N484AA

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 73,987 hrs · 38,953 cycles

LEFT 1 DOOR PORTABLE EMER LIGHT FAILED TEST. REPLACED LT NR 1 DOOR PORTABLE EMER LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: TRIM MOTOR — INOPERATIVE (HORIZ STAB) · airframe 72,904 hrs · 38,347 cycles

ORD CREW REPORTED RUNAWAY STAB TRIM FULL NOSE DOWN. EMERGENCY DECLARED FLIGHT LANDED ORD WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED PRIMARY STAB TRIM MOTOR. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: GENERATOR — FAILED (LEFT) · airframe 71,196 hrs · 37,366 cycles

DFW CREW REPORTED LT GENERATOR FAILED & AUXILIARY POWER UNIT WOULD NOT START. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: DUCT — LEAKING (BLEED AIR SYS) · airframe 71,095 hrs · 37,307 cycles

TUS CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED ON CLIMB OUT. EMERGENCY DECLARED FLIGHT RETURNED TUS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED CARD 36-95-14 & REPAIRED ASSOCIATED LEAKS. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,794 hrs · 36,590 cycles

LONGERON 23 LEFT CRACKED AT STATION 200 AT BELTFRAME ATTACH POINT. ACCOMPLISHED LONGERON 23 LEFT SPLICE REPAIR FROM STATIONS 190 TO 229 PER SRM 53-02-00.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,794 hrs · 36,590 cycles

LONGERON 24 LEFT CRACKED AT STATION 200 AT BELTFRAME ATTACH POINTS. ACCOMPLISHED LONGERON 24L SPLICE REPAIR FROM STATIONS 165 TO 229 PER SRM 53-02-00.

Part: START VALVE — FAILED (LT ENGINE) · airframe 67,856 hrs · 35,472 cycles

MEM - INFLIGHT HSV-DFW. CREW REPORTED LEFT ENGINE START VALVE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT DIVERTED MEM LANDED WITHOUT INCIDENT. LEFT ENGINE START VALVE INDICATION WAS PLACARD PER MEL AND FLIGHT CONTINUED TO DESTINATION. REPLACED START VALVE AT SAN ON 06/01/2012. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,222 hrs · 35,127 cycles

RIGHT CUSP FROM STATIONS 237 TO 313 CORRODED. REPLACED CUSP PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,222 hrs · 35,127 cycles

RIGHT CUSP FROM STATIONS 313 TO 316 CORRODED. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,222 hrs · 35,127 cycles

RIGHT CUSP AT STATION 915 CORRODED. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,222 hrs · 35,127 cycles

SEAT TRACK NUMBER 5 CORRODED FROM STATIONS 203 TO 205. REPLACED SEAT TRACK AND SPLICE PER SRM 53-05-00.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,222 hrs · 35,127 cycles

AFT CARGO DOOR JAMB UPPER WEB HAS CORROSION SEVERAL PLACES BETWEEN STATIONS 1155 TO 1212. INSTALLED FASTENERS PER SRM 51-30-05 AND SRM 51-30-02.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,222 hrs · 35,127 cycles

AFT CARGO DOOR JAMB UPPER WEB HAS CORROSION SEVERAL PLACES BTWN STATIONS 1155 TO 1212. REPLACED WEB PER AARD 51-10-00-5.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,222 hrs · 35,127 cycles

AFT CARGO DOORWAY LOWER BEAM VERTICAL LEG HAS CORROSION SEVERAL PLACES BETWEEN STATIONS 1155 TO 1212. INSTALLED DOOR BEAM DOUBLER REPAIR PER AARD 53-10-00-3.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,222 hrs · 35,127 cycles

CORROSION ON SUBFLOOR, STATIONS 220 TO 226, RIGHT BUTTLINES 47 TO 50. INSTALLED SERVICEABLE CUSP SHEET FROM STATIONS 218 TO 237 RIGHT PER AARD 51-10-00-5 AND AARD 53-20-00-16.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 67,222 hrs · 35,127 cycles

CORROSION ON RIGHT NUMBER AFT TIE-DOWN TRACK AT FASTENER HOLES STATIONS 1212 TO 1287. INSTALLED AFT RIGHT TIEDOWN TRACK PER SRM 51-30-01.

Part: ATTACH FITTING — DAMAGED (FUSELAGE) · airframe 67,222 hrs · 35,127 cycles

AFT CARGO STATION 1174 DOORWAY INTERCOSTAL ATTACH CLIP HOLE ELONGATED. REMOVED AND INSTALLED NEW CLIP PER AARD 51-10-00-5 AND DRAWING 5936065.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 67,222 hrs · 35,127 cycles

FRAME FOOT AT STATION 218 GOUGED. INSTALLED NEW FOOT FITTING AT STATION 218 PER SRM 51-30-05 AND SRM 51-30-01.

Part: CASTING — CRACKED (RT SPOILER) · airframe 67,222 hrs · 35,127 cycles

RIGHT WING, GROUND SPOILER CASTING CRACKED IN OUTBOARD FORWARD RADIUS AREA. REMOVED AND INSTALLED RIGHT GROUND SPOILER CASTING PER AARD 51-10-00-5 AND SRM 51-30-02.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 67,222 hrs · 35,127 cycles

SUBFLOOR CRACKED UNDER FORWARD GALLEY DRAIN PAN. ROUTED OUT DAMAGED MATERIAL AND INSTALLED DOUBLER REPAIR AS PER AARD 53-20-00-16.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 67,222 hrs · 35,127 cycles

RIGHT STATION 915 CUSP CRACKED. CUT OUT DAMAGED MATERIAL AND INSTALLED DOUBLER REPAIR AS PER AARD 53-20-00-16.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 67,222 hrs · 35,127 cycles

LEFT CUSP FROM STATIONS 633 TO 635 DAMAGED. INSTALLED DOUBLER FROM STATIONS 632 TO 639 PER AARD 53-20-00-16.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 67,222 hrs · 35,127 cycles

LOWER LEFT VAULT DOOR STOP ON JAMB INTERNAL SUPPORT IS CRACKED. REPLACED STOP FITTING PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,222 hrs · 35,127 cycles

RIGHT STATION 838, OUTBOARD OF NUMBER 6 SEAT TRACK, CUSP SHEET HAS CORROSION AT LIGHTENING HOLE. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR AS PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 67,222 hrs · 35,127 cycles

AFT CARGO DOOR OUTER SKIN HAS 5 DENTS IN AN AREA BETWEEN THE NUMBER 4 AND 5 BEAM. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM 53-04-03 FIGURE 3.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 67,222 hrs · 35,127 cycles

RIGHT ELEVATOR HAS PUNCTURE HOLE ON BOTTOM SKIN. INSTALLED REPAIR DOUBLER PER SRM 55-03-00 AND EA COMP-55-022099 DATED 2/27/2012.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 66,513 hrs · 34,723 cycles

DFW - CAPTAIN REPORTED SLIGHT POWER INCREASE THEN LOUD CRACK/BOOM SOUND WAS HEARD WITH SLIGHT SHAKING IN STICK NO FLUCTUATIONS IN PARAMETERS WERE NOTED. STRONG BURNING SMELL WAS INSIDE CABIN AND COCKPIT WAS THEN NOTED. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. NO FAULTS WERE FOUND. REPLACED LEFT AFT SMOKE DETECTOR IN MID CARGO. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CIRCUIT BREAKER — DEFECTIVE (AUTOPILOT SYS) · airframe 66,181 hrs · 34,538 cycles

DFW - CREW REPORTED CIRCUIT BREAKER 17 POPPED CAUSING AUTOPILOT AND AUTO-THROTTLES TO DISCONNECT. YAW DAMP OFF LIGHT AND MACH TRIM INOPERATIVE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CIRCUIT BREAKER 17 AND FLIGHT GUIDANCE CONTROL PANEL. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

DFW RIGHT NUMBER 1 DOOR EMERGENCY EXIT LIGHT LENS IS BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT RIGHT NUMBER 1 DOOR.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,394 hrs · 30,855 cycles

FORWARD CARGO DOOR THRESHOLD PAN IS CORRODED. REPAIRED PER SRM 53-05-00.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,394 hrs · 30,855 cycles

CORROSION UNDER THE G1 GALLEY DRAIN PAN SUBFLOOR. INSTALLED DOUBLER UNDER G1 GALLEY DRAIN PAN SUBFLOOR PER AARD 53-20-00-16.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,394 hrs · 30,855 cycles

CORROSION ON RIGHT CUSP AREA LOWER SURFACE AFT OF STATION 160. REPAIRED CUSP PER EA MD80-53-005680.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 58,812 hrs

LGA - EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

BOS - EMERGENCY LIGHTS AT AFT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 21DEF FOR EMERGENCY LIGHT AT AFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD CENTER AISLE FOR EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

SFO - EMERGENCY FLOOR LIGHT AT RIGHT SIDE OF CABIN INOPERATIVE. RELAMPED EMERGENCY FLOOR LIGHT AT RIGHT SIDE OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DUCT — BLOWN (ANTI ICE SYSTEM)

TPA INFLIGHT - LEFT FIRE WARNING ACTIVATED AFTER DURING CLIMB. RETURNED TO TPA AND LANDED WITHOUT INCIDENT. FIRE WARNING STOPPED AFTER REDUCING THROTTLE TO IDLE. REPLACED ANTI-ICE DUCT AND UPPER COWLING. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: APU — LEAKING

DFW INFLIGHT T1200/15JAN AFTER TAKE OFF BLUE HAZE WAS REPORTED IN CABIN. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. SMOKE DISSIPATED PRIOR TO LANDING. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. FOUND APU LEAKING OIL. CHANGED APU AND ACCOMPLISHED PACK BURN AND CHANGED COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DOOR — OPEN (NLG)

RIC INFLIGHT T1107/23JAN - NOSE GEARS WOULD NOT RETRACT. LANDED RIC WITHOUT INCIDENT. AFTER LANDING NOSE GEAR FOUND OPEN. CLOSED NOSE GEAR DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BRAKE — OVERHEATED (MLG)

PIT - ABORTED TAKEOFF DUE TO RIGHT HAND COMPRESSOR STALL. UPON ABORT BRAKES OVERHEATED AND TIRE LOST PRESSURE. REPLACED TIRES AND BRAKES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW EMERGENCY LIGHTS BETWEEN ROWS 27 AND 29 INOPERATIVE. REPLACED BATTERY PACK BETWEEN ROWS 17 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TURBINE BLADES — FAILED (RT ENGINE)

ORD EN ROUTE ORD-AUS ON TAKEOFF RIGHT ENGINE FAILED AT NOSE ROTATION. ENGINE SHUT DOWN AND AIRCRAFT RETURNED ORD WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE DUE TO TURBINE BLADE FAILURE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CORROSION ON NR 1 SEAT TRACK AT STA 1278. INSTALLED PLUG AT STA 1278, NR 1 SEAT TRACK IAW SRM AND TREATED AND PRIMED.

Part: LONGERON — CRACKED (FUSELAGE)

CRACK ON LONGERON 46 AT STA 700. CRACKED IN SECTION NEXT TO LOWER ATTACH FASTENER. SPLICED IN NEW SECTION OF LONGERON FROM STA 180 TO STA 235.

Part: SIGN — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT EXIT SIGN OVER R2 DOOR INOPERATIVE. REPLACED R2 DOOR EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (TAIL CONE)

BOS - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT PATH LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT AFT TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (COCKPIT)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD COCKPIT EMERGENCY EXIT LIGHT DIM. RELAMPED OVERHEAD COCKPIT EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: APU — LEAKING (APU BAY)

DFW - FLT 1639 - ON TAKEOFF SMOKE NOTICED IN CABIN THEN QUICKLY DISSIPATED. REAPPEARED DURING DESCENT TO DFW. LANDED DFW WITHOUT INCIDENT. REPLACED AUXILIARY POWER UNIT, ACCOMPLISHED PACK BURNOUT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND AREA OF SKIN GROUND OUT FROM PREVIOUS DAMAGE WITH NO EDGE DISTANCE TO FASTENERS. INSTALLED DOUBLER PER SRM 53-05 FIG 80 SHEET NR 1. (M)

Part: SKIN — GOUGED (FUSELAGE)

TUL - FOUND GOUGE AT STATION 1309 BETWEEN LONGERON 19R AND 18R. REWORKED GOUGE, DYE CHECKED. NO CRACKS FOUND INSTALLED DOUBLER PER SRM 53-04. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON NR 2 SEAT TRACK STATION 1309-1195. REMOVED AND REPLACED NR 2 SEAT TRACK STATION 1185-1309 PER SRM 53-05 FIG 4F. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP. REPAIRED USING HI-LOCK FASTENERS AND SRM 53-01 FIG 4. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON CUSP STATION 644 RIGHT. CUT AWAY CORROSION AND INSTALLED DOUBLER PER SRM 53-01-4 SHEET 3. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION IN SEAT TRACK NR 1 STATION 1207-1211. INSTALLED NEW NR 1 SEAT TRACK FROM STATION 1174-1308 PER 51-10-4 AND 51-10-4A. (M)

Part: CASTING — CORRODED (VERTICAL STAB)

TUL - FOUND RIGHT AND LEFT BORES AND FACES PITTED OF SIDE LOAD CASTING, LOCATED ON VERTICAL STAB BETWEEN STAB HINGE BEARING LUGS. INSTALLED NEW SIDE LOAD CASTING PER SRM 51-01. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION IN SEAT TRACK NR 1 STATION 1230 TO 1237. INSTALLED NEW NR 1 SEAT TRACK FROM STATION 1174-1308 PER SRM 51-10-4 AND 51-10-4A. (M)

Part: LONGERON — CRACKED (FUSELAGE)

TUL - FOUND LONGERON 4L CRACKED AT STATION 160. INSTALLED NEW SECTION OF LONGERON 4L STATION 160 PER SRM 53-02 FIG 18 PAGE 48. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 4. INSTALLED PLUG PER SRM 53-05 FIG 4. (M)

Part: SEAT TRACK — GOUGED (FUSELAGE)

TUL - FOUND NR 1 SEAT TRACK GOUGED STATION 1084-1087. ROUTED OUT DAMAGE AND INSTALLED PLUG PER AARD 53-20-00-10. (M)

Part: BEAM — CORRODED (DOOR JAMB)

TUL - FOUND CORROSION ON DOOR JAMB BEAM STATION 1155-1211. INSTALLED NEW DOOR JAMB BEAM FROM STATION 1117-1250 PER MM 51-30-0, 51-30-1. (M)

Part: FITTING — CRACKED (FUSELAGE)

TUL - FOUND STATION 1155 AT L28R CORROSION ON FITTING ALSO CRACKED. REPLACED FITTING PER SRM 51-01. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN DENTED AT STATION 294 BETWEEN STRINGER 19 AND 20 RT. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04 PAGE 33 TO 35 FIG 12B SHEET 2. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON TOP OF RIGHT LEFT OF NR 5 TRACK STATION 201-204. ROUTED OUT AREA OF CORROSION AND INSTALLED PLUG AT STATION 201 TO 204 ON SEAT TRACK NR 5 PER SRM 53-05 FIG 4A. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 6 STATION 670-693. REMOVED AREA OF NR 6 TRACK OUT OF LIMITS, FROM CORROSION REMOVAL, INSTALLED SEAT TRACK PLUG PER SRM 53-05 FIG 4. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 6. ROUTED OUT DAMAGED AREA, INSTALLED PLUG PER AARD 53-20-00-10. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SEAT TRACK NR 6. ROUTED OUT DAMAGE. INSTALLED PLUG PER AARD 53-20-00-10. (M)

Part: COALESCER BAGS — CONTAMINATED (A/C BAY)

JAX - FLT 0758 - EN ROUTE MIA/BDL, FUEL ODOR DETECTED IN CABIN. AIRCRAFT DIVERTED TO JAX AND LANDED WITHOUT INCIDENT. REPLACED COALESCER BAGS AND ACCOMPLISHED AIR CONDITIONING PACK BURN OUT PROCEDURE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SENSOR — DEFECTIVE (NLG)

DFW - FLT 1900 - EN ROUTE SLC-DFW - AFTER TAKEOFF AND PLACING HYDRAULIC PUMPS TO LOW SETTING THE RED NOSE GEAR ANNUNCIATOR LIGHT ILLUMINATED. AIRCRAFT SLOWED AND PLACED HYDRAULIC PUMPS TO HIGH AND CYCLED GEAR. AFTER HYDRAULC PUMPS WERE REPLACED TO LOW AGAIN ALL GEAR INDICATOR LIGHTS REMAINED EXTINGUISHED. LANDED DFW WITHOUT INCIDENT. REPLACE NOSE GEAR UP SENSOR AND CYCLED LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WEB — CORRODED (BS 294-313)

TUL - CUSPLINE WEB HAS CORROSION BETWEEN STATION 294 - STATION 313 OUTBOARD NR 6 SEAT TRACK. INSTALLED CUSP DOUBLER OUTBOARD NR 6 SEAT TRACK PER SRM 53-01 FIG 4 SH 3. (M)

Part: JAMB — CORRODED (CARGO DOOR)

TUL - FOUND CONSTANT AREA BEYOND LIMITS PER AARD 53-10-00-3, CONDITION 5. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-10-00-3 AND 53-10-00-10. (M)