N945AX

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,466 hrs · 60,206 cycles

RIGHT FORWARD MAIN FRAME AT FUSELAGE STA 699 WAS CRACKED BEYOND LIMITS OF DC-9 S/B 53-131. CRACK RAN BETWEEN POINTS H - I. REPLACED FRAME IAW ABX EA 53400322-001-4, WO 600204273.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,466 hrs · 60,206 cycles

LEFT FORWARD MAIN FRAME AT FUSELAGE STA 699 WAS CRACKED BEYOND LIMITS OF DC-9 S/B 53-131. CRACK RAN BETWEEN POINTS G - J. REPLACED FRAME IAW ABX EA 53400321-001-4, WO 600204273.

Part: SKIN — CRACKED (AFT CARGO DOOR) · airframe 57,393 hrs · 60,129 cycles

AFT LOWER CARGO DOOR SKIN WAS CRACKED AT THE DOOR HANDLE CUTOUT. REMOVED CRACKS, INSTALLED SCUFF PLATE IAW DC-9 SRM 52-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 57,393 hrs · 60,129 cycles

CUSP WEB CRACKED IN TWO AREAS FS 237 TO FS 254, RIGHT BUTTLINE 45 TO RIGHT BUTTLINE 54. REPAIRED CUSP WEB IAW DC-9 SRM 53-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,393 hrs · 60,129 cycles

SKIN CRACKED ABOVE RIGHT PYLON AT RIVET, STA 1038, LONGERON 12 RIGHT. REPAIRED CRACK IAW DC-9 SRM 53-31-0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,393 hrs · 60,129 cycles

SKIN CRACKED ABOVE LEFT PYLON AT RIVET, STA 1038, LONGERON 12 LEFT. REPAIRED CRACK IAW DC-9 SRM 53-31-0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,393 hrs · 60,129 cycles

A .5 INCH CRACK COMING OUT OF FASTENER HOLE AT FORWARD LOWER CARGO DOOR UPPER CORNER FUSELAGE SKIN. INSTALLED REPAIR IAW EA 53100110-001.

Part: STRUCTURE — CONTAMINATED (MLG DOOR) · airframe 56,540 hrs · 59,255 cycles

UPON INITIAL GEAR EXTENSION, GEAR DID NOT EXTEND. AUX/ALT HYDRAULIC PUMPS WERE ON. ENGINE HYDRAULIC PUMPS WERE HIGH HYDRAULIC PRESSURE / QUANTITY WERE NORMAL. AFTER APPROXIMATELY 20 SECONDS, CREW RECYCLED LANDING GEAR AND GEAR EXTENDED NORMALLY. FOUND EXCESSIVE WATER COMING FROM INSIDE THE GEAR DOORS. LUBRICATED GEAR AND DRAINED WATER. OPS CHECKED GOOD IAW DC-9 MM 32-30-00-2-0003. OPS CHECKED GOOD AND NO DEFECTS NOTED.

Part: WIRE — UNSECURE (CHART HOLDER) · airframe 56,460 hrs · 59,174 cycles

FIRST OFFICERS YOKE LIGHT SPARKED WHEN LIFTED. SECURED WIRING TO CHART HOLDER IAW MM. OPS CHECKED GOOD.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,385 hrs · 59,105 cycles

RIGHT L ANGLE AT STA 965, LBL 30 - 52, HAD HEAVY CORROSION. REPLACED L ANGLE IAW DC-9 SRM.

Part: DOUBLER — CRACKED (CABIN) · airframe 56,385 hrs · 59,105 cycles

LEFT MAIN FRAME AT F.S. 699 WAS CRACKED IN FORWARD POCKET AT/BETWEEN "Z" CLIP ATTACH BOLTS. REPAIRED MAIN FRAME ON E.A. 53400110-001-1 AND DC-9 SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,385 hrs · 59,105 cycles

FLOORBEAM AT STA 995 WAS CORRODED ON THE TOP FLANGE AT LEFT BUTT LINE 46. REPAIRED FLOOR BEAM IAW DC-9 SRM.

Part: FITTING — CRACKED (CABIN) · airframe 56,385 hrs · 59,105 cycles

FORWARD SIDE OF AFT PRESSURE BULKHEAD RIGHT VENTRAL DOOR WEB SUPPORT ANGLE WAS CRACKED. REPLACED SUPPORT ANGLE IAW DC-9 SRM 51-10-4, 51-30-2 AND 51-30-5.

Part: FITTING — CRACKED (AFT CARGO) · airframe 56,385 hrs · 59,105 cycles

AFT LOWER CARGO DOOR, #3 BEAM AFT END FITTING WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #0345.

Part: FITTING — CRACKED (AFT CARGO) · airframe 56,385 hrs · 59,105 cycles

AFT LOWER CARGO DOOR, #2 BEAM FORWARD END FITTING WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #0345.

Part: CLIP — CRACKED (AFT CARGO) · airframe 56,385 hrs · 59,105 cycles

AFT LOWER CARGO DOOR, INNER ANGLE AT #2 BEAM FITTING AREA WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #0345.

Part: FITTING — CRACKED (AFT CARGO) · airframe 56,385 hrs · 59,105 cycles

AFT LOWER CARGO DOOR, #4 BEAM AFT END FITTING WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #0345.

Part: LONGERON — CRACKED (FWD. CARGO) · airframe 56,385 hrs · 59,105 cycles

LONGERON 29 LEFT CRACKED BETWEEN F.S. 579 AND 596. CRACKED ON BOTH VERTICAL FLANGES. REPAIRED LONGERON IAW REA D553-45780MR.

Part: PANEL — CRACKED (AFT CARGO) · airframe 56,385 hrs · 59,105 cycles

AFT LOWER CARGO DOOR, OUTER PAN CRACKED AT BLIND NUT AND BULGED OUT AT SAME LOCATION LOWER AFT CORNER. REPLACED AFT LOWER CORNER DOOR IAW DC-9 MM AND NON ROUTINE #0345.

Part: CLIP — CRACKED (AFT CARGO) · airframe 56,385 hrs · 59,105 cycles

AFT LOWER CARGO DOOR, #5 BEAM FORWARD END FITTING WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #0345.

Part: FRAME — CORRODED (FWD. CARGO) · corrosion level 2 · airframe 56,385 hrs · 59,105 cycles

LEVEL II CORROSION ON FRAME AT STA. 446, AFT SIDE, BETWEEN LONGERON 28 LEFT AND 28 RIGHT. REPAIRED FRAME IAW DC-9 SRM 53-03.

Part: SPLICE — CRACKED (FWD. CARGO) · airframe 56,385 hrs · 59,105 cycles

LONGERON 30 END FITTING BETWEEN F.S. 579 AND 596 CRACKED ON BOTH VERTICAL FLANGES. REPLACED END FITTINGS IAW DC-9 SRM.

Part: SKIN — CRACKED (RUDDER) · airframe 56,385 hrs · 59,105 cycles

RUDDER TOP RIGHT SIDE HAD LARGE CRACK. REPLACED RUDDER IAW DC-9 SRM.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 56,181 hrs · 58,876 cycles

UPON SELECTING GEAR DOWN, NOSE GEAR UNSAFE LIGHT ILLUMINATED AND NOSE GEAR GREEN LIGHT DID NOT COME ON. GEAR WARNING HORN SOUNDED. RECYCLED GEAR, ALL INDICATIONS NORMAL. OPS CHECKED GOOD IAW DC-9 MM 32-60.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,806 hrs · 58,485 cycles

WHEN EMERGENCY LIGHTS WERE SELECTED ON, THE PEANUT LIGHTS DID NOT ILLUMINATE. REPLACED THE EMERGENCY LIGHT BATTERY/CHARGER PACK IAW DC-9 MM.

Part: OUTFLOW VALVE — FAILED (AFT FUSELAGE)

AUTO-PRESSURIZATION WAS INOPERATIVE. AIRCRAFT WOULD NOT DEPRESSURIZE UNTIL LANDING. OBSERVED STRONG ELECTRICAL SMELL. REPLACED OUTFLOW VALVE ACTUATOR.

Part: CUSP WEB — CRACKED (BS 945)

DURING C-CHECK, FOUND CUSP WEB RIGHT SIDE CRACKED AT STATION Y-945. REPLACED CUSP WEB IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: BULKHEAD T-CAP — CORRODED (BS 617)

DURING C-CHECK, FOUND PRESSURE BULKHEAD T-CAP CORRODED AT STATION Y-617. REPAIRED T-CAP IAW ABX REA D953-32890 MR.

Part: WEB — CRACKED (BS 617)

DURING C-CHECK, FOUND CUSP WEB CRACKED AT STATION 617 RIGHT SIDE. REPLACED CUSP WEB IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: LONGERON — CRACKED (BS 598)

DURING C-CHECK, FOUND LONGERON 30 FLANGE CRACKED UNDER AFT END CAP STATION Y-598. REPAIRED LONGERON IAW DC9 SRM 53-02-00.

Part: FRAME — CRACKED (BS 1076)

DURING C-CHECK, FOUND FRAME CRACKED AT STATION 1076 AND LONGERON 13 RIGHT. REPLACED SECTION OF FRAME IAW DC9 SRM 53-03.

Part: FITTING — CRACKED (BS 1076)

DURING C-CHECK, FOUND FITTING CRACKED BELOW LONGERON 16 LEFT ON THE AFT SIDE OF STATION 1076 FRAME. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: HINGE — CRACKED (LT WING)

DURING C-CHECK, FOUND LEFT AILERON INBOARD HINGE FITTING CRACKED AT SPAR MOUNT HOLE. REPLACED HINGE IAW DACO DWG 5910515.

Part: BULKHEAD TEE — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND A CRACK INDICATION IN THE AFT PRESSURE BULKHEAD NR 6 TEE CAP. REPAIRED IAW ABX EA 53-120037-006.

Part: FRAME — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND OUTBOARD END OF THE AFT PRESSURE BULKHEAD FRAME CRACKED AT LONGERON 15 LEFT. REPAIRED IAW DC9 SRM 51-30-5 AND 51-20-0.

Part: ACTUATOR — CORRODED (LT SPOILER)

DURING C-CHECK, FOUND LEFT OUTBOARD SPOILER ACTUATOR VALVE BODY EXFOLIATED AND VALVE LINK MOUNT AREA CRACKED. REPLACED ACTUATOR IAW ABX EA 2760D019-001.

Part: WEB — CRACKED (BS 598)

DURING C-CHECK, FOUND CUSP WEB CRACKED FORWARD AND AFT OF FRAME AT STATION 598 RIGHT SIDE. REPLACED CUSP WEB IAW DC9 SRM 51-30-2 AND 51-30-1.

Part: DOUBLER — CORRODED (BS 718)

DURING C-CHECK, FOUND DOUBLER FORWARD AND AFT OF STATION 718 CORRODED. REPLACED DOUBLER IAW DC9 SRM 51-30-5.

Part: LONGERON — CORRODED (BS 1089)

DURING C-CHECK, FOUND LONGERON 14 LEFT CORRODED AT STATION 1089. REPLACED LONGERON SECTION IAW DC9 SRM 51-30-2.

Part: WEB — CRACKED (BS 598)

DURING C-CHECK, FOUND CUSP WEB CRACKED FORWARD AND AFT OF FRAME AT STATION 598, LEFT SIDE. REPLACED CUSP WEB IAW DC9 SRM 51-30-1 AND 51-30-2.

Part: PANEL — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND CORROSION ON LEFT LOWER SLANT PANEL CAP. REPAIRED IAW ABX REA D953-32811MR.

Part: DOUBLER — CORRODED (AFT FUSELAGE)

DURING C-CHECK, FOUND CORROSION AT THE AFT END OF THE PRESSURIZATION OUTFLOW VALVE SCOOP. REPLACED DOUBLER IAW DC9 SRM 51-30-2.

Part: SKIN — CRACKED (BS 897)

DURING C-CHECK, FOUND FUSELAGE SKIN BULGED AND CRACKED .125 AT FASTENER HOLE UNDER LONGERON 30 AT STA 897. REPAIRED IAW ABX REA D953-22433-MR.

Part: FITTING — CRACKED (BS 560)

DURING C-CHECK, FOUND VERTICAL SUPPORT CRACKED AT LOWER END AT LONGERON 23R AND STA 560. REPAIRED SUPPORT FITTING IAW DC9 DWG NR K05159.

Part: FRAME — CORRODED (BS 851)

DURING C-CHECK, FOUND EXFOLIATION CORROSION ON THE AFT FLANGE OF FRAME AT STA 851 BETWEEN LONGERON 29L AND 29R.

Part: ANGLE — CRACKED (LT PYLON)

DURING C-CHECK, FOUND LOWER PYLON TO FUSELAGE ATTACK ANGLE AT LEFT PYLON LEADING EDGE CRACKED. REPAIRED ANGLE IAW DC9 SRM 54-04.

Part: FITTING — CRACKED (RT TE FLAP)

DURING C-CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1.

Part: FITTING — SPLIT (BS 965)

DURING C-CHECK, FOUND FITTING ON FLOOR SUPPORT AT STA 965 AND RBL 22, BELOW AFT INBOARD EDGE OF PYLON BULKHEAD SPLIT. REPLACED FITTING IAW DC9 SRM 51-30-1.

Part: ANGLE — CRACKED (BS 980)

DURING C-CHECK, FOUND INTERCOSTAL ATTACH ANGLE CRACKED AT STA 980 BETWEEN LONGERON 27L AND 28L. REPLACED ANGLE IAW DACO DWG 9915550 AND DC9 SRM 51-30-5.

Part: FLOOR — CRACKED (BS 200-207-218)

DURING C-CHECK, FOUND SUB-FLOOR CRACKED, STA 207 AT RBL 22, STA 200 AT RBL 4, AND STA 218 AT LBL 3 AND 9. REPAIRED CRACKED SUB-FLOOR IAW DC9 SRM 53-01.

Part: FITTING — CRACKED (LT WING)

DURING C-CHECK, FOUND THE LEFT WING INBD SPOILER TORSION BAR CENTER SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-22.

Part: PROX SWITCH — DEFECTIVE (RT MLG)

AFTER TAKEOFF, RT GEAR UNSAFE LIGHT REMAINED ON. *S/D* REPLACED PROXIMITY SWITCH CONTROL AND ADJUSTED TARGET. OPS CHECKED GOOD IAW DC9 MM 32-60-03.

Part: BATTERY — DISCHARGED (CABIN)

AFTER TAKEOFF, RT GEAR UNSAFE LIGHT REMAINED ON.

Part: FLAP VANE — DELAMINATED (LT TE FLAP)

THE LEFT INBOARD FLAP VANE HAD 4 AREAS OF DELAMINATION OF THE UPPER INBOARD MIDDLE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.

Part: TR LINK — CRACKED (RT ENGINE)

DURING COMPLIANCE OF AD'S 75-14-06, 90-18-03 SB'S 78-36, 78-38, 78-40 AND 78-66, FOUND RIGHT THRUST REVERSER OUTBOARD UPPER DRIVER LINK HAD A CRACK INDICATION. REPLACED RIGHT THRUST REVERSER OUTBOARD UPPER DRIVER LINK IAW DC-9 MM 78-31-5. LINK FOUND TO BE CRACKED AND WAS SCRAPPED.

Part: BOLT — DEFECTIVE (LT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND BOLT CAUSING CHAFING ON THE LEFT MAIN LANDING GEAR OUTBOARD DOOR. REPLACED BOLT IAW DC-9 SRM 53-01.

Part: PLATE — MISSING (LT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND CHAFE STRIP MISSING ON THE LEFT MAIN LANDING GEAR OUTBOARD DOOR. REPLACED CHAFE STRIP IAW DC-9 SRM 51-20-00.

Part: SEAL — TORN (LT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE OUTBOARD TRAILING EDGE SEAL ON THE LEFT OUTBOARD MAIN LANDING GEAR DOOR TORN. REPLACED SEAL IAW DC-9 SRM 51-30-2.

Part: DRIVE LINK — CRACKED (LT SPOILER)

DURING COMPLIANCE OF AD 85-01-03 AND SB'S 27-228, 27-229 AND 27-240, FOUND THE LEFT WING OUTBOARD SPOILER DRIVE LINK HAD A CRACK INDICATION. REPLACED THE LEFT WING OUTBOARD SPOILER DRIVE LINK IAW DC-9 MM 27-61-01.

Part: TR UNIT — DEFECTIVE (NR 1 ENGINE)

JOLT FELT IN FLIGHT AT 13,000 FEET, ENGINE INSTRUMENTS NORMAL, NO COCKPIT INDICATION OF MALFUNCTION. CARGO INSPECTED IN FLIGHT BY FIRST OFFICER. EMERGENCY DECLARED FOR LANDING. LANDING NORMAL, EXCEPT LEFT ENGINE THRUST REVERSER DID NOT GET BLUE LIGHT. INSPECTION IN BLOCKS SHOWED LEFT THRUST REVERSER DAMAGE. INSPECTED NR 1 ENGINE, FOUND NR 1 THRUST REVERSER UPPER DOOR DEPLOYED. BOTH UPPER AND LOWER DOORS DAMAGED. ALSO, DAMAGE TO THE NR 1 PYLON AT THE AFT LOWER ENGINE MOUNT AREA. REMOVED NR 1 ENGINE TO FACILITATE PYLON REPAIR, THEN REINSTALLED ENGINE AFTER REPAIR, REF M17 WORKPACK. REPLACED NR 1 THRUST REVERSER ASSEMBLY AND OPS CHECKED GOOD ON GROUND RUN.

Part: DOUBLER — CRACKED (RT WINDOW FRAME)

DURING COMPLIANCE OF A.D. 90-80-3; S.B. 56-11, X-RAY INDICATED A CRACK IN THE RIGHT EYEBROW WINDOW RETAINER. REPLACED DOUBLER IAW DOUGLAS REWORK DRAWING 5952965.

Part: DOUBLER — CRACKED (LT WINDOW FRAME)

DURING COMPLIANCE OF A.D. 90-18-3; S.B. 56-11, X-RAY INDICATED CRACK IN THE LEFT EYEBROW WINDOW RETAINER. REPLACED DOUBLER IAW DOUGLAS REWORK DRAWING 5952965.

Part: BUSHINGS — WORN (RT MLG)

DURING OFF WING OVERHAUL PROCEDURES, FOUND BUSHINGS WORN. REPAIRED IAW ABX REA D932-12004-MR.

Part: JAMB — CORRODED (CARGO DOOR)

DURING C-CHECK INSPECTION, FOUND LEVEL I CORROSION ON THE AFT LOWER CARGO DOOR JAMB WEB. REPAIRED WEB IAW ABX REA D953-10732-MR.

Part: BLKHD TEE — CORRODED (FS 1039)

DURING C-CHECK INSPECTION, FOUND LEVEL I CORROSION ON BULKHEAD TEE AT STA 1039 BETWEEN LONGERON 30 AND 26L. REPAIRED TEE IAW ABX REA D953-10761-MR.

Part: FLOOR BEAM — DAMAGED (FS 996)

DURING C-CHECK INSPECTION, A PRIOR REPAIR TO THE FLOOR BEAM AT STA 996, RBL35 WAS REMOVED TO REVEAL SEVERAL CUTOUTS IN THE UPPER FLANGE OF THE ANGLE. FLOOR BEAM WAS REPAIRED IAW ABX REA D953-10768-MR.

Part: GUSSET — DAMAGED (FS 965)

DURING C-CHECK INSPECTION, FOUND A GUSSET CHAFED AT STA 965, LONGERON 4R AND 4L. REPAIRED GUSSET IAW ABX REA D953-10730-MR.

Part: PANEL — CRACKED (FS 83)

DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR UPPER WHEEL WELL PRESSURE PANEL WAS FOUND CRACKED AT STA 83. REPAIRED PANEL IAW SB 53-187.