Douglas DC-9-33F

Service difficulty reports · 1,681

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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 = 'DC933F'
  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 ABXA9600209Floor Panel · corrodedDURING C-CHECK INSPECTION, FOUND CORRODED FLOOR PANELS AT STA 160. REPAIRED IAW ABX REA D953-13783-MR.Dec 7, 1995 · N931AX · Doug DC933F · Fuselage Floor PanelSDR ABXA9600208Floor Panel · corrodedDURING C-CHECK INSPECTION, FOUND CORRODED FLOOR PANELS AT STA 160. REPAIRED IAW ABX REA D953-13783-MR.Dec 7, 1995 · N931AX · Doug DC933F · Fuselage Floor PanelSDR ABXA9600207Floor Panel · corrodedDURING C-CHECK INSPECTION, FOUND CORRODED FLOOR PANEL AT STA 160. REPAIRED IAW ABX REA D953-13783-MR.Dec 7, 1995 · N931AX · Doug DC933F · Fuselage Floor PanelSDR ABXA9600205Floor Panel · corrodedDURING C-CHECK INSPECTION, FOUND FLOOR PANEL CORRODED AT STA 193. REPAIRED IAW ABX REA D953-13771-MR.Dec 7, 1995 · N931AX · Doug DC933F · Fuselage Floor PanelSDR ABXA9600204Floor Panel · corrodedDURING C-CHECK INSPECTION, FOUND FLOOR PANEL CORRODED AT STA 193. REPAIRED IAW ABX REA D953-13771-MR.Dec 7, 1995 · N931AX · Doug DC933F · Fuselage Floor PanelSDR ABXA9600203Cusp · corrodedDURING C-CHECK INSPECTION, FOUND EXCESSIVE CORROSION ON CUSP BETWEEN STA 218 TO 290 LBL 54. REPAIRED IAW ABX REA D953-13758-MR.Dec 6, 1995 · N931AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9600231Support · corrodedDURING C-CHECK INSPECTION FOUND LEVEL 2 CORROSION ON THE LONGITUDINAL FLOOR SUPPORT BETWEEN LONGERONS 27R AND 28R, BETWEEN STA 332 AND STA 351. MANUFACTURED FLOOR SUPPORT IAW ABX DRAWING K05554 AND INSTALLED IAW DC-9 SRM 51-30-2.Dec 5, 1995 · N931AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9600221Blkhd Web · corrodedDURING C-CHECK INSPECTION, FOUND BULKHEAD WEB AT STA 110 CORRODED AT LONGERONS 27R AND 25R. REPAIRED IAW ABX REA D953-13722-MR.Dec 4, 1995 · N931AX · Doug DC933F · Fuselage Main, BulkheadSDR ABXA9600230Stiffener · crackedDURING C-CHECK INSPECTION, FOUND STIFFENER JUST RIGHT OF AUXILIARY LANDING GEAR STRUCTURE CRACKED. REPAIRED IAW ABX DRAWING K05159.Nov 30, 1995 · N931AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9600223Longeron · crackedDURING C-CHECK INSPECTION, FOUND LONGERON 16L CRACKED AT STA 965. REPAIRED LONGERON IAW DC-9 SRM 51-30-2 AND 51-30-5.Nov 30, 1995 · N931AX · Doug DC933F · Fuselage Main, Longeron/StringerSDR ABXA9600225Longeron · crackedDURING C - CHECK INSPECTION, FOUND LONGERON 17R CRACKED AT STA 980. REPAIRED LONGERON IAW DC-9 SRM 53-03, FIGURE 2.Nov 29, 1995 · N931AX · Doug DC933F · Fuselage Main, Longeron/StringerSDR ABXA9600224Longeron · crackedDURING C-CHECK INSPECTION, FOUND LONGERON 17L CRACKED AT STA 980 AND STA 965. REPAIRED IAW DC-9 SRM 51-30-2 AND 51-30-5.Nov 29, 1995 · N931AX · Doug DC933F · Fuselage Main, Longeron/StringerSDR 96ZZZX225Seat Track · corrodedDURING OP-15, FOUND CORROSION ON GALLEY FLOOR, RT INBOARD SEAT TRACK, UNDER NR 2 GALLEY, STA 234 AND STA 210. REPLACED SEAT TRACK SECTION PER SRM 53-05. AIRCRAFT TOTAL TIME: 64,684 HOURS, 61,704, CYCLES.Nov 29, 1995 · N937F · Doug DC933F · Fuselage, Seat/Cargo Attach FittingsSDR ABXA9600226Fitting · crackedDURING C-CHECK INSPECTION, FOUND THIRD BEAM ON SERVICE DOOR AFT END FITTING CRACKED. REPLACED BRACKET IAW DC-9 SRM 51-30-2.Nov 28, 1995 · N931AX · Doug DC933F · Service DoorsSDR 96ZZZX227Longeron · crackedSTL - DURING OP-15, FOUND A .25 INCH CRACK IN LONGERON 10R, STA 465. REPAIRED PER SRM 53-11-2, FIGURE 2. AIRCRAFT TOTAL TIME: 64,684 HOURS, 61,704 CYCLES.Nov 24, 1995 · N937F · Doug DC933F · Fuselage Main, Longeron/StringerSDR 96ZZZX226Floor Beam · crackedSTL - DURING OP-15, FOUND A 1.50 INCH CRACK IN FLOOR BEAM STA 200. REPAIRED PER ARA 8794. AIRCRAFT TOTAL TIME: 64,684 HOURS, 61,704 CYCLES.Nov 24, 1995 · N937F · Doug DC933F · Fuselage Main, Floor BeamSDR ABXA9500929Dnlock Switch · intermittentRIGHT MAIN GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT CAME ON. RECYCLED GEAR AND ALL INDICATIONS WERE NORMAL. REPLACED MAIN GEAR DOWNLOCK SWITCH IAW DC-9 SUPP. M.M. OPS CHECKED GOOD.Oct 31, 1995 · N935AX · Doug DC933F · Landing Gear Position and WarningSDR ABXA9500945Spar Cap · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON LOWER SURFACE OF AFT UPPER SPAR CAP, FORWARD FLANGE ON RIGHT HORIZONTAL STABILIZER. REPAIRED IAW ABX REA D955-13276-MR.Oct 25, 1995 · N930AX · Doug DC933F · Horizontal Stabilizer, Spar/RibSDR ABXA9500753Oil Line · leakingLEFT ENGINE SHUT DOWN FOR FLUCTUATING OIL PRESSURE AND ZERO QUANTITY INDICATION. TOTAL WINDMILL TIME WAS LESS THAN 1.5 MINUTES. REPLACED TWO OIL LINES OFF THE FUEL/OIL COOLER TO GEAR BOX IAW DC-9 M.M. 79-20. LEAK CHECKED GOOD.Oct 2, 1995 · N930AX · Doug DC933F · Engine Oil Distribution (Airframe Furnished)SDR ABXA9500782Rod Ends · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR DRIVER ROD ENDS WORN. REPLACED DRIVER ROD IAW DC-9 OH MANUAL 32-10-6.Sep 26, 1995 · N932AX · Doug DC933F · Landing Gear Door Retract SectionSDR ABXA9500781Door · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGE LUGS WORN AND ONE LUG MISSING A BUSHING. REPLACED OUTBOARD DOOR IAW DC-9 MM 32-12-1.Sep 26, 1995 · N932AX · Doug DC933F · Landing Gear DoorsSDR EIAA9544Wire · brokenDEN - ON DESCENT THROTTLES IDLE, NOSE GEAR UNSAFE LIGHT NOT ILLUMINATED. GEAR DOWN, 'NOSE LANDING GEAR' GREEN LIGHT NOT ILLUMINATED. GEAR HORN FUNCTIONS NORMALLY. VISUALLY CHECKED GEAR DOWN AND LOCKED. FOUND BROKEN WIRE AFT OF NOSE GEAR, WIRE G-2116-B24. Sep 16, 1995 · N933F · Doug DC933F · Landing Gear System WiringSDR ABXA9500883Frame · damagedDURING C-CHECK INSPECTION, AN ELONGATED BARREL NUT HOLE WAS DISCOVERED BETWEEN LONGERONS 27R AND 28R AT STA 897. REPAIRED IAW ABX REA D953-12783-MR.Sep 9, 1995 · N935AX · Doug DC933F · Fuselage Main, FrameSDR ABXA9500884Vane · dentedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 92-22-08, THE LEFT WING UPPER MOVEABLE VANE WAS FOUND DENTED. REPLACED VANE IAW DC-9 MM 27-51-2.Sep 8, 1995 · N935AX · Doug DC933F · Wing Miscellaneous StructureSDR ABXA9500880Doubler · damagedDURING C-CHECK INSPECTION AN EXISTING REPAIR WAS FOUND DAMAGED ON THE FORWARD UPPER CORNER OF THE FORWARD ENTRY DOOR. REPAIRED IAW ABX REA D953-12658-MR.Sep 8, 1995 · N935AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9500882Floorbeam · corrodedDURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A FLOORBEAM AT STA 294, LBL 1. REPAIRED IAW ABX REA D953-12742-MR.Sep 7, 1995 · N935AX · Doug DC933F · Fuselage Main, Floor BeamSDR ABXA9500879Fitting · crackedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 92-22-08, FOUND A FITTING CRACKED ON THE AFT SIDE OF A FLOORBEAM AT STA 965, RBL 49. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.Sep 7, 1995 · N935AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9500876Shear Tie · crackedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 92-22-08, FOUND A CRACKED SHEAR TIE AT STA 996, LONGERON 18L. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-2 AND 51-30-5.Sep 1, 1995 · N935AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9500875Shear Tie · crackedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 92-22-08, FOUND A CRACKED SHEAR TIE AT STA 996, LONGERON 18R. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-2 AND 51-30-5.Sep 1, 1995 · N935AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9500877Shear Tie · crackedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 92-22-08, FOUND A CRACKED SHEAR TIE AT STA 950, LONGERON 15R. REPLACED SHEAR TIE IAW DC-9SRM 51-30-2 AND 51-30-5.Aug 31, 1995 · N935AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9500878Bushing · wornDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 91-22-07, ASB 32-244, FOUND THE LEFT MAIN OUTBOARD LANDING GEAR DOOR HINGE WORN. HINGE BUSHINGS REPLACED IAW DC-9 MM 32-12-1.Aug 28, 1995 · N935AX · Doug DC933F · Landing Gear DoorsSDR ABXA9500832Fitting · crackedDURING COMPLIANCE OF AD 82-06-02, SB 55-32, FOUND A CRACK AT FORWARD UPPER RIGHT HAND HI-LOCK IN THE REAR SPAR FITTING. REPLACED CONSTANT SECTION IAW DC-9 SRM 51-30-1.Aug 24, 1995 · N932AX · Doug DC933F · Horizontal Stabilizer StructureSDR ABXA9500881Skin · gougedDURING C-CHECK INSPECTION, THE FUSELAGE SKIN AT STA 440 AND LONGERON 16L WAS FOUND GOUGED. REPAIRED IAW ABX REA D953-12668-MR.Aug 5, 1995 · N935AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA9500662Link · crackedDURING COMPLIANCE OF A.D. 85-01-03; S.B.'S 27-288, 27-229, EAAD 27-32091, FOUND THE LEFT OUTBOARD SPOILER DRIVE LINK HAD A CRACK INDICATION. REPLACED LEFT OUTBOARD SPOILER DRIVE LINK ISW DC-9 SUPP. M.M. 27-61-1.Aug 3, 1995 · N930AX · Doug DC933F · Drag Control SystemSDR ABXA9500584Indicator Wire · openDURING CLIMB, LEFT GEAR UNSAFE LIGHT DID NOT ILLUMINATE DURING GEAR RETRACTION. DID NOT ILLUMINATE DURING IDLE FLIGHT WHILE IN DESCENT. FOUND WIRE 1G206024 OPEN. REPLACED WIRE IAW DC-9 WDM 32-61-0. LANDING GEAR SYSTEM OPS CHECKED NORMAL IAW DC-9 SUPP MM 32Jul 24, 1995 · N933AX · Doug DC933F · Landing Gear Position and WarningSDR ABXA9500560Engine · failedON TAKEOFF ROLL, HEARD A LOUD EXPLOSION, FOLLOWED BY A VIBRATION AND A LOSS OF POWER ON THE LEFT ENGINE. EGT REACHED 680 DEGREES. REPLACED THE NR 1 ENGINE IAW ABX JOB CARD J7001. OPS CHECKED GOOD, NO LEAKS NOTED AT THIS TIME.Jun 15, 1995 · N934AX · Doug DC933F · Engine (Turbine/Turboprop)SDR ABXA9500430Frame · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON THE ROLLED ZEE FRAME AT STA 530 ON THE UPPER FLANGE AT LONGERON 30. REPAIRED FRAME IAW ABX REA D953-11525-MR.May 6, 1995 · N933AX · Doug DC933F · Fuselage Main, FrameSDR ABXA9500381Clearview Window · looseRIGHT CLEARVIEW WINDOW HARD TO OPEN. NUT LOOSE ON UPPER FORWARD GUIDE BLOCK. TIGHTENED NUT AS REQUIRED, CYCLED WINDOW THIRTY TIMES WITH NO BINDING NOTED AT THIS TIME IAW DC-9 MM, CHAPTER 56-10-3.May 4, 1995 · N931AX · Doug DC933F · Flight Compartment WindowsSDR ABXA9500429Frame · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON THE FUSELAGE FRAME AT STATION 134 BETWEEN LONGERONS 24R AND 25R. REPAIRED FRAME IAW ABX REA D953-11505-MR.May 1, 1995 · N933AX · Doug DC933F · Fuselage Main, FrameSDR ABXA9500422Skin · damagedDURING C-CHECK INSPECTION, A PREVIOUSLY INSTALLED DOUBLE STACK REPAIR WAS REMOVED FROM THE LOWER AFT CORNER OF THE FORWARD ENTRY DOOR CUTOUT ON THE FUSELAGE SKIN. THE REPAIR HAD BEEN CLASSIFIED AS TEMPORARY. REPAIRED SKIN IAW ABX REA D953-11400-MR.May 1, 1995 · N933AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA9500425Skin · damagedDURING C-CHECK INSPECTION, THE FUSELAGE SKIN WAS FOUND TO HAVE A DOUBLE DRILLED HOLE JUST FORWARD OF STA 718R AT CUSP. REPAIRED SKIN IAW ABX REA D953-11414-MR.Apr 28, 1995 · N933AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA9500434Fitting · crackedDURING C-CHECK INSPECTION, A BATHTUB FITTING WAS FOUND CRACKED AT STA 370 LONGERON 22R. REPLACED IAW DC-9 SRM 51-30-2 AND 51-30-5.Apr 27, 1995 · N933AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9500432Intercostal · crackedDURING C-CHECK INSPECTION, AN INTERCOSTAL WAS FOUND CRACKED AT STA 503 LONGERON 19R. REPLACED IAW DC-9 SRM 51-30-5.Apr 27, 1995 · N933AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9500424Skin · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON THE RIGHT WING UPPER SKIN AT XCW 20. REPAIRED IAW ABX REA D957-11411-MR.Apr 27, 1995 · N933AX · Doug DC933F · Wing, Plate/SkinSDR ABXA9500423Skin · damagedDURING C-CHECK INSPECTION, A CREASE WAS FOUND IN THE FUSELAGE SKIN JUST FORWARD OF THE FORWARD LOWER CARGO DOOR, BETWEEN LONGERONS 26R AND 25R. THE CREASE SPANNED FROM STATIONS 367 TO 341. REPAIRED THE SKIN IAW ABX REA D953-11408-MR.Apr 26, 1995 · N933AX · Doug DC933F · Fuselage Main, Plate/SkinSDR ABXA9500374Doubler · crackedDURING COMPLIANCE OF AD 85-01-02, SB 53-137, FOUND LEFT UPPER CORNER OF AFT PRESSURE BULKHEAD VENTRAL DOOR DOUBLER CRACKED IN RADIUS. REPAIRED IAW DC-9 SB 53-137, SERVICE REWORK DRAWING SR0J060088 AND ABX REA D953-11481-SB.Apr 26, 1995 · N930AX · Doug DC933F · Fuselage Main, BulkheadSDR ABXA9500431Floor Panel · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE COCKPIT CENTER FLOOR PANEL. REPLACED THE PANEL IAW DC-9 SRM 51-30-2, 51-30-1.Apr 25, 1995 · N933AX · Doug DC933F · Fuselage Floor PanelSDR ABXA9500436Fitting · crackedDURING C-CHECK INSPECTION, FOUND LONGERON 28R END FITTING CRACKED AT STA 566. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-2.Apr 24, 1995 · N933AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9500433Support · crackedDURING C-CHECK INSPECTION, A MAIN FLOOR SUPPORT WAS FOUND CRACKED AT STA 598 LBL 36. REPLACED IAW DC-9 SRM 51-30-5.Apr 24, 1995 · N933AX · Doug DC933F · Fuselage Miscellaneous StructureSDR ABXA9500438Fitting · crackedDURING C-CHECK INSPECTION, FOUND LONGERON 29L END FITTING CRACKED AT STA 583. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1.Apr 22, 1995 · N933AX · Doug DC933F · Fuselage Miscellaneous Structure
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