航空 发表于 2011-4-23 10:39:30

CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure

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航空 发表于 2011-4-23 10:39:37

Page 1 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>1- Background<BR> On June, 21, 2002, SWA CFM56-7B ESN 874265 experienced a commanded IFSD after the oil filter<BR>bypass light illuminated in flight.<BR> Ground investigation revealed metal debris in the AGB/TGB MCD.<BR> During further removal of the AGB, it was found :<BR> liberation of key locks coming from the 3 studs that secure the roller bearing outer race to AGB<BR>housing,<BR> wear-ovalization of the AGB housing at the 3 threaded holes receiving the 3 studs,<BR> good condition of the 3 studs remained attached with the roller bearing outer race,<BR> excessive radial play on all five AGB mounts links,<BR> residual AGB alignment condition (dim. &laquo; A &raquo; - dim. &laquo; B &raquo;) checked at 0.051’ (1,29mm) vs. .002’<BR>(0,05mm) required,<BR> good condition of horizontal drive shaft splines (no visual wear).<BR>2- Engine and AGB history<BR> CFM56-7B22 ESN 874265 delivered in July 1998 installed on #2 on Boeing 737-700 N7183W.<BR> One maintenance action reported on AGB since EIS related to HMU replacement (line 6) made in july<BR>1999 without any connection with failed line 3 roller bearing.<BR> Engine &amp; AGB TSN/CSN = 14804/9478 and 14268/9112 since HMU replacement.<BR> AGB quality inquiry revealed one minor deviation : 6 tooth dim. of line 3 gearshaft check -4μm under mini.<BR>limit (42,765 vs. 42,769 to 42,823 required) ; accepted thru departure record DN 15H06030A.<BR>Page 2 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>3- Part identification (see charts 9 &amp; 20)<BR> AGB P/N 340-046-503-0 S/N WQ 1193<BR> Damaged control alternator made of :<BR> Stator P/N 9387M17P09 S/N HTL 10296<BR> Rotor P/N 9387M16P02 S/N HTLR 4329<BR> Gearshaft line 3 P/N 340-051-801-0 S/N UN 00225 equipped with :<BR> Failed roller bearing P/N 301-480-926-0 S/N UR 29717<BR> Ball bearing P/N 305-115-306-0 S/N UR 29633<BR> Ball bearing housing P/N 335-301-000-0<BR> Starter pad assy P/N 340-047-802-0 equipped with :<BR> gearshaft line 4 P/N 340-051-901-0 S/N UN 07643<BR> Fuel pump – HMU pad assy equipped with :<BR> Gearshaft line 5 P/N 340-055-202-0 S/N UR 00454<BR> Gearshaft line 6 P/N 335-302-902-0 S/N UN 21379<BR> Gearshaft line 7 P/N 335-303-002-0 S/N U 28596<BR> AGB links returned for wear on spherical bearings :<BR> Adjustable turnbuckle link P/N 340-029-501-0 equipped with 2 links P/N 340-103-701 / 801<BR> Rear links (x2) P/N 340-029-401-0<BR> Upper link P/N 340-032-801-0<BR>Page 3 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>4- Findings<BR>4-1 Parts as received (see chart 9)<BR> All the 5 gearshafts from lines 3 to 7 and associated pads were reinstalled on AGB housing.<BR> Control alternator stator &amp; rotor were received removed and badly worn by rotor sectorial interference (90°).<BR> On the alternator rotor the wear is limited to one sector compare to the stator that is affected on 360°.<BR>4-2 After AGB disassy (see charts 10 &amp; 11)<BR> Line 3 (control alternator) roller bearing outer race found totally loose due to hole elongation of the 3 securing<BR>studs that machined the AGB housing over 10mm long in gearshaft rotation opposite direction.<BR> As a consequence of the roller bearing outer race looseness, respective centering diameters of both outer race<BR>and AGB housing hole were affected by superficial fretting – wear.<BR> Examination of all other studs installed in the AGB housing did not reveal any unusual shaking or unlocked<BR>condition especially related to the similar studs.<BR>4-3 Gearshaft line 3 (control alternator)<BR> Inspection of gearshaft input splines, matching with horizontal drive shaft, as well as gear teeth showed good<BR>condition.<BR> Bearing journals : good condition (no wear readable).<BR>4-3-1 Line 3 ball bearing<BR> Good condition (no spalling, no corrosion, no shaking evidence except local fretting marks on 1 out of the 3<BR>outer race securing lugs.<BR>Page 4 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>4-3-2 Line 3 roller bearing<BR> Outer race : general quite good condition except : (see chart 12)<BR> dents caused by particles related to roller and inner raceway spalling.<BR> presence on outer raceway of double superficial wear lines (shiny appearance) formed<BR>by the roller ends passing through the inner raceway sectorial spalling demonstrates<BR>that the outer race stud breakaway and subsequent axial displacement of the outer race<BR>(~1,5mm) likely occurred as a consequence of vibrations induced by inner ring spalling.<BR> fretting wear on outer diameter (already mentioned),<BR> good condition of shoulders with no roller contact indication .<BR> Rollers : all of the 14 rollers are affected by dents and spalling craters only distributed on track fwd edge and<BR>consistent with dents observed on fwd edge of outer raceway (see chart 13).<BR> Cage : good condition. Note the unusual roller contact mark characterized by a conical shape with larger<BR>contact area on fwd side of cage separator.<BR> Inner race : (see charts 14 &amp; 15)<BR> sectorial spalling (~90°) initiated from the forward edge of the track and more developed on the fwd<BR>edge,<BR> maximum spalling depth measured about 0,1mm,<BR> after reinstallation of the alternator rotor as it was initially, the inner raceway sectorial spalling<BR>appears to be located in the quite same angular position as the alternator rotor sectorial wear.<BR> good condition of the remaining portion only affected by dents and a blue discoloration of the track on fwd<BR>edge.<BR>Control alternator damage is the result of rotor interfering with stator , due to rotor offset motion<BR>consecutive to sectorial spalling of the roller bearing inner race and subsequent outer race looseness.<BR>Page 5 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>4-4 Other gearshafts &amp; associated bearings<BR> Inspection of all other received gearshafts and associated bearings did not revealed significant findings especially<BR>regarding :<BR> tooth pattern : no significant wear,<BR> exposed roller bearings : good condition of rollers and outer raceway,<BR> ball bearings : no hard point or defect detectable by hand rotation.<BR>4-5 Additional exam<BR>4-5-1 Dimensional (see chart 16)<BR> Except the dimension related to alternator rotor for which we don’t have the B/P limits, all the other checked<BR>dimensions meet specifications.<BR>4-5-2 Metallurgical examination of Line 3 roller bearing inner race and rollers (see charts 17 to 19)<BR> Inner race : examination of the 2 cross sections made through the spalling sector revealed : (see charts 17 &amp; 18)<BR> some white spots characterized by butterfly appearance corresponding to material ferrite transformation<BR>indicative of material fatigue damaging.<BR> general correct M50 microstructure : normal carbide distribution, fine martensitic needles, correct hardness (63<BR>HRC vs 61 to 64),<BR> microstructure hammered condition as secondary damage.<BR> Rollers : correct hardness (63,5 HRC) and M50 microstructure except usual hammering condition of spalling cracks<BR>(chart 19).<BR>Metallurgical exam of inner raceway showed presence of butterflies facing sectorial spalling typical of fatigue<BR>material damaging<BR>Page 6 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>5- AGB links examination (see chart 20 to 23)<BR> Quite good condition of upper link exhibiting only few axial and radial gap (0,15mm &amp; 0,05mm respectively) at<BR>spherical bearing matching with AGB upper mount.<BR> Bad condition of all 3 other received links affected by heavy wear (1,7mm axial max, 0,55 radial max) at each<BR>spherical bearing consistent with wrong AGB adjustment measured by customer prior AGB removal (see table<BR>of chart 20).<BR> On condition : (see charts 21 &amp; 22)<BR> spherical bearings mainly worn on one side locally dug on 1 sector by interference with one of the 2<BR>shoulders designed to keep in place the anti friction liner bonded to the outer ring,<BR> mount to interference marks.<BR> Good condition of ball bearing bores receiving the pins (no wear noticable).<BR> After cutting of the bearing exhibiting the maximum play : (see chart 23)<BR> anti-friction liner partially missing on one side,<BR> heavy wear of bearing outer journal at anti-friction missing location and adjacent shoulder that totally<BR>disappeared by rubbing with spherical inner journal,<BR> hammered condition of spherical journal only noticeable at remaining–missing transition of anti-friction liner.<BR> The above findings, similar to those already done on Southwest –7B ESN 875402, confirm the spherical<BR>bearing wear mechanism induced by relative movement of the bearing elements under vibrations.<BR>Except upper link found in quite good condition, spherical bearing of all other 3 links exhibited heavy wear<BR>as a consequence of vibrations as already identified on Southwest –7B ESN 875402 engine.<BR>Page 7 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>6- AGB spherical bearing wear<BR> During removal of this AGB for the above bearing failure, spherical bearing of AGB links were found<BR>worn.<BR> 4 out of the 5 links were returned for investigation.<BR> Except quite good condition of upper link, all spherical bearings of the 3 rear links exhibited heavy wear<BR>(until 1,7mm in axial direction and 0,55mm in radial) caused by relative movement of bearing elements<BR>under dynamic loads.<BR> These findings are consistent with the wear mechanism already identified on Southwest –7B ESN<BR>875402 after TSN/CSN = 10857/6864.<BR>Note ; change in design study in progress to introduce new spherical plain bearing.<BR>Page 8 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>7 – Conclusion : AGB input gearshaft “line 3” roller bearing failure<BR> Bearing failure cause : inner raceway spalling<BR> Consequences<BR> spalling of all the 14 balls<BR> looseness of both cage rails<BR> shaking - break away of outer race securing 3 studs,<BR> machining of AGB housing by rotation of the outer race and associated 3 studs over 10mm long,<BR> alternator rotor offset and contamination until interference with alternator stator…<BR> Dimensional part inspection did not show any nonconformity.<BR> Metallurgical examination of the inner race did not reveal any material anomaly other than material fatigue<BR>evidenced by the presence of subsurface fatigue butterflies in raceway .<BR> Operating time accumulated by this bearing (14804h/9478cy) and spalling mechanism (initiation at inner<BR>raceway fwd edge and subsequent roller spalling on fwd ends) leads to make an hypothesis that bearing<BR>failure is consecutive to a constant inner race radial load potentially induced by an alternator rotor<BR>unbalance ; however, no analysis on alternator parts to verify this hypothesis could be done, due to their<BR>high damage condition<BR> Note : ESN874265’s is 1st reported case of failed AGB input gearshaft bearing SEIS in the CFM56-7B<BR>20thSept.02, Southwest ESN 874171, TSN 16160 / CSN 10408 suffered a similar event; CFM has<BR>requested hardware of this 2nd event back for investigation .<BR> No relation ship between roller bearing failure and AGB link wear has been evidenced ; CFMI experience on<BR>CFM56-3 &amp; -7B shows AGB misalignment consequences to be either ball bearing damage or horizontal drive<BR>shaft crack-separation without any noticed consequence on roller bearing condition.<BR>Page 9 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>Starter pad assy Line 3 gearshaft<BR>MFP-HMU pad assy<BR>Control<BR>alternator<BR>1 &amp; 2- AGB as received<BR>3 &amp; 4- Control alternator stator - rotor wear condition resultant from rotor offset<BR>3-<BR>4-<BR>5- Line 3 ball bearing view : no<BR>evidence of damage<BR>AGB<BR>Wear<BR>on 360°<BR>Sectorial<BR>wear (90°)<BR>Page 10 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>Cross section showing line 3 configuration<BR>1- General view of line 3 gearshaft after removal 2- Wear of outer race OD &amp; condition of<BR>the 3 studs remained attached with the outer race<BR>3 &amp; 4- Housing wear condition : elongation of the 3 stud holes and bore matching with outer race<BR>Roller bearing outer race found<BR>break away from AGB housing<BR>3- 4-<BR>Failed<BR>bearing<BR>Page 11 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>Detail views showing AGB housing hole elongation<BR>10mm = stud<BR>displacement<BR>Thread marks<BR>Gearshaft<BR>rotation<BR>direction<BR>Page 12 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>1- Roller bearing outer raceway : general<BR>quite good condition<BR>First superficial<BR>wear lines<BR>formed<BR>before studs<BR>breakaway<BR>2- Picture 1 detail showing the quite good condition of the roller<BR>track except double wear lines caused by roller ends.<BR>Second superficial<BR>wear lines<BR>formed<BR>after studs<BR>breakaway<BR>&amp; 1,5mm outer race<BR>axial displacement<BR>1,5mm (outer race rearward displacement)<BR>Page 13 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>1- Roller &amp; cage view : good condition<BR>of the cage but all 14 rollers exhibit<BR>spalling evidence at fwd edge side 2- Detail of spalling condition at fwd edge side<BR>representative of all 14 rollers<BR>3- Complementary views showing roller<BR>condition representative of the 14.<BR>Spalling Sliding<BR>marks<BR>Fwd face<BR>Page 14 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>1- 3- 2-<BR>1 to 3- Rotor/gearshaft relative angular positions - matching marks<BR>Control alternator rotor Line 3 gearshaft<BR>4- Same angular position of bearing inner<BR>raceway spalled sector and alternator rotor wear sector<BR>5- (opposite to 4-) quite good condition of both<BR>alternator rotor &amp; roller bearing inner raceway<BR>Sectorial<BR>spalling<BR>(115°)<BR>Wear<BR>sector<BR>(90°)<BR>Page 15 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>1 &amp; 2- Roller bearing inner race sector spalling<BR>originating from fwd edge of the raceway<BR>3 &amp; 4- Good condition of race - out of spalled sector - .<BR>Note : blue discoloration of fwd edge of roller raceway<BR>Initiation<BR>area<BR>Blue<BR>discoloration<BR>Roller<BR>passing<BR>direction<BR>Page 16 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>Dia. Dia.OR<BR>A<BR>Dia.<BR>Dia.B IR<BR>Dim. checked B/P<BR>Values<BR>Measured values<BR>Prior removal After removal Comments<BR>Dia. A 34,992 to 35 --- 34,999 to 35,000 Conform (interference fit = 28μm)<BR>Dia. B / outer race 61,991 to 62,000 --- 62,00 Conform<BR>Dia. B / AGB housing 61,80 to 62,20 --- 61,98 Conform<BR>Dia. IR 40,35 (at spalling location)<BR>to 40,475 (90° apart) 40,450<BR>Dia. OR<BR>Defined through<BR>radial clearance<BR>--- 56,475<BR>Roller dia. 8 --- 7,996 to 7,997<BR>Correct values and radial gap<BR>32μm vs. 31 to 50 required<BR>IR shoulder width Defined through axial<BR>gap --- 8,03<BR>Roller length 8 --- 7,997 to 7,999<BR>Correct axial gap<BR>31 to 33μm vs. 20 to 50 required<BR>Dia. C / gearshaft 12,976 to 12,994 --- 12,975<BR>Dia. C / rotor 13,000 to 13.010 --- 12,990<BR>Correct<BR>Dia. D / gearshaft 22,199 to 22,221 --- 22,20<BR>Dia. D / rotor 22.238 to 22.250 --- 22,24<BR>Correct<BR>Dia. E 35,026 to 35,038 --- 35,028 Conform<BR>Dia. F 45,026 to 45,038 --- 45,030 Conform<BR>Page 17 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>A<BR>B<BR>1- Location of<BR>cross sections<BR>made through inner race<BR>2- Labeled “A” micrographic view showing axial grain flow.<BR>2- Typical M50 microstructure except hammering<BR>condition underneath spalling damage<BR>3- Detail showing correct martensitc microstructure<BR>with small carbide networks<BR>Good condition of the shoulders free from wear and or overheat<BR>Inner race track<BR>Roller passing<BR>direction<BR>Page 18 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>1 to 3- Cross section labeled “B” on previous chart<BR>6- Hammered condition of the microstructure as<BR>a consequence of repetitive roller impact when<BR>passing spalling step<BR>4- Spalling cracks and correct<BR>microstructure<BR>5- Fatigue butterfly detail<BR>1- End of spalling at roller entry side 2- Spalling sector close to initiation site 3- End of spalling at roller exit side<BR>Page 19 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>1- Illustration showing location<BR>of cross section<BR>2- Micrographic view of spalling cracks<BR>3- Spalling cracks detail 4- Typical correct M50 microstructure 5- Spalling crack with flaking partially liberated<BR>Roller rotation direction<BR>Page 20 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>Upper link<BR>Rear link “1”<BR>Rear link “2”<BR>Adjustable turnbuckle link<BR>Upper link Rear link “Characterization 1” Adjustable link Rear link “2”<BR>of axial and<BR>radial gap Axial Radial Axial Radial Axial Radial Axial Radial<BR>Spherical bearing<BR>“A”<BR>0,15<BR>mm<BR>0,05<BR>mm<BR>1.20<BR>mm<BR>0,25<BR>mm<BR>0,90<BR>mm<BR>0,25<BR>mm<BR>1,30<BR>mm<BR>0,55<BR>mm<BR>Spherical bearing<BR>“B” 0 0 0,35<BR>mm<BR>0,13<BR>mm<BR>1,70<BR>mm<BR>0,50<BR>mm<BR>0,95<BR>mm<BR>0,40<BR>mm<BR>Spherical bearing<BR>“C” 0 0 --- --- --- --- --- ---<BR>A<BR>C B<BR>A B<BR>A B<BR>A B<BR>View of received AGB links randomly repositioned due to the none marking of the parts prior disassembly<BR>Axial<BR>Radial<BR>Page 21 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>Adjustable turnbuckle link<BR>2 &amp; 3- Detail showing wear condition of each ball bearings<BR>Wear<BR>groove<BR>Wear<BR>groove<BR>Wear<BR>Page 22 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>1 to 3- Supposed rear upper link views showing<BR>wear condition of ball bearings<BR>4 to 6- Same as above for supposed rear lower link<BR>Interference wear marks<BR>Page 23 CFM Proprietary Data Unauthorized Disclosure Prohibited<BR>CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure<BR>1 &amp; 2- Complementary views showing the wear condition of both outer journal<BR>and anti-friction liner partially missing<BR>3- Wear condition of the ball bearing<BR>4- Detail of fretting wear condition<BR>associated with missing anti-friction liner<BR>5- Preferential contact area on 6- Illustration showing missing<BR>shoulder at 1 outer ring side<BR>Shoulder<BR>still present<BR>Shoulder<BR>totally<BR>worn out<BR>Anti-friction<BR>liner<BR>Portion of inner ring surface<BR>free from significant wear

zippo1983 发表于 2011-5-3 02:24:08

Portion of inner ring surface
free from significant wear

且行 发表于 2011-6-2 11:13:05

:victory:&nbsp;

kinran 发表于 2011-6-2 21:42:11

:victory: :victory:

bocome 发表于 2011-7-31 05:38:36

CFM56-7B - Southwest - ESN874265 - AGB input gearshaft roller bearing failure
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