N908AX

Part: WIRE — BROKEN (MLG INDICATOR) · airframe 58,677 hrs · 60,571 cycles

RT MAIN GEAR DOWN INDICATION "GREEN LIGHT" INTERMITTENT. CHECKED WITH ALT MAIN GEAR INDICATION. SHOWED GEAR DOWN. DID A MISSED APPROACH AND DECLARED AN EMERGENCY. VERIFIED NO RIGHT GEAR INDICATION, ALT SYS GOOD, FOUND CORROSION ON SWITCH S1-184 AND CONNECTOR P1-129. CONNECTOR P1-129 HAD THREE BROKEN WIRES AT PINS. REMOVED AND REPLACED CONNECTOR P1-129 AND SWITCH S1-184 IAW DC-9 MM 32-61-00 AND 32-60-01-2. COMPLIED WITH GEAR SWING IAW DC-9 MM 32-60-00-22A1-23. OPS CHECKED GOOD.

Part: LATCH — JAMMED (COCKPIT DOOR) · airframe 57,863 hrs · 59,741 cycles

COCKPIT DOOR LATCH JAMMED. DISASSEMBLED COCKPIT DOOR LATCH ASSEMBLY, FOUND HANDLE JAMMED. FREED JAM AND REASSEMBLED. OPS CHECKED GOOD IAW DC-9 MM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 57,773 hrs · 59,653 cycles

RIVET ROW FOUND CRACKED AT STA 76.550 UNDER CO-PILOT'S WINDSHIELD WIPER BETWEEN APPROXIMATELY LONGERON 3 AND 4 RIGHT. REPAIRED AREA IAW EA 53100075-003-2.

Part: ANGLE — CRACKED (LT PYLON) · airframe 57,773 hrs · 59,653 cycles

LEFT PYLON UPPER ATTACH ANGLE WAS CRACKED AT STA 1019. REPAIRED AREA IAW DC-9 SRM 54-04.

Part: FITTING — CRACKED (RT MLG WW) · airframe 57,773 hrs · 59,653 cycles

SLANT PANEL INBOARD ANGLE FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2, 51-10-4, AND 51-30-1.

Part: ACTUATOR — CRACKED (MLG DOOR) · airframe 57,773 hrs · 59,653 cycles

FITTING FORWARD OF DOOR ACTUATOR CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 57,773 hrs · 59,653 cycles

LONGERON 17 RIGHT HAD 2 CRACKS AT EACH LOCATION, FS 389, FS 408 AND FS 427. REPAIRED LONGERON 17 RIGHT FROM STA 388 TO 446 IAW DC-9 SRM 53-02.

Part: AMPLIFIER — FAILED (SMOKE DETECTION) · airframe 57,721 hrs · 59,597 cycles

CARGO SMOKE LIGHT ON IN FLT. COULD NOT DUPLICATE. INSPECTED WIRING, TAPPED ON DETECTORS & AMPLIFIER, LIGHT REMAINED OUT. FOR PRECAUTION, R & R BOTH SMOKE DETECTORS & SMOKE DETECTOR AMP. PERFORMED CHECK USING LIQUID SMOKE. SYSTEM OPS CHECKED GOOD IAW DC-9 AMM 26-10-07-2. THE SMOKE DETECTORS THAT WERE REMOVED AS PRECAUTION, WERE NOT CONFIRMED FAILURES. SMOKE DETECTOR AMPLIFIER THAT WAS REPLACED AS PRECAUTION, PASSED THE FUNCTIONAL PART OF TEST, BUT FAILED MEGGER PORTION OF TEST. INSULATION RESISTANCE OUT OF SPEC & VARIED. IT APPEARED TO BE A FAULT OF RELAY INSIDE AMP. NO WAY OF KNOWING HOW THAT PROBLEM WOULD AFFECT A/C, OR WHAT KIND OF CONDITION IT WOULD CAUSE. PART WAS QUARANTINED FOR FURTHER TESTING.

Part: UPLOCK — OUT OF ADJUST (MLG) · airframe 57,538 hrs · 59,412 cycles

CYCLED MAIN LANDING GEAR AT 210 KNOTS, 3000 FT, CLEAN UPON RETRACT. RIGHT MAIN LANDING GEAR UNSAFE LIGHT STAYED ON. ADJUSTED RIGHT MAIN LANDING GEAR DOOR UPLATCH IAW DC-9 MM AND WORK ACCOMPLISHED ON W.O. NR 2003908. OPS CHECKED GOOD.

Part: CONTROL PANEL — DEFECTIVE (COCKPIT) · airframe 57,090 hrs · 59,024 cycles

AIRCRAFT SHOOK VIOLENTLY WHEN AUTO PILOT TURNED ON. TURNED OFF AND TRIED AGAIN. SAME RESULTS. TURNED OFF AUTO PILOT, NOTICED NO YOKE MOVEMENT. REMOVED AND REPLACED AUTO PILOT CONTROLLER. SYSTEM OPS CHECKED GOOD IAW DC-9 MM 22-10-00-5.

Part: ELEVATOR — JAMMED (TAIL) · airframe 57,000 hrs · 58,912 cycles

ELEVATOR JAMMED, WOULD NOT PULL BACK WHILE PERFORMING CONTROL CHECK. INSPECTED ELEVATOR TABS, CONTROL VALVES, FOLLOW UP MECHANISMS, LOAD FEEL AND CENTERING SPRING, VISIBLE PORTIONS OF CABLE RUNS IN TAIL COMPARTMENT AND E/E COMPARTMENT. NO DEFECTS FOUND. CONTROL COLUMN FORCES AND FLIGHT CONTROL SURFACE MOVEMENT CHECK, GOOD IAW MM.

Part: SKIN — CORRODED (STA. 872 - 940) · corrosion level 2 · airframe 56,857 hrs · 58,790 cycles

DURING ROUTINE LINE OPERATIONS AT ILN, MAINTENANCE DISCOVERED CORROSION ON THE FUSELAGE SKIN, LOCATED AT THE LOWER CARGO DOOR JAMB, FORWARD LOWER CORNER. THE DAMAGE TO THE SKIN WAS TRIMMED OUT AND A NEW SECTION OF SKIN WAS SPLICED IN, IAW DC-9 SRM 53-04, FIG. 12 C. THIS SKIN WAS FABRICATED FROM 2024-T3 X .063". OTHER PERTINENT DETAILS OF THIS REPAIR CAN BE FOUND IN W.O. 2002908. REF: REA D953-45018-MR.

Part: DOUBLER — CORRODED (STA. 872 - 940) · corrosion level 2 · airframe 56,857 hrs · 58,790 cycles

DURING ROUTINE LINE OPERATIONS AT ILN, MAINTENANCE DISCOVERED CORROSION ON THE FUSELAGE SKIN RESULTING IN THE DISCOVERY OF CORROSION ON THE INTERNAL DOUBLER P/N 5910158-24. THE DAMAGE TO THE INTERNAL DOUBLER WAS TRIMMED OUT AND A NEW SECTION SPLICED IN IAW DC-9 SRM 53-04, FIG. 12 C. THE INTERNAL DOUBLER WAS FABRICATED FROM 7075-T6 X .063". OTHER PERTINENT DETAILS OF THIS REPAIR CAN BE FOUND IN W.O. 2002908. REF: REA D953-45018-MR.

Part: LATCH — OUT OF ADJUST (RT MLG) · airframe 56,853 hrs · 58,788 cycles

RIGHT GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. UPLATCH CHECK FAILED (GEAR DOOR OPEN LIGHT CAME ON AND GEAR EXTENDED). WHEN THE GEAR HANDLE WAS PLACED IN UP POSITION, RIGHT GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT WENT OUT. RIGHT GEAR RETRACTED NORMALLY. ADJUSTED AND TESTED RIGHT MAIN GEAR DOOR LATCH MECHANISM IAW DC-9 MM 32-31-04. OPS CHECKED GOOD.

Part: BRACKET — OUT OF ADJUST (RT MLG) · airframe 56,850 hrs · 58,786 cycles

AFTER TAKEOFF WITH GEAR HANDLE UP, THE RIGHT GEAR RED UNSAFE LIGHT ILLUMINATED. RECYCLED THE GEAR WITH NO CHANGE. THE GEAR UPLATCH CHECK ALSO FAILED. ADJUSTED THE TENSION ON THE RIGHT MAIN GEAR DOOR ROLLER BRACKET AND SPRING ASSEMBLY IAW DC-9 MM 32-31-04-2-0103. ALSO CHECKED AND RIGGED THE RIGHT LANDING GEAR DOOR LATCH TORQUE TUBE IAW DC-9 MM 32-31-04-2-1003. CYCLED THE GEAR THREE TIMES. OPS CHECKED GOOD.

Part: DOUBLER — CRACKED (EXT. FUSELAGE) · airframe 56,792 hrs · 58,719 cycles

CRACK IN FUSELAGE SKIN AT STATION 994, LONGERON 12 RIGHT, BETWEEN 2 RIVETS AND EXTENDING 1/4" PAST BOTH RIVETS. REPAIRED CRACK IAW DC-9 DWG SR09530151 AND E.A. 5311005-034.

Part: CAP — CRACKED (FUSELAGE) · airframe 56,792 hrs · 58,719 cycles

LONGERON END CAP CRACKED NR 11 RIGHT. INSTALLED NEW END CAP NR 11 RIGHT IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 56,792 hrs · 58,719 cycles

AFT PRESSURE BULKHEAD SIDE SKIN SPLICED AT Z 14.00. SPLICE NOT IAW DOUGLAS AFT PRESSURE BULKHEAD RE-WORK. SPLICED NEW SECTION (LOWER) OF RIGHT AFT PRESSURE BULKHEAD WEB IAW REA D953-44534-MR AND DOUGLAS DWG J060088.

Part: DOUBLER — CRACKED (RIGHT WING) · airframe 56,792 hrs · 58,719 cycles

ANGLED DOUBLER COMMON TO #7 SLAT TRACK RIB INBOARD AND FRONT SPAR CRACKED. REPAIRED AREA IAW DC-9 SRM 57-09.

Part: RIB — CRACKED (RT WING) · airframe 56,792 hrs · 58,719 cycles

NR 8 SLAT TRACK INBOARD LEADING EDGE RIB ANGLE COMMON TO ROLLERS CRACKED AT AFT LOWER VERTICAL LEG. REPLACED RIB IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: DOUBLER — CRACKED (EXT. FUSELAGE) · airframe 56,792 hrs · 58,719 cycles

5" CRACK TOP OF FUSELAGE AT #1 LONGERON IN AFT PRESSURE BULKHEAD AREA. REPAIRED CRACK IAW DC-9 DWG SR0953151 AND E.A. 5311005-034.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 56,694 hrs · 58,600 cycles

DURING PREFLIGHT CHECK, FOUND THE EMERGENCY CABIN LIGHTS INOPERATIVE. REPLACED THE BATTERY POWER SUPPLY IAW DC-9 MM. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 56,430 hrs · 58,322 cycles

AFT COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC-9 AMM 33-53-02-4-0001. OPS CHECKED GOOD.

Part: PANEL — DELAMINATED (LT WING) · airframe 56,003 hrs · 57,806 cycles

LEFT WING TRAILING EDGE PANEL DELAMINATED. MAINTENANCE REPLACED PANEL IAW DC-9 MM.

Part: SPLICE — CRACKED (BULKHEAD) · airframe 56,003 hrs · 57,806 cycles

AFT PRESSURE BULKHEAD TEE CAP SPLICE CRACKED. MAINTENANCE REPLACED THE SPLICE IAW DC-9 SRM 51-30-5.

Part: WEB — CRACKED (FUSELAGE) · airframe 56,003 hrs · 57,806 cycles

CUSP WEB CRACKED AT FS 218. MAINTENANCE REPLACED THE CUSP WEB IAW DC-9 SRM 51-30-1.

Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 56,003 hrs · 57,806 cycles

AFT LOWER CARGO DOOR FORWARD STIFFENER CRACKED. MAINTENANCE REPLACED THE STIFFENER IAW DRAWING 5913304-11.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,003 hrs · 57,806 cycles

FLOORBEAM SUPPORT CRACKED AT FS 560. MAINTENANCE REPAIRED THE SUPPORT IAW DC-9 SRM DRAWING K05159.

Part: INTERCOSTAL — CRACKED (CARGO FLOOR) · airframe 56,003 hrs · 57,806 cycles

UPPER CARGO FLOOR INTERCOSTAL CRACKED. MAINTENANCE REPLACED THE INTERCOSTAL END CLIPS IAW DC-9 MM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 56,003 hrs · 57,806 cycles

AFT VENTRAL DOOR BEAM WAS FOUND TO BE CRACKED. MAINTENANCE REPLACED VENTRAL DOOR BEAM IAW DC-9 MM.

Part: TEE CHORD — CRACKED (FUSELAGE) · airframe 56,003 hrs · 57,806 cycles

AFT PRESSURE BULKHEAD NR 2 TEE CRACKED. MAINTENANCE REPLACED THE TEE IAW ABX EA 53120033-006.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,003 hrs · 57,806 cycles

FUSELAGE SKIN CRACKED AND BULGED AT FS 990L. MAINTENANCE REPAIRED THE DAMAGE IAW ABX REA 953-38967.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 56,003 hrs · 57,806 cycles

AFT PRESSURE BULKHEAD DOOR FRAME HAS A CRACKED DOUBLER. REPAIRED DOUBLER IAW ABX REA D953-38986.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,003 hrs · 57,806 cycles

INTERCOSTAL AT FS 579 - 598 HAD LEVEL ONE CORROSION. MAINTENANCE REPLACED THE INTERCOSTAL IAW DC-9 SRM 51-30-2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,003 hrs · 57,806 cycles

AFT LOWER CARGO DOOR NR 1 BEAM FITTING CRACKED. MAINTENANCE REPLACED THE NR 1 BEAM END FITTING IAW DC-9 SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 56,003 hrs · 57,806 cycles

AFT LOWER CARGO DOOR BEAM NR 2 END FITTING CRACKED. MAINTENANCE REPLACED THE END FITTING IAW SRM 51-30-5.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,003 hrs · 57,806 cycles

FLOORBEAM SUPPORT CRACKED AT LOWER INBOARD FASTENER. MAINTENANCE REPAIRED IAW DC-9 SRM DRAWING K05159.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,003 hrs · 57,806 cycles

FUSELAGE FRAME CRACKED AT FS 680. MAINTENANCE REPLACED FRAME IAW ABX REA 953-38971-MR.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 56,003 hrs · 57,806 cycles

INTERCOSTAL GUSSET CRACKED AT FS 465. MAINTENANCE REPLACED THE GUSSET IAW DC-9 SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,982 hrs · 57,779 cycles

DURING PRE-DEPARTURE CHECK, COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCYLIGHTS POWER SUPPLY BATTERIES.

Part: LATCH — LACK OF LUBE (COCKPIT DOOR)

COCKPIT DOOR WOULD NOT OPEN FROM CABIN SIDE. LUBRICATED COCKPIT DOOR LATCH MECHANISM, OPS CHECKED GOOD.

Part: VANE — DELAMINATED (RT TE FLAP)

RIGHT FLAP INBOARD FIXED VANE DELAMINATED 2 PLACES ON LOWER SURFACE. REPLACED VANE ASSEMBLY IAW DC9 MM 27-51-3.

Part: FITTING — CRACKED (LT MLG WW)

KEEL WEB FORWARD ATTACH ANGLE FITTING CRACKED AT LEFT SIDE. REPLACED ANGLE IAW DC9 SRM 51-30-3 AND 51-30-1.

Part: LONGERON — CRACKED (LT MLG WW)

LONGERON 20 LEFT CRACKED AT AFT END OF TRAPEZOIDAL PANEL. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: FLOORBEAM — CRACKED (BS 351)

FLOORBEAM CRACKED AT STATION 351 BL 0 TO LBL 5. REPAIRED FLOORBEAM IAW ABX REA D953-27445MR.

Part: SHEAR TIE — CRACKED (BS 980)

SHEAR TIE FORMER CRACKED AT STATION 980 BELOW LONGERON 14 RIGHT. REPLACED SHEAR TIE IAW DC9 SRM 53-30-02.

Part: LONGERON — CRACKED (FRAME 996)

LONGERON 18R CRACKED AT FRAME STATION 996. REPLACED ANGLE IAW DC9 SRM 51-30-5.

Part: TRAPEZOID PANEL — CRACKED (LT MLG WW)

LEFT TRAPEZOIDAL PANEL UPPER OUTBOARD FLANGE CRACKED STARTING AT 6TH FASTENER HOLE RUNNING THROUGH 8TH FASTENER HOLE INTO RADIUS OF THE VERTICAL FLANGE. REPLACED TRAPEZOIDAL PANEL IAW DC9 S/B'S 53-10D, 53-115 AND 53-182.

Part: LONGERON — CRACKED (BS 905)

LONGERON 16 RIGHT WAS CRACKED AT STATION 905. REPAIRED IAW DC9 SRM 53-02.

Part: FRAME — CRACKED (BS 980)

FRAME AT STATION 980 CRACKED AT LONGERON 16 LEFT. REPAIRED FRAME IAW DC9 SRM 53-03 AND DACO DWG 9958238.

Part: LONGERON — CRACKED (BS 965)

LONGERON 12 RIGHT CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: FRAME — CRACKED (BS 389)

FUSELAGE FRAME CRACKED AT STATION 389 AND LONGERON 5 RIGHT. REPAIRED FRAME IAW DC9 SRM 53-03.

Part: LONGERON — CRACKED (BS 945)

LONGERON 17 RIGHT CRACKED AT STATION 945. REPAIRED IAW DC9 SRM 53-02.

Part: SHEAR TIE — CRACKED (BS 945)

FUSELAGE FRAME SHEAR TIE CRACKED BELOW LONGERON 15 LEFT AT STATION 945. REPLACED SHEAR TIE IAW DC9 SRM 51-10-4 AND 51-30-2.

Part: LONGERON — CRACKED (BS 718)

LONGERON 3 RIGHT CRACKED AT STATION 718. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: LONGERON — CRACKED (BS 965)

LONGERON 13 LEFT CRACKED AT STATION 965 LOWER ATTACH BOLT. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: DOOR — UNSERVICEABLE (COCKPIT)

COCKPIT ENTRY DOOR WAS DIFFICULT TO OPEN AND CLOSE. REPLACED COCKPIT ENTRY DOOR, OPS CHECKED GOOD.

Part: WINDOW — OUT OF ADJUST (RT COCKPIT)

DURING PRE-DEPARTURE CHECK, FOUND THE FIRST OFFICER'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT UNLOCK. ADJUSTED FORE AND AFT ADJUSTMENT STOPS TO UPPER TRACK IAW DC9 MM 56-10-3.

Part: WINDOW — OUT OF ADJUST (RT COCKPIT)

FIRST OFFICER'S CLEAR VIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. READJUSTED THE FIRST OFFICER'S WINDOW IAW DC9 MM CHAPTER 56.

Part: WINDOW LOCK — OUT OF ADJUST (COCKPIT)

FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT OPEN. CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN FULLY. ADJUSTED UPPER LOCK ON THE FIRST OFFICER'S CLEARVIEW WINDOW. RESECURED TRIM ON CAPTAIN'S CLEARVIEW WINDOW.

Part: PRESSURE PANEL — CRACKED (BS 83)

DURING C-CHECK, FOUND THE UPPER PRESSURE PANEL STA 83 CRACKED AT THE LEFT CUSP. REPAIRED PRESSURE PANEL IAW DC-9 SB 53-187.

Part: PANEL — SEPARATED (LT SPOILER)

DURING C-CHECK, FOUND THE LT OUTBOARD SPOILER PANEL SEPARATED AT THE CENTER FITTING. REMOVED AND REPLACED THE OUTBOARD SPOILER PANEL IAW ABX DC9 MM SUPP 27-61-1.

Part: BRACKET — CORRODED (RT SPOILER)

DURING C-CHECK, FOUND THE RT OUTBOARD SPOILER CONTROL BRACKET ASSEMBLY CORRODED. REMOVED AND REPLACED THE SPOILER CONTROL BRACKET IAW DC9 MM 20-16-0 AND 27-60-0.

Part: FRAME — CORRODED (BS 889)

DURING C-CHECK, FOUND STA 889 FRAME EXFOLIATED BETWEEN LONGERONS 21L AND 23L. *S/D* REPLACED FRAME IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FRAME — CRACKED (BS 699)

DURING C-CHECK, FOUND THE RT MAIN FRAME AT FS 699 FORWARD UPPER FLANGE CRACKED AT THE SEAT TRACK ATTACH ZEE ANGLE OUTBOARD ATTACH HOLE. REPAIRED THE MAIN FRAME IAW DC-9 SB 53-131 AND ABX REA D953-202248-MR. (REPAIR DOUBLER PN 5935650 INSTALLED).

Part: CUSP WEB — CRACKED (BS 598-617)

DURING C-CHECK, FOUND THE LEFT CUSP WEB CRACKED BETWEEN FS 598 AND 617. REPAIRED CUSP WEB IAW DC-9 SRM 53-01.

Part: FITTING — CRACKED (RT WING)

DURING C-CHECK, FOUND THE OUTBOARD SPOILER TORSION BAR OUTBOARD SUPPORT FITTING CRACKED AT THE UPPER END. *S/D* REPLACED TORSION BAR IAW DC9 SRM 51-30-1 AND 51-30-8.

Part: CUSP WEB — CRACKED (BS 598-617)

DURING C-CHECK, FOUND THE LT CUSP WEB CRACKED BETWEEN FS 598 AND 617. *S/D* REPAIRED CUSP WEB IAW DC9 SRM 51-30-1 AND 51-30-2.

Part: TR LINK — CRACKED (NR 1 ENGINE)

DURING C-CHECK, FOUND THE NR 1 ENGINE THRUST REVERSER LOWER INBOARD DRIVE LINK CRACKED AT THE FORWARD GREASE FITTING. *S/D* REPLACED DRIVE LINK IAW DC9 MM 78-31-5.

Part: ANGLE — CRACKED (NR 1 PYLON)

DURING C-CHECK, FOUND THE TOP ANGLE FOR THE 4TH WEB FORWARD FROM THE END OF THE LT PYLON TRAILING EDGE CRACKED. *S/D* REPAIRED IAW DC9 SRM 54-50.

Part: INTERCOSTAL — CRACKED (BS 218)

DURING C-CHECK, FOUND THE UPPER CARGO COMPARTMENT FLOORBEAM INTERCOSTAL CRACKED ON THE AFT SIDE OF FLOORBEAM AT FS 218 AND BL 0. *S/D* REPAIRED IAW DC9 SRM 53-15-0.

Part: FRAME — CRACKED (BS 699)

DURING C-CHECK, FOUND THE RT MAIN FRAME AT FS 699 FWD UPPER FLANGE CRACKED AT THE SEAT TRACK ATTACH ZEE ANGLE OUTBOARD ATTACH HOLE. *S/D* REPAIRED IAW DC9 SRM 51-30-2.

Part: BULKHEAD WEB — CRACKED (BS 37)

DURING C-CHECK, FOUND THE RT SIDE BULKHEAD WEB AT FS 37 CRACKED AT A RIVET. *S/D* REPAIRED WEB IAW DC9 SRM 53-01.

Part: LONGERON — CRACKED (BS 362)

DURING C-CHECK, FOUND APPROXIMATE 6 INCH CRACK IN THE FLANGE OF LONGERON 30 AT STA 362. *S/D* REPLACED LONGERON FROM FS 354 TO 409 IAW DC9 SRM 53-02.

Part: INTERCOSTAL — CRACKED (BS 256)

DURING C-CHECK, FOUND THE UPPER CARGO FLOORBEAM INTERCOSTAL CRACKED AT THE FORWARD SIDE OF THE FLOORBEAM AT FS 256 AND THE ZERO BUTT LINE. *S/D* REPAIRED IAW DC9 SRM 53-15-0.

Part: FLOOR PANEL — CRACKED (CARGO COMP)

DURING C-CHECK, FOUND THE FLOOR PANEL AT STA 218 BETWEEN SEAT TRACK BL 0.0 AND RBL 9.0 CRACKED. REPAIRED IAW DC9 SRM 53-21-0.

Part: BRACKET — CRACKED (RT WING)

DURING C-CHECK, FOUND THE RT FLAP FOLLOW-UP PULLEY UPPER BRACKET AT FLAP HINGE 164 CRACKED. *S/D* REPLACED BRACKET IAW DC9 MM 20-10-1.

Part: PRESSURE PANEL — CRACKED (BS 83)

DURING C-CHECK, FOUND THE UPPER PRESSURE PANEL CRACKED TWO PLACES AT FS 83 AT THE LT CUSP AND RT CUSP. *S/D* REPAIRED IAW DC9 SRM 53-21-0.

Part: WINDOW — STUCK (RT COCKPIT)

FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT OPEN. (EMERGENCY COCKPIT EXIT). OPENED AND CLOSED FIRST OFFICER'S WINDOW SEVERAL TIMES. OPS CHECKED NORMAL.

Part: WINDOW — LACK OF LUBE (RT COCKPIT)

FIRST OFFICER'S CLEARVIEW EMERGENCY EXIT WINDOW WOULD NOT OPEN. CLEANED AND LUBED UPPER LOCKING MECHANISM, OPERATION CHECKS GOOD IAW DC-9 MM 56-10-3.

Part: UNSAFE LIGHT — ILLUMINATED (LT MLG)

UPON GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH. FERRIED AIRCRAFT FROM MEM TO ILN. WORK IN PROGRESS AT THIS TIME.

Part: ROLLER ASSY — DEFECTIVE (LT MLG DOOR)

DURING GEAR UPLATCH CHECK, LEFT GEAR UNSAFE LIGHT ILLUMINATED AND COULD NOT BE EXTINGUISHED USING THE ABNORMAL PROCEDURE. REPLACED LEFT MAIN LANDING GEAR DOOR LATCH ROLLER ASSEMBLY IAW DC9 OHM 32-11-5, OPS CHECKED GOOD.

Part: BUSHING — WORN (RT MLG DOOR)

RIGHT GEAR UNSAFE LIGHT WOULD NOT GO OUT IN FLIGHT. COMPLETED ABNORMAL PROCEDURE BUT GEAR LIGHT WOULD NOT GO OUT. REPLACED RIGHT MAIN LANDING GEAR DOOR HINGE BUSHING AND ADJUSTED THE MAIN LANDING GEAR DOOR LATCH ASSEMBLY IAW DC-9 MM 32-31-4.

Part: CONNECTOR — CORRODED (RT MLG)

RIGHT GEAR UNSAFE LIGHT CAME ON DURING UPLATCH CHECK, RECYCLED GEAR, LIGHT WAS STILL ON, RIGHT HYDRAULIC SYSTEM 3000 PSI.\N\N\N\N\NCLEANED WIRING TERMINALS AT TERMINAL STRIP IN RIGHT WING ROOT. LUBRICATED GEAR. PERFORMED GEAR INDICATION TEST IAW DC-9 SUPP M.M. 32-60-01.

Part: BATTERIES — DISCHARGED (CABIN)

ON PRE-DEPARTURE CHECK, FOUND COCKPIT EMERGENCY LIGHTING INOPERATIVE. REPLACED EMERGENCY LIGHTING BATTERIES IAW DC-9 M.M. 33-10-00.

Part: SPAR CAP — CORRODED (WS 530)

DURING C-CHECK INSPECTION, FOUND RIGHT WING AFT SPAR LOWER CAP CORRODED 12 INCHES FROM THE OUTBOARD AILERON HINGE. REPAIRED IAW DC-9 SRM 57-09, FIGURE 11 AND ABX REA D957-14179.

Part: PRESSURE PANEL — CORRODED (BS 737-756)

DURING C-CHECK INSPECTION, FOUND CORROSION ON THE PRESSURE PANEL BETWEEN RBL 37 AND LBL 37 STA 737 TO 756. REPAIRED IAW ABX REA D953-14154-MR.

Part: SEAT TRACK — CRACKED (BS 278-872)

DURING C-CHECK INSPECTION, FOUND THE MAIN CABIN SEAT TRACKS CRACKED, WORN AND CORRODED AT PERMANENT LOCK ATTACH POINTS. REPAIRED IAW ABX REA RE-14184-MR.

Part: JAMB — DAMAGED (BS 200)

DURING C-CHECK INSPECTION, FOUND THE ENTRY DOOR AFT JAMB INNER SKIN AT STA 200 DENTED AND TORN. REPAIRED IAW ABX REA D953-14173-MR.

Part: ANGLE — CRACKED (LT FLAP)

DURING C-CHECK INSPECTION, FOUND THE LEFT WING OUTBOARD FLAP HINGE ATTACH ANGLE INSIDE THE FLAP CRACKED. REPLACED ANGLE IAW DC-9 SRM 51-30-1.

Part: ANGLE — CRACKED (RT FLAP)

DURING C-CHECK INSPECTION, FOUND THE RIGHT WING OUTBOARD FLAP ATTACH ANGLE INSIDE FLAP CRACKED. REPLACED ANGLE IAW DC-9 SRM 51-30-1.

Part: SPAR CAP — CORRODED (WS 530)

DURING C-CHECK INSPECTION, FOUND CORROSION ON THE RIGHT WING LOWER SPAR CAP AT XW-530. REPAIRED IAW ABX REA D957-14078-MR.

Part: SKIN — BLENDED (CARGO DOOR)

DURING C-CHECK INSPECTION, FOUND DEEP BLEND OUT ON AFT EDGE OF THE FORWARD LOWER CARGO DOOR SKIN. REPAIRED IAW ABX REA D952-14076-MR.

Part: FITTING — CRACKED (RT FLAP)

DURING C-CHECK INSPECTION, FOUND THE UPPER FITTING INSIDE OUTBOARD EXPANSION JOINT ON THE RIGHT FLAP CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2 AND 51-30-1.

Part: ANGLE — CRACKED (RT PYLON)

DURING C-CHECK INSPECTION, FOUND THE RIGHT PYLON UPPER ATTACH ANGLE CRACKED NEAR THE CENTER. REPAIRED IAW DC-9 SRM 54-04, FIGURE 10.

Part: ANGLE — CRACKED (RT PYLON)

DURING C-CHECK INSPECTION, FOUND THE RIGHT PYLON UPPER ATTACH ANGLE CRACKED NEAR THE FORWARD END. REPAIRED IAW DC-9 SRM 54-04, FIGURE 10.

Part: TRAILING EDGE — DELAMINATED (RT WING)

DURING C-CHECK INSPECTION, FOUND THE RIGHT WING OUTBAORD TRAILING EDGE ASSEMBLY DELAMINATED. REPAIRED IAW DC-9 SRM 51-70-2.

Part: BEARING — WORN (RT AILERON)

DURING C-CHECK INSPECTION, FOUND THE RIGHT AILERON TRIM TAB LINKAGE WORN. REPLACED TRIM TAB LINKAGE BEARINGS IAW DC-9 MM 20-10-1.