Service difficulty reports · 55
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR COMA0110004Frame · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-012 AND 132-012 THE FUSELAGE FRAME 20 CHANNEL BETWEEN STRINGERS 20L AND 20R WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURE REPAIR MANUAL STANDARD PRACTICES AND SRM 53-10-04 FIGURE 201 ASDR COMA0010108Floorbeam · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121-01I, THE LT FLOOR PROP AT FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, REV IR, 5-3-00.SDR COMA0010123Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.
See all 55 reportsOther aircraft with N263CA · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N263CA is registered now to the first aircraft listed.