N909AX

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,720 hrs · 66,617 cycles

WHILE COMPLYING WITH EA 53300036, FOUND CRACKED FRAME, REF AD 2002-21-09. REPLACED FRAME IAW DC9 SRM 51-30-02 AND 51-30-05.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 49,720 hrs · 66,617 cycles

WHILE COMPLYING WITH EA 53300036, FOUND CRACKED BRACKET, REF AD 2002-21-09. REPLACED BRACKET IAW DC9 SRM 51-30-02 AND 51-30-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,720 hrs · 66,617 cycles

WHILE COMPLYING WITH EA 53300036, FOUND CRACKED FRAME, REF AD 2002-21-09. REPAIRED AREA IAW DC9 SRM 5303 FIG 34.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,720 hrs · 66,617 cycles

WHILE COMPLYING WITH EA 53300036, FOUND CRACKED CLIP FOR INTERCOSTAL, REF AD 2002-21-09. FABRICATED AND INSTALLED NEW CLIP IAW DWG 9957899 AND DC9 SRM 51-30-05.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 49,720 hrs · 66,617 cycles

WHILE COMPLYING WITH EA 53300036, FOUND CRACKED ANGLE, REF AD 2002-21-09. REPLACED ANGLE IAW DC9 SRM 51-30-05.

Part: FITTING — CRACKED (FUSELAGE) · airframe 49,720 hrs · 66,617 cycles

WHILE COMPLYING WITH EA 53300036, FOUND CRACKED INTERCOSTAL CLIP, REF AD 2002-21-09. FABRICATED AND INSTALLED IAW DWG 9957899 AND DC9 SRM 51-30-5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,720 hrs · 66,617 cycles

WHILE COMPLYING WITH EA 53300036, FOUND CENTER FRAME CRACKED AT BOTH ENDS, REF AD 2002-21-09. REPAIRED BOTH ENDS OF FRAME IAW DC9 SRM 53-03 FIG 34. TWO CRACKS: .75 INCH AND .86 INCH.

Part: ATTACH BRACKET — CORRODED (CARGO BAY) · airframe 49,663 hrs · 66,563 cycles

FORWARD LOWER CARGO ATTACH BRACKETS CORRODED AT NUT PLATES - STA 389 AND 408, LEFT BUTT LINE 33. REMOVED CORROSION AT STA 389 AND 408, LEFT BUTT LINE 33 IAW DC9 SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 49,663 hrs · 66,563 cycles

FLOOR TRACK CRACKED AND CORRODED AT STA 389, LEFT BUTT LINE 44. REPAIRED TRACK IAW DC9 SRM.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 49,663 hrs · 66,563 cycles

FUSELAGE FRAME UPPER ATTACH BRACKET CRACKED AT LEFT BUTT LINE 54, APPROXIMATELY FS 412. REMOVED AND REPLACED FITTING IAW DC9 REA D953-55887-MR.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 49,663 hrs · 66,563 cycles

INTERCOSTAL AT 28 RIGHT WAS CRACKED AROUND BOLT HOLE AT FS 596. REPAIRED INTERCOSTAL IAW DC9 SSRM DWG K05159.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 49,663 hrs · 66,563 cycles

INTERCOSTAL CRACKED IN CEILING STRUCTURE AT FL 256, LEFT BUTT LINE 22. REPAIRED INTERCOSTAL IAW DC9 SSRM DWG K05159.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 49,663 hrs · 66,563 cycles

LEFT CUSP WEB AT STA 960 CRACKED AT LIGHTNING HOLE. REPAIRED AREA IAW DC9 SRM 53-01.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 49,663 hrs · 66,563 cycles

RIGHT CUSP WEB AT STA 943 - 965 CRACKED AT 4 PLACES. REPAIRED CUSP WEB IAW DC9 SRM 53-01.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 49,663 hrs · 66,563 cycles

LEFT WING AFT SPAR HAD CRACKED VERTICAL SUPPORT BRACKET NEAR INBOARD SPOILER ACTUATOR. REPLACED BRACKET IAW DC9 SRM.

Part: MOUNT — CRACKED (AFT CARGO DOOR) · airframe 49,663 hrs · 66,563 cycles

UPPER STOP MOUNT ON AFT LOWER CARGO DOOR FORWARD FLANGE WAS CRACKED. REMOVED AFT LOWER CARGO DOOR. REPLACED HINGE. REINSTALLED DOOR AND TESTED DOOR WARNING IAW DC9 MM 51-31-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 49,341 hrs · 66,250 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,748 hrs · 65,615 cycles

DURING PREDEPARTURE CHECK FOUND COCKPIT EMERGENCY LIGHTS WOULD NOT TEST. DEFERRED NR 47327 REMOVED AND REPLACED BATTERIES IN PACK IAW AMM.OPS CHECKED GOOD. DEFERRED IAW GMM. ITEM 2 A12 FOR BATTERY PACK REPLACEMENT WITHIN 3 FLIGHT DAYS. PLACARD INSTALLED, CODE 2 CLEAR, NR 47327 REPLACED EMERGENCY POWER BATTERY PACK ASSY. REF AMM 33-53-00. OPS CHECKED GOOD, PLACARD REMOVED.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 48,410 hrs · 65,296 cycles

OUTBOARD SEAT TRACK AT FS 579 LEFT BLOWN AT SPLICE. REMOVED AND REPLACED LEFT OUTBOARD SEAT TRACK FS 579 - 560.

Part: SUPPORT ANGLE — CRACKED (BS 660) · airframe 48,410 hrs · 65,296 cycles

CENTER TANK UPPER SUPPORT ANGLE WAS CRACKED AT STA 660, LEFT BUTT LINE 42. REMOVED AND REPLACED SUPPORT ANGLE IAW DC-9 SRM.

Part: SHEAR TIE — CRACKED (CENTER WING) · airframe 48,410 hrs · 65,296 cycles

RIGHT XCW "0" STRINGER 17 - 18, HAD CRACKED SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIPS IAW DC-9 SRM.

Part: SHEAR TIE — CRACKED (CENTER WING) · airframe 48,410 hrs · 65,296 cycles

RIGHT XCW 23 STRINGER 15 - 16, HAD CRACKED SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIP IAW DC-9 SRM.

Part: OUTFLOW VALVE — CORRODED (CABIN PRESSURE) · airframe 48,410 hrs · 65,296 cycles

CORROSION AROUND FASTENERS ON SUGAR SCOOP BETWEEN STA 945 - 965. REMOVED AND REPLACED OUTFLOW VALVE NOZZLE VALVE IAW DC-9 MM 21-32-05-4-0002.

Part: PAN — CRACKED (FWD CARGO DOOR) · airframe 48,410 hrs · 65,296 cycles

CRACK IN OUTER PAN AT FASTENER AFT EDGE STOP NR 3. REPAIRED CRACK IAW DC-9 SRM 52-03.

Part: INTERCOSTAL — CRACKED (FWD CARGO) · airframe 48,410 hrs · 65,296 cycles

INTERCOSTAL CRACKED BETWEEN STA 484 AND 503 AT LONGERON 30 FORWARD LOWER CARGO. REPAIRED AREA IAW DWG K05159 AND DC-9 SRM 51-30-5.

Part: ATTACH BRACKET — CRACKED (LT FLAP HINGE) · airframe 48,410 hrs · 65,296 cycles

LEFT INBOARD FLAP HINGE ATTACH BRACKET CRACKED IN TWO PLACES INSIDE FLAP. MOVED AND REPLACED LEFT INBOARD FLAP HINGE ATTACH BRACKET IAW DC-9 DWG 5914872.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 48,410 hrs · 65,296 cycles

LONGERON 20 LT AFT OF TRAP PANEL FITTING CRACKED. REMOVED AND REPLACED LONGERON 20 LT IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: SKIN — CORRODED (RT AILERON) · airframe 48,410 hrs · 65,296 cycles

SEVERAL AREAS OF CORROSION (BULGING SKIN) EVIDENT ON BOTTOM SKIN OF RIGHT AILERON. REPAIRED AREA IAW DC-9 SRM.

Part: ENGINE — STALLED (LEFT) · airframe 47,815 hrs · 64,735 cycles

LEFT ENGINE COMP STALLED AND STARTED TO VIBRATE. PULLED THROTTLE BACK TO IDLE AND DIVERTED TO BDL. REMOVED AND REPLACED NR 1 ENGINE IAW DC-9 AMM 72 AND ABX JOB CARDS. OPS CHECKED GOOD.

Part: PLATE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 47,314 hrs · 64,298 cycles

HORIZONTAL STABILIZER REMOVABLE STRESS PLATE HAD LEVEL II CORROSION, PITTING, ON EXTERIOR SURFACE AND LOWER LIP. REPAIRED AREA IAW DC-9 JOB CARD 9341004, AND DC-9 SRM.

Part: ATTACH FITTING — CRACKED (INTERCOSTAL) · airframe 47,314 hrs · 64,298 cycles

CRACKED FITTING ON INTERCOSTAL STA. 996, BETWEEN LONGERON 28 - 27 RT. REPLACED FITTING IAW DC-9 SRM 51-30-5.

Part: DOUBLER — CRACKED (CABIN) · airframe 47,314 hrs · 64,298 cycles

WINDOW INTERIOR DOUBLER CRACKED FORWARD LOWER CORNER, F.S. 579 RIGHT. REPAIRED DOUBLER IAW DC-9 SRM AND DWG K05159.

Part: FITTING — CRACKED (LONGERON) · airframe 47,314 hrs · 64,298 cycles

CRACKED LONGERON END FITTING STA. 756, LONGERON 29 LEFT. REPLACED LONGERON 29 LEFT END FITTING IAW DC-9 SRM.

Part: ATTACH FITTING — CRACKED (CARGO TRACK) · airframe 47,314 hrs · 64,298 cycles

CRACKED ATTACH FITTING STA. 980, BETWEEN LONGERON 28 - 27 RT. REPLACED ATTACH FITTING IAW DC-9 SRM 51-30-5.

Part: ANNUNCIATOR — DEFECTIVE (COCKPIT) · airframe 46,817 hrs · 63,811 cycles

BEFORE TAKE-OFF, ELECTRICAL BURNING ODOR AND SMOKE IN COCKPIT APPEARED. VERIFIED PROBLEM, FOUND WATER INTRUSION IN LEFT FLIGHT DIRECTOR MODE ANNUNCIATOR ASSEMBLY. REMOVED AND REPLACED CAPTAIN'S FLIGHT DIRECTOR MODE ANNUNCIATOR. OPS CHECKED GOOD IAW DC-9 MM 34-25-00.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,193 hrs · 63,188 cycles

UPPER CARGO DOOR, UPPER FORWARD CORNER STRUCTURE CRACKED INSIDE FUSELAGE. INSTALLED REPAIR DOUBLER ON UPPER CARGO DOOR, UPPER FORWARD CORNER DOOR PAN STRUCTURE IAW DC-9 SRM 51-30-5 AND 53-01.

Part: FITTING — CRACKED (LT MLG WW) · airframe 46,193 hrs · 63,188 cycles

KEEL FITTING IN LEFT WHEEL WELL, FORWARD OF INBOARD GEAR DOOR ACTUATOR CRACKED AT TOP CENTER AT WING ATTACH POINT. STOP DRILLED CRACK IAW DC-9 SRM 51-10-4. REPAIRED KEEL FITTING IAW DC-9 SRM 53-03.

Part: LONGERON — CRACKED (CARGO BAY) · airframe 46,193 hrs · 63,188 cycles

LONGERON 2 LEFT CRACKED AT STATION 1076. REPLACED LONGERON SECTION IAW DC-9 SRM.

Part: LONGERON — CRACKED (CARGO BAY) · airframe 46,193 hrs · 63,188 cycles

LONGERON 2 RIGHT CRACKED AT STATION 1076. REPLACED CRACKED SECTION OF LONGERON IAW DC-9 SRM 53-11-4, 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (CABIN) · airframe 46,193 hrs · 63,188 cycles

LONGERON 17 LEFT AT STATION 965 WAS CRACKED. REPLACED LONGERON 17 LEFT FROM STATION 958 TO STATION 996 IAW DC-9 SRM 53-02.

Part: LONGERON — CRACKED (CABIN) · airframe 46,193 hrs · 63,188 cycles

LONGERON 13 LEFT AT STATION 965 WAS CRACKED. REPAIRED LONGERON 13 LEFT FROM STATION 956 TO STATION 996 IAW DC-9 SRM 53-02.

Part: SPAR CAP — CORRODED (HORIZONTAL STAB) · airframe 46,193 hrs · 63,188 cycles

LEVEL 1 CORROSION INSIDE OF HORIZONTAL STABILIZER ON INSIDE OF FRONT SPAR, TOP CAP, BETWEEN TWO FASTENERS AT APPROXIMATELY STATION XFS 163.3. REPAIRED HORIZONTAL STABILIZER FRONT SPAR TOP CAP IAW REA D955-43008MR.

Part: FITTING — CRACKED (AFT CARGO) · airframe 46,193 hrs · 63,188 cycles

AFT LOWER CARGO DOOR #1 BEAM AFT END FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: FRAME — CRACKED (CABIN) · airframe 46,193 hrs · 63,188 cycles

FRAME AT STATION 408 WAS CRACKED AT LONGERON ATTACHMENT 17 RIGHT. REPAIRED FRAME AT STA. 408 IAW DC-9 SRM 53-03.

Part: DOOR — CRACKED (MLG) · airframe 46,193 hrs · 63,188 cycles

INBOARD MAIN LANDING GEAR DOOR CRACKED JUST BELOW ACTUATOR ATTACH FITTING. REMOVED AND REPLACED DOOR IAW DC-9 SRM 51-30-5 AND 51-30-7. REPAIRED INNER CRACKED SKIN IAW REA D952-42986. REINSTALLED DOOR ASSEMBLY IAW DC-9 MM 32-1-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,193 hrs · 63,188 cycles

MAIN ENTRY DOOR STAIR CUTOUT HAD CRACK AT LOWER AFT CORNER. REPAIRED LOWER AFT CORNER OF AIRSTAIR CUTOUT IAW DC-9 SRM 53-94.

Part: BATTERY — DISCHARGED (CABIN) · airframe 46,104 hrs · 63,105 cycles

ON SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC-9 AMM 33-53-00-8-0001.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 46,034 hrs · 63,042 cycles

EMERGENCY LIGHTS IN FLIGHT COMPARTMENT INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERIES IAW DC-9 AMM 33-53-00-4-0109. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 45,746 hrs · 62,779 cycles

EMERGENCY LIGHTS INOP, WOULD NOT TEST. REPLACED EMERGENCY BATTERIES AND BATTERY PACK IAW DC-9 MM 33-53-00.

Part: DOOR — OPEN (NLG) · airframe 45,477 hrs · 62,485 cycles

VIBRATIONS WERE NOTED FROM THE NOSE OF THE AIRCRAFT AFTER LANDING GEAR RETRACTION. CREW RECYCLED THE LANDING GEAR, VIBRATION RETURNED UPON RETRACTION. THE AIRCRAFT RETURNED TO THE FIELD. THE RIGHT NOSE LANDING GEAR DOOR WAS NOTED TO BE OPEN DURING THE TAXI IN. MAINTENANCE INSPECTED CLEANED AND LUBRICATED THE NOSE LANDING GEAR RETRACT ASSY AND NOSE LANDING GEAR DOOR LATCH, IAW DC-9 MM 32-31-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 45,259 hrs · 62,275 cycles

EMERGENCY LIGHTS VERY DIM. REPLACED EMERGENCY LIGHTS BATTERIES. OPS CHECKED GOOD.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 45,008 hrs · 62,010 cycles

DURING C-CHECK, FOUND HORIZONTAL STAB CENTER SECTION ATTACH POINT FITTING CORRODED. REPLACED ATTACH FITTING IAW DC9 SRM 51-30-5.

Part: FITTING — CRACKED (CARGO BAY) · airframe 45,008 hrs · 62,010 cycles

DURING ''''C'''' CHECK, FOUND FLOORBEAM STRUT FITTING CRACKED AT STATION 851 AND LONGERON 23 LEFT. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,008 hrs · 62,010 cycles

DURING ''C'' CHECK, FOUND FUSELAGE SKIN CRACKED AT RIGHT NOSE LANDING GEAR AFT DOOR. REPAIRED FUSELAGE SKIN IAW DC9 SRM 53-05.

Part: PAN — CRACKED (CARGO DOOR) · airframe 45,008 hrs · 62,010 cycles

DURING ''C'' CHECK, FOUND AFT LOWER CARGO DOOR PAN CRACKED AT PREVIOUS REPAIR. REPAIRED CARGO DOOR PAN IAW REA D952-36742-MR.

Part: INTERCOSTAL — CORRODED (CARGO BAY) · airframe 45,008 hrs · 62,010 cycles

DURING ''C'' CHECK, FOUND CORROSION ON FLOORBEAM INTERCOSTAL AT STAION 984 AND RBL 30 RIGHT. REPAIRED IAW DC9 SRM DRAWING K05159.

Part: FITTING — CRACKED (FUSELAGE) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND FLOORBEAM STRUT FITTING CRACKED AT STATION 851 RIGHT AND LONGERON 23 RIGHT. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND WINDOW FRAME CRACKED AT STATION 699. REPAIRED IAW ABX DWG K05159.

Part: SKIN — CRACKED (RT WING) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND LOWER SURFACE OF WING TIP CRACKED AT STATION XW561. WELDEDWING TIP IAW ABX DWG K05818.

Part: FRAME — CRACKED (CARGO BAY) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND LEFT WINDOW FRAME CRACKED AT STATION 737. REPAIRED IAW DC9 SRM DWG K05159.

Part: CAP — CRACKED (HORIZONTAL STAB) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND LEFT HORIZONTAL STABILIZER CAP CRACKED OUTBOARD OF ELEVATOR CONTROL VALVE. REPLACED CAP IAW DC9 SRM 51-30-5.

Part: LONGERON — CRACKED (CARGO BAY) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND LONGERON 12 RIGHT CRACKED AT STATION 965. REPLACED LONGERON SECTION IAW DC9 SRM 51-30-2.

Part: FITTING — CRACKED (CARGO BAY) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND FLOORBEAM STRUT CRACKED AT LONGERON 23 AND STATION 773. REPLACED STRUT FITTING IAW DC9 SRM 51-30-5.

Part: PAN — CRACKED (CARGO DOOR) · airframe 45,008 hrs · 2,126 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND FLOORBEAM STRUT CRACKED AT LONGERON 23 LEFT AT STATION 945. REPLACED STRUT FITTING IAW DC9 SRM 51-30-5.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND CUSP WEB CORRODED AND CRACKED AT STRINGER 18 RIGHT AND STATION 313. REPLACED CUSP WEB IAW DC9 SRM 51-30-1 AND 51-30-2.

Part: PAN — CRACKED (CARGO BAY DOOR) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND AFT LOWER CARGO DOOR INNER PAN CRACKED. REPAIRED DOOR IAW DC9 SRM 52-05.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 45,005 hrs · 2,126 cycles

DURING C-CHECK, FOUND LONGERON 13 LEFT CRACKED AT STATION 965. REPLACED LONGERON SECTION IAW DC9 SRM 51-30-05.

Part: FITTING — CRACKED (AFT CARGO BAY) · airframe 45,005 hrs · 2,126 cycles

DURING C-CHECK, FOUND FLOOR SUPPORT FITTING CRACKED AT LONGERON 23 RIGHT AND STATION 851. REPLACED FITTING IAW DC9 SRM 51-30-2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND LONGERON 16 RIGHT CRACKED AT STATION 945. REPLACED LONGERONSECTION IAW DC9 SRM 51-30-2.

Part: FRAME — CRACKED (WINDOW FRAME) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK FOUND RIGHT WINDOW FRAME CRACKED AT STATION 639. REPLACED WINDOWFRAME IAW DC9 SRM 51-30-5.

Part: FITTING — CRACKED (CARGO BAY) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND FLOORBEAM STRUT FITTING CRACKED AT STATION 851 AND LONGERON 23 LEFT. REPLACED STRUT FITTING IAW DC9 SRM 51-30-5 AND 51-30-2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND LONGERON 2 LEFT CRACKED AT STATION 200. REPLACED LONGERON SECTION IAW DC9 SRM 51-30-5.

Part: FRAME — CRACKED (CENTER WING) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND LONGERON 26 LT WEB CRACKED AT STATION 639. REPLACED WEB IAW DC9 SRM 53-03.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND WINDOW FRAME CRACKED. REPAIRED WINDOW FRAME IAW SRM DWG K05159.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND AFT LOWER CARGO DOOR NR 1 BEAM CRACKED. REPAIRED IAW DC9 SRM52-01.

Part: FITTING — CRACKED (CARGO BAY) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND FLOORBEAM STRUT FITTING CRACKED AT STATION 984 AND STRINGER 23 RIGHT. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: FITTING — CRACKED (CARGO BAY) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND FLOORBEAM STRUT CRACKED AT STATION 870 AND STRINGER 23 RIGHT. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: FITTING — CRACKED (CARGO BAY) · airframe 45,008 hrs · 2,126 cycles

DURING C-CHECK, FOUND FLOORBEAM STRUT FITTING CRACKED AT STATION 794 STRINGER23 RIGHT. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: ANGLE — CRACKED (RT TE FLAP)

DURING C-CHECK, FOUND OUTBOARD ATTACH ANGLE FOR RIGHT FLAP OUTBOARD HINGE CRACKED. REPLACED OUTBOARD SUPPORT ANGLE AND FORMER IAW DC9 SRM 51-30-1 AND 51-30-2.

Part: PANEL — DELAMINATED (LT WING)

DURING C-CHECK, FOUND LEFT WING UPPER OUTBOARD BONDED PANEL, FORWARD OF AILERON, DELAMINATED. REPLACED LEFT WING UPPER OUTBOARD BONDED PANEL IAW DC9 SRM 51-30-1, 51-30-2, AND 51-10-4.

Part: FITTING — CORRODED (CARGO DOOR)

DURING C-CHECK, FOUND CARGO DOOR NR 6 SPOOL FITTING ASSY PITTED. REMOVED CORROSION IAW SRM 53-05.

Part: FITTING — CORRODED (CARGO DOOR)

DURING C-CHECK, FOUND CARGO DOOR NR 2 SPOOL FITTING ASSY PITTED. REMOVED CORROSION IAW SRM 53-05.

Part: VANE — DELAMINATED (RT TE FLAP)

DURING C-CHECK, FOUND RIGHT CENTER FIXED VANE DELAMINATED. REPLACED FIXED VANE IAW DC9 MM 27-51-14.

Part: FITTING — CORRODED (CARGO DOOR)

DURING C-CHECK, FOUND CARGO DOOR NR 5 SPOOL FITTING ASSY PITTED. REMOVED CORROSION IAW SRM 53-05.

Part: FRAME — CRACKED (BS 980)

DURING C-CHECK, FOUND FRAME CRACKED AT LONGERON 17 RIGHT FS 980. REPAIRED FRAME IAW DC9 SRM 53-03.

Part: SKIN — CRACKED (BS 69.5)

DURING C-CHECK, FOUND NOSE SKIN CRACKED AT FS 69.5 LONGERON 15 LEFT. REPAIRED IAW EA 53100074-003-3.

Part: TRAP PANEL — CRACKED (LT WING)

DURING C-CHECK, FOUND LEFT FORWARD UPPER HORIZONTAL TRAPEZOIDAL PANEL CRACKED PAST 4TH HOLE. REPAIRED HORIZONTAL TRAPEZOIDAL PANEL IAW DC9 SRM 57-09.

Part: BULKHEAD TEE — CORROSION (BS 756)

DURING C-CHECK, FOUND CORROSION ON UPPER SURFACE OF THE FORWARD LEG OF THE TEE-ANGLE AT STATION 756 BL O.O. REPAIRED BULKHEAD TEE-ANGLE IAW REA D953-24842-MR.

Part: FITTING — CORRODED (CARGO DOOR)

DURING C-CHECK, FOUND CARGO DOOR NR 4 SPOOL FITTING ASSY PITTED. REMOVED CORROSION IAW SRM 53-05.

Part: SLAT — CRACKED (RT WING)

DURING C-CHECK, FOUND FITTING CRACKED AT PIVOT POINT ON RT/OUTBOARD SLAT ASSY. REPAIRED UNIT IAW DC-9 SRM.

Part: BATTERIES — DISCHARGED (CABIN)

EMERGENCY LIGHTS WERE DIM. REPLACED EMERGENCY LIGHT BATTERIES.

Part: RETRACT MECH — LACK OF LUBE (NLG)

WHEN GEAR SELECTED DOWN, MAIN GEAR CAME DOWN AND LOCKED. GEAR DOORS CYCLED NORMALLY. NOSE GEAR WOULD NOT COME DOWN, NO NOSE GEAR INDICATION AT ALL. RECYCLED GEAR, SAME RESULT. COMPLIED WITH ABNORMAL PROCEDURES, FREE FELL NOSE LANDING GEAR. GEAR CAME DOWN AND LOCKED. MAIN LANDING GEAR CYCLED NORMALLY. LUBRICATED NOSE LANDING GEAR MECHANISM AND PERFORMED GEAR SWING WITH AND WITHOUT GEAR DOORS HOOKED UP. NO DEFECTS NOTED.

Part: LINK ASSY — DEFECTIVE (NLG DOOR)

IN CRUISE AT FL 350, NOSE GEAR DOOR CAME OPEN. REPLACED LEFT NOSE LANDING GEAR DOOR LINK ASSY S/N DEC 1218. REPLACED RIGHT NOSE LANDING GEAR DOOR LINK ASSY S/N HGF 339.

Part: PANEL — CRACKED (LT MLG WW)

DURING C-CHECK, THE LEFT WHEEL WELL PRESSURE PANEL AT STA 83 WAS FOUND CRACKED. THE PANEL WAS REPAIRED IAW REA D953-18295-MR.

Part: TRUNNION FTTING — CRACKED (RT MLG)

DURING C-CHECK, THE AUX LANDING GEAR RT TRUNNION FITTING WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM.

Part: FITTING — CRACKED (BS 465)

DURING C-CHECK, THE FLOORBEAM TO FRAME FITTING AT STA 465 LONG 181 WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM 51-30-5.

Part: ANGLE — CRACKED (BS 1076)

DURING C-CHECK, THE FRAME ATTACH ANGLE AT STA 1076 LONG 17 LT WAS FOUND CRACKED. THE ANGLE WAS REPLACED IAW DC9 SRM 51-30-1.

Part: LONGERON — CORRODED (BS 1089)

DURING C-CHECK, THE LONGERON AT STA 1089 AT LONG 7 LT WAS FOUND CORRODED. THE LONGERON WAS REPLACED IAW DC9 SRM 53-02, FIGURE 2.

Part: FITTING — CRACKED (BS 917)

DURING C-CHECK, THE FLOORBEAM SUPPORT FITTING AT STA 917 LONG 241 WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM 51-30-5.

Part: FITTING — CRACKED (BS 389)

DURING C-CHECK, THE FRAME TO FLOORBEAM ATTACH FITTING AT STA 389 LONG 18 LT WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM 51-30-1.

Part: PANEL — DELAMINATED (RT WING)

DURING C-CHECK, THE RT WING INBOARD UPPER BONDED PANEL WAS FOUND DELAMINATED. THE PANEL WAS REPLACED IAW DC9 SRM 51-30-1.

Part: VANE — DELAMINATED (RT TE FLAP)

FLAP VANE IS DELAMINATED AND WATER LOGGED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, THE LONGERON AT STA 965 AT LONG 17 RT WAS FOUND CRACKED. THE LONGERON WAS REPLACED IAW DC9 SRM 53-02, FIGURE 4.

Part: SEAT TRACK — DAMAGED (BS 313)

DURING C-CHECK, THE SEAT TRACK AT STA 313 RBL 40 WAS FOUND DAMAGED. THE SEAT TRACK WAS REPLACED IAW DC9 SRM 51-30-1.

Part: DOUBLER — CRACKED (NR 2 PYLON)

DURING C-CHECK, THE PYLON ANGLE DOUBLER JUST AFT OF THER 13TH STAGE BLEED DUCT WAS FOUND CRACKED. THE DOUBLER WAS REPLACED IAW DC9 SRM 51-30-5.

Part: SEAT TRACK — CORRODED (BS 176-218)

DURING C-CHECK, THE SEAT TRACK AT STA 176 TO 218 RBL 40 WAS FOUND CORRODED. THE SEAT TRACK WAS REPLACED IAW DC9 SRM 51-30-1.

Part: LONGERON — CORRODED (BS 1089)

DURING C-CHECK, THE LONGERON AT STA 1089 AT LONG 9 LT WAS FOUND CORRODED. THE LONGERON WAS REPLACED IAW DC9 SRM 51-30-2.

Part: BRACKET — CRACKED (LT ENTRY DOOR)

DURING COMPLIANCE OF AD 92-22-08, FOUND LEFT MAIN ENTRY DOOR INTERNAL ATTACH BRACKET CRACKED. REPLACED BRACKET IAW DC9 SRM 51-10-4 AND SRM 51-30-5.

Part: JAMB — DAMAGED (SERVICE DOOR)

DURING C-CHECK, THE SERVICE DOOR FORWARD JAMB WAS FOUND DAMAGED AND CORRODED. THE JAMB WAS REPLACED IAW DC9 SRM 51-30-2.

Part: DOUBLER — CORRODED (LT MLG WW)

DURING C-CHECK, THE LEFT WHEEL WELL PRESSURE PANEL DOUBLER WAS FOUND CORRODED. THE DOUBLER WAS REPLACED IAW DC9 SRM 51-30-5.

Part: LONGERON — CORRODED (BS 1104)

DURING C-CHECK, THE LONGERON AT STA 1104 AT LONG 9 LT WAS FOUND CORRODED. THE LONGERON WAS REPLACED IAW DC9 SRM.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, THE LONGERON AT STA 965 AT LONG 6 LT WAS FOUND CRACKED. THE LONGERON WAS REPLACED IAW DC9 SRM 51-02, FIGURE 4.

Part: INTERCOSTAL — DAMAGED (BS 351-370)

DURING C-CHECK, AN INTERCOSTAL FROM STA 351 TO 370 AT LONG 29 RT WAS FOUND DAMAGED. THE INTERCOSTAL WAS REPLACED IAW DC9 SRM 51-30-2.

Part: FITTING — CRACKED (BS 691)

DURING C-CHECK, A FITTING AT STA 691 IN THE LT KEEL AREA WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM 51-30-5.

Part: TAB — DELAMINATED (RT AILERON)

THE RIGHT AILERON TAB WAS DELAMINATED ON BOTH THE UPPER AND LOWER CORNER. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN IAW DC-9 SRM.

Part: LONGERON — CRACKED (BS 160)

DURING C-CHECK, A LONGERON AT STA 160 AT LONG 4 LT WAS FOUND CRACKED. THE LONGERON WAS REPLACED IAW DC9 SRM 53-02, FIGURE 2.

Part: DOOR LATCH — MALFUNCTIONED (NLG)

AFTER TAKEOFF AND RAISING THE GEAR, HEARD BANGING SOUND COMING FROM THE NOSE WHEEL WELL. RECYCLED THE GEAR, SAME SOUND, TOOK THIS TO MEAN A GEAR DOOR WAS UNABLE TO LATCH CLOSED. CONTINUED ON TO TRI WITH THE GEAR EXTENDED SINCE THAT SEEMED TO LOCK THE DOOR IN PLACE. SUSPECT NOSE GEAR DOOR NOT LATCHED PROPERLY. CLEANED AND LUBED, GROUND OPS CHECKED GOOD IAW DC-9 MM 32-20.

Part: LINKAGE — DEFECTIVE (RT NLG DOOR)

FORWARD NOSE GEAR DOORS WILL NOT RETRACT. RECYCLED GEAR, NO HELP. REPLACED RIGHT NOSE GEAR LINKAGE IAW DC-9 MM.

Part: SKIN — PUNCTURED (BS 436)

ONE INCH HOLE IN FUSELAGE BETWEEN REAR OF FORWARD BELLY DOOR AREA AND STATIC PORT. THE HOLE WAS CAUSED BY SNOW PLOW MAKING CONTACT WITH FUSELAGE. FABRICATED AND INSTALLED REPAIR IAW REPAIR ENGINEERING AUTHORIZATION D953-14048-MR.

Part: SKIN — DAMAGED (FS 205)

DURING C-CHECK INSPECTION, THREE DENTS WITH GOUGES WERE FOUND JUST AFT OF THE FORWARD ENTRY DOOR BETWEEN LONGERONS 14 AND 15L. REPAIRED IAW ABX REA D953-12498-MR.

Part: RETAINER — CRACKED (FWD FUSELAGE)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, FOUND THE RIGHT OVERHEAD WINDOW OUTER RETAINER CRACKED. REPAIRED IAW ABX EA NR AD-56-03239-MA.

Part: SKIN — DAMAGED (FWD FUSELAGE)

DURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 94-03-01, A PREVIOUS REPAIR AND INTERNAL DOUBLER WAS FOUND DAMAGED AT THE UPPER FORWARD CORNER OF THE FORWARD ENTRY DOOR JAMB. REPAIRED IAW ABX REA D953-12388-MR.

Part: LONGERON — DEFECTIVE (BS 1089)

DURING C-CHECK INSPECTION, FOUND A LONGERON SPLICE AT STA 1089, LONGERON 12R MISSING A FASTENER. REPAIRED IAW ABX REA D953-12433-MR.

Part: SKIN — CRACKED (BS 996)

DURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 81-26-03, SB A53-147, FOUND A CRACK IN THE FUSELAGE SKIN AT STA 996, LONGERON 7 AND 8L. REPAIRED IAW ABX REA D953-12407-MR.