N938AX

Part: CUSP WEB — CRACKED (AFT CARGO) · airframe 62,988 hrs · 66,767 cycles

NUMEROUS CRACKS IN LEFT CUSP WEB, FS 945 TO 965. REPLACED LEFT CUSP WEB IAW DC-9 SRM 51-30-1 AND 51-30-2.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 62,988 hrs · 66,767 cycles

LEFT CUSP CRACKED AT STA 880. REPLACED LEFT CUSP BETWEEN FS 832 TO 899 IAW DC-9 SRM 51-30-2 AND 51-30-1.

Part: SKIN — CORRODED (FUSELAGE) · airframe 62,988 hrs · 66,767 cycles

EXTERIOR FUSELGAE SKIN AT STA 180, LONGERON 30 CORRODED. REPAIRED FUSELAGE SKIN AT STA 180, LONGERON 30.

Part: FRAME — CRACKED (FUSELAGE) · airframe 62,988 hrs · 66,767 cycles

LEFT MAIN FRAME STA 718 WAS CRACKED BEYOND LIMITS. REPLACED MAIN FRAME IAW JOB CARD EA 53400323-001-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,988 hrs · 66,767 cycles

FLOORBEAM CORRODED AT STA 937, RIGHT BUTTLINE 18. REPAIRED FLOORBEAM IAW DC-9 SRM 53-05.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 62,988 hrs · 66,767 cycles

LONGERON 12 RIGHT CRACKED AT FRAME STA 944. REPAIRED LONGERON 12 RIGHT, FS FRAME 944 IAW DC-9 SRM 53-02.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 62,988 hrs · 66,767 cycles

LONGERON 17 RIGHT CRACKED AT FRAME STA 560. REPLACED DAMAGED SECTION OF LONGERON IAW DC-9 SRM 53-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,988 hrs · 66,767 cycles

SKIN WAS CRACKED AT MAIN ENTRY DOOR CUTOUT, UPPER AFT STOP. REPAIRED MAIN ENTRY DOOR CORNER IAW DC-9 SRM 53-05.

Part: WARNING LIGHT — MALFUNCTIONED (MLG) · airframe 62,952 hrs · 66,736 cycles

RT GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKE OFF. LIGHT EXTINGUISHED AFTER APPROXIMATELY 2 MINUTES FOLLOWING RECYCLING OF GEAR. UNABLE TO DUPLICATE. INSPECTED UPLOCK AND DOWNLOCK LIMIT SWITCHES AND VISIBLE WIRING IAW WIRING MANUAL. OPERATIONAL CHECK GOOD ON GEAR SWING. NO DEFECTS NOTED.

Part: HINGE — RUSTED (T/E FLAP) · airframe 62,041 hrs · 65,754 cycles

RUST BLEEDING FROM RIGHT WING CENTER FLAP HINGE INBOARD UPPER ATTACH STUD. REPLACED FORWARD CENTER FLAP HINGE IAW DC-9 MM 57-4-01-2-0001.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 62,041 hrs · 65,754 cycles

FORWARD LOWER CARGO DOOR NR 2 BEAM FORWARD FITTING CRACKED AT FASTENER. REPLACED FITTING IAW DC-9 SRM 51-30-5.

Part: DOOR — CRACKED (LT MLG) · airframe 62,041 hrs · 65,754 cycles

CRACK IN UPPER FORWARD CORNER OF INBOARD GEAR DOOR. REPLACED PAN IAW DC-9 SRM 51-30-1, 51-30-2, 51-30-5 AND 51-30-8.

Part: SWITCH — DEFECTIVE · airframe 61,224 hrs · 64,924 cycles

LEFT MAIN GEAR UNSAFE LIGHT ILLUMINATED AFTER LANDING GEAR WAS RETRACTED. LANDING GEAR HANDLE WAS RECYCLED AND LIGHT WENT OUT. REPLACED THE LEFT MAIN GEAR DOWNLOCK SWITCH. OPS CHECKED GOOD IAW DC-9 MM 32-60-01-2.

Part: PANEL — DELAMINATED (RT WING) · airframe 60,905 hrs · 64,623 cycles

UPPER INBOARD TRAILING EDGE BONDED PANEL WAS DELAMINATED. REPLACED PANEL IAW DC-9 SRM 51-30-2 AND 51-30-1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 60,905 hrs · 64,623 cycles

LONGERON 29 LEFT VERTICAL LEG CRACKED AT SPLICE BETWEEN STATION 408 - 427. REPLACED SECTION OF LONGERON 29 LEFT STATION 408 - 427 IAW DC-9 SRM 53-02, FIG 14 AND DC-9 SRM 51-30-5.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 60,905 hrs · 64,623 cycles

KEEL SUPPORT L-ANGLE CRACKED INSIDE LEFT KEEL, AFT SIDE UNDER RESERVOIR. INSTALLED NEW FITTING IAW DC-9 SRM 51-30-1, AND 51-30-5.

Part: POWER SUPPLY — INOP (CABIN)

EMERGENCY EVACUATION LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SOURCE.

Part: FITTING — CRACKED (BS 617)

DURING C-CHECK, FOUND CRACK IN FUSELAGE FRAME ATTACH FITTING AT STATION 617, BELOW LONGERON 18 RIGHT. REPLACED FITTING IAW DC9 SRM 51-10-4 AND 51-30-5.

Part: PAN — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR INNER AND OUTER PANS TO BE CRACKED. REPAIRED IAW ABX REA D952-33186.

Part: SPAR CAP — CRACKED (RT WING)

DURING C-CHECK, FOUND RIGHT WING LOWER SPAR CRACKED. REPAIRED IAW DC9 DRAWINGS M07181 AND J060173.

Part: SPAR CAP — CRACKED (RT WING)

DURING C-CHECK, FOUND RIGHT WING AFT LOWER SPAR CRACKED AT HOLE NR 4. REPAIRED IAW DC9 SERVICE REWORK DRAWING J060123 AND ABX DRAWING M07181.

Part: LONGERON — CRACKED (BS 945)

DURING C-CHECK, FOUND LONGERON 13 RIGHT CRACKED AT STATION 945. SPLICED LONGERON 13 RIGHT IAW DC9 SRM 53-02.

Part: FITTING — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR BEAM END FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: ANGLE — CRACKED (NR 2 PYLON)

DURING C-CHECK, FOUND RIGHT PYLON HAD CRACKED WEB AT LOWER ATTACH ANGLE. REPLACED ANGLE IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (BS 200)

DURING C-CHECK, FOUND LONGERON 2 LEFT CRACKED AT STATION 200. REPLACED LONGERON 2 LEFT FROM STATION 194 TO 230 IAW DC9 SRM 53-02.

Part: ANGLE — CRACKED (NR 2 PYLON)

DURING C-CHECK, FOUND RIGHT PYLON LEADING EDGE INBOARD LOWER ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 54-04.

Part: FITTING — CRACKED (LT WING)

DURING C-CHECK, FOUND FITTING CRACKED AT LEFT WING SLAT DRIVE. REPLACED FITTING IAW ABX REA D957-33196.

Part: FRAME — CRACKED (BS 658)

DURING C-CHECK, INSPECTION FOUND FUSELAGE FRAME STATION 658 CRACKED BELOW LONGERON 18 LEFT. REPAIRED FRAME IAW DC9 SRM 53-03.

Part: LONGERON — CRACKED (BS 945)

DURING C-CHECK, INSPECTION FOUND LONGERON 17 RIGHT CRACKED AT STATION 945. REPAIRED IAW DC9 SRM 53-02.

Part: LONGERON — CRACKED (BS 965)

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

Part: BATTERY — DEPLETED (CABIN)

EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES.

Part: LATCH — DEFECTIVE (COCKPIT DOOR)

COCKPIT ENTRY DOOR LATCH STICKS, WOULD NOT RELEASE. REPLACED COCKPIT ENTRY LATCH.

Part: LATCH — LOOSE (COCKPIT DOOR)

COCKPIT DOOR WAS JAMMED. SECURED HARDWARE ON DOOR LATCH ASSY.

Part: CUSP WEB — CRACKED (BS 408)

DURING C-CHECK, FOUND RIGHT CUSP WEB AT STATION 408 CRACKED. REPLACED CUSP WEB IAW DC9 SRM 51-30-2.

Part: BULKHEAD ANGLE — CORRODED (BS 690)

DURING C-CHECK, FOUND THE SLANT PANEL ANGLE STATION 690 AND LBL 8 CORRODED. REPAIRED ANGLE IAW ABX REA D953-22465-MR.

Part: LONGERON — CRACKED (BS 718)

DURING C-CHECK, FOUND LONGERON NR 1 CRACKED AT STA 718. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: FITTING — CRACKED (BS 965)

DURING C-CHECK, FOUND VERTICAL SUPPORT FITTING AT STA 965 FLOORBEAM CRACKED ON RIGHT SIDE IN AFT LOWER CARGO COMPT. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: LONGERON — CRACKED (BS 699)

DURING C-CHECK, FOUND LONGERON 6L CRACKED AT STA 699. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: LONGERON — CRACKED (BS 945)

DURING C-CHECK, FOUND LONGERON 16L CRACKED FORWARD OF STA 945. REPLACED LONGERON FROM STA 935-965 IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: WEB — CRACKED (NR 2 PYLON)

DURING C-CHECK, FOUND RIGHT PYLON VERTICAL WEB CRACKED FORWARD AND INBOARD OF THE AFT ENGINE MOUNT. REPLACED WEB IAW DC9 SRM 54-10-00 AND 51-10-5.

Part: ANGLE — CRACKED (NR 2 PYLON)

DURING C-CHECK, FOUND RIGHT PYLON TO FUSELAGE UPPER ATTACH ANGLE CRACKED AT STA 980. REPLACED ANGLE IAW DC9 SRM 54-04.

Part: SUBFLOOR — CRACKED (BS 149)

DURING C-CHECK, FOUND THE SUBFLOOR DIAPHRAM CRACKED AT STA 149, BL 0.0 AND STA 160 BL 0.0. REPAIRED SUBFLOOR IAW DC9 SRM 53-01.

Part: ANGLE — CRACKED (NR 1 PYLON)

DURING C-CHECK, FOUND ANGLE JUST INBD OF AFT ENGINE MOUNT IN NR 1 PYLON CRACKED AT LOWER FASTENER. REPLACED ANGLE IAW DC9 SRM 51-30-1.

Part: LONGERON — CRACKED (BS 639)

DURING C-CHECK, FOUND LONGERON 3R CRACKED AT STA 639. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: INTERCOSTAL — CRACKED (BS 996)

DURING C-CHECK, FOUND INTERCOSTAL CRACKED AFT OF STATION 996 AT LONGERON 5R. REPAIRED INTERCOSTAL IAW DC9 SRM K05159.

Part: FITTING — CORRODED (WS 477)

DURING C-CHECK, FOUND THE RIGHT WING, LOWER OUTBOARD HORIZONTAL FLANGE OF THE BULKHEAD/AILERON HINGE FITTING AT STA XRS477 INSIDE THE FUEL VENT TANK CORRODED BEYOND LIMITS. INSTALLED REPAIR IAW ABX REA D957-22556MR.

Part: WEB — CRACKED (BS 617-639)

DURING C-CHECK, FOUND THE LEFT CUSP WEB CRACKED AT STA 617, 639 AND 658. REPLACED CUSP WEB IAW DC9 SRM 51-10-04.

Part: FITTING — CRACKED (BS 680)

DURING C-CHECK, FOUND FLOORBEAM VERTICAL SUPPORT FITTING AT STA 680 AND LBL 44 CRACKED. REPLACED FITTING IAW DC9 SRM 51-10-4.

Part: BLKHD DOUBLER — CRACKED (AFT PRESS BULKHD)

DURING C-CHECK COMPLIANCE WITH S/B 53-137, FOUND DOUBLER CRACKED RADIALLY IN UPPER RIGHT AND UPPER LEFT CORNERS. REPAIRED DOUBLER IAW ABX REA D953-22492-MR AND DC9 S/B 53-137.

Part: LONGERON — CRACKED (FUSELAGE)

DURING C-CHECK, FOUND LONGERON 17R CRACKED AT STATIONS 275, 313, 389, AND 408. REPAIRED CRACKED SECTIONS OF LONGERON IAW DC9 SRM 53-02.

Part: INTERCOSTAL — CORRODED (BS 996)

DURING C-CHECK, FOUND INTERCOSTAL AT STA 996 AND LONGERON 13L EXFOLIATED. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-5.

Part: INTERCOSTAL — CORRODED (BS 945-965)

DURING C-CHECK, FOUND INTERCOSTAL AT STA 945-965 AND LONGERON 29 RT CORRODED. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2.

Part: CUSP WEB — CORRODED (BS 218-237)

DURING C-CHECK, FOUND CUSP WEB AT STA 218-237 RIGHT SIDE CORRODED. REPAIRED CUSP WEB IAW DC9 SRM 51-30-1.

Part: CUSP WEB — CRACKED (BS 200-218)

DURING C-CHECK, FOUND CUSP WEB AT STA 200-218 RIGHT SIDE CRACKED. REPAIRED CUSP WEB IAW ABX REA D953-22396-MR.

Part: FITTING — CORRODED (BS 237)

DURING C-CHECK, FOUND THE RIGHT FRAME FOOT AT STA 237 CORRODED. REPLACED FRAME FOOT IAW DC9 SRM 51-30-1.

Part: SKIN — CRACKED (BS 996)

DURING C-CHECK COMPLIANCE WITH AD 96-10-11 AND S/B DC9-53A147, FOUND CRACKS IN EXTERIOR SKIN AT FS 996 BETWEEN LONGERONS 2L-3L, 3L-4L, 4L-5L AND 5L-6L. REPAIRED CRACKS IAW ABX EA 53-11005-104.

Part: FITTING — CORRODED (BS 256)

DURING C-CHECK, FOUND THE RIGHT FRAME FOOT AT STA 256 CORRODED. REPLACED FRAME FOOT IAW DC9 SRM 51-30-1.

Part: SKIN — CORRODED (BS 996)

DURING C-CHECK COMPLIANCE WITH AD 96-10-11 AND S/B 53A147, FOUND CRACKS IN EXTERIOR SKIN AT FS 996 BETWEEN LONGERONS 3R-4R. REPAIRED CRACKS IAW ABX EA 53-11005-104.

Part: ANGLE — CRACKED (BS 186)

DURING C-CHECK, FOUND FORWARD LT ENTRY DOOR DRAIN PAN SUPPORT ANGLE CRACKED AT LBL 55 AND STATION 186. REPLACED ANGLE IAW DC9 SRM 51-30-8.

Part: WINDOW — OUT OF ADJUST (COCKPIT)

FIRST OFFICER'S CLEARVIEW SLIDING WINDOW (EMERG EXIT) WAS BINDING. ADJUSTED WINDOW IAW DC9 MM 56-10-3.

Part: WINDOW — OUT OF ADJUST (COCKPIT)

CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN FULLY. BINDS WHEN UNLOCKED. ADJUSTED CAPTAIN' S CLEAR VIEW WINDOW IAW DC9 MM 56-10-03.

Part: LATCH — WORN (COCKPIT DOOR)

AFTER LANDING, COCKPIT DOOR WAS JAMMED AND WOULD NOT OPEN FROM INSIDE. THE COCKPIT. REPLACED COCKPIT DOOR LOCK.

Part: DOOR — JAMMED (COCKPIT)

DURING POST-FLIGHT INSPECTION, FOUND COCKPIT DOOR JAMMED AND WOULD NOT OPEN. LUBRICATED COCKPIT DOOR AND OPERATED SEVERAL TIMES. DOOR OPERATES NORMAL IAW DC9 MM CHAPTER 52.

Part: BATTERIES — DISCHARGED (CABIN)

EMERGENCY LIGHTS IN COCKPIT WEAK. REPLACED EMERGENCY LIGHT BATTERIES.

Part: FITTING — CRACKED (RT SPOILER)

DURING COMPLIANCE OF AD 85-01-03 AMEND 39-4977: RT OUTBOARD SPOILER FITTING CRACKED. REPLACED FITTING IAW DC-9 M/M 27-61-1.

Part: WINDOW ASSY — LACK OF LUBE (RT COCKPIT)

FIRST OFFICERS CLEAR VIEW WINDOW HARD TO OPEN AND OCCASIONALLY BINDS. LUBED FIRST OFFICERS CLEAR VIEW WINDOW ASSEMBLY.

Part: TEE CAP — CORRODED (WS 69)

DURING C-CHECK INSPECTION, FOUND CORROSION ON STA XRS 69 T-CAP IN THE LEFT WING. REPAIRED IAW ABX REA D957-15418-MR.

Part: FITTING — CRACKED (LT TE FLAP)

DURING C-CHECK INSPECTION, FOUND ATTACH FITTINGS INSIDE THE LEFT FLAP CRACKED. REPLACED IAW DC-9 SRM 51-30-2.

Part: FITTING — CRACKED (LT TE FLAP)

DURING C-CHECK INSPECTION, FOUND ATTACH FITTINGS INSIDE THE LEFT FLAP CRACKED. REPLACED IAW DC-9 SRM 51-30-2.

Part: SPAR — CORRODED (LT WING)

DURING C-CHECK INSPECTION, FOUND CORROSION ON THE LEFT WING UPPER SPAR. REPAIRED IAW ABX REA D957-15400-MR.

Part: SPAR — CORRODED (LT WING)

DURING C-CHECK INSPECTION, FOUND CORROSION ON THE LEFT WING LOWER SPAR. REPAIRED IAW ABX REA D957-15400-MR.

Part: FRAME — ELONGATED HOLES (BS 718)

DURING C-CHECK INSPECTION, FOUND HOLES ELONGATED ON THE FRAMES AT STA 718 LEFT AND RIGHT. REPAIRED IAW ABX REA D953-15434-MR.

Part: FRAME — ELONGATED HOLES (BS 718)

DURING C-CHECK INSPECTION, FOUND HOLES ELONGATED ON THE FRAMES AT STA 718 LEFT AND RIGHT. REPAIRED IAW ABX REA D953-15434-MR.

Part: STRINGER — CORRODED (RT WING)

DURING C-CHECK INSPECTION, FOUND STRINGER NR 12 IN THE RIGHT WING CORRODED. REPAIRED IAW ABX REA D957-15435-MR.

Part: SKIN — OIL CANNING (BS 996 - 1019)

DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN OIL CANNING BELOW THE NR 2 PYLON AT STA 996 TO 1019. REPAIRED IAW ABX REA D953-15411-MR.

Part: BULKHEAD DOUBLER — DOUBLE DRILLED (BS 996)

DURING C-CHECK INSPECTION, FOUND A DOUBLE DRILLED HOLE ON THE AFT PRESSURE BULKHEAD ABOVE THE RIGHT UPPER CORNER OF THE VENTRAL DOOR. REPAIRED IAW ABX REA D953-15423-MR.

Part: BULKHEAD DOUBLER — CRACKED (AFT FUSELAGE)

DURING C-CHECK INSPECTION, FOUND CRACKED AFT PRESSURE BULKHEAD STIFFENER DOUBLER BETWEEN LONGERONS 15L AND 16L. REPLACED IAW DC-9 SRM 51-30-5.

Part: BULKHEAD CLIP — CRACKED (AFT FUSELAGE)

DURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD STIFFENER ATTACH CLIP CRACKED AT LONGERON 14R. REPLACED IAW DC-9 SRM 51-30-5.

Part: SKIN — GOUGED (BS 332)

DURING C-CHECK INSPECTION, FOUND GOUGE IN THE FUSELAGE SKIN AT STATION 332, LONGERON 23R. REPAIRED IAW ABX REA D953-15370-MR.

Part: CLIP — CRACKED (BS 996)

DURING C-CHECK INSPECTION, FOUND CRACKED CLIP AT CUSP WEB TO FRAME STA 996 AT LONGERON 18L. REPLACED CLIP IAW DC-9 SRM 51-10-4 AND 51-30-5.

Part: BRACKET — CRACKED (RT TE FLAP)

DURING C-CHECK INSPECTION, FOUND RIGHT FLAP BRACKETS CRACKED AT STA 353. REPLACED IAW DC-9 SRM 51-30-2.

Part: BRACKET — CRACKED (RT TE FLAP)

DURING C-CHECK INSPECTION, FOUND RIGHT FLAP BRACKETS CRACKED AT STA 353. REPLACED IAW DC-9 SRM 51-30-2.

Part: SCRAPER — WORN (HORIZ STAB)

DURING C-CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE ICE SCRAPER HAD A HOLE IN IT. REPAIRED IAW DC-9 SRM 55-01 FIGURE 2, SHEET 2.

Part: LINK — WORN (LT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, INSPECTION OF THE LEFT MAIN LANDING GEAR DOOR AND ATTACHMENTS, FOUND THE ARTICULATING DOOR LINK HAD EXCESSIVE PLAY. REPLACED THE LEFT ARTICULATING DOOR LINK ATTACH BOLT.

Part: SKIN — CORRODED (RT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-244 INSPECTION OF THE RIGHT MAIN LANDING GEAR DOOR AND ATTACHMENTS, FOUND A SKIN BULGE ON THE ARTICULATING DOOR. REPLACED THE RIGHT MAIN LANDING GEAR ARTICULATING DOOR IAW DC-9 MM 32-12-1.

Part: WINDOW — OUT OF ADJUST (LT COCKPIT)

DURING PREFLIGHT, BOTH CAPTAIN'S AND FIRST OFFICER'S SLIDING WINDOWS LOCKING MECHANISM LOCATED ON THE TOP FORWARD PART OF THE WINDOW, INTERMITTENTLY WILL NOT RELEASE. THIS RESULTING IN THE WINDOW NOT OPENING. ADJUSTED CAPTAIN'S AND FIRST OFFICER'S SLIDING WINDOWS IAW DC-9 MM 56-10. OPS CHECKED GOOD.

Part: WINDOW — OUT OF ADJUST (RT COCKPIT)

DURING PREFLIGHT, BOTH CAPTAIN'S AND FIRST OFFICER'S SLIDING WINDOWS LOCKING MECHANISM LOCATED ON THE TOP FORWARD PART OF THE WINDOW, INTERMITTENTLY WILL NOT RELEASE. THIS RESULTING IN THE WINDOW NOT OPENING. ADJUSTED CAPTAIN'S AND FIRST OFFICER'S SLIDING WINDOWS IAW DC-9 MM 56-10. OPS CHECKED GOOD.