N627AA
Registered owner: PEREGRINE HOWARD PARTNERS II LP, LA (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.
36 reports on file, 1995-12-22 – 2011-03-23.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 64,677 hrs · 22,973 cycles
CROWN SKIN BY BODY STATION 394 STRINGER 4 LEFT DAMAGED. ACCOMPLISHED DOUBLER REPAIR PER EA B757-53-015839.
Part: SKIN — CRACKED (FUSELAGE) · airframe 64,677 hrs · 22,973 cycles
CRACK IN UPPER SKIN BETWEEN BODY STATIONS 377 TO 395 AT STRINGER 4 LEFT LAP SPLICE. REPAIRED DOUBLER PER EA B757-53-015839.
Earlier reports · 1995–2010 · 34 reports
2010
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,602 hrs · 22,592 cycles
INTERIOR EMERGENCY LIGHTS BETWEEN SEATS 9D AND 15D DIM. REPLACED BATTERY PACK AT M10799. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,339 hrs · 22,506 cycles
RIGHT FORWARD OVERWING EMERGENCY HATCH EXIT FORWARD EMERGENCY LIGHT ABOVE EXIT INOPERATIVE. REPLACED FORWARD EMERGENCY EXIT LAMP. OPS CHECKS GOOD.
Part: TACH GENERATOR — DEFECTIVE (NR 2) · airframe 62,848 hrs · 22,331 cycles
SJU - INFLIGHT BGI-MIA. CREW REPORTED RIGHT ENGINE N3 ERRATIC IN FLIGHT, VARIES FROM 86 PERCENT TO 71 PERCENT. FLIGHT DIVERTED SJU LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO N3 TACH-GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,500 hrs · 21,845 cycles
AFT ROW 26 EMERGENCY LIGHTS OUT. REPLACED BATTERY PACK FOR ROW 26 EMERGENCY LIGHTS. OPS CHECKED NORMAL.
2009
Part: CONTROL PANEL — FAILED (CABIN) · airframe 60,954 hrs · 21,649 cycles
EMERGENCY LIGHT OVER DOORS AND CEILING INOPERATIVE. REPLACED CONTROL PANEL.
Part: PAN — GOUGED (PAX DOOR) · airframe 60,524 hrs · 21,502 cycles
LEFT NUMBER 1 PASSENGER ENTRY DOOR HAS DOOR HANDLE GOUGE IN PAN RADIUS. INSTALLED NEW DOOR HANDLE PAN PER ESO 90283.
Part: ACCESS PANEL — CRACKED (LE SLAT) · airframe 60,524 hrs · 21,502 cycles
NUMBER 1 SLAT AFT SIDE ACCESS PANEL IS CRACKED AT FASTENER. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 57-43-00-4.
Part: GATE — CRACKED (DOOR) · airframe 60,524 hrs · 21,502 cycles
TOP GATE CRACKED AT ROD END ATTACH LOCATION. REMOVED AND REPLACED UPPER GATE NUMBER 1 DOOR PER ESO 90283.
Part: SLAT — CORRODED (RT WING) · corrosion level 2 · airframe 60,524 hrs · 21,502 cycles
CORROSION FOUND ON NUMBER 10 SLAT 102 INCHES FROM THE INBOARD END. INSTALLED FLUSH-DOUBLER PER SRM 57-43-01-2R.
Part: SLAT — CORRODED (LT WING) · corrosion level 2 · airframe 60,524 hrs · 21,502 cycles
NUMBER 1 LEADING EDGE SLAT HAS CORROSION AT FASTENER HEAD 65 INCHES FROM OUTBOARD EDGE. REMOVED CORROSION PER MM 51-00-53 AND INSTALLED DOUBLER PER AARD 57-43-00-1.
Part: SLAT — CORRODED (LT WING) · corrosion level 2 · airframe 60,524 hrs · 21,502 cycles
NUMBER 1 LEADING EDGE SLAT HAS CORROSION AROUND FASTENER HEAD AT 30 INCHES FROM INBOARD EDGE. REMOVED CORROSION PER MM 51-00-53 AND INSTALLED DOUBLER PER AARD 57-43-00-1.
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 60,524 hrs · 21,502 cycles
PREVIOUSLY BLENDED CORROSION AREA ON NUMBER 1 LEADING EDGE SLAT 30 INCHES FROM INBOARD EDGE IS BEYOND LIMITS PER SRM 57-43-01 DETAIL V. REMOVED DAMAGED SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.
Part: SPAR — DAMAGED (RT WING) · airframe 60,524 hrs · 21,502 cycles
RIGHT WHEEL LEADING-EDGE SPAR HAS DAMAGE AT 102 INCHES FROM INBOARD END. INSTALLED DOUBLER REPAIR PER AARD 51-70-00-3.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 60,472 hrs · 21,481 cycles
RIGHT NUMBER THREE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED RIGHT NUMBER THREE DOOR EXTERIOR EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 60,472 hrs · 21,481 cycles
LOWER AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED AFT EXTERIOR EMERGENCY LIGHT.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 59,772 hrs · 21,252 cycles
VERTICAL STIFFENER CRACKED AT STATION 700. REPAIRED IAW SRM.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 59,772 hrs · 21,252 cycles
FLOOR SUPPORT CRACKED. REPAIRED IAW SRM.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 59,772 hrs · 21,252 cycles
VERTICAL STIFFENER CRACKED. REPAIRED IAW SRM.
2008
Part: PLACARD — DAMAGED (CABIN)
DFW RT AFT EMERGENCY LIGHT EXIT IDENTIFIER PLACARD IS DAMAGED. REPLACED PLACARD FOR RT AFT EMERGENCY LIGHT EXIT IDENTIFIER. SYSTEM GROUND CHECKED NORMAL OPS.
Part: PLACARD — DAMAGED (CABIN)
DFW LT AFT EMERGENCY LIGHT EXIT IDENTIFIER PLACARD IS DAMAGED. REPLACED PLACARD FOR LT AFT EMERGENCY LIGHT EXIT IDENTIFIER. SYSTEM GROUND CHECKED NORMAL OPS.
Part: PLACARD — DAMAGED (CABIN)
DFW LT FORWARD EMERGENCY LIGHT EXIT IDENTIFIER PLACARD IS DAMAGED. REPLACED PLACARD FOR LT FORWARD EMERGENCY LIGHT EXIT IDENTIFIER. SYSTEM GROUND CHECKED NORMAL OPS.
Part: LAMP — MISSING (EMERGENCY LIGHT)
DFW - EMERGENCY LIGHT AT SEAT ROW 12DEF MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 12DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SHROUD — DAMAGED (EMERGENCY LIGHT)
DFW - EMERGENCY LIGHT AT SEAT ROW 12DEF HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 12DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (EMERGENCY LIGHT)
DFW - EMERGENCY LIGHT AT SEAT ROW 12DEF MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 12DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
LAX - EMERGENCY LIGHTS AT AFT THREE SEATS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT THREE SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHT UNARMED ANNUNCIATOR HAS ONE BULB INOPERATIVE. RELAMPED EMERGENCY LIGHT UNARMED ANNUNCIATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: SLIDE — INOPERATIVE (L1 DOOR)
TPA - INADVERTENTLY DEPLOYED L1 SLIDE DURING TROUBLESHOOTING OF GIRT BAR. SLIDE DEPLOYMENT UNSUCCESSFUL. REPLACED L1 SLIDE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: GIRT BAR — MISINSTALLED (L1 DOOR)
MEX - L1 DOOR SLIDE LIGHT INOPERATIVE. REINSTALLED GIRT BAR AT L1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: SPRING — DAMAGED (GIRT BAR)
DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, ONE GIRT BAR SPRING OUT OF ADJUSTMENT. ADJUSTED ONE GIRT BAR SPRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY — NOT SEATED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD BAG BIN EMERGENCY EXIT LIGHTS AT 20D, 22C, AND 24D INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: WIRE HARNESS — DISCONNECTED (CABIN)
LAX - SEAT 1EF EMERGENCY LIGHT HARNESS DISCONNECTED. RECONNECTED HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: SOCKET — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 21D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SET 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1999
Part: WIRE — LOOSE (ROW 27DEF)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 27DEF INOPERATIVE. RE-SECURED WIRE TO EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 27DEF. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1995
Part: HOSE — LEAKING (LT MLG)
LAX - FLT NR 41 - DURING APPROACH TO LAX WHEN LANDING GEAR LOWERED AND FLAPS EXTENDED, LEFT HYDRAULIC QUANTITY WENT TO ZERO AND LOST ALL LEFT HYDRAULIC PRESSURE. ACCOMPLISHED QRH PROCEDURE AND AIRCRAFT LANDED LAX WITHOUT INCIDENT. INSTALLED LANDING GEAR PINS AND AIRCRAFT TOWED TO GATE. REPLACED HYDRAULIC PRESSURE HOSE TO LEFT MAIN LANDING GEAR DOWNLOCK ACTUATOR. SERVICED HYDRAULIC SYSTEM. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. REMOVED LANDING GEAR PINS. (M)