N866GA

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 52,996 hrs · 36,396 cycles

AFTER DEPARTURE, ACFT WAS CLIMBING & ACCELERATING THRU 1300 MSL & 180 KNOTA. NO PRIMARY OR SECONDARY TRIM WAS AVAILABLE. ALL CB WERE IN, QRH WAS REF. ACFT WAS LEVELED AT 5000 MSL & SLOWED TO 210 KNOTS. SPEED CONTROL KNOB WAS NOT FUNCTIONING & WOULD NOT CONTROL SALMON SPEED BUGS. ACFT RETURNED, NORMAL LANDING WAS MADE. AFTER AUTO PILOT WAS ENGAGED TRIM BEGAN WORKING AGAIN. INSPECTED HORIZONTAL JACKSCREW AREA, NO DEFECTS NOTED MM 27-40-00. PERFORMED OPERATIONS CHECK OF HORIZONTAL STAB TRIM ADJUSTMENT TEST OF BRAKE OVERRIDE SWITCH, OPERATIONS CHECKED GOOD IAW AMM 27-40-00-5-3. INSPECTED HORIZONTAL STAB TRIM CONTROL WHEEL, CONTROL HANDLES & ALT TRIM SWITCHES, ALL SWITCHES OPERATED NORMALLY, NO DISCREPANCIES FOUND IAW AMM 27-40-09-5-6. PERFORMED DFGS SWITCHES, BUTTONS & RTS, NO DEFECTS NOTED. OPERATIONS CHECKED GOOD IAW AMM 22-01-05.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,929 hrs · 36,357 cycles

FORWARD OVERWING EMER EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONS CHECKED GOOD IAW 33-53-00.

Part: SWITCH — FAILED (READING LIGHT) · airframe 52,770 hrs · 36,271 cycles

AFT FLIGHT ATTENDANT REPORTS BURNED TOAST ODOR NEAR PSU 37DEF, SAW SMOKE NEAR PSU APPROXIMATELY 1 HOUR INTO FLIGHT. PERFORMED CABIN ODOR & SMOKE TROUBLESHOOTING WORK CARD 21-059-002. FOUND PSU READING LIGHT SWITCH FROM SEAT 37D DEFECTIVE. SWITCH IS DEACTIVATED & PLACED ON NEF 25-01H-02 SIT 2 CAT D DMI 18412, PLACARD INSTALLED.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 52,309 hrs · 36,019 cycles

CRACKED CUSP WEB AT FS 220 & LBL 45 IN CABIN. CUT OUT & REMOVED DAMAGE AREA. FABRICATED DOUBLER, FILLER, LOCATED, DRILLED & INSTALLED REPAIR PARTS IAW SRM 51-70-4 FIG 2. WORK ACCOMPLISHED ON WO 248644 M301 ITEM 434 & WO 1011747 2000-0182.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,309 hrs · 36,019 cycles

SEAT TRACK IS CORRODED AT FS 200, LBL 22. REMOVED SEAT TRACK, INSTALLED SERVICEABLE SEAT TRACK IAW SRM 51-30-1. WORK ACCOMPLISHED ON WO 248644 M301 ITEM 364 & WO 1011747 2000-0124.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY)

RIGHT SIDE AFT LAVATORY SMOKE DETECTOR LIGHT IS ILLUMINATED. ALARM SOUNDED & THEN STOPPED WITHIN MINUTES. CLOSED LAVATORY IAW QRH 26.9 & RT SIDE AFT LAVATORY SMOKE DETECTOR. OPERATIONS CHECKED NORMAL IAW 26-14-00.

Part: STRUCTURE — CRACKED (CARGO DOOR)

AFT CARGO DOOR, AFT SIDE, HAS MULTIPLE CRACKS JUST BELOW AFT TORQUE TUBE. CUTOUT DAMAGED AREA, FABRICATED, LOCATED, DRILLED, REPAIRED PARTS & INSTALLED PERMANENT REPAIR IAW SRM 52-05 PAR 26 FIG 26B.

Part: BATTERY — DISCHARGED (CABIN)

ROW 24 & 25 OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R BATTERIES AT ROW 24 & 25. OPERATIONS CHECKED NORMAL IAW AMM 33-50-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00, SYS OPS CHECKED NORMAL. ACFT BEEN RETURNED TO SERVICE.

Part: LONGERON — CRACKED (FUSELAGE)

LONGERON 4L CRACKED THROUGH FASTENER HOLES AT STATION 160. CRACK LENGTH .300". REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, REPAIR SPLICE AND LONGERON SECTION AND INSTALLED.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: UNKNOWN — FAILED (LT MLG)

FLIGHT CREW PERSONNEL REPORTED UPON LANDING ON 25L AT LAS, A VIOLENT VIBRATION OCCURRED. CAME TO A FULL STOP I WAS INFORMED THAT THE LEFT MLG WAS PERPENDICULAR TO THE FUSELAGE. MAINTENANCE DEPARTMENT PERSONNEL REMOVED AND REPLACED THE LEFT MLG ASSY IAW MD80 AMM 32-11-01. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BALLAST — DEFECTIVE (CABIN)

LIGHT SMOKE AND ELECTRICAL FUMES COMING FROM PSU 30AC. MX NOTE; DURING TROUBLESHOOTING FOUND SIDEWALL LIGHT BALLAST BURNT, NO OTHER DEFECTS NOTED. REMOVED AND REPLACED BALLAST ON ROW 30AC IAW AMM 33-21-03, OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: INTERCOSTAL — CORRODED (FUSELAGE)

E AND E COMPARTMENT HAS CORRODED INTERCOSTAL AT FS 208, RBL 7, INBOARD SIDE OF DRAIN MAST. REMOVED AND REPLACED INTERCOSTAL IAW MD80 SRM 51-30-1 AND 51-30-2.

Part: SKIN — DAMAGED (L1 DOOR)

L1 DOOR DOES NOT MEET REPAIR REQUIREMENTS PER SRM 52-03 PARA 3. REPAIR L1 DOOR IAW MD80 SRM 52-05 FIG 55, 51-30-05, 51-30-01, 52-12-0, 51-10-3 PARA 14 & 21, AMM 25-22-00 AND 52-11-01 AND 52-11-02.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: CARGO TRACK — CORRODED (CARGO BAY)

WHILE IN WORK AT MAINTENANCE BASE; BOW1C/3C/51/54, FOUND LT TIE DOWN TRACK CORRODED BEYOND LIMITS IN AFT CARGO STA 1270-1309, ADDRESSED AS REQUIRED.

Part: WEB — PUNCTURED (FUSELAGE)

WHILE IN WORK AT MAINTENANCE BASE, BOW 1C/3C/51/54; FOUND PUNCTURE IN WEB LT SIDE STA CANT 1497 APPROX .75 INCH LONG, INSTALLED DOUBLER PER SRM 53-01 FIG 2, SHEET 3.

Part: WEB — CORRODED (FUSELAGE)

WHILE IN WORK AT MAINTENANCE BASE; BOW 1C/3C/51/54, FOUND CORROSION ON WEB AT STA 1212-1215. ADDRESSED AS REQUIRED.

Part: WEB — PUNCTURED (FUSELAGE)

WHILE IN WORK, BOW 1C/3C/51/54, FOUND PUNCTURE IN WEB BELOW CATWALK TORQUE TUBE 6 INCHES OUTBOARD OF LEFT AIRSTAIR LIGHT STA 1497CANT, PUNCTURE 1FT LONG. INSTALLED DOUBLER PER SRM 53-01 FIG 2, SHEET 3.

Part: WEB — PUNCTURED (FUSELAGE)

WHILE IN WORK AT MAINTENANCE BASE; BOW1C/3C/51/54, FOUND PUNCTURE IN WEB LEFT SIDE STA CANT 1497, APPROX .75 INCH LONG, INSTALLED DOUBLER PER SRM 53-01 FIG 2 SHEET 3.

Part: WEB — PUNCTURED (FUSELAGE)

WHILE IN WORK AT MAINTENANCE BASE; BOW1C/3C/51/54, FOUND PUNCTURE IN WEB APPROX 1FT LONG BELOW CATWALK 5FT OUTBOARD OF RT AIRSTAIR LIGHT, INSTALLED DOUBLER PER BOEING SRM 53-01 FIG 2, SHEET 3.

Part: SUPPORT FITTING — CRACKED (SPOILER ACTUATOR)

GROUND SPOILER ACTUATOR SUPPORT FITTING CRACKED, FORWARD INBOARD SIDE RIGHT WING, ADDRESSED AS REQUIRED.

Part: LONGERON — CRACKED (FUSELAGE)

WHILE IN WORK AT MAINTENANCE BASE; BOW 1C/3C/51/54. FOUND LONG 2R CRACKED AFT STA 1418. AA-58 6280638, ADDRESSED AS REQUIRED.

Part: SKIN — DENTED (FUSELAGE)

DENT IN RIGHT FUSELAGE STA 1307, LONG 20, ID 24. ADDRESSED AS REQUIRED.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE)

WHILE IN WORK AT MAINTENANCE BASE; BOW 1C/3C/51/54 SEAT TRACK SUPPORT ANGLE FOR NR 2 TRACK AT STA 927 WAS FOUND CRACKED. ADDRESSED AS REQUIRED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: BALLAST — MALFUNCTIONED (CABIN)

SMOKE COMING OUT OF OVERHEAD BIN AT ROW 9 AC, PULLED CIRCUIT BREAKER AND DISCONNECTED BALLAST. REPLACED LIGHT BALLAST AT ROW 9 AC, RESET CIRCUIT BREAKER. PERFORMED SYS OPS CHECK. ACFT OK TO RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: DOWNLOCK SENSOR — OUT OF ADJUST (NLG)

NLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. QRH COMPLIED WITH BY FLIGHT CREW. NLG RED UNSAFE REMAINED ILLUMINATED. AIRCRAFT RETURNED TO THE FIELD (LAS). NO EMERGENCY DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DEPARTMENT INSPECTED AND ADJUSTED THE NLG DOWNLOCK SENSOR IAW AMM 32-60-65. PERFORMED GEAR SWING, OPS CHECK GOOD IAW AMM 32-60-00. AIRCRAFT RETURNED TO SERVICE.

Part: GYRO — MALFUNCTIONED (NR 2 DIRECTIONAL)

FLIGHT 431 SHV/LAS - FLIGHT CREW REPORTED THAT DURING CRUISE, HEADING FAIL ON BOTH FMS'S. 30 DEGREE SPLIT BETWEEN F/O'S NAV DISPLAY AND RMI, QRH 31.2 PROCEDURE APPLIED. LAS VEGAS MAINTENANCE REPORT THAT THEY REMOVED AND REPLACED THE NR 2 DIRECTIONAL GYRO. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 34-21-09. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

LAS - MAINTENANCE FOUND THE L1 DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPERATIONALLY CHECKED GOOD IAW MM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

OVERHEAD EMERGENCY LIGHT INOPERATIVE AT ROW 21. MAINTENANCE RELAMPED THE OVERHEAD EMERGENCY LIGHT AT ROW 21. SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

LAS - MAINTENANCE REPORTED LEFT SIDE EXTERIOR EMERGENCY OVERWING LIGHT INOPERATIVE. MAINTENANCE RELAMPED EMERGENCY LIGHT. SYSTEM OPERATIONALLY CHECKS GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

LAS - MAINTENANCE REPORTED EMERGENCY OVERHEAD LIGHT INOPERATIVE AT ROW 14. MAINTENANCE RELAMPED THE EMERGENCY OVERHEAD LIGHT, SYSTEM OPERATIONALLY CHECKS GOOD IAW AMM 33-53-01. AIRCRAFT RETURNED TO SERVICE.

Part: STRUCTURE — VIBRATION (UNKNOWN)

ENROUTE LAS TO ICT A/C ENCOUNTERED POCKET OF SEVERE TURBULENCE AND ON RETURN FLT ICT TO LAS CREW REPORTED MODERATE AIRFRAME VIBRATION STRONGEST IN FWD FUSELAGE, SIMILAR TO HAVING FULL SPOILER DEFLECTION AND LANDING LIGHTS EXTENDED IN CRUISE FLT. THROTTLE SETTINGS WERE CHECKED AND AT 80 TO 87 PERCENT N1, VIBRATION WAS MAX. FLT WAS DIVERTED TO DEN AND LANDED W/O INCIDENT. MX INSPECTED A/C AND FOUND NO DEFECTS, PERFORMED HIGH POWER ENGINE RUNS WITH NO VIBRATION NOTED AND OBSERVED NOSE BULLETS FOR OSCILLATIONS WITH NONE NOTED. A/C WAS FERRIED TO LAS AND MX COMPLETED THE TURBULENCE INSPECTION IAW MM 05-51-02 SCHEDULE A WITH NO DAMAGE NOTED. MX PERFORMED AN INSPECTION OF THE NR 2 FLT SPOILER IAW MM 27-60-00 WIT