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|
Attributes | |
ACN | 261150 |
Time | |
Date | 199401 |
Day | Sat |
Local Time Of Day | 1801 To 2400 |
Place | |
Locale Reference | airport : bwi |
State Reference | MD |
Altitude | msl bound lower : 1500 msl bound upper : 3000 |
Environment | |
Flight Conditions | VMC |
Light | Night |
Aircraft 1 | |
Controlling Facilities | tracon : bwi tower : bwi |
Operator | common carrier : air carrier |
Make Model Name | DC-9 Undifferentiated or Other Model |
Operating Under FAR Part | Part 121 |
Flight Phase | descent : approach landing : go around other |
Route In Use | enroute : on vectors |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : flight engineer pilot : atp |
Experience | flight time last 90 days : 140 flight time total : 6000 flight time type : 500 |
ASRS Report | 261150 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : atp |
Events | |
Anomaly | aircraft equipment problem : critical |
Independent Detector | other flight crewa |
Resolutory Action | flight crew : declared emergency flight crew : overcame equipment problem other |
Consequence | Other |
Supplementary | |
Primary Problem | Aircraft |
Narrative:
Upon lowering of landing gear at OM the green nose gear down and lock light did not illuminate. The captain initiated a missed approach. I attempted to change the 2 bulbs but was unsuccessful due to its position in the socket and the low altitude turbulence encountered. There is no push to test function on a DC9 model aircraft. The captain ordered me to accomplish the appropriate checklist, I went off frequency and did a visual inspection of the nose down lock and confirmed it appeared down. We accomplished a fly by and the tower confirmed the gear appeared down. Tower instructed us to climb straight ahead but due to our fuel situation captain had me tell them we will make a tight left turn and make the approach. We switched to approach for vectors back to the ILS. We had the emergency equipment stand by and briefed the cabin for a possible emergency landing. As we landed and the nose touched down, 1 of the 2 down and lock lights illuminated, on the taxi in they both illuminated. Corrective actions: push to test function should be installed. Human factors: I firmly believe a 2-MAN crew is pushing the limit on this situation especially in turbulence and a low fuel state brought about by the company's trying to save cost and dispatching with minimum fuel. But I also feel our company as the best emergency training available. Callback conversation with reporter revealed the following information: reporter revealed that the problem of changing the nose gear bulbs (2) was exacerbated by the turbulence. He had pulled the cover off the bulbs and even had a pair of pliers to facilitate the removal but due to the turbulence, got shocked twice in the ensuing attempts. The visual inspection of the nose gear and the determination of being 'over center' was difficult at best and was covered within the air carrier safety review of the incident the next day. The post-flight inspection failed to find a switch problem. The changing of the light bulbs seemed to fix the problem. Flight landed with 40 mins of fuel, about 3000 pounds which the first officer did not think was too much. He doesn't appreciate the fuel saving procedures that acrs follow.
Original NASA ASRS Text
Title: GAR INITIATED AFTER DC-9 CREW NOTED THAT THERE WAS NOT A GEAR DOWN INDICATION FOR THE NOSE GEAR. NIGHT OP.
Narrative: UPON LOWERING OF LNDG GEAR AT OM THE GREEN NOSE GEAR DOWN AND LOCK LIGHT DID NOT ILLUMINATE. THE CAPT INITIATED A MISSED APCH. I ATTEMPTED TO CHANGE THE 2 BULBS BUT WAS UNSUCCESSFUL DUE TO ITS POS IN THE SOCKET AND THE LOW ALT TURB ENCOUNTERED. THERE IS NO PUSH TO TEST FUNCTION ON A DC9 MODEL ACFT. THE CAPT ORDERED ME TO ACCOMPLISH THE APPROPRIATE CHKLIST, I WENT OFF FREQ AND DID A VISUAL INSPECTION OF THE NOSE DOWN LOCK AND CONFIRMED IT APPEARED DOWN. WE ACCOMPLISHED A FLY BY AND THE TWR CONFIRMED THE GEAR APPEARED DOWN. TWR INSTRUCTED US TO CLB STRAIGHT AHEAD BUT DUE TO OUR FUEL SIT CAPT HAD ME TELL THEM WE WILL MAKE A TIGHT L TURN AND MAKE THE APCH. WE SWITCHED TO APCH FOR VECTORS BACK TO THE ILS. WE HAD THE EMER EQUIP STAND BY AND BRIEFED THE CABIN FOR A POSSIBLE EMER LNDG. AS WE LANDED AND THE NOSE TOUCHED DOWN, 1 OF THE 2 DOWN AND LOCK LIGHTS ILLUMINATED, ON THE TAXI IN THEY BOTH ILLUMINATED. CORRECTIVE ACTIONS: PUSH TO TEST FUNCTION SHOULD BE INSTALLED. HUMAN FACTORS: I FIRMLY BELIEVE A 2-MAN CREW IS PUSHING THE LIMIT ON THIS SIT ESPECIALLY IN TURB AND A LOW FUEL STATE BROUGHT ABOUT BY THE COMPANY'S TRYING TO SAVE COST AND DISPATCHING WITH MINIMUM FUEL. BUT I ALSO FEEL OUR COMPANY AS THE BEST EMER TRAINING AVAILABLE. CALLBACK CONVERSATION WITH RPTR REVEALED THE FOLLOWING INFO: RPTR REVEALED THAT THE PROB OF CHANGING THE NOSE GEAR BULBS (2) WAS EXACERBATED BY THE TURB. HE HAD PULLED THE COVER OFF THE BULBS AND EVEN HAD A PAIR OF PLIERS TO FACILITATE THE REMOVAL BUT DUE TO THE TURB, GOT SHOCKED TWICE IN THE ENSUING ATTEMPTS. THE VISUAL INSPECTION OF THE NOSE GEAR AND THE DETERMINATION OF BEING 'OVER CTR' WAS DIFFICULT AT BEST AND WAS COVERED WITHIN THE ACR SAFETY REVIEW OF THE INCIDENT THE NEXT DAY. THE POST-FLT INSPECTION FAILED TO FIND A SWITCH PROB. THE CHANGING OF THE LIGHT BULBS SEEMED TO FIX THE PROB. FLT LANDED WITH 40 MINS OF FUEL, ABOUT 3000 LBS WHICH THE FO DID NOT THINK WAS TOO MUCH. HE DOESN'T APPRECIATE THE FUEL SAVING PROCS THAT ACRS FOLLOW.
Data retrieved from NASA's ASRS site as of July 2007 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.