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 DALA2018081305045Pan · crackedCRACKED RT RING PAN, BS 845. THE RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 2, VOL 1.SDR DALA2018081305044Pan · crackedCRACKED LT RING PAN, BS 1079, 1098, 1117, AND 1136. THE RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 2, VOL 1.SDR DALA2018081305043Pan · crackedCRACKED RT RING PAN AT BS 1155, 1174, 1231, 1250, AND 1288. THE RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 2, VOL 1.SDR DALA2018081305042Floor Support · crackedCRACKED FLOOR SUPPORT BL 0, BTW BS 1344 & 1364. THE FLOOR SUPPORT WAS REPLACED IAW SRM 53-10-03, VOL III.SDR DALA2018081305041Support · crackedCRACK SUPPORT ON THE LT TUNNEL BETWEEN BS 76 AND 69 WITHIN THE NLG WHEEL WELL. THE SUPPORT WAS REPLACED IAW SRM 51-30-05, VOL.SDR DALA2018081305040Longeron · crackedCRACKED LONGERON 2R, BS 575. THE LONGERON WAS REPAIRED IAW SRM 53-10-01, PAR 4, VOL I.SDR DALA2018081305048Web · damagedSTEERING ACTUATOR MADE CONTACT WITH LEFT NOSE GEAR SUPPORT WEB. REMOVED DAMAGE ON NLG SUPPORT WEB IAW SRM 53-90-01. PERFORMED DVI OF REPAIR AREA PER MD-90 SRM 53-90-01, NO OTHER DAMAGE NOTED. FABRICATED DOUBLERS & FILLER PER MD-90 SRM 53-90-01. INSTALLED DOUBSDR DALA2018081305047Uplock Sensor · failedNLG UNSAFE INDICATION AFTER TAKEOFF WITH GEAR HANDLE UP. AFTER CYCLING NLG, ENCOUNTERED NG DOOR NOISE. LOWERED GEAR AND HAD ALL NORMAL INDICATIONS. RETURNED TO DEPARTURE, WITH HYDRAULIC PRESSURES NORMAL. FOUND THE UPLOCK SENSOR D1-31 IN POOR CONDITION. IMPEDSDR DALA201808135038Cusp Web · corrodedCORROSION FOUND ON THE RT CUSP WEB, BS 756, RBL 54 - 58 . THE CUSP WEB WAS REPAIRED IAW SRM 53-20-02, FIG 18, VOL. I.SDR DALA201808135037Cusp Web · crackedCRACKED RT CUSP WEB, BS 897 TO 907, RBL 54 AND 56. THE CUSP WEB WAS REPAIRED SRM 53-20-02, VOL 1.SDR DALA2018081004976Cusp Web · dentedDENT FOUND ON THE RT CUSP WEB, BS 334 TO 336, BETWEEN LBL 51 AND 54 IN THE PAX CABIN. DAMAGED AREA WAS REPAIRED IAW SRM 53-00-01, FIG 2, VOL L.SDR DALA2018080644881O-Ring · leakingATTENDANTS REPORTED A FUEL ODOR FROM ROW 27 AND BACK. INSPECTED EXTERNAL AREAS OF THE ACFT, APU FUEL SHROUD DRAIN AND APU INLET. NO EVIDENCE OF FUEL LEAKS. CHANGED COALESCER BAGS FOR BOTH SIDES. FOUND AN O-RING INSIDE THE WATER SEPARATOR. CLEANED INSIDE SDR DALA2018080644880Battery Pack · inoperativeOVERWING EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE, LOWER INTERIOR EXIT SIGNS. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-55-03. OK FOR SERVICE.SDR DALA2018080604882Door · damagedA CRACK WAS FOUND ON THE FWD UPPER CORNER OF RAM ACCESS DOOR LAND STRUCTURE. REPAIRED IAW SRM 55-30-03, VOL 1.SDR DALA2018073104783Pin · disengagedDURING W/C 2561-2001 FOUND PARACHUTE PINS TO BE DISENGAGED ON L1 DOOR. SLIDE REQUIRES CHANGE. R&R L1 DOOR SLIDE PER W/C 2561-464.SDR DALA2018073104782Frame · crackedTAIL INTERIOR CANTED FRAME CBS 1520 AFT WEB NEAR 2 CLOCK POSITION IS CRACKED AT INR T-CHORD. REPAIRED STA 1520 CANTED BULKHEAD FRAME PRI 569819-14AD REV 0 AND ERA 569819-14AD REV ORIGINAL SECTION I.SDR DALA2018073104785Battery Pack · dischargedEMERGENCY LIGHT EXIT SIGN AT SEAT 34 INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT SEAT 32C IAW AMM 33-51-03.SDR DALA2018073104784Skin · departedON T-OFF ACT INFORMED US A PIECE OF ALUMINUM/METAL PART WAS FOUND ON THE RUNWAY. INSPECTED AND FOUND NR 1 ENG CNA AFT INNER SKIN MISSING. INSTALLED SERVICEABLE COMMON NOZZLE ASSEMBLY. ENGINE CLOSED AND T/R OPS CK GOOD. A/C OK FOR SVC.SDR DALA2018072704719Light · disconnectedDURING SERVICE CHECK FOUND TAIL COMPARTMENT EMERGENCY LIGHT INOP. FOUND LIGHT UNPLUGGED. RECONNECTED, OPS CHECK GOOD. OK FOR SVC.SDR DALA2018072704718Not Reported · corrodedSUB FLOOR UNDER FLOOR BOARDS 221GF AND 221HF IS IN CORRODED AT FASTENER HOLES BETWEEN STA 168 AND STA 200. REPAIRED W/ REF TO PRI 570298-14, REV 0; PRI 570298-14, REV 1 AND ERA 570298-14, REV ORIG.SDR DALA2018072704717Frame · not reportedERA 569819-14 SECTION I ISSUED FOR REPAIR TO STA 1520 NEAR L7R. REPAIRED STA 1520 CANTED BULKHEAD FRAME REF PRI 569819-14AD REV ORIGINAL.SDR DALA2018072504674Frame · crackedTAIL INTERIOR CANTED FRAME CBS 1520 AFT WEB NEAR 10 CLOCK POSITION IS CRACKED AT INNER T-CHORD. REPAIRED WEB REF SRM 53-10-03 FIG 9C.SDR DALA2018072404640Skin · crackedLEFT SIDE FUSELAGE APPROXIMATE LOCATION FRAME 1496 BETWEEN STRINGER 3 AND 4. TWO CRACK INDICATION WITH BAY MARKED. REPAIRED PER PRI 570252-14 REV 0,1,2 AND ERA 570252-14 REV ORIGINAL.SDR DALA2018071904561Battery · dischargedL1 AND L2 DOOR HANDLE EMERGENCY EXIT SIGNS INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY/BATTERY IAW AMM 33-51-03 OPS CHECK GOOD.SDR DALA2018071204449Wire · brokenDURING SERVICE CHECK FOUND AFT ACCESSORY COMPARTMENT EMERGENCY LIGHT L2-847 INOP. FOUND WIRES BROKEN AT LIGHT CONNECTOR REPAIRED PER WDM 33-51-14 OPS CHECK GOOD OK FOR SVC.SDR DALA2018071004438Spoiler · damagedLEFT WING OUTBOARD FLIGHT SPOILER INBOARD SIDE CONTACT WEAR ON SPOILER AND WING TRAILING EDGE AT STOP PAD AREA. REPLACED STOP PAD PER SRM 57-20-03 AND REPAIRED SPOILER DAMAGE PER SRM 57-50-01.SDR DALA2018071004437Stop Fitting · wornLEFT WING OUTBOARD FLIGHT SPOILER OUTBOARD SIDE CONTACT WEAR ON SPOILER AND WING TRAILING EDGE AT STOP PAD AREA. REMOVED AND REPLACED INBD AND OTBD SPOILER STOP PADS. REPAIRED TRAILING EDGE SUPPORT PER PRI 569818-14 REV 0 AND ERA 569818-14 REV, SRM REF 57-50-0SDR DALA2018070304344Wire · burnedRED NOSE GEAR UNSAFE LIGHT ON. PERFORMED BITE CHECK OF PSEU, RECEIVED CODES 310-PROX CARD,380 LOGIC CARD,457-NOSE LOCKED SENSOR WIRING. FOUND ARCHED AND BURNT WIRES M421B18, M420B18, L317C20, L319C20, L328C20, L329C20, G236KL20RD, G236L20BL, L408H18, L408J18, SDR DALA2018070204343Wire · brokenAFT ACCESSORY COMPARTMENT LT SIDE OF CATWALK HAS INOP EMERGENCY LIGHT. IDENTIFIED FIXTURE AS L2-845. RANG FROM P1-1211 TO R5-3803, R5-3804. FOUND R5-3803 OPEN, INSPECTED FURTHER AND FOUND WIRE BROKEN IN AMPHENOL CONNECTER. RETERMINATED WIRE AND REINSERTED INTOSDR DALA2018070204346Control Unit · malfunctionedATO, ON THROTTLE RUN-UP DURING T/O AT APPROX 1.20-1.28 PER, "FIRE, RT ENG" AURAL TONE, RED LIGHT RT HANDLE, AND MASTER CAUTION LIGHTS. RED LIGHT STAYED ON PERSISTENTLY AFTER RUNNING QRH. THE CREW BLEW THE FIRE BOTTLES AND CFR WAS DISPATCHED TO THE AIRCRAFT. RESDR DALA2018070304347Slide · unserviceableFOUND L1 SLIDE PACK RETAINING PINS HAD FALLEN OUT OF EYELETS. R&R SLIDE PACK ON L1 DOOR PER AMM 25-61 AND W/C 2561-4641 A/C OK FOR SVC.SDR DALA2018070304345Light · inoperativeFWD GALLEY EMER. EXIT SIGN HAS SEVERAL INOP BULBS. RELAMPED FWD GALLEY EMER EXIT SIGN LIGHT BULBS PER AMM 33-51-18. OPS CHECKS GOOD.SDR DALA2018062904273Power Supply · inoperativeTWO EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY IAW MM 33-50. OP CHECKED GOOD.SDR DALA2018062904274Cable · bindingAFT VENTRAL STAIRS INOPERATIVE WILL NOT OPEN. DURING CHECKS, FOUND THE CONTROL CABLE ASSY FROM THE HANDLE BINDING IN THE OPEN DIRECTION. R & R BRACKET ASSEMBLY. REPLACED AFT VENTRAL STAIRS TELEFLEX CABLE.SDR DALA2018062704241Web · corrodedCORROSION ON WEB ON STEP 5 AT VENTRAL STAIRWAY. WAS ACCOMPLISHED PER NDT SPM 04-00-07 PAR 5 FIG 3; ORIGINAL THICKNESS IS 0.040" AND MINIMUM REMAINING THICKNESS IS 0.024" THEREFORE AREA IS OUT OF LIMITS PER ER/A: 511165-14MA REV D. WEB ON STEP 5 AT VENTRAL STAISDR DALA2018062804240Rod · corrodedCORROSION ON ROD P/N NAS354-4-270 AND ROD-END P/N XREP3F4S181. ROD AND ROD-END 2EA WERE REPLACED PER AMM 27-26-01-420-801. ROD AND ROD-END 2EA WERE ADJUSTED PER AMM 27-26-01-820-801 FUNCTIONAL TEST OF THE RUDDER THROW LIMITER WAS PERFORMED PER MD90 AMM 27-26-0SDR DALA2018062604228Compressor · damagedDIV - TO ICT FOR LEFT ENGINE COMPRESSOR STALL AT FLIGHT LEVEL 260. ASSOCIATED RISING EGT. ENGINE POWER REDUCED TO IDLE, COMPRESSOR STALLS DISCONTINUED. ENGINE WAS NOT SHUT DOWN. FLIGHT DIVERTED TO ICT. BORESCOPED ENGINE FOUND 3RD, 5TH AND 6TH STAGE HPC DAMAGE.SDR DALA2018062654223Acm · seizedAT THE GATE, USING HUFFER AIR, HOT AIR ODOR AND REPORTED HAZE IN THE CABIN. AFTER STARTING THE NR 1 ENGINE, DISCONNECTED EXTERNAL AIR AND SWITCHED TO ENGINE AIR, CABIN AIR SUPPLY TEMP HIGH. ENGINE SHUTDOWN. LEFT ACM FOUND LOW ON OIL, RIGHT ACM FOUND TO BESDR DALA2018062604225Panel · missingPANEL MISSING ON THE NR 1 ENGINE PYLON. INSTALLED A REPLACEMENT PANEL IAW AMM 20-10. OK FOR SERVICE.SDR DALA2018062654221Spar · corrodedLEFT WING UPPER PANELS FOUND THE AFT SPAR, LOWER FWD CHORD EXFOLIATED AT XRS 545.38. ACCOMPLISHED A PERMANENT REPAIR ON AFT SPAR IAW ER/A 568227-14, REV ORIGINAL. HFEC ACCOMPLISHED.SDR DALA2018062654220Skin · crackedWHILE ACCOMPLISHING OPEN HOLE INSPECTION IAW PRI 568225-14, R1, STEP 7, FOUND A CRACKED INDICATION ON THE NR 7 LT WING UPPER SURFACE XOS 324, REAR SPAR. ACCOMPLISHED A PERMANENT REPAIR IAW ER/A 268226-14, REV ORIGINAL. HFEC ACCOMPLISHED.SDR DALA2018062764227Skin · damagedDAMAGE FOUND ON THE DORSAL FIN SKIN, FWD OF ACCESS PANEL, AT FASTENER HOLES BY BSS 52. REMOVED THE DAMAGE AND REPAIRED IAW SRM 55-30-05, FIG 20, SHEET 3. AND APPLIED PROTECTIVE COATINGS.SDR DALA2018062654222Power Supply · inoperativeL1 DOOR UPPER EXIT EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE POWER SUPPLY.SDR DALA2018062764226Tab · damagedRUDDER TAB HAD FOUR AREAS OF MISSING PAINT AND FLAME SPRAY ON THE RT SIDE ALL UNDER FOUR SQUARE INCHES NOT LONGER THAN 2 INCHES IN ANY DIRECTION, AND ARE SEPARATED BY MORE THAN 2 INCHES AND NOT TOTALING MORE THAN 20 SQUARE INCHES. REPAIRED THE RUDDER TAB IAW SSDR DALA2018062524219Skin · damagedDAMAGE ON DORSAL FIN SKIN FWD OF ACCESS PANEL AT FASTENER HOLES BY STA 2FS-52. REMOVED NUT PLATE STRIP AND BACKING PLATE. TRIMMED DAMAGE PER MD 90 SRM 55-30-05. FABRICATED REPAIR DOUBLER FROM 7075-0.050, FILLER .040 7075-0 AND SPLICE .050 7075-0. INSTALLED REPSDR DALA2018062204130Line · leakingON LANDING, THE FLIGHT CREW STARTED THE APU WHILE TAXING TO THE GATE. SMOKE ODOR STARTED TO FILL THE PASSENGER CABIN. CREW SHUTDOWN THE APU AND THE SMOKE ODOR DISSIPATED. FOUND A HYDRAULIC LINE AT THE ANTI-SKID RETURN SOV LEAKING IN LEFT WHEEL WELL. SECURSDR DALA2018062604224Door Frame · crackedDURING A WALK AROUND, FOUND THE FWD RT MAIN GEAR DOOR FRAME CHANNEL CRACKED AT SEVERAL PLACES. REMOVED AND REPLACED THE DOOR FRAME CHANNEL IAW DWG 5930584. OPS CHECKED RT MLG DOOR.SDR DALA2018062104121Skate Angle · crackedRIGHT SKATE ANGLE WAS CRACKED AT THE BASE OF THE VERTICAL STAB, UNDER THE LEADING EDGE. REMOVED AND REPLACED THE ANGLE.SDR DALA2018062104120Shear Tie · crackedCRACKED SHEAR TIE AT BS 1494 OTBD OF LEFT DORSAL FITTING. REMOVED AND REPLACED THE SHEAR TIE IAW DWG 9953016-29.SDR DALA2018061904062Brake · fireSHIP 9250 - BRAKE/TIRE - NUMBER 4 BRAKE SMOKING/FLAMES UPON ARRIVAL. FUSE PLUGS BLOWN, TIRES FLAT. CORRECTIVE ACTION: REPLACED NUMBER 3 AND 4 WHEEL ASSEMBLIES. REPLACED NUMBER 4 BRAKE. INSPECTED AXLE WITH NO DAMAGE NOTED. PERFORMED ANTISKID WHEEL SPIN UP TEST
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