N994DL

Service difficulty reports · 236

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 = 'N994DL' 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 DALA2016040502657Skin · damagedDELAMINATED OTBD FLAP MID VANE LOWER SURFACE BS XVZ=220 AT RT WING. DAMAGE TO THE INTERNAL STRUCTURE OF THE MID VANE OF THE RT WING FLAP ARE OUT OF LIMITS BY CORROSION FOR REPLACE AND REPAIR. OTBD FLAP MID VANE AT RT WING WAS REPLACED IAW SRM 57-50-14, FIG 2Mar 25, 2016 · N994DL · Doug MD88 · Trailing Edge FlapsSDR DALA2016032602312Vane · delaminatedDELAMINATED INBD FLAP OTBD VANE XOVIF=68 BELOW RUB STRIP, ON LT WING. VANE REPAIRED IAW SRM 57-03D, PAR II.Mar 25, 2016 · N994DL · Doug MD88 · Trailing Edge FlapsSDR DALA2016032802372Skin · dentedTWO DENTS ON PREVIOUS REPAIR DOUBLER OF LT WING SLAT PANEL NR 2. SLAT PANEL NR 2 OF LT WING WAS REPLACED AND WAS REMOVED, INSTALLED ON CARD NR 105, ZONE 10.Mar 24, 2016 · N994DL · Doug MD88 · Leading Edge DevicesSDR DALA2016032602313Longeron · crackedCRACK ON LONGERON 4R BS 1437. LONGERON REPAIRED IAW SRM 53-02, FIG 18, SRM 51-10-2A, 51-10-4, 51-10-3, PAR 14, 21, SRM 51-30-2, AND 51-30-5 A.Mar 24, 2016 · N994DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016032502307Support · crackedCRACKS ON ATTACH POINT SUPPORTS ON RAM AIR DUCT 3EA. CRACKS ON ATTACH POINT SUPPORTS ON RAM AIR DUCT WERE REPAIRED, WELDED IAW ER/A 494638-14MA REV B AND SOPM 20-10-19, PAR C4 AND TREATED AND PAINTED IAW SRM 51-10-3.Mar 24, 2016 · N994DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016032502302Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1303C AT LT WING. CORROSION WAS FOUND ON SETTLEMENT AREA AND FUEL ACCESS 1303C WAS REPLACED UNDER CONDITION III IAW SRM 51-22-2A.Mar 24, 2016 · N994DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016032502301Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1409C AT RT WING. CORROSION WAS FOUND ON SETTLEMENT AREA AND FUEL ACCESS 1409C WAS REPLACED UNDER CONDITION III IAW SRM 51-22-2A.Mar 24, 2016 · N994DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016032502300Cusp Web · corrodedCORROSION ON RT CUSP BETWEEN BS 1060-1079, & 1098-1117 BETWEEN RBL 54 TO 60. REPAIRED IAW SRM 53-05, FIG 131A-7 AND 51-10-3, PAR 21-14.Mar 24, 2016 · N994DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016032502298Floor Panel · crackedCRACK ON FLOOR PANEL AND DISBONDED CHANNEL NR 200A. FLOOR PANEL WAS REPAIRED IAW SRM 51-70-01D, PARA 10.Mar 24, 2016 · N994DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016032502297Door Frame · crackedCRACKED FITTING ON VENTRAL DOOR JAMB STRUCTURE BS 1358, X=11, Z15 AT AFT PRESSURE BULKHEAD. FITTING ON VENTRAL DOOR JAMB WAS REPLACED IAW SRM 51-30-2, 51-10-4, 51-10-3 PAR 21, 14 AND 51-3-5.Mar 24, 2016 · N994DL · Doug MD88 · Fuselage Main, StructureSDR DALA2016032502296Floorbeam · crackedCRACK ON FLOORBEAM BS 927 BELOW SEAT TRACK LBL 54. FLOORBEAM WAS REMOVED & REPLACED IAW SRM 51-30-2, 51-30-5 AND 51-30-1.Mar 24, 2016 · N994DL · Doug MD88 · Fuselage Main, Floor BeamSDR DALA2016032502295Support · crackedCRACK ON BEAM SUPPORT ON BS 927 BELOW SEAT TRACK LBL 4 -12. BEAM SUPPORT WAS REMOVED, NEW BEAM SUPPORT WAS REPLACED AND INSTALLED IAW SRM 51-30-5.Mar 24, 2016 · N994DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016032402276Access Panel · corrodedCORROSION ON RT WING FUEL ACCESS 1456C COUNTERSINK HOLES. FUEL ACCESS 1456C WAS REPAIRED BY CONDITION II IAW SRM 51-22-2A.Mar 23, 2016 · N994DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016032402275Access Panel · corrodedCORROSION ON LT WING FUEL ACCESS 1367C COUNTERSINK HOLES. REPAIRED IAW CONDITION II IAW SRM 51-22-2A.Mar 23, 2016 · N994DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016032602310Floor Panel · delaminatedDELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.Mar 22, 2016 · N994DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016032302243Cusp Web · corrodedCORROSION ON CUSP WEB RT X=-54 TO X=-60 BETWEEN BS 1174 AND BS 1193. DAMAGE WAS REMOVED, NEW ITEMS WERE FABRICATE IAW SRM 53-05, FIG 131A-1 53-05 PAR 166 ORIGINAL.Mar 22, 2016 · N994DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016032302242Floor Support · crackedCRACKED ON REPAIR DOUBLER AND CRACKED BEYOND STOP DRILL ON FLOOR SUPPORT X 00 BETWEEN BS 788 - 769. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-5 51-10-4 51-10-3 PAR 14, 21 AND DWG: 9936580, REV BW.Mar 22, 2016 · N994DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016032302239Longeron · crackedCRACKED LONGERON 4R AND BS 905. REPAIRED IAW SRM 53-02 FIG 18, 51-10-3 PARR 14, 21 AND 51-30-2.Mar 22, 2016 · N994DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016032302238Seat Track · corrodedCORROSION ON RT SEAT TRACK, BS 894 - 934 AND X -54 AT FLOOR STRUCTURE. SEAT TRACK REPAIRED IAW SRM 53-05 FIG 4A AND 51-10-3 PAR 14, 21.Mar 22, 2016 · N994DL · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016032302237Stop Fitting · crackedCRACKS ON DOOR STOP CLIPS NRS 1 AND 12 AT LT AFT OVERWING EMERGENCY EXIT. CLIPS WERE REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-2, 51-10-3 PAR 14/21 AND DWG 9957735, REV G.Mar 22, 2016 · N994DL · Doug MD88 · Fuselage Main, StructureSDR DALA2016032502299Cusp Web · corrodedCORROSION ON RT CUSP WEB BETWEEN BS 596-617 AND RBL 54 - 60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13, 51-10-3 PAR 14 AND 21, 51-30-2, 51-30-5.Mar 20, 2016 · N994DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016032102139Support · crackedCRACKED NUT ON HORIZONTAL STABILIZER LONGITUDINAL TRIM ACTUATING MECHANISM UPPER SUPPORT. NUT ON HORIZONTAL STABILIZER LONGITUDINAL TRIM ACTUATING MECHANISM UPPER SUPPORT WAS REPLACED IAW AMM 27-41-1.Mar 20, 2016 · N994DL · Doug MD88 · Horizontal Stabilizer StructureSDR DALA2016032102134Cusp Web · crackedCRACKED WEB, BS 232 X=34-60 RT AT W1. NEW CUSP WEB WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-10-4, 51-10-3, PAR 14/21, 51-30-1, 51-30-2, 51-30-5.Mar 20, 2016 · N994DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016032102128Ferrule · damagedDAMAGE FERRULES ON FLOOR PANEL. REPLACED FERRULE IAW AMM 53-20-01-201.Mar 20, 2016 · N994DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016032002146Skin · dentedSEVERAL DENTS OUTER SKIN BETWEEN BEAM 2 AND 5 AT AFT CARGO COMPARTMENT DOOR. DENTS WERE ATTENDED IAW ETI-88-16-115, ERA 543210-14, REV ORIGINAL. PERFORM A GVI OF THE DAMAGED AREAS WITHIN EVERY 3, 800 FLIGHT CYCLES. AFTER SECTION I ACCOMPLISHED OF ERA 543210-1Mar 19, 2016 · N994DL · Doug MD88 · Cargo/Baggage DoorsSDR DALA2016032102140Bracket · damagedDAMAGE ON LT OTBD BEARING BRACKET JUST IN BEARING AREA AT ELEVATOR MECHANISM. LT OTBD BEARING BRACKET WAS REPLACED IAW AIPC 27-30-00 AND WILL BE INSTALLED UNDER JIC A/C 0994, CARD 2730-4234.Mar 19, 2016 · N994DL · Doug MD88 · Elevator StructureSDR DALA2016032002121Floor Panel · corrodedCORROSION ON FLOOR PANEL 160G AT W1. FLOOR PANEL WAS REPLACED IAW SRM 51-30-2, 51-10-2 AND 51-10-3, PAR 14, 21, 38 AND DWG: 9957828. REV "Y".Mar 19, 2016 · N994DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016032002113Cusp Web · corrodedCORROSION ON RT CUSP WEB BS 1234 BETWEEN X=-54 TO X=-60 AT PAX CABIN. CUSP WEB WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 131A-7 AND 51-10-3, PAR 21 AND 14.Mar 19, 2016 · N994DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016032002110Cusp Web · corrodedCORROSION ON LT CUSP WEB ON BS 529 BETWEEN X=57 TO X=60 AT PAX CABIN. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-9.Mar 19, 2016 · N994DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016032002108Strap · crackedCRACKED STRAP ON BEAM NR 6 AT L1 DOOR. STRAP ON BEAM NR 6 AT WAS REPLACE IAW SRM 51-30-2, 51-10-3 PAR 14 AND 21, AND 51-10-4.Mar 19, 2016 · N994DL · Doug MD88 · Passenger/Crew DoorsSDR DALA2016032002107Intercostal · crackedCRACKED INTERCOSTAL BETWEEN BEAMS 4-5 AT L1 DOOR. INTERCOSTAL BETWEEN BEAM 4-5 L1 DOOR WAS REPLASE IAW SRM 51-30-2, 51-10-3 PAR. 14 AND 21, 51-10-4 AND DWG: 9955763, REV: M.Mar 19, 2016 · N994DL · Doug MD88 · Passenger/Crew DoorsSDR DALA2016032002106Structure · brokenBROKEN LOWER SECTION OF RUDDER L/E. LOWER SECTION OF RUDDER L/E WAS REPAIRED IAW SRM 51-70-01AD PAR 3.Mar 19, 2016 · N994DL · Doug MD88 · Rudder StructureSDR DALA2016032002105Skin · damagedEXPOSED METALLIZED AND DAMAGED PAINT ON RT AND LT SKINS OF RUDDER. METALLIZED AND DAMAGED PAINT ON RT AND LT SKIN OF RUDDER WAS REPAIRED IAW ER/A 092613-14MA, REV A.Mar 19, 2016 · N994DL · Doug MD88 · Rudder, Plate/SkinSDR DALA2016032002103Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1436C AT RT WING. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.Mar 19, 2016 · N994DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016032002102Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1355C AT LT WING. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.Mar 19, 2016 · N994DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016032002101Access Panel · corrodedCORROSION ON COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1307C AT LT WING. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.Mar 19, 2016 · N994DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016032002100Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1371C AT LT WING. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.Mar 19, 2016 · N994DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016032002099Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1373C AT LT WING. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.Mar 19, 2016 · N994DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016032002098Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1377C AT LT WING. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.Mar 19, 2016 · N994DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016032002097Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1466C AT RT WING. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.Mar 19, 2016 · N994DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016032002096Skin · dentedDENT FWD EDGE BETWEEN BEAM 1 AND 3 OUTER SKIN AT AFT CARGO COMPARTMENT DOOR. DENTS WERE ATTENDED IAW ETI-88-16-115, ERA 543210-14, REV ORIGINAL.Mar 19, 2016 · N994DL · Doug MD88 · Cargo/Baggage DoorsSDR DALA2016031802081Frame · crackedCRACKED FRAME BS 1322 AND LONGERON 17L. DAMAGED FRAME AREA WERE REMOVED, HFEC INSPECTION WAS PERFORMED ON FRAME, REPAIR PARTS AND REWORKED AREA WERE TREATED, PAINTED, INSTALLED IAW SRM 51-10-2, 51-10-2A, 51-10-3 PAR 14/21, 51-30-1, 51-30-2, 51-30-5, 51-30-3, Mar 17, 2016 · N994DL · Doug MD88 · Fuselage Main, FrameSDR DALA2016031802080Exhaust Duct · crackedCRACKED APU EXHAUST DUCT AT FUSELAGE SKIN. EXHAUST DUCT APU AT FUSELAGE SKIN WAS REPAIRED, REWELDED IAW ER/A 473221-14 MA, REV ORIGINAL.Mar 17, 2016 · N994DL · Doug MD88 · APU Exhaust SystemSDR DALA2016031802077Longeron · crackedCRACK ON LONGERON 16L AND BS 1437 AT AFT ACCESSORY COMPARMENT. SECTION OF LONGERON WAS REPLACED IAW SRM 53-14, 4, 51-30-2, 51-30-5, 51-10-4, 51-10-1, 51-10-3 PAR 14, 21.Mar 17, 2016 · N994DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016031802074Floor Panel · delaminatedDELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.Mar 17, 2016 · N994DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016031802072Cusp Web · corrodedCORROSION ON PREVIOUS CUSP WEB REPAIR DOUBLER BETWEEN BS 1155 AND 1174, RT X -44 TO X -60. CORROSION WAS ATTENDED IAW SRM 51-30-2, 51- 10-3, PARS 14 AND 21, 53-05, FIG 131A-5.Mar 17, 2016 · N994DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016031702047Door Frame · corrodedCORROSION ON WEB BETWEEN LONGERON 9 - 24R BS 629 - 700 MID CARGO BAY DOOR FRAME. CORROSION REMOVED IAW SRM 51-10-3, PAR 26, 14, 21 UT MD/DC NDT SPM 04-00-07, PAR 5, FIG 3.Mar 16, 2016 · N994DL · Doug MD88 · Fuselage Main, StructureSDR DALA2016031702046Cusp Web · crackedDUE TO EXCESSIVE CORROSION ON CRACKED CUSP WEB BETWEEN BS 826 AND 845, RBL 54 - 60. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-16, 51-10-3 PAR 14 AND 21, 51-30-2.Mar 16, 2016 · N994DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016031702045Channel · crackedCRACKS ON FLOOR CHANNEL. CHANNEL REPAIRED IAW 53-05, FIG 131B.Mar 16, 2016 · N994DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016031602023Pan · crackedDURING REMOVAL OF THE STOP WAS FOUND CRACK ON INNER PAN OF AFT CARGO DOOR. REPAIRED IAW SRM 52-03-D FIG 10. FOUND WITHIN LIMITS IAW SRM 52-03, FIG. 10.Mar 15, 2016 · N994DL · Doug MD88 · Cargo/Baggage Doors
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