N883GA

Part: WARNING LIGHT — ILLUMINATED (NLG) · airframe 38,928 hrs · 32,821 cycles

(EMERGENCY DECLARED) MID TAKE ROLL. NOSE GEAR SEEMED TO BE BOTTOMING OUT AFTER ROTATION & GEAR WAS NOT RETRACTED. THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED & WOULD NOT EXTINGUISH. LOUD SOUND OF WIND ALSO INDICATED GEAR WAS NOT UP & LOCKED. COMPLIED W/ QRH 32.9. DUE TO PREVIOUS NOSE GEAR ISSUES, EXTENDED GEAR HANDLE AND DID NOT RETRACT AGAIN. ALL 3 GREEN GEAR LIGHTS ILLUMINATED W/ NO RED LIGHTS. LANDED SOFTLY AT 134,000LBS WITH NO FURTHER ABNORMALITIES. / FOUND NLG STRUT COLLAPSED AND HYDRAULIC FLUID LEAKING. C/W NLG STRUT REPACK IAW TASK 32-047-003. NO LEAKS NOTED. AIRCRAFT OK FOR SERVICE. PERFORMED NLG EXTENSION AND RETRACTION IAW AMM 32-30-00-2. OPS CHECK GOOD AT THIS TIME."

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,485 hrs · 32,125 cycles

EVIDENCE OF CORROSION AT LONGERON 29R, STATION 726. ALSO CRACK EMANATING FROM RIVET IN SAME AREA. ACCOMPLISHED ERO 5334-007, REPAIR OF CORROSION DAMAGE AT LOWER FUSELAGE SKIN AT STATION 726, LONGERON 28R - 30.

Part: SKIN — CRACKED (FUSELAGE)

HAS A RIVET WITH A CRACK EMANATING FROM IT & ASSOCIATED CORROSION IN THAT AREA. DIMENSION OF CRACK IS ½ OF AN INCH. AREA OF CORROSION AS EVIDENCED BY BULGING SKIN IS 1 INCH BY 1 1/4. UNABLE TO ACCESS THE CORRODED AREA FROM INSIDE THE CARGO COMPARTMENT AS IT IS UNDERNEATH LONGERON 29R.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,462 hrs · 32,112 cycles

EMERGENCY LIGHTS IN TAIL COMPARTMENT ARE INOPERATIVE. R & R BATTERIES TO BOTH EMER POWER SUPPLY B5-27 & B5-28. OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,293 hrs · 32,023 cycles

EMERGENCY BATTERIES NEED CHARGED. EMER LIGHTS OPERATIONAL, CHECKED OK.

Part: TRIM SYSTEM — MALFUNCTIONED (PITCH TRIM) · airframe 56,252 hrs · 32,001 cycles

ALL PRIMARY PITCH TRIM FAILED ON DEPARTURE. AFTER COMPLETION OF QRH PRIMARY PITCH, TRIM OPERATES NORMAL. THIS LOG TRANSFERRED TO LOG 578598. SEE LOG PAGE 578598 FOR CORRECTIVE ACTION.

Part: VANE — OUT OF TOLERANCE (AOA) · airframe 55,912 hrs · 31,830 cycles

ON FINAL, BELOW 1200 AGL RECEIVED BOTH STALL INDICATION & AUTO SLAT FAIL CAUTION MSGS ON OAP. PERFORMED AR 511257 AUTO SLAT FAIL TROUBLE SHOT. FOUND RT AOA VANE OUT OF TOLERANCE. REPLACED VANE IAW MM 34-19-02-1. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

OVERHEAD EMER LIGHT IN FWD GALLEY INOPERATIVE. RELAMPED FWD GALLEY EMER LIGHT IAW AMM 33-50-00.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 55,774 hrs · 31,757 cycles

REFERENCE LOG PAGE 564424 ITEM 1. EMER EXIT LIGHTS OVERWING INOPERATIVE, RT & LT. RELAMPED RT & LT OVERWING EXIT EMER LIGHTS. OPERATIONS CHECKED GOOD IAW MM 26-60-00.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 55,774 hrs · 31,757 cycles

OVERHEAD EMER LIGHTS INOPERATIVE AT SEAT ROW 33 & 34. R & R BATTERY POWER SUPPLY AT SEAT ROW 33 & 34. OPERATIONS CHECKED GOOD IAW MM 25-60-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 55,774 hrs · 31,757 cycles

EMERGENCY LIGHTS INOPERATIVE ROWS 24 & 25. EMER EXIT LT & RT EMER LIGHT INOPERATIVE ROW 25 ISLE LT. REPLACED EMER EXIT ROWS LIGHT EMER BATTERY'S. OPERATIONS CHECKED GOOD IAW AMM 33-53-00.

Part: APU — LEAKING (APU BAY) · airframe 55,451 hrs · 31,600 cycles

AFTER PARKING AT THE GATE, THE CABIN & COCKPIT FILLED WITH SMOKE & AN ODOR. APU WAS RUNNING & PACKS WERE ON. NOTICED ON WALK AROUND AFT BELLY OF ACFT HAD DRIPPING OIL. PERFORMED MX IAW TC 21-059-008 & TC FO592102. PLACED APU ON MEL 49-01 SIT 1 CAT C DMI 15254. M PROCEDURES COMPLIED WITH. PLACARD INSTALLED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,717 hrs · 31,241 cycles

FOUND ON WAKE-UP. EMER LIGHTS AT ROW 34 INOPERATIVE. REPLACED BATTERIES FOR EMER LIGHTS AT ROW 34 IAW AMM 33-53-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,680 hrs · 31,224 cycles

FOUND ON WAKE UP, EMER LIGHTS INOPERATIVE AT ROWS 32 & 24. REPLACED BATTERIES. OPERATIONS CHECKED GOOD IAW AMM 33-53-01.

Part: INDICATION SYS — ACTIVATED (COCKPIT) · airframe 54,417 hrs · 31,096 cycles

RT ENG EGT 645 FOR 30 TO 40 SECONDS. NO LOG PAGE OR MI YET, 8/14 MI OPEN. ADDITIONAL INFO TO BE ADDED WHEN AVAILABLE.

Part: ACM — FAULTY (AC BAY)

CABIN TEMP EXCEEDS 38C THRU 15,000 FT DURING CLIMB OUT & WILL NOT DECREASE REF LOG PAGE 508152. REPLACED LT ACM IAW MM 21-51-01. PERFORMED OPERATIONS & LEAK CHECK IAW MM 21-00-00, OPERATIONS CHECKED NORMAL. OK FOR SERVICE, ALSO REF LOG PG 494591 RT PRESS REG IAW 21-31-02.

Part: BATTERY PACK — INOPERATIVE (CABIN)

AFT EXIT OVERWING LIGHTS OUT. REPLACED BATTERY PACK FOR AFT OVERWING EMER LIGHTS IAW AMM 33-50-00.

Part: BATTERY — DISCHARGED (CABIN)

OVERWING EMER EXIT LIGHTS INOPERATIVE. R & R BATTERIES FOR OVERWING EMER EXIT LIGHTS IAW AMM 33-53-00. OPERATIONS CHECKED GOOD.

Part: WIRE — OUT OF POSITION (CABIN)

AFT CABIN OVER DOOR EMERGENCY LIGHT INOPERATIVE, FOUND ON WAKE-UP. REPLACED POWER SUPPLY, NO HELP. FOUND T2 & T7 WIRES WERE SWAPPED. RESTORED WIRES TO CORRECT TERMINALS. OPERATIONS CHECKED GOOD IAW WMD 33-51-11 & 33-51-12.

Part: TAB — DELAMINATED (LT ELEVATOR)

LEFT ELEVATOR INBD TAB, (CONTROL TAB, OTBD AFT CORNER REPAIR DELAMINATED. REMOVED DAMAGE DOUBLER, FABRICATED REPAIR PARTS & INSTALLED IAW SRM 51-70-2.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

AFT CABIN FLASHLIGHT NOT FLASHING. REPLACED AFT CABIN EMERGENCY FLASHLIGHT BATTERY & OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — DEFECTIVE (CABIN)

EMERGENCY LIGHTS FLASHED ON & OFF DURING CRUISE. R & R POWER SUPPLY AT STATION 223 IAW AMM CH 33-53-00, OPERATIONS CHECKED GOOD.

Part: FAN — MALFUNCTIONED (CARGO BAY)

FLIGHT ATTENDANT CALLED UP COMPLAINING OF BURNING SMELL BETWEEN ROWS 18 - 21. AFTER 7 MINUTES SMELL WENT AWAY. COMPLIED WITH TASK CARD F0592102 CABIN ODOR, SMOKE & TROUBLE SHOT. LOUD GRINDING NOISE COMING FROM CABIN FLOOR AT ROWS 15 - 18 LT SIDE. PULLED CARGO COMPARTMENT HEATER BREAKERS & GRINDING NOISE SILENCED. R & R FWD CARGO COMPARTMENT HEATING FAN IAW AMM 21-41-02, OPERATIONS CHECKED GOOD PN ON 25130-1 ROW 12CA BALLAST INOPERATIVE. REPLACED BALLAST & OPERATIONS CHECKD GOOD IAW AMM 33-21-03 PN ON D773-11-00.

Part: BATTERY — DISCHARGED (CABIN)

DURING A ROUTINE OVERNIGHT SERVICE CHECK INSP MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX PERSONNEL R & R THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-00, SYS OPS CHECK WAS NORMAL. THE ACFT 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: CUSP WEB — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT CUSP WEB CORRODED BETWEEN FLOORBEAMS AT STATION 1174 TO 1193 RBL 52. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER REPAIR.

Part: CUSP WEB — CORRODED (FUSELAGE)

AFT CARGO COMPARTMENT TO CABIN CSP WEB CORRODED BETWEEN STATION 1193 TO 1211 AT RBL 52. REMOVED DAMAGE AREA AND INSTALLED FILLER AND DOUBLER.

Part: DOOR FRAME — CRACKED (FUSELAGE)

AFT ENTRY DOOR FRAME CRACKED AT LEFT UPPER CORNER.

Part: WEB — CRACKED (LT ENGINE)

LEFT ENGINE INLET COWL AFT WEB CRACKED AT ACCESS PANEL FASTENER AT 4:30 O'CLOCK POSITION.

Part: PAN — CHAFED (FUSELAGE)

FWD ACCESSORY DOOR JAMB PAN CHAFED AT FWD END IN LOWER RADIUS.

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: SEAT TRACK — DAMAGED (FUSELAGE)

PASSENGER CABIN RIGHT SEAT TRACK RBL 22 STA 927 TO 1003 HAD DOUBLE DRILLED HOLES. REMOVED AND REPLACED TRACK WITH SPLICE IAW MD80-SRM 5305.

Part: SKIN — CORRODED (FUSELAGE)

FOUND CORROSION ON INNER SKIN UNDER BELLY DRAIN RIGHT SIDE OF LONG 30 APPROX STA 731. REMOVED AND REPAIRED FUSELAGE SKIN.

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: 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: UNKNOWN — SPARKS (COCKPIT)

WHILE TAXIING OUT A LARGE SPARK APPEARED OUT OF THE GLARE SHIELD PANEL, REPOSITIONED WIRES IAW 56-10-01. OPS CHECK OF WINDSHIELD TEMP CONTROLLER IAW 30-41-00, OPS CHECK NORMAL AT THIS TIME. 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: 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: BEAM — CORRODED (CARGO DOORWAY)

DURING BOW 1C/2C/S1/S2/S4, WO 94586 CORROSION WAS FOUND ON THE AFT CARGO DOOR BEAM THAT WAS OUT OF LIMITS STA 1155 TO 1211. ADDRESSED AS REQUIRED.

Part: CUSP WEB — CRACKED (BS 228)

DURING BOW 1C/2C/S1/S2/S4, IN THE CABIN FOUND CRACK IN LEFT CUSP AT STA 228. ADDRESSED AS REQUIRED.

Part: CUSP WEB — CRACKED (BS 218-237)

DURING BOW 1C/2C/S1/S2/S4, LEFT CUSP WAS FOUND CRACKED BETWEEN STA 218 - 237. ADDRESSED AS REQUIRED.

Part: CUSP WEB — DAMAGED (BS 905)

DURING BOW 1C/2C/S1/S2/S4, CUSP MEMBRANE COLLAR FOUND DAMAGED AT STA 905 RIGHT. ADDRESSED AS REQUIRED.

Part: CUSP WEB — CRACKED (BS 225)

DURING BOW 1C/2C/S1/S2/S4, RIGHT CUSP AT STA 225 FOUND CRACKED, OUTBOARD OF SEAT TRACK 6. ADDRESSED AS REQUIRED.

Part: SEAT TRACK — CRACKED (BS 927)

DURING BOW 1C/2C/S1/S2/S4 FOUND NR 5 SEAT TRACK SUPPORT CASTING CRACKED AT STA 927, JUST ABOVE FUEL TANK. REPLACED SUPPORT CASTING MPN 3925812.2 PER SRM 51-01, REF E58 6446902 ADDRESSED AS REQUIRED.

Part: BATTERY PACK — NO TEST (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: UNKNOWN — UNKNOWN

AIRCRAFT 883GA, FLIGHT 762 DURING CRUISE FLIGHT THE CARGO SMOKE DETECTOR LOOP LIGHT ILLUMINATED. FLIGHT CREW FOLLOWING QRH PROCEDURES TESTED THE SYSTEM BY PRESSING AND HOLDING THE WARN/CAUTION LTS TEST SWITCH AND ALL CDSCP LIGHTS ILLUMINATED. RETESTING THE SYSTEM AND ALL CHECKS WERE NORMAL. THE MAINTENANCE CONTROL DEPARTMENT DISPATCHED ON CALL MAINTENANCE AND VISUALLY INSPECTED ALL DETECTORS, NO DAMAGE NOTED. PERFORMED SEVERAL BITE TESTS AND ALL CHECKS WHERE NORMAL. AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: LIGHT — NO TEST (CABIN)

DURING A ROUTINE OVERNIGHT RON CHECK MAINTENANCE INSPECTION, LAS VEGAS MAINTENANCE REPORTED A FORWARD EMERGENCY EXIT PORTABLE LIGHT WOULD NOT TEST. LAS VEGAS MAINTENANCE FURTHER REPORT THE REMOVAL AND INSTALLATION OF AN EMERGENCY EXIT PORTABLE LIGHT. A SATISFACTORY OPERATIONAL TEST WAS ACCOMPLISHED PER AMM 33-53-00. THE AIRPLANE HAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (WING)

DURING A ROUTINE MAINTENANCE INSPECTION MAINTENANCE REPORTED AN APPARENT CRACK IN AN UPPER WING SURFACE PANEL AT APPROXIMATELY WING STATION 48.00. FURTHER INSPECTION REVEALED A CRACK OF APPROXIMATELY 13-INCHES LENGTH IN THE COMPOSITE PANEL AT WING STATION 47.95. A TEMPORARY REPAIR WAS ACCOMPLISHED ON THE CRACKED PANEL PER ENGINEERING REPAIR ORDER 5704-001. THE AIRPLANE HAS RETURNED TO SERVICE.