Douglas DC-9-31

Service difficulty reports · 7,433

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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 aircraft_model_key = 'DC931'
  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 9500849927Chord · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN FS 110 LOWER CHORD ANGLE, NOSE WHEEL WELL RIGHT TUNNEL. REPAIRED PER EA X9-53-51.Jan 12, 1995 · N8920E · Doug DC931 · Fuselage Miscellaneous StructureSDR 9500749997Fire Loop · malfunctionedINBOUND TO MSN, THE NR 2 FIRE WARNING ILLUMINATED. SYSTEM FAILED OPERATIONAL TEST OF THE SECONDARY LOOP. PULLED THE FIRE HANDLE SHUTTING DOWN NR 2 AND DISCHARGED BOTH FIRE BOTTLES. FOUND 'B' LOOP HAD MALFUNCTIONED. PLACED THE 'B' LOOP ON MEL. INSPECTED ENJan 12, 1995 · N8933E · Doug DC931 · Fire DetectionSDR USAA951153Skin · crackedPIT - DURING C-3 CHECK CARD 9-46-80-146, FOUND .3750 INCH CRACK BOTH SIDES OF 4TH DOOR STOP HOLE FROM BOTTOM, STATION 200 LEFT. INSTALLED DOUBLER PER EA NR 311550. (M)Jan 11, 1995 · N916VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA950198Door Pan · crackedPIT - DURING Q-1 CHECK, INSPECTION FOUND .25 INCH CRACK AT RT FWD EMERGENCY EXIT DOOR AT UPPER AFT CORNER STOP 14 PAN AREA. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-20-03. (W)Jan 11, 1995 · N929VJ · Doug DC931 · Emergency ExitsSDR ABXA9500091Panel · crackedDURING C-CHECK INSPECTION, THE NOSE LANDING GEAR UPPER WHEEL WELL PRESSURE PANEL WAS FOUND CRACKED AT STA 83. REPAIRED PANEL IAW SB 53-187.Jan 11, 1995 · N945AX · Doug DC931 · Fuselage Miscellaneous StructureSDR 9502449945Hinge · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN NR 3 FLAP HINGE FASTENER BORES. REPAIRED PER XEA X9-27-12.Jan 11, 1995 · N8925E · Doug DC931 · Trailing Edge FlapsSDR 9500779927Frame · crackedDURING PERIODIC CHECK, FOUND 12 INCH CRACK IN THE FS 1132 FRAME AT LONGERONS 17L - 19L. REPLACED LOWER FRAME PER DWG 9911877 AND SRM 51-30-2.Jan 11, 1995 · N8920E · Doug DC931 · Fuselage Main, FrameSDR 9500669979Instr Amplifier · malfunctionedCAPTAIN'S GYRO FLAG APPEARED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED CAPTAIN'S ATTITUDE DIRECTIONAL INDICATOR WITH NO HELP. REPLACED INSTRUMENT AMPLIFIER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO GATE.Jan 11, 1995 · N9343 · Doug DC931 · Attitude and Direction Data SystemSDR ABXA9500089Angle · failedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 89-08-10 AND S.B.'S A53-154 AND A53-223, FOUND RIGHT DORSAL FIN ATTACH ANGLE BUCKLED AND FASTENERS PULLED. REPLACED RIGHT DORSAL FIN ATTACH ANGLE IAW DC-9 SRM 53-05, FIGURE 23 AND SB'S A53-154 AND A53-223.Jan 10, 1995 · N904AX · Doug DC931 · Fuselage, Stabilizer Attach FittingsSDR 9500769910Fitting · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN FS 928 FRAME ATTACH FITTING AT FLOOR LEVEL. REPLACED PER SRM 51-30-5.Jan 10, 1995 · N960N · Doug DC931 · Fuselage Miscellaneous StructureSDR 9500759910Fitting · crackedDURING PERIODIC CHECK, FOUND CRACK IN FS 908 FRAME ATTACH FITTING AT FLOOR LEVEL. REPLACED PER SRM 51-30-5.Jan 10, 1995 · N960N · Doug DC931 · Fuselage Miscellaneous StructureSDR 9500519927Fitting · crackedDURING PERIODIC CHECK, FOUND RADIUS CRACK IN BELT FRAME ATTACH FITTING FS 676 ABOVE LONGERON 29L. REPLACED FITTING PER SRM 51-30-2.Jan 10, 1995 · N8920E · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950150Skin · crackedPIT - DURING Q-1 CHECK INSPECTION, FOUND A .75 INCH CRACK AT STATION 101 BETWEEN LONGERON 27R AND 28R SKIN. INSTALLED DOUBLER TYPE REPAIR PER SRM 53-01 FIG 2 SHEET 3. (Z)Jan 9, 1995 · N929VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA950079Floor Skin · corrodedPIT - DURING Q-1 CHECK INSPECTION ACCOMPLISHED CORROSION TASK C45-53301 AND C46-53303 FOUND LEVEL I CORROSION ON SUBFLOOR SKIN UNDER THRESHOLD AT STATION 160-200. AREA WAS PREVIOUSLY 6 INCH BY 14 INCH. CUT OUT CORRODED AREA AND SPLICED IN NEW SECTION OF SUBFJan 9, 1995 · N977VJ · Doug DC931 · Fuselage Floor PanelSDR USAA950078Floor Skin · corrodedPIT - DURING Q-1 CHECK INSPECTION ACCOMPLISHED CORROSION TASK C46-53303 INSIDE OF SERVICE DOOR STATION 200 FOUND LEVEL I CORROSION ON SUBFLOOR. CUT OUT CORRODED AREA AND SPLICED IN NEW SECTION OF SUBFLOOR PER SRM 53-01 FIG 2. (Z)Jan 9, 1995 · N977VJ · Doug DC931 · Fuselage Floor PanelSDR USAA950077Floor Beam · grooved/workPIT - DURING Q-1 CHECK INSPECTION FOUND DEEP GROOVES IN FLOOR BEAM STATION 465 CAUSED BY FLOORBOARD. INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 20/20A. (Z)Jan 9, 1995 · N977VJ · Doug DC931 · Fuselage Main, Floor BeamSDR 9500509945Fitting · crackedDURING PERIODIC CHECK, FOUND CRACK IN CENTER WING TANK FITTING XCW O, BETWEEN WING STRINGERS 17 - 18. REPLACED FITTING PER SRM 51-10-4.Jan 9, 1995 · N8925E · Doug DC931 · Wing Miscellaneous StructureSDR 9500499945Keel Beam · crackedDURING PERIODIC CHECK, FOUND 10 INCH CRACK AND CORROSION IN RIGHT SIDE KEEL BEAM FS 604 - 637 BETWEEN LONGERON 28R - 29R. REPLACED BEAM PER SRM 51-30-2.Jan 9, 1995 · N8925E · Doug DC931 · Fuselage Main, KeelSDR USAA950103Switch · faultyPIT - FLIGHT 0310 - CREW COULD NOT GET A GREEN LIGHT ON THE NOSE GEAR. THE GEAR WAS RECYCLED AND THE NOSE GEAR GREEN DOWNLOCK LIGHT CAME ON. MAINTENANCE REPLACED THE NOSE GEAR DOWNLOCK SWITCH. (W)Jan 7, 1995 · N943VJ · Doug DC931 · Landing Gear Position and WarningSDR 9500649908Release Mech · out of adjustDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE USING THE INTERIOR HANDLE. ADJUSTED RELEASE MECHANISM.Jan 7, 1995 · N958N · Doug DC931 · Aerodynamic FairingsSDR 9500489927Spar Chord · crackedDURING PERIODIC CHECK, FOUND CRACKS IN THE LEFT HORIZONTAL STABILIZER AFT SPAR UPPER 'T' CAP BETWEEN NR3 - NR4 HINGES AND LOWER 'T' CAP (OUTBOARD END). REPAIRED BOTH PER SRM 55-02.Jan 7, 1995 · N8920E · Doug DC931 · Horizontal Stabilizer, Spar/RibSDR 9500479945Spar Chord · crackedDURING PERIODIC CHECK, FOUND CRACKS IN THE HORIZONTAL STABILIZER AFT SPAR 'T' CAPS LEFT SIDE LOWER (XHS 205-211) AND RIGHT SIDE UPPER (XHS 188). REPAIRED BOTH PER SRM 55-02.Jan 7, 1995 · N8925E · Doug DC931 · Horizontal Stabilizer, Spar/RibSDR 9500469945Fitting · crackedDURING PERIODIC CHECK, FOUND CRACKS IN ATTACH FITTINGS FS 996 AT LONGERONS 27R, 24L, AND AT INTERCOSTAL BETWEEN LONGERON 27L AND 28L. REPLACED ALL FITTINGS PER SRM 51-30.Jan 7, 1995 · N8925E · Doug DC931 · Fuselage Miscellaneous StructureSDR 9500459947Fitting · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON 'FISHTAIL' FITTING FS 604 AT LONGERON 28R. REPLACED FITTING PER SRM 51-01 AND DWG 5911418.Jan 7, 1995 · N8938E · Doug DC931 · Fuselage Miscellaneous StructureSDR 9500449947Bracket · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN BOTH LEFT AND RIGHT HORIZONTAL STABILIZER 'A' BRACKETS UPPER FASTENER BORES. OVERSIZED BORES AND INSTALLED BUSHINGS PER EA 99-094108 AND -094107 RESPECTIVELY.Jan 7, 1995 · N8938E · Doug DC931 · Horizontal Stabilizer StructureSDR 9500309930Control Cable · brokenEXCESSIVE VIBRATION WAS COMING FROM THE NOSE LANDING GEAR AREA AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO MSO AND LANDED WITHOUT INCIDENT. UPON INSPECTION, FOUND NOSE GEAR DOOR STOP CABLE BROKEN. REMOVED BROKEN CABLE; CLOSED AND SECURED NOSE GEAR DOORS. Jan 7, 1995 · N89S · Doug DC931 · Landing Gear Door Retract SectionSDR USAA950080Longeron · crackedPIT - DURING Q-1 CHECK INSPECTION, FOUND .25 INCH CRACK AT STATION 200, LONGERON 15L INNER SKIN WEB AT RIVET. INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 2. (W)Jan 6, 1995 · N977VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA950075Floor Beam · corrodedPIT - DURING Q-1 CHECK INSPECTION ACCOMPLISHED CORROSION TASK NR C58-53300 ON THE RT LAV FLOOR BEAM STATION 990 GROUND LEVEL I CORROSION (PREVIOUSLY REWORKED). INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 20A. (W)Jan 6, 1995 · N977VJ · Doug DC931 · Fuselage Main, Floor BeamSDR ABXA9500088Angle · defectiveDURING C-CHECK INSPECTION WHILE COMPYING WITH AD 89-08-10 AND S.B.'S A53-154 AND A53-223, FOUND LEFT DORSAL FIN ATTACH ANGLE HAD ONE FASTENER HEAD MISSING AND SEVERAL FASTENERS NOT PORPERLY SEATED. REPLACED FASTENERS IAW DC-9 SRM 51-30-1 AND 51-30-5.Jan 6, 1995 · N904AX · Doug DC931 · Fuselage, Stabilizer Attach FittingsSDR USAA950073Cusp Membrane · crackedPIT - DURING Q-1 CHECK INSPECTION, FOUND 1 INCH CRACK AT CUSP MEMBRANE AT STATION 598 RIGHT. SPLICED IN SECTION OF CUSP MEMBRANE PER SRM 53-05 FIG 96. (W)Jan 5, 1995 · N977VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA950005Eel Batt Pack · dischargedEWR - THE FLOOR LEVEL EMERGENCY LIGHTS PAST ROW 17 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BAD SECTION OF WIRE AND REPLACED THE BATTERY PACK. (W)Jan 5, 1995 · N995VJ · Doug DC931 · Emergency LightingSDR 9500199955Uplock Switch · malfunctionedDURING APPROACH INTO MSP, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED FOR LANDING. PERFORMED GO-AROUND AND UTILIZED EMERGENCY GEAR EXTENSION PROCEDURES. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. REPLACED THE NOSE GEAR UPLOCK SWITCHJan 4, 1995 · N922RW · Doug DC931 · Landing Gear Position and WarningSDR USAA950004Downlock Switch · inoperativeORF - FLT 956 - ON GEAR EXTENSION AT PHF, THE RT MAIN GEAR INDICATED UNSAFE. THE GEAR WAS RECYCLED AND THE INDICATION WAS STILL UNSAFE. THE CAPTAIN MADE A VISUAL INSPECTION WHICH SHOWED OK. THE FLIGHT DIVERTED TO ORF. WHILE MAKING A LOW PASS OVER THE RUNWAJan 3, 1995 · N967VJ · Doug DC931 · Landing Gear Position and Warning
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