N979AX

Part: THERMAL SWITCH — DEFECTIVE (COCKPIT) · airframe 63,473 hrs · 75,185 cycles

DURING DESCENT INTO PIE, THERE WAS A ELECTRICAL SMELL IN THE COCKPIT NEAR FIRST OFFICER'S CLEARVIEW WINDOW. INSPECTED WIRING BEHIND RIGHT CONSOLE, OVERHEAD CONSOLE AND WIRING HARNESS IN E & E COMPARTMENT. NO BURNT OR DAMAGED WIRING NOTED. SUSPECT FIRST OFFICER'S CLEARVIEW WINDOW THERMAL SWITCH. REPLACED THERMAL SWITCH IAW DC9 MM 30-41-02.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 63,447 hrs · 75,162 cycles

AFT PRESSURE BULKHEAD LEFT DOOR CORNER SKIN HAD RADIAL CRACK OF UNKNOWN LENGTH IN LOWER INBOARD PORTION ONLY. NO PREVIOUS REPAIRS INSTALLED. REPAIRED LEFT LOWER CORNER DOOR OF AFT PRESSURE BULKHEAD IAW DWG J060088-525.

Part: STRUCTURE — CORRODED (COCKPIT) · airframe 63,447 hrs · 75,162 cycles

COCKPIT SUBFLOOR CHAFED IN SEVERAL LOCATIONS AT STA 160 AND 148. REPAIRED AREA IAW DC9 SRM 53-01.

Part: FITTING — CORRODED (FUSELAGE) · airframe 63,447 hrs · 75,162 cycles

FITTING EXFOLIATED ON SLANT PANEL UNDER LEFT BUTT LINE 22 AT STA 737. REPLACED FITTING IAW DC9 SRM.

Part: BULB — INOPERATIVE (MLG INDICATOR) · airframe 63,299 hrs · 75,022 cycles

LEFT MAIN GEAR GREEN DOWNLOCK LIGHT FAILED TO COME ON FOR LANDING. ALT GEAR LIGHT INDICATED GEAR DOWN. RECYCLED LANDING GEAR AND LIGHT CAME ON AFTER A TIME. FOUND BOTH LEFT GEAR INDICATION LIGHT BULBS MUSHROOMED AT CONTACTS. RELAMPED BULB AS REQUIRED. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,240 hrs · 74,953 cycles

EMERGENCY EXIT LIGHTS GO OFF AFTER 5 SECONDS. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8-0001.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 63,022 hrs · 74,722 cycles

EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC9 MM 33-53-02-4.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 62,152 hrs · 73,864 cycles

SHEAR TIE CRACKED AT LONGERON 27 LEFT, FS 695. REPAIRED IAW DC-9 SSRM DWG K05159 AND DC-9 SRM 51-30-5.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,152 hrs · 73,864 cycles

END FITTING LONGERON 30, CRACKED FS 644, LEFT SIDE. REMOVED AND REPLACED END FITTING AT LONGERON 30, FS 644 IAW DC-9 SRM 51-30-5.

Part: FITTING — CRACKED (BS 617) · airframe 62,152 hrs · 73,864 cycles

LONGERON 25 LEFT, END FITTING CRACKED, STA 617. REMOVED AND REPLACED LONGERON 25 LEFT END FITTING IAW DC-9 SRM.

Part: PAN — CRACKED (AFT CARGO DOOR) · airframe 62,152 hrs · 73,864 cycles

AFT LOWER CARGO DOOR CRACK INDICATION IN RADIUS OF OUTER, ADJACENT TO TOP MOST STOP. REPAIRED DOOR IAW DC-9 SRM 52-03, 51-30-7, 51-30-1, 51-20-0 AND 51-30-5.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 61,064 hrs · 72,753 cycles

EMERGENCY LIGHTS INOPERATIVE, LOW CHARGE. REPLACED EMERGENCY LIGHT BATTERY PACK POWER SUPPLY IAW DC9 MM. OPS CHECK GOOD.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 60,977 hrs · 72,674 cycles

LONGERON 30 CRACKED LEFT AND RIGHT FLANGES SM 243 - 245. REPLACED LONGERON 30, STA 230 - 265 IAW REA D953-48386MR.

Part: RIB — CRACKED (RT WING L/E) · airframe 60,977 hrs · 72,674 cycles

RIGHT WING LEADING EDGE NOSE RIB INBOARD SIDE OF NR 1 SLAT DRIVER HAD 2 CRACKS ON REPAIR MARKED, REA 43261, CRACKED IN FORWARD RADIUS AND AFT BETWEEN HI-LOKS. REPLACED LEADING EDGE RIB IAW DC-9 SRM 51-30-5 AND 51-30-2.

Part: SOCKET — WORN (MLG INDICATOR) · airframe 60,535 hrs · 72,209 cycles

ON GEAR EXTENSION INTO PIE, GEAR DOOR OPEN LIGHT NEVER ILLUMINATED. BULB CHECKED GOOD. GEAR RECYCLED. ON NEXT EXTENSION IT DID NOT COME ON BUT ONLY FOR 1 SECOND, NOT THE NORMAL 30 SECONDS. VERIFIED, FOUND GEAR DOOR OPEN LAMP WORN WHICH CAUSED AN INTERMITTENT PROBLEM. OPS CHECKED GOOD IAW DC-9 AMM 32-60-00-0.

Part: COALESCER BAG — DIRTY (A/C BAY) · airframe 60,132 hrs · 71,775 cycles

AIR CONDITIONING SMELLED DURING HIGH POWER SETTINGS. REPLACED BOTH COALESCER BAGS IAW DC9 MM 21-20-02-2.

Part: COALESCER BAG — DIRTY (A/C BAY) · airframe 60,112 hrs · 71,755 cycles

AIR CONDITIONING SUPPLY AIR SMELLED HOT OR OILY AT HIGHER (CRUISE) POWER SETTINGS. REPLACED BOTH WATER SEPARATOR COALESCER BAGS IAW DC9 MM 21-20-02-2.

Part: BULKHEAD — CRACKED (RT WING) · airframe 59,900 hrs · 71,533 cycles

RIGHT WING LEADING EDGE BULKHEAD CRACKED AT LOWER FASTENER ON INBOARD SIDE OF NR 2 SLAT TRACK. REPAIRED AREA IAW DC-9 REA D957-43261.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 59,900 hrs · 71,533 cycles

UPPER HORIZONTAL STIFFENER CRACKED ON OUTBOARD END FORWARD FACE OF AFT PRESSURE BULKHEAD RIGHT SIDE. REPAIRED STIFFENER IAW DC-9 SSRM K05159.

Part: WEB — CRACKED (FUSELAGE) · airframe 59,900 hrs · 71,533 cycles

CUSP WEB CRACKED AT STATION 239 RBL 56. REPAIRED AREA IAW DC-9 SRM 53-01.

Part: LONGERON — CRACKED (FWD. CARGO) · airframe 59,900 hrs · 71,533 cycles

LONGERON 30 CRACKED AT LEFT FLANGE STATION 232 UNDER SPLICE. REPAIRED AREA IAW DC-9 REA D953-43229.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,900 hrs · 71,533 cycles

FUSELAGE FRAME STATION 1152 WAS CRACKED AT LONGERON 15 RIGHT. REPAIRED CRACKED SECTION OF FRAME AT STATION 1152 LONGERON 15 RIGHT IAW DC-9 SRM 53-03.

Part: DOOR — CRACKED (EXT. FUSELAGE) · airframe 59,900 hrs · 71,533 cycles

LEFT ENTRY DOOR LOWER AFT CORNER SKIN WAS CRACKED. REPAIRED ENTRY DOOR SKIN IAW DC-9 SRM 52-05.

Part: DOUBLER — CRACKED (LT MLG DOOR) · airframe 59,900 hrs · 71,533 cycles

REPAIR CRACKED ON FORWARD UPPER CORNER OF INBOARD GEAR DOOR. REPAIRED AREA IAW DC-9 SRM 52-05. REINSTALLED INBOARD MAIN LANDING GEAR DOOR IAW DC-9 MM 32-12-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,900 hrs · 71,533 cycles

SKIN CRACKED AT LEFT REAR CUTOUT FOR LEFT AFT NOSE GEAR DOOR. REPAIRED IAW DC-9 SRM 53-01. INSTALLED ROD IAW DC-9 MM 20-16-0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,900 hrs · 71,533 cycles

FORWARD LOWER CORNER CUTOUT HAD APPROXIMATELY .1250 INCH CRACK. REPAIRED DAMAGED AREA IAW DC-9 SRM 51-10-2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,900 hrs · 71,533 cycles

CRACK IN THE FORWARD SERVICE DOOR HOLD OPEN CUP. REPLACED THE FORWARD SERVICE DOOR HOLD OPEN CUP IAW DC-9 SRM 51-30-5.

Part: ROD END — CORRODED (RT MLG DOOR) · airframe 59,900 hrs · 71,533 cycles

RIGHT MAIN LANDING GEAR OUTBOARD DOOR LINKAGE ROD (FROM CRANK TO DOOR) CORRODED AT DOOR END. RIVET WAS CORRODED, RUST BLEEDING FROM ROD END, PLAY WHERE ROD END ATTACHES TO ROD. REPLACED DOOR ROD PANEL IAW DC-9 AMM.

Part: BATTERY — DISCHARGED (FUSELAGE) · airframe 55,355 hrs · 51,753 cycles

THE COCKPIT EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE COCKPIT EMERGENCY LIGHT BATTERIES IAW DC-9 MM 33-53-00. LATER ON 02/13/01 MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY AS A RELIABILITY PRECAUTION IAW DC-9 MM 33-53-02.

Part: SWITCH — DEFECTIVE (LEFT MLG) · airframe 58,971 hrs · 70,703 cycles

UPON LOWERING LANDING GEAR ON APPROACH, THE LEFT MAIN LANDING GEAR GREEN DOWN AND LOCKED INDICATION LIGHT WOULD NOT ILLUMINATE. CREW COMPLIED WITH ABNORMAL CHECKIST. MAINTENANCE INSPECTED AND REPLACED THE LEFT MAIN LANDING GEAR DOWN LOCK SWITCH. OPS CHECKS WERE SATISFACTORY IAW DC-9 MM 32-60-01.

Part: CYLINDER — WORN (RT MLG WW) · airframe 58,771 hrs · 70,533 cycles

ON GEAR RETRACTION OUT OF ILN, RIGHT GEAR UNSAFE AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES, LIGHTS REMAINED ON. REPLACED RIGHT MAIN LANDING GEAR RETRACT CYLINDER.

Part: SPAR — CRACKED (LT ELEVATOR)

TOP OF LEFT ELEVATOR SPAR CRACKED IN 8 PLACES, STATION 204 TO 220. REPLACED ELEVATOR SPAR IAW DC9 DWG 9918450.

Part: WIRE — BROKEN (RT MLG DOWNLOCK)

NO RIGHT MAIN LANDING GEAR INDICATION WITH THE GEAR HANDLE DOWN. PERFORMED GEAR RECYCLE, ALTERNATE GEAR INDICATION CONFIRMED GEAR DOWN AND LOCKED. GOT GPWS GEAR, TOO LOW ON FINAL. SATISFACTORY LANDING ACCOMPLISHED AFTER FLY-BY GEAR INSPECTION. REPAIRED BROKEN WIRE TO RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH.

Part: WIRE — FAILED (E & E COMPT)

DURING TAXI OUT, HEARD POPPING NOISE FROM AC BUS AND OBSERVED ELECTRICAL SMOKE. REPLACED BURNT WIRES AT AC BUS.

Part: SPAR — CRACKED (LT ELEVATOR)

WHILE COMPLYING WITH AD 79-19-02, FOUND LEFT ELEVATOR CRACKED IN FRONT SPAR AREA. REPLACED ELEVATOR IAW DC9 MM 27-30-02 AND 27-30-03.

Part: LONGERON — CRACKED (BS 1041)

DURING C-CHECK, FOUND CRACK IN LONGERON 16 LT, STATION 1041. REPAIRED IAW DC9 SRM 53-02.

Part: LONGERON — CRACKED (BS 1021)

DURING C-CHECK, FOUND CRACK IN LONGERON 17 RT, STATION 1021. REPLACED LONGERON SECTION IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: SPAR — CRACKED (LT ELEVATOR)

LEFT ELEVATOR SPAR CRACKED IN 4 PLACES. REPAIRED UNIT IAW DC9 SRM.

Part: LATCH — DEFECTIVE (COCKPIT DOOR)

AFTER LANDING, FOUND COCKPIT DOOR WOULD NOT OPEN FROM THE OUTSIDE. REPLACED COCKPIT DOOR LATCH.

Part: BLKHD STIFFENER — CRACKED (AFT PRESS BLKD)

DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT LONGERON 15R AND 16R. REPLACED STIFFENER IAW DC9 SRM 51-30-5.

Part: BLKHD STIFFENER — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT LONGERON 14R. REPLACED STIFFENER IAW DC9 SRM 51-30-5.

Part: FRAME — GOUGED (BS 756-775)

DURING C-CHECK, FOUND WINDOW FRAME BETWEEN STA 756 TO 775 RIGHT SIDE GOUGED. REPLACED WINDOW FRAME (P/N 591228507).

Part: FITTING — CRACKED (HORIZ STAB)

DURING C-CHECK, FOUND THE FITTING AT THE AFT END OF THE HORIZONTAL STABILIZER CENTER SPAR BOX CRACKED AT THE UPPER FLANGE FOR PANEL NUMBER 3902. REPLACED FITTING IAW DACO DRAWING 5912981 AND DC9 S/B 55-32.

Part: SKIN — DAMAGED (BS 737-794)

DURING C-CHECK, FOUND THE WINDOW BELT PANEL (P/N 9911535-1) BETWEEN FUSE STA 737 TO 794, RIGHT SIDE WAS DAMAGED. REPLACED WINDOW BELT PANEL, IAW DC9 SRM 51-30-2.

Part: BULKHEAD SKIN — GOUGED (AFT PRESS BULK)

DURING C-CHECK, FOUND GOUGES ON THE AFT PRESSURE BULKHEAD SKIN FORWARD SIDE AT LONGERON STA 23R. BLENDED OUT GOUGES, INSTALLED DOUBLER IAW ABX REA NR D953-18898-MR.

Part: RIB — CRACKED (WS 531)

DURING C-CHECK, FOUND THE LEFT WING LEADING EDGE RIB JUST INBD OF STA XRS 531 IS CRACKED INSIDE RADIATING FROM HI-LOCK. REPLACED RIB IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: PIN — WORN (RT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07 ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR WING MOUNTED HINGE WORN. REPLACED HINGE PINS IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: BUSHING — WORN (LT MLG ACTUATOR)

DURING COMPLIANCE OF AD 91-22-07 ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD ACTUATOR ROD END BUSHINGS WORN. REPLACED SPACERS IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: BUSHING — WORN (RT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07 ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR WING MOUNTED HINGE WORN. REPLACED HINGE BUSHINGS IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: BATTERY PACK — DISCHARGED (CABIN)

UPON COCKPIT INSPECTION, FOUND EMERGENCY LIGHT SWITCH IN THE ON POSITION. EMERGENCY BATTERIES VOLTS AT ZERO. REPLACED TWO EACH NICAD BATTERIES FOR EMERGENCY LIGHTING SYSTEM IAW DC-9 SUPP MM 33-53-0 AND OPS CHECKED GOOD.

Part: ENGINE — SEIZED (RIGHT)

RIGHT ENGINE SEIZED ON TAKEOFF ROLL. TAKEOFF ABORTED. REPLACED RIGHT ENGINE.

Part: SKIN — CORRODED (FS 993)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND MULTIPLE DAMAGED AND CORRODED AREAS ON THE AFT LOWER CARGO COMPARTMENT DOOR JAMB. REPAIRED DOOR JAMB IAW ABX REA D953-11800-MR.

Part: DOOR JAMB — CORRODED (FS 993)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE AFT LOWER CARGO DOOR INTERNAL WEB ON THE DOOR JAMB CORRODED. REPAIRED AFT LOWER CARGO DOOR JAMB WEB IAW ABX REA D953-11804-MR.

Part: HINGE FITTING — WORN (LT TE FLAP)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT OUTBOARD FLAP HINGE FITTING BEARING HOLE ELONGATED. REPAIRED IAW ABX REA D927-12127-MR.

Part: BEARINGS — WORN (BS 775)

DURING D - CHECK INSPECTION WHILE COMPLYING WITH A.D. 91-22-07; A.S.B. 32-244, FOUND THE RIGHT OUTBOARD MAIN LANDING GEAR DOOR ACTUATING ROD ASSEMBLY HAD WORN BEARINGS. REPLACED ACTUATING ROD END AND BEARINGS IAW DC-9 M.M., CHAPTER 32-10-6.

Part: WINDOW BELT — CORRODED (FS 756)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT WINDOW BELT AT FS 756 HAD PREVIOUS CORROSION BLEND OUTS THAT WERE BEYOND SRM LIMITS. REPAIRED RIGHT WINDOW BELT SECTION NR 27R IAW ABX REA D953-12047-MR.

Part: LE SKIN — CORRODED (RT ENGINE PYLON)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A PREVIOUS REPAIR CORRODED AT THE LEADING EDGE OF THE RIGHT ENGINE PYLON. REPAIRED IAW ABX REA D953-11882-MR.

Part: BLKHD TEE — GOUGED (FS 1072)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LOWER T-CAP GOUGED IN TWO PLACES AT LONGERON 30. REPLACED LOWER T-CAP SECTIONS IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.

Part: SEAL DEPRESSOR — DAMAGED (FS 200)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT FORWARD ENTRY DOOR SEAL DEPRESSOR DAMAGED AT LONGERON 10L. REPLACED SEAL DEPRESSOR IAW DC-9 SRM CHAPTER 51-30-2.

Part: JAMB — CRACKED (FS 200)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD ENTRY DOOR JAMB INNER SKIN CRACKED AT LONGERON 11L. REPAIRED ENTRY DOOR JAMB INNER SKIN IAW ABX REA D953-11995-MR.

Part: JAMB — CRACKED (FS 1165)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT AND RIGHT VENTRAL STAIRWAY JAMBS CRACKED AT EXISTING REPAIRS. REPAIRED VENTRAL STAIRWAY JAMBS IAW ABX REA D953-11964-MR.

Part: SPAR CAP — DAMAGED (WS 164)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A PREVIOUS REPAIR ON THE RIGHT WING REAR SPAR AT WS 164.0. REMOVED REPAIR, INSPECTED AREA IAW ASB 57-146. REPAIRED AREA IAW ABX REA D957-11745-MR.

Part: SKIN — NO EDGE DISTANT (FS 541-643)

DURING D-CHECK ACCEPTANCE INSPECTION WHILE REPLACING THE RIGHT WINDOW BELT PANEL, FROM FS 541 TO 643, FOUND THE PANEL HAD NO EDGE DISTANCE ON ONE FASTENER IN THE LOWER AFT CORNER. REPAIRED IAW ABX REA D953-11945-MR.

Part: WEB — DAMAGED (FS 1041)

DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, WHILE REPLACING THE LEFT CUSP WEB AT FS 1041, THE WEB WAS CUT SHORT OF REQUIRED INSTALLATION UNDER THE FRAME FOOT, STA 1041 LEFT SIDE. REPAIRED CUSP WEB IAW ABX REA D953-11947-MR.

Part: LONGERON — CORRODED (FS 879-1031)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 30 CORRODED BETWEEN FS 879 AND FS 1031. REPLACED LONGERON 30 SECTION IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.

Part: FITTING — CORRODED (VERT STAB)

WHILE COMPLYING WITH C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE HORIZONTAL STABILIZER, LEFT INBOARD HINGE ATTACH LUG ON THE VERTICAL STABILIZER CORRODED IN THE BEARING BORE. REPAIRED IAW ABX REA D955-11-55-MR.

Part: SKIN — CORRODED (ELEVATOR)

DURING CARGO MOD, DC-9 ELEVATOR OFF WING PROCEDURES, FOUND LEVEL 2 CORROSION ON THE LOWER OUTBOARD SKIN AROUND DOUBLERS. REPLACED SKIN IAW DC-9 SRM 55-21-0.

Part: SKIN — CORRODED (LT ELEVATOR)

DURING CARGO MOD, DC-9 ELEVATOR OFF WING PROCEDURES, FOUND LEVEL 2 CORROSION ON THE CENTER SKIN. REPLACED CENTER SKIN IAW DC-9 SRM 55-21-0.

Part: PAN — DENTED (FS 200)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE SERVICE DOOR JAMB PAN DENTED AT BAYONET FITTING. REPAIRED SERVICE DOOR PAN IAW ABX REA D953-11734-MR.

Part: WINDOW BELT — MISDRILLED (FS 465)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND DURING REPLACEMENT OF WINDOW BELT PANEL, THAT THE UPPER AND LOWER AFT CORNER FASTENER HOLES HAD SHORT EDGE DISTANCE AT FS 465R. REPAIRED WINDOW BELT PANEL IAW ABX REA D953-11822-MR.

Part: PAN — DAMAGED (FS 200)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE SERVICE DOOR PAN REQUIRED REPAIR DUE TO ACCOMPLISHMENT OF CUSP ANGLE REPAIRS. REPAIRED SERVICE DOOR PAN IAW ABX REA D953-11737-MR.

Part: BLKHD WEB — CHAFED (FS 1072)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE AFT PRESSURE BULKHEAD CHAFED ON THE LEFT SIDE BELOW THE LOWER FIRE EXTINGUISHER BOTTLE. REPAIRED AFT PRESSURE BULKHEAD WEB IAW ABX REA D953-11758-MR.

Part: SKIN — CORRODED (FS 794-879)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE AFT LOWER CARGO COMPARTMENT FORWARD EXTERIOR SKIN FROM LONGERON 26L TO 26R CORRODED FROM FS 794 TO FS 879. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTERS 51-104, 51-30-2 AND 51-30-5 AND PFEA D953-9883.

Part: LONGERON — CORRODED (FS 794)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 30 BLENDED. CORROSION WAS BEYOND SRM LIMITS AT FS 794. REPLACED LONGERON 30 IAW DC-9 SRM CHAPTERS 51-30-1, 51-30-5 AND 51-10-4.

Part: FITTING — GOUGED (VERT STAB)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT AND RIGHT ATTACH FITTINGS ON THE VERTICAL STABILIZER GOUGED AT HORIZONTAL STABILIZER JACKSCREW GIMBAL ATTACH POINTS. REPAIRED FITTINGS IAW ABX REA D955-11779-MR.

Part: BLKHD FASTENER — MISLOCATED (FS 1041)

DURING D - CHECK INSPECTION, FOUND THE BULKHEAD AT FS 1041, VERTICAL BRACE, LOWER FASTENER, HAD IMPROPER EDGE DISTANCE ON THE LEFT SIDE. REPAIRED BRACE IAW ABX REA D953-11754.

Part: WINDOW BELT — MISDRILLED (FS 389)

DURING D-CHECK ACCEPTANCE INSPECTION, WHILE REPLACING THE WINDOW BELT PANEL AT FS 389, FOUND THE UPPER AND LOWER AFT CORNER FASTENER HOLES HAD SHORT EDGE DISTANCE. REPAIRED WINDOW BELT IAW ABX REA D953-11780-MR.

Part: DOOR ARM — WORN (BS 775)

DURING D - CHECK INSPECTION WHILE COMPLYING WITH A.D. 91-22-07; A.S.B. 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR HAD EXCESSIVE PLAY ON FLYING DOOR ARM. REPLACED RIGHT MAIN LANDING GEAR DOOR ARM ASSEMBLY AND BEARINGS IAW DC-9 M.M., CHAP. 32-10-6.

Part: TRUNNION FITTING — CORRODED (LT MLG)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT MAIN LANDING GEAR TRUNNION FITTING CORRODED AT THE FORWARD ATTACH LUG. REPLACED TRUNNION FITTING IAW ABX EA SB57-03131-MA.

Part: WINDOW BELT — MISDRILLED (FS 541-636)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT WINDOW BELT SECTION FROM FS 541 TO FS 636 HAD SHORT RIVET EDGE DISTANCE ON ONE FASTENER. REPLACED WINDOW BELT SECTION IAW DC-9 SRM CHAPTERS 51-30-2, 51-30-5 AND REPAIRED SHORT EDGE DISTANCE AREA IAW ABX REA D953-11707-MR.

Part: INTERCOSTAL — DAMAGED (FS 180)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND AN INTERCOSTAL AT FS 180 AND BL 0 TO LBL 22 HAD AN IMPROPER REPAIR. REPAIRED IAW ABX REA D953-11736-MR.

Part: STRINGER — DAMAGED (WS 200)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEFT WING STRINGER NR 26 HAD PREVIOUS REPAIR AT XRS 200 THAT WAS NOT IAW THE SRM. REPAIRED LEFT WING STRINGER IAW ABX REA D957-11735-MR.

Part: FLOORBEAM — CHAFED (FS 200)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A FLOORBEAM CHAFED AT FS 200 IN THE MAIN CABIN. REPAIRED FLOORBEAM AT FS 200 IAW ABX REA D953-11699-MR.

Part: INTERCOSTAL — CRACKED (BS 37-44)

DURING D - CHECK INSPECTION, FOUND THE UPPER SIDE CRACKED ON AN INTERCOSTAL, BETWEEN FS 37 AND FS 44. REPLACED INTERCOSTAL IAW DC-9 SRM, CHAPTERS 51-30-2 AND 51-30-5.

Part: PAN — DAMAGED (FS 370-442)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR PAN DENTED AND BOWED. ALSO, THERE WERE SOME DOUBLE DRILLED RIVET HOLES. REPAIRED FORWARD LOWER DOOR JAMB PAN IAW ABX REA D953-11714-MR.

Part: SKIN — CRACKED (FS 101)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A PREVIOUSLY INSTALLED RIGHT SKIN DOUBLER CRACKED AT AFT HINGE OF RIGHT NOSE LANDING GEAR AFT DOOR. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-10-2.

Part: RETAINER — CRACKED (BS 680)

DURING D - CHECK INSPECTION, FOUND THE LEFT WINDOW SEAL RETAINER CRACKED IN THE UPPER FORWARD CORNER AT FS 680. REPAIRED IAW ABX REA D953-11589.

Part: SKIN — CORRODED (FS 1197-1231)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT AFT FUSELAGE SKIN PANEL FROM FS 1197 TO FS 1231 CORRODED UNDER THE RAIN GUTTER. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.

Part: PYLON BLKHD — CRACKED (FS 1041)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT PYLON BULKHEAD CRACKED SEVERAL PLACES AT FS 1041. REPLACED BULKHEAD WEB IAW DC-9 SRM CHAPTERS 51-30-1, 51-30-2 AND DOUGLAS DRAWING NR 9912243.

Part: SKIN — CORRODED (FS 1197-1244)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT AFT FUSELAGE SKIN PANEL FROM FS 1197 TO FS 1244, CORRODED UNDER THE RAIN GUTTER. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTER 51-30-2.

Part: SKIN — GOUGED (VERT STAB)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT VERTICAL STABILIZER SKIN GOUGED UNDER THE LOWER HORIZONTAL STABILIZER FAIRING. REPLACED VERTICAL STAB SKIN IAW DC-9 SRM CHAPTER 51-30-2.

Part: BLKHD ANGLE — DAMAGED (BS 1041)

DURING D - CHECK INSPECTION, FOUND THE BULKHEAD AT FS 1041, LOWER ATTACH ANGLE FASTENER HOLES OVERSIZED ON THE LEFT SIDE. REPLACED ATTACH ANGLE IAW DC-9 SRM, CHAPTER 51-30-4.

Part: SKIN — CORRODED (FS 1197-1231)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT AFT FUSELAGE PANEL FROM FS 1197 TO 1231 CORRODED BELOW THE RAIN GUTTER. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTER 51-30-2.

Part: ANGLE — CRACKED (FS 1152)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE OUTBOARD LEFT PYLON WEB UPPER ATTACH ANGLE CRACKED. REPLACED UPPER WEB ATTACH ANGLE IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.

Part: SKIN — CORRODED (FS 1197-1244)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT AFT FUSELAGE SKIN PANEL FROM FS 1197 TO FS 1244 CORRODED UNDER THE RAIN GUTTER. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTER 51-30-2.

Part: EYEBROW WINDOW — DELAMINATED (FS 133.4)

DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE CAPTAIN'S EYEBROW WINDOW DELAMINATED. REPLACED CAPTAIN'S EYEBROW WINDOW IAW DC-9 MM CHAPTER 56-10-4.