N982AX

Part: DOOR FRAME — CRACKED (CABIN) · airframe 72,164 hrs · 84,108 cycles

LEFT AFT UPPER DOOR JAMB CRACKED, EMERGENCY EXIT, IN 2 PLACES. REPAIRED LEFT AFT UPPER DOOR JAMB IAW DC-9 SRM 53-05.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 72,164 hrs · 84,108 cycles

SERVICE DOOR THRESHOLD SKIN BULGING AT STA 176, RIGHT BUTT LINE 58. REPAIRED AREA IAW DC-9 SRM 51-10-2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,164 hrs · 84,108 cycles

SHEAR TIE CRACKED IN RADIUS FRAME STA 813 BETWEEN LONGERON 29 LEFT AND 30. REPAIRED SHEAR TIE IAW DC-9 SRM 53-03 AND DWG SR09530212.

Part: RETAINER — CRACKED (CABIN WINDOW) · airframe 72,164 hrs · 84,108 cycles

STA 756, LONGERON 15 RIGHT, HAD CRACK AT WINDOW RETAINER. REMOVED AND REPLACED DAMAGED CLIP. FABRICATED AND INSTALLED NEW CLIP IAW DACO DWG 3914137 AND DC-9 SRM 51-30-5.

Part: RETAINER — CRACKED (CABIN WINDOW) · airframe 72,164 hrs · 84,108 cycles

STA 598, LONGERON 10 RT, HAD CRACK AT WINDOW RETAINER. REPAIRED WINDOW RETAINER AT FS 598, LONGERON 10 RIGHT IAW DC-9 SSRM DWG K07226.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,164 hrs · 84,108 cycles

LOWER LEG OF FLOORBEAM WAS CORRODED ON UPPER AND LOWER SURFACE AT STA 313, BUTTLINE 38 RIGHT. REPAIRED FLOORBEAM IAW DC-9 SRM 53.

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 71,758 hrs · 83,714 cycles

NOSE LANDING GEAR LIGHT WAS NOT ILLUMINATED ON GEAR EXTENSION. RECYCLED GEAR, LIGHT CAME ON. INSPECTED NOSE LANDING GEAR WIRING FOR CONTINUITY & PIN ENGAGEMENT AT SWITCH CONNECTORS. INSPECTED SWITCHES FOR SECURITY AND OPERATION. CYCLED NOSE LANDING GEAR 10 TIMES, ALL POSITION & WARNING INDICATIONS WERE IMMEDIATE & NORMAL PER DC9 MM 32-60-00.

Part: WIRE — BURNED (BUSS PANEL) · airframe 71,075 hrs · 83,004 cycles

WIRE BURNED ON PHASE C, GROUND SERVICE BUS POWER PANEL, WIRE HV X22810C. REMOVED BURNED AREA OF WIRE AND REPLACED WIRE END CONNECTOR. INSTALLED WIRE TO GROUND SERVICE BUS PHASE C IAW DC9 MM 20-50-01-2-0001. OPS CHECK GOOD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 71,029 hrs · 82,970 cycles

CRACK IN FRAME ATTACH ANGLE AT STA 1038 ABOVE LONGERON 18 LT. REPAIRED ANGLE IAW DC-9 SSRM DWG K05159.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,029 hrs · 82,970 cycles

FRAME CRACKED AT FS 1076 AND LONGERON 19 LEFT. REPAIRED FRAME AT FS 1076 IAW DC-9 SRM 53-03.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 71,029 hrs · 82,970 cycles

LEFT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON A RIB TOWARD THE TOP END OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 71,029 hrs · 82,970 cycles

LEFT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON A RIB IN THE MIDDLE OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 71,029 hrs · 82,970 cycles

RIGHT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON RIB IN THE MIDDLE OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 71,029 hrs · 82,970 cycles

RIGHT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON A RIB AT THE BOTTOM OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159.

Part: RIB — CRACKED (RT WING) · airframe 71,029 hrs · 82,970 cycles

END OF LEADING EDGE RIB RIGHT WING CRACKED AT STA 353. REPAIRED DAMAGED RIB IAW DC-9 SRM 57-06.

Part: PANEL — CRACKED (LT WING) · airframe 70,774 hrs · 82,681 cycles

WHILE PERFORMING ROUTINE LINE MAINTENANCE, A FUEL LEAK WAS DISCOVERED AT THE LT WING FUEL PANEL 1307. FURTHER INSPECTION REVEALED A CRACK ON THE FUEL PANEL FLANGE. REPAIRED CRACK IAW DC-9 SRM 57-03, FIG 23.

Part: DUCT — DISCONNECTED (A/C BAY) · airframe 70,199 hrs · 82,091 cycles

AT FL 350, CABIN ALTITUDE INCREASED TO 9,500 ALONG WITH THE RIGHT GENERATOR TRIPPING OFF LINE. RESET GENERATOR. PERFORMED DESCENT TO 14,000 CABIN ALTITUDE WAS REGAINED AT APPROXIMATELY 17,000 TO 18,000. PACK PRESSURE NORMAL AS WELL AS ELECTRICAL PARAMETERS AT TIME OF THE PRESSURIZATION PROBLEM. PERFORMED LEAK CHECK OF THE LEFT AND RIGHT AC PACKS AND DUCTS. FOUND RIGHT AC DUCT JUST AFT OF COALESCER BAG DISCONNECTED AND COALESCER BAG MISSING. INSTALLED NEW COALESCER AND RECONNECTED DUCT. PERFORMED ENGINE RUN AND OPS CHECK OF RIGHT GENERATOR. NO DEFECTS NOTED. ALSO PRESSURIZED AIRCRAFT WITH RIGHT PACK. NO FURTHER LEAKS OR DEFECTS NOTED IAW DC9 MM 21-20-02 AND 21-00-00.

Part: WIRE — BROKEN (NLG) · airframe 69,893 hrs · 81,806 cycles

ON LANDING AT BDL, NO GREEN GEAR LIGHT. RECYCLED LANDING GEAR, THE GREEN LIGHT ILLUMINATED. REPAIRED BROKEN WIRES TO THE NOSE GEAR UP LIMIT SWITCH CONNECTOR (P1-134) AND REPLACED THE UP LIMIT SWITCH AS A PRECAUTION. OPS CHECKED GOOD IAW DC9 MM 32-60-01-02.

Part: SWITCH — DEFECTIVE (NOSE) · airframe 69,865 hrs · 81,774 cycles

ON INITIAL GEAR EXTENSION AT ILN, NOSE GEAR DID NOT INDICATE DOWN/LOCKED. SUBSEQUENT RETRACTION/EXTENSION CYCLE YIELDED NORMAL INDICATION. REPLACED THE NOSE GEAR DOWN LOCK SWITCH IAW DC-9 MM 32-60-02.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 69,863 hrs · 81,772 cycles

ON INITIAL GEAR EXTENSION AT ILN, NOSE LANDING GEAR DID NOT INDICATE DOWN/LOCKED. SUBSEQUENTIAL RETRACT/EXTENSION CYCLE YIELDED NORMAL INDICATION. PERFORMED FUNCTIONAL CHECK IAW DC-9 MM 32-60-00-2-0101, NORMAL INDICATION AT THIS TIME.

Part: RIB — CRACKED (RIGHT WING) · airframe 69,859 hrs · 81,768 cycles

RIGHT WING LEADING EDGE RIB (JUST INBOARD OF #2 SLAT TRACK) CRACKED AT THE LOWER ATTACH FASTENER. REPAIRED RIB IAW DC-9 REA D957-43342.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 69,859 hrs · 81,768 cycles

CRACK IN FORWARD ACCESSORY COMPARTMENT DOOR JAMB, APPROXIMATELY 1.5 INCH LONG, LOCATED ALONG THE UPPER AFT SIDE OF JAMB. REPAIRED DOOR JAMB IAW DC-9 SRM 51-10-3 AND 51-20.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,859 hrs · 81,768 cycles

CUSP WEB CRACKED (AFT WEB) AT FS 236, LONGERON 18 LEFT. REPAIRED AREA IAW DC-9 SRM 53-01.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,859 hrs · 81,768 cycles

CUSP WEB CRACKED BETWEEN FS 945 AND 965, LEFT SIDE. REPAIRED CRACKED AREA IAW DC-9 SRM 53-01.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,859 hrs · 81,768 cycles

FRAME FOOT, WEB CRACKED AT FS 996, LONGERON 18 LEFT. REPLACED WEB IAW DC-9 SRM 53-11-3 AND 51-30-5.

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 69,859 hrs · 81,768 cycles

HEAVY CORROSION ON FRAME SPLICE ANGLE ON AFT SIDE OF FRAME AT STATION 943, ABOVE LONGERON 29 LEFT. REPLACED SPLICE ANGLE IAW DC-9 SRM 51-30-5.

Part: FRAME — CORRODED (AFT CARGO) · airframe 69,859 hrs · 81,768 cycles

HEAVY CORROSION ON UPPER CARGO FLOOR FRAME AT STATION 929 ABOVE TWO FASTENERS THAT HOLD THE AFT LOWER CARGO DOOR HOLD OPEN HOOK. REMOVED CORROSION AND INSTALLED REPAIR IAW DC-9 SRM 53-05.

Part: FRAME — CORRODED (FWD. CARGO) · airframe 69,859 hrs · 81,768 cycles

FRAME WAS CORRODED AT STATION 332, FROM LONGERON 29 LEFT TO LONGERON 29 RIGHT. REPAIRED FRAME IAW DC-9 SRM.

Part: FITTING — CRACKED (F.S. 604) · airframe 69,859 hrs · 81,768 cycles

LONGERON 28 RIGHT HAD CRACKED END FITTING AFT OF F.S. 604 "P" DOME. REPLACED END CAP IAW DC-9 SRM 51-30-5.

Part: INTERCOSTAL — CRACKED (AFT CARGO) · airframe 69,859 hrs · 81,768 cycles

CRACK IN INTERCOSTAL LONGERON 27 LEFT, STATION 761. REPAIRED AREA IAW DC-9 DOUGLAS DWG 9915574.

Part: FITTING — CRACKED (F.S. 604) · airframe 69,859 hrs · 81,768 cycles

LONGERON 29 RIGHT HAD CRACKED END FITTING AFT OF F.S. 604 "P" DOME. REPLACED END CAP IAW DC-9 SRM 51-30-5.

Part: ENGINE — FAILED (LEFT) · airframe 69,646 hrs · 81,525 cycles

CLIMBING THROUGH FL 190, CREW HEARD A LOUD POP AND NOTICED THE LEFT ENGINE HAD DECREASED TO 1.35 EPR AND THE EGT HAD INCREASED TO 550. OPERATED ENGINE AT REDUCED POWER AND RETURNED TO LAND. REPLACED THE NR 1 ENGINE IAW DC-9 JOB CARD 9090010 AND DC-9 8A & 8B. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 69,568 hrs · 81,452 cycles

CREW REPORTED ON APPROACH DOOR OPEN LIGHT WOULD NOT PRESS TO TEST. DID FLY BY, TOWER REPORTED DOORS CLOSED. RELAMPED GEAR DOOR OPEN LIGHT PRESS TO TEST INDICATOR. OPS CHECKED GOOD IAW DC-9 MM.

Part: BATTERY — DISCHARGED (FUSELAGE) · airframe 69,112 hrs · 81,009 cycles

EMERGENCY LIGHTS WOULD NOT OPERATE WHEN SWITCH WAS SELECTED ON. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY IAW DC-9 MM 33-52-02.

Part: CONTACTOR — DIRTY (BATTERY) · airframe 69,111 hrs · 81,008 cycles

EMERGENCY LIGHTS WOULD NOT TEST DURING PRE-DEPARTURE CHECK. MAINTENANCE INSPECTED AND CLEANED THE EMERGENCY LIGHT BATTERY CONTACTS AND RESEATED BATTERIES IN THE CHARGER. OPS CHECKED GOOD IAW DC-9 MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 68,677 hrs · 80,572 cycles

DURING C-CHECK, FOUND INTERCOSTAL TO FLOORBEAM ATTACH ANGLE CRACKED AT STATION 617, LEFT BL 44. REPLACED ANGLE IAW DC9 SRM 51-30-5.

Part: PANEL — CRACKED (FUSELAGE) · airframe 68,677 hrs · 80,572 cycles

DURING C-CHECK, FOUND RIGHT TRAP PANEL CRACKED AT TOP OUTBOARD FLANGE. REPLACED RIGHT TRAP PANEL IAW DC9 SRM 51-30-5, AND DC9 S/B 53-182.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 68,677 hrs · 80,572 cycles

DURING C-CHECK FOUND FLOOR SUPPORT TO INTERCOSTAL STRAP CRACKED AT STATION 737 OUTBOARD OF RIGHT BL 22. INSTALLED SPLICE IAW DC9 SRM 51-30-02.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 68,677 hrs · 80,572 cycles

DURING C-CHECK, FOUND THE FORWARD LOWER CARGO INTERCOSTAL WEB CRACKED. REPLACED FORWARD CARGO DOOR WEB IAW DC9 SRM 51-30-2.

Part: PAN — CRACKED (CARGO DOOR) · airframe 68,677 hrs · 80,572 cycles

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

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 68,677 hrs · 80,572 cycles

DURING C-CHECK, FOUND CRACK AT UPPER ANTI-COLLISION LIGHT ATTACH PLATE. REPAIRED IAW ABX REA D953-37600MR.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 68,677 hrs · 80,572 cycles

DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES.

Part: CIRCUIT BREAKER — FAILED (COCKPIT)

EMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHTING 5 AMP CIRCUIT BREAKER IAW DC9 MM 33-53, OPS CHECKED GOOD.

Part: WEB — CORRODED (BS 756-752)

DURING C-CHECK, FOUND PRESSURE DECK WEB CORRODED BEYOND LIMITS AT STATION 756 TO 752, RBL 15. REPAIRED PRESSURE DECK WEB IAW DC9 SRM 53-04.

Part: FRAME — CRACKED (FRAME 1076)

DURING C-CHECK, FOUND FRAME 1076 CRACKED AT LONGERONS 2L AND 2R. REPAIRED FRAME IAW DC9 SRM 53-03.

Part: BRACKET — CORRODED (LT TE FLAP)

DURING C-CHECK, FOUND LEFT FLAP INBOARD AFT HINGE BRACKET CORRODED AT PIVOT POINT. REPLACED AFT HINGE BRACKET IAW DC9 SRM.

Part: BLKHD STIFFENER — CRACKED (BS 1087)

DURING C-CHECK, FOUND STIFFENER CRACKED AT AFT SIDE OF BULKHEAD 1087, BL 0.0. REPLACED STIFFENER IAW DC9 SRM 51-30-5 AND 51-10-4.

Part: SHEAR-TIE — CRACKED (BS 980)

DURING C-CHECK, FOUND FRAME SHEAR-TIE CRACKED AT STATION 980 AND LONGERON 14R. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: SHEAR-TIE — CRACKED (BS 945)

DURING C-CHECK, FOUND FRAME SHEAR-TIE CRACKED AT STATION 945 BETWEEN LONGERONS 15R AND 16R. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-5.

Part: LONGERON — CRACKED (BS 794-813)

DURING C-CHECK, FOUND LONGERON 30 CRACKED AT SPLICE BETWEEN STATION 794 TO 813. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: FRAME — CRACKED (BS 980)

DURING C-CHECK, FOUND FRAME AT STATION 980 CRACKED BETWEEN LONGERONS 14R AND 17R. REPAIRED FRAME IAW DC9 SRM 53-03.

Part: LONGERON — CRACKED (BS 1076)

DURING C-CHECK, FOUND LONGERON 2R CRACKED AT STATION 1076. REPAIRED LONGERON 2R IAW DC9 SRM 53-02.

Part: BLKHD FITTING — CRACKED (RT PYLON)

DURING C-CHECK, FOUND RIGHT PYLON BULKHEAD AT STATION 965 INBOARD ATTACH FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: FITTING — CRACKED (LT TE FLAP)

DURING C-CHECK, FOUND LEFT FLAP OUTBOARD HINGE INTERNAL ATTACH FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-2.

Part: STIFFENER — CRACKED (BS 760)

DURING C-CHECK, FOUND STIFFENER ON LONGERON 28R, AT STATION 760 CRACKED. INSTALLED NEW STIFFENER IAW DC9 SRM 51-30-2 AND 57-30-5.

Part: SKIN — CRACKED (BS 194)

DURING C-CHECK, FOUND SKIN CRACKED AT STATION 194, LONGERON 22L. REPAIRED SKIN IAW ABX EA 53300001-003.

Part: FITTING — CRACKED (BS 600)

DURING C-CHECK, FOUND CENTER WING FORWARD SPAR ATTACH FITTING AT STATION 600 AND LONGERON 24R CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: LONGERON — CRACKED (BS 160)

DURING C-CHECK, FOUND LONGERON 25L CRACKED AT STATION 160. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: SKIN — CRACKED (BS 1080)

DURING C-CHECK, FOUND INTERNAL FUSELAGE SKIN AT STATION 1080 CRACKED BETWEEN LONGERON 1R AND 2R. REPAIRED IAW DC9 SRM 53-04.

Part: LONGERON — CRACKED (BS 1076)

DURING C-CHECK, FOUND LONGERON 2L CRACKED AT STATION 1076. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, FOUND LONGERON 12R CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM DWG K05864.

Part: BULKHEAD WEB — CORRODED (LT PYLON)

DURING C-CHECK, FOUND LEFT PYLON BULKHEAD FORWARD LOWER SIDE CORRODED. REPLACED WEB ON PYLON BULKHEAD IAW DC9 SRM 51-30-2, 51-30-5, AND 51-30-1.

Part: ANGLE — CRACKED (VERT STAB)

DURING C-CHECK, FOUND VERTICAL STABILIZER ATTACH ANGLE RIGHT SIDE CRACKED AT LOWER AFT CORNER. REPAIRED ANGLE IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: STIFFENER — CRACKED (BS 760)

DURING C-CHECK, FOUND STIFFENER ON LONGERON 30 AT STATION 760 CRACKED. REPAIRED STIFFENER IAW DC9 SRM DWG K05159.

Part: STIFFENER — CRACKED (BS 760)

DURING C-CHECK, FOUND STIFFENER ON LONGERON 28L, STATION 760, CRACKED. REPLACED STIFFENER IAW DC9 SRM 51-30-2, 51-30-5 AND DC9 SRM DWG 5956040.

Part: SHEAR-TIE — CRACKED (BS 980)

DURING C-CHECK, FOUND FRAME SHEAR-TIE AT STATION 980 AND LONGERON 14L CRACKED. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (BS 945)

DURING C-CHECK, FOUND LONGERON 16R CRACKED AT STATION 945. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: LONGERON — CRACKED (BS 200)

DURING C-CHECK, FOUND LONGERON 24L CRACKED AT STATION 200. REPAIRED IAW DC9 SRM 53-02.

Part: WEB — CRACKED (BS 658)

DURING C-CHECK, FOUND RIGHT CUSP WEB CRACKED UNDER FLOOR TRACK AT RBL 54, STATION 658. REPAIRED IAW DC9 SRM 53-01.

Part: FLOORBEAM — CORRODED (BS 965)

DURING C-CHECK, FOUND FLOORBEAM AT STATION 965 CORRODED FROM LBL 22 TO LBL 44. REPAIRED FLOORBEAM IAW ABX REA D953-25565MR.

Part: BULKHEAD FITTING — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD DOOR JAMB FITTING CRACKED JUST ABOVE DOOR WARNING SWITCH. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: ANGLE — CRACKED (NR 2 PYLON)

DURING C-CHECK, FOUND VERTICAL ANGLE/BRACKET CRACKED ON OUTBOARD SIDE OF NR 2 PYLON, UNDER THROTTLE CONDUIT JAM NUT. REPLACED BRACKET/ANGLE IAW DC9 SRM.

Part: SUPPORT — CRACKED (BS 680)

DURING C-CHECK, FOUND FLOORBEAM SUPPORT CRACKED STATION 680 AND RBL 44. REPLACED SUPPORT FITTING IAW DC9 SRM 51-30-1 AND 51-30-2.

Part: FLOORBEAM — CRACKED (BS 680)

DURING C-CHECK, FOUND FLOORBEAM AT STATION 680 AND LBL 54 CRACKED. REPLACED FLOORBEAM IAW DC9 SRM 51-30-1, 51-30-2, AND 51-30-5.

Part: BATTERIES — DISCHARGED (CABIN)

WHEN TESTING EMERGENCY LIGHTS, LIGHTS WENT FROM DIM TO OFF IN 5 SECS. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES.

Part: SWITCH — DEFECTIVE (LT MLG)

WHEN LANDING GEAR WAS PLACED DOWN, THREE GREEN LIGHTS AND THE GEAR DOOR OPEN LIGHT REMAINED ON. REPLACED MAIN LANDING GEAR DOOR POSITION SWITCH.

Part: BULB — DEFORMED (GEAR INDICATOR)

WHEN SELECTING GEAR HANDLE TO NEUTRAL DURING UPLOCK CHECK, THE LEFT MAIN GEAR GREEN LIGHT CAME ON. RECYCLED GEAR AND LIGHT STAYED ON. CHECKED PROXIMITY SWITCH LIGHT AND LIGHT WAS OFF WITH GEAR UP. VERIFIED, FOUND DEFORMED BULB IN LEFT MLG (GREEN) LIGHT SOCKET. REPLACED BULB.

Part: FRAME — CRACKED (BS 699)

DURING C-CHECK INSPECTION, FOUND CRACKED FRAME STA 699 LEFT. REPLACED FRAME IAW DC9 SB 53-131.

Part: SEAT TRACK — WORN (CARGO COMPT)

DURING C-CHECK INSPECTION, FOUND UPPER CARGO COMPARTMENT SEAT TRACKS LOBES WORN BEYOND LIMITS. INSERT REPAIR INSTALLED IAW ABX EA 53470018.

Part: FRAME — CRACKED (BS 1121)

DURING C-CHECK INSPECTION, FOUND CANTED FRAME WEB STA 1121 CRACKED. REPAIRED WEB IAW DC9 SRM 53-01.

Part: FRAME — CORRODED (BS 851)

DURING C-CHECK, FOUND FRAME FLANGE CORRODED BEYOND LIMITS AT STATION 851 LONGERONS 5 TO 6 RIGHT. REMOVED CORROSION, REPAIRED FRAME IAW ABX SUPPLEMENTAL SRM DWG K05159.

Part: SKIN — CRACKED (BS 965)

DURING C-CHECK INSPECTION, FOUND REPAIR ON FUSELAGE SKIN AT STATION 965, LONGERON 13 T0 14 LEFT TO BE BENT AND DISTORTED. INSTALLED DOUBLER REPAIR IAW REA DC953-18792-MR.

Part: RIB — CRACKED (LT HORIZ STAB)

DURING C-CHECK INSPECTION, FOUND LEFT HAND HORIZONTAL STABILIZER INBOARD LEADING EDGE HAS A CRACKED RIB ON LOWER AFT END SECOND RIB FROM INBOARD. REPAIRED CRACKED RIB IAW DC9 SRM 55-02.

Part: SKIN — CRACKED (BS 965)

DURING C-CHECK INSPECTION, FOUND REPAIR ON FUSELAGE SKIN STATION 965, LONGERON 13 TO 14 RIGHT TO BE BENT AND DISTORTED. INSTALLED REPAIR DOUBLER PER ABX REA D953-18792-MR.

Part: SKIN — CRACKED (BS 965)

DURING C-CHECK, FOUND FUSELAGE SKIN, AT STA 965 LONGERON 13 TO 14 RIGHT, TO BE CRACKED AND TORN. REPAIR WAS ACCOMPLISHED IAW ABX REA D953-18818-MR.

Part: SKIN — CRACKED (BS 965)

FOUND THE FUSELAGE SKIN AT STA 965 LONGERON 13 AND 14 LEFT TO BE CRACKED AND TORN. REPAIRED AREA IAW ABX REA D953-18818-MR.

Part: RIB — CRACKED (VERTICAL STAB)

DURING C-CHECK INSPECTION, FOUND TWO LEADING EDGE PANEL RIBS CRACKED. REPAIRED LEADING EDGE RIBS IAW DC9 SRM 55-01.

Part: SKIN — EXCESS BLENDOUT (WS 1115)

DURING C INSPECTION, FOUND A DEEP BLENDOUT ON NR 1 SLAT DRIVE TRACK CUTOUT IN LEADING EDGE SKIN. REPAIRED IAW ABX REA D957-18774.

Part: SPOILER — CORRODED (LT WING)

LEFT OUTBOARD SPOILER CORRODED AND CRACKED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.

Part: FRAME — CRACKED (BS 945)

DURING C-CHECK INSPECTION, FOUND SEVERE DENT AND CRACK AT STATION 945, LONGERON 5 RT. INSTALLED NEW FRAME SEGEMENT AT STATION 945 IAW DC9 SRM 51-30-02, 51-30-05.

Part: COALESCER — DIRTY (LT/RT)

AFTER TAKEOFF, GOT OIL SMELL IN COCKPIT, ALL INSTRUMENT INDICATIONS WERE NORMAL. REPLACED LEFT AND RIGHT COALESCER BAGS.

Part: UPLATCH MECH — LACK OF LUBE (LT MLG)

UNSATISFACTORY UPLATCH CHECK DEPARTING. LEFT MAIN LANDING GEAR GREEN LIGHT ON BRIGHT, NO GEAR DOOR OPEN LIGHT. RECYCLED LANDING GEAR, SECOND UPLATCH CHECK WAS SATISFACTORY. LUBED LEFT MAIN LANDING GEAR AND LEFT MAIN LANDING GEAR UPLATCH MECHANISM. PERFORMED OPERATIONAL CHECK OF UPLATCH SYSTEM, OPS CHECK GOOD IAW DC-9 SUPP MM 32-60-00.

Part: SKIN — GOUGED (WS 214)

DURING C INSPECTION, FOUND A DEEP GOUGE IN NR 2 SLAT DRIVE TRACK CUTOUT IN LEADING EDGE SKIN. REPAIRED IAW ABX REA D957-18788.

Part: JAMB — DENTED (BS 200)

DURING C-CHECK INSPECTION, FOUND SERVICE DOOR JAMB DENTED. REPAIRED IAW ABX REA D953-12952-MR.

Part: INTERCOSTAL — DAMAGED (BS 370)

DURING C-CHECK INSPECTION, FOUND MISDRILLED HOLES IN THE INTERCOSTAL AT STA 370, LONGERON 28R. REPAIRED IAW ABX REA D953-13047-MR.

Part: FORMER — MISDRILLED (BS 370)

DURING C-CHECK INSPECTION, FOUND MISDRILLED HOLES IN THE FORMER AT STA 370, LONGERON 28R. REPAIRED IAW ABX REA D953-13047-MR.

Part: DOUBLER — CORRODED (BS 917)

DURING C-CHECK INSPECTION, FOUND EXCESSIVE CORROSION ON AFT LOWER CARGO DOOR DOUBLER. REPAIRED DOUBLER IAW ABX REA D953-12953-MR.

Part: SKIN — CORRODED (BS 917)

DURING C-CHECK INSPECTION AND PSE INSPECTION 53.09.035A, AD 94-03-01, FOUND EXCESSIVE CORROSION ON THE FUSELAGE SKIN. REPAIRED SKIN IAW ABX REA D953-12953-MR.

Part: WEB — CUT (BS 699-737)

DURING C-CHECK INSPECTION, IT WAS NECESSARY TO CUT CUSP WEB FOR ACCESS TO DO OTHER REPAIRS. REPAIRED CUSP WEB IAW ABX REA D953-13050-MR.

Part: WEB — CUT (BS 699-737)

DURING C-CHECK INSPECTION, IT WAS NECESSARY TO CUT CUSP WEB FOR ACCESS TO DO OTHER REPAIRS. REPAIRED CUSP WEB IAW ABX REA D953-13050-MR.

Part: WEB — CUT (BS 699-737)

DURING C-CHECK INSPECTION, IT WAS NECESSARY TO CUT CUSP WEB FOR ACCESS TO DO OTHER REPAIRS. REPAIRED CUSP WEB IAW ABX REA D953-13050-MR.

Part: WEB — CUT (BS 699-737)

DURING C-CHECK INSPECTION, IT WAS NECESSARY TO CUT CUSP WEB FOR ACCESS TO DO OTHER REPAIRS. REPAIRED CUSP WEB IAW ABX REA D953-13050-MR.

Part: SKIN — DAMAGED (BS 105)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 94-03-01, FOUND FUSELAGE SKIN DENTED AND CRACKED AT STA 105, LONGERON 18L. REPAIRED IAW ABX REA D953-13037-MR.

Part: WEB — CUT (BS 699-737)

DURING C-CHECK INSPECTION, IT WAS NECESSARY TO CUT CUSP WEB FOR ACCESS TO DO OTHER REPAIRS. REPAIRED CUSP WEB IAW ABX REA D953-13050-MR.

Part: FLOORBEAM — CORRODED (BS 389)

DURING C-CHECK INSPECTION, FOUND CORROSION ON FLOORBEAM AT STA 389 AT RBL 44. REPAIRED IAW ABX REA D953-13029-MR.

Part: SKIN — DAMAGED (BS 168)

DURING C-CHECK INSPECTION, FOUND A DENT WITH A GOUGE IN FUSELAGE SKIN STA 168, LONGERON 19R. REPAIRED IAW ABX REA D953-12980-MR.

Part: SKIN — DAMAGED (BS 206)

DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED WITH A GOUGE AT STA 206, LONGERON 19R. REPAIRED IAW ABX REA D953-12989-MR.

Part: SKIN — CORRODED (BS 298.5)

DURING C-CHECK INSPECTION, FOUND CORROSION ON FUSELAGE SKIN IN AREA OF NR 2 ADF LOOP ANTENNA, STA 298.5, BETWEEN LONGERON 1 AND 2L. REPAIRED IAW ABX REA D953-12973-MR.

Part: FLOORBEAM — GOUGED (BS 389)

DURING C-CHECK INSPECTION, FOUND FLOORBEAM STA 389, GOUGED. REPAIRED IAW ABX REA D953-13009-MR.

Part: SKIN — DAMAGED (BS 897)

DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DAMAGED AT THE FORWARD EDGE OF THE ALC DOOR CUTOUT. REPAIRED IAW ABX REA D953-13004-MR.

Part: SKIN — DENTED (BS 80)

DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED AND GOUGED AT STA 80, LONGERON 18. REPAIRED IAW ABX REA D953-12995-MR.

Part: BLKHD SKIN — DAMAGED (BS 996)

DURING C-CHECK INSPECTION, FOUND DAMAGE AT FORWARD SIDE OF AFT PRESSURE BULKHEAD SKIN. REPAIRED IAW ABX REA D953-13005-MR.

Part: SKIN — DAMAGED (BS 189)

DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED WITH A GOUGE AT STA 189, LONGERON 19R. REPAIRED IAW ABX REA D953-12988-MR.

Part: SKIN — DAMAGED (BS 937)

DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED AND GOUGED AT STA 937, LONGERON 23. REPAIRED IAW ABX REA D953-12993-MR.

Part: ANGLE — CRACKED (WS 48)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND RIGHT WING TO FUSELAGE GUSSET ANGLE AT STA 48 CRACKED. REPAIRED IAW DC-9 SB 57-103.

Part: BLKHD SKIN — GOUGED (BS 996)

DURING C-CHECK INSPECTION, FOUND A GOUGE IN THE AFT SIDE OF THE AFT PRESSURE BULKHEAD. REPAIRED IAW ABX REA D953-12990-MR.

Part: ANGLE — CRACKED (WS 48)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND LEFT WING TO FUSELAGE GUSSET ANGLE AT STA 48 CRACKED. REPAIRED IAW DC-9 SB 57-103.

Part: SKIN — DAMAGED (BS 110-218)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND LIGHTNING STRIKES FROM STA 110 TO 218, LONGERON 26R. REPAIRED IAW DC-9 SRM 53-04 FIG 38.

Part: SKIN — DENTED (BS 115)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND DENT IN THE FUSELAGE SKIN AT STA 115, LONGERON 21L. REPAIRED IAW DC-9 SRM 53-04 FIG 38 VIEW 1.

Part: ANGLE — MISSING (NLG DOOR)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND SERVICE BULLETIN FITTINGS MISSING FROM NOSE LANDING GEAR DOORS. REPAIRED FITTINGS IAW DC-9 SRM 51-30-1, 51-30-2, 51-30-4 AND INSTALLED DOUBLERS IAW EA NR FS-53-03529-MA.

Part: BLKHD SKIN — GOUGED (BS 1046)

DURING C-CHECK INSPECTION, FOUND THE INLET DUCT GOUGED THE BULKHEAD SKIN AT STA 1046. REPAIRED IAW ABX REA D953-12991-MR.

Part: FRAME — CRACKED (BS 718)

DURING C-CHECK INSPECTION, FOUND MAIN FRAME STA 718 CRACKED ON RIGHT SIDE. REPAIRED IAW ABX REA D953-12966-SB.

Part: TE PANEL — DELAMINATED (WS 445-509)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND WING TRAILING EDGE PANEL FORWARD OF RIGHT AILERON DELAMINATED. REPLACED PANEL IAW DC-9 SRM 51-30-1 AND 51-30-2.

Part: SKIN — REQ'D REPAIR (BS 160)

DURING C-CHECK AND PSE INSPECTIONS, FOUND PREVIOUS REPAIR AT FORWARD UPPER CORNER OF ENTRY DOOR CUTOUT. REPAIRED IAW ABX REA D953-12981-MR.

Part: FRAME — CRACKED (BS 718)

DURING C-CHECK INSPECTION, FOUND MAIN FRAME STA 718 CRACKED ON LEFT SIDE. REPAIRED IAW ABX REA D953-12966-SB.

Part: PAN — CRACKED (BS 148)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND UPPER FORWARD END OF SERVICE DOOR HOLD OPEN LATCH PAN CRACKED AT WELD. REPLACED LATCH PAN IAW DC-9 SRM 51-30-2.

Part: ANGLE — CRACKED (BS 110)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND PANEL 110 SUPPORT ANGLE CRACKED. FABRICATED AND INSTALLED NEW ANGLE IAW PFEA NR PFE-D953-10918 AND DC-9 SRM 51-30-5.

Part: PANEL — DELAMINATED (WS 363-414)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND LEFT WING UPPER BONDED PANEL FORWARD OF AILERON DELAMINATED. REPLACED PANEL IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: DOOR — DELAMINATED (LT MLG DOOR)

DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR DOOR DELAMINATED. REPLACED DOOR IAW DC-9 M.M. 32-12-1.