GE CF6-50C2

Service difficulty reports · 719

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Query with SQL
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 = 'CF650C2'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 22AA20090502Panel · puncturedDURING INSP, FOUND A PUNCTURE ON HORIZONTAL STABILIZER TIP T/E UPPER PANEL STA XE 247 - 344 RT DUE NR 2 ENGINE DEBRIS. HORIZONTAL STABILIZER TIP T/E UPPER PANEL STA XE 247 - 344 PINCTURE RT REPAIR WAS ACCOMPLISHED IAW IAAC EO ARW-090413.Mar 26, 2009 · N526MD · Doug DC1030 · Horizontal Stabilizer, Plate/SkinSDR 22AA20090503Panel · puncturedDURING INSPECTION WAS FOUND A PUNCTURE ON HORIZONTAL STABILIZER TIP T/E UPPER PANEL STA XE 344 - 461 RT DUE NR 2 ENGINE DEBRIS. HORIZONTAL STABILIZER TIP T/E UPPER PANEL STA XE 344 - 461 PUNCTURE RT REPAIR WAS ACCOMPLISHED IAW IAAC EO ARW-090414 BY TAMPA CARGMar 26, 2009 · N526MD · Doug DC1030 · Horizontal Stabilizer, Plate/SkinSDR 22AA20090504Skin · damagedRT SIDE OTBD AT HORIZONTAL STABILIZER TRAILING EDGE UPPER AND CENTER SECTION UPPER DAMAGE PERFORATION DUE TO NR 2 ENGINE DEBRIS. REFERENCE N/R NR 007. EWO'S ARW 55-001, ARW 55-002, ARW 55-003 WERE ACCOMPLISHED AT OTBD SECTION OF RT HORIZONTAL STABILIZER AND Mar 26, 2009 · N526MD · Doug DC1030 · Horizontal Stabilizer, Plate/SkinSDR DHLA200800013Mec · failedNR 1 ENGINE FAILED TO ACCELERATE WHEN TAKEOFF POWER WAS APPLIED. REJECTED PRIOR TO 70 KTS AT 5 DEGREE AMBIENT TEMP PRESS ALT 1360'. REMOVED AND REPLACED NR 1 MEC IAW MM 73-21-01. OPS CHECKS SERVICEABLE, NO LEAKS NOTED. MPA C/W IAW JRH.Feb 18, 2009 · N365DH · Airbus A300B42C · Fuel Controlling SystemSDR 22AA20090202Pump · failedNR1 ENGINE HAS A VIBRATION. LOSS CHANNEL 3 IN FLIGHT. RUDDER TRIM LOCKED UP IN FLIGHT AT ZERO POSITION AND FLIGHT CONTROL BECAME STIFF WITH SOME VIBRATION AFTER FLAP EXTENSION. PERFORMED VIBRATION CHECK ON ENGINE S/N 517620 NR1 POSITION IAW AMM 72-00-00 PAGE Feb 15, 2009 · N524MD · Doug DC1030F · Hydraulic Pump (Electric/Engine), MainSDR FDEA200902120509Garlock Seal · leakingNR 2 ENG OIL DROPPED TO 1 QT TO 10 QTS DROPPED TO 6 QTS MONITORED IT. DROPPED 1 QT EVERY 30 MIN TO 3 QTS. PULLED NR 2 THROTTLE TO IDLE REST OF FLT. WENT DOWN TO 1 QT. AFTER SHUTDOWN QTY WENT TO 5 QTS, TEMPS & PRESSURE NORMAL. INSPECTED & FOUND APPROX 1 QFeb 12, 2009 · N301FE · Doug MD1030F · Hydraulic Pump (Electric/Engine), MainSDR CLCA614-01091Fire Warning · illuminatedDURING CLIMB THROUGH 210, NR 2 ENGINE FIRE LIGHT AND WARNING WHERE ACTIVATED. SHUTDOWN PROCEDURE COMPLETED.Jan 22, 2009 · N614GC · Doug DC1030F · Fire DetectionSDR WRLA2009012Unknown · fumesN3 PACKS PRODUCED FUMES IN CABIN. INSPECTED NR 3 ENG INLET AND EXHAUST, CHECKS OK. INSPECTED BREATHERS, CHECKS OK. CHECKED CHIP DETECTOR AND RAN ENG, CHECKS OK.Jan 17, 2009 · N14075 · Doug DC1030 · Air Distribution SystemSDR 22AA20090102Manifold · crackedAT APPROXIMATELY 1740 Z. ENGINE NR 1 FAILED FUEL PRESSURE, APPROXIMATELY 50 PSI. ATTEMPTED TO START, CROSS FEED FAILED. DIVERT TO SKCL. REMOVED AND REPLACED LT, RT Y-FUEL MANIFOLD NR 1 ENGINE IN ACCORDING WITH MAINTENANCE MANUAL 73-11-01. NO LEAKS NOTED. Jan 6, 2009 · N478CT · Doug DC1030F · Engine Fuel DistributionSDR WRLA2008108Hydraulic System · malfunctionedWHILE EXTENDING SLATS, FELT A BUMP; NR 1 HYD SYS LOST FLUID AND PRESSURE, COMPLETED CHECKLIST AND PROCEEDED WITH UNEVENTFUL LANDING AND PARKING. C/A: OPEN Dec 27, 2008 · N137 · Doug DC1030 · Hydraulic System, MainSDR 22AA20081202Engine · failedON TAKEOFF AT 800FT NR 1 ENGINE FAILED. ENGINE REPLACEMENT IN PROGRESS. ACCOMPLISHED RED BORDER 025093. REMOVED AND REPLACED NR 1 ENGINE IAW WORK CARD 141R7101M, PERFORMED ENGINE RUN UP IAW MM 71-00-00, 71-06-00; OPERATION NORMAL, NO LEAKS NOTED.Dec 11, 2008 · N524MD · Doug DC1030F · Engine (Turbine/Turboprop)SDR CA081208011Cowling · delaminated(CAN) ON DESCENT INTO YYC, WITH POWER LEVERS AT IDLE, THE ACFT SHUDDERED MOMENTARILY. THE NR 2 THRUST REVERSER UNLOCK LIGHT ILLUMINATED AND IN-FLIGHT SHUT DOWN OF NR 2 ENGINE WAS CARRIED OUT. THE ACFT LANDED WITHOUT INCIDENT AND AN INSPECTION WAS CARRIED OUTNov 26, 2008 · Engine Thrust ReverserSDR 08FDEA04795Engine · malfunctionedAT 2 00 INTO FLIGHT GOT EGT FLUCTUATING UP TO 1065 DEGREES CELSIUS TO VALUE S AT OR BELOW NORMAL. RETARDED THROTTLE TO IDLE AND RAN CHECKLIST EGT STILL FLUCTUATING WILDLY SO WE PERFORMED ENG SHUTDOWN. NO OTHER INDICATIONS OF SEVERE DAMAGE, BUT WITH EGT STILLNov 8, 2008 · N304FE · Doug MD1030F · Engine (Turbine/Turboprop)SDR FDEA200811084795Engine · overtempAFTER 2 HOURS INTO FLT GOT EGT FLUCTUATING UP TO 1065 DEGREES CELSIUS TO VALUES AT OR BELOW NORMAL. RETARDED THROTTLE TO IDLE AND RAN CKLIST. EGT STILL FLUCTUATING WILDLY SO PERFORMED ENG SHUTDOWN. NO OTHER INDICATIONS OF SEVERE DAMAGE, BUT WITH EGT STILL Nov 8, 2008 · N304FE · Doug MD1030F · Engine (Turbine/Turboprop)SDR 22AA20081004Engine · malfunctionedAFTER TAKEOFF HEARD LOUD NOISE. TOWER ADVISED, FLAMES COMING FROM AIRCRAFT AND NR 1 ENGINE EGT WENT TO RED LINE. ENGINE SHUTDOWN ON ITS OWN. ENGINE CHANGE IN PROGRESS. Oct 25, 2008 · N526MD · Doug DC1030F · Engine (Turbine/Turboprop)SDR WRLA2008090Cable · misriggedDURING MAINTENANCE L4 DOOR FAILED TO OPEN WITH DOOR ARMED, EMERGENCY MODE. REMOVED LININGS, RIGGED AIR RELEASE CABLE AND ARMING ROD IAW DC10 MM 52-12-00. OPS CHECK GOOD. SERVICED DOOR OPENING RESERVOIR IAW DC10 MM 52-12-00. REPLACED L4 DOOR AND SURROUND LIOct 22, 2008 · N14075 · Doug DC1030 · Passenger/Crew DoorsSDR WRLA2008076Insulation · out of positionFLT T8000/RMS/25 DURING FLIGHT BURN ODOR WAS NOTED IN COCKPIT AND CABIN. FLIGHT ATTENDANT OBSERVED LIGHT SMOKE AND BURN ODOR EMANATING FROM FORWARD AND MID GALLEY VENTS. C/A REMOVED INSULATION MATERIAL DEBRIS FROM THE INSIDE OF THE LAV VENT DUCT ASSY. LAV/GSep 25, 2008 · N136WA · Doug DC1030 · Passenger Compartment EquipmentSDR WRLA2008074Skin · corrodedDURING INSPECTION FOUND CORROSION RT MLG WW. STA 1505 AT LONGERON 35R SKIN, INTERCOSTAL AND FRAME ATTACH. REF DELTA NR 41.Sep 9, 2008 · N303WL · Doug DC1030F · Fuselage Main, Plate/SkinSDR WRLA2008075Intercostal · corrodedDURING INSPECTION FOUND CORROSION RT MLG WW. STA 1505 AT LONGERON 31R, INTERCOSTAL SKIN ATTACH. REF DELTA NR40.Sep 9, 2008 · N303WL · Doug DC1030F · Fuselage Miscellaneous StructureSDR WRLA2008072Bolt · shearedDURING C-CHECK INSPECTION FOUND 1 BOLT SHEARED AND RUSTED, AND 1 BOLT RUSTED AT RT WING ROOT FUSELAGE ANGLE. FUSELAGE STA 1371. REAMED HOLES, EDDY CURRENT INSPECTION ACCOMPLISHED, MFG AND INSTALLED TAPERED WASHERS, TREAT, PRIME, SEAL AND PAINT IAW ENGINEERINAug 26, 2008 · N139WA · Doug DC10 · Fuselage Miscellaneous StructureSDR CLCA080802Tube · damagedNR (3) ENG FIRE WARNING CAME ON DURING CLIMB THROUGH 22KFT. ENG WAS SHUTDOWN IAW AOM PROCEDURE E-12, ACFT FUEL WAS DUMPED, AND ACFT RETURNED TO DEPARTURE. UPON EXTERIOR INSP OF THE ENG, DISCOVERED THE SEALS TO THE HIGH PRESSURE TURBINE (HPT), COOLING TUBE WAS Aug 15, 2008 · N614GC · Doug DC1030F · Engine (Turbine/Turboprop)SDR WRL2008F00006Stringer · corrodedDURING INSPECTION FOUND LEVEL 2 CORROSION ON STR 36L AT FSTA 766 (N/R 19). (A)Jul 21, 2008 · N137WA · Doug DC1030 · Fuselage Main, Longeron/StringerSDR 08FDEA02982Engine · failedDURING DEPARTURE NR 1 ENGINE HAD LOUD BANG AND VIBRATION. NR 1 ENG TO IDLE AND THEN OIL QUANTITY WENT TO ZERO, NO N1. PERFORMED PHASE 1'S AND QRH PROCEDURE. RETURN TO MEM FOR ENGINE OUT LANDING. MX MEM, INSPECTED NR 1 ENGINE. FOUND OIL PUDDLED IN EXHAUSJul 18, 2008 · N314FE · Doug DC1030F · Engine (Turbine/Turboprop)SDR FDEA200807182982Engine · failedDURING DEPARTURE NR 1 ENGINE HAD LOUD BANG AND VIBRATION. NR 1 ENG TO IDLE AND THEN OIL QUANTITY WENT TO ZERO, NO N1. PERFROMED PHASE 1'S AND QRH PROCEDURE. RETURN TO MEM FOR ENGINE OUT LANDING. MX MEM - INSPECTED NR 1 ENGINE. FOUND OIL PUDDLED IN EXHAUJul 18, 2008 · N314FE · Doug DC1030F · Engine (Turbine/Turboprop)SDR 08FDEA01419Compressor · stalledNR 3 ENGINE COMPRESSOR STALL IN CRUISE SHAKING. AIRCRAFT FLUCTUATION OF N1,-THROTTLE AT IDLE N137 PERCENT EGT 600-700 DEG INFLIGHT ENGINE SHUTDOWN, RESIDUAL FUEL FLOW AFTER SHUTDOWN 800 LBS FF. REMOVED AND REPLACED THE #3 ENGINE. PERFORMED IDLE AND FLT IDLEApr 15, 2008 · N315FE · Doug DC1030F · Turbine Engine Compressor SectionSDR FDEA200804151419Engine · failedNR 3 ENGINE COMPRESSOR STALL IN CRUISE SHAKING. AIRCRAFT FLUCTUATION OF N1, THROTTLE AT IDLE N137 PERCENT EGT 600-700 DEG. INFLIGHT ENGINE SHUTDOWN, RESIDUAL FUEL FLOW AFTER SHUTDOWN 800 LBS FF. REMOVED AND REPLACED THE NR 3 ENGINE. PERFORMED IDLE AND FLT Apr 15, 2008 · N315FE · Doug DC1030F · Engine (Turbine/Turboprop)SDR WRLA2008044Slide · dislodgedL1 DOOR SLIDE DROPPED OUT WHEN DOOR OPENED PNEUMATICALLY, SLIDE DID NOT DEPLOY CORRECTLY. REMOVED AND REPLACED SLIDE ASSY IAW MM 25-61-01. SERVICED PNEUMATIC DOOR ASSIST.Apr 14, 2008 · N14075 · Doug DC1030 · Escape SlideSDR WRLA2008043Oven · malfunctionedEDDP/KBGR OVEN 609 AFT GALLEY ON FOR 5 MIN. THEN GRAY AND WHITE SMOKE BILLOWED OUT, SHUT OFF OVEN. ITEM PLACED ON DMI PER MEL 25-29-01 CAT C DUE 04/17/08. REMOVED AND REPLACED OVEN 609, DMI CLEARED 04/10/08.Apr 6, 2008 · N14075 · Doug DC1030 · Buffet/GalleysSDR WRNA200800006Engine · failedAFTER TAKEOFF FROM MFM, CLIMBING THROUGH 15,000 FEET A LOUD EXPLOSION WAS HEARD FROM NR 1 ENGINE FOLLOWED BY SEVERE VIBRATION, ENGINE WAS RETARDED TO IDLE POWER, VIBRATION CONTINUED FOLLOWED BY LOW OIL PRESS LIGHT AND EGT INCREASE TO 963 DEGREES C. ENGINE WASMar 16, 2008 · N505TA · Airbus A300B4203 · Engine (Turbine/Turboprop)SDR WRLA2008039Skin · corrodedDURING C-CHECK INSPECTION FOUND RIGHT WING UPPER SURFACE AT REAR SPAR, FROM XORS 264 TO XORS 480 SKIN CORRODED AT SEVERAL PLACES. REPAIRED RIGHT WING SURFACE AT REAR SPAR FROM XORS 264 - XORS 480 AT AREAS OF CORROSION PER ECRA 242NW-57-DC10-017.Mar 13, 2008 · N138WA · Doug DC1030 · Wing, Plate/SkinSDR WRLA2008037Panel · damagedDURING C-CHECK INSPECTION FOUND UPPER FWD RUDDER PANEL 376VL HAS 2EA SCREW HOLES ELONGATED. REPAIRED UPPER FWD RUDDER PANEL 376VL SCREW HOLES PER ECRA 242NW-55-DC10-014 AND ECRA, 242NW-55-DC10-015.Mar 7, 2008 · N138WA · Doug DC1030 · Rudder Miscellaneous StructureSDR WRLA2008038Panel · damagedDURING C-CHECK INSPECTION FOUND UPPER RUDDER PANEL 376RL 2EA SCREW HOLES DAMAGED. REPAIRED UPPER RUDDER PANEL 376RL SCREW HOLES PER ECRA 242NW-55-DC10-014, 242NW-55-DC10-015.Mar 7, 2008 · N138WA · Doug DC1030 · Rudder Miscellaneous StructureSDR WRLA2008033Bolt · shearedDURING C-CHECK INSPECTION FOUND RIGHT HAND MAIN LANDING GEAR WHEEL WELL INTERIOR OUTBOARD BULKHEAD STA 1481 30 INCHES BELOW THE HORIZONTAL BULKHEAD AFT SIDE OF THE VERTICAL SUPPORT BEAM HAS A BOLT HEAD SHEARED OFF. REAMED HOLE TO REMOVE THE DEFECT AND ACCOMPLFeb 29, 2008 · N138WA · Doug DC1030 · Fuselage Main, BulkheadSDR ARWA20080204Engine · stalledDURING ROTATION, NR 3 ENGINE SUFFERED COMPRESSOR STALL AND THE TOWER AND VICINITY AIRCRAFT NOTED FIRE COMING OUT OF ENGINE AFT END. REMOVED AND REPLACED NR 3 ENGINE IN ACCORDANCE WITH ARROW AIR WORK CARD 143R7101M AND DC-10 M/M 71-00-00. PERFORMED ENGINE RUNFeb 23, 2008 · N478CT · Doug DC1030F · Engine (Turbine/Turboprop)SDR WRLA2008036Skin Panel · corrodedDURING C-CHECK INSPECTION FOUND CORROSION ON THE FUSELAGE SKIN PANELS IN AREA OF THE WING TO BODY FAIRINGS AT LT STA 1531 TO 1821 BETWEEN L-35L AND L-46L AND RT STA 1531 TO 1700 BETWEEN L-43R AND L-46R. REMOVED LWR AFT RUB STRIPS FROM A/C AT AFT WING TO BODY Feb 23, 2008 · N138WA · Doug DC1030 · Fuselage Main, Plate/SkinSDR WRLA2008023Skin · corrodedDURING MAINTENANCE INSPECTION AT SAA, CORROSION FOUND ON CENTER WING UPPER SKIN LT SIDE, APPROX STA XCW101. REPAIRED PER SAA EA 010-5710-11-A0232 REV A.Feb 11, 2008 · N136WA · Doug DC1030 · Wing, Plate/SkinSDR WRLA2008024Doubler · corrodedDURING MAINTENANCE INSPECTION AT SAA, CORROSION FOUND BETWEEN SKIN PANEL DOUBLER AND DOOR JAMB DOUBLER NEAR STA 1704 BETWEEN LONGERONS 45R-46R. REPAIRED PER SAA EA 010-5330-11-A1230 REV NC.Feb 11, 2008 · N136WA · Doug DC1030 · Fuselage Main, Plate/SkinSDR WRLA2008034Skin · corrodedDURING C-CHECK INSPECTION FOUND CORROSION AT Y1531L AFT OF LT MLG WHEEL WELL OUTBOARD SIDE. REMOVED CORROSION AND REPAIRED AREA AT Y1531L AFT OF LT MLG WHEEL WELL OUTBOARD SIDE IAW ECRA 242NW-53-DC10-012.Feb 5, 2008 · N138WA · Doug DC1030 · Fuselage Main, Plate/SkinSDR WRLA2008035Skin · dentedDURING C-CHECK INSPECTION FOUND DENT ON THE FWD CARGO DOOR APPROX 12" FROM THE BOTTOM OF THE DOOR, OUT OF LIMITS PER DC10 SRM 53-20-00. REMOVED DAMAGE AND REPAIRED ON FWD CARGO DOOR APPROX 12" FROM THE BOTTOM OF THE DOOR PER ECRA 242NW-52-DC10-010 AND VOL II Jan 23, 2008 · N138WA · Doug DC1030 · Cargo/Baggage DoorsSDR WRLA2008013Indicator · malfunctionedKDOV/EDDP TAS/SAT INSTRUMENT OFF FLAGS APPEARED, 10 MINS LATER SMOKE EMINATED BRIEFLY FROM INSTRUMENT, TAS/SAT C/B PULLED CONDITION WENT AWAY, MX CONTROL ADVISED. REMOVED AND REPLACED TAS/SAT GAUGE, OPS NORMAL MM 34-15-00. DMI'S CLOSED.Jan 22, 2008 · N303WL · Doug DC1030F · Airspeed/Mach IndicatorSDR WRNA200700062B-Nut · looseAFTER LEVELING OFF AT 27,000' OBSERVED STEADY DECLINE IN OIL QUANTITY OF NUMBER 1 ENGINE, RETURNED TO FIELD AND MADE A SAFE LANDING, NO LOSS OF OIL PRESSURE. FOUND AND SECURED A LOOSE 'B' NUT AT AFT BEARING LINE, RE-SERVICED OIL AND ACCOMPLISHED LEAK CHECK, NDec 18, 2007 · N504TA · Airbus A300B4203 · Turbine Engine Oil SystemSDR WRLA2001129Cable Assy · misriggedDURING MAINTENANCE INSPECTION L4 PASSENGER DOOR FAILED PNEUMATIC TEST. RIGGED AIR RESERVOIR AIR RELEASE CABLE PER DC10 AMM 52-12-00 PAGE 534. ADJUSTED L4 DOOR EMERGENCY BACKLOCK PER DC10 AMM 52-12-00 PAGE 530A. PERFORMED PNEUMATIC TEST OF THE L4 DOOR PER DCDec 1, 2007 · N14075 · Doug DC1030 · Passenger/Crew DoorsSDR WRLA2008048Shear Tie · crackedDURING C CHECK INSPECTION, FOUND BULKHEAD SHEAR TIE CRACKED STA 2123 LBL 8. REPAIRED PER SRM 53-30-00 FIG 2B, REF SAA JOB NR 78326250001.Nov 27, 2007 · N137WA · Doug DC1030 · Fuselage Internal Mounting StructureSDR WRLA2008047Skin · crackedDURING C CHECK INSPECTION, FOUND FUSELAGE EXTERIOR SKIN PUNCTURED, CRACKED, CREASED AT RT NOSE JACKPAD POINT STA 593 L45R. REPAIRED PER SAA EA NR 010-5320-11-A1239.Nov 27, 2007 · N137WA · Doug DC1030 · Fuselage Main, Plate/SkinSDR WRLA2008046Shear Tie · crackedDURING C CHECK INSPECTION, FOUND UPPER TORQUE BOX AFT BULKHEAD STA 2123 RBL 8, SHEAR TIE CRACKED. REPAIRED PER SRM 53-30-00, REF SAA JOB NR 78326260001.Nov 23, 2007 · N137WA · Doug DC1030 · Fuselage Internal Mounting StructureSDR ARWA20071102Valve · erraticON INITIAL TAKEOFF ROLL, UPON ADVANCING THE POWER LEVERS TO MAX TAKEOFF THRUST NR 1 ENGINE REVERSER PRESSURE LIGHT ILLUMINATED; CANCELLED THE TAKEOFF. LIGHT WENT OUT WHEN POWER WAS REDUCED TO IDLE. REVERSER NR 1 PREVIOUS DEACTIVATED AND SECURED LOCK, TRANSFENov 20, 2007 · N524MD · Doug DC1030 · Engine Thrust ReverserSDR ARWA20071002Engine · vibrationDURING CLIMB-OUT, NR 3 ENGINE HEAVY VIBRATION. TROUBLESHOT NR 3 ENGINE PER TAFI 72-00-00; FOUND VIBRATION AT FUEL LEVER AND THROTTLE, OUT OF ADJUSTMENT. ADJUSTED FUEL LEVER PER DC-10 M/M 76-12-00 AND THROTTLE PER DC-10 M/M 76-11-00. OPERATIONAL CHECK NORMALOct 18, 2007 · N524MD · Doug DC1030 · Engine (Turbine/Turboprop)SDR UPS07M50788Fire Loop · shortedINSPECTION TYPE:N/A AFTER LANDING RECEIVED LVL 3 ENG 3 FIRE DET ALERT. FOLLOWED PROCEDURE W/FIRE AGENT DISCHARGED. REMOVED AND REPLACED NR 3 ENG UPPER FIRE DETECTOR LOOP ASSY PER MM 26-11-03-4. REMOVED AND REPLACED FDCU PER MM 26-11-02-4. P/N ON/OFF 8038-0Oct 1, 2007 · N260UP · Doug MD11F · Fire DetectionSDR WRLA2007101Ring · missingDURING C-CHECK FOUND NR 3 ENGINE FIRE EXTINGUISHING LINE JOINT RING MISSING. REF N/R 67308. 10-12-07 INSTALLED JOINT RING REF DC10 AMM 26-21-04 REV.81. LEAK CHECKED REF DC10 AMM 26-21-04-201 REV.81. Sep 26, 2007 · N303WL · Doug DC1030F · Extinguishing SystemSDR WRLA2007099Longeron Splice · crackedDURING C-CHECK FOUND LONGERON LT 44 JOINT SECTION AT STA 1986 CRACKED. N/R 67297. LONGERON JOINT REPLACED REF.BOEING DWG NGA6313 AND DC10 SRM VOL.1 53-30-00 FIG.5 REV. MAY 15/96.Sep 25, 2007 · N303WL · Doug DC1030F · Fuselage Main, Longeron/Stringer
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