Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CALA9800702Hyd Lines · puncturedTHE A SYSTEM HYDRAULIC FLUID LEVEL DROPPED TO ZERO WHILE ON DESCENT INTO PHL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND TWO HYDRAULIC FLEX LINES AT LT ELEVATOR PCU PUNCTURED. THE FLEX LINES WERE REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECSDR CALA9701684Line · leakingTHE AIRCRAFT LOST A-HYDRAULIC SYSTEM WHILE EN ROUTE. THE AIRCRAFT WAS DIVERTED TO BUF WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT WING AFT SPAR PRESSURE HYDRAULIC LINE LEAKING. A FLEX LINE WAS INSTALLED AND A DIP WAS ISSUED TO REPLACE THE LSDR CALA9701243Pcu · inoperativeA/C ATTEMPTED TO BANK LT WITH YAW DAMPER ON AND AUTOPILOT ENGAGED WHILE CLIMBING THRU 17,000 FT. THE YAW DAMPER WAS SWITCHED OFF AND ROLL ARRESTED. BANK ANGLE DID NOT EXCEED 15 DEG. APPROPRIATE CHECKLISTS COMPLETED AND THE FLT CONTINUED W/O PROBLEM. THE RUDDERSDR CAL950463Uplock Sensor · inoperativeFLT NR 9860 - CLE - THE RT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CYCLING THE GEAR DID NOT HELP. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. THE RT MLG UPLOCK SENSOR WAS REMOVED AND REPLACED. THE GEAR WAS SWSDR CAL950405Skin · crackedGSO - INSPECTION FOUND FUSELAGE SKIN FASTENER HOLES CRACKED IN SEVERAL PLACES BETWEEN WL 207.5 AND 234.35, SECTION 41. THE CRACKS WERE APPROXIMATELY .25 INCH LONG. THE CRACKED AREA WAS REMOVED. DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW EA 5310-0SDR CAL950404Skin · crackedGSO - INSPECTION FOUND FUSELAGE SKIN FASTENER HOLES CRACKED IN SEVERAL LOCATIONS BETWEEN BS 188-251.6 RIGHT SIDE. THE CRACKS WERE APPROXIMATELY .25 INCH LONG. THE CRACKED SECTION OF SKIN WAS REMOVED. REPAIR DOUBLER S AND FILLERS WERE FABRICATED AND INSTALLESDR CAL950403Skin · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN EXTERNAL SKIN AT STRINGER 4L, STATION 908. THE CRACKED AREA WAS CUTOUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2. (W)SDR CAL950402Frame · corrodedGSO - INSPECTION FOUND CORROSION ON FRAME ABOVE STRINGER 26R AT STATION 529. A NEW FRAME AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2. (W)SDR CAL950401Frame · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME BETWEEN S20L AND S21L AT STATION 440. THE FRAME WAS REMOVED AND REPLACED IAW BOEING DRAWING NR 65C25113 AND EA 5310-01211. (W)SDR CAL950400Frame · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME BETWEEN S20L AND S21L AT STATION 500. THE CRACKED SECTION OF FRAME WAS CUTOUT. A NEW SECTION OF FRAME WAS FABRICATED AND INSTALLED IAW BOEING BLUE PRINT NR 65C25113 AND EA 5310-01211. (W)SDR CAL950399Frame · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN FRAME BETWEEN S20L AND S21L AT STATION 480. THE CRACKED SECTION OF FRAME WAS CUOTUT. A NEW SECTION OF FRAME WAS INSTALLED IAW BOEING DRAWING NR 65C25113 AND EA 5310-01211. (W)SDR CAL950398Frame · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME BETWEEN S22L AND S23L AT STATION 460. THE CRACKED FRAME WAS REMOVED AND A NEW FRAME AND DOUBLERS WERE INSTALLED IAW BOEING PRINT NR 65C25113. (W)
Other aircraft with N14208 · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N14208 now.