Douglas DC-8F-54

Service difficulty reports · 194

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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 = 'DC8F54'
  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 97ZZZX714Fitting · crackedDURING ROUTINE INSPECTION, FOUND RIGHT MLG FITTING CRACKED BEYOND FLYABLE LIMITS. AIRCRAFT PLACED ON INACTIVE STATUS PENDING REPLACEMENT OF FITTING.Dec 7, 1996 · N7046H · Doug DC8F54 · Wing, Landing Gear Attach FittingsSDR ZIAA96074Connector · dirtyMHR - DURING CLIMB-OUT, NR 3 ENGINE FIRE WARNING CAME ON. SHUT DOWN THE ENGINE, DISCHARGED BOTH RIGHT WING FIRE BOTLES. RETURNED TO MHR. INSPECTED ENGINE, FOUND NO EVIDENCE OF FIRE. INSPECTED FIRE DETECTION SYSTEM AND CLEANED CONNECTOR ON LOWER LOOP. RESIDec 4, 1996 · N8041U · Doug DC8F54 · Fire DetectionSDR RRXA96168Hyd Line · failedDURING CRUISE HYDRAULIC QUANTITY DROPPED TO AUX LEVEL. HYDRAULIC LOSS QRH PROCEDURE WAS CALLED OUT. MAINTENANCE REMOVED AND REPLACED THE RETURN LINE TO THE NR 3 ENGINE HYDRAULIC PUMP, OPERATIONAL CHECK OF THE SYSTEM WAS GOOD.Dec 4, 1996 · N992CF · Doug DC8F54 · Hydraulic System, MainSDR CKSA96191Lockout Cylinder · reqd serviceWHEN 35 DEGREES FLAPS WERE SELECTED, FLAPS CAME DOWN TO 25 DEGREES, MISSED APPROACH. SELECTED FLAPS 35 DEGREES, FLAPS CAME DOWN TO 25 DEGREES UNTIL AIRCRAFT SLOWED TO 145 KIAS, THEN FLAPS LOWERED TO 35 DEGREES. BLED AND SERVICED FLAP LOCKOUT CYLINDER PER MM Oct 30, 1996 · N806CK · Doug DC8F54 · Trailing Edge Flap Control SystemSDR CKSA96188Skin · puncturedON WALKAROUND, FOUND HOLE IN SIDE OF AIRCRAFT AT STATION 480 JUST AFT OF A-PIT. AIRCRAFT REPAIRED PER SRM 53-4-0, 53-2-1 WITH A CLASS TWO REPAIR, REFERENCE EA 96-296. REINSPECT WITHIN 12,000 CYCLES, REPETITIVE INSPECT AT 4,000 CYCLES THEREAFTER.Oct 23, 1996 · N806CK · Doug DC8F54 · Fuselage Main, Plate/SkinSDR 96ZZZM1441Switch · roller missingAFTER TAKEOFF MIA, RIGHT MAIN GEAR LIGHT UNSAFE LIGHT ON AFTER GEAR RETRACTION. FOLLOWED ABNORMAL PROCEDURES AND LIGHT STAYED ON. RETURNED TO MIA AND MADE LANDING WITHOUT INCIDENT. FOUND RIGHT DOOR LATCH SWITCH ROLLER MISSING. REPLACED SWITCH CHECKS OK PEROct 21, 1996 · N426FB · Doug DC8F54 · Landing Gear Position and WarningSDR TC8A96066Bulb · malfunctionedCARGO SMOKE LIGHT CAME ON DURING FLIGHT WITHOUT ANY VISIBLE SMOKE IN THE CARGO COMPARTMENT. RELAMPED NR 2 SMOKE DETECTOR, SYSTEM OPS CHECKS NORMAL AS PER MM 26-10-5.Oct 17, 1996 · N802CK · Doug DC8F54 · Smoke DetectionSDR TC8A96065Fire Wire · brokenNUMBER 1 ENGINE FIRE WARNING OPERATING IN AN INTERMITTENT MANNER. REPAIRED BROKEN WIRE AT FIRE WALL DOOR LOOP PLUG, SYSTEM OPS CHECKS NORMAL AS PER MM 26-10-1.Oct 17, 1996 · N802CK · Doug DC8F54 · Fire DetectionSDR TC8A96064Bleed Valve · malfunctionedNUMBER 3 ENGINE VERY SLOW TO ACCELERATE. REMOVED AND REPLACED NUMBER 3 ENGINE INTERSTAGE BLEED VALVE, ENGINE RUN-UP IAW MM CHAPTER 72-00, ALL PARAMETERS WERE NORMAL.Oct 16, 1996 · N802CK · Doug DC8F54 · Compressor Bleed ValveSDR RRXA96134Skin · corrodedDURING A DROP IN MAINTENANCE INSPECTION, FOUND CORROSION DAMAGE TO LAV SERVICE PORT INNER SKIN DOUBLER PAST LIMITATIONS IAW DC-8 SRM, AT Y=330 AND LONGERON 25 RIGHT. INSTALLED REPAIR DOUBLER IAW DER APPROVED ENGINEERING SKETCH B46-R01, TREATED AREA IAW DC-8 SOct 14, 1996 · N992CF · Doug DC8F54 · Fuselage Main, Plate/SkinSDR 96ZZZX5871Spar · crackedDURING C-CHECK INSPECTION, FOUND NR 1 PYLON UPPER OUTBOARD SPAR CRACKED. REMOVED AND REPLACED NR 1 PYLON UPPER OUTBOARD SPAR IAW DOUGLAS DRAWING 5895081. (X)Oct 8, 1996 · N57FB · Doug DC8F54 · Nacelle/Pylon StructureSDR 96ZZZX5627Spar · crackedDURING C-CHECK INSPECTION, FOUND NR 1 PYLON UPPER OUTBOARD SPAR CRACKED. REMOVED AND REPLACED NR 1 PYLON UPPER OTBD SPAR IAW DOUGLAS DRAWING 5895081.Oct 8, 1996 · N57FB · Doug DC8F54 · Nacelle/Pylon StructureSDR 96ZZZM1429Hyd Line · rupturedON APPROACH MIA, EXPERIENCED LOSS OF HYDRAULIC QUANTITY. COMPLETED EMERGENCY CHECKLIST AND LANDED MIA WITHOUT INCIDENT. INSPECTION REVEALED RUPTURED HYDRAULIC LINE AT NR 2 HYD PUMP. REPLACED BOTH HYDRAULIC PUMPS AND LINE. AIRCRAFT RETURNED TO SERVICE. (M)Oct 4, 1996 · N7046H · Doug DC8F54 · Hydraulic System, MainSDR RRXA96088Retract Mech · malfunctionedLANDING GEAR WOULD NOT RETRACT AFTER TAKE0FF. AIRCRAFT MADE SUDDEN HARD PULL TO LEFT JUST BEFORE ROTATION. INSPECTED LANDING GEAR, NO DEFECTS NOTED. OPS CHECKED LANDING GEAR LEVER GOOD IAW MM CH 32-6-1, OPS CHECK GOOD ON GEAR SWING.Oct 3, 1996 · N991CF · Doug DC8F54 · Landing Gear Retraction/Extension SystemSDR 96ZZZX5795Link Rod · wornAFTER TAKEOFF MIAMI AND GEAR RETRACTION, EXPERIENCED VIBRATION IN NOSE GEAR AREA. RETURNED TO MIA. MADE LANDING WITHOUT INCIDENT. INSPECTION REVEALED LEFT NOSE LANDING GEAR DOOR OPEN AND FORWARD DOOR LINK STRUT WOULD NOT LOCK DOOR IN UP POSITION. REPLACED Sep 25, 1996 · N54FA · Doug DC8F54 · Landing Gear Door Retract SectionSDR TC8A96057Tr Line · looseNR 2 ENGINE FIRE WARNING, SECURED ENGINE. FOUNDED PNEUMATIC LINES LOOSE AT AFT REVERSER AREA. TIGHTENED LINES, RAN UP TO T/O POWER 1.83 EPR, COULD NOT DUPLICATE THE ITEM MM 78-7-0 AND 71-00.Sep 1, 1996 · N802CK · Doug DC8F54 · Engine Thrust ReverserSDR TC8A96056Fire Sensor · looseNR 2 FIRE INDICATION AFTER TAKEOFF, C/W TCA QRH-2 CHECKLIST, RETURNED TO GRU. FOUND LT FWD COWLING SENSOR LOOP CLAMP LOOSE. TIGHTENED, CHECKED FOR PNEUMATIC LEAKS, RAN THE ENGINE AS PER MM 26-10-0, OPS NORMAL.Aug 31, 1996 · N802CK · Doug DC8F54 · Fire DetectionSDR 96ZZZM1289Ballast · defectiveAFTER LANDING MIAMI, INSTRUMENT WHITE LIGHT BALLAST STARTED TO SMOKE. PULLED CIRCUIT BREAKER. INSPECTION REVEALED DEFECTIVE BALLAST. REPLACED BALLAST AND RETURNED AIRCRAFT TO SERVICE.Aug 18, 1996 · N426FB · Doug DC8F54 · Flight Compartment LightingSDR TC8A96054Tire · blewNR 6 TIRE BLEW DURING TAXI, AIRCRAFT NOT MOVED AFTER TIRE BLEW. REMOVED AND REPLACED NR 6 TIRE IAW DC-8 MM 32-40-1. BRAKE INSPECTED FOR FREEDOM OF MOVEMENT AND BLED. TIRE BLEW DUE TO BRAKE DRAGGING.Aug 14, 1996 · N802CK · Doug DC8F54 · TireSDR 96ZZZM1247Rod Assy · brokenAFTER TAKEOFF, PARAMARIBO, EXPERIENCED LOUD NOISE AND SLIGHT VIBRATION IN NOSE AREA. DIVERTED TO POS AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED A BROKEN ROD ASSY AT THE STRUT END ON THE AFT RIGHT NOSE GEAR DOOR. REPLACED ROD ASSEMBLY, PERFORMED GEAR SAug 6, 1996 · N426FB · Doug DC8F54 · Landing Gear Door Retract SectionSDR TC8A96050Pressurization · malfunctionDISCREPANCY: UNABLE TO MAINTAIN CABINPRESSURIZATION. CORRECTIVE ACTION: FOUND AFT L/H PAX DOOR NOT SECURE.SECURED DOOR OPS CHECK GOOD.Jul 30, 1996 · N802CK · Doug DC8F54 · Cabin Pressure Control SystemSDR TC8A96049Engine · failedDISCREPANCY: NR 3 ENGINE VIBRATION ON CLIMB-OUT. AIRCRAFT YAWED AND EPR DROPPED. IN-FLIGHT SHUT DOWN COMPLETED. CSD DISCONNECTED. CORRECTIVE ACTION: REMOVED AND REPLACED NR 3 ENGINE, CHECK GROUND OPS RUN-UP OK IAW MM 71-00.Jul 25, 1996 · N802CK · Doug DC8F54 · Engine (Turbine/Turboprop)SDR 96ZZZX3635Clevis · crackedDURING C-CHECK INSPECTION, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE INBOARD FLAP. REPAIRED CLEVIS BY INSTALLING A 2.0 INCH BY 2.0 INCH DOUBLER MADE OF .125 A1S1 301 1/2 H MATERIAL IAW EO 960511. 8110-3 ISSUED BY DER SW-713.Jul 5, 1996 · N426FB · Doug DC8F54 · Trailing Edge FlapsSDR 96ZZZX3634Clevis · crackedDURING C-CHECK INSPECTION, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE LOWER TANG OF THE RIGHT WING INBOARD FLAP LOWER CLEVIS. REPAIRED CLEVIS BY INSTALLING A 2.0 INCH BY 2.0 INCH DOUBLER MADE OF .125 A1S1 301 1/2 H MATERIAL IAW EO 9606181. 8110-Jul 5, 1996 · N426FB · Doug DC8F54 · Trailing Edge FlapsSDR 96ZZZM1229Clevis · crackedDURING C-CHECK INSPECTION, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE LOWER TANG OF THE RIGHT WING INBOARD FLAP LOWER CLEVIS. REPAIRED CLEVIS BY INSTALLING A 2 INCH BY 2 INCH DOUBLER MADE OF .125 A1S1 301 1/2 H MATERIAL IAW EO 9606181. 8110-3 ISJul 5, 1996 · N426FB · Doug DC8F54 · Trailing Edge FlapsSDR 96ZZZM1228Clevis · crackDURING C-CHECK INSPECTION, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE LOWER TANG OF THE CLEVIS ON THE LEFT WING INBOARD FLAP. REPAIRED CLEVIS BY INSTALLING A 2 INCH BY 2 INCH DOUBLER MADE OF .125 A1S1 301 1/2 H MATERIAL IAW EO 960511. 8110 ISSUEJul 5, 1996 · N426FB · Doug DC8F54 · Trailing Edge FlapsSDR ZIAA96019Engine Mount · brokenLAX - DURING MAINTENANCE ON NR 4 ENGINE FOUND ENGINE AFT MOUNT, LEFT ARM, THREADED PORTION BROKEN OFF. REPLACED THE ARM WITH A SERVICEABLE PART TIME ON MOUNT SINCE LAST SHOP VISIT, 319 HOURS AND 78 CYCLES. (M)Jun 27, 1996 · N8052U · Doug DC8F54 · Engine Mount SectionSDR 96ZZZM1007Cover · detachedAFTER TAKEOFF SJU EXPERIENCED RUMBLING NOISE IN NOSE WHEEL WELL. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED COVER CURTAINS INSIDE NOSE WHEEL WELL WERE DETACHED. SECURED CURTAINS AND RETURNED AIRCRAFT TO SERVICE. (M)May 25, 1996 · N54FA · Doug DC8F54 · Accessory CompartmentSDR ZIAA96016Detection Loop · chafedHUF - DURING CLIMB-OUT, SHUT DOWN NR 4 ENGINE DUE TO FIRE WARNING INDICATION. VISUALLY INSPECTED, FOUND UPPER DETECTION LOOP CHAFED. REPLACED DETECTION LOOP. OPERATIONAL CHECKED GOOD. NO EVIDENCE OF FIRE FOUND. (M)May 16, 1996 · N8042U · Doug DC8F54 · Fire DetectionSDR ZIAA96014Tr Seq Valve · leakingHUF - DURING CRUISE, SHUT DOWN NR 4 ENGINE DUE TO FIRE WARNING INDICATION. FOUND THRUST REVERSER SEQUENCE VALVE LEAKING AND BLOWING HOT AIR ON THE FIRE DETECTION LOOP. REMOVED AND REPLACED SEQUENCE VALVE. OPERATIONAL CHECK GOOD. (M)May 9, 1996 · N8042U · Doug DC8F54 · Engine Thrust ReverserSDR ZIAA96013Fire Warning · activatedLAX - DURING CLIMB-OUT, SHUT DOWN NR 4 ENGINE DUE TO FIRE WARNING INDICATION. VISUALLY INSPECTED, OHM'D AND CHECKED FIRE DETECTION LOOPS FOR SHORTS. ALL CHECKS FOUND SATISFACTORY. NO DEFECTS NOTED. NO EVIDENCE OF FIRE FOUND. (M)May 9, 1996 · N8042U · Doug DC8F54 · Fire DetectionSDR TC8A96043Connector · looseSBBG/SBBG - FLR 12403 - ON TAXI, CAPTAIN'S HORIZON GYRO FLAG INDICATED. TROUBLESHOT SYSTEM, FOUND LOOSE CANNON PLUG, RESET AND RE-TIGHTENED. OPS CHECKS OK. (X)May 5, 1996 · N802CK · Doug DC8F54 · Attitude Gyro and Indicating SystemSDR 96ZZZM1244Hyd Hose · rupturedON TAKEOFF MIA, NOTED LOSS OF HYDRAULIC QUANTITY. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED A RUPTURED HOSE ON THE RUDDER ACCUMULATOR. REPLACED HOSE, SERVICED HYD SYSTEM AND RETURNED AIRCRAFT TO SERVICE. (M)Apr 24, 1996 · N54FA · Doug DC8F54 · Hydraulic System, MainSDR 96ZZZM873Controller · overheatedIN CRUISE EXPERIENCED O-ZONE ODOR AND INTERMITTENT SMOKE FROM BEHIND INSTRUMENT PANEL WHEN AUTO-PILOT WAS ENGAGED. GROUND INSPECTION REVEALED AUTOPILOT CONTROLLER WAS SHORTED/OVERHEATED. REPLACED CONTROLLER AND AIRCRAFT RETURNED TO SERVICE.Apr 19, 1996 · N426FB · Doug DC8F54 · Autopilot SystemSDR TC8A96011Clamp · looseENGINE FIRE NR 3 AT FL 280, FIRE EXTINGUISHED. POST FLIGHT NR 3 ENGINE, NO FIRE DAMAGE DETECTED CONTRARY TO COCKPIT WARNING PROCEDURES. DETERMINED FIRE WARNING CAUSED BY LEAK AT PNEUMATIC DUCT ATTACHING CLAMP. REMOVED AND REPLACED CLAMP AND DID ENGINE RUN AMar 23, 1996 · N802CK · Doug DC8F54 · Fire DetectionSDR TC8A96010Wire · failedNR 3 ENGINE FIRE WARNING, NO FIRE. ISOLATED FIRE SENSOR ELEMENT ON AFT DOOR AND REPAIRED WIRES AT CANNON PLUG. CHECKED AS PER MM 26-0-3, OPS NORMAL. (M)Mar 22, 1996 · N802CK · Doug DC8F54 · Fire Protection System WiringSDR TC8A96007Clamp · looseNR 3 ENGINE FIRE WARNING LIGHT AND BELL COMES ON, PROCEED AS FOM. FOUND CLAMP LOOSE ON PNEUMATIC MANIFOLD TO PYLON. REPOSITIONED AND TIGHTENED CLAMP, OPS CHECK GOOD IAW DC-8 MM 36-0. (M)Mar 19, 1996 · N802CK · Doug DC8F54 · Fire DetectionSDR 96ZZZX1688Ballast · shortedON CLIMB-OUT MIAMI, EXPERIENCED BURNING ELECTRICAL ODOR WITH SMOKE COMING FROM FIRST OFFICER'S FLOOR PANEL. RETURNED TO MIAMI AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED LIGHT BALLAST TRANSFORMER SHORTED IN PEDESTAL. REPLACED BALLAST AND RETURNED AIRCRMar 12, 1996 · N54FA · Doug DC8F54 · Flight Compartment LightingSDR TC8A96003Clamp · looseSBCF/SBGR - FLT 03301 - FALSE ENGINE FIRE ALARM NR 3. TIGHTENED CLAMP AT STARTER VALVE, CHECKED IAW 80-1-0, NORMAL. (X)Feb 3, 1996 · N802CK · Doug DC8F54 · Engine Start Valves/ControlsSDR TC8A96002Fire Loop · malfunctionedSBGR - FL 02604 - FALSE FIRE ALARM ON NR 3 ENGINE ON MCT (MAXIMUM CONTINUOUS TAKEOFF). ISOLATED ENGINE FIRE LOOP. CHECKED PER MM 26-2-0. (X)Jan 27, 1996 · N802CK · Doug DC8F54 · Fire DetectionSDR TC8A96001Pneumatic Line · looseSBGR/SBGR - FLT 2405 - NR 1 ENGINE FIRE ALARM CAME 'ON' DURING CLIMB, SHORTLY AFTER TAKEOFF. TIGHTENED PNEUMATIC LINE AT AFT REVERSER SYSTEM. CHECK OPS OK IAW MM 78-02. (X)Jan 25, 1996 · N802CK · Doug DC8F54 · Pneumatic Distribution SystemSDR 96ZZZX222Hose · leakingSJU - DURING CLIMB, EXPERIENCED LOSS OF HYDRAULIC FLUID AND QUANTITY. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED A PIN HOLE IN THE PRESSURE HOSE TO THE RUDDER STANDBY HYDRAULIC PUMP. REPLACED HYDRAULIC PRESSURE HOSE AND RETURNED AIRCRADec 16, 1995 · N54FA · Doug DC8F54 · Hydraulic System, MainSDR 96ZZZX221Fuse Holder · failedMIA - ON APPROACH MIA, EXPERIENCED STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT. INSPECTION REVEALED A BLOWN 2-AMP FUSE IN THE PILOT'S OVERHEAD PANEL. REPLACED DEFECTIVE FUSE HOLDER AND RETURNED AIRCRAFT TO SERVICE.Dec 12, 1995 · N7046H · Doug DC8F54 · Flight Compartment LightingSDR 96ZZZM1119Frame · corrosionDURING D-CHECK INSPECTION, FOUND CORROSION WAS FOUND ON THE FORWARD CIRCUMFERENCIAL FRAME AT FS 310 BETWEEN LONGERON 29L AND 34L. CUT OUT THE DAMAGED FRAME BY CUTTING MIDWAY BETWEEN LONGERON 28L AND 29L AND BETWEEN LONGERON 34L AND 35L. REPLACED WITH AN IDENNov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Main, FrameSDR 96ZZZM1118Angle · corrosionDURING D-CHECK INSPECTION, FOUND CORROSION ON THE CENTER TANK LOWER END ANGLE AT FS 700 LEFT. CUT OFF THE LOWER 9 INCHES OF MATERIAL FROM THE ANGLE AND INSTALLED A SPLICE ANGLE OF .125 17-7PH TH1050 MATERIAL IAW EO 9508081. 8110-3 ISSUED BY DER SW-713. (M)Nov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Miscellaneous StructureSDR 96ZZZM1117Floor Beam · corrosionDURING D-CHECK INSPECTION, CORROSION WAS FOUND ON THE LOWER FORWARD AND AFT FLANGES OF THE FLOOR BEAM AT STATION 877. REMOVED ALL CORROSION AND BLENDED TO A 63 MICRO INCH FINISH. INSTALLED TWO 24.0 INCH .063 AISI 301 1/2H DOUBLER IAW EO 9503211. 8110-3 ISSUNov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Main, Floor BeamSDR 96ZZZM1116Skin · corrosionDURING D-CHECK INSPECTION, CORROSION WAS FOUND ON THE UPPER AND LOWER SKIN CENTER SKIN PANELS OF THE RT ELEVATOR FROM STATION XE 133 TO STATION XE 246. REMOVED THE DAMAGED SKIN PANELS FROM THE ELEVATOR AND INSTALLED A NEW IDENTICAL SKIN PANEL OF .040 2024-T3 Nov 24, 1995 · N54FA · Doug DC8F54 · Elevator, Plate/SkinSDR 96ZZZM1115Skin · corrosionDURING D-CHECK INSPECTION, CORROSION WAS FOUND ON THE UPPER AND LOWER INBOARD SKIN PANELS OF THE RT ELEVATOR FROM STATION XE 32 TO STATION XE 133. REMOVED EACH DAMAGED SKIN PANELS FROM THE ELEVATOR AND INSTALLED A NEW IDENTICAL SKIN PANEL OF .040 2024-T3 IAE Nov 24, 1995 · N54FA · Doug DC8F54 · Elevator, Plate/SkinSDR 96ZZZM1114Skin · corrosionDURING D-CHECK INSPECTION, CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER UPPER AND LOWER SURFACES OF SKIN FROM STATION XE 221 TO XE 272. REMOVED THE DAMAGED UPPER AND LOWER SKIN PANELS AND FABRICATED PANELS OF .808 7075-T6 MATERIAL. ALSO, REPLACED EACH BEANov 24, 1995 · N54FA · Doug DC8F54 · Horizontal Stabilizer, Plate/SkinSDR 96ZZZM1113Skin · corrosionDURING D-CHECK INSPECTION, CORROSION WAS FOUND ON LEFT HORIZONTAL STABILIZER UPPER AND LOWER SURFACES OF SKIN FROM STATION XE 221 TO XE 272. REMOVED THE DAMAGED UPPER AND LOWER SKIN PANELS AND FABRICATED PANELS OF .080 7075-T6 MATERIAL. ALSO, REPLACED EACH BNov 24, 1995 · N54FA · Doug DC8F54 · Horizontal Stabilizer, Plate/Skin
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