AN EMBRAER 145 IN CLB AT FL210 EXPERIENCED A SLOW INTERMITTENT LOSS OF CABIN PRESSURE CAUSED BY A DEFECTIVE ELECTRICAL CONNECTOR ON THE AUTOPRESSURE CONTROLLER.

Date: 1999-11 · Aircraft: Bandeirant Undifferentiated or Other Model · Phase: climb

Anomalies: aircraft-equipment-problem-critical

Synopsis

AN EMBRAER 145 IN CLB AT FL210 EXPERIENCED A SLOW INTERMITTENT LOSS OF CABIN PRESSURE CAUSED BY A DEFECTIVE ELECTRICAL CONNECTOR ON THE AUTOPRESSURE CONTROLLER.

Narrative

CLBING THROUGH FL210; WE RECEIVED A WARNING OF AN AUTOPRESSURIZATION FAILURE AND DISCOVERED THAT THE CABIN ALT WAS 10000 FT. THE CAPT CALLED FOR THE EMER PROC CHKLIST; BUT THE CHKLIST DID NOT ADDRESS THIS EVENT. ATC WAS ADVISED THAT WE NEEDED AN IMMEDIATE DSCNT TO BELOW 10000 FT; AND AFTER A 40 DEG R TURN FOR TFC BELOW; WE WERE CLRED TO 9000 FT. THE CABIN ALT CONTINUED TO CLB AT A SLOW; PROGRESSIVE RATE; BUT NOT A CONSISTENT RATE. I FOLLOWED THE APPROPRIATE CHKLIST IN OUR COMPANY'S AOM IN AN ATTEMPT TO CTL THE CABIN PRESSURE MANUALLY. THE CAPT MADE A CTLED DSCNT ON AUTOPLT AT INITIALLY 3000 FPM AND REDUCED THE DSCNT TO 2500 FPM. WE COMPLETED THE CHKLIST JUST PRIOR TO LEVELING OFF AND INFORMED THE FLT ATTENDANT OF WHAT HAD OCCURRED. SHE INFORMED US THAT THE OXYGEN MASKS HAD DEPLOYED AND THE PAX WERE USING THEM. WE CONTACTED OUR COMPANY AND ADVISED WE WOULD RETURN TO DFW. OTHER THAN A SHALLOW DSCNT; WE MADE A NORMAL APCH AND LNDG. THE CAPT; AND I AGREE; DID NOT CONSIDER IT NECESSARY TO EFFECT AN EMER DSCNT OR A FULL RAPID DECOMPRESSION PROC BECAUSE WE DID NOT HAVE A RAPID DECOMPRESSION. WE ALSO DID NOT PUT ON OUR OWN OXYGEN MASKS BECAUSE THE CABIN ALT DID NOT CLB OVER 13000 FT AND WE WERE ALREADY DSNDING. HAD THE CABIN ALT CLBED DRAMATICALLY OR ATC NOT ALLOW US TO DSND; WE WOULD HAVE DECLARED AN EMER AND CALLED FOR OXYGEN MASKS. I FEEL THAT THE CAPT WAS IN FULL CTL OF THE SIT AND AT NO TIME WAS THE CREW; PAX; OR ACFT IN JEOPARDY. CALLBACK CONVERSATION WITH RPTR REVEALED THE FOLLOWING INFO: THE RPTR STATED THE ACFT WAS AN EMBRAER 145 AND THE DECOMPRESSION WAS CAUSED BY A DEFECTIVE ELECTRICAL CONNECTOR ON THE AUTOPRESSURE CONTROLLER. THE RPTR SAID THE FAILURE MADE THE PRESSURIZATION SYS OPERATE INTERMITTENTLY RELEASING THE CABIN PRESSURE GRADUALLY. THE RPTR SAID THE CREW OXYGEN MASKS WERE NOT USED AS THE PRESSURE WAS NOT A RAPID LOSS.

Source: NASA Aviation Safety Reporting System (public domain). Reports are voluntary submissions and are not verified by NASA.