N963AX

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,310 hrs · 42,697 cycles

FLOORBEAM STA 180, LEFT BUTT LINE 22 WAS CRACKED ON OUTBOARD SIDE OF INTERCOSTAL. REPAIRED FLOOR IAW REA D953-56651.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 40,310 hrs · 42,697 cycles

FLOORBEAM ANGLE AT STA 180 CRACKED AT BUTT LINE 0, AFT SIDE OF FLOORBEAM, LEFT SIDE OF INTERCOSTAL. REMOVED AND REPLACED ANGLE IAW DC9 SRM 51-30-5.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,310 hrs · 42,697 cycles

INTERCOSTAL CRACKED FS 180 AT LEFT BUTT LINE 22. REPAIRED INTERCOSTAL IAW DC9 SRM 53-01 FIGURE 2.

Part: PANEL — CORRODED (FUSELAGE) · airframe 40,310 hrs · 42,697 cycles

SUBFLOOR PANEL 1B WAS CORRODED. FABRICATED AND INSTALLED NEW PANEL IAW DC9 SRM 51-10-4.

Part: PAN — CRACKED (FWD CARGO DOOR) · airframe 40,310 hrs · 42,697 cycles

FORWARD LOWER CARGO DOOR CRACKED IN RADIUS (LOWER FORWARD AT LOCK MECHANISM ON INNER PAN). REPAIRED FORWARD LOWER CARGO DOOR IAW DC9 SRM 52-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,310 hrs · 42,697 cycles

AFT LOWER CARGO FRAME PUNCTURED AND CRACKED AT FS 927, BETWEEN LONGERON 29 - 30. REPAIRED FRAME AT FS 927, LONGERON 29 - 30 IAW DC9 SRM 53-03, FIGURE 5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,207 hrs · 42,571 cycles

WHILE COMPLYING WITH EA 53300036, FOUND FRAME CRACKED. REPAIRED FRAME IAW DC9 SRM 53-03, FIGURE 34.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,207 hrs · 42,571 cycles

WHILE COMPLYING WITH EA 53300036, FOUND CRACKED FRAME. REPAIRED FRAME IAW DC9 SRM 53-03, FIGURE 34.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,207 hrs · 42,571 cycles

WHILE COMPLYING WITH EA 53300036, FOUND CRACKED FRAME. REPAIRED FRAME IAW DC9 SRM 53-03, FIGURE 34.

Part: PAN — CRACKED (FUSELAGE) · airframe 39,020 hrs · 41,459 cycles

FORWARD LOWER CARGO DOOR PAN CRACKED AT AFT HOLD OPEN FITTING. REPAIRED CRACKED DOOR PAN IAW SSRM K05159.

Part: RETAINER — CRACKED (COCKPIT) · airframe 39,020 hrs · 41,459 cycles

CRACKS NOTED ON X-RAY INSPECTION AT CAPTAIN'S OVERHEAD WINDOW RETAINER. REMOVED AND REPLACED CRACKED DOUBLER IAW SRM 51-30-2.

Part: FITTING — CRACKED (EXIT DOOR) · airframe 39,020 hrs · 41,459 cycles

RT FORWARD OVERWING EXIT DOOR HAD A CRACKED FITTING AT FORWARD LOWER CORNER. REMOVED DAMAGED FITTING AND INSTALLED NEW FITTING IAW SRM 57-30-5 AND 51-30-2.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,519 hrs · 41,028 cycles

EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERIES IAW DC-9 AMM 33-53-02-4. OPS CHECKED GOOD.

Part: LATCH — LACK OF LUBE (COCKPIT WINDOW) · airframe 37,501 hrs · 40,337 cycles

ON TAXI IN, DISCOVERED FIRST OFFICER'S WINDOW WOULD NOT OPEN. OPENED WINDOW, CLEANED AND LUBED LATCHING MECHANISM. WINDOW CHECKED GOOD IAW MM 56-10-03-4.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 37,148 hrs · 40,076 cycles

FS 775, INBOARD OF STRINGER NR 3 LEFT AT FASTENER HOLE, 1 EA CRACK INDICATION. REPAIRED AREA IAW DC-9 SRM 53-04.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 37,148 hrs · 40,076 cycles

UPPER RIGHT VENTRAL DOOR STOP FITTING ON AFT PRESSURE BULKHEAD WAS CRACKED. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 37,148 hrs · 40,076 cycles

AXIAL CRACK IN AFT PRESSURE BULKHEAD AT RIGHT UPPER CORNER OF VENTRAL DOOR CUT OUT. REPAIRED AREA IAW REA D953-49498MR.

Part: FITTING — CRACKED (FWD. CARGO) · airframe 35,432 hrs · 38,801 cycles

FORWARD LOWER CARGO DOOR AFT STOP FITTING AT END OF INTERCOSTAL CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: FORMER — CRACKED (FWD. CARGO) · airframe 35,432 hrs · 38,801 cycles

FORWARD LOWER CARGO DOOR, LOWER FORWARD STOP INTERCOSTAL FORMER WAS CRACKED. REPLACED BRACKET IAW DC-9 SRM 51-30-1 AND 51-30-2.

Part: PAN — CRACKED (CARGO DOOR) · airframe 35,432 hrs · 38,801 cycles

OUTER PAN WAS CRACKED AT BEAM 3 ON AFT END OF AFT LOWER CARGO DOOR. REPLACED DOOR IAW DC-9 MM.

Part: PAN — CRACKED (AFT CARGO) · airframe 35,432 hrs · 38,801 cycles

AFT LOWER CARGO DOOR HAD CRACKED INTERIOR DOOR STOP FITTING AT AFT UPPER CORNER. REPLACED AFT LOWER CARGO DOOR ON N.R. #0350 IAW DC-9 MM.

Part: PAN — CRACKED (AFT CARGO) · airframe 35,432 hrs · 38,801 cycles

FORWARD END OF AFT LOWER CARGO DOOR HAD CRACKED PANES AT DOORSTOP CUTOUT AT BEAMS 1, 2, AND 3. REPLACED DOOR ON N.R. #0350 AND IAW DC-9 MM.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 35,432 hrs · 38,801 cycles

CRACK INDICATION ON NR 6 AFT PRESSURE BULKHEAD 'T' AT LONGERON 14 LEFT AND 'P' DOME RADIAL. REPLACED NR 6 'T' CAP IAW EA 53120037-006.

Part: PAN — CRACKED (AFT CARGO) · airframe 35,432 hrs · 38,801 cycles

AFT LOWER CARGO DOOR INNER PAN WAS CRACKED NEAR FORWARD LATCH HOOK AT ROLLER CUTOUT. REPLACED AFT LOWER CARGO DOOR ON N.R. #0350 AND IAW DC-9 MM.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 35,432 hrs · 38,801 cycles

VERTICAL REMOVEABLE LEADING EDGE RIB WAS CRACKED, LEFT SIDE NR 12. REPAIRED AREA IAW DC-9 SSRM K05159, SRM 51-30-2 AND 51-30-5.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 35,432 hrs · 38,801 cycles

VERTICAL REMOVABLE LEADING EDGE RIB WAS CRACKED LEFT SIDE NR 1. REPAIRED AREA IAW ABX DC-9 SSRM K05159, SRM 51-30-2 AND 51-30-5.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 35,432 hrs · 38,801 cycles

VERTICAL REMOVABLE LEADING EDGE RIB WAS CRACKED RIGHT SIDE NR 3. REPAIRED AREA IAW DC-9 ABX SSRM K05159, SRM 51-30-2 AND 51-30-5.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 35,432 hrs · 38,801 cycles

VERTICAL REMOVABLE LEADING EDGE RIB WAS CRACKED LEFT SIDE NR 4. REPAIRED AREA IAW DC-9 ABX SSRM K05159, SRM 51-30-2 AND 51-30-5.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 35,432 hrs · 38,801 cycles

VERTICAL REMOVABLE LEADING EDGE RIB WAS CRACKED LEFT SIDE NR 7. REPAIRED AREA IAW DC-9 ABX SSRM K05159, SRM 51-30-2 AND 51-30-5.

Part: CONTROL UNIT — FAILED (ANTI-SKID SYS) · airframe 33,865 hrs · 37,621 cycles

UPON LANDING WHEN BRAKES WERE APPLIED, THE BRAKES DID NOT OPERATE. WITH THE ANTI-SKID SYSTEM SELECTED OFF, BRAKING ACTION RETURNED. MAINTENANCE INSPECTED AND REPLACED THE ANTI-SKID CONTROL UNIT IAW DC-9 MAINTENANCE MANUAL 32-43-04.

Part: FAIRING — CORRODED (EMPENNAGE) · corrosion level 2 · airframe 33,719 hrs · 37,538 cycles

RIGHT UPPER HORSECOLLAR HORIZONTAL FAIRING FOUND WORN AND CORRODED. MAINTENANCE INSPECTED AND REPLACED THE RIGHT UPPER HORSECOLLAR FAIRING IAW DC-9 MM 55-10-00.

Part: FITTING — CRACKED (SPOILER) · airframe 33,719 hrs · 37,538 cycles

INBOARD SPOILER TORSION BAR CENTER SUPPORT FITTING WAS FOUND CRACKED. MAINTENANCE INSPECTED AND REPLACED THE FITTING IAW DC-9 SRM 51-30-5.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,719 hrs · 37,538 cycles

FUSELAGE SKIN WAS CRACKED FORWARD OF STATION 1072, BELOW LONGERON 14R. MAINTENANCE INSPECTED AND REPAIRED THE CRACKED AREA IAW ABX REA D953-39613.

Part: FAIRING — DELAMINATED (EMPENNAGE) · airframe 33,719 hrs · 37,538 cycles

LEFT UPPER HORSECOLLAR WAS FOUND DELAMINATED. MAINTENANCE INSPECTED AND REPLACED THE HORSECOLLAR IAW DC-9 SRM 51-30-1.

Part: JACKSCREW — CORRODED (STABILIZER) · corrosion level 2 · airframe 33,719 hrs · 37,538 cycles

CORROSION WAS LOCATED ON THE STABILIZER JACKSCREW THREADS, RIGHT HAND SIDE. MAINTENANCE INSPECTED AND REPLACED THE JACKSCREW ASSY AND ACME NUT IAW DC-9 MM 27-40-01.

Part: SKIN — DELAMIINATED (RT AILERON TAB)

DURING C-CHECK, FOUND RIGHT AILERON TRIM TAB DELAMINATED. REPLACED TRIM TAB IAW DC9 MM 27-10-5 AND ABX REA D927-31543.

Part: VANE — DELAMINATED (RT WING)

DURING C-CHECK, FOUND RIGHT INBOARD FLAP FIXED VANE DELAMINATED. REPLACED FLAP FIXED VANE IAW DC9 MM 27-50.

Part: PAN — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND AFT LOWER CARGO DOOR PAN CRACKED. REPAIRED IAW ABX REA D952-31557.

Part: PROX BOX — DEFECTIVE (LT MLG)

DURING FERRY FLIGHT AFTER TAKEOFF, THE RED LEFT GEAR UNSAFE LIGHT REMAINED ON, RECYCLED GEAR. REPLACED THE PROX BOX PER DC-9 SUPP MM, OPS CHECKED GOOD.

Part: SPAR — CRACKED (RT HORIZ STAB)

DURING D-CHECK, FOUND THE RT HORIZ STAB REAR SPAR LOWER SPAR CAP CRACKED WHERE IT BOLTS TO THE CENTER BOX SECTION. *S/D* NO DEFECT, PERFORMED DYE PEN INSPECTION AND NO CRACKS NOTED.

Part: RIB — CRACKED (VERT STAB)

DURING D-CHECK, FOUND THE VERT STAB LEADING EDGE LOWER SECTION NR 5 RIB CRACKED AT THE LT AFT END. *S/D* REPAIRED RIB IAW ABX DC9 SSRM DWG K05159.

Part: RIB — CRACKED (VERT STAB)

DURING D-CHECK, FOUND THE VERT STAB LEADING EDGE LOWER SECTION NR 3 RIB CRACKED AT THE RT AFT END. *S/D* REPAIRED RIB IAW ABX DC9 SSRM DWG K05159.

Part: RIB — CRACKED (VERT STAB)

DURING D-CHECK, FOUND THE VERT STAB LEADING EDGE LOWER SECTION NR 6 RIB CRACKED AT THE LT AFT END. *S/D* REPAIRED IAW ABX DC9 SSRM DWG K05159.

Part: WEB — CRACKED (BS 218)

DURING D-CHECK, FOUND THE LT CUSP WEB CRACKED AT FS 218. *S/D* REPLACED CUSP WEB IAW DC9 SRM 51-30-2.

Part: RIB — CRACKED (VERT STAB)

DURING D-CHECK, FOUND THE VERT STAB LEADING EDGE LOWER SECTION NR 2 RIB CRACKED AT THE RT AFT END. *S/D* REPAIRED RIB IAW ABX DC9 SSRM DWG K05159.

Part: RIB — CRACKED (RT WING)

DURING D-CHECK, FOUND THE RT WING LEADING EDGE FIRST RIB INBD OF NR 2 SLAT TRACK CRACKED AT LOWER SPAR. REMOVED AND REPLACED RIB IAW DC9 SRM 51-30-1, 51-30-2, 51-30-5.

Part: BLKHEAD ANGLE — CRACKED (AFT PRESS BLKHD)

DURING D-CHECK, FOUND THE AFT PRESSURE BULKHEAD HORIZONTAL BEAM ATTACH ANGLE IS CRACKED AT LONGERON 15L. *S/D* REPLACED ATTACH ANGLE IAW DC9 SB 53-166.

Part: RIB — CRACKED (VERT STAB)

DURING D-CHECK, FOUND THE VERT STAB LEADING EDGE LOWER SECTION NR 5 RIB CRACKED AT THE AFT END. *S/D* REPAIRED IAW ABX DC9 SSRM DWGK05159.

Part: DOOR — CORRODED (LT MLG)

DURING D-CHECK, FOUND THE LT MAIN LANDING GEAR OUTBD TRAILING EDGE DOOR IS CORRODED. *S/D* REMOVED CORROSION, TREATED AND PRIMED IAW DC9 SRM 51-10-3 AND 51-10-3B.

Part: DOOR — CORRODED (RT MLG)

DURING D-CHECK, FOUND THE RT MAIN LANDING GEAR OUTBD TRAILING EDGE DOOR IS CRACKED AND CORRODED. *S/D* REPLACED SEAL AND REMOVED CORROSION, TREATED AND PRIMED. IAW DC9 SRM 51-10-3 &51-10-3B.

Part: RIB — CRACKED (VERT STAB)

DURING D-CHECK, FOUND THE VERT STAB LEADING EDGE LOWER SECTION NR 6 RIB CRACKED AT THE RT AFT END. *S/D* REPAIRED RIB IAW DC9 SSRM DWG K05159.

Part: PANEL — CORRODED (RT WING)

DURING D-CHECK, FOUND THE RIGHT WING LOWER SURFACE MOST INBOARD TRIANGLE BONDED PANEL IS CORRODED. *S/D* REPLACED RIGHT WING INBOARD LOWER BONDED PANEL IAW DC9 SRM 51-30-1, 51-30-2 AND ABX EA AD57-03068 MR.

Part: PANEL — DELAMINATED (WS 4455-477)

DURING D-CHECK, FOUND THE RIGHT WING TRAILING EDGE PANEL LOWER SURFACE DELAMINATED BETWEEN STA XRS 445 TO 477. *S/D* REPLACED RIGHT WING OUTBOARD TRAILING EDGE PANEL IAW DC9 SRM 51-30-1 AND 51-30-2.

Part: ANGLE — CRACKED (NR 2 ENG PYLON)

DURING D-CHECK, FOUND NR 2 ENGINE PYLON UPPER ATTACH ANGLE CRACKED AND RIVET HEADS ARE POPPED. *S/D* REPAIRED CRACKED ANGLE IAW DC9 SRM 54-04.

Part: LONGERON — CRACKED (BS 1041)

DURING D-CHECK, FOUND LONGERON 17R CRACKED AT STA 1041. *S/D* REPLACED CRACKED SECTION OF LONGERON IAW DC9 SRM CHAPTER 53-02, 51-30-2 AND 51-30-5.

Part: BULKHEAD ANGLE — CRACKED (AFT PRESS BLKHD)

DURING D-CHECK, FOUND THE AFT PRESS BULKHEAD ATTACH ANGLE AT LONGERON 14R CRACKED. *S/D* REPLACED ATTACH ANGLE IAW DC9 SB 53-166.

Part: SKIN — CORRODED (HORIZ STAB)

DURING D-CHECK, FOUND EXFOLIATION CORROSION ON THE RT HORIZONTAL STAB LEADING EDGE INBOARD END CENTER SECTION. *S/D* REPAIRED CORROSION IAW ABX REA D955-20734.

Part: BLKHD ANGLE — CRACKED (AFT PRESS BLKHD)

DURING D-CHECK, FOUND THE AFT PRESS BULKHEAD ATTACH ANGLE BETWEEN LONGERON 15R AND 16R CRACKED. *S/D* REPLACED ATTACH ANGLE IAW DC9 SB 53-166.

Part: PANEL — DELAMINATED (WS 353-383)

DURING D-CHECK, FOUND THE RIGHT WING TRAILING EDGE PANEL LOWER SURFACE DELAMINATED BETWEEN STA XRS 353 TO 383. *S/D* REPLACED RT WING TRAILING EDGE PANEL IAW DC9 SRM 51-30-1 AND 51-30-2.

Part: FLOORBEAM — CRACKED (BS 237)

DURING D-CHECK, FOUND FLOORBEAM CRACKED AT FS 237 AND LBL 7. *S/D* REPAIRED IAW ABX REA D953-20604 MR.

Part: BLKHEAD ANGLE — CRACKED (AFT PRESS BLKHD)

DURING D-CHECK, FOUND THE AFT PRESSURE BULKHEAD HORIZONTAL BEAM ATTACH ANGLE IS CRACKED AT LONGERON 12L. *S/D* REPLACED ATTACH ANGLE IAW DC9 SB 53-166.

Part: BLKHD SHEAR TIE — CRACKED (BS 1042)

DURING D-CHECK, FOUND THE LT PYLON BULKHEAD STA 1042 SHEAR TIE CRACKED BELOW LONGERON 14L. *S/D* REPLACED SHEAR TIE IAW DC9 SRM 53-02.

Part: BLKHEAD ANGLE — CRACKED (AFT PRESS BLKHD)

DURING D-CHECK, FOUND THE AFT PRESSURE BULKHEAD HORIZONTAL BEAM ATTACH ANGLE IS CRACKED AT LONGERON 14L. *S/D* REPLACED UPPER ATTACH ANGLE AND REPAIRED LOWER ANGLE IAW DC9 SB 53-166.