N990DL

Service difficulty reports · 238

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N990DL' AND registry_match = 'registration'
  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 DALA2016020100778Pan · crackedCRACKED INNER PAN AFT EDGE WITHBEAM 1 OF MID CARGO DOOR. CRACK INNER PAN AFT EDGE WITH BEAM 1 WAS ACCOMPLISHED INSPECTION. 2 CRACKS WERE FOUND 1.843 AND 0.250" LENGTH IAW SRM 06-10-01-001. CRACK WAS STOPPED IAW SRM 51-01, 21, A AND STEPS 1, 2 HFEC INSPECTIONJan 31, 2016 · N990DL · Doug MD88 · Cargo/Baggage DoorsSDR DALA2016020100777Longeron · crackedCRACKED LONGERON 3L WITH FRAME BS 1437 SECTION LONGERON WAS REPAIRED IAW SRM 51-30-5, 53-02, FIG 18, 51-10-4 AND 51-10-3.Jan 31, 2016 · N990DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016020100775Intercostal · crackedCRACKED INTERCOSTAL BETWEEN BS 1497 CANT TO 1510 CANT APPROXIMATELY 7 HRS POSITION. INTERCOSTAL WAS R & R IAW SRM 51-30-2 AND D/DWG 9917701, REV ORG.Jan 31, 2016 · N990DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016020100774Frame · crackedCONTINUE CRACK AFTER STOP DRILL ON REPAIR FRAME 1418 WITH LONG 2R. CRACK WAS DRILLED, ANGLE WAS REMOVED, SUPPORT WAS REMOVED, NEW ANGLE WAS FABRICATED AND TREATED AND PAINTED. SUPPORT WAS INSTALLED IAW IAW SRM 53-03, FIG 31A. FRAME WAS REPLACED IAW SRM 53-0Jan 31, 2016 · N990DL · Doug MD88 · Fuselage Main, FrameSDR DALA2016020100773Longeron · crackedCRACK LONGERON 9R WITH FRAME, BS 1380. LONGERON 9 RT WAS REPAIRED IAW SRM 53-02, FIG 18, AND DRILLED AND ADJUSTED IAW 51-10-4 AND WAS TREATED AND PAINT IAW SRM 51-10-3, PAR 21 AND 14 AND WAS INSTALLED IAW SRM 51-30-5 AND 51-30-2.Jan 31, 2016 · N990DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016111608865Intercostal · corrodedCORROSION ON INTERCOSTAL UPPER SURFACE BELOW OF LT TIE DOWN TRACK STA Y= 1307 TO Y= 1322. INTERCOSTAL WAS REPLACED.Jan 30, 2016 · N990DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016013100772Cusp Web · corrodedCORROSION ON RT CUSP WEB UPPER AND LOWER SURFACE BETWEEN X=-54 TO X=-60 FROM BS 636 TO 639 AND 682 TO 684. CUSP WEB IN STA 636 TO 639 WAS REPAIRED IAW SRM 53-05, FIG 131A-1. CUSP WEB IN STA 682 TU 684 WAS REPAIRED IAW SRM 53-05, FIG 131A-21.Jan 30, 2016 · N990DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016013100771Fairing · crackedCRACK ON SETTLEMENT AREA OF ANTI-FLOAT FAIRING. RT ELEVATOR. REPAIR WAS ACCOMPLISHED IAW ET 88-16-030, REV 2 AND ER/A 541630-14, REV ORIGINAL.Jan 30, 2016 · N990DL · Doug MD88 · Elevator StructureSDR DALA2016013100768Access Panel · corrodedCORROSION ON COUNTERSKIN AND SEATING AREA OF FUEL ACCESS PLATE NR 1311C. FUEL ACCESS WAS REPLACED IAW SRM 51-22-2A.Jan 30, 2016 · N990DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016013100766Former · crackedCRACKED FORMERS ON BS ZFS=23 LT SIDE AND BS ZFS=23 AND 36 AT VERTICAL STABILIZER L/E INTERNAL STRUCTURE. CRACKED FORMERS WERE REPAIRED IAW SRM 55-02D, FIG 27.Jan 30, 2016 · N990DL · Doug MD88 · Vertical StabilizerSDR DALA2016013100765Cusp Web · corrodedCORROSION ON CUSP WEB BS 503 TO BS 598 BETWEEN X=-54TO X= -60 AT CABIN PASSENGER. CUSP WEB WAS REPLACED DUE TO EXCESIVE DAMAGE IAW SRM 53-05, FIG 131A, 24.Jan 30, 2016 · N990DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016013100764Pan · crackedCRACK PAN ON AFT EDGE BELOW STOP 5 AT MID CARGO DOOR. CRACKS WERE REWORKED IAW SRM 52-03D, FIG 10.Jan 30, 2016 · N990DL · Doug MD88 · Cargo/Baggage DoorsSDR DALA2016013100763Stiffener · crackedCRACK STIFFENER AT FRAME BS 1463 CANT BETWEEN PROTECTION LONG 7L TO 8L. STIFFENER WAS REPLACED IAW SRM 51-30-5, 51-10-3 PARA 14 AND 21, 51-30-3 AND DWG 9911839-29.Jan 30, 2016 · N990DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016013100759Floor Panel · damagedDAMAGE FERRULES ON FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.Jan 29, 2016 · N990DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016013100758Floor Panel · damagedDAMAGE FERRULES ON FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.Jan 29, 2016 · N990DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016013000756Skin · damagedDAMAGE METALLIZED ON RUDDER TAB, CARD 162, ZONE 100. DAMAGE METALLIZED WAS REPAIRED IAW SRM 51-70-1AD.Jan 29, 2016 · N990DL · Doug MD88 · Rudder, Plate/SkinSDR DALA2016013000755Pan · crackedCRACK AFT EDGE PAN WITH BEAM 5 OF MID CARGO DOOR. AFT EDGE PAN WITH BEAM 5 OF MID CARGO DOOR WAS REPAIRED IAW SRM 52-03D, FIG 8.Jan 29, 2016 · N990DL · Doug MD88 · Cargo/Baggage DoorsSDR DALA2016013000753Skin · corrodedCORROSION ON LT WING OTBD FLAP OTBD VANE LOWER SKIN AT BS XV2: 246 APPROXIMATELY CARD 122, ZONE 10. LT OTBD FLAP OTBD VANE WAS REPLACED IAW SRM 57-50-14, FIG 2A.Jan 29, 2016 · N990DL · Doug MD88 · Trailing Edge FlapsSDR DALA2016013000751Doubler · wornWEAR ON DOUBLER AT CUTOUT ELEVATOR ACCESS. DOUBLER WAS R & R IAW SRM 53-34-0, 51-30-2 AND 51-10-3 PAR 21, 14.Jan 29, 2016 · N990DL · Doug MD88 · Elevator, Plate/SkinSDR DALA2016012900719Finger Doubler · corrodedCORROSION ON INTERNAL FINGER DOUBLER BETWEEN BS 1174-1193 BELOW LONGERON 26L AT AFT CARGO COMPARTMENT C3. FINGER DOUBLER WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR 14, 21 AND 38, AND 53-04-5, FIG 7.Jan 28, 2016 · N990DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2016012900717Longeron · crackedCRACKED LONGERON 8L AT BS 1309 AT FUSELAGE CABIN STRUCTURE. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, 51-30-2, 51-30-5 AND 51-10-3, PARR 14, 21.Jan 28, 2016 · N990DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016012900713Skin · dentedDENTS ON OTBD SKIN BETWEEN BEAM 3 TO 4, 6 DENTS AND BEAM 4 TO 5, 5 DENTS AT MID CARGO DOOR. NEW SKIN WAS REPLACED IAW SRM 51-30-2 AND DWG 5910141, REV FE.Jan 28, 2016 · N990DL · Doug MD88 · Cargo/Baggage DoorsSDR DALA2016012900712Skin · dentedDENTS ON OTBD SKIN BETWEEN BEAM 1 AND 2, 1 DENTS BEAM 2 AND 3, 1 DENT BEAM 4 AND 5, 8 DENTS AND BEAM UPPER EDGE, 1 DENT AT AFT CARGO DOOR. SKIN WAS REPLACE IAW SRM 51-30-2, 51-30-5, DWG 5910141, REV. FE.Jan 28, 2016 · N990DL · Doug MD88 · Cargo/Baggage DoorsSDR DALA2016012900709Longeron · crackedCRACK LONGERON 13R WITH FRAME BS 1380. LONGERON WAS REMOVED AND NEW SECTION LONGERON WAS DRILLED AND ADJUSTED TREATED AND PAINTED INSTALLED AND EXHAUST WAS INSTALLED IAW SRM 51-30-5, 51-30-2, 51-10-4, 51-10-3, PAR 21, 14.Jan 28, 2016 · N990DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016012800691Floor Panel · delaminatedDELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.Jan 27, 2016 · N990DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016012800685Floorbeam · damagedCORROSION ON REPAIR DOUBLER OF FLOORBEAM BETWEEN X=18 TO X=24, BS 1309 AT FLOOR STRUCTURE CAB. DOUBLER WAS REPLACED IAW SRM 51-10-3, PAR 14, 21 AND 38, 51-30-5 AND 53-05 FIG 20A.Jan 27, 2016 · N990DL · Doug MD88 · Fuselage Main, Floor BeamSDR DALA2016012700664Pan · crackedCRACK ON PAN FWD EDGE BEAM NR 4 AT R1 DOOR. PAN WAS REPAIRED IAW SRM 52-03D, FIG 3, 51-01 PAR 21, 51-30-1, 51-30-4.Jan 26, 2016 · N990DL · Doug MD88 · Service DoorsSDR DALA2016012700662Isolator · corrodedCORROSION ON INNER SURFACE OF HOUSING BOLTS ON RT ENGINE AFT VIBRATION ISOLATOR. ON RT ENGINE AFT VIBRATION ISOLATOR WAS CLEANED AND CORROSION WAS FOUND. DUE TO CORROSION REPLACED AND INSTALLED IAW AMM 71-20-02-201 AND PS 900-1-2-1, NR 01.Jan 26, 2016 · N990DL · Doug MD88 · Engine Mount SectionSDR DALA2016012700660Floor Panel · delaminatedDELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.Jan 26, 2016 · N990DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016012700658Beam · crackedCRACKED BEAM NR 4 FWD EDGE AT FWD SERVICE DOOR. NEW BEAM WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-10-4, 51-10-3 PAR 14/21 AND 51-30-2 AND 51-30-5.Jan 26, 2016 · N990DL · Doug MD88 · Service DoorsSDR DALA2016012700656Fitting · corrodedCORROSION ON FRAME FITTING BS 522. FITTING WAS REPLACED IAW SRM 51-10-8, 51-10-3 PAR 14, 21.Jan 26, 2016 · N990DL · Doug MD88 · Fuselage Main, Attach FittingsSDR DALA2016012700654Angle · crackedCRACK FRAME CLIP ON BS 1437 BETWEEN LONGERON 16 - 17R. CLIP WAS REMOVED AND WAS FABRICATED IAW SRM 51-30-5 AND IAW DWG 9911840-75, REV DC AND NEW CLIP WAS INSTALLED IAW SRM 51-30-5.Jan 26, 2016 · N990DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016012700653Pan · crackedCRACK FWD EDGE PAN WITH BEAM NR 5 OF FWD CARGO DOOR. CRACK ON FWD EDGE PAN WITH BEAM NR 5 WAS REPAIRED IAW SRM 52-03D, FIG 8.Jan 26, 2016 · N990DL · Doug MD88 · Cargo/Baggage DoorsSDR DALA2016012700652Floor Panel · corrodedCORROSION ON FLOOR PANEL 160G IN PAX CABIN. THE FLOOR PANEL WAS REPLACED IAW SRM 51-30-2 AND DWG 9957828, REV AB.Jan 26, 2016 · N990DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016012700651Longeron · corrodedCORROSION ON LONGERON 23L, BETWEEN BS 1287 - 1307. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 19, 51-30-2, 51-30-5, AND 51-10-3, PAR 26-21, 14.Jan 26, 2016 · N990DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016020300822Retainer · crackedCRACK AND WEAR RETAINER SEAL AT FWD CARGO DOOR. RETAINERS WERE FABRICATED IAW SRM 52-33-0, FIG 1.Jan 25, 2016 · N990DL · Doug MD88 · Cargo/Baggage DoorsSDR DALA2016012600635Angle · crackedCRACKED FWD CLIP ON BEAM NR 1 AT FWD PASSENGER ENTRANCE DOOR L1. CLIP ON BEAM NR 1 AT FWD WAS REPLACE IAW DWG 9955752, REV K, 51-10-2 51-10-3 PARA 14 AND 21, 51-30-2.Jan 25, 2016 · N990DL · Doug MD88 · Passenger/Crew DoorsSDR DALA2016012600634Structure · damagedWEAR AND BEND FWD AND AFT LOWER EXTERNAL DOUBLERS AT FWD CARGO DOOR. DOUBLERS FWD AND AFT LOWER WERE REPLACED IAW ERA: 486624-14MA, REV ORIGINAL.Jan 25, 2016 · N990DL · Doug MD88 · Cargo/Baggage DoorsSDR DALA2016012600633Pan · crackedCRACK FWD EDGE PAN WITH BEAM NR 1 OF FWD CARGO DOOR. CRACK ON FWD EDGE PAN WITH BEAM NR 1 OF FWD CARGO DOOR. WAS REPAIRED IAW SRM 52-3D, FIG 8.Jan 25, 2016 · N990DL · Doug MD88 · Cargo/Baggage DoorsSDR DALA2016012600632Attach Angle · corrodedCORROSION ON ANGLE ATTACH LOWER DOOR JAMB OF VENTRAL STAIRWAY BETWEEN 18 TO 18, BS 1350. AREA WAS REPAIRED IAW SRM 53-05, FIG 34 AND 51-10-3 PAR 21 AND 14.Jan 25, 2016 · N990DL · Doug MD88 · Fuselage Main, Attach FittingsSDR DALA2016012600631Floor Support · crackedCRACKED FLOOR SUPPORT JUST NEXT TO 6 PULLEY BRACKET, 18 BS 1348. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 51-10-3, PAR 14 AND 21, 51-30-1, 51-30-2, 51-30-05A AND 53-01, FIG 2.Jan 25, 2016 · N990DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016012600630Door Frame · wornWEAR ON FWD ACCESSORY COMPARMENT DOOR JAMB. WEAR WAS ATTENDED IAW SRM 51-10-3, 53-01, ER/A 527558-14, REV ORIG.Jan 25, 2016 · N990DL · Doug MD88 · Fuselage Main, StructureSDR DALA2016012600629Floor Panel · crackedCRACK ON FLOOR PANEL. FLOOR PANEL REPAIRED IAW SRM 53-05, FIG 131B, 51-10-3, PAR 14 AND 21, 21-30-2.Jan 25, 2016 · N990DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016012600626Beam · crackedCRACKED BEAM NR 1 AFT EDGE AT FWD PASSENGER ENTRANCE DOOR L1. BEAM NR 1 AFT EDGE WAS REPAIR IAW SRM 52-05D, FIG 81, SHEET 3, 51-30-1, 51-10-3 PAR. 14 AND 21.Jan 25, 2016 · N990DL · Doug MD88 · Passenger/Crew DoorsSDR DALA2016012600623Pan · crackedCRACK AFT EDGE PAN WITH BEAM NR 1 OF FWD CARGO DOOR. CRACK ON AFT EDGE PAN WITH BEAM NR 1 OF FWD CARGO DOOR WAS REPAIRED IAW SRM 52-03D, FIG. 8.Jan 25, 2016 · N990DL · Doug MD88 · Cargo/Baggage DoorsSDR DALA2016012600621Frame · corrodedCORROSION ON FRAME, BS 1380 BETWEEN LONGERON 24L TO 24R. FRAME BS 1380 WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR 14 AND 21 AND DWG 9912246-115.Jan 25, 2016 · N990DL · Doug MD88 · Fuselage Main, FrameSDR DALA2016020300823Intercostal · crackedCRACKED INTERCOSTAL FROM BS 1287 TO BS 1307 X=0 AND 1271 TO 1287 X=5 AT PAX CABIN. INTERCOSTAL WAS REPAIRED IAW SRM 53-01, FIG 2 AND 51-10-3, PAR 21 AND 14 OTHER INTERCOSTAL WAS REPLACE ON BS 1287 TO 1307 X=0 WAS REPLACED IAW SRM 51-30-5 AND 51-30-2.Jan 24, 2016 · N990DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016012500558Skin · wornWORN PREVIOUS REPAIR DOUBLER ON HOLD OPEN HOOK AREA AT PASSENGER ENTRANCE DOOR L1. REPAIR DOUBLER WAS REPLACED IAW ERA 486216-14 MA, REV A.Jan 24, 2016 · N990DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2016012500557Beam · crackedCRACKED BEAM NR 8 AFT EDGE AT PASSENGER ENTRANCE DOOR L1. BEAM NR 8 AFT WAS REPAIR IAW SRM 52-05, D FIG 111, SHEET 3, 51-30-1, 51-30-2, AND 51-30-5.Jan 24, 2016 · N990DL · Doug MD88 · Passenger/Crew DoorsSDR DALA2016012500553Intercostal · corrodedCORROSION ON INTERCOSTAL BETWEEN LOWER EDGE AND BEAM NR 1 BS 655 OF MID CARGO DOOR. DAMAGE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.Jan 23, 2016 · N990DL · Doug MD88 · Cargo/Baggage Doors
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