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 DALA2018022701208Frame · corrodedCORROSION FOUND ON THE FRAME WEB AFT FACE AT BS 1395 BETWEEN LONGERONS 27R & 27L. THE FRAME WAS REPAIRED IAW SRM 51-11-01, FIG 1, VOL 1.SDR DALA2018022601137Floor Panel · crackedINITIAL INSPECTION : CRACKED CHANNEL ON FLOOR PANEL 222VG, 222QG, 222KG, 222FG, 221XF, 221TF, 222AG, 222AWG, 222ANG, 222YF, 223JF, 222ADF IN PAX CABIN. FLOOR GENERATION PANEL 222VG, 222QG, 222KG, 222FG, 221XF, 221TF, 222AG, 222AWG, 222ANG, 222YF, 223JF, 222ADSDR DALA2018022601146Pan · crackedCRACKED RINGPANS (2EA) ON LT/RT WINDOW UPPER AFT CORNER OF STA 1003. (CRACK LONG 0.400") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022601145Pan · crackedCRACK ON RINGPAN LOWER CORNER FWD STA 1156 RT SIDE. (CRACK LONG 0.385") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022601144Pan · crackedCRACK ON RINGPAN OF WINDOW UPPER CORNER AFT STA 1135 AND LOWER CORNER FWD STA 1154 LT SIDE. (CRACK LONG 0.380") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022601143Pan · crackedCRACK ON RINGPAN OF WINDOW UPPER CORNER AFT STA 1078 LT SIDE. (CRACK LONG 0.0405") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022601142Pan · crackedCRACK ON RINGPAN OF WINDOW UPPER CORNER AFT STA 1116 LT SIDE. (CRACK LONG 0.380") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022601141Pan · crackedCRACK ON RING PAN AFT UPPER CORNER STA Y=1155 RT. (CRACK LONG 0.0380") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022601140Pan · crackedCRACK ON RING PAN FWD UPPER CORNER STA Y= 1002 AND FWD LWR STA Y= 1136 RT. (CRACK LONG 0.400") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022601139Floor Support · corrodedCORROSION ON FLOOR STRUCTURE SUPPORT AT STA 200, BTW X=7 TO X=-7LT/RT, X=8 TO X=14 LT AND STA 196, X=14 TO X =44 LT SIDE. CORROSION 2 IN REF NRC 00643 SUPPORTS WERE REPLACED 3 E/A PER SRM 51-30-02 AND 51-30-05.SDR DALA2018022601136Pan · crackedCRACK ON RING PAN FWD UPPER CORNER STA Y= 522 AND AFT LWR STA Y=943 RT. (CRACK LONG 0.380") AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022601135Pan · crackedCRACK ON RINGPAN OF WINDOW UPPER CORNER AFT STA 1097 AND LOWER CORNER FWD STA 1079 LT SIDE. AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022601134Pan · crackedCRACK ON RINGPAN UPPER CORNER AFT STA 1154 AND LOWER CORNER FWD STA 1137 LT SIDE. AREA WAS REPAIRED PER VOL I SRM 56-20-02 FIG 3.SDR DALA2018022801260Warning System · false activationFIRE LOOP B ENG 01 ILLUMINATED PRIOR TO DEPARTURE. T/S PER FIM 26-11-00-810-802 BITE CHK PER AMM 26-11 AND OPS CHK AMM 26-11. ALL CHKS GOOD NO DISCREPANCIES NOTED AT THIS TIME.SDR DALA2018022701209Skin · crackedWHILE PERFORMING LOW FREQUENCY EDDY CURRENT INSPECTION OF THE LT HORIZONTAL STABILIZER UPPER AFT SKIN PANEL IAW AMDS CARD 5510-01073-01 STEP 8 NOTED APPROX 0.5" CRACK INDICATION NEAR AFT BARREL NUT HOLES MARKED CRACKED LOCATION LFEC CONFIRMED CRACK.SDR DALA2018022701207Spar Cap · crackedWHILE PERFORMING OPEN HOLE EDDY CURRENT INSPECTION OF THE LT HORIZONTAL STAB REAR SPAR UPPER CAP (STEP 11 AMDS CARD 5510-01073-01), A VERTICAL CRACK INDICATION. CLEANED HOLE AND RECHECK IAW NDTSPM 06-10-001-003, CRACK INDICATION RUNS VERTICAL ABOVE HOLE AT 1 3SDR DALA2018022601138Longeron · crackedCRACK ON LONG 12 LT STA Y=1486 AT AFT ACCESSORY COMPARTMENT. LONG 12 LT STA Y=1486 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER VOL I SRM 53-10-01 FIG 7.SDR DALA2018022601133Floor Support · corrodedCORROSION OUT OF LIMITS ON FLOOR SUPPORT STA 200, X-7 TO X-44 AT CPAX W1(RT SIDE). LEVEL CORROSION 2 FLOOR SUPPORT WAS REPLACED PER SRM VOL II 51-30-02 AND 51-30-05.SDR DALA2018022601132Intercostal · crackedCRACK FLOOR STRUCTURE INTERCOSTAL BTW STA 1344 TO STA 1364, X=-0 CTR. NEW INTERCOSTAL BTW STA 1344 TO STA 1364, X=-0 WAS REPLACED PER VOL II SRM 51-30-02.SDR DALA2018022601131Splice · crackedLATE FINDING CRACK ON AFT LOWER INTERNAL SPLICE AT LT MLG DOOR. (CRACK LENGTH=4") AFT LOWER INTERNAL SPLICE AT LT MLG DOOR WAS REPAIRED PER CMM 32-17-05 REPAIR 2.SDR DALA2018022601130Web · crackedCRACKED WEB STA Y=218, X= -26 AT E&E COMPARTMENT CEILING AREA. DIMENSIONS CRACKS, 1.125", .750" WEB WAS REPAIRED PER VOL I SRM 53-00-01 FIG 6 AND VOL II SRM 51-30-02.SDR DALA2018022401122Floor Panel · damagedTWO SOFT SPOTS IN GALLEY FLOOR. FOUND ONE SOFT SPOT AT GALLEY AISLE THRESHOLD, AND ONE SPOT AT R1 GALLEY DOOR THRESHOLD. BOTH EXCEED ALLOWABLE DAMAGE LIMITS, WIP 957193. REMOVED RIGHT FWD GALLEY, REMOVED DAMAGE FLOORBOARDS 221LK, 221KF. 221QF STILL REQ. REPLACSDR DALA2018022401121Seat Track · corrodedCORROSION ON SEAT TRACK X=-22, BTW STA 200 TO STA 237 RT SIDE. LEVEL CORROSION 2 SEAT TRACK WAS REPLACED X=-22 STA Y=200 TO Y=266 PER SRM 51-30-01 AND 51-30-05 VOLUME II.SDR DALA2018022401120Seat Track · corrodedINITIAL INSPECTION. CORROSION ON SEAT TRACK X=-44, BTW STA 200 TO STA 256 RT SIDE. SEAT TRACK WAS REPLACED PER SRM 51-30-01 AND 51-10-05 VOLUME II.SDR DALA2018022301082Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PLATES NR 520AT, 520JB, 520DT ON LT WING. (CORROSION LEVEL 2) FUEL ACCESS PLATES NR 520DT, 520JB AND 520AT WAS REPLACED PER SRM VOL I 57-00-04 PAR 4 CONDITION II.SDR DALA2018022301081Web · corrodedINITIAL INSPECTION. CORROSION ON WEB STA Y=195, X=-55 AT E/E. (CORROSION LEVEL 2 ) MEMBRANE WAS REPAIRED PER VOL I SRM 51-11-01.SDR DALA2018022201056Beam · crackedINITIAL INSPECTION: CRACK ON BEAM 1 BTW STA Y195/200 AT FWD ENTRY DOOR L1. BEAM NR 1 BTW STA Y: 195-200 WAS REPAIRED PER SRM VOL I 52-10-02 PARAGRAPH 6, FIG 5.SDR DALA2018022201055Support · corrodedCORROSION ON FLOOR STRUCTURE SUPPORT BTW STA160 TO STA 200, X=7 TO X=-7 LT/RT SIDE. FLOOR SUPPORT WERE REPLACED PER SRM 51-30-01 VOL II.SDR DALA2018022201054Seat Track · corrodedOUT OF LIMITS CORROSION ON LT SEAT TRACK X=44 BTW STA Y 1277-1279 AT PASSENGER CABIN. AREA WAS REPAIRED PER VOL I SRM 53-40-01 FIG 2.SDR DALA2018022101053Shim · corrodedINITIAL INSPECTION: CORROSION ON SHIMS BELOW LOWER FITTING STA Y=1231 AT AFT CARGO DOOR. SHIMS BELOW LOWER FITTING STA Y=1231 AT AFT CARGO DOOR WERE REPLACED PER SRM 51-30-02, 51-30-05, 51-30-01 VOL II.SDR DALA2018022101052Power Supply · inoperativeMULTIPLE EMER LIGHTS IN F/C INOP. REMOVED & REPLACED APPLICABLE BATTERY POWER SUPPLY. OPS CHECK GOOD.SDR DALA2018022101051Wire · disconnectedTAIL COMP CATWALK ONE EMER LIGHT INOP. RECONNECTED WIRES & OPS CHECK GOOD.SDR DALA2018022101050Skin · crackedCRACK ON RAM AIR SCOPE AT VERTICAL STABILIZER LEADING EDGE. CRACKS ON RAM AIR SCOPE AT VERTICAL STABILIZER LEADING EDGE, WERE REPAIRED (WELDED) PER ER/A 382101-14MA REV H.SDR DALA2018022101022Cusp Web · crackedINITIAL INSPECTION, CRACK LT CUSP MEMBRANE ON STA Y=883 AT PASSENGER CABIN. REPAIRED PER VOL I SRM 53-20-02 FIG 6.SDR DALA2018022101021Cusp Web · puncturedINITIAL INSPECTION, PUNCTURE ON LT CUSP MEMBRANE STA Y=928 AT PASSENGER CABIN. DOUBLER WAS REMOVED ON STA Y=928 LT PER VOL II S-R-M 51-30-02 AND 51-30-01. PREVIOUS REPAIR DOUBLER WAS FABRICATED PER VOL II SRM 53-10-03, NEW DOUBLER WAS INSTALLED PER VOL II SRM SDR DALA2018022101020Seat Track · corrodedOUT OF LIMITS CORROSION ON SEAT TRACK BTW STA Y=1260-1263 AND X=22 AT PASSENGER CABIN. CORROSION 2 AREA WAS REPAIRED PER VOL I SRM 53-40-01 FIG 2.SDR DALA2018022101019Seat Track · corrodedOUT OF LIMITS CORROSION ON LT SEAT TRACK X=44 BTW STA Y 1262-1264 AT PASSENGER CABIN. AREA WAS REPAIRED PER VOL I SRM 53-40-01 FIG 2.SDR DALA2018021901001Battery Pack · dischargedEXIT LIGHTS ABOVE WING EXIT DOORS AT ROW 27 INOP. R&R BATTERY PACK AT ROW 27 PER AMM 33-51 CKS GOOD.SDR DALA2018021901000Web · crackedINITIAL INSPECTION. CRACKED WEB STA Y=133, X=7 AT COCKPIT FLOOR STRUCTURE. CRACK .750" AREA WAS REPAIRED PER SRM 53-00-01 PAR 8 FIG 6 VOL I.SDR DALA2018021800970Cusp Web · puncturedPUNCTURE ON THE RT CUSP WEB BETWEEN BS 1136 AND 1140, RBL 54 AND 60. REPAIRED IAW SRM 53-00-01, PARAGRAPH 5C, (2), (B), FIG 2.SDR DALA2018021800969Web · crackedCRACKED WEB, BS 1231. THE WEB WAS REPLACED IAW DWG 9957994, REV N, SRM 51-30-02, AND 51-30-05, VOL II.SDR DALA2018021800968Angle · crackedA CRACK ON THE ANGLE BETWEEN BEAM 5 AND INTERNAL PAN, BS 1231 AT AFT CARGO DOOR. THE ANGLE WAS REPLACED IAW SRM 51-30-02, 52-30-05, AND DRAWING 9957884, REV N.SDR DALA2018021700962Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PLATES NBR 520CT AND 620CT ON LH/RH WINGS. FUEL ACCES PLATES 520CT AND 620CT WERE REPLACED DUE TO BLEND OUT REPAIR IS NOT PERMITED PER MD-90 SRM VOL I 57-00-04 PAR 4 CONDITION III .
(LP0428283)SDR DALA2018021500938Light · inoperativeCEILING EXIT SIGN INOP AT 26 ABC-DEF. RELAMPED EXIT SIGN AT 26ABC-DEF CEILING REF AMM 33-51. CKS OK.SDR DALA2018021500937Light · unknownEMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE LOCATIONS:603. INSTALLED LIGHT STRIP PER AMM 33-41 OPS CK NORMAL MCO/PLAC RMVD.SDR DALA2018021400903Motor · failedSTRONG BURNING ODOR IN THE GALLEY, TURN OFF THE GALLEY POWER AND THE ODOR DISAPPEARED. FOUND THE FIRST CLASS LAVATORY SMOKE DETECTOR FAN MOTOR SEIZED AND EXTREMELY HOT. REPLACED THE FAN IAW AMM WDM 23-17.SDR DALA2018021400902Frame · crackedCANTED FRAME BS 1567 FOUND CRACKED AT THE UPPER TAILCONE GUIDE PIN. INSTALLED A DOUBLER IAW PRI 565774-14.SDR DALA2018021200858Relay · failedDURING WALK AROUND, ODSERVED OVERWING EMERGENCY LIGHT ON, ALSO ON EOAP EMERGENCY POWER AUTO FAULT AND MWCC STATUS MESSAGE. TROUBLESHOT FOUND EMERGENCY LIGHT WILL NOT TURN ON FROM COCKPIT SWITCH WILL WORK ON THE F/A FWD PANEL BUT WILL NOT TURN OFF AT F/A PANESDR DALA2018020900812Rib · damaged13 OF THE LOWER ATTACHMENT HOLES IN THE CENTER RIB ASSEMBLY, WERE FOUND TO BE OUT OF TOLERANCE. MAINTENANCE OVERSIZE THE HOLES IN THE RIB AND INSTALLED REPAIR BUSHINGS.SDR DALA2018030301348Floorboard · delaminatedDELAMINATED FLOORBOARD IN THE FORWARD GALLEY. A NEW FLOORBOARD WAS INSTALLED DURING C-CHECK ON N/R 302.
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