N951AX

Part: INTERCOSTAL — CRACKED (BS 427-446) · airframe 56,878 hrs · 44,666 cycles

FRAME BETWEEN STA 427 AND 446 CRACKED AT APPROXIMATELY 435. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM.

Part: FLOOR SUPPORT — CRACKED (BS 1056-1072) · airframe 56,878 hrs · 44,666 cycles

LEFT FLOOR TRACK END FITTING/CLIP CRACKED AND ATTACHING INTERCOSTAL WAS CORRODED UNDER NUT PLATES, STA 1056 - 1072, LONGERON 27 - 28 LEFT. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM 51-30-1.

Part: ANGLE — CRACKED (FUSLEAGE) · airframe 56,878 hrs · 44,666 cycles

THE TEE ANGLE CRACKED, FORWARD DOOR JAMB, INBOARD MOUNT. REMOVED AND REPLACED TEE ANGLE IAW DC9 SRM 51-30-5.

Part: POWER SUPPLY — DEFECTIVE (EMERGENCY LIGHT) · airframe 56,807 hrs · 44,604 cycles

EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW MM 33-53-02-4.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,517 hrs · 44,458 cycles

DURING INSPECTION OF FUSELAGE SKIN AT LONGERON 22, FOUND SKIN CRACKED AT LOWER AFT CORNER OF AIR STAIR DOOR, STA 200. REPAIRED CRACK IAW ABX EA 5300001-003-2.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 53,513 hrs · 43,076 cycles

RIGHT CUSP WEB CRACKED AT EXISTING REPAIR, STA 1021 - 1041, RIGHT BUTT LINE 50. REMOVED AND REPLACED CUSP AT STA 1021 - 1041 IAW DC-9 SRM 53-03 AND 51-30-4.

Part: ATTACH ANGLE — CRACKED (RT PYLON) · airframe 53,513 hrs · 43,076 cycles

UPPER PYLON ATTACH ANGLE CRACKED AT FORWARD END. REPAIRED AREA IAW DC-9 SRM 54-04.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 53,513 hrs · 43,076 cycles

FORWARD UPPER STOP TEE FITTING CRACKED FORWARD LOWER CARGO DOOR. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-5.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 53,513 hrs · 43,076 cycles

AFT PRESSURE BULKHEAD RIGHT SIDE DOOR JAMB STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 53,513 hrs · 43,076 cycles

FLOOR SUPPORT AT STA 1072 WAS CORRODED TOP AND BOTTOM SIDE LONGERON 28 LEFT - LONGERON 28 RIGHT. REMOVED AND REPLACED FLOOR SUPPORT SECTIONS IAW DC-9 SRM 51-30-2, 51-30-5, AND SSRM DRAWING K05159.

Part: ENGINE — DEFECTIVE (LEFT) · airframe 52,424 hrs · 42,543 cycles

LEFT ENGINE LOW OIL QUANTITY 0, LOW OIL PRESSURE 35 PSI, OIL PRESSURE LIGHT ON, SHUT DOWN LEFT ENGINE. FROM PDX, MADE DIVERSION TO YAK. REMOVED AND REPLACED LEFT ENGINE IAW DC-9 JOB CARD 9090010 ON WP 600204098. OPS CHECKED GOOD IAW DC-9 MM.

Part: LIGHT — SHORTED (COCKPIT) · airframe 51,338 hrs · 42,032 cycles

ODOR OF WIRES BURNING FOLLOWED BY MAP AND BRIEFCASE CIRCUIT BREAKER TRIPPED, AND LOSS OF THOSE LIGHTS. ODOR WENT AWAY. CAPTAIN'S MAP LIGHT LENS ASSEMBLY SHORTED ON MOUNTING PLATE. REPOSITIONED AND SECURED LENS ASSEMBLY. OPS CHECKED GOOD IAW DC-9 MM.

Part: CHANNEL — CRACKED (LT MLG DOOR) · airframe 51,014 hrs · 41,882 cycles

LEFT MAIN LANDING GEAR INBOARD DOOR CRACKED AT FORWARD HINGE. REPLACED PAN SECTION AND REPAIRED AREA, REINSTALLED DOOR IAW DC-9 MM 32-12-01-2 AND SRM 52-05, 53-05, AND 51-30-1.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 51,014 hrs · 41,882 cycles

AFT LOWER CARGO DOOR BEAM NR 2 END FITTING CRACKED ON AFT SIDE. REPLACED AFT LOWER CARGO DOOR BEAM NR 2 END FITTING IAW DC-9 SRM 51-30-5.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 51,014 hrs · 41,822 cycles

SHEAR TIE CRACKED, FS 1021 AT LONGERON 14 RIGHT. REPLACED SECTION OF SHEAR TIE IAW DC-9 SRM.

Part: PIVOT ASSY — LACK OF LUBE (RT MLG) · airframe 50,965 hrs · 41,820 cycles

RIGHT MAIN LANDING GEAR CAME OUT ON UPLATCH CHECK. RECYCLED LANDING GEAR AND RECEIVED NORMAL INDICATION. FOUND UPLOCK PIVOT BOLT BOUND UP TO HOOK AND STRUCTURE IMPEDING MOVEMENT OF HOOK. PULLED, CLEANED AND LUBRICATED PIVOT BOLT AND BOSS. INSTALLED REMOTE HYDRAULIC PUMP TO UPLATCH ACTUATOR AND VERIFIED OPS OF ACTUATOR. PERFORMED GEAR SWING AND LEAK CHECK OF LINES. OPS CHECKED GOOD.

Part: UPLOCK SWITCH — FAILED (RT MLG) · airframe 50,900 hrs · 41,800 cycles

RT GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. LIGHT WENT OUT AFTER GEAR WAS RECYCLED. ALL INDICATIONS WERE NORMAL. REPLACED RIGHT GEAR UPLOCK SWITCH IAW MM 32-60-01-2. ALSO FOUND CANNON PLUG P1-1150 VERY CORRODED, REPLACED PLUG. OPS CHECKED GOOD.

Part: PIN — BENT (LANDING GEAR) · airframe 50,875 hrs · 41,792 cycles

AFTER TAKEOFF, RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER INITIAL RETRACTION. THERE WAS NO ASSOCIATED YAW OR NOISE. AFTER RECYCLING GEAR, ALL INDICATIONS WERE NROMAL. FOUND PIN A BENT ON R5-1150. STRAIGHTENED PIN. OPS CHECKED GOOD IAW DC-9 AMM 32-60-00.

Part: DRAIN — FROZEN (SPOILERS) · airframe 50,288 hrs · 41,513 cycles

DEPLOYING SPOILERS CREATED A LT ROLL OF 5 DEGREES PER SECOND. AILERONS BINDED DURING APPROACH, AILERONS HEAVY DURING APPROACH. FOUND SLAT PANEL DRAINS BLOCKED BY ICE, WATER LEAKED OUT OF SLANT PANEL AND DOWN ONTO AILERON AND SPOILER CABLES, FREEZING THEM UP. THAWED ALL AND CHECKED. OPS CHECKED GOOD IAW DC-9 MM CHAPTER 27.

Part: PANEL — CORRODED (RT. WHEEL WELL) · airframe 48,695 hrs · 40,658 cycles

RIGHT SLANT PANEL HAD CORROSION AROUND NUT PLATES, LOWER EDGE FROM INBOARD TO OUTBOARD. REPLACED SLANT PANEL IAW DC-9 SRM 51-30-2, 51-10-4, 51-30-1 AND 51-20-6.

Part: ANGLE — CRACKED (LT. WHEEL WELL) · airframe 48,695 hrs · 40,658 cycles

LEFT WHEEL WELL ATTACH ANGLE CRACKED IN RADIUS, JUST OUTBOARD OF THE TRAP PANEL, ABOVE THE HYDRAULIC SERVICE ACCESS. REPLACED ANGLE IAW DC-9 SRM.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 48,695 hrs · 40,658 cycles

LEFT WHEEL WELL OUTBOARD SLANT PANEL ATTACH ANGLE EXFOLIATED AT LOWER FASTENER. LOCATED AND DRILLED SLANT PANEL ATTACH ANGLE IAW DC-9 SRM 51-30-5.

Part: PANEL — CORRODED (LT. WHEEL WELL) · airframe 48,695 hrs · 40,658 cycles

LEFT SLANT PANEL CORRODED AROUND NUTPLATES. REPLACED SLANT PANEL IAW DC-9 SRM 51-30-1.

Part: RELAY — MALFUNCTIONED (HORIZ STAB) · airframe 48,490 hrs · 40,584 cycles

DURING DESCENT, ALTERNATE LONGITUDINAL TRIM RAN AWAY. AUTOPILOT AND ALTERNATE TRIM CIRCUIT BREAKERS PULLED. COULD NOT DUPLICATE ON GROUND. REPLACED ALTERNATE TRIM BRAKE RELAY R20-14 AND UP AND DOWN RELAYS R20-12 AND R20-13 AS A PRECAUTION. OPS CHECKED GOOD IAW DC-9 MM 27-40-00-2.

Part: LOCK — DISCONNECTED (COCKPIT) · airframe 47,689 hrs · 40,251 cycles

THE PILOTS CLEARVIEW WINDOW AFT LOCK WAS DISCONNECTED. MAINTENANCE INSPECTED AND RECONNECTED THE AFT LOCK AS REQUIRED.

Part: BATTERY PACK — DIRTY (CABIN) · airframe 47,249 hrs · 40,041 cycles

EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE INSPECTED AND CLEANED EMERGENCY LIGHT BATTERY PACK AT FSD AND RETURNED THE A/C TO SERVICE. UPON ARRIVAL AT ILN, MAINTENANCE REPLACED EMERGENCY LIGHT PACK AS A RELIABILITY PRECAUTION IAW DC9 MM 33-02-4.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,070 hrs · 39,947 cycles

EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHTS POWER SUPPLY BATTERIES IAW DC-9 MM 33-53-02-4-0001.

Part: WHEEL — JAMMED (CABIN PRESSURE) · airframe 46,471 hrs · 39,682 cycles

TOP OF DESCENT UPON SETTING LANDING ELEVATION, CABIN CLIMB INDICATOR SHOWED 1500 FPM CLIMB, WENT ON OXYGEN, WENT TO MANUAL. COULD NOT CONTROL. PRESSURIZATION WHEEL JAMMED. OPS CHECKED AUTO AND MANUAL PRESSURIZATION. AIRCRAFT PRESSURIZED TO 7.5 PSI. NO LEAKS NOTED. SYSTEM OPS CHECKED GOOD IAW DC9 MM CHAPTER 21.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,483 hrs · 39,204 cycles

CENTER KEEL FUSELAGE SKIN EXTERIOR BETWEEN MAIN LANDING GEAR INBOARD WHEEL WELL DOORS CORRODED. REPLACED SKIN IAW DC9 SRM 51-30-2.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,483 hrs · 39,204 cycles

FUSELAGE SKIN CORRODED UNDER LEFT STATIC PORT PLATE. REPAIRED SKIN IAW DC9 SRM 53-04.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 45,484 hrs · 39,204 cycles

ATTACH ANGLE CRACKED INSIDE AFT PRESSURE DOME DOOR AT UPPER DOOR HINGE. REPLACED ANGLE (P/N 9915565-157) IAW DC9 SRM 51-30-2.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 45,484 hrs · 39,204 cycles

RIGHT DORSAL FIN ATTACH ANGLE CRACKED FORWARD OF AFT END OF ANGLE, 12 INCHES LONG. REPAIRED ANGLE IAW DC9 SRM 53-05, FIGURE 23.

Part: PAN — CRACKED (E/E BAY DOOR) · airframe 45,484 hrs · 39,204 cycles

ELECTRONIC COMPARTMENT DOOR PAN IS CRACKED AT ALL FOUR CORNERS. REPLACED ELECTRONIC COMPARTMENT DOOR.

Part: ATTACH FITTING — CRACKED (CARGO BAY) · airframe 45,484 hrs · 39,204 cycles

AFT ENTRY DOOR LEFT LOWER STOP FITTING CRACKED AT FORWARD ATTACH POINT, 19 INCHES ABOVE FLOOR LEVEL. REPLACED FITTING IAW DC9 SRM 51-30-2.

Part: PANEL — DELAMINATED (LT WING) · airframe 45,484 hrs · 39,204 cycles

TRAILING EDGE PANEL FORWARD OF OUTBOARD END OF LEFT AILERON DELAMINATED. REPLACED TRAILING EDGE PANEL IAW DC9 SRM 51-30-1.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 45,484 hrs · 39,204 cycles

FORWARD LOWER CARGO DOOR EXTERIOR SKIN CRACKED AT CENTER BEAM FORWARD ATTACH FITTING. REPAIRED IAW ABX REA D952-36797.

Part: HINGE — CRACKED (RT MLG DOOR) · airframe 45,484 hrs · 39,204 cycles

RIGHT MAIN LANDING GEAR DOOR HINGE CRACKED AT LOBE. REPLACED HINGE IAW DC9 SRM 51-30-1.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 45,484 hrs · 39,204 cycles

FORWARD LOWER CARGO COMPARTMENT DOOR INTERCOSTAL WEB CRACKED AT UPPER AFT DOOR STOP. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 45,484 hrs · 39,204 cycles

RIGHT FLOORBEAM TO KEEL ATTACH FITTING AT STATION 737 CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,484 hrs · 39,204 cycles

FUSELAGE SKIN CRACKED AT STATION 1152 AND LONGERON 14 LEFT. REPAIRED SKIN IAW DC9SRM 53-04.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,484 hrs · 39,204 cycles

RIGHT CUSP WEB CRACKED AT STATION 1041. REPAIRED IAW DC9 SRM 53-01.

Part: ANGLE — CRACKED (SERVICE DOOR) · airframe 45,484 hrs · 39,204 cycles

FORWARD SERVICE DOOR ATTACH ANGLE CRACKED INSIDE LIGHTENING HOLE, FORWARD UPPER CORNER OF DOOR AT UPPER BEAM TO DOOR PAN. REPLACED ANGLE IAW DC9 SRM 51-30-5.

Part: WEB — CRACKED (FUSELAGE) · airframe 45,484 hrs · 39,204 cycles

FORWARD SUB FLOOR CRACKED AT STATION 203 AND RBL 22. REPAIRED SUB FLOOR IAW DC9 SRM53-0.

Part: ATTACH FITTING — CRACKED (CARGO BAY) · airframe 45,484 hrs · 39,204 cycles

SEAT TRACK ATTACH FITTING CRACKED AT STA 370. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: FITTING — CRACKED (CARGO BAY) · airframe 45,484 hrs · 39,204 cycles

AFT ENTRY DOOR FRAME LEFT SIDE STOP FITTING CRACKED AT FORWARD END, 36 INCHES ABOVE FLOOR LEVEL. REPLACED FITTING IAW DC9 SRM 51-30-2.

Part: MECHANISM — LACK OF LUBE (LACK OF LUBE)

COULD NOT RETRACT GEAR AFTER TAKEOFF. OVER RODE GEAR HANDLE RELEASE AND PUT HANDLE IN UP POSITION. AUTO PRESSURE WAS INOPERATIVE, AUTO SPOILER 'DO NOT USE' LIGHT WAS ILLUMINATED. FOLLOWED ABNORMAL PROCEDURES. LUBRICATED GROUND SHIFT MECHANICAL SECTOR.

Part: WEB — CRACKED (BS 1013)

DURING C-CHECK, FOUND CUSP WEB CRACKED AT STATION 1013 RIGHT. REPLACED SECTION OF CUSP WEB IAW DC9 SRM 53-01.

Part: WEB — CRACKED (BS 1036)

DURING C-CHECK, FOUND CUSP WEB STATION 1036 LEFT CRACKED. REPAIRED CUSP WEB IAW ABX REA D953-25107MR.

Part: ANGLE — CRACKED (AFT FUEL TANK)

DURING C-CHECK, FOUND ANGLE IN AFT FUEL TANK CRACKED. REPAIRED IAW ABX REA D953-25121MR.

Part: PAN — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR PAN CRACKED. REPLACED CARGO DOOR.

Part: FITTING — CRACKED (RT MLG DOOR)

DURING C-CHECK, FOUND RIGHT MAIN LANDING GEAR DOOR ACTUATOR ATTACH FITTING CRACKED. REPLACED RIGHT MAIN LANDING GEAR DOOR.

Part: PANEL — CRACKED (RT WING)

DURING C-CHECK, FOUND RIGHT WING PANEL NR 1220 CRACKED. REPAIRED PANEL IAW DC9 SRM 57-06.

Part: VANE — DELAMINATED (RT TE FLAP)

DURING C-CHECK, FOUND THE RW MOVEABLE VANE DELAMINATED UNDER THE CHAFE STRIP. *S/D* REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.

Part: JAMB — CORRODED (BS 965-973)

DURING C-CHECK, FOUND THE DOOR JAMB WEB AT F/STA 965 TO 973 LONG 26R TO 27R CORRODED. REPAIRED IAW SBX DC9 SRM DWG K05485-7005.

Part: SEAT TRACK — CORRODED (BS 294-484)

DURING C-CHECK, FOUND THE SEAT TRACK AT F/STA 294 TO 484 BL 0 CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW DC9 SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: WEB — CRACKED (BS 1039)

DURING C-CHECK, FOUND THE RT CUSP WEB AT F/STA 1039 RBL 46 CRACKED. REPAIRED CUSP WEB IAW DC9 SRM 53-01, FIGURE 2 AND 51-30-1.

Part: SPLICE PLATE — CORRODED (BS 973)

DURING C-CHECK, FOUND THE FUSELAGE FRAME SPLICE PLATE F/STA 973, LONG 27L TO 29L CORRODED. REPLACED SPLICE PLATE IAW DC9 SRM 51-30-2 AND 51-10-3.

Part: PANEL — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND THE INTERIOR FUSELAGE FLANGE FOR THE LEFT KIDNEY PANEL NR 5115 CORRODED AROUND AND UNDER SEVERAL NUT PLATES. REPAIRED IAW ABX REA D953-19588.

Part: TORSION BAR — CORRODED (LT SPOILER)

DURING C-CHECK, FOUND LW INBD SPOILER TORSION BAR AT CAM ASSY IS CORRODED. REMOVED AND REPLACED INBD SPOILER TORSION BAR, CAM AND REACTION ARM IAW DC9 TEMP REV 27-61-6 AND 27-453.

Part: FLOORBEAM — CRACKED (BS 237)

DURING C-CHECK, FOUND FLOORBEAM CRACKED AT F/STA 237, BL 0. REPAIRED IAW ABX REA D953-19459-MR.

Part: TORSION BAR — CORRODED (RT SPOILER)

DURING C-CHECK, FOUND RW INBD SPOILER TORSION BAR AT CAM ASSY IS CORRODED. REMOVED AND REPLACED INBD SPOILER TORSION BAR, CAM AND REACTION ARM IAW DC9 MM 27-61-6.

Part: INTERCOSTAL — CRACKED (BS 851)

DURING C-CHECK, FOUND CRACKED INTERCOSTAL AT F/STA 851 AND RBL 02. REPAIRED IAW DC9 ABX SUPPLEMENTAL SRM DWG NR K05159.

Part: CUSP WEB — CRACKED (BS 1023)

DURING C-CHECK, FOUND CUSP WEB AT STA 1023 AND LBL 56 CRACKED. REPAIRED CUSP WEB IAW DC9 SRM 53-01.

Part: SKIN — CORRODED (FWD FUSELAGE)

DURING C-CHECK, FOUND SKIN BULGED AT NOSE LANDING GEAR DOOR AFT HINGE. REPAIRED IAW DC9 SRM 53-04.

Part: SKIN — CORRODED (BS 619)

DURING C-CHECK, FOUND FUSELAGE SKIN AT F/STA 619 AND LONGERON 30 BULGED AND CORRODED. REPAIRED IAW DC9 SRM 53-04.

Part: SKIN — CRACKED (BS 110)

DURING C-CHECK, FOUND SKIN CRACKED AT LONGERONS 27 AND 28 LT AT F/STA 110. REPAIRED CRACKED SKIN IAW DC9 SRM 53-04.

Part: LONGERON — CORRODED (BS 992)

DURING C-CHECK, FOUND LONGERON 23L AT STA 992 IS HEAVILY CORRODED. REMOVED AND REPLACED LONGERON IAW DC9 SRM 51-30-2.

Part: FITTING — CRACKED (BS 718)

DURING C-CHECK, FOUND VERTICAL FLOOR SUPPORT FITTING CRACKED AT F/STA 718 RBL 44. REPLACED FITTING (P/N 3925812-2) IAW DC9 MM 51-30-2.

Part: SPAR CAP — CRACKED (LT HORIZ STAB)

DURING C-CHECK, FOUND LT HORIZONTAL STABILIZER UPPER REAR SPAR CAP CRACKED AT OUTBOARD END. REPAIRED SPAR CAP IAW DC9 SRM 55-02.

Part: INTERCOSTAL — CRACKED (BS 351-370)

DURING C-CHECK, FOUND INTERCOSTAL AT LONG 29L F/STA 351 TO 370 CRACKED. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2.

Part: VALVE — DEFECTIVE (CABIN)

AIRCRAFT LOST ALL CABIN PRESSURE FROM FL 350, COULD NOT CONTROL MANUALLY OR AUTOMATICALLY. FOUND FORWARD PRESSURIZATION VALVE OPENING AT 7.6 PSI. REPLACED FORWARD SAFETY VALVE IAW DC-9 MM AND OPS CHECKED GOOD.

Part: VANE — DELAMINATED (LT FLAP)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND LEFT FLAP FORWARD MOVEABLE VANE DELAMINATED. REPLACED VANE IAW DC-9 SUPP MM 27-51-2.

Part: SKIN — CRACKED (RT FLAP)

DURING C-CHECK INSPECTION, FOUND A CRACK IN THE RIGHT FLAP UPPER SKIN. REPAIRED IAW ABX REA D957-13446-MR.

Part: SPAR CAP — CORRODED (WS 566)

DURING C-CHECK INSPECTION, FOUND RIGHT WING REAR SPAR UPPER CAP CORRODED AT XRS 566 TO 568. REPAIRED IAW ABX REA D957-13436-MR.

Part: SKIN — DEFECTIVE (BS 540)

DURING C-CHECK INSPECTION, FOUND OIL CANNING ON EXTERIOR SKIN AT STA 540, BETWEEN LONGERONS 21R AND 22R. REPAIRED IAW ABX REA D953-13477-MR.

Part: FITTING — CRACKED (RT FLAP)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND RIGHT FLAP OUTBOARD HINGE ATTACH FITTING CRACKED. REPLACED ATTACH FITTING IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: FITTING — CRACKED (RT FLAP)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND RIGHT FLAP OUTBOARD HINGE ATTACH FITTING CRACKED. REPLACED ATTACH FITTING IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: SKIN — DAMAGED (AFT PRESS BULK)

WHILE ACCOMPLISHING A.D. 89-06-04, FOUND THE AFT PRESSURE BULKHEAD CHAFED. REPAIRED IAW ABX REA D953-12012-MR.