N877GA

Part: SERVO VALVE — FAILED (LT BRAKE) · airframe 38,553 hrs · 27,407 cycles

THE CREW WAS USING AUTO BRAKES FOR LANDING. THE AUTO BRAKES WERE DISENGAGED BETWEEN 120 - 100 KTS BY APPLYING MANUAL BRAKING. WHEN THE AUTO BRAKE SYS WAS DISENGAGED THE CREW FELT A JOLT BUT THE ACFT STAYED ON THE CENTERLINE THROUGHOUT THE ROLLOUT. THE ACFT WAS BROUGHT TO A STOP ON THE RNWY & THE CREW NOTED A SLIGHT LIST TO THE LT. THE FIRE DEPART WAS CALLED OUT TO INSPECT THE ACFT ON THE RNWY. AT THE TIME OF THE CALL THE CREW WAS UNCLEAR IF ONE OR BOTH LT MAIN TIRES WERE BLOWN. REPLACED 1 & 2 MLG. REPLACED LT MLG BRAKES 1 & 2 IAW AMM 32-42-01 LEAK CHECKED GOOD IAW SAME. PERFORMED TROUBLESHOOTING IAW MM 32-43-00-1-0. FOUND LT OTBD DUAL SERVO CONTROL VLV NOT RELEASING LT BRAKES FROM LT HYD SYS DURING SKID TEST. R & R LT OTBD CONTROL SERVO VLV IAW MM 32-43-03. OPERATIONS & LEAK CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,064 hrs · 27,159 cycles

EMERGENCY LIGHT ABOVE ROW 8 INOPERATIVE. R & R EMER LIGHT BULB ABOVE ROW 8 IAW 33-53-00. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 37,968 hrs · 27,112 cycles

AFTER GEAR RETRACTION, RT MAIN GEAR UNSAFE LIGHT, REMAINED ON. FOLLOWED QRH 32.9, RED GEAR LIGHT ON WITH GEAR HANDLE UP. AFTER GEAR EXTENSION & RETRACTION, RED LIGHT EXTINGUISHED. PERFORMED PROXIMITY SENSOR ELEC UNIT TEST IAW AMM 32-60-04-02-0, NO DEFECTS NOTED. INSPECTED SWITCHES ON ALL 3 GEARS, NO DEFECTS NOTED. OK FOR FURTHER FLIGHT.

Part: SWITCH — DEFECTIVE (AUTOBRAKE SYS) · airframe 37,945 hrs · 27,099 cycles

AUTO BRAKES DISENGAGE ON TOUCHDOWN. R & R AUTO BRAKE DISCONNECT SWITCH S1-441 IAW AMM 32-44-00-2-0. OPERATIONS CHECKED GOOD.

Part: SWITCH — DEFECTIVE (COCKPIT) · airframe 37,945 hrs · 27,099 cycles

LANDING GEAR HORN WOULD NOT SILENCE ON VARIOUS CONFIGURATIONS, FLAP & SLATS 0, SLATS EXTENDED FLAPS 15. R & R LG SILENCE HORN SWITCH. OPERATIONS CHECKED GOOD IAW AMM 31-51-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 37,922 hrs · 27,087 cycles

TAIL COMPARTMENT CEILING EMER EXIT LIGHTS INOPERATIVE. R & R BATTERIES IN POWER SUPPLY. OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 37,828 hrs · 27,039 cycles

AT FL 290, THE FLOW LIGHT ON & THE CABIN BEGAN CLIMBING AT 1000 FEET A MINUTE. CREW ASKED FOR A DESCENT & EXECUTED QRH 21.7 CABIN PRESS OFF SCHEDULE OR ERRATIC CHECKLIST. THE CABIN GOT UP TO 11000 FEET AT ITS HIGHEST POINT. ATC HAD DECLARED THE EMER FOR THE ACFT. ONCE AT 9000 FEET THE CREW REGAINED CONTROL OF THE PRESSURIZATION SYS & ASKED ATC TO STAND DOWN FROM AN EMER SITUATION & CONTINUED. THE ARRIVAL & LANDING WERE UNEVENTFUL, THE PAX MASKS WERE NOT DEPLOYED. THE CAPTAIN WROTE UP THE DISCREPANCY, THE CREW & PAXS WILL SWAP ACFT & CONTINUE.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 37,795 hrs · 27,018 cycles

ON TAKEOFF ROLL, THE FLIGHT ATTENDANTS REPORTED THE SMELL OF FUMES. BOTH PILOTS SMELT THE SAME FUMES. CABIN & FIRE QRH & AIR CON SMOKE & FUMES QRH COMPLETED. NO FURTHER DEFECTS NOTED. PERFORMED CABIN, ODOR & SMOKE TROUBLESHOOTING TASK CARD 21-059-002. NO DEFECTS FOUND IAW TC 21-059-002. OK FOR CONTINUED SERVICE.

Part: PROXIMITY SENSOR — FAILED (RT MLG DOOR) · airframe 37,786 hrs · 27,014 cycles

AFTER GEAR RETRACTION WE HAD RT RED GEAR LIGHT WITH GEAR HANDLE UP. AFTER QRH PROCEDURE, NOW HAD RT GEAR & NOSE GEAR RED LIGHT WITH GEAR HANDLE UP. ALSO HAD AN AUTO SPOILER FAIL MGS. ADJUSTED RT MAIN GEAR LATCH MECHANISM IAW MM 32-31-04. PERFORMED PROXIMITY SENSOR TEST, NLG PROXIMITY SENSORS PASSED, RT MAIN GEAR DOOR SENSOR FAILED. R & R RT MAIN GEAR DOOR PROXIMITY SENSOR IAW MM 32-60-05. AUTO SPOILER FAIL MSG INDUCED BY RED UNSAFE INDICATION. AUTO SPOILERS OK IAW MM 27-60-00. PERFORMED MULTIPLE EXTENSION & RETRACTION TEST OF ALL 3 GEAR IAW MM 32-30-00. ALL CHECKED NORMAL.

Part: SENSOR — OUT OF ADJUST (SPOILER) · airframe 37,594 hrs · 26,898 cycles

AT APPROX 2000 FEET ON APPROACH, SPOILER DEPLOYED, LIGHT ILLUMINATED. COMPLETED 360' TURN & LIGHT REMAINED ON. AFTER RESTARTING, APPROACH LIGHT ILLUMINATED INTERMITTENTLY & FINALLY EXTINGUISHED AT 1000 FEET. NO ADVERSE EFFECT NOTED DURING TURN. ADDITIONAL INFORMATION ADDED RELATED TO EMER DECLARED, ON THE APPROACH FOR LANDING. AT ABOUT 2,000 FEET SPOILER DEPLOYED, ANNUNCIATOR CAME ON. ASKED FOR A 360 DEGREE TURN TO ACCESS THE SITUATION. AFTER THE TURN, DECLARED AN EMER, AT ABOUT 1,000 FEET THE SPOILER DEPLOYED & ANNUNCIATOR WENT OUT. FOUND LT INBD FLIGHT SPOILER, SPOILER DEPLOYED SENSOR OUT OF ADJUSTMENT. ADJUSTED SENSOR IAW AMM 27-61-05-2-0. COMPLIED WITH PROXIMITY SENSOR BITE TEST IAW AMM 32-60-00 101. ALL CHECKED NORMAL.

Part: UNKNOWN — ODOR (CABIN)

IAW FLIGHT ATTENDANTS, ALL, THEY COULD SMELL A CHEMICAL, BURNT, FOUL SMELL ALL THROUGHOUT THE CABIN FROM TAKE OFF POWER TO ABOUT 15 MIN AFTER TAKEOFF. TAKE OFF INDICATIONS WERE NORMAL, TO TAKEOFF, BLEEDS ON. PERFORMED INSPECTION & TROUBLESHOOTING IAW TC 21-059-002, NO DEFECTS NOTED. OK FOR CONTINUED SERVICE.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 36,393 hrs · 26,321 cycles

LEFT FWD OVERWING EMER EXIT SIGN HAS ONE LAMP OUT. RELAMPED LIGHT FIXTURE IAW AMM 33-50-00. CHECKED GOOD AT THIS TIME.

Part: MANIFOLD — DEFECTIVE (BRAKE SYSTEM) · airframe 36,122 hrs · 26,184 cycles

ON LANDING AUTO BRAKES DISARMED AUTOMATICALLY UPON TOUCHDOWN WITH AUTO BRAKES SET AT MED. TROUBLE SHOT IAW AMM 32-44-00. FOUND LAND MANIFOLD BAD. REPLACED LAND MANIFOLD IAW AMM 32-44-00. OPERATIONS & LEAK GOOD.

Part: SKIN — SCRATCHED (FUSELAGE)

UPPER ETERNAL FUSELAGE SKIN SCRATCHED OUT OF LIMITS AT STATION 349 UNDER VHF ANTENNA. BLENDED TO REMOVE DAMAGE, HFEC INSPECTED WITH NO CRACKS NOTED. FABRICATED REPAIRS SHIM & DOUBLER, LOCATED, DRILLED & INSTALLED IAW EA 10-2014-055.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY AISLE LIGHTS INOPERATIVE 28 - 29. REPLACED BATTERIES IN BATTERY PACK FOR EMERGENCY AISLE LIGHTS 28 - 29. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: BATTERY — DISCHARGED (CABIN)

COCKPIT OVERHEAD LIGHTS DO NOT COME ON WITH EMERGENCY LIGHT TEST. R & R BATTERIES FOR EMERGENCY LIGHTS IN FWD SECTION IAW AMM 33-50-00, OPERATIONS TESTED GOOD.

Part: BATTERY — DISCHARGED (CABIN)

MID CABIN OVERWING EXIT DOOR AFT EMERGENCY LIGHT LOWER INOPERATIVE, BATTERIES ARE OUT OF DATE. R & R BATTERY IAW AMM 33-53-00, OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT)

IN ACCORDANCE WITH MEL 25-09 SIT 1 DMI 5542, AFT CABIN FLASHLIGHT NOT BLINKING. R & R AFT CABIN FLASHLIGHT BATTERY PACK IAW AMM 25-60-00, OPERATIONS CHECKED GOOD. THIS CLEARS MEL 25-09 SIT 1, DMI 5542, INOPERATIVE PLACARD REMOVED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

CENTER ISLE EMERGENCY LIGHTS AT 29 &31 INOPERATIVE. REPLACED BATTERY PACK BATTERIES FOR 29-31, OPS CK GOOD REF AMM 33-53-00.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN)

FWD F/A STATION UPPER EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT IAW AMM 25-60-00. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK, 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: FRAME — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT FS FRAME 1309 LOWER FLANGE IS CORRODED BETWEEN LONGERON 28R TO 28L. REPAIRED DAMAGED AREA OF FRAME.

Part: DOOR FRAME — CRACKED (FUSELAGE)

VENTRAL DOOR SURROUND REVEAL CRACK IN UPPER LEFT CORNER. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER.

Part: DOOR FRAME — GOUGED (CARGO DOOR)

FORWARD CARGO DOOR HYDRO-FORMED FRAME HAS SEVERAL GOUGES AT AFT LOWER CORNER. FABRICATED REPAIR DOUBLER AND INSTALLED.

Part: LONGERON SPLICE — CORRODED (BS 1463 L12L)

FS 1461 LONGERON SPLICE 12L CORRODED. REPLACED LONGERON SPLICE.

Part: DOUBLER — CHAFED (TE FLAP VANE)

RIGHT O/B FLAP L/B VANE LEADING EDGE DOUBLER CHAFED AT I/B CORNER. REPLACED DOUBLER.

Part: DOUBLER — CHAFED (TE FLAP VANE)

RIGHT L/B FLAP L/B VANE LEADING EDGE DOUBLER CHAFED. REPLACED DOUBLER.

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 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: SKIN — CORRODED (FUSELAGE)

AFT LAV SERVICE PANEL CUTOUT CORRODED BETWEEN FUSELAGE SKIN AND DOUBLER STATION 1309 JUST ABOVE LONGERON 22L.

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: CUSP WEB — CORRODED (FUSELAGE) · airframe 33,173 hrs · 24,710 cycles

CABIN FLOOR CUSP WEB CORRODED OUT OF LIMITS AT STA 370 RBL 47. REMOVED DAMAGED CUSP WEB, FABRICATED, LOCATED, DRILLED CUSP WEB DOUBLER AND INSTALLED IAW MD 80SRM 51-70-4 FIGURE 1 WEB SPLICE REPAIR.

Part: BATTERY — DISCHARGED (E&E BAY)

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: 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 RELAMPED, 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 — 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: VANE — GOUGED (TE FLAP)

RIGHT WING INBOARD FLAP VANE GOUGE AT XV2 223. PERMANENT REPAIR APPLIED 4" X 11" EXTERNAL DOUBLER FROM XV2 221 TO XV2 225 IAW BOEING MD80 SRM 57-03 PAGE 27 WITH EXAMPLE 'B" DOUBLER.

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: LENS — MISSING (CABIN)

IT HAS BEEN REPORTED BY THE FLIGHT CREW THE EMERGENCY EVACUATION LIGHTING SYSTEM HAS BEEN FOUND TO BE DEFECTIVE. FLOOR PATH LIGHTING STRIP IS MISSING THE LENS COVER. MAINTENANCE DEPARTMENT PERSONNEL HAVE INSPECTED THE SYSTEM AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN)

SMELL COMING FROM AIR CONDITIONING PACKS ON APU AIR, LEAK CHECKED APU AND VERIFIED ACM SERVICE LEVELS. INSPECTED COALESCER BAGS AND FOUND OK FOR CONTINUED SERVICE. FOUND NO DEFECTS WITH APU OR AIR CONDITIONING SYSTEM. REF AMM 49-10-00 AND 21-10-00.

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: ENGINE — MALFUNCTIONED (RIGHT)

DURING CLIMB, RIGHT ENGINE OIL TEMP BEGAN CLIMBING, FOLLOWED BY OIL QUANTITY FALLING. ENGINE WAS SHUTDOWN IN FLIGHT, OIL TEMP REACHED 199FT. REMOVED AND REPLACED RIGHT ENGINE IAW ALLEGIANT TASK CARD R0807106, ENGINE OPS AND LEAK CHECKS 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 — 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: 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: 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: LIGHT — 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 EMERGENCY EXIT LIGHT ASSY 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: ATTACH ANGLE — CRACKED (PYLON)

LEFT EXTERNAL FUSELAGE AT CENTER FRAME 1463 PYLON UPPER ATTACH ANGLE CRACKED. TRIMMED OUT DAMAGED AREA, FABRICATED ANGLE REPAIR AND INSTALLED AS PER SRM MD80 54-04.

Part: SKIN — CHAFED (VERTICAL STAB)

LEFT AND RIGHT AFT SECTION OF VERTICAL STAB HAS CHAFE MARK, BURNISHED OUT AND MEASURED, FOUND TO BE OUT OF LIMITS AS PER 55-01, MD80SRM. REMOVED SKIN SECTION AT LEFT AND RIGHT AFT VERTICAL STABILIZER AND REPLACED AS PER MD80 SRM 51-30-2.

Part: SKIN — GOUGED (VERTICAL STAB)

LEFT SIDE VERTICAL STABILIZER SKIN EDGE UNDER FWD LOWER BANANA FAIRING PREVIOUS GOUGE REPAIR IS GETTING WORSE. TRIMMED OUT DAMAGE, REMOVED PREVIOUS REPAIR AND INSTALLED NEW REPAIR AS PER RES 2002302-2.

Part: SEAT TRACK — CORRODED (FUSELAGE)

CORROSION AT SEAT TRACK SECTION STA 237, RBL 22. FOUND CORROSION TO BE OUT OF LIMITS. CUT OUT DAMAGED SECTION AND REPLACED WITH NEW SECTION AS PER SRM MD80 53-05.

Part: FRAME — CORRODED (FUSELAGE)

CORROSION AT AFT CARGO BAY STA 1271 FRAME AT LONGERON 30 AFT FACE. REMOVED DAMAGED SECTION AND SPLICE NEW SECTION PER SRM 53-03.

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: SHEAR TIE — BROKEN (FUSELAGE)

DURING BOW 1C/2C/3C/S1/S2/S4/S5/2A, FOUND SHEAR TIE END PIECE BROKEN AT STATION 769 BETWEEN L12L - L22L. ADDRESSED AS REQUIRED.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSP, MAINT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MAINT REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (K)

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT)

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. (A)

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. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED 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: CONTROL VALVE — LEAKING (RUDDER)

FLIGHT 758 PSM/SFB, THE FLIGHT CREW REPORTED THAT THE RIGHT HYDRAULIC SYSTEM PRESSURE AND QUANTITY READINGS DROPPED BELOW THE USEABLE MINIMUMS, PHASE OF FLIGHT NOT REPORTED. ITEM NR 2 ON THE SAME LOG PAGE REPORTS THAT "DURING MANUAL GEAR EXTENSION THE NOSE GEAR WOULD NOT EXTEND. AFTER EXHAUSTING ALL OPTIONS, LANDED W/NOSE GEAR RETRACTED. SUCCESSFUL EVACUATION FOLLOWED." THE RIGHT HYDRAULIC SYSTEM LEAK WAS DISCOVERED AT THE RUDDER CONTROL VALVE SUPPLY LINE CHECK VALVE CONNECTION TO THE PIPING. THE CAUSE OF THE LEAK IS UNDER INVESTIGATION BY THE NTSB AND FAA. THE FAILURE WHICH PREVENTED THE NOSE LANDING GEAR FROM EXTENDING DURING THE ATTEMPTED ALTERNATE GEAR EXTENSION OPERATION IS UNDER INVESTIGATION BY THE

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING A ROUTINE OVERNIGHT SERVICE CHECK SANFORD MAINTENANCE REPORTED THAT THE TAILCONE EMERGENCY LIGHTS WOULD NOT TEST. THEY FURTHER REPORT THEY RELAMPED THE TAILCONE EMERGENCY LIGHT ASSEMBLIES. A SATISFACTORY OPERATIONAL TEST WAS ACCOMPLISHED PER AMM 33-53-00.THE AIRPLANE HAS RETURNED TO SERVICE.

Part: POWERPACK — INOPERATIVE (EMERGENCY LIGHT)

LAS - MAINTENANCE FOUND THE L2 DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE POWER PACK. OPERATIONALLY CHECKED GOOD IAW MM 33-53-00. AIRCRAFT RETURNED TO SERVICE.