GE CF6-50 series

Service difficulty reports · 201

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE engine_model_key = 'CF650'
  ORDER BY difficulty_date DESC"

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SDR UIEA2010062800072Stringer · bentNRC: 0979 "LOWER DECK" B/T STA 360-380 S 35R STRINGER LOWER FLANGE IS BENT. (DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH STRINGER REPAIR AND FILLER P/N N523MC NRC 979 1/2 PER SRM 53-10-03 FIG 3. FASTENERS INSTL PER SRM 51-30-02)Jun 28, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Longeron/StringerSDR UIEA2010062700063Stringer · bentNRC0974, LOWER DECK STA 380, 400 STR 37R STRINGER UPPER FLANGE IS BENT (DAMAGED PORTION OF STRINGER REMOVED. REINFORCED AREA WITH NEW SEGMENT AND REPAIR STRINGER REMOVED. REINFORCED AREA WITH NEW SEGMENT AND REPAIR STRINGER PN N523MC NRC 971 -/2 IAW SRM 53-1Jun 27, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Longeron/StringerSDR UIEA2010062700067Stringer · twistedNRC: 1397, STA 440, STR 41-L FOUND TWIST STR AND NBSP; TURN TO AT LOWER DECK (P-6 AREA)(DAMAGED AREA TRIMMED OUT. REINFORCED AREA WITH NEW ZEE PN N523MC NRC 1397-1 IAW SRM 53-10-03 FIG 3, FASTENER INSTL IAW SRM 51-30-02).Jun 27, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Longeron/StringerSDR UIEA2010062700062Stringer · bentNRC 0973 LOWER DECK STA 380-400, STR 39R, STRINGER UPPER FLANGE IS BENT. (DAMAGED PORTION OF TRIMMED OUT REINFORCED AREA WITH NEW SEGMENT AND REPAIR STRINGER PN 523 NRC 1/2 IAW SRTM 53-10-03 FIG 3. FASTENERS INSL IAW SRM 51-30-02).Jun 27, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Longeron/StringerSDR UIEA2010062700082Floor Support · crackedNRC 0925 'MAIN DECK FLOOR OMEGA' CRACK ON OMEGA LBL 75, CHANNEL BETWEEN STA 910 TO 1000 AND TWIST. (DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH NEW OMEGA AND SPLICE PN N523MC, NRC 925 1/2 IAW SRM 53-10-05, FIG 19. FASTENER INSTL IAW SRM 51-30-02).Jun 27, 2010 · N523MC · Boeing 7472D7B · Fuselage Miscellaneous StructureSDR UIEA2010062600047Seat Track · crackedDURING C-CHECK, FLANGE OF SEAT TRACK AT BS 910-1500 LBL 75 CRACKED. DAMAGE CUT OUT AND REPLACED WITH NEW SECTIONS OF SEAT TRACK WITH SPLICE ANGLES INSTALLED AND WAS DOCUMENTED ON IAI NRC1325, NRC1378, NRC924, NRC925 AND NRC 1254 RESPECTIVELY. CLASS A PERMANEJun 26, 2010 · N523MC · Boeing 7472D7B · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2010062500043Fairing · crackedRT LEST440-528 HORIZONTAL STAB L/E OTBD FAIRING HAS 6 CRACKS AT RIB ANGLES PERFORMED MAJOR REPAIR IAW RAM256 - NRC1141 - SRM 55-10-06 FIG 1.Jun 25, 2010 · N523MC · Boeing 7472D7B · Horizontal Stabilizer StructureSDR UIEA2010062500046Skin · corrodedDURING C-CHECK, A BULGE WAS DETECTED IN AN EXISTING REPAIR DOUBLER ON SKIN AT BS 460 AND S41-42L. DAMAGED REPAIR DOUBLER WAS REMOVED AND SUBSEQUENT DISCOVERED DRILL STARTS IN THE SKIN WERE TRIMMED OUT. THE DISCREPANT AREAS WERE THEN REPAIRED IAW NRC 0011 AND Jun 25, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR UIEA2010062500048Skin · dentedDURING C-CHECK, A DENT/WRINKLE WAS DETECTED IN SKIN OF RT FLAP NR 18 L/E AT 29 INCHES FROM THE INBD EDGE LOOKING AFT. DAMAGE WAS TRIMMED OUT AND REPAIRED IAW INRC 0386 AND SRM 57-50-03, FIG 3, SHEET 4, DETAIL III FIG 1.Jun 25, 2010 · N523MC · Boeing 7472D7B · Trailing Edge FlapsSDR UIEA2010062500066Seat Track · crackedNRC: 1254 CRACK ON SEAT TRACK CHANNEL, RBL 75 BETWEEN STA 1480 TO 1500 (DAMAGED AREA TRIMMED OUT REINFORCED AREA WITH TRACK AND SPLICE PN N523MC, NRC 1254 1/2 IAW SRM 53-10-05, FIG 19. FASTENERS INSTL IAW SRM 51-30-02).Jun 25, 2010 · N523MC · Boeing 7472D7B · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2010062500087Floor Support · crackedNRC 1325 "MAIN DECK" STA 560 LBL 99 FLOOR SUPPORT IS CRACKED IAW SRM 53-10-05, FIG 19 AND FASTENERS INSTL IAW SRM. (DAMAGED AREA REMOVED NEW FABRICATED PN N523MC, NRC 1325 IAW SRM 53-10-05, FIG 19, FASTENERS INSTL IAW SRM 51-30-02).Jun 25, 2010 · N523MC · Boeing 7472D7B · Fuselage Miscellaneous StructureSDR UIEA2010062400064Stringer · bentNRC 0978 "LOWER DECK" B/T STA 360 - 380 STR 38R STRINGER LOWER FLANGE IS BENT. (DAMAGED AREA TRIMMED OUT, REINFORCED AREA WITH ENW REPAIR. STRINGER AND FILLER PN B523MC NRC 978 1/2 IAW SRM 53-10-03, FIG 3. INSTALL FASTENERS IAW SRM 51-30-02).Jun 24, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Longeron/StringerSDR UIEA2010062200065Stringer · crackedNRC: 1124 FWD CARGO, CRACK ON STR 38R BETWEEN STA 500-520 (DAMAGED PORTION OF STRINGER REMOVED, REINFORCED AREA WITH NEW SEGMENT AND REPAIR. STRINGER PN B523MC NRC 1124 1-2 REPAIR IAW SRM 53-10-03, FIG 3 & AMP; FASTENER INSTL IAW SRM 51-30-02).Jun 22, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Longeron/StringerSDR UIEA2010062100058Skin · corrodedNRC: 011 -BULGE BY 2.5" X 2.3" X 0.037" ON EXT FUSELAGE, SKU EXISTING REPAIR DOUBLER EDGE BS 440-460 AND STR 43L-44L. (EXISTING REPAIR REMOVED THE WORK ACCOMPLISHED IAW J/C NO 0B011-R1 USING DOUBLER PN N523MC, NRC 011-1 FASTENERS INSTALLED IAW SRM 51-30-02).Jun 21, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR UIEA2010062100060Stringer Clip · crackedNRC: STA 360 AFTER REMOVAL CRACKED STR CLIP FOR REPLACEMENT WAS FOUND CRACK ON THE STR 7R.(DAMAGED AREA TRIMMED OUT AREA REINFORCED WITH REPAIR STRINGER AND SPLICE PN N523MC, NRC 1333 1/3 IAW SRM 53-10-03, FIG 3, FASTENERS INSTL IAW SRM 51-30-02).Jun 21, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Attach FittingsSDR FDEA201006172047Unknown · smokeCREW AND JUMPSEATER SMELLED ACRID ELEC ODOR FOLLOWED BY CONSIDERABLE AMOUNT OF SMOKE IN COCKPIT. DECLARED EMERGENCY AND LANDED.Jun 17, 2010 · N321FE · Doug MD1030F · Air Distribution SystemSDR UIEA2010061400076Stringer · crackedNRC: 964 "LOWER DECK" STA 320, 2 EA CRACKS (1 EA ON STR UPPER FLANGE AND 2 ON STR WEB) ON STR 35R. (DAMAGED AREA TRIMMED OUT. REINFORCED AREA WITH NEW SEGMENT AND REPAIR STRINGER PN N523MC, NRC 964 1/2 IAW SRM 53-10-03 FIG 3 AND FASTENERS ISNTL IAW SRM 51-30-Jun 14, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Longeron/StringerSDR FDEA201006111959Skin · damagedDURING WALKAROUND FOUND NR 2 ENGINE PATIO ACCESS DOOR MISSING. CALLED MOCC AND UPLOAD PICTURES. SKIN HAS A HOLE WITH THIS MEASURES 2 INCHES LONG 1.5 INCH WIDE. TAILCONE ASSY TO BE REPLACED TAILCONE ASSY REMOVED PER MM 53-52-00-2. INSTALLED TAILCONE IAW AJun 11, 2010 · N303FE · Doug MD1030F · Aerodynamic FairingsSDR UIEA2010060800027Skin · delaminatedDURING WALK AROUND INSP BEING PERFORMED, MX FOUND THE- LEADING EDGE PANEL - LOWER SURFACE EXTERNAL SKIN WITH DELAMINATION DAMAGE (AREA: MEASURES 33.0 IN. X 36 IN.) (REF FIGURE 1).(EO4757A497 DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED INJun 8, 2010 · N540MC · Boeing 747243B · Wing, Plate/SkinSDR UIEA2010060600028Floor Panel · damagedDURING CARGO LOADING AT DOV; MX FOUND DAMAGE TO THE MAIN DECK FLOORBOARD AT BS 1080, RBL 45. THE DAMAGE TO THE MD FLOORBOARD PANEL AT BS1080, RBL45 AIS S FOLLOWS: THE DAMAGE IS ABOUT 7 INCHES LONG AND ABOUT .5 INCH WIDE, AND .2500 INCH DEEP. (DISPOSITION WAS MJun 6, 2010 · N522MC · Boeing 7472D7B · Fuselage Floor PanelSDR UIEA2010060300059Cargo Track · damagedNRC 0494 SWELLING ON AFT CARGO TRACK UPPER FLANGE BETWEEN STA1900-1920 RBL 25 (DAMAGED AREA TRIMMED OUT IAW SRM 51-10-01, REINFORCED WITH EXTRUDED REPAIR ANGLE, REPAIR STRIP, TRACK SECTION PN B523MC 494 1,2,3 IAW SRM 53-1-05 FIG 5 FASTENERS INSTL IAW SRM 51-30Jun 3, 2010 · N523MC · Boeing 7472D7B · Fuselage, Seat/Cargo Attach FittingsSDR 2010F00120Skin · delaminatedPYLON NR2, SKIN PYLON NR2 DELAMINATION ( RT INNER SIDE ) BETWEEN NAC STA 201.4 TO NAC STA 286,00.Jun 2, 2010 · N765SA · Boeing 7472F6B · Nacelle/Pylon, Plate/SkinSDR CNMA20100026Slide · defectiveDOOR 3L EVACUATION SLIDE REMOTE PRESURE PRESS TO TEST INDICATOR LIGHT STAYS ON CONTINUOUSLY. REPLACED L-3 DOOR SLIDE ASSY - OPS CHECK NORMAL. OK FOR SERVICE. M/M REF. 25-61.Jun 2, 2010 · N270AX · Doug DC1030 · Escape SlideSDR UIEA2010053000019Skin · bulgedBULGE BY 1.3 X 1.0 X 0.025" ON EXT FUSELAGE SKIN STA 2140 STR 36L-37L (STA AREA) (THE BULGE WAS FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-00, FIG 1A.)May 30, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR UIEA2010053000020Skin · bulgedBULGE BY 1.2 X 1.1 X 0.013" ON EXT. FUSELAGE SKIN STA 2160-2180 STR 42L-44L (THE BULGE FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01, FIG 1A.)May 30, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR UIEA2010053000022Skin · damagedDAMAGED AREA BY 6.0 X 3.0" ON EXTERNAL FUSELAGE SKIN AT STRINGER AREA BS 160-180 S-42AL (DAMAGED AREA FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01, FIG 1A).May 30, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR UIEA2010051600009Skin · bulgedBULGE BY 1.5X 1.0 X 0.024" AND ADJACENT DENT BY 3.2 X 1.5 X 0.014" ON EXTERNAL FUSELAGE SKIN BS 580-600 S-44R-45R (BULGE AND DENT FOUND IN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01 FIG 1A.)May 16, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR UIEA2010051600012Skin · dentedDENT ON EXTERNAL FUSELAGE SKIN BY 4.0 X 2.5 X 0.039" BS 500-520 S-35R-36R (DENT FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01, FIG 1A).May 16, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR UIEA2010051600013Skin · bulged2 EA BULGES BY MAX 1.0 X 1.0 X 0.024" ON EXTERNAL FUSELAGE SKIN BS 540-560 S-41R-42R (2 EA BULGES FOUND WITHIN ALLOWABLE LIMITS).May 16, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR UIEA2010051600014Skin · bulgedBULGE BY 2.0 X 2.0 X 0.022" ON EXTERNAL FUSELAGE SKIN BS 520-540 S42R-43R (BULGE FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01.)May 16, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR UIEA2010051600015Skin · damagedPREVIOUSLY REWORKED AREA ON EXTERNAL FUSELAGE SKIN BS 380-400 S-38R-39R BY 2.0 X 1.6 X 0.011 X 0.010" (NOTED AREA FOUND WITHIN ALLOWABLE DAMAGE; LIMITS IAW SRM 53-30-01, FIG 1.)May 16, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR UIEA2010051600016Skin · dented2 EA ADJACENT DENTS ON INSP; EXTERNAL FUSEALGE SKIN BS 380-400 S-37R-38R UPR 1.25 X 1.0 X 0.008" AND LWR 0.8 X 0.7 X 0.010" (2 EA DENTS FOUND WITHIN ALLOWABLE DAMAGE AND INSP;LIMITS IAW SRM 53-30-01 FIG 1A)May 16, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR UIEA2010051600017Skin · bulgedBULGE BY 1.0 X 0.8 X 0.025" ON EXTERNAL FUSELAGE SKIN BS 320-340 ABOVE S-39R (BULGE FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01, FIG 1A.)May 16, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR UIEA2010051600018Skin · dentedDENT BY 1.8 X 1.5 X 0.016" ON EXTERNAL FUSEALGE SKIN BS 380-400 ABOVE S-41L(DENT FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-01, FIG 1A)May 16, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR FDEA201005121519Wire Harness · damagedON CLIMB OUT OF ANC - NR3 ENGINE EGT GAGE FLUCTUATED WILDLY OUT OF 20,000 FT HIT 1020 GOT "ENG 3 EXCEEDANCE ALL ENG 3 OIL, TEM, PRESSURE SHOWED NORMAL DUMPED FUEL RETURNED TO DEPARTURE. ANC R EGT INDICATION NORMAL AFTER SHUTDOWN, VISUAL INSP OF HARNESS AMay 12, 2010 · N314FE · Doug MD1030F · Engine Indicating System WiringSDR FDEA201004291395Skin · wornRT WING L/E DROOPED EXT FOUND DEEP WEAR ON SKIN. REPAIRED AREA IAW SRM 57-10-00, VOL I, FIG 39.Apr 29, 2010 · N315FE · Doug DC1030F · Wing, Plate/SkinSDR 22AA201000068Stud · damagedOIL PRESSURE NR 2 GAUGE DROPPED TO ZERO AND NR 2 OIL PRESS LOW LIGHT CAME ON, ENGINE SHUTDOWN IAW CHECK LIST. FOUND OIL LEAK COMING FROM CRANK PAD COVER, INSTALLED 1EA COVER PAD STUD, REINSTALLED 1EA COVER PAD STUD IAW GE SPM 70-48-01, REINSTALLED COVER PAD IAApr 25, 2010 · N524MD · Doug DC1030 · Engine (Turbine/Turboprop)SDR FDEA201004211265Longeron · corrodedLT WING UPPER SIDE WING TO FUSELAGE FILLETS. AFTER REMOVING THE FILLETS 151 FT AND 151 ET WITH NRC NR N00866 THE FOLLOWING DEFECT HAVE BEEN FOUND EXFOLIATION CORROSION ON LONGERON. PERFORMED REPAIR IAW E.A. 8-5310-137606Apr 21, 2010 · N320FE · Doug DC1030F · Fuselage Main, Longeron/StringerSDR UIEA201000189Rib · corrodedLT STABILIZER STA 281 RIB LOWER CORD SURFACE CORRODED. LEVEL 1. DAMAGED CHORD REMOVED NEW FABRICATED. PN 65B03680-29 IAW DWG 65B03680-28 AND NR A004088G002. USING WITH FASTENERS IAW SRM 51-30-02.Apr 8, 2010 · N524MC · Boeing 7472D7B · Horizontal Stabilizer StructureSDR CNMA20100005Fan · shortedAFTER T/O, BURNED SMELL FROM "A" ZONE WAS NOTICED. CABIN AIR RECIRC FAN NR1 SW WAS TRIPPED, BUT FAN NR15 WAS STILL THERE IN AFT "A" ZONE, SO ALL RECIRC FANS TURNED OFF (OK AFTER THAT). R & R WITH NEW FAN IAW 21-22-10. OPS CHECK GOOD.Mar 12, 2010 · N810AX · Doug DC1030 · Air Distribution FanSDR UIEA2010022300139Fairing · puncturedWING TO BODY FAIRING AT BS 1680 WITH A PUNCTURE/DAMAGE (HONEYCOMB EXPOSURE) MEASURING 2.5 IN. X 0.5 IN (REF FIG 1) (PERFORMED A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 OF EO 4753B253 PART 1 OF WORK INSTRUCTIONS. SCHEDULE REPEAT INSP AT EVERY 3 FC AND PERMANFeb 23, 2010 · N522MC · Boeing 7472D7B · Aerodynamic FairingsSDR 22AA201000035Line · leakingDURING CLIMB OUT, NR 1 HYD SYS START LOOSING FLUID, INITIATION PROCEDURE ON ALT PROCEDURES CHECK LIST, HYD FLUID LOST, DURING CLIMB OUT TO CRUISE NR 2 ENG FAIL, SECURED ENGINE IAW CHECK LIST. DUMP FUEL TO MAX LANDING WEIGHT TO LANDING, DURING POST FLIGHT FOUNJan 22, 2010 · N524MD · Doug DC1030 · Hydraulic System, MainSDR FDEA201001070028Sensor · malfunctionedREJECTED TAKEOFF DUE TO ENGINE EXCEEDANCE, NR 3 N1 AT 131.7%. EXCEEDANCE OCCURED WHILE INITIALLY SETTING POWER FOR TAKEOFF. AIRSPEED <50 KNOTS. VIA 3 SHOWED NO EXCEEDANCES FOR NR 3 ENG. REMOVED AND REPLACED NR 3 N1 FAN TACH PER MM 77-11-01-2 . RAN NR 3 ENG Jan 7, 2010 · N312FE · Doug MD1030F · Engine Indicating SystemSDR EIAA200900129Mec · malfunctionedREJECTED TAKEOFF, NR 4 ENGINE DID NOT MAKE TAKEOFF POWER. REMOVED AND REPLACED MEC IAW 73-21-01. REMOVED AND REPLACED USV FEEDBACK CABLE IAW MM 75-31-03. REMOVED AND REPLACED USV ACTUATORS IAW MM 73-31-02. REMOVED AND REPLACED FUEL PUMP IAW MM 73-11-01. ONov 24, 2009 · N487EV · Boeing 747230B · Fuel Control/Turbine EnginesSDR FDEA200910213623Skin · crackedRT WING OTBD FLAP UPPER SURFACE FOUND CRACKED ON SKIN. REPAIRED SKIN IAW SRM 57-10-00, FIG 85, SHT 3, VOL I.Oct 21, 2009 · N315FE · Doug DC1030F · Trailing Edge FlapsSDR 22AA200900025Tire · failedON LANDING, NR 4 TIRE FAILED. DEBRIS FROM TIRE CAUSED SLIGHT DAMAGE TO LWR OTBD GEAR DOOR. REMOVED NR 4 TIRE ASSY AND INSPECTED RT LANDING GEAR AXLE, NO DEFECT NOTED. REPLACED NR 4 TIRE ASSY IAW MM 32-41-02, REMOVED AND REPLACED NR 3 MAIN TIRE ASSY IAW MM 3Sep 20, 2009 · N524MD · Doug DC1030 · TireSDR FDEA200908263089Rib · crackedRT WING INTERNAL L/E FOUND CRACK 1 INCH LONG ON INTERNAL RIB AT STA XOS 691 REPAIR FORMER IAW SRM 57-00-01 VOL 1, FIG 10, SHT 1.Aug 26, 2009 · N321FE · Doug DC1030F · Wing, Rib/BulkheadSDR CLCA08152009.1Engine · fodDURING TAKEOFF ROLL (MIA) NR 1 ENGINE VIBRATION OCCURRED FOLLOWED BY LOUD COMPRESSOR STALL. ABORTED TAKEOFF, ENGINE SHUT DOWN AND CAC EMERGENCY PROCEDURES FOLLOWED. RETURNED TO RAMP WITHOUT INCIDENT. INSPECTED NR 1 ENGINE, FOUND SEVERAL PARTICLES OF METAL IAug 15, 2009 · N47888 · Doug DC1030F · Turbine Engine Compressor SectionSDR CNMA20090019Slide · false indicationR4-DOOR SLIDE INOP (SLIDE LIGHT REMAINS ON). REPLACED R4 DOOR SLIDE - OPS CHECK NORMAL. MM REF. 25-61.Aug 5, 2009 · N270AX · Doug DC1030 · Escape SlideSDR 22AA20090404Slide · unwanted deployLOG PAGE NR 130754: L-1 DOOR INADVERTED OPENED (BY GROUND HANDLER) WHILE ARMED DEPLOYING SLIDE. ENTERED ON DMI NR 22611 IAW MEL 52-10-2, CATEGORY ''C''. REMOVED AND REPLACED L1 EVACUATION SLIDE/RAFT CONTAINER IN ACCORDING WITH DC-10 MAINTENANCE MANUAL 25-61-01Apr 30, 2009 · N478CT · Doug DC1030F · Escape Slide
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