N904AX

Part: BATTERY PACK — DEFECTIVE (EMERGENCY LIGHTS) · airframe 61,005 hrs · 48,255 cycles

EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK IAW DC9 AMM CHAPTER 33.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 59,981 hrs · 47,354 cycles

EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8-0001.

Part: ENGINE — DEFECTIVE (NR 1) · airframe 59,932 hrs · 47,319 cycles

LEFT OIL PRESSURE LOW ANNUNCIATOR CAME ON AFTER TAKEOFF. PRESSURE AND OIL QUANTITY BOTH QUICKLY WENT TO -0-. ENGINE POWER REDUCED TO IDLE AND THEN SHUTDOWN. EMERGENCY DECLARED FOLLOWED BY NORMAL LANDING. ENGINE RAN ABOUT 2 MINUTES AFTER OIL SYSTEM FAILURE. REPLACED NR 1 ENGINE IAW JC 9090010 REFERENCE WORK ORDER 600254026.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,724 hrs · 47,169 cycles

LEFT FORWARD MAIN FRAME FS 699 AFT FLANGE CRACKED AT POINTS F - E AND POINTS H - I. REQUIRED 5935650 REPAIR INSTALLED. REPLACED LEFT FORWARD MAIN FRAME FS 699 IAW DC9 JOB CARD EA53400321-001-2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 59,724 hrs · 47,169 cycles

LONGERON 30 CRACKED AT SPLICE FS 484-503. REMOVED DAMAGED LONGERON 30 AND REPLACED WITH NEW LONGERON FROM FS 417-590 IAW DC9 SRM 53-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,724 hrs · 47,169 cycles

FUSELAGE SKIN WAS CRACKED AT MAIN ENTRY DOOR STOP ON AFT SIDE OF DOOR CUTOUT FORTH FROM TOP. REPAIRED FUSELAGE SKIN IAW DC9 SRM.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 59,724 hrs · 47,169 cycles

PREVIOUS REPAIR FOUND AT BOTTOM AFT 2 DOOR STOPS OF FORWARD PASSENGER DOOR (REFER TO NEA53100033-001). REMOVED AND INSTALLED REPAIR IAW DWG SR09530252.

Part: KNOB — LOOSE (COCKPIT DOOR) · airframe 59,135 hrs · 46,717 cycles

COCKPIT DOOR LATCH MECHANISM INOP FROM OUTSIDE COCKPIT AND DOOR WAS DIFFICULT TO OPEN AND CLOSE. RESECURED SCREWS IN DOOR HANDLE OPERATES PROPERLY AT THIS TIME.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,233 hrs · 46,031 cycles

LEFT MAIN FRAME AT STA 718, CRACKED BEYOND LIMITS IN WHEEL WELL AREA AT PREVIOUS REPAIR. REMOVED AND REPLACED FRAME IAW DC-9 SRM.

Part: OIL TANK — CRACKED (NR 2 ENGINE) · airframe 57,870 hrs · 45,721 cycles

AIR DIVERSION, EMERGENCY DECLARED, IN FLIGHT SHUT DOWN. AIRCRAFT DIVERTED TO SHV AFTER DEPARTURE FROM SAT WITH REPORT OF OIL PRESSURE LOSS ON NR 2 ENGINE. ENGINE OIL QUANTITY DROPPED TO ZERO, OIL TEMPERATURE BEGAN TO CLIMB. OIL PRESSURE DROPPED TO 35 PSI. NR 2 ENGINE SHUTDOWN. AIR DIVERT TO SHV. FOUND CRACK IN OIL TANK ADJACENT TO OIL QUANTITY PROBE. REMOVED AND REPLACED OIL TANK IAW DC-9 MM 79-10-01-2-0001. REMOVED OIL SCREEN ELEMENTS AND INSPECTED FOR METAL AND FOREIGN MATTER, NONE FOUND. ACCOMPLISHED IAW P&W 72-00. PERFORMED ENGINE RUN IAW DC-9 MM 71-00-00-5-007. NO LEAKS NOTED. OPS CHECKED GOOD.

Part: FITTING — CRACKED (KEEL AREA) · airframe 56,901 hrs · 44,871 cycles

LONGERON END CRACKED, LEFT CANTED KEEL AREA, JUST AFT OF FORWARD "P" DOME, LONGERON 29 LEFT. REPLACED LONGERON 29 LEFT END CAP IAW DC-9 SRM 51-30-5.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,901 hrs · 44,871 cycles

CORROSION AROUND INTERCOSTAL NUTPLATES UPPER AND LOWER SURFACE, BETWEEN LONGERON 28 LEFT AND LONGERON 27 LEFT, F.S. 979 - 996. REPLACED INTERCOSTAL IAW DOUGLAS DRAWING 9915550 AND DC-9 SRM 51-30-2 AND 51-30-5.

Part: SUPPORT — CRACKED (AFT CARGO) · airframe 56,901 hrs · 44,871 cycles

FS 851 RIGHT VERTICAL FLOOR SUPPORT FITTING CRACKED. INSTALLED NEW STRUT SUPPORT IAW DC-9 SRM 51-30-5 AND 51-30-2.

Part: SUPPORT — CRACKED (CARGO DOORWAY) · airframe 56,901 hrs · 44,871 cycles

THE AFT LOWER CARGO DOOR JAMB, FORWARD LATCH PIN MOUNT WAS CRACKED. REPLACED THE FORWARD LATCH PIN SUPPORT IAW DC-9 SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,901 hrs · 44,871 cycles

FUSELAGE SKIN WAS CRACKED AT STA. 1096, BETWEEN LONGERON 2 LEFT AND LONGERON 3 LEFT. REPAIRED AREA IAW DC-9 SRM 53-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,817 hrs · 44,800 cycles

DURING PREDEPARTURE CHECK, EMERGENCY LIGHTS ON OVERHEAD PANEL WERE INOPERATIVE. REPLACED THE EMERGENCY POWER SUPPLY BATTERIES. OPS CHECKED GOOD IAW DC-9 MM 33-53-02-4-0001.

Part: FAN — BURNED OUT (E & E BAY) · airframe 56,680 hrs · 44,683 cycles

STRONG ELECTRICAL BURNING ODOR IN COCKPIT. RADIO RACK COOLING FAN FOUND TO BE SOURCE OF BURNING ODOR. REPLACED RADIO RACK COOLING FAN IAW MM. OPS CHECKED GOOD.

Part: COMPUTER — DEFECTIVE (ELEC. COMP.) · airframe 56,393 hrs · 44,484 cycles

DURING CLIMB THROUGH FL 180, AUTOPILOT GAVE AN UNCOMMANDED RIGHT RUDDER INPUT. AN UNCOMMANDED RIGHT RUDDER INPUT OCCURRED WITH AUTOPILOT DISENGAGED, USED MANUAL RUDDER WITH YAW DAMPER ON AND SERVO ON. REPLACED THE STABILITY AUGMENTATION COMPUTER IAW DC-9 MM 22-11-01-2.

Part: WINDOW — LACK OF LUBE (COCKPIT) · airframe 56,380 hrs · 44,472 cycles

FIRST OFFICER'S WINDOW WOULD NOT OPEN. INSPECTED, CLEANED AND LUBRICATED IAW DC-9 AMM 56-10-03. OPS CHECKED GOOD.

Part: ACCESS PANEL — MISSING (WINDOW RELEASE) · airframe 56,140 hrs · 44,301 cycles

AFTER TAKEOFF, LOUD WINDSTREAM NOISE FROM THE CAPTAIN'S SIDE OF AIRCRAFT. AIRCRAFT WOULD NOT PRESSURIZE. REINSTALLED THE CAPTAIN'S EMERGENCY WINDOW RELEASE ACCESS PANEL. PRESSURIZATION OPS CHECKED NORMAL IAW DC-9 MM.

Part: REGULATOR VALVE — STUCK (A/C BAY) · airframe 55,461 hrs · 43,815 cycles

CABIN PRESSURIZATION WOULD NOT HOLD 5.4 PSI AT FL250, WOULD NOT HOLD MAX DIFFERENTIAL. WITH ENGINE ANTI-ICE ON, WOULD NOT HOLD CABIN BELOW 10,000 FEET. PNEUMATIC PRESSURE GAUGE INDICATED 30 PSI IN CRUISE WITH PNEUMATIC CROSSFEEDS CLOSED. AFTER PRESSURE WAS BLEED OFF WITH AIRFOIL ANTI-ICE, THE 30 POUNDS OF PNEUMATIC PRESSURE RETURNED IN APPROXIMATELY 10 SECONDS. CREW DONNED THEIR OXYGEN MASKS DUE TO THE CONDITION. FOUND THE LEFT AIR CONDITIONING PRESSURE REGULATOR VALVE STUCK OPEN. REPLACED THE LEFT AIR CONDITIONING PRESSURE REGULATOR VALVE IAW DC-9 MM 21-31-01-2-0003.

Part: FRAME — CRACKED (CABIN) · airframe 55,409 hrs · 43,774 cycles

RIGHT SIDE FUSELAGE FRAME 617 WAS CRACKED ON THE FORWARD SIDE JUST UNDER FLOOR CUSP ON TOP ROW OF FASTENERS. REPAIRED AREA IAW REA D953-41707MR.

Part: BATTERY — DISCHARGED (FUSELAGE) · airframe 54,965 hrs · 43,485 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 33-53-00.

Part: BATTERY — DISCHARGED (FUSELAGE) · airframe 54,965 hrs · 43,485 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 33-53-00.

Part: BATTERY PACK — DISCHARGED (FUSELAGE) · airframe 54,941 hrs · 43,474 cycles

CABIN EMERGENCY LIGHTS WERE INOPERATIVE DURING PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW DC-9 MM 33-53-02.

Part: VANE — DELAMINATED (TE FLAP)

DURING D-CHECK, FOUND THE LEFT FLAP CENTER FIXED VANE DELAMINATED AT OUTBOARD END. REPLACED FIXED VANE IAW DC9 MM 27-51-3.

Part: CUSP — CRACKED (BS 218 - 237)

DURING D-CHECK, FOUND LEFT CUSP WEB CRACKED AT STATION 218. REPLACED CUSP WEB FROM STATION 218 TO 237 IAW DC9 SRM 51-30-2.

Part: VANE — DELAMINATED (TE FLAP)

DURING D-CHECK, FOUND THE RIGHT FLAP CENTER FIXED VANE DELAMINATED ON UPPER SURFACE. REPLACED FIXED VANE IAW DC9 MM 27-51-3.

Part: PANEL — CORRODED (LEFT WING)

DURING D-CHECK, FOUND BONDED PANEL AT INBOARD LOWER TRAILING EDGE OF LEFT WING CORRODED. REPLACED PANEL IAW DC9 SRM 51-30-2.

Part: VANE — DELAMINATED (RT TE FLAP)

DURING D-CHECK, FOUND RIGHT FLAP, INBOARD FIXED VANE DELAMINATED ON LOWER SURFACE. REPLACED FIXED VANE IAW DC9 MM 27-51-3.

Part: LONGERON — CORRODED (BS 945 - 980)

DURING D-CHECK, FOUND LONGERON 22 RIGHT CORRODED BETWEEN STATION 945 AND 980. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: ANGLE — CORRODED (LT MLG WW)

DURING D-CHECK, FOUND LEFT WHEEL WELL LATERAL CONTROL MIXER TOP ATTACH ANGLE CORRODED AT OUTBOARD TOP END. REPLACED ANGLE IAW DC9 SRM 51-20-0 AND 51-30-5.

Part: WEB — CRACKED (BS 813 - 832)

DURING D-CHECK, FOUND LEFT CUSP WEB CRACKED AT STATION 813 - 832. REPAIRED CUSP WEB IAW DC9 SRM 53-01.

Part: INTERCOSTAL — CORRODED (BS 980 - 996)

DURING D-CHECK, FOUND INTERCOSTAL BETWEEN STATIONS 980 - 996 AND LONGERONS N27 AND 28 LEFT CORRODED AROUND NUT PLATES. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FITTING — CRACKED (CARGO BAY)

DURING D-CHECK, FOUND FITTING BELOW FORWARD SPAR OF CENTER WING TANK AT LONGERON 24 LEFT CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-2.

Part: FITTING — CRACKED (CARGO BAY)

DURING D-CHECK, FOUND FITTING BELOW FORWARD SPAR OF CENTER WING TANK AT LONGERON 24 RIGHT CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-2.

Part: PANEL — DELAMINATED (SPOILER)

DURING D-CHECK, FOUND THE RIGHT OUTBOARD SPOILER PANEL DELAMINATED ON UPPER SURFACE. REPLACED SPOILER PANEL IAW DC9 SMM 27-61-01..

Part: WEB — CORRODED (BS 737)

DURING D-CHECK, FOUND THE UPPER PRESSURE PANEL IN THE LEFT WHEEL WELL STATION 737 BULGED AND CORRODED AROUND FASTENERS. REPLACED WEB IAW DC9 SRM 51-30-2, 51-30-1, 51-30-5.

Part: SKIN — CORRODED (LT WING)

DURING D-CHECK, FOUND CORROSION ON THE LEFT WING TRAILING EDGE INBOARD LOWER BONDED DOUBLER. REPLACED BONDED DOUBLER.

Part: FITTING — CRACKED (FUSELAGE)

DURING D-CHECK, FOUND FITTING AT FORWARD RIGHT CORNER OF KEEL WEB CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: PANEL — DELAMINATED (SPOILER)

DURING D-CHECK, FOUND LEFT OUTBOARD SPOILER PANEL DELAMINATED. REPLACED SPOILER PANEL IAW DC9 SMM 27-60-01.

Part: DOUBLER — CRACKED (BS 696)

DURING D-CHECK, FOUND KEEL WEB DOUBLER AT STATION 696 CRACKED. REPAIRED IAW DC9 SRM 53-01.

Part: FLOORBEAM — CRACKED (BS 737)

DURING D-DHECK, FOUND LEFT FLOORBEAM CRACKED AT STATION 737 OUTBOARD LOWER FLANGE. REPAIRED IAW ABX REA D953-34148-MR.

Part: CUSP — CRACKED (BS 617)

DURING D-CHECK, FOUND RIGHT CUSP WEB CRACKED AT STATION 617. REPAIRED CUSP WEB IAW DC9 SRM 53-01.

Part: PANEL — CORRODED (BS 744 - 754)

DURING D-CHECK, FOUND LEFT WHEEL WELL UPPER PRESSURE PANEL HEAVILY CORRODED BETWEEN STATION 744 TO 754 AND LBL 38-45. REPLACED UPPER PRESSURE PANEL IAW DC9 SRM 51-30-2, 51-30-1, 51-30-5, AND DACO DRAWING 9910155.

Part: BRACKET — CRACKED (EMERGENCY EXIT)

DURING C-CHECK, FOUND INTERIOR BRACKET IN LOWER LEFT CORNER OF THE RIGHT FORWARD EMERGENCY EXIT DOOR CRACKED. REPLACED BRACKET IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: FITTING — CRACKED (BS 579)

DURING D-CHECK, FOUND FLOOR SUPPORT FITTING AT STATION 579 AND LONGERON 23 LEFT CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: WEB — CRACKED (BS 614)

DURING D-CHECK, FOUND LEFT CUSP WEB CRACKED AT STATION 614. REPAIRED CUSP WEB IAW DC9 SRM 53-01.

Part: FLOOR — CORRODED (BS 140-160)

DURING D-CHECK, FOUND COCKPIT FLOOR PANEL CORRODED FROM STATION 140-160 AND RBL 10-48. REPLACED FLOOR PANEL IAW DC9 SRM 53-21-0.

Part: FITTING — CRACKED (BS 980)

DURING D-CHECK, FOUND LEFT VERTICAL SUPPORT FITTING CRACKED AT STATION 980. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: STIFFNER — CRACKED (AFT PRESS BLKHD)

DURING D-CHECK, FOUND AFT PRESSURE BULKHEAD, NR 2 RADIAL STIFFENER CRACKED. REPLACED STIFFENER IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FITTING — CRACKED (AFT LWR CARGO)

DURING D-CHECK, FOUND RIGHT VERTICAL SUPPORT FITING CRACKED IN TWO PLACES AT STATION 832. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-2.

Part: FITTING — CRACKED (AFT LOWER CARGO)

DURING D-CHECK, FOUND LEFT VERTICAL SUPPORT FITTING CRACKED AT STATION 794. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FITTING — CRACKED (FWD LWR CARGO)

DURING D-CHECK, FOUND RIGHT VERTICAL SUPPORT FITTING CRACKED AT STATION 332. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FITTING — CRACKED (BS 813)

DURING C-CHECK, FOUND RIGHT VERTICAL SUPPORT FITTING AT STATION 813 CRACKED IN TWO PLACES. REPLACED FITTING AW DC9 SRM 51-10-4 AND 51-30-5.

Part: FLOOR PANEL — CRACKED (COCKPIT)

DURING C-CHECK, FOUND COCKPIT FLOOR PANEL CRACKED AT STATION 132 AND RBL 4.0. REPLACED FLOOR PANEL IAW DC9 SRM 53-21-0 AND DACO DWG 9957827.

Part: FRAME — CRACKED (BS 1104)

DURING D-CHECK, FOUND CANTED FRAME AT STATION 1104 CRACKED AT LONGERONS 15, 16 AND 20 LEFT AND LONGERONS 5, 14 AND 18 RIGHT. REPLACED THREE FRAME SECTIONS IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FITTING — CRACKED (BS 869)

DURING C-CHECK, FOUND RIGHT VERTICAL SUPPORT FITTING CRACKED AT STATION 869. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FRAME — CRACKED (BS 1076)

DURING D-CHECK, FOUND FRAME CRACKED AT STATION 1076 AND LONGERON 19 RIGHT. REPLACED FRAME IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FRAME — CRACKED (BS 58)

DURING D-CHECK, FOUND FUSELAGE FRAME CRACKED AT STATION 58 AND 12 O'CLOCK POSITION. REPAIRED FRAME IAW DC9 SRM 53-03.

Part: FITTING — CORRODED (BS 913)

DURING D CHECK, FOUND VERTICAL FLOOR SUPPORT FITTING CORRODED AT STATION 813 AND LONGERON 23 RIGHT. REPLACED FITTING IAW DC9 SRM 51-30-2.

Part: FITTING — CRACKED (BS 484)

DURING D-CHECK, FOUND FLOOR SUPPORT FITTING CRACKED AT STATION 484 AND LONGERON 23 RIGHT. REPAIRED IAW DC9 SRM 51-30-2.

Part: SKIN — DELAMINATED (RT SPOILER)

DURING D-CHECK, FOUND RIGHT INBOARD GROUND SPOILER DELAMINATED ON UPPER SURFACE. REPAIRED SPOILER IAW DC9 SRM 51-70-2.

Part: FITTING — CRACKED (BS 484)

DURING D-CHECK, FOUND FLOOR SUPPORT FITTING CRACKED AT STATION 484 AND LONGERON 23 LEFT. REPLACED FITTING IAW DC9 SRM 51-30-2.

Part: FITTING — CRACKED (BS 889)

DURING C-CHECK, FOUND VERTICAL SUPPORT FITTING CRACKED, LEFT SIDE AT STATION 889. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FRAME — CRACKED (BS 794)

DURING C-CHECK, FOUND CABIN WINDOW RETAINER FRAME CRACKED AT STATION 794, AFT LOWER CORNER. REPAIRED IAW ABX REA D953-33951.

Part: FITTING — CRACKED (BS 794)

DURING C-CHECK, FOUND VERTICAL SUPPORT FITTING AT STATION 794 CRACKED ON THE RIGHT SIDE. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: BRACKET — CORRODED (COCKPIT)

DURING C-CHECK, FOUND FORWARD, INBOARD FOOT OF THE RUDDER PEDAL ASSEMBLY ATTACH BRACKET CORRODED. REPLACED BRACKET ASSEMBLY IAW DC9 MM 20-16-0.

Part: STIFFNER — CRACKED (NR 1 PYLON)

DURING C-CHECK, FOUND NR 1 PYLON INTERIOR WEB STIFFENER BETWEEN 8TH AND 13TH DUCT CRACKED AT END. REPLACED STIFFENER IAW DC9 SRM 54-10-0.

Part: ANGLE — CRACKED (LT TE FLAP)

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

Part: ANGLE — CRACKED (LTTE FLAP)

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

Part: FRAME — CRACKED (BS 579)

DURING C-CHECK, FOUND CABIN WINDOW RETAINER FRAME CRACKED AT STATION 579, FORWARD LOWER CORNER. REPAIRED IAW ABX REA D953-33951.

Part: FITTING — CRACKED (BS 867)

DURING C-CHECK, FOUND LEFT VERTICAL SUPPORT FITTING AT STATION 869 CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1.

Part: FRAME — CRACKED (BS 579)

DURING C-CHECK, FOUND RIGHT SIDEWALL FRAME FOOT CRACKED AT STATION 579 AND LONGERON 18 RIGHT. REPLACED FOOT IAW DC9 SRM 51-10-4 AND 51-30-2.

Part: SUPPORT — CRACKED (BS 237)

DURING C-CHECK, FOUND RIGHT FLOOR SUPPORT STRUT CRACKED AT STATION 237. REPLACED STRUT IAW DC9 SRM 51-30-5.

Part: FITTING — CRACKED (CARGO BAY)

DURING C-CHECK, FOUND INTERCOSTAL FITTING CRACKED IN UPPER AFT CORNER OF AFT LOWER CARGO DOOR. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: LONGERON — CRACKED (BS 982)

DURING C-CHECK, FOUND LONGERON 30 CRACKED AT STATION 982. REPAIRED IAW DC9 SRM 51-30-5.

Part: BRACKET — CRACKED (BS 756)

DURING D-CHECK, FOUND LEFT SIDEWALL WINDOW STIFFENER BRACKET CRACKED AT STATION 756. REPLACED BRACKET IAW DC9 SRM 51-30-5 AND DACO DWG 39141371.

Part: WEB — CORRODED (BS 160 - 218)

DURING D-CHECK, FOUND WIDESPREAD CORROSION ON THE UPPER CARGO COMPARTMENT SUB FLOOR MEMBRANE, FROM STATION 160 TO 218 AND LBL 54.5 AND RBL 54.5. REPLACED SUB FLOOR MEMBRANE IAW DC9 SRM 51-30-1.

Part: BULKHEAD — CORRODED (FUSELAGE)

DURING D-CHECK, FOUND THE FORWARD PRESSURE PANEL, LEFT FORWARD CORNER OF KEEL AREA FINGER DOUBLER CORRODED. REPLACED FINGER DOUBLER IAW DC9 SRM 51-30-2.

Part: FITTING — CORRODED (CARGO BAY)

DURING D-CHECK, FOUND FITTING JUST BELOW CENTER WING TANK FRONT SPAR IN FORWARD LOWER CARGO COMPARTMENT CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-5 AND 51-20-0.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING MAINTENANCE PREFLIGHT, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHTS POWER SUPPLY IAW DC9 MM, OPS CHECKED GOOD.

Part: BATTERIES — DISCHARGED (CABIN)

EMERGENCY EVACUATION LIGHTS WERE INOPERATIVE. REPLACED NICAD BATTERIES.

Part: WIRE — LOOSE (CABIN)

COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. CLEANED AND SECURED THE LOOSE/CORRODED GROUND STUD.

Part: BATTERY — DISCHARGED (CABIN)

CABIN EMERGENCY LIGHTS WOULD NOT TEST DURING PREFLIGHT. REPLACED EMERGENCY LIGHT BATTERY PACK.

Part: BULB — FAILED (COCKPIT)

COCKPIT OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. RELAMPED COCKPIT EMERGENCY LIGHTS. OPS CHECKED NORMAL.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, FOUND LONGERON 12R CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: PAN — CRACKED (LT MLG DOOR)

DURING C-CHECK, FOUND LEFT MAIN LANDING GEAR DOOR PAN CRACKED AT FORWARD SIDE. REPAIRED DOOR PAN IAW DC9 SRM 52-05.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, FOUND LONGERON 16R CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: WEB — CRACKED (CARGO COMPT)

DURING C-CHECK, FOUND CUSP WEB CRACKED AT STATION 920, 921, 925, 940, AND 945 AT RBL 54. REPAIRED CUSP WEB IAW DC9 SRM 51-30-13, 51-30-2 AND 51-30-5.

Part: SLANT PANEL — CORRODED (BS 690)

DURING C-CHECK, FOUND RIGHT SLANT PANEL STATION 690 CORRODED UNDER POTTED CAPS, AROUND THE FLOATING NUT-PLATES, BETWEEN RBL 22 AND RBL 44. REPLACED SLANT PANEL IAW DC9 SRM 51-30-2.

Part: LONGERON — CRACKED (BS 180)

DURING C-CHECK, FOUND LONGERON 3L CRACKED JUST AFT OF STATION 180. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, FOUND LONGERON 13L CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, FOUND LONGERON 13R CRACKED AT PYLON BULKHEAD AND STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: FITTING — CORRODED (BS 690)

DURING C-CHECK, FOUND RIGHT OUTBOARD T-FITTING BETWEEN FUSELAGE AND RIGHT SLANT PANEL CORRODED AT STATION 690. REPLACED T-FITTING IAW DC9 SRM 51-30-5.

Part: LONGERON — CRACKED (BS 160-197)

DURING C-CHECK, FOUND LONGERON 4L CRACKED AT STATION 160 AND 197. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: BULKHEAD SKIN — CRACKED (BS 996)

DURING ACCOMPLISHMENT OF DC9 SERVICE BULLETIN 53-A14, FOUND AFT PRESSURE BULKHEAD TEE CAP UPPER SKIN SPLICE CRACKED WITH SHEARED RIVETS AT FUSELAGE STATION 996. REPAIRED IAW DOUGLAS SERVICE REWORK DRAWING J060143 AND ABX REA D953-2250-MR.

Part: POWER SUPPLY — DEFECTIVE (COCKPIT)

DURING SERVICE CHECK, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW DC-9 MM.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHT BATTERIES.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN THE EMERGENCY LIGHT BATTERY PACK IAW DC-9 SUPP MM 33-51-0.

Part: BEAM — CRACKED (FWD SERV DOOR)

FOUND FWD SERVICE DOOR UPPER HINGE BEAM CRACKED, HOLD OPEN HOOK PAN CRACKED, SUPPORT ANGLE CRACKED. REPAIRED IAW DC9 SRM 51-30-5.

Part: LINK — NOT SECURED (RT COCKPIT)

FIRST OFFICERS CLEARVIEW WINDOW BROKEN. RESCURED AFT LOCK BAR, LOWER AFT LINKAGE ROD BY REPLACING THE RETAINING PIN. THE WINDOW WAS NOT BROKEN.

Part: RETAINER — CRACKED (BS 110)

DURING COMPLIANCE OF AD 90-18-03, FOUND THAT THE LEFT OVERHEAD WINDOW RETAINER WAS CRACKED. REPAIRED WINDOW RETAINER IAW ABX REA D956-13175-MR.

Part: BULB — FAILED (PILOTS MAP LIGHT)

CAPTAIN'S MAP LIGHT HEATED UP TO THE POINT THAT IT COULD NOT BE TOUCHED. THE PLASTIC HEATED AND CAUSED FUMES IN THE COCKPIT. REPLACED BULB AND OPERATED LIGHT FOR 30 MINUTES, NO FUMES OR EXCESS HEAT NOTED.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

DURING SERVICE CHECK, FOUND THE EMERGENCY LIGHTS INOP. REPLACED THE EMERGENCY LIGHTING BATTERY PACK. OPS CHECKED GOOD IAW DC-9 SUPP MM 33-54-0.

Part: BLKHD T CAP — CRACKED (BS 996)

DURING COMPLIANCE OF A.D. 89-06-04 AND 89-16-12; A.S.B. A53-231 AND A53-232, FOUND AFT PRESSURE BULKHEAD CRACKED AT LONGERON 16L. REPLACED T-CAP IAW DC-9 S.B. A53-231.

Part: WEB — CORRODED (FS 996)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH S.B. 53-241, FOUND LEVEL I CORROSION ON WEB AT LONGERONS 29L AND 27R, STA. 996. REPAIRED IAW ABX REA D953-10786-MR.

Part: ANGLE — CORRODED (FS 996)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH S.B. 53-241 FOUND LEVEL I CORROSION ON ANGLE FROM LONGERON 25R TO 27L, STA. 996. REPAIRED IAW ABX REA D953-10786-MR.

Part: WEB — CORRODED (BS 996)

DURING C-CHECK, INSPECTION WHILE COMPLYING WITH SB 53-241, FOUND LEVEL I CORROSION ON WEB AT LONGERONS 29L AND 27R, STA 996. REPAIRED IAW REA D953-10787-MR.

Part: INTERCOSTAL — DAMAGED (FS 446)

DURING C-CHECK INSPECTION FOUND INTERCOSTAL AT LONGERON 8L, STA. 446, ON AFT SIDE OF CARGO DOOR FRAME HAD A HOLE DRILLED IN RADIUS. REPAIRED IAW ABX REA D953-10779-MR.

Part: FRAME — GOUGED (FS 446)

DURING C-CHECK INSPECTION, FOUND FRAME STA 446 GOUGE BLEND OUT IN OUTSIDE RADIUS ADJACENT TO LONGERON 8L. REPAIRED GOUGE BLEND OUT PER ABX REA D953-10779-MR.

Part: BLKHD TEE — GOUGED (FS 965)

DURING C-CHECK INSPECTION, FOUND BULKHEAD STA 965 INBOARD T-CAP HAD GOUGES AND DRILL STARTS FROM LONGERON 18L TO 18R, FORWARD AND AFT EDGES. REPAIRED IAW DC-9 SRM 53-01 FIGURE 1 SHEET 3 AND ABX REA D953-10788-MR.

Part: SPOILER — CORRODED (LT WING)

DURING C-CHECK INSPECTION FOUND LEVEL II CORROSION, EXFOLIATION AND SEVERAL POPPED RIVETS ON THE SPOILER PANEL LOWER SURFACE. REPLACED SPOILER PANEL IAW DC-9 M.M. 27-62-1.

Part: FRAME — DAMAGED (FS 598)

DURING C-CHECK INSPECTION, FOUND HOLE IN FRAME 598 AT LONGERON 10L. REPAIRED FRAME IAW DC-9 SRM 51-30-2 AND ABX REA D953-10764-MR.

Part: TRAP PANEL — ELONGATED HOLES (FS 58)

WHILE COMPLYING WITH SB 57-129R4, FOUND HOLES IN THE LEFT TRAPEZOID PANEL COMMON TO VERTICAL ATTACH FITTING, OUT OF ROUND AND THE SECOND HOLE FROM BOTTOM STEPPED INSIDE. REPAIRED HOLES IAW DC-9 SRM 51-30-5. STEPPED HOLE REPAIRED IAW ABX REA D957-10786.

Part: DOOR JAMB — CORRODED (FS 917)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH SB 53-241, FOUND AFT LOWER CARGO DOOR JAMB WEB HAD LEVEL I CORROSION. REPAIRED IAW ABX REA D953-10762-MR.

Part: DOOR JAMB — CORRODED (FS 917)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH SB 53-241, FOUND AFT LOWER CARGO DOOR JAMB WEB HAD LEVEL I CORROSION. REPAIRED WEB IAW ABX REA D953-10762-MR.

Part: LINK — WORN (LT MLG DOOR)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR FLYING DOOR LINK HAD EXCESSIVE PLAY. REPLACED LINK ASSEMBLY IAW DC-9 MM 32-12-1.

Part: ROD ASSEMBLY — WORN (LT MLG DOOR)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR FLYING DOOR ROD ASSEMBLY HAD EXCESSIVE PLAY. REPLACED ROD ASSEMBLY IAW DC-9 MM 32-12-1.

Part: SKIN — CRACKED (FS 955)

DURING C-CHECK INSPECTION, FOUND THE FUSELAGE SKIN CRACKED AT STA'S 945 THROUGH 965, JUST BELOW LONGERON 14L. REPAIRED SKIN IAW ABX REA D953-10758-MR.

Part: FRAME — DAMAGED (FS 598)

DURING C-CHECK AND CORROSION INSPECTIONS, FOUND DRILL START IN EDGE OF FRAME 598 AT LONGERON 7R. REPAIRED IAW ABX REA D953-10764-MR, FIGURE 3.

Part: FRAME — DAMAGED (FS 598)

DURING C-CHECK AND CORROSION INSPECTIONS, FOUND FOUR DRILL STARTS IN FRAME 598 BETWEEN LONGERONS 8L AND 10L. REPAIRED PER ABX REA D953-10764-MR, FIGURE 1.

Part: SKIN — CRACKED (FS 990)

DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACKED AT STA 990 AND LONGERON 14R. REPAIRED IAW ABX REA D953-10771-MR.

Part: FRAME — DAMAGED (FS 737)

DURING C-CHECK AND CORROSION INSPECTIONS, FOUND PREVIOUS BLENDOUT ON FRAME STA 737. REPAIRED IAW ABX REA D953-10759-MR.

Part: ARM — WORN (RT MLG DOOR)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR FLYING DOOR ARM WORN. REPLACED ROD END IAW DC-9 MM 32-12-1.

Part: FRAME — DAMAGED (FS 756)

DURING C-CHECK INSPECTION, FOUND DRILL START IN FRAME 756 JUST ABOVE LONGERON 10R. REPAIRED IAW ABX REA D953-10729-MR.

Part: FRAME — DAMAGED (FS 617)

DURING C-CHECK INSPECTION, FOUND DRILL STARTS IN FRAME 617 BETWEEN LONGERONS 9L AND 10L. REPAIRED IAW ABX REA D953-10744-MR.

Part: WEB — DENTED (FS 996)

DURING C-CHECK INSPECTION, FOUND DENT IN LEFT P-DOME SKIN AT APPROXIMATELY THE 10:00 O'CLOCK POSITION. REPAIRED DENT IAW ABX REA D953-10728-MR.

Part: ANGLE — FAILED (FS 1087)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 89-08-10 AND S.B.'S A53-154 AND A53-223, FOUND RIGHT DORSAL FIN ATTACH ANGLE BUCKLED AND FASTENERS PULLED. REPLACED RIGHT DORSAL FIN ATTACH ANGLE IAW DC-9 SRM 53-05, FIGURE 23 AND SB'S A53-154 AND A53-223.

Part: WEB — DAMAGED (FS 996)

DURING C-CHECK, INSPECTION FOUND DRILL STARTS IN LEFT P-DOME SKIN WEB. REPAIRED IAW ABX REA D953-10713-MR.

Part: WEB — DENTED (FS 996)

DURING C-CHECK INSPECTION, FOUND P-DOME DENTED AT APPROXIMATELY THE 2:00 O'CLOCK POSITION. REPAIRED DENT IAW ABX REA D953-10735-MR.

Part: FRAME — DAMAGED (FS 658)

DURING C-CHECK INSPECTION, FOUND DRILL START ON FRAME 658 AT LONGERON 7L. REPAIRED IAW ABX REA D953-10731-MR.

Part: WEB — DENTED (FS 996)

DURING C-CHECK INSPECTION, FOUND P-DOME DENTED AT APPROXIMATELY THE 12:30 O'CLOCK POSITION. REPAIRED DENT IAW ABX REA D953-10735-MR.

Part: WEB — DENTED (FS 996)

DURING C-CHECK INSPECTION, FOUND TWO DENTS IN RIGHT P-DOME SKIN BETWEEN THE 2:00 AND 3:00 O'CLOCK POSITIONS. REPAIRED DENTS IAW ABX REA D95310735-MR.

Part: ANGLE — DEFECTIVE (FS 1087)

DURING C-CHECK INSPECTION WHILE COMPYING WITH AD 89-08-10 AND S.B.'S A53-154 AND A53-223, FOUND LEFT DORSAL FIN ATTACH ANGLE HAD ONE FASTENER HEAD MISSING AND SEVERAL FASTENERS NOT PORPERLY SEATED. REPLACED FASTENERS IAW DC-9 SRM 51-30-1 AND 51-30-5.