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.

SDR DALA2018051503010Intercostal · crackedTAILCONE INTERCOSTAL CRACKED BELOW RUDDER ACTUATOR ROD END AT BS 1567. FABRICATED A NEW INTERCOSTAL AND INSTALLED.May 2, 2018 · N924DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018051503009Angle · crackedANGLE CRACKED AT BS 1472, LONGERON 2R. REMOVED AND REPLACED THE ANGLE IAW DRAWING 9964460.May 2, 2018 · N924DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018051503008Angle · crackedANGLE CRACKED AT BS 1475. REMOVED AND REPLACED THE ANGLE AT LONGERON 2L IAW DRAWING 9964460.May 2, 2018 · N924DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018050102951Battery Pack · inoperativeDURING A SERVICE CHECK, FOUND THE FWD GALLEY FLIGHT ATTENDANT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AT B5-235 IAW AMM 33-51-03. OK FOR SERVICE.Apr 30, 2018 · N947DN · Doug MD9030 · Emergency LightingSDR DALA2018050102950Battery Pack · inoperativeDURING A SERVICE CHECK, THE VENTRAL DOOR EMERGENCY EXIT SIGN AND OTHER CEILING EMERGENCY LIGHTS FAILED TO TEST. PERFORMED TROUBLESHOOTING IAW WDM 33-51-12, FOUND TWO BATTERY PACKS DAMAGED B5-239 AND B5-237, REMOVED AND REPLACED THE BATTERY PACKS. OPS CHApr 30, 2018 · N916DN · Doug MD9030 · Emergency LightingSDR DALA2018043002905Battery Pack · inoperativeAFT BULKHEAD EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. R & R THE BATTERY PACK. OPS TESTED NORMAL.Apr 30, 2018 · N914DN · Doug MD9030 · Emergency LightingSDR DALA2018043002906Airstair · out of adjustTAIL STAIR CATWALK OUT OF RIG, BINDS AND CATCHES WHEN LOWERING AND WHEN RAISING. ADJUSTED TAIL STAIR CATWALK IAW AMM 53-25-01. OPS OK FOR SERVICE.Apr 27, 2018 · N960DN · Doug MD9030 · Entrance StairsSDR DALA2018042702849Shear Tie · crackedFOUND THE BS 1488.009 SHEAR TIE BETWEEN LONGERONS 2L & 3L CRACKED. REMOVED AND REPLACED THE SHEAR TIE.Apr 26, 2018 · N960DN · Doug MD9030 · Fuselage Internal Mounting StructureSDR DALA2018042702848Angle · crackedBS 1503.801, ANGLE WAS FOUND CRACKED BETWEEN LONGERON 1 & 3. REMOVED AND REPLACED THE ANGLE IAW SRM 53-10-04, AND 51-30-05.Apr 26, 2018 · N960DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018042702847Shear Tie · crackedFOUND THE BS 1503.801, SHEAR TIE BETWEEN LONGERONS 1 & 3 RIGHT CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW DWG 9911840.Apr 26, 2018 · N960DN · Doug MD9030 · Fuselage Internal Mounting StructureSDR DALA2018042702846Shear Tie · crackedBS 1503.801 SHEAR TIE BETWEEN LONGERONS 1 & 3 WAS FOUND CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW DWG 9911840, SRM 53-10-04, AND 51-30-05 JOB.Apr 26, 2018 · N960DN · Doug MD9030 · Fuselage Internal Mounting StructureSDR DALA2018042502808Shear Tie · crackedBS 1473.107. SHEAR TIE AT LONGERONS 2L & 2R CRACKED. REMOVED THE SHEAR TIE. MANUFACTURED A NEW SHEAR TIE IAW SRM 52-10-04. INSTALLED IAW SRM 53-10-04, AND 51-30-05.Apr 24, 2018 · N960DN · Doug MD9030 · Fuselage Internal Mounting StructureSDR DALA2018042402767Battery Pack · inoperativeR1 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK. EMERGENCY LIGHTS TESTED NORMAL.Apr 21, 2018 · N934DN · Doug MD9030 · Emergency LightingSDR DALA2018041902634Tire · failedTIRE FAILURE DURING TAKE OFF ROLL. ABS LIGHT CAME ON JUST PRIOR TO ROTATION. FLIGHT CONTINUED AND LANDED WITH NO ISSUES. FOUND THE NR 3 MAIN TIRE FAILED. REPLACED THE NR 3 AND 4 MAIN WHEEL ASSEMBLIES. REPLACED THE NR 3 BRAKE ASSEMBLY AND ANTISKID TRANSDUCERApr 19, 2018 · N934DN · Doug MD9030 · TireSDR DALA2018041802594Slide · damagedAFT TAILCONE SLIDE WAS FOUND TO BE UNWRAPPING. REMOVED AND INSTALLED SLIDE IAW 2561-4643.Apr 17, 2018 · N913DN · Doug MD9030 · Escape SlideSDR DALA2018041202383Power Supply · inoperativeDURING A SERVICE CHECK, FOUND OVERWING EMERGENCY EXIT EXTERNAL LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY B5-125 IAW AMM 33-51-03. LIGHTS OPS CHECKED NORMAL. OK FOR SERVICE.Apr 11, 2018 · N935DN · Doug MD9030 · Emergency LightingSDR DALA2018040902314Ring · defectiveDIV INTO DEN DUE TO RIGHT ENGINE IN INFLIGHT SHUT DOWN CAUSED BY LOW OIL PRESSURE. MTC FOUND OIL LEAKING FROM VSCF GENERATOR DRIVE PAD DRAIN. WINDMILLING INSPECTIONS PERFORMED AND VSCF SEAL FACE AND ROTATING RING REPLACED. LEAK CHECKS PERFORMED AND AIRCRAFT REApr 8, 2018 · N934DN · Doug MD9030 · Turbine Engine Oil SystemSDR DALA2018040502197Wire · brokenOVERHEAD EMERGENCY LIGHT AT ROW 21 WILL NOT ILLUMINATE. DURING INSPECTION FOUND WIRE BROKEN AT TERMINAL. REPAIRED THE WIRE. OPS CHECKED GOOD.Apr 5, 2018 · N940DN · Doug MD9030 · Light System WiringSDR DALA2018040302176Structure · corrodedFOUND CORROSION IN THE E & E BAY ABOVE AVIONICS RACK UNDER FWD GALLEY, BETWEEN BS 200 - 218.Apr 2, 2018 · N908DA · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018040302143Relay · failedDURING TAKE OFF, ENGAGED AUTO-THROTTLES AT 70 KNOTS. DC BUSS OFF MESSAGE APPEARED ON THE EPCU ANNUNCIATOR PANEL. ALL OTHER SYSTEMS & INDICATIONS NORMAL BEFORE AND AFTER ATO. PERFORMED NO GO ODI PREVENTION CHECK LIST. FOUND DC EMERGENCY POWER TRANSFER RELAY Apr 1, 2018 · N960DN · Doug MD9030 · DC Power Distribution SystemSDR DALA2018033102084Access Panel · damagedELONGATE HOLES ON ACCESS PANEL 370TL ON THE VERTICAL STABILIZER. THE ACCESS PANEL WAS REPAIRED IAW ER/A 567293-14, REV ORIGINAL, AND ETI-90-18-022, REV 1.Mar 30, 2018 · N912DN · Doug MD9030 · Vertical Stabilizer, Plate/SkinSDR DALA2018032902027Shutoff Valve · failedWHILE BOARDING, THE CREW REPORTED AN ANTI-SKID FAULT, FOLLOWED BY AN ELECTRICAL ODOR IN THE COCKPIT. REPLACED THE ANTI-SKID RETURN SHUTOFF VALVE. REPLACED THE APU STARTER AND COALESCER BAGS FOR THE ODOR. TERMINATED A BROKEN WIRE AT TERMINAL C642T20.Mar 29, 2018 · N952DN · Doug MD9030 · Brake Anti-Skid SectionSDR DALA2018070504360Structure · crackedWHILE PERFORMING VISUAL INSPECTION PER SRM 55-30-04 P 4, FOUND CRACK TO GO EXCEEDED PAST STOP DRILLS AND TO BE PAST MAX TOLERANCE. PERFORMED FPI INSPECTION OF SUBJECT AREA TO MARK ENDS OF CRACKS PER SRM 55-30-05. COMPLETED PERM REPAIR PER SRM 55-30-05 PAR 5.Mar 26, 2018 · N920DN · Doug MD9030 · Vertical StabilizerSDR DALA2018032501878Flashlight · inoperativeFOUND FLASHLIGHT UNDER F/A SEAT BY L1 DOOR OUT OF HOLSTER AND LIGHT NOT ILLUMINATED. FLASHLIGHT HOLDER BROKEN. REMOVED AND REPLACED FLASHLIGHT AND CRADLE ASSY PER MD90 AMM 25-60. CHECKED GOOD. REPLACED EMERGENCY STRAP.Mar 25, 2018 · N941DN · Doug MD9030 · Emergency EquipmentSDR DALA2018032601925Cable · damagedAFT ENTRY DOOR EMERGENCY TAILCONE RELEASE FAILED. DOOR ROD FAILED TO RELEASE CABLE QUADRANT AT DOOR UPPER FRAME. PULL TEST EXCEEDED LIMIT OF 15LBS. ACTUAL PULL TEST 40LBS TO BY PASS DOOR IN. LUBED CABLE ND REPLACED CABLE IAW AMM 20-52. OPS NORMAL WITHIN LIMITMar 24, 2018 · N942DN · Doug MD9030 · Aerodynamic FairingsSDR DALA2018032601924Cable · frayedTAILCONE EMERGENCY RELEASE LOCK CABLE FOR SUPPORT FITTING FRAYED AT CABLE BALL END. REPLACED THE CABLE IAW AMM 20-52.Mar 24, 2018 · N942DN · Doug MD9030 · Aerodynamic FairingsSDR DALA2018032601923Cable · damagedTAILCONE EMERGENCY RELEASE LOCK CABLE FORWARD OF TEE PIN FAILED TO RELEASE FROM SUPPORT FITTING, WHEN THE TEE PIN CAME OUT. REPLACED THE CABLE IAW AMM 20-52.Mar 24, 2018 · N942DN · Doug MD9030 · Aerodynamic FairingsSDR DALA2018032401861Angle · crackedCRACKED RT ANGLE TO ATTACH VERTICAL STABILIZER P/N 5912188-50 IN REF 5530-01034-0102. REPLACED PER SRM VOL I 51-30-02 AND 51-30-05.Mar 23, 2018 · N912DN · Doug MD9030 · Vertical Stabilizer Miscellaneous StructureSDR DALA2018032301847Floor Panel · not reportedPERFORM PERMANET REPAIR PER ER/A 560348-14 REV ORIG FLOOR PANELS NBRS 221KF AND 221LF WERE FABRICATED, REPLACED AND IDENTIFIED PER VOL 1 SRM 53-20-03 PAR 5 AND ER/A 560348-14 REV ORIGINAL AND WERE INSTALLED PER ER/A 560348-14 REV ORIGINAL.Mar 22, 2018 · N912DN · Doug MD9030 · Fuselage Floor PanelSDR DALA2018032201839Wire · burnedAUX HYD PUMP CB TRIPPED. FOUND WIRE BURNED AT LOC B1-110 ON RT AUX HYD PUMP CB T1. REMOVED SAFETY WIRE FROM RT AUX HYS PUMP. REPLACED BUS BA5R T1-SEE 24-50-00-19 SHEET 2 ITEM 55-A PHASE. REPLACED RT AUX HYD PUMP CB B1 764 50 A. SEE WDM 29-21-00 PG 1. PERFORMEMar 20, 2018 · N921DN · Doug MD9030 · Hydraulic Power System WiringSDR DALA2018031901802Support · corrodedAFTER REMOVE FLOOR PANELS IN REF LOG 3112788. CORROSION WAS FOUND ON AFT EVACUATION SLIDE LATCH SUPPORT X=-53 FROM STA Y=180 TO 200 AT FWD WET AREA. SLIDE LATCH SUPPORT WAS REPLACED PER SRM VOL II 51-30-01.Mar 18, 2018 · N912DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018031701777Bracket · crackedDURING INSPECTION, FOUND A CRACKED BRACKET ON FWD BULKHEAD AT THE RT UPPER ENGINE THRUST REVERSER. THE BRACKET WAS REPLACED.Mar 16, 2018 · N963DN · Doug MD9030 · Engine Thrust ReverserSDR DALA2018031901778Power Supply · inoperativeL2 DOOR SMALL EMERGENCY EXIT SIGN INOPERATIVE. REPLACED THE POWER SUPPLY & BATTERY.Mar 16, 2018 · N926DH · Doug MD9030 · Emergency LightingSDR DALA2018031601729Battery Pack · inoperativeDURING AN A CHECK, FOUND THE EXIT SIGN B5-231 BATTERY INOPERATIVE. REPLACED THE BATTERY AND CHECKED GOOD.Mar 16, 2018 · N940DN · Doug MD9030 · Emergency LightingSDR DALA2018031601727Rib · crackedCRACK ON RIB OF FIXED LEADING EDGE INTERIOR SURFACE SATA XOS 530 APROX LT WING. RIB WAS REPLACED PER SRM VOL II 51-30-02 AND 51-30-05, DWG 9919331-39 REV N.Mar 15, 2018 · N963DN · Doug MD9030 · Wing SparSDR DALA2018031401679Beam · crackedCRACK RT/LT WHEEL WELL DOOR JAMB INTERNAL SKIN STA Y= 47 AT NLG. BEAM WAS REPAIRED PER SRM VOL I 53-90-01 PAR 8. (LENGHT CRACK WAS 0.500"), FOR BEAM RT WAS ISSUED A NRC SERIAL NUMBER 00982 TO SEPARATE TYPE REPAIR, REPAIRED UNDER LOG 0463002.Mar 13, 2018 · N963DN · Doug MD9030 · Fuselage Main, StructureSDR DALA2018031401678Web · crackedCRACK ON WEB AT STA CANT Y=1542 AND 1HRS POSITION VENT BOX LOUVERS AREA AT AFT ACCESSORY COMPARTMENT. WEB WAS REMOVED PER VOL II SRM 51-30-02 DAMAGE WAS REMOVED PER SRM 53-00-01 PAR 8 FIG 6. REPAIR PARTS WERE FABRICATED PER SRM VOL I 53-00-01 PAR 8 FIG 6. REPAMar 13, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018031401677Skin · crackedCRACK RT WHEEL WELL DOOR JAMB INTERNAL SKIN STA Y=47 AT NLG. REPAIRED PER REV ETI-90-18-013 REV 4 AND ER/A 566722-14 REV ORIGINAL.Mar 13, 2018 · N963DN · Doug MD9030 · Fuselage Main, FrameSDR DALA2018031401676Intercostal · corrodedCORROSION ON INTERCOSTAL STA Y= 163 PROTECTION LONG 28L AT INNER FUSELAGE STRUCTURE E&E COMPARTMENT AREA. REPLACED PER SRM VOL II 51-30-02 AND 51-30-05, DWG 9911549 REV D.Mar 13, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018031301586Engine · failedAIR TURNBACK DUE TO A NR 1 ENGINE COMPRESSOR STALL AND BLUE FLAMES COMING FROM THE ENGINE AFTER TAKE-OFF, DURING CLIMB AT 2,300 FEET. THE FLIGHT CREW FOLLOWED THE QRH AND SHUT DOWN THE ENGINE AND RETURNED TO DEPARTURE. EGT EXCEEDANCE OF 730 DEG C. AN OVERWEIGHMar 13, 2018 · N929DN · Doug MD9030 · Engine (Turbine/Turboprop)SDR DALA2018031301584Web · damagedVERTICAL STAB WEB AT STA YV 157.7 LEFT SIDE NEAR STAB SCREWJACK HAS DAMAGE. REPAIR PER ERA 566268-14 REV ORG.Mar 12, 2018 · N911DA · Doug MD9030 · Vertical Stabilizer Miscellaneous StructureSDR DALA2018031301583Support · crackedCRACK ON INBD/OUTBD WEB SUPPORTS (2EAS) STA CANT 1542 AND 1HRS POSITION VENT BOX LOUVERS AREA AT AFT ACCESSORY COMPARTMENT. ANGLES WERE REPLACE PER VOL II SRM 51-30-05 AND DWG 9923630-5 REV L AND 9911839-158 REV DP.Mar 12, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018031301582Frame · corrodedCORROSION ON FRAME OF STA Y 1362 BTW LONGS 29R-26L AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2 WAS REPAIRED PER SRM VOL I 53-10-02 FIG 2.Mar 12, 2018 · N963DN · Doug MD9030 · Fuselage Main, FrameSDR DALA2018031301581Angle · crackedCRACK ON WEB ANGLE STA CANT 1542 AT 11 HRS POSITION AFT ACCESORY COMPARTMENT VENT BOX LOUVERS AREA. ANGLE WAS REPLACE PER VOL II SRM 51-30-05, SRM 51-30-01 AND 51-30-02.Mar 12, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018031301580Angle · crackedCRACK ON AFT ACCESORY COMPARTMENT VENT BOX LOUVER UPPER ANGLE STA CANT 1520 AND 1HRS POSITION. ANGLE WAS REPLACE PER VOL II SRM 51-30-05 AND 51-30-02.Mar 12, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018031201555Skin · crackedCRACK ON SKIN CUTOUT ON LT AFT NLG DOOR AFT HINGE AT EXTERNAL FUSELAGE. SKIN CUTOUT ON LT AFT NLG DOOR AFT HINGE AT EXTERNAL WAS REPAIRED PER SRM VOL I 53-30-01 PAR 14, AND VOL II 51-30-02 AND 51-30-05.Mar 11, 2018 · N963DN · Doug MD9030 · Fuselage Main, Plate/SkinSDR DALA2018031201554Longeron · crackedCRACKED LONG 20 LT STA Y= 1050 AT LT MLG WHEEL WELL AREA. LONG 20 LT STA Y= 1050 WAS REPAIRED (CRACK 1") PER SRM VOL I 53-10-01 FIG 9.Mar 11, 2018 · N963DN · Doug MD9030 · Fuselage Main, Longeron/StringerSDR DALA2018031201553Fitting · corrodedCORROSION ON SEVERAL CLIPS FROM STA Y 1212-1269 LONG 19R AT AFT CARGO COMPARTMENT DOOR JAMB. CLIPS WERE REPLACED PER SRM VOL II 51-10-05.Mar 11, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous StructureSDR DALA2018031101551Longeron · corrodedCORROSION LEVEL 2. CORROSION ON LONG 30 STA Y=218 AT INNER STRUCTURE E/E COMPARTMENT. LONGERON 30 BTW STA Y=160-229 WAS REPLACED PER SRM VOL II 51-30-02 AND 51-30-05.Mar 10, 2018 · N963DN · Doug MD9030 · Fuselage Main, Longeron/StringerSDR DALA2018031001550Fitting · corrodedCORROSION ON CLIP SUPPORT OF STA Y=1212 AT AFT CARGO COMPARTMENT. CLIP WAS REPLACED PER SRM VOL II 51-30-05 DWG 5936660 REV BZ.Mar 9, 2018 · N963DN · Doug MD9030 · Fuselage Miscellaneous Structure
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