N988AX

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,202 hrs · 58,778 cycles

LONGERON 24 RT END CAP AT STA 945 WAS CORRODED. REPLACED END CAP IAW SRM 51-30-2 AND 51-30-5.

Part: SKIN — CORRODED (FWD CARGO DOOR) · corrosion level 2 · airframe 57,202 hrs · 58,778 cycles

FORWARD LOWER CARGO DOORS EXTERIOR SKIN HAD PITTING, CORROSION AT AFT LOWER CORNER. REPLACED DOOR ON NR 0399 IAW SRM.

Part: PAN — DEFECTIVE (FWD CARGO DOOR) · airframe 57,202 hrs · 58,778 cycles

FORWARD LOWER CARGO DOOR HAD DEFECT INDICATION IN OUTER PAN ALONG UPPER EDGE AT FORWARD STOP PAD AREA. REPLACED DOOR ON NR 0399 IAW SRM.

Part: PAN — CRACKED (FWD CARGO DOOR) · airframe 57,202 hrs · 58,778 cycles

FORWARD LOWER CARGO DOORS OUTER PAN HAD CRACK INDICATION IN OUTER RADIUS OF FORWARD HINGE. REPLACED DOOR ON NR 0399 IAW SRM.

Part: PAN — CRACKED (FWD CARGO DOOR) · airframe 57,202 hrs · 58,778 cycles

FORWARD LOWER CARGO DOOR OUTER PAN CRACKED AT FASTENER HOLE AT UPPER FORWARD CORNER. REPLACED FORWARD LOWER CARGO DOOR ON N.R. 0399 IAW DC-9 SRM.

Part: PAN — CRACKED (FWD CARGO DOOR) · airframe 57,202 hrs · 58,778 cycles

FORWARD LOWER CARGO DOORS OUTER PAN WAS CRACKED AT HI-LOCK ALONG AFT EDGE, CENTER STOP PAD AREA. REPLACED DOOR ON NR 0399 IAW SRM.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 57,202 hrs · 58,778 cycles

LONGERON 4 LT CRACKED AT FS 160 SPLICED SECTION OF LONGERON IAW SRM 53-02.

Part: BEAM — CRACKED (AFT CARGO DOOR) · airframe 57,202 hrs · 58,778 cycles

AFT LOWER CARGO DOOR BEAM NR 1 BOTH FORWARD AND AFT END FITTINGS CRACKED. REPLACED FITTINGS S914025-501 AND 3914025-502 IAW SRM 51-30-1 AND 51-30-5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,202 hrs · 58,778 cycles

RT MAIN FRAME STA 699 WAS CRACKED IN FORWARD UPPER FLANGE BETWEEN Z-CLIP FASTENERS. REPAIRED MAIN FRAME RT 699 IAW EA 53400120-001-1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,202 hrs · 58,778 cycles

FUSELAGE SKIN CRACKED AT RIVET ON LONGERON 22 LT BETWEEN FS 180-200. REPAIRED ON EA 53300031-001.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,202 hrs · 58,778 cycles

BULGE IN FUSELAGE SKIN AT CABIN OUTFLOW NOZZLE. REPLACED SECTION OF LONGERON FROM APPROXIMATELY STA. 955-990 IAW SRM.

Part: LOCK PIN — OUT OF ADJUST (COCKPIT WINDOW) · airframe 57,173 hrs · 58,747 cycles

FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT GLIDE BACK TO FULL OPER POSITION. ADJUSTED CLEARVIEW WINDOW ECCENTRIC LOCK PIN. WINDOW OPENS AND CLOSES SMOOTHLY.

Part: DOWNLOCK SWITCH — MALADJUSTMENT (NLG) · airframe 57,131 hrs · 58,696 cycles

NOSE GEAR RED UNSAFE INDICATOR WOULD NOT ILLUMINATE WITH THROTTLES AT IDLE. PRESS TO TEST OK, HAD TO RECYCLE GEAR TO OBTAIN NOSE GEAR GREEN SAFE LIGHT. TESTED NOSE GEAR DOWNLOCK SWITCH. COULD NOT DUPLICATE. REPLACED THE NOSE GEAR DOWNLOCK SWITCH AS A PRECAUTION IAW DC9 MM 32-60-01-2-0101. OPS CHECK GOOD ON GEAR SWING.

Part: WINDOW — STUCK (COCKPIT) · airframe 57,014 hrs · 58,578 cycles

FIRST OFFICER'S SIDE WINDOW WAS STUCK SHUT. INSTALLED A MISSING NUT AT ROD END AT TOP OF WINDOW AND SECURED LOOSE LOCK BAR TRIM. WINDOW OPERATES NORMALLY.

Part: CONTROL CABLE — LACK OF LUBE (MLG) · airframe 56,208 hrs · 57,746 cycles

WITH LANDING GEAR RETRACTED, GEAR DOOR OPEN LIGHT AND RIGHT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLING GEAR, HAD NO EFFECT ON THIS CONDITION. FERRIED AIRCRAFT BACK TO ILN UNDER FERRY PERMIT 002-003. REMOVED, CLEANED, LUBRICATED AND REINSTALLED DOOR SEQUENCING CABLE IAW DC-9 MM 32-31-00-4-0001 AND ADJUST TEST IAW DC-9 MM 32-31-00-5-00-01. REPLACED SHEARED RIVETS IAW DC-9 SRM 51-30-2.

Part: LANDING GEAR — MALFUNCTIONED (NLG & MLG) · airframe 56,018 hrs · 57,559 cycles

AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. HYDRAULICS WERE NORMAL, NO OTHER ABNORMAL INDICATIONS. RECYCLED GEAR, OPS CHECKED GOOD. NO FURTHER DIFFICULTIES. INSPECTED ALL THREE LANDING GEAR AND DOORS. NO DEFECTS NOTED. CYCLED LANDING GEAR FOUR TIMES IAW DC-9 MM 32-30-00-2-0001. OPS CHECKED GOOD EACH TIME.

Part: CONNECTOR — DAMAGED (MLG INDICATOR) · airframe 55,597 hrs · 57,107 cycles

ON APPROACH IN ILN SELECTED GEAR DOWN. DID NOT GET RIGHT MAIN LANDING GEAR DOWN GREEN LIGHT. RECYCLED AND ACCOMPLISHED THE GEAR HANDLE DOWN ABNORMAL CHECK LIST IN THE DC-9 OPS MANUAL. AIRCRAFT DID A GO-AROUND. FOUND AND REPAIRED BROKEN WIRE IN CONNECTOR PLUG. (PIN 5 IN RIGHT MAIN LANDING GEAR DOWNLOCK) IAW DC-9 WDM 32-60-01-2-0101. GEAR INDICATION OPS CHECKED GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,199 hrs · 56,707 cycles

CRACK ON FRAME AT FS 980 AND LONGERON 16 LEFT. REPAIRED FRAME IAW DC-9 SRM 53-03, FIGURE 32.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,199 hrs · 56,707 cycles

FLOORBEAM AT STATION 275 LBL 50 HEAVILY CORRODED. REPAIRED FLOORBEAM IAW DC-9 SRM DWG K07411.

Part: SOCKET — INTERMITTENT (COCKPIT) · airframe 54,981 hrs · 56,463 cycles

THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED INTERMITTANTLY AFTER GEAR WAS FULLY RETRACTED, AND CONTINUED TO INTERMITTANTLY ILLUMINATE FOR THE REMAINDER OF THE FLIGHT. FLIGHT CREW RECYCLED THE LANDING GEAR. MAINTENANCE INSPECTED AND REPLACED THE RIGHT MAIN LANDING GEAR UNSAFE INDICATION LIGHT SOCKET IAW DC-9 MM 32-61-00. LANDING GEAR INDICATION OPS CHECKED GOOD ON GEAR SWING CHECKS.

Part: SOCKET — INTERMITTENT (COCKPIT) · airframe 54,981 hrs · 56,463 cycles

THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED INTERMITTANTLY AFTER GEAR WAS FULLY RETRACTED, AND CONTINUED TO INTERMITTANTLY ILLUMINATE FOR THE REMAINDER OF THE FLIGHT. FLIGHT CREW RECYCLED THE LANDING GEAR. MAINTENANCE INSPECTED AND REPLACED THE RIGHT MAIN LANDING GEAR UNSAFE INDICATION LIGHT SOCKET IAW DC-9 MM 32-61-00. LANDING GEAR INDICATION OPS CHECKED GOOD ON GEAR SWING CHECKS.

Part: WARNING SYSTEM — MALFUNCTIONED (MLG)

ON DEPARTURE OUT OF DSM, WHEN THE LANDING GEAR WAS RETRACTED, THREE GEAR UNSAFE LIGHTS REMAINED ILLUMINATED. RECYCLED THE GEAR WITH NORMAL OPERATION. ON APPROACH INTO CIA, WHEN THE GEAR WAS LOWERED, THE NOSE LANDING GEAR TOOK LONGER THAN NORMAL TO LOCK DOWN. CHECKED FOR FLUID LOSS/LEAKS, NONE NOTED. INSPECTED LANDING GEAR CONTROL SYSTEM, NO DEFECTS FOUND. PERFORMED ADJUSTMENT TEST OF POSITION AND WARNING SYSTEM. OPS CHECKS GOOD.

Part: PAN — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR PAN CRACKED AT NR 5 BEAM AT THE FORWARD UPPER CORNER AND THE FORWARD LOWER CORNER. REPAIRED DOOR PAN IAW DC9 SRM 52-03.

Part: INTERCOSTAL — CRACKED (BS 200-207)

DURING C-CHECK, FOUND INTERCOSTAL CRACKED BETWEEN STATION 200 AND 207 AT LONGERON 11 RIGHT. REPAIRED INTERCOSTAL IAW DC9 SRM DWG 05159.

Part: SPLICE — CRACKED (BS 718)

DURING C-CHECK, FOUND FLOORBEAM TO FRAME SPLICE PLATE CRACKED STATION 718 LEFT SIDE. REPLACE SPLICE PLATE IAW DC9 SRM.

Part: POWER SUPPLY — INOP (CABIN)

DURING PREDEPARTURE CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHTS DIM AND FLICKERING. REPLACED EMERGENCY LIGHT POWER SUPPLY.

Part: SPRING — WEAK (COCKPIT)

DURING PREFLIGHT WAS UNABLE TO OPEN CAPTAIN'S CLEARVIEW WINDOW. REPLACED AFT LOWER LATCH HOOK RETURN SPRING AND LUBRICATED WINDOW.

Part: WINDOW — LACK OF LUBE (COCKPIT)

CAPTAIN'S SLIDING WINDOW JAMMED WHEN OPENING. CLEANED AND LUBRICATED WINDOW IAW DC9 MM.

Part: LINK — CRACKED (NR 2 ENGINE)

DURING COMPLIANCE WITH AD 96-10-11, FOUND NR 2 ENGINE LOWER RIGHT THRUST REVERSER DRIVER LINK CRACKED. REPLACED THRUST REVERSER DRIVER LINK IAW DC9 MM 78-31-5.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, FOUND LONGERON 13R CRACKED AT STATION 965. REPAIRED FRAME IAW DC9 SRM 53-02.

Part: FRAME — CRACKED (BS 980)

DURING C-CHECK, FOUND FRAME CRACKED AT LONGERON 17R AND STATION 980. REPAIRED FRAME IAW DC9 SRM 53-03.

Part: SHEAR TIE — CRACKED (BS 965)

DURING C-CHECK, FOUND SHEAR TIE CRACKED AT LONGERON 17R AND STATION 965. REPLACED SHEAR TIE IAW DC9 SRM 51-30-5.

Part: LONGERON — CRACKED (BS 965)

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

Part: LONGERON — CRACKED (BS 237)

DURING C-CHECK, FOUND LONGERON 17R CRACKED AT STATION 237. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: LONGERON — CRACKED (BS 965)

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

Part: LINK — CRACKED (NR 2 ENGINE)

DURING COMPLIANCE WITH AD 96-10-11, FOUND NR 2 ENGINE UPPER LEFT THRUST REVERSER DRIVER LINK CRACKED. REPLACED THRUST REVERSER DRIVER LINK IAW DC9 MM 78-31-5.

Part: WINDOW HANDLE — BROKEN (COCKPIT)

FIRST OFFICER'S CLEARVIEW WINDOW (EMERGENCY EXIT) WOULD NOT EASILY OPEN. REPLACED CLEARVIEW WINDOW HANDLE ASSEMBLY.

Part: DOOR JAMB — CORRODED (FS 370-427)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON FORWARD LOWER CARGO COMPARTMENT DOOR JAMB AT LONGERON 29R FS 370 TO FS 427. REPLACED DOOR JAMB AND U-CHANNEL IAW DC-9 SRM CHAPTER 51-30-2.

Part: DOUBLER — DAMAGED (FS 408)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE INNER DOUBLER CUT OUT AT BOTTOM OF LOWER CARGO DOOR JAMB AT FS 408. REPAIRED INNER DOUBLER IAW ABX REA D953-10895-MR.

Part: FITTING — CORRODED (RUDDER)

DURING D-CHECK ACCEPTANCE INSPECTION WHILE PERFORMING DC-9 RUDDER OFF WING INSPECTION FOUND LEVEL II CORROSION ON FITTING. REPLACED FITTING IAW DC-9 OVERHAUL MANUAL 27-20-1.

Part: DOUBLER — CORRODED (FS 83)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE STEEL PLATE ALONG THE CENTER WINDSHIELD LOWER FRAME RUSTED AND HAD POPPED RIVETS. CLEANED AND TREATED PLATE IAW DC-9 SRM CHAPTER 51-10-3 AND REPLACED FASTENERS IAW DC-9 SRM CHAPTERS 51-30-2, 51-30-5 AND ABX REA D953-10945.

Part: DOOR — DAMAGED (FS 160)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD AIRSTAIR DOOR HAD A REPAIR ON A CRACK AT THE INNER RIB THAT WAS NOT IAW THE SRM. REPAIRED IAW ABX REA D952-10953-MR.

Part: SPAR — CRACKED (XRS 164)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT WING REAR SPAR CRACKED AT INBOARD LOWER HOLE FOR INBOARD FLAP HINGE. REPAIRED ANGLE IAW ABX REA D957-10642-SB.

Part: FITTING — CORRODED (FS 604)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON WING TO FUSELAGE FITTING ON TOP OF CENTER WING SECTION, RIGHT SIDE, AT STATION XCW 58 AND FS 604. REPLACED FITTING IAW DC-9 SRM CHAPTERS 51-30-5 AND 51-20-0.

Part: SKIN — CORRODED (FS 218-256)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT FORWARD FUSELAGE SKIN HAD CORROSION AND A PREVIOUS REPAIR THAT WAS NOT IAW THE SRM, FROM FS 218 TO 256 AND BETWEEN LONGERON'S 14 AND 16 RIGHT. REPAIRED FUSELAGE SKIN IAW ABX REA D953-10849-MR.

Part: FRAME — GOUGED (FS 362)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND FUSELAGE FRAME GOUGED AT FS 362, BETWEEN LONGERON 29 AND 30R. REPAIRED FUSELAGE FRAME IAW ABX REA D953-10947-MR.

Part: LONGERON — CRACKED (FS 237)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 30 CRACKED AT FS 237. REPLACED LONGERON 30 FROM FS 237 TO FS 579, IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.

Part: BASE — CORRODED (LT FLAP)

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

Part: FRAME — CORRODED (FS 1089)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE FUSELAGE FRAME TEE AT FS 1089 BETWEEN LONGERON 11 AND 12 LEFT. REPAIRED TEE IAW ABX REA D953-10888-MR.

Part: STIFFENER — CORRODED (FS 1089)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON STIFFENER ON AFT FACE OF CANTED BULKHEAD 1089 AT LONGERON 6 LEFT. REPLACED STIFFENER IAW DC-9 SRM CHAPTER 51-30-2.

Part: STIFFENER — CORRODED (FS 1089 BLKHD)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON STIFFENER ON AFT FACE OF CANTED BULKHEAD 1089 AT LONGERON 8 LEFT. REPLACED STIFFENER IAW DC-9 SRM CHAPTER 51-30-2.

Part: ANGLE — CRACKED (FS 650)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A L ANGLE CRACKED ABOVE THE CENTER WING TANK AT FS 650 AND LBL 44. REPLACED ATTACH ANGLE IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.

Part: STIFFENER — CORRODED (FS 1089 BLKHD)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON STIFFENER ON AFT FACE OF CANTED BULKHEAD 1089 AT LONGERON 11 LEFT. REPLACED STIFFENER IAW DC-9 SRM CHAPTER 51-30-2.

Part: RIB CAP — CRACKED (YN 170)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A CRACK ON THE NR 2 ENGINE PYLON RIB CAP AT STATION YN 170. REPAIRED RIB CAP IAW ABX REA D954-10691-MR.

Part: FRAME — CORRODED (FS 1121)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE FUSELAGE FRAME AT FS 1121, UPPER PORTION OF -17 FRAME BETWEEN LONGERON 29 LEFT TO 29 RIGHT. REPAIRED FUSELAGE FRAME IAW ABX REA D953-10916-MR.

Part: FITTING — CRACKED (FS 1121)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND FUSELAGE FRAME FITTING CRACKED AT FS 1121. REPLACED FITTING IAW DC-9 SRM CHAPTERS 51-30-2, 51-30-5 AND 51-30-3.

Part: SKIN — DAMAGED (FS 889)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND AN IMPROPER REPAIR ON THE FUSELAGE EXTERIOR SKIN AT FS 889 AND LONGERON 21 RIGHT. REPAIRED SKIN IAW ABX REA D953-10806-MR.

Part: LONGERON — CORRODED (FS 333)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON LONGERON 27, RIGHT LOWER SURFACE, AFT OF FS 333. REPLACED LONGERON 27 RIGHT IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.

Part: SPAR — CORRODED (LT FLAP)

DURING D-CHECK ACCEPTANCE INSPECTION WHILE PERFORMING DC-9 FLAP OFF WING INSPECTION ON LEFT FLAP, FOUND LEVEL II CORROSION ON LOWER AFT SPAR. BLENDED AND TREATED FOR CORROSION PER DC-9 SRM 51-10-3. REPAIRED SPAR IAW DC-9 SRM 57-06.

Part: SPAR — CORRODED (LT FLAP)

DURING D-CHECK ACCEPTANCE INSPECTION WHILE PERFORMING DC-9 FLAP OFF WING INSPECTION ON LEFT FLAP, FOUND LEVEL II CORROSION ON UPPER AFT SPAR AT STA. FLS. 114. BLENDED AND TREATED FOR CORROSION PER DC-9 SRM 581-10-3. REPAIRED SPAR PER DC-9 SRM 57-06.

Part: CAP — CORRODED (LT FLAP)

DURING D-CHECK ACCEPTANCE INSPECTION WHILE PERFORMING DC-9 FLAP OFF WING INSPECTION ON THE LEFT FLAP, FOUND LEVEL II CORROSION ON LEADING EDGE NOSE CAP AT STA. XFLS 176. REPLACED IAW DC-9 SRM 57-50-9.

Part: PANEL — DELAMINATED (WS 164)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND DELAMINATION ON THE RIGHT WING INBOARD GROUND SPOILER PANEL. REPLACED PANEL IAW DC-9 M.M. 27-62-1.

Part: SKIN — CORRODED (LT ELEV TAB)

DURING OFF WING INSPECTION PROCEDURES FOUND LEVEL II CORROSION ON THE LEFT ELEVATOR TAB INBOARD LOWER SKIN. REPAIRED IAW DC-9 SRM 57.

Part: SKIN — CORRODED (FS 229-512)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD LOWER FUSELAGE SKIN FROM FS 229 TO FS 512, FROM LONGERON 18R TO 26R, HAD NUMEROUS AREAS OF CORROSION AND PREVIOUS REPAIRS. REPLACED SKIN FROM FS 229 TO FS 512 IAW ABX REA D953-10751-MR AND DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.

Part: PANEL — CORRODED (XRS 509)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE RIGHT WING OUTBOARD TRAILING EDGE PANEL JUST FORWARD OF THE AILERON. REPLACED PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.

Part: BULKHEAD SKIN — DENTED (FS 996)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A DENT AND PUNCTURE IN AFT PRESSURE BULKHEAD SKIN, FORWARD FACE, BETWEEN LONGERON 29R AND 30R APPROXIMATELY EIGHT INCHES UP FROM TEE CAP. REPAIRED IAW DC-9 SRM CHAPTER 53-01, FIGURE 1, SHEET 2.

Part: SPAR CAP — CORRODED (WS 494.5)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE LEFT WING LOWER REAR SPAR TEE CAP AT STATION XRS 494.5. REPAIRED LEFT WING LOWER SPAR CAP IAW ABX REA D957-10793-MR.

Part: PANEL — DELAMINATED (WS 414)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION AND DELAMINATION ON THE LEFT WING TRAILING EDGE BONDED PANEL JUST FORWARD OF LEFT AILERON. REPLACED PANEL IAW DC-9 SRM 51-30-1 AND 51-30-2.

Part: SPAR CAP — CORRODED (WS 509-563)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE RIGHT WING REAR SPAR LOWER TEE CAP FROM XRS 509 TO XRS 563. REPAIRED RIGHT WING REAR SPAR IAW ABX REA D957-10641-MR.

Part: FLOOR BEAM — CORRODED (FS 965)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE FLOOR BEAM AT FS 965 AT RBL 22. REPAIRED FLOOR BEAM IAW ABX REA D953-10811-MR.

Part: LONGERON — CRACKED (FS 256-351)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 29L CRACKED AFT OF STATION 256 AND 351. REPLACED LONGERON 29L FROM FS 237 TO FS 522 IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.

Part: SKIN — CORRODED (FS 996)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON A SKIN REPAIR ON AFT FUSELAGE SKIN FROM FS 996 TO FS 1034 AT LONGERON 23 LEFT. REPAIRED AFT FUSELAGE SKIN IAW ABX REA D953-10834-MR.

Part: FRAME — CRACKED (FS 1132)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A CRACK ON THE FUSELAGE FRAME 1132, LEFT SIDE BELOW CATWALK. REPLACED FRAME IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.

Part: RIB — CORRODED (LT FLAP)

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

Part: SKIN — CORRODED (FS 802-996)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON AFT FUSELAGE LOWER SKIN FROM FS 802 TO FS 996, BETWEEN LONGERON 26 RIGHT TO 26 LEFT. REPLACE LOWER SKIN FROM FS 802 TO FS 996 IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.

Part: SKIN — CORRODED (FS 120)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON FUSELAGE SKIN FORWARD OF E AND E COMPARTMENT ENTRY DOOR BETWEEN LONGERON 28 RIGHT AND 29 RIGHT. REPAIRED IAW DC-9 SRM CHAPTER 53-01, FIGURE 4, SHEET 3.

Part: SPAR — CORRODED (XRS 488-560)

DURING C-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE LOWER FLANGE OF THE RIGHT WING LOWER REAR SPAR FROM XRS 488 TO XRS 560. REPAIRED RIGHT WING LOWER REAR SPAR IAW ABX REA D957-10795-MR.

Part: RETAINER — CRACKED (FS 120)

DURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH A.D. 90-18-03; S.B. 56-11, REV 3 X-RAY INSPECTION OF THE RIGHT COCKPIT EYEBROW WINDOW RETAINER, FOUND A CRACK INDICATION. REPAIRED CRACK IAW ABX REA D956-10760 AND EA NR AD-56-3239.

Part: RETAINER — CRACKED (FS 120)

DURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH A.D. 90-18-03; SB 56-11, REV 3 X-RAY INSPECTION OF LEFT COCKPIT EYEBROW WINDOW RETAINER, FOUND A CRACK INDICATION. REPAIRED CRACK IAW ABX REA D956-10760 AND EA NR AD-56-3239.

Part: PANEL — DELAMINATED (XRS 69)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION AND DELAMINATION ON THE LEFT WING UPPER BONDED PANEL INBOARD OF THE GEAR TRUNNION. REPLACED UPPER BONDED PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.

Part: SPAR CAP — CORRODED (WS 387-395)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE RIGHT WING LOWER SPAR CAP BETWEEN XRS 387 AND XRS 395. REPAIRED RIGHT WING REAR LOWER SPAR CAP IAW ABX REA D957-10715-MR.

Part: RETAINER — CORRODED (FS 120)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE CAPTAIN'S CLEARVIEW WINDOW RETAINER. REPAIRED RETAINER IAW ABX REA D953-10757-MR.

Part: SKIN — CORRODED (FS 588-669)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON FUSELAGE EXTERIOR SKIN FROM FS 588 SPLICE TO FS 669 SPLICE AT LONGERON 26 LEFT TO 26 RIGHT. REPLACED SKIN IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.

Part: SPAR — CORRODED (WS 488-520)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE LEFT WING LOWER REAR SPAR FROM STATION XRS 488 TO XRS 520. REPAIRED LEFT WING LOWER REAR SPAR IAW ABX REA D957-10692-MR.

Part: SKIN — GOUGED (FS 150)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT FUSELAGE SKIN GOUGED AT THE ENTRY DOOR FORWARD JAMB, SECOND PRESSURE STOP FROM BOTTOM. REPAIRED SKIN IAW ABX REA D953-10696-MR.

Part: SPAR — CORRODED (XRS 385-390)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE LEFT WING LOWER REAR SPAR CAP BETWEEN XRS 385 AND XRS 390. REPAIRED LEFT WING LOWER REAR SPAR CAP IAW ABX REA D957-10773-MR.

Part: ANGLE — CORRODED (FS 604)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD END OF THE CANTED KEEL ATTACH ANGLE HAD CORROSION REMOVAL THROUGH TWO FASTENER HOLES. REPAIRED CANTED KEEL ATTACH ANGLE IAW ABX REA D953-10752-MR.

Part: SPAR CAP — CORRODED (WS 515)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION BLEND OUT THAT EXCEEDED THE SRM LIMITS. LEFT WING REAR SPAR AT APPROXIMATELY WING STATION XRS 515. REPAIRED LEFT WING REAR SPAR TEE CAP IAW ABX REA D957-10701-MR.

Part: FLOOR BEAM — CORRODED (FS 996)

DURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH EA FS533747, FOUND A FLOOR BEAM UPPER CAP AND WEB CORRODED AT FS 996 BETWEEN RBL 47 AND LBL 47. REPLACED UPPER FRAME CAP AND REPAIRED WEB IAW ABX REA D953-10666-MR.