N941AX

Part: FITTING — CRACKED (LT TE FLAP) · airframe 58,210 hrs · 62,453 cycles

LEFT FLAP HAD CRACKED FITTING AT SPLICE BETWEEN NR 4 AND 5 REMOVEABLE TRAILING EDGE SEGMENTS. REPLACED 2 EACH NEW FITTINGS IAW DC-9 SRM 51-30-2 AND 51-30-1. P/N: 9955813-509 AND -507.

Part: PANEL — CRACKED (VERTICAL STAB) · airframe 58,210 hrs · 62,453 cycles

LT AND RT ANGLES INSIDE WRAP PANEL FORWARD OF RAM AIR SCOOP WERE CRACKED. REPLACED ANGLES IAW DC-9 SRM 51-30-2 AND 51-30-5. P/N: 5912188-49 AND -50.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 58,210 hrs · 62,453 cycles

LONGERON 30 CRACKED, STA. 588. REPAIRED LONGERON 30 IAW REA D953-49676MR. REPAIRED FRAME AT FS 579 IAW DC-9 SRM 53-03.

Part: DOOR FRAME — CRACKED (BULKHEAD) · airframe 58,210 hrs · 62,453 cycles

AFT PRESSURE BULKHEAD DOOR JAMB LEFT UPPER STOP FITTING CRACKED ON HORIZONTAL LEG. REPLACED FITTING IAW DC-9 SRM 51-30-2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 58,210 hrs · 62,453 cycles

LONGERON 29 LT CRACKED AT STA. 588. REPAIRED LONGERON 29 LT IAW DC-9 SRM 53-02 AND REA D953-49676MR.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 58,210 hrs · 62,453 cycles

ANGLE CRACKED ON FORWARD SIDE OF LEFT FORWARD OVERWING EXIT DOOR JAMB AT FS 617, LONGERON 15 LT. REPLACED ANGLE IAW DC-9 SRM 51-30-2.

Part: SKIN — CORRODED (LT ELEVATOR) · airframe 58,210 hrs · 62,453 cycles

LEFT ELEVATOR LOWER SKIN WAS BULGED AND CORRODED AROUND FASTENERS AND DOUBLER. REPAIRED ELEVATOR IAW DC-9 SRM.

Part: PANEL — CORRODED (LT TE FLAP) · corrosion level 2 · airframe 58,210 hrs · 62,453 cycles

LEFT FLAP LOWER OUTBOARD SURFACE HAD NUMEROUS PLACES WITH SURFACE CORROSION AND EVIDENCE OF INNER CORROSION. SKIN BULGED AROUND RIVET HEADS. REPAIRED TRAILING EDGE SEGMENT IAW DC-9 SRM.

Part: SPACER — WORN (LT MLG) · airframe 57,670 hrs · 61,877 cycles

GEAR DOOR OPEN LIGHT AND LEFT GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF. FOUND LEFT MAIN DOOR LATCH SWITCH ACTUATOR BINDING. REMOVED AND REPLACED SPACER, REINSTALLED SWITCH. PERFORMED GEAR SWING. OPS CHECKED GOOD IAW DC-9 MM 32-10-00.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 57,248 hrs · 61,437 cycles

FORWARD CARGO DOOR AFT HINGE FORWARD ATTACH ANGLE ON HINGE HAD CORROSION. REPLACED ATTACH ANGLE IAW DC-9 SRM.

Part: LONGERON — CRACKED (CABIN) · airframe 57,248 hrs · 61,437 cycles

LONGERON 4 LEFT, CRACKED AT F.S. 200. REPLACED LONGERON IAW DC-9 SRM.

Part: ATTACH ANGLE — CRACKED (LEFT PYLON) · airframe 57,248 hrs · 61,437 cycles

PYLON LOWER ATTACH ANGLE FORWARD END WAS CRACKED. REPAIRED PYLON LOWER ATTACH ANGLE FORWARD END IAW DC-9 SRM 54-04 AND SSRM DWG #K07439.

Part: TERMINAL — DIRTY (BATTERY PACK) · airframe 56,683 hrs · 60,826 cycles

EMERGENCY LIGHTS INOPERATIVE. CLEANED TERMINALS ON BATTERIES IN EMERGENCY BATTERY PACK AS REQUIRED. OPS CHECKED GOOD IAW DC-9 MM.

Part: SWITCH — DEFECTIVE (NG WELL) · airframe 56,589 hrs · 60,724 cycles

A NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE INSPECTED AND ADJUSTED THE NOSE LANDING GEAR DOWN LOCK SENSOR AND REPLACED THE LEFT FORWARD NOSE GEAR DOOR ACTUATOR DUE TO A NONE ADJUSTABLE EYEBOLT. ADJUSTMENT AND TEST PROCEDURES WERE COMPLETED IAW DC-9 MM 32-60-01 AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PAN — CRACKED (FUSELAGE) · airframe 56,263 hrs · 60,380 cycles

FORWARD LOWER CARGO DOOR PAN WAS CRACKED AT THE NR 3, 4 AND 10 DOOR STOPS. MAINTENANCE INSPECTED AND REPLACED THE FORWARD CARGO DOOR IAW DC-9 MM 52-31-00.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,263 hrs · 60,380 cycles

CORROSION WAS FOUND AT FUSELAGE STATION 1121 ON FWD SIDE OF WEB, JUST OUTBOARD AND BELOW PULLY BRACKET. MAINTENANCE INSPECTED AND REPAIRED THE CORRODED AREA IAW ABX REA D953-400600.

Part: SPOILER — CRACKED (RT WING) · corrosion level 2 · airframe 56,263 hrs · 60,380 cycles

THE RIGHT WING OUTBOARD SPOILER HAD A LARGE AREA THAT WAS CORRODED. THE SPOILER WAS ALSO FOUND TO BE CRACKED. MAINTENANCE INSPECTED AND REPLACED THE SPOILER IAW DC-9 MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,263 hrs · 60,380 cycles

WEB AT FS 200 STRINGER 8L WAS CRACKED AND MISSING A SECTION OF MATERIAL. MAINTENANCE INSPECTED AND REPLACED THE WEB.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,263 hrs · 60,380 cycles

FLOORBEAM UPPER ANGLE AT FUSELAGE STATION 996 HAD A 4 INCH CRACK. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW ABX REA D953-40085.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,263 hrs · 60,380 cycles

CORROSION WAS FOUND BENEATH LEFT SIDE OF FUSELAGE STATIC PORT FS 446 AND 465. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-9 SRM 53-04.

Part: LATCH — STUCK (COCKPIT DOOR)

COCKPIT DOOR LATCH WAS STUCK IN LOCKED POSITION. DISASSEMBLED AND REALIGNED THE DOOR LATCH ASSEMBLY.

Part: TAB — DELAMINATED (RUDDER)

DURING C-CHECK, FOUND RUDDER TRIM TAB DELAMINATED. REPLACED RUDDER TRIM TAB IAW DC9 MM 27-20-2.

Part: PANEL — CORRODED (WS 111.5)

DURING C-CHECK, FOUND LEFT WING UPPER TRAILING EDGE PANEL AT STATION XRS 111.500. REPLACED PANEL IAW DC9 SRM 51-30-1 AND 51-10-4.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, FOUND LONGERON 13 RIGHT CRACKED AT STATION 965. REPLACED LONGERON SECTION IAW DC9 SRM 53-02-0.

Part: PAN — CRACKED (SERV DOOR)

DURING C-CHECK, FOUND SERVICE DOOR PAN CRACKED. REPAIRED IAW DC9 SRM 52-03-00 AND 51-30-1.

Part: FRAME — CRACKED (CARGO COMPT)

DURING C-CHECK, FOUND MAIN FRAME CRACKED IN UPPER CARGO COMPARTMENT. REPAIRED IAW DC9 S/B 53-131 AND DWG 5935650-503.

Part: PANEL — DELAMINATED (RT WING)

DURING C-CHECK, FOUND RIGHT WING TRAILING EDGE UPPER HONEYCOMB PANEL DELAMINATED. REPLACED PANEL IAW DC9 SRM 51-30-1.

Part: LATCH — BINDING (COCKPIT)

COCKPIT DOOR LATCHING MECHANISM BINDING AND STICKS IN CLOSED POSITION. DISASSEMBLED, CLEANED, LUBRICATED AND REASSEMBLED LATCH ASSEMBLY. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS WERE EXTREMELY DIM. REPLACED EMERGENCY LIGHT POWER SUPPLY.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS WERE FLICKERING AND VERY DIM. REPLACED EMERGENCY LIGHT BATTERIES.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS WERE DIM. REPLACED EMERGENCY LIGHT BATTERIES.

Part: BATTERY — DISCHARGED (CABIN)

COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED COCKPIT EMERGENCY LIGHT BATTERIES, OPS CHECKED GOOD.

Part: FRAME — CRACKED (BS 965)

DURING C-CHECK, FOUND FRAME AT STA 965 LOWER FLANGE CRACKED AT FASTENER HOLE ABOVE LONGERON 30. REPAIRED FRAME IAW DC9 SRM 53-03.

Part: FRAME — CRACKED (BS 980)

DURING C-CHECK, FOUND FUSELAGE FRAME CRACKED AT STA 980 AND LONGERON 16L. REPLACED FRAME AND SHEAR TIE IAW DC9 SRM 51-30-5 AND 51-30-2.

Part: SKIN — CORRODED (BS 990)

DURING C-CHECK, FOUND CORROSION UNDER THE WATER DEFLECTOR FOR THE APU AT STA 990. REPAIRED SKIN IAW ABX REA D953-21621-MR.

Part: JAMB — CORRODED (BS 370-427)

DURING C-CHECK, FOUND FWD LOWER CARGO COMPARTMENT DOOR JAMB WEB HEAVILY CORRODED IN SEVERAL AREAS ON THE UPPER SURFACE BETWEEN STA 370 AND 427. REPLACED THE DOOR JAMB WEB IAW DC9 SRM 51-30-2.

Part: INTERCOSTAL — CRACKED (BS 917-937)

DURING C-CHECK, FOUND INTERCOSTAL BETWEEN FS 917 TO 937, AND BL 0 CRACKED. REPLACED THE INTERCOSTAL IAW DC9 SRM 51-30-2.

Part: LONGERON — CRACKED (BS 965-980)

DURING C-CHECK, FOUND LONGERON 30 CORRODED AT STA 965 TO 980. REPLACED LONGERON IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (BS 418)

DURING C-CHECK, FOUND LONGERON 30 CRACKED ON BOTH HORIZONTAL LEGS APPROX 5 INCHES LONG AT STA 418. REPLACED LONGERON IAW DC9 SRM 53-02, FIG 14.

Part: BULKHEAD RADIAL — CRACKED (BS 996)

DURING C-CHECK, FOUND AFT PRESS BULKHEAD RADIAL AFT SIDE AT FS 996, LONGERON 25L IS CRACKED IN THE RADIUS. REPAIRED RADIAL IAW DC9 ABX SSRM DRAWING K05159.

Part: BULKHEAD WEB — CORRODED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND CORROSION ON THE AFT PRESSURE BULKHEAD WEB FWD SIDE, LONGERON 23R TO 23L. REPAIRED AFT PRESSURE BULKHEAD WEB IAW DC9 SRM 53-03.

Part: LONGERON — CORRODED (BS 870-919)

DURING C-CHECK, FOUND LONGERON 29L CORRODED BETWEEN STA 870 AND 919. REPAIRED LONGERON IAW DC9 SRM 51-10-3 AND ABX REA D953-21614-MR.

Part: BULKHEAD FITTING — CORRODED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND THE CENTER FITTING AT LONGERON 30 THAT ATTACHES TO THE AFT PRESSURE BULKHEAD T-CAP HEAVILY CORRODED. REPLACED FITTING IAW ABX NEA 53120035-006, ITEM 8.

Part: FLOORBEAM — CRACKED (BS 351)

DURING C-CHECK, FOUND FLOORBEAM CRACKED AT PULLEY BRACKET ATTACH HOLE, STA 351, LBL 6. REPAIRED FLOORBEAM IAW DC9 SRM 53-05.

Part: DOUBLER — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND NR 1 DME ANTENNA INTERNAL DOUBLER EXFOLIATED. FABRICATED INTERNAL DOUBLER (P/N 5911408-39) AND REPAIR DOUBLER (P/N J060258-3) AND INSTALLED IAW DC9 SRM 51-10-3, 51-10-4, AND 51-30-2.

Part: DOUBLER — CORRODED (BS 437)

DURING C-CHECK, FOUND HEAVY CORROSION ON THE INTERNAL DOUBLER FOR NR 2 DME ANTENNA STA 437, BETWEEN LONGERON 30L AND 29L. REPAIRED INTERNAL DOUBLER IAW DC9 SRM 53-04 AND SRO 9530107-13 AND -15.

Part: SKIN — CORRODED (BS 268)

DURING C-CHECK, FOUND UPPER FUSELAGE SKIN AT FS 268 UNDER NR 1 ADF ANTENNA PITTED AND CORRODED BEYOND LIMITS. REPAIRED IAW ABX REA D953-21628-MR.

Part: INTERCOSTAL — CRACKED (BS 427-416)

DURING C-CHECK, FOUND INTERCOSTAL BETWEEN STA 427 AND 416 AT LONGERON 29L CRACKED. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-5.

Part: WEB — CRACKED (BS 960)

DURING C-CHECK, FOUND THE LT AFT CUSP WEB STA FS 960 CRACKED. REPLACED CUSP WEB IAW DC9 SRM 51-30-2, 51-30-5, AND 51-30-1.

Part: JAMB — CORRODED (CARGO COMPT)

DURING C-CHECK, FOUND THE FWD LOWER CARGO COMPARTMENT LOWER DOOR JAMB PAN CRACKED, BULGED, AND CORRODED. REPLACED LOWER SECTION OF DOOR JAMB PAN IAW DC9 SRM 53-05.

Part: LONGERON — CORRODED (BS 756-809)

DURING C-CHECK, FOUND LONGERON 30 AND SPLICE CORRODED BEYOND LIMITS AT STA 756 TO 809. REPLACED LONGERON FITTING AND SPLICE IAW DC9 SRM 51-30-5 AND 51-30-2.

Part: REAR SPAR — CRACKED (RT PYLON)

DURING C-CHECK, FOUND THE RT PYLON UPPER REAR SPAR IN THE AFT ACCESSORY COMPARTMENT CRACKED. REPAIRED REAR SPAR ANGLE IAW ABX REA D953-21647.

Part: FRAME — CORRODED (BS 996)

DURING C-CHECK, FOUND FUSELAGE FRAME AT STA 996 AND LONGERON 17 TO 18 LT CORRODED. REPAIRED FRAME IAW DC9 SRM 53-00.

Part: DOUBLER — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND THE CENTER WING FUEL TANK LOWER SURFACE KEEL FINGER DOUBLER CORRODED BEYOND LIMITS AT STRINGER 11 RT SIDE. REPAIRED IAW ABX REA D957-21575-MR.

Part: SKIN — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND FUSELAGE EXTERIOR SKIN HEAVILY CORRODED UNDER FWD LOWER CARGO DOOR SCUFF PLATE. REPAIRED SKIN IAW ABX REA D953-21576MR.

Part: INTERCOSTAL — CRACKED (BS 228)

DURING C-CHECK, FOUND INTERCOSTAL AT STA 228 CRACKED AT NUTPLATE HOLE, BETWEEN LONG 27R AND 28R. FABRICATED INTERCOSTAL IAW DACO DWG 991554, AND REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, FOUND LONGERON 16R CRACKED ON AFT SIDE OF THE PYLON BULKHEAD STA 965. REPLACED LONGERON IAW DC9 SRM 53-02.

Part: LONGERON — CRACKED (BS 980/965)

DURING C-CHECK, FOUND LONGERON 17L CRACKED AT STA 980 AND 965. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: MEMBRANE — CRACKED (BS 148)

DURING C-CHECK, FOUND COCKPIT SUBFLOOR CRACKED AT STA 148 BL 0. REPAIRED SUBFLOOR MEMBRANE IAW DC9 SRM 53-01.

Part: ANGLE — CRACKED (LT PYLON)

DURING C-CHECK, FOUND THE LT PYLON INTERIOR LOWER OUTBOARD SPLICE ANGLE AT BOTTOM OF ENGINE MOUNT BOLT CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-5 AND MM 20-16-00.

Part: FRAME — CORRODED (BS 1132)

DURING C-CHECK, FOUND THE CANTED FRAME STA 1132 AT LONGERON 16R CORRODED BEYOND LIMITS. REPAIRED IAW DC9 ABX SSRM DWG K05159.

Part: LONGERON — CRACKED (BS 237)

DURING C-CHECK, FOUND LONGERON 2L CRACKED JUST FWD OF STA 237. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: LONGERON — CORRODED (BS 853-858)

DURING C-CHECK, FOUND LONGERON 30 CORRODED BEYOND LIMITS AT STA 853 TO 858 AND 917 TO 948. REPAIRED LONGERON IAW ABX REA D953-21595-MR.

Part: PANEL — CRACKED (RT WING)

DURING C-CHECK, FOUND RT WING INBOARD LOWER BONDED PANEL CRACKED ON LOWER SIDE. REPLACED BONDED PANEL IAW DC9 SRM 51-20-0, 51-30-2, AND 51-10-4.

Part: INTERCOSTAL — CORRODED (BS 1132-1143)

DURING C-CHECK, FOUND INTERCOSTAL BETWEEN CANTED FRAME AT STA 1132 AND 1143, LONGERON 20R CORRODED BEYOND LIMITS. REPAIRED IAW DACO DWG 9911946, SRN 51-60-0, 51-30-2 AND 5-30-5.

Part: DOOR PAN — CRACKED (CARGO COMPT)

DURING C-CHECK, FOUND THE FWD LOWER CARGO COMPARTMENT DOOR PAN CRACKED AT THE FWD LOWER EDGE AT A BARREL NUT. REPAIRED DOOR IAW DC9 SRM 52-03 FIG 1.

Part: LONGERON — CORRODED (BS 622-658)

DURING C-CHECK, FOUND LONGERON 28R IN RT CANTED KEEL, STA 622 TO 658 CORRODED BEYOND LIMITS. REPLACED LONGERON IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: MEMBRANE — CORRODED (BS 160-218)

DURING C-CHECK, FOUND THE FWD SUBFLOOR BETWEEN STA 160 TO 218, AND LBL 44.5 TO RBL 44.5 CORRODED OUT OF LIMITS UNDER SEAT TRACKS. REPLACED SUBFLOOR MEMBRANE IAW STC DWG 53-AA-30.

Part: JAMB — CRACKED (CARGO COMPT)

DURING C-CHECK, FOUND THE SERVICE DOOR JAMB AFT WEB (P/N 5910085-11) CRACKED. REPAIRED IAW DOUGLAS DRAWING 5910085 AND DC9 SRM 51-10-2.

Part: BULKHEAD FITTING — CRACKED (LT PYLON)

DURING C-CHECK, FOUND THE INBOARD BOTTOM FOOT CRACKED AT THE INBOARD BOTTOM SIDE OF THE LEFT PYLON BULKHEAD. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1.

Part: FITTING — CRACKED (BS 996)

DURING C-CHECK, FOUND FITTING CRACKED AT STA 996 BETWEEN LONGERON 28L AND 27L (AT AFT END OF INTERCOSTAL). REPLACED FITTING IAW DC-9 SRM 51-30-5.

Part: INTERCOSTAL — CORRODED (BS 490)

DURING C-CHECK, FOUND INTERCOSTAL IN CEILING OF FORWARD LOWER CARGO COMPARTMENT HEAVILY CORRODED AT TWO MOUNT HOLES, STA 490. REPLACED INTERCOSTAL IAW DC-9 SRM 51-10-4 AND 51-30-2.

Part: INTERCOSTAL — CRACKED (BS 465-484)

DURING C-CHECK, FOUND INTERCOSTAL BETWEEN STA 465 AND 484 AT LONGERON 29L AND 30 CRACKED WITH TWO GUSSETS ALSO CRACKED. REPLACED INTERCOSTAL GUSSETS 5911412-39 AND 41, IAW DC-9 SRM 51-30-2.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, FOUND LONGERON 13L AT STA 965 CRACKED. REPAIRED LONGERON IAW DC-9 SRM 53-02, FIGURE 18.

Part: SKIN — CORRODED (LT AILERON)

DURING C-CHECK, FOUND THE UPPER SURFACE OF THE LEFT AILERON, INBOARD END CORRODED THROUGH. REPLACED LEFT AILERON IAW DC-9 M/M 27-10-1 AND 27-10-0.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS WOULD NOT EXTINGUISH WHEN SWITCH WAS PLACED IN ANY POSITION. REPLACED STATIONARY BATTERY PACK IAW DC9 SMM 33-53-0.

Part: SLIDING WINDOW — DIRTY (RT COCKPIT)

FIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. CLEANED DEBRIS FROM FORWARD UPPER CORNER OF WINDOW LINKAGE, WINDOW OPERATES OK IAW DC-9 MM.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS ILLUMINATE WHEN BATTERY SWITCH IS TURNED OFF. REPLACED EMERGENCY LIGHT BATTERIES.

Part: ENGINE — DEFECTIVE (LEFT)

AFTER 23 MINUTES OF FLIGHT, LEFT ENGINE FLAMED OUT. ATTEMPTED RESTART TO NO AVAIL. DECLARED EMERGENCY AND LANDED AT PIT WITHOUT FURTHER INCIDENT. REPLACED NR 1 ENGINE IAW MIP WORK CARD J7001. PART TOTAL CYCLES, 34,936.

Part: TAB — DELAMINATED (LT ELEVATOR)

DURING C-CHECK INSPECTION, FOUND LEFT ELEVATOR OUTBOARD TAB DENTED AND DELAMINATED. REPLACED TAB IAW DC-9 MM 27-30-4.

Part: VANE — DELAMINATED (LT TE FLAP)

DURING C-CHECK INSPECTION, FOUND LEADING EDGE OF THE LEFT WING NR 2 FIXED VANE DELAMINATED. REPLACED VANE IAW DC-9 MM 27-51-3.

Part: SPAR CAP — CORRODED (LT HORIZ STAB)

DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON THE LEFT HORIZONTAL STABILIZER SPAR UPPER CAP. REPAIRED IAW ABX REA D955-14656-MR.

Part: SPAR CAP — CORRODED (RT HORIZ STAB)

DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON THE RIGHT HORIZONTAL STABILIZER SPAR, UPPER CAP. REPAIRED IAW ABX REA D955-14630-MR.

Part: SPAR CAP — CORRODED (RT HORIZ STAB)

DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON THE RIGHT HORIZONTAL STABILIZER SPAR UPPER CAP. REPAIRED IAW ABX REA D955-14630-MR.

Part: RIB — CRACKED (VERT STAB)

DURING C-CHECK INSPECTION, FOUND THE VERTICAL STABILIZER TOP LEADING EDGE HAD A CRACKED LEFT RIB BELOW PANEL 6307. REPAIRED IAW DC-9 SUPP SRM DRAWING K05159.

Part: RIB — CRACKED (VERT STAB)

DURING C-CHECK INSPECTION, FOUND THE VERTICAL STABILIZER LEADING EDGE RIB CRACKED. REPAIRED IAW DC-9 SUPP SRM DRAWING K05159.

Part: RIB — CRACKED (VERT STAB)

DURING C-CHECK INSPECTION, FOUND THE VERTICAL STABILIZER LEADING EDGE RIB CRACKED. REPAIRED IAW DC-9 SUPPLEMENTAL SRM DRAWING K05159.

Part: FRAME — CRACKED (BS 617)

DURING C-CHECK INSPECTION, FOUND FRAME AT STA 617 RIGHT CRACKED. REPAIRED IAW DC-9 SRM 53-03, FIGURE 16.

Part: BRACKET — CRACKED (BS 658)

DURING C-CHECK INSPECTION, FOUND FLOOR SUPPORT BRACKET ATTACH ANGLE CRACKED AT STA 658. REPLACED BRACKET IAW DC-9 SRM 51-30-5.

Part: SKIN — GOUGED (BS 180)

DURING C-CHECK INSPECTION, FOUND DEEP GOUGES IN THE FUSELAGE SKIN AT THE EDGE OF THE ENTRANCE DOOR. REPAIRED IAW ABX REA D953-14638-MR.

Part: FITTING — CRACKED (BS 680)

DURING C-CHECK INSPECTION, FOUND A CRACK IN THE SEAT TRACK TO BEAM SUPPORT FITTING AT STA 680, LBL 44. REPLACED FITTING IAW DC-9 SRM 51-30-2 AND 51-30-1.

Part: RIB — CRACKED (VERT STAB)

DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED. REPAIRED IAW DC-9 SUPP SRM DRAWING K05159.

Part: RIB — CRACKED (VERT STAB)

DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED. REPAIRED IAW DC-9 SUPP SRM DRAWING K05498.

Part: RIB — CRACKED (VERT STAB)

DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED. REPAIRED IAW DC-9 SUPP SRM DRAWING K05498.

Part: BRACKET — CRACKED (BS 680)

DURING C-CHECK INSPECTION, FOUND FLOOR SUPPORT BRACKET CRACKED AT STA 680, RBL 45. REPLACED IAW DC-9 SRM 51-30-5.

Part: ANGLE — CRACKED (LT PYLON)

DURING C-CHECK INSPECTION, FOUND A CRACK AROUND FASTENER ON THE LEFT PYLON UPPER ATTACH ANGLE. REPAIRED IAW DC-9 SRM 54-04, FIG 10.