A CRJ200; IN DSCNT; DECLARED AN EMER AND SHUT DOWN THE R ENG DUE TO REVERSER UNLOCK LIGHT; SINGLE CHIME; AND REV ICON IN R ENG N1 DISPLAY.

2006-03 · NASA ASRS report 692390

Date: 2006-03 · Aircraft: Regional Jet 200 ER/LR (CRJ200) · Phase: approach

Anomalies: aircraft-equipment-problem-critical

Synopsis

A CRJ200; IN DSCNT; DECLARED AN EMER AND SHUT DOWN THE R ENG DUE TO REVERSER UNLOCK LIGHT; SINGLE CHIME; AND REV ICON IN R ENG N1 DISPLAY.

Narrative

I WAS THE PF FROM ZZZ TO ZZZ1. WE WERE DSNDING OUT OF APPROX FL250 TO 12000 FT IN VMC CONDITIONS WITH ZZZ1 ARPT IN SIGHT; WITH THE AUTOPLT ENGAGED; THE POWER LEVERS AT FLIGHT IDLE THRUST; AND THE THRUST REVERSER ARM SWITCHES IN THE DISARMED/OFF POSITION; WHEN THE EICAS DISPLAYED AN AMBER 'R REV UNLOCKED' MESSAGE; A SINGLE CHIME AND AN AMBER 'REV' ICON ON THE R ENG N1 DISPLAY. THE CAPT REACHED FOR THE QRH AND I BEGAN TO SLOW THE ACFT FROM APPROX 300 KTS TO 250 KTS BY ARRESTING OUR VERT DSCNT FROM 2500 FPM TO 500 FPM. I INFORMED ATC THAT WE WERE WORKING A PROBLEM AND THAT WE COULD NO LONGER MAKE THE ASSIGNED SPD AND XING RESTRICTION PREVIOUSLY GIVEN. CTR REQUESTED TO KEEP HIM ADVISED IF WE NEEDED ASSISTANCE. THE CAPT BEGAN TO READ OUT THE IMMEDIATE ACTION ITEMS PER THE QRH SUCH AS 'AFFECTED THRUST LEVER CONFIRM AT IDLE' (FLT IDLE WAS THE POSITION THAT BOTH THRUST LEVERS WERE ALREADY AT); THE QRH THEN DIRECTS THE PLT TO PROCEED TO THE EMER PROCS SECTION AND 'AFFECTED THRUST REVERSER EMER STOW;' THEN THE CAPT DEPRESSED THE EMER STOW SWITCH. THE QRH THEN ASKS 'AFFECTED THRUST REVERSER IS STOWED (STOW INDICATED BY IMPROVED AIRPLANE HANDLING AND NORMAL OPERATION OF AFFECTED THRUST LEVER). I STATED TO THE CAPT THAT I SAW NO ADVERSE YAW OR FELT ANY TYPE OF ABNORMAL ACFT BUFFET. SINCE WE DID NOT SEE A CHANGE TO THE EICAS OR THE AMBER 'REV' ICON ON THE N1 GAUGE; THE CAPT PROCEEDED TO THE 'NO' SECTION. THE QRH CALLED FOR THE 'AIRSPD NOT MORE THAN 200 KTS;' I ADVISED ATC AND CONTINUED TO SLOW THE ACFT IN A GRADUAL DSCNT OF LESS THAN 500 FPM TO OUR ASSIGNED ALT OF 12000 FT. THE QRH CALLED FOR 'AFFECTED THRUST REVERSER OFF/DO NOT ARM' (WHICH WAS THE POSITION OF BOTH THRUST REVERSER SWITCHES PRIOR TO THE BEGINNING OF THE PROB). THE QRH CONTINUED 'APU START' AND 'APU GEN ON' WHICH THE CAPT COMPLETED. THE QRH THEN STATED 'SINGLE ENG PROCS ACCOMPLISH;' AT THIS POINT THE CAPT PAUSED AND STATED THAT HE DID NOT WANT TO SHUT THE ENG DOWN. I AGREED AND I EXPRESSED THAT IT WAS NOT MY DESIRE TO NEEDLESSLY SHUT THE ENG DOWN. I SUGGESTED THAT WE CALL MAINT CTL AS I HAD DONE AT OTHER ACRS I HAD WORKED FOR; HE FELT THAT WE DID NOT HAVE TIME FOR THAT COURSE AND I DID NOT PRESS THE ISSUE SINCE I WAS BUSY MONITORING THE RADIO AND THE AUTOPLT. THE CAPT BEGAN TO READ THE QRH AGAIN TO VERIFY THAT THERE WASN'T SOMETHING HE HAD MISSED IN THE PROCESS. WHEN HE GOT TO THE STATEMENT; 'AFFECTED THRUST REVERSER IS STOWED (STOW INDICATED BY IMPROVED AIRPLANE HANDLING AND NORMAL OPERATION OF AFFECTED THRUST LEVER) HE READ IT TWICE AND STATED THAT HE DID NOT SEE HOW THE THRUST REVERSER WAS IN NORMAL OPERATION NOW. I AGREE THAT I DID NOT SEE HOW THE THRUST REVERSER WAS NORMAL SINCE WE STILL HAD AN AMBER 'REV' ICON AND AN AMBER 'R REV UNLOCKED.' STILL AT THIS POINT THE THRUST LEVERS WERE AT IDLE AND WE WERE IN A SLOW SPD DSCNT TO 12000 FT. AGAIN THE CAPT STATED THAT HE DID NOT WANT TO SHUT DOWN THE ENG BUT HE FELT THE QRH WAS ONLY LEADING US TO THAT COURSE OF ACTION. THE CAPT WAS NOT SURE WHAT THE PROB EXACTLY WAS. WAS THE PROB REALLY GOING TO GET WORSE AT A LOW ALT IF WE DID NOT SHUT THE ENG DOWN? WAS THE THRUST REVERSER REALLY DEPLOYED OR NOT; OR WAS THIS JUST AN INDICATION PROB? THE CAPT FELT THAT SHUTTING THE ENG DOWN WAS THE SAFEST COURSE OF ACTION GIVEN THE FACT THAT NOTHING HAD CHANGED AND WE DID NOT REALLY KNOW THE TRUE NATURE OF THE PROB. ZZZ1 HAD VMC CONDITIONS; WE WERE CLR OF ALL TERRAIN AND HAD THE ARPT IN SIGHT. WE BOTH FELT AT THE TIME THAT THE CHKLIST WAS AMBIGUOUS AT BEST AND THAT THE CHKLIST DID NOT ADDRESS THIS TYPE OF SITUATION EXPRESSLY. OUR TRAINING ON THE ACFT FOR A L OR R REV UNLOCKED MESSAGE WAS FAR DIFFERENT FROM THIS. IN TRAINING WE WERE GIVEN A TKOF SCENARIO IN WHICH THE PROB OCCURRED AT A LOW ALT AND THE ACFT BUFFETED VIOLENTLY UNTIL THE EMER STOW WAS PUSHED AND THE BUFFETING WENT AWAY; OR IF THE BUFFETING CONTINUED; THE ENG WAS SHUT DOWN AS PER THE QRH. IN EITHER CASE; ONE WAS SATISFIED THAT THE SITUATION WAS UNDER CTL ONCE THE QRH WAS COMPLETED.IN OUR SITUATION; NEITHER THE CAPT OR MYSELF COULD STATE WITH CERTAINTY THAT THE R THRUST REVERSER WAS CONTAINED TO A SAFE AND LOCKED POSITION AND THAT AT SOME POINT ON APCH AND LNDG IT COULD DEPLOY FURTHER; CAUSING LOSS OF DIRECTIONAL CTL. THEREFORE; THE CAPT DECIDED TO SHUT THE ENG DOWN AND PERFORM THE SINGLE ENG PROCS QRH. WE RAN THE SINGLE ENG PROCS QRH; I DECLARED AN EMER TO ATC; THE AUTOPLT DISENGAGED WITH A LOSS OF THE R GENERATOR. I TRANSFERRED THE AUTOPLT TO CAPT'S SIDE AND I STATED THAT IT MADE MORE SENSE FOR HIM TO TAKE THE CTLS AND FOR ME TO COMPLETE THE QRH; WHICH WE DID. WE COMPLETED ALL PERTINENT CHKLISTS. I INFORMED THE FLT ATTENDANT AND I MADE A PA ANNOUNCEMENT TO THE PAX THAT WE HAD SHUT DOWN THE R ENG FOR PRECAUTIONARY REASONS AND WE WERE ABOUT 7 MINUTES FROM LNDG AT ZZZ1; WE WOULD NOT HAVE TO EVACUATE THE ACFT OR BRACE FOR AN EMER; BUT WE WOULD MAKE A NORMAL LNDG. I THEN ADVISED COMPANY ON OPS FREQ. THE CAPT LANDED THE ACFT AT ZZZ1 WITHOUT INCIDENT AND WE CLRED THE RWY AND TAXIED NORMALLY TO THE TERMINAL WHERE THE PAX DEPLANED AS NORMAL. AFTER ALL PAX HAD DEPLANED; MAINT CAME ABOARD THE ACFT AND INFORMED US THE R THRUST REVERSER TRANSLATING COWL WAS OPEN APPROX ONE INCH. IT IS MY PERSONAL OPINION THAT QRH SHOULD BE RE-WRITTEN TO STATE THAT AFTER DEPRESSING THE EMER STOW BUTTON AND IN ANY CASE THAT THE AMBER 'REV' ICON AND THE AMBER 'R REV UNLOCKED' WILL OR WILL NOT REMAIN ON THE EICAS. THIS WOULD GIVE THE CREW A BETTER UNDERSTANDING IF THE EMER STOW SWITCH HAS FAILED OR OPERATED CORRECTLY IN A FLT IDLE DSCNT SITUATION.CALLBACK CONVERSATION WITH RPTR REVEALED THE FOLLOWING INFO: THE RPTR STATED THEY HAD ALL THE INDICATIONS THE REVERSER WAS DEPLOYED WITH THE EICAS 'R REVERSER UNLOCK' MESSAGE; THE SINGLE CHIME AND THE REV ICON IN THE R ENG N1 DISPLAY. THE EMER STOW SWITCH WAS ACTIVATED AND DID NOT CHANGE THE REVERSER INDICATIONS AND THE AIRPLANE FLEW THE SAME AS BEFORE THE SWITCH WAS ACTIVATED. THE ONLY THING MISSING WAS THE BUFFETING THE QRH DESCRIBED. THE DECISION WAS MADE TO FOLLOW THE BOOK AND SHUT DOWN THE ENG AND DECLARE AN EMER. A LATER MEETING WITH THE CHIEF PLT ABOUT THE INCIDENT REVEALED MAINT FOUND THE REVERSER OUT OF RIG.

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

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