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 DALA2015022601703Cusp Web · corrodedCORROSION ON LT CUSP WEB MEMBRANE, STA Y=682, BETWEEN X=55 AND X=59, TASK 53-211-01. REMOVED CORROSION. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-20-02, FIG 18 AND 51-10-03.SDR DALA2015022601700Seat Track · corrodedCABIN SEAT TRACK, RBL 44 CORRODED, BS200-237 SEVERAL AREAS. TASK 53-211-02. R & R SECTION OF SEAT TRACK IAW SR 09530085, REV D AND SRM 53-20-01.SDR DALA2015022501697Cusp Web · corrodedRT CABIN CUSP WEB BS 598-617, RBL60 CORRODED. TASK 53-211-01. REMOVED CORROSION. FOUND TO BE OUT LIMITS. FABRICATED AND INSTALLED NEW CUSP WEB IAW SRM 51-10-05 AND DWG 9940443, REV A.SDR DALA2015022501695Bracket · brokenBROKEN BRACKET ON INBD FLIGHT SPOILER TORSION BAR, STA XRS=209 AT LT WING. INSTALLED NEW BRACKET IAW AMM.SDR DALA2016102607687Cusp Web · corrodedCORROSION ON LEFT HAND CUSP MEMBRANE FROM STA 750 TO 767 BETWEEN X=55/60 TASK 53-211-01. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-20-02, 51-10-03 AND 51-30-02.SDR DALA2015022401705Unknown · smokeAFTER LANDING, WHITE/GREY SMOKE FIRST CLASS BACK TO MID CABIN. DIMINSHED VISABILITY. TROUBLESHOT. NO TROUBLE FOUND. R & R COALESCER BAGS AND PERFORMED DUCT BURNOUT. OK FOR SERVICE.SDR DALA2015022501696Cusp Web · corrodedMAIN CABIN LT CUSP WEB CORRODED, BS 904-984, LBL 50. TASK 53-211-02. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-20-03, FIG 7 AND 51-10-03.SDR DALA2015022801924Cusp Web · corrodedRIGHT MAIN CABIN CUSP WEB CORRODED BS 1136-1153, RBL 60. TASK 53-211-02. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW CUSP WEB IAW SRM 53-20-02, 51-10-03 AND 53-40-02, FIG 26.SDR DALA2015022301647Cusp Web · corrodedCORROSION ON RT CUSP WEB, X 54 TO X 60 BETWEEN BS 929 - 940. FOUND OUT OF LIMITS AND WAS REPAIRED.SDR DALA2015022301646Support Fitting · corrodedCORROSION ON SUPPORT FITTING, BS 198 AND X 44. SUPPORT REPLACED IAW SRM 53-10-01, FIG 10 AND 51-30-02.SDR DALA2015022601650Skin · crackedFUSELAGE SKIN, BS 1395-1376, LONGERON L10 - 11R CRACKED. REPAIRD IAW ERA 523447-14A.SDR DALA2015022301653Lanyard · frayedFORWARD ENTRY DOOR GIRT BAR LANYARD FRAYED. R & R LANYARD IAW AMM 25-61.SDR DALA2015022601652Structure · handler errorJETWAY DAMAGED, FUSELAGE AFT OF L1 DOOR. COMPLIED WITH EAR 533293-14, SECTION I AND ER 533293-14, SECTION II.SDR DALA2015022301649Cusp Web · corrodedCORROSION ON LT CUSP MEMBRANE, BS 767 - 807 BETWEEN X 55 AND X 60. AREA OUT OF LIMITS. CORROSION REMOVED IAW ERA 520318-14MA, REV O.SDR DALA2015022601651Web · crackedCRACK ON INTERNAL WEB AT BS 200, LONGERON 15L. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED A REPAIR IAW SRM 53-60-02, FIG 15 AND 51-10-03.SDR DALA2015021801438Unknown · smokeHAZE AND SMOKE APPEARED DURING LANDING IN THE CABIN. ODOR WAS MUSTY AND NOTHING APPEARED TO BE BURNING. HAZE DISAPPEARED IN LESS THAN 5 MINUTES. APU WAS NOT RUNNING WHEN HAZE APPEARED. INSPECTED AND TROUBLESHOT PNEUMATIC SYSTEM. R & R RT TI SENSOR IAW MM. SDR DALA2015021701279Bulb · inoperativeMIDDLE OVERHEAD EMERGENCY LIGHT FWD OF AFT RAFT COMPARTMENT BULBS INOPERATIVE. REPLACED THE BULBS. OPS CHECKED GOOD.SDR DALA2015021701282Battery Pack · inoperativeCEILING EMERGENCY LIGHTS INOPERATIVE AT SEATS 23, 24 AND 26 RT SIDE. R & R BATTERY AND POWER SUPPLY IAW AMM. OPS CHECKED NORMAL.SDR DALA2015021701281Skin · bentL1 DOOR LOWER FORWARD FLANGE HAS SLIGHT BEND. INSPECTED AND STRAIGHTENED IAW SRM 52-01-01.SDR DALA2015021701280Pin · disengagedL1 DOOR SLIDE PIN IS NOT ENGAGED AT LOWER LOCATION. R & R L1 DOOR SLIDE IAW AMDS 2561-4641.SDR DALA2015022301648Cusp Web · corrodedCORROSION FOUND ON LT CUSP WEB, BETWEEN BS 846-974. REMOVED CORROSION FOUND TO BE OUT OF LIMITS.SDR DALA2015021301437Support Fitting · gougedLEFT MLG ACTUATOR RETRACT SUPPORT FITTING BEARING BORE IS GOUGED. MACHINED BORE TO 1.533. WITHIN LIMITS IAW DWG SR09570087. ACCOMPLISHED FPI OF LMLG ACTUATOR RETRACT SUPPORT FITTING BEARING BORE IAW PS 900-6-3 NR 2.SDR DALA2015021301226Skin · damagedLIGHTNING STRIKE DAMAGE TO THE FUESELAGE SKIN AT BS 53, JUST BELOW THE FRP. REPAIRED IAW ERA 92-533013.SDR DALA2015021301436Support Fitting · gougedRIGHT MLG ACTUATOR RETRACT SUPPORT FITTING BUSHING BORE IS GOUGED. MACHINED BORE TO 2.2835. WITHIN LIMITS IAW DWG SR09570087. ACCOMPLISHED FPI OF RMLG ACTUATOR RETRACT SUPPORT FITTING BUSHING BORE IAW PS 900-6-3, NR 2.SDR DALA2015021101221Frame · crackedON HFEC INSPECTION OF OVERWING FRAME, BS 962, HAD A CRACK INDICATION. R & R THE FRAME, IAW AMDS 5310-01375-09 LT.SDR DALA2015021101219Frame · crackedHFEC INSPECTION OF OVERWING FRAME HAS A CRACK INDICATION. FRAME REPLACED IAW DWG SR90530027.SDR DALA2015030501947Seat Track · corrodedCABIN SEAT TRACK, RBL 58 CORRODED, SCRATCHED AND BARE METAL SEVERAL AREAS. BS 21-569, TASK 53-211-01. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-40-01, FIG 6.SDR DALA2015021201227Skin · damagedTWO LIGHTNING STRIKES NEAR F/O WINDOW. REPAIRED ON CARDS 1-25.SDR DALA2015021201224Skin · gougedAFT CARGO DOOR INBD SKIN GOUGED NEAR AFT LATCH. FOUND PUNCTURE IN RADIUS AND GOUGE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-02.SDR DALA2015021201223Skin · damagedLIGHTNING STRIKE AT FASTENER, BS 53.25, RT BELOW F/O PITOT TUBE. REPAIRED IAW ERA 533013-14, REV A.SDR DALA2015021201222Skin · damagedLIGHTNING STRIKE AT FASTENER, BS 53, RT BELOW FIRST OFFICERS PITOT TUBE. REPAIRED IAW ERA 53013-14, REV A.SDR DALA2015021001218Strap · corrodedMID CARGO REPAIR SPACER STRAP HAS CORROSION, BS 693-750. R & R REPAIR SPACER STRAP IAW SRM 53-60-02, FIG 9.SDR DALA2015020901017Pin · missingL1 DOOR SLIDE PIN MISSING. R & R SLIDE ASSEMBLY.SDR DALA2015030501945Channel · corrodedCORROSION IN FORWARD LAVATORY FITTING AND CHANNEL ON FLOOR AFT CENTER OF FLOOR. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIRED PART IAW SRM 51-20-00 AND 51-30-02.SDR DALA2015020500914Coalescer Bag · odorON LANDING, F/A NOTICED YELLOW SWEET SMELLING SMOKE COMING FROM VENTS. MAINTENANCE RAN ENGINES AND REVERSER WITH NO FINDINGS. CHANGED COALESCER BAGS AND PERFORMED DUCT BURNOUT. OK FOR SERVICE.SDR DALA2015020400912Wire · brokenAFT AIRSTAIR EMERGENCY LIGHT L2-848 HAS BROKEN A WIRE AND THE LIGHT IS INOPERATIVE. REPAIRED THE WIRE IAW SWPM. OPS CHECKED GOOD.SDR DALA2015022001645Door Frame · corrodedFORWARD CARGO DOOR LOWER FORWARD FRAME CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED A REPAIR IAW SRM 53-60-02 AND 51-30-02.SDR DALA2015020400913Lamp · inoperativeMID CABIN CEILING EMERGENCY EXIT SIGN IS INOPERATIVE. REPLACED THE LAMPS. OPS CHECKED GOOD.SDR DALA2015020200840Transmitter · leakingON GROUND, WITH EXTERNAL AIR CONNECTED, STRONG ODOR OF FUEL AND EXHAUST FUMES FROM MID TO AFT OF ACFT. ODOR WAS PRESENT THROUGH MID CLIMB. MAINTENANCE FOUND FUEL FLOW TRANSMITTER LEAKING ON NR 1 ENGINE. R & R UPPER FLANGE O-RING IAW AMM. LEAK CHECK AND PACSDR DALA2015013000841Skin · crackedTHE UPPER AFT SKIN PANEL ON THE RT SIDE OF THE HORIZONTAL STABILIZER WAS FOUND CRACKED DURING INSPECTION. REPAIRED IAW ERA 531274-14, REV O.SDR DALA2015020200839Door · obstructedCOCKPIT DOOR JAMMED IN FLIGHT. MAINTENANCE FOUND D-RING FOR EMERGENCY EGRESS, NOT STOWED IN LATCHES. D-RING WAS JAMMED IN THE DOOR HINGE. REMOVED AND STOWED THE D-RING IN PLACE. OPS CHECKED GOOD.SDR DALA2015020200838Skin · crackedUPPER AFT SKIN PANEL ON THE RT SIDE OF THE HORIZONTAL STABILIZER WAS FOUND CRACKED. PERFORMED A BONDED REPAIR IAW ERA 531274-14AD.SDR DALA2015012800681Line · disconnectedFLIGHT CREW NOTICED IT TOOK MORE POWER THAN NORMAL TO TAXI TO GATE. BRAKE TEMPERATURE WAS NORMAL. APPROACHED GATE, BRAKE TEMP BEGAN TO RISE. TEMP ROSE TO MAX AND BRAKE BEGAN TO SMOKE. FIRE DEPARTMENT EXTINGUISHED A SMALL FLAME. MAINTENANCE FOUND NR 1 BRASDR DALA2015012800680Bulb · inoperativeTWO BULBS INOPERATIVE ON CATWALK EMERGENCY EXIT SIGN. REPLACED THE BULBS. OPS CHECKED GOOD.SDR DALA2015012800682Starter · failedREPORTED ELECTRICAL ODOR IN CABIN DURING PUSHBACK. MAINTENANCE FOUND APU STARTER ON FIRE. MAINTENANCE PUT OUT FIRE WITH PORTABLE FIRE EXTINGUISHER, PULLED AND COLLARED APU CONTROL AND STARTER CIRCUIT BREAKERS. APU REMOVED AND COMPARTMENT CLEANED. APU, LT ASDR DALA2015012300588Attach Bracket · corrodedCORROSION AROUND RIVETS OF D-RING ATTACH BRACKETS, TWO ON TAILCONES SLIDE VALISE. R & R THE ATTACH BRACKETS IAW SRM 51-30-02.SDR DALA2015012300590Latch · wornTAILCONE RELEASE SPADES WORN UPPER RT AND LOWER LT. REMOVED AND INSTALLED NEW LATCH SPADES IAW AMM 53-52-01.SDR DALA2015012300589Angle · corrodedLOWER CABLE RELEASE ANGLE PIN CORRODED. R & R THE ANGLE IAW MM 53-52-01.SDR DALA2015012300587Frame · corrodedAFT ACCESSORY COMPARTMENT, FRAME BS 1520 BETWEEN LONGERONS 1 - 24L, LOWER END OF FRAME HAS SEVERAL SPOTS WITH CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED A REPAIR IAW DWG 9911839, REV DP, SRM 51-30-02 AND 51-30-03.SDR DALA2015012100420Attach Angle · crackedRIGHT VERTICAL FIN ATTACH ANGLE DOUBLER, AT FIN AFT SPAR, HAS 2 CRACKS. REPAIRED IAW PRI 510815-14, REV A, SEC II, FINAL ERA 510815-14.
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