N965AX

Part: SWITCH — MALFUNCTIONED (NLG) · airframe 62,839 hrs · 58,922 cycles

DURING GEAR EXTENSION, NOSE DOWN AND LOCKED INDICATION DID NOT ILLUMINATE. RECYCLED GEAR. RECEIVED CORRECT INDICATION. REMOVED AND REPLACED NOSE GEAR SWITCH IAW DC9 MM 32-66-01-2-0101. ADJUSTMENT ACCOMPLISHED IN WORK PACK, W/O 600260610.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 62,833 hrs · 58,916 cycles

COCKPIT EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTTERIES IN EMERGENCY EXIT BATTERY PACK. OPS CHECKED GOOD IAW DC9 MM 33-53-00-8-0001.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 62,295 hrs · 58,379 cycles

EMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-008.

Part: PAN — CRACKED (PAX DOOR) · airframe 61,849 hrs · 58,017 cycles

AFT UPPER CORNER OF MAIN ENTRY DOOR PAN WAS CRACKED. REPAIRED AREA IAW DC-9 SRM 52-05.

Part: SPAR — CRACKED (RT PYLON) · airframe 61,849 hrs · 58,017 cycles

RIGHT AFT PYLON SPAR WEB WAS CRACKED AT LIGHTNING HOLE, LONGERON 13 RIGHT. REPAIRED CRACK IAW DC-9 SRM 53-01.

Part: SEAT TRACK — CRACKED (CABIN) · airframe 61,849 hrs · 58,017 cycles

SEAT TRACK CRACKED AT STA 200, RIGHT BUTT LINE 10. REMOVED AND REPLACED SEAT TRACK RIGHT BUTT LINE 10, FS 200 TO FS 155 IAW DC-9 SRM 51-30-2 AND 51-30-1.

Part: RIB — CRACKED (RIGHT WING) · airframe 61,849 hrs · 58,017 cycles

CRACKED RIB AT RIGHT WING TRAILING EDGE, STA XRS 133. REMOVED, REPAIRED AND REINSTALLED RIB AT RIGHT WING STA XRS 133 IAW DC-9 SSRM K05159 AND DC-9 SRM 51-30-2 AND 51-30-5.

Part: WINDOW FRAME — CRACKED (CABIN) · airframe 61,849 hrs · 58,017 cycles

TOP FORWARD CORNER OF WINDOW FRAME ON AFT SIDE OF STA 737 RIGHT HAD A SMALL CRACK. REPAIRED AREA IAW DC-9 SSRM K07226.

Part: WINDOW FRAME — CRACKED (CABIN) · airframe 61,849 hrs · 58,017 cycles

TOP FORWARD CORNER OF WINDOW FRAME ON AFT SIDE OF STA 737 LEFT WAS CRACKED. REPAIRED AREA IAW DC-9 SSRM K07226.

Part: SEAT TRACK — CRACKED (CABIN) · airframe 61,849 hrs · 58,017 cycles

SEAT TRACK RT BUTT LINE 9, FS 200, CRACKED. REMOVED AND REPLACED SEAT TRACK IAW DC-9 SRM 51-30-1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,849 hrs · 58,017 cycles

FS 1114 RIGHT SKIN CRACKED 8 1/2 INCHES UP FROM ENGINE PYLON. REPAIRED AREA FS 1114 RIGHT IAW DC-9 SRM.

Part: VANE — CRACKED (RT WING TE FLAP) · airframe 61,849 hrs · 58,017 cycles

RIGHT FLAP INBOARD FIXED VANE SKIN CRACKED ADJACENT TO REPAIR. REMOVED AND REPLACED INBOARD FIXED VANE IAW DC-9 SRM.

Part: STIFFENER — CRACKED (NR 1 NACELLE) · airframe 60,162 hrs · 56,715 cycles

NR 1 PYLON INTERNAL UPPER HORIZONTAL STIFFENER CRACKED ON INBOARD END, ABOVE FUEL LINE SHROUD. REPAIRED AREA NOTED IAW DC-9 SSRM K05159 AND DC-9 SRM 51-30-5.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,162 hrs · 56,715 cycles

SHEAR TIE CRACKED AT FS 718 LONGERON 5 RIGHT. INSTALLED NEW SECTION OF SHEAR TIE IAW DC-9 SRM 53-03.

Part: SHEAR TIE — CRACKED (CABIN) · airframe 60,162 hrs · 56,715 cycles

SHEAR TIE REPAIR CRACKED FS 1021, BETWEEN LONGERON 15 LEFT AND LONGERON 16 LEFT. REMOVED CRACKED SECTION, LOCATED AND DRILLED NEW FRAME FORMER IAW DC-9 SRM 51-1-4 AND 53-03, INSTALLED IAW DC-9 SRM 51-30-2.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 60,162 hrs · 56,715 cycles

EXTERIOR SURFACE OF VERTICAL STABILIZER AT FORWARD RIGHT FUSELAGE ATTACH POINT HAD CRACK. REMOVED AND REPLACED VERTICAL ATTACH ANGLE IAW DC-9 SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 60,162 hrs · 56,715 cycles

SHEAR TIE REPAIR HAD CRACK INDICATION FS 1021, BETWEEN LONGERON 15 RT AND LONGERON 14 RT. REPAIRED AREA IAW DC-9 SRM 53-03.

Part: INTERCOSTAL — CRACKED (FWD CARGO DOOR) · airframe 60,162 hrs · 56,715 cycles

FORWARD LOWER CARGO DOOR INTERCOSTAL WEB CRACKED AT LOWER AFT SIDE BY DOOR STOP MARKED AS NR 6. REMOVED AND REPLACED INTERCOSTAL IAW DC-9 MM AND ON ABX NON ROUTINE CARD 0228.

Part: WEB — CRACKED (FUSELAGE) · airframe 58,359 hrs · 55,491 cycles

CUSP WEB BTN, FS 1021-1041, LEFT SIDE WAS CRACKED (2 PLACES) EACH COMING OUT OF A LIGHTENING HOLE. REPAIRED DAMAGED CUSP WEB IAW DC-9 SRM 53-01.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 58,359 hrs · 55,491 cycles

CRACKED ANGLE AT STATION 775, RIGHT UPPER WHEEL WELL AT LONGERON 20. REPLACED ANGLE AND REPAIRED AREA IAW DC-9 SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 58,359 hrs · 55,491 cycles

FRAME FOOT FITTING CORRODED AT STATION 946 LEFT. REPLACED FRAME FOOT IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: FITTING — CORRODED (FUSELAGE) · airframe 58,359 hrs · 55,491 cycles

FRAME FOOT FITTING CORRODED AT FS 927 LEFT. REPLACED FRAME FOOT IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: ANGLE — CRACKED (CABIN) · airframe 58,359 hrs · 55,491 cycles

ANGLE CRACKED ON AFT SIDE OF FRAME AT STATION 1021, BETWEEN LONGERON 15 LEFT AND LONGERON 16 LEFT. REPLACED ANGLE IAW DC-9 SRM 53-03.

Part: FITTING — CORRODED (FUSELAGE) · airframe 58,359 hrs · 55,491 cycles

FRAME FOOT FITTING AT STATION 927 RIGHT WAS CORRODED. REPLACED FRAME FOOT IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: PANEL — DELAMINATED (LT WING) · airframe 58,359 hrs · 55,491 cycles

PANEL 1502 HAD 2 EACH AREAS OF DELAMINATION AND 1 SPOT OF LEVEL 1 CORROSION ON EXTERIOR SURFACE. REPLACED THE BUTE DOOR IAW DC-9 SRM 51-30-5.

Part: SKIN — CRACKED (EXT. FUSELAGE) · airframe 58,359 hrs · 55,491 cycles

SKIN CRACKED AT RIGHT AFT NOSE GEAR DOOR AFT CUT-OUT. REPAIRED AREA IAW DC-9 SRM 53-05.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,359 hrs · 55,491 cycles

CRACK IN FUSELAGE EXTERIOR SKIN AT STATION 1222, LONGERON 15 RIGHT. REPAIRED CRACK IAW DC-9 SRM 53-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,342 hrs · 54,136 cycles

FUSELAGE SKIN WAS CRACKED AT STATION 1208 AND LONGERON 14 RIGHT. REPAIRED IAW DC9 SRM 53-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,342 hrs · 54,136 cycles

FUSELAGE SKIN CRACKED AT STATION 1208 AND LONGERON 14 RIGHT. REPAIRED SKIN IAW DC9 SRM 53-01.

Part: PANEL — DELAMINATED (LT WING) · airframe 56,342 hrs · 54,136 cycles

LEFT WING TRAILING EDGE, LEFT BOTTOM, INBOARD BONDED PANEL WAS DELAMINATED. REPLACED LEFT INBOARD BONDED PANEL.

Part: RIB — CRACKED (LT WING) · airframe 56,342 hrs · 54,136 cycles

LEFT WING LEADING EDGE RIB CRACKED AT AFT END BETWEEN SLAT STATION XOS-481 AND 530. REPAIRED RIB IAW DC9 SRM.

Part: RIB — CRACKED (LT WING LE) · airframe 56,342 hrs · 54,136 cycles

LEFT WING LEADING EDGE RIB CRACKED AT AFT END BETWEEN STATION X0S 481 AND X0S 530. REPAIRED IAW DC9 SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 56,342 hrs · 54,136 cycles

ANGLE CRACKED AT LEFT WING LEADING EDGE SKIN SPLICE, STATION XRS 267. REPLACED ANGLE IAW DC9 SRM 51-30-5.

Part: PAN — CRACKED (CARGO DOOR) · airframe 56,342 hrs · 54,136 cycles

AFT LOWER CARGO DOOR PAN LOWER LEADING EDGE FLANGE CRACKED ADJACENT TO UPLATCH. REPLACEDDOOR.

Part: JACKSCREW — CORRODED (HORIZONTAL STAB) · airframe 56,006 hrs · 53,914 cycles

CORRODED THREADS ON JACKSCREW. REPLACED JACKSCREW.

Part: FITTING — CRACKED (BS 1152)

DURING C-CHECK, FOUND LEFT HEAT EXCHANGER AFT, OUTBOARD MOUNT FITTING CRACKED AT LONGERON 6 LEFT AND STATION 1152. REPLACED MOUNT FITTING IAW DC9 SRM 51-30-01.

Part: FLOORBEAM — CORRODED (BS 541)

DURING C-CHECK, FOUND FLOORBEAM CORRODED AT STATION 541 AND BLO 0.0. REPAIRED IAW DC9 SRM 53-05.

Part: FRAME — CORRODED (BS 484)

DURING C-CHECK, FOUND FRAME AT STATION 484 CORRODED FROM LONGERON 29 RIGHT TO 29 LEFT. REPAIRED FRAME IAW DC9 SRM 53-03.

Part: INTERCOSTAL — CRACKED (BS 541-560)

DURING C-CHECK, FOUND INTERCOSTAL CRACKED AT STATION 541-560 AND BLO 0.0. REPAIRED INTERCOSTAL IAW DC9 SRM 51-30-02.

Part: BULKHEAD FITTING — CRACKED (BS 1041)

DURING C-CHECK, FOUND PYLON BULKHEAD LOWER FLOOR FITTING CRACKED AT STATION 1041 AND RBL 30. REPAIRED IAW DC9 SRM 54-12.

Part: BULKHEAD FITTING — CRACKED (BS 1115)

DURING C-CHECK, FOUND AFT PYLON BULKHEAD ATTACH FITTING CRACKED AT STATION 1115 AND LONGERON 15R. REPLACED FITTING IAW DC9 SRM 51-30-01 AND 51-30-02.

Part: BATTERIES — DISCHARGED (CABIN)

DURING PREFLIGHT, EMERGENCY LIGHTS ILLUMINATED, THEN WENT OUT. REPLACED EMERGENCY LIGHT BATTERIES.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS WERE WEAK. REPLACED BATTERY PACK.

Part: RIB — CRACKED (RT HORIZ STAB)

DURING C-CHECK, FOUND THE RT HORIZONTAL STAB OUTBOARD LEADING EDGE SECTION MOST INBOARD RIB INBOARD FROM OUTBOARD TIP CRACKED. REPAIRED RIB IAW DC9 SRM DRAWING NR K05159.

Part: BELLCRANK — CORRODED (HORIZ STAB)

DURING C-CHECK, FOUND THE LONGITUDINAL TRIM CABLE BELLCRANK ARM (P/N 5914177-503) CORRODED. REMOVED AND REPLACED ARM IAW DC9 MM 20-10-0 AND 20-16-0.

Part: FRAME — CRACKED (BS 1132)

DURING C-CHECK, FOUND FRAME AT F/STA 1132 LONGERON 2R CRACKED. REPAIRED FRAME IAW DC9 SRM 53-03, FIGURE 32.

Part: INTERCOSTAL — CRACKED (BS 1231)

DURING C-CHECK, FOUND INTERCOSTAL AND INTERCOSTAL CLIP CRACKED UNDER WALKWAY PLATFORM AT STA 1231. REPLACED INTERCOSTAL AND CLIP IAW DC9 SRM 51-30-2.

Part: FLANGE — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR LOWER TRAILING EDGE FLANGE BENT AND CRACKED. REPAIRED FLANGE IAW DC9 SRM 52-05.

Part: RIB — CRACKED (RT HORIZ STAB)

DURING C-CHECK, FOUND THE RT HORIZONTAL STAB INBOARD LEADING EDGE SECTION, INBOARD RIB CRACKED AT LOCK BOLT. REPAIRED RIB IAW DC9 SRM DRAWING NR K05159.

Part: LONGERON — CRACKED (BS 256)

DURING C-CHECK, FOUND LONGERON 17R CRACKED AT F/STA 256. REPLACED CRACKED SECTION OF LONGERON FROM F/STA 230 TO 265 IAW DC9 SRM 53-02.

Part: RIB — CRACKED (RT HORIZ STAB)

DURING C-CHECK, FOUND THE RT HORIZONTAL STAB OUTBOARD LEADING EDGE SECTION, 5TH RIB INBOARD FROM OUTBOARD TIP CRACKED. REPAIRED RIB IAW DC9 SRM DRAWING NR K05159.

Part: FITTING — CRACKED (BS 718)

DURING C-CHECK, FOUND THE FLOOR SUPPORT FITTING AT F/STA 718 AND RBL 44 CRACKED AT LOWER END. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: TR DOOR — CRACKED (NR 1 ENGINE)

DURING C-CHECK, FOUND THE UPPER THRUST REVERSER DOOR OUTBOARD EXTERIOR FLANGE CRACKED. REPLACED FLANGE IAW DC9 SRM 51-10-4, 51-30-2 AND 51-30-8.

Part: FRAME — CORRODED (BS 1072)

DURING C-CHECK, FOUND THE FRAME AT F/STA 1072 CORRODED BETWEEN LONGERONS 17R AND 18R. REMOVED CORROSION AND REPAIRED IAW ABX REA D953-19271-MR AND REA D953-19275.

Part: DOUBLER — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND THE RT KIDNEY PANEL NR 5114A AFT ATTACH FLANGE DOUBLER CORRODED. TRIMMED OUT CORRODED SECTION OF DOUBLER AND REPAIRED IAW ABX REA D953-19275.

Part: CUSP WEB — CORRODED (BS 237-256)

DURING C-CHECK, FOUND THE CUSP WEB BETWEEN F/STA 237 TO 256 LT SIDE CORRODED. REPLACED CORRODED SECTION OF CUSP WEB IAW ABX REA D953-19274-MR.

Part: FITTING — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND THE AFT LOWER CARGO COMPARTMENT DOOR HORIZONTAL BEAM NR 5 FORWARD END FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: ANGLE — BROKEN (NR 2 PYLON)

DURING C-CHECK, FOUND THE NR 2 PYLON INTERIOR CANTED WEB LOWER ANGLE BROKEN OFF AT FORWARD CORNER IN ACCESS AREA 8206A. REPLACED ANGLE IAW DC9 SRM 51-30-2 AND 51-30-8.

Part: BRACKET — CHAFED (RT SPOILER)

DURING C-CHECK, FOUND THE RIGHT WING INBOARD SPOILER PULLEY BRACKET CHAFED BEYOND LIMITS. REPLACED PULLEY BRACKET IAW DC9 SRM 51-30-1.

Part: TR DOOR — CRACKED (NR 1 ENGINE)

DURING C-CHECK, FOUND THE LOWER THRUST REVERSER DOOR OUTBOARD EXTERIOR FLANGE CRACKED. REPLACED FLANGE IAW DC9 SRM 51-10-4, 51-30-2 AND 51-30-8.

Part: TR DOOR — CRACKED (NR 1 ENGINE)

DURING C-CHECK, FOUND THE UPPER THRUST REVERSER DOOR INBOARD EXTERIOR FLANGE CRACKED. REPLACED FLANGE IAW DC9 SRM 51-10-4, 51-30-2 AND 51-30-8.

Part: INVERTER — DEFECTIVE (E/E COMPT)

DURING EMERGENCY INVERTER TEST, SMELLED HOT EQUIPMENT. REPLACED EMERGENCY INVERTER IAW DC-9 MM 24-20-0, OPS CHECKED GOOD.

Part: LINK ASSY — WORN (RT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-224 R2, FOUND LINK ASSEMBLY FOR RIGHT MAIN LANDING GEAR ARTICULATING DOOR WORN. REPLACED LINK ASSEMBLY IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: BUSHING — WORN (LT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07, ASB 32-244 R2, FOUND LEFT OUTBOARD MAIN LANDING GEAR DOOR ARTICULATING CRANK PIVOT POINT WORN. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: BOLT — WORN (LT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-244 R2, FOUND LEFT OUTBOARD MAIN LANDING GEAR ARTICULATING CRANK PIVOT POINT WORN. REPLACED BOLT IAW DC-9 OVERHAUL MANUAL 32-10-06.

Part: WASHER — WORN (LT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-244 R2, FOUND LEFT OUTBOARD MAIN LANDING GEAR ARTICULATING CRANK PIVOT POINT WORN. REPLACED WASHER IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: BULB — DEFECTIVE (CABIN)

FIRST OFFICERS EMERGENCY LIGHTING INOPERATIVE. RELAMPED, OPS CHECKED GOOD PER DC-9 MM 33-10-0.

Part: BATTERY — CORRODED (CABIN)

EMERGENCY LIGHTS INOPERATIVE. CLEANED CORRODED BATTERY CONTACTS, OPS CHECKED GOOD PER DC-9 SMM 33-53-0.

Part: EADI — DEFECTIVE (NR 1)

CAPTAIN'S EADI WENT BLANK AND PRODUCED SMOKE AND FUMES IN THE COCKPIT (IN-FLIGHT). REPLACED NR 1 EADI (FOUND SMOKE ODOR IN D.U. FAN) IAW DC-9 M.M. PART TOTAL CYCLES, 3,670.

Part: FITTING — CORRODED (LT AILERON)

DURING DC-9 AILERON OFF WING INSPECTION, FOUND LEVEL 2 CORROSION ON THE FITTING ASSEMBLY AROUND BUSHING HOLE. REPLACED FITTING ASSEMBLY IAW DC-9 OVERHAUL MANUAL 27-10-2.

Part: RETRACT MECH — MALFUNCTIONED (LANDING GEAR)

ILN - AFTER TAKEOFF WITH GEAR SELECTOR UP, ALL THREE UNSAFE LIGHTS AND GEAR DOOR OPEN LIGHTS REMAINED ILLUMINATED. ALL THREE GEARS APPEARED TO REMAIN DOWN. RECYCLED GEAR, RETRACTED NORMALLY WITH NORMAL INDICATIONS. JACKED AIRCRAFT AND PERFORMED SIX GEAR RETRACTIONS AND INDICATIONS WERE NORMAL. CHECKED RIGGING OF LANDING GEAR, CONTROL VALVE AND EMERGENCY EXTENSION AND ALL CHECKED OK IAW DC9 SUPPLEMENTAL MM, CHAPTER 32.

Part: VANE — DELAMINATED (LT TE FLAP)

DURING C-CHECK INSPECTION, FOUND LEFT INBOARD FIXED VANE DELAMINATED. REPLACED FIXED VANE IAW DC-9 MM 27-51-3.

Part: SKIN — DAMAGED (BS 427-475)

DURING C-CHECK INSPECTION, FOUND MULTIPLE DENTS, GOUGES AND CREASES ON THE FUSELAGE SKIN AFT OF FORWARD LOWER CARGO COMPARTMENT DOOR CUTOUT. REPAIRED IAW ABX REA D953-12891-MR.

Part: CAP — CORRODED (BS 110)

DURING C-CHECK INSPECTION, FOUND CORROSION ON LOWER T-CAP AT STATION 110 BETWEEN LONGERONS L26L TO L27L AND L26R TO L27R. REPAIRED IAW ABX REA D953-12890-MR.

Part: SKIN — WRINKLED (FWD FUS)

DURING C-CHECK INSPECTION, FOUND SKIN WRINKLED JUST AFT OF NOSE LANDING GEAR DOOR JAMB ON THE LEFT SIDE. REPAIRED IAW ABX REA D953-12886-MR.

Part: SKIN — GOUGED (BS 786)

DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN GOUGED AT STA 786 UNDER LONGERON 30. REPAIRED IAW ABX REA D953-12820-MR.

Part: SKIN — CRACKED (BS 1067)

DURING C-CHECK INSPECTION, FOUND TWO CRACKS IN THE SKIN AT STATION 1067. REPAIRED IAW ABX REA D953-12818-MR.

Part: SKIN — DENTED (BS 473)

DURING C-CHECK INSPECTION, FOUND SKIN DENTED AND CREASED AT STATION 473 BETWEEN LONGERONS 20R AND 21R. REPAIRED IAW ABX REA D953-12817-MR.

Part: LONGERON — CORRODED (BS 794)

DURING C-CHECK INSPECTION, FOUND CORROSION ON LONGERON 30, STA 794. REPAIRED IAW ABX REA D953-12820-MR.

Part: SKIN — DENTED (BS 360)

DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED AT STATION 360 AT LONGERON 23R. REPAIRED IAW ABX REA D953-12812-MR.

Part: SKIN — CORRODED (BS 712)

DURING C-CHECK INSPECTION, FOUND LEVEL 1 CORROSION ON SKIN AT STATION 712, BETWEEN LONGERONS 18R AND 19R. REPAIRED IAW ABX REA D953-10808-MR.

Part: SKIN — DEFECTIVE (BS 294-351)

DURING C-CHECK INSPECTION, FOUND TWO COLD WORKED AREAS BETWEEN STATION 294 AND 351 AT LONGERONS 20 TO 22R. REPAIRED IAW ABX REA D953-12805-MR.

Part: SKIN — DENTED (BS 256)

DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED AT STATION 256 BETWEEN LONGERONS 18R AND 19R. REPAIRED IAW ABX REA D953-12810-MR.

Part: TAB — DELAMINATED (LT AILERON)

DURING C-CHECK INSPECTION, FOUND LEFT AILERON CONTROL TAB DELAMINATED. REPLACED TAB IAW DC-9 MM 27-10-2.

Part: BLKHD SKIN — CRACKED (BS 1072)

DURING C-CHECK INSPECTION, FOUND A 2.125 INCH CRACK AT AFT PRESSURE BULKHEAD SKIN. REPAIRED IAW ABX REA D953-12807-MR.

Part: SUPPORT — CRACKED (BS 465)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND CRACKED FLOOR SUPPORT ON FRAME 465 AT LONGERON 29R. REPAIRED FLOOR SUPPORT IAW SUPP MM DRAWING NR K05018.

Part: TAB — DELAMINATED (LT AILERON)

DURING C-CHECK INSPECTION, FOUND LEFT AILERON TRIM TAB DELAMINATED. REPLACED TRIM TAB IAW DC-9 MM 27-10-5.

Part: TIE — DAMAGED (BS 1056)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND DAMAGED AREA IN THE RADIUS OF THE SHEAR TIE STA 1056 ABOVE LONGERON 12L. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-2.

Part: GUSSET — CRACKED (BS 180)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND LIGHTENING HOLE GUSSET PLATE CRACKED AT FLOORBEAM STA 180. REPLACED GUSSET IAW DC-9 SRM 51-30-5 AND ENGINEERING MEMO 95-01.

Part: ANGLE — CRACKED (BS 1072)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND A CRACK IN THE UPPER AND LOWER ATTACH ANGLES ON THE APB STIFFENER AT LONGERON 15R. REPAIRED IAW DC-9 SUPP DRAWING NR K05159.

Part: ANGLE — CRACKED (BS 1072)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND A CRACK IN THE ATTACH ANGLE ON APB STIFFENER BETWEEN LONGERONS 15R TO 16R. REPLACED ANGLE IAW DC-9 SUPP SRM DRAWING NR K05159.

Part: ANGLE — CRACKED (BS 1072)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND A CRACK IN THE ATTACH ANGLE ON APB STIFFENER, BETWEEN LONGERONS 16L TO 17L. REPAIRED IAW DC-9 SUPP DRAWING NR K05159.

Part: ANGLE — CRACKED (BS 1072)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND A CRACK IN THE ATTACH ANGLE ON APB STIFFENER BETWEEN LONGERONS 12L TO 13L. REPLACED ANGLE IAW DC-9 SRM 51-30-5 AND 51-30-2.

Part: ROLLER — OUT OF ADJUST (LT CV WINDOW)

DURING PREFLIGHT INSPECTION, FOUND CAPTAIN'S SLIDING WINDOW WOULD NOT OPEN. FOUND LOWER ROLLER OUT OF TRACK. REALIGNED ROLLER. CAPTAIN'S WINDOW OPS CHECKED GOOD IAW DC-9 M.M.

Part: DRIVE LINK — CRACKED (TR UNIT)

DURING COMPLIANCE OF AD 75-14-06, AD 90-18-03, SB'S 78-36, 78-38, 78-40 AND 78-66, FOUND OUTBOARD LOWER THRUST REVERSER DRIVE LINK HAD A CRACK INDICATION. REPLACED OUTBOARD LOWER THRUST REVERSER DRIVE LINK IAW DC-9 MM 78-32, LINK WAS SCRAPPED.