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 96521Light · inoperativeDURING SERVICE CHECK, FOUND AFT CABIN EMERGENCY FLASH LIGHT LED NOT FLASHING. MAINTENANCE REMOVED AND REPLACED AFT CABIN EMERGENCY FLASHLIGHT.SDR 9619869613Connector · looseDURING FLIGHT, THE EMERGENCY EVACUATION LIGHTS ON SEATS KEEP FLASHING ON AND OFF. FOUND QUICK DISCONNECT CONNECTOR AT FS 250 LOOSE. RECONNECTED, OPERATIONAL CHECK NORMAL.SDR GTIA96NK201Oxy Hose · failedDURING CLIMB-OUT OF 18,000 FEET, CREW OXYGEN BOTTLE INDICATED JUST BELOW 1500 PSI. RETURNED TO DTW. SHUT OFF BOTTLE AT 1300 PSI. WITH BOTTLE OFF, OXYGEN STILL DECREASED TO 1200 PSI. REMOVED AND REPLACED CREW OXYGEN BOTTLE. FOUND CRACKED OXYGEN FITTING ON SDR GTIA96NK200Door Frame · crackedDURING X-RAY INSPECTION OF THE AFT PRESS BULKHEAD VENTRAL STAIR DOOR FRAME, A 1.375 IN CRACK WAS DISCOVERED AT THE UPPER LEFT CORNER. EVAULATED CRACK AS DESCRIBED PER SB53-137R4 PG 19 GROUP 22 COND 4. THE AIRCRAFT IS OK FOR CONTINUED SERVICE PER SB53-137R4 PASDR CA961001012Coffee Maker · elect short(CAN) CREW REPORTED BURNING SMELL COMING FROM COFFEE MAKER. COFFEE MAKER REPLACED.SDR 9619979950Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 12 THROUGH 14 INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.SDR 9619839609Bulkhead Web · crackedDURING LINE CHECK, FOUND A .375 INCH CRACK IN THE AFT PRESSURE BULKHEAD -13 SKIN AT THE UPPER LEFT DOOR STOP FITTING, LBL 6. ALSO, FOUND A CRACK IN THE UPPER RIGHT DOOR JAMB FITTING BEHIND THE STOP. REPLACED FITTING PER SRM 51-30-2 AND REPAIRED THE SKIN CRACSDR MWEA96516Power Supply · inoperativeDURING SERVICE CK, FOUND RT NACELLE LIGHT INOP. REPLACED BATTERY POWER SUPPLY, OPS CHECK GOOD.SDR MWEA96515Floor Beam · corrodedDURING INSP, CORROSION FOUND ON FLOOR BEAM TOP FLANGE STA 389 AROUND TWO HOLES 12 INCHES INBD LT SIDE. REPAIRED FLOOR BEAM IAW SRM 53-05.SDR MWEA96514Skin · chafedDURING INSP, RT WING LEADING EDGE WAS FOUND TO HAVE A CHAFED AREA ON BOTH SIDES OF THE NR 1 SLAT DRIVE TRACK. MAINT COMPLIED WITH REPAIR IAW SRM 57-06A, FIG 4.SDR MWEA96513Seat Track · wornDURING INSP, IT WAS FOUND THAT THE F/O'S LOWER AFT SEAT TRACKS INBD AND OUTBD HAD WORN ADJUSTMENT HOLES FOR THE SEAT LOCKING PIN. REPAIRED THE TRACKS IAW SRM 53-05, FIG 28.SDR MWEA96512Skin · chafedDURING INSP, RT WING L/E WAS FOUND CHAFED BY SCREWS JUST OUTBD OF VORTILON. COMPLETED REPAIR IAW SRM 57-06A, FIG 4.SDR MWEA96511Skin · chafedDURING INSP, BOTH LT AND RT SIDES OF VERT STAB CANOE FWD END EXTERNAL SKINS WERE HEAVILY CHAFED FROM THE FAIRINGS. REPLACED THE SKINS IAW SRM 55-31-0.SDR MWEA96510Frame · corrodedDURING INSP, FWD CARGO PIT STA 237 FRAME WAS FOUND CORRODED BETWEEN LONG 29L AND 29R. FABRICATED PARTS AND INSTALLED IAW SRM 53-03, FIG 2A.SDR MWEA96509Frame · corrodedDURING INSP, FWD CARGO PIT STA 256 FRAME WAS FOUND CORRODED FROM LONG 29L TO 29R. FABRICATED PARTS AND INSTALLED IAW SRM 53-03, FIG 2A.SDR MWEA96508Frame · corrodedDURING INSP, FWD CARGO PIT STA 313 FRAME WAS FOUND CORRODED ON FRONT SIDE FROM LONG 29L TO 29R. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-03, FIG 2A.SDR MWEA96507Longeron · crackedDURING INSP, LONG 4L WAS FOUND CRACKED AT FRAME ATTACH POINT AT STA 699. REPAIRED LONGERON 4L IAW DWG SR09530128.SDR MWEA96506Doubler · crackedDURING INSP, A CRACKED INTERCOSTAL WAS FOUND AT STA 180, 18 INCHES LEFT OF CENTER UNDER THE SUBFLOOR. REPAIRED THE INTERCOSTAL IAW SRM 53-01, FIG 2.SDR MWEA96505Rib · corrodedDURING INSP, LT WING RIB STA 164 BOTTOM INBD FLANGE AT STRINGER 16 WAS FOUND CORRODED. COMPLETED REPAIR IAW DAC TELEX SVC-MSP-0667/DLP DATED 9 AUG 96.SDR MWEA96504Access Panel · corrodedDURING INSP, RT WING LARGE LEADING EDGE LOWER ACCESS PANEL WAS FOUND TO HAVE CORROSION AT STA XRS 140. FABRICATED A REPAIR AND INSTALLED IAW SRM 57-01.SDR MWEA96503Spar · corrodedDURING INSP, RT WING REAR SPAR LOWER TEE CAP HORIZONTAL LEG BLEND OUT REPAIR AT STA XRS 179 REQUIRED EVALUATION. FABRICATED AND INSTALLED A REPAIR IAW SRM 57-09, FIG 11.SDR MWEA96502Spar Cap · crackedDURING INSP, A 1.25 INCH CRACK FOUND IN RT ELEVATOR UPPER SPAR CAP AT STA XE151. COMPLETED A REPAIR IAW SRM 55-02 FIG 9, CONFIGURATION -503.SDR MWEA96501Angle · crackedDURING INSP, A CANTED FRAME FWD ATTACH ANGLE WAS FOUND CRACKED AT STA 1121 BETWEEN LONG 17 AND 18R APPROX 6 INCHES. FABRICATED AND INSTALLED A REPAIR IAW SRM 53-01, FIG 2 SHEET 4.SDR MWEA96500Angle · corrodedDURING INSP, STIFFENERS IN AFT ACCESS COMPT OF FRAME 1132 WEB RT SIDE AT LONG 12 AND 13 RT WERE FOUND SEVERELY CORRODED. CLEANED UP THE CORROSION AND INSTALLED A NEW L-ANGLE IAW SRM 51-30-2.SDR MWEA96499Stiffener · corrodedDURING INSP, A STIFFENER WAS FOUND EXFOLIATED IN AFT ACCESS COMPARTMENT ON CANTED FRAME WEB AT STA 1132 AND LONG 12L. INSTALLED NEW STIFFENER IAW SRM 51-30-2.SDR MWEA96498Bracket · crackedDURING INSP, STRUCTURE UNDER THE RT CATWALK RETRACT CABLE ARM SUPPORT BRACKET WAS FOUND CRACKED. REPAIRED STRUCTURE IAW SRM 53-01 FIG 2, SHEET 4.SDR MWEA96497Skin · chafedDURING INSP, LT AND RT SIDES OF THE VERTICAL STAB CANOE AFT END EXTERNAL SKINS WERE HEAVILY CHAFED FROM THE FAIRINGS. REPLACED SKINS IAW SRM 55-31-0.SDR MWEA96496Skin · corrodedDURING INSP, FOUND A SMALL AREA OF SURFACE CORROSION ON BOTTOM SKIN OF LT PYLON. FOUND CORROSION OUT OF LIMITS AND FABRICATED A REPAIR IAW SRM 54-01, FIG 2 AND INSTALLED IAW SRM 51-30.SDR MWEA96495Jamb · crackedDURING INSP, AN INTERCOSTAL WAS FOUND CRACKED IN FWD CARGO DOOR FWD JAMB AT STA 380, CRACKED PAST A STOP DRILL. COMPLETED REPAIR IAW SRM 53-01.SDR MWEA96494Frame · corrodedDURING INSP, MODERATE CORROSION FOUND ON THE AFT SIDE OF FRAME 389 IN FWD CARGO COMPT AT LONGERON 30. REPAIRED FRAME IAW SRM 51-10-2A.SDR MWEA96493Longeron · crackedDURING INSP, LONG 17R WAS FOUND CRACKED AT STA 965. COMPLETED A REPAIR IAW SRM 53-02, FIG 2.SDR MWEA96492Angle · corrodedDURING INSP, LT CUSP ANGLE IN LT LAV AREA WAS FOUND MODERATELY EXFOLIATED AT STA 990. COMPLETED A REPAIR TO CUSP ANGLE IAW SRM 53-05, FIG 25.SDR MWEA96491Skin · crackedDURING INSP, FUSELAGE SKIN WAS FOUND CRACKED IN LT LAV AT STA 992. REPAIRED THE SKIN IAW SRM 53-04, FIG 46.SDR MWEA96490Angle · corrodedDURING INSP, RT LAV CUSP ANGLE WAS FOUND SEVERELY EXFOLIATED AT STA 975. REPLACED CORRODED SECTION OF CUSP ANGLE PER SRM 53-05, FIG 25.SDR MWEA96489Bulkhead Web · crackedDURING INSP, RT LAV FWD BULKHEAD WAS FOUND CRACKED IN NUMEROUS PLACES AT THE LOWER EDGE FWD SIDE STA 965. REPAIRED THE BULKHEAD PER SRM 53-03 FIG 21.SDR MWEA96488Frame · crackedDURING INSP, A FRAME WAS FOUND CRACKED WHERE IT ATTACHES TO THE LONGERON AT FRAME STA 980, LONG 17R. REPAIRED THE FRAME IAW SRM 53-03, FIG 32.SDR MWEA96487Spar · corrodedDURING INSP, FOUND RT WING HAD EXFOLIATION CORROSION IN TWO PLACES ON FRONT SPAR FWD LOWER TANG AT STA XRS-167 AND XRS-200-210. COMPLETED REPAIRS IAW DAC TELEX DATED 6 AUG 96.SDR MWEA96486Spar Cap · corrosionDURING INSP, RT WING LOWER FWD FLANGE OF SPAR CAP WAS FOUND WITH SEVERE EXFOLIATION CORROSION FROM STA XRS 295 TO 324. COMPLETED REPAIR IAW DAC TELEX SVC-MSP-0630/RMK DATED 31 JULY 96.SDR MWEA96485Steps · crackedDURING INSP, THE AFT AIRSTAIR THREE STEPS FROM BOTTOM HAS CRACKED RT SIDE. COMPLETED A REPAIR IAW SRM 52-01, SHEET 4.SDR MWEA96484Doubler · crackedDURING INSP, A 1 INCH CRACK WAS FOUND IN LT LOWER VENTRAL DOOR JAMB CORNER ON AFT SIDE. FABRICATED AND INSTALLED A REPAIR IAW SB 53-137R4.SDR MWEA96483Doubler · crackedDURING INSP, A 1.5 INCH CRACK WAS FOUND IN VENTRAL DOOR JAMB ANGLE DOUBLER BOTTOM RT END. REPAIRED ANGLE DOUBLER IAW SRM 51-30.SDR MWEA96482Frame · crackedDURING INSP, AFT ACCESSORY FRAME WAS FOUND CRACKED AT STA 1076 AT LONG 2L AND 2R. REPAIRED FRAMES IAW SRM 53-03, FIG 32.SDR MWEA96481Angle · crackedDURING INSP, LT PYLON TO FUS UPPER ATTACH ANGLE WAS FOUND CRACKED AT STA 935, 965 AND 1019. COMPLETED REPAIRS IAW SRM 54-04, FIG 10.SDR MWEA96480Angle · crackedDURING INSP, RT PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED IN 2 PLACES FWD EDGE OF LEADING EDGE. INSTALLED A REPAIR IAW SRM 54-04, FIG 10.SDR MWEA96479Fitting · damagedDURING INSP, FOUND PREVIOUS DAMAGE TO LONG 2R, 3R HAT CHANNEL LIP BETWEEN STA 640 AND 658 FITTINGS FOR ANTI-COLLISION LIGHT MOD. REPAIRED DAMAGED AREAS IAW SRM 53-01, FIG 2 SHEET 4.SDR MWEA96478Floor Beam · corrosionDURING INSP, FLOOR BEAM UPPER LEG AT STA 313, 12 INCHES INBD OF LONG 18L HAD A 1 INCH AREA OF EXFOLIATION CORROSION. FABRICATED AND INSTALLED A REPAIR IAW SRM 53-05, FIG 20A.SDR MWEA96477Window Frame · crackedDURING INSP, A CABIN WINDOW FRAME FWD LOWER LEG WAS FOUND CRACKED APPROX .1875 INCH FROM EDGE AT STA 600, LONG 15R. REPAIRED CRACK IAW SRM 53-01 FIG 2, SHEET 4.SDR MWEA96476Longeron · crackedDURING INSP, LONGERON 4L AND 3R WERE FOUND CRACKED AT FRAME ATTACH POINTS AT STA 756. SPLICED IN NEW SECTIONS OF LONGERON IAW DAC DWG SR09530128.SDR MWEA96475Longeron · crackedDURING INSP, LONG 5L AND 6L WERE FOUND CRACKED AT FRAME ATTACH POINTS AT STA 699. REPLACED SECTION OF LONGERONS IAW DAC DWG SR09530128.SDR MWEA96474Doubler · crackedDURING INSP, LT AND RT UPPER VENTRAL DOOR JAMB DOUBLERS WERE FOUND CRACKED. REPLACED DOUBLERS IAW SRM 51-30-2.
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