N861GA

Part: FAN — FAILED (RADIO RACK) · airframe 62,938 hrs · 31,473 cycles

STRONG ELECTRICAL BURNING ODOR IN CABIN. R & R RADIO RACK FAN.

Part: DOUBLER — CORRODED (BS 237-256) · corrosion level 2 · airframe 62,958 hrs · 31,488 cycles

FWD LAVATORY SERVICE PANEL CUTOUT CORRODED AT LOWER EDGE. REPAIRED THE DOUBLER IAW EA 30-2017-042.

Part: BEAM — CORRODED (CAROG DOORWAY) · corrosion level 2 · airframe 62,958 hrs · 31,488 cycles

AFT CARGO DOOR LOWER BEAM CORRODED AROUND FASTENERS. REMOVED AND REPLACED THE AFT CARGO DOOR LOWER FRAME CUTOUT BEAM IAW SRM 51-30-5.

Part: ANGLE — CORRODED (BS 1211) · corrosion level 2 · airframe 62,958 hrs · 31,488 cycles

TRANSITION ANGLE IS CORRODED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-30-5, PARA 7 & 8.

Part: LONGERON — CORRODED (BS 160-180) · corrosion level 2 · airframe 62,958 hrs · 31,488 cycles

LONGERON CORRODED IN E & E BAY. REMOVED AND REPLACED THE LONGERON IAW SRM 51-30-2 FIG 1.

Part: FORMER — CRACKED (VERTICAL STAB) · airframe 62,958 hrs · 31,488 cycles

VERTICAL STABILIZER FIXED LEADING EDGE LT AND RT FORMERS CRACKED. REMOVED AND REPLACED FORMERS IAW SRM 51-30-2 AND DRAWING 9911881.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 62,812 hrs · 31,416 cycles

STRANGE SOUND AND BURNING SMELL EMANATING FROM BEHIND F/O'S INSTRUMENT PANEL. INST COOLING FAN CB PULLED, SOUND AND SMELL EXTINGUISHED.

Part: VERTICAL GYRO — FAILED (NR 1 & 2) · airframe 616,770 hrs · 30,837 cycles

ON CLIMB OUT AUTOTHROTTLES, AUTOPILOT, FLIGHT DIRECTOR & FMA'S FAILED. FLIGHT RETURNED & PRIOR TO LANDING ALL SYSTEMS RETURNED TO NORMAL. WO 299267 TO R & R NR 1 & 2 VERTICAL GYROS IAW AMM 34-23-01. PERFORMED RTS IAW AMM 22-01-05. TEST IS GO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 60,669 hrs · 30,304 cycles

CANTILEVER BULKHEAD CRACKED ABOVE TAIL SLIDE STATION 1431, BETWEEN LONGERON 54 - 56, APPEARS 2.5"" LONG. REPAIRED CANTILEVER BULKHEAD IAW SRM 53-03 FIG 38C.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,668 hrs · 30,303 cycles

DURING A CFT LAYOVER, THE FS 1416 CANTED BULKHEAD WAS FOUND WITH A CRACK IN THE FRAME WEB. THE CRACK IS LOCATED APPROX BETWEEN LONGERON 4R - 5R & MEASURES APPROX 2.55 INCHES LONG, GOING THROUGH ONE FASTENER LOCATION. THE FRAME WEB IS MADE FROM 7075-T6 CLAD ALUMINUM. THE ACFT WILL BE POSITIONED TO A MX FACILITY ON A FERRY FLIGHT. MORE INFO WILL BE UPDATED WHEN AVAILABLE.

Part: CSD — MALFUNCTIONED (RT ENGINE) · airframe 60,346 hrs · 30,131 cycles

RIGHT CSD ABOVE REDLINE & OVER TEMP. COMPLIED WITH QRH & DISCONNECTED RT CSD. PLACED ON MEL 24-01 SIT 1 CAT B DMI 17446, MX ACTIONS COMPLIED WITH, PLACARD INSTALLED.

Part: CADC — FAILED (NR 1)

ON DESCENT, CADC NR 1 & CADC NR 2 FAILED. AUTO THROTTLE & AUTO PILOT DISCONNECTED MOMENTARILY & AIRSPEED DISCREPANCY OF 30KTS BETWEEN AIRSPEED INDICATOR, UNDER FLIGHT FAULT REVIEW, FOUND ONLY CADC NR 1 FAILED. R & R CADC 1 IAW AMM 34-16-01. OPERATIONS CHECKED GOOD, LEAK CHECKED GOOD. RTS SHOWS GO AT THIS TIME.

Part: LIGHT — INOPERATIVE (EXTERIOR)

EXTERNAL EMER LIGHTS INOPERATIVE, LT ONLY. RELAMPED LT EXTERNAL EMER LIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: POWER SUPPLY — DEFECTIVE (CABIN)

ROW 34 EMER LIGHTS VERY DIM. CHECKED BATTERIES, CHECKS GOOD AT 1.3 PLUS VOLTS. REPLACED POWER SUPPLY. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,127 hrs · 29,491 cycles

AFT CABIN DOOR EMER LIGHTS INOPERATIVE. R & R AFT CABIN DOOR EMER LIGHT BATTERIES & OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

Part: FAIRING — CORRODED (FUSELAGE)

RIGHT FUSELAGE AT WING BODY FAIRINGS HAS NUMEROUS SPOTS OF CORROSION AT ATTACHMENT POINTS. FABRICATED DOUBLER, LOCATED, DRILLED PARTS & INSTALLED PERMANENT REPAIR IAW MD80 SRM 51-30-5 & 53-04, PAR 7, FIG 57.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

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

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 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 — MALFUNCTIONED (CABIN)

SMOKE IN THE CABIN NEAR ROW 20 A-C. RECIRC FAN CIRCUIT BREAKER WAS PULLED. REMOVED & REPLACED UPPER SIDEWALL LIGHT BALLAST & RE-SECURED RECIRC FAN CIRCUIT BREAKER.

Part: SKIN — CANNING (FUSELAGE)

RIGHT FUSELAGE SKIN STA 339 LONGERON 27-28 OIL CANNED FROM PREVIOSULY INSTALLED REPAIR. ACCOMPLISHED DAMAGE TRIM OUT. FABRICATED EXTERNAL DOUBLER, INTERNAL FINGER DOUBLER STRAPS, LOCATED DRILLED AND INSTALLED.

Part: LINE — LOOSE (APU)

FLIGHT CREW REPORTED SMOKE IN CABIN (4/2, 4/6,4/8) BLUE SMOKE IN CABIN WHEN RUNNING RIGHT AC PACK FROM APU. MAINTENANCE PERSONNEL FOUND OIL LEAKING ON LEFT SIDE OF APU BETWEEN PLENUM AND ACCESSORY GEARBOX DRIVE. REMOVED TIGHTENED LOOSE OIL LINE AND RE-INSTALLED APU IAW TASK CARD R0594902, OPS AND LEAK CHECK GOOD. AIRCRAFT 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: POWER SUPPLY — INOPERATIVE (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: 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 — MALFUNCTIONED (CABIN PRESSURE)

FLIGHT CREW REPORTED, WOULD NOT HOLD RATED PRESSURE AT ALTITUDE WITH OUTFLOW VALVE CLOSED. CABIN CLIMB AT 5-600 FPM AND CABIN ALT AT 9,000 AT FL 29,000, CABIN CONTINUED CLIMBING UNTIL REACHING FL 21,000. MAINTENANCE PERSONNEL PERFORMED OPS CHECK ON PRESSURIZATION WITH APU AIR IAW MM 21-30-00. NO DEFECTS NOTED, ALSO PERFORMED EXTERNAL FOR LEAKS, NO MAJOR LEAKS FOUND, AIRCRAFT OK FOR EVALUATION FLIGHT. AIRBORNE SYSTEM TEST SATISFACTORY.

Part: SKIN — DENTED (FUSELAGE)

DENT AT STA 1309 AT LONGERON 27-28L IS OUT OF LIMITS PER MD80 SRM 53-04, FIG 38, COND 1B, TABLE C, ITEM 1. REPAIRED IAW DRAWING SG09530002.

Part: BALLAST — DEFECTIVE (CABIN)

AFTER STARTING NR 2 ENGINE, BURNING RUBBER / PLASTIC SMELLING AREA AFT OF L2 DOOR, ROW 32 TO 36 AREA. SMELL OCCURRED PRIOR TO STARTER CUT OUT- 30 PERCENT N2. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED THE AIRCRAFT AND FOUND THE LIGHT BALLAST DEFECTIVE. REMOVED AND REPLACED BALLAST IAW AMM 33-21-03. SYSTEM OPS CHECKS NORMAL AND AIRCRAFT RETURNED TO SERVICE.

Part: SERVICE PANEL — CORRODED (AFT LAV)

REPLACED AFT LAV SERVICE PANEL PAN BECAUSE OF CORROSION IN THE LOWER FWD CORNER E58 6198554.

Part: SKIN — BULGED (FUSELAGE)

FUSELAGE SKIN IS BULGING AT THE LOWER FWD CORNER OF THE AFT LAV SERVICE PANEL CUTOUT.

Part: LONGERON — DAMAGED (BS 1306 L22L)

REPLACED DAMAGED LONGERON.

Part: BEAM — CORRODED (CARGO DOOR)

INSTALLATION OF REPAIR DOUBLER OVER CORRODED AFT CARGO DOOR BEAM, DOUBLER P/N SR09520008-18 PER AA E50 80559 DATED 01/13/2009.

Part: DOUBLER — CORRODED (FUSELAGE)

CORROSION ON DOUBLER AT LOWER FORWARD CORNER OF FORWARD LAVATORY SERVICE PANEL.

Part: SKIN — CORRODED (ZONE 100)

FUSELAGE BELLY SKIN BULGING AT L30 STATION 748-752. CUTOUT CORROSION, INSTALLED DOUBLER PER ESO 80559, DATED 1-13-2009 AND 53-04, FIGURE 12B.

Part: CSD — UNKNOWN (LEFT)

FLIGHT 2305 DPC/MKE. FLIGHT CREW REPORT THAT THE LEFT CSD OIL TEMP WENT TO RED LINE - DISCONNECTED LEFT CSD. MAINTENANCE REPORT, FLUSHED THE LEFT CSD AND SERVICED IT TO THE CORRECT LEVEL WITH OIL. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 24-10-00. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT MAINTENANCE INSPECTION MAINTENANCE REPORTED THAT THE AISLE EMERGENCY LIGHTS AT ROWS 7 THROUGH 11 WOULD NOT TEST. MILWAUKEE MAINTENANCE FURTHER REPORT THE REMOVAL AND REPLACEMENT OF AN EMERGENCY LIGHT POWER SUPPLY BATTERY PACK AT FUSELAGE STATION 500. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MILWAUKEE MAINTENANCE REPORTED THAT THE FLIGHT DECK EMERGENCY LIGHTS WOULD NOT TEST. MILWAUKEE MAINTENANCE FURTHER REPORT THE REMOVAL AND REPLACEMENT OF THE BATTERY PACK AT EMERGENCY LIGHT POWER SUPPLY BS-23. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: SENSOR — OUT OF ADJUST

FLIGHT 516 IDA/LAS - FLIGHT CREW REPORT "L ICE PROTECT TEMP HIGH" ANNUNCIATOR ILLUMINATED WITH AIRFOIL ANTI-ICE ON. QRH PROCEDURE APPLIED AND LIGHT EXTINGUISHED. LAS VEGAS MAINTENANCE TROUBLESHOT THE SYSTEM TO A FAULTY LT TEMPERATURE SENSOR. REMOVED AND REPLACED TEMP SENSOR PER AMM 30-10-06. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER 30-10-00. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: FAIRING — DEPARTED

SFB - SFG, AIR RETURN TO SFB PER DISPATCHES INSTRUCTIONS. BANANA FAIRING FELL OFF AIRCRAFT AS REPORTED BY DISPATCH. MAINTENANCE INSTALLED LEFT UPPER BANANA FAIRING IAW BOEING MD-80 MM 55-10-03 PAGE 501 THRU 507. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

MAINTENANCE REPORTED EMERGENCY FLOOR ESCAPE LIGHTING ROW 5-8 AC/ RT INOPERATIVE. MAINTENANCE INSTALLED NEW LEAD ASSEMBLY WIRE AT FOR ROWS 5-8 AC RT. SYSTEM OPERATIONALLY CHECKS NORMAL IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE SWITCH — FAILED (APU)

LAS TO FNL - CREW REPORTED APU AUTO SHUTDOWN DUE TO LOW OIL PRESSURE IN FLIGHT. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED OIL PRESSURE LOW SWITCH IAW MM 49-90-03. APU OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

LAS - MAINTENANCE REPORTED LEFT AND RIGHT OVERWING EMERGENCY EVACUATION LIGHTS INOPERATIVE. MAINTENANCE INSTALLED A SERVICEABLE POWER SUPPLY. SYSTEM OPERATIONALLY CHECKS GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE.

Part: CSD — OVERSERVICED (LEFT)

CUN - CREW REPORTED LEFT CSD OIL ANNUNCIATOR ILLUMINATED ON CLIMB-OUT WITH LEFT CSD INDICATOR AT RED LINE. CREW REDUCED THRUST, INDICATION DROPPED BETWEEN YELLOW ARCS, THEN RIGHT CSD OIL ANNUNCIATOR ILLUMINATED AND RIGHT CSD INDICATOR AT RED LINE. DURING DESCENT BOTH CSD’S INDICATED NORMAL WITH POWER REDUCED. AIRCRAFT LANDED IN AN OVERWEIGHT CONDITION WITHOUT INCIDENT. MAINTENANCE COMPLETED OVERWEIGHT LANDING INSPECTION IAW MM 05-51-04 WITH NO DAMAGE FOUND. MAINTENANCE FOUND CSD’S OVER-SERVICED, DRAINED SUFFICIENT OIL TO BRING CSD’S TO PROPER LEVEL AND INSPECTED CHIP DETECTORS. AIRCRAFT RETURNED TO SERVICE .

Part: LIGHT — INOPERATIVE (CABIN)

LAS - MAINTENANCE REPORTED AFT EMERGENCY LIGHTS AND STANDBY POWER EMERGENCY LIGHT ROW 8 INOPERATIVE. MAINTENANCE RE-LAMPED AFT EMERGENCY LIGHTS AND STANDBY POWER EMERGENCY LIGHT AT ROW 8 IAW MM 33-50-00. EMERGENCY LIGHTS OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

MAINTENANCE REPORTED TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHT BATTERY PACK. SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE.

Part: FRAME — DAMAGED (CARGO DOOR)

MAINTENANCE REPORTED AFT CARGO PIT DOOR FRAME DAMAGED AT AFT LOWER CORNER. AIRCRAFT WAS FERRIED TO GYR FOR REPAIR. TIMCO ACCOMPLISHED EXTERNAL DOUBLER REPAIRS APPROVED BY SRM 53-05 FIG. 106 AND 117 PER REPAIR SCHEME PROVIDED VIA TIMCO REO-A00288 REV. IR DATED 10 OCT 04. AIRCRAFT RETURNED TO SERVICE.

Part: SEAL — LEAKING (LT PACK)

AFTER NORMAL TAKEOFF ROLL AT APPROXIMATELY 600 FT TO 800 FT AGL MASTER WARNING LIGHT ILLUMINATED, TRIGGERED BY TAIL COMPARTMENT TEMPERATURE HIGH LIGHT. CREW FOLLOWED QRH PROCEDURES AND RETURNED TO AIRPORT, NO EMERGENCY DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. CONTRACT MAINTENANCE FOUND BLEED LEAK IN TAIL COMPARTMENT. AIRCRAFT FERRIED FOR REPAIR. MAINTENANCE REPLACED 2 EACH PERRY SEALS ON THE LT PACK IAW MD80-MM 36-00-00. SYSTEM OPERATIONALLY CHECKED GOOD. NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: TIRE — LOW (NLG)

ON DEPARTURE, UPON APPLYING TAKEOFF POWER, THE AIRCRAFT STARTED TO ROLL DOWN THE RUNWAY NORMALLY. AT ABOUT 60 KNOTS THE NOSE WHEEL STARTED TO SHAKE UNCONTROLLABLY. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT TAXIED BACK TO THE GATE. MAINT INSP THE NOSE WHEELS, GEAR AND TORQUE LINKS. NO DEFECT WAS NOTED. FURTHER INSP FOUND THAT BOTH NOSE TIRES WERE ABOUT 25 PSI LOW ON PRESSURE. THE TIRES WERE SERVICED WITH NITROGEN AND THE AIRCRAFT RELEASED TO SERVICE. THE CREW INIATED ANOTHER TAKEOFF. THE AC PERFORMED NORMALLY. THE FLIGHT CONTINUED TO LAS WHERE THE AC LANDED WITHOUT FURTHER INCIDENT.(K)