N980AX

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,791 hrs · 84,381 cycles

SHEAR TIE CRACKED AT STA 1090, 8 INCHES OUTBOARD OF RT CENTER LINE. REMOVED AND REPLACED SHEAR TIE AT STA 1090 IAW DC-9 SRM 51-30-5 AND 53-30-2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,791 hrs · 84,381 cycles

FUSELAGE SKIN CRACKED FS 1090, APPROXIMATELY 2 INCHES TO THE RIGHT SIDE OF VERTICAL STAB, SKIN CRACKED OUT OF HI-LOK APPROXIMATELY .25 INCH LONG. REPAIRED FUSELAGE SKIN AT FS 1090, RIGHT SIDE OF VERTICAL STAB IAW DC-9 SRM 53-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,791 hrs · 84,381 cycles

FUSELAGE SKIN CRACKED FS 1090, ONE O'CLOCK POSITION FACING AFT. CRACK APPROXIMATELY 2.5 INCHES LONG, LEFT SIDE OF VERTICAL STABILIZER. MANUFACTURED REPAIR DOUBLER FROM 2014T6 .063 PO 408448187. REPAIRED AREA IAW DC-9 SRM 53-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,791 hrs · 84,381 cycles

FUSELAGE SKIN CRACKED FS 1090, APPROXIMATELY 4 INCHES TO THE LEFT OF VERTICAL STAB. MANUFACTURED REPAIR DOUBLER FROM 2014-T6 .063 PO 408448187. REPAIRED AREA IAW DC-9 SRM 53-01.

Part: ANGLE — CORRODED (MLG WW BULKHEAD) · corrosion level 2 · airframe 72,190 hrs · 83,888 cycles

LEFT WHEEL WELL AFT BULKHEAD UPPER ANGLE CORRODED AT BUTTLINE 0. REPAIRED ANGLE IAW REA D953-51024-MR.

Part: LONGERON — CRACKED (E & E BAY) · airframe 72,190 hrs · 83,888 cycles

LONGERON 23 LEFT CRACKED AT STA 200. REPAIRED LONGERON IAW DC-9 SRM 53-02.

Part: BATTERY — DISCHARGED (CABIN) · airframe 71,845 hrs · 83,557 cycles

EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW AMM 33-00-00.

Part: CONNECTOR — DAMAGED (OVERHEAT DETECT) · airframe 71,082 hrs · 82,866 cycles

AFTER TAKEOFF, TAIL COMPARTMENT TEMP HIGH ILLUMINATED. ACCOMPLISHED EMERGENCY PROCEDURE CHECKLIST AND ANNUNCIATOR REMAINED ILLUMINATED. LANDED WITHOUT INCIDENT. REPLACED CONNECTOR P1-387, AFTER FINDING WIRES SHORTED AND TOUCHING EACH OTHER. TAIL COMPARTMENT WAS COOL UPON ARRIVAL. OPS CHECKED GOOD AT ILN.

Part: FITTING — CRACKED (REAR SPAR) · airframe 71,052 hrs · 82,839 cycles

RIGHT INBOARD FIXED VANE NR 2 SUPPORT CRACKED. REPLACED BROKEN FITTING IAW DC-9 SRM 51-30-2.

Part: FITTING — CRACKED (PYLON BULKHEAD) · airframe 71,052 hrs · 82,839 cycles

AFT LOWER INBOARD FITTING CRACKED FS 965 PYLON BULKHEAD RIGHT SIDE. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 71,052 hrs · 82,839 cycles

LT FORWARD MAIN FRAME FS 699 CRACKED ON FORWARD FLANGE FROM BOLT IN RADIUS. REPLACED FRAME ON JOB CARD EA 53400321-001.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 71,052 hrs · 82,839 cycles

RIGHT AFT VERTICAL STAB TO FUSELAGE ATTACH ANGLE WAS CRACKED. REPAIRED ANGLE IAW DC-9 SRM 53-05.

Part: CONTROL CABLE — CONTAMINATED (THROTTLE) · airframe 70,770 hrs · 82,601 cycles

THROTTLES EXTREMELY DIFFICULT TO MOVE DURING FLIGHT. EXPECTED ICE CONTAMINATION. CLEANED AND LUBRICATED CABLES AND FAIRLEADS ABOVE FORWARD BAG BIN. ICE REMNENTS NOTED ON GILL LINER ABOVE BAG BIN. THROTTLE MOVEMENT NORMAL. REMOVED ICE. MOPPED CARGO COMPARTMENT AS REQUIRED.

Part: FLANGE — CRACKED (RIGHT FLAP) · airframe 70,633 hrs · 82,494 cycles

RIGHT FLAP INBOARD FIXED VANE GOUGED ON UPPER SURFACE DUE TO CRACKED ATTACH ANGLE. REPLACED FIXED VANE AND CRACKED VANE ATTACH ANGLE IAW DC-9 SRM 51-30-05 AND DC-9 MM 27-51-03-2-0002.

Part: CUSHION — DEFECTIVE (COCKPIT) · airframe 70,409 hrs · 82,308 cycles

FIRST OFFICER'S SEAT CUSHION DID NOT FIT OR ATTACH TO SEAT FRAME PROPERLY. SOMETIMES RESTRICTED AFT MOVEMENT OF CONTROL COLUMN. REPLACED FIRST OFFICER'S SEAT CUSHION AS REQUIRED IAW DC-9 MM.

Part: SWITCH — DEFECTIVE (NG WELL) · airframe 69,708 hrs · 81,804 cycles

DURING DEPARTURE WHEN LANDING GEAR WAS RETRACTED, A RED NOSE GEAR UNSAFE LIGHT ILLUMINATED. THE LANDING GEAR WAS RECYCLED AND THE GEAR RETRACTED NORMALLY. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR UPLOCK AND DOWN LOCK SWITCHES. OPERATIONAL CHECKS WERE COMPLETED IAW DC-9 MM 32-60-01, AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 69,706 hrs · 81,801 cycles

SPLICE FITTING AT FUSELAGE STATION 229, L18R WAS FOUND TO BE CRACKED. MAINTENANCE REPLACED THE FITTING IAW DC-9 SRM 51-30-1.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 69,706 hrs · 81,801 cycles

THE LEFT AFT EMERGENCY EXIT DOOR INNER JAMB WAS CRACKED ON UPPER INTERIOR AFT CORNER ADJACENT TO HANDLE. MAINTENANCE REPAIRED THE AREA IAW DC-9 SRM 52-05.

Part: RIB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,706 hrs · 81,801 cycles

CORROSION FOUND ON RIB LOCATED IN THE RIGHT NOSE WHEEL TUNNEL STATION 100, BELOW PRESSURE WEB. MAINTENANCE INSTALLED A DOUBLER IAW DC-9 SRM 51-30-2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,706 hrs · 81,801 cycles

THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT THE AFT LOWER CORNER OF SERVICE DOOR CUT OUT. MAINTEANCE REPAIRED THE AREA IAW ABX EA 53100123-001.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,706 hrs · 81,801 cycles

FRAME WAS FOUND CRACKED AT FUSELAGE STATION 980,L16L. MAINTENANCE REPAIRED THE FRAME IAW DC-9 SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,706 hrs · 81,801 cycles

SHEAR TIE REPAIR WAS FOUND TO BE CRACKED AT FUSELAGE STATION 945 L14R. MAINTENANCE REPLACED THE SHEAR TIE IAW DC-0 SRM 51-30-2.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,706 hrs · 81,801 cycles

SHEAR TIE WAS FOUND CRACKED AT FUSELAGE STATION 1059 L17L. MAINTENANCE REPLACED THE SHEAR TIE SECTION IAW DC-9 SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,706 hrs · 81,801 cycles

MAIN FRAME AT STATION 737R WAS CRACKED BETWEEN "Z" ANGLE FASTENERS. MAINTENANCE REPAIRED THE FRAME IAW ABX EA 53400320-001-1.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 69,706 hrs · 81,801 cycles

SHEAR TIE REPAIR WAS FOUND TO BE CRACKED AT FUSELAGE STATION 980, L16R. MAINTENANCE REPLACED THE SHEAR TIE IAW DC-9 SRM AND ABX DRAWING N07080.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,706 hrs · 81,801 cycles

THE CABIN FLOOR LH VERTICAL SUPPORT UPPER FITTING WAS FOUND TO BE CRACKED AT STA 965. MAINTENANCE REPLACED THE CABIN FLOOR LH VERTICAL SUPPORT UPPER FITTING IAW DC-9 SRM 51-30-5.

Part: ANGLE — CRACKED (L PYLON) · airframe 69,706 hrs · 81,801 cycles

THE UPPER PYLON ATTACH ANGLE WAS FOUND TO BE CRACKED AT THE FORWARD END. MAINTENANCE REPAIRED THE ANGLE IAW DC-9 SRM 54-04 FIG. 10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,706 hrs · 81,801 cycles

MAIN FRAME AT STATION 718L WAS CRACKED BETWEEN "Z" ANGLE FASTENERS. MAINTENANCE REPAIRED THE FRAME IAW ABX EA 53400210-001-1.

Part: FAIRING — CORRODED (VERTICAL STAB)

WHILE COMPLYING WITH A C-CHECK INSPECTION, FOUND LOWER RIGHT SIDE HORSE COLLAR CORRODED. REPLACED LOWER RIGHT SIDE HORSE COLLAR IAW DC9 MM 55-10-0 AND DC9 SRM 51-30-1.

Part: DOUBLER — CORRODED (FUSELAGE)

WHILE COMPLYING WITH A C CHECK INSPECTION, FOUND LEFT SIDE STATIC PORT INTERNAL DOUBLER CORRODED. REPLACED INTERNAL DOUBLER IAW DC9 SRM 51-30-2.

Part: COLUMN — CRACKED (COCKPIT)

WHILE COMPLYING WITH A C CHECK INSPECTION, FOUND FIRST OFFICER'S CONTROL COLUMN CRACKED. REPLACED FIRST OFFICER'S CONTROL COLUMN REF DOUGLAS SERVICE BULLETIN.

Part: FITTING — CRACKED (RT MLG WW)

WHILE COMPLYING WITH A C CHECK INSPECTION, FOUND RIGHT WHEEL WELL KEEL TO FLOORBEAM ATACH FITTING CRACKED AT STA 737. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: FITTING — CRACKED (RT MLG WW)

WHILE COMPLYING WITH A C CHECK INSPECTION, FOUND RIGHT WHEEL WELL KEEL TO FLOORBEAM ATTACH FITTING CRACKED AT STA 718. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: INTERCOSTAL — CRACKED (CARGO BAY)

WHILE COMPLYING WITH A C CHECK INSPECTION, FOUND FORWARD LOWER CARGO DOOR INTERCOSTAL WEB CRACKED. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-1.

Part: PANEL — CRACKED (LT MLG WW)

UPPER OUTBOARD FLANGE OF LEFT TRAP PANEL CRACKED IN AREA OF HYDRAULIC LINES. VERIFIED WITH EDDY CURRENT INSPECTION. REPLACED LEFT TRAP PANEL IAW REA NR D953-35095-MR AND DC9 SERVICE BULLETIN 53-182.

Part: RELAY — FAILED (COCKPIT)

EMERGENCY DC BUS OFF LIGHT ILLUMINATED ON GENERATOR INOP CROSS-TIE CHECK. FOUND CONTACTS BETWEEN TERMINALS B1 AND B2 OPEN ON RELAY R2-19. REPLACED RELAY IAW DC9 MM, OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (RT MLG)

DURING LANDING GEAR RETRACTION, THE RIGHT GEAR UNSAFE (RED) LIGHT REMAINED ILLUMINATED. RECYCLED GEAR. NO CHANGE. GREEN LIGHT REMAINED OUT. WITH GEAR DOWN, LIGHTS WERE NORMAL. REPAIRED SHORTED WIRE AT TERMINAL STRIP S3-66.

Part: VALVE — FAILED (LANDING GEAR)

AFTER TAKEOFF, GEAR HANDLE SELECTED UP, THE NOSE LANDING GEAR AND MAIN LANDING GEAR UNSAFE LIGHTS REMAINED ILLUMINATED. GEAR WAS RECYCLED THREE TIMES WITH THE SAME RESULT. REPLACED LANDING GEAR CONTROL VALVE IAW DC9 MM 32-32-0.

Part: SHEAR TIE — CRACKED (BS 1019)

DURING C-CHECK, FOUND FRAME SHEAR TIE AT STATION 1019 CRACKED BETWEEN LONGERON 14L AND 15L. REPLACED SHEAR TIE IAW DC9 SRM 51-30-5.

Part: FLOORBEAM — CRACKED (BS 351)

DURING C-CHECK, FLOORBEAM AT STATION 351 BL6 LEFT WAS FOUND CRACKED. REPAIRED IAW ABX REA D953-23658-MR.

Part: FITTING — CORRODED (BS 604)

DURING C-CHECK, LEVEL II CORROSION WAS FOUND ON LONGERON 28 RIGHT END CAP STATION 604. REPLACED IAW DC9 SRM 51-10-03.

Part: BLKHD FITTING — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, AFT PRESSURE BULKHEAD DOOR RIGHT VERTICAL SUPPORT FITTING WAS FOUND CRACKED. REPLACED FITTING IAW DC9 SRM 51-10-04.

Part: ANGLE — CRACKED (NR 1 PYLON)

DURING C-CHECK, THE LEFT UPPER PYLON ATTACH ANGLE WAS FOUND CRACKED. REPAIRED IAW DC9 SRM 54-04.

Part: LONGERON — CRACKED (BS 756)

DURING C-CHECK, LONGERON 5 RIGHT WAS FOUND CRACKED AT STATION 756. REPAIRED IAW DC9 SRM 51-30-1.

Part: FITTING — CORRODED (BS 604)

DURING C-CHECK, LEVEL II CORROSION WAS FOUND ON LONGERON 27 RIGHT AND END CAP AT STATION 604. REPLACED FITTING IAW DC9 SRM 51-30-2.

Part: SPLICE — CRACKED (BS 794-813)

DURING C-CHECK, LONGERON SPLICE AT STATION 794-813, LONGERON 30 WAS FOUND CRACKED. REPLACED IAW DC9 SRM 53-02.

Part: HINGE — CRACKED (LT TE FLAP)

DURING C-CHECK, THE LEFT FLAP CENTER HINGE WAS FOUND CRACKED. REPLACED IAW DC9 MM 27-50-1.

Part: UPLATCH — WORN (RT MLG DOOR)

AFTER GEAR RETRACTION ON TAKEOFF, THE RIGHT GEAR UNSAFE LIGHT REMAINED ON. RECYCLED GEAR AND PERFORMED UPLATCH CHECK WITH NORMAL INDICATION. REPLACED RIGHT MAIN LANDING GEAR DOOR UPLATCH ASSEMBLY IAW DC9 MM 32-31-4.

Part: UNSAFE LIGHT — ILLUMINATED (RT MLG)

AFTER GEAR RETRACTION, THE RIGHT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. IN THE GEAR UP-LATCH CHECK POSITION, THE GEAR DOOR UNSAFE LIGHT ILLUMINATED. RECYCLED GEAR DOWN AND UP, NORMAL OPERATION. PERFORMED ADJUSTMENT/TEST IAW DC9 MM 32-31-4, FOUND NO DEFECTS. OPERATED LANDING GEAR SEVERAL TIMES, PERFORMED UP-LATCH CHECK. OPS CHECKED NORMAL. NO DEFECTS NOTED.

Part: BATTERY — DISCHARGED (CABIN)

COCKPIT EMERGENCY LIGHTS WERE VERY DIM. REPLACED BATTERIES. OPS CHECKED GOOD.

Part: WINDOW — BINDING (COCKPIT)

CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) EXTREMELY HARD TO OPERATE. SANDED DOWN WINDOW EPOCAST SEAL AND LUBRICATED WINDOW LINKAGE.

Part: DOOR LATCH — OUT OF ADJUST (RT MLG)

ON TAKEOFF, RIGHT GEAR UNSAFE LIGHT ILLUMINATED. GEAR UPLATCH CHECK UNSATISFACTORY. CYCLED GEAR TWICE WITH SAME RESULTS (GEAR DOOR OPEN LIGHT ILLUMINATED DURING UPLATCH CHECK) WITH AERODYNAMIC BUFFETING. INSTALLED A .030 SHIM UNDER THE GEAR DOOR LATCH ROLLERS IAW DC-9 MM 32-31-4.

Part: SWITCH — DEFECTIVE (RT MLG)

AFTER TAKEOFF, RT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. AFTER SECOND RECYCLE, LIGHT WENT OUT. *S/D* REPLACED RIGHT MAIN LANDING GEAR WARNING SWITCH. CHECKED SECURITY OF ALL ATTACHMENTS AND COMPONENTS. RAN LANDING GEAR THROUGH 15 CYCLES IAW DC9 MM 32-61-01, NO DEFECTS NOTED.

Part: UPLATCH MECH — LACK OF LUBE (RT MLG)

AFTER TAKEOFF, RIGHT GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. RECYCLED GEAR, NO CHANGE, FOLLOWED BY THE GEAR DOOR OPEN LIGHT ILLUMINATING. TURNED ON THE RIGHT HYDRAULIC PUMP AND THE GEAR DOOR OPEN LIGHT WENT OUT WITH THE GEAR UNSAFE LIGHT REMAINING ON. FLEW TO ILN WITH THE PUMP ON AT .70 MACH. CLEANED AND LUBRICATED THE RIGHT GEAR UPLATCH MECHANISM, PERFORMED ADJUSTMENT AND TEST IAW DC-9 SUPP MM 32-60-00, OPS CHECKED GOOD.

Part: WINDOW — LACK OF LUBE (LT COCKPIT)

CAPTAIN'S SLIDING WINDOW VERY HARD TO OPEN AND GREASE ON LINKAGE. LUBED CAPTAIN'S CLEARVIEW WINDOW AND CHECKED RIG IAW DC-9 MM 56-10-3.

Part: WINDOW — OUT OF ADJUST (LT COCKPIT)

CAPTAIN'S CLEARVIEW WINDOW VERY HARD TO OPEN AND CLOSE. ADJUSTED CAPTAIN'S CLEARVIEW WINDOW IAW DC-9 MM 56-10-3.

Part: WINDOW — OUT OF ADJUST (LT COCKPIT)

CAPTAIN'S WINDOW WILL NOT CLOSE. ADJUSTED CAPTAIN'S CLEARVIEW WINDOW AND ASSOCIATED MECHANISM'S IAW DC-9 MM 56-10-3.

Part: FRAME — CRACKED (BS 1074)

DURING C-CHECK, THE CANTED FRAME AT STA 1074 WAS FOUND CRACKED AT LONGERON 4 LT. REPAIRED IAW REA D953-16684-MR.

Part: FRAME — CRACKED (BS 1155)

DURING C-CHECK, THE CANTED FRAME AT STA 1155 WAS FOUND CRACKED AT LONGERON 4 LT. REPAIRED IAW REA D953-16713-MR.

Part: FRAME — CRACKED (BS 1104)

DURING C-CHECK, THE CANTED FRAME AT STA 1104 WAS FOUND CRACKED AT LONGERON 4 LT. REPAIRED IAW REA D953-16685-MR.

Part: FRAME — CRACKED (BS 1121)

DURING C-CHECK, THE CANTED FRAME AT STA 1121 WAS FOUND CORRODED AND CRACKED AT LONGERON 5 LT. REPAIRED IAW DC-9 SRM.

Part: ANGLE — CRACKED (VERTICAL STAB)

DURING C-CHECK, THE VERTICAL STABILIZER INTER SPAR BOX FORWARD LOWER ATTACH ANGLE WAS FOUND CRACKED. REPAIRED IAW REA D955-16656-MR.

Part: FRAME — CRACKED (BS 1155)

DURING C-CHECK, THE CANTED FRAME AT STA 1155 WAS FOUND CRACKED AT LONGERON 4 RT. REPAIRED IAW REA D953-16713-MR.

Part: ANGLE — CRACKED (NR 2 PYLON)

DURING C-CHECK, A CRACK WAS FOUND IN THE UPPER PYLON TO FUSELAGE ATTACH ANGLE. REPLACED ANGLE IAW DC-9 SRM.

Part: FRAME — CRACKED (BS 718)

DURING C-CHECK, THE FUSELAGE MAIN FRAME AT STA 718 RT WAS FOUND CRACKED BEYOND A PREVIOUS REPAIR. REPAIRED IAW REA D953-16620.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LONGERON 17L CRACKED AT FRAME 965. REPLACED IAW DC-9 SRM.

Part: LONGERON — CRACKED (BS 980)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LONGERON 17R CRACKED AT FRAME 980. REPLACED IAW DC-9 SRM.

Part: LONGERON — CRACKED (BS 980)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LONGERON 17L CRACKED AT FRAME 980. REPLACED IAW DC-9 SRM.

Part: SPLICE — CRACKED (WS 267)

DURING C-CHECK, THE LEFT WING LEADING EDGE SPLICE WAS FOUND CRACKED AT STA 267. REPLACED SPLICE IAW DC-9 SRM.

Part: SPLICE — CRACKED (WS 111)

DURING C-CHECK, THE LEFT WING LEADING EDGE SPLICE WAS FOUND CRACKED AT STA 111. REPLACED SPLICE IAW DC-9 SRM.

Part: DNLOCK SWITCH — DEFECTIVE (RT MLG)

AFTER TAKEOFF, LANDING GEAR WAS RETRACTED AND RIGHT GEAR UNSAFE LIGHT REMAINED ON. GEAR WAS RECYCLED, LIGHT STAYED ON. UPLATCH CHECK WAS ACCOMPLISHED, GEAR UNSAFE LIGHT WENT OUT. REPLACED RIGHT MAIN GEAR DOWN LOCK SWITCH PER DC-9 SUPP MM 32-60-01, OPS CHECK GOOD.

Part: FITTING — CRACKED (FWD SERV DOOR)

DURING COMPLIANCE OF AD 81-10-10, AD 90-18-03, SB'S 52-125, REV 5 AMD SB 52-127 REV 2, FOUND SERVICE DOOR TORQUE TUBE UPPER ATTACH FITTING HOUSING ASSEMBLY CRACKED. REPLACED UPPER ATTACH FITTING IAW DC-9 MM.

Part: CRANK ASSY — BROKEN (FWD SERV DOOR)

DURING COMPLIANCE OF AD'S 81-10-10 AND 90-18-03 SB'S 52-125 REV 5 AND SB 52-127, REV 2, FOUND CRANK ASSEMBLY SERVICE DOOR OPEN LATCH BROKEN. REPLACED CRANK ASSEMBLY IAW DC-9 MM.

Part: LINK — WORN (BS 111)

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

Part: POWER SUPPLY — INOPERATIVE (CABIN)

WITH A/C POWER OFF, BATTERY OFF AND EMERGENCY LIGHT SWITCH OFF, EMERGENCY LIGHTS REMAIN ON. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW DC9 MM 33-56.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

DURING MONDAY MORNING CHECK, FOUND EMERGENCY LIGHTS DIM. REPLACED BATTERIES IN BATTERY PACK. OPS CHECK BATTERY PACK IAW DC-9 SUPP MM 33-53-0.

Part: SKIN — GOUGED (FS 160)

DURING C-CHECK, INSPECTION FOUND SKIN GOUGED IN TWO PLACES, 12 AND 18 INCHES FROM BOTTOM OF DOOR JAMB ON FORWARD SIDE. REPAIRED IAW ABX REA D953-11260-MR.

Part: FRAME — MISDRILLED (FS 937)

DURING C-CHECK, INSPECTION FOUND THREE HOLES DRILLED AT EDGE OF ALC DOOR JAMB AT STA 937. REPAIRED IAW ABX REA D953-11237-MR.

Part: FLOORBEAM — GOUGED (BS 945)

DURING C-CHECK, INSPECTION FOUND FLOORBEAM AT STA 945 GOUGED ON FORWARD FACE, RBL 1. REPAIRED IAW ABX REA D953-11238-MR.

Part: JAMB — CRACKED (BS 160)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 94-03-01, FOUND THE UPPER FORWARD CORNER OF SERVICE DOOR JAMB HAD A CRACK IN THE EXTERIOR SKIN AT RIVET STA 160. TO GAIN ACCESS TO REPAIR SKIN THE WEB WAS CUT AT STA 184.375. REPAIRED CRACKED SKIN IAW DC-9 SRM 53-05 FIGURE 38 AND 51-30-5. INSTALLED WEB SPLICE IAW ABX REA D953-11251-MR.

Part: STRINGER — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING UPPER SURFACE OF STRINGER NR 17. BLENDED IAW DC-9 SRM 51-10-3.

Part: T CAP — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LOWER T-CAP ON LEFT WING BETWEEN STRINGERS 20 TO 21. BLENDED IAW DC-9 SB 57-98.

Part: T CAP — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING LOWER T-CAP BETWEEN STRINGERS 19 TO 20. BLENDED IAW DC-9 SB 57-98.

Part: T CAP — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING LOWER T-CAP AT FORWARD AND AFT FLANGES ON STRINGER NR 20. BLENDED IAW DC-9 SB 57-98.

Part: T CAP — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING T-CAP BETWEEN STRINGERS 21 TO 22. BLENDED IAW DC-9 SB 57-98.

Part: CAP — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING LOWER T-CAP BETWEEN STRINGERS 22-23. BLENDED IAW DC-9 SB 57-98.

Part: FRAME — CORRODED (BS 110)

DURING C-CHECK, INSPECTION FOUND LEVEL II CORROSION ON FUSELAGE FRAME AT STA 110, RIGHT NOSE WHEEL TUNNEL, LOWER AFT CORNER. REPAIRED FRAME IAW ABX REA D953-11209-MR.

Part: SKIN — CORRODED (BS 937)

DURING C-CHECK, INSPECTION FOUND LEVEL I CORROSION ON INSIDE OF OUTER SKIN, JUST AFT OF ALC DOOR JAMB AT STA 937. REPAIRED IAW ABX REA D953-11223-MR.

Part: ROD END — WORN (WS 111.5)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR ACTUATING ROD OUTBOARD END HAD EXCESSIVE PLAY. REPLACED ROD END IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: SKIN — BUCKLED (BS 37)

DURING C-CHECK, INSPECTION FOUND SKIN JUST ABOVE LEFT FORWARD CORNER OF FORWARD NOSE GEAR DOOR BUCKLED. REPAIRED SKIN IAW ABX REA D953-11207-MR.

Part: RIB — GOUGED (WS 123)

DURING C-CHECK, INSPECTION FOUND DEEP GOUGE ON RIGHT WING ADJACENT TO TELESCOPIC SLAT BLEED AIR DUCT. REPAIRED IAW ABX REA D957-11203-MR.

Part: CAP — CRACKED (WS 58)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND RIGHT WING LOWER T-CAP CRACKED IN THE RADIUS JUST AFT OF STRINGER NR 16. BLENDED IAW DC-9 SRM 51-10-3.

Part: STRINGER — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING ON TOP OF STRINGER NR 20. BLENDED IAW DC-9 SRM 51-10-3 AND 57-01.

Part: STRINGER — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER 23R. BLENDED IAW DC-9 SRM 51-10-3 AND 57-01.

Part: STRINGER — GOUGED (WS 58)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN RIGHT WING STRINGER NR 20. BLENDED IAW DC-9 SRM 57-01.

Part: STRINGER — GOUGED (WS 58)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 15, RIGHT WING. BLENDED IAW DC-9 SRM 57-01.

Part: STRINGER — GOUGED (WS 58)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 11, RIGHT WING. BLENDED IAW DC-9 SRM 57-01.

Part: STRINGER — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER NR 13, RIGHT WING. BLENDED IAW DC-9 SRM 51-00-1 AND 57-01.

Part: STRINGER — GOUGED (WS 58)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 18, RIGHT WING. BLENDED IAW DC-9 SRM 57-01.

Part: STRINGER — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER NR 11, RIGHT WING. BLENDED CORROSION IAW DC-9 SRM 51-22-1 AND 57-01.

Part: STRINGER — GOUGED (WS 58)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03; SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 13, RIGHT WING. BLENDED IAW DC-9 SRM 57-01.

Part: CAP — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING LOWER T-CAP, AFT OF STRINGER NR 11. BLENDED IAW DC-9 SRM 51-10-3.

Part: STRINGER — GOUGED (WS 58)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 16, RIGHT WING. BLENDED IAW DC-9 SRM 57-01.

Part: CAP — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING LOWER T-CAP, BETWEEN STRINGERS 11-12. BLENDED IAW DC-9 SB 57-98.

Part: STRINGER — GOUGED (WS 58)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 23R. BLENDED IAW DC-9 SRM 57-01.

Part: STRINGER — GOUGED (WS 58)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 12, RIGHT WING. BLENDED IAW DC-9 SRM 57-01.

Part: STRINGER — GOUGED (WS 58)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 14, RIGHT WING. BLENDED IAW DC-9 SRM 57-01.

Part: STRINGER — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER NR 16, RIGHT WING. BLENDED IAW DC-9 SRM 51-22-1 AND 57-01.

Part: STRINGER — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER NR 17, RIGHT WING. BLENDED IAW DC-9 SRM 51-22-1 AND 57-01.

Part: STRINGER — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER NR 12, RIGHT WING. BLENDED IAW DC-9 SRM 51-22-1 AND 57-01.

Part: STRINGER — GOUGED (WS 58)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03; SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 17, RIGHT WING. BLENDED IAW DC-9 SRM 57-01.

Part: STRINGER — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON STRINGER NR 22, LOWER FORWARD LEG. BLENDED IAW DC-9 SB 57-98.

Part: CAP — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING LOWER T-CAP, INSIDE BARREL NUT HOLES IN STRINGERS NR 12, 13, 14, 15, 16, 17, 18, 19 AND 21. BLENDED IAW DC-9 SRM 51-10-3 AND SB 57-98.

Part: CAP — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING LOWER T-CAP HORIZONTAL FLANGE INSIDE BARREL NUT HOLES IN STRINGERS 11, 14, 16, 18, 20 AND 21. BLENDED IAW DC-9 SB 57-98.

Part: HINGE — GOUGED (WS 111.5)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR HINGE DEEPLY GOUGED. REPLACE DOOR HINGE IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: DOOR — DELAMINATED (WS 111.5)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR AFT EDGE LOWER CORNER DELAMINATED. SEALED LEFT MAIN LANDING GEAR OUTBOARD DOOR AFT EDGE LOWER CORNER IAW DC-9 SRM 51-20-0. REPLACED RIVETS IAW DC-9 SRM 51-30-2.

Part: ARM ASSY — WORN (WS 111.5)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR FORWARD LINKAGE CONNECTING POINT HAD EXCESSIVE PLAY. REPLACED ARM ASSEMBLY IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: HINGE — WORN (WS 111.5)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR ARTICULATING DOOR HINGE HAD EXCESSIVE PLAY. REPLACED HINGE IAW DC-9 SRM 51-30-2 AND DC-9 OVERHAUL MANUAL 32-10-6.