N942AX

Part: FRAME — CRACKED (CABIN) · airframe 55,449 hrs · 59,131 cycles

AFT LEFT MAIN FRAME, STA 737, REQUIRED REPLACEMENT DUE TO CRACKS. REMOVED AND REPLACED AFT LEFT MAIN FRAME STA 737 IAW JOB CARD EA 53400325-001-4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,449 hrs · 59,131 cycles

FORWARD RIGHT MAIN FRAME, STA 699, REQUIRED REPLACEMENT. CRACKED BEYOND LIMITS OF REPAIR. REMOVED AND REPLACED RIGHT MAIN FRAME, STA 699 IAW JOB CARD EA 53400322-001-4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,449 hrs · 59,131 cycles

FORWARD LEFT MAIN FRAME, STA 699 WAS CRACKED WITHIN REPAIRABLE LIMITS. REPAIRED MAIN FRAME, STA 699 LT IAW DC-9 SERVICE REWORK DRAWING 5933650 AND JOB CARD EA 63400110-001-1.

Part: CHARGER — DEFECTIVE (MASTER) · airframe 54,959 hrs · 58,619 cycles

IN FLIGHT, BATTERY CHARGER WAS CHARGING BATTERY CONTINUALLY AT 20 AMPS, THE BATTERY WAS AT 38 TO 39 VOLTS. REMOVED AND REPLACED BOTH MAIN BATTERIES, BATTERY CHARGER, AND BATTERY SENSOR IAW DC-9 AMM 24-30-01-4-0001 AND 24-30-02-2-001. OPS CHECKED GOOD.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 54,493 hrs · 58,162 cycles

LONGERON 30, DEEPLY PITTED AT FS 756. REPAIRED LONGERON 30 IAW DC-9 SRM 53-02.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,493 hrs · 58,162 cycles

FUSELAGE EXTERIOR SKIN HAD BULGE AT APPROXIMATELY STA 589, LONGERON 18 RIGHT. REPAIRED AREA IAW REA D958-47172MR AND DC-9 SRM 51-10-3.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 54,493 hrs · 58,162 cycles

EVIDENCE OF CORROSION DETECTED AROUND FORWARD LOWER CARGO DOOR JAMB LOWER SET SCREW FITTINGS, BETWEEN SKIN LAYERS. REPAIRED AREA IAW REA D953-47181MR AND DC-9 SRM 53-05.

Part: SPAR CAP — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 54,493 hrs · 58,162 cycles

LEFT HORIZONTAL STABILIZER REAR UPPER SPAR CORRODED JUST INBOARD OF XHS 68. REPAIRED AREA IAW REA D955-47165 AND DC-9 SRM.

Part: FLOORBEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 54,493 hrs · 58,162 cycles

FLOORBEAM WAS EXFOLIATED AT FS 408 DIRECTLY ABOVE FORWARD LOWER CARGO DOOR CUTOUT AND OUTBOARD OF RIGHT BUTT LINE 54. REPAIRED AREA IAW REA D953-47171 AND DC-9 SRM.

Part: SKIN — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 54,493 hrs · 58,162 cycles

BULGE IN FLAP SKIN AND CUPPED HEAD FASTENERS UPPER SURF AT INBOARD EXPANSION JOINT. REPLACED SKIN AND REINSTALLED INBOARD FLAP SECTION IAW DC-9 SRM.

Part: PRESSURE PANEL — CORRODED (RT MLG WW) · corrosion level 2 · airframe 54,493 hrs · 58,162 cycles

ONE SHEARED FASTENER AND SKIN BULGED AT DOUBLER RIGHT WHEEL WELL UPPER PRESSURE PANEL, STA 716, RIGHT BUTT LINE 56. REPAIRED AREA IAW REA D953-47174.

Part: FITTING — CRACKED (FUSELAGE) · airframe 53,518 hrs · 57,179 cycles

A CRACK WAS INDICATED ON THE AFT PRESSURE BULKHEAD TEE FITTING NR 6, L14L. MAINTENANCE INSPECTED AND REPLACED THE TEE FITTING IAW ABX EA 53120037-006.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,518 hrs · 57,179 cycles

FUSELAGE FRAME AT STATION 1076 WAS FOUND TO HAVE THREE CRACKS AT FASTENERS L13L AND L14L. MAINTENANCE INSPECTED AND REPLACED THE AFFECTED SECTION OF THE FRAME FROM LONGERON 10L TO 17L IAW DC-9 SRM 53-03.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,518 hrs · 57,179 cycles

FLOOR SUPPORT AT FUSELAGE STATION 945 WAS FOUND TO BE CORRODED ABOVE LONGERON 30. MAINTENANCE MANUFACTURED AND INSTALLED A SUPPORT SPLICE IAW DRAWING 99577 AND DC-9 SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 53,518 hrs · 57,179 cycles

RADIAL 5A ON AFT PRESSURE BULKHEAD WAS FOUND TO BE CRACKED. REPAIRED THE RADIAL IAW SERVICE BULLETIN 53-166-W.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 53,518 hrs · 57,179 cycles

UPPER OUTBOARD ATTACH ANGLE ON RADIAL 5A, FWD SIDE, WAS FOUND TO BE CRACKED. MAINTENANCE REPLACED THE ATTACH ANGLE IAW ABX EA 53120037-006.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,518 hrs · 57,179 cycles

THE CENTER SEAT TRACK AT STATION 237-275 WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW DC-9 SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,194 hrs · 56,830 cycles

A FIVE INCH CREASE WAS NOTED ON THE FUSELAGE OUTER SKIN, APPROX 24 INCHES AFT AND 24 INCHES BELOW MAIN ENTRY DOOR. MAINTENANCE REPAIRED AREA IAW DC-9 SRM 53-04 FIG 12B.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 53,027 hrs · 56,684 cycles

EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE DURING PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHTING POWER PACK ASSEMBLY, IAW DC-9 MM CHAPTER 33. OPS CHECKED GOOD.

Part: SUPPORT — CRACKED (BS 658)

DURING C-CHECK, FOUND FLOORBEAM SUPPORT CRACKED STATION 658, RBL 22. REPLACED FLOORBEAM SUPPORT IAW DC9 SRM 51-30-2.

Part: FRAME — CRACKED (BS 737)

DURING C-CHECK, FOUND STATION 737 RT MAIN FRAME CRACKED. REPAIRED CRACK IAW REA D95335059 MR.

Part: PAN — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR PAN AND SKIN CRACKED. REPAIRED IAW REA D95235065 AND SRM 52-05 FIGURE 50 SHEET 2.

Part: WIRE — LOOSE (CABIN)

EMERGENCY LIGHTS WERE DIM AND INTERMITTENT. FOUND GROUND WIRE AT EMERGENCY BATTERY PACK LOOSE AND CORRODED. CLEANED AND REINSTALLED GROUND WIRE, OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK.

Part: INTERCOSTAL — CRACKED (E/E COMPT)

DURING C-CHECK, FOUND INTERCOSTAL CRACKED AT STATION 180 TO 200 LONGERON 30. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: ANGLE — CRACKED (RT MLG WW)

DURING C-CHECK, FOUND FORWARD LOWER INBOARD CORNER ATTACH ANGLE CRACKED AT EDGE OF RIGHT WHEEL WELL STRUCTURE. REPLACED ANGLE IAW DC9 SRM 51-30-1.

Part: SUB FLOOR — CRACKED (BS 205)

DURING C-CHECK, FOUND SUB FLOOR CRACKED AT STATION 205 AND LBL 22 AND STATION 200 AT BL 0. REPAIRED SUB FLOOR IAW DC9 SRM 53-01.

Part: FRAME — CORRODED (BS 446)

DURING C-CHECK, FOUND FRAME AT STATION 446 AND LONGERON 28L TO 29R CORRODED. REPAIRED FRAME IAW DC9 SRM 53-03.

Part: BULKHEAD ANGLE — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD, FORWARD RIGHT SIDE 3RD STIFFENER ATTACH ANGLE CRACKED. REPAIRED ANGLE IAW DC9 SB 53-166 AND CACO DWG 941558.

Part: WEB — CRACKED (BS 260)

DURING C-CHECK, FOUND CUSP WEB STATION 260 RIGHT SIDE CRACKED. REPAIRED CUSP WEB IAW ABX REA D953-23794-MR AND REA 953-23777MR.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS WILL NOT SHUT OFF. REPLACED EMERGENCY LIGHTS POWER SUPPLY, OPS CHECKED GOOD IAW DC-9 MM.

Part: SEAT — DEFECTIVE (LT COCKPIT)

CAPTAIN'S SEAT SLIPS DOWN DURING TAKEOFF. REPLACED CAPTAIN'S SEAT IAW DC-9 MM.

Part: SKIN — GOUGED (BS 427-475)

DURING C-CHECK, FOUND SKIN GOUGED AFT OF FLC DOOR. REPAIRED IAW ABX REA D953-16631-MR.

Part: FRAME — CORRODED (BS 1089)

DURING C-CHECK, CANTED FRAME WEB AT FS 1089 CORRODED. REPAIRED IAW ABX REA D953-16618-MR.

Part: SKIN — GOUGED (BS 110-229)

DURING C-CHECK, FOUND FUSELAGE SKIN GOUGED FROM STATION 208 TO 223, BETWEEN LONGERON 24R TO 25R. REPAIRED IAW ABX REA D953-16659-MR.

Part: FITTING — CRACKED (RT SPOILER)

DURING C-CHECK, FOUND RIGHT WING INBOARD SPOILER TORQUE TUBE CENTER SUPPORT FITTING CRACKED. REPLACED IAW DC-9 SRM 51-30-1, 51-30-2, 51-30-5.

Part: SKIN — DENTED (BS 334)

DURING C-CHECK, FOUND 2 DENTS IN FUSELAGE SKIN AND WINDOW BELT DOUBLER AT FS 334. REPAIRED IAW ABX REA D953-16639-MR.

Part: INTERCOSTAL — CRACKED (BS 699-718)

DURING C-CHECK AND COMPLIANCE WITH AD 88-24-08, FOUND CRACKED INTERCOSTAL BETWEEN FRAMES 699 TO 718 AT LONGERON 6L. FABRICATED NEW INTERCOSTAL IAW DC-9 DWG 9958242-3, INSTALLED IAW DC-9 SRM 51-30-2.

Part: DOOR — CRACKED (LT MLG)

DURING C-CHECK AND COMPLIANCE WITH AD 88-24-08, FOUND LEFT MLG INBOARD DOOR CRACKED AT FORWARD UPPER CORNER. REPLACED DOOR IAW DC-9 SUPPLEMENTAL M/M 32-12-01.

Part: SKIN — TORN (BS 200)

DURING C-CHECK FOUND ENTRY DOOR AFT JAMB INNER SKIN TORN AT FS 200. REPAIRED IAW ABX REA D953-16621-MR.

Part: LATCH CUP — CRACKED (PAX DOOR)

DURING C-CHECK, FOUND ENTRY DOOR HOLD OPEN LATCH CUP CRACKED. REPAIRED IAW ABX REA D952-16507.

Part: WEB — CRACKED (BS 237-317)

DURING C-CHECK, FOUND CUSP WEB BETWEEN FS 237 TO 317 CRACKED AND CORRODED. REPAIRED IAW ABX REA D953-16630-MR.

Part: BULKHEAD WEB — GOUGED (BS 996)

DURING C-CHECK, FOUND GOUGES ON APB WEB AT LONGERON 28L AT TEE CAP. REPAIRED IAW ABX REA D953-16658-MR.

Part: SEAT TRACK — CRACKED (BS 690)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND SEAT TRACK CRACKED AT RBL 22 AT STA 690. REPAIRED IAW ABX EA NR FS-53-04023-MA.

Part: SEAT TRACK — WORN (BS 220-275)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND RBL 22 SEAT TRACK WORN STA 220, 275. REPAIRED IAW ABX EA NR FS-53-04023-MA.

Part: SHEAR TIE — CRACKED (BS 945)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND SHEAR TIE CRACKED AT FS 945. INSTALLED NEW SHEAR TIE IAW DC-9 SRM 51-30-2.

Part: SPAR CAP — CRACKED (RT HORIZ STAB)

DURING C-CHECK FOUND RIGHT HORIZONTAL STABILIZER FRONT SPAR LOWER CAP CRACKED, AT XFS 180. REPAIRED IAW ABX REA D955-15489-MR.

Part: RIB — CRACKED (VERTICAL STAB)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, SECOND FROM BOTTOM LEFT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.

Part: RIB — CRACKED (VERTICAL STAB)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, LOWER LEFT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.

Part: RIB — CRACKED (VERTICAL STAB)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, SECOND FROM BOTTOM RIGHT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.

Part: RIB — CRACKED (VERTICAL STAB)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, LOWER RIGHT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.

Part: RIB — CRACKED (VERTICAL STAB)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, CANTED RIB RIGHT SIDE. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.

Part: RIB — CRACKED (VERTICAL STAB)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, FOURTH FROM BOTTOM RIGHT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.

Part: RIB — CRACKED (VERTICAL STAB)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, FIFTH FROM BOTTOM RIGHT. \N\N\N\N\N REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.

Part: RIB — CRACKED (VERTICAL STAB)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, UPPER RIGHT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.

Part: RIB — CRACKED (VERTICAL STAB)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED, SEVENTH FROM BOTTOM LEFT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.

Part: LONGERON — CRACKED (BS 756)

DURING C-CHECK AND COMPLIANCE WITH AD 88-24-08, FOUND LONGERON 5R CRACKED AT FRAME 756. REPAIRED IAW DC-9 SRM 53-02, FIGURE 2.

Part: RIB — CRACKED (VERTICAL STAB)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED, FOURTH FROM BOTTOM LEFT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.

Part: SEAT TRACK — WORN (BS 313-522)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND SEAT TRACK WORN AT STA 313 TO STA 522, RBL 22. BLENDED IAW DC-9 SRM 53-05, AG 4B.

Part: LONGERON — CRACKED (BS 756)

DURING C-CHECK AND COMPLIANCE WITH AD 88-24-08, FOUND LONGERON 4L CRACKED AT FRAME 756. REPAIRED IAW DC-9 SRM 53-02, FIGURE 2.

Part: SEAT TRACK — WORN (BS 605-630)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND SEAT TRACK BL 0 WORN FROM STA 605 TO 630. BLENDED IAW DC-9 SRM 53-05, FIGURE 4B.

Part: RIB — CRACKED (VERTICAL STAB)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED, SEVENTH FROM BOTTOM RIGHT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.

Part: RIB — CRACKED (VERTICAL STAB)

DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED, EIGHTH FROM BOTTOM LEFT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.

Part: LONGERON — CRACKED (BS 718)

DURING C-CHECK AND COMPLIANCE WITH AD 88-24-08, FOUND LONGERON 5L CRACKED AT FRAME 718. REPAIRED IAW DC-9 SRM 53-02, FIGURE 2.

Part: PRESSURE PANEL — CRACKED (NLG WW)

DURING C-CHECK, FOUND PRESSURE PANEL CRACKED IN LEFT TUNNEL AREA OF NOSE WHEEL WELL. REPAIRED IAW DC-9 S/B 53-187.

Part: CLAMP — LOOSE (RT PACK)

PRESSURIZATION FLOW LIGHT CAME ON AT FL 350 AND CABIN ALTITUDE ROSE TO 12,000 FT. CREW DONNED OXYGEN MASKS. SELECTED STANDBY, FLOW LIGHT WENT OUT THEN CAME BACK ON. OUTFLOW VALVE FULLY CLOSED, FLOW LIGHT WENT OUT AT APPROXIMATELY 12,000 FT. SECURED LOOSE CLAMP ON THE RIGHT PACK DUCT OUTLET.

Part: LINK — WORN (RT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR LINK ATTACHING POINT AT THE DOOR HAD EXCESSIVE SIDE TO SIDE PLAY. REPLACED LINK ON RIGHT MAIN LANDING GEAR OUTBOARD DOOR IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: LINK — WORN (RT MLG DOOR)

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

Part: SENSOR — DEFECTIVE (NLG)

AFTER TAKEOFF, DURING UPLATCH CHECK, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. CYCLED GEAR. NOSE GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH. REPLACED NOSE DOWNLOCK SENSOR IAW DC-9 SUPP. M.M. 32-60-1. OPS CHECKED GOOD.

Part: CONTROL VALVE — DEFECTIVE (LANDING GEAR)

RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED ENTIRE TRIP. DURING UPLATCH CHECK GEAR DOOR OPEN LIGHT ILLUMINATED, GEAR WAS RECYCLED. REPLACED LANDING GEAR CONTROL VALVE IAW DC-9 MM 32-32-1 PAGES 201 TO 205. SYSTEM OPS CHECKED GOOD IAW DC-9 MM 32-32-0 PAGES 201 TO 203.

Part: CONNECTOR — DIRTY (RT MLG)

AFTER TAKEOFF AT LBB, RIGHT RED GEAR UNSAFE LIGHT ILLUMINATED WHEN GEAR WAS RETRACTED. RECYCLED GEAR, NO HELP. FOLLOWED ABNORMAL CHECKLIST WITH GEAR HANDLE UP AND RIGHT HYDRAULIC PUMP ON HIGH, AFTER FIFTEEN MINUTES OF FLIGHT GEAR DOOR OPEN LIGHT CAME ON. AFTER ONE HOUR, GEAR DOOR OPEN LIGHT WENT OUT. RED RIGHT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RIGHT MAIN LANDING GEAR DOWNLOCK PROXIMITY SWITCH CANNON PLUG NOT FULLY SEATED AND DIRTY. RIGHT MAIN GEAR DOOR CANNON PLUG DIRTY. CLEANED CANNON PLUGS AND RETIGHTENED. PERFORMED GEAR SWING, OPS CHECKED GOOD IAW DC-9 SUPP MM 32-60-0. REPLACED PROXIMITY CONTROL BOX. PERFORMED GEAR SWING IAW DC-9 SUPP MM 32-60-0.

Part: DOOR LIGHT — ILLUMINATED (RT MLG DOOR)

UPON GEAR RETRACTION, RED UNSAFE LIGHT FOR RIGHT MAIN ILLUMINATED. DURING UPLATCH CHECK, GEAR DOOR OPEN LIGHT CAME ON ALSO. AFTER PLACING GEAR HANDLE TO UP, RED UNSAFE LIGHT FOR RIGHT MAIN AND GEAR DOOR OPEN LIGHT EXTINGUISHED. CONTINUED FLIGHT WITH RIGHT HYDRAULIC PUMP ON HIGH. CYCLED GEAR AND DOORS IAW DC-9 MM CHAPTER 32-30-0, OPS CHECKED GOOD.

Part: CAP — CORRODED (RT ELEVATOR)

DURING DC-9 ELEVATOR OFF WING INSPECTION, FOUND LEVEL II CORROSION ON THE INBOARD LEADING EDGE CAP OF THE RIGHT ELEVATOR. REPLACED WITH SERVICEABLE CAP IAW DC-9 SRM 27-30.

Part: CHANNEL — CORRODED (STA. 897 - 937)

DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON A FLOOR SUPPORT BETWEEN STA.'S 897 THROUGH 937. REPAIRED IAW ABX REA D953-11215.

Part: CAP — CRACKED (STA YN-174)

DURING C-CHECK INSPECTION, FOUND THE NR 1 ENGINE PYLON CLOSING RIB CAP CRACKED AT STA. YN-174. REPAIRED IAW ABX REA D954-11218-MR.

Part: CUSP — CRACKED (STA. 994)

DURING C-CHECK INSPECTION, THE RIGHT CUSP TEE WAS FOUND CRACKED AT STA. 994. REPAIRED IAW ABX REA D953-11118-MR.

Part: RETAINER — CRACKED (COCKPIT)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING A.D. 90-18-03; S.B. 56-11, REV. 3, FOUND THE RIGHT COCKPIT OVERHEAD WINDOW RETAINER CRACKED. REPAIRED IAW DC-9 SRM 56-01, FIG. 3.

Part: RETAINER — CRACKED (COCKPIT)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING A.D. 90-18-03; S.B. 56-11, REV. 3, FOUND THE LEFT COCKPIT OVERHEAD WINDOW RETAINER CRACKED. REPAIRED IAW DC-9 SRM 56-01, FIG. 3.

Part: SKIN — DENTED (STA. 209)

DURING C-CHECK INSPECTION, FOUND A DENT IN THE FUSELAGE SKIN AT STATION 209 ABOVE LONGERON 18R. REPAIRED IAW ABX REA D953-11134-MR.

Part: SKIN — DENTED (STA. 209)

DURING C-CHECK INSPECTION, FOUND A DENT IN THE FUSELAGE SKIN AT STA. 209 BELOW LONGERON 18R. REPAIRED IAW ABX REA D953-11134-MR.

Part: SUPPORT — DAMAGED (STA. 160 - 200)

DURING C-CHECK INSPECTION, FOUND THE FLOOR PANEL SUPPORT TO HAVE A HOLE WITH SHORT EDGE DISTANCE, A DOUBLE DRILLED HOLE AND TWO HOLES WITH SHORT EDGE DISTANCE BETWEEN THEM, STA. 160 THROUGH 200, RBL 44. REPAIRED IAW ABX REA D953-11137-MR.

Part: CAP — CORRODED (VERT STABILIZER)

DURING C-CHECK INSPECTION, A PREVIOUS REPAIR TO THE LEFT VERTICAL STABILIZER WAS FOUND WITH LEVEL I CORROSION. REMOVAL OF THE REPAIR REVEALED THE REAR SPAR CAP HAD BEEN SPLICED. REPAIRED IAW ABX REA D955-1116-MR.

Part: WEB — CRACKED (STA. 960)

DURING C-CHECK INSPECTION, FOUND A CUSP WEB AT STATION 960, LBL 48 CRACKED. REPAIRED IAW DC-9 SRM 51-30-2.

Part: SPLICE — CRACKED (STA. 955)

DURING C-CHECK INSPECTION, LONGERON 30 SPLICE WAS FOUND CRACKED AT STA. 955. REPLACED SPLICE IAW DC-9 SRM 53-02-147.

Part: WEB — CRACKED (STA. 960)

DURING C-CHECK INSPECTION, FOUND A CUSP WEB AT STATION 960, RBL 48 CRACKED. REPAIRED IAW DC-9 SRM 51-30-2.

Part: FITTING — CRACKED (STA. 965)

DURING C-CHECK INSPECTION, A VERTICAL CABIN FLOOR SUPPORT FITTING WAS FOUND CRACKED AT STA. 965, LBL 34. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1.

Part: LONGERON — CRACKED (STA. 579 - 584)

DURING C-CHECK INSPECTION, LONGERON 29L WAS FOUND TO BE CRACKED BETWEEN STA. 579 AND 584. REPAIRED IAW ABX REA D953-11090-MR.

Part: BUSHING — WORN (RT MLG)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING A.D. 91-22-07; A.S.B. 32-244, THE RIGHT MAIN LANDING GEAR FLYING DOOR WAS FOUND WITH SEVERAL BUSHINGS WORN. REPLACED BUSHINGS IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: DRAIN BOSS — CRACKED (NR 2 ENGINE)

DURING COMPLIANCE OF AD 87-11-07, PRATT AND WHITNEY ASB 5676, FOUND CRACK INDICATION ON FORWARD LOWER COMBUSTION CHAMBER OUTER CASE DRAIN BOSS. REPLACED ENGINE IAW ABX WORKCARD RJT 7001.