N990AX

Part: BATTERY — DISCHARGED (MAIN CABIN) · airframe 64,022 hrs · 60,711 cycles

OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-02-4-0001.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,102 hrs · 59,750 cycles

RADIAL CRACK IN AFT PRESSURE BULKHEAD UPPER LEFT CORNER LOCATED 11.25" LEFT OF CENTER. STOP DRILL 250 IAW DC9 SRM 51-10-4.

Part: BATTERY — DEFECTIVE (EMERGENCY LIGHT) · airframe 62,869 hrs · 59,508 cycles

DURING PRE-DEPARTURE CHECK FOUND EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00.

Part: RELAY — INOPERATIVE (CABIN PRESSURE) · airframe 62,747 hrs · 59,379 cycles

LOST PRESSURIZATION AT FL 290. PRESSURE CONTROLLER WOULD NOT LOCK. DESCENDED TO 2000, GAINED MANUAL CONTROL. DECLARED AN EMERGENCY. TROUBLESHOOTING DISCOVERED R2-55 RELAY TO BE BAD, REPLACED RELAY. ALSO REPLACED R20227. REPLACED LEFT GROUND SHIFT RELAY R2-4. PERFORMED ADJUST/TEST OF CABIN PRESSURE CONTROL IAW DC-9 AMM 21-32-00, PAGE A & B THROUGH COMPLETION. ALL OPS CHECKED GOOD. SEE WORK PACK 2005990 FOR WORK ACCOMPLISHED.

Part: FITTING — CRACKED (CENTER WING SEC) · airframe 62,132 hrs · 58,731 cycles

LONGERON END FITTING CRACKED AT RIGHT CANTED KEEL AREA, LONGERON 29 RIGHT. REMOVED AND REPLACED LONGERON END FITTING AT CANTED KEEL AREA IAW DC-9 SRM 51-30-5.

Part: VANE — DELAMINATED (RT WING FLAP) · airframe 62,132 hrs · 58,731 cycles

RIGHT FLAP INBOARD FIXED VANE UPPER SURFACE AT XRS 164, LOCATED BETWEEN CHAFE STRIPS WAS DELAMINATED BEYOND LIMITS OF 15 SQ INCHES. REMOVED AND REPLACED INBOARD FIXED VANE IAW DC-9 SRM.

Part: INTERCOSTAL — CRACKED (AFT CARGO) · airframe 62,132 hrs · 58,731 cycles

INTERCOSTAL END FITTING CRACKED AT STA 1072, LEFT SIDE. REPLACED FITTING IAW DC-9 SRM 51-30-5.

Part: CRANK ASSY — CORRODED (RUDDER) · airframe 62,132 hrs · 58,731 cycles

RUDDER CRANK ASSEMBLY IN AFT ACCESSORY / TAIL WAS BLEEDING RUST. REPLACED RUDDER CRANK ASSEMBLY IAW DC-9 MM.

Part: SPAR CAP — CRACKED (LT PYLON) · airframe 62,132 hrs · 58,731 cycles

LEFT PYLON FORWARD UPPER SPAR CAP CRACKED AT SECOND FASTENER INBOARD OF FUSELAGE LOFT LINE. REPAIRED IAW JOB CARD EA 54100011-102 AND EA 54100011-001.

Part: SKIN — CORRODED (WING CTR SEC.) · airframe 62,132 hrs · 58,731 cycles

TEE CAP FS 618, LONGERON 30, HAD POPPED AND BULGING WEB SEEN FROM AFT SIDE. REPAIRED AREA IAW REA D953-50780 MR.

Part: SPAR CAP — CRACKED (RIGHT WING) · airframe 62,132 hrs · 58,731 cycles

RIGHT WING REAR SPAR UPPER CAP WAS CRACKED RIGHT BUTT LINE 2. REPAIRED AREA IAW DC-9 SRM.

Part: VOLT REGULATOR — BURNED (APU) · airframe 61,174 hrs · 57,721 cycles

SMOKE IN UPPER CARGO COMPARTMENT AND COCKPIT. INSPECTED AND FOUND APU GENERATOR CONTROL PANEL AND APU VOLTAGE REGULATOR BURNED. INSPECTED WIRING FOR DAMAGE, NONE NOTED. INSPECTED AC BUS CONTROL FOR DAMAGE, NONE NOTED. INSPECTED FOR ANY CIRCUIT BREAKERS TRIPPED, NONE WERE TRIPPED. INSPECTED APU STARTER WIRES, TERMINALS AND APU GENERATOR WIRES, NO DAMAGE NOTED. REMOVED AND REPLACED APU VOLTAGE REGULATOR AND APU AC GEN CONTROL PANEL. APU GENERATOR AND VOLTAGE REGULATOR OPS CHECKED GOOD IAW DC-9 MM 24-20-02-5-0, ALSO CROSSTIE CHECKED GOOD FOR THE APU IAW DC-9 1 SERVICE CHECK.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,034 hrs · 57,583 cycles

CRACK IN UPPER LEFT CORNER OF THE VENTRAL DOOR JAMB. REPAIRED AREA IAW REA D953-45345-MR.

Part: PANEL — DEFECTIVE (COCKPIT) · airframe 60,469 hrs · 56,981 cycles

ON SHORT FINAL AT BHM, THE NR 9 CARGO SMOKE DETECTOR STARTED BLINKING. NO SMOKE OBSERVED. REPLACED THE SMOKE DETECTOR PANEL. OPS CHECKED GOOD IAW DC-9 MM.

Part: SMOKE DETECTOR — DEFECTIVE (CABIN) · airframe 60,468 hrs · 56,979 cycles

WHILE DESCENDING THROUGH APPROXIMATELY 18,000 FEET, THE #9 UPPER CARGO SMOKE DETECTOR BLINKED FOR APPROXIMATELY 3 MINUTES. CREW COMPLETED EMERGENCY CHECKLIST. LIGHT WENT OUT AND STAYED OUT. NO SMOKE OBSERVED. REPLACED THE #9 UPPER SMOKE DETECTOR UNIT. OPS CHECKED GOOD IAW DC-9 MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 60,244 hrs · 56,757 cycles

FRAME TO HAT CHANNEL FITTING OUTBOARD VERTICAL LEG CRACKED AT STATION 600, LONGERON 29 RIGHT. REPLACED FITTING IAW DC-9 SRM 51-30-5.

Part: FITTING — CRACKED (CABIN) · airframe 60,244 hrs · 56,757 cycles

LOWER AFT INBOARD FITTING CRACKED AT 1041 BULKHEAD LEFT. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: FITTING — CRACKED (LEFT KEEL) · airframe 60,244 hrs · 56,757 cycles

FRAME TO HAT CHANNEL FITTING INBOARD VERTICAL LEG CRACKED AT STATION 600, LONGERON 29 LEFT. REPLACED FITTING IAW DC-9 SRM 51-30-5.

Part: FRAME — CRACKED (CABIN) · airframe 60,244 hrs · 56,757 cycles

FRAME AT STATION 737 RIGHT UPPER FORWARD FLANGE WAS CRACKED. REPLACED FRAME AT STATION 737 RIGHT IAW DC-9 SRM.

Part: PAN — CRACKED (FUSELAGE)

DURING C-CHECK, FOUND OUTER DOOR PAN CRACKED. REPAIRED DOOR PAN IAW ABX REA D952-34585.

Part: CONTROL CABLE — LACK OF LUBE (LANDING GEAR)

UNABLE TO LOWER GEAR LEVER. AFTER SEVERAL ATTEMPTS, WAS ABLE TO MOVE LEVER TO DOWN POSITION AND GEAR EXTENDED NORMALLY. SUSPECT ICE FORMED AROUND LANDING GEAR EXTENSION CONTROL CABLES. CLEANED WATER FROM AREA AND LUBRICATED CABLES.

Part: ANGLE — CRACKED (BS 776)

DURING C-CHECK, FOUND ATTACH ANGLE CRACKED STATION 776, RIGHT WHEEL WELL AT LONGERON 20R. REPLACED ANGLE IAW DC9 SRM 51-30-5, 51-30-1 AND DACO DWG 9923435.

Part: SHEAR TIE — CRACKED (BS 1171)

DURING C-CHECK, FOUND SHEAR-TIE CRACKED AT STATION 1171 BETWEEN LONGERONS 2R AND 3R. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: ANGLE — CRACKED (VERT STAB)

DURING C-CHECK, FOUND VERTICAL STABILIZER AFT SPAR LEFT VERTICAL Z ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-5 AND DACO DWG 5912123.

Part: ANGLE — CRACKED (VERT STAB)

DURING C-CHECK, FOUND VERTICAL STABILIZER AFT SPAR, RIGHT VERTICAL Z ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-5 AND DACO DWG 5912123.

Part: FITTING — CRACKED (BS 1041)

DURING C-CHECK, FOUND FRAME VERTICAL SUPPORT FITTING CRACKED AT STATION 1041 AND LBL 30. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: BATTERY — DISCHARGED (CABIN)

DURING POST FLIGHT INSPECTION, EMERGENCY LIGHTS FLICKERED, WENT OUT AND THEN CAME BACK ON. REPLACED EMERGENCY LIGHTS BATTERY PACK.

Part: RELAY — DEFECTIVE (NLG)

NOSE GEAR DOWN LOCK LIGHT GREEN REMAINS ILLUMINATED AT ALL TIMES. RECYCLED GEAR WITH THE SAME RESULTS. REPLACED RELAY R2-28, NOSE GEAR INDICATION OPS CHECKS GOOD IAW DC-9 SUPP MM 32-60-0. ALSO, REPLACED THE NOSE LANDING GEAR UPLOCK SWITCH (S1-91) AS A PRECAUTION.

Part: LIGHT PLATE — DEFECTIVE (LEFT)

SMOKE APPEARED AT COMPARATOR RESET BUTTON, LEFT AC ISOLATED AND OPERATIONS WERE NORMAL. REPLACED COMPARATOR TEST LIGHT PANEL IAW DC-9 M.M. 33-10.

Part: TRACK — CHAFED (LT TE FLAP)

WHILE COMPLYING WITH C INSPECTION, FOUND THE LEFT FLAP TRACK AND BUS CABLE CHAFED THROUGH, APPROXIMATELY 2 FEET FROM CABLE BALL END. REMOVED AND REPLACED LEFT HAND FLAP TRACK, CARRIAGE AND BUS CABLE IAW DC-9 MAINTENANCE MANUALS CHAPTERS 27-50-0 AND 27-50-1.

Part: VANE — DELAMINATED (RT TE FLAP)

WHILE COMPLYING WITH A C INSPECTION, FOUND THE RIGHT FLAP AFT MOVEABLE VANE DELAMINATED. REMOVED AND REPLACED AFT MOVEABLE VANE IAW DC-9 MAINTENANCE MANUAL CHAPTER 27-51-02

Part: VANE — CHAFED (LT TE FLAP)

THE LEFT WING INBOARD FIXED FLAP VANE WAS HEAVILY CHAFFED AND DAMAGED ON BOTH THE UPPER AND LOWER INBOARD EDGE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.

Part: VANE — DELAMINATED (RT TE FLAP)

THE RIGHT WING AFT FLAP VANE WAS DELAMINATED ON INBOARD TRAILING EDGE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.

Part: DOOR — DELAMINATED (RT MLG)

WHILE COMPLYING WITH C INSPECTION, FOUND THE RIGHT MAIN LANDING GEAR WING MOUNTED DOOR DISBONDED AROUND THE CRANK ARM ATTACH FITTING. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOOR IAW DC-9 MAINTENANCE MANUAL CHAPTER 32-12-1.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS COME ON AFTER AIRCRAFT POWER IS REMOVED. REPLACED EMERGENCY LIGHT POWER SUPPLY.

Part: EEL SWITCH — DEFECTIVE (COCKPIT)

DURING SERVICE CHECK, FOUND THE EMERGENCY LIGHTS INTERMITTENT IN TEST. REPLACED THE EMERGENCY LIGHT SWITCH AND OPS CHECKED GOOD IAW DC-9 SUPP MM 33-53-00.

Part: SKIN — DAMAGED (FS 198)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A REPAIR AT THE AFT LOWER CORNER OF THE LEFT FORWARD ENTRY DOOR NOT IAW DC-9 SRM. REPAIRED DOOR JAMB SKIN IAW ABX REA D953-11405-MR.

Part: TRAP PANEL — CRACKED (FS 756)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT TRAPEZOIDAL PANEL CRACKED AT THE MAIN LANDING GEAR UP STOP BUMPER. REPLACED LEFT TAPEZOIDAL PANEL IAW DC-9 SB 53-182.

Part: SPOILER PANEL — CORRODED (XRS 324)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT OUTBOARD SPOILER PANEL DELAMINATED. REPLACED PANEL IAW DC-9 MM 27-61-1.

Part: SKIN — DELAMINATED (LT SPOILER)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT OUTBOARD SPOILER PANEL DELAMINATED. REPLACED LEFT OUTBOARD SPOILER PANEL IAW DC-9 MM CHAPTER 27-61-1.

Part: SKIN — DELAMINATED (RT SPOILER)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT WING INBOARD SPOILER TRAILING EDGE DELAMINATED. REPLACED RIGHT INBOARD SPOILER PANEL IAW DC-9 MM CHAPTER 27-61-1.

Part: FRAME — CRACKED (FS 737)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 78-07-05 AND SB 53-131, FOUND RIGHT MAIN FUSELAGE FRAME AT FS 737 CRACKED. REPAIRED RIGHT MAIN FRAME AT FS 737 IAW DC-9 SB 53-131.

Part: CHANNEL — CRACKED (FS 1152)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A MOUNT CHANNEL CRACKED AT FS 1152 AND LONGERON 14R. REPAIRED CHANNEL IAW ABX REA D925-11297 AND RE-INSTALLED CHANNEL IAW DC-9 SRM 51-30-2.

Part: SKIN — CRACKED (LT WING LE)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT WING LEADING EDGE CRACKED JUST INBOARD OF THE NR 5 SLAT OUTBOARD TRACK. REPAIRED CRACK IAW ABX REA D957-11284.

Part: SKIN — GOUGED (WS 64)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT WING LOWER SKIN GOUGED AND CHAFED AT TRAILING EDGE, OUTBOARD OF THE MAIN LANDING GEAR DOOR JAMB. REPAIRED RIGHT WING LOWER SKIN IAW ABX REA D957-11255-MR.

Part: BASE — CORRODED (LT TE FLAP)

DURING D-CHECK ACCEPTANCE INSPECTION WHILE ACCOMPLISHING DC-9 OFF WING INSPECTION, FOUND LEVEL II CORROSION ON THE LEFT FLAP BASE FOR SPRING. REPLACED WITH NEW BASE FOR SPRING IAW DC-9 OVERHAUL MANUAL 27-50-1.

Part: DOUBLER — CORRODED (WS 111.5)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT WING UPPER MAIN LANDING GEAR DOUBLER CORRODED IN PREVIOUS BLENDOUTS. REPLACED RIGHT WING UPPER MAIN LANDING GEAR DOUBLER IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.

Part: FRAME — CRACKED (FS 756)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 78-07-05 AND SB 53-131, FOUND THE RIGHT FUSELAGE MAIN FRAME CRACKED AT FS 756. REPLACED RIGHT MAIN FRAME IAW DC-9 SRM 51-30-1, 51-30-2 AND SB 53-131.

Part: SKIN — GOUGED (FS 332)

WHILE COMPLYING WITH C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A GOUGE AFT OF A PREVIOUS REPAIR AT FS 332 AND LONGERON 25R. REPAIRED SKIN IAW ABX REA D953-11278-MR.

Part: BLKDH — CORRODED (FS 1072)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE AFT PRESSURE BULKHEAD LOWER TEE CAP AT FS 1072 CORRODED AT LONGERON 30. REPLACED AFT PRESSURE BULKHEAD LOWER TEE CAP SECTION IAW DC-9 SRM CHAPTER 51-30-2 AND 51-30-5.

Part: DOOR JAMB — CORRODED (FS 993)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE WEB AROUND THE AFT BAG BIN DOOR JAMB CORRODED. REPAIRED WEB IN JAMB AREA IAW ABX REA D953-11279-MR.

Part: BULKHEAD — CRACKED (FS 1072)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A CRACK IN THE UPPER LEFT HORIZONTAL EDGE OF THE AFT VENTRAL STAIR DOOR. REPAIRED IAW ABX REA D953-11275-SB REV A.

Part: SKIN — CRACKED (FS 198)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A CRACK INDICATION COMING OUT OF AFT LOWER PRESSURE STOP HOLE ON THE FORWARD ENTRY DOOR JAMB. REPAIRED SKIN AT FORWARD ENTRY DOOR IAW ABX REA D953-11122-MR.

Part: SKIN — GOUGED (FS 440-462)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN EXISTING REPAIR BETWEEN FS 440 AND 462, FROM LONGERON 24L AND 25L WAS GOUGED AND DOUBLE DRILLED. REPAIRED FUSELAGE SKIN IAW ABX REA D953-11258-MR.

Part: FRAME — CRACKED (FS 756)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 78-07-05 AND SB 53-131, FOUND THE LEFT FUSELAGE MAIN FRAME AT FS 756 CRACKED. REPLACED MAIN FRAME AT FS 756 IAW DC-9 SB 53-131.

Part: INTERCOSTAL — GOUGED (FS 184)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN ANGLE GOUGED AT FS 184 AND LBL 56, ABOVE THE AIR STAIR DOOR SWITCH. REPAIRED INTERCOSTAL IAW ABX REA D953-11252-MR.

Part: SUPPORT — CRACKED (FS 908)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT VERTICAL FRAME SUPPORT CRACKED AT FS 908 IN AFT BAG BIN. REPLACED FRAME SUPPORT IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: BLKHD FORMER — CRACKED (FS 1072)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A RADIAL STIFFENER CRACKED ON FORWARD FACE OF AFT PRESSURE BULKHEAD FS 1072 AND LONGERON 14L. REPLACED STIFFENER IAW DC-9 SB 53-166 AND SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: BLKHD SUPPORT — CRACKED (FS 794)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE HORIZONTAL WALL SUPPORT FOR FORWARD BULKHEAD IN AFT BAG BIN CRACKED AT LONGERON 22 R. REPLACED SUPPORT IAW DC-9 SRM 51-30-2.

Part: BLKHD SUPPORT — CRACKED (FS 794)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE HORIZONTAL WALL SUPPORT FOR FORWARD BULKHEAD IN AFT BAG BIN CRACKED AT 22R. REPLACED SUPPORT IAW DC-9 SRM 51-30-2.

Part: PANEL — CRACKED (FS 756)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT TRAPEZOIDAL PANEL CRACKED AT THE MAIN LANDING GEAR UP STOP BUMPER PAD. REPLACED RIGHT TRAPEZOIDAL PANEL IAW DC-9 SB 53-182.

Part: RIB — CORRODED (RT FLAP)

DURING D-CHECK ACCEPTANCE INSPECTION WHILE ACCOMPLISHING DC-9 FLAP OFF WING INSPECTION, FOUND LEVEL II CORROSION ON THE RIGHT FLAP INBOARD RIB BEARING BORE. REPAIRED INBOARD RIB HOLE FOR BEARING IAW DC-9 SRM 57-02, FIGURE 7, PAGE 11.

Part: SKIN — CORRODED (FS 1197-1208)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE AFT FUSELAGE SKIN CORRODED ALONG LONGERON 20L BETWEEN FS 1197 AND FS 1208. REPLACED SKIN SECTION IAW DC-9 SRM 51-30-2.

Part: RETRACT MECH — WORN (FS 775)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR DOOR BUSHINGS WORN IN ACTUATING ARM. REPLACED FITTING IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: FRAME — CRACKED (FS 1152)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND FUSELAGE FRAME AT FS 1152 CRACKED AT LONGERON 14R. REPLACED FRAME IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: SKIN — DAMAGED (FS 617)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A FUSELAGE SKIN REPAIR AT FS 617 BETWEEN LONGERONS 28R AND 28L NOT IAW DC-9 SRM. REPAIRED FUSELAGE SKIN IAW ABX REA D953-11104-MR.

Part: FLOORBEAM — DAMAGED (FS 1072)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND REPAIRS ON FLOORBEAM AT FS 1072, LBL 46 AND 48 NOT IAW THE SRM. REPAIRED FLOORBEAM IAW ABX REA D953-11128MR.

Part: LONGERON — CORRODED (FS 879-1031)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LONGERON 30 CORRODED FROM FS 908 TO FS 946 IN AFT BAG BIN. REPLACED LONGERON SECTION IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: FLOORBEAM — DAMAGED (FS 1072)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND REPAIRS ON FLOORBEAM AT FS 1072, LBL 46 AND 48 NOT IAW THE SRM. REPAIRED FLOORBEAM IAW ABX REA D 953-11128-MR.

Part: DOOR JAMB — DENTED (FS 200)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE SERVICE DOOR JAMB AFT STRUCTURE DENTED IN THE BAYONET AREA. REPAIRED RIGHT HAND SERVICE DOOR JAMB IAW DC-9 SRM 53-05 FIGURE 42.

Part: BUSHING — MISSING (FS 756)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT MAIN LANDING GEAR FLYING DOOR HAD ONE MISSING BUSHNG IN THE HINGE LOBE. INSTALLED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: BUSHINGS — WORN (FS 775)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR ACTUATING ROD BUSHINGS WORN. REPLACED BUSHINGS IAW DC-9 OVERHAUL MANUAL.

Part: SKIN — CHAFED (FS 1367)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT VERTICAL SKIN CHAFED UNDER HORIZONTAL STABILIZER FAIRING. REPLACED SKIN IAW DC-9 SRM CHAPTER 51-30-2.

Part: INTERCOSTAL — CRACKED (FS 180)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN INTERCOSTAL CRACKED AT FS 180, LBL 42. REPAIRED INTERCOSTAL IAW DC-9 SRM SUPPLEMENTAL DRAWING NR K05195.

Part: WEB — CORRODED (FS 984)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 94-03-01, FOUND THE RIGHT CUSP WEB AT FS 984 HAD LEVEL II CORROSION. REPLACED RIGHT CUSP WEB FROM FS 973 TO 1041 IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.

Part: FITTING — CORRODED (FS 1013)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 94-03-01, FOUND THE RIGHT FUSELAGE FRAME TEE FITTING AT FS 1013 HAD LEVEL II CORROSION. REPLACED FUSELAGE FRAME TEE FITTING IAW DC-9 SRM 51-30-5.

Part: WEB — CORRODED (FS 946)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 94-03-01, FOUND THE RIGHT CUSP WEB AT FS 946 HAD LEVEL II CORROSION. REPLACED RIGHT CUSP WEB IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: WEB — CRACKED (FS 218)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE CUSP WEB CRACKED AT FS 218, LBL 55. REPLACED CUSP WEB FROM FS 218 TO FS 237 IAW DC-9 SRM 51-30-2.

Part: FITTING — CORRODED (FS 984)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 94-03-01, FOUND THE RIGHT FUSELAGE FRAME FITTING AT FS 984 HAD LEVEL II CORROSION. REPLACED RIGHT TEE FITTING IAW DC-9 SRM 51-30-5.

Part: FITTING — CORRODED (FS 1005)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 94-03-01, FOUND THE RIGHT FUSELAGE FRAME TEE FITTING HAD LEVEL II CORROSION AT FS 1005. REPLACED RIGHT FUSELAGE FRAME FITTING AT FS 1005 IAW DC-9 SRM 51-30-5.

Part: ANGLE — CORRODED (RT FLAP)

DURING D-CHECK ACCEPTANCE INSPECTION WHILE ACCOMPLISHING DC-9 FLAP OFF WING INSPECTION, FOUND LEVEL II CORROSION ON THE RIB ANGLE. REPLACED RIB ANGLE IAW DC-9 SRM 57-50-9.

Part: ANGLE — CRACKED (FS 655)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT HAND FLOOR BEAM ATTACH ANGLE CRACKED AT FS 655. REPLACED ATTACH ANGLE IAW DC-9 SRM 51-30-5.

Part: RIB — CRACKED (WS 128)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT WING NR 2 INBOARD SLAT TRACK FITTING CRACKED AT LOWER ATTACHMENT. REPLACED FITTING IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (FS 718)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LONGERON 2R CRACKED AT FS 718. REPLACED LONGERON SECTION IAW DC-9 SRM 53-02 FIGURE 2.

Part: LONGERON — CRACKED (FS 718)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 88-24-08 REV 2; SB A53-230 REV 3, FOUND LONGERON 2R CRACKED AT FS 718. REPAIRED LONGERON IAW DC-9 SRM 53-02 FIGURE 2.

Part: LONGERON — CRACKED (FS 794)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 88-24-08 REV 2; SB A53-230 REV 3, FOUND LONGERON 3R CRACKED AT FS 794. REPAIRED LONGERON IAW DC-9 SRM 53-02 FIGURE 2.

Part: LONGERON — CRACKED (FS 794)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LONGERON 3R CRACKED AT FS 794. REPLACED LONGERON SECTION IAW DC-9 SRM 53-02 FIGURE 2.

Part: LONGERON — CRACKED (FS 775)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LONGERON 4R CRACKED AT FS 775. REPLACED LONGERON SECTON IAW DC-9 SRM 53-02 FIGURE 2.

Part: LONGERON — CRACKED (FS 775)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 88-24-08 REV 2; SB A53-230 REV 3, FOUND LONGERON 4R CRACKED AT FS 775. REPAIRED LONGERON IAW DC-9 SRM 53-02 FIGURE 2.

Part: LONGERON — CRACKED (FS 408)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, WHILE COMPLYING WITH AD 94-03-01, FOUND LONGERON 17R CRACKED AT FS 408. REPAIRED LONGERON IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: DOOR JAMB — CRACKED (FS 207)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT MAIN ENTRY DOOR JAMB WEB CRACKED AT FS 207 AND LONGERON 11L AND 15L. REPAIRED IAW DC-9 SRM SUPPLEMENTAL DRAWING K05012.