N557AN
Registered owner: PAC BLUE AEROSPACE, AK (owner ≠ operator)
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.
51 reports on file, 1995-11-11 – 2015-02-24.
Part: CONNECTOR — DISCONNECTED (ZONE 200) · airframe 67,949 hrs · 35,427 cycles
TAIL COMPARTMENT STAIRS SIDEWALL AFT LIGHT INOPERATIVE. FOUND CONNECTOR OFF, RE-CONNECTED IAW SP. PERFORMED OPERATIONAL CHECK IAW AMM 33-53-00. SYS CHECKED NORMAL.
Part: CONNECTOR — DISCONNECTED (ZONE 200) · airframe 67,949 hrs · 35,427 cycles
TAIL COMPARTMENT OVERHEAD LIGHTS INOPERATIVE. FOUND CONNECTOR OFF, RECONNNECTED IAW SP. PERFORMED OPERATIONAL CHECK IAW AMM 33-53-00. SYS CHECKED NORMAL.
Earlier reports · 1995–2014 · 49 reports
2014
Part: LIGHT — MISSING (CABIN) · airframe 67,739 hrs · 35,298 cycles
SEAT 22D EMER LIGHT ASSEMBLY IS MISSING. INSTALLED NEW LIGHT ASSEMBLY IAW AMM 33-60-98-401 & PERFORMED CHECK IAW AMM 33-60-98-501. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (AC BAY) · airframe 66,115 hrs · 34,328 cycles
EMERGENCY LIGHT OVER TAIL CONE SLIDE FAILED TO OPERATE DURING TEST. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT OVER TAIL CONE, OPERATIONS CHECKED NORMAL.
2013
Part: CHARGER — INOPERATIVE (CABIN) · airframe 64,913 hrs · 33,610 cycles
EMERGENCY LIGHTS CONTROLLED BY BATTERY PACK B5-28 INOPERATIVE ON TEST. R & R BATTERY CHARGER AT B5-28, OPERATIONS CHECKED NORMAL
Part: CASTING — CRACKED (RT WING) · airframe 64,371 hrs · 33,269 cycles
RT HAND WING, INBD CASTING CRACKED AT NR 4 SLAT TRACK. INSTALLED SERVICEABLE CASTING FITTING IAW AARD 51-00-05-1 & DRAWING 9937490.
Part: RIB — CRACKED (LT WING) · airframe 64,371 hrs · 33,269 cycles
LT HAND WING LE CASTING CRACKED AT TOP INBD OF NR 4 SLAT TRACK. INSTALLED NEW RIB IAW AARD 51-00-05-1 & DRAWING 9937490.
2012
Part: TARGET — MISSING (LT MLG) · airframe 61,016 hrs · 31,330 cycles
ORD - CREW REPORTED GEAR DOOR OPEN LIGHT REMAINS ON WITH GEAR RETRACTED. EMERGENCY DECLARED FLIGHT LANDED ORD WITHOUT INCIDENT. AIRCRAFT LANDED WITH BOTH MAIN LANDING GEAR DOORS DOWN. AIRCRAFT REMOVED FROM SERVICE. FOUND LEFT GEAR DOOR MISSING TARGET/SENSOR AND BRACKET. REPLACED TARGET/SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.
2011
Part: SENSOR — INOPERATIVE (AC BAY) · airframe 59,113 hrs · 30,269 cycles
DFW - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. ACCOMPLISHED QRH PROCEDURES AND LIGHT DID EXTINGUISH. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT AND LEFT TAIL COMPARTMENT HIGH TEMPERATURE SENSORS. SYSTEM GROUND CHECK NORMAL OPERATION.
2010
Part: LONGERON — CRACKED (FUSELAGE) · airframe 56,877 hrs · 29,015 cycles
LONGERON 2 RIGHT AT 1418 CRACKED. ACCOMPLISHED LONGERON REPAIR PER AARD 53-30-00-2 AND EA MD80-53-013235.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,877 hrs · 29,015 cycles
CRACKED SHEAR TIE AT STATION 1437 AND LONGERON 2 LEFT. INSTALLED SERVICABLE SHEAR TIE PER SRM"S 53-05-00, 51-30-05, 51-30-02.
Part: DIAPHRAGM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,877 hrs · 29,015 cycles
FORWARD CABIN SUBFLOOR IS CORRODED BEYOND LIMITS FROM STATIONS 200 TO 218 JUST AFT OF FORWARD SERVICE DOOR. DOUBLER WAS INSTALLED PER AARD 53-20-00-16.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,877 hrs · 29,015 cycles
CRACKED FRAME AT STATION 1418 AND LONGERON 2 LEFT. INSTALLED DOUBLER PER AARD 5310-00-15 AND SRM 51-30-05.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,877 hrs · 29,015 cycles
SHEAR TIE CRACKED AFT SIDE 1451 LONGERON 2 LEFT. INSTALLED NEW SERVICEABLE SHEAR TIE AFT OF STATION 1451 LONGERON 2 LEFT PER SRM 53-30-05.
Part: SKIN — GOUGED (FUSELAGE) · airframe 56,877 hrs · 29,015 cycles
GOUGE FOUND IN SKIN AT STATION 210 LONGERON 19 LEFT. MEASURES .029 DEEP X .025 AFTER BLENDING ACCOMPLISHED. PERFORMED PERMANENT REPAIR PER EA MD80-53-013084 DATED 9/20/2010.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,877 hrs · 29,015 cycles
CUSP MEMBRANE AT FORWARD ENTRY AREA, IS CORRODED AT LEFT BUTTLINE 60 FROM STATIONS 160 TO 200. INSTALLED CUSP MEMBRANE PER AARD 53-20-00-16.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 56,877 hrs · 29,015 cycles
INTERCOSTAL CRACKED BETWEEN FLOORBEAMS STATION 1271 TO 1287 AT CENTER. REPLACED CRACKED INTERCOSTAL PER SRM 51-30-05 AND EA MD80-51-013029.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,877 hrs · 29,015 cycles
CORROSION ON SUPPORT ANGLE AT STATIONS 200 TO 208 RIGHT CUSP LINE. INSTALLED NEW SUPPORT ANGLE AT STATIONS 200 TO 208 RIGHT CUSP PER SRM 51-01-00 AND SRM 51-30-05.
Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 56,877 hrs · 29,015 cycles
G-1 GALLEY MOUNT HOLES OVERSIZED AT STATION 160 AT RIGHT BUTTLINE 45 TO 51 THROUGH FLOORBEAM. INSTALLED REPAIR STRAP ON TOP OF FLOORBEAM STATION 160 RIGHT BUTTLINE 42 TO 58 PER EA MD80-53-013020.
Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,877 hrs · 29,015 cycles
CABIN GALLEY TIE-DOWN CORRODED AT STATION 218 RIGHT BUTTLINE 10. INSTALLED DOUBLER ON SUBFLOOR PER AARD 53-20-00-16. INSTALLED UPPER G2 GALLEY MOUNT PER SRM 51-30-05.
Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 56,877 hrs · 29,015 cycles
CABIN SUBFLOOR IS CORRODED BEYOND LIMITS STATIONS 160 TO 200 INBOARD OF FORWARD SERVICE DOOR. INSTALLED REPAIR DOUBLER AND FACTORY DOUBLER AT STATIONS 160 TO 200 PER AARD 53-20-00-16.
Part: STRAP — DAMAGED (FUSELAGE) · airframe 56,877 hrs · 29,015 cycles
FORWARD CARGO 2 SCREW GOUGES IN STRUCTURE INBOARD SIDE OF RIGHT TIE DOWN TRACK AT STATION 360 TO 370. REMOVED AND REPLACED STRAP PER SRM 51-10-03.
Part: MEMBRANE — PUNCTURED (FUSELAGE) · airframe 56,877 hrs · 29,015 cycles
SUBFLOOR PUNCTURED STATION 148 RIGHT BUTTLINE 9. INSTALLED DOUBLER PER AARD 53-20-00-16.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 56,877 hrs · 29,015 cycles
AFT ACCS SHEAR TIE CRACKED AFT SIDE OF 1451 AFT OF LONGERON 2 RIGHT. INSTALLED NEW SERVICEABLE SHEAR TIE AFT SIDE OF 1451 FRAME LONGERON 2 RIGHT PER SRM 51-30-05.
Part: BRACKET — CRACKED (ZONE 200) · airframe 56,877 hrs · 29,015 cycles
VAULT DOOR CUT OUT RIGHT MID JAMB BRACKET CRACKED. INSTALLED NEW BRACKET PER SRM 51-30-02.
Part: SEAT TRACK — CORRODED (BS 224) · corrosion level 2 · airframe 56,877 hrs · 29,015 cycles
NUMBER 4 SEAT TRACK INBOARD FLANGE CORRODED STATION 224. INSTALLED STRAP PER AARD 53-20-00-13.
Part: BRACKET — CRACKED (ZONE 200) · airframe 56,877 hrs · 29,015 cycles
VAULT DOOR CUTOUT RIGHT LOWER JAMB BRACKET CRACKED. INSTALLED NEW BRACKET PER SRM 51-30-02.
Part: SKIN — GOUGED (FUSELAGE) · airframe 56,877 hrs · 29,015 cycles
DEEP GOUGE IN SKIN BELOW CUSP LINE AT STATION 229.7. INSTALLED DOUBLER, FILLER AND FINGER DOUBLER PER SRM 53-04-00 FIGURE 12B.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,877 hrs · 29,015 cycles
SEAT TRACK NUMBER 3 OUT OF LIMITS AT STATION 1304. INSTALLED NEW NUMBER 3 SEAT TRACK SECTION STATIONS 1262 TO 1304 AND SPLICE AT STATION 1262 AS PER SRM 53-05-00 FIGURE 4F.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 56,877 hrs · 29,015 cycles
LONGERON 5 LEFT STATION 1309 HAS CRACKS AFT SIDE. INSTALLED LONGERON SPLICE REPAIR PER SRM 53-02-00.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 56,877 hrs · 29,015 cycles
VAULT DOOR CUTOUT RIGHT TOP JAM BRACKET CRACKED. INSTALLED NEW BRACKET PER SRM 51-30-02.
Part: SUPPORT — CRACKED (RT MLG WW) · airframe 56,877 hrs · 29,015 cycles
RIGHT MAIN LANDING GEAR WHEEL WELL - GREEN BRACKET CRACKED AT TOP OF WHEEL WELL DOOR ACTUATOR. REMOVED AND INSTALLED SERVICEABLE SHELF ABOVE RIGHT MAIN LANDING GEAR DOOR ACTUATOR PER SRM 51-30-5.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 56,877 hrs · 29,015 cycles
VAULT DOOR CUTOUT MID-JAMB BRACKET CRACKED LEFT SIDE. REMOVED AND REPLACED BRACKET PER SRM 51-01-00.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 56,877 hrs · 29,015 cycles
LEFT WINDOW FRAME BETWEEN STATIONS 1022 AND 1003 AFT TOP CRACKED MARKED. INSTALLED REPAIR ANGLE PER AARD 53-10-00-25.
2009
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,083 hrs · 26,931 cycles
AFT ACCESSORY, FORWARD SIDE OF FRAME 1418 CRACKED AT STRINGER 2 LEFT. INSTALLED DOUBLER PER SRM 53-03-00 AND EA MD80-53-005869.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,083 hrs · 26,931 cycles
AFT ACCESSORY, FORWARD SIDE OF FRAME 1418 CRACKED AT STRINGER 2 RIGHT. INSTALLED DOUBLER PER SRM 53-03-00 AND EA MD80-53-005869.
2008
Part: BATTERY PACK — DISCHARGED (CABIN) · 51,552 cycles
LGA EXTERIOR EMERGENCY LIGHTS AT AFT RT AND LT HAND FUSELAGE INOPERATIVE. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHTS AT AFT RT AND LT HAND FUSELAGE. SYSTEM GROUND CHECKED NORMAL OPS.
2007
Part: LENS — MISSING (CABIN)
LGA - EMERGENCY ESCAPE PATH LIGHTING AT SEAT 23D HAS MISSING LENS COVER. REPLACED LENS COVER FOR EMERGENCY ESCAPE PATH LIGHTING AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: BATTERY PACK — DISCHARGED (CABIN)
LAX - OVERHEAD EMERGENCY LIGHTS ABOVE AFT FLIGHT ATTENDANT STATION INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS ABOVE AFT FLIGHT ATTENDANT STATION. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: BATTERY PACK — DISCHARGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT AFT AIR STAIR. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: BATTERY — NOT SEATED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, AFT CEILING EMERGENCY EXIT LIGHTS AT AFT JUMP SEAT INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONTACTOR — DIRTY (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS L2-690-691 INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY PACK — LOOSE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHTS AT ROW 18-21 ARE DIM. SECURED BATTERY PACK AT ROW 18-21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY PACK — LOOSE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS AT SEATS 20D THROUGH 17D INOPERATIVE. ADJUSTED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY — NOT SEATED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS BETWEEN ROWS 28-31 INOPERATIVE. RESEATED EMERGENCY EXIT LIGHTS BATTERY ON BATTERY PACK B5-107. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2001
Part: BATTERY PACK — DISCHARGED (AIRSTAIRS)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AFT AIRSTAIRS DIM. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: FAN BLADE — VIBRATES (NR 1 ENGINE)
DFW - FLT 1027 - EN ROUTE DFW-SAT, DETECTED VIBRATION AT NR 1 SIDE ENGINE. NR 1 SIDE ENGINE VIBRATION DID NOT SUBSIDE AFTER THROTTLE REDUCTION. AIR INTERRUPTED, RETUREND DFW AND LANDED WITHOUT FURTEHR INCIDENT. REPLACED NR 1 SIDE ENGINE. REPLACED FIRST STAGE FAN BLADE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: APU — LEAKING (AFT FUSELAGE)
IAH - FLT 2082 - AFTER TAKEOFF, STRONG BURNING OIL SMELL ALONG WITH SMOKE IN CABIN. RETURNED AND LANDED IAH WITHOUT INCIDENT. APU BEING USED AS SUPPLEMENTAL ELECTRICAL SOURCE. REPLACED APU AND ACCOMPLISHED HIGH PRESSURE PNEUMATIC BURNOUT AND PACK BURNOUT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1997
Part: CONNECTOR — LOOSE (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY FOUND INOPERATIVE. RE-SECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1996
Part: SEAT BELT — DEFECTIVE (CABIN)
SNA - FLT 1820 - DURING TAKEOFF ROLL AT SNA, THE LAND LIGHT ILLUMINATED AND CREW ABORTED TAKEOFF. DURING ABORTED TAKEOFF SEAT BELT 25F CAME APART. AIRCRAFT CAME TO A HALT WITHOUT FURTHER INCIDENT. REPLACED SEAT BELT 25F AND ROUTED OLD BELT TO TUL. (M)
1995
Part: BATTERY CHGR — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT SIGN LIGHTS ON LT AND RT AFT OVERWING EXITS INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)