N975AX

Part: BULKHEAD — CORRODED (AFT CARGO) · airframe 57,978 hrs · 53,007 cycles

AFT LOWER CARGO, AFT BULKHEAD WEB AND ANGLE EXFOLIATED AT RIGHT BUTT LINE 4 INCHES AT BOTTOM SIDE. REPAIRED DAMAGED IAW ABX ENGINEERING TO DUPLICATE PRODUCTION SPLICE IAW DACO DWG 9915561 AND DC9 SRM 51-30-0.

Part: FRAME — CRACKED (FS 1209) · airframe 57,978 hrs · 53,007 cycles

FS 1209 CANTED FRAME CRACKED BETWEEN LONGERON 14 AND 15 LEFT SIDE. REPAIRED IAW DC9 SRM 53-01.

Part: SKIN — CRACKED (BS 1197) · airframe 57,978 hrs · 53,007 cycles

AFT FUSELAGE SKIN CRACKED 2 PLACES APPROXIMATELY FS 1197, LEFT SIDE. REPAIRED AREA IAW DC9 SRM 53-01.

Part: BULKHEAD — CORRODED (AFT CARGO) · airframe 57,978 hrs · 53,007 cycles

AFT LOWER CARGO, AFT BULKHEAD WEB EXFOLIATED AT LEFT BUTT LINE 18 INCHES AT TOP. REPAIRED DAMAGE IAW DC9 SRM 53-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 57,539 hrs · 52,513 cycles

EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES FOR EMERGENCY LIGHTS IAW DC9 AMM 33-51-00. OPS CHECKED GOOD. DEFERRED: DI 50256 - EMERGENCY BATTERY PACK IAW DC9 MM 33-53-008. CLEARED: DI 50256. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK IAW DC9 MM 33-53-02-4-0001. SYSTEM OPS CHECKED GOOD. PLACARD REMOVED.

Part: WIRE — BROKEN · airframe 57,009 hrs · 52,041 cycles

WHEN CIRCUIT BREAKER FOR CLEARVIEW & EYEBROW WINDOWS WAS PUSHED IN DURING FLIGHT, CONSIDERABLE ARCHING AND SPARKS CAME FROM CAPTAIN'S CLEARVIEW WINDOW BUY THE TERMINAL BLOCK. REPAIRED A BROKEN WIRE AT THE TERMINAL BLOCK AND REPLACED THE TERMINAL BLOCK IAW DC9 AMM 30-41-00-2.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 56,693 hrs · 51,724 cycles

UPPER CARGO LEFT SIDE BUTT LINE 44 HAD FLOOR PANEL BULGED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK AT STA 973 - 1071, LEFT BUTT LINE 44 ON JOB CARD 0349 IAW DC-9 SRM.

Part: SEAT TRACK — BROKEN (CABIN) · airframe 56,693 hrs · 51,724 cycles

SEAT TRACK BROKEN IN UPPER CARGO COMPARTMENT AT FS 1041 AND LEFT BUTT LINE 44.5. SPLICED IN NEW SECTION OF SEAT TRACK AT FS 1041 - 965, LEFT BUTT LINE 44.5 IAW DC-9 SRM 53-05.

Part: BULKHEAD — CRACKED (LT PYLON) · airframe 56,693 hrs · 51,724 cycles

WEB ON LEFT PYLON BULKHEAD WAS OIL CANNED AND CRACKED AT LOWER INBOARD LIGHTNING HOLE. REPAIRED AREA IAW DC-9 SRM 53-01.

Part: ATTACH ANGLE — CRACKED (LT ENG PYLON) · airframe 56,693 hrs · 51,724 cycles

NR 1 PYLON UPPER ATTACH ANGLE HAD 1 MISSING FASTENER AND CRACKED AT STA 1056. REPAIRED AREA IAW DC-9 SRM 54-04.

Part: LONGERON — CRACKED (CABIN) · airframe 56,693 hrs · 51,724 cycles

LONGERON 17 RIGHT CRACKED AT PYLON BULKHEAD. SPLICED IN REPAIR ON LONGERON 17 RIGHT AT PYLON BULKHEAD IAW DC-9 DWG K05864 AND DC-9 SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 56,693 hrs · 51,724 cycles

DOOR JAMB WAS CRACKED AT TOP LEFT STOP AT INBOARD RIVET. REPAIRED DOOR JAMB AT TOP LEFT IAW DC-9 SRM 53-05.

Part: FRAME — CORRODED (FWD CARGO) · airframe 56,693 hrs · 51,724 cycles

AFT LOWER SECTION OF FRAME CORRODED FS 503, LONGERON 29 LEFT TO LONGERON 29 RIGHT. REPAIRED FRAME IAW DC-9 SRM 53-03.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,693 hrs · 51,724 cycles

AFT FUSELAGE HAD 7 EXTERNAL SKIN CRACKS FROM CANTED STA 1197 TO 1208, LONGERON 13 LEFT TO LONGERON 14 LEFT. CRACK LENGTHS FROM .5 TO .75 INCHES. REPAIRED AREA IAW DC-9 SRM 53-01 AND 53-10.

Part: SPLICE — CRACKED (CABIN) · airframe 56,693 hrs · 51,724 cycles

INBOARD FRAME FOOT ON AFT SIDE OF LEFT PYLON BULKHEAD WAS CRACKED. REPLACED CRACKED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 56,693 hrs · 51,724 cycles

CORROSION ON FLOOR TRACK STA 889 TO STA 1072, LEFT SIDE. REMOVED AND REPLACED TRACK IAW DC-9 SRM 51-30-1.

Part: FITTING — CRACKED (LT MLG) · airframe 56,693 hrs · 51,724 cycles

BRACE FROM UPPER PRESSURE PANEL TO FUSELAGE CRACKED AT BOTTOM BOLT ATTACH POINT 56 INCHES LT BUTTLINE AND 19 INCHES AFT OF MAIN FRAME. REMOVED AND REPLACED BRACE IAW DC-9 SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 55,366 hrs · 50,627 cycles

FS 1152 LEFT SIDE OF AFT VENTRAL STAIR CUTOUT FRAME FITTING CRACKED. INSTALLED NEW FITTING IAW DC-9 SRM 51-30-5.

Part: ATTACH FITTING — CRACKED (ELEVATOR TAB) · airframe 55,366 hrs · 50,627 cycles

RIGHT ELEVATOR GEARED TAB ATTACH FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2.

Part: WEB — CRACKED (FUSELAGE) · airframe 55,366 hrs · 50,627 cycles

RIGHT CUSP WEB CRACKED JUST FORWARD OF FS 1041 BULKHEAD. REPAIRED RIGHT CUSP WEB JUST FORWARD OF FS 1041 IAW DC-9 SRM 53-01.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,366 hrs · 50,627 cycles

CRACKED SHEAR TIE FS 1021 JUST BELOW LONGERON 14 RIGHT. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5.

Part: WEB — CRACKED (PAX DOOR) · airframe 55,366 hrs · 50,627 cycles

MAIN ENTRY DOOR INTERIOR WEB JUST FORWARD OF DOOR HANDLE WAS CRACKED. REPLACED WEB IAW DC-9 SRM 51-30-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,366 hrs · 50,627 cycles

CORROSION ON SEAT TRACK AT STA 275, 294, 320, 351, 380 AND 408. REPLACED CENTER SEAT TRACK STA 160 - 588 IAW DC-9 SRM 51-30-1 AND SSRM K05406.

Part: SKIN — CORRODED (T/E FLAP) · corrosion level 2 · airframe 55,366 hrs · 50,627 cycles

BULGE IN SKIN, CUPPED FASTENERS, FLAP LOWER SURFACE AT NR 3 EXPANSION JOINT. REPLACED LOWER SKIN IAW DC-9 SRM 51-30-2.

Part: ATTACH FITTING — CORRODED (LT ELEVATOR) · corrosion level 2 · airframe 55,366 hrs · 50,627 cycles

LT ELEVATOR WAS CORRODED ON UPPER SURFACE AT OUTBOARD BALANCE HORN ATTACH FITTING. REPLACED LT ELEVATOR ATTACH FITTING CLIP.

Part: SKIN — CORRODED (T/E FLAP) · corrosion level 2 · airframe 55,366 hrs · 50,627 cycles

BULGE IN SKIN, CUPPED FASTENERS FLAP UNDER SURFACE NR 2 EXPANSION JOINT. REPLACED UPPER AND LOWER FLAP SEGMENT SKIN.

Part: WEB — CRACKED (FUSELAGE) · airframe 54,534 hrs · 50,052 cycles

FOUND NUMEROUS CRACKS IN AFT CUSP WEB, LEFT HAND SIDE APPROXIMATELY AT FS 1002. REPAIRED CUSP WEB IAW DC-9 SRM 53-01.

Part: LANDING GEAR — MALFUNCTIONED (NLG) · airframe 54,311 hrs · 49,903 cycles

UPON GEAR EXTENSION FOR APPROACH, NOSE GEAR DID NOT EXTEND (NO GREEN LIGHT/NOSE LIGHT DID NOT SHOW). GEAR RECYCLED AFTER GO-AROUND. NOSE GEAR EXTENDED NORMALLY. INSPECTED NOSE LANDING GEAR DOWNLOCK SWITCH WIRING, NO DEFECTS NOTED. LUBED NOSE LANDING GEAR. REPLACED THE NOSE LANDING GEAR DOWN AND LOCK BULBS. PERFORMED EXTENSION AND RETRACTION TEST. NO DEFECTS NOTED IAW DC-9 AMM 32-20-00-2-0001.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,085 hrs · 49,746 cycles

DURING MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES IAW DC-9 AMM 33-53-02. OPS CHECKED GOOD.

Part: SENSOR — FAULTY (CABIN TEMP) · airframe 53,807 hrs · 49,564 cycles

AFTER TAKEOFF, AIRCRAFT DID NOT HOLD PRESSURE AND FORWARD CARGO DOOR LIGHT CAME ON AND OFF IN FLIGHT. REPLACED THE CABIN/FLIGHT RATE OF CHANGE/HIGH LIMIT TEMPERATURE SENSOR IAW DC-9 MM 21-61-03-2.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,750 hrs · 49,515 cycles

EMERGENCY LAMP BY THE OVERHEAD FORWARD ATTENDANCE PANEL (THE AFT LAMP INOPERATIVE). REPOSITIONED CONTACT LEVEL POINT (DOOR CONTACT) AND RELAMPED IAW DC-9 AMM 33-55-00-4.

Part: CONTROL UNIT — DEFECTIVE (E/E BAY) · airframe 53,197 hrs · 49,088 cycles

CARGO FIRE WARNING INDICATED FORWARD BELLY FIRE. SHORTLY AFTER, FIRE LIGHT WENT OUT, FORWARD SMOKE INOPERATIVE LIGHT CAME ON. THEN REPEATED FIRE WARNING AGAIN. COMPLETED EMERGENCY PROCEDURE. REPLACED THE CENTRAL CONTROL UNIT. OPS CHECKED GOOD IAW DC-9 AMM 26-15-00-5.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 53,163 hrs · 49,067 cycles

CREW REPORTED LOWER CARGO FIRE WARNING AT ILN ON GROUND. CFR WAS DISPATCHED TO AIRCRAFT. CFR REPORTED NO FIRES. NO DEFECTS NOTED. SYSTEM CHECKED GOOD IAW DC-9 MM 26.

Part: SKIN — CORRODED (WINDOW BELT) · airframe 51,543 hrs · 48,057 cycles

RIGHT WINDOW BELT DOUBLER CORRODED AT WINDOW NR 14. REPLACED WINDOW BELT AT FUSELAGE STATION 465 - 541 IAW DC9 SRM 51-30-2.

Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 51,543 hrs · 48,057 cycles

SUB FLOOR CRACKED AT STATION 200 AND RBL 22. REPAIRED CRACK IAW DC9 SRM 53-01.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,543 hrs · 48,057 cycles

SUPPORT T-FITTING CRACKED AND CORRODED ON OUTBOARD SIDE OF WHEEL WELL AT APPROX STA 775. REPLACED FORWARD AND AFT FITTINGS IAW DC9 SRM 51-10-4, AND 51-30-5.

Part: FITTING — CORRODED (FUSELAGE) · airframe 51,543 hrs · 48,057 cycles

LEVEL 1 CORROSION ON T-FITTING OUTBOARD SIDE OF WHEEL WELL AT APPROX STA 770. REPLACED T-FITTING IAW DC9 SRM 51-10-4, AND 51-30-5.

Part: DOOR — CORRODED (NLG) · corrosion level 2 · airframe 51,543 hrs · 48,057 cycles

LEFT FORWARD NOSE LANDING GEAR DOOR CORRODED AT AFT END UNDER DEFLECTOR. REPLACED DOOR IAW DC9 MM 32-22-01-2-0004.

Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 51,543 hrs · 48,057 cycles

CRACK IN SUB FLOOR AT STATION 180 AND RBL 4.0. REPAIRED IAW DC9 SRM 53-04.

Part: SHEAR TIE — CRACKED (BS 1056)

DURING C-CHECK, FOUND SHEAR TIE CRACKED AT FS 1056 BETWEEN LONGERON 14L AND 16L. REPLACED SHEAR TIE AND CLIPS IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: WEB — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR STRUCTURE CRACKED ABOVE THE FORWARD HINGE. REPLACED WEB AND FITTING IAW DC9 SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: SHEAR TIE — CRACKED (BS 1021)

DURING C-CHECK, FOUND CRACKED SHEAR TIE AT FS 1021 BETWEEN LONGERON 14L AND 15L. REPLACED SHEAR TIE IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: SHEAR TIE — CRACKED (BS 1021)

DURING C-CHECK, FOUND A CRACKED SHEAR TIE AT FS 1021 BETWEEN LONGERON 15L AND 16L. REPLACED SHEAR TIE IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: RIB — CRACKED (VERT STAB)

DURING C-CHECK, FOUND RIB CRACKED IN THE VERTICAL STABILIZER LEADING EDGE. REPLACED RIB IAW DC9 SRM CHAPTERS 51-30-2 AND 51-30-5.

Part: SHEAR TIE — CRACKED (BS 1021)

DURING C-CHECK, FOUND SHEAR TIE CRACKED AT FS 1021 BELOW LONGERON 14 RT. REPAIRED SHEAR TIE IAW DC9 SRM 53-03, FIG 6.

Part: ROD END — WORN (RT COCKPIT)

FIRST OFFICER'S CLEARVIEW WINDOW DIFFICULT TO OPEN. REPLACED THE FORWARD LOWER ROD END ON THE WINDOW LINKAGE, OPS CHECK GOOD IAW DC-9 MM 56-10-3.

Part: SPRING — MISSING (RT COCKPIT)

AT DEPARTURE TIME, FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT FUNCTION CORRECTLY, HARD TO CLOSE. REINSTALLED THE ACTUATING SPRING FOR THE AFT LOWER WINDOW LATCH, OPS CHECK GOOD IAW DC-9 MM 56-10-3.

Part: TR BUCKET — CRACKED (NR 2 ENGINE)

DURING C-CHECK, THE LOWER THRUST REVERSER BUCKET WAS FOUND CRACKED. THE BUCKET WAS REPLACED IAW DC9 MM 78-30-2.

Part: FITTING — CORRODED (FUSELAGE)

DURING C-CHECK, THE AFT JACK PAD ATTACH FITTING WAS FOUND CORRODED. THE FITTING WAS REPLACED IAW DC-9 SRM 51-30-2.

Part: FRAME — CRACKED (BS 737)

DURING C-CHECK, WHILE ACCOMPLISHING AD 78-07-05, THE MAIN FRAME AT STA 737 LEFT WAS FOUND CRACKED. THE FRAME WAS REPAIRED IAW S/B 53-131 AND REA D953-17522-MR.

Part: SEAT TRACK — CORRODED (BS 195)

DURING C-CHECK, THE SEAT TRACK AT STA 195RBL 44, WAS FOUND CORRODED. THE SEAT TRACK WAS REPAIRED IAW REA D953-17543-DE AND THE DC9 SRM. 51-30-1.

Part: SKIN — DAMAGED (PAX DOORWAY)

DURING C-CHECK, THE FUSELAGE SKIN ON THE AFT SIDE OF THE FWD ENTRY DOOR LOWER CORNER WAS FOUND DAMAGED. THE SKIN WAS REPAIRED IAW REA D953-17518.

Part: VANE — DELAMINATED (RT TE FLAP)

DURING C-CHECK, THE FLAP AFT MOVEABLE VANE WAS FOUND DELAMINATED. THE VANE WAS REPLACED IAW DC-9 MM 27-51-2.

Part: ANGLE — CRACKED (PYLON)

DURING C CHECK, THE LOWER PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPAIRED IAW DC9 SRM 54-04, FIG.10.

Part: DOUBLER — CRACKED (PYLON)

DURING C-CHECK, THE ENGINE PYLON BULKHEAD DOUBLER WAS FOUND CRACKED. THE DOUBLER WAS REPLACED IAW DC-9 SRM 51-30-5.

Part: DOUBLER — CRACKED (FUSELAGE)

DURING C-CHECK, THE FUSELAGE SKIN DOUBLER AT THE MAIN ENTRY DOOR WAS FOUND CRACKED. THE DOUBLER WAS REPLACED IAW DC-9 SRM 51-30-5.

Part: ANGLE — CRACKED (NR 2 PYLON)

DURING C-CHECK, THE LOWER PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPAIRED IAW DC9 SRM 54-04, FIG.10.

Part: DAMPER CRANK — CORRODED (RT AILERON)

DURING C-CHECK, THE AILERON DAMPER CRANK WAS FOUND CORRODED. THE DAMPER WAS REPLACED IAW DC-9 MM 27-10-4.

Part: VANE — CORRODED (RT TE FLAP)

DURING C-CHECK, THE FLAP FORWARD MOVEABLE VANE WAS FOUND CORRODED. THE VANE WAS REPLACED IAW DC-9 MM 27-51-1.

Part: FRAME — CRACKED (BS 737)

DURING C-CHECK, WHILE ACCOMPLISHING AD 78-07-05, THE MAIN FRAME AT STA 737 RT, WAS FOUND CRACKED. THE FRAME WAS REPAIRED IAW REA DC953-17522-MR.

Part: FRAME — CRACKED (BS 737)

DURING C-CHECK, WHILE ACCOMPLISHING AD 78-07-05, THE FUSELAGE MAIN FRAME AT STA 737LT WAS FOUND CRACKED. THE FRAME WAS REPAIRED IAW REA D953-17522-MR AND S/B 53-131.

Part: CARRIAGE — WORN (RT TE FLAP)

DURING C-CHECK, THE FLAP CARRIAGE ROLLERS WERE FOUND WORN. THE CARRIAGE WAS REPLACED IAW DC9 SUP MM 27-51-5.

Part: FRAME — CRACKED (BS 737)

DURING C-CHECK, WHILE ACCOMPLISHING AD 78-07-05, THE MAIN FRAME AT STA 737 LT WAS FOUND CRACKED. THE FRAME WAS REPAIRED IAW REA DC953-17522-MR.

Part: ANGLE — CRACKED (NR 1 PYLON)

DURING C CHECK, THE LOWER PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPAIRED IAW DC-9 SSRM DRAWING NR K-05683.

Part: ANGLE — CRACKED (BS 1041)

DURING C CHECK, THE SEAT TRACK ATTACH ANGLE AT STA 1041 LONG 27 LT, WAS FOUND CRACKED. THE ANGLE WAS REPLACED IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: VANE — CORRODED (RT TE FLAP)

THE RIGHT WING FORWARD FLAP VANE WAS CORRODED ALONG THE TRAILING EDGE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.

Part: ANGLE — CRACKED (NR 2 PYLON)

DURING C-CHECK, THE PYLON UPPER FUSELAGE ATTACH ANGLE AT STA 1072, WAS FOUND CRACKED. THE ANGLE WAS REPAIRED IAW DC-9 SRM 54-04, FIG.10.

Part: COWL FRAME — GOUGED (NR 1 ENGINE)

DURING C-CHECK, THE UPPER COWL INBOARD LONGERON FRAME WAS FOUND GOUGED. THE COWL WAS REPAIRED IAW ABX DWG K05013.

Part: ANGLE — CRACKED (FUSELAGE)

DURING C-CHECK, THE VENTRAL STAIR RIGHT HINGE ATTACH ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPLACED IAW DC9 SRM 51-10-4.

Part: VANE — DELAMINATED (RT TE FLAP)

THE RIGHT AFT FLAP VANE HAD LARGE AREA'S OF DELAMINATION ON BOTH THE UPPER AND LOWER TRAILING EDGE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC9 SRM.

Part: TR FAIRING — CRACKED (NR 1 PYLON)

DURING C-CHECK, THE LOWER THRUST REVERSER BUCKET FAIRING WAS FOUND CRACKED. THE FAIRING WAS REPLACED IAW DC-9 SRM 51-30-2.

Part: ANGLE — CRACKED (NR 1 PYLON)

DURING C-CHECK, THE PYLON UPPER SPAR CAP ANGLE AT THE OUTBOARD END WAS FOUND CRACKED. THE ANGLE WAS REPLACED IAW REA D954-17521.

Part: GUIDE RAIL — GOUGED (BS 218)

DURING C-CHECK, THE GUIDE RAIL AT STA 218 LBL 45, WAS FOUND GOUGED. THE GUIDE RAIL WAS REPLACED IAW DC-9 SRM.

Part: TR FAIRING — CRACKED (NR 1 ENGINE)

DURING C-CHECK, THE UPPER THRUST REVERSER BUCKET FAIRING WAS FOUND CRACKED. THE FAIRING WAS REPLACED IAW DC-9 SRM 51-30-2.

Part: TAB — WORN (RT AILERON)

DURING C-CHECK, THE AILERON TRIM TAB INBOARD HINGE WAS FOUND WORN. THE TRIM TAB WAS REPLACED IAW DC-9 MM 27-10-5.

Part: CARRIAGE — WORN (LT TE FLAP)

DURING C-CHECK, THE FLAP CARRIAGE ASSEMBLY WAS FOUND WORN. THE CARRIAGE ASSEMBLY WAS REPLACED IAW DC-9 SUP MM 27-51-5.

Part: SEAT TRACK — CORRODED (BS 190)

DURING C CHECK, THE SEAT TRACK AT STA 190 RBL 22 WAS FOUND CORRODED. THE TRACK WAS REPAIRED IAW DC-9 SRM 53-05, FIG. 4A.

Part: DEPRESSOR — CRACKED (RT MLG DOOR)

DURING C-CHECK, THE MAIN LANDING GEAR OUTBOARD DOOR SEAL DEPRESSOR WAS FOUND CRACKED. THE DEPRESSOR WAS REPLACED IAW DC-9 SRM 51-30-2.

Part: BEARING — WORN (LT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND THE LEFT MAIN LANDING GEAR DOOR ROD ASSEMBLY BEARING WORN AT WELL ON OUTBOARD MAIN LANDING GEAR DOOR. REPLACED BEARING IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: BEARING — WORN (RT MLG DOOR)

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

Part: AIR DISTR — ODOR (COCKPIT)

ORD - AFTER TAKEOFF, CREW REPORTED A STRONG RUBBER ODOR. INSPECTED TIRES, NOSE BRAKES AND ENGINE INLETS, FOUND NO DEFECTS.

Part: SLIDING WINDOW — OUT OF ADJUST (COCKPIT)

DURING POST FLIGHT INSPECTION, FOUND FIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. CLEANED TRACK, REPOSITIONED OPERATING ASSEMBLY AT TOP OF WINDOW AND LUBRICATED. OPS CHECKED GOOD IAW DC-9 MM.

Part: EEL POWER SUPPLY — DEFECTIVE (CABIN)

DURING SERVICE CHECK, EMERGENCY LIGHTS STAYED ON WHEN SWITCH PLACED IN OFF POSITION. REPLACED EMERGENCY EXIT LIGHT SUPPLY IAW DC-9 SUPP MM 33-54-0. OPS CHECKED GOOD.

Part: LE SKIN — DENTED (NR 3 SLAT)

DURING C - CHECK INSPECTION, FOUND DENT IN THE LEADING EDGE OF THE NR 3 SLAT ON THE LEFT WING. REPAIRED IAW DC-9 SRM 57-03, FIG. 14A.

Part: ANGLE — CRACKED (WS 360)

DURING C - CHECK INSPECTION, FOUND LEFT FLAP ATTACH ANGLE FOR OUTBOARD HINGE CRACKED INSIDE THE FLAP. REPLACED ANGLE IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: ANGLE — CRACKED (WS 360)

DURING C - CHECK INSPECTION, FOUND LEFT FLAP ATTACH ANGLE FOR OUTBOARD HINGE CRACKED INSIDE THE FLAP. REPLACED ANGLE IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: FITTING — CRACKED (WS 137)

DURING C - CHECK INSPECTION, FOUND RIGHT WING SLAT ACTUATING MECHANISM INBOARD ATTACH FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: LE SKIN — DENTED (NR 1 SLAT)

DURING C - CHECK INSPECTION, FOUND DENT IN LEADING EDGE OF THE NR 1 SLAT ON THE LEFT WING. REPAIRED IAW DC-9 SRM 57-03, FIG. 14A.

Part: BOLT — WORN (LT MLG DOOR)

DURING C - CHECK INSPECTION AND COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT OUTBOARD MAIN LANDING GEAR DOOR ARM ASSEMBLY HAD EXCESSIVE PLAY. REPLACED BOLT IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: FITTING — WORN (LT MLG DOOR)

DURING C - CHECK INSPECTION AND COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT OUTBOARD MAIN LANDING GEAR DOOR LINK ASSEMBLY HAD EXCESSIVE PLAY. REPLACED FITTING IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: EEL BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHTS VERY DIM. REPLACED THE EMERGENCY LIGHT BATTERIES IAW DC-9 MM CHAPTER 33. OPS CHECKED GOOD.

Part: ANGLE — CRACKED (LT PYLON)

DURING COMPLIANCE OF CORROSION TASK 80-54300, FOUND NR 1 ENGINE UPPER PYLON TO FUSELAGE ATTACH ANGLE TO BE CRACKED. REPAIRED IAW ABX REA D954-11280-MR.

Part: ANGLE — CRACKED (RT PYLON)

DURING COMPLIANCE OF CORROSION TASK 80-54300, FOUND THE NR 2 ENGINE LOWER PYLON TO FUSELAGE ATTACH ANGLE CRACKED. REPAIRED IAW ABX REA D954-11280-MR.

Part: ANGLE — CRACKED (RT PYLON)

DURING COMPLIANCE OF CORROSION TASK 80-54300, FOUND THE NR 2 ENGINE UPPER PYLON TO FUSELAGE ATTACH ANGLE CRACKED. REPAIRED IAW ABX REA D954-112080-MR.

Part: ANGLE — CRACKED (LT PYLON)

DURING COMPLIANCE OF CORROSION TASK 80-54300, FOUND THE NR 1 ENGINE LOWER PYLON TO FUSELAGE ATTACH ANGLE CRACKED. REPAIRED IAW ABX REA D954-11280-MR.