N939AX

Part: FLOORBEAM — CRACKED (BS 175) · airframe 54,723 hrs · 45,423 cycles

FLOORBEAM CRACKED TO LIGHTENING HOLE APPROXIMATELY STA 175, BUTT LINE 0. REPAIRED AREA IAW REA D953-55576MR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,723 hrs · 45,423 cycles

AFT RIGHT MAIN FRAME HAD CRACK AT FORWARD AND AFT FLANGES, MUST BE REPLACED PER NEA 53400102-002-30. REMOVED AND REPLACED RIGHT MAIN FRAME IAW DC9 EA 53400326-001-2. CRACK LENGTHS WERE 1" AND 1 1/4".

Part: BULKHEAD — CRACKED (RT PYLON) · airframe 54,723 hrs · 45,423 cycles

RIGHT PYLON BULKHEAD AT STA 965 HAD CRACKED ATTACH FITTING AT RIGHT BUTT LINE 32. REMOVED AND REPLACED FITTING IAW DAC DWG 9912243.

Part: ATTACH ANGLE — CORRODED (BS 965) · airframe 54,723 hrs · 45,423 cycles

UPPER SURFACE OF PYLON BULKHEAD TO FLOORBEAM ATTACH ANGLE AT STA 965 CORRODED FROM RIGHT BUTT LINE 55, RIGHT BUTT LINE 36. FABRICATED AND INSTALLED NEW PYLON BULKHEAD TO FLOORBEAM ATTACH ANGLE IAW DAC DWG 9912243.

Part: SHEAR TIE — CRACKED (BS 945 S15-16R) · airframe 54,723 hrs · 45,423 cycles

SHEAR TIE CRACKED AT FS 945, BETWEEN LONGERON 15 RIGHT AND LONGERON 16 RIGHT. REMOVED AND REPLACED SHEAR TIE IAW DC9 SRM 51-30-2, 51-30-5 AND 51-30-1.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,723 hrs · 45,423 cycles

AFT PRESSURE BULKHEAD LOWER DOOR CORNER HAD A CRACK IN SKIN. THE REPAIR INSTALLED DID NOT MATCH ANY CONFIGURATION OF DWG J060088 IN NUMBER, PLACEMENT AND MATERIAL OF DOUBLERS. REMOVED PREVIOUS REPAIR. NO CRACKS FOUND. REPAIRED LOWER DOOR CORNER IAW SERVICE REWORK DWG J060088-519 CONFIGURATION.

Part: FRAME — CORRODED (BS 718) · corrosion level 2 · airframe 54,723 hrs · 45,423 cycles

LOWER POCKETS IN MAIN FRAME IN LEFT WHEEL WELL HAD CORROSION AROUND LOWER VERTICAL ATTACH BOLTS. CLEANED, TREATED CORROSION AROUND LOWER VERTICAL ATTACH BOLT ON LEFT MAIN FRAME 718 AIW DC9 SRM.

Part: RIB — CRACKED (LT WING) · airframe 54,723 hrs · 45,423 cycles

LEFT WING XRS 164, RIB FITTING CRACKED. REMOVED AND REPLACED RIB AT LEFT WING XRS 164 IAW DC9 SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,723 hrs · 45,423 cycles

AFT PRESSURE BULKHEAD LEFT UPPER DOOR CORNER HAD 2 CRACKS THAT NEEDED TO BE STOP DRILLED. REMOVED OUTSIDE DOUBLER, STOP DRILLED CRACKS IAW SRO J060088. REINSTALLED DOUBLER IAW SRO J060088 AND DC9 SRM 51-30-5. CRACK LENGTHS WERE 7/8", 3/4" AND 1".

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 54,705 hrs · 45,409 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY SUPPLY POWER PACK IAW DC9 MM 33-53-00.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 54,570 hrs · 45,293 cycles

AIRCRAFT LOST PRESSURIZATION AT 6500 FT IN DESCENT TO ILN, BOTH PACKS ON. CHECKED TAIL COMPARTMENT FOR LOOSE AND BLOWN DUCTS. NO DEFECTS FOUND. PERFORMED ADJ/TEST OF CABIN PRESSURE CONTROL WITH PNEUMATIC SOURCE IAW DC9 MM 21-32-00-2-0101. SYSTEM OPERATES NORMAL.

Part: CONTROL PANEL — DEFECTIVE (NR 2 COMM) · airframe 54,568 hrs · 45,292 cycles

NR 2 COM FREQUENCY SELECTOR WAS REPORTED AS INOPERATIVE BY CREW. ELECTED TO REROUTE FLIGHT 122 ICT TO ILN, OVERFLEW SGF. ON L/P 033705-049/2, NR 2 COM FREQUENCY SELECTOR OCCASIONALLY DIALED WRONG FREQUENCY. VOLUME AND SELECTOR KNOBS WHEN WIGGLED SHORTED OUT VOLUME AND FREQUENCY. REMOVED AND REPLACED NR 2 COM/NAV CONTROL PANEL IAW DC9 AMM 23-20-02-2.

Part: SKIN — CRACKED (FUSELAGE) · corrosion level 2 · airframe 52,985 hrs · 43,775 cycles

DURING LINE MAINTENANCE, FOUND FUSELAGE SKIN CRACKED AND BULGED AT STA 759, LONGERON 29 RIGHT. REPAIRED SKIN IAW DC-9 SRM 53-04, FIG 12B.

Part: SKIN — CRACKED (FUSELAGE) · corrosion level 2 · airframe 52,985 hrs · 43,775 cycles

DURING LINE MAINTENANCE, FOUND FUSELAGE SKIN CRACKED AND CORRODED AT STA 917 AND LONGERON 28 RIGHT. REPAIRED SKIN IAW REA D953-49934MR.

Part: FITTING — CORRODED (TE FLAP) · airframe 52,424 hrs · 43,237 cycles

FLAP HINGE STUDS AT FLAP FITTING STA. 267 HEAVILY CORRODED. REPLACED FLAP HINGE IAW DC-9 MM 57-40-01-2-0001.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,464 hrs · 43,237 cycles

CABIN FLOORBEAM INTERCOSTAL BETWEEN STA. 256 AND 275, BUTT LINE O, CRACKED FORWARD END. REPLACED INTERCOSTAL IAW DC-9 SSRM K05159.

Part: ROD — OUT OF ADJUST (WINDOW) · airframe 51,463 hrs · 42,223 cycles

CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. FOUND UPPER HOOK NOT CLEARING TO ALLOW WINDOW TO OPEN. ADJUSTED UPPER ROD WINDOW IAW DC-9 MM, OPS CHECKED GOOD.

Part: FITTING — CRACKED (AFT CARGO) · airframe 51,299 hrs · 42,061 cycles

AFT LOWER CARGO DOOR #2 BEAM, AFT END FITTING WAS CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2, 51-30-1, 51-20-0.

Part: SKIN — CANNING (FUSELAGE) · airframe 51,299 hrs · 42,061 cycles

FUSELAGE EXTERIOR SKIN WAS OIL CANNING UNDER THE NR 2 PYLON, FORWARD OF STATION 965 IN TWO BAYS. REPAIRED IAW DC-9 SRM 53-04.

Part: TRACK — DIRTY (COCKPIT WINDOW) · airframe 51,259 hrs · 42,025 cycles

CAPTAIN'S CLEAR VIEW WINDOW WAS STUCK CLOSED. OPENED WINDOW AND CLEANED THE TRACK. OPS CHECKED GOOD IAW DC-9 MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,173 hrs · 41,945 cycles

THE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES IAW DC-9 MM 33-53-00. THE EMERGENCY LIGHT BATTERY PACK WAS DEFERRED FOR REPLACEMENT. THE EMERGENCY LIGHT BATTERY PACK WAS REPLACED.

Part: WIRE — DAMAGED (LT MLG) · airframe 50,705 hrs · 41,448 cycles

THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED INTERMITTANTLY. THE FLIGHT RETURNED TO ILN TO COMPLETE REPAIRS. MAINTENANCE INSPECTED AND REPAIRED A WIRE FOR CONNECTOR P1-130 PIN NR 4. LANDING GEAR OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WINDOW — SEIZED (COCKPIT) · airframe 50,638 hrs · 41,375 cycles

CREW WAS UNABLE TO OPERATE CAPTAINS CLEARVIEW WINDOW. THE AIRCRAFT RETURNED TO BLOCKS. MAINTENANCE INSPECTED AND LUBRICATED THE CAPTAINS CLEAR VIEW WINDOW IAW DC-9 MM. OPS CHECKED GOOD.

Part: WINDOW — OUT OF ADJ (COCKPIT) · airframe 50,070 hrs · 40,856 cycles

CAPTAIN''S CLEARVIEW WINDOW (EMERGENCY EXIT) WOULD NOT OPEN. ADJUSTED CAM FOLLOWER VERTICAL AND EXTENSION ADJUSTMENTS.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 50,068 hrs · 40,853 cycles

DURING D-CHECK, FOUND INTERNAL DOUBLER CORRODED AT STATION 579 AND LONGERON 30. REPLACED DOUBLER IAW DC9 SRM 51-30-2.

Part: FITTING — CORRODED (RT MLG WW) · corrosion level 2 · airframe 50,068 hrs · 40,853 cycles

DURING D-CHECK, FOUND CENTER TANK TO SLANT PANEL FITTING CORRODED. REPLACED FITTING IAW DC9 SRM 51-10-4.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,068 hrs · 40,853 cycles

DURING D-CHECK, FOUND SLANT PANEL OUTBOARD FITTING, STATION 699 CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1.

Part: TANK — CORRODED (CENTER WING) · airframe 50,068 hrs · 40,853 cycles

DURING D-CHECK, FOUND AFT EDGE OF UPPER CENTER TANK PLATING CORRODED AT STATION XCW 20. REPAIRED IAW ABX REA D957-36744.

Part: FITTING — CRACKED (FUSELAGE) · airframe 50,068 hrs · 40,853 cycles

DURING D-CHECK, FOUND PYLON SUPPORT BULKHEAD FITTING CORRODED AT STATION 965 LEFT. REPLACED SUPPORT FITTING IAW DC9 SRM 51-30-5.

Part: FITTING — CORRODED (LT WING) · airframe 50,068 hrs · 40,853 cycles

DURING D-CHECK, FOUND NR 1 SLAT TRACK FITTING CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-2.

Part: FITTING — CRACKED (CARGO BAY) · airframe 50,068 hrs · 40,853 cycles

DURING D-CHECK, FOUND LONGERON 29 RIGHT END FITTING AT STATION 604 CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: CAP — CORRODED (CENTER FUSELAGE) · corrosion level 2 · airframe 50,068 hrs · 40,853 cycles

DURING ''D'' CHECK, FOUND TEE CAP CORRODED AT STA 604 BETWEEN LONGERON 29L AND 30. REPAIRED TEE CAP IAW DC9 SRM 53-03.

Part: FITTING — CRACKED (CARGO BAY) · airframe 50,068 hrs · 40,853 cycles

DURING D-CHECK, FOUND LONGERON 30 SPLICE FITTING CRACKED AT STATION 602. REPLACEDFITTING IAW DC9 SRM 51-10-2.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 50,068 hrs · 40,853 cycles

DURING D-CHECK, FOUND RIGHT HORIZONTAL STABILIZER OUTBOARD RIB CRACKED. REPLACED RIB IAW DC9 SRM 51-30-1.

Part: FLOORBEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 50,068 hrs · 40,853 cycles

DURING ''''D'''' CHECK, FOUND FLOORBEAM CORRODED AT STA 313 AND LBL 40. REPAIRED FLOORBEAM IAW DC9 SRM 53-05.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,068 hrs · 40,853 cycles

DURING D-CHECK, FOUND INTERCOSTAL WEB CORRODED AT STATION 945 - 965 AND LONGERON 19 RIGHT. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-5.

Part: SPLICE — CORRODED (CABIN) · corrosion level 2 · airframe 50,068 hrs · 40,853 cycles

DURING ''D'' CHECK, FOUND SEAT TRACK SPLICE CORRODED ON LOWER SIDE, STATION 395, RBL 8. REPLACED SPLICE IAW DC9 SRM 51-30-1.

Part: GUSSET — CORRODED (CARGO BAY) · corrosion level 2 · airframe 50,068 hrs · 40,853 cycles

DURING ''D'' CHECK, FOUND CORROSION ON GUSSET PLATES AT STATION 965, LONGERON 19R. REPLACED GUSSETS IAW DC9 SRM 51-30-5.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 50,068 hrs · 40,853 cycles

DURING D-CHECK, FOUND CORROSION ON DOUBLER, STATION 1087 AND LONGERON 1 LEFT. REPLACED DOUBLER IAW DC9 SRM 51-30-2.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 50,068 hrs · 40,853 cycles

DURING D-CHECK, FOUND CORRODED INTERCOSTAL BETWEEN STATION 218 AND 237 AT LONGERON 28 LEFT. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,068 hrs · 40,853 cycles

DURING D-CHECK, FOUND NOSE WHEEL WELL UPPER PRESSURE PANEL STIFFENER CORRODED. REPLACEDPRESSURE PANEL STIFFENER IAW DC9 SRM.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 50,068 hrs · 40,853 cycles

DURING D-CHECK INSPECTION, FOUND LEFT VERTICAL STAB TO FUSELAGE ATTACH ANGLE CRACKED AT STATION 1109. REPAIRED ANGLE IAW ABX REA D953-36544-MR.

Part: FITTING — CORRODED (RT WING) · airframe 50,068 hrs · 40,853 cycles

RIGHT OUTBOARD SLAT IDLER TRACK FITTING HAD HEAVY CORROSION/EXFOLIATION AT 3 MOUNT HOLES. REPLACED RIGHT NR 1 LEADING EDGE SLAT.

Part: WEB — CRACKED (CABIN) · airframe 50,068 hrs · 40,853 cycles

LEFT CUSP WEB CRACKED AT STATION 596 AND RBL 44. REPLACED CUSP WEB IAW DC9 SRM51-30-2.

Part: CONTROL VALVE — ICED UP (LANDING GEAR)

ON APPROACH, LANDING GEAR HANDLE WAS 'FROZEN' IN THE UP POSITION. ACCOMPLISHED DC9 ABNORMAL PROCEDURES. EMERGENCY GEAR EXTENSION, RESULTED IN UNEVENTFUL LANDING. REMOVED ICE FROM LANDING GEAR CONTROL VALVE CABLES, RESET EMERGENCY EXTENSION CONTROLS. CYCLED LANDING GEAR CONTROL VALVE, OPS CHECKED GOOD.

Part: FLOORBEAM — CRACKED (BS 965)

ILN - DURING C-CHECK, FOUND UPPER SURFACE OF FLOORBEAM STA 965 RBL 8.0 TO RBL 21 CORRODED. REPAIRED IAW DC9 SRM 51-10-32 AND DWG K05019. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)

Part: ANGLE — CRACKED (RT TE FLAP)

ILN - DURING C-CHECK, FOUND RIGHT FLAP OUTBOARD HINGE OUTBOARD INTERIOR ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-1 AND SRM 51-30-2. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)

Part: FITTING — CRACKED (LT VENTRAL DOOR)

ILN - DURING C-CHECK, FOUND LOWER LEFT VENTRAL DOOR STOP SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-2 AND SRM 51-30-5. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)

Part: SKIN — CRACKED (FUSELAGE)

ILN - DURING C-CHECK, FOUND NR 2 ADF LOOP ANTENNA AREA EXTERIOR FUSELAGE SKIN CRACKED AROUND HOLE FOR ANTENNA LEAD WIRE. REPAIRED SKIN IAW ABX REA D953-24811-MR. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)

Part: FRAME — CORRODED (BS 180)

ILN - DURING C-CHECK, FOUND FUSELAGE FRAME AT STA 180 AND LONGERONS 22R- 27R CORRODED. REPAIRED FRAME IAW DC9 SRM 53-03. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)

Part: WEB — CORRODED (BS 965)

ILN - DURING C-CHECK, FOUND CUSP WEB CORRODED AT STA 965 BETWEEN RBL 44 ND RBL 54.5, IN LIGHTENING HOLE AREA BETWEEN STA 945 - STA 965. REPAIRED CUSP WEB IAW ABX REA D953-24862-MR. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)

Part: FRAME — CRACKED (BS 980)

ILN - DURING C-CHECK, FOUND FUSELAGE FS 980 CRACKED AT LONGERON 17R. REPAIRED FRAME IAW DC9 SRM 53-03. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)

Part: TEE — CORRODED (BS 946/980)

ILN - DUIRNG C-CHECK, FOUND CUSP TEE ANGLES AT LONGERON 18R AND STA 946 - STA 980 CORRODED ON LOWER SIDE. REPAIRED IAW DC9 SRM 53-05. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X)

Part: LONGERON — CRACKED (BS 160)

DURING C-CHECK, FOUND LONGERON 4L CRACKED AT STATION 160. REPAIRED LONGERON IAW DC-9 SRM 53-02.

Part: SPAR CAP — CORRODED (RT WING)

DURING C-CHECK, FOUND RIGHT WING UPPER SPAR CAP CORRODED BEYOND LIMITS UNDER AND AROUND THE NUT PLATE JUST OUTBOARD OF RIGHT AILERON. REPAIRED IAW ABX REA D957-24791-MR.

Part: MEMBRANE — CRACKED (BS 120)

DURING C-CHECK, FOUND THE SUBFLOOR MEMBRANE CRACKED AT STATION 120 ABOVE THE AILERON LOAD FEEL CENTERING SPRING ON RIGHT SIDE. REPAIRED SUBFLOOR MEMBRANE IAW DC-9 SRM 53-01.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, FOUND LONGERON 16R CRACKED AT STATION 965. REPAIRED LONGERON IAW DC-9 SRM 53-02.

Part: FITTING — CRACKED (RT WING SPOILER)

DURING C-CHECK, FOUND RIGHT OUTBOARD SPOILER TORSION BAR CENTER SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30 AND 51-30-2.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, FOUND LONGERONS 17L AND 17R CRACKED AT STATION 965 AND 980. REPAIRED LONGERONS IAW DC-9 SRM 53-02.

Part: BLKHD STIFFENER — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND STIFFENER CRACKED, RIGHT SIDE OF AFT PRESSURE BULKHEAD DOOR JAMB APPROXIMATELY 18 ABOVE FLOOR. REPLACED STIFFENER IAW DC-9 SRM 51-30-5 AND 51-30-2.

Part: SWITCH — SHORTED (LT MLG)

LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH THE GEAR HANDLE UP. RECYCLED GEAR, NO CHANGE. REPAIRED SHORTED PIN NR 6 ON THE LEFT MAIN LANDING GEAR DOWN LOCK LIMIT SWITCH. OPS CHECKED GOOD ON GEAR SWING.

Part: AIR DISTRIBUTION — ODOR (CABIN)

IN FLIGHT THERE WAS A FAINT ODOR OF KEROSENE OR JET FUEL. ALL FUEL INDICATIONS WERE NORMAL. AFTER A COUPLE OF MINUTES THE ODOR WAS NO LONGER DISTINGUISHABLE. INSPECTED BOTH A/C PACKS. FOUND NO DEFECT. RAN BOTH PACKS, BOTH SYSTEMS CHECKED GOOD. NO ODOR DETECTED.

Part: BULKHEAD JAMB — CRACKED (BS 996)

DURING C-CHECK, FOUND VENTRAL DOOR JAMB CRACKED AT UPPER RIGHT CORNER. REPAIRED IAW ABX REA D953-17620-MR, D953-17964-MR.

Part: FLOOR SUPPORT — CORRODED (BS 351-408)

DURING C-CHECK, FOUND LEFT FLOOR STRAP CORRODED BETWEEN STA 351 - 408. REPLACED IAW ABX SSRM DWG K05554.

Part: SPAR WEB — CRACKED (HORIZONTAL STAB)

DURING C-CHECK, FOUND CRACK IN HORIZONTAL STAB CENTER SECTION REAR SPAR WEB. REPLACED IAW DC9 S/B 55-32 AND ABX REA D955-17703-IR, D955-17643.

Part: ANGLE — CRACKED (BS 655-661)

DURING C-CHECK, FOUND CRACKED ANGLE AT UPPER SURFACE OF CENTER TANK STA. 661, 655. REPLACED IAW DC9 SRM 51-30-5.

Part: SPAR CAP — CORRODED (WS 267)

DURING C-CHECK, FOUND RIGHT WING REAR SPAR UPPER CAP CORRODED AT STA XRS 267. REPAIRED IAW ABX REA D957-17950-MR.

Part: FITTING — CORRODED (BS 218)

DURING C-CHECK, FOUND CORRODED FRAME FITTING AT STA 218. REPLACED IAW DC9 SRM 51-30-1, 51-30-5.

Part: SKIN — CRACKED (LT TE FLAP)

DURING C-CHECK, FOUND CRACK ON LEFT FLAP LEADING EDGE. REPAIRED IAW ABX REA D957-17672-MR.

Part: DOOR JAMB — CRACKED (BS 996)

DURING C-CHECK, FOUND RIGHT LOWER CORNER OF VENTRAL DOOR JAMB CRACKED. REPAIRED IAW ABX REA D953-17615.

Part: ANGLE — CRACKED (BS 639)

DURING C-CHECK, FOUND FLOOR PANEL SUPPORT ANGLE CRACKED AT STA 639. REPLACED IAW DC9 SRM 51-30-2, DOUGLAS DWG. NR 5914617.

Part: SHEAR TIE — CRACKED (BS 890)

DURING C-CHECK, FOUND CRACKED SHEAR TIE STA 890. REPLACED IAW DC9 SRM 51-30-2, 51-30-5, DOUGLAS DWG NR9915578.

Part: CUSP — CORRODED (BS 313-389)

DURING C-CHECK, FOUND CORRODED CUSP WEB AT STA 313 - 389. REPAIRED IAW DC9 SRM 53-01, FIGURE 1, SHEET 3.

Part: FRAME — CORRODED (BS 237)

DURING C-CHECK, FOUND CORRODED FRAME STA 237 AT LONGERON 30. REPAIRED IAW DC9 SRM 53-03, FIGURE 2A.

Part: CUSP — CORRODED (BS 218-256)

DURING C-CHECK, FOUND CORRODED CUSP WEB BETWEEN STA 218 - 256, LEFT SIDE. REPLACED IAW DC9 SRM 51-30-2, 51-30-5, 51-30-1.

Part: FITTING — CORRODED (BS 313)

DURING C-CHECK, FOUND LEVEL 2 CORROSION ON FLOOR TO FRAME ATTACH FITTING STA 313. REPLACED IAW DC9 SRM 51-30-1, 51-30-5.

Part: WEB — CRACKED (BS 852)

DURING C-CHECK, FOUND CUSP WEB CRACKED AT STA 852, LEFT SIDE. REPAIRED IAW ABX REA D953-17673-MR.

Part: SHEAR TIE — CRACKED (BS 980)

DURING C-CHECK, FOUND VERTICAL SHEAR TIE CRACKED AT STA 980. REPAIRED IAW ABX REA D953-17666.

Part: VANE — DELAMINATED (RT TE FLAP)

THE RIGHT WING CENTER FLAP VANE HAD DELAMINATION ON THE UPPER MID SURFACE BETWEEN RUBSTRIPS. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.

Part: VANE — GOUGED (RT TE FLAP)

THE RIGHT WING INBOARD FLAPS VANE WAS GOUGED AT THE MID RUBSTRIPS. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.

Part: FLOOR SUPPORT — CORRODED (BS 218)

DURING C-CHECK, FOUND CORRODED FLOOR SUPPORT AT STA 218. REPLACED FLOOR SUPPORT IAW DC9 SRM 51-30-5.

Part: PANEL — DELAMINATED (LT WING)

DURING C-CHECK, FOUND BONDED PANEL BELOW ANTI-SKID VALVES DELAMINATED. REPLACED PANEL IAW DC9 SRM 51-30-1.

Part: SHEAR TIE — CORRODED (BS 622)

DURING C-CHECK, FOUND CORROSION ON AFT SIDE OF FRAME AND SHEAR TIE STA 622. REPLACED SHEAR TIE IAW DC9 SRM 51-10-4, 51-30-5.

Part: FITTING — CRACKED (BS 680)

DURING C-CHECK, FOUND VERTICAL FITTING AT UPPER SURFACE OF CENTER TANK STA 680 CRACKED. REPLACED IAW DC-9 SRM 51-30-2, 51-30-5.

Part: ANGLE — CRACKED (BS 639)

DURING C-CHECK, FOUND CRACKED FLOOR PANEL SUPPORT ANGLE STA 639. REPLACED ANGLE IAW DC-9 SRM 51-30-2.

Part: FITTING — CRACKED (BS 680)

DURING C-CHECK, FOUND VERTICAL FITTING CRACKED AT UPPER SURFACE OF CENTER TANK STA 680. REPLACED IAW DC-9 SRM 51-10-4, 51-30-2, 51-30-5.

Part: SHEAR TIE — CRACKED (BS 980)

DURING C-CHECK, FOUND CRACKED SHEAR TIE AT STA 980. REPLACED IAW DC9 SRM 51-30-2, 51-30-5, REA D953-17707.

Part: VANE — DENTED (RT TE FLAP)

THE RIGHT INBOARD FLAP VANE WAS DEEPLY DENTED AND DELAMINATED ON THE UPPER SIDE AT THE CENTER RUBSTRIPS. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.

Part: TRIM — LOOSE (RT CV WINDOW)

FIRST OFFICER'S CLEARVIEW WINDOW WILL NOT OPEN. REGLUED INTERIOR TRIM IN PLACE.

Part: SWITCH — MALFUNCTIONED (NLG)

DURING APPROACH TO ILN, DID NOT GET GREEN LIGHT FOR NOSE GEAR. RECYCLED TWICE AND RECEIVED GREEN LIGHT. MAINTENANCE DID NOT VERIFY. CLEANED AND RESEATED PLUG, REPLACED SWITCH AND BULBS AS A PRECAUTIONARY MEASURE IAW DC-9 MM 32-60-1. PERFORMED GEAR SWING IAW DC-9 32-30-0. OPS CHECKED GOOD.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

DURING PREFLIGHT INSPECTION, FOUND EMERGENCY LIGHTS VERY DIM. REPLACED EMERGENCY BATTERIES IAW DC9 MM.

Part: SKIN — DENTED (FS 465-503)

DURING C-CHECK INSPECTION FOUND NUMEROUS DENTS, GOUGES AND STATIC DISCHARGE MARKS IN THE RIGHT FUSELAGE SKIN AT FS 465 - 503. REPAIRED IAW ABX REA D953-11829-MR.

Part: SKIN — BLENDED (BS 794-813)

DURING C-CHECK INSPECTION FOUND, FUSELAGE SKIN, STA. 794 - 813 LEFT SIDE, BLENDED. REPAIRED IAW ABX REA D953-11840-MR.

Part: JAMB — CORRODED (BS 380-427)

DURING C-CHECK INSPECTION, FOUND FORWARD LOWER CARGO DOOR JAMB INTERNAL DOUBLER AND DOOR JAMB PAN CORRODED. REPAIRED IAW ABX REA D953-11776-MR.

Part: SKIN — DENTED (FS 313)

DURING C-CHECK INSPECTION, FOUND FIVE SHARP DENTS IN THE RIGHT FUSELAGE SKIN AT FS 313 AND LONGERONS 24 AND 25R. REPAIRED IAW ABX REA D953-11837-MR.

Part: SPAR CAP — CORRODED (XRS 540)

DURING C-CHECK INSPECTION, FOUND CORROSION ON THE LEFT WING AFT SPAR UPPER CAP. REPAIRED IAW ABX REA D957-11819-MR.

Part: BRACKET — CHAFED (BS 110)

DURING C-CHECK INSPECTION, FOUND NR 1 ENGINE THRUST REVERSER CABLE RUN NR 47 CHAFING THROUGH PULLEY BRACKET BELOW COCKPIT PEDESTAL, APPROXIMATELY STA. 110. REPAIRED IAW ABX REA D953-11824-MR.

Part: SKIN — DAMAGED (BS 237-256)

DURING C-CHECK INSPECTION, FOUND 9-G NET CHANNEL HAD IMPROPERLY LOCATED HOLES THROUGH THE FINGER DOUBLER AT STA. 237 TO 256 AT LONGERONS NR 1 AND NR 2. REPAIRED IAW ABX REA D953-11796-MR.

Part: DOUBLER — CRACKED (BS 133)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D 90-80-03; S.B. 56-1, FOUND CRACKS AROUND RIVETS AND EDGE OF DOUBLER AT UPPER AFT CORNER OF RIGHT CLEARVIEW WINDOW. ALSO DISCOVERED A CRACKED RETAINER SKIN AROUND WINDOW AFTER DOUBLER WAS REMOVED. REPAIRED IAW DOUGLAS SERVICE REWORK DRAWING NR 5952965.

Part: SKIN — GOUGED (FS 125)

DURING C-CHECK INSPECTION, FOUND FORWARD ENTRY DOOR HOLD OPEN LATCH HITTING FORWARD LOWER CORNER OF LATCH PIN CUTOUT. REPAIRED IAW DC-9 SRM 53-04, FIG. 24 AND ABX REA D953-11777-MR.

Part: BUSHING — WORN (RT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND SECONDARY LINKAGE CLEVIS ON RIGHT MAIN LANDING GEAR OUTBOARD DOOR DRIVE ROD WORN. REPLACED BUSHING ON LINK ASSEMBLY IAW DC-9 MM 32-10-0.

Part: BOLT — WORN (RT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND SECONDARY LINKAGE CLEVIS ON RIGHT MAIN LANDING GEAR OUTBOARD DOOR DRIVE ROD WORN. REPLACED BOLT ON LINK ASSEMBLY IAW DC-9 MM 32-10-0.

Part: BUSHING — WORN (LT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND SECONDARY LINKAGE CLEVIS ON LEFT MAIN OUTBOARD GEAR DOOR DRIVE ROD WORN. REPLACED BUSHING ON LINK ASSEMBLY ON LEFT MAIN GEAR OUBOARD DRIVE ROD IAW DC-9 MM 32-10-0.

Part: ROD END — WORN (RT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR DRIVE ROD END WORN. REPLACED ROD END ARM ASSEMBLY IAW DC-9 MM 32-10-0.

Part: BOLT — WORN (LT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND SECONDARY LINKAGE CLEVIS ON LEFT MAIN OUTBOARD GEAR DOOR DRIVE ROD WORN. REPLACED BOLT ON LINK ASSEMBLY IAW DC-9 MM 32-10-0.