Source: https://www.federalregister.gov/documents/2008/10/22/E8-25048/airworthiness-directives-boeing-model-737-100--200--200c--300--400-and--500-series-airplanes
Timestamp: 2018-04-22 15:07:08
Document Index: 385836824

Matched Legal Cases: ['art 1', 'art 2', 'art 1', 'art 2', 'art 1', 'art 1', 'art 2', 'art 3', 'art 3', 'art 1', 'art 1', 'art 2']

We must receive comments on this proposed AD by December 8, 2008.
Deactivation or Modification of the Outboard Landing Lights
https://www.federalregister.gov/d/E8-25048 https://www.federalregister.gov/d/E8-25048
We propose to adopt a new airworthiness directive (AD) for certain Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. For certain airplanes, this proposed AD would require deactivation or modification of the wiring to the outboard landing lights, until the wire bundles and electrical connectors have been replaced. For all airplanes, this proposed AD would also require an inspection for any broken, damaged, or missing fairleads, grommets, and wires in the four electrical junction boxes of the main wheel well, and corrective actions if necessary. For certain airplanes, this proposed AD would also require replacement of certain wire bundles for the landing lights and fuel shutoff valves, and related investigative, other specified, and corrective actions if necessary. For certain airplanes, this proposed AD would also require replacement of certain electrical connectors and backshell clamps. This proposed AD results from reports of uncommanded engine shutdowns and burned and damaged wire bundles associated with the outboard landing lights and engine fuel shutoff valves. This proposed AD also results from reports of damaged and missing grommets and broken and damaged fairleads in the electrical junction boxes of the main wheel well. We are proposing this AD to prevent a hot short between the outboard landing light and fuel shutoff valve circuits, which could result in an uncommanded engine shutdown. We are also proposing this AD to prevent corrosion of the electrical connectors of the wing rear spars, which could result in short circuits and consequent incorrect functioning of airplane systems needed for safe flight and landing.
You may send comments by any of the following methods:Start Printed Page 62938
We invite you to send any written relevant data, views, or arguments about this proposed AD. Send your comments to an address listed under the ADDRESSES section. Include “Docket No. FAA-2008-1116; Directorate Identifier 2007-NM-231-AD” at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this proposed AD. We will consider all comments received by the closing date and may amend this proposed AD because of those comments.
We have received reports of uncommanded engine shutdowns and burned and damaged wire bundles where the wire bundle exits the main wheel well in the area of the wing rear spar on Boeing Model 737-300, -400, and -500 series airplanes. Investigation revealed that the uncommanded engine shutdowns were caused by uncommanded closure of the engine fuel shutoff valves, which resulted from short circuits between the 115 volt alternating current (VAC) circuits of the outboard landing lights and the 28 volt direct current (VDC) circuits of the engine fuel shutoff valves. This short circuit causes the valve to move towards the closed position. Failure of the valve occurs shortly after reaching the closed position due to exposure of the 28-VDC valve to 115-VAC power from the outboard landing light circuit. The loss of ability to reopen the valve prevents restarting the engine due to the unavailability of fuel. Uncommanded closure of the fuel shutoff valve due to a hot short between the outboard landing light and the fuel shutoff valve circuits, if not corrected, could result in an uncommanded engine shutdown.
Subsequently, Boeing published Boeing Service Bulletin 737-28-1241, dated April 7, 2006, to provide instructions for replacing certain wire bundles with new, re-designed wire bundles to prevent short circuits between the outboard landing light and engine fuel shutoff valve circuits. After issuing that service bulletin, Boeing discovered that some of the replacement wire bundles were inadvertently assembled and delivered with electrical connectors and backshells having a cadmium-plated finish instead of an anodized aluminum finish. The electrical connectors and backshells are located on the rear spar of the left and right wings. The cadmium-plated connectors and backshells corrode quickly when exposed to potassium-based de-icing fluids. This corrosion leads to moisture ingress into the electrical connectors and subsequent corrosion of the electrical contacts within the electrical connectors. This condition, if not corrected, could result in short circuits and consequent incorrect functioning of airplane systems needed for safe flight and landing.
We have also received reports of damaged and missing grommets and broken and damaged fairleads in the electrical junction boxes of the main wheel well on Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. Although there is no evidence that these wiring discrepancies have contributed to uncommanded engine shutdowns, the wiring in this area includes the wire bundles for the engine fuel shutoff valves, as well as wiring for other systems needed for continued safe flight and landing of the airplane.
We have reviewed Boeing Alert Service Bulletin 737-33A1140, dated May 22, 2006, for Model 737-300, -400, and -500 series airplanes. The service bulletin specifies accomplishing the actions in either Part 1 or Part 2 of the Accomplishment Instructions. Part 1 describes procedures for deactivating the outboard landing lights. The deactivation includes installing collars and “do not close” tags on the circuit breakers for the outboard landing lights, and capping and stowing the wires from the circuit breakers. Part 2 describes procedures for modifying the wiring to the outboard landing lights. The modification includes capping and stowing the existing wires to the outboard landing lights, and routing new wires to the outboard landing lights.
We have also reviewed Boeing Service Bulletin 737-28-1241, Revision 1, dated August 31, 2007, for Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. Part 1 of the Accomplishment Instructions of the service bulletin applies to certain Model 737-300, -400, and -500 series airplanes. Part 1 describes procedures for replacing certain wire bundles for the landing lights and fuel shutoff valves with new, re-designed wire bundles, and doing related investigative, other specified, and corrective actions if necessary. The related investigative actions include (1) doing a detailed inspection for any broken, damaged, or missing grommet where the wire bundles go from the wheel well to the wing and (2) doing a detailed inspection for any broken, damaged, or missing fairleads, any damaged or missing grommets, and any chafed or damaged wires or wire bundles in the electrical junction boxes of the main wheel well. The other specified actions include (1) removing any additional outboard landing light wires from the wire bundles installed in accordance with Boeing Alert Service Bulletin 737-33A1140 and (2) terminating the outboard landing lights at the circuit breakers, as necessary. The corrective actions include (1) replacing any broken, damaged, or missing fairlead with a new fairlead, (2) replacing any damaged or missing grommet with a new grommet, and (3) repairing or Start Printed Page 62939replacing any chafed or damaged wires and wire bundles with new wires and wire bundles.
Part 2 of the Accomplishment Instructions of Boeing Service Bulletin 737-28-1241 describes procedures for doing a detailed inspection for any broken, damaged, or missing fairleads, any damaged or missing grommets, and any chafed or damaged wires or wire bundles in the four electrical junction boxes of the main wheel well, and doing the corrective actions as necessary.
Part 3 of the Accomplishment Instructions of Boeing Service Bulletin 737-28-1241 applies to certain Model 737-300, -400, and -500 series airplanes on which the wire bundle replacement was done in accordance with the original issue of the service bulletin, dated April 7, 2006. Part 3 describes procedures for replacing certain electrical connectors and backshell clamps with new, improved electrical connectors and backshell clamps.
Accomplishing the applicable actions specified in Boeing Service Bulletin 737-28-1241 would end the need for accomplishing the deactivation or modification specified in Boeing Alert Service Bulletin 737-33A1140.
Boeing Alert Service Bulletin 737-33A1140 and Boeing Service Bulletin 737-28-1241 specify prior or concurrent accomplishment of Boeing Special Attention Service Bulletin 737-28-1196, dated December 5, 2002; Revision 1, dated March 13, 2003; Revision 2, dated August 21, 2003; or Revision 3, dated April 1, 2004. Boeing Special Attention Service Bulletin 737-28-1196 describes procedures for changing the wire connections for the engine fuel shutoff valves and the outboard landing lights.
For Model 737-300, -400, and -500 series airplanes, deactivation or modification of the wiring to the outboard landing lights, until the wire bundles and electrical connectors have been replaced.
For all airplanes, a detailed inspection for any broken, damaged, or missing fairleads, any damaged or missing grommets, and any chafed or damaged wires or wire bundles in the four electrical junction boxes of the main wheel well, and corrective actions if necessary.
For certain airplanes, replacement of certain wire bundles for the landing lights and fuel shutoff valves with new, re-designed wire bundles, and related investigative, other specified, and corrective actions if necessary.
For certain airplanes, replacement of certain electrical connectors and backshell clamps with new, improved electrical connectors and backshell clamps.
Although Boeing Service Bulletin 737-28-1241 and Boeing Alert Service Bulletin 737-33A1140 specify prior or concurrent accomplishment of Boeing Special Attention Service Bulletin 737-28-1196, this proposed AD would not require that action. The accomplishment of Boeing Special Attention Service Bulletin 737-28-1196 is already required by AD 2005-10-11, amendment 39-14088 (70 FR 28419, May 18, 2005).
We estimate that the actions specified in Boeing Alert Service Bulletin 737-33A1140 would affect about 511 Model 737-300, -400, and -500 series airplanes of U.S. registry. Operators may accomplish either the deactivation or modification.
We estimate that the deactivation would take about 1 work-hour per product to comply with this proposed AD. The average labor rate is $80 per work-hour. Based on these figures, we estimate the cost of the deactivation to the U.S. operators to be $40,880, or $80 per product.
We estimate that the modification would take about 31 work-hours per product to comply with this proposed AD. The average labor rate is $80 per work-hour. Required parts for the modification would cost about $573 per product. Based on these figures, we estimate the cost of modification to the U.S. operators to be $1,560,083, or $3,053 per product.
We estimate that the actions specified in Boeing Alert Service Bulletin 737-28-1241 would affect up to 891 Model 737-100, -200, -200C, -300, -400, and -500 series airplanes of U.S. registry. The following table provides the estimated costs, at an average labor rate of $80 per work-hour, for U.S. operators to comply with the actions specified in that service bulletin.
We determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would not have a substantial direct effect on the States, on the relationship between the national Government and the States, or on the distribution of power and responsibilities among the various levels of government.Start Printed Page 62940
Boeing: Docket No. FAA-2008-1116; Directorate Identifier 2007-NM-231-AD.
(a) We must receive comments by December 8, 2008.
(f) For Model 737-300, -400, and -500 series airplanes identified in Boeing Alert Service Bulletin 737-33A1140, dated May 22, 2006 (“the alert service bulletin”): Within 180 days after the effective date of this AD, accomplish the actions specified in either paragraph (f)(1) or (f)(2) of this AD. Accomplishing the applicable actions required by paragraph (g) of this AD terminates the requirements of this paragraph.
(1) Deactivate the outboard landing lights, by accomplishing all of the actions specified in Part 1 of the Accomplishment Instructions of the alert service bulletin.
The Master Minimum Equipment List (MMEL) prohibits dispatching an airplane for night operations with deactivated outboard landing lights in the event that either of the inboard landing lights fail. Operators should note that, if the outboard landing lights are deactivated in accordance with Part 1 of the service bulletin, there is no MMEL relief allowing for this configuration for night operations should any inboard landing light fail.
(2) Modify the wiring to the outboard landing lights, by accomplishing all of the actions specified in Part 2 of the Accomplishment Instructions of the alert service bulletin.
(1) Replace the wire bundles for the landing lights and fuel shutoff valves with new, re-designed wire bundles, and do the related investigative, other specified, and corrective actions, as applicable. The related investigative, other specified, and corrective actions must be done before further flight after the replacement.
[FR Doc. E8-25048 Filed 10-21-08; 8:45 am]