TEST FUNCTION INOPERATIVE. REPLACED EMERGENCY LIGHTS POWER SUPPLY. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOP (CABIN)

EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHTS POWER SUPPLY.

Part: LATCH — LACK OF LUBE (COCKPIT DOOR)

DURING MAINTENANCE SERVICE CHECK, FOUND COCKPIT DOOR LATCH STUCK. LUBRICATED LATCH, OPS CHECKED GOOD.

Part: BLKHD FITTING — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD FITTING BETWEEN FIRST AND SECOND RADIAL CRACKED. *S/D* REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: BLKHD SKIN — CORRODED (AFTPRESS BLKHD)

DURING C-CHECK, FOUND BULGE IN P-DOME SKIN LONGERON 16R. *S/D* REPAIRED IAW DC9 SRM 53-01.

Part: BLKHD STIFFENER — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND CRACK IN P-DOME STIFFENER AT LONGERON 12R. *S/D* REPAIRED IAW SRM DWG KO5159.

Part: SKIN — CORRODED (LT WING)

DURING C-CHECK, FOUND LEFT WING LOWER SURFACE AT LEADING EDGE HAS DEEP BLENDOUTS AROUND HI-LOKS AND INBOARD AT JACK PAD. *S/D* REPAIRED IAW ABX REA D957-20711MR AND SRM CH 51.

Part: RIB — CORRODED (E/E COMP DOOR)

DURING C-CHECK, FOUND RIB INSIDE E AND E DOOR BULGED. *S/D* REPAIRED IAW SRM 52-42.

Part: PROX BOX — DIRTY (LT MLG)

LT MAIN LANDING GEAR UNSAFE (RED) LIGHT ILLUMINATED WHEN GEAR LOWERED FOR LANDING. ABNORMAL PROCEDURES FOLLOWED. RECYCLED GEAR, NO CHANGE. LANDING WAS UNEVENTFUL. CLEANED PINS AND REMOVED MOISTURE FROM PROXIMITY BOX.

Part: LONGERON — CRACKED (BS 1041)

DURING C-CHECK, FOUND CRACK IN LONGERON 17 LEFT, STA 1041. REPLACED LONGERON SECTION IAW DC9 SRM 53-02.

Part: LONGERON — CRACKED (BS 1041)

DURING C-CHECK, FOUND CRACK IN LONGERON 17RT AT STA 1041. REPLACED LONGERON SECTION IAW DC-9 SRM 53-02.

Part: FITTING — CRACKED (RT WING)

DURING C-CHECK, FOUND ATTACH FITTING AT AFT INBD END OF RT HAND UPPER BONDED PNL CRACKED. REPLACED FITTING IAW DC-9 SRM 51-31-1.

Part: BRACKET — CRACKED (LT WING)

FITTING CRACKED INSIDE PANEL 1547A, LEFT FLAP. REPLACED BRACKET IAW DC-9 SRM 51-30-5.

Part: ROD END — WORN (RT MLG DOOR)

DURING COMPLIANE WITH AD 92-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR ARTICULATING DOOR LINK BEARING WORN ON OUTBOARD MAIN LANDING GEAR DOOR FOR ROD ASSEMBLY. REPLACED ROD END AND SHIMMED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: UPLOCK SW — DEFECTIVE (MLG)

LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. RECYCLED GEAR, LIGHT WENT OUT AFTER TWO MINUTES, THEN ILLUMINATED BRIEFLY AGAIN. REPLACED LEFT MAIN LANDING GEAR UPLOCK SWITCH IAW DC-9 SUPPLEMENTIAL MM 32-60-1.

Part: HINGE — WORN (RT MLG DOOR)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 91-22-07, ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR HINGE WORN. REPLACED HINGE IAW DC-9 SRM 51-10-3.

Part: STRUT — REQD SERVICE (NLG)

AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT RAISE AND AIRCRAFT FAILED TO GO INTO FLIGHT MODE. PRIOR TO LANDING, LANDING GEAR RETRACTION WAS ATTEMPTED AND LANDING GEAR RETRACTED NORMALLY AND AIRCRAFT WENT INTO FLIGHT MODE. FOUND NOSE STRUT SLOW TO EXTEND DUE TO WATER IN THE STRUT FREEZING. FLUSHED AND SERVICED THE NOSE STRUT WITH HYDRAULIC FLUID PER DC9 MM, CHAPTER 32-21-2. GROUND SHIFT MECHANISM WAS OPS CHECKED IAW DC9 MM, CHAPTER 32-23-1.

Part: INTERCOSTAL — CRACKED (BS 503-522)

DURING C-CHECK INSPECTION, A FLOOR INTERCOSTAL WAS FOUND CRACKED BETWEEN STR 503 AND 522R. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-5.