N932AX

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 48,960 hrs · 38,408 cycles

COCKPIT EMERGENCY LIGHTS WERE DIM DURING TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-02.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 48,675 hrs · 38,159 cycles

FOUND EMERGENCY LIGHTS TO BE VERY DIM. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-02.

Part: SHEAR TIE — CRACKED (BS 1019) · airframe 48,284 hrs · 37,869 cycles

SHEAR TIE DOUBLER CRACKED AT STA. 1019 BETWEEN LONGERON 13-14. REMOVED AND REPLACED DOUBLER IAW ABX DWG K05159.

Part: PANEL — CORRODED (TE FLAP) · airframe 48,284 hrs · 37,869 cycles

RIGHT FLAP SEGMENT FROM OUTBOARD EDGE LOWER SURFACE ATTACH POINTS WERE SEPARATING AND CORRODED BETWEEN SKINS. REPLACED SKIN AND DOUBLER IAW DC9 REA C057-52966.

Part: STRAP — CRACKED (FUSELAGE) · airframe 48,284 hrs · 37,869 cycles

PYLON UPPER REAR SPAR STRAP BROKEN APART AT NR 2 PYLON. REMOVED AND REPLACED SPAR STRAP IAW SRM 51-30-1 AND 51-30-5.

Part: ATTACH ANGLE — CRACKED (CABIN) · airframe 48,284 hrs · 37,869 cycles

VENTRAL DOOR UPPER LEFT ATTACH ANGLE CRACKED AROUND RIVET. REMOVED, FABRICATED, AND INSTALLED NEW ANGLE IAW DC9 SRM 51-30-5.

Part: SHEAR TIE — CRACKED (BS 1038) · airframe 48,284 hrs · 37,869 cycles

RIGHT AFT PYLON BULKHEAD FLANGE CRACKED AT STA 1038, LONGERON 14 RIGHT. REMOVED AND REPLACED PYLON BULKHEAD FLANGE (SHEAR TIE) IAW DC9 SRM.

Part: SHELF — CRACKED (BS 1038) · airframe 48,284 hrs · 37,869 cycles

CRACKED FLANGE ON RT AFT PYLON BULKHEAD GUSSET SHELF AT STA. 1038, LONGERON 15 RT. REMOVED AND REPLACED GUSSETT SHELF IAW SRM 51-30-2.

Part: DOUBLER — CORRODED (BS 332-351) · airframe 48,284 hrs · 37,869 cycles

CORROSION ON ANTENNA PLATE, STA 332 - 351, LONGERON 30 - 29 LEFT. REMOVED AND REPLACED DOUBLER IAW DC9 SRM.

Part: HOUSING — CRACKED (DOOR HOLD OPEN) · airframe 48,284 hrs · 37,869 cycles

HOLD OPEN HOOK SUPPORT STRUCTURE INSIDE SERVICE DOOR WAS CRACKED AT LOWER SHAFT BEARING MOUNT. REPLACED FITTING IAW DC9 SRM.

Part: SKIN — CORRODED (TE FLAP) · airframe 48,284 hrs · 37,869 cycles

RIGHT FLAP SECOND FROM OUTBOARD TRAILING EDGE SEGMENT UPPER SURFACE HAD 3 AREAS THAT WERE BULGED. REMOVED SEGMENT, REMOVED AND REPLACED SKIN IAW DC9 SRM 51-30-2.

Part: SKIN — CORRODED (KEEL BS 600) · airframe 48,284 hrs · 37,869 cycles

CRACK IN FUSELAGE KEEL SKIN AT STA 600 BETWEEN LONGERON 30 - 29 LEFT. REPAIRED AREA IAW DC9 SRM 53-04 AND REA D953-52948MR.

Part: FITTING — CRACKED (BS 604) · airframe 48,284 hrs · 37,869 cycles

END FITTING CRACKED LONGERON 29 RIGHT AT FS 604. REMOVED AND REPLACED END FITTING IAW DC9 SRM 51-30-5.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 48,284 hrs · 37,869 cycles

FOUND CORROSION ON SUBFLOOR AT FLOORBEAM FS 135, RIGHT BUTT LINE 28 TO 40. REPAIRED CORRODED AREA IAW DC9 SRM 53-01.

Part: FLOORBEAM — CORRODED (BS 135) · airframe 48,284 hrs · 37,869 cycles

CORROSION ON SUBFLOOR AT FLOORBEAM FS 135, LEFT BUTTLINE 14. REPAIRED CORRODED AREA IAW DC9 SRM 53-01.

Part: SWITCH — OUT OF POSITION (MLG) · airframe 48,277 hrs · 37,864 cycles

AFTER TAKEOFF WHEN THE GEAR WAS RAISED, GOT THE TAKEOFF WARNING HORN. LOWERED THE GEAR TO EXTINGUISH THE HORN. AFTER THE SLATS AND FLAPS WERE UP, GEAR WAS RAISED WITH NO FURTHER PROBLEMS. TAKEOFF WARNING TESTS OK. GEAR WARNING TEST FAILED AT 5 DEGREES FLAP POSITION. FOUND LANDING GEAR WARNING SWITCH (A2-85) AT FLAP CONTROL DRUM BEING ACTUATED BY CONTROL DRUM CABLE RETAINING SAFETY WIRE. REPOSITIONED SWITCH TO ALIGN WITH CENTER OF ACTUATING CAM. GEAR WARNING TEST OK. REF AMM 27-53-01, DC9-1.

Part: BEARING — WORN (MLG DOORS) · airframe 47,727 hrs · 37,445 cycles

DURING GEAR RETRACTION AFTER TAKEOFF, GEAR OPEN LIGHT ILLUMINATED. REMAINED ON FOR INFLIGHT PORTION, EXTINGUISHED DURING GEAR EXTENSION FOR LANDING. REMOVED AND REPLACED WORN BEARINGS AND HINGE PINS ON LEFT AND RIGHT MAIN LANDING GEAR INBOARD DOORS IAW DC-9 OHM 32-13-5. PERFORMED ADJUSTMENT TEST IAW DC-9 AMM 32-30-00-2. PLACARD REMOVED.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 47,537 hrs · 37,297 cycles

EMERGENCY EXIT LIGHT WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES IAW DC-9 AMM 33-53-00. OPS CHECKED GOOD.

Part: ATTACH FITTING — BROKEN (FUSELAGE) · airframe 46,769 hrs · 36,597 cycles

ATTACH FITTING AND ANGLE AFT SIDE OF FRAME 1087 AT 12:30 POSITION, BROKEN. REPLACED IAW DC-9 SRM 51-30-1, 51-30-5 AND 51-30-2.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 46,769 hrs · 36,597 cycles

SEAT TRACK UPPER INBOARD FLANGE CORRODED AROUND FASTENER HOLES AT FS 908 - 945, RBL 44 AND FLANGE CRACKED AT FS 945. REPLACED SEAT TRACK IAW DC-9 SRM 51-30-1 AND 53-05.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 46,769 hrs · 36,597 cycles

LEFT VERTICAL STABILIZER ATTACH ANGLE CRACKED. REPAIRED ANGLE IAW DC-9 SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 46,769 hrs · 36,597 cycles

SHEAR TIE CRACKED FS 965 AT LONGERON 16 LEFT. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: CLIP — CRACKED (LT WING LE) · airframe 46,769 hrs · 36,597 cycles

WING LEADING EDGE SPLICE ANGLE AND DOUBLER CRACKED JUST OUTBOARD OF NR 6 SLAT TRACK. REPLACED ANGLE / DOUBLER IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: GROUND WIRE — LOOSE (CABIN) · airframe 45,682 hrs · 35,653 cycles

RIGHT OVERHEAD EMERGENCY LIGHT DIM. TIGHTENED GROUND WIRE ON RIGHT OVERHEAD EMERGENCY LIGHT FIXTURE. OPS CHECKED GOOD IAW AMM.

Part: CLIP — CRACKED (FUSELAGE) · airframe 45,605 hrs · 35,580 cycles

CRACKED SHEAR TIE AT STA. 1076 (AFT SIDE) BETWEEN LONGERONS 15 - 16 LEFT. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,605 hrs · 35,580 cycles

STA 980 FRAME REPAIR BELOW LONGERON 14 RIGHT WAS CRACKED. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5 AND 51-30-2.

Part: SUPPORT — CRACKED (AFT CARGO) · airframe 45,605 hrs · 35,580 cycles

FLOOR SUPPORT FITTING AT F.S. 980 LONGERON 28 LEFT CRACKED UNDER STRAP. REPLACED SUPPORT FITTING IAW DC-9 SRM 51-30-5.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,605 hrs · 35,580 cycles

CRACK IN BELLY SKIN STA 465 BETWEEN LONGERON 29 LEFT TO 30. REPAIRED CRACK IN BELLY SKIN IAW REA D953-45748MR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 45,605 hrs · 35,580 cycles

FLOOR SUPPORT AT FS 996 LONGERON 30, HEAVILY EXFOLIATED AND BROKEN OFF. REPLACED FLOOR SUPPORT IAW DC-9 SRM 51-30-5.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 45,605 hrs · 35,580 cycles

LONGERON END CRACKED JUST AFT OF FORWARD "P" DOME ON LONGERON 29 LEFT. REPAIRED AREA IAW DC-9 SRM.

Part: CLIP — CRACKED (CENTER WING) · airframe 45,605 hrs · 35,580 cycles

CLIP CRACKED FRONT SIDE OF FRAME AT F.S. 637 AT LONGERON 29 LEFT. REPLACED CLIP IAW DC-9 SRM 51-30-5.

Part: FORMER — CRACKED (CENTER WING) · airframe 45,605 hrs · 35,580 cycles

CRACK AT OUTBOARD END OF FRAME F.S. 658 AND LONGERON 27 RIGHT CANTED KEEL AREA. REPAIRED FRAME IAW DC-9 SSRM DWG. #K05159.

Part: SKIN — CORRODED (CENTER WING) · airframe 45,605 hrs · 35,580 cycles

EXFOLIATION ON LOWER CENTER WING SKIN - XCW 20, AT STRINGER 19 RIGHT. REPAIRED AREA IAW DC-9 SRM 52-03.

Part: SUPPORT — CRACKED (RIGHT WING) · airframe 45,605 hrs · 35,580 cycles

INBOARD SPOILER ACTUATOR OUTBOARD SUPPORT FITTING WAS CRACKED AT UPPER FLANGE. REPLACED SUPPORT IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: FORMER — CRACKED (RIGHT WING) · airframe 45,605 hrs · 35,580 cycles

THIRD LEADING EDGE RIB OUTBOARD OF #11 SLAT TRACK CRACKED AT AFT UPPER END. REPLACED RIB IAW DC-9 SRM 51-30-2, 51-30-5, AND 51-10-3B.

Part: WEB — CORRODED (FUSELAGE) · airframe 45,605 hrs · 35,580 cycles

LEVEL I CORROSION ON SUB-FLOOR SEVERAL PLACES, BUTT LINE '0', OUTBOARD TO LONGERON 18 RIGHT, FS 133.4 TO FS 148. REPAIRED AREA IAW DC-9 SRM 53-01.

Part: COALESCER BAG — DIRTY (A/C BAY) · airframe 44,608 hrs · 34,691 cycles

THERE WAS AN OIL SMELL COMING FROM BOTH A/C PACKS. CLEANED RIGHT COALESCER FILTER AND REPLACED THE LEFT COALESCER FILTER IAW DC-9 MM 21-20-02.

Part: RHEOSTAT — DEFECTIVE (COCKPIT) · airframe 44,455 hrs · 34,567 cycles

THE CAPTAIN''S MAP LIGHT WAS SMOKING. MAINTENANCE DEFERRED THE MAP LIGHT PER THE DC-9 MEL AND RETURNED THE AIRCRAFT TO SERVICE. ON 04/26/01 MAINTENANCE INSPECTED AND REPLACED THE CAPTAIN''S MAP LIGHT RHEOSTAT IAW DC-9 MM 33-10-00.

Part: ANGLE — CORRODED (CNTR WING BOX) · corrosion level 2 · airframe 44,451 hrs · 34,564 cycles

AN L-ANGLE AT FS 637 LBL 44 THROUGH LBL 54 WAS CORRODED ON THE UPPER SIDE OF THE CENTER FUEL TANK PANEL. MAINTENANCE REPAIRED THE AREA IAW DC-9 SRM 51-30-1, 51-30-5 AND DOUGLAS DRAWING 5910464.

Part: SPAR — CORRODED (WING) · corrosion level 2 · airframe 44,451 hrs · 34,564 cycles

THE REAR SPAR UPPER PLANK WAS FOUND TO HAVE INTERGRANULAR CORROSION, BELOW AND ADJACENT TO SLAT PANEL 24 INCHES TO THE LEFT OF THE KEEL. MAINTENANCE REPAIRED THE AREA IAW ABX REA D957-40679.

Part: BATTERY — DISCHARGED (CABIN)

COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY BATTERIES.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHTS WERE INOPERATIVE. RESET TRANSFER BUS 5 AMP CIRCUIT BREAKER.

Part: POWER SUPPLY — DISCHARGED (CABIN)

ON PRE-DEPARTURE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY.

Part: HINGE — CRACKED (RT MLG DOOR)

DURING C-CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR INBOARD DOOR HINGE CRACKED. REPLACED HINGE IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: DOUBLER — CORRODED (BS 965)

DURING C-CHECK, FOUND FUSELAGE SKIN AND DOUBLER CORRODED AT STATION 965 AND LONGERON 22 LEFT. REPLACED DOUBLER IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: SHEAR TIE — CRACKED (BS 980)

DURING C-CHECK, FOUND SHEAR-TIIE CRACKED AT STATION 980 AND LONGERON 14 LEFT. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2, 51-30-5 AND ABX REA 953-32623.

Part: ANGLE — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND FORWARD FACE OF AFT PRESSURE BULKHEAD, OUTBOARD LEFT ATTACH ANGLE, CRACKED AT LONGERON 15 LEFT. REPLACED ANGLE IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: SKIN — CRACKED (BS 1121 & 1132)

DURING C-CHECK, FOUND FUSELAGE EXTERIOR SKIN PANEL CRACKED IN TWO LOCATIONS, STATION 1121 AND 1132, AT 9 O'CLOCK POSITION. REPLACED SKIN IAW DC9 SRM 51-30-02.

Part: FITTING — CRACKED (BS 946)

DURING C-CHECK, FOUND FITTING CRACKED AT STATION 946 AND LONGERON 23 LEFT. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: FRAME — CRACKED (BS 718)

DURING C-CHECK, FOUND RIGHT MAIN FRAME CRACKED AT STATION 718. REPLACED MAIN FRAME IAW DC9 SERVICE BULLETIN 53-131 AND 53-182.

Part: FITTING — CRACKED (BS 658)

DURING C-CHECK, FOUND CRACKED VERTICAL SUPPORT BRACKET UNDER LBL 44 SEAT TRACK STATION 658. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: SHEAR TIE — CRACKED (BS 1087)

DURING C-CHECK, FOUND SHEAR-TIE CRACKED AT STATION 1087 AND LONGERON LEFT. REPLACED SHEAR-TIE IAW DC9 SRM 51-10-2 AND 51-30-1.

Part: BRACKET — CRACKED (CARGO DOORWAY)

DURING C-CHECK, FOUND MAIN CARGO DOOR LOWER JAMB BRACKET CORRODED. REPLACED BRACKET IAW DC9 SRM 51-10-04.

Part: WEB — CRACKED (BS 313)

DURING C-CHECK, FOUND RIGHT CUSP WEB CRACKED AT STATION 313 RBL 49. REPAIRED IAW DC9 SRM 53-01-00.

Part: WINDOW — STUCK (LT COCKPIT)

CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. LUBRICATED LINKAGE ON CAPTAIN'S CLEARVIEW WINDOW.

Part: WINDOW — STICKING (LT COCKPIT)

CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. LUBRICATED UPPER HINGE LOCK.

Part: WINDOW — OUT OF ADJUST (LT COCKPIT)

CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. ADJUSTED CAPTAIN'S CLEARVIEW WINDOW IAW DC9 MM 56-10-3.

Part: WINDOW — STUCK (LT COCKPIT)

CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED FORWARD WINDOW AFT ADJUSTMENT ON CAPTAIN'S CLEARVIEW WINDOW.

Part: TRIM — OUT OF POSITION (COCKPIT)

CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. REPOSITIONED WINDOW TRIM.

Part: WINDOW — LACK OF LUBE (LT COCKPIT)

CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT ) WOULD NOT OPEN. RELEASED UPPER LOCK BAR, CLEANED AND LUBRICATED LINKAGE. OPS CHECKED GOOD.

Part: BLKHD STIFFENER — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER AT 996 AND LONGERON 14L LOWER FLANGE CRACKED. REPAIRED STIFFENER IAW DC9 S/B 53-166, SERVICE REWORK DWG J060110 VIEW V-V AND DACO DWG PL 9915558.

Part: CUSP WEB — CRACKED (BS 955)

DURING C-CHECK, FOUND RIGHT CUSP WEB AT FS 955 CRACKED APPROX 4 LONG. REPAIRED CUSP WEB IAW ABX REA D953-22256.

Part: BLKHD STIFFENER — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER AT STA 996 AND LONGERON 14R LOWER FLANGE CRACKED. REPAIRED STIFFENER IAW DC9 S/B 53-166, SERVICE REWORK DWG J060110 VIEW V-V AND DACO DWG PL 9915558.

Part: FLOORBEAM — CORRODED (BS 937)

DURING C-CHECK, FOUND FLOORBEAM LOWER FLANGE CORRODED AT STA 937, BL 0.0. REPAIRED FLOORBEAM IAW ABX REA D53-22192MR.

Part: TRAP PANEL — CORRODED (LT MLG WW)

DURING C-CHECK, FOUND LEFT TRAPEZODIAL PANEL UPPER HORIZONTAL FLANGE EXFOLIATED AND CRACKED. REPLACED TRAPEZODIAL PANEL IAW DC9 S/B 53-182 AND DC9 SRM 51-30-1.

Part: FITTING — CORRODED (LT MLG WW)

DURING C-CHECK, FOUND THE LEFT PORK-CHOP FITTING CORRODED. REPLACED FITTING IAW DC9 S/B 53-182 AND DC9 SRM 51-30-1.

Part: LONGERON — CRACKED (BS 965)

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

Part: LONGERON — CRACKED (BS 965)

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

Part: ANGLE — CRACKED (NR 1 PYLON)

DURING C-CHECK, FOUND UPPER PYLON ATTACH ANGLE CRACKED AT STA 980. REPAIRED ANGLE IAW DC9 SRM 54-04.

Part: FITTING — CORRODED (BS 980)

DURING C-CHECK, FOUND FUSELAGE FRAME MOUNT FOOT FITTING STA 980 LONGERON 18L CORRODED, (LT SIDE). REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: ANGLE — CRACKED (NR 2 PYLON)

DURING C-CHECK, FOUND ANGLE IN NR 2 ENGINE PYLON CRACKED AT AFT LOWER SPAR STRAP ABOVE PANEL 8212. REPLACED ANGLE IAW DC9 SRM 51-30-1.

Part: LONGERON — CRACKED (BS 160)

DURING C-CHECK, FOUND LONGERON 4L CRACKED AT STA 160. REPAIRED LONGERON 4L IAW DC9 SRM 53-02.

Part: DOUBLER — CORRODED (BS 996)

DURING C-CHECK, FOUND EXFOLIATION CORROSION IN INTERNAL FUSELAGE SKIN DOUBLER AT STA 996 JUST BELOW LONGERON 17R. REPLACED FILLER DOUBLER IAW DC9 SRM 51-30-1.

Part: PRESS PANEL — CRACKED (RTMLG WW)

DURING C-CHECK, FOUND RT WHEEL WELL PRESSURE PANEL CRACKED OUTBOARD AND AFT OF MAIN FRAME 718, UPPER CORNER OF AFT FLANGE. REPLACED DOUBLER IAW DC9 SRM 51-30.

Part: FLAP VANE — GOUGED (LT TE FLAP)

THE LEFT OUTBOARD FLAP VANE HAS TWO GOUGES THROUGH THE SKIN ON THE INBOARD LEADING EDGE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.

Part: LINKAGE — WORN (LT MLG DOOR)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR LINKAGE WORN. REPLACED WORN PARTS IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: LINKAGE — WORN (LT MLG DOOR)

DURING C-CHECK INSPECTION AND COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR LINKAGE WORN. REPLACED WORN PART IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: LINKAGE — WORN (LT MLG DOOR)

DURING C-CHECK INSPECTION AND COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR LINKAGE WORN. REPLACED WORN PARTS IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: SPOILER — CRACKED (LT WING)

THE LEFT OUTBOARD SPOILER WAS CRACKED AT THE CENTER HINGE CUP. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.

Part: LINKAGE — WORN (LT MLG DOOR)

DURING C-CHECK INSPECTION AND COMPLIANCE OF AD 91-220-7, ASB 32-244, FOUND LEFT FLYING DOOR LINKAGE WORN. REPLACED WORN PARTS IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: LINKAGE — WORN (LT MLG DOOR)

DURING C-CHECK INSPECTION AND COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR LINKAGE WORN. REPLACED WORN PARTS IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: HINGE — WORN (LT MLG DOOR)

DURING C-CHECK INSPECTION AND COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR ARTICULATING DOOR HINGE WORN. REPLACED HINGE IAW DC-9 SRM 51-30-2.

Part: FLOOR PANEL — PUNCTURED (COCKPIT)

DURING C-CHECK INSPECTION, FOUND COCKPIT FLOOR PANEL PUNCTURED AFT OF THE PILOT'S CONTROL COLUMN. REPAIRED IAW DC-9 SRM 53-21-0, FIGURE 2B.

Part: BULKHEAD TEE CAP — CRACKED (BS 996)

DURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD T-CAP CRACKED AT APPROXIMATELY LONGERON 27L. REPLACED T-CAP IAW DC-9 SRM 53-03, FIGURE 37A.

Part: BULKHEAD TEE — TRIMMED (BS 996)

DURING C-CHECK INSPECTION AND AFT PRESSURE BULKHEAD T-CAP CHANGE, LONGERON 25 LEFT TEE WAS TRIMMED FOR ACCESS. REPAIRED IAW ABX REA D953-15276-MR.

Part: PAN — CRACKED (BS 176)

DURING C-CHECK INSPECTION, FOUND CRACKED CUP ASSEMBLY AT STA 176, RBL 22. FABRICATED PAN IAW DOUGLAS DRAWING NR 922405 AND INSTALLED IAW DC-9 SRM 51-30-2.

Part: PAN — CRACKED (BS 176)

DURING C-CHECK INSPECTION, FOUND CRACKED CUP ASSEMBLY AT STA 176, BL 0. FABRICATED PAN IAW DOUGLAS DRAWING NR 922405 AND INSTALLED IAW DC-9 SRM 51-30-2.

Part: PAN — CRACKED (BS 176)

DURING C-CHECK INSPECTION, FOUND CRACKED CUP ASSEMBLY AT STA 176, LBL 44. FABRICATED PAN IAW DOUGLAS DRAWING NR 9922405 AND INSTALLED IAW DC-9 SRM 51-30-2.

Part: PAN — CRACKED (BS 176)

DURING C-CHECK INSPECTION, FOUND CRACKED CUP ASSEMBLY AT STA 176, LBL 22. FABRICATED PAN IAW DOUGLAS DRAWING NR 922405 AND INSTALLED IAW DC-9 SRM 51-30-2.

Part: PAN — CRACKED (BS 176)

DURING C-CHECK INSPECTION, FOUND CRACKED CUP ASSEMBLY AT STA 176, RBL 44. FABRICATED PAN IAW DOUGLAS DRAWING NR 9922405 AND INSTALLED IAW DC-9 SRM 51-30-2.

Part: SUBFLOOR — DAMAGED (BS 160 - 200)

DURING C-CHECK INSPECTION, FOUND SUBFLOOR DAMAGED AT STA 160 TO 200. REPAIRED IAW DC-9 SRM 53-01 FIGURE 2, SHEET 3.

Part: DOOR — WORN (RT WING)

DURING C-CHECK AND COMPLIANCE OF AD 91-22-07 ASB 32-244, FOUND THE RIGHT FLYING DOOR LINKAGE WORN AND THE SEAL CRACKED. REPLACED DOOR IAW DC-9 MM.

Part: PANEL — CORRODED (BS 737)

DURING C-CHECK INSPECTION, FOUND CORROSION ON UPPER SURFACE OF THE AFT CENTER PRESSURE PANEL. REPAIRED IAW ABX REA D953-15270-MR.

Part: CUSP — CRACKED (BS 237 - 242)

DURING C-CHECK INSPECTION, FOUND CUSP WEB CRACKED AT STA 237 TO 242 RIGHT. REPLACED CUSP IAW DC-9 SRM 51-30-1 AND 51-30-2.

Part: WEB — CORRODED (BS 218)

DURING C-CHECK INSPECTION, FOUND EXFOLIATION CORROSION THROUGH SUBFLOOR AT STA 218, RBL 22 TO RBL 44. REPAIRED IAW ABX REA D953-15251-MR.

Part: FRAME — DAMAGED (BS 465)

DURING C-CHECK INSPECTION, FOUND FRAME 465 HAD A HOLE IN THE RADIUS AT LONGERON 16L. REPAIRED IAW DC-9 SUPP SRM K05159.

Part: LONGERON — CRACKED (BS 408)

DURING C-CHECK INSPECTION, FOUND LONGERON 17R CRACKED AT STA 408. REPAIRED IAW DC-9 SRM 53-02, FIGURE 2.

Part: CUSP — CRACKED (BS 870 - 889)

DURING C-CHECK INSPECTION, FOUND CUSP WEB CRACKED AT STA 870 TO 889 LEFT. REPAIRED IAW DC-9 SRM 53-01, PAGE 11.

Part: FRAME — CRACKED (BS 696)

DURING C-CHECK INSPECTION, FOUND CRACKED FRAME AT STA 696 AT LEFT CANTED KEEL. REPAIRED IAW DC-9 SRM 53-03, FIGURE 12.

Part: LONGERON — CRACKED (BS 980)

DURING C-CHECK INSPECTION, FOUND LONGERON 17L CRACKED AT STA 980. REPAIRED IAW DC-9 SRM 53-02, FIGURE 2.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK INSPECTION, FOUND LONGERON 17R CRACKED AT PYLON BULKHEAD. REPAIRED IAW DC-9 SRM 53-02, FIGURE 2.

Part: CUSP — CRACKED (BS 256)

DURING C-CHECK INSPECTION, FOUND CUSP WEB CRACKED AFT OF STA 256 RIGHT. REPAIRED IAW DC-9 SRM 53-01 FIGURE 2, SHEET 2 AND 51-10-3.

Part: FRAME — CRACKED (BS 675)

DURING C-CHECK INSPECTION, FOUND CRACKED FRAME AT STA 675 AT LEFT CANTED KEEL. REPLACED DOUBLER IAW DC-9 SRM 53-03, FIGURE 12.

Part: CUSP — CORRODED (BS 332 - 351)

DURING C-CHECK INSPECTION, FOUND RIGHT SIDE CUSP WEB CORRODED FROM STA 332 TO 351. REPAIRED IAW DC-9 SRM 53-01, FIGURE 2.

Part: CUSP — CRACKED (BS 218)

DURING C-CHECK INSPECTION, FOUND CUSP WEB CRACKED AT STA 218 RIGHT. REPAIRED IAW DC-9 SRM 53-01, FIGURE 2.

Part: CUSP — CRACKED (BS 275)

DURING C-CHECK INSPECTION, FOUND CUSP WEB CRACKED AT STA 275, LONGERON 18R. REPAIRED IAW DC-9 SRM 53-01, FIGURE 2.

Part: DN LOCK SWITCH — DEFECTIVE (NLG)

NOSE GEAR GREEN DOWN LIGHT WENT OUT WITH GEAR EXTENSION, CYCLED LANDING GEAR, LIGHT FLICKERED OUT AND ON AGAIN. VERIFIED, FOUND PIN 'C' BROKEN OFF OF NOSE GEAR DOWNLOCK SWITCH. REMOVED BROKEN PIN FROM CONNECTOR PLUG AND REPLACED NOSE GEAR DOWNLOCK SWITCH PER DC-9 MM 32-60-0. SYSTEM GROUND CHECKS GOOD.

Part: DOOR — WORN (LT MLG)

DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGE LUGS WORN AND ONE LUG MISSING A BUSHING. REPLACED OUTBOARD DOOR IAW DC-9 MM 32-12-1.

Part: ROD ENDS — WORN (LT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR DRIVER ROD ENDS WORN. REPLACED DRIVER ROD IAW DC-9 OH MANUAL 32-10-6.

Part: FITTING — CRACKED (HORIZ STAB)

DURING COMPLIANCE OF AD 82-06-02, SB 55-32, FOUND A CRACK AT FORWARD UPPER RIGHT HAND HI-LOCK IN THE REAR SPAR FITTING. REPLACED CONSTANT SECTION IAW DC-9 SRM 51-30-1.