N956AX

Part: CIRCUIT BREAKER — DEFECTIVE (CABIN PRESSURE) · airframe 40,541 hrs · 44,949 cycles

COULD NOT PRESSURIZE AIRCRAFT IN AUTO OR MANUAL. FOUND CABIN PRESSURE CONTROL 2 AMP CIRCUIT BREAKER WOULD NOT RESET. REPLACED 2 AMP CIRCUIT BREAKER. PRESSURIZED AIRCRAFT TO 6 PSI, AIRCRAFT PRESSURIZED NORMALLY PER AMM CHAPTER 21.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 40,434 hrs · 44,842 cycles

INTERCOSTAL AT STA 180, LEFT BUTT LINE 19 ON BOTH SIDES OF FLOOR BEAM WAS CRACKED. REPAIRED INBOARD INTERCOSTAL STA 180, LEFT BUTT LINE 19 IAW DC9 SRM. OUTBOARD INTERCOSTAL TO BE REPAIRED ON NON ROUTINE 0523.

Part: CARGO TRACK — CORRODED (FWD CARGO ABY) · airframe 40,434 hrs · 44,842 cycles

UPPER CARGO TRACKS WERE CORRODED AT FLOOR PANEL 3F ATTACH POINTS. REPAIRED SEAT TRACK IAW REA D957-56383.

Part: FITTING — CRACKED (FUSELAGE) · airframe 40,434 hrs · 44,842 cycles

LONGERON END FITTING CRACKED ON FORWARD END LONGERON 26 RIGHT INSIDE KIDNEY AREA. REMOVED AND REPLACED LONGERON END FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,434 hrs · 44,842 cycles

LITE CORROSION ON UPPER CARGO CENTER SEAT TRACK STA 256 - 294. REPLACED SECTION OF TRACK IAW DC9 51-30-1.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,434 hrs · 44,842 cycles

INTERCOSTAL CRACKED AT STA 370, LONGERON 30 AND 2 GUSSETS GOUGED. REMOVED AND REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 40,278 hrs · 44,684 cycles

WHILE COMPLYING WITH WINDOW FRAME MOD EA53000041, FOUND CRACKED FRAME. REPAIRED AREA IAW DC9 SRM 53-03, FIG 34.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 40,278 hrs · 44,684 cycles

WHILE COMPLYING WITH WINDOW FRAME MOD EA 53000041, FOUND CRACKED FRAME. REPAIRED AREA IAW DC9 SRM 53-03, FIG 34.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 40,278 hrs · 44,684 cycles

WHILE COMPLYING WITH WINDOW FRAME MOD EA 53000041, FOUND CRACKED FRAME. REPAIRED AREA IAW DC9 SRM 53-03, FIG 34.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 39,773 hrs · 44,174 cycles

ON PRE-DEPARTURE CHECK, FOUND EMERGENCY LIGHTING INOPERATIVE. REMOVED AND REPLACED POWER BATTERY PACK IAW DC9 MM 33-53-02-4, OPS CHECKED GOOD.

Part: STUD — BROKEN (FLAP HINGE) · airframe 39,104 hrs · 43,476 cycles

RIGHT WING OUTBOARD FLAP HINGE, STA 333, INBOARD LOWER STUD BROKEN OFF. REMOVED AND REPLACED ALL 4 STUDS IAW JOB CARD 92410004 AND DC-9 SRM.

Part: PRESSURE PANEL — CORRODED (LT MLG WW) · airframe 39,104 hrs · 43,476 cycles

AREA OF EXFOLIATION ON UPPER PRESSURE PANEL, MAIN FRAME AREA. REMOVED AND REPLACED DOUBLERS IAW DC-9 SRM 51-30-5.

Part: WEB — CRACKED (FUSELAGE) · airframe 38,085 hrs · 42,304 cycles

WEB CRACKED FS 200 LONGERON 8 LEFT. REPAIRED AREA IAW REA-D953-48739.

Part: FITTING — CRACKED (CARGO DOOR BEAM) · airframe 38,085 hrs · 42,304 cycles

CARGO DOOR BEAM NR 2 AFT END FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-5.

Part: ATTACH ANGLE — CRACKED (AFT FUSELAGE) · airframe 38,085 hrs · 42,304 cycles

NR 1 ENGINE UPPER PYLON ATTACH ANGLE WAS CRACKED AT STA 1114. REPAIRED AREA IAW DC-9 SRM 54-04.

Part: SKIN — CRACKED (AFT FUSELAGE) · airframe 38,085 hrs · 42,304 cycles

FUSELAGE SKIN WAS CRACKED AT LONGERON 3 RIGHT, STA 1163. REPAIRED SKIN WITH DOUBLER IAW DC-9 SRM 53-01.

Part: FITTING — CRACKED (LT WHEEL WELL) · airframe 38,085 hrs · 42,304 cycles

FITTING INSIDE OF KEEL AT STA 737 CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-5.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 38,085 hrs · 42,304 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 38,085 hrs · 42,304 cycles

FUSELAGE SKIN BULGED AND RIVET PULLED AT STA 1072. REPAIRED AREA IAW DC-9 SRM 53-04.

Part: SWITCH — FAULTY (NLG) · airframe 37,835 hrs · 42,048 cycles

DURING CRUISE FLIGHT, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. RIGHT HYDRAULIC SWITCH ON, 3000 PSI DID NOT RESOLVE THE PROBLEM. WHEN GEAR SELECTED DOWN, UNSAFE LIGHT REMAINED ILLUMINATED. GEAR DOWN LIGHT REMAINED OFF. DECLARED EMERGENCY. REPLACED THE NOSE GEAR DOWN LOCK SWITCH IAW AMM 32-60-01-2. SWUNG THE GEAR SEVERAL TIMES, OPERATIONAL CHECK GOOD.

Part: CONTROL BOX — DEFECTIVE (E & E) · airframe 37,573 hrs · 41,768 cycles

RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. GEAR RECYCLED. ABNORMAL COMPLIED WITH FOR RETURN FLIGHT TO ILN. REMOVED AND REPLACED PROX. CONTROL BOX. PERFORMED ADJUSTMENT TEST OF LANDING GEAR POSITION AND WARNING INDICATION SYSTEM IAW DC-9 MM 32-60-00-2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 37,035 hrs · 41,178 cycles

TEE FITTING WAS CRACKED - FORWARD END OF INTERCOSTALS, AT STA 218, L28L AND L28R. REPLACED FITTING IAW DC-9 SRM 51-30-1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 37,035 hrs · 41,178 cycles

FITTING WAS CRACKED OVER L29L AT FS 675. REPLACED CRACKED FITTING IAW DC-9 SRM 51-30-5.

Part: FITTING — CRACKED (SPOILER) · airframe 37,035 hrs · 41,178 cycles

INBOARD SPOILER TORSION BAR CENTER SUPPORT FITTING WAS CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-5.

Part: LINE — BROKEN (NR 2 ENGINE) · airframe 36,443 hrs · 40,674 cycles

DURING CRUISE, THE NR 2 ENGINE AT 240, A LOUD BANG OCCURRED WITH AN IMMEDIATE DROP IN THE EPR FROM 1.85 TO 1.60. N1 AND N2 DROPPED APPROXIMATELY 20 PERCENT FROM THE PREVIOUS SETTING. NO OTHER WARNING INDICATED. EMERGENCY DECLARED. AIR DIVERTED INTO STL. FOUND PS4 LINE AT THE TOP OF THE ENGINE BROKEN AT THE FITTING. REPLACED THE PS4 LINE PER REA D971-42069. GROUND RAN ENGINE TO TAKEOFF POWER AND CHECKED ANTI-SURGE BLEED SCHEDULING IAW DC-9 AMM 71-00-00-5. ALL SYSTEMS OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,440 hrs · 40,671 cycles

EMERGENCY EVACUATION LIGHTS WOULD NOT TEST. REPLACED THE EMERGENCY LIGHTS BATTERIES. OPS CHECKED GOOD IAW DC-9 AMM 33-53-02-4.

Part: FITTING — CRACKED (LEFT WING) · airframe 36,431 hrs · 40,666 cycles

DURING REPLACEMENT OF THE LEFT WING LOWER AFT SPAR, INSPECTION FOUND WING BULKHEAD ATTACH FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-5.

Part: FITTING — CRACKED (LEFT WING) · airframe 36,431 hrs · 40,666 cycles

DURING REPLACEMENT OF THE LEFT WING LOWER AFT SPAR, INSPECTION FOUND WING BULKHEAD ATTACH FITTING CRACKED. LOCATED AT STATION XRS 111, STRINGER 11. REPLACED FITTING IAW DC-9 SRM 51-30-5.

Part: FITTING — CRACKED (LT MLG WW) · airframe 36,429 hrs · 40,664 cycles

DURING PREFLIGHT, CREW REPORTED FUEL SEEP FROM THE WHEEL WELL AREA. INSPECTION FOUND A CRACK 1 INCH LONG ABOVE THE SKI FITTING NEAR THE VERTICAL ATTACH FITTING IN THE LEFT WHEEL WELL.

Part: SENSOR — FAILED (PROXIMITY) · airframe 35,669 hrs · 40,118 cycles

A NOSE LANDING GEAR UNSAFE INDICATION LIGHT ILLUMINATED IN FLIGHT. THE LIGHT EXTINGUISHED WHEN THE LANDING GEAR WAS SELECTED DOWN DURING APPROACH FOR LANDING. MAINTENANCE INSPECTED AND REPLACED THE PROX SENSOR CONTROL UNIT IAW DC-9 MM 32-60-01. OPS CHECKED GOOD.

Part: PAN — CRACKED (CARGO DOOR) · airframe 35,470 hrs · 39,991 cycles

AFT LOWER CARGO DOOR INNER PAN CRACKED AT AFT HINGE CUTOUT. REPAIRED AFT LOWER CARGO DOOR IAW DC9 REA D952-38414.

Part: FLOORBEAM — CRACKED (CABIN) · airframe 35,470 hrs · 39,991 cycles

FLOORBEAM WAS CRACKED AT STA 718 LT BUTT LINE. REPLACED FLOORBEAM SECTION AT STA 718 LEFT SIDE IAW DC9 SRM 51-30-2 & 51-30-5.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 35,470 hrs · 39,991 cycles

FLOORBEAM VERTICAL SUPPORT WAS CRACKED AT STA 718 RT BUTT LINE 44 ABOVE CENTER TANK. REPLACED FLOORBEAM VERTICAL SUPPORT IAW DC9 SRM 51-30-1 & 51-30-5.

Part: FLOORBEAM — CRACKED (CABIN) · airframe 35,470 hrs · 39,991 cycles

FLOORBEAM WAS CRACKED AT STATION 718 RT BUTT LINE 54. REPLACED FLOORBEAM AT STA 718 IAW DC9 SRM.

Part: INTERCOSTAL — CRACKED (CARGO BAY) · airframe 35,470 hrs · 39,991 cycles

AFT LOWER CARGO STA 1013 0 BUTT LINE INTERCOSTAL CRACKED AT UPPER AFT CORNER (CEILING). REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2.

Part: PAN — CRACKED (CARGO DOOR) · airframe 35,470 hrs · 39,991 cycles

FORWARD LOWER CARGO DOOR OUTER PAN CRACKED AT UPPER AFT HINGE BRACKET IN RADIUS NEAR DOOR STOP. REPAIRED CRACKED PAN IAW DC9 SRM REF: 52-03.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 35,470 hrs · 39,991 cycles

PRESSURE PANEL DOUBLER IN RIGHT WHEEL WELL AT STA 756 WAS CRACKED. REPLACED PRESSURE PANEL DOUBLER IAW DC9 DWG NR 9910155.

Part: PAN — CRACKED (CARGO DOOR) · airframe 35,470 hrs · 39,991 cycles

FORWARD LOWER CARGO DOOR OUTER PAN CRACKED AT UPPER FORWARD HINGE BRACKET. REPLACED HINGE BRACKET IAW DC9 SRM REF: 51-30-1. REPAIRED CRACKED PAN IAW DC9 SRM REF: 52-03.

Part: SWITCH — MALFUNCTIONED (ACM BAY)

AT APPROXIMATELY 17,000 FEET CLIMBING OUT OF KMEM, CABIN PRESSURE STARTED DECREASING FOLLOWED BY THE CABIN PRESSURE WARNING LIGHT ILLUMINATING. DONNED OXYGEN MASKS AND DESCENDED TO 10,000 FEET. BOTH AIR CONDITIONING PACKS WOULD CYCLE ON AND OFF. COULD NOT GAIN CONTROL OF THEM. REPLACED LEFT AND RIGHT SECOND SEGMENT CLIMB SWITCHES IAW DC9 MM 21-31-09.

Part: POWER SUPPLY — FAILED (CABIN)

EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY.

Part: BATTERY PACK — DISCHARGED (CABIN)

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

Part: VANE — DELAMINATED (RT TE FLAP)

RIGHT WING FLAP CENTER FIXED VANE DELAMINATED ON LOWER SURFACE AT INBOARD END. REPLACED VANE IAW DC9 MM 27-51-3.

Part: LONGERON — CRACKED (BS 1056 & 1041)

LONGERON 17 LEFT CRACKED AT STATION 1056 AND 1041. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: WEB — CRACKED (BS 1041)

RIGHT CUSP WEB CRACKED AT STATION 1041 UNDER RIGHT OUTBOARD SEAT TRACK. REPAIRED CUSP WEB IAW DC9 SRM 53-01.

Part: LONGERON — CRACKED (BS 1041)

LONGERON 16 RIGHT CRACKED AT STATION 1041. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: LONGERON — CRACKED (BS 1041)

LONGERON 17 RIGHT CRACKED AT STATION 1041. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: WEB — CRACKED (BS 1041)

LEFT OUTBOARD CUSP WEB AT STATION 1041 FRAME, CRACKED IN 3 PLACES UNDER LEFT OUTBOARD SEAT TRACK, LBL 54. REPAIRED CUSP WEB IAW DC9 SRM 53-04.

Part: CONNECTOR — CORRODED (RT MLG)

DURING INITIAL CLIMB, AFTER RAISING THE LANDING GEAR, THE RIGHT GEAR UNSAFE LIGHT REMAINED ON. RECYCLED THE GEAR, LIGHT STILL REMAINED ON. LIGHT WENT OUT AFTER THREE MINUTES, WITH THE ENGINE DRIVEN HYDRAULIC PUMPS IN HIGH. CLEANED CORROSION FROM PROXIMITY SWITCH CANNON PLUG. OPS CHECKED GOOD.

Part: ACTUATOR FITTING — CRACKED (RT MLG DOOR)

DURING C-CHECK, FOUND THE RT MLG DOOR ACTUATOR ATTACH FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND ADJUSTED DOOR AND ACTUATOR IAW 32-32-4 AND 32-10-0.

Part: TAB — DELAMINATED (LT AILERON)

DURING C-CHECK, FOUND THE LT AILERON CONTROL TAB DELAMINATED. *S/D* REPLACED LT AILERON IAW DC9 MM 27-10-2.

Part: BRACKET — CRACKED (AFT ACCESS COMP)

DURING C-CHECK, FOUND THE RT GROUND COOLING FAN ATTACH BRACKET ON FRAME 1163 INBOARD LEG CRACKED AT BOTTOM RIVET. REPLACED BRACKET IAW DC-9 SRM 51-30-5 AND 51-30-2.

Part: SHEAR TIE — CRACKED (BS 1052)

DURING C-CHECK, FOUND A CRACKED SHEAR TIE AT LONG 16L STA 1052. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5.

Part: ANGLE — CRACKED (LT PYLON)

DURING C-CHECK, FOUND THE LT PYLON STIFFENER ANGLE CRACKED AT STA 980. REPAIRED IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: CUSP WEB — TORN (BS 1000)

DURING C-CHECK, FOUND CUSP WEB TORN AT STA 1000 RBL 52. REPAIRED CUSP WEB IAW DC-9 SRM 53-01.

Part: BRACE — CRACKED (BS 775)

DURING C-CHECK, FOUND THE FWD SIDE BRACE AT FS 775 AT THE OUTBOARD SIDE OF THE RT MLG WHEEL WELL CRACKED. REPLACED BRACE ASSY IAW DC9 SRM 51-30-1.

Part: SEAT TRACK — CORRODED (BS 492-530)

DURING C-CHECK, FOUND SEAT TRACK AT RBL 22 AND STA 492 TO 530 CORRODED BEYOND LIMITS. REPLACED SEAT TRACK IAW DC-9 SRM 53-05.

Part: TAB — DELAMINATED (RT ELEVATOR)

DURING C-CHECK, FOUND THE RIGHT ELEVATOR CONTROL TAB DELAMINATED. *S/D* REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.

Part: TRIM TAB — DELAMINATED (LT AILERON)

DURING C-CHECK, FOUND LEFT HAND AILERON TRIM TAB DELAMINATED. *S/D* REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS.

Part: SHEAR TIE — CRACKED (BS 1052)

DURING C-CHECK, FOUND A CRACKED SHEAR TIE AT LONG 16L AND STA 1052. *S/D* REPAIRED SHEAR TIE IAW DC9 SRM 51-30-2.

Part: BRACKET — CRACKED (BS 785)

DURING C-CHECK, FOUND CRACKED BRACKET IN THE AFT SIDE ON RT MLG WHEEL WELL AT FS 785 AND LONG 22R. REPLACED BRACKET IAW DC-9 SRM 51-30-5.

Part: FRAME — CRACKED (BS 1244)

DURING C-CHECK, FOUND THE CANTED FRAME AT STA 1244 CRACKED ON RT SIDE 1 FT BELOW THE SPLICE AT THE RUDDER POWER PACK LINE. REPAIRED IAW ABX REA D953-20187MR.

Part: VANE — DELAMINATED (RT TE FLAP)

DURING C-CHECK, FOUND RIGHT WING CENTER FIXED VANE DELAMINATED ON THE UPPER SURFACE. *S/D* REPLACED ALL HONEYCOMB CORE DOUBLERS AND SKIN.

Part: FITTING — CRACKED (RT MLG ACTUATOR)

DURING C-CHECK, FOUND THE RT MAIN LANDING GEAR DOOR ACTUATOR ATTACH FITTING IS CRACKED. *S/D* REPLACED FITTING IAW DC9 SRM 51-30-1.

Part: CONTROL TAB — CORRODED (LT ELEVATOR)

DURING C-CHECK, FOUND THE LT ELEVATOR CONTROL TAB UPPER AND LOWER SURFACE CORRODED AT THE L/E SEAM. *S/D* REPAIRED UNIT COMPLETE.

Part: FITTING — CRACKED (CARGO DOOR)

DURING C-CHECK, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR BOTTOM INTERNAL STIFFENER AND THE FORWARD AND AFT FITTINGS CRACKED. *S/D* REPAIRED IAW DC-9 SRM 52-30-00.

Part: FITTING — CRACKED (BS 775)

DURING C-CHECK, FOUND THE RT FLOORBEAM TO KEEL ATTACH FITTING FS 775 CRACKED. *S/D* REPLACED FITTING IAW DC9 S/B 53-80.

Part: CUSP WEB — CRACKED (BS 655)

DURING C-CHECK, FOUND THE CUSP WEB CRACKED IN THREE PLACES AT STA 655 RBL 54. *S/D* REPLACED CUSP WEB IAW DC9 SRM 51-30-1.

Part: CONNECTOR — BENT (RT MLG DOOR)

DURING CLIMB, GEAR DOOR LIGHT REMAINED ON WITH GEAR RETRACTED. RECYCLED GEAR WITH NO CHANGE. FOUND CONNECTOR P1-1154 WITH BENT PIN C. STRAIGHTENED PIN AND REINSTALLED CONNECTOR, OPS CHECKED IAW DC9 MM 32-00.

Part: DISPLAY — DEFECTIVE (RT COCKPIT)

FIRST OFFICERS EADI FAILED INFLIGHT, A SLIGHT BURNING ODOR WAS NOTICED IMMEDIATELY AFTERWARDS. REPLACED FIRST OFFICERS DU 2 IAW DC-9 SUPP MM 34-20-0.

Part: POWER SUPPLY — DEFECTIVE (CABIN)

EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW DC-9 MM 33-53-0.

Part: BOLT — WORN (RT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT HAND MAIN LANDING GEAR OUTBOARD DOOR LINKAGE TO HAVE EXCESSIVE PLAY AT LINKAGE ROD PIVOT POINT. REPLACED ATTACH BOLT IAW DC9 OVERHAUL MANUAL 32-10-6.

Part: BUSHING — WORN (RT MLG DOOR)

DURING COMPLIANCE OF AD 91-22-07; ASB 32-244 FOUND RIGHT HAND MAIN LANDING GEAR OUTBOARD LINKAGE TO HAVE EXCESSIVE PLAY AT LINKAGE ROD PIVOT POINT. REPLACED LINKAGE ROD BUSHING IAW DC9 OVERHAUL MANUAL 32-10-6.

Part: SKIN — CORRODED (BS 623)

DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON FUSELAGE SKIN AT STA 623 BETWEEN LONGERONS 25L AND 25R. REPAIRED IAW DC-9 SRM 53-04, FIGURE 43.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING PREDEPARTURE CHECK, FOUND EMERGENCY LIGHTS DIM. REPLACED NICAD BATTERIES IN EMERGENCY LIGHTS POWER SUPPLY IAW DC-9 SUPP MM 33-50-0. OPS CHECKED GOOD.

Part: ROD END — WORN (LT MLG DOOR)

DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD DOOR ATTACH ROD END LOOSE IN ATTACH ROD. REPLACED ROD ASSEMBLY IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: BUSHING — WORN (RT MLG DOOR)

DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND BUSHING FOR ATTACH ROD TO FOLLOW UP ROD WORN ON RIGHT MAIN LANDING GEAR OUTBOARD DOOR. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: BUSHING — WORN (RT MLG DOOR)

DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND BUSHING WORN IN THE ARM ASSEMBLY ON THE RIGHT OUTBOARD MAIN LANDING GEAR DOOR. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6.

Part: BUSHING — WORN (LT MLG DOOR)

DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND WORN BUSHING IN ARM ASSEMBLY ON THE LEFT OUTBOARD MAIN LANDING GEAR DOOR. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6.