N947AX

Part: ACTUATOR — BROKEN (RT WING SLAT) · airframe 61,400 hrs · 61,762 cycles

DURING MAINTENANCE INSPECTION AT RDU, ON RIGHT WING, FOUND SLAT ACTUATOR ASSEMBLY BROKEN. REMOVED AND REPLACED SLAT ACTUATOR CYLINDER ASSEMBLY IAW DC9 MM. OPS CHECKED GOOD. WORK ACCOMPLISHED ON WO 600240033.

Part: FITTING — CRACKED (LT MLG WW) · airframe 61,391 hrs · 61,755 cycles

LEFT WHEEL WELL (KEEL AREA) LONGERON ATTACH END FITTING AT STA 750, LEFT BUTT LINE 8 (BELOW HYD RESERVOIR) HAD A 6 - 8 INCH CRACK ON VERTICAL LEG. REMOVED AND REPLACED ATTACH END FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: INDICATION SYS — MALFUNCTIONED (MLG) · airframe 61,328 hrs · 61,690 cycles

ON FINAL APPROACH, GEAR DOOR OPEN LIGHT REMAINED ON WITH 3 GREEN INDICATIONS. WENT AROUND ON APPROACH, RECYCLED GEAR, GEAR DOOR OPEN LIGHT EXTINGUISHED. JACKED AIRCRAFT, CYCLED LANDING GEAR SEVERAL TIMES, NO DEFECTS NOTED. OPS CHECKED GOOD, REF AMM 32-60-00.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 61,074 hrs · 61,431 cycles

LEFT BULKHEAD SPAR STUB (HORIZONTAL WEB) AT FS 1039 APPROX LONGERON 15 LEFT CRACKED ON BOTTOM COMING FROM INBOARD FORWARD BOLT HOLE. STOP DRILLED/REPAIRED IAW DC-9 SRM 53-01.

Part: PAN — CRACKED (PAX DOOR) · airframe 61,074 hrs · 61,431 cycles

PASSENGER ENTRY DOOR PAN CRACKED IN 3 LOCATIONS ON FORWARD SIDE. REMOVED AND REPLACED MAIN ENTRY DOOR IAW DC-9 MM 52-11-00-5-001. WORK ACCOMPLISHED ON NON ROUTINE 0311. (2 EACH - 5 INCH CRACKS, 1 EACH - 2 INCH CRACKS).

Part: PAN — CRACKED (FUSELAGE) · airframe 61,074 hrs · 61,431 cycles

PASSENGER ENTRY DOOR PAN CRACKED ABOVE UPPER DOOR HINGE MOUNT APPROX 3 INCHES EMANATING FROM PREVIOUS REPAIR. REPLACED DOOR ON NON ROUTINE 0311 AND IAW DC-9 MM.

Part: PAN — CRACKED (DOOR SEGMENT) · airframe 61,074 hrs · 61,431 cycles

PASSENGER ENTRY DOOR PAN CRACKED IN 3 LOCATIONS ON FORWARD SIDE, 2 EACH 5 INCH CRACKS, 1 EACH 2 INCH CRACK. REMOVED AND REPLACED MAIN ENTRY DOOR IAW DC-9 MM 52-11-00-5-001.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 61,074 hrs · 61,431 cycles

STA 218 FLOOR SUPPORT HAD INTERGRANULAR CORROSION ON LOWER SIDE. REMOVED AND REPLACED FLOOR SUPPORT IAW DC-9 SRM 51-30-5.

Part: DOOR — CRACKED (LT MAIN) · airframe 61,074 hrs · 61,431 cycles

LT MAIN ENTRY DOOR FORWARD UPPER CORNER APPEARED TO BE CRACKED. DOOR REPLACED ON NON ROUTINE 0311, IAW DC-9 MM.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 60,909 hrs · 61,251 cycles

GEAR DOOR OPEN LIGHT DID NOT GO OUT AFTER EXTENDING ON APPROACH TO ILN, WENT ON MISSED APPROACH. RECYCLED GEAR AND LIGHT WENT OUT. CYCLED GEAR DOORS SEVERAL TIMES, LIGHT OPS CHECKED GOOD IAW DC-9 MM 32-30-00.

Part: PROXIMITY SWITCH — MALFUNCTIONED (MLG) · airframe 60,357 hrs · 60,669 cycles

GO AROUND-MISSED APPROACH-GEAR RECYCLE. UPON PLACING MLG HANDLE IN THE DOWN POSITION FOR LANDING, MLG DOWN LIGHT FAILED TO ILLUMINATE. AFTER RUNNING ABNORMALS, DISCOVERED THE MLG WARNING CIRCUIT BREAKER WAS OUT. RESET CIRCUIT BREAKER AND EXTENDED MLG. AFTER SECOND EXTENSION, THREE GREEN LIGHTS ILLUMINATED. AND MLG CHECKED DOWN ALSO ON USING MAIN GEAR PROXIMITY SWITCHES. LANDING SOUNDED AND APPEARED TO WORK NORMALLY THE ENTIRE FLIGHT. FOUND WIRE AT P1-132 PIN 7 OPEN TO S3-65 TERMINAL 2, REPAIRED WIRE 1G206D24. WHILE PULLING IN WIRE, WIRE G207K24 AND 1G205C24 BROKE AT ENVIRONMENT SPLICES IN CONDUIT. REPAIRED WIRES IAW DC-9 WDM 32-41-00 LEFT LANDING GEAR OPS CHECKED GOOD IAW DC-9 AMM 32-60-00.

Part: FITTING — CRACKED (LT MLG WW) · airframe 60,050 hrs · 60,350 cycles

FITTING IN LEFT WHEEL WELL STA 699, LEFT BUTT LINE '10' CRACKED. REPLACED FITTING IAW DC-9 SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 60,050 hrs · 60,350 cycles

CUSP WEB CRACKED AT RIGHT BUTT LINE 54 BETWEEN FS 945 - 965. REPAIRED CRACK IAW DC-9 53-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,050 hrs · 60,350 cycles

FUSELAGE SKIN CRACKED AT MAIN ENTRY DOOR UPPER/AFT STOP. REPAIRED AREA IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,050 hrs · 60,350 cycles

FUSELAGE SKIN HAD 1.5 INCH TEAR/CRACK IN SKIN FORWARD ENTRANCE DOOR CUTOUT FORWARD SIDE BETWEEN STOP F4 AND F5. REPAIRED AREA IAW REA D953-48357MR.

Part: DOOR — CRACKED (BULKHEAD) · airframe 60,050 hrs · 60,350 cycles

AFT PRESSURE BULKHEAD DOOR CRACKED AT LOWER HINGE. REPLACED AREA NOTED IAW DC-9 SRM 52-05, 51-30-5 AND 51-30-1.

Part: CHANNEL — CRACKED (BULKHEAD DOOR) · airframe 60,050 hrs · 60,350 cycles

AFT PRESSURE BULKHEAD DOOR CRACKED AT UPPER HINGE. REPAIRED DOOR IAW DC-9 SRM 52-05.

Part: INTERCOSTAL — CRACKED (EMERGENCY EXIT) · airframe 60,050 hrs · 60,350 cycles

LEFT AFT OVERWING DOOR HAD CRACKED INTERCOSTAL AT LATCH HANDLE. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 60,050 hrs · 60,350 cycles

LEFT AFT OVERWING DOOR HAD CRACKED DOOR PAN AT STOP NR 6. REPAIRED AREA IAW DC-9 SRM 52-05.

Part: SPAR CAP — CRACKED (CENTER WING) · airframe 60,050 hrs · 60,350 cycles

CRACK ON UPPER SPAR CAP REAR SPAR XCW '0' TO XCW '10' RIGHT. REPAIRED AREA IAW DC-9 SRM.

Part: WINDOW — MISALIGNED (COCKPIT) · airframe 59,769 hrs · 60,071 cycles

FIRST OFFICER'S WINDOW WOULD NOT OPEN. FOUND SCREW IN UPPER FORWARD CORNER OF FIRST OFFICER'S WINDOW TO BE TO LONG AND MIS-ALIGNED WINDOW TRACK. REPLACED WITH SHORTER SCREW. WINDOW OPS CHECKED GOOD IAW DC-9 MM 56.

Part: LOCK — STICKING (COCKPIT WINDOW) · airframe 59,769 hrs · 60,071 cycles

FIRST OFFICER'S CLEAR VIEW WINDOW WOULD NOT OPEN. FOUND UPPER WINDOW LOCK STICKING. CLEANED AND LUBRICATED LOCK. OPS CHECKED GOOD IAW DC-9 MM 56.

Part: PUSHROD — DISCONNECTED (MLG) · airframe 59,717 hrs · 60,013 cycles

AFTER TAKE-OFF, UNABLE TO RAISE GEAR HANDLE. RAN CHECK LIST AND DETERMINED THAT AIRCRAFT FAILED TO GO INTO FLIGHT MODE (GROUND SHIFT IN GROUND MODE) - PULLED CIRCUIT BREAKERS AND DETERMINED THAT THE GROUND SHIFT WAS BAD. FOUND GROUND SHIFT MECHANISM PUSHROD DISCONNECTED. ATTACHED PUSHROD SHIFT MECHANISM IAW DC-9 MM 32-52-07-2-001.

Part: WEB — CRACKED (FUSELAGE) · airframe 59,048 hrs · 59,366 cycles

CUSP WEB CRACKED BETWEEN FS 945 - 965, LONGERON 18 LEFT. REPAIRED AREA, DOUBLER INSTALLED ON CUSP WEB IAW DC-9 SRM 53-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,048 hrs · 59,366 cycles

CRACK INDICATION IN SKIN BETWEEN 2 FASTENERS, BETWEEN LONGERON 5 RIGHT AND LONGERON 6 RIGHT AT FS 996. INSTALLED PERMANENT REPAIR IAW DC-9 EA 53110005.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,787 hrs · 59,103 cycles

EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERY PACK POWER SUPPLY IAW DC-9 MM. OPS CHECKED GOOD.

Part: LINK — WORN (LT MLG) · airframe 58,470 hrs · 58,791 cycles

THE MAIN LANDING GEAR FAILED GEAR UPLATCH CHECKS AFTER TAKEOFF. THE FLIGHT CREW COMPLIED WITH ABNORMAL CHECKLIST. MAINTENANCE INSPECTED AND REPLACED THE LEFT MAIN LANDING GEAR DOOR, LATCH TO DOOR JAMB LINK ASSY IAW DC-9 MM 32-31-04. MAINTENANCE INSPECTED AND REPLACED THE LEFT MAIN LANDING GEAR OVER CENTER LINK SWITCH (P/N 7000010101ABX, S/N 11504) AS A PRECAUTION. THE LEFT MAIN LANDING GEAR INDICATION WIRING WAS ALSO INSPECTED FOR DEFECTS. THE LANDING GEAR INDICATION LIGHT BULBS WERE REPLACED AND OPERATION CHECKS WERE COMPLETED.

Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 57,905 hrs · 58,193 cycles

EMERGENCY EXIT LIGHTS REMAINED ON AFTER POWER WAS REMOVED AND THE SWITCH WAS OFF. REPLACED EMERGENCY LIGHT POWER SUPPLY.

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 57,902 hrs · 58,189 cycles

DURING C-CHECK, FOUND HORIZONTAL CENTER SECTION HINGE BORE CORRODED. REPAIRED IAW ABX REA D955-37167MR.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 57,902 hrs · 58,187 cycles

DURING C-CHECK, FOUND VERTICAL STABILIZER SKIN CRACKED AT PANEL NR 3703. REPLACED SKIN IAW DC9 SRM 51-30-1.

Part: ANGLE — CRACKED (RT FLAP) · airframe 57,902 hrs · 58,189 cycles

DURING C-CHECK, FOUND RIGHT FLAP OUTBOARD HINGE, OUTBOARD SUPPORT ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-1.

Part: HINGE FITTING — CORRODED (HORIZONTAL STAB) · airframe 57,902 hrs · 58,189 cycles

DURING C-CHECK, FOUND HORIZONTAL STABILIZER CENTER SECTION HINGE BORE CORRODED. REPAIRED IAW ABX REA D955-37167MR.

Part: ANGLE — CRACKED (LT FLAP) · airframe 57,902 hrs · 58,189 cycles

DURING C-CHECK, FOUND LEFT FLAP OUTBOARD HINGE ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-2.

Part: ANGLE — CRACKED (LEFT FLAP) · airframe 57,902 hrs · 58,189 cycles

DURING C-CHECK, FOUND THE LEFT FLAP OUTBOARD HINGE ATTACH ANGLE CRACKED. REPLACED ANGLEIAW DC9 SRM 51-30-2.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 57,902 hrs · 58,189 cycles

DURING C-CHECK, FOUND THE VERTICAL STABILIZER SKIN CRACKED UNDER PANEL NR 3804. REPLACED SKIN IAW DC9 SRM 51-30-1.

Part: ANGLE — CRACKED (RT TE FLAP) · airframe 57,902 hrs · 58,189 cycles

DURING C-CHECK, FOUND THE OUTBOARD FLAP HINGE AFT FITTING, INBOARD ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-1.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 57,902 hrs · 58,189 cycles

DURING C-CHECK, FOUND SUPPORT ANGLE AFT SIDE OF STATION 37 BULKHEAD CRACKED IN 2 PLACES. REPLACED ANGLE IAW DC9 SRM 51-30-2.

Part: ATTACH FITTING — CORRODED (HORZONTAL STAB) · airframe 57,902 hrs · 58,189 cycles

DURING C-CHECK, FOUND THE HORIZONTAL STABILIZER CENTER SECTION CENTER HINGE BOLT FITTING CORRODED INSIDE THE LEFT HINGE BOLT HOLE. REPLACED FITTING IAW DC9 SRM 51-30-1.

Part: SEAT — WORN (COCKPIT)

CAPTAIN'S SEAT VERTICAL MOVEMENT ADJUSTMENT RELEASES INADVERTENTLY. SEAT SLIDES TO FLOOR WITHOUT ACTUATION. REPLACED CAPTAIN'S SEAT.

Part: SEAT — LACK OF LUBE (LT COCKPIT)

CAPTAIN'S SEAT MOVED AFT AND DOWN, UNCOMMANDED, ON TAKEOFF. LUBRICATED SEAT ADJUSTMENT MECHANISM AND CHECKED LOCKING PIN ENGAGEMENT. NO DEFECTS NOTED.

Part: FRAME — CORRODED (BS 484)

DURING C-CHECK, FOUND FRAME AT STATION 484, LONGERON 29 LEFT AND 29 RIGHT. REPLACED SECTION OF FRAME IAW DC9 SRM 53-03.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, FOUND CRACK IN LONGERON 16 RIGHT AT STATION 965. REPLACED SECTION OF LONGERON IAW DC9 SRM 53-02.

Part: FRAME — CRACKED (BS 980)

DURING C-CHECK, FOUND CRACK IN FUSELAGE FRAME AT STATION 980, LONGERON 16 LEFT. REPLACED FRAME SECTION IAW DC9 SRM 53-03.

Part: SWITCH — MALFUNCTION (LT MLG)

GEAR UPLATCH CHECK NOT SATISFACTORY, THE LEFT MAIN GEAR INDICATION REMAINED GREEN. RECYCLED GEAR DOWN, ALL 3 GEAR HAD NO UNSAFE LIGHT. RAISED GEAR, LEFT GEAR GREEN LIGHT STAYED ON, NO GEAR DOOR OPEN LIGHT. REPLACED LEFT MAIN GEAR DOWNLOCK SWITCH, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS ILLUMINATED WITH POWER OFF AND LIGHT SWITCH IN THE OFF POSITION. REPLACED EMERGENCY LIGHT BATTERY PACK.

Part: BATTERY — DISCHARGED (CABIN)

DURING SERVICE CHECK, WHEN ALL POWER WAS REMOVED FROM AIRCRAFT, EMERGENCY LIGHTS STAYED ON. REPLACED EMERGENCY LIGHT BATTERIES.

Part: DOOR — CRACKED (CARGO DOOR)

DURING C-CHECK, THE FORWARD LOWER CARGO DOOR SKIN AND PAN WAS FOUND CRACKED. THE DOOR WAS REPLACED IAW DC9 MAINTANCE MANUAL 52-31-0.

Part: FRAME — CRACKED (BS 718/737)

RIGHT SIDE FRAMES STATION 718 AND 737 AFT FLANGE CRACKED. REPAIRED FRAME STATION 718 AND 737 IAW ABX REA D95-18588-MR.

Part: SKIN — CORRODED (CTR FUSELAGE)

DURING C-CHECK, THE CENTER FUSELAGE SKIN UNDER THE NR 1 ADF LOOP ANTENNA WAS FOUND CORRODED. THE SKIN WAS REPAIRED IAW DC9 REA D953-18649-SB.

Part: FRAME — CRACKED (BS 718)

DURING C-CHECK, THE CENTER FUSELAGE AT MAIN FRAME STATION 718 RIGHT WAS FOUND CRACKED. THE FRAME WAS REPAIRED IAW DC9 REA D953-18588-MR.

Part: VANE — DELAMINATED (RT TE FLAP)

DURING C-CHECK, THE RIGHT WING CENTER FIXED VANE WAS FOUND DELAMINATED. THE VANE WAS REPLACED IAW DC9 MAINTANCE MANUAL 27-51-3.

Part: VANE — DELAMINATED (RT TE FLAP)

DURING C-CHECK, THE RIGHT WING INBOARD FIXED VANE WAS FOUND DELAMINATED. THE VANE WAS REPLACED IAW DC9 MAINTANCE MANUAL 27-51-3.

Part: FITTING — CRACKED (NR 2 LE SLAT)

RIGHT WING INBOARD SLAT TRACK FITTING AT NR 2 TRACK CRACKED. REPLACED NR 2 SLAT TRACK FITTING, IAW DC9 SRM 51-30-01.

Part: BULKHEAD TEE — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, THE AFT PRESSURE BULKHEAD TEE WAS FOUND CRACKED AT LONGERON 14 LEFT. WHILE ACCOMPLISHING AD 96-16-04. THE TEE WAS REPLACED IAW SRM 51-30-2.

Part: SKIN — CORRODED (RT TE FLAP)

DURING C-CHECK, THE RIGHT WING INBOARD FLAP SKIN WAS FOUND CORRODED. THE SKIN WAS REPLACED IAW REA D957-18612-MR.

Part: BULKHEAD TEE — CRACKED (AFT PRESS BLKHD)

EDDY CURRENT INDICATES CRACK IN AFT PRESSURE BULKHEAD TEE, THIRD RADIAL FROM FLOOR, LEFT SIDE. INSTALLED SPLICE REPAIR IAW DC-9 SRM 51-30-1.

Part: PANEL — DELAMINATED (RT WING)

RT WING UPPER TRAILING EDGE BONDED PANEL DELAMINATED. REPLACED BONDED PANEL.

Part: LINKAGE — DAMAGED (LT MLG DOOR)

DURING C-CHECK, THE LEFT WING MAIN LANDING GEAR DOOR LINKAGE WAS FOUND DAMAGED. THE LINKAGE WAS REPLACED IAW DC9 OVERHAUL MANUAL 32-10-6.

Part: RUDDER — CRACKED (EMPENNAGE)

X-RAY OF RUDDER INDICATED TWO INTERNAL CRACKS. REPLACED RUDDER.

Part: ANGLE — CRACKED (FUSELAGE)

ATTACH ANGLE CRACKED BETWEEN FUSELAGE SKIN AND LEFT AFT ADF PANEL SUPPORT FR -756 JUST BELOW LONGERON 20 LEFT. REPLACED CRACKED ANGLE.

Part: VANE — DELAMINATED (RT TE FLAP)

RIGHT WING INBOARD FIXED VANE DELAMINATED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS.

Part: SHEAR TIE — DAMAGED (BS 1059)

DURING C-CHECK, THE FUSELAGE SKIN WAS FOUND BULDGED AT STATION 1059 AT LONGERON 18 LEFT. THE CORRODED SHEAR TIE WAS REPLACED IAW DC9 SRM 51-30-2.

Part: VANE — DELAMINATED (RT TE FLAP)

RIGHT FLAP VANE FOUND DELAMINATED ON UPPER SURFACE AND LEADING EDGE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.

Part: ANGLE — CRACKED (PYLON/FUSELAGE)

DURING C-CHECK, THE UPPER PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPLACED IAW DC9 SRM 51-30-5.

Part: PANEL — CORROSION (RT WING)

RT WING TRAILING EDGE HAS LEVEL 1 CORROSION. REPLACED TRAILING EDGE PANEL.

Part: PANEL — DELAMINATED (RT WING)

DURING C-CHECK, THE RIGHT WING OUTBOARD BONDED TRAILING EDGE PANEL WAS FOUND DELAMINATED. THE PANEL WAS REPLACED IAW DC9 SRM.

Part: FITTING — CRACKED (NR 2 SLAT TRACK)

DURING C-CHECK, THE RIGHT WING NR 2 INBOARD SLAT TRACK FITTING WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM 51-30-5.

Part: RIB — CRACKED (LT WING)

DURING C-CHECK, THE LEFT WING NR 2 SLAT TRACK INBOARD RIB WAS FOUND CRACKED. THE RIB WAS REPLACED IAW DC9 SRM 51-30-1.

Part: DOUBLER — CRACKED (BS 718)

DURING C-CHECK, THE WHEEL WELL PRESSURE PANEL DOUBLER AT STATION 718 WAS FOUND CRACKED. THE DOUBLER WAS REPLACED IAW DC9 SRM 51-30-5.

Part: TR DRIVE LINK — CRACKED (NR 1 ENGINE)

DURING C-CHECK, THE NR 1 ENGINE LOWER INBOARD THURST REVERSER DRIVER LINK WAS FOUND CRACKED. THE LINK WAS REPLACED IAW DC9 MAINTANCE MANUAL 78-31-5.

Part: TR DRIVE LINK — CRACKED (NR 1 ENGINE)

NUMBER ONE ENGINE LOWER INBOARD THRUST REVERSER DRIVER LINK CRACKED. REPLACED DRIVER LINK IAW DC9 MM 78-31-05.

Part: FITTING — CRACKED (NR 1 SLAT TRACK)

DURING C-CHECK, THE RIGHT WING NR 1 INBOARD SLAT TRACK FITTING WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM 51-30-5.

Part: FITTING — CRACKED (NR 1 SLAT TRACK)

DURING C-CHECK, THE LEFT WING NR 1 OUTBOARD SLAT TRACK FITTING WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM 51-30-5.

Part: ACTUATOR FTG — CRACKED (RT LE SLAT)

DURING C-CHECK, THE RIGHT WING SLAT ACTUATOR INBOARD ATTACH FITTING WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM 51-30-5.

Part: FITTING — CRACKED (NR 1 SLAT TRACK)

DURING C-CHECK, THE LEFT WING NR 1 INBOARD SLAT TRACK FITTING WAS FOUND CRACKED. THE FITTING WAS REPAIRED IAW REA D957-18609-MR.

Part: DOOR — CRACKED (CARGO COMPT)

DOOR PAN CRACKED. REPAIRED PER DC9 SRM.

Part: TAB — DELAMINATED (RT AILERON)

UPPER SIDE HAS SEVERAL ONE INCH DIA DELAMINATED AREAS. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.

Part: FITTING — CRACKED (LT LE FLAP)

LT OUTBOARD SLAT TRACK, NR 1 SLAT TRACK, FITTING CRACKED. REPLACED SLAT TRACK FITTING.

Part: BATTERY — DEFECTIVE (CABIN)

COCKPIT EMERGENCY OVERHEAD LIGHTING STAYS ON AFTER AIRCRAFT POWER OFF. REPLACED BATTERIES IN EMERGENCY BATTERY PACK IAW DC-9 M.M. 33-53-0.

Part: COALESCER BAGS — DIRTY (LT/RT)

UNUSUAL SMELL FROM AIR CONDITIONING VENTS. INSPECTED RAM AIR AND HEAT EXCHANGER DUCTS, NOTHING FOUND. REPLACED THE WATER SEPARATOR COALESCER BAGS.

Part: TR DRIVE LINK — CRACKED (NR 2 ENGINE)

DURING COMPLIANCE OF AD 75-14-06, AD 90-18-03; SB'S 78-36, 78-38, 78-40 AND 78-66, FOUND A CRACK INDICATION ON THE NR 2 ENGINE UPPER OUTBOARD THRUST REVERSER DRIVER LINK. REMOVED LINK IAW DC-9 MM 78-31-5. LINK CRACKED, SCRAPPED LINK.

Part: HINGE — WORN (LT MLG DOOR)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING A.D. 91-22-07; A.S.B. 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGE HALF ON THE WING WORN. REPAIRED IAW DC-9 S.B. 32-244.

Part: SKIN — DAMAGED (CENTER FUSELAGE)

DURING C-CHECK INSPECTION, FOUND THE FUSELAGE SKIN DAMAGED AT THE PRIMARY STATIC PORT. REPAIRED IAW ABX REA D953-118-41-MR.

Part: BLKHD FRAME — DAMAGED (FS 110)

DURING C-CHECK INSPECTION, FOUND THE LOWER HORIZONTAL FRAME ON THE AFT SIDE OF 110 BULKHEAD GOUGED AT LONGERON 28L. REPAIRED IAW ABX REA D953-11833-MR.

Part: ANGLE — CRACKED (VERT STAB)

DURING C- CHECK INSPECTION WHILE ACCOMPLISHING A.D. 89-08-10; S.B.'S A53-154 AND A53-223, FOUND THE RIGHT DORSAL FIN ATTACH ANGLE CRACKED. REPLACED THE ANGLE IAW DC-9 SRM 53-05-23.

Part: BUSHING — WORN (LT MLG DOOR)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING A.D. 91-22-07; A.S.B. 32-244, FOUND THE LEFT OUTBOARD LANDING GEAR DOOR LATERAL ATTACH ROD ATTACH PLATE BUSHING WORN. REPAIRED IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: ATTACH ROD — WORN (LT MLG)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT OUTBOARD LANDING GEAR DOOR LATERAL ATTACH ROD, ROD WORN. REPAIRED IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: EEL POWER SUPPLY — DEFECTIVE (CABIN)

COCKPIT EMERGENCY LIGHTS INTERMITTENTLY GO DIM TO BRIGHT. REPLACED EMERGENCY POWER SUPPLY. OPS CHECKED GOOD IAW DC-9 MM 33-53-0.

Part: EEL SWITCH — INTERMITTENT (CABIN)

CABIN EMERGENCY LIGHTS ILLUMINATE INTERMITTENTLY IN FLIGHT. REPLACED CABIN EMERGENCY LIGHT SWITCH PER DC-9 MM. OPS CHECKED NORMAL.