N997DL

Service difficulty reports · 244

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 = 'N997DL' 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 DALA2016043003496Tripler · crackedCRACKED PRODUCTION TRIPLER BS 1438 BETWEEN 1 TO 2 RT AT AFT ACCESSORY COMPARTMENT. PRODUCTION DOUBLER ABOVE REPORTED WAS REPLACED IAW DWG 5912141, REV BR AND SRM 51-30-2 /51-30-5/51-10-3.Apr 29, 2016 · N997DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2016043003495Skin · crackedCRACKED SKIN SPLICE BETWEEN 1418 AND 1437 BETWEEN LONGERON 2RT AND 3RT AT, AAC. REPAIR WAS ACCOMPLISHED IAW ETI 88-16-147 AND ERA 545100-14, REV ORIGINAL.Apr 29, 2016 · N997DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2016043003492Tee Fitting · scratchedSCRATCH ON 1338 TEE LOWER SECTION BETWEEN LONGER ON 29LT AND 30 AFT SURFACE AT AAC. TEE "CAP" BETWEEN LONGERON 23RT TO 23LT FROM BS 1338 WAS REPLACED IAW SRM 51-30-2 , 51-30-5 AND 53-03D PARA 32, FIG 37A.Apr 29, 2016 · N997DL · Doug MD88 · Fuselage Main, Attach FittingsSDR DALA2016043003491Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1460C. ACCESS PLATE NR 1460C WAS REPLACED IAW SRM 51-22-2A COND II.Apr 29, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016043003490Frame · crackedCRACKED FRAME FITTING BS 1437 BETWEEN LONG 1 AND 2R. FITTING WAS REPLACED IAW DWG 9953016, REV AT AND 51-30-5.Apr 29, 2016 · N997DL · Doug MD88 · Fuselage Main, FrameSDR DALA2016050203505Channel · crackedCRACKED W-CHANNEL ON FLOOR PANEL 886 C. NEW CHANNEL WAS INSTALLED ON THE RT SIDE OF THE FLOOR PANEL 886C IAW DWG 9936639, REV P DRILLED SRM 51-10-4, REMOVED SRM 51-30-1.Apr 28, 2016 · N997DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016050203504Channel · bentBENT W-CHANNEL ON FLOOR PANEL 826D. NEW CHANNEL WAS INSTALLED ON THE LEFT SIDE OF THE FLOOR PANEL NR 826D IAW DWG 9936639, REV P. DRILLED SRM 51-10-4, REMOVED SRM 51-30-1.Apr 28, 2016 · N997DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016042903425Skin · dentedSEVERAL DENTS ON UPPER LOWER SURFACE AT CONTROLTAB AT LT ELEVATOR. LT ELEVATOR CONTROL TAB WAS REPLACED AND INSTALLED IAW AMM 27-30-03-201.Apr 28, 2016 · N997DL · Doug MD88 · Elevator, Plate/SkinSDR DALA2016042903423Frame · corrodedCORROSION OUT OF LIMITS ON FRAME DOUBLERS BS 1309 BETWEEN LONGERON 29R AND 29L . REPAIR DOUBLERS WERE REPLACED IAW SRM 51-30-5, 53-03, FIG 2A.Apr 28, 2016 · N997DL · Doug MD88 · Fuselage Main, FrameSDR DALA2016042903420Skin · damagedDAMAGE ON EXTERNAL FUSELAGE SKIN BS 492 BETWEEN LONGERON 25 - 26R. FOUND WITHIN LIMITS IAW SRM 53-04-1, PAGE 7.D CONDITION 1A. HFEC INSPECTION WAS ACCOMPLISHED ON EXTERNAL FUSELAGE SKIN. NO CRACKS WERE FOUND IAW 53-04-01, PAR 7D, 1, B .Apr 28, 2016 · N997DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2016042803398Skin · delaminatedDELAMINATED SKIN BELOW PREVIOUS REPAIR. SKIN BELOW PREVIOUS REPAIR WAS REPAIRED IAW SRM 57-03D, PAR. 11.Apr 26, 2016 · N997DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2016042703354Door Frame · wornWEAR ON FWD APU DOOR JAMB BETWEEN X=0 AND X=14 AT ACC. ALL WEAR WAS WELDED, REPAIRED IAW ER/A 094719-14MA.Apr 26, 2016 · N997DL · Doug MD88 · Fuselage Main, StructureSDR DALA2016042703349Web · corrodedCORROSION ON RT, LT WEBS BS 1338. WEBS RT, LT WERE REMOVED, FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-30-5 AND 53-14-3, FIG 7.Apr 26, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016042703348Frame · corrodedCORROSION ON FRAME TEE BS 1380 BETWEEN LONGERON 25 LT AND 25 RT AT ACCESSORY FRAME TEE FROM BS 1380 BETWEEN LONGERON 25 LT AND 25 RT WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.Apr 26, 2016 · N997DL · Doug MD88 · Fuselage Main, FrameSDR DALA2016042703357Skin · dentedDENTS ON OUTER SKIN OF C3 CARGO COMPARTMENT DOOR BETWEEN BEAMS 5, 2, 3 AND 4. SKIN WAS REPLACED IAW SRM 51-30-2.Apr 25, 2016 · N997DL · Doug MD88 · Cargo/Baggage DoorsSDR DALA2016042703356Cargo Track · corrodedCORROSION ON TIE TRACK BETWEEN BS 1041 AND X=18 RT AT AFT CARGO COMPARTMENT. DUE TO EXCESSIVE DAMAGE, TIE TRACK WAS REPLACED IAW SRM 51-10-3, 14-21, 51-10-4, 51-30-2, 51-30-1, FROM BS 1007 TO 1155.Apr 25, 2016 · N997DL · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016042603305Ferrule · brokenBROKEN FERRULE ON FLOOR PANEL. REPLACED FERRULE IAW AMM 53-20-01-201.Apr 25, 2016 · N997DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016042603303Longeron · crackedCRACKED LONGERON 2 LT BS 1418. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, 51-10-3, PAR 14, 21 AND 51-30-5.Apr 25, 2016 · N997DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016042503293Longeron · crackedCRACKED LONGERON 16L, BS 1437 AT ACC. CRACKED LONGERON SECTION WAS REPLACED IAW DC-9/MD-80 SRM 53-14-4, FIG 2, 51-30-2, 51-30-5 PAR 8 AND 7.Apr 24, 2016 · N997DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016042503291Door Frame · corrodedCORROISON ON WEB OF DOOR FRAME BETWEEN BS 1148 - 1155 AND BETWEEN LONGERON 25 TO 26R AT AFT CARGO COMPARTMENT. THE WEB WAS REPAIRED IAW SRM 53-01, FIG 4 51-10-3 PAR, 14, 21, 38, AND 51-30-2.Apr 24, 2016 · N997DL · Doug MD88 · Fuselage Main, StructureSDR DALA2016042703355Skin · delaminatedDELAMINATED ON UPPER AND LOWER SKIN ON INBD VANE OTBD FLAP BETWEEN BS XV1=117 TO 121 AND BS XV1=124.5 APPROXIMATELY AT RT WING ING. UPPER AND LOWER SKIN ON INBD VANE OTBD FLAP BETWEEN BS=XV1=117 TO 121 AND BS -XV1=124.5 APPROXIMATELY AT RT WING REPAIRED IAW SApr 23, 2016 · N997DL · Doug MD88 · Trailing Edge FlapsSDR DALA2016042603300Frame · crackedCRACKED FRAME BS 1437 LONGERON 8 L. DAMAGE AREA WAS REPAIRED IAW SRM 51-70-4 AND DWG 9911840, REV DC.Apr 23, 2016 · N997DL · Doug MD88 · Fuselage Main, FrameSDR DALA2016042403240Cargo Track · corrodedCORROSION ON RT CARGO TRACK BETWEEN BS 1250 TO 1271 AT AFT CARGO COMPARTMENT. CARGO TRACK WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5, 51-10-4 AND 51-10-3 PAR 21 AND 14.Apr 23, 2016 · N997DL · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016042403239Longeron · crackedCRACK ON LONGERON 4 LT AND BS 1437 AT AFT ACCESORIES COMPARTMEMT. CRACK ON LONGERON 4LT WAS REPAIRED IAW SRM 53-02, FIG 18, 51-30-5, 51-10-3.Apr 22, 2016 · N997DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016042303235Ferrule · delaminatedDELAMINATED AND MISSING FERRULES ON FLOOR PANEL. DAMAGE FERRULE REPLACED IAW AMM 53-20-01-201.Apr 22, 2016 · N997DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016042503248Skin · corrodedCORROSION ON BARREL NUTS HORIZONTAL STABILIZER XH=7, NR 11, 12 AND 14. ALSO XH=-7, 10, 11 AND 13. REPAIR WAS PERFORMED IAW ER/A 545116-14 REV ORIGINAL.Apr 21, 2016 · N997DL · Doug MD88 · Horizontal Stabilizer, Plate/SkinSDR DALA2016042503247Skin · corrodedCORROSION ON HORIZONTAL STABILIZER RT BARREL NUT XH= -7 HOLE 14 . REPAIR WAS PERFORMED IAW ER/A 545116-14, REV ORIGINAL.Apr 21, 2016 · N997DL · Doug MD88 · Horizontal Stabilizer, Plate/SkinSDR DALA2016042303233Structure · crackedCRACKED CLIP ON BS 1309 AND LONG BETWEEN LONG 15 AND 16RT SUDE AT C PAX. CLIP WAS REPLACED IAW SRM 51-30-5 AND DWG 9912243.Apr 21, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016042303232Intercostal · crackedCRACKED INTERCOSTAL X= 10 AND X=-10 STA Y=39 AT WHEEL/WELL AREA OF NLG. INTERCOSTAL WAS REPAIRED IAW SRM 51-30-2, 53-01 FIG 2 AND DWG 9911500, REV DH.Apr 21, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016042203230Access Panel · corrodedCORROSION ON COUNTERSINK AREA OF FUEL ACCESS PLATE NR 1371C. FUEL ACCESS PLATE WAS REPLACED.Apr 21, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016042203227Access Panel · corrodedCORROSION ON COUNTERSINK OF FUEL ACCESS PLATE NR 1470C. FUEL ACCESS PLATE WAS REPLACED.Apr 21, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016042203226Floor Panel · delaminatedDELAMINATION ON FLOOR PANEL. FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201.Apr 21, 2016 · N997DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016042203222Structure · corrodedCORROSION ON HOLE OTBD LUG OF LEVER SUPPORT AT LT FLIGHT SPOILER. THIS REPAIR WAS PERFORMED IAW ER/A 545124-14, REV ORIGINAL.Apr 21, 2016 · N997DL · Doug MD88 · SpoilersSDR DALA2016042203221Structure · corrodedELONGATED HOLE INBD LUG OF LEVER SUPPORT AT LT INBD FLIGHT SPOILER. THIS REPAIR WAS PERFORMED IAW ER/A 545123-14, REV ORIGINAL.Apr 21, 2016 · N997DL · Doug MD88 · SpoilersSDR DALA2016042203220Structure · corrodedCORROSION ON HOLE INBD, OTBD LUG OF LEVER SUPPORT AT RT INBD FLIGHT SPOILER. THIS REPAIR WAS PERFORMED IAW ER/A 545123-14, REV ORIGINAL.Apr 21, 2016 · N997DL · Doug MD88 · SpoilersSDR DALA2016042203219Structure · corrodedCORROSION ON HOLE OTBD LUG OF LEVER SUPPORT AT RT OTBD FLIGHT SPOILER. REPAIR WAS PERFORMED IAW ER/A 545124-14, REV ORIGINAL.Apr 21, 2016 · N997DL · Doug MD88 · SpoilersSDR DALA2016042203229Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1462C. FUEL ACCESS PLATE WAS REPLACED.Apr 20, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016042203228Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1355C. FUEL ACCESS PLATE WAS REPLACED.Apr 20, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016042203209Frame · crackedCRACKED FRAME BS 1418 BETWEEN LONGERONS 3 LT AND 3 RT. STIFFENER WAS REPLACED IAW SRM 51-30-5, 51-10-3 PAR 21 AND 14 AND DWG 5913595, REV AP.Apr 20, 2016 · N997DL · Doug MD88 · Fuselage Main, FrameSDR DALA2016042103207Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1456C. FUEL ACCESS PLATE WAS REPLACED.Apr 20, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016042103206Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1414C. FUEL ACCESS PLATE WAS REPLACED.Apr 20, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016042103205Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1367C. FUEL ACCESS PLATE WAS REPLACED.Apr 20, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016042103204Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1454C. FUEL ACCESS PLATE WAS REPLACED.Apr 20, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016042103203Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1361C. FUEL ACCESS PLATE WAS REPLACED.Apr 20, 2016 · N997DL · Doug MD88 · Wing, Plate/SkinSDR DALA2016042103142Intercostal · crackedCRACKED INTERCOSTAL BETWEEN BS 1287 - 1309. INTERCOSTAL WAS REMOVED TO FACILITATE THE REPAIR AND POSTERIORILY REINSTALLED IAW SRM 51-30-2 AND 51-30-5. REPAIR ACCOMPLISHED IAW ER/A 380521-14MA, REV ORIGINAL.Apr 20, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016042003132Floor Panel · puncturedPUNCTURES ON FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20- 01-201.Apr 18, 2016 · N997DL · Doug MD88 · Fuselage Floor PanelSDR DALA2016041903028Cusp Web · corrodedCORROSION ON CUSP WEB UPPER AND LOWER SURFACE FROM 1041-1060 BETWEEN X=54 -X=60 LT SIDE. AREA WAS REPAIRED IAW SRM 53-05, FIG 131, A-6, 51-10-3 PAR 14, 21, 38 , 51-30-2, 51-30-5, 51-30-1.Apr 18, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016041802992Pan · crackedCRACK ON RING PAN STRUCTURE AT FWD LOWER CORNER AND AFT UPPER CORNER BETWEEN BS 1193-1212 RT SIDE. FASTENERS AND DAMAGE WERE REMOVED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122 AND ER/A 487747-14MA, REV ORIGINAL AND 4Apr 16, 2016 · N997DL · Doug MD88 · Fuselage Main, StructureSDR DALA2016041802986Channel · crackedCRACK ON CHANNEL AT FLOOR PANEL NR 693A. CRACK ON CHANNEL WAS ATTENDED IAW SRM 53-05 FIG 131B, SH 3, 51-10-3 PAR 14, 21 AND 38, 51-30-2.Apr 16, 2016 · N997DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016041802985Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1466C. FOUND NR 1 HOLE OUT OF LIMITS WITH .571" BUSHING WAS FABRICATED AND INSTALLED WITH OD .329" AND COUNTERSINK .508" IAW SRM 51-22-2A, PAR 6, COND II.Apr 16, 2016 · N997DL · Doug MD88 · Wing, Plate/Skin
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