N924AX

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 69,556 hrs · 66,450 cycles

COCKPIT EMERGENCY LIGHTS DIM DURING TEST. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT BATTERIES IAW DC9 AMM 33-53-00-80001. FUNCTIONAL CHECK IAW DC9 AMM 33-53-00-50001. REMOVED AND REPLACED EMERGENCY POWER BATTERY SUPPLY IAW DC9 MM 24-30-22. OPS CHECKED GOOD.

Part: FITTING — CRACKED (BS 965) · airframe 69,146 hrs · 66,041 cycles

FITTING CRACKED ABOVE FLOORBEAM, FS 965 AT APPROXIMATELY LEFT BUTT LINE 24. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: FRAME — CRACKED (BS 718) · airframe 69,146 hrs · 66,041 cycles

LEFT, CENTER MAIN FRAME, STA 718, WAS CRACKED AT POINTS J & G IN FORWARD AND AFT FLANGES AND POINTS F TO E IN FORWARD FLANGE. CRACK ASLO EXTENDS ABOVE 9" REPAIR IN LEFT WHEEL WELL. MAIN FRAME TO BE REPLACED IAW EA 53400323-001-2.

Part: PANEL — CRACKED (RT MLG WW) · airframe 69,146 hrs · 66,041 cycles

RIGHT TRAP PANEL OUTBOARD UPPER FORWARD HORIZONTAL FLANGE CRACKED OUT OF AFT SIDE OF FIRST FASTENER HOLE THROUGH FASTENER HOLES NR 2, NR 3, NR 4 AND NR 5, AND INTO FASTENER HOLE NR 6. REPAIRED RIGHT TRAP PANEL IAW DC9 SRM 57-09.

Part: SWITCH — LOOSE (LIGHT) · airframe 69,042 hrs · 65,940 cycles

WHILE EXTENDING LANDING LIGHT FOR ARRIVAL, SPARKS FLEW FROM BEHIND PANEL. TRACED PROBLEM TO LOOSE NOSE LIGHT SWITCH, SECURED SWITCH. OPERATIONAL CHECK GOOD.

Part: ACCESS DOOR — UNLATCHED (FUSELAGE) · airframe 68,818 hrs · 65,712 cycles

ON T/O, NO PRESSURIZATION, CABIN CLIMBED AT SAME RATE AS AIRCRAFT. AC PACKS SHOWED 27 PSI ON BOTH SIDES, CABIN FLOW CONTROL VALVE WAS FULLY CLOSED. INSPECTED A/C FOUND ALL EXTERIOR DOORS CLOSED. FOUND AFT BULKHEAD ACCESS DOOR UNLATCHED. RESECURED DOOR. PRESSURIZED A/C. OPS CHECKED GOOD.

Part: SWITCH — DEFECTIVE (NLG POS WARN) · airframe 68,569 hrs · 65,464 cycles

ON APPROACH, NOSE GEAR SAFE FAILED TO ILLUMINATE. RAN ABNORMAL, GEAR RECYCLE, LANDED WITHOUT PROBLEM. VERIFIED WORN PADDLE ON NOSE LANDING GEAR DOWN SWITCH. REMOVED AND REPLACED GEAR DOWN SWITCH IAW DC-9 MM 32-60-01-2-0101. OPS CHECKED GOOD.

Part: CONNECTOR — LOOSE (POSITION SWITCH) · airframe 67,687 hrs · 64,540 cycles

EMERGENCY DECLARED, HAD GEAR DOOR OPEN LIGHT IN CRUISE FLIGHT. PERFORMED ABNORMALS, NO HELP. ON APPROACH, AFTER GEAR EXT, STILL HAD DOOR OPEN LIGHT. PERFORMED ABNORMALS. PULLED EMERGENCY GEAR RELEASE. MECHANICS MET THE AIRCRAFT. TIED DOORS UP AND PINNED ALL 3 GEAR. VERIFIED LOOSE CONNECTOR ON DOOR POSITION SWITCH. RESECURED PLUG, OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CRACKED (AFT CARGO BAY) · airframe 68,074 hrs · 64,960 cycles

LEFT INBOARD FLOOR SUPPORT FITTING CRACKED AT STA 945. REPLACED FITTING AT LEFT FLOOR TRACK, AFT LOWER CARGO, STA 945 IAW DC-9 SRM 51-30-5.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 68,074 hrs · 64,960 cycles

FORWARD LOWER CARGO DOOR INTERCOSTAL ANGLE WAS CRACKED AT THE FORWARD LOWER STOP AREA. REPLACED ANGLE FORWARD LOWER STOP DOOR IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: INTERCOSTAL — CRACKED (AFT CARGO BAY) · airframe 68,074 hrs · 64,960 cycles

CENTER INTERCOSTAL AT LOWER EDGE OF AFT LOWER CARGO DOOR HAD CRACKED ATTACH ANGLE. REPLACED ANGLE IAW DC-9 SRM 51-30-5.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 68,074 hrs · 64,960 cycles

DOUBLE SEAT TRACK CORRODED AT FS 996, RIGHT BUTT LINE 6. REPLACED TRACK AT RIGHT BUTT LINE 6 AT STA 965 - 1019 IAW DC-9 SRM 51-30-1.

Part: SEAT TRACK — CRACKED (CABIN) · airframe 68,074 hrs · 64,960 cycles

CENTER SEAT TRACK CRACKED AND CORRODED AT FS 996. SPLICED IN NEW SECTION OF TRACK STA 926 - 1019 IAW DC-9 SRM K05406 AND SRM 51-30-1.

Part: FRAME — CRACKED (LT WHEEL WELL) · airframe 68,074 hrs · 64,960 cycles

CRACK IN THE MAIN FRAME AFT POCKET, EXTENDED TO THE MAIN ATTACH BOLT. CRACK LENGTH 1.625 AND 2.170. REPAIRED IAW SERVICE REWORK DRAWING 5934375-505 IAW ABX REA D953-50391. INITIATED WATCH ITEM 924-035 FOR REPETITIVE INSPECTION INTERVALS OF 1600 FLIGHT HOURS FOR CRACK GROWTH PROGRESSION.

Part: FRAME — CRACKED (RT WHEEL WELL) · airframe 68,074 hrs · 64,960 cycles

CRACK IN THE FORWARD POCKET EXTENDED FROM THE MAIN ATTACH HOLE TO THE FIRST REPAIR ATTACH HOLE. RIGHT MAIN FRAME REPLACED IAW EA 53400324-001-2 AND WORK ACCOMPLISHED ON NR 0271.

Part: DOWNLOCK SWITCH — DEFECTIVE (MLG) · airframe 68,017 hrs · 64,905 cycles

DURING GEAR EXTENSION, THE NOSE LANDING GEAR LIGHT DID NOT ILLUMINATE WHILE THE NOSE GEAR UNSAFE LIGHT STAYED LIT. THE GEAR WAS RECYCLED. AFTER ONE MINUTE, THE NOSE GEAR CAME DOWN AND LOCKED. REMOVED AND REPLACED THE NOSE LANDING GEAR DOWNLOCK SWITCH IAW DC-9 MM 32-60-10. OPS CHECKED GOOD IAW DC-9 MM.

Part: RELAY — FAILED (ELECTRICAL) · airframe 67,110 hrs · 63,930 cycles

DURING FLIGHT, AUTOPILOT DISCONNECTED, EADI AND EHSI PICTORIAL APPEARED TO HAVE ALL SYMBOLS RAPIDLY SPINNING. SELECTED SG-3, REALIGNED EADI AND EHSI. BUT WHEN CONNECTING AUTOPILOT, AIRCRAFT WOULD RAPIDLY DIVE AND BANK. SERVOS COULD BE HEARD GYRATING AND SERVO INDICATIONS WERE FLUCTUATING. AT PARKING, FOUND EMERGENCY AC BUS FEED CIRCUIT BREAKER OUT. OPS CHECKED AC BUS FEED SYSTEM IAW DC-9 AMM 24-50-00-2. FOUND AC EMERGENCY POWER TRANSFER RELAY R2-47 TO BE INOPERATIVE. REMOVED AND REPLACED RELAY R2-47, ALSO REPLACED AC BUS FEED EMERGENCY CIRCUIT BREAKER FOR PRECAUTION. BOTH UNITS REMOVED AND REPLACED IAW DC-9 24-50-00-2. OPS CHECKED GOOD.

Part: WINDOW — STUCK (COCKPIT) · airframe 67,088 hrs · 63,913 cycles

CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED LOWER AFT HOOK FITTING IAW DC-9 MM 56-10-3-5-0002. OPS CHECKED GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,082 hrs · 63,910 cycles

FRAME AT STA 81, LONGERON 11 LEFT, CRACKED. REPAIRED FRAME IAW DC-9 SSRM DWG K05159.

Part: FORMER — CRACKED (FUSELAGE) · airframe 67,082 hrs · 63,910 cycles

SHEAR TIE AT F.S. 1019, LONGERON 14 - 15 LEFT, CRACKED. REPLACED SHEAR TIE IAW DC-9 SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,082 hrs · 63,910 cycles

CRACKED END FITTING STATION 604, LONGERON 28, LEFT. REPLACED FITTING IAW DC-9 SRM 51-30-5.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 67,082 hrs · 63,910 cycles

SHEAR TIE AT F.S. 1019, LONGERON 14 - 15 RIGHT, CRACKED. REPLACED SHEAR TIE IAW DC-9 SSRM K05159.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 67,082 hrs · 63,910 cycles

FLOORBEAM SEVERLY CORRODED AT AFT LOWER CARGO DOOR HOLD-OPEN HOOK, FS 937, RIGHT BUTT LINE 12. REPAIRED FLOORBEAM IAW DC-9 SSRM K07411.

Part: DOUBLER — CRACKED (RT MLG WW) · airframe 67,082 hrs · 63,910 cycles

DOUBLER AT RIGHT WHEEL WELL UPPER PRESSURE PANEL CRACKED AT STATION 720, RIGHT BUTT LINE 55. REMOVED DOUBLER AND INSTALLED NEW DOUBLER IAW DWG NR 9910155 AND DC-9 SRM 51-30-3.

Part: FRAME — CRACKED (LEFT KEEL) · airframe 67,082 hrs · 63,910 cycles

FRAME STATION 622 CRACKED AT LEFT CANTED KEEL. REPAIRED FRAME IAW DC-9 SRM K05159.

Part: PANEL — CRACKED (RUDDER) · airframe 67,082 hrs · 63,910 cycles

CRACK FOUND INTERNAL OF RUDDER LOOKING FORWARD LT SIDE THROUGH PANEL NR 6515. REPLACED RUDDER IAWA DC-9 MM 27-20-01-4-0001.

Part: DOUBLER — CORRODED (RT. WHEEL WELL) · airframe 67,082 hrs · 63,910 cycles

CORROSION ON RIGHT WHEEL WELL UPPER PRESSURE PANEL DOUBLER STATION 722, RIGHT BUTT LINE 56. FABRICATED NEW DOUBLER IAW DWG #9910155 AND DC-9 SRM.

Part: DOUBLER — CRACKED (RT MLG WW) · airframe 67,082 hrs · 63,910 cycles

DOUBLER AT RIGHT WHEEL WELL UPPER PRESSURE PANEL CRACKED AT STATION 76, RIGHT BUTT LINE 55. REMOVED DOUBLER AND INSTALLED NEW DOUBLER IAW DWG NR 9919155 AND DC-9 SRM 51-30-3.

Part: SWITCH — FAULTY (LT MLG DOOR) · airframe 66,796 hrs · 63,620 cycles

ON FINAL APPROACH, GEAR DOOR OPEN LIGHT WOULD NOT EXTINGUISH. RECYCLED GEAR AND LIGHT STILL DID NOT GO OUT. EXTENDED GEAR LIGHT ON AT FLAPS 15 DEGREES. WHEN FLAPS 25 DEGREES SELECTED, LIGHT WENT OUT. EXECUTED MISSED APPROACH. CONFIGURED TO EXT/15 DEGREES GEAR UP WITH NORMAL INDICATIONS. ON NEXT APPROACH, ALL INDICATIONS WERE NORMAL. FOUND LEFT MAIN LANDING GEAR DOOR SWITCH BAD. REPLACED THE DOOR SWITCH. OPS CHECKED GOOD IAW DC-9 MM 32-60-03.

Part: SWITCH (COCKPIT) · airframe 66,680 hrs · 63,490 cycles

WHEN CENTER FORWARD BOOST PUMP WAS TURNED ON, SPARKS CAME OUT OF THE PANEL AND TWO CIRCUIT BREAKERS TRIPPED.REPLACED THE FORWARD CENTER BOOST PUMP ON/OFF SWITCH.

Part: COALESCER BAG — DIRTY (A/C BAY) · airframe 66,090 hrs · 62,882 cycles

OIL SMELL WAS COMING FROM THE AIR CONDITIONING OUTLETS. UNABLE TO DETERMINE FROM WHICH PACK. DUCT TEMPERATURES WERE NORMAL. REPLACED THE LEFT AND RIGHT COALESCER BAGS IAW DC-9 MM 21-20-00.

Part: LONGERON — CRACKED (PYLON BLKHD.) · airframe 65,957 hrs · 62,748 cycles

CRACKED LONGERON 17 LEFT AT PYLON BULKHEAD. REPLACED LONGERON 17 LEFT IAW DC-9 SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,957 hrs · 62,748 cycles

FLOOR BEAM SUPPORT ANGLE AT 617 LEFT BUTT LINE 20 CRACKED. REPLACED ANGLE BRACKET IAW DC-9 SRM 51-30-5.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 65,957 hrs · 62,748 cycles

RIGHT F.S. 699 MAIN FRAME INBOARD POCKET UPPER FORWARD FLANGE CRACKED IN AREA OF "Z" ANGLE. INSTALLED REPAIR ANGLE DOUBLER IAW DC-9 E.A. 53400120-001-1.

Part: SOCKET — CONTAMINATED (COCKPIT) · airframe 65,919 hrs · 62,719 cycles

THE NOSE LANDING GEAR DOWN AND LOCKED (GREEN) LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE CREW PERFORMED ABNORMAL CHECKLIST AND COMPLETED A GEAR RE-CYCLE. MAINTENANCE INSPECTED AND CLEANED DEBRIS FROM THE NOSE LANDING GEAR GREEN LIGHT SOCKET. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FUSELAGE) · airframe 65,721 hrs · 62,527 cycles

COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERIES IAW DC-9 MM 33-53-00. LATER ON 02/13/01 THE EMERGENCY LIGHT POWER SUPPLY WAS ALSO REPLACED FOR RELIABILITY CONCERNS.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 65,362 hrs · 62,191 cycles

DURING LOAD CROSS-CHECK, LOWER AFT CARGO COMPARTMENT FIRE LIGHT AND THE MASTER WARNING LIGHT ILLUMINATED. SHUT ENGINES DOWN AND EVACUATED THE AIRCRAFT. INSPECTED FOR SIGNS OF FIRE OR SMOKE, NONE FOUND. CARGO SMOKE DETECTOR SYSTEM TESTED GOOD.

Part: SKIN — CRACKED (BS 427)

DURING C-CHECK, FOUND FUSELAGE SKIN CRACKED AT STATION 427 AND LONGERON 23. REPAIRED IAW DC9 SRM 53-05 AND D953-33534MR.

Part: WEB — CRACKED (BS 598)

DURING C-CHECK, FOUND RIGHT CUSP WEB CRACKED AT STATION 598. REPAIRED IAW DC9 SRM 53-01.

Part: LONGERON — CRACKED (BS 945)

DURING C-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 945. REPLACED LONGERON 17 LEFT AT STATION 945 IAW DC9 SRM 51-30-2.

Part: PRESSURE PANEL — CRACKED (BS 83)

DURING C-CHECK, FOUND UPPER PRESSURE PANEL AT STATION 83 CRACKED. REPAIRED IAW ABX REA D953-33358MR.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS WERE INTERMITTENT. REPLACED EMERGENCY LIGHT BATTERIES IAW DC9 MM 33-53-02, OPS CHECKED GOOD.

Part: LINK — CRACKED (NR 2 ENG TR UNIT)

WHILE COMPLYING WITH AD 75-14-06, FOUND UPPER LEFT THRUST REVERSER DRIVER LINK CRACKED ON NR 2 ENGINE. REPLACED THRUST REVERSER DRIVER LINK IAW DC9 MM 78-31-05.

Part: LINK — CRACKED (NR 2 ENG TR UNIT)

WHILE COMPLYING WITH AD 75-14-06, FOUND LOWER LEFT THRUST REVERSER DRIVER LINK CRACKED ON NR 2 ENGINE. REPLACED THRUST REVERSER DRIVER LINK IAW DC9 MM 78-31-05.

Part: STIFFENER — CRACKED (RT PYLON)

DURING C-CHECK, FOUND STIFFENER CRACKED ON NR 2 PYLON WHERE THROTTLE CABLE PASSES THROUGH OUTBOARD SIDE OF PYLON. REPLACED STIFFENER IAW DACO DWG 9958220 AND DC9 SRM 51-30-2.

Part: LONGERON — CRACKED (BS 718)

DURING C-CHECK, FOUND LONGERON 5R CRACKED AT STATION 718. REPAIRED LONGERON IAW DC9 SERVICE REWORK DWG SR09530128.

Part: LONGERON — CRACKED (BS 690)

DURING C-CHECK, FOUND LONGERON 7L CRACKED AT STATION 690. REPAIRED LONGERON IAW DC9 SERVICE REWORK DWG SR09530128.

Part: TR LINK — CRACKED (NR 2 ENGINE)

DURING C-CHECK, FOUND THE UPPER RIGHT THRUST REVERSER LINK CRACKED. REPLACED LINK IAW DC9 MM 78-31-5.

Part: WEB — CRACKED (BS 963)

DURING C-CHECK, FOUND 2 CRACKS IN CUSP WEB AT STATION 963, RIGHT SIDE. REPAIRED WEB IAW DC9 SRM 53-01.

Part: SHEAR TIE — CRACKED (BS 945)

DURING C-CHECK, FOUND SHEAR TIE BETWEEN LONGERON 14L AND 16L STATION 945 CRACKED. REPLACED SHEAR TIE IAW DC9 SRM 51-30-5.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, FOUND LONGERON 17L CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: TR LINK — CRACKED (NR 1 ENGINE)

DURING C-CHECK, FOUND THE LOWER RIGHT THRUST REVERSER LINK CRACKED. REPLACED LINK IAW DC9 MM 78-31-5.

Part: FLOORBEAM — CORRODED (BS 965)

DURING C-CHECK, FOUND EXFOLIATION CORROSION BETWEEN ANGLE AND FLOORBEAM LOWER FLANGE ON BEAM AT STATION 965 RBL 8. REPAIRED FLOORBEAM IAW ABX REA D953-22983-MR.

Part: SKIN — CRACKED (BS 1038)

DURING C-CHECK, FOUND CRACKED FUSELAGE SKIN AT STATION 1038 AND LONGERON 14L. REPAIRED SKIN IAW DC9 SRM 53-04.

Part: LATCH BOLT — DEFECTIVE (COCKPIT DOOR)

DURING PREFLIGHT FOUND COCKPIT DOOR DIFFICULT TO OPEN.\N\N\N\N\N\NREMOVED AND REPLACED DOOR LATCH BOLT.

Part: SEAL — CUT (NR 2 ENGINE)

CLIMBING OUT AT 15,500 MSL ALTITUDE, RIGHT ENGINE OIL PRESSURE LOW ANNUNCIATOR LIGHT ILLUMINATED. RIGHT ENGINE OIL PRESSURE WAS 25 PSI AND OIL QUANTITY WAS ZERO. PRECAUTIONARY ENGINE SHUTDOWN IAW ENGINE SECURING CHECKLIST. RETURNED TO RDU. *S/D* FOUND RIGHT ENGINE MAIN OIL FILTER O-RING SEAL DAMAGED. REPLACED SEAL IAW DC9 MM 79-20-6, NO LEAKS NOTED.

Part: BULB — DEFECTIVE (NLG)

DURING GEAR UPLATCH CHECK, THE LEFT GEAR UNSAFE AND THE GREEN NOSE GEAR LIGHT ILLUMINATED. NO VIBRATION OR EXCESS NOISE WAS NOTED. RECYCLED GEAR, NO CHANGE. TAPPED ON CASE FOR GREEN LANDING GEAR LIGHT AND LIGHT WENT OUT. REPLACED LIGHT BULB IN THE NOSE LANDING GEAR LIGHT ASSY.

Part: HINGE — WORN (RT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT HAND MAIN LANDING GEAR OUTBOARD DOOR HAD EXCESSIVE PLAY AT HINGE. BUSHED HINGE LOBES IAW DC9 OVERHAUL MANUAL 32-10-6.

Part: ARM — WORN (RT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT HAND MAIN LANDING GEAR OUTBOARD DOOR TRANSITION ARM WORN. REPLACED ARM IAW DC9 OVERHAUL MANUAL 32-10-6.

Part: ARM — WORN (LT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND LEFT HAND MAIN LANDING GEAR OUTBOARD DOOR TRANSITION ARM WORN. REMOVED ARM IAW DC9 OVERHAUL MANUAL 32-10-6.

Part: POWER SUPPLY — DEFECTIVE (CABIN)

EMERGENCY LIGHTS CAME ON WHEN POWER IS REMOVED FROM AIRCRAFT. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW DC-9 MM 33-53-0.

Part: PAN — CRACKED (EMER EXIT DOOR)

FOUND OVERWING DOOR PAN CRACKED. REPAIRED IAW ABX REA D952-15926-MR.

Part: SKIN — CRACKED (EMER EXIT DOOR)

FOUND DOOR PAN, AND INNER SKIN CRACKED. REPAIRED IAW ABX REA D952-16211-MR, AND DC9 SRM 52-01.

Part: FLAP VANE — CRACKED (LT TE FLAP)

THE LEFT FORWARD FLAP VANE HAD THE INBOARD STOP SUPPORT CRACKED AND INDICATIONS OF CORROSION. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.

Part: HYD LINE — LEAKING (RT WING)

ON FINAL APPROACH, RIGHT HYDRAULIC SYSTEM FAILED WITH LOSS OF ALL HYDRAULIC FLUID WHEN FLAPS WERE SELECTED TO 5 DEGREES. FOUND A HYDRAULIC LINE IN THE RIGHT WING ROOT AREA LEAKING. INSTALLED A TEMPORARY FLEX LINE IAW SPM 29.01.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

DURING MAINTENANCE INSPECTION, FOUND COCKPIT EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK IAW DC9 MM ABX SUPPLEMENT 33-53-0. SYSTEM OPS CHECKS GOOD.

Part: FITTING — CRACKED (AFT PLUG DOOR)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 80-02-16, THE AFT PRESSURE DOME PLUG DOOR LUG SHOWED A CRACK INDICATION ON THE X-RAY. FITTING WAS REPLACED IAW DC-9 SRM 51-30-5.

Part: TR LINK — NICKED (NR 2 ENGINE)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 75-14-06, A.D.90-18-03, S.B.'S 78-36, 78-38, 78-40, 78-66, FOUND BY EDDY CURRENT INSPECTION TWO EACH CRACK INDICATIONS ON THE INBOARD LOWER THRUST REVERSER LINK ON THE NR 2 ENGINE. BLENDED NICKS ON THRUST REVERSER DRIVE LINK IAW DC-9 OVERHAUL MANUAL, CHAPTER 78-30-1.

Part: STRINGER — GOUGED (WS 58)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D.90-18-03, S.B. 57-98, FOUND GOUGES ON TOP OF STRINGER NR 13 NEAR BARREL NUT HOLE. REMOVED GOUGES ON TOP OF STRINGER NR 13 IAW DC-9 SRM 57-03.

Part: STRINGER — GOUGED (WS 58)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 90-18-03, S.B. 57-98, FOUND GOUGES IN STRINGER NR 11 BARREL NUT HOLE IN RIGHT WING. REMOVED GOUGES IN STRINGER NR 11 BARREL NUT HOLE IAW DC-9 SRM 57-03.