Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR E6RA200124002Regulator · failedON TAKE-OFF, NUMBER 2 GENERATOR FAILED. TAKE-OFF ABORTED AND AIRCRAFT RETURNED TO GATE. SWAPPED NUMBER 2 GENERATOR CONTROL UNIT (GCU) WITH APU GCU AND CONFIRMED FAILURE. INOPERATIVE GCU WAS DEFERRED IN ACCORDANCE WITH MEL. GCU WAS FUNCTIONALLY TESTED IN ACCORSDR EE4Y2000002Skin · debondedDURING HEAVY MAINTENANCE INSPECTION, LEFT WING INBOARD FLAP TRAILING EDGE SKIN WAS FOUND DISBONDED AT THREE DIFFERENT LOCATIONS. TOTAL AREA DAMAGED WAS 89 SQUARE INCHES. REASON FOR THIS DAMAGE WAS UNKNOWN. (X)SDR EE4Y2000005Intercostal · crackedDURING HEAVY MAINTENANCE INSPECTION, FOUND FORWARD CARGO COMPARTMENT INTERCOSTAL CRACKED AT BS 500 AND BS 460, AND STR 2L.. REASON FOR THIS DAMAGE WAS UNKNOWN. (X)SDR EE4Y2000003Skin · delaminatedDURING HEAVY MAINTENANCE INSPECTION FOUND RIGHT WING OUTBOARD FLAP LOWER KSI MID-SECTION DELAMINATED BETWEEN WBL 390 AND WBL 397. REASON FOR THIS DAMAGE WAS UNKNOWN. (X)SDR EE4Y2000001Skin · canningDURING HEAVY MAINTENANCE INSPECTION, FOUND SKIN WITH OIL CAN DAMAGE AT BS 331 BETWEEN STR 24R AND STR 25R. REASON FOR THIS DAMAGE WAS UNKNOWN. (X)SDR EE4Y2000006Frame · dentedDURING HEAVY MAINTENANCE INSPECTION, FOUND FORWARD CARGO COMPARTMENT BS 550B FRAME DENTED BETWEEN STR 23L AND STR 24L.. REASON FOR THIS DAMAGE WAS UNKNOWN. (X)SDR EE4Y2000004Cargo Track · corrodedDURING HEAVY MAINTENANCE INSPECTION, FOUND TIE DOWN SUPPORT BASE AND STRAP CORRODED IN FORWARD CARGO COMPARTMENT AT BS 440 AND BS 460, BETWEEN STR 20L AND STR 25L.. REASON FOR THIS DAMAGE WAS UNKNOWN. (X)
Other aircraft with N621AC · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N621AC is registered now to the first aircraft listed.