Douglas DC-10-30F

Service difficulty reports · 1,152

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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 aircraft_model_key = 'DC1030F'
  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 97FDEA00719Connector · dirty97-0197 - WITH GEAR RETRACTED RED NOSE GEAR UNSAFE LIGHT ON F/E PANEL INTERMITTENT ON (NO LIGHT ON FWD PANEL) RECYCLED GEAR NO CHANGE. INSPECTED NOSE GEAR PROX SWITCHES FOR DAMAGE ALL OK PROX BOX. REMOVED AND CLEANED ELECTRICAL PINS GOOD BITE TEST NOW OK FOROct 8, 1997 · N319FE · Doug DC1030F · Landing Gear Position and WarningSDR WRLA97111Control Cable · out of adjDURING TAXI-OUT FOR TAKEOFF, FLIGHT CREW NOTED THE RIGHT OUTBOARD SPOILER DID N OT ACHIEVE FULL DEFLECTION DURING FLIGHT CONTROL CHECKS. FLIGHT CREW ELECTED TO RETURN TO GATE FOR MAINTENANCE ACITON. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTEOct 5, 1997 · N107WA · Doug DC1030F · Drag Control SystemSDR 97FDEA00642Control Cable · cutON POSTFLT CHECK, FOUND LT WING OUTBOARD SLAT NR 3 DRIVE EXTEND CABLE HAD BEEN CUT OFF. REMOVED AND REPLACED LEFT SLAT NR 3 DRIVE EXTEND CABLE PER MM 27-89-03-4 AND ADJUSTED SLAT SYSTEM PER MM 27-80-00-5. REMOVED AND REPLACED DAMAGED METAL SEALS FOR LT SLAT Sep 7, 1997 · N302FE · Doug DC1030F · Leading Edge Slat Control SystemSDR G6OA013Battery · dischargedWHILE ACCOMPLISHING GROUND CHECKS, THE FLIGHT CREW FOUND EMERGENCY LIGHTS WOULD NOT TEST. GROUND MAINTENANCE INVESTIGATED AND DETERMINED THE BATTERY POWER SUPPLY WAS INOPERATIVE. THE BATTERY POWER SUPPLY WAS REPLACED IAW DC-10 MM 33-51-01. (X)Aug 5, 1997 · N603GC · Doug DC1030F · Emergency LightingSDR G6OA12Control Linkage · lack of lubeDURING APPROACH CONFIGURATION AT 2,500 FEET, FLAP LIMIT CHANNEL INOP LIGHT ON AT FLIGHT ENGINEER'S PANEL. FLAP HANDLE COULD NOT BE MOVED FROM ZERO AFTER OVERRIDE WAS SELECTED. FLIGHT CREW DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. GROUND MAINTENANCE CLEJul 18, 1997 · N601GC · Doug DC1030F · Trailing Edge Flap Control SystemSDR G6OA011Switch · missingDURING C-CHECK MAINTENANCE, A PASSENGER OXYGEN CHECK WAS ACCOMPLISHED. THE LAVATORY OXYGEN MASK FAILED TO DEPLOY AT 14,440 FEET ALTITUDE. INVESTIGATION REVEALED THE ANEROID SWITCH HAD NOT BEEN INSTALLED. IT WAS DETERMINED THE ANEROID SWITCH AND ITS ASSOCIATEJun 27, 1997 · N603GC · Doug DC1030F · Passenger Oxygen SystemSDR G6OA010Engine · failedGVA - AT LIFT OFF, CREW REPORTED A LOUD BANG FOLLOWED BY VIBRATION, N1, AND N2 DECAYING, EGT RISE AND LOW FUEL FLOW INDICATIONS FOR NR 1 ENGINE. TOWER REPORTED LARGE FLAME FROM THE TAIL PIPE. NR 1 ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNEDJun 23, 1997 · N602GC · Doug DC1030F · Engine (Turbine/Turboprop)SDR G6OA009Battery · dischargedGROUND MAINTENANCE WHILE PERFORMING PREVENTIVE MAINTENANCE FOUND THE EMERGENCY LIGHT SYSTEM WOULD NOT TEST. THE SYSTEM WAS INVESTIGATED AND THE BATTERY POWER SUPPLY WAS REPLACED IAW DC-10, MM 33-51-01. (X)Jun 4, 1997 · N600GC · Doug DC1030F · Emergency LightingSDR 97FDEA00283Switch · malfunctionUPON RETRACTION ON TAKEOFF, THE GEAR WARNING HORN AND ALL RED GEAR LIGHTS CAME ON STEADY. GEAR HANDLE WAS CYCLED DOWN AND WARNING LIGHTS AND HORN TURNED OFF. GEAR WAS RAISED AGAIN WITH NORMAL INDICATION. CHECKED ALL THREE THROTTLE SWITCHES FOR CONTINUITY. May 16, 1997 · N301FE · Doug DC1030F · Landing Gear Position and WarningSDR G6OA008Oil Line · looseSEL - AFTER TAKEOFF, CREW REPORTED LOSS OF OIL QUANTITY AND OIL PRESSURE FOR NR 1 ENGINE. THE NR 1 ENGINE WAS SHUT DOWN. AIRCRAFT RETURNED TO SEL AND LANDED WITHOUT FURTHER INCIDENTS. NO EMERGENCY WAS DECLARED. GROUND MAINTENANCE DURING INSPECTION OF NR 1 May 5, 1997 · N601GC · Doug DC1030F · Turbine Engine Oil SystemSDR 97FDEA00234Fire Bottle · malfunctionAFTER TAKEOFF, AGENT LOW LIGHT ILLUMINATED ON NR 2 ENGINE. FLIGHT RETURNED TO SFS AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE, NR 1 FIRE BOTTLE AND SQUIBS.Apr 16, 1997 · N310FE · Doug DC1030F · Extinguishing SystemSDR 97FDEA00225Switch · malfunctionALL 4 GEAR LIGHTS AT F/O AND S/O PANEL REMAINED RED AFTER RAISING HANDLE. RECYCLED TWICE TO GET LIGHTS TO GO OUT, FEFI 32-30AA. FELT LIKE GEAR CAME UP EACH TIME. SUSPECT INDICATION. ENT BY: 033247 RPT BY: 096524. REMOVED AND REPAIRED MICRO SWITCH IN LANDApr 8, 1997 · N312FE · Doug DC1030F · Landing Gear Position and WarningSDR 97FDEA00215Door · damaged97-0215 NRT STBD SIDE AIR CONDITIONING DOOR FOUND DAMAGE ON PREF LIGHT. CANNIBALIZED THE NR 3 AIR COND COMP DOOR ASSY BETWEEN A/C N313FE'S AIR COND COMP DOOR. DOOR OPERATION CHECKS OK.Apr 7, 1997 · N309FE · Doug DC1030F · Air Conditioning DoorsSDR 97FDEA00221Bracket · crackedLT WING, O/B L/E SLAT DRIVE MECHANISM, OUTER BRACKET ASSY HAS CRACK INDICATION IN FWD FLANGE FILLET RADIUS. EDDY CURRENT INDICATION.Apr 3, 1997 · N308FE · Doug DC1030F · Leading Edge Slat Control SystemSDR SCNA97065Bypass Valve · failedNR 2 PACK OVERHEATED AND WAS SHUT OFF. SMELLED SMOKE IN THE CABIN DUE TO HIGH PACK TEMPERATURES. PLACED NR 2 PACK ON MEL UNTIL REPLACEMENT OF NR 2 TURBINE BYPASS VALVE.Mar 8, 1997 · N601GC · Doug DC1030F · Cabin Cooling SystemSDR 97FDEA00065Proximity Unit · failedRIGHT MAIN LANDING GEAR LIGHT REMAINED ON RED AFTER GEAR RETRACTION ON TAKEOFF, F/O PANEL ONLY. GEAR WAS CYCLED DOWN AT BACK UP AND ALL INDICATIONS WERE NORMAL WITH RIGHT MAIN RED LIGHT OUT. REMOVED AND REPLACED PROXIMITY ELECTRONICS UNIT AS PER TAFI 32-30-0Jan 25, 1997 · N303FE · Doug DC1030F · Landing Gear Position and WarningSDR WRLA97004Strainer Light · illuminatedDURING TAXIING OUT, FLT CREW NOTICED NR 3 ENGIEN OIL STRAINER CLOG LIGHT ON. CREW ELECTED TO RETURN TO GATE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL PULLED OIL SCREEN AND NO DEBRIS WAS FOUND. REPLACED SCREEN. GROUND RUN EJan 18, 1997 · N107WA · Doug DC1030F · Engine Oil Indicating SystemSDR SCNA96434Oil System · overservicedHAD SMOKE IN FLIGHT COMPARTMENT. TURNED OFF NUMBER 1 PACK AND PROBLEM STOPPED. WHILE TROUBLESHOOTING, DRAINED 1 GALLON FROM OVERSERVICED NUMBER 2 ENGINE, OPS CHECKED GOOD.Dec 5, 1996 · N601GC · Doug DC1030F · Turbine Engine Oil SystemSDR 96FDEA01690Piccolo Tube · leakingAIRCRAFT WING ANTI-ICE SET UP FOR USE ON TAKEOFF, ABOUT 10 TO 15 SECONDS AFTER LIFT OFF. NR 1 MANIFOLD FAIL LIGHT ILLUMINATED. TURNING OFF WING ANTI-ICE TURNED OFF MANIFOLD FAIL LIGHT. TROUBLESHOT SYSTEM FOUND NR 5 LEFT HAND SLAT PICCOLO TUBE OUTBOARD END LNov 22, 1996 · N315FE · Doug DC1030F · Airfoil Anti/De-ice SystemSDR SCNA96378Engine · failedDURING CLIMB, EXPERIENCED EXTREME VIBRATION AND NUMBER 3 ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED. RETARDED NUMBER 3 ENGINE THROTTLES AND LIGHT EXTINGUISHED. AFTER SEVERAL MINUTES, OIL PRESSURE DROPPED RAPIDLY, ENGINE FIRE LIGHT ILLUMINATED AND SMOKE ENTERNov 11, 1996 · N602GC · Doug DC1030F · Engine (Turbine/Turboprop)SDR 96FDEA01651Anti-Ice Valve · malfunctionedAFTER TAKEOFF, THE NR 2 ANTI-ICE COWL DUCT FAIL LIGHT ILLUMINATED. A NOTE IN THE MEL FOR THE ANTI-ICE WRITE-UP SAID TO REDUCE NR 2 THROTTLE TO IDLE AND USE ONLY IN EMERGENCY CONDITION. COMPLIED. LIGHT WENT OUT WHEN THROTTLE WAS RETARDED. LIGHT ON APPROXINov 6, 1996 · N307FE · Doug DC1030F · Air Intake Anti/De-Ice SystemSDR SCNA96320Fire Loop · intermittantFIRE LOOP-B ON ENGINE NUMBER 2 ILLUMINATED INTERMITTANTLY DURING FLIGHT. TROUBLESHOT SYSTEM PER MM 26-11-03 AND FOUND CANNON PLUG P1-8004 PUSHED BACK. RESEATED PIN, CLEANED ALL CONNECTIONS AND OPS CHECKED SYSTEM.Oct 26, 1996 · N602GC · Doug DC1030F · Fire DetectionSDR SCNA96314Temp Controller · failedRIGHT WINDSHIELD ANTI-ICE POPPED CIRCUIT BREAKER. THE SMELL OF SMOKE OCCURRED BREIFLY AND THEN DISSIPATED. SECURED WINDOW ANTI-ICE. REMOVED AND REPLACED WINDSHIELD TEMPERATURE CONTROLLER.Oct 17, 1996 · N601GC · Doug DC1030F · Windshield/Door Rain/Ice RemovalSDR 96FDEA01574Actuator · malfunctionedON TAKEOFF, THE NOSE LIGHT ON BOTH PANELS REMAINS RED. HYD SYS 3 WAS NORMAL, RAN THE RED TAB PROCEDURES AND LANDING GEAR SHOWED 4 GEAR LIGHT WITH GEAR HANDLE DOWN. TRIED TO RAISE THE GEAR AGAIN WITH NO SUCCESS, RED LIGHT STILL ON WITH HANDLE UP. LOWERED GEAOct 11, 1996 · N302FE · Doug DC1030F · Landing Gear ActuatorSDR 96FDEA01565Control Handle · lack of lubeWHEN GEAR SELECTED DOWN BOTH PILOTS AND S/O PANEL IND FOUND RED LIGHTS. RAN RED TAB PROCEDURE, PER CHECKLIST WHEN ALTERNATE GEAR HANDLE RAISED, GOT FOUR GEAR DOWN GREEN LIGHTS BOTH PANELS. LANDED DOV WITHOUT INCIDENT. MX FOUND LANDING GEAR LEVER NOT RETRACTOct 5, 1996 · N307FE · Doug DC1030F · Landing Gear SelectorSDR WRLA96041Fuel Filter · cloggedDURING TAXIING OUT, FLIGHT CREW NOTED NR 2 ENGINE FUEL FILTER PRESSURE DROP LIGHT ON, AIRCRAFT RETURNED TO GATE. MAINTENANCE PERSONNEL REPLACED FUEL FILTER, GROUND RUN THE AIRCRAFT, NO FAULT NOTED. AIRCRAFT RETURNED TO SERVICE. (M)Oct 2, 1996 · N107WA · Doug DC1030F · Engine Fuel DistributionSDR 96FDEA01516Skin · corrosionSNRM 6022, RT WING AT STA XCW118 TOP SURFACE OF WING HAS HEAVY CORROSION JUST FWD OF R3 DOOR. *S/D* BURNISHED CORROSION CK BY NDT AND FOUND TO BE WITHIN LIMITS PER SRM 57-10-00 FIG 61. TREATED, PRIMED.Sep 20, 1996 · N318FE · Doug DC1030F · Wing, Plate/SkinSDR 96FDEA01489Hi-Lock Collars · missingSNRM NR 0352, VERTICAL STABILIZER ALL COLLARS MISSING FROM HI-LOCKS BETWEEN AFT H-11 BOLTS THAT ATTACH UPPER VERICAL STABILIZER TO LOWER VERTICAL STABILER. REF LAX C-CH-02, SNRM NR 0352.Sep 16, 1996 · N322FE · Doug DC1030F · Vertical StabilizerSDR SCNA96253Smoke Detector · malfunctionedOBSERVED A MOMENTARY LOWER CARGO FIRE INDICATION. CHECKED FORWARD CARGO SMOKE DETECTOR IN ACCORDANCE WITH TAFI 26-14-00, CLEANED PLUG AND TESTED SEVERAL TIMES ON GROUND.Sep 15, 1996 · N602GC · Doug DC1030F · Smoke DetectionSDR 96FDEA01490Tension Strap · crackedSMRM NR 00506, RT WING, O/B FLAP I/B HINGE O/B SIDE TENSION STRAP IS CRACKED AT THE LOWER BOLT HOLE LOWER FLANGE. *S/D* REMOVED AND REPLACED TENSION STRAP BRACKET AS PER SRM 51-00-01 VOL NR I.Sep 14, 1996 · N322FE · Doug DC1030F · Wing Miscellaneous StructureSDR 96FDEA01476Prox Control · malfunctionedON TAKEOFF, AFTER GEAR UP RIGHT MAIN GEAR RED LIGHT ILLUMINATED ON BOTH FRONT AND S/O PANEL RECYCLED GEAR AND LIGHT WENT OUT ON APPROACH TO ATL BEFORE GEAR DOWN RIGHT MAIN GEAR LIGHT AGAIN ILLUMNA, ON FRONT PANEL ONLY S/O PANEL NO LIGHT FACT 11SEP96 22:30 ATSep 13, 1996 · N303FE · Doug DC1030F · Landing Gear Position and WarningSDR SCNA96247Smoke Detector · inoperativeDURING LINE CHECK, NUMBER 3 LOWER AFT CARGO SMOKE DETECTOR DID NOT TEST. RELAMPED AND TESTED NORMAL.Sep 7, 1996 · N603GC · Doug DC1030F · Smoke DetectionSDR 96FDEA01435V-Panel · missingUPON WALK AROUND, FOUND THE V-PANEL ON NR 3 ENGINE PYLON RIPPED AWAY. INSTALLED V-PANEL ON PYLON FARING. ALSO, REPAIRED DAMAGED PYLON FARING HONEYCOMB PANEL OUTBOARD PER DC-10 STRUCTURE REPAIR MANUAL 51-10-00.Sep 4, 1996 · N322FE · Doug DC1030F · Nacelle/Pylon StructureSDR SCNA96242Smoke Ind Light · inoperativeLOWER AFT CARGO SMOKE DETECTOR NR 4 DOES NOT TEST ON ENGINEERS PRE-FLIGHT. RELAMPED LOWER AFT CARGO SMOKE DETECTOR NR 4 IN ACCORDANCE WITH MM 26-14-01. OPS CHECKED GOOD.Aug 31, 1996 · N600GC · Doug DC1030F · Smoke DetectionSDR SCNA96241Slide Assy · inoperativeTHE L1 DOOR SLIDE REMOTE PRESS-TO-TEST INDICATOR LIGHT STAYS ON. BOTTLE PRESSURE CHECKS OK. REPLACED L1 DOOR SLIDE ASSEMBLY PER MM 52. INSPECTED SLIDE INSTALLATION AND OPS CHECKED REMOTE TEST SYSTEM.Aug 29, 1996 · N600GC · Doug DC1030F · Escape SlideSDR SCNA96238Bulb · inopFOUND LOWER AFT CARGO SMOKE DETECTOR NR 2 WILL NOT TEST. REPLACED BULB ON LOWER AFT CARGO SMOKE DETECTOR AND OPS CHECKED IN ACCORDANCE WITH MM 26-00-00.Aug 26, 1996 · N601GC · Doug DC1030F · Smoke DetectionSDR 96FDEA01397Lock Sensor · malfunctionedON T/O, NOSE GEAR WOULD NOT INDICATE UP AND LOCKED ON BOTH FRONT AND S/OS PANEL. CYCLED GEAR SEVERAL TIMES WITH NO UP AND LOCKED INDICATION. DOWN AND LOCKED OK, COMPLIED WITH RED TABS, DUMPED LANDED. VISUALLY INSPECTED NOSE GEAR AND DOOR, NO DAMAGED NOSE LAAug 25, 1996 · N302FE · Doug DC1030F · Landing Gear Position and WarningSDR SCNA96240Connectors · dirtyNR 2 FIRE LOOP-A WAS FLASHING DURING DESCENT AND APPROACH. CLEANED CONNECTOR, CHECKED LOOP-A SYSTEM FOR SHORTS. NO SHORTS FOUND, OPS CHECKED GOOD.Aug 24, 1996 · N603GC · Doug DC1030F · Fire DetectionSDR SCNA96239Smoke Detector · broken wireFOUND BULK COMPARTMENT SMOKE DETECTOR TEST BULB WIRE BROKEN. SOLDERED BROKEN WIRE AND SMOKE DETECTOR OPS CHECKED GOOD.Aug 24, 1996 · N601GC · Doug DC1030F · Smoke DetectionSDR SCNA96214O-Ring · cutDURING FLIGHT NOTICED THAT THE NUMBER 2 ENGINE OIL QUANTITY WAS AT 0 AND THE OIL PRESSURE WAS FLUCTUATING BETWEEN 20 PSI AND 40 PSI. AFTER MONITORING, THE OIL PRESSURE DROPPED BELOW RED LINE AND NUMBER 2 OIL PRESSURE LIGHT ILLUMINATED. NUMBER 2 ENGINE WAS SHAug 7, 1996 · N603GC · Doug DC1030F · Hydraulic Pump (Electric/Engine), MainSDR SCNA96203Gear Indication · malfunctionedFOUND ENGINEER'S PANEL LANDING GEAR INDICATOR SHOWING UNSAFE ON RIGHT MAIN. GROUND OPS TESTED NORMAL.Jul 24, 1996 · N602GC · Doug DC1030F · Landing Gear Position and WarningSDR SCNA96201Indicator · inoperativeFOUND CENTER LANDING GEAR INDICATION INOP AT PILOTS AND FLIGHT ENGINEERS STATIONS. REPLACED CENTER GEAR ANNUNCIATOR ON FLIGHT ENGINEER PANEL AND RELAMPED FIRST OFFICERS CENTER GEAR LIGHT.Jul 21, 1996 · N601GC · Doug DC1030F · Landing Gear Position and WarningSDR 96FDEA01198Warning Light · illuminatedDURING CLIMBOUT, AIR COND DOORS LIGHT ILLUMINATED INTERMITTENTLY. AS AIRSPEED INCREASED TO 300 KTS LIGHT ILLUM, STEADY ON DESCENT, LIGHT EXTINGUISHED BELOW 250 KTS. AIRCRAFT RELEASED FOR SERVICE PER MEL/CDL 52-4 CATEGRORY C EXPIRATION, 17 JULY 96. INSPECTEDJul 8, 1996 · N305FE · Doug DC1030F · Air Conditioning DoorsSDR 96ZZZX3858Drive Motor · failedDOOR 4L FAILED TO OPEN IN EMERGENCY MODE DURING DITCHING DEMONSTRATION. TROUBLESHOOTING FOUND THE FAILURE OCCURRED IN THE PNEU DRIVE MOTOR. PNEU DRIVE MOTOR IS 'ON CONDITION' WITH OPS CHECK DUE IN 1,000-HOUR INTERVALS.Jun 28, 1996 · N10MB · Doug DC1030F · Passenger/Crew DoorsSDR 96FDEA01157Door · out of adjustVCP: BOTH CABIN DOORS DID NOT SEAL AND A/C WOULD NOT PRESSURIZE. ADJUSTED DOORS PER MM 52-11-00, PG 520. PRESSURED A/C USING APU, LEAK CHECKED OK.Jun 19, 1996 · N302FE · Doug DC1030F · Passenger/Crew DoorsSDR 96FDEA01038Indication · malfunctionedAFTER GO-AROUND, NOSE GEAR RED LIGHT ON AT BOTH PANELS WITH HANDLE UP, HYD SYS-3 NORMAL. PUT HANDLE DOWN AND BOTH LIGHTS GREEN ON NOSE GEAR. PERFORMED BITE CHECK ON PROXIMITY BOX, FOUND NO DEFECTS. PERFORMED GEAR RETRACTION TEST PER MM 32-60-00, UNABLE TO DMay 29, 1996 · N302FE · Doug DC1030F · Landing Gear Position and WarningSDR 96FDEA1020Hyd Pump · leakingTOTAL LOSS OF HYDRO SYSTEM NR 3 ON CLIMBOUT, PERFORMED RED TAB PROCEDURE AND LANDED 35/EXT 16L SEA WITHOUT INCIDENT. MAINTENANCE FOUND 2/3 REVIISABLE MOTOR PUMP LEAKING. REMOVED AND REPLACED 2/3 REVIISABLE MOTOR PUMP PER M/M 29-22-01, LEAK AND OPS CHECK GOODMay 22, 1996 · N319FE · Doug DC1030F · Hydraulic Pump (Electric/Engine), MainSDR 96FDEA00998Stringer · crackedRIGHT WING STR 41 OUTBOARD HOLE HAS VERTICAL CRACK AT 2 O/C POSITION INTO UPPER STR RADIUS APPROX .3125 INCH LONG. REF: EO 8-5710-7-4310.May 17, 1996 · N304FE · Doug DC1030F · Wing, Longeron/StringerSDR 96FDEA00975Spar Chord · shearedSNRM 4358, NR 3 PYLON UPPER LT SPAR CHORD AFT AREA EXHIBITS TWO SHEARED HOCK BOLTS HEADS INSIDE PYLON.May 15, 1996 · N304FE · Doug DC1030F · Nacelle/Pylon StructureSDR 96FDEA00974Spar Chord · shearedSNRM 4145, NR 1 PYLON UPPER SPAR WEB STA 363, 1 FASTENER HEAD HAS SHEARED OFF.May 15, 1996 · N304FE · Doug DC1030F · Nacelle/Pylon Structure
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