Douglas DC-9-32F

Service difficulty reports · 517

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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 = 'DC932F'
  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 98ZZZX2383Seat Track · wornDURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT RBL 8.5. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUGH 98ZZZX2391.Jun 26, 1998 · N932F · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR 98ZZZX2382Seat Track · wornDURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT RBL 8.5. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUGH 98ZZZX2391.Jun 26, 1998 · N932F · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR 98ZZZX2381Seat Track · wornDURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 16.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUGH 98ZZZX2391.Jun 26, 1998 · N932F · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR 98ZZZX2380Seat Track · wornDURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 16.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUGH 98ZZZX2391.Jun 26, 1998 · N932F · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR 98ZZZX2379Seat Track · wornDURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 16.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUGH 98ZZZX2391.Jun 26, 1998 · N932F · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR 98ZZZX2378Seat Track · wornDURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 16.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUGH 98ZZZX2391.Jun 26, 1998 · N932F · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR 98ZZZX2377Seat Track · wornDURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 16.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUGH 98ZZZX2391.Jun 26, 1998 · N932F · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR 98ZZZX2376Seat Track · wornDURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 16.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUGH 98ZZZX2391.Jun 26, 1998 · N932F · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR 98ZZZX2375Seat Track · wornDURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 16.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUGH 98ZZZX2391.Jun 26, 1998 · N932F · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR 98ZZZX2374Seat Track · wornDURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 37. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUGH 98ZZZX2391.Jun 26, 1998 · N932F · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR 98ZZZX2372Seat Track · wornDURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 37. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUGH 98ZZZX2391.Jun 26, 1998 · N932F · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR 98ZZZX2371Seat Track · wornDURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 37. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUGH 98ZZZX2391.Jun 26, 1998 · N932F · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR 98ZZZX2370Seat Track · wornDURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 37. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUGH 98ZZZX2391.Jun 26, 1998 · N932F · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR 98ZZZX2369Seat Track · wornDURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 37. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUGH 98ZZZX2391.Jun 26, 1998 · N932F · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR 98ZZZX2368Seat Track · wornDURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 37. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUGH 98ZZZX2391.Jun 26, 1998 · N932F · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR 98ZZZX2367Seat Track · wornDURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 37. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2368 THROUGH 98ZZZX2391.Jun 26, 1998 · N932F · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR ABXA9800447Bulb · failedCOCKPIT OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. RELAMPED COCKPIT EMERGENCY LIGHTS. OPS CHECKED NORMAL.May 12, 1998 · N904AX · Doug DC932F · Emergency LightingSDR ABXA9800300Pan · crackedDURING C-CHECK, FOUND LEFT MAIN LANDING GEAR DOOR PAN CRACKED AT FORWARD SIDE. REPAIRED DOOR PAN IAW DC9 SRM 52-05.Apr 2, 1998 · N904AX · Doug DC932F · Landing Gear DoorsSDR ABXA9800299Longeron · crackedDURING C-CHECK, FOUND LONGERON 3L CRACKED JUST AFT OF STATION 180. REPAIRED LONGERON IAW DC9 SRM 53-02.Apr 2, 1998 · N904AX · Doug DC932F · Fuselage Main, Longeron/StringerSDR ABXA9800298Longeron · crackedDURING C-CHECK, FOUND LONGERON 12R CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02.Apr 2, 1998 · N904AX · Doug DC932F · Fuselage Main, Longeron/StringerSDR ABXA9800297Longeron · crackedDURING C-CHECK, FOUND LONGERON 16R CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02.Apr 2, 1998 · N904AX · Doug DC932F · Fuselage Main, Longeron/StringerSDR ABXA9800296Slant Panel · corrodedDURING C-CHECK, FOUND RIGHT SLANT PANEL STATION 690 CORRODED UNDER POTTED CAPS, AROUND THE FLOATING NUT-PLATES, BETWEEN RBL 22 AND RBL 44. REPLACED SLANT PANEL IAW DC9 SRM 51-30-2.Apr 2, 1998 · N904AX · Doug DC932F · Fuselage Miscellaneous StructureSDR ABXA9800295Web · crackedDURING C-CHECK, FOUND CUSP WEB CRACKED AT STATION 920, 921, 925, 940, AND 945 AT RBL 54. REPAIRED CUSP WEB IAW DC9 SRM 51-30-13, 51-30-2 AND 51-30-5.Apr 2, 1998 · N904AX · Doug DC932F · Fuselage Miscellaneous StructureSDR ABXA9800278Longeron · crackedDURING C-CHECK, FOUND LONGERON 13L CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02.Mar 27, 1998 · N904AX · Doug DC932F · Fuselage Main, Longeron/StringerSDR ABXA9800277Longeron · crackedDURING C-CHECK, FOUND LONGERON 13R CRACKED AT PYLON BULKHEAD AND STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02.Mar 27, 1998 · N904AX · Doug DC932F · Fuselage Main, Longeron/StringerSDR ABXA9800265Fitting · corrodedDURING C-CHECK, FOUND RIGHT OUTBOARD T-FITTING BETWEEN FUSELAGE AND RIGHT SLANT PANEL CORRODED AT STATION 690. REPLACED T-FITTING IAW DC9 SRM 51-30-5.Mar 26, 1998 · N904AX · Doug DC932F · Fuselage, Wing Attach FittingsSDR ABXA9800264Longeron · crackedDURING C-CHECK, FOUND LONGERON 4L CRACKED AT STATION 160 AND 197. REPAIRED LONGERON IAW DC9 SRM 53-02.Mar 26, 1998 · N904AX · Doug DC932F · Fuselage Main, Longeron/StringerSDR ABXA9800035Bulkhead Skin · crackedDURING ACCOMPLISHMENT OF DC9 SERVICE BULLETIN 53-A14, FOUND AFT PRESSURE BULKHEAD TEE CAP UPPER SKIN SPLICE CRACKED WITH SHEARED RIVETS AT FUSELAGE STATION 996. REPAIRED IAW DOUGLAS SERVICE REWORK DRAWING J060143 AND ABX REA D953-2250-MR.Jan 15, 1998 · N904AX · Doug DC932F · Fuselage Main, BulkheadSDR EIAA970177Door Latch · malfunctionedBIL - LOG PAGE: F32722 - AFTER TAKEOFF, GEAR DOOR WOULD NOT CLOSE. AIRCRAFT RETURNED TO BIL, NO PROBLEMS DURING LANDING. BYPASS DOOR OPEN. CLOSED DOOR AND MAIN DOOR CLOSED NORMALLY. (X)Jun 19, 1997 · N935F · Doug DC932F · Landing Gear Door Retract SectionSDR EIAA970173Tire · failedOAK - LOG PAGE: F77497 - DURING THE TAKEOFF ROLL AT 135K, A LOUD NOISE WAS HEARD FOLLOWED BY AIRCRAFT VIBRATION. AFTER TAKEOFF, THE GEAR WAS LEFT EXTENDED AND AIRCRAFT RETURNED TO OAK, NO PROBLEMS DURING LANDING. FIRE DEPT RELAYED INFO THAT NR 3 TIRE WAS BLMay 29, 1997 · N935F · Doug DC932F · TireSDR ABXA9700673Battery · dischargedEMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHT BATTERIES.Apr 11, 1997 · N904AX · Doug DC932F · Emergency LightingSDR ABXA9701184Skin · delaminatedFOUND LEFT WING SPOILER UPPER AND LOWER SKIN DELAMINATED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.Apr 10, 1997 · N905AX · Doug DC932F · SpoilersSDR ABXA9701131Skin · delaminatedLEFT INBOARD FLAP VANE OUTER SKIN 40 PERCENT DELAMINATED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.Apr 10, 1997 · N905AX · Doug DC932F · Trailing Edge FlapsSDR ABXA9700547Link Assy · defectiveIN CRUISE AT FL 350, NOSE GEAR DOOR CAME OPEN. REPLACED LEFT NOSE LANDING GEAR DOOR LINK ASSY S/N DEC 1218. REPLACED RIGHT NOSE LANDING GEAR DOOR LINK ASSY S/N HGF 339.Apr 9, 1997 · N909AX · Doug DC932F · Landing Gear Door Retract SectionSDR EIAA970084Scraper · damagedPAJN - LOG PAGE: F32570 - AFTER TAKEOFF AT PAJN, LANDING GEAR HANDLE WOULD NOT MOVE TO RETRACT POSITION, NOSE WHEEL WAS STEERABLE. FOUND NOSE GEAR STRUT SCRAPPER RING BINDING. REPACKED STRUT WITH NEW O-RINGS AND SCRAPPER. (X)Mar 28, 1997 · N935F · Doug DC932F · Nose/Tail Landing Gear Strut/AxleSDR EIAA970076Torque Link · lack of lubePDX - ON DEPARTURE FROM KPDX, UNABLE TO RAISE LANDING GEAR. NOSE WHEEL WAS STEERABLE AND STILL IN GROUND MODE GCR. FOUND NOSE GEAR TORQUE LINKS VERY STIFF AND DRY, CAUSING BINDING WHEN THE STRUT EXTENTION WAS VARIED WITH NITROGEN. LUBED TORQUE LINKS PER MM.Mar 4, 1997 · N935F · Doug DC932F · Landing Gear Retraction/Extension SystemSDR EIAA96101Strut · req'd serviceAFTER TAKEOFF, AIRCRAFT WOULD NOT SHIFT INTO FLIGHT MODE. LANDING GEAR DID RETRACT. SERVICED NOSE LANDING GEAR. (M)Dec 22, 1996 · N935F · Doug DC932F · Nose/Tail Landing Gear Strut/AxleSDR EIAA9679Angles · crackedSAT - FORWARD CARGO BAY BS 598 STRINGER 28R BOTH HORIZONTAL AND VERTICAL PANEL SUPPORT ANGLES ARE CRACKED. FABRICATED AND INSTALLED HORIZONTAL ANGLE PER SRM 51-30-2, 53-21-0 FIG 7C SHEET 1 AND 3. FABRICATED AND INSTALLED VERTICLE ANGLE PER SRM 51-30-2, 53-01Nov 1, 1996 · N935F · Doug DC932F · Fuselage Miscellaneous StructureSDR EIAA9678Fitting · crackedSAT - FORWARD CARGO BAYFRAME 237 FLOOR SUPPORT FITTING AT LONGERON 24R IS CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-30-2. (M)Oct 30, 1996 · N935F · Doug DC932F · Fuselage Miscellaneous StructureSDR EIAA9677Floor Strut · crackedSAT - FORWARD CARGO BAYFRAME 237 FLOOR SUPPORT STRUT AT LONGERON 24R IS CRACKED. REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT STRUT AT FR 237 LONGERON 24R PER DAC DRAWING 5922079 AND SRM 51-30-2. (M)Oct 30, 1996 · N935F · Doug DC932F · Fuselage Miscellaneous StructureSDR EIAA9676Support · corrodedSAT - FORWARD CARGO BAY FRAME 362 FLOOR SUPPORT IS CORRODED AT STRINGER 28R. FABRICATED AND INSTALLED FLOOR SUPPORT CHANNEL FROM BS 218 TO 285 AND 285 TO 362 PER SRM 53-21-0, 53-01 FIGURE 2 AND 51-21-3. (M)Oct 30, 1996 · N935F · Doug DC932F · Fuselage Miscellaneous StructureSDR EIAA9675Floor Panel · corrodedSAT - FORWARD CARGO BAY FLOOR PANEL NR 3 IS CORRODED. REPAIRED FLOOR PANEL PER SRM 51-70-2. (M)Oct 30, 1996 · N935F · Doug DC932F · Fuselage Floor PanelSDR EIAA9674Tie Down Rails · corrodedSAT - AFT CARGO BAY LEFT AND RIGHT TIE DOWN RAILS BS 756 TO 900 CORRODED. FABRICATED AND INSTALLED TIE DOWN RAILS PER SRM 53-21-0 FIGURE 8 AND 51-30-2. (M)Oct 30, 1996 · N935F · Doug DC932F · Fuselage, Seat/Cargo Attach FittingsSDR EIAA9673Bulkhead Chord · corrodedSAT - BULKHEAD 756 UPPER T-CHORD CORRODED LBL 22 TO LBL 31. FABRICATED AND INSTALLED BULKHEAD T-CHORD SECTION BS 756 LBL 22 TO LBL 31 PER SRM 53-01 FIG 2, 51-10-3 AND 53-14-3. (M)Oct 30, 1996 · N935F · Doug DC932F · Fuselage Main, BulkheadSDR EIAA9672Frame · corrodedSAT - FRAME 237 LONGERON 24R CORRODED. FABRICATED AND INSTALLED REPAIR SPLICE TO FRAME BS 237 LONGERON 24R PER SRM 53-03 FIGURE 2A. (M)Oct 30, 1996 · N935F · Doug DC932F · Fuselage Main, FrameSDR EIAA9671Floor Support · corrodedSAT - FS 996 LOWER SUPPORT ANGLE HAS EXFOLIATION CORROSION FROM LONGERON 25L TO 25R. FABRICATED AND INSTALLED FLOOR SUPPORT ANGLE FS 996 FROM LONGERON 26L TO 29R PER SRM 53-01 FIG 2 AND SRM 53-11-3. (M)Oct 30, 1996 · N935F · Doug DC932F · Fuselage Miscellaneous StructureSDR EIAA9670Floor Support · corrodedSAT - FORWARD CARGO COMPARTMENT FRAME 362 TO FORWARD BULKHEAD HAS LIGHT SURFACE CORROSION ON FLOOR SUPPORT AT STATION 28R. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED REPLACEMENT CHANNEL LE IAW SRM 51-30-2 FROM STATION 218 TO 285, FROM AREA 285 TO 362. ROct 30, 1996 · N935F · Doug DC932F · Fuselage Miscellaneous StructureSDR EIAA9669Angle · crackedSAT - FORWARD CARGO COMPARTMENT STATION 598, STRINGER 28R HORIZONTAL AND VERTICAL PANEL SUPPORT ANGLES ARE CRACKED. FABRICATED AND INSTALLED HORIZONTAL ANGLE IAW SRM 51-30-0, FIGURE 76 SHEET 1 AND 3. REMOVED DAMAGED AREA ON VERTICAL ANGLE IAW SRM 53-01 FIGUROct 30, 1996 · N935F · Doug DC932F · Fuselage Miscellaneous StructureSDR EIAA9668Frame · crackedSAT - AFT CARGO HAS CRACKS IN FRAME 908-937 UPPER CEILING WEB AT STRIGNER 19L ABOVE AFT CARGO DOOR LIGHT. STOP DRILLED CRACKS, PERFORMED EDDY CURRENT INSPECTION ON STOP DRILL HOLES, FABRICATED DOUBLER AND INSTALLED PER SRM 51-10-3, 53-11-3 FIGURE 1, 2 AND 3, Oct 30, 1996 · N935F · Doug DC932F · Fuselage Main, FrameSDR EIAA9667Jamb · corrodedSAT - CORRODED FORWARD CARGO LOWER DOOR JAMB AT STATION 370-427. FABRICATED NEW SECTION AND INSTALLED PER SRM 53-05 FIG 44, 51-30-2 AND 51-10-3. (M)Oct 30, 1996 · N935F · Doug DC932F · Fuselage Miscellaneous Structure
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