N54FA, cancelled Apr 9, 2013

Service difficulty reports · 31

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N54FA' AND deregistration_id = 'N54FA-2013-04-09'
  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 99ZZZM29Strut · crackedCREW REPORTED FINDING A HYDRAULIC LEAK ON NOSE LANDING GEAR DURING PRE-FLIGHT GYE. FOUND CRACK IN NLG OLEO OUTER CYLINDER APPROX 6 INCH FROM TOP, APPROX 1.5 INCH LONG UNDER DATA PLATE. REPLACE NLG OLEO ASSEMBLY PER MM 32-2-0. (M)Oct 19, 1998 · N54FA · Doug DC8F54 · Nose/Tail Landing Gear Strut/AxleSDR 98ZZZM870Unknown · odorON ARRIVAL GYE, REPORTED SMOKE ODOR FROM UNKNOWN SOURCE IN COCKPIT AND CABIN. ON GROUND, RAN ENGINES AND PRESSURIZED AIRCRAFT TO CHECK NASI PNEUMATIC FLOW CONTROL SYSTEM IAW STC ST466CH. NO SMOKE ODOR WAS NOTED IN AIRCRAFT. AIRCRAFT WAS RETURNED TO SERVICE Jul 14, 1998 · N54FA · Doug DC8F54 · Air Distribution SystemSDR 98ZZZM498Line · brokenIN CRUISE BOG TO MIA EXPERIENCED LOSS OF HYDRAULIC QTY. EXECUTED ABNORMAL PROCEDURES AND LANDED MIA WITHOUT INCIDENT. AIRCRAFT TOWED OFF RUNWAY. INSPECTION REVEALED A BROKEN HYDRAULIC LINE IN THE LEFT WHEEL WELL. REPLACED HYDRAULIC LINE, SERVICED SYSTEM ANDJun 25, 1998 · N54FA · Doug DC8F54 · Hydraulic System, MainSDR 97ZZZX4181Transformer · failedILN/MCO - EN ROUTE, CIRCUIT BREAKER FOR FLIGHT ENGINEER WHITE LIGHTS AND OVERRIDE CONTROL CIRCUIT BREAKER TRIPPED. SMELLED SMOKE. FOUND DIMMING TRANSFORMER AT FAULT. ENTERED ON DMI PER MEL 33-1 AND CONTINUED IN SERVICE.Aug 27, 1997 · N54FA · Doug DC8F54 · Flight Compartment LightingSDR 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 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 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 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 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 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/SkinSDR 96ZZZM1112Skin · corrosionDURING D-CHECK INSPECTION, LEFT WING UPPER SKIN CORROSION WAS FOUND IN VARIOUS PLACES BETWEEN WING STATION 554 AND 659. REMOVED ALL CORROSION DAMAGE AND BLENDED THE AREA OUT TO A 63 MICRO INCH FINISH. INSTALLED 35 INCH BY 63.5 INCH .100 7075-T6 DOUBLER IAW ENov 24, 1995 · N54FA · Doug DC8F54 · Wing, Plate/SkinSDR 96ZZZM1111Skin · corrosionDURING D-CHECK INSPECTION, RIGHT WING LOWER SKIN OF INBOARD AILERON HAD CORROSION AT OUTBOARD END OF AILERON SKIN. CUT AND REMOVED CORRODED SKIN PANEL AND INSTALLED NEW IDENTICAL REPLACEMENT PANEL OF .050 2024-T3 MATERIAL WITH A .063 2024-T3 SPLICE PLATE IAW Nov 24, 1995 · N54FA · Doug DC8F54 · AileronsSDR 96ZZZM1110Skin · corrosionDURING D-CHECK INSPECTION, RIGHT WING LOWER SKIN OF OUTBOARD AILERON HAD CORROSION AT LOWER OUTBOARD SKIN PANEL. CUT AND REMOVED CORRODED SKIN PANEL AND INSTALLED NEW IDENTICAL REPLACEMENT PANEL OF .050 2024-T3 MATERIAL IAW EO 9507251. 8110-3 ISSUED BY DER SNov 24, 1995 · N54FA · Doug DC8F54 · AileronsSDR 96ZZZM1109Plating · corrosionDURING D-CHECK INSPECTION, FOUND CORROSION ON THE UPPER PLATING OF THE RIGHT WING UPPER SURFACE AT STATION XRS 600. CUT AND REMOVED CORRODED PLATING AND INSTALLED A 2 INCH BY 80 INCH .100 7075-T3 FILLER WITH 47 BY 84 INCH .100 7075-T6 DOUBLER IAW EO 9510181. Nov 24, 1995 · N54FA · Doug DC8F54 · Wing, Plate/SkinSDR 96ZZZM1108Skin · corrosionDURING D-CHECK INSPECTION, RT WING AT THE OUTBOARD END OF THE UPPER AND LOWER SKIN OF THE OUTBOARD FLAP CORROSION DAMAGE WAS FOUND. CUT AND REMOVED THE AREA OF CORRODED SKIN AND INSTALLED A .050 2924-T3 MATERIAL DOUBLER WITH A .063 2024-T3 SPLICE PLATE IAW EONov 24, 1995 · N54FA · Doug DC8F54 · Trailing Edge FlapsSDR 96ZZZM1107Frame · corrodedDURING D-CHECK INSPECTION, FUSELAGE FRAME AT FS 500 IN THE CABIN BETWEEN LONGERONS 9 AND 10 RIGHT FOUND CRACK. CUT OUT THE DAMAGED MATERIAL. INSTALLED A 2.25 FILLER FROM AN IDENTICAL FRAME SECTION AND INSTALLED TWO 11.0 INCH .050 AISI 301 1/2H REPAIR DOUBLERNov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Main, FrameSDR 96ZZZM1106Frame · corrosionDURING D-CHECK INSPECTION, FUSELAGE FRAME AT FUSELAGE STATION 540, 560 AND 580 WERE FOUND WITH CORROSION DAMAGE ALONG THE LOWER SEVERAL INCHES WHERE THEY JOIN THE FLOOR ATTACH FITTING. CUT EACH OF THE 3 FRAMES AT A LOCATION 19 INCHES ABOVE THE FLOOR LEVEL ANDNov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Main, FrameSDR 96ZZZM1105Skin · corrosionDURING D-CHECK INSPECTION, FOUND CORROSION DAMAGE ON THE LOWER EDGE OF THE FUSELAGE SKIN PANEL JUST FORWARD OF LONGERON 24 CLEVIS AND RUNNING FORWARD FOR ABOUT 32 INCHES AT STATION 850. CORROSION WAS CUT OUT AND INSTALLED TWO 40 BY 8.5 INCHES .100 AISI 3011/2Nov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Main, Plate/SkinSDR 96ZZZM1104Skin · corrosionDURING D-CHECK INSPECTION, FOUND CORROSION ON SEVERAL AREAS OF FUSELAGE SKIN FROM FS 1140 TO 1340 FROM L31 LEFT TO L31 RIGHT. REMOVED AND REPLACED LOWER FUSELAGE SKIN IAW SRM 51-21-1. ALSO, TREATED AND PRIMED ALL AREAS IAW SRM 51-1-8. (M)Nov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Main, Plate/SkinSDR 96ZZZM1103Skin · corrosionDURING D-CHECK INSPECTION, CORROSION AND DENTS WERE FOUND BELOW THE AFT PASSENGER DOOR FUSELAGE SKIN. CUT OUT ALL CORROSION AND DENTS ON DAMAGED SKIN. INSTALLED A 36.5 BY 6.5 INCH .090 7075-T6 FILLER WITH A 66 INCH BY 24.5 INCH .100 7075-T6 QQ-A-250/13 REPAINov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Main, Plate/SkinSDR 96ZZZM1102Skin · corrosionDURING D-CHECK INSPECTION, CORROSION WAS FOUND ON SEVERAL AREAS OF FUSELAGE SKIN FROM FS 610 TO 670 AND FROM L31 RT TO L31 LT. REMOVED AND REPLACED LOWER FUSELAGE SKIN IAW SRM 51-1-21. ALSO, TREATED AND PRIMED ALL AREAS IAW SRM 51-1-8. (M)Nov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Main, Plate/SkinSDR 96ZZZM1101Skin · corrosionDURING D-CHECK INSPECTION, CORROSION WAS FOUND ON THE UPPER AND LOWER SKIN CENTER PANELS OF THE LEFT ELEVATOR FROM STATION XE 133 TO STATION XE 246. REMOVED THE DAMAGED SKIN PANELS FROM THE ELEVATOR AND INSTALLED A NEW IDENTICAL SKINS PANEL OF .040 2024-T3 IANov 24, 1995 · N54FA · Doug DC8F54 · Elevator, Plate/SkinSDR 96ZZZM1100Skin · corrosionDURING D-CHECK INSPECTION, CORROSION WAS FOUND ON THE UPPER AND LOWER INBOARD SKIN PANELS OF THE LEFT ELEVATOR FROM STATION XE 32 TO STATION XE 133. REMOVED EACH DAMAGED SKIN PANEL FROM THE ELEVATOR AND INSTALLED A NEW IDENTICAL SKIN PANEL OF .040 2024-T3 IAWNov 24, 1995 · N54FA · Doug DC8F54 · Elevator, Plate/SkinSDR 96ZZZM1099Skin · corrosionDURING D-CHECK INSPECTION, CORROSION WAS FOUND ON SEVERAL AREAS OF FUSELAGE SKIN FROM FS 430 TO 610 AND FROM LONGERON 31 RIGHT TO LONGERON 31 LEFT. REMOVED AND REPLACED LOWER FUSELAGE SKIN FROM FS 430 TO 610 AND FROM L31 RIGHT TO L31 LEFT IAW SRM 51-1-21. ALNov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Main, Plate/SkinSDR 96ZZZM1098Floor Beam · corrosionDURING D-CHECK INSPECTION, CORROSION FOUND ON THE WEB OF THE FLOOR BEAM AT FS 920 UNDER OUTBOARD TRACK. DAMAGED AREA WAS CUT OUT AND INSTALLED 14 BY 7 INCHES .063 301 1/2H MIL-S-5059 DOUBLER WITH A 2 INCH .188 7075-T6 FILLER IAW EO 9508221, 8110-3 ISSUED BY DNov 24, 1995 · N54FA · Doug DC8F54 · Fuselage Main, Floor Beam
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