Douglas DC-9-32
Service difficulty reports · 12,755
Newest first. General aviation reporting is voluntary.
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 = 'DC932' 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.
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 = 'DC932' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 97ZZZM295Frame · corrodedAFT CARGO HAS SEVERAL SPOTS OF CORROSION ON CIRCUMFERENTIAL FRAME AT STATION 917, CORROSION EXTENDS UNDER FINGERS OF ATTACH ANGLE. CUT OUT CORRODED AREA BETWEEN STRINGER 27 AND 28-29 BEYOND LIMITS .020. ROLLED 2 FRAME REPAIR SPLICE IAW DC-9 SRM 53-05 PAGE 4GSDR 97ZZZM293Frame · corrodedAFT CARGO HAS HEAVY CORROSION ON CIRCUMFERENTIAL FRAME BETWEEN STRINGERS 29L-29R AT STATION 830. CUT OUT CORRODED SECTION OF FRAME IAE DC-9 SRM 53-03 FIG 2A. FABRICATED 1 FILLER 7075-0-071, 4 SPLICE ANGLES 7075-0-.080, HEAT TREAT TO T6 IAE DC-9 SRM 51-10-2A,SDR 97ZZZM292Intercostal · corrodedAFT CARGO HAS CORROSION ALONG INTERCOSTAL BETWEEN STATION 850-890. MECHANICALLY REMOVED CORROSION IAW DC-9 SRM 51-10-3, .003 MATERIAL LOSS CHECKED WITH DME A1244, WITHIN LIMITS IAW DC-9 SRM 53-04 FIG 38 TREATED AND PRIMED IAW DC-9 SRM 51-10-3 AT AFT CARGO ALOSDR 97ZZZM291Intercostal · corrosionDURING A SCHEDULED INSPECTION AT AERO CORP IN THE AFT CARGO AREA, CORROSION ALONG THE INTERCOSTAL BETWEEN STATION 850-890, STRINGER 29R. MECHANICALLY REMOVED CORROSION IAW DC-9 SRM 51-10-3 .003 MATERIAL, CHECKED WITH DME A1244, WITHIN LIMITS IAW DC-9 SRM 53-0SDR 97ZZZM290Frame · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN THE AFT CARGO AREA CORROSION WAS FOUND ON CIRCUMFERENTIAL FRAME AT STATION 870 BETWEEN STRINGER 29L AND 29R. REMOVED FASTENERS TO FOM, MECHANICALLY REMOVED CORROSION MATERIAL LOSS LESS THAN .003 WITHIN LIMITS TREASDR 97ZZZM289Frame · corrodedAFT CARGO HAS CORROSION ON CIRCUMFERENTIAL FRAME AT STATION 850 BETWEEN STRINGERS 29L AND 29R. MECHANICALLY REMOVED CORROSION IAW DC-9 SRM 51-10-3 MATERIAL LOSS .005 WITHIN LIMITS IAW DC-9 SRM 53-04 FIG 38 TREAT AND PRIME IAW DC-9 SRM 51-10-3. (M)SDR 97ZZZM288Frame · corrodedAFT CARGO HAS CORROSION ON CIRCUMFERENTIAL FRAME BETWEEN STRINGERS 29L AND 29R STATION 810. REMOVED FASTENERS IAW DC-9 SRM 51-30-1, 51-30-1, 51-30-1, 51-30-5. MECHANICALLY REMOVED CORROSION MATERIAL LOSS LESS THAN .005 IAW DC-9 SRM 51-10-3. TREATED AND PRIMSDR 97ZZZM287Frame · corrodedAFT CARGO HAS CORROSION ON CIRCUMFERENTIAL FRAME BETWEEN STRINGERS 29L AND 29R AT STATION 790. MECHANICALLY REMOVED CORROSION MATERIAL LOSS LESS THAN .003 WITHIN LIMITS IAW DC-9 SRM 51-10-3. REMOVED FASTENERS AND STIFFENERS, ANGLES TWO TO FORM. TREATED AND SDR 97ZZZM286Frame · corrodedAFT CARGO HAS CORROSION ON CIRCUMFERENTIAL FRAME BETWEEN STRINGERS 29L AND 29R, STATION 770. CORROSION OUT OF LIMITS IAW DC-9 SRM 53-01 FIG 1, PREPARED REPAIR AREA AND FABRICATED REPAIR SPLICE, FILLER AND REPAIR PLATES IAW DC-9 SRM 53-03 FIG 2. TREATED AND PSDR 97ZZZM282Frame · crackedAFT CARGO STATION 945 HAS CIRCUMFERENTIAL FRAME WITH CRACK IN RADIUS AT STRINGER 30. DISASSEMBLED CIRCUMFERENTIAL TO ACCESS WELD IAW DC-9 SRM 51-30-2, WELDED REPAIR IAW EA 12-5321-29-C1056 USING 4951 OPT ROD, DYE PENETRATED INSPECTION PERFORMED, NO CRACKS FOUSDR 96ZZZX6069Frame · corrodedAFT CARGO HAS SEVERAL SPOTS OF CORROSION ON CIRCUMFERENTIAL FRAME AT STA 917, CORROSION EXTENDS UNDER FINGERS OF ATTACH ANGLE.SDR 96ZZZX6068Intercostal · corrodedAFT CARGO HAS CORROSION ALONG INTERCOSTAL BETWEEN STATIONS 850-890, STRINGER 29.SDR 96ZZZX6067Intercostal · corrodedAFT CARGO HAS CORROSION ALONG INTERCOSTAL BETWEEN STA 850 - STA 890, STR 28.SDR 96ZZZX6066Frame · corrodedAFT CARGO HAS CORROSION ON CIRCUMFERENTIAL FRAME AT STA 870 BETWEEN STRINGERS 29L AND 29R.SDR 96ZZZX6065Frame · corrodedAFT CARGO HAS CORROSION ON CIRCUMFERENTIAL FRAME AT STA 850 BETWEEN STRINGERS 29L AND 29R.SDR 96ZZZX6064Frame · corrodedAFT CARGO HAS CORROSION ON CIRCUMFERENTIAL FRAME BETWEEN STRINGERS 29L AND 29R, STA 810.SDR 96ZZZX6063Frame · corrodedAFT CARGO HAS CORROSION ON CIRCUMFERENTIAL FRAME BETWEEN STRINGERS 29L AND 29R AT STA 790.SDR 96ZZZX6062Frame · corrodedAFT CARGO HAS CORROSION ON CIRCUMFERENTIAL FRAME BETWEEN STRINGERS 29L AND 29R, STA 770.SDR 96ZZZX6061End Cap · corrodedAFT CARGO HAS HEAVY CORROSION NEAR FWD BULKHEAD AT STA 750 AT STRINGERS 29L-29R END CAP AT STR 30.SDR 96ZZZX6060Frame · corrodedAFT CARGO HAS HEAVY CORROSION ON CIRCUMFERENTIAL FRAME BETWEEN STRINGERS 29L-29R AT STA 830.SDR 96ZZZX6044Frame · crackedAFT CARGO STA 945 HAS CIRCUMFERENTIAL FRAME WITH CRACK IN RADIUS AT STR 30.SDR 9624739951Switch Pack · failedUPON RAISING GEAR AFTER TAKEOFF, GEAR WARNING HORN SOUNDED CONTINUOUSLY. RECYCLED GEAR SEVERAL TIMES, BOTH CLEAN AND FLAPS 15. CYCLED THROTTLES UP AND PUSHED HORN OFF BUTTON, HORN CEASED. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE CHASDR 9624509603Fitting · crackedDURING LINE CHECK, FOUND A CRACK IN THE AFT ENTRY DOOR UPPER RIGHT DOOR STOP FITTING. REPLACED FITTING (P/N 4917923-501) PER SRM 51-30-5.SDR 9614739951Switch · failedUPON RAISING GEAR AFTER TAKEOFF, GEAR WARNING HORN SOUNDED CONTINUOUSLY. RECYCLED GEAR SEVERAL TIMES, BOTH CLEAN AND FLAPS 15. CYCLED THROTTLES UP AND PUSHED HORN OFF BUTTON, HORN CEASED. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE CHASDR CA961125006Light Base · shorted(CAN) SHORTLY AFTER SELECTING GEAR UP, RIGHT MAIN LANDING GEAR LIGHT CAME ON. (GEAR UNSAFE LIGHT OUT) LANDING RECYCLED LIGHT WENT OUT. AFTER ANOTHER SHORT PERIOD LEFT GEAR LIGHT CAME ON AND THEN WENT OUT. NORMAL LANDING CARRIED OUT. MAINTENANCE CHECK REVEALED SDR 9624389614Web · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT CUSP MEMBRANE AND FITTING AT FS 851, LONGERON 18R. REPAIRED CUSP AND REPLACED THE FITTING PER SRM 51-10-03, 51-30-02.SDR 9624379986Wing Attach Ftg · corrodedDURING H-CHECK, FOUND CORROSION ON THE CENTER WING FITTING AT FS 600 AND LONGERON 19R. REPLACED FITTING PER SRM 51-10, 51-30-1.SDR MWEA96629Power Supply · inoperativeDURING SERVICE CHECK FOUND TAIL COMPARTMENT WALKWAY EMERGENCY LIGHTS STAY ILLUMUNIATED WHEN POWER IS OFF. MTC REMOVED AND REPLACED BATTERY POWER SUPPLY. OPS CHECK GOOD. RETURNED A/C TO SERVICE.SDR MWEA96628Light · inoperativeDURING SERVICE CHECK FOUND FWD ENTRY EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FWD ENTRY EMERGENCY LIGHT ASSY. OPS CHECK GOOD. RETURNED A/C TO SERVICE.SDR CA961125009Elect Receptacle · shorted(CAN) FLIGHT ATTENDANT REPORT SMOKE & SPARKS COMING FROM GALLEY OVEN AT POSITION #19. MAINTENANCE ACTION INVOLVED INSTALLING NEW RECEPTACLE AND OVEN CHECKED SERVICEABLE.SDR 9624319986Fitting · crackedDURING H-CHECK, FOUND A CRACKED FLOOR STRUCTURE FITTING AT FS 996, LBL 25. REPLACED FITTING (P/N 94FS481223-103) PER SRM 51-30-0.SDR 9624309986Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE AFT ENTRY DOOR LOWER RIGHT STOP FITTING. REPLACED FITTING PER SRM 51-30-2.SDR 9624299986Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE FS 579 FRAME FITTING BETWEEN THE UPPER FORWARD LUGS. REPAIRED FRAME (PSE 53.09.015) PER SRM 51-30-5.SDR 9624289986Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE LONGERON 10R END FITTING AT FS 617. REPLACED FITTING (PSE 53.09.003) PER SRM 51-10-2.SDR 9624279614Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FLOOR SUPPORT FITTING AT FS 832, LONGERON 28R. REPLACED FITTING PER SRM 51-10-3, 51-30-2, 51-30-5.SDR 9624109603Switch · malfunctionedDURING CLIMB-OUT OF MEM, GEAR DOOR OPEN LIGHT CAME ON. FOLLOWED COM PROCEDURE AND LIGHT REMAINED ON. RECYCLED GEAR AND LIGHT REMAINED ON. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED LEFT GEAR DOOR SWITCH. OPERATIONAL CHECK OK.SDR MWEA96626Skin · chafedDURING C-CHECK, FOUND LT VERTICAL STABILIZER SKIN GOUGED UPPER AND LOWER SECTIONS WHERE FAIRINGS CHAFING. REPLACED UPPER AND LOWER SKIN SECTIONS IAW SRM 51-30-2.SDR MWEA96625Door Frame · crackedDURING C-CHECK, FOUND CRACK EMANATING FROM UPPER DOOR STOP PAD IN AFT ENTRANCE DOOR FRAME. MAINTENANCE INSTALLED DOUBLER REPAIR IAW SRM 53-01, FIG 2 SHEET 4.SDR 97ZZZX1783Structure · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION FOUND AROUND NUTPLATES ON LT AND RT KIDNEY PANELS (AFT OF AUXILIARY FUEL TANK). REMOVED STR'S 30, 29R, 29L, 28R, 28L, 27R, 27L, 26R, 26L, INTERCOSTALS 26L AND 27L, AND 26R AND 27R, FRAMES 580, 585, 600, ANSDR 97ZZZX1779Frame · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP, THE AFT CARGO PIT, SUPPORT FRAME ABOVE LONGERON 30 AT STA 996 IS CORRODED. MECHANICALLY REMOVED CORROSION FROM STR 23R TO STR 23L. LESS THAN .002 INCH MATERIAL LOSS. WITHIN LIMITS IAW DC9 SRM 51-10-3 AND SRM 53-01 SDR 97ZZZX1778Frame · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP, FOUND FRAMES STA 130 AND STA 160 CORRODED BETWEEN LONGERON 28L AND LONGERON 28R. MECHANICALLY REMOVED CORROSION IAW DC9 SRM 51-10-3, MATERIAL LOSS LESS THAN .003 INCH (DEPTH GAUGE NR A-0299) WITHIN LIMITS IAW DC9 SRSDR 97ZZZX1777Frame · corrosionDURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND ON THE FRAME AT STA 120 AT 28L TO LONGERON 28R. REMOVED CORROSION, ALODINED AND PRIMED IAW DC9 SRM 51-10-3 AND SRM 53-02 FIG 1. MATERIAL LOSS LESS THAN .005 INCH, NDT METHOD DME NR A-1244.SDR 97ZZZX1776Vertical Beam · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP, FOUND VERTICAL BEAM AT STA 218 LONGERON 30 CORRODED. MECHANICALLY REMOVED CORROSION IAW DC9 SRM 51-10-3, MATERIAL LOSS LESS THAN .003 INCH (DEPTH GAUGE NR A-0299) WITHIN LIMITS IAW DC9 SRM 53-01 FIG 1, ALODINED AND SDR 97ZZZX1775Support · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP, FOUND FLOOR SUPPORT AT STA 218 CORRODED ABOVE LONGERON 29L. REMOVED CORROSION IAW DC9 SRM 51-10-3. CORROSION REMOVED FROM EDGE OF FLANGE .005 INCH, WITHIN LIMITS IAW DC9 SRM 53-01 FIG 1. ALODINED AND PRIMED IAW DCSDR 97ZZZX1774Longeron · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP, FOUND LONGERON 28L CORRODED STA 180 - STA 200. MECHANICALLY REMOVED CORROSION IAW DC9 SRM 51-10-3. MATERIAL LOSS LESS THAN .002 INCH (DEPTH GAUGE NR A-0299) WITHIN LIMITS IAW DC9 SRM 53-01 FIG 1, ALODINED AND PRIMESDR 97ZZZX1773Longeron · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP, FOUND LONGERON 28L AND INTERCOSTAL CORRODED BETWEEN STA 160 AND STA 180. REMOVED INTERCOSTAL IAW DC9 SRM 51-30-2, MECHANICALLY REMOVED CORROSION IAW DC9 SRM 51-10-3. MATERIAL LOSS LESS THAN .005 INCH (DEPTH GAUGE NSDR 97ZZZX1772Subfloor · corrosionDURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND ON THE SUB-FLOOR BETWEEN STA 130 AND STA 140 BL 13R. REMOVED CORRODED AREA, FABBED UP DOUBLER AND FILLER IAW DC9 SRM 51-10-4. ALODINED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED DOUBLER AND FILLSDR 97ZZZX1771Floor Panel · corrosionDURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION FOUND ON THE COCKPIT FLOOR CENTER PANEL. REMOVED CENTER COCKPIT FLOOR IAW DC9 SRM 51-30-1, MECHANICALLY REMOVED CORROSION FROM HAT SECTIONS. LESS THAN .001 INCH REMOVED, FOUND WITHIN LIMITS IAW DC9 SRM 51SDR 97ZZZX1762Longeron · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP., LONGERON 27R WAS FOUND CORRODED FROM STA 110 TO STA 160. BLENDED OUT CHAFE MARKS IAW DC9 SRM 53-01, FIG 2. MATERIAL OUT OF LIMITS IAW DC9 SRM 53-01, FIG 2. PERFORMED FIBERGLASS REPAIR OF INTERIOR MOLDING PANELS ISDR 97ZZZX1761Floor Beam · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP., THE AFT CARGO PIT CABIN FLOOR BEAM AT STA 980 WAS FOUND CORRODED AT BL 34R. MECHANICALLY REMOVED CORROSION TO .075 INCH, FOUND TO BE OUT OF LIMITS IAW DC9 SRM 53-05 FIG 20A. CUT OUT CORRODED AREA FROM RBL 18 TO RB
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