N930AX

Part: BEAM — CRACKED (CARGO DOORWAY) · airframe 62,495 hrs · 39,317 cycles

FORWARD LOWER CARGO DOOR BEAM END CRACKED NR 4 BEAM FORWARD END STEEL CAP. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,495 hrs · 39,317 cycles

CRACKED FITTING AT P-DOME DOOR JAMB - LOWER. REMOVED AND REPLACED FITTING IAW DC9 SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 62,495 hrs · 39,317 cycles

CRACKED FITTING RIGHT BUTT LINE 6 AT P-DOME DOOR JAMB - LOWER. REMOVED AND REPLACED FITTING IAW DC9 SRM.

Part: SHEAR TIE — CRACKED (BS 945 S15R) · airframe 62,495 hrs · 39,317 cycles

SHEAR TIE FS 945 LONGERON 15 RIGHT WAS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW DC9 SRM 51-30-5.

Part: FRAME — CRACKED (BS 737) · airframe 62,495 hrs · 39,317 cycles

LEFT AFT MAIN FRAME STA 737 WAS CRACKED ON UPPER INBOARD FORWARD FLANGE BETWEEN Z-CLIP FASTENERS. REPAIRED MAIN FRAME STA 737 LEFT IAW EA 53400310.

Part: CUSP WEB — CRACKED (BS 945-965) · airframe 62,495 hrs · 39,317 cycles

LEFT CUSP CRACKED BETWEEN FS 945 - 965. REMOVED AND REPLACED SECTION OF CUSP IAW DC9 SSRM DWG K07259 AND DC9 SRM 51-30-2.

Part: SHEAR TIE — CRACKED (BS 945 L14-15L) · airframe 62,495 hrs · 39,317 cycles

SHEAR TIE CRACKED 2 PLACES FS 945, LONGERON 14 - 15 LEFT. REPAIRED SHEAR TIE IAW DC9 SRM.

Part: SHEAR TIE — CRACKED (BS 965 L14R) · airframe 62,495 hrs · 39,317 cycles

SHEAR TIE FS 965 LONGERON 14 RIGHT CRACKED. REPAIRED CRACKED SHEAR TIE IAW DC9 SRM 53-03.

Part: SEAT TRACK — CORRODED (BS 190-214) · airframe 62,495 hrs · 39,317 cycles

SEAT TRACK CORRODED INSIDE TOP OF DOUBLE TRACK AT FS 214 - 190, RIGHT BUTT LINE 22. REPAIRED SEAT TRACK IAW DC9 SSRM K05406.

Part: ATTACH ANGLE — CRACKED (LT PYLON) · airframe 62,495 hrs · 39,317 cycles

LEFT PYLON LOWER ATTACH ANGLE WAS CRACKED FS 990. REPAIRED LOWER PYLON ATTACH ANGLE IAW DC9 SRM.

Part: VANE — CORRODED (LT WING TE FLAP) · airframe 62,495 hrs · 39,317 cycles

LEFT FLAP INBOARD FIXED VANE UPPER AND LOWER SURFACES CORRODED. REMOVED AND REPLACED LEFT FLAP INBOARD FIXED VANE IAW DC9 MM 27-51-03-2-0002.

Part: BRACKET — CRACKED (VERTICAL STAB) · airframe 62,495 hrs · 39,317 cycles

VERTICAL STABILIZER UPPER RUDDER ATTACH HINGED BRACKET - RIGHT - CRACKED. REMOVED AND REPLACED RUDDER BRACKET IAW DC9 SRM.

Part: ATTACH ANGLE — CRACKED (VERTICAL STAB) · airframe 62,495 hrs · 39,317 cycles

VERTICAL STABILIZER RIGHT ATTACH ANGLE COMMON TO FUSELAGE CRACKED - AFT. REPAIRED RIGHT VERTICAL STABILIZER ATTACH ANGLE IAW DC9 SRM 53-05.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 61,960 hrs · 38,891 cycles

EMERGENCY LIGHT BATTERY DEAD. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC9 AMM 33-53-02-4. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 61,344 hrs · 38,416 cycles

ON SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00-8.

Part: INTERCOSTAL — CRACKED (BS 718-699) · airframe 60,954 hrs · 38,090 cycles

INTERCOSTAL AT LONGERON 11 LEFT, FS 718 - 699 CRACKED ON ONE END. REPAIRED AREA IAW DC-9 SRM 53-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,954 hrs · 38,090 cycles

FORWARD FUSELAGE SKIN AFT OF LEFT NOSE WHEEL WELL CRACKED IN SEVERAL PLACES. FABRICATED DOUBLER/INSTALLED IAW DC-9 SRM 51-30-2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,954 hrs · 38,090 cycles

LEFT FORWARD MAIN FRAME CRACKED AT FORWARD AND AFT FLANGE POINTS G & J. MAIN FRAME REQUIRES REPLACEMENT PER NEA53400100-002-30 AND ES00914. REMOVED AND REPLACED LEFT FORWARD MAIN FRAME IAW EA 53400321-001-3.

Part: CHANNEL — CORRODED (BS 313) · airframe 60,954 hrs · 38,090 cycles

RIGHT FLOOR CHANNEL CORRODED ON UPPER AND LOWER SURFACE, FORWARD OF FRAME FS 313. CORRODED AREAS BEYOND LIMITS. REMOVED BAD SECTION FROM APPROXIMATELY STR 308 - 360. FABRICATED REPLACEMENT SECTION AS NEEDED AND RE-INSTALLED.

Part: CONNECTOR — DIRTY (MLG) · airframe 59,896 hrs · 37,240 cycles

ON INITIAL GEAR EXTENSION, RED NOSE LIGHT DID NOT ILLUMINATE DURING GEAR EXTENSION WITH NO GREEN LIGHT. RECYCLED GEAR WITH ONLY MOMENTARY FLICKER OF RED NOSE LIGHT. GREEN NOSE LIGHT EVENTUALLY ILLUMINATED AND WAS VERIFIED. ALL OTHER INDICATIONS NORMAL. INSPECTED SYSTEM IN NOSE GEAR WHEEL WELL, FOUND CORROSION P1-133 NOT SECURED, RESECURED, VERIFIED SWITCH SECURITY, CLEANED CONNECTOR AT SWITCH SW-1-9. SYSTEM WORKS WITH GOOD INDICATION ON GROUND IAW MFG AMM 32-51-00 AND 32-00.

Part: WEB — CRACKED (FWD CARGO) · airframe 59,542 hrs · 36,929 cycles

CUSP WEB CRACKED AT FS 310 ABOVE LONGERON 20 LT. REPAIRED AREA IAW SRM 53-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,542 hrs · 36,929 cycles

CRACKED FRAME AT LONGERON 2 LT, STA. 1076. REPLACED SECTION OF FRAME BETWEEN LONGERON 3 LT AND 3 RT IAW DC-9 SRM 51-30-5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,542 hrs · 36,929 cycles

CRACKED FRAME AT LONGERON 2 RT, STA. 1076. REPLACED SECTION OF FRAME BETWEEN 3 LT AND 3 RT IAW SRM 51-30-5.

Part: SKIN — CORRODED (FUSELAGE) · airframe 59,542 hrs · 36,929 cycles

SKIN AT FS 610 BETWEEN LONGERON 28 LT AND LONGERON 28 RT WAS SEVERLY CORRODED, EXFOLIATED AND BULGED. CUT OUT CORROSION AREA OF SKIN, INSTALLED REPAIR DOUBLER / FILLER IAW SRM 53-01.

Part: JACKSCREW — CORRODED (HORIZONTAL STAB) · airframe 59,542 hrs · 36,929 cycles

JACKSCREW THREADS HAD AREAS WHICH WERE PITTED. REMOVED AND REPLACED HORIZONTAL JACKSCREW IAW DC-9 MM 27-40-01.

Part: FITTING — RUSTED (FUSELAGE) · airframe 58,319 hrs · 35,852 cycles

STEEL BEAM ABOVE THE RIGHT CLEARVIEW WAS RUSTED ON THE AFT END, BOTH INSIDE AND OUTSIDE OF BEAM. REPLACED BEAM IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: PANEL — DELAMINATED (LEFT WING) · airframe 58,319 hrs · 35,852 cycles

LEFT WING LOWER INBOARD BONDED PANEL HAD A LARGE AREA OF DELAMINATION AROUND FASTENERS. REPLACED BONDED PANEL IAW DC-9 SRM 51-30-1 AND 51-30-2.

Part: TEE CHORD — CRACKED (FUSELAGE) · airframe 58,319 hrs · 35,852 cycles

AFT PRESSURE BULKHEAD NR 2 TEE HAD 2 VERTICAL CRACKS APPROXIMATELY 1 INCH IN LENGTH AT LONGERON 14 RIGHT AND LONGERON 16 RIGHT. REPLACED THE NR 2 TEE IAW EA 53120033-006 AND REA D953-44179.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 58,319 hrs · 35,852 cycles

CRACK INDICATION IN PAN AND HI-LOK AT THE NR 1 BEAM AFT END AFT LOWER CARGO DOOR. REPLACED THE OUTER SKIN AND PAN IAW DC-9 SRM 51-30-2.

Part: CONTACTOR — DIRTY (BATTERY PACK) · airframe 57,962 hrs · 35,508 cycles

COCKPIT EMERGENCY LIGHTS WOULD NOT COME ON. CLEANED BATTERY PACK AND CONTACTS. SYSTEM OPS CHECKED GOOD IAW DC-9 AMM 33-53-02-4-0001.

Part: BATTERY — DEFECTIVE (CABIN) · airframe 57,962 hrs · 35,508 cycles

COCKPIT EMERGENCY LIGHTS WOULD NOT COME ON. REPLACED EMERGENCY LIGHT BATTERIES IAW DC-9 AMM 33-53-0-2-4-0001.

Part: LIGHT — MALFUNCTIONED (COCKPIT) · airframe 57,937 hrs · 35,483 cycles

COCKPIT EMERGENCY LIGHTS WOULD NOT TEST. MECHANIC WENT TO GET NEW BATTERIES. UPON MECHANIC'S RETURN, THE CREW INFORMED HIM THAT THE LIGHTS WERE WORKING, BUT ONE BULB WAS OUT. WHEN MECHANIC WIGGLED THE BULB IT CAME ON. REPLACED THE BULB AS A PRECAUTION.

Part: WINDOW — LACK OF LUBE (COCKPIT) · airframe 57,832 hrs · 35,382 cycles

CREW REPORTED THAT THE FIRST OFFICER'S CLEAR VIEW WINDOW WOULD NOT OPEN. LUBRICATED THE UPPER LOCK BAR. OPERATIONAL CHECKED GOOD.

Part: FITTING — CRACKED (CARGO BAY) · airframe 56,800 hrs · 34,634 cycles

FLOOR SUPPORT STRUT FITTING CRACKED AT STATION 870R. REPLACED FLOOR SUPPORT STRUT IAW DC9 SRM 51-30-5.

Part: FITTING — CRACKED (CABIN) · airframe 56,800 hrs · 34,634 cycles

FLOOR SUPPORT FITTING CRACKED AT STATION 851R. REPLACED SUPPORT FITTING IAW DC9 SRM51-30-1.

Part: FITTING — CRACKED (CABIN) · airframe 56,800 hrs · 34,634 cycles

FLOOR SUPPORT FITTING CRACKED AT STATION 775R. REPLACED FLOOR SUPPORT IAW DC9 SRM 51-30-5.

Part: LONGERON — CRACKED (CABIN) · airframe 56,800 hrs · 34,634 cycles

LONGERON 17 RIGHT CRACKED AT STATION 465. REPLACED LONGERON SECTION IAW DC9 SRM 53-02.

Part: LONGERON — CRACKED (CABIN) · airframe 56,800 hrs · 34,634 cycles

LONGERON 17 RIGHT CRACKED AT HI-LOKS AT STATION 389. REPAIRED IAW DC9 SRM 53-02.

Part: FRAME — CRACKED (PAX DOOR) · airframe 56,800 hrs · 34,634 cycles

FORWARD ENTRY DOOR VERTICAL FRAME CRACKED AFT OF DOOR HANDLE. REPLACED FRAME IAW DC9 SRM 51-30-2.

Part: FITTING — CRACKED (CABIN) · airframe 56,800 hrs · 34,634 cycles

FLOOR SUPPORT FITTING CRACKED AT STATION 917L. REPLACED SUPPORT FITTING IAW DC9 SRM51-30-5.

Part: FITTING — CRACKED (CABIN) · airframe 56,800 hrs · 34,634 cycles

FLOOR SUPPORT FITTING CRACKED AT STATION 798. REPLACED FLOOR SUPPORT FITTING IAW DC9 SRM 51-30-5.

Part: LONGERON — CRACKED (CABIN) · airframe 56,800 hrs · 34,634 cycles

LONGERON 17 RIGHT CRACKED AT HI-LOKS AT STATION 408. REPAIRED IAW DC9 SRM 53-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,800 hrs · 34,634 cycles

FUSELAGE SKIN CORRODED AT STATION 945 - 955 AND LONGERON 27 RIGHT - 29 RIGHT. REPAIRED SKIN IAW DC9 SRM 53-04.

Part: SEAT TRACK — CRACKED (CABIN) · airframe 56,800 hrs · 34,634 cycles

SEAT TRACK CRACKED AT STATION 614 AND LBL 20. REPLACED SECTION OF SEAT TRACK IAWDC9 SRM 51-30-1.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 56,800 hrs · 34,634 cycles

L-ANGLE CRACKED AT RIGHT PYLON BULKHEAD, BELOW LONGERON 15 RIGHT AT STATION 1038. REPLACED ANGLE IAW DC9 SRM.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES.

Part: TRIM — LOOSE (COCKPIT WINDOW)

FIRST OFFICER'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. REMOVED LOOSE TRIM, WINDOW OPENS NORMALLY.

Part: TRIM — OUT OF ADJUST (COCKPIT WINDOW)

FIRST OFFICER'S CLEARVIEW WINDOW WAS DIFFICULT TO OPEN. REPOSITIONED WINDOW TRIM AROUND FIRST OFFICER'S CLEARVIEW WINDOW. OPS CHECKED GOOD.

Part: FITTING — CRACKED (NR 1 PYLON)

DURING C-CHECK, FOUND NR 1 ENGINE PYLON INTERIOR FITTING AT STATION 1038 LONGERON 15L CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-0.

Part: STRAP — CRACKED (NR 1 PYLON)

DURING C-CHECK, FOUND NR 1 RIGHT PYLON SPAR UPPER CAP STRAP CRACKED. REPLACED SPAR CAP STRAP IAW ABX REA D954-26516 AND DWG 5917717.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, FOUND LONGERON 16L CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: SHEAR TIE — CRACKED (BS 945)

DURING C-CHECK, FOUND SHEAR TIE CRACKED AT STATION 945 BETWEEN LONGERON 15 RIGHT AND 16 RIGHT. REPLACED SHEAR TIE IAW DC9 SRM 51-30-5.

Part: BULKHEAD FTG — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD DOOR JAMB FITTING CRACKED BETWEEN 1ST AND 2ND RADIALS. REPLACED FITTING IAW DC9 SRM 51-30-02.

Part: SHEAR TIE — CRACKED (BS 945)

DURING C-CHECK, FOUND SHEAR TIE CRACKED AT STATION 945 BETWEEN LONGERON 14 LEFT AND 15 LEFT. REPLACED SHEAR TIE IAW DC9 SRM 51-30-2.

Part: STRAP — CRACKED (NR 2 PYLON)

DURING C-CHECK, FOUND NR 2 RIGHT PYLON SPAR UPPER CAP STRAP CRACKED. REPLACED SPAR CAP STRAP IAW ABX REA D954-26516 AND DWG 5917717.

Part: BRACKET — CRACKED (RT TE FLAP)

DURING C CHECK, FOUND RIGHT FLAP OUTBOARD HINGE INTERIOR FITTING, OUTBOARD ATTACH BRACKET CRACKED. REPLACED BRACKET IAW DC9 SRM 51-30-1.

Part: FITTING — CRACKED (BS 680)

DURING C-CHECK, FOUND FLOORBEAM SUPPORT FITTING ABOVE CENTER WING CRACKED AT LOWER END, STATION 680, RBL 43. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: BRACKET — CRACKED (LT TE FLAP)

DURING C CHECK, FOUND LEFT FLAP OUTBOARD HINGE INTERIOR FITTING, OUTBOARD ATTACH BRACKET CRACKED. REPLACED BRACKET IAW DC9 SRM 51-30-1.

Part: LONGERON — CRACKED (BS 160)

DURING C-CHECK, FOUND LONGERON 4L CRACKED AT STATION 160. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: FITTING — CRACKED (BS 680)

DURING C-CHECK, FOUND FLOORBEAM SUPPORT FITTING ABOVE CENTER WING CRACKED AT LOWER END, STATION 680 , LBL 43. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: SKIN — CRACKED (FUSELAGE)

DURING C-CHECK, FOUND FUSELAGE SKIN CRACKED AFT OF NOSE LANDING GEAR, AFT RIGHT DOOR HINGE. REPAIRED SKIN IAW DC9 SRM 53-05.

Part: BRACKET — CRACKED (RT TE FLAP)

DURING C-CHECK, FOUND RIGHT FLAP OUTBOARD, INTERIOR FITTING, INBOARD ATTACH BRACKET CRACKED. REPLACED BRACKET IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: BRACKET — CRACKED (LT TE FLAP)

DURING C-CHECK, FOUND LEFT FLAP OUTBOARD HINGE INTERIOR FITTING INBOARD ATTACH BRACKET CRACKED. REPLACED BRACKET IAW DC9 SRM 51-30-1 AND 51-30-5.

Part: WEB — CRACKED (BS 955)

DURING C-CHECK, FOUND CUSP WEB CRACKED AT STATION 955, LEFT SIDE. REPAIRED CUSP WEB IAW DC9 SRM 53-01.

Part: FRAME — CRACKED (BS 737)

DURING C-CHECK, FOUND RIGHT FUSELAGE MAIN FRAME STATION 737 CRACKED AT OUTBOARD POCKET, UPPER FLANGE. REPAIRED IAW ABX REA D953-26518MR.

Part: BRACKET — CRACKED (LT SPOILER)

LEFT WING SPOILER ACTUATOR BRACKET, LOWER SURFACE CRACKED. REPAIRED UNIT COMPLETE.

Part: BATTERY PACK — DISCHARGED (CABIN)

COCKPIT EMERGENCY LIGHTS WERE DIM. REPLACED BATTERY PACK.

Part: LINE — RUPTURED (RT MLG WW)

RIGHT HYDRAULIC FLUID QUANTITY DROPPED TO 0. REPAIRED HYDRAULIC LINE AT THE AUXILIARY PUMP FILTER, OPS CHECKED GOOD IAW DC9 MM.

Part: SWITCH — DEFECTIVE (LT MLG DOOR)

GEAR DOOR OPEN LIGHT ILLUMINATED DURING UPLATCH CHECK. RECYCLED GEAR, LIGHT EXTINGUISHED. UPLATCH CHECK OK. REPLACED THE LEFT MAIN LANDING GEAR DOOR POSITION SWITCH.

Part: VANE — DENTED (RT TE FLAP)

DURING C-CHECK, FOUND RIGHT HAND FLAP UPPER MOVEABLE VANE PITTED AND DENTED. *S/D* REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.

Part: SPOILER — DELAMINATED (RT WING)

DURING C-CHECK, FOUND RT OUTBOARD SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PANEL IAW DC9 MM 27-61-1.

Part: FLOORBEAM — CORRODED (BS 965)

DURING C-CHECK, FOUND FORWARD SIDE OF FLOORBEAM AT F/STA 965 AND RBL 28 CORRODED. REPAIRED IAW ABX REA D953-19422-MR.

Part: BULKHEAD DOOR — CRACKED (AFT PRESS BLKHD)

DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD VENTRAL DOOR LT BEAM (P/N 3917853-1) CRACKED. REMOVED AND REPLACED BEAM IAW DC9 SRM 51-30-5.

Part: PRESSURE PANEL — CORRODED (RT MLG WW)

DURING C-CHECK, FOUND RT MLG WHEEL WELL OVERHEAD PRESSURE PANEL AT RBL 54 CORRODED. REPAIRED IAW ABX REA D953-19455.

Part: SKIN — DELAMINATED (RT TE FLAP VANE)

DURING C-CHECK, FOUND RT FLAP INBOARD FIXED VANE TOP SURFACE DELAMINATED. *S/D* REMOVED AND REPLACED SKIN, HONEYCOMB CORE AND INTERNAL DOUBLERS. REPAIRED IAW DC9 SRM.

Part: SEAT TRACK — CORRODED (BS 195)

DURING C-CHECK, FOUND SEAT TRACK AT RBL 22, F/STA 195 CORRODED. REPLACED CORRODED SECTION IAW SRM 51-30-1, 51-30-2 AND ABX SSRM DRAWING K05406.

Part: BRACKET — CRACKED (BS 237)

DURING C-CHECK, FOUND BRACKET AT F/STA 237 BETWEEN LONGERONS 27R AND 28R CRACKED. REPLACED BRACKET IAW DACO DWG 9915554-11 AND DC9 SRM 51-30-2 AND 51-30-5.

Part: BRACKET — CORRODED (NLG WW)

DURING C-CHECK, FOUND THE NOSE WHEEL STEERING FOLLOW UP DIFFERENTIAL BRACKET CORRODED WITH LARGE PITS ADJACENT TO SPRING. REPLACED BRACKET IAW 20-16-0.

Part: ANGLE — CRACKED (NR 2 PYLON)

DURING C-CHECK, FOUND NR 2 PYLON UPPER FUSELAGE ATTACH ANGLE AT F/STA 1038 CRACKED. STOP DRILLED AND REPAIRED IAW DC9 SRM 50-04, FIGURE 10.

Part: BULKHEAD WEB — CRACKED (LT PYLON)

DURING C-CHECK, FOUND THE LT PYLON BULKHEAD WEB CRACKED AT INBOARD END 5 ABOVE THE FLOOR LINE. REMOVED AND REPLACED THE WEB IAW DC9 SRM 51-30-5 AND 51-30-2.

Part: LONGERON — CRACKED (BS 957-996)

DURING C-CHECK, FOUND LONGERON 17R CRACKED AT THE RT PYLON BULKHEAD, FORWARD SIDE. REPLACED LONGERON 17R FROM F/STA 957 TO 996 IAW DC9 SRM 53-02.

Part: RUDDER PEDAL ARM — CRACKED (RT COCKPIT)

DURING C-CHECK, FOUND THE FIRST OFFICER'S RUDDER PEDAL ADJUSTMENT LUG CRACKED. REPLACED RUDDER PEDAL ARM (P/N 59654351) IAW ABX EA AD-27-03966.

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

DURING C-CHECK, FOUND THE WINDOW FRAME BETWEEN F/STA 639 TO 658 CRACKED AT UPPER FORWARD CORNER RT SIDE. REPAIRED WINDOW FRAME IAW ABX DC9 SUPPLEMENT SRM K05159.

Part: BLKHEAD FITTING — CRACKED (RT PYLON)

DURING C-CHECK, FOUND THE RT PYLON BULKHEAD FORWARD ATTACH FITTING AT FLOOR AND RBL 30 CRACKED. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5 AND 51-30-1.

Part: SKIN — DELAMINATED (RT SPOILER)

RIGHT WING SPOILER DELAMINATED, UPPER AND LOWER SKIN. REPLACED ALL HONEYCOMB CORE DOUBLERS AND SKIN.

Part: POWER SUPPLY — DEFECTIVE (CABIN)

EMERGENCY LIGHTS COME ON WHEN BATTERY SWITCH IS TURNED OFF, EMERGENCY LIGHT SWITCH WAS IN THE OFF POSITION. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW THE DC-9 M.M. 33-53-0.

Part: DOOR — DELAMINATED (RT MLG)

DURING COMPLIANCE WITH AD 91-22-07, ASB 32-244 FOUND RIGHT FLYING DOOR DELAMINATED. REPAIRED THE RIGHT FLYING DOOR IAW DC-9 SRM 52-02 PAGE 1.

Part: BUSHING — WORN (LT MLG DOOR)

DURING COMPLIANCE WITH AD 91-22-07, ASB 32-244 FOUND LEFT FLYING DOOR LINKAGE WORN. REPLACED THE BUSHING TO THE LEFT FLYING DOOR LINKAGE IAW DC-9 M/M 20-10-1.

Part: OIL CLOG LIGHT — ILLUMINATED (RT ENGINE)

DURING FLIGHT, RIGHT OIL STRAINER CLOGGING ANNUNCIATOR CAUTION LIGHT ILLUMINATED. RIGHT THROTTLE WAS REDUCED TO IDLE, LIGHT REMAINED ILLUMINATED, PRECAUTIONARY SHUT-DOWN OF RIGHT ENGINE WAS ACCOMPLISHED. REPLACED THE RIGHT ENGINE OIL SCREEN, MEGGED THE WIRES TO THE RIGHT ENGINE OIL FILTER DIFFERENTIAL PRESSURE SWITCH, GROUND RAN THE RIGHT ENGINE. OPS CHECKED GOOD.

Part: SPAR CAP — CORRODED (HORIZ STAB)

DURING C-CHECK INSPECTION, FOUND CORROSION ON LOWER SURFACE OF AFT UPPER SPAR CAP, FORWARD FLANGE ON RIGHT HORIZONTAL STABILIZER. REPAIRED IAW ABX REA D955-13276-MR.

Part: OIL LINE — LEAKING (LT ENGINE)

LEFT ENGINE SHUT DOWN FOR FLUCTUATING OIL PRESSURE AND ZERO QUANTITY INDICATION. TOTAL WINDMILL TIME WAS LESS THAN 1.5 MINUTES. REPLACED TWO OIL LINES OFF THE FUEL/OIL COOLER TO GEAR BOX IAW DC-9 M.M. 79-20. LEAK CHECKED GOOD.

Part: LINK — CRACKED (LT SPOILER)

DURING COMPLIANCE OF A.D. 85-01-03; S.B.'S 27-288, 27-229, EAAD 27-32091, FOUND THE LEFT OUTBOARD SPOILER DRIVE LINK HAD A CRACK INDICATION. REPLACED LEFT OUTBOARD SPOILER DRIVE LINK ISW DC-9 SUPP. M.M. 27-61-1.

Part: DOUBLER — CRACKED (AFT PRESS BLKHD)

DURING COMPLIANCE OF AD 85-01-02, SB 53-137, FOUND LEFT UPPER CORNER OF AFT PRESSURE BULKHEAD VENTRAL DOOR DOUBLER CRACKED IN RADIUS. REPAIRED IAW DC-9 SB 53-137, SERVICE REWORK DRAWING SR0J060088 AND ABX REA D953-11481-SB.

Part: BUSHING — WORN (LT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR DOUBLE TO SINGLE LINK TO HAVE EXCESSIVE PLAY. 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 ARTICULATING DOOR LINK ARM TO HAVE EXCESSIVE PLAY. REPLACED FITTING 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 RIGHT MAIN LANDING GEAR ARTICULATING DOOR LINK BEARING TO HAVE EXCESSIVE PLAY. REPLACED LINK IAW DC-9 OVERHAUL MANUAL 32-106.

Part: EEL BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS WILL NOT TEST. REPLACED BATTERIES. OPS CHECKED NORMAL IAW DC-9 SUPP MM 33-53-00.

Part: DN LOCK SW — CORROSION (LT MLG)

LEFT MAIN LANDING GEAR DOWN INDICATOR DID NOT ILLUMINATE ON INITIAL GEAR EXTENSION. CYCLED LANDING GEAR AND LIGHT ILLUMINATED. FOUND CORROSION IN THE LEFT GEAR DOWNLOCK SWITCH AND MOISTURE IN THE CANNON PLUG. CLEANED CORROSION FROM SWITCH AND REMOVED MOISTURE FROM THE CANNON PLUG. OPS CHECKED GOOD DURING GEAR SWING IAW DC-9 SUPPLEMENTAL M.M. 32-60-00.