N901AX

Part: COALESCER BAG — CONTAMINATED (AIR DISTRIBUTION) · airframe 55,258 hrs · 60,446 cycles

VERY STRONG ODOR (MUSTY) WAS PRESENT FROM TAKE-OFF THROUGH FIRST 20 TO 30 MINUTES OF FLIGHT. CLOSING A/C VENTS WOULD DECREASE THE INTENSITY OF THE ODOR BUT WOULDN'T ELIMINATE IT. REPLACED BOTH WATER SEPARATOR COALESER BAGS IAW DC-9 MM 21-20-02-2-0001.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,002 hrs · 60,159 cycles

CANTED FRAME 1137 HAD 2 EACH CRACKS COMMON TO STIFFENERS AT 11 AND 1 O'CLOCK POSITIONS. REPLACED LEFT AND RIGHT FRAMES IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: FORMER — CRACKED (LEFT WING L/E) · airframe 55,002 hrs · 60,159 cycles

3RD LEADING EDGE NOSE RIB, OUTBOARD OF #11 SLAT TRACK, WAS CRACKED AT FASTENER, LOWER FORWARD END. REPLACED LEFT WING LEADING EDGE RIB FORMER IAW DC-9 SRM 51-30-2, 51-30-5 AND 51-10-3.

Part: RIB — CRACKED (LT WING) · airframe 55,002 hrs · 60,159 cycles

CRACK INDICATION ON AFT END OF LEADING EDGE NOSE RIB, INBOARD OF NR 10 SLAT TRACK. REPAIRED NOSE RIB IAW REA D957-44307-MR.

Part: RIB — CRACKED (LT WING) · airframe 55,002 hrs · 60,159 cycles

4 EACH LEADING EDGE NOSE RIBS BETWEEN TRACKS 10 AND 11, HAD CRACK INDICATIONS AT AFT EDGES. REPAIRED NOSE RIBS AT STATIONS XRS 466-473-479-491 IAW REA D957-44307-MR.

Part: LIGHT — SHORTED (COCKPIT) · airframe 54,446 hrs · 59,585 cycles

THE FIRST OFFICERS OVERHEAD MAP LIGHT WENT OUT AND CAME BACK ON. A BURNING ELECTRICAL SMELL WAS NOTED. THE ASSOCIATED MAP LIGHT CIRCUIT BREAKER OPENED, NO FURTHER PROBLEMS WERE NOTED. MAINTENANCE INSPECTED AND FOUND EVIDENCE OF THE LIGHT ASSY TOUCHING A CAM LOCK RECEPTACLE WHEN TURNED EXCESSIVELY. MAINTENANCE REPOSITIONED THE LIGHT ASSY AS REQUIRED TO PREVENT CONTACT AND RETURNED THE AIRCRAFT TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES IAW DC9 AMM 33-53-02-04.

Part: JACKSCREW — CORRODED (HORIZ STAB) · airframe 54,173 hrs · 59,286 cycles

THE HORIZONTAL STABILIZER JACKSCREW ASSEMBLY WAS FOUND TO HAVE PITTING CORROSION ON THE THREADED AREA. MAINTENANCE REPLACED THE JACKSCREW ASSEMBLY IAW DC-9 MM 27-40-01.

Part: SEPARATOR — CONTAMINATED (LEFT) · airframe 53,858 hrs · 58,971 cycles

DURING TAKEOFF ROLL BETWEEN V1 AND VR THE COCKPIT FILLED WITH A STRONG BURNING ODER. THE CREW ABORTED TAKEOFF AND RETURNED TO BLOCK. MAINTENANCE INSPECTED THE NUMBER ONE AND NUMBER TWO ENGINE INLETS, OUTLETS AND PNEUMATIC DUCTS FOR RESIDUES. MAINTENANCE INSPECTED LEFT AND RIGHT ACM DUCTING. NO DEFECTS FOUND. GROUND RAN BOTH ENGINES AND DETERMINED ODER WAS GENERATING FROM THE LEFT AIRCONDITIONING PACK. DEFERRED LEFT AIRCONDITIONING PACK IAW 21-1A.

Part: LOCK — JAMMED (COCKPIT DOOR) · airframe 53,832 hrs · 58,945 cycles

FLIGHT DECK DOOR LOCK JAMMED IN THE LOCKED AND CLOSED POSITION. MAINTENANCE INSPECTED TIGHTENED, AND LUBRICATED THE DOOR LOCK, IAW DC9 MM 52-00-00. OPS CHECKED GOOD.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 53,773 hrs · 58,887 cycles

LEFT FLAP INBOARD FIXED VANE WAS DELAMINATED 280 SQ IN ON UPPER SURFACE AND 145 SQIN ON LOWER SURFACE. REPLACED FIXED VANE IAW DC9 MM.

Part: PIN — CORRODED (HORIZONTAL STAB) · airframe 53,773 hrs · 58,887 cycles

HORIZONTAL STABILIZER RING ASSY WAS FOUND TO HAVE CORRODED PIN ASSYS AFTER SUPPORTASSY WAS DISASSEMBLED. REPLACED PIN ASSYS IAW DC9 OHM 27-41-1.

Part: RING ASSEMBLY — CORRODED (HORIZONTAL STAB) · airframe 53,773 hrs · 58,887 cycles

HORIZONTAL STABILIZER RING ASSY WAS FOUND TO HAVE CORRODED BUSHINGS WHEN SUPPORT ASSY WAS DISASSEMBLED. REPLACED BUSHINGS IAW DC9 OHM 27-41-1.

Part: FRAME — CRACKED (RT MLG WW) · airframe 53,773 hrs · 58,887 cycles

RIGHT WHEEL WELL MAIN FRAME 718 CRACKED AT THE FWD INBOARD AND OUTBOARD FLANGES AND AT THE AFT FLANGE. REPAIRED IAW ABX REA D953-38639MR.

Part: STRUCTURE — CRACKED (CABIN) · airframe 53,773 hrs · 58,887 cycles

CRACK AT END OF NR 3 RADIAL ON NR 6 T-CAP APPROXIMATELY .25 INCH LENGTH. REPLACED NR 6 T-CAP IAW ABX EA 53120037-006.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,773 hrs · 58,887 cycles

INTERCOSTAL AT LONGERON 29 LEFT CRACKED BETWEEN STATION 351 AND 370. REPLACED INTERCOSTAL (P/N 9957911-3AX) IAW DC9 SRM 51-30-2.

Part: RETAINER — CRACKED (CABIN) · airframe 53,773 hrs · 58,887 cycles

UPPER FORWARD CORNER WINDOW RETAINER RING WAS CRACKED JUST AFT OF FRAME 598. REPAIRED RETAINER IAW DC9 SRM K07226.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 53,773 hrs · 58,887 cycles

LONGERON 2 LEFT CRACKED AT FUSELAGE STA 200. INSTALLED NEW SECTION OF LONGERON FROM STATION 190 - 212 IAW DC9 SRM 53-02.

Part: WINDOW — STUCK (COCKPIT) · airframe 53,707 hrs · 58,827 cycles

CAPTAIN''''S CLEARVIEW WINDOW WILL NOT OPEN. FOUND WINDOW LINKAGE STICKING. OPERATED WINDOW SEVERAL TIMES. WINDOW OPENS NORMALLY AT THIS TIME.

Part: BATTERY — DISCHARGED (CABIN)

CABIN EMERGENCY LIGHTS WOULD NOT ILLUMINATE WITH SWITCH IN ON POSITION. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES.

Part: FRAME — CORRODED (BS 1039)

STATION 1039 CORRODED AFT OF APU ENCLOSURE AT RBL 18. REPAIRED IAW DC9 SRM 53-01.

Part: FITTING — CRACKED (LEFT MLG)

LEFT AUX GEAR FITTING CRACKED. REPLACED LEFT AUX GEAR FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: FITTING — CRACKED (RIGHT MLG)

RIGHT AUX GEAR FITTING CRACKED. REPLACED RIGHT AUX GEAR FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: INTERCOSTAL — CRACKED (BS 1076)

INTERCOSTAL CRACKED AT STATION 1076 AND LONGERON 28 RIGHT. REPAIRED IAW DC9 SRM 53-01.

Part: GENERATOR — FAILED (LT ENGINE)

EN ROUTE, ALL AIRCRAFT LIGHTING AND RADAR PICTURE INTENSITY STARTED FLUCTUATING. LEFT GENERATOR VOLTS AND FREQS WERE FLUCTUATING, WIND SHEAR ANNUNCIATOR AND WARNING CAME ON. ALL ELECTRICAL POWER FAILED. EMERGENCY POWER REMAINED ON. AC CROSS-TIE ILLUMINATED. REPLACED LEFT ENGINE DRIVEN GENERATOR.

Part: INDICATION — MALFUNCTIONED (LDG GEAR DOOR)

GEAR DOOR OPEN LIGHT REMAINED ON DURING APPROACH. EXECUTED GO-AROUND, RECYCLED LANDING GEAR AND GEAR DOOR OPEN LIGHT EXTINGUISHED. GEAR DOOR OPEN POSITION INDICATION LIGHT OPS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS WOULD NOT TEST OR ILLUMINATE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES.

Part: INDICATION — MALFUNCTIONED (LDG GEAR DOOR)

GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. RECYCLED GEAR AT 200 KTS, LIGHT REMAINED ON. RECYCLED GEAR AT 250 KTS, LIGHT WENT OUT. VISUALLY INSPECTED GEAR AND WHEEL WELL AREA. NO DEFECTS NOTED. OPERATED GEAR. ALL INDICATIONS WERE NORMAL.

Part: WINDOW — STUCK (LT COCKPIT)

CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. LUBRICATED WINDOW, OPS CHECKED GOOD.

Part: WINDOW — LACK OF LUBE (COCKPIT)

CAPTAIN'S SLIDING CLEAR VIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. ADJUSTED CAPTAIN'S CLEAR VIEW WINDOW IAW DC9 MM.

Part: WINDOW — LACK OF LUBE (COCKPIT)

UNABLE TO OPEN CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT). WINDOW OPENED AFTER SEVERAL ATTEMPTS. WHEN RECLOSED, WINDOW WOULD NOT REOPEN. LUBRICATED TRACK AND ROLLERS, WINDOW OPS CHECKED GOOD.

Part: TR LINK — CRACKED (NR 2 ENGINE)

DURING COMPLIANCE WITH AD 96-10-11 AND 75-14-06, FOUND FORWARD, UPPER RIGHT THRUST REVERSER LINK CRACKED. REPLACED THRUST REVERSER DRIVE LINK IAW DC9 MM 78-31-5.

Part: WINDOW — BINDING (LT COCKPIT)

CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN WITH NORMAL PRESSURE. LUBRICATED CAPTAIN'S CLEARVIEW WINDOW AND RESECURED WINDOW TRIM.

Part: WINDOW — BINDING (LT COCKPIT)

CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. FOUND WINDOW TRIM BINDING WINDOW ACTUATING ROD. RESECURED TRIM, WINDOW OPERATED NORMAL.

Part: BLKHD FITTING — CRACKED (LT PYLON)

DURING C-CHECK, FOUND THE LT PYLON BULKHEAD INBOARD FITTING CRACKED STA 965. INBOARD CORNER CRACKED. REPLACED FITTING, IAW DC-9 SRM.

Part: BLKHD STIFFENER — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD LT UPPER NR 1 RADIAL INBOARD CORNER CRACKED. REPLACED RADIAL STIFFENER IAW DC-9 SRM.

Part: FLOORBEAM — CORRODED (BS 579)

DURING C-CHECK, FOUND THE UPPER CARGO COMPARTMENT FLOORBEAM AT FS 579 AND LBL 44 TO 50 CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM IAW ABX REA D953-20570-MR.

Part: BULKHEAD FRAME — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB UPPER DOOR FRAME CRACKED IN TWO PLACES. REPLACED FRAME IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: WEB — CORRODED (COCKPIT)

DURING C-CHECK, FOUND THE CENTER COCKPIT SUBFLOOR WEB CORRODED THROUGH. REPAIRED IAW ABX REA D953-20290.

Part: JAMB — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR JAMB WEB CRACKED AT STA 366 LONGERON 28 RIGHT AND 27 RIGHT. REPLACED DOOR JAMB WEB P/N 5910142505 IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: SUBFLOOR — CRACKED (BS 200)

DURING C-CHECK, FOUND CRACK IN SUBFLOOR STA 200 RBL 8.5. REPAIRED CRACK IN SUBFLOOR STA 200 IAW DC-9 SRM 53-01.

Part: FLOOR PANEL — CRACKED (COCKPIT)

DURING C-CHECK, FOUND LEFT COCKPIT FLOOR PANEL CRACKED. REPAIRED COCKPIT FLOOR PANEL IAW DC-9 SRM 53-01.

Part: FLOORBEAM — CORRODED (BS 965)

DURING C-CHECK, FOUND FLOORBEAM CORRODED STA 965 LBL 30. REPAIRED IAW DC-9 SRM 53-05.

Part: FLOOR PANEL — CRACKED (COCKPIT)

DURING C-CHECK, FOUND CENTER COCKPIT FLOOR PANEL CORRODED BEYOND LIMITS AND CRACKED. FABRICATED P/N 9957827-3 FLOOR PANEL IAW DOUGLAS DRAWING 9957827.

Part: SHEAR TIE — CRACKED (BS 945)

DURING C-CHECK, FOUND SHEAR TIE CRACKED AT STA 945 BETWEEN LONGERON 14 AND 15. REPLACED SHEARTIE IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: BULKHEAD SKIN — CORRODED (BS 604)

DURING C-CHECK, FOUND LEVEL 2 CORROSION AT PRESSURE BULKHEAD STA 604. SKIN BULGING AND RIVETS SHEARED. REMOVED CORROSION AND TREATED AREA IAW 51-10-3. REPLACED FOUR FINGER DOUBLERS P/N 5914865-9-11-17-18 IAW DWG 5914865 AND DC-9 SRM 51-30-2 AND 51-30-5.

Part: CUSP WEB — CRACKED (BS 598)

DURING C-CHECK, FOUND THE LT CUSP WEB AT STA 598 CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2 AND 51-30-1.

Part: SKIN — CORRODED (FUSELAGE)

DURING C-CHECK, FOUND THE EXTERIOR FUSELAGE SKIN CORRODED BEYOND LIMITS AT THE BOTTOM OF THE FORWARD LOWER CARGO DOOR CUT OUT WHERE THE SCUFF PLATE WAS REMOVED. FUSELAGE SKIN IS BULGED BETWEEN THE EXTERIOR SKIN AND INTERIOR DOUBLER. REPAIRED FUSELAGE SKIN IAW ABX REA D953-20325-MR.

Part: CUSP WEB — CRACKED (BS 579-598)

DURING C-CHECK, FOUND THE RT CUSP WEB CRACKED BETWEEN FS 579 AND FS 598 NEXT TO HORSE SHOE DOUBLER. REMOVED AND REPLACED THE CUSP WEB IAW 51-30-1 AND 51-30-2.

Part: WINDOW FRAME — CRACKED (BS 699-718)

DURING C-CHECK, FOUND THE LOWER FORWARD CORNER OF THE LT SIDE CABIN WINDOW FRAME BETWEEN STA 699 - 718 CRACKED. REPAIRED WINDOW FRAME IAW ABX REA D953-20563.

Part: WINDOW FRAME — CRACKED (BS 699-718)

DURING C-CHECK, FOUND THE UPPER AFT CORNER ATTACH ANGLE THE RT SIDE CABIN WINDOW FRAME BETWEEN STA 699 - 718 CRACKED. REPAIRED WINDOW FRAME IAW ABX REA D953-20563.

Part: WINDOW FRAME — CRACKED (BS 639-658)

DURING C-CHECK, FOUND THE UPPER FORWARD CORNER AND LOWER AFT CORNER OF THE RT SIDE CABIN WINDOW FRAME BETWEEN STA 639 - 658 CRACKED. REPAIRED WINDOW FRAME IAW ABX REA D953-20563.

Part: PANEL — DELAMINATED (LT WING TE)

DURING C-CHECK, FOUND THE LEFT WING INBOARD UPPER TRAILING EDGE PANEL DELAMINATED BEYOND LIMITS. REMOVED AND REPLACED TRAILING EDGE PANEL IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-20-0.

Part: DRIVE CRANK — CORRODED (RUDDER)

DURING C-CHECK, FOUND THE RUDDER DRIVE CRANK CORRODED BEYOND LIMITS ON THE SPLINES. REPLACED THE RUDDER CRANK IAW DC-9 MM.

Part: FLOORBEAM — CORRODED (BS 160)

DURING C-CHECK, FOUND THE FLOORBEAM CAP AT FS 160 SEVERELY CORRODED ON THE RT SIDE OF THE BEAM. *S/D* REPAIRED FLOORBEAM IAW ABX REA D953-20339-MR.

Part: BLKHD FITTING — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB FITTING P/N 3917624-517, LT SIDE, CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2 AND 51-30-1.

Part: BLKHD FITTING — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB FITTING P/N 3917624-519, LT SIDE, CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: CUSP WEB — CRACKED (BS 908)

DURING C-CHECK, FOUND THE LT CUSP WEB AT STA 908 IS CRACKED AT LIGHTENING HOLE. REPLACED FITTING IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: BLKHD FITTING — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND A RADIAL CRACK AND A BEND RADIUS CRACK IN THE LT UPPER CORNER OF THE AFT PRESSURE BULKHEAD DOOR JAMB. REPAIRED AFT PRESSURE BULKHEAD DOOR JAMB LT UPPER CORNER IAW DC-9 SB 53-137 AND ABX REA D953-20562-MR.

Part: WINDOW FRAME — CRACKED (BS 639-658)

DURING C-CHECK, FOUND THE UPPER FORWARD CORNER OF THE WINDOW FRAME BETWEEN STA 639 AND 658 RT SIDE IS CRACKED. *S/D* REPAIRED WINDOW FRAME IAW ABX REA D953-20563.

Part: PRESS BULKHEAD — CORRODED (BS 604)

DURING C-CHECK, FOUND THE PRESSURE BULKHEAD AT FS 604 IN FORWARD LOWER CARGO COMPARTMENT BEHIND THE AUX FUEL TANK BULGED AND CORRODED IN 4 PLACES WITH THE RIVET HEADS SHEARED OFF, AT THE TOP OF THE BULKHEAD WING STA'S X 4 LT AND X 24 LT AND AT THE BOTTOM OF THE BULKHEAD BETWEEN LONGERONS 27R AND 28R, AND LONGERONS 29R AND 30. *S/D* FABRICATED AND REPLACED FINGER DOUBLER 5914865-9, 5914865-11, 5914865-17 AND 5914865-18 IAW DACO DWG 5914865 AND DC-9 SRM 51-30-2 AND 51-30-5.

Part: WINDOW FRAME — CRACKED (BS 699-718)

DURING C-CHECK, FOUND THE UPPER AFT CORNER OF THE WINDOW FRAME ATTACH ANGLE BETWEEN STA 699 AND 718 RT SIDE CRACKED. *S/D* REPAIRED IAW ABX REA D953-20563.

Part: CUSP WEB — CRACKED (BS 294-313)

DURING C-CHECK, FOUND THE RT CUSP WEB CRACKED AT LIGHTENING HOLE AT STA 294 TO 313. REPAIRED CUSP WEB IAW DC9 SRM 53-01.

Part: HINGE — FROZEN (LT TE FLAP)

DURING C-CHECK, FOUND THE FLAP HINGE ASSY AT XRS 167 BOLT FROZEN AND HAS ROTATED OUT OF THE RETAINER AND HAS GOUGED THE OUTBOARD SIDE OF THE FLAP HINGE FITTING. CLEANED AND TREATED CORROSION AND REPLACED BOLT.

Part: CUSP WEB — CRACKED (BS 579-598)

DURING C-CHECK, FOUND THE RT CUSP WEB CRACKED BETWEEN FS 579 AND 598. *S/D* REPLACED CUSP WEB IAW DC9 SRM 51-30-1 AND 51-30-2.

Part: WINDOW FRAME — CRACKED (BS 639-658)

DURING C-CHECK, FOUND THE LOWER AFT CORNER OF THE WINDOW FRAME BETWEEN STA 639 AND 658 RT SIDE IS CRACKED. *S/D* REPAIRED WINDOW FRAME IAW ABX REA D953-20563.

Part: DUCT — CRACKED (RADIO RACK)

DURING C-CHECK, FOUND THE RADIO RACK COOLING FAN EXHAUST IN FUSELAGE UPPER AND LOWER CORNERS CRACKED. *S/D* REPAIRED DUCT IAW ABX REA D953-2065 AND DC-9 SRM 51-10-38 AND 51-30-2.

Part: WINDOW FRAME — CRACKED (BS 699-718)

DURING C-CHECK, FOUND THE UPPER FORWARD CORNER OF THE WINDOW FRAME BETWEEN STA 699 AND 718 LT SIDE CRACKED. *S/D* REPAIRED WINDOW FRAME IAW ABX REA D953-20563.

Part: BLKHD FITTING — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND A BEND RADIUS CRACK IN THE AFT PRESSURE BULKHEAD DOOR JAMB UPPER RT CORNER. *S/D* REPAIRED IAW DC9 S/B 53-137 AND ABX REA D953-20562MR.

Part: EXHAUST DUCT — CRACKED (APU)

DURING C-CHECK, FOUND A CRACK IN THE APU CASE NEXT TO THE THERMOSTAT BOSS, VISIBLE LOOKING FORWARD THROGH THE EXHAUST DUCT BELOW THE FLANGE. *S/D* REPLACED THE EXHAUST DUCT FLANGE IAW GARRET OHM 49-22-05.

Part: WEB — CRACKED (BS 366)

DURING C-CHECK, FOUND FORWARD LOWER CARGO COMPARTMENT DOOR JAMB WEB CRACKED AT STA 366 AND CORRODED. *S/D* REPLACED DOOR JAMB WEB IAW DC-9 SRM 51-30-2, 51-30-5.

Part: CUSP WEB — CRACKED (BS 598)

DURING C-CHECK, FOUND THE RT CUSP WEB JUST FORWARD OF STA 598 CRACKED. REPLACED CUSP WEB IAW DC9 SRM 51-30-1.

Part: SUBFLOOR — CORRODED (RT COCKPIT)

DURING C-CHECK, FOUND THE RT COCKPIT SUB FLOOR CORRODED IN SEVERAL PLACES. REPAIRED SUB FLOOR IAW ABX REA D953-20290-MR.

Part: SHEAR TIE — CRACKED (BS 945)

DURING C-CHECK, FOUND A SHEAR TIE CRACKED AT STA 945 BETWEEN LONGERON 14R AND 15R WITH 4 RIVETS MISSING. *S/D* REMOVED AND REPAIRED SHEAR TIE IAW DC-9 SRM 51-30-02 AND 51-30-05.

Part: PANEL — DELAMINATED (LT WING TE)

DURING C-CHECK, FOUND THE LEFT WING INBOARD UPPER HONEYCOMB TRAILING EDGE PANEL DELAMINATED BEYOND LIMITS. *S/D* REPLACED PANEL (P/N 591216-47) IAW DC-9 SRM 51-30-1.

Part: BATTERY — DISCHARGED (CABIN)

DURING MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS IN COCKPIT WEAK ON TEST. REPLACED EMERGENCY LIGHT BATTERY.

Part: SEAT TRACK — FAILED (FS 783/872)

DURING TAKEOFF ROLL, FS 694 SEAT TRACK FAILED PUSHING THE 'C' CONTAINER LOCK OUT OF THE SEAT TRACK. TWO BALLAST PALLETS AND ONE 'C' CONTAINER. TORE THE SEAT TRACK LOCKS FROM THE SEAT TRACKS AT FS 783 AND 872, WHICH WERE IN LOCKING POSITION. THE RIGHT PYLON BULKHEAD ABSORBED THE IMPACT, CONTAINERS CAME TO REST AT FS 965. THE CREW SECURED THE FREIGHT AND THE FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. INSPECTED PER REA D953-14079. REPAIRED PER REA D953-14153, D953-14159, D953-14079 AND THE DC-9 SRM. REFERENCE WORK ORDER NR DMG 454. REA'S D925-14089 THROUGH 14152 WERE ISSUED TO THE DC-9 FLEET TO PROVIDE INCREASED SUPPORT.

Part: WINDSHIELD — BROKEN (LT COCKPIT)

OUTER PANE OF CAPTAIN'S WINDSHIELD SHATTERED AT FL 330, DURING CLIMB TO FL350. CREW DECLARED AN EMERGENCY AND LANDED AT IAH WITHOUT FURTHER INCIDENT. REPLACED WINDSHIELD IAW DC-9 MM 56-10-2.

Part: LINK — WORN (LT MLG O/B DOOR)

DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR LINK TO HAVE EXCESSIVE PLAY. REPLACED LINK IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: ROD END — WORN (LT MLG O/B DOOR)

DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR, DOOR TO GEAR LINKAGE INBOARD ROD END WORN. REPLACED ROD END IAW DC-9 OVERHAUL MANUAL 32-10-6.