N905AX

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 56,437 hrs · 45,249 cycles

EMERGENCY LIGHTING INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-02-4.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,931 hrs · 44,111 cycles

EVIDENCE OF CORROSION EMITTING FROM FINGER DOUBLER JUST FORWARD OF FS 332 TO 351, LONGERON 26 RT OUTBOARD AND INBOARD SIDES. REPAIRED CORRODED SKIN IAW DC-9 SRM 53-04.

Part: PANEL — CRACKED (RT WHEEL WELL) · airframe 54,931 hrs · 44,111 cycles

RIGHT BUTT LINE '0' ANGLE FITTING COMMON TO KEEL WEB AND RIGHT SLANT PANEL CRACKED. REPLACED ANGLE IAW DC-9 SRM 51-30-5.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,931 hrs · 44,111 cycles

SKIN BULGING AND RIVET HEAD POPPED AT STA 949, LONGERON 24 LEFT. REPLACED LONGERON 24 LEFT, FS 927-996 IAW DC-9 SRM 51-30-2, 51-30-5 AND 53-02.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 54,931 hrs · 44,111 cycles

SKIN BULGING, RIVETS CUPPED AT STA 342, LONGERON 29 RIGHT AND LONGERON 28 RIGHT. REMOVED FASTENERS, EVALUATED. SPLICED LONGERON IAW DC-9 SRM.

Part: RELAY — FAILED (PRIMARY TRIM) · airframe 54,581 hrs · 43,855 cycles

DURING INITIAL CLIMB, PRIMARY TRIM C/B 0A TRIPPED, ALTERNATE TRIM WORKED FINE. ELECTED TO PULL PRIMARY TRIM C/B'S 0B AND 0C. CONTINUED FLIGHT USING AUTOPILOT. WHEN REMOVING CREW BAGS, NOTICED STRONG ELECTRICAL SMELL (BURNT ODOR) IN BELLY'S 1 AND 2. FOUND UPPER PRIMARY LONG TRIM RELAY BURNT. REMOVED AND REPLACED RELAY IAW DC-9 MM 27-40-04 AND WORK PACK WO 2004905.

Part: WIRE — BROKEN (ICE SENSOR) · airframe 54,309 hrs · 43,654 cycles

IN CLIMB, BOTH MASTER CAUTIONS ILLUMINATED, DIVERTED TO SGF. INSTALLED NEW LEFT THERMAL CONTROL AMPLIFIER, BITE TEST SHOWED PROBLEM IN SENSOR ON CIRCUIT. FOUND WIRES ON LEFT ICE PROTECT TEMP HIGH SENSOR BROKEN, SPLICED WIRES IAW DC-9 MM 20-50-1. OPS CHECKED GOOD.

Part: CHANNEL — DAMAGED (FUSELAGE) · airframe 53,865 hrs · 43,267 cycles

FOUND BOLT PULLED OUT OF C-CHANNEL AT NR 11 9G NET ARM AT STA 207. DAMAGE WAS AT PREVIOUSLY REPAIRED AREA. REPAIRED DAMAGED AREA IAW REA D953-49568MR. REINSTALLED 9G NET ARM IAW DC-9 SRM 51-3-0.

Part: SUPPORT — FAILED (FUSELAGE) · airframe 53,864 hrs · 43,266 cycles

ON POST FLIGHT INSPECTION, MAINTENANCE DISCOVERED 1 9G NET SUPPORT PULLED FROM FUSELAGE MOUNT. REPAIRED DAMAGED AREA IAW REA D953-49569MR. REINSTALLED 9G NET ARM IAW DC-9 SRM 51-3-0.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,341 hrs · 42,808 cycles

COCKPIT SUBFLOOR HAD AREAS OF LEVEL II CORROSION, STA 160 RPL 32 TO 54. REPAIRED AREA IAW DC-9 SRM.

Part: PRESSURE PANEL — CRACKED (LT WHEEL WELL) · airframe 53,341 hrs · 42,808 cycles

PRESSURE PANEL LEFT WHEEL WELL AT FS 718 LEFT BUTT LINE 36 APPROXIMATELY, CRACKED. REPAIRED RPESSURE PANEL IAW REA D953-48107.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,341 hrs · 42,808 cycles

CORROSION BETWEEN LONGERON 26 LT AND SKIN BETWEEN STA. 775 AND 813. REPAIRED AREA IAW DC-9 SRM.

Part: FLOOR SUPPORT — CRACKED (FWD CARGO) · airframe 53,341 hrs · 42,808 cycles

CABIN FLOOR SUPPORT FITTING FS 434 LONGERON 18 LEFT CRACKED AT UPPER HORIZONTAL FLANGE BETWEEN FASTENERS AND HAD LEVEL I CORROSION ON AFT SIDE. REPLACED FITTING AND REPAIRED AREA IAW DC-9 SRM 51-10-3.

Part: FLOOR SUPPORT — CRACKED (FWD CARGO) · airframe 53,341 hrs · 42,808 cycles

LEFT FLOOR SUPPORT STRUT TO FRAME ATTACH BRACKET CRACKED AT STA. 275, BETWEEN LONGERON 24 LEFT AND 25 LEFT. REPLACED LEFT FLOOR SUPPORT STRAP TO FRAME ATTACH BRACKET IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,341 hrs · 42,808 cycles

LEFT FLOOR SUPPORT STRUT TO FRAME ATTACH FITTING CRACKED STA. 237 BETWEEN LONGERON 24 LEFT AND 25 LEFT. REPLACED SUPPORT IAW DC-9 SRM.

Part: SKIN — CORRODED (AFT CARGO) · corrosion level 2 · airframe 53,341 hrs · 42,808 cycles

CORROSION BETWEEN LONGERON 26 RIGHT AND SKIN, BETWEEN STA 794 AND 813. REPAIRED AREA IAW DC-9 SRM 53-04.

Part: FLOOR SUPPORT — CRACKED (FWD CARGO) · airframe 53,341 hrs · 42,808 cycles

RIGHT FLOOR SUPPORT STRUT END FITTING STA 313 CRACKED AT LONGERON 23 RIGHT. REPLACED FLOOR SUPPORT STRUT IAW DC-9 SRM.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,341 hrs · 42,808 cycles

LEVEL II CORROSION BUTT LINE '0' F.S. 180 AT SHACKLE BOX. REPLACED SUBFLOOR DOUBLER WITH NEW FABRICATED DOUBLER AND INSTALLED IAW DC-9 SRM 53-01, 53-10-4, 53-10-3, 51-30-1, AND 51-30-2.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,341 hrs · 42,808 cycles

LEVEL II CORROSION ON SUBFLOOR AT RIGHT BUTT LINE 44 F.S. 180 SHACKLE BOX. REPAIRED AREA IAW DC-9 SRM 53-01.

Part: FITTING — CRACKED (FUSELAGE) · airframe 53,341 hrs · 42,808 cycles

LT FRAME 294 ENG. FITTING CRACKED AT CARGO FLOOR ATTACH POINT. REPLACED FITTING IAW DC-9 SRM 51-10-4, 51-30-5 AND 51-30-1.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,341 hrs · 42,808 cycles

BULGE IN FUSELAGE SKIN, CUPPED OR BROKEN FASTENERS, FS 332, LONGERON 30. REPLACED DAMAGED AREA IAW DC-9 SRM.

Part: PRESSURE PANEL — CORRODED (LT WHEEL WELL) · corrosion level 2 · airframe 53,341 hrs · 42,808 cycles

PRESSURE PANEL DOUBLER WAS BULGING LEFT BUTT LINE 8 TO LEFT BUTT LINE 16, FS 756. REPLACED LOWER T-ANGLE OF FLOORBEAM FS 756, BUTT LINE 56 RIGHT TO BUTT LINE 54 IAW DC-9 SRM 51-30-2, 51-30-5 AND REA D953-48132.

Part: STRUCTURE — CORRODED (LT WHEEL WELL) · corrosion level 2 · airframe 53,341 hrs · 42,808 cycles

LEFT WHEEL WELL STA 712, BUTT LINE 53 RETAINER CORRODED AND RIVETS POPPED. REPLACED RETAINER FROM FS 699 AND 756 LEFT BUTT LINE 30 TO LEFT BUTT LINE 56 IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: STRUCTURE — CORRODED (RT WHEEL WELL) · airframe 53,341 hrs · 42,808 cycles

RIGHT WHEEL WELL UPPER AFT CORNER STA. 756, BUTT LINE '0' - BUTT LINE '4', CORROSION ON KEEL ANGLE AND BULGES UNDER RETAINER. REPAIRED AREA IAW REA D953-48136MR. REMOVED PREVIOUS REPAIR FROM AFT UPPER KEEL ANGLE, REPAIRED IAW DC-9 SRM 53-05.

Part: SPAR — CRACKED (CENTER WING) · airframe 52,198 hrs · 41,897 cycles

LEFT WHEEL WELL, JUST OUTBOARD OF STATION ZERO, CENTER TANK ON REAR SPAR, UPPER INBOARD CORNER, HAD A CRACK. REPAIRED AREA IAW DC-9 SRM 51-30-5 AND 57-09.

Part: SUPPORT — CRACKED (LEFT WING) · airframe 52,198 hrs · 41,897 cycles

VERTICAL SUPPORT FOR SLAT MECHANISM MOUNT HAD A CRACK AT LOWER INBOARD MOUNT BOLT. REPLACED VERTICAL SUPORT IAW DC-9 SRM 51-30-5.

Part: SKIN — CORRODED (FUSELAGE) · airframe 50,728 hrs · 40,826 cycles

FUSELAGE SKIN BUBBLED AT LONGERON 30 BETWEEN STATION 445 AND 465. REPAIRED IAW DC9 SRM 53-04.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 50,728 hrs · 40,826 cycles

LONGERON 29 LEFT CRACKED BELOW SPLICE BETWEEN STATION 408 AND 427. REPLACED LONGERON SECTION.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 50,728 hrs · 40,826 cycles

LONGERON 30 CRACKED BELOW SPLICE BETWEEN STATION 408 AND 427. REPLACED LONGERON 30BETWEEN STATION 408 AND 427.

Part: STRUCTURE — CRACKED (PRESSURE DOME) · airframe 50,728 hrs · 40,826 cycles

CRACK ON PRESSURE DOME RADIAL NR 1. REPLACED RADIAL IAW DC9 SRM 51-30-2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 50,728 hrs · 40,826 cycles

LONGERON 17 RIGHT CRACKED AT STATION 945. REPLACED LONGERON IAW DC9 SRM.

Part: SHEAR TIE — CRACKED (CABIN) · airframe 50,728 hrs · 40,826 cycles

SHEAR TIE CRACKED AT STATION 945 BELOW LONGERON 14 LEFT. REPAIRED SHEAR TIE IAW DC9 SRM.

Part: PANEL — DELAMINATED (RT WING) · airframe 50,728 hrs · 40,826 cycles

RIGHT WING LOWER INBOARD BONDED PANEL HAS 4 INCH DELAMINATION. REPLACED PANEL IAW DC9 SRM51-30-2.

Part: DOOR — DELAMINATED (LT WING) · airframe 50,728 hrs · 40,826 cycles

LEFT BUTE DOOR NR 1502 WAS DELAMINATED. REPLACED BUTE DOOR.

Part: PAN — CORRODED (BS 718)

DURING C-CHECK, FOUND LEFT WHEEL WELL PRESSURE PANEL RETAINER PAN AT STATION 718 CORRODED. REPAIRED IAW ABX REA D953-25980MR.

Part: KEEL BEAM — CRACKED (BS 737)

DURING C-CHECK, FOUND KEEL BEAM CORRODED AND CRACKED IN THE RIGHT WHEEL WELL, AFT UPPER CORNER AT STATION 737. REPAIRED IAW ABX REA D953-25903MR.

Part: BATTERY — DISCHARGED (CABIN)

COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED POWER SUPPLY BATTERIES.

Part: SEAT — LACK OF LUBE (RT COCKPIT)

FIRST OFFICER'S SEAT WAS DIFFICULT TO LOCK IN FULL FORWARD POSITION. SEAT SLID BACK ON INITIATION OF TAKEOFF ROLL. SEAT UNLOCKED ON FINAL APPROACH INTO ILN WITH FIRST OFFICER FLYING AIRCRAFT. LUBRICATED FIRST OFFICER'S SEAT LINKAGE. SEAT OPERATES NORMALLY. LOCKS IN ALL POSITIONS IAW DC 9 MM.

Part: FITTING — CRACKED (BS 937)

DURING C-CHECK, THE FLOORBEAM SUPPORT STRUT FITTING AT STA 937 LONG 24 LT WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM.

Part: VANE — DELAMINATED (LT TE FLAP)

DURING C-CHECK, THE INBOARD FIXED VANE WAS FOUND DELAMINATED. THE VANE WAS REPLACED IAW DC9 MM.

Part: FITTING — CRACKED (CTR FUSELAGE)

DURING C-CHECK, THE FITTING JUST BELOW THE PYLON BULKHEAD LBL 44 AT STA 965 WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM.

Part: SKIN — DELAMINATED (LT SPOILER)

FOUND LEFT WING SPOILER UPPER AND LOWER SKIN DELAMINATED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.

Part: SKIN — DELAMINATED (LT TE FLAP VANE)

LEFT INBOARD FLAP VANE OUTER SKIN 40 PERCENT DELAMINATED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.

Part: HINGE — CORRODED (RT TE FLAP)

DURING C-CHECK, THE CENTER FLAP FORWARD HINGE AND ATTACH STUDS WERE FOUND CORRODED. THE HINGE WAS REPLACED IAW DC9 MM.

Part: HINGE — CORRODED (RT TE FLAP)

DURING C-CHECK, THE INBOARD FLAP FORWARD HINGE AND ATTACH STUDS WERE FOUND CORRODED. THE HINGE WAS REPLACED IAW DC9 MM.

Part: HINGE — CORRODED (LT TE FLAP)

DURING C-CHECK, THE INBOARD FORWARD FLAP HINGE AND ATTACH STUDS WERE FOUND CORRODED. THE HINGE WAS REPLACED IAW DC9 MM.

Part: SUPPORT — CRACKED (BS 945)

DURING C-CHECK, THE FLOOR SUPPORT STRUT AT STA 945 LONG 23 LT WAS FOUND CRACKED. THE SUPPORT WAS REPLACED IAW DC9 SRM.

Part: HINGE — CORRODED (LT TE FLAP)

DURING C-CHECK, THE CENTER FORWARD FLAP HINGE AND ATTACH STUDS WERE FOUND CORRODED. THE HINGE WAS REPLACED IAW DC9 MM.

Part: FRAME — CRACKED (BS 1076)

DURING C-CHECK,THE FRAME AT STA 1076 LONG 20 RT WAS FOUND CRACKED. THE FRAME WAS REPLACED IAW DC9 SRM.

Part: SUPPORT — CRACKED (BS 889)

DURING C-CHECK, THE FLOOR SUPPORT STRUT AT STA 889 LONG 23 LT WAS FOUND CRACKED. THE SUPPORT WAS REPLACED IAW DC9 SRM.

Part: SUPPORT — CRACKED (BS 813)

DURING C-CHECK, THE FLOOR SUPPORT STRUT AT STA 813 LONG 23 RT WAS FOUND CRACKED. THE SUPPORT WAS REPLACED IAW DC9 SRM.

Part: FITTING — CRACKED (LT SPOILER)

DURING C-CHECK, THE INBOARD SPOILER CENTER ATTACH FITTING PLATE WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 MM.

Part: DRIVE LINK — CRACKED (LT SPOILER)

DURING C-CHECK WHILE ACCOMPLISHING AD 90-18-03, THE INBOARD SPOILER DRIVE LINK WAS FOUND CRACKED. THE LINK WAS REPLACED IAW DC9 MM.

Part: BLKHD RECEPTICLE — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK WHILE ACCOMPLISHING AD 79-24-01, THE AFT PRESSURE BULKHEAD DOOR RETAINER RECEPTICLE WAS FOUND CRACKED. THE RECEPTICLE WAS REPLACED IAW DC9 SRM.

Part: DRIVE LINK — CRACKED (RT SPOILER)

DURING C-CHECK WHILE ACCOMPLISHING AD 90-18-03, THE INBOARD SPOILER DRIVE LINK WAS FOUND CRACKED. THE LINK WAS REPLACED IAW DC9 MM.

Part: SUPPORT — CRACKED (BS 851)

DURING C-CHECK, THE FLOOR SUPPORT STRUT AT STA 851 LONG 23 RT WAS FOUND CRACKED. THE SUPPORT WAS REPLACED IAW DC9 SRM.

Part: BRACKET — CORRODED (NR 3 LE SLAT)

DURING C-CHECK, THE NR 3 SLAT TRACK CABLE PULLEY BRACKET WAS FOUND CORRODED. THE BRACKET WAS REPLACED IAW DC9 MM.

Part: SUPPORT — CRACKED (BS 832)

DURING C-CHECK, THE FLOOR SUPPORT STRUT AT STA 832 LONG 23 RT WAS FOUND CRACKED. THE SUPPORT WAS REPLACED IAW DC9 SRM.

Part: INTERCOSTAL — CRACKED (BS 581-869)

DURING C-CHECK, AN INTERCOSTAL AT STA 851 TO 869 LONG 29 RT WAS FOUND CRACKED. THE INTERCOSTAL WAS REPLACED IAW DC9 SRM.

Part: WEB — CORRODED (BS 946-965)

DURING C-CHECK, THE WEB BETWEEN STA 946 AND 965 LBL 22 WAS FOUND CORRODED. THE WEB WAS REPLACED IAW DC9 SRM.

Part: INTERCOSTAL — CRACKED (BS 889-897)

DURING C-CHECK, AN INTERCOSTAL AT STA 889 TO 897 LONG 30 WAS FOUND CRACKED. THE INTERCOSTAL WAS REPLACED IAW DC9 SRM.

Part: INTERCOSTAL — CRACKED (BS 364)

DURING C-CHECK, AN INTERCOSTAL AT STA 364 LONG 29 LT WAS FOUND CRACKED. THE INTERCOSTAL WAS REPLACED IAW DC9 SRM.

Part: ANGLE — CRACKED (WS 385)

DURING C-CHECK, THE WING LEADING EDGE RIB SUPPORT ANGLE WAS FOUND CRACKED AT STA 385. THE ANGLE WAS REPAIRED IAW DC9 SRM.

Part: ANGLE — CRACKED (WS 410/424)

DURING C-CHECK, THE WING LEADING EDGE RIB SUPPORT ANGLE WAS FOUND CRACKED AT STA 410 AND 424. THE ANGLE WAS REPAIRED IAW DC9 SRM.

Part: ANGLE — CRACKED (WS 373)

DURING C-CHECK, THE WING LEADING EDGE RIB SUPPORT ANGLE WAS FOUND CRACKED AT STA 373. THE ANGLE WAS REPAIRED IAW DC9 SRM.

Part: TRAP PANEL — CRACKED (RIGHT)

DURING C-CHECK WHILE ACCOMPLISHING S/B 53-100, THE RT TRAPEZOIDAL PANEL WAS FOUND CRACKED AT THE UPPER FORWARD END. THE PANEL WAS REPAIRED IAW DC9 S/B 53-100.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY BATTERY PACK INTERMITTENT OPERATION. REPLACED EMERGENCY BATTERY PACK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING SERVICE CHECK, IT WAS NOTED EMERGENCY EXIT LIGHTS DO NOT EXTINGUISH WITH SWITCH IN OFF POSITION WHEN AIRCRAFT POWER IS TURNED OFF. REPLACED EMERGENCY LIGHT'S BATTERY POWER SUPPLY IAW DC-9 MM 33-53-0.

Part: RETAINER — CRACKED (BS 128)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03 AND SB 56-11 REV 3, FOUND EVIDENCE OF CRACKS ON TWO FASTENER HOLES ON THE LEFT EYEBROW WINDOW RETAINER, DURING X-RAY INSPECTION. REPLACED RETAINER IAW DC-9 SRM 51-30-2.

Part: SKIN — WORN (LT TE FLAP)

DURING C-CHECK INSPECTION, FOUND LEFT FLAP TOP SIDE SKIN HAD A WORN SPOT AFT OF THE INBOARD END OF THE NR 3 FIXED VANE. REPAIRED IAW ABX REA D957-12653-MR.

Part: FITTING — CORRODED (BS 737)

DURING C-CHECK INSPECTION, FOUND FITTING ON LEFT FUSELAGE SKIN THAT TIES INTO THE MAIN FRAME AND INTO LEFT TRAPEZOID PANEL HAD CORROSION IN THE BOLT HOLE. REPAIRED IAW ABX REA D953-12649-MR.

Part: FAIRING — CRACKED (VERT STAB)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND RIGHT UPPER HORIZONTAL TO VERTICAL STABILIZER FAIRING CRACKED AT FORWARD END. REPAIRED FAIRING IAW DC-9 SRM 55-03 FIG 17.

Part: BLKHD WEB — CRACKED (BS 996)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03, AND SB 53-174 REV 3, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT FOUR HOLES AT THE TEE SPLICE PLATE ABOVE FRP, RIGHT SIDE. REPAIRED IAW DC-9 SB 53-174.

Part: BLKHD WEB — CRACKED (BS 996)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 81-26-03, 90-18-03 AND SB 53-147 REV 7, ASB 53-147 REV 4, FOUND CRACKS ON THE AFT PRESSURE BULKHEAD WEB AT SPLICE ABOVE LONGERON 13R AND 11R. REPAIRED IAW ABX REA D953-12628-SB.

Part: TAB — DENTED (RUDDER)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND SEVERAL SMALL DENTS AND SCRATCHES ON LEFT SIDE OF RUDDER TAB. REPLACED RUDDER TAB IAW DC-9 MM 27-20-2.

Part: RETAINER — CRACKED (BS 128)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03, SB 56-11 REV 3, FOUND CRACKS ON THE EYEBROW WINDOW RETAINER AT FASTENER HOLE ON THE RIGHT SIDE OF AIRCRAFT. REPLACED RETAINER IAW DC-9 SRM 51-30-2 AND 51-30-1.

Part: BLKHD PLATE — GOUGED (BS 996)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03 AND SB 53-174 REV 3, FOUND RIGHT AFT PRESSURE BULKHEAD SPLICE PLATE GOUGED. REPLACED SPLICE PLATE IAW DC-9 SRM 53-11-3 AND 51-30-5.

Part: BLKHD PLATE — GOUGED (BS 996)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03 AND SB 53-174 REV 3, FOUND LEFT AFT PRESSURE BULKHEAD SPLICE PLATE GOUGED. REPLACED SPLICE PLATE IAW DC-9 SRM 53-11-3 AND 51-30-5.

Part: BLKHD PLATE — GOUGED (BS 996)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03 AND SB 53-174 REV 3, FOUND RIGHT AFT PRESSURE BULKHEAD SPLICE PLATE GOUGED. REPLACED SPLICE PLATE IAW DC-9 SRM 53-11-3 AND 51-30-5.

Part: BLKHD PLATE — GOUGED (BS 996)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03 AND SB 53-174 REV 3, FOUND LEFT AFT PRESSURE BULKHEAD SPLICE PLATE GOUGED. REPLACED SPLICE PLATE IAW DC-9 SRM 53-11-3 AND 51-30-5.

Part: BLKHD T-CAP — GOUGED (BS 996)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03 AND SB 53-174 REV 3, FOUND LEFT AFT PRESSURE BULKHEAD T-CAP AFT SIDE GOUGED. BLENDED IAW DC-9 SRM 51-01 FIG 1.

Part: DOOR — DELAMINATED (WS 324)

DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND LEFT WING OUTBOARD BUTE DOOR HAD TWO AREAS OF DELAMINATION. REPLACED BUTE DOOR IAW DC-9 SRM 51-30-1 AND 51-30-2.

Part: STUD — CRACKED (RT TE FLAP HINGE)

DURING COMPLIANCE OF A.D. 79-03-01; S.B. 57-118, FOUND THE RIGHT OUTBOARD FLAP HINGE, INBOARD LOWER ATTACH STUD INDICATED A CRACK BY THE ULTRASONIC INSPECTION. REPLACED STUD IAW DC-9 M.M. 57-40-1.

Part: LOCK — OUT OF ADJUST (CAPT WINDOW)

DURING POST FLIGHT INSPECTION FOUND CAPTAIN'S SLIDING WINDOW HARD TO OPEN. ADJUSTED UPPER LOCK. OPS CHECKED SEVERAL TIMES. OPS CHECKED GOOD IAW DC-9 M.M.

Part: DOOR — DELAMINATED (RT MLG)

DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR DELAMINATED. REPLACED THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR IAW DC-9 MM 32-12-1.

Part: DOOR — DELAMINATED (LT MLG)

DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD ARTICULATING DOOR DELAMINATED. REPLACED OUTBOARD ARTICULATING DOOR IAW DC-9 OVERHAUL MANUAL 32-10-6 AND DC-9 MM 32-12-1.