N920DE, cancelled Nov 29, 2022

Service difficulty reports · 178

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 = 'N920DE' AND deregistration_id = 'N920DE-2022-11-29'
  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 DALA2020012500595Line · leakingAFTER LANDING & STARTING THE APU & SHUTTING DOWN RIGHT ENGINE WE SMELLED A DIRTY SOCK SMELL WITH SOULE HAZE IN CABIN SHUT DOWN RIGHT PACK & IT DIDN'T GET WORSE BUT DIDN'T GO AWAY. FOUND LEAK COMING FROM RT RUDDER CONTROL PRESSURE LINE . REPLACED LINE C/W NO GOJan 24, 2020 · N920DE · Doug MD88 · Hydraulic System, MainSDR DALA2020011300211Unknown · odorAT TAKEOFF A STRONG RUBBER TIRE SMELL FILLED THE CABIN NOI VIBRATION OR ANY OTHER INDICATION OF A PROBLEM SMELL WAS STRONG BUT DISSIPATED IN APPX 2 MIN.C/W AMDS CARD 2120-2367 PNEUMATIC DISTRIBUTION T/S. ALO AMDS CARD 7100-2619 PNEUMATIC SYSTEM DUCT BURN APU WJan 12, 2020 · N920DE · Doug MD88 · Air Distribution SystemSDR DALA2019101215864Battery · missingLAVATORY SMOKE DETECTOR BATTERY MISSING. REPLACED THE BATTERY, OP CKS NML.Oct 10, 2019 · N920DE · Doug MD88 · Smoke DetectionSDR DALA2019051403011Light · inoperativeEMERGENCY LIGHT OVER DOOR AT 24A INOP. RELAMPED SAME OPS NML REF AMM 33-52. (LP4751576)May 14, 2019 · N920DE · Doug MD88 · Emergency LightingSDR DALA2019030801553Relay · defectiveAFTER TAKE OFF SMELL OF BURNT RUBBER IN COCKPIT AND CABIN. DISSIPATED QUICKLY. GONE BY APPROXIMATELY 10,000 FEET. R/R RECIRC FAN. NO HELP. REPLACED RELAY R2-278. (LP5733780)Mar 7, 2019 · N920DE · Doug MD88 · Air Distribution SystemSDR DALA2019021100875Wire Harness · damagedEMERGENCY PATH LIGHT INOP @ PX 19&22. R/R SEAT WIRING HARNESS AT PAX 19&22 CKS GOOD PER AMM MD88 33-53. (LP5277974)Feb 11, 2019 · N920DE · Doug MD88 · Light System WiringSDR DALA2018100405888Nose Cowl · dentedDURING INSP. FOUND DENT ON NR 1 ENG INLET NOSE COWL AT 10 O'CLOCK POSITION. DENT MEASURES 2.25" X 1.25" & 0.344 DEEP & APPROX 10 O'CLOCK POSITION. PEFORMED TIME LIMITED REPAIR PER ERA 572070-14 SECTION I. NO CRACKS NOTED. REPLACED NR 1 ENGINE NOSE COWL PER RI Oct 3, 2018 · N920DE · Doug MD88 · Engine Cowling SystemSDR DALA2018050803134Battery Pack · dischargedDURING EMERGENCY LIGHT TEST DO NOT TURN ON, EXTERNAL LIGHTS ON FUSELAGE. REPLACED BATTERY PACK P/N60-1177-9IN AFT CARGO. OPS CHECKS OK.May 4, 2018 · N920DE · Doug MD88 · Emergency LightingSDR DALA201805173006Slide · malfunctionedDURING INITIAL INSPECTION, FOUND THAT THE FIRING LANYARD TO CONNECT MANUAL INFLATION HANDLE WAS MISSING ON THE L2 DOOR SLIDE, THE SAME SLIDE WAS FOUND WRAPPED AROUND WITH A NYLON CORD. L2 DOOR SLIDE WAS REMOVED AND REPLACED IAW AMM 25-62-00.May 2, 2018 · N920DE · Doug MD88 · Escape SlideSDR DALA2018050202977Frame · wornWORN FRAME ON STA Y=1510 CANT BTW 4-8 HRS POSITION AT AFT ACCESSORIES COMPARTMENT. FRAME WAS BLENDED OUT PER SRM 53-01 FIG. 1, FRAME BTW 6 AND 8 POSITION FOUND WITHIN LIMITS. FRAME AT 4 HRS POSITION MINIMUM REMAINING THICKNESS IS 0.027" THEREFORE IT IS OUT OFMay 1, 2018 · N920DE · Doug MD88 · Fuselage Main, FrameSDR DALA2018050102952Spar Cap · crackedDUE A CRACK ON RT HORIZONTAL STABILIZER REAR SPAR CAP, REMOVE AND INSTALL RUDDER. RUDDER WAS REMOVED AND INSTALLED UNDER AMDS 2720-4421 JOB 000-0030.Apr 30, 2018 · N920DE · Doug MD88 · Horizontal Stabilizer, Spar/RibSDR DALA2018043002894Rib · crackedCRACKED RIB, XRS 214, RT WING LEADING EDGE INNER STRUCTURE. THE RIB WAS REPLACED IAW SRM 51-30-2.Apr 29, 2018 · N920DE · Doug MD88 · Wing, Rib/BulkheadSDR DALA2018043002893Cusp Web · corrodedCORROSION FOUND ON THE RT CUSP WEB, UPPER & LOWER SURFACES, RBL 54 TO 60 BETWEEN BS 484 TO 503. THE CUSP WEB WAS REPLACED IAW SRM 5130-2, 51-30-1, AND 51-30-5.Apr 29, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2018043002892Spar Cap · crackedCRACK FOUND ON THE RT HORIZONTAL STABILIZER REAR SPAR CAP. THE SPAR CAP WAS REPLACED IAW 5510-4135.Apr 29, 2018 · N920DE · Doug MD88 · Horizontal Stabilizer, Spar/RibSDR DALA2018042902889Frame · crackedCRACK FOUND ON THE FRAME AT BS 1474, AT THE 8 HRS POSITION IN THE AFT ACCESORY BAY. THE FRAME WAS REPAIRED IAW ER/A 567630-14, REV ORIGINAL, & ETI-88-18-033, REV ORIGINAL.Apr 28, 2018 · N920DE · Doug MD88 · Fuselage Main, FrameSDR DALA2018042802885Frame · wornFRAME FOUND WORN OUT OF LIMITS, BS 1485, BETWEEN THE 9 AND 10 HRS POSITION. THE FRAME WAS REPAIRED IAW ER/A 567923-14, REV ORIGINAL, AND ETI-88-18-039, REV 2.Apr 28, 2018 · N920DE · Doug MD88 · Fuselage Main, FrameSDR DALA2018042802882Frame · crackedA CRACK WAS FOUND ON THE FRAME WEB BS 1437, LONGERON 8L. REPAIRED IAW ERA 567707-14, REV ORIGINAL, AND ETI-88-18-021, R3.Apr 27, 2018 · N920DE · Doug MD88 · Fuselage Main, FrameSDR DALA2018042702844Pan · corrodedCORROSION FOUND ON THE LOWER PAN, BS 370 TO 427, LONGERONS 23R TO 28R AT THE CARGO DOOR FRAME. THE PAN WAS REPAIRED IAW ETI-88-18-025, REV 1, AND ER/A 567912-14, REV ORIGINAL.Apr 27, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2018042702845Skin · damagedFOUND DAMAGED ALUMINUM FLAME SPRAY, LT & RT SIDES, SEVERAL AREAS. ON THE RUDDER. THE FRAME SPRAY WAS REPARIED IAW ERA.092613-14MA, REV C.Apr 26, 2018 · N920DE · Doug MD88 · Rudder, Plate/SkinSDR DALA2018042602825Finger Doubler · corrodedCORROSION ON THE FINGER DOUBLER BETWEEN BS 1210 AND 1215, LONGERON 26L. FOUND TO BE OUT OF LIMITS. THE FINGER DOUBLER WAS REPLACED IAW SRM 53-04, FIG 12E, & SRM 51-30-2.Apr 25, 2018 · N920DE · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2018042502804Skin · damagedCRACKS, PUNCTURES AND WEAR FOUND ON THE FIXED LEADING EDGE SKIN BETWEEN XFS 60 - 70, RT WING. REPAIRED IAW ERA 567673-14, REV B, AND ETI -88-18-031, REV 6.Apr 23, 2018 · N920DE · Doug MD88 · Wing SparSDR DALA2018042302706Floor Panel · corrodedCORRODED FLOOR PANEL. THE FLOOR PANEL WAS REPLACED IAW AMM 53-20-01.Apr 22, 2018 · N920DE · Doug MD88 · Fuselage Floor PanelSDR DALA2018042202697Floor Panel · damagedDELAMINATED COMPOSITE MATERIAL, PUNCTURES ON CHANNELS AND CORROSION ON STRAP AT FLOOR PANEL 200A. THE FLOOR PANEL AND CHANNELS WERE REPAIRED IAW SRM 51-70-1D, PAR. 10. AND DWG 9952523, REV Y.Apr 21, 2018 · N920DE · Doug MD88 · Fuselage Floor PanelSDR DALA2018042202695Frame · crackedCRACKED FRAME BS 1474, LONGERON 18R IN THE AFT ACCESORIES BAY. THE FRAME WAS REPAIRED IAW ER/A 567556-14, REV ORIGINAL, & ETI-88-18-023 R1.Apr 21, 2018 · N920DE · Doug MD88 · Fuselage Main, FrameSDR DALA2018042202694Cusp Web · corrodedCORROSION ON CUSP WEB LOWER SURFACE BS 1155 TO 1212, RBL 54 TO 60 IN THE AFT CARGO BAY. REPLACED IAW SRM 53-05, FIG 131A-24, SRM 51-30-2, & 51-30-5.Apr 21, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2018042102685Shear Tie · crackedCRACK ON THE SHEAR TIE BS 1380, LONGERON 15R IN THE AFT ACCESORIES COMPARTMENT. THE SHEAR TIE WAS REPLACED IAW SRM 51-30-5, & DWG 9912246, REV CY.Apr 20, 2018 · N920DE · Doug MD88 · Fuselage Internal Mounting StructureSDR DALA2018042002660Frame Angle · crackedAFTER REMOVING CORROSION, A CRACK WAS FOUND ON THE CAP ANGLE ATTACHED TO STAIRWAY FRAME, BETWEEN BS 1401 - 1405, LT SIDE. THE CAP ANGLE WAS REPLACED IAW SRM 51-30-2.Apr 19, 2018 · N920DE · Doug MD88 · Fuselage Main, FrameSDR DALA2018042002657Skin · corrodedCORROSION FOUND ON THE FUSELAGE SKIN BETWEEN BS 769 - 776, LONGERONS 27R - 28R. THE SKIN WAS REPAIRED IAW SRM 53-04, FIG 57.Apr 19, 2018 · N920DE · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2018041802587Tee Fitting · corrodedCORROSION ON THE TEE FITTING, BS 1380 BETWEEN LONGERONS 25L & 25R. THE TEE FITTING WAS REPLACED IAW SRM 51-30-2, AND 51-30-5.Apr 17, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2018041802586Floor Support · damagedELONGATED HOLE ON THE FLOOR SUPPORT BS 826, RBL 22. REPAIRED IAW ERA 567554-14, REV ORIG, AND ETI-88-18-022, REV ORIG.Apr 17, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2018041702528Frame · crackedA CRACK WAS FOUND ON THE FRAME, BS 1510. THE FRAME WAS REPLACED IAW SRM 51-30-1, 51-30-2, AND 51-30-5.Apr 17, 2018 · N920DE · Doug MD88 · Fuselage Main, FrameSDR DALA2018041702533Vane · delaminatedDURING INSPECTION, DELAMINATED WAS FOUND ON THE PREVIOUS DOUBLER REPAIR ON OTBD FLAP VANE OF OTBD FLAP, LT WING. THE FLAP VANE WAS REPLACED IAW SRM 57-04, PAR. 5Apr 16, 2018 · N920DE · Doug MD88 · Trailing Edge FlapsSDR DALA2018041702530Tab · dentedDURING INSPECTION, FOUND SEVERAL DENTS ON UPPER SKIN AT THE RT CONTROL TAB. THE RT CONTROL TAB WAS REPLACED IAW 55-04 PAR 2.Apr 16, 2018 · N920DE · Doug MD88 · Elevator, Tab StructureSDR DALA2018041702521Fitting · crackedCRACKED FITTINGS AT THE RT AND LT SIDES AT AFT CABIN BULKHEAD DOOR FRAME. FITTINGS REPLACED IAW SRM 51-30-2, 51-30-5, AND 51-30-1.Apr 16, 2018 · N920DE · Doug MD88 · Fuselage Main, Attach FittingsSDR DALA2018041602514Tab · dentedSEVERAL DENTS ON UPPER SKIN AT THE LT GEARED TAB. THE TAB WAS REPLACED IAW 55-04, PAR 2.Apr 15, 2018 · N920DE · Doug MD88 · Elevator, Tab StructureSDR DALA2018041602513Tab · debondedDISBONDED UPPER AND LOWER SKIN AT LT ANTI FLOAT TAB, XEFT 160. THE LT ANTI-FLOAT TAB WAS REPLACED IAW 55-04, PAR 2.Apr 15, 2018 · N920DE · Doug MD88 · Elevator, Tab StructureSDR DALA2018041502435Channel · crackedCRACK CHANNEL ON GENERATION FLOOR NBR 313A, 313E, 389G, 541F, 617G, 927A AND 927E. CHANNEL ON GENERATION FLOOR NBR 313A, 313E, 389G, 541F, 617G AND 927E WERE REPAIR PER DC-9/MD-80 SRM 53-05 FIG.131B AND 131C (SHEET 1 ), AND FLOOR PANEL NBR. 927A WAS REPLACED PApr 14, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2018041402429Access Panel · corrodedCORROSION ON RH FUEL ACCESS PLATES NBR 1436C, 1454C, 1414C, 1478C AND 1470C. FUEL ACCES PLATE 1454C, 1436C, 1414C, 1478C AND 1470C WERE REPLACED PER DC9/MD-80 SRM 51-22-2A. (LP0507595)Apr 13, 2018 · N920DE · Doug MD88 · Wing, Plate/SkinSDR DALA2018041402427Access Panel · corrodedCORROSION ON LH FUEL ACCESS PLATES NBR 1311C, 1335C AND 1363C. ACCESS PLATE NBR 1311C, 1335C AND 1363C WERE REPLACED PER DC-9/MD-80 SRM 51-22-2A PAR 6 (LP0507458)Apr 13, 2018 · N920DE · Doug MD88 · Wing, Plate/SkinSDR DALA2018041402432Fitting · crackedCRACK ON SHEAR CLIP STA Y= 1380 LONG 15L AT AFT ACCESSORIES COMPARTMENT. FRAME CLIP WAS REPLACED PER SRM 53-14-4 & DWG 9912246 REV CY.Apr 13, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2018041402431Floor Panel · damagedELONGATED HOLES ON COCKPIT FLOOR PANEL NR 120B LT SIDE. FLOOR WAS REPAIRED (PERMANENT REPAIR) PER DC-9/MD-80 SRM 53-01 FIG 4 (SHEET4).Apr 13, 2018 · N920DE · Doug MD88 · Fuselage Floor PanelSDR DALA2018041402430Floor Panel · crackedCRACK COCKPIT RT FLOOR PANEL NR 120D. FLOOR PANEL WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-01 FIG 2 (SHEET3).Apr 13, 2018 · N920DE · Doug MD88 · Fuselage Floor PanelSDR DALA2018041402428Floor Panel · crackedCRACK UPPER SKIN ON GENERATION FLOOR NR 465E AND 826G. FLOOR NR 465E AND 826G WERE REPAIRED (AS A PERMANENT REPAIR) PER SRM 53-01 FIG.2 (SHEET3) AND FIG 4 (SHEET4).Apr 13, 2018 · N920DE · Doug MD88 · Fuselage Floor PanelSDR DALA2018041302407Access Panel · corrodedCORROSION ON LH/RH FUEL ACCESS PLATES NBR 1303C AND 1409C IN REF AMDS 2000-2636. DUE TO BLEND OUT REPAIR IS NOT PERMITTED ON THE UPPER WING ACCESS DOOR (P/N 3912757) DUE TO THE REDUCED AREA OF THE CONDUCTIVE INTERFACE. FUEL ACCESS DOOR 1409C AND 1303C WERE REPApr 12, 2018 · N920DE · Doug MD88 · Wing, Plate/SkinSDR DALA2018041302406Floor Support · crackedCRACKED FLOOR SUPPORT, BS 1271 TO 1287, LBL 2. REPAIRED IAW SRM 53-01, PAR. 4 FIG.2, SHEET 4.Apr 12, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2018041102337Floor Panel · crackedINITIAL INSPECTION CRACKS ON FLOOR PANELS NBRS 168B, 200C, 160A, 389F AND 1003B AT PAX CAB. FLOOR PANELS NBRS 168B, 200C, 160A ,389F AND 1003B WERE FABRICATED REPLACED AND IDENTIFIED PER MD88 A.M.M. 53-20-01-201 AND WERE INSTALLED PER ROUTINE TASK CARD 001-007Apr 11, 2018 · N920DE · Doug MD88 · Fuselage Floor PanelSDR DALA2018041102336Floor Panel · delaminatedINITIAL INSPECTION DELAMINATION ON FLOOR PANELS NBRS 160D, 120C, 160C, 160E, 200D, 200B, 1174E, 160F, 617D, 617E, 617F, 769E, 769F, AND 826E. FLOOR PANELS NBRS 160D, 120C, 160C, 160E, 200D, 200B, 1174E, 160F, 617D, 617E 617F, 769E, 769F, AND 826E WERE FABRICATApr 11, 2018 · N920DE · Doug MD88 · Fuselage Floor PanelSDR DALA2018041202380Cusp Web · corrodedCORROSION ON RT CUSP WEB STA Y =1072 AT CPAX. CORROSION 2: REPAIR WAS ACCOMPLISHED (PERMANENT REPAIR) PER SRM53-05 FIG 131-A-13.Apr 11, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2018041202378Longeron · crackedCRACK LONG 12L STA Y=1437 AT AFT ACCESSORIES COMPARTMENT. LONG 12L STA Y=1437 AT AFT ACCESSORIES WAS REPAIR ( AS A PERMANENT REPAIR )PER SRM 53-02-FIG.18, SRM 51-30-5 AND SRM 51-30-2.Apr 11, 2018 · N920DE · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2018041202374Cusp Web · corrodedCORROSION ON LT CUSP WEB STA X=54 TO X=60 BTW STA Y=674 AND Y=693. CORROSION 2; LT CUSP WEB STA X=54 TO X=60 BTW STA Y=674 AND Y=693 WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-05 FIG 131A-9.Apr 11, 2018 · N920DE · Doug MD88 · Fuselage Miscellaneous Structure
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