N933AX

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 48,064 hrs · 53,375 cycles

ON APPROACH, WHEN LANDING GEAR WAS EXTENDED, THE NOSE GEAR UNSAFE LIGHT DID NOT ILLUMINATE INITIALLY, THEN IT DID ILLUMINATE. WHEN GEAR WAS EXTENDED, THE NOSE GEAR GREEN LIGHT WAS INOPERATIVE. RECYCLED GEAR WITH NO IMPROVEMENT. REPLACED NLG INDICATOR BULBS AND INDICATION WORKED NORMAL. COULD NOT DUPLICATE THE DISCREPANCY. FOUND PIN NR 2 TO NOSE GEAR DOWN AND LOCKED SWITCH SLIGHTLY RECESSED. RESEATED NR 2 PIN AND REPLACED THE DOWNLOCK SWITCH AS A PRECAUTION IAW DC9 MM 32-60-01-2-0.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 48,064 hrs · 53,375 cycles

VENTRAL DOOR JAMB LOWER RIGHT STOP PAD HAD FITTING CRACKED .5 INCH AND BROKEN FASTENERS. REMOVED AND REPLACED BROKEN FITTINGS IAW DC9 SRM 51-30-2.

Part: WIRE — BROKEN (COCKPIT LIGHT) · airframe 47,166 hrs · 52,502 cycles

FIRST OFFICER'S BRIEFCASE LIGHT EMITTED ELECTRICAL SPARKS OUT OF THE LIGHT/LENSE AREA. MAINTENANCE REPAIRED BROKEN WIRE AT BRIEFCASE LIGHT. OPS CHECKED OK IAW ABX MAINTENANCE MANUAL 33-10.

Part: PANEL — DEBONDED (LT WING) · airframe 47,111 hrs · 52,442 cycles

LT WING OB UPPER TRAILING EDGE PANEL HAD SKIN DAMAGE AT STA. XRS 516. SKIN DEBONDED AND ROLLED BACK FROM THE LEADING EDGE PANEL. DAMAGED AREA MEASURED 6 INCHES LONG BY 18 INCHES WIDE. DEFERRED: NR 45199. TEMP REPAIRED IAW REA D957-52280. CLEARED: DI NR 45199. REPAIRED BONDED PANEL IAW SRM 57-30-2 AND 57.01 FIG 3 SHEET 2.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 46,881 hrs · 52,195 cycles

INTERCOSTAL AT STA 194 IN AIRSTAIR DOOR WAS CRACKED AND CORRODED. REPLACED INTERCOSTAL IAW DC-9 SRM 53-30-2.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,881 hrs · 52,195 cycles

CRACK IN VENTRAL DOOR JAMB STRUCTURE AT UPPER RIGHT CORNER. REPAIRED DAMAGED VENTRAL DOOR JAMB IAW DC-9 SRM 53-05.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,881 hrs · 52,195 cycles

CRACK IN FUSELAGE SKIN AT SERVICE DOOR CUTOUT LOWER AFT CORNER. REPAIRED IAW REA D953-51475MR AND DC-9 SRM 53-05.

Part: ATTACH BRACKET — CORRODED (FUSELAGE) · airframe 46,881 hrs · 52,195 cycles

FORWARD AIRSTAIR COMPARTMENT FOUND CORROSION ON DOOR SWITCH AND ATTACH BRACKET. REPLACED ATTACH BRACKET AND WEB IAW DC-9 DWG 9922405 AND DC-9 SRM.

Part: PAN — CORRODED (FUSELAGE) · airframe 46,881 hrs · 52,195 cycles

NUMEROUS SPOTS OF CORROSION ON FORWARD LOWER CARGO DOOR CUTOUT PAN WEB. CLEANED AND TREATED CORROSION IAW DC-9 SRM 51-10-3.

Part: PAN — CORRODED (FUSELAGE) · airframe 46,881 hrs · 52,195 cycles

SERVICE DOOR THRESHOLD LOWER PAN HAD A BULGE AND 3 EACH POPPED RIVETS AT AFT CORNER. REPAIRED DOOR JAMB PAN IAW DC-9 SRM 53-05.

Part: STRUCTURE — CRACKED (ENTRY DOOR) · airframe 46,881 hrs · 52,195 cycles

MAIN ENTRY DOOR CRACKED LOWER HINGE CUTOUT. REPLACED MAIN ENTRY DOOR ON NON ROUTINE 0311 IAW DC-9 SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 46,881 hrs · 52,195 cycles

CORROSION AT FUSELAGE FRAME AND FLOOR SUPPORT AREA STA 200, LONGERON 18 RIGHT AREA. REMOVED FLOOR PANEL AND J-CHANNEL AND RE-INSTALLED. ALL CORROSION WORK COMPLETED ON NON ROUTINE 0259 IAW DC-9 SRM 51-30-1.

Part: FRAME — CORRODED (FUSELAGE) · airframe 46,881 hrs · 52,195 cycles

CORROSION ON FRAME FS 832 LONGERON 30. REPAIRED IAW DC-9 SRM 53-03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 46,881 hrs · 52,195 cycles

SEAT TRACK AT LEFT BUTTLINE 44 WAS CORRODED BETWEEN STA 214 AND 224. REPAIRED TRACK AND SPLICED IN NEW SECTION OF TRACK IAW DC-9 SRM 53-05.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 46,881 hrs · 52,195 cycles

FLOOR STRAP SUPPORT ANGLE EXFOLIATED FS 364 AT LONGERON 28 RIGHT. REMOVED AND REPLACED ANGLE IAW DC-9 SRM 51-30-5.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 46,881 hrs · 52,195 cycles

FLOOR STRAP SUPPORT ANGLE CRACKED AFT SIDE OF FRAME FS 503 AT LONGERON 28 RIGHT. REMOVED AND REPLACED ANGLE IAW DC-9 SRM 51-30-5.

Part: FITTING — CRACKED (FUSELAGE) · airframe 46,881 hrs · 52,195 cycles

LONGERON END FITTING CRACKED, LONGERON 26 LEFT AT APPROXIMATELY 612, AFT OF P-DOME. REPLACED END FITTING IAW DC-9 SRM 51-30-5.

Part: ATTACH FITTING — CRACKED (RT MLG WW) · airframe 46,881 hrs · 52,195 cycles

RIGHT WHEEL WELL BULKHEAD TO KEEL ATTACH FITTING FS 718 CRACKED. REPLACED FITTING IAW DC-9 SERVICE BULLETIN 53-80.

Part: FITTING — CRACKED (FUSELAGE) · airframe 46,881 hrs · 52,195 cycles

LONGERON END FITTING CRACKED, LONGERON 26 RIGHT AT APPROXIMATELY 612 - AFT OF P-DOME. INSTALLED NEW END FITTING P/N 3924028-501 IAW DC-9 SRM 51-30-5.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 45,720 hrs · 51,116 cycles

FORWARD LOWER CARGO DOOR LOWER AFT STOP FITTING INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2.

Part: ANGLE — CRACKED (LT PYLON) · airframe 45,720 hrs · 51,116 cycles

TWO ANGLES CRACKED (UPPER AND LOWER) IN LEFT PYLON, UNDER PANEL 8111. REPLACED ANGLES IAW SRM 51-30-2 AND 51-30-1.

Part: WIRE — BURNED (HYD PUMP) · airframe 45,695 hrs · 51,088 cycles

RIGHT AUXILIARY HYDRAULIC PUMP POWER WIRES BURNED THROUGH. REMOVED AND REPLACED THE RIGHT AUXILIARY PUMP. OPS CHECKED GOOD IAW DC-9 AMM 29-10-06-2-0001.

Part: LOCK — BROKEN (WINDOW) · airframe 45,659 hrs · 51,035 cycles

DURING PRE "D" CHECK, MAINTENANCE FOUND THAT THE FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT OPEN. FOUND THE UPPER LOCK BAR BROKEN. REMOVED AND REPLACED THE UPPER LOCK BAR AND ADJUSTED IAW DC-9 MM 56-10-03-5. OPS CHECKED GOOD.

Part: FITTING — CRACKED (CABIN) · airframe 44,659 hrs · 50,154 cycles

MAIN CARGO DOOR FITTING WAS CRACKED IN TWO PLACES, F.S. 313 LONGERON 15 - 16 LEFT. REPAIRED FRAME IAW REA D952-42464-MR.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 44,659 hrs · 50,154 cycles

INTERCOSTAL ATTACH ANGLES WERE CRACKED INSIDE THE ANTI-COLLISION LIGHT PANEL AT THE RIGHT BUTT LINE 8.0 AND THE LEFT BUTT LINE FS 743. REPLACED THE ANGLES IAW DC-9 SRM 51-30-1, P/N 9923459-46 AND 9923459-45.

Part: CLIP — CRACKED (FUSELAGE) · airframe 44,659 hrs · 50,154 cycles

SHEAR TIE WAS CRACKED BETWEEN LONGERON "0" AND "1" LEFT AT F.S. 1087, ON AFT SIDE. REPLACED CRACKED SHEAR TIE IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: CLIP — CRACKED (CABIN) · airframe 44,659 hrs · 50,154 cycles

LEFT FUSELAGE FRAME SHEAR TIE WAS CRACKED AT STATION 945 BETWEEN LONGERON 15 LEFT AND 16 LEFT. REPAIRED SHEAR TIE IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,659 hrs · 50,154 cycles

FORWARD LOWER CARGO LOWER DOOR JAMB HAD CORROSION BULGE BETWEEN THE LOWER STOPS. REPAIRED AREA IAW REA D953-42441-MR. LEVEL  CORROSION.

Part: SUPPORT — CRACKED (AFT CARGO) · airframe 44,659 hrs · 50,154 cycles

90 DEGREE FITTING WAS CRACKED ON THE END OF LONGERON 28 RIGHT, BOTTOM OF FLOOR PANEL SUPPORT BOTTOM SIDE F.S. 756. REPLACED SUPPORT IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,659 hrs · 50,154 cycles

F.S. 737 WAS CRACKED ON THE FORWARD UPPER FLANGE BETWEEN THE OUTBOARD FASTENERS. FRAME WAS REPLACED ON JOB CARD E.A. 53400326-001-3.

Part: FITTING — CRACKED (AFT CARGO) · airframe 44,659 hrs · 50,154 cycles

RIGHT UPPER CARGO FLOOR BEAM VERTICAL ATTACH FITTING WAS CRACKED. REPLACED THE ATTACH FITTING IAW DC-9 SRM 51-30-5.

Part: RHEOSTAT — SHORTED (COCKPIT) · airframe 43,579 hrs · 49,078 cycles

DURING DESCENT INTO BOS, ACRID FUMES EMITTED FROM THE FIRST OFFICER'S INSTRUMENT PANEL. REPLACED FIRST OFFICER'S BRIEFCASE LIGHT RHEOSTAT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,552 hrs · 49,044 cycles

COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY POWER SUPPLY.

Part: FRAME — CRACKED (BS 699)

RIGHT MAIN FRAME AT STATION 699 WAS CRACKED AT THE UPPER INBOARD, FORWARD FLANGE (PT.K - PT.J, REF: SERVICE SKETCH 2765B, SHEET 7). REPAIRED FRAME IAW ABX REA D953-35455MR.

Part: SKIN — CORRODED (FUSELAGE)

FUSELAGE SKIN UNDER LEFT STATIC PORT PLATE WAS CORRODED. REPAIRED SKIN IAW DC9 SRM 53-04, FIGURE 3.

Part: FRAME — CRACKED (BS 737)

RIGHT MAIN FRAME STATION 737 WAS CRACKED BETWEEN SEAT TRACK SUPPORT BOLTS UPPER AFT INBOARD FLANGE (BETWEEN PT G AND PT J, REF: SERVICE SKETCH 2765B, SHEET 7). REPAIRED FRAME IAW ABX REA D953-35470MR.

Part: PLATE — CRACKED (HORIZ STAB)

RIGHT HORIZONTAL STAB PLANK WAS CRACKED AT STRINGER NR 1 XHS 204 AND STRINGER NR 2 STATION FHS 244. REPAIRED PLANK IAW DC9 SRM 55-02, FIGURE 16.

Part: FITTING — CRACKED (BS 718)

RIGHT WHEEL WELL BULKHEAD TO KEEL VERTICAL FITTING AT STATION 718 WAS CRACKED. REPLACED FITTING IAW ABX REA D953-35458MR.

Part: FITTING — CRACKED (CARGO DOOR)

AFT LOWER CARGO COMPARTMENT DOOR UPPER BEAM FORWARD END FITTING WAS CRACKED. REPLACED END FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: PLATE — CRACKED (HORIZ STAB)

RIGHT HORIZONTAL STAB PLANK WAS CRACKED AT STRINGER NR 2 AND NR 3 STATION XFS 40.7 UPPER PLANK. REPAIRED PLANK IAW DC9 SRM 55-02, FIGURE 16.

Part: TAB — DELAMINATED (RUDDER)

RUDDER TAB HAD AREAS OF DELAMINATION AND SURFACE CORROSION. REPLACED RUDDER TAB IAW DC9 MM 27-20-2.

Part: FITTING — CRACKED (HORIZ STAB)

RIGHT HORIZONTAL STAB OUTBOARD END FITTING WAS CRACKED AT THE UPPER FORWARD FLANGE. REPLACED FITTING IAW DC9 SRM 51-30-1, 51-30-2, 51-30-5.

Part: FRAME — CRACKED (CARGO BAY)

LEFT MAIN FRAME STATION 718 WAS CRACKED AT THE FORWARD AND AFT UPPER INBOARD FLANGES EXTENDING INBOARD UNDER THE FLOORBEAM SPLICE ANGLES BETWEEN PT K - PT J AND RUNNING PAST PT 5, REF: SERVICE SKETCH 2765B, SHEET 7. REPLACED FRAME IAW ABX REA D953-35438MR.

Part: YOKE — CORRODED (NR 2 PYLON)

NR 2 ENGINE FORWARD MOUNT YOKE ASSEMBLY WAS CORRODED. REPLACED YOKE ASSEMBY IAW DC9 MM 71-20-3.

Part: SWITCH — MALFUNCTIONED (LT MLG WW)

AFTER TAKEOFF, THE GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. RECYCLED LANDING GEAR, LIGHT EXTINGUISHED. REPLACED LEFT GEAR DOOR SWITCH.

Part: BULB — FAILED (LDG GEAR DOOR)

AFTER GEAR RETRACTION, GEAR DOOR OPEN LIGHT ILLUMINATED. RECYCLED GEAR AND LIGHT WENT OUT. CHECKED LANDING GEAR DOORS AND SWITCHES, NO DEFECTS NOTED. RELAMPED THE OPEN DOOR LIGHT.

Part: TEE CAP — CORRODED (LT HORIZ STAB)

DURING C-CHECK, FOUND LEFT HORIZONTAL STABILIZER AFT UPPER TEE CAP EXFOLIATED AT HINGE POINT, AT STATION 204. REPAIRED TEE CAP IAW ABX REA D955-23948 MR.

Part: ANGLE — CRACKED (NR 2 PYLON)

DURING C-CHECK, FOUND RIGHT PYLON STRUCTURE CRACKED AT STATION 1033 OUTBOARD OF PANEL 8206 BOTTOM OF PYLON. REPLACED ANGLE IAW DC9 SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 937)

DURING C-CHECK, FOUND UPPER CARGO COMPARTMENT FLOORBEAM AT STATION 937 LOWER TEE CAP CORRODED BEYOND LIMITS BETWEEN BL 0 AND LBL 40 TO 54. REPAIRED FLOORBEAM IAW ABX REA D953-24050 MR.

Part: INTERCOSTAL — CORRODED (BS 992-945)

DURING C-CHECK, FOUND INTERCOSTAL AT STATION 929 TO 945 AND LONGERON 11L CORRODED BEYOND LIMITS. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: INTERCOSTAL — CORRODED (BS 465-484)

DURING C-CHECK, FOUND INTERCOSTAL AT STATION 465 TO 484 AND LONGERON 6 L CORRODED BEYOND LIMITS. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FLOORBEAM — CORRODED (LT MLG WW)

DURING C-CHECK, FOUND THE LOWER TEE CAP OF THE FLOORBEAM THAT ATTACHES TO THE TOP OF THE AFT BULKHEAD OF THE LEFT WHEEL WELL EXFOLIATED. REPAIRED IAW ABX REA D953-23942-MR.

Part: FITTING — CRACKED (BS 775)

DURING C-CHECK, FOUND FLOORBEAM VERTICAL SUPPORT LOWER FITING AT STATION 775 AND LONGERON 23L CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-05.

Part: LONGERON — CRACKED (BS 446)

DURING C-CHECK, FOUND LONGERON 2R CRACKED AT STATION 446. REPAIRED LONGERON IAW DC9 SRM 53-02-00.

Part: LONGERON — CRACKED (BS 945)

DURING C-CHECK, FOUND LONGERON 16L CRACKED AT HI-LOCK STATION 945. REPAIRED LONGERON IAW ABX DC9 SSRM DWG K05864.

Part: INTERCOSTAL — CORRODED (BS 218-237)

DURING C-CHECK, FOUND INTERCOSTAL AT STATION 218-237 AND LONGERON 28R CORRODED BEYOND LIMITS. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FRAME — CRACKED (BS 484)

DURING C-CHECK, FOUND FUSELAGE FRAME CRACKED AT STATION 484, AND LONGERON 29L. REPLACED FRAME FROM LONGERONS 28L TO 28R IAW DC9 53-03-00.

Part: INTERCOSTAL — CORRODED (BS 870-889)

DURING C-CHECK, FOUND INTERCOSTAL AT LONGERON 8R STATION 870-889 CORRODED BEYOND LIMITS. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2 AND 51-30-3.

Part: INTERCOSTAL — CORRODED (BS 218-237)

DURING C-CHECK, FOUND INTERCOSTAL AT STATION 218-237 AND LONGERON 28L CORRODED BEYOND LIMITS. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: ANGLE — CRACKED (BS 718)

DURING C-CHECK, FOUND FRAME STATION 718 SUPPORT ANGLE CRACKED ON LONGERON 20. REPLACED ANGLE IAW DC9 SRM 51-30-1 AND DACO DWG 9958209.

Part: FITTING — CRACKED (BS 332)

DURING C-CHECK, FOUND FUSELAGE FRAME FITTING CRACKED AT STATION 332 NEAR LONGERON 24 RT. REPLACED FRAME FITTING IAW DC9 SRM 51-30-5.

Part: ANGLE — CRACKED (SERVICE DOOR)

DURING C-CHECK, FOUND ATTACH ANGLE CRACKED AT FWD END OF SERVICE DOOR UPPER MOST BEAM. REPLACED ANGLE IAW DC9 SRM 51-30-52 AND 51-30-1.

Part: WARNING SWITCH — MALFUNCTIONED (LT MLG)

WHEN GEAR RETRACTED, LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLED GEAR, LIGHT WENT OUT WHEN GEAR DOWN. LIGHT ILLUMINATED AGAIN WHEN GEAR RETRACTED. LANDING WAS UNEVENTFUL. REPLACED MLG POSITION WARNING SWITCH, OPS CHECKED GOOD IAW DC9 MM 32-60-01.

Part: SPAR CAP — CRACKED (RT TE FLAP)

DURING C-CHECK, THE FLAP LOWER SPAR CAP WAS FOUND CRACKED AT STATION 295, NR BF-667. THE FLAP WAS REPAIRED IAW REA D957-17300-MR.

Part: FITTING — CORRODED (CENTER FUSELAGE)

DURING C-CHECK, THE CENTER FUEL TANK OUTBOARD ATTACH FITTING WAS FOUND CORRODED, NR BF-399. THE FITTING WAS REPLACED IAW DC9 SRM.

Part: CUSP WEB — CRACKED (BS 960)

DURING C-CHECK, THE RIGHT CUSP WEB AT STATION 960 WAS FOUND CRACKED, NR BF-698. THE WEB REPLACED IAW DC9 SRM.

Part: CUSP WEB — CRACKED (BS 960)

DURING C-CHECK, A CUSP WEB AT STATION 960 WAS FOUND CRACKED, NR BF-698. THE CUSP WEB WAS REPAIRED IAW DC-9 SRM.

Part: CUSP WEB — CRACKED (BS 965)

DURING C-CHECK, THE RIGHT CUSP WEB AT STATION 965 WAS FOUND CRACKED, NR BF-631. THE WEB WAS REPLACED IAW DC9 SRM.

Part: SUPPORT — CORRODED (BS 980)

DURING C-CHECK, A FLOOR SUPPORT AT STATION 980 RBL 22 WAS FOUND CORRODED, NR BF-692. THE SUPPORT WAS REPAIRED IAW DC9 SRM.

Part: VANE — DELAMINATED (LT TE FLAP)

DURING C-CHECK, THE INBOARD FIXED VANE UPPER SURFACE WAS FOUND DELAMINATED, NR AF-851. THE VANE WAS REPLACED IAW DC9 MM.

Part: PANEL — DELAMINATED (RT WING)

DURING C-CHECK, BONDED PANEL 1249 WAS FOUND DELAMINATED, NR BF-421. THE PANEL WAS REPLACED IAW DC9 SRM.

Part: RIB — CRACKED (LT TE FLAP)

DURING C-CHECK, THE LEFT WING FLAP RIB AT THE OUTBOARD HINGE WAS FOUND CRACKED, NR AF-937. THE RIB WAS REPAIRED IAW DC9 SRM.

Part: PANEL — DELAMINATED (RT WING)

DURING C-CHECK, BONDED PANEL 1246 WAS FOUND DELAMINATED, NR BF-419. THE PANEL WAS REPLACED IAW DC9 SRM.

Part: VANE — CORRODED (LT TE FLAP)

DURING C-CHECK, THE LEFT WING INBOARD FIXED VANE WAS FOUND CORRODED, NR AF-851. THE VANE WAS REPLACED IAW DC-9 MM.

Part: VANE — DELAMINATED (LT TE FLAP)

DURING C-CHECK, THE LEFT WING FORWARD MOVEABLE VANE WAS FOUND DELAMINATED, NR AF-850. THE VANE WAS REPLACED IAW DC9 MM.

Part: BRACKETS — CRACKED (RT WING)

DURING C-CHECK, THE RIGHT WING INBOARD AND OUTBOARD HINGE ATTACH BRACKETS WERE FOUND CRACKED AT STATION 353, NR AF-904. THE BRACKETS WERE REPLACED IAW DC9 SRM.

Part: VANE — DELAMINATED (LT TE FLAP)

DURING C-CHECK, THE FORWARD MOVEABLE VANE UPPER SURFACE WAS FOUND DELAMINATED, NR AF-850. THE VANE WAS REPLACED IAW DC9 MM.

Part: FORMER — CRACKED (BS 980)

DURING C-CHECK, A FORMER AT STATION 980 BELOW LONGERON 14 RIGHT WAS FOUND CRACKED, NR BF-601. THE FORMER WAS REPLACED IAW DC9 SRM.

Part: FORMER — CRACKED (BS 980)

DURING C-CHECK, A FORMER AT STA 980 LONGERON 14 LT WAS FOUND CRACKED, NR BF-60. THE FORMER WAS REPLACED IAW DC9 SRM.

Part: BULKHEAD CLIP — CRACKED (LT PYLON)

DURING C-CHECK, A CLIP ON THE LT PYLON BULKHEAD STA 965, WAS FOUND CRACKED. THE CLIP WAS REPLACED IAW DC SRM.

Part: FITTING — CORRODED (BS 980)

DURING C-CHECK, A FRAME FITTING AT STATION 980, RIGHT CUSP WAS FOUND CORRODED, NR BF-598. THE FITTING WAS REPLACED IAW DC-9 SRM.

Part: FORMER — CRACKED (BS 980)

DURING C-CHECK, THE FORMER AT STA 980 AT LONG 16LT WAS FOUND CRACKED. THE FORMER WAS REPLACED IAW DC SRM.

Part: SKIN — CRACKED (BS 965)

DURING C-CHECK, FUSELAGE SKIN AT STATION 965 BELOW LONGERON 16 RIGHT WAS FOUND CRACKED, NR BF-495. THE SKIN WAS REPAIRED IAW REA DC953-17291.

Part: LONGERON — CRACKED (BS 980)

DURING C-CHECK, THE LONGERON AT STA 980 LONG 17LT, WAS FOUND CRACKED. THE LONGERON WAS REPLACED IAW DC9 SRM.

Part: TAB — DENTED (LT AILERON)

THE LEFT WING AILERON CONTROL TAB HAD SEVERAL DENTS ON THE UPPER SURFACE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.

Part: FRAME — CORRODED (BS 980)

DURING C-CHECK, A FRAME AT STATION 980 LONGERON 18 RIGHT WAS FOUND CORRODED, NR BF-596. THE FRAME WAS REPAIRED IAW DC-9 SRM.

Part: FORMER — CRACKED (BS 980)

DURING C-CHECK, A FORMER AT STATION 980 LONGERON 16 RIGHT WAS FOUND CRACKED, NR BF-597. THE FORMER WAS REPLACED IAW DC-9 SRM.

Part: SKIN — CRACKED (BS 960)

DURING C-CHECK, THE FUSELAGE SKIN WAS FOUND CRACKED AT STATION 960 BELOW LONGERON 16 RIGHT, NR BF-665. THE SKIN WAS REPAIRED IAW REA D953-17291-MR.

Part: BULKHEAD CLIP — CRACKED (BS 965)

DURING C-CHECK, A CLIP WAS FOUND CRACKED AT THE PYLON BULKHEAD STATION 965 LONGERON 17 RT, NR BF-600. THE CLIP WAS REPLACED IAW DC9 SRM.

Part: FRAME — CORRODED (BS 980)

DURING C-CHECK, THE FRAME AT STA 980 LONG 18RT TO 6RT WAS FOUND CORRODED. THE FRAME WAS REPLACED IAW DC9 SRM.

Part: FITTING — CORRODED (BS 980)

DURING C-CHECK, A FRAME FITTING AT STATION 980 RIGHT CUSP WAS FOUND CORRODED, NR BF-598. THE FITTING WAS REPLACED IAW DC9 SRM.

Part: SKIN — CRACKED (BS 965)

DURING C-CHECK, FUSELAGE SKIN AT STATION 965 BELOW LONGERON 16 RIGHT WAS FOUND CRACKED, NR BF-665. THE SKIN WAS REPAIRED IAW REA DC953-17291.

Part: LONGERON — CRACKED (BS 980)

DURING C-CHECK, THE LONGERON AT STATION 980 AND 17 RIGHT WERE FOUND CRACKED, NR BF-622. THE LONGERON WAS REPLACED IAW DC-9 SRM.

Part: BULKHEAD CLIP — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, A CLIP WAS FOUND CRACKED AT THE AFT PRESSURE BULKHEAD LONGERON 17 RIGHT, NR BF-624. THE CLIP WAS REPAIRED IAW DC9 SRM.

Part: INTERCOSTAL — CORRODED (BS 980-996)

DURING C-CHECK, AN INTERCOSTAL STA 980 TO 996 BELOW LONG 124RT WAS FOUND CORRODED. THE INTERCOSTAL WAS REPLACED IAW DC SRM.

Part: ANGLE — CRACKED (RT WING)

DURING C-CHECK, THE RIGHT WING LOWER ATTACH OF OUTBOARD EXPANSION JOINT WAS FOUND CRACKED, NR AF-905. THE ANGLE WAS REPLACED IAW DC-9 SRM.

Part: INTERCOSTAL — CORRODED (BS 980-996)

DURING C-CHECK, AN INTERCOSTAL AT STATION 980 TO 996 WAS FOUND CORRODED AT LONGERON 14 LT, NR BF-602. THE INTERCOSTAL WAS REPLACED IAW DC9 SRM.

Part: SPAR — CRACKED (RT TE FLAP)

DURING C-CHECK, THE FLAP SPAR CAP AT STATION XFLS 298 WAS FOUND CRACKED, NR BF-667. THE SPAR WAS REPAIRED IAW REA DC957-17300-MR.

Part: BRACKET — CRACKED (RT WING)

DURING C-CHECK, THE FLAP OUTBOARD EXPANSION JOINT BRACKET WAS FOUND CRACKED, NR AF-905. THE BRACKETS WERE REPLACED IAW DC-9 SRM.

Part: BULKHEAD CLIP — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, A CLIP WAS FOUND CRACKED AT THE AFT PRESSURE BULKHEAD LONGERON 12 RIGHT, NR BF-625. THE CLIP WAS REPAIRED IAW DC9 SRM.

Part: LEADING EDGE — CORRODED (RT TE FLAP)

DURING C-CHECK, THE FLAP LEADING EDGE SECTION INTERIOR BONDED DOUBLER WAS FOUND CORRODED, NR BF-564. THE LEADING EDGE WAS REPLACED IAW DC9 SRM.

Part: BULKHEAD CLIP — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, A CLIP WAS FOUND CRACKED AT THE AFT PRESSURE BULKHEAD LONGERON 14 LEFT, NR BF-627. THE CLIP WAS REPAIRED IAW DC9 SRM.

Part: BULKHEAD CLIP — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, A CLIP WAS FOUND CRACKED AT THE AFT PRESSURE BULKHEAD LONGERON 15 LEFT, NR BF-626. THE CLIP WAS REPAIRED IAW DC9 SRM.

Part: TAB — DENTED (LT AILERON)

THE LEFT AILERON TAB HAD NUMEROUS DENTS ON BOTH THE UPPER AND LOWER SURFACES. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.

Part: LONGERON — CRACKED (BS 980)

DURING C-CHECK, LONGERON 17 LEFT AT STATION 980 WAS FOUND CRACKED, NR BF-599. THE LONGERON WAS REPLACED IAW DC-9 SRM.

Part: FITTING — CRACKED (RT WING)

DURING C-CHECK, THE NR 2 SLAT TRACK INBOARD SUPPORT FITTING WAS FOUND CRACKED, NR BF-259. THE FITTING WAS REPLACED IAW DC-9 SRM.

Part: SEAT TRACK — CORRODED (BS 957-965)

DURING C-CHECK, THE SEAT TRACK FROM STATION 957 TO 965 WAS FOUND EXFOLIATED AT LBL 44, NR BF-543. THE SEAT TRACK WAS REPLACED IAW DC-9 SRM.

Part: LONGERON — CORRODED (BS 443)

DURING C-CHECK, A WEB AT STATION 443 LONGERON 14 LT WAS FOUND CORRODED, NB BF-637. THE WEB WAS REPLACED IAW DC-9 SRM.

Part: LONGERON — CRACKED (BS 294)

DURING C-CHECK, THE LONGERON AT STA 294 LONG 17RT, WAS FOUND CRACKED. THE LONGERON WAS REPLACED IAW DC9 SRM.

Part: LONGERON — CRACKED (BS 313)

DURING C-CHECK, THE LONGERON AT STA 313 LONG 17RT WAS FOUND CRACKED. THE LONGERON WAS REPLACED IAW DC9 SRM.

Part: FLOORBEAM — CORRODED (BS 980)

DURING C-CHECK, A FLOORBEAM AT STATION 980 RBL 22.0 WAS FOUND CORRODED, NR BF-692. THE FLOORBEAM WAS REPAIRED IAW DC-9 SRM.

Part: WEB — CRACKED (BS 965)

DURING C-CHECK, THE RIGHT CUSP WEB WAS FOUND CRACKED AT STATION 965, NR BF-631. THE WEB WAS REPLACED IAW DC-9 SRM.

Part: RIB — CRACKED (LT WING)

DURING C-CHECK, THE LEADING EDGE RIB INBOARD OF DE-ICE DUCT WAS FOUND CRACKED, NR AF-793. THE RIB WAS REPAIRED IAW DC9 SRM.

Part: LONGERON — CRACKED (BS 980)

DURING C-CHECK, LONGERON 17 RIGHT AT STATION 980 WAS FOUND CRACKED, NR BF-622. THE LONGERON WAS REPLACED IAW DC-9 SRM.

Part: LONGERON — CRACKED (BS 408)

DURING C-CHECK, LONGERON 17 RIGHT AT STATION 408 WAS FOUND CRACKED, NR BF-378. THE LONGERON WAS REPLACED IAW DC-9 SRM.

Part: FITTING — CORRODED (BS 598)

DURING C-CHECK, THE CENTER FUEL TANK UPPER OUTBOARD ATTACH FITTING WAS FOUND CORRODED AT STATION 598 RIGHT, NR BF-399. THE FITTING WAS REPLACED IAW DC-9 SRM.

Part: ANGLE — CRACKED (BS 655)

DURING C-CHECK, THE CENTER FUEL TANK UPPER ATTACH ANGLE WAS FOUND CRACKED AT STATION 655 LBL, NR BF-422. THE ANGLE WAS REPLACED IAW DC-9 SRM AND REA D957-17305-MR.

Part: LONGERON — CRACKED (BS 294)

DURING C-CHECK, LONGERON 17 RIGHT AT STATON 294 WAS FOUND CRACKED, NR BF-375. THE LONGERON WAS REPLACED IAW DC-9 SRM.

Part: LONGERON — CRACKED (BS 313)

DURING C-CHECK, LONGERON 17 RIGHT AT STATION 313 WAS FOUND CRACKED, NR BF-376. THE LONGERON WAS REPLACED IAW DC-9 SRM.

Part: LONGERON — CRACKED (BS 389)

DURING C-CHECK, LONGERON 17 RIGHT AT STATION 389 WAS FOUND CRACKED, NR BF-377. THE LONGERON WAS REPLACED IAW DC-9 SRM.

Part: WEB — CORRODED (BS 775-794)

DURING C-CHECK, THE RIGHT CUSP WEB AT STATION 775 TO 794 WAS FOUND CORRODED, NR BF-495. THE WEB WAS REPAIRED IAW DC-9 SRM.

Part: LINKAGE — WORN (RT MLG DOOR)

DURING C-CHECK, THE LEFT WING LEADING EDGE RIB WAS FOUND CRACKED INBOARD OF ANTI-ICE DUCT, NR AF-798. THE RIB WAS REPAIRED IAW DC9 SRM.

Part: CUSP WEB — CORRODED (BS 775-794)

DURING C-CHECK, THE RIGHT CUSP WEB FROM STATION 775 TO 794 WAS FOUND CORRODED, NR BF-495. THE WEB WAS REPAIRED IAW DC9 SRM.

Part: WEB — CORRODED (BS 443)

DURING C-CHECK, THE WEB AT STA 443 AT LONG 14LT WAS FOUND CORRODED. THE WEB WAS REPAIRED IAW DC SRM.

Part: VANE — DELAMINATED (RT TE FLAP)

THE RIGHT WING FORWARD FLAP VANE UPPER SURFACE WAS DELAMINATED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.

Part: HINGE — WORN (LT MLG DOOR)

DURING C-CHECK, THE LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGE WAS FOUND WORN, NR AF-843. THE HINGE WAS REPLACED IAW DC-9 SRM.

Part: VANE — DELAMINATED (LT TE FLAP)

LEFT WING FIXED VANE DELAMINATED. REPLACED ALL HONEYCOMB CORE DOUBLERS AND SKIN.

Part: BRACKET — CRACKED (RT WING)

DURING C-CHECK, THE FLAP OUTBOARD HINGE ATTACH BRACKET WAS FOUND CRACKED, NR AF-904. THE BRACKETS WERE REPLACED IAW DC-9 SRM.

Part: LONGERON — CRACKED (BS 389)

DURING C-CHECK, THE LONGERON AT STA 389 LONG 17RT, WAS FOUND CRACKED. THE LONGERON WAS REPLACED IAW DC9 SRM.

Part: LONGERON — CRACKED (BS 408)

DURING C-CHECK, THE LONGERON AT STA 408 LONG 17RT, WAS FOUND CRACKED. THE LONGERON WAS REPLACED IAW DC9 SRM.

Part: ANGLE — CRACKED (MLG DOOR)

DURING C-CHECK, THE LANDING GEAR INBOARD DOOR UPPER ATTACH ANGLE WAS FOUND CRACKED, NR BF-859. THE ANGLE WAS REPAIRED IAW ABX DRAWING K05818.

Part: SPLICE — CRACKED (LT WING)

DURING C-CHECK, THE LEADING EDGE SKIN SPLICE OUTBOARD OF NR 6 TRACK WAS FOUND CRACKED, NR AF-796. THE RIB WAS REPAIRED IAW DC9 SRM.

Part: SPLICE — CRACKED (LT WING)

DURING C-CHECK, THE WING LEADING EDGE SKIN SPLICE WAS FOUND CRACKED JUST OUTBOARD OF NR 6 SLAT TRACK, NR AF-796. THE CRACK WAS REPAIRED IAW DC-9 SRM.

Part: UPLATCH — LACK OF LUBE (MLG DOORS)

GEAR DOOR OPEN LIGHT STAYED ON AFTER LOWERING GEAR. WE RECYCLED GEAR AND LIGHT WENT OUT AFTER THE GEAR HAD BEEN DOWN FOR APPROXIMATELY 30 SECONDS. CLEANED AND LUBED MAIN LANDING GEAR DOOR UPLATCH HOOKS AND ROLLERS. OPERATIONAL CHECKED THE GEAR DOOR UNSAFE SWITCHES AND GEAR DOORS IAW DC-9 MM.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS INOPERATIVE. FOUND CIRCUIT BREAKER POPPED. REPLACED EMERGENCY LIGHT POWER SUPPLY.

Part: DNLOCK SWITCH — DEFECTIVE (NLG)

NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AND NO NOSE GEAR GREEN LIGHT. RECYCLED GEAR AND COMPLETED GEAR ABNORMAL CHECKLIST. REPLACED NOSE LANDING GEAR DOWNLOCK SWITCH AND REMOVED OVERCENTER LINKAGE SHIMS AS PER MM SUPP 32-60-01 AND MM 32-21-3. OPS CHECKED GOOD ON GROUND AND GEAR SWING.

Part: BUSHING — WORN (RT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR DOOR ARTICULATING DOOR LINKAGE WORN. REPLACED BUSHINGS IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: BUSHING — WORN (LT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGES WORN. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: FITTING — WORN (LT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR ARTICULATING DOOR LINKAGE WORN. REPLACED FITTING IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: INDICATOR WIRE — OPEN (LT MLG)

DURING CLIMB, LEFT GEAR UNSAFE LIGHT DID NOT ILLUMINATE DURING GEAR RETRACTION. DID NOT ILLUMINATE DURING IDLE FLIGHT WHILE IN DESCENT. FOUND WIRE 1G206024 OPEN. REPLACED WIRE IAW DC-9 WDM 32-61-0. LANDING GEAR SYSTEM OPS CHECKED NORMAL IAW DC-9 SUPP MM 32-60-00.

Part: FRAME — CORRODED (FS 503)

DURING C-CHECK INSPECTION, FOUND CORROSION ON THE ROLLED ZEE FRAME AT STA 530 ON THE UPPER FLANGE AT LONGERON 30. REPAIRED FRAME IAW ABX REA D953-11525-MR.

Part: SKIN — DAMAGED (FWD FUSELAGE)

DURING C-CHECK INSPECTION, A PREVIOUSLY INSTALLED DOUBLE STACK REPAIR WAS REMOVED FROM THE LOWER AFT CORNER OF THE FORWARD ENTRY DOOR CUTOUT ON THE FUSELAGE SKIN. THE REPAIR HAD BEEN CLASSIFIED AS TEMPORARY. REPAIRED SKIN IAW ABX REA D953-11400-MR.

Part: FRAME — CORRODED (FS 134)

DURING C-CHECK INSPECTION, FOUND CORROSION ON THE FUSELAGE FRAME AT STATION 134 BETWEEN LONGERONS 24R AND 25R. REPAIRED FRAME IAW ABX REA D953-11505-MR.

Part: SKIN — DAMAGED (FS 718)

DURING C-CHECK INSPECTION, THE FUSELAGE SKIN WAS FOUND TO HAVE A DOUBLE DRILLED HOLE JUST FORWARD OF STA 718R AT CUSP. REPAIRED SKIN IAW ABX REA D953-11414-MR.

Part: SKIN — CORRODED (WS 20)

DURING C-CHECK INSPECTION, FOUND CORROSION ON THE RIGHT WING UPPER SKIN AT XCW 20. REPAIRED IAW ABX REA D957-11411-MR.

Part: INTERCOSTAL — CRACKED (FS 503-522)

DURING C-CHECK INSPECTION, AN INTERCOSTAL WAS FOUND CRACKED AT STA 503 LONGERON 19R. REPLACED IAW DC-9 SRM 51-30-5.

Part: FITTING — CRACKED (FS 370)

DURING C-CHECK INSPECTION, A BATHTUB FITTING WAS FOUND CRACKED AT STA 370 LONGERON 22R. REPLACED IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: SKIN — DAMAGED (FS 367-341)

DURING C-CHECK INSPECTION, A CREASE WAS FOUND IN THE FUSELAGE SKIN JUST FORWARD OF THE FORWARD LOWER CARGO DOOR, BETWEEN LONGERONS 26R AND 25R. THE CREASE SPANNED FROM STATIONS 367 TO 341. REPAIRED THE SKIN IAW ABX REA D953-11408-MR.

Part: FLOOR PANEL — CORRODED (COCKPIT)

DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE COCKPIT CENTER FLOOR PANEL. REPLACED THE PANEL IAW DC-9 SRM 51-30-2, 51-30-1.

Part: SUPPORT — CRACKED (FS 598)

DURING C-CHECK INSPECTION, A MAIN FLOOR SUPPORT WAS FOUND CRACKED AT STA 598 LBL 36. REPLACED IAW DC-9 SRM 51-30-5.

Part: FITTING — CRACKED (FS 566)

DURING C-CHECK INSPECTION, FOUND LONGERON 28R END FITTING CRACKED AT STA 566. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-2.

Part: FITTING — CRACKED (FS 583)

DURING C-CHECK INSPECTION, FOUND LONGERON 29L END FITTING CRACKED AT STA 583. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1.

Part: LONGERON — CRACKED (FS 375-579)

DURING C-CHECK INSPECTION, FOUND LONGERON 30 CRACKED AT STA 415. REPLACED LONGERON IAW DC-9 SRM 51-30-5, 51-30-7 AND 51-30-1.

Part: FLOORBEAM — CORRODED (FS 756-737)

DURING C-CHECK INSPECTION, FOUND CORROSION ON THE LOWER FLOORBEAM ATTACH TEE AT STA 756, FROM APPROXIMATELY X EQUALS -18 TO OUTBOARD END. REPAIRED IAW ABX REA D953-11425-MR.

Part: LONGERON — CRACKED (FS 475-579)

DURING C-CHECK INSPECTION, FOUND LONGERON 30 CRACKED AT STA 579. REPLACED LONGERON IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: PANEL — CORRODED (FS 751)

DURING C-CHECK INSPECTION, FOUND CORROSION ON THE UPPER SIDE OF THE PRESSURE PANEL AT X EQUALS A D953-11427-MR.

Part: LINK — CRACKED (RT SPOILER)

DURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 85-01-03, FOUND THE RIGHT WING INBOARD SPOILER DRIVE LINK CRACKED. REPLACED LINK IAW DC-9 MM 27-61-1.

Part: BEAM — CORRODED (FS 737)

DURING C-CHECK INSPECTION, FOUND CORROSION ON A FLOORBEAM AT STA 737R RBL 44. REPAIRED BEAM IAW ABX REA D953-11422-MR.

Part: FITTING — CRACKED (RT SPOILER)

DURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 85-01-03, FOUND THE RIGHT WING INBOARD SPOILER AFT ATTACH FITTING CRACKED. REPLACED THE FITTING IAW DC-9 MM 27-61-1.

Part: LINK — CRACKED (LT SPOILER)

DURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 85-01-03, FOUND THE LEFT WING INBOARD SPOILER DRIVE LINK CRACKED. REPLACED LINK IAW DC-9 OVERHAUL MANUAL 27-61-1.

Part: LINK — CRACKED (RT SPOILER)

DURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 85-01-03, FOUND THE RIGHT WING OUTBOARD SPOILER DRIVE LINK CRACKED. REPLACED THE LINK IAW DC-9 MM 27-61-1.

Part: LINK — CRACKED (LT SPOILER)

DURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 85-01-03, FOUND THE LEFT WING OUTBOARD SPOILER DRIVE LINK CRACKED. REPLACED IAW DC-9 SUPP MM 27-61-1.

Part: WIRE — OPEN (RT MLG)

WHEN LANDING GEAR EXTENDED, RIGHT GEAR UNSAFE AND RIGHT LANDING GEAR LIGHTS DID NOT ILLUMINATE. RECYCLED GEAR. RIGHT LANDING GEAR UNSAFE LIGHT DID NOT ILLUMINATE. RIGHT LANDING GEAR LIGHT ILLUMINATED. REPAIRED WIRE NR 2G206E24 NEAR TERMINAL BOARD S3-66 PER STANDARD PROCEDURES AND PRINT NR 32-61-00. CYCLED GEAR. OPS CHECKED GOOD.