N902AX

Part: WIRE — DAMAGED (COCKPIT) · airframe 55,123 hrs · 58,656 cycles

DURING TAXI, WHEN FIRST OFFICER PERFORMED TAXI CHECK LIST, THERE WAS A POPPING SOUND AND SPARKS EMITTING FROM THE OVERHEAD ON THE CAPTAIN'S SIDE. REPLACED LEFT WINDSHIELD ANTI-ICE TEMPERATURE SENSOR WIRING IAW DC-9 MM 20-50-01-2. OPS CHECKED GOOD.

Part: BRACKET — CRACKED (LT MGL WW) · airframe 54,861 hrs · 58,438 cycles

LEFT LATERAL CONTROL MIXER BRACKET CRACKED. REPLACED LEFT LATERAL CONTROL MIXER IAW DC-9 MM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 54,861 hrs · 58,438 cycles

LONGERON 30 HEAVILY PITTED AT FS 756. REPAIRED AREA IAW DC-9 SRM 53-01.

Part: SHEAR TIE — CRACKED (AFT CARGO) · airframe 54,861 hrs · 58,438 cycles

FS 996 BETWEEN LONGERON 18 RIGHT - LONGERON 19 RIGHT, SHEAR TIE CRACKED. REPLACED SHEAR TIE AT STA 996, LONGERON 18 RIGHT - LONGERON 19 RIGHT IAW DC-9 SRM 51-30-5.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,861 hrs · 58,438 cycles

CORRODED SKIN BULGING FS 950 - 960, APPROXIMATELY BETWEEN LONGERON 27 RIGHT - LONGERON 29 RIGHT. REPAIRED AREA IAW DC-9 SRM 51-30-2.

Part: WEB — CRACKED (FUSELAGE) · airframe 54,861 hrs · 58,438 cycles

CUSP WEB CRACKED AT STA 889 TO 929, LEFT SIDE. REPLACED CUSP WEB FROM LEFT BUTT LINE 55, FS 900 - FS 965 IAW DC-9 SRM.

Part: RIB — CRACKED (RT. ELEVATOR) · airframe 54,704 hrs · 58,302 cycles

RIGHT ELEVATOR CRACKED ON INBOARD BULKHEAD COMMON TO FORWARD TORQUE TUBE. CRACK WAS IN LOWER FLANGE AT SPLICE AREA TO HINGE FITTING. VERIFIED WITH X-RAY AND BORESCOPE VISUAL. REPLACED RIGHT ELEVATOR IAW DC-9 MM.

Part: FILTER — LEAKING (LT ENGINE) · airframe 54,700 hrs · 58,298 cycles

WHILE CLIMBING THRU 14,000 FT, LEFT OIL PRESSURE LOW LIGHT CAME ON. OIL PRESSURE SHOWED ABOUT 15 PSI. OIL QUANTITY RAPIDLY DECREASED TOWARDS ZERO. SHUT DOWN THE LT ENGINE. INSPECTED AND FOUND NR 1 ENGINE OIL FILTER HOUSING HAD 1 EA. STUD PULLED LOOSE, OIL DISPERSED THRU CAP. REPLACED THE NR 1 ENGINE IAW MM. (JOB CARDS UNDER W.O. NR 600163221).

Part: SWITCH — DEFECTIVE · airframe 54,430 hrs · 58,089 cycles

AFTER TURNING ON WINDSHIELD HEAT, A BURNING SMELL WAS NOTED IN THE COCKPIT. THE SMELL WENT AWAY AFTER TURNING OFF WINDSHIELD HEAT. REPLACED THE WINDSHIELD HEAT SWITCH. OPS CHECKED GOOD IAW DC-9 MM.

Part: SWITCH — DEFECTIVE · airframe 54,430 hrs · 58,089 cycles

WITH ANTI-FOG CIRCUIT BREAKERS PULLED, NO BURNING SMELL NOTED. WITH ANTI-FOG CIRCUIT BREAKERS IN, A BURNING SMELL WAS NOTED. REPLACED THE WINDSHIELD HEAT SWITCH. OPS CHECKED GOOD IAW DC-9 MM.

Part: ODOR — DETECTED (COCKPIT) · airframe 54,423 hrs · 58,083 cycles

STRONG ELECTRICAL BURNING SMELL IN COCKPIT. VERIFIED SMELL. INSPECTED EPC, RELAY PANEL, E&E COMPARTMENT AND THE GYRO COMPARTMENT. OPERATED PACK ONE AT A TIME. NO SMELL NOTED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,872 hrs · 57,696 cycles

EMERGENCY LIGHTS INTERMITTENTLY INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC-9 MM 33-53-02-4.

Part: TRIM MOTOR — CONTAMINATED (AILERON)

UNABLE TO MOVE AILERON TRIM KNOB IN CRUISE FLIGHT. INSPECTED AILERON TRIM TAIL SYSTEM. FOUND AFT ACTUATOR TO HAVE WATER CONTAMINATION. CLEANED, INSPECTED AND LUBED LEFT AND RIGHT TRIM ACTUATOR AS PER DC9 O/H MANUAL 27-10-6. PERFORMED AILERON TRIM CONTROL CABLE TENSION CHECK AND AILERON TRIM TAB TRAVEL CHECK. OPS CHECKED GOOD IAW DC9 MM 27-10-02. NO FURTHER DEFECTS NOTED.

Part: BULKHEAD — CRACKED (FUSELAGE)

DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED ON RIGHT SIDE. REPAIRED AFT PRESSURE BULKHEAD IAW DC9 SRM 53-05.

Part: FITTING — CRACKED (BS 965)

DURING C-CHECK, FOUND FITTING AT STATION 965 RBL 36 JUST BELOW FORWARD RIGHT PYLON CRACKED. REPLACED FITTING IAW DC9 SRM.

Part: CLIP — CRACKED (FUSELAGE)

DURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD HORIZONTAL STIFFENER, 4TH UP FROM FRP RIGHT SIDE, CLIP CRACKED. REPLACED CLIP IAW DC9 SRM 51-30-5.

Part: STIFFENER — CRACKED (FUSELAGE)

DURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD STIFFENER LEFT SIDE, 4TH UP FROM FRP AT OUTBOARD END CRACKED. REPAIRED STIFFENER IAW DC9 SRM DWG K05159.

Part: FITTING — CRACKED (FUSELAGE)

DURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB FITTING CRACKED AT INBOARD END OF THIRD HORIZONTAL STIFFENER RIGHT SIDE. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FRAME — CORRODED (BS 917)

DURING C-CHECK, FOUND THE FUSELAGE FRAME AT STATION 917 AND LONGERON 23 LEFT CORRODED. REPLACED FRAME IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FITTING — CRACKED (FUSELAGE)

DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD DOOR JAMB FITTING CRACKED AT INBOARD END OF FIRST HORIZONTAL STIFFENER LEFT SIDE. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: PAN — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND THE AFT LOWER CARGO COMPARTMENT DOOR OUTER PAN CRACKED IN THREE PLACES. REPAIRED DOOR PAN IAW ABX REA D95234667.

Part: FITTING — CRACKED (BS 636)

WHILE COMPLYING WITH A C-CHECK INSPECTION FOUND LONGERON FITTING CRACKED AT STATION 636 AND LONGERON 29 RIGHT. REPLACED BRACKET IAW DC9 SRM 51-30-5.

Part: LATCH — LOOSE (COCKPIT DOOR)

COCKPIT DOOR WOULD NOT OPEN FROM OUTSIDE. INTERNAL LATCH TRACK HAD JUMPED TRACK DUE TO LOOSE SCREW. RESET TRACK AND TIGHTENED SCREW.

Part: SWITCH — DEFECTIVE (RT NLG)

WHEN LANDING GEAR WAS EXTENDED, GEAR DOOR OPEN LIGHT WOULD NOT EXTINGUISH. RECYCLED GEAR, LIGHT WOULD NOT GO OUT WITH GEAR IN THE UP POSTION. PERFORMED ABNORMAL PROCEDURE. LANDING WAS UNEVENTFUL. REPLACED RIGHT INBOARD GEAR DOWN SWITCH.

Part: FITTING — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND AFT LOWER CARGO COMPARTMENT DOOR INTERIOR FITTING P/N 3914025-502 CRACKED AT DOOR LEADING EDGE NEXT TO UPLATCH MECHANISM. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: FITTING — CORRODED (BS 313)

DURING C-CHECK, FOUND FRAME MOUNT FITTING AT STATION 313, RIGHT SIDE CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: SHEAR TIE — CRACKED (FRAME 945)

DURING C-CHECK, FOUND SHEAR-TIE CRACKED BETWEEN LONGERONS 14R AND 16R AT FRAME 945. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2.

Part: ANGLE — CRACKED (NR 2 PYLON)

DURING C-CHECK, FOUND THE RIGHT PYLON INTERIOR ATTACH ANGLE CRACKED AT THE AFT ENGINE MOUNT UPPER SPAR LUG. REPLACED ANGLE IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: FITTING — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND AFT LOWER CARGO DOOR FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: FITTING — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND AFT LOWER CARGO COMPARTMENT DOOR INTERIOR FITTING P/N 3914025-2 CRACKED. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: SHEAR TIE — CRACKED (FRAME 945)

DURING C-CHECK, FOUND SHEAR-TIE CRACKED BETWEEN LONGERONS 14L AND 16L AT FRAME 945. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS IN COCKPIT ILLUMINATED WHEN POWER WAS REMOVED. REPLACED EMERGENCY BATTERY POWER SUPPLY IAW SUPP MM 33-53-0.

Part: WINDOW — LACK OF LUBE (RT COCKPIT)

FIRST OFFICER'S WINDOW WAS BINDING WHEN OPENED. CHECKED RIGGING OF FIRST OFFICER'S CLEAR VIEW WINDOW AND LUBRICATED WINDOW IAW DC-9 MM.

Part: WINDOW — FROZEN (LT COCKPIT)

CAPTAINS WINDOW DIFFICULT TO OPEN. COULD NOT DUPLICATE, SUSPECT ICE, OPS CHECKED GOOD PER DC-9 MM 56-10-3.

Part: BUSHING — CRACKED (RT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-244 R2 FOUND BUSHING, CRACKED ON RT SIDE OF AIRCRAFT, ON WING MOUNTED SECTION OF HINGE, MAIN LANDING GEAR DOOR. REPLACED BUSHING PER DC-9 OVERHAUL MANUAL 20-10-7.

Part: DOOR JAMB — NOT TRIMMED (BS 996)

DURING C-CHECK, AFT VENTRAL DOOR LOWER JAMB WEBS WERE FOUND TO HAVE A PRIOR TRIM OUT ALONG AFT EDGE. ALSO, DURING COMPLIANCE WITH AD 85-01-02. REPAIRED IAW ABX REA D953-16420-MR.

Part: RIVETS — MISINSTALLED (BS 256-313)

DURING C-CHECK AND COMPLIANCE WITH AD 96-07-51, FOUND CHERRY RIVETS INSTALLED IN FUSELAGE SKIN REPAIRS FROM STA 256 TO 313. REMOVED CHERRY LOCK RIVETS AND INSTALLED SOLID FASTENERS IAW DC-9 SRM 51-30-2, 53-30-5, 51-30-1.

Part: LONGERON — CORRODED (BS 160 218)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEVEL 2 CORROSION ON LONGERONS 28R, SKIN AND FRAMES AT STA 160 TO 200. REPLACED IAW DC-9 SRM 51-30-2, 51-30-5.

Part: LONGERON — CORRODED (BS 160-218)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEVEL 2 CORROSION ON LONGERONS 29R, SKIN AND FRAMES AT STA 160 TO 200. REPLACED IAW DC-9 SRM 51-30-2, 51-30-5.

Part: LONGERON — CORRODED (BS 160-218)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEVEL 2 CORROSION ON LONGERONS 30R, SKIN AND FRAMES AT STA 160 TO 200. REPLACED IAW DC-9 SRM 51-30-2, 51-30-5.

Part: DOUBLER — CORRODED (BS 160-218)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEVEL 2 CORROSION ON LONGERONS, SKIN AND FRAMES AT STA 160 TO 200. REPLACED DOUBLER IAW DC-9 51-30-2, 51-30-5.

Part: LONGERON — CORRODED (BS 160-218)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEVEL 2 CORROSION ON LONGERONS 27R, SKIN AND FRAMES AT STA 160 TO 200. REPLACED IAW DC-9 SRM 51-30-2, 51-30-5.

Part: LONGERON — CORRODED (BS 160-218)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEVEL 2 CORROSION ON LONGERONS 29L, SKIN AND FRAMES AT STA 160 TO 200. REPLACED IAW DC-9 SRM 51-30-2, 51-30-5.

Part: FLOORBEAM — DRILLED (BS 965)

DURING C-CHECK, FOUND A MISDRILLED HOLE IN UPPER CAP OF FLOORBEAM AT STA 965. REPAIRED IAW ABX REA D953-16391-MR.

Part: FRAME — CORRODED (BS 180)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEVEL 2 CORROSION ON LONGERONS 30R, SKIN, FRAMES AT STA 160 TO 218. REPAIRED FRAME IAW DC-9 SRM 53-04, FIGURE 2A.

Part: FORMER — DEFECTIVE (BS 980)

DURING C-CHECK, THE FOOT OF THE FORMER AT STA 980 WAS REMOVED. REPAIRED IAW ABX REA D953-16348-MR.

Part: BEAM — CRACKED (SERVICE DOOR)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND TOP HORIZONTAL BEAM CRACKED ON SERVICE DOOR. REPLACED IAW DC-9 SRM 51-30-2, 51-30-5.

Part: LONGERON — DAMAGED (BS 256)

DURING C-CHECK AND COMPLIANCE WITH AD 96-07-51, FOUND LONGERON 2L DAMAGED AT STA 256. REPAIRED IAW DC-9 SRM 53-02, FIGURE 2.

Part: TAB — CRACKED (RUDDER)

FOUND RUDDER TAB TRAILING EDGE CRACKED AND DENTED. REPAIRED TRAILING EDGE SKINS PER DC9 SRM 51-70-2.

Part: BEAM — CRACKED (SERVICE DOOR)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND SECOND FROM TOP HORIZONTAL BEAM CRACKED ON SERVICE DOOR. REPLACED IAW DC-9 SRM 51-30-2, 51-30-5.

Part: VORTILON — DENTED (LT WING)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEFT WING VORTILON LEADING EDGE WITH PIN HOLES AND DENTS. REPAIRED IAW ABX REA 953-16330.

Part: SKIN — DENTED (BS 180)

DURING C-CHECK, DENTS WERE FOUND ON FUSELAGE SKIN AT FS 180 BETWEEN LONGERONS 20R TO 23R. REPAIRED IAW ABX REA D953-16160-MR.

Part: SKIN — DENTED (BS 229)

DURING C-CHECK, FUSELAGE SKIN AT 229 WAS FOUND DENTED AND CRACKED. REPAIRED IAW ABX REA D953-16209-MR.

Part: VANE — GOUGED (RT TE FLAP)

RIGHT HAND INBOARD FLAP VANE HAS GOUGED SKINS. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.

Part: FLOORBEAM — CORRODED (BS 200)

DURING C-CHECK, FOUND STA 200 FLOORBEAM UPPER CAP CORRODED AND WAS BLENDED OUT OF LIMITS. REPAIRED IAW ABX REA D953-16329-MR.

Part: DOUBLER — CRACKED (RT COCKPIT)

DURING COMPLIANCE OF AD 90-18-03; SB 56-11 REV 3, EAAD 56-3956-MA, FOUND STEEL DOUBLER CRACKED AT UPPER AFT CORNER OF THE RIGHT EYEBROW WINDOW FRAME. REPLACED DOUBLER IAW DC-9 SRM 51-30-2.

Part: DOUBLER — CRACKED (LT EYEBROW)

DURING COMPLIANCE OF AD 90-18-03; SB 56-11 REV 3; EAAD 56-3956MA, FOUND DOUBLER CRACKED AT UPPER AFT CORNER OF LEFT EYEBROW WINDOW FRAME. REPLACED DOUBLER IAW DC-9 SRM 51-30-2.

Part: CYL ATTACH — CORRODED (LT MLG)

DURING OFF WING OVERHAUL PROCEDURES, FOUND CORROSION IN THE ATTACHMENT HOLES. REPAIRED IAW ABX REA D932-12028-MR.

Part: BUSHING — WORN (BS 111)

DURING C - CHECK INSPECTION WHILE COMPLYING WITH A.D. 91-22-07; A.S.B. 32-244, FOUND THAT THE OUTBOARD GEAR DOOR ACTUATOR ROD END BUSHING WAS WORN. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: DNLOCK SWITCH — DEFECTIVE (NLG)

ON APPROACH, THE NOSE GEAR DOWN LIGHT DID NOT ILLUMINATE. VISUALLY CHECKED GEAR FOR DOWN AND LOCKED, CONTINUED WITH NORMAL OPERATION IAW DC9 ABNORMAL CHECKLIST. REMOVED AND REPLACED THE NOSE DOWN LOCK SWITCH IAW DC 9 MM. SYSTEM OPS CHECKED GOOD.

Part: VANE — CORRODED (LT TE FLAP)

DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE LEFT WING UPPER MOVEABLE VANE. REPLACED VANE IAW DC-9 M.M. 27-51-2.

Part: VANE — CRACKED (LT TE FLAP)

DURING C-CHECK INSPECTION, FOUND THE LEFT WING CENTER FIXED VANE CRACKED AT THE CENTER SUPPORT. REPLACED VANE IAW DC-9 M.M. 27-51-3.

Part: VANE — CORRODED (LT TE FLAP)

DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE LEFT WING INBOARD FLAP FIXED VANE. REPLACED VANE IAW DC-9 M.M. 27-51-3.

Part: VANE — CORRODED (LT TE FLAP)

DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE LEFT WING OUTBOARD FLAP FIXED VANE. REPLACED VANE IAW DC-9 M.M. 27-51-3.

Part: FLOOR BEAM — CORRODED (FS 935)

DURING C-CHECK INSPECTION, FOUND CORROSION ON THE L0WER FLANGE OF THE FLOOR BEAM AT STA 935, RBL 15. REPAIRED FLOOR BEAM IAW ABX REA D953-10973-MR.

Part: DOUBLER — CORRODED (BS 585)

DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON AN INTERNAL DOUBLER UNDER LONGERON 26L AT STA 585. REPAIRED DOUBLER IAW ABX REA D953-10868-MR.

Part: INTERCOSTAL — CRACKED (BS 560-579)

DURING C-CHECK INSPECTION, FOUND A CRACK IN THE INTERCOSTALS BETWEEN STA 560 AND STA 579, BETWEEN LONGERONS 27 AND 28. REPAIRED INTERCOSTALS IAW ABX REA D953-10925-MR.

Part: SKIN — CORRODED (FS 917)

DURING C-CHECK INSPECTION, FOUND CORROSION ON THE FUSELAGE SKIN IN THE AREA OF THE NR 1 DOOR STOP OF THE AFT LOWER CARGO DOOR. REPAIRED FUSELAGE SKIN IAW ABX REA D953-10873-MR.

Part: SKIN — CORRODED (BS 813)

DURING C-CHECK INSPECTION FOUND CORROSION IN THE FUSELAGE SKIN LAP AT STA 813, LONGERON 26L FUSELAGE SKIN REPAIRED IAW ABX REA D953-10877-MR.

Part: TEE CAP — CORRODED (XCW 58.5)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING A.D. 90-18-03; S.B. 57-98, FOUND A CRACK AND CORROSION ON THE LEFT WING LOWER STA 58.5 TEE CAP. REPLACED TEE CAP IAW EA AD-57-03766-MR.

Part: TAB — CORRODED (RT ELEVATOR)

DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE RIGHT ELEVATOR GEAR TAB. REPLACED TAB IAW DC-9 M.M. 27-30-4.

Part: TEE CAP — CORRODED (XCW 58.5)

DURING C-CHECK INSPECTION, WHILE ACCOMPLISHING A.D. 90-18-03; S.B. 57-98, FOUND A CRACK AND CORROSION ON THE LEFT WING LOWER TEE CAP AT STA XCW 58.5. RIGHT WING TEE CAP WAS ALSO REPLACED DUE TO DISCREPANCIES NOTED ON THE LEFT TEE CAP IAW EA AD-57-03766-MR.

Part: SKIN — CORRODED (FS 110)

DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE STA 110 FUSELAGE SKIN. REPAIRED FUSELAGE SKIN IAW ABX REA D953-10867-MR.

Part: BLKHD TEE — CORRODED (FS 110)

DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE STA 110 BULKHEAD LOWER TEE CAP. TEE CAP WAS REPAIRED IAW ABX REA D953-10867-MR.

Part: SKIN — DENTED (FS 218.0)

DURING C-CHECK INSPECTION, FOUND A DENT ON THE FUSELAGE SKIN AT STA 218, LONGERON 17L. REPAIRED FUSELAGE SKIN IAW ABX REA D953-10854-MR.

Part: TRAP PANEL — CRACKED (CENTER FUSELAGE)

DURING C-CHECK INSPECTION, THE RIGHT TRAPEZOIDAL PANEL WAS FOUND CRACKED BETWEEN THREE EACH BOLTS ON THE HORIZONTAL FLANGE JUST FORWARD OF THE FIXED SIDE BRACE ATTACH POINT. REPLACED PANEL IAW DC-9 SERVICE BULLETIN 53-182.

Part: FITTING — DAMAGED (FS 897.0)

DURING C-CHECK INSPECTION, FOUND A DOUBLE DRILLED HOLE IN THE FITTING AT STA 897.0 AND RBL 54.5. REPAIRED FITTING IAW ABX REA D953-10844-MR.

Part: FLOOR BEAM — DAMAGED (FS 897.0)

DURING C-CHECK INSPECTION, FOUND A DOUBLE DRILLED HOLE IN THE FLOOR BEAM AT STA 897.0 AND RBL 54.5. REPAIRED FLOOR BEAM IAW ABX REA D953-10844-MR.

Part: SPLICE — CORRODED (FWD LWR CARGO)

DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON LONGERON 30 SPLICE, FORWARD OF STA 560. REPLACED LONGERON 30 SPLICE IAW DC-9 SRM 53-02, FIGURE 14.

Part: FRAME — CRACKED (FS 718)

DURING C-CHECK INSPECTION, THE RIGHT FUSELAGE MAIN FRAME AT STA 718 WAS FOUND CRACKED IN THE RIGHT WHEELWELL. REPLACED RIGHT MAIN FRAME IAW SERVICE BULLETIN 53-131.

Part: FLOOR BEAM — CRACKED (BS 680)

DURING C-CHECK INSPECTION, FOUND A FLOOR BEAM CRACKED WITH DOUBLE DRILLED HOLES AT STA 680, LBL 54.5. REPAIRED FLOOR BEAM IAW ABX REA D953-10828-MR.

Part: BRACKET — CRACKED (LT TE FLAP)

DURING C-CHECK INSPECTION, THE LEFT FLAP OUTBOARD HINGE ATTACH BRACKETS WERE FOUND CRACKED. REPLACED BRACKETS IAW DC-9 SRM 51-30-2, 51-30-1 AND 51-30-5.