Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CNMA20110032Drive Assy · shearedA/P OUT OF TRIM LT CAME ON INTERMITTENTLY DURING FLT. STAYED ON FOR 30 SEC TO 3 MTS. NO PITCH TRIM CHANGE DURING ILLUMINATION. TURNED OFF AP & ACFT IN TRIM DURING DESCENT. ACFT DECENDED THROUGH SET ALT TURNED OFF AP & NOTICED ACFT WAS VERY OUT OF TRIM, INSDR CNMA20110029Oven · burnedAFT GALLEY OVEN FIRE. INSIDE OF 2-21. FOLLOWED QRH PROCEDURES. CONTINUED (ALL OVENS NEED TO BE CLEANED) R & R OVEN IAW 25-30 CLEANED ALL OTHER OVENS. NO EXCESS DRIPPINGS OR CRUMBS.SDR CNMA20110002Engine · failedNR 2 ENG SHUTDOWN DURING CLIMB ACCOMPLISHED QRH PROCEDURE. REPLACED NR 2 ENGINE PER CARD 10UN-201 OPS CHECK NORMAL LEAK CHECKED OK POWER ASSURANCE OK.SDR CNMA20100009Support · brokenFLOOR PANEL CHANNEL SUPPORT IS BROKEN BS 1997 LBL 65. DAMAGED FLOOR SUPPORT REMOVED AND NEW FABRICATED P/N OAI-53-0002 PER SRM VOL 3 53-16-01 FIG 10B ITEM 29 AND OMNI GMM 4.45. INSTALLED WITH RIVETS PER SRM VOL 2 51-35-01 PAGE 1.SDR CNMA20100008Floor Support · corrodedCORROSION ON TEE CITO AFT BODY PRESSURE BULKHEAD AND FLOOR PANEL SUPPORT BS 2007 RBL 18-25. DAMAGED AREA TRIMMED OUT AND REINFORCED AREA WITH SPLICE ANGLE AND CHANNEL P/N N531AX-N514-1/-2 PER SRM VOL 1 53-40-00 FIG 16 AND INSTALLED WITH FASTENERS PER SRM VOL SDR CNMA20100007Support · corrodedCORROSION ON FLOOR PANEL CHANNEL SUPPORT BS 1997 - 2007 RBL 20. DAMAGED FLOOR SUPPORT REMOVED AND NEW FABRICATED P/N: OAI-53-0006 PER SRM VOL 3 53-16-01 FIG 10B ITEM 20 AND OMNI GMM 445 INSTALLED WITH FASTENERS PER SRM VOL 2 51-38-01 PAGE 1.SDR CNMA20100006Floor Support · corrodedCORROSION ON TEE CITO AFT BODY PRESSURE BULKHEAD AND FLOOR PANEL SUPPORT BS 2007 LBL 55. DAMAGED AREA TRIMMED OUT AND REINFORCED AREA WITH SPLICE ANGLE & CHANNEL PLATE & STRAP P/N: N531AX-NRC515-1/-2/-3/-4 PER SRM VOL 1 53-40-00 FIG 1G & SRM VOL 1 53-70-00 FISDR CNM2008F00001Engine · overheatedDURING CLIMB THRU 15000 FT N2 103.4 TAT +20 NACELLE TEMP WAS 240 DEGREE C PREV SUPPLY SELECTED OFF AXCELL TEMP DECREASED 10 DEGREES C STILL 40 DEGREE C ABOVE QRH CHARTED VALVE (NR 1 ENG). (K)