N925AX

Part: FLOOR SUPPORT — CORRODED (FWD CARGO) · airframe 40,885 hrs · 52,134 cycles

STA 218 FLOOR SUPPORT WAS CORRODED ABOVE LONGERON 30. REPAIRED FRAME AT FS 218, LONGERON 30 IAW DC-9 SRM 53-03.

Part: FLOOR SUPPORT — CRACKED (AFT CARGO BAY) · airframe 40,885 hrs · 52,134 cycles

FLOOR SUPPORT STRAP, ATTACH ANGLE CRACKED, FS 768 AT LONGERON 27 RIGHT. REPLACED ANGLE IAW DC-9 SRM 51-30-5.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 40,885 hrs · 52,134 cycles

AFT LOWER CARGO DOOR, TRAILING EDGE NR 5 BEAM END FITTING CRACKED. INSTALLED NEW FITTING IAW DC-9 SRM 51-30-5 AND 51-30-2.

Part: SKIN — CORRODED (LEFT WING) · airframe 40,885 hrs · 52,134 cycles

RIGHT WING UPPER SKIN CORRODED AND PULLED RIVETS JUST INBOARD OF SPOILER ACTUATOR. REPLACED SECTION OF STRINGER AND SPLICE IAW DC-9 SRM 51-70-5 AND 51-30-5.

Part: WIRE — BURNED (NR 1 CIRCUIT) · airframe 40,646 hrs · 51,703 cycles

PRIMARY TRIM NR 1 CIRCUIT BREAKER TRIPPED. FOUND WIRES C104C10, C1203C10, C1202C10, C1202B10, C1203B10, C1204B10, C1213A10, C1213B10, C1211B10 BURNED. FOUND WIRE C1205D16 NOT CONNECTED. FOUND RELAY R20-16 BADLY BURNED. REPAIRED ALL WIRING AND REPLACED RELAYS R20-16 AND R20-15 IAW DC-9 WIRING DIAGRAM MANUAL 24-41-01. OPS CHECKED GOOD IAW DC-9 MM.

Part: LINK — CRACKED (THRUST REVERSER) · airframe 40,462 hrs · 51,428 cycles

NR 2 LOWER AFT LEFT THRUST REVERSER DRIVER LINK WAS CRACKED. REPLACED THE NR 2 LOWER LEFT DRIVE LINK IAW DC-9 MM 78-31-05-2-0001, NEA 7830001, TASK NEA 13435, AD 75-14-06, AD 96-10-11, AND SERVICE BULLETIN 78-66.

Part: STIFFENER — CRACKED (RT WING) · airframe 40,267 hrs · 51,124 cycles

OUTBOARD STATION 91.00, FRONT SPAR VERTICAL STIFFENER, UPPER PORTION WAS CRACKED. REPLACED STIFFENER IAW DC-9 SRM.

Part: SKIN — CRACKED (RT MLG DOOR) · airframe 40,267 hrs · 51,124 cycles

RIGHT MAIN LANDING GEAR DOOR INNER SKIN CRACKED JUST AFT OF THE FORWARD HINGE FITTING. REPAIRED CRACKED AREA IAW DC-9 SRM 52-01.

Part: FITTING — CRACKED (CABIN) · airframe 40,267 hrs · 51,124 cycles

LEFT OVER WING EXIT DOOR PAN STIFFENER ANGLES ON OUTER PAN CRACKED 5 INCHES. REPLACED STOPS IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,267 hrs · 51,124 cycles

AUXILIARY SUPPORT FRAME CRACKED IN AFT ACCESSORY COMPARTMENT FLOOR SUPPORT, FORWARD OF MAIN FRAME AT STATION 908. REPLACED FRAME IAW DC-9 SRM DWG 505159 AND DC-9 SRM 51-30-2.

Part: ANGLE — CRACKED (LEFT WING) · airframe 40,267 hrs · 51,124 cycles

OUTBOARD LOWER FASTENER HOLE ON ATTACH ANGLE CRACKED WHERE WING TO FUSELAGE FAIRING ATTACHES AT F.S. 585. REPLACED ANGLE IAW DC-9 SRM 51-30-1 AND DC-9 DWG 9915547.

Part: FINGER DOUBLER — DEBONDED (LT WING) · airframe 40,267 hrs · 51,124 cycles

OUTBOARD REMOVABLE TRAILING EDGE LOWER SKIN FINGER DOUBLERS WERE DEBONDED. REPLACED UPPER/LOWER SKINS IAW REA D957-43379.

Part: CONTROL CABLE — LACK OF LUBE (T/E FLAP) · airframe 40,220 hrs · 51,053 cycles

FINAL APPROACH, AIRCRAFT IN A TRIMMED DESCENT ON GLIDESLOPE, FLAPS 30, N1-60 PERCENT ON BOTH ENGINES, SPEED 10 + OVER TARGET 139. WENT TO FLAP 40, AIRCRAFT ROLLED RIGHT NOTICEABLE, 1 1/2 UNITS LEFT TO TRIM. INSPECTED AILERON AND FLAP CABLE SYSTEM. ALSO INSPECTED AILERON TRIM SYSTEM. NO DEFECTS FOUND. VERIFIED FLAP POSITION INDICATION BY USING FLAP PROTRACTOR, CHECKED GOOD. LUBRICATED FLAP AND AILERON SYSTEM. OPS CHECKED GOOD.

Part: INDICATOR — SHORTED (MLG) · airframe 39,581 hrs · 50,110 cycles

AFTER SELECTING LANDING GEAR DOWN, NOSE GEAR SAFE LIGHT DID NOT ILLUMINATE. NO RED GEARWARNING LIGHT. PERFORMED ABNORMAL PROCEDURES AND GO-AROUND. VISUALLY CHECKED GEAR DOWN ANDLOCKED. LANDING WAS UNEVENTFUL. FOUND NOSE GEAR DOWN LIGHT ASSEMBLY INTERNALLY SHORTED. REPLACED LIGHT ASSEMBLY. PERFORMED GEAR SWING. OPS CHECKED GOOD.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 39,530 hrs · 50,027 cycles

FLOORBEAM WEB AT STATION 786 AND LBL 13.0 IS EXFOLIATED. REPAIRED IAW ABX REA D957-38011.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 39,530 hrs · 50,027 cycles

LEFT AND RIGHT RADIAL STIFFENERS NR 14 WERE CRACKED. REPLACED IAW DC9 SRM 51-30-5.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 39,530 hrs · 50,027 cycles

LONGERONS 23 AND 24 LEFT WERE CORRODED AT STATIONS 817 - 823. REPAIRED LONGERONS 23 AND 24 LEFT IAW DC9 SRM 50-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,530 hrs · 50,027 cycles

FRAME OUTSIDE FLANGE CRACKED AT STATION 801 AND LONGERON 17 LEFT. REPLACED FRAME IAW DC9 SRM 52-03.

Part: SHEAR TIE — CRACKED (CABIN) · airframe 39,530 hrs · 50,027 cycles

EXTRUSION FORWARD OF AFT PRESSURE BULKHEAD T-CAP AT LONGERON 18 LEFT WAS CRACKED AT FLOOR LINE. REPLACED SHEAR TIE ANGLE IAW DC9 SRM 51-30-2.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 39,530 hrs · 50,027 cycles

FLOOR SUPPORT WAS CRACKED AT CUSP LINE JUST FORWARD OF PRESSURE DOME ON RIGHT SIDE. REPAIRED IAW DC9 SRM.

Part: STIFFENER — CRACKED (RT WING SPAR) · airframe 39,530 hrs · 50,027 cycles

REAR SPAR STIFFENER WAS CRACKED AT STATION XRS 313. REPLACED STIFFENER IAW DC9 SRM 51-30-5.

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,530 hrs · 50,027 cycles

LONGERON FITTING CRACKED AT STATION 585 AND LONGERON 11 LEFT. REPLACED FITTING IAWDC9 SRM 51-30-5.

Part: PAN — CRACKED (CARGO DOOR) · airframe 39,530 hrs · 50,027 cycles

FORWARD LOWER CARGO DOOR INBOARD SIDE OF PAN WAS CRACKED. INSTALLED DOUBLER IAW DC9 SRM 52-05.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,530 hrs · 50,027 cycles

LONGERON 30 HAD LEVEL 2 CORROSION AT STATION 642. REPLACED LONGERON IAW DC9 SRM 53-02.

Part: SKIN — DELAMINATED (SPOILER) · airframe 39,530 hrs · 50,027 cycles

RIGHT INBOARD SPOILER WAS DELAMINATED. REPLACED SPOILER IAW DC9 MM 27-62-01.

Part: HINGE — CRACKED (RT FLAP) · airframe 39,530 hrs · 50,027 cycles

RIGHT FLAP HINGE CRACKED AT STATION 351. REPLACED FLAP HINGE.

Part: WINDOW — STUCK (LT COCKPIT)

CAPTAIN'S CLEAR VIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. LUBRICATED CAPTAIN'S CLEAR VIEW WINDOW TRACK. OPS CHECKED GOOD.

Part: LINK — OUT OF ADJUST (NLG)

AFTER TAKEOFF WITH GEAR HANDLE IN UP POSITION, THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. GEAR CYCLED DOWN NORMALLY. ON RETRACTION, NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. AIR TURNBACK TO ILN. RESHIMMED NOSE LANDING GEAR ACTUATOR LINK AND ADJUSTED NOSE LANDING GEAR DOOR.

Part: RETAINER — CRACKED (LT COCKPIT)

DURING C-CHECK, FOUND LEFT WINDOW RETAINER CRACKED. REPAIRED CRACK IAW DC9 SERVICE REWORK DRAWING 5952965.

Part: JAMB — CRACKED (SERVICE DOOR)

DURING C-CHECK, FOUND SERVICE DOOR JAMB INTERNAL WEB CRACKED 2 PLACES AT UPPER HINGE CUTOUT, STATION 160. REPAIRED IAW ABX REA D953-25631.

Part: ANGLE — CRACKED (NR 1 PYLON)

DURING C-CHECK, FOUND NR 1 LOWER PYLON ATTACH ANGLE CRACKED IN RADIUS ON FORWARD EDGE. REPAIRED ANGLE IAW DC9 SRM 54-04.

Part: FITTING — CRACKED (LT TE FLAP)

DURING C-CHECK, FOUND LEFT FLAP INBOARD FIXED VANE OUTBOARD ATTACH SUPPORT FITTING BROKEN. REPLACED FITTING IAW DC9 SRM 51-30-2, 52-30-5, AND DACO DWG 9957773.

Part: LATCH — LOOSE (COCKPIT DOOR)

COCKPIT DOOR EXTREMELY DIFFICULT TO OPEN FROM CABIN. TIGHTENED DOOR HANDLE/LATCH ASSEMBLY, OPS CHECKED GOOD.

Part: SKIN — CRACKED (BS 544)

DURING C-CHECK, FOUND THE FUSELAGE SKIN CRACKED 4 INCHES LONG AT LONGERON 18R, FS 544. REPAIRED CRACKED SKIN IAW DC9 SRM 53-04, FIGURE 12B.

Part: SPAR CAP — CORRODED (WS 40)

DURING C-CHECK, FOUND THE CENTER WING SPAR AFT VERTICAL FACE OF THE SPAR CAP AT STA XCW -40 SEVERLY CORRODED. REPAIRED IAW ABX REA D957-19174-MR.

Part: FITTING — CRACKED (BS 786)

DURING C-CHECK, FOUND THE FLOORBEAM FITTING AT F/STA 786 LT CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5 AND 51-30-1.

Part: BULKHEAD WEB — CRACKED (BS 786)

DURING C-CHECK, FOUND THE UPPER CARGO BULKHEAD AT F/STA 786 LT WEB CRACKED. REPAIRED IAW ABX REA D953-19255-MR.

Part: WEB — CORRODED (BS 786)

DURING C-CHECK, FOUND THE CUSP WEB AT F/STA 786 LT CORRODED. REPLACED CUSP WEB IAW DC9 SRM 51-30-2.

Part: DOOR PAN — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND THE FORWARD CARGO COMPARTMENT DOOR PAN CRACKED BOTH SIDES OF NR 1 PRESSURE STOP. REPAIRED UPPER CRACK IAW DC9 SRM 52-05, FIGURE 50 AND LOWER CRACK IAW DC9 SRM 52-03, FIGURE 1.

Part: BULKHEAD FITTING — CRACKED (WS 69)

DURING C-CHECK, FOUND THE RIGHT WING BULKHEAD FITTING AT W/STA XRS 69 BETWEEN STRINGERS 12 AND 13 INSIDE LT WING FUEL TANK CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-05.

Part: RIB — CRACKED (WS 172)

DURING C-CHECK, FOUND THE RIGHT WING LEADING EDGE RIB AT STA 172 CRACKED. CUTOUT CRACKED SECTION OF RIB, AND REPAIRED IAW ABX REA D957-19252.

Part: FLOORBEAM — CORRODED (BS 786)

DURING C-CHECK, FOUND THE FLOORBEAM AT F/STA 786 CORRODED AT LBL 27 ON TOP SIDE. REPAIRED IAW ABX REA D953-19248-MR.

Part: TRAPEZOIDAL PNL — CRACKED (RT MLG WW)

DURING C-CHECK, FOUND THE RT TRAPEZOIDAL PANEL CRACKED JUST ABOVE THE RT MLG FIXED STRUT ATTACH POINT. REPLACED TRAPEZOIDAL PANEL IAW DC9 SRM 57-09, FIGURE 34 AND DACO SB 53-182.

Part: FRAME — CRACKED (BS 801)

DURING C-CHECK, FOUND FUSELAGE FRAME STA 801 CRACKED AT LONGERON 17R. REMOVED AND REPLACED CRACKED SECTION OF FRAME IAW DC9 SRM 53-03, FIGURE 32.

Part: SKIN — DAMAGED (BS 408)

DURING C-CHECK, FOUND FUSELAGE SKIN DAMAGED AT STA 408, LONGERON 21L. REPAIRED SKIN IAW DC9 SRM 53-04, FIGURE 38, SHT 20.

Part: FITTING — CRACKED (RT MLG WW)

DURING C-CHECK, FOUND THE RT FLOORBEAM TO KEEL WEB ATTACH FITTING AT FS 585 CRACKED. REPLACED RT FLOORBEAM ATTACH FITTING IAW ABX REA D953-19152-MR, DC9 SRM 51-30-5.

Part: FITTING — CRACKED (BS 218)

DURING C-CHECK, FOUND FORWARD INTERCOSTAL FS 218 BETWEEN LONG 27 AND 28 L CRACKED. REPLACED ATTACH ANGLE (FITTING) P/N 5956034-527 PER DC9 SRM 51-30-2.

Part: FLOORBEAM — CRACKED (BS 503)

DURING C-CHECK, FOUND FLOORBEAM AT FS 503 AND LBL 57 CRACKED. REPLACED FLOORBEAM IAW DC9 SRM.

Part: SKIN — CORRODED (RT TE FLAP VANE)

RIGHT INBOARD FIXED VANE HAS HOLE IN SKIN AND CORRODED. REPLACED ALL HONEYCOMB CORE DOUBLERS AND SKIN.

Part: LONGERON — CRACKED (FUSELAGE)

DURING THE C-CHECK INSPECTION, FOUND THE FORWARD END OF LONGERON 20R CRACKED. REPAIRED LONG 20R IAW DC9 SRM, FIGURE 9.

Part: DOOR — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND DOOR PAN CRACKED. REPAIRED CRACK PER DC9 SRM.

Part: SUBFLOOR — CRACKED (BS 207)

DURING C-CHECK, FOUND THE FORWARD SUBFLOOR MEMBRANE CRACKED AT FS 207 AND LBL 26. REPAIRED FORWARD SUBFLOOR MEMBRANE IAW DC9 SRM 53-01, FIGURE 1.

Part: LONGERON — CRACKED (BS 313-332)

DURING C-CHECK, FOUND LONGERON 29 LT CRACKED AT SPLICE FS 313 TO 332. REMOVED CRACKED SECTION OF LONGERON, MACHINED NEW SPLICE AND REPAIRED IAW ABX REA D953-19175.

Part: ANGLE — CRACKED (LT WING)

DURING C-CHECK, FOUND REAR SPAR TRAILING EDGE RIB ANGLE ADJACENT TO OUTBOARD FLAP HINGE FITTING IS CRACKED. REMOVED AND REPLACED ANGLE IAW DC9 SRM 51-30-1.

Part: ANGLE — CRACKED (RT PYLON)

DURING C-CHECK, FOUND AN ANGLE CRACKED INSIDE THE RT PYLON AT THE AFT OUTBOARD CORNER OF PANEL NR 8206. REPLACED ANGLE IAW DC9 SRM 51-30-2.

Part: HINGE — CRACKED (LT MLG DOOR)

DURING C-CHECK, FOUND MLG INBOARD DOOR HINGE AFT LUG CRACKED. REPLACED MLG DOOR HINGE HALF IAW DC9 SRM 51-30-1.

Part: BEAM — CRACKED (SERVICE DOOR)

DURING C-CHECK, FOUND THE FORWARD SERVICE DOOR BEAM AT UPPER HINGE CUTOUT IS CRACKED. REPAIRED DOOR BEAM IAW DC9 SRM 52-05.

Part: SKIN — DENTED (BS 165)

DURING C-CHECK, FOUND EXTERIOR FUSELAGE SKIN DENTED AT FS 165 AND LONG 21R - 22R. REPAIRED DENT IAW DC9 SRM 53-04, FIGURE 38, VIEW F.

Part: FITTING — CRACKED (LT SPOILER)

DURING C-CHECK, FOUND TWO LEFT WING INBOARD SPOILER TORQUE TUBE SUPPORT FITTINGS CRACKED. REPLACED SUPPORT FITTINGS IAW DC9 SRM 51-30-5.

Part: FITTING — CRACKED (BS 786)

DURING C-CHECK, FOUND FLOORBEAM FITTING ATTACHED TO LEFT PYLON BULKHEAD AT FS 786 CRACKED. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: ANGLE — CRACKED (RT MLG WW)

DURING C-CHECK, FOUND ANGLE AT LONGERON 20 RT AND FORWARD END OF TRAPEZIODAL PANEL IS CRACKED AND CORRODED. REMOVED AND REPLACED ANGLE IAW DC9 SRM 51-30-1.

Part: MEMBRANE — CRACKED (BS 207)

DURING C-CHECK, FOUND THE FORWARD SUBFLOOR MEMBRANE CRACKED AT FS 207 AND LBL 26. REPAIRED FORWARD SUBFLOOR MEMBRANE IAW DC9 SRM 53-01.

Part: FITTING — CORRODED (RT MLG WW)

DURING C-CHECK, FOUND ATTACH FITTING OUTBOARD OF THE TRAPEDZOIDAL PANEL MOST FORWARD HOLE COMMON TO TRAP PANEL CORRODED INSIDE. REPLACED FITTING IAW DC9 SRM 51-30-5 AND 51-30-1.

Part: MOUNT — CHAFED (NR 1 ENGINE)

DURING C-CHECK, FOUND NR 1 ENGINE FORWARD LOWER MOUNT YOKE CHAFED ON INSIDE WALL AT 12 O'CLOCK POSITION. REMOVED AND REPLACED FORWARD YOKE AND VIBRATION ABSORBERS IAW DC9 MM.

Part: LONGERON — CORRODED (BS 408)

STATION 408, LONGERON 30 HAS BULGE IN SKIN. REPAIRED IAW DC-9 SRM 53-04, FIG 12B. INTERCOSTAL AT STATION 408, LONGERON 30 IS CORRODED. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2.

Part: ANGLE — DENTED (BS 20)

DURING C-CHECK INSPECTION, FOUND LEFT UPPER KEEL WEB ANGLE AT STRINGER 17 HAD A HI-LOCK THAT HAD DENTED THE ANGLE. REPAIRED IAW ABX REA D953-12409-MR.

Part: DOOR FRAME — MISDRILLED (BS 758)

DURING C-CHECK INSPECTION, FOUND MISDRILLED HOLES IN DOOR JAMB AREA OF AFT LOWER COMPARTMENT. REPAIRED IAW ABX REA D953-12393-MR.

Part: SPAR CAP — CORRODED (WS 524)

DURING C-CHECK INSPECTION, FOUND RIGHT WING AFT SPAR LOWER CAP CORRODED AROUND NUTPLATES OUTBOARD OF AILERON. REPAIRED IAW ABX REA D957-12414-MR.

Part: JAMB — CORRODED (BS 718-758)

DURING C-CHECK INSPECTION, FOUND LOWER AFT CARGO DOOR JAMB CORRODED AT STA 718 TO 758. REPAIRED IAW ABX REA D953-12365-MR.

Part: DOOR JAMB — MISDRILLED (BS 758)

DURING C-CHECK INSPECTION, FOUND MISDRILLED HOLES IN DOOR JAMB AREA OF AFT LOWER CARGO COMPARTMENT. REPAIRED IAW ABX REA D953-12393-MR.

Part: DOOR JAMB — MISDRILLED (BS 758)

DURING C-CHECK INSPECTION, FOUND MISDRILLED HOLES IN DOOR JAMB AREA OF AFT LOWER CARGO COMPARTMENT. REPAIRED IAW ABX REA D953-12393-MR.

Part: BUSHING — WORN (LT MLG)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 91-22-07, ASB 32-244, FOUND LEFT OUTBOARD GEAR DOOR BEARING ON FORK ASSEMBLY WORN. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: ROD END — WORN (RT MLG DOOR)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT OUTBOARD GEAR DOOR FORWARD LONG ROD ASSEMBLY HAD A WORN EYEBOLT. REPLACED ROD END IAW DC-9 OHM 32-10-6.

Part: BLKHD WEB — CORRODED (BS 817)

DURING C-CHECK INSPECTION, FOUND A GOUGE AND LEVEL I CORROSION IN TWO PLACES ON AFT PRESSURE BULKHEAD WEB FORWARD SIDE, BETWEEN FIVE-THIRTY AND SIX-THIRTY POSITIONS. REPAIRED IAW ABX REA D 953-12405-MR.

Part: SKIN — CORRODED (BS 718)

DURING C-CHECK INSPECTION, FOUND CORROSION ON FUSELAGE SKIN FORWARD OF AFT BAG BIN. REPAIRED IAW ABX REA D953-12392-MR.

Part: FAIRING — CORROSION (FS 699-718)

DURING C-CHECK INSPECTION, FOUND LEVEL I CORROSION ALONG THE PARAMETER OF THE LEFT AFT WING TO BODY FAIRING. REPAIRED IAW ABX REA D953-12379-MR.

Part: TE WEDGE — CRACKED (RUDDER)

DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 87-08-02, SB 55-23 REV 5, FOUND DEFECT IN RUDDER TRAILING EDGE PHENOLIC WEDGE DURING X-RAY INSPECTION. REPLACED PHENOLIC WEDGE IAW DC-9 SRM 51-30-2.

Part: ANGLE — CRACKED (LT PYLON)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-8, FOUND LEFT UPPER PYLON ANGLE CRACKED ATSTA 860. REPAIRED IAW DC-9 SRM 54-04 FIG 10.

Part: GEAR DOOR — BENT (LT MLG)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 91-22-07, ASB 32-244, FOUND TRAILING EDGE OF LEFT OUTBOARD GEAR DOOR BENT. REPLACED SEAL IAW DC-9 SRM 51-30-2.