Boeing MD-90-30
Service difficulty reports · 6,066
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 = 'MD9030' 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 = 'MD9030' 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 DALA2015080504831Skin · crackedBS 1474, STR 2L SKIN CRACKED UNDER SHEAR CLIP. REPAIRED IAW ERA 538124-14, REV ORIG.SDR DALA2015080504830Skin · crackedFUSELAGE SKIN CRACKED AT NOSE W/W RT AFT DOOR AFT HINGE CUTOUT. REPAIRED REF SRM 53-30-01, FIG 17 VOL 1.SDR DALA2015080204789Slide · no testTAIL CONE DROPPED AS REQUIRED, SLIDE DID NOT DEPLOY, FOUND EVIDENCE OF SLIDE EXPANSION INSIDE OF CONTAINER. REPLACED SLIDE.SDR DALA2015120307355Control Valve · failedSTRONG ELECTRICAL SMELL ON FINAL. SMOKE IN COCKPIT AND CABIN. FOUND LEFT ACM SEIZED. R & R ACM AND LT PACK TEMP CONTROL VALVE IAW AMM. OPERATION CHECKS OK. PERFORMED DUCT BURNOUT IAW MM. NO ODOR NOTED.SDR DALA2015073104780Splice · looseL/E SPLICE, ZFS= 52.267, LT SIDE HAS 37 LOOSE FASTENERS. REMOVED LOOSE FASTENERS. CLEANED AND CHECKED HOLES. OK IAW DWG SG09550004, REV D.SDR DALA2015073104779Splice · looseL/E SPLICE, ZFS= 52-267, RT SIDE HAS 27 LOOSE FASTENERS. REMOVED LOOSE FASTENERS. CLEANED AND CHECKED HOLES IAW DWG SG09550004, REV D.SDR DALA2015073104778Fitting · crackedTAIL INTERIOR UPPER BATH TUB FITTING CRACKED AT BS 1494, AFT SIDE OF FRAME LBL 6. R & R IAW DWG5930609.SDR DALA2015072904777Release Cable · frayedTAILCONE JETTISON CABLE FRAYED. R & R CABLE.SDR DALA2015072904745Structure · leakingDIVERTED DUE TO OIL FUME ODOR IN CABIN. RT GENERATOR OFF AND RT AC POWER FAULT WITH CORRESPONDING LOSS OF AC POWER. RT GENERATOR OVERHEAT STATUS MESSAGE ON EOAP. SHORTLY AFTER ENGINE GENERATOR FAILURE, APU WAS STARTED. F/A REPORTED A SMOKE OIL FUME ODOR ISDR DALA2015072704658Unknown · odorELECTRICAL WIRE BURNING ODOR IN AFT PART OF CABIN DURING DESCENT. QRH GALLEY POWER AND SIDEWALL LIGHTS TURNED OFF. ODOR DISSIPATED. MAINTENANCE TROUBLESHOT. NO ODORS NOTED. REPLACED COALESCER BAGS AND RECIRICULATION FAN FILTER. COMPLETED DUCT BURN OUT. ASDR DALA2015072704655Battery Pack · failedF/A REPORTED A BURNING ACRID ODOR NEAR EXIT ROW AFTER TAKEOFF. MAINTENANCE FOUND EMERGENCY LIGHT BATTERY OVERCHARGED AND HOT OVER EXIT DOOR. R & R POWER SUPPLY AND BATTERY PACK IAW AMM. OPS CHECKED GOOD.SDR DALA2015072704657Blower · failedON POWER UP OF THE AIRCRAFT, RAMP AGENT REPORTED SPARKS AND ELECTRICAL FUMES COMING FROM LOWER RT SIDEWALL OF CARGO BIN 6. MAINTENANCE FOUND LAVATORY BLOWER TO BE THE SOURCE. R & R LAV BLOWER ASSY IAW AMM. OK FOR SERVICE.SDR DALA2015072704656Turnbuckle · brokenDURING SERVICE CHECK, FOUND CABLE AND TURNBUCKLE ASSY ON RT SIDE OF VENTRAL CATWALK BROKEN. REPLACED TURNBUCKLE ON RT SIDE. OPS CHECKED GOOD.SDR DALA2015072204652Cusp Web · crackedCUSP MEMBRANE CRACKED, BS 962, L18R. REPAIRED IAW SRM 53-20-02.SDR DALA2015071504451Skin · crackedSKIN CRACKED AT BS 1542, LT SIDE JUST OTBD OF AIRSTAIR CUTOUT. REPAIRED IAW SRM 53-00-01, FIG 6.SDR DALA2015070904278Lamp · inoperativeSEVERAL EMERGENCY EXIT LIGHTS WERE INOPERATIVE IN AFT VENTRAL STAIRWAY. REPLACED THE LAMPS. OPS CHECKED OK.SDR DALA2015070604125Skate Angle · crackedVERTICAL STABILIZER LT SKATE ANGLE CRACKED. DOUBLER REPAIRED IAW SRM 55-30-05.SDR DALA2015070704277Support Channel · crackedVENTRAL STABILIZER ACTUATOR SUPPORT CHANNEL CRACKED. REPAIRED IAW PRI ERA 537315-14.SDR DALA2015070704276Skin · crackedSKIN CRACKED, AFT SIDE OF BS 1475 BETWEEN STRINGERS 1 - 2R. REPAIRED IAW SRM 53-30-01, FIG 16 AND PRI/ERA 537342-14, REV O.SDR DALA2015070504124Longeron · crackedLONGERON 2L CRACKED AT BS 1475. REPAIRED IAW SRM 53-30-01, FIG 14.SDR DALA2015070504121Skin · crackedSKIN CRACKED AFT SIDE OF BS 1475 BETWEEN STRINGERS 1 - 2R. REPAIRED IAW SRM 53-30-01, RIG 16 AND ERA 537336-14, REV O.SDR DALA2015070704281Skin · crackedFUSELAGE SKIN CRACKED, BS 1494, BETWEEN STRINGERS 3 - 4R. REPAIRED IAW SRM 53-00-01.SDR DALA2015070904280Lanyard · unsecureL1 DOOR SLIDE LANYARD FOUND LOOSE. R & R THE SLIDE IAW AMDS 2561-4641.SDR DALA2015070704279Battery Pack · unsecureOVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE FROM ROW 13-21. FOUND BATTERY PACK UNSEATED, SEATED THE BATTERY. OPS CHECKED OK.SDR DALA2015072904744Skin · corrodedWING REAR SPAR, XRS 164 - 150 SKIN CORRODED. REPAIRED IAW ERA 513402-14, REV A.SDR DALA1614799221Longeron Splice · not reportedFUSELAGE, LONGERON L2L AND L2R, SPLICE REPAIR, STATION 1475537329-14MA.SDR DALA1515069229Longeron · damagedLONGERON L2L AND L2R, SPLICE REPAIR, BS 1475, REPAIRED IAW ERA 537329-14MA.SDR DALA2015070604123Skin · crackedFUSELAGE SKIN CRACKED, BS 1475, L2R. REPAIRED IAW ERA 537336.SDR DALA2015070604122Battery Pack · inoperativeEMERGENCY ESCAPE LIGHTING FOR CAT WALK FOUND INOPERATIVE. R & R THE BATTERY PACK IAW WDM. OPS CHECKED OK.SDR DALA2015070604126Shear Tie · crackedSHEAR TIE CRACKED BS 1475, STR 2R. SHEAR TIE REPLACED.SDR DALA201604502642Skin · damagedFOUND BARREL NUT BORES 22 AND 24, NO EDGE MARGIN ON LT FORWARD SKIN PANEL, MULTIPLE EMS REQUIRED. LIMITED RELEASE, UPON INSTALLATION OF THIS STABILIZER ONTO AN ACFT, THE INSTALLER MUST ATTACH AND COMPLY WITH ERA 542565-14, SECTION III. O/H IAW CMM 55-10-01 WISDR DALA2015062603977Frame · crackedLEFT FUSELAGE OVERWING FRAME AT BS 924 CRACKED AT CUSP WEB. R & R OVERWING FRAME AT BS 924 IAW AMDS 5310-01375-07-LT AND DWG SR90530027, CONFIG -7009.SDR DALA2015062503975Release Cable · failedTAILCONE FAILED TO RELEASE DURING FUNCTIONAL CHECK. REPLACED TELEFLEX CABLE IAW AMDS 5352-7116.SDR DALA2015062503976Skin · crackedFOUND CRACK ON FUSELAGE SKIN, LT SIDE, BS 1531. REPAIRED IAW SRM 53-00-01.SDR DALA2015062203895Catwalk · malfunctionedVENTRAL STAIR CATWALK WILL NOT STOW IN THE UP POSITION. R & R CLEVIS TO VENTRAL STAIR CATWALK IAW MM. OPS CHECKS OK.SDR DALA2015062203896Blade · damagedNR 2 ENGINE HAS FOD DAMAGE TO SEVERAL BLADES AND NOSE COWL. R & R 1ST STAGE FAN BLADES IAW AMM. PERFORMED VIBE SURVEY AND FAN BALANCE IAW AMM. CHECKS OK.SDR DALA2015062103894Nose Cowl · damagedRIGHT ENGINE NOSE COWL DAMAGED BY FOD EVENT. R & R NOSE COWL IAW AMM. PERFORMED ANTI-ICE CHECK.SDR DALA2015061903897Frame · crackedFRAME TAB IS CRACKED BEYONE LIMITS. R & R FS 962 RT FRAME IAW AMDS 5310-01375-09 AND DWG SR90530027.SDR DALA2015061203807Slide · malfunctionedWHILE CLOSING THE L1 DOOR THE SLIDE DEPLOYED. R & R L1 DOOR SLIDE.SDR DALA2015061503809Lanyard · brokenL1 DOOR SLIDE PARACHUTE PIN SAFETY LANYARD FOUND BROKEN. SECURED THE LINE WITH SAFETY STRING V-T-295 TO CLOVE HITCH IAW CMM.SDR DALA2015061503808Slide · unserviceableVENTRAL DOOR AFT SLIDE UNSERVICABLE. R & R SLIDE IAW AMDS 5352-7116.SDR DALA2015060903806Angle · corrodedCORROSION ON ANGLES LOCATED ON RT WING OTBD FLAP INNER STRUCTURE, XRS 164. FLAP AND VANES WERE R & R .SDR DALA2015060803805Slide · malfunctionedR1 SERVICE DOOR SLIDE DID NOT DEPLOY EXCEPT BY MANUAL TAB ONLY. R & R SLIDE.SDR DALA2015060803716Frame · crackedCANTED FRAME, BS 1508 AT LONGERON 1L CRACKED. REPAIRED IAW PRI 536755-14, REV 1 AND COMPLIED WITH ERA 536755-14, REV O.SDR DALA2015061003715Panel · crackedDURING A TAILCONE DROP, TAILCONE LOWER T/E PANEL WAS CRACKED AND DENTED. COMPLIED WITH ERA 463180-14MA PERMANENT REPAIR.SDR DALA2015060703714Fitting · crackedTAIL BATHTUB FITTING CRACKED AT RBL 6, AFT SIDE OF BS 1494. REPAIRED IAW PRI 536718-14, REV O. AND COMPLIED WITH ERA 536718-14, REV O.SDR DALA2015060703713Doubler · crackedINNER DOUBLER CRACKED AT LT AND RT SIDES. R & R IAW SRM 51-00-01.SDR DALA2015060703712Attach Angle · crackedFORWARD FORMER RT ATTACH ANGLE IS CRACKED, BS 1478. R & R THE ATTACH ANGLE IAW SRM 51-00-01.SDR DALA2015060403599Skin · corrodedCORROSION ON RT WING UPPER SKIN STA XRS=240. REPAIRED IAW ERA 534378-14 AD, REV O. LP 1976805.SDR DALA2015060103598Structure · corrodedCORROSION ON FIXED L/E AFT LOWER EDGE STA XRS=240. REPAIRED IAW ETI90-15052, REV 1 AND ERA 534406-14, REV O.
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