N959AX

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 41,444 hrs · 44,790 cycles

ANGLE CRACKED AT FASTENER - LEFT SIDE JUST FORWARD OF TIP FAIRING. REMOVED FORMER, FABRICATED NEW FORMER IAW DWG 9911981. REINSTALLED FORMER IAW DC9 SRM 51-30-2.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 41,444 hrs · 44,790 cycles

SEAT TRACK AT STA 180 (APPROXIMATELY) LEFT BUTT LINE 44 WAS CRACKED ON OUTBOARD FLANGE. REMOVED AND REPLACED TRACK SECTION FROM FS 160 TO 226, LEFT BUTT LINE 44. INSTALLED TRACK IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,444 hrs · 44,790 cycles

SEAT TRACK AT STA 427 CORRODED BETWEEN LONGERON 28 LEFT AND LONGERON 27 LEFT. REMOVED AND REPLACED SECTION OF TRACK AT STA 427, LONGERON 28 LEFT IAW DOUGLAS DWG 5922344, AND DC9 SRM 51-30-1 AND 51-30-2.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,444 hrs · 44,790 cycles

CEILING INTERCOSTAL STA 180, LEFT BUTT LINE 30 - 54 WAS CRACKED AT INBOARD END. REMOVED DRIP PAN TO FOM, INSTALLED REPAIR DOUBLERS: -05, 015, 017, 021 AND -19 IAW DC9 SRM 53-05, FIGURE 75.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,444 hrs · 44,790 cycles

INTERCOSTAL ANGLE CRACKED AT STA 237, BUTT LINE 0. STOP DRILLED AND REPAIRED CRACK IAW SSRM K05159. INSTALLED HI-LOKS IAW DC9 SRM 51-30-5.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 41,444 hrs · 44,790 cycles

CUSP WEB HAD 3 CRACKS, FS 1021 TO 1041 LEFT SIDE. REPAIRED CUSP WEB IAW DC9 SRM. CRACK LENGTHS 7/8", 3/4", AND 1".

Part: FITTING — CRACKED (AFT CARGO DOOR) · airframe 41,444 hrs · 44,790 cycles

AFT LOWER CARGO DOOR BEAM 1 AFT END FITTING CRACKED AT FASTENER. REMOVED AND REPLACED AFT LOWER CARGO DOOR BEAM NR 1 AFT FITTING.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 41,444 hrs · 44,790 cycles

FLOORBEAM AND INTERCOSTAL ATTACH CLIP WERE BROKEN AND CRACKED AT FS 180, LEFT BUTT LINE 22. REPAIRED FLOORBEAM AND INTERCOSTAL ATTACH CLIP IAW DC9 SRM 53-01, FIGURE 2, SHEET 3.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 41,230 hrs · 44,531 cycles

ON PRE-FLIGHT, EMERGENCY LIGHTS WOULD NOT COME ON IN THE -ON- POSITION. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-02-4-0001.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,048 hrs · 44,364 cycles

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

Part: THERMAL SWITCH — ARCED (COCKPIT) · airframe 40,659 hrs · 43,995 cycles

CAPTAIN'S CLEARVIEW ANTI-FOG TEMPERATURE SENSOR ARCING. REPLACED CAPTAIN'S CLEARVIEW WINDOW ANTI-FOG THERMAL SWITCH IAW DC9 MM 30-41-02-2-0001.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 40,201 hrs · 43,529 cycles

HORIZONTAL STABILIZER CENTER SPAR BOX SKIN CRACKED ON UPPER SKIN, JUST FORWARD OF STRESS PLATE. COMPLIED WITH REA D955-53041 AND REPAIRED AREA.

Part: STIFFENER — CRACKED (CABIN) · airframe 38,655 hrs · 42,341 cycles

P-DOME STIFFENER OUTBOARD END CLIP CRACKED AT LONGERON 14 RIGHT. REMOVED AND REPLACED CLIP IAW DC-9 DWG 9915558.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 38,655 hrs · 42,341 cycles

P-DOME STIFFENER OUTBOARD END CLIP CRACKED IN RADIUS AT LONGERON 12 RIGHT. REMOVED AND REPLACED CLIP IAW DC-9 DWG 9915558.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 38,655 hrs · 42,341 cycles

P-DOME STIFFENER OUTBOARD END CLIP CRACKED AT LONGERON 12 LEFT, TOP AND BOTTOM. REPAIRED LOWER STIFFENER. REPLACED UPPER CLIP IAW DC-9 DWG J060110.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 38,655 hrs · 42,341 cycles

P-DOME STIFFENER OUTBOARD END CLIP CRACKED AT LONGERON 15 LEFT. REPAIRED STIFFENER IAW DC-9 DWG J060110.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 38,655 hrs · 42,341 cycles

P-DOME STIFFENER OUTBOARD END CLIP CRACKED AT LONGERON 14 LEFT. REPAIRED IAW DC-9 SERVICE BULLETIN 53-166.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 38,655 hrs · 42,341 cycles

SPOT OF EXFOLIATION ON SHEAR TIE, AFT SIDE OF FS 1123 CANTED AT LONGERON 3 LEFT. INSTALLED NEW CLIP, AFT SIDE FS 1123, LONGERON 3 LEFT IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: INTERCOSTAL — CRACKED · airframe 37,027 hrs · 41,182 cycles

INTERCOSTAL CRACKED AT STA. 973, LONGERON 28 RIGHT. REPLACED INTERCOSTAL IAW DC-9 SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,061 hrs · 40,478 cycles

EMERGENCY LIGHTS BATTERIES LOW. REPLACED THE EMERGENCY LIGHTS BATTERIES IAW DC-9 AMM 33-53-00-8. OPS CHECKED GOOD.

Part: CONTROL PANEL — FAILED (COCKPIT) · airframe 35,154 hrs · 39,819 cycles

IN CRUISE, THE AIRCRAFT EXPERIENCED A RIGHT GENERATOR FAILURE WITH A CROSS TIE LOCKOUT. THE GENERATOR WAS RESET AND IT FAILED AGAIN. THE CREW DECLARED AN EMERGENCY. MAINTENANCE INSPECTED AND DEFERRED THE RIGHT A/C GENERATOR IAW DC-9 MEL. ON 03/31/01 MAINTENANCE INSPECTED AND REPLACED THE GENERATOR CONTROL PANEL AND REMOVED THE DEFERRAL FROM THE AIRCRAFT.

Part: WINDOW — DRY (COCKPIT) · airframe 34,239 hrs · 39,209 cycles

FIRST OFFICER''S CLEARVIEW WINDOW WOULD NOT OPEN DURING TAXI. LUBRICATED THE UPPER LOCK HINGE.

Part: PANEL — DELAMINATED (LT SPOILER)

DURING C-CHECK, FOUND LEFT OUTBOARD SPOILER DELAMINATED AT INBOARD FORWARD CORNER. REPLACED SPOILER PANEL IAW DC9 MM 27-61-1.

Part: ANGLE — CRACKED (RTTE FLAP)

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

Part: LONGERON — CRACKED (BS 1056)

DURING C-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 1056. REPLACED LONGERON SECTION IAW DC9 SRM 53-02-00.

Part: BULKHEAD TEE — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD NR 2 TEE CAP CRACKED AT THIRD RADIAL. REPLACED NR 2 TEE CAP IAW ABX EA 531-20033-001.

Part: TR BUCKET — CRACKED (NR 1 ENGINE)

DURING C-CHECK, FOUND NR 1 ENGINE UPPER THRUST REVERSER BUCKET INBOARD LOWER SKIN CRACKED AFT OF IDLER LINK ATTACH POINT. REPLACED NR 1 ENGINE UPPER THRUST REVERSER BUCKET.

Part: STIFFENER — CRACKED (AFT FUSELAGE)

DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD, AFT SIDE STIFFENER CRACKED AT BOTTOM OF VENTRAL DOOR CUTOUT. REPAIRED IAW DC9 SRM DRAWING K05159.

Part: ANGLE — CRACKED (NR 2 PYLON)

DURING C-CHECK, FOUND THE NR 2 PYLON UPPER ATTACH ANGLE CRACKED AT FORWARD END. REPAIRED ANGLE IAW DC9 SRM 54-04.

Part: LATCH — OUT OF ADJUST (RT COCKPIT)

FIRST OFFICER'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. FOUND UPPER LATCHING BAYONET OUT OF ADJUSTMENT. ADJUSTED LINKAGE, OPS CHECKED GOOD.

Part: WINDOW — STUCK (RT COCKPIT)

FIRST OFFICER'S CLEARVIEW WINDOW (EMERGENCY EXIT) WOULD NOT OPEN DURING PREFLIGHT. LOCKING MECHANISM WAS STUCK. UNSTUCK, CLEANED AND LUBRICATED LOCKING MECHANISM GUIDE PIN, OPS CHECKED GOOD.

Part: LATCH — OUT OF POSITION (COCKPIT DOOR)

UNABLE TO OPEN COCKPIT DOOR. REPOSITIONED LATCH ON DOOR JAMB.

Part: SUBFLOOR — CRACKED (BS 160)

DURING MOD/D-CHECK, FOUND THE COCKPIT SUBLOOR AT STA 160 CRACKED THREE PLACES BETWEEN RBL 20 AND RBL 26. REPAIRED IAW DC9 SRM 53-01.

Part: SUBFLOOR — CRACKED (BS 148-160)

DURING MOD/D-CHECK, FOUND THE COCKPIT SUBFLOOR AT STA 148-160 AND RBL 40-RBL 54 CRACKED. REPAIRED IAW DC9 SRM 53-01.

Part: SPAR — CRACKED (WS 164)

DURING MOD/D-CHECK, FOUND THE RIGHT WING LOWER REAR SPAR CRACKED 1.375 INCH LONG JUST INBOARD OF STA 164 FLAP HINGE FITTING ATTACH STUD. REPAIRED REAR SPAR IAW ABX EA 51110027002.

Part: PANEL — CORRODED (LT WING)

DURING MOD/D-CHECK, FOUND THE LEFT WING UPPER INBOARD TRAILING EDGE PANEL HONEYCOMB STRUCTURE CORRODED. REPLACED TRAILING EDGE PANEL IAW DC9 SRM 51-30-2.

Part: FITTING — CRACKED (ACCESS COMPT)

DURING MOD/D-CHECK, FOUND LEFT SUPPORT BRACKET FITTING IN AFT ACCESSORY COMPARTMENT CORRODED AND CRACKED. REPLACED BRACKET FITTING IAW DC9 SRM 51-30-2.

Part: BRACKET — CORRODED (VENTRAL DOORWAY)

DURING MOD/D-CHECK, FOUND THE AFT VENTRAL STAIR DOOR JAMB BRACKET CORRODED. REPLACED BRACKET IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: DOOR JAMB — CORRODED (BS 1135)

DURING MOD/D-CHECK, FOUND THE AFT VENTRAL DOOR AFT JAMB WEB FS 1135 FRAME CORRODED, LONGERON 24L TO 24R. REPLACED WEB IAW DC9 SRM 51-30-2, AND DACO DWG 9915559.

Part: FRAME — CORRODED (BS 1114)

DURING MOD/D-CHECK, FOUND FRAME AT STA 1114 CORRODED FROM LONGERON 24L TO 24R. REPLACED FRAME T-CAP IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FRAME — CORRODED (BS 1114)

DURING MOD/D-CHECK, FOUND FUSELAGE FRAME AT STA 1114 HEAVILY CORRODED BETWEEN LONGERON 24L AND 24R. REPLACED FRAME IAW DC9 SRM 51-30-2.

Part: ANGLE — CORRODED (VENTRAL DOORWAY)

DURING MOD/D-CHECK, FOUND THE AFT VENTRAL STAIR DOOR JAMB ANGLE CORRODED. REPLACED ANGLE IAW DC9 SRM 51-30-2 AND 51-30-5. ADDITIONAL PARTS JAMB, (P/N 991190-401), ANGLE (P/N 9919662-12).

Part: FITTING — CORRODED (ACCESS COMPT)

DURING MOD/D-CHECK, FOUND SUPPORT BRACKET FITTING IN AFT ACCESSORY COMPARTMENT CORRODED AND CRACKED. REPLACED BRACKET FITTING IAW DC9 SRM 51-30-2.

Part: STIFFENER — CORRODED (BS 1197)

DURING MOD/D-CHECK, FOUND STIFFENER CORRODED AT AFT SIDES OF STA 1197 AND LONGERON 13R. REPLACED STIFFENER IAW DC9 SRM 51-30-5 AND DACO DWG 9911839.

Part: PANEL — CORRODED (LT WING)

DURING C-CHECK, FOUND FUEL ACCESS PANEL NR 5912369-509 CORRODED BEYOND LIMITS. REPLACED PANEL.

Part: FITTING — CORRODED (LT MLG)

DURING MOD/D-CHECK, FOUND THE LT MLG TRUNNION FITTING CORRODED BEYOND LIMITS AT THE LOWER OUTBD FLANGE AND THE SIDE BRACE ATTACH LUG. REPLACED TRUNNION FITTING IAW ABX EA 57430025003.

Part: SHEAR TIE — CRACKED (BS 1185)

DURING MOD/D-CHECK, FOUND AFT ACCESSORY COMPARTMENT FRAME STA 1185 SHEAR TIE JUST LT OF LONGERON 1 CRACKED, 8 INCHES LONG. REPLACED SHEAR TIE.

Part: FORMER — CRACKED (BS 1132)

DURING MOD/D-CHECK, FOUND A FORMER AT STA 1132 BULGED AND CRACKED BETWEEN LONGERONS 13R AND 14R. REPAIRED FORMER IAW DC9 SRM 53-03.

Part: FRAME — CORRODED (BS 577)

DURING MOD/D-CHECK, FOUND FRAME AT STA 577 CORRODED JUST OUTBD OF LONGERON 27R. REPLACED FRAME IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FITTING — CORRODED (BS 1153)

DURING MOD/D-CHECK, FOUND THE VENTRAL STAIR DOOR JAMB FITTING ON THE RT SIDE AT STA 1153 CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-1, 51-30-2, AND 51-30-5.

Part: PANEL — CORRODED (WS 353-445)

DURING MOD/D-CHECK, FOUND THE RT WING TRAILING EDGE HONEYCOMB PANEL BETWEEN STA XRS 353 TO 445 LOWER SURFACE CORRODED FIVE PLACES AT THE TRAILING EDGE OF THE PANEL AND BULGED AROUND SEVERAL FASTENER HOLES ON THE UPPER SURFACE. REPLACED TRAILING EDGE PANEL IAW DC9 SRM 51-30-2 AND 51-30-1.

Part: SKIN — CORRODED (BS 1197-1231)

DURING MOD/D-CHECK, FOUND THE FUSELAGE EXTERIOR SKIN CORRODED THROUGH BETWEEN CANTED STA 1197 TO 1231 AND LONGERON 18L TO THE VENTRAL STAIR DOOR JAMB. REPLACED SKIN IAW DC9 SRM 51-30-2 AND 51-10-3.

Part: WEB — CRACKED (LT PYLON)

DURING MOD/D-CHECK, FOUND THE LT PYLON INTERIOR OUTBD AFT WEB CRACKED. REPLACED WEB IAW DC9 SRM 51-30-2, 51-30-5, AND DACO DWG 9958221.

Part: DOOR — DELAMINATED (LT MLG)

DURING MOD/D-CHECK, FOUND LT MLG OUTBD DOOR DELAMINATED. REPLACED LT MLG OUTBD DOOR IAW ABX EA 323110001-102.

Part: JAMB — CORRODED (CARGO DOOR)

DURING MOD/D-CHECK, FOUND THE AFT LOWER CARGO COMPARTMENT DOOR JAMB WEB CORRODED. REPLACED WEB IAW DC9 SRM 51-30-21 AND 51-30-5.

Part: ANGLE — CRACKED (LT PYLON)

DURING MOD/D-CHECK, FOUND THE LT PYLON INTERIOR OUTBD AFT ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-2, 51-30-5, AND DACO DWG 9958221.

Part: FORMER — CORRODED (BS 655)

DURING MOD/D-CHECK, FOUND CANTED KEEL BEAM AREA FORMER AT STA 655 RT SIDE CORRODED. REMOVED AND REPLACED FORMER IAW SC9 SRM 51-30-1, 51-30-2, AND 51-30-5.

Part: SPAR WEB — CORRODED (LT WING)

DURING MOD/D-CHECK, FOUND THE LEFT WING AUX SPAR WEB CORRODED AT THE LOWER OUTBOARD EDGE OF THE TRUNNION. REPLACED THE WEB IAW DACO DWG 9919401.

Part: FITTING — CRACKED (BS 1072)

DURING MOD/D-CHECK, FOUND THE INTERCOSTAL FITTING AT STA 1072 CRACKED BETWEEN LONGERONS 22R AND 28R. REPLACED FITTING IAW DC9 SRM 51-30-2.

Part: SKIN — CORRODED (BS 1197)

DURING MOD/D-CHECK, FOUND THE FUSELAGE EXTERIOR SKIN CORRODED, AND BULGED WITH POPPED RIVETS AT CANTED STA 1197 AND LONGERON 27R. REMOVED AND REPLACED SKIN IAW DC9 SRM 53-32-0.

Part: FITTING — CRACKED (HORIZ STAB)

DURING MOD/D-CHECK, FOUND THE LEFT ELEVATOR OUTBOARD HINGE FITTING CRACKED AT THE HORIZONTAL STABILIZER UPPER ATTACH HOLE. REPLACED ELEVATOR HINGE FITTING IAW DC9 SRM 51-30-1.

Part: WEB — CRACKED (BS 655)

DURING MOD/D-CHECK, FOUND THE RT CUSP WEB CRACKED AT STA 655. REMOVED AND REPLACED CUSP WEB IAW DC9 SRM 51-30-2 AND 51-30-1.

Part: HINGE — CRACKED (CARGO COMP)

DURING MOD/D-CHECK, FOUND VENTRAL DOOR JAMB LOWER HINGE CRACKED. REPLACED LOWER HINGE IAW DC9 SRM 51-30-1 AND 51-30-2.

Part: FITTING — CRACKED (CARGO COMP)

DURING MOD/D-CHECK, FOUND VENTRAL DOOR JAMB FITTING CRACKED AT RBL 12, 18 UP FROM FLOOR. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: SHEAR TIE — CRACKED (BS 617)

DURING MOD/D-CHECK, FOUND SHEAR TIE AT STA 617 AND LONGERON 18L CRACKED. REPLACED SHEAR TIE IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (BS 1041)

DURING MOD/D-CHECK, FOUND LONGERON 17R CRACKED AFT OF STA 1041. REPLACED LONGERON IAW DC9 SRM 53-02.

Part: FITTING — CRACKED (CARGO COMP)

DURING MOD/D-CHECK, FOUND VENTRAL DOOR JAMB FITTING CRACKED AT RBL 12, 36 UP FROM FLOOR. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (BS 1041)

DURING MOD/D-CHECK, FOUND LONGERON 17L CRACKED AFT OF STA 1041. REPLACED LONGERON IAW DC9 SRM 53-02, FIG 18.

Part: SKIN — CORRODED (BS 1197)

DURING MOD/D-CHECK, FOUND FUSELAGE EXTERIOR SKIN CORRODED THROUGH AT STA 1197 FROM LONGERON 24L TO VENTRAL STAIR JAMB. REPLACED SKIN IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FLOORBEAM — CORRODED (BS 1041)

DURING MOD/D-CHECK, FOUND FLOORBEAM UPPER CAP FLANGE STA 1041 AND LBL 20 CORRODED. REMOVED AND REPLACED FLOORBEAM UPPER CAP FLANGE.