N949AX

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 56,657 hrs · 57,539 cycles

DOUBLER ATTACHED TO FUSELAGE SKIN AT FUEL SHROUD WAS CORRODED, LONGERON 20 AREA. REMOVED AND INSTALLED NEW DOUBLER IAW DC9 SRM.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 56,657 hrs · 57,539 cycles

LONGERON 20 INBOARD AT LEFT WHEEL WELL CORRODED AT STA 718. REMOVED LONGERON 20. DRILLED LONGERON 20 P/N 5914259-501AX, IAW DOUGLAS DWG 5914579 AND DC9 SRM 51-10-4. REINSTALLED LONGERON 20 IAW DWG 5914579, DC9 SRM 51-30-5 AND 51-30-1.

Part: PRESSURE PANEL — CORRODED (BS 708) · airframe 56,657 hrs · 57,539 cycles

WHEEL WELL PRESSURE PANEL WAS BULGED AND CRACKED AT APPROXIMATELY FS 708, BUTT LINE 0. REPAIRED WHEEL WELL PRESSURE PANEL APPROXIMATELY FS 708 IAW DC9 REA D953-55487.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 56,657 hrs · 57,539 cycles

LOWER LEG OF SEAT TRACK CORRODED AT STA 699, RIGHT BUTT LINE 10. BLENDED OUT OF LIMITS. REMOVED SEAT TRACK FROM STA 663 - 763 AND FLOOR PANEL 8F. REINSTALLED NEW SEAT TRACK IAW DC9 SRM DWG K05482. RE-INSTALLED FLOOR PANEL 8F IAW DC9 SRM 51-30-1.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,657 hrs · 57,539 cycles

CORROSION AT AND AROUND INTERCOSTAL STA 737 - 756, LEFT BUTT LINE 22. INSTALLED INTERCOSTAL IAW DC9 SRM 51-30-5.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,657 hrs · 57,539 cycles

INTERCOSTAL AT LONGERON 29 RIGHT CORRODED BETWEEN LONGERON 29 RIGHT AND INTERCOSTAL FROM STA 965 - 980, BULGED ON INBOARD LEGS. REMOVED AND REPLACED INTERCOSTAL LONGERON 29 RIGHT, FS 965 TO 980 IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FRAME — CORRODED (BS 718) · airframe 56,657 hrs · 57,539 cycles

CRACK WITH EXFOLIATION ABOVE RADIUS ON FORWARD SIDE OF FRAME AT STA 718, APPEARED TO BE IN THE WEB AREA. REPLACED FRAME ON EA 53400323-001-2.

Part: FRAME — CORRODED (FUSELAGE) · airframe 56,657 hrs · 57,539 cycles

FORWARD LOWER CARGO FRAME CORRODED AT FS 465 BETWEEN LONGERON 28 LEFT AND LONGERON 28 RIGHT. REMOVED CORROSION AND REPLACED SECTION OF FRAME IAW DC9 SRM 53-03.

Part: WEB — CRACKED (FUSELAGE) · airframe 55,840 hrs · 56,679 cycles

STA 1038 BULKHEAD AT LONGERON 13 LEFT WAS CRACKED AT LIGHTENING HOLE. REPAIRED IAW DC-9 SRM 53-01.

Part: FRAME — CRACKED (AFT CARGO) · airframe 55,840 hrs · 56,679 cycles

FRAME CRACKED FS 889 AT LONGERON 29 LEFT. REPAIRED CRACKED FRAME FLANGE IAW DC-9 SRM DWG K05159.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,811 hrs · 55,582 cycles

INTERCOSTAL CRACKED AT FORWARD CONDUIT HOLE, STA 155, 43 INCHES UP FROM FLOOR RIGHT SIDE. REPAIRED AREA IAW DC-9 SRM 53, 51-30-2 AND 51-30-5.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 54,811 hrs · 55,582 cycles

UPPER AFT DOOR STOP FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,766 hrs · 54,543 cycles

DURING LINE MAINTENANCE VISIT, FUSELAGE SKIN WAS CRACKED AT THE FORWARD ENTRY DOOR, UPPER AFT CORNER, STATION 218, LONGERON 7 LEFT. REPAIRED FUSELAGE SKIN IAW DC-9 SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 53,676 hrs · 54,439 cycles

CUSP WEB CRACKED AT SEAT TRACK HOLE RIGHT BUTT LINE 54, STATION 795. REPAIRED CUSP WEB IAW DC-9 SRM 51-00.

Part: FORMER — CRACKED (CABIN) · airframe 53,676 hrs · 54,439 cycles

SHEARTIE AT STATION 980 WAS CRACKED AT LONGERON 14 LEFT. REPLACED SHEARTIE IAW DC-9 SRM 51-30-5.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 53,676 hrs · 54,439 cycles

LONGERON 17 LEFT WAS CRACKED ON UPPER AND LOWER FLANGE AT STATION 945 FRAME. REPAIRED AREA IAW DC-9 SRM 53-02.

Part: ACM — MALFUNCTIONED (A/C BAY) · airframe 53,459 hrs · 54,204 cycles

TOP OF DESCENT SAW AND SMELLED ELECTRIC SMOKE IN COCKPIT. SMOKE CLEARED THEN RECURRED. REQUESTED PRIORITY LANDING. LANDING NORMAL. NO ABNORMAL ELECTRICAL INDICATIONS. CHECKED ELECTRICAL SYSTEM FOR BURNING, NOTHING FOUND. RAN ENGINES AND APU PRESSURE A/C FAINT SMELL OF SMOKE NOTED. NOTICED LEFT PACK OUTPUT VERY LOW BUT PRESSURE NORMAL. FOUND LEFT ACM MOTOR OIL LOW, CHECKED WATER SEPARATOR. FOUND EVIDENCE OF OIL IN SOCK AND SOCK SMELLED BURNED. REPLACED SOCK. REPLACED LEFT COOLING TURBINE. OPS CHECKED GOOD IAW DC-9 MM 21-51-01-2-0002.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, FOUND LONGERON 17L CRACKED FS 965. REPLACED SECTION OF LONGERON 17L FS 965 IAW DC9 SRM 53-02.

Part: LONGERON — CRACKED (BS 160)

DURING C-CHECK, FOUND LONGERON 4 LEFT AT FS 160 CRACKED. REPLACED NEW SECTION OF LONGERON IAW DC9 SRM 53-02.

Part: WEB — CORRODED (BS 945)

DURING C-CHECK, FOUND CUSP WEB CORRODED FS 945, LBL 50-54. REPLACED SECTION OF LEFT CUSP WEB 945L IAW ABX REA 953 24 702 MR.

Part: SKIN — CORRODED (BS 946-950)

DURING C-CHECK, FOUND FUSELAGE SKIN CORRODED FS 946-950 LONGERON 27R - LONGERON 29R. REPLACED DOUBLERS FS 945-980 LONGERON 27R TO LONGERON 29R, IAW DC9 MM 51-30-2.

Part: SKIN — CORRODED (BS 756-760)

DURING C-CHECK, FOUND CORROSION ON LONGERON 30 AND ADJACENT FUSELAGE SKIN LONGERON 29R TO LONGERON 30R, FS 756-760. REPAIRED FUSELAGE SKIN IAW ABX REA D953 24724.

Part: FRAME — CORRODED (BS 917)

DURING C-CHECK, FOUND CORROSION ON FRAME 917 AT LONGERON 29L-LONGERON 29R. REPAIRED IAW DC9 SRM 53-03.

Part: FRAME — CRACKED (BS 718)

DURING C-CHECK, FOUND LEFT MAIN FRAME FS 718 CRACKED. REPAIRED LEFT FUSELAGE MAIN FRAME FS 718 IAW ABX REA D953- 24732-SB.

Part: WINDOW — BINDING (COCKPIT)

CAPTAIN'S SIDE WINDOW (EMERG EXIT) WOULD NOT OPEN. ADJUSTED WINDOW TRIM AND LUBRICATED UPPER SLIDE TRACK.

Part: WINDOW — BINDING (LT COCKPIT)

CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. LUBRICATED LOCKBAR, CHECKED RIGGING AND OPERATION OF WINDOW. OPS CHECKED GOOD.,

Part: BATTERY — DISCHARGED (CABIN)

COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED BATTERY PACK. OPS CHECKED GOOD.

Part: WINDOW LOCK — STUCK (COCKPIT)

CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. FREED THE TOP LOCK ON WINDOW, OPS CHECKED GOOD.

Part: BULKHEAD TEE CAP — CORRODED (BS 996)

DURING C-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD TEE CAP CORRODED FROM LONGERON 27 RIGHT TO LONGERON 30. REPAIRED AFT PRESSURE BULKHEAD T-CAP IAW DC-9 SRM CHAPTER 53-03 FIGURE 37.

Part: SKIN — CORRODED (BS 604)

DURING C-INSPECTION, FOUND THE FUSELAGE SKIN BULGING AROUND FASTNERS AT FS 604 AT LONG 30. REPLACED TEE CAP AND DOUBLERS IAW ABX REA D953-18329MR AND D953-18288MR.

Part: FLOORBEAM — CORRODED (BS 939)

DURING C-INSPECTION, FOUND THE LOWER CHANNEL ON FLOORBEAM AT FS 939 CORRODED AT NUT PLATES FROM LONGERON 18 RIGHT TO LONGERON 18 LEFT. REPLACED FLOORBEAM SUPPORT CHANNELS IAW DC-9 SRM CHAPTER 51-30-2.

Part: FLOORBEAM — CORRODED (BS 937)

DURING C-INSPECTION, FOUND LEVEL 2 CORROSION ON FLOORBEAM AT FS 937 LOWER FLANGE RBL 10 TO RBL 18. REPAIRED FLOORBEAM IAW ABX REA D953-18328MR AND DC-9 SRM CHAPTER 53-05, FIGURE 65.

Part: CLIP — CRACKED (BS 980)

DURING C-INSPECTION, FOUND SHEAR TIE CLIP CRACKED AT FS 980 BELOW LONGERON 14 RIGHT. REPLACED SHEAR TIE CLIP AT FS 980 FROM LONGERON 13 RIGHT TO 17 RIGHT IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.

Part: WEB — CRACKED (BS 617)

DURING C-INSPECTION, FOUND THE RIGHT CUSP WEB IN MAIN CARGO COMPARTMENT CRACKED AT FS 617 AND RBL 56. REPLACED CUSP PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.

Part: SPAR CAP — CORRODED (RT HORIZ STAB)

DURING C-INSPECTION, FOUND THE RIGHT HORIZONTAL STAB FORWARD FACE OF THE UPPER REAR SPAR HAS LEVEL 2 CORROSION AT APPROXIMATE STATION XHS 140. REPAIRED RT HORIZONTAL UPPER REAR SPAR CAP IAW ABX REA D955-18175MR.

Part: VANE — DELAMINATED (RT TE FLAP)

DURING C-INSPECTION, FOUND THE RIGHT FLAP INBOARD FIXED VANE DELAMINATED. REPLACED RT INBOARD FIXED VANE IAW DC-9 MAINTENANCE MANUAL, CHAPTER 27-51-3.

Part: VANE — DELAMINATED (LT TE FLAP)

LEFT WING INBOARD VANE DELAMINATED. REPLACED HONEYCOMB CORE, DOUBLERS AND SKIN.

Part: VANE — DELAMINATED (RT TE FLAP)

THE RIGHT WING INBOARD FIXED FLAP VANE HAD DELAMINATION ON THE UPPER SURFACE BETWEEN RUBSTRIPS. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN IAW DC-9 SRM.

Part: VANE — CORRODED (LT TE FLAP)

LEFT INBOARD FIXED VANE CHAFFED AND CORRODED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.

Part: CLIP — CRACKED (BS 945)

DURING C-INSPECTION, FOUND A SHEAR TIE CLIP CRACKED AT FS 945 BELOW LONGERONS 14 RIGHT AND 15 RIGHT. REPLACED SHEAR TIE CLIP AT FS 945 IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.

Part: RIB — CRACKED (VERT STAB)

DURING C-INSPECTION, FOUND VERTICAL STAB LEADING EDGE 4TH RIB CRACKED RIGHT SIDE AT AFT END. REPAIRED CRACK IAW DC-9 SUPPLEMENTAL SRM DRAWING K05159.

Part: SPAR CAP — CORRODED (RT HORIZ STAB)

DURING C-INSPECTION, FOUND THE RIGHT HORIZONTAL STAB INTER SPAR BOX HAS A CORROSION BLEND OUT THAT WAS BLENDED BEYOND LIMITS AT XHS 130. REPAIRED RT HORIZONTAL UPPER REAR SPAR CAP IAW ABX REA D955-18175MR.

Part: RIB — CRACKED (VERT STAB)

DURING C-INSPECTION, FOUND VERTICAL STAB LEADING EDGE LOWER SECTION 5 RIB CRACKED, LEFT SIDE AT AFT END. REPAIRED CRACK IAW DC-9 SUPPLEMENTAL SRM DRAWING K05159.

Part: SPAR CAP — CORRODED (LT HORIZ STAB)

DURING C-INSPECTION, FOUND LT HORIZONTAL STAB UPPER REAR SPAR CAP AT XHS 181.0 CORRODED. REPAIRED LT HORIZONTAL REAR SPAR CAP IAW ABX REA D955-18219MR.

Part: GUSSET — CRACKED (BS 737)

DURING C-INSPECTION, FOUND A GUSSET CRACKED ON THE FLOORBEAM AT FS 737 RIGHT BL 30. REPLACED GUSSET IAW DC-9 SRM CHAPTER 51-30-2.

Part: DOUBLER — CRACKED (WS 267)

DURING C-INSPECTION, FOUND THE RIGHT WING LEADING EDGE SKIN SEAM DOUBLER AND ATTACH ANGLE AT WS 267 CRACKED. REPLACED LEADING EDGE SEAM DOUBLER IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.

Part: RIB — CRACKED (VERT STAB)

DURING C-INSPECTION, FOUND THE VERTICAL STAB LEADING EDGE REMOVABLE SECTION NR 8 CANTED RIB CRACKED LT SIDE AT AFT END. REPAIRED CRACK IAW DC-9 SUPPLEMENTAL SRM DRAWING K05159.

Part: DOOR — CRACKED (LT MLG)

DURING C-INSPECTION, FOUND THE LOWER CORNER OF THE LEFT MLG OUTBOARD ARTICULATING DOOR CRACKED. REPLACED THE DOOR IAW DC-9 SRM CHAPTER 51-30-2.

Part: RIB — CRACKED (VERT STAB)

DURING C-INSPECTION, FOUND THE VERTICAL STAB LEADING EDGE REMOVABLE SECTION NR 3 RIB CRACKED LEFT SIDE AT AFT END. REPAIRED CRACK IAW DC-9 SUPPLEMENTAL SRM DRAWING K05159.

Part: RIB — CRACKED (VERT STAB)

DURING C-INSPECTION, FOUND THE VERTICAL STAB LEADING EDGE REMOVABLE SECTION NR 7 RIB CRACKED LEFT SIDE AT AFT END. REPAIRED CRACK IAW DC-9 SUPPLEMENTAL SRM DRAWING K05159.

Part: TAB — DAMAGED (RT AILERON)

THE RIGHT AILERON TAB WAS DAMAGED, HOLE IN UPPER OUTBOARD SKIN. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.

Part: AILERON — CORRODED (RT WING)

DURING C-INSPECTION, FOUND THE RIGHT AILERON LOWER SURFACE HAS CORROSION BULGES AT AILERON DAMPNERS. REPLACED RIGHT AILERON IAW DC-9 MAINTENANCE MANUAL CHAPTER 27-10-1 AND 27-10-2.

Part: SWITCH — DIRTY (RT MLG)

RETRACTED THE LANDING GEAR AFTER TAKEOFF. RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED. RECYCLED THE LANDING GEAR AND ALL INDICATIONS NORMAL. ALL INDICATIONS WERE NORMAL WHEN THE LANDING GEAR WAS LOWERED FOR LANDING. CLEANED GEAR INDICATION SWITCHES AND PERFORMED GEAR SWING IAW DC-9 M.M. 7-11-07 AND 32-00.

Part: UPLATCH MECH — DEFECTIVE (RT MLG)

PERFORMING LANDING GEAR UPLATCH CHECK, THE RIGHT GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT ILLUMINATED. CYCLED THE GEAR DOWN AND UP, LIGHT WENT OUT AND THE GEAR UPLATCH CHECKED NORMAL. REPLACED THE RIGHT MAIN LANDING GEAR UPLATCH MECHANISM. GROUND CHECKED NORMAL IAW DC-9 MM 32-31-4 AND DC-9 SUPP MM 32-60-00.

Part: UPLATCH ASSY — OVERTORQUED (RT MLG)

RIGHT GEAR UNSAFE LIGHT ILLUMINATED ON GEAR RETRACTION. RECYCLED GEAR, NO HELP. ON UPLATCH CHECK, GEAR DOOR OPEN LIGHT ILLUMINATED. RAISED HANDLE, KEPT RIGHT HYDRAULIC PRESSURE AT 3,000 PSI. FOUND HARDWARE ON UPLATCH MECHANISM OVER TORQUED NOT ALLOWING THE LATCH HOOK TO MOVE INTO POSITION. RETORQUED HARDWARE IAW DC-9 MM 32-31-4, OPS CHECK GOOD ON GEAR SWING.

Part: UPLATCH SWITCH — DEFECTIVE (RT MLG)

RIGHT HAND MAIN GEAR UNSAFE LIGHT ON AFTER TAKEOFF. RECYCLED LANDING GEAR, LIGHT WENT OUT. PERFORMED GEAR UPLATCH CHECK, ALL SYSTEMS NORMAL. REPLACED RIGHT MAIN LANDING GEAR UPLATCH SWITCH IAW DC-9 SUPP MM 32-60-01, OPS CHECK GOOD.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING PRE-FLIGHT INSPECTION, FOUND THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED THE NICAD BATTERIES IN THE EMERGENCY LIGHT POWER SUPPLY PACK IAW DC-9 SUPP. M.M. 33-53-0.

Part: DOOR FRAME — CRACKED (FS 170)

DURING COMPLIANCE OF AD'S 81-10-10, 90-18-03, SB'S 52-125 AND 52-127, FOUND FORWARD SERVICE DOOR BOTTOM BEAM HAD VISUAL AND EDDY CURRENT CRACK INDICATIONS. REPLACED SERVICE DOOR AND ADJUSTED IAW DC-9 MM 52-41-0.

Part: DOOR FRAME — CRACKED (FS 170)

DURING COMPLIANCE OF AD'S 81-10-10 AND 90-18-03, SB'S 52-125 AND 52-127, FOUND FORWARD SERVICE DOOR, SECOND FROM THE TOP BEAM HAD VISUAL AND EDDY CURENT CRACK INDICATIONS. REPLACED SERVICE DOOR AND ADJUSTED IAW DC-9 MM 52-41-0.

Part: DOOR FRAME — CRACKED (FS 170)

DURING COMPLIANCE OF AD'S 81-10-10 AND 90-18-03, SB'S 52-125 AND 52-127, FOUND THE FORWARD SERVICE DOOR UPPER BEAM HAD VISUAL AND EDDY CURRENT CRACK INDICATIONS. REPLACED SERVICE DOOR AND ADJUSTED IAW DC-9 MM 52-41-0.

Part: SKIN — HOLES ELONGATED (FS 1087)

DURING C-CHECK INSPECTION, FOUND LOOSE SCREWS ON THE VERTICAL STABILIZER, LEFT SIDE FORWARD BOTTOM ATTACH ANGLE. REPAIRED IAW ABX REA D953-11728-MR.

Part: DOUBLER — CRACKED (FS 125)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 56-11, REV 3, FOUND CRACKED DOUBLER AROUND RIGHT CLEARVIEW WINDOW FRAME UPPER AFT CORNER. REPAIRED BY REPLACING DOUBLER IAW DC-9 SRM 51-30-2 AND 51-30-1.

Part: SKIN — CORRODED (FS 268)

DURING C-CHECK INSPECTION, FOUND LEVEL I CORROSION AROUND THE NR 1 AND NR 2 ADF LOOP ANTENNAS ON THE UPPER FUSELAGE SKIN. REPAIRED IAW ABX REA D953-11673-MR.

Part: SKIN — GOUGED (FS 425)

DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN GOUGED AT STA 425 LONGERON 30. REPAIRED IAW ABX REA D953-11709-MR.

Part: JAMB — PUNCTURED (FS 383)

DURING C-CHECK INSPECTION, FOUND FLC DOOR JAMB WEB PUNCTURED AT STA 383 AND LONGERON 29R. REPAIRED IAW ABX REA D953-11695-MR.

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 RIGHT WING LOWER T-CAP BETWEEN STRINGERS 17 TO 18, 18 TO 19 AND 19 TO 20 AT STA XCW 58. REMOVED CORROSION IAW DC-9 SRM 51-10-3.

Part: BUSHING — WORN (WS 111.5)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT FLYING DOOR DRIVE ROD OUTBOARD END HAD SIDE PLAY. REPLACED BUSHINGS IAW DC-9 MM 32-10-6.

Part: BRACKET — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION AND CRACKED BRACKET BETWEEN STRINGERS 15 AND 16 AT STA XCW 58 ON THE RIGHT WING. REPLACED BRACKET IAW DC-9 SRM 51-30-5. CLEANED CORROSION BELOW BRACKET IAW DC-9 SRM 51-10-3.

Part: STRINGER — CORRODED (WS 58)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL 1 CORROSION INSIDE BARREL NUT HOLE IN STRINGER 16, RIGHT WING. REMOVED CORROSION IAW DC-9 SB 57-98, 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 1 CORROSION ON LEFT WING LOWER T-CAP BETWEEN STRINGERS 11 TO 12 AND 16 TO 17 AT STA XCW 58. REMOVED CORROSION IAW DC-9 SRM 51-10-3.

Part: JAMB — DAMAGED (FS 160)

DURING C-CHECK INSPECTION, FOUND ENTRY DOOR CUTOUT SKIN AND REPAIR SEPARATED AT UPPER FORWARD CORNER. REPAIRED IAW DC-9 SRM 53-05 FIGURE 25A AND ABX REA D953-11613-MR.

Part: ARM — WORN (WS 111.5)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT FLYING DOOR ARTICULATING DOOR DRIVE ROD END HAD SIDE PLAY. REPLACED ARM IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: BUSHING — WORN (WS 111.5)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR DRIVE ROD OUTBOARD END HAD SIDE PLAY. REPLACED BUSHINGS IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: DOOR — DENTED (WS 111.5)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR ARTICULATING DOOR HAD DENT ON INBOARD END. REPLACED DOOR IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: FITTING — WORN (WS 111.5)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR ARTICULATING DOOR FORWARD DRIVE LINK HAD SIDE PLAY. REPLACED DRIVE LINK ATTACH FITTING IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: DOOR — DAMAGED (WS 111.5)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEVEL 1 CORROSION, SHEARED FASTENERS AND CHAFING ON LEFT FLYING DOOR. ALSO, FOUND SKIN BENT AT AFT END OF HINGE. REPLACED FLYING DOOR IAW DC-9 MM 32-12-1.