N895GA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
29 reports on file, 2008-02-14 – 2013-02-03.
Part: FLOORBEAM — CORRODED (FUSELAGE)
CORROSION NOTED ON FLOORBEAM AT STATION 237. REMOVED CORRODED AREAS, FABRICATED FILLERS AND REPAIR ANGLE AND INSTALLED.
Earlier reports · 2008–2012 · 28 reports
2012
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: SKIN — CRACKED (VERTICAL STAB)
REPAIRED CRACK IN VERTICAL STAB LEADING EDGE RAM AIR DUCT SKIN IAW EA 10-2012-066 AND MD80 SRM 55-05 PAR 6. REPAIRED CRACK IN VERTICAL STAB LEADING EDGE RAM AIR INLET DUCT SKIN IAW AAR/STS 10-2012-2066 PERMANENT REPAIR.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS)
DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN POWER SUPPLY BATTERY PACK. AN OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.
2011
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: 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.
2010
Part: DOOR FRAME — CRACKED (FUSELAGE)
AFT CABIN PRESSURE BULKHEAD DOOR JAMB HAS TWO CRACKS IN THE UPPER RIGHT CORNER FACING AFT (LEFT CORNER). REPAIRED VENTRAL DOOR JAMB UPPER RIGHT SIDE FACING AFT (LEFT CORNER) IAW MD80 SRM 53-05 FIG 29.
Part: SHEAR TIE — CORRODED (FUSELAGE)
AFT CARGO FRAME SHEAR TIE CORRODED AT FS 1231 BETWEEN LONGERON 27R AND 28R. REMOVED AND REPLACED FS 1231 FRAME SHEAR TIE IAW MD 80 SRM 51-30-2 AND 51-10-03.
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: 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 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.
2009
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 BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.
Part: SKIN — WORN (FUSELAGE)
LOWER FWD EXTERIOR SKIN ON FUSELAGE WORN ON FWD JAMB, FWD ENTRY DOOR.
Part: BRACKET — CORRODED (BS 1212)
FOUND CORROSION ON BRACKET AT STA 1212.
Part: MOUNT — CORRODED (ZONE 200)
G1 GALLEY FWD OUTBOARD MOUNT CORRODED.
Part: MOUNT — CORRODED (GALLEY)
G1 GALLEY MOUNT HAS CORROSION INSIDE GALLERY MOUNT HOLE.
Part: CUSP WEB — CORRODED (ZONE 100)
CORROSION ON LOWER SIDE OH LEFT CUSP WEB STA 1136 TO 1155.
Part: FRAME — CRACKED (ZONE 200)
CANT FRAME AT STA 1510 CRACKED AT LT TAILCONE ALIGNMENT PIN APPROXIMATELY AT 7 O'CLOCK.
Part: BRACKET — CRACKED (ZONE 100)
LEFT BRACKET CRACKED AFT SIDE OF BULKHEAD 37 ABOVE SHELF.
Part: BRACKET — CRACKED (ZONE 100)
RIGHT BRACKET CRACKED AFT SIDE OF BULKHEAD 37 ABOVE SHELF.
Part: CUSP WEB — CORRODED (ZONE 100)
CORROSION ON BOTTOM SIDE OF LEFT CUSP WEB BETWEEN STA 522 AND 541.
Part: LONGERON — CRACKED (ZONE 100)
LONGERON 5R IS CRACKED AT THE OUTBOARD LEG LOCK FASTENER AT THE AFT SIDE OF 1309 BULKHEAD.
Part: FRAME — CRACKED (ZONE 100)
STA 1463 CANT FRAME WEB CRACKED, ABOVE LT LOWER BOX
Part: CUSP WEB — CORRODED (ZONE 100)
STA 826 LEFT CORROSION ON CUSP WEB.
Part: LONGERON — CRACKED (ZONE 100)
FOUND LONGERON 12 LT CRACKED AT STA 1287 FRAME ATTACH FASTENERS, UPPER AND LOWER.
Part: CUSP WEB — CRACKED (ZONE 100)
ONE INCH CRACK IN CUSP WEB AT STA 806 RIGHT SIDE.
Part: BATTERY PACK — INOPERATIVE (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 BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE.
2008
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
IT HAS BEEN REPORTED BY THE FLIGHT CREW THE EMERGENCY EVACUATION LIGHTING SYSTEM HAS BEEN FOUND TO BE DEFECTIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS. AN OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.