N923DL, cancelled Apr 8, 2019

Service difficulty reports · 172

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 = 'N923DL' AND deregistration_id = 'N923DL-2019-04-08'
  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 DALA2017121808668Lamp · inoperativeBOTH FWD CABIN DOOR EMERGENCY LIGHTS OUT. RELAMPED BOTH FWD CABIN DOOR EMERGENCY LIGHT ASSYS PER MD88 AMM 33-53. OPS CHECKED GOOD. (LP3869586)Dec 17, 2017 · N923DL · Doug MD88 · Emergency LightingSDR DALA2017092507064Engine · failedAT APPROXIMATELY 85 KTS DUE TO HEARING A BANG & THE NR 2 ENGINE EGT AT 750 DEGREES. ABORTED TAKEOFF. STOPPED ON RUNWAY, FIRE DEPT SPRAYED THE NR 2 ENGINE AS PRECAUTION. FOUND METAL IN TAIL PIPE AND TURBINE DAMAGE. ENGINE CHANGE COMPLETED.Sep 25, 2017 · N923DL · Doug MD88 · Engine (Turbine/Turboprop)SDR DALA2017022501572Skin · corrodedBULGING FUSELAGE SKIN BS 680 - 700 BETWEEN LONGERONS 29L-29R. THE SKIN WAS REPAIRED IAW ETI-88-17-068 REV. 6, AND ER/A 554161-14 REV. ORIGINAL.Feb 24, 2017 · N923DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2017022501571Access Panel · corrodedCORROSION ON ACCESS PANEL ON RT WING. THE ACCESS PANEL WAS REPAIRED IAW SRM 51-22-2A, PAR 6, CONDITION II (C).Feb 24, 2017 · N923DL · Doug MD88 · Wing, Plate/SkinSDR DALA2017022401527Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PANEL. CORROSION MEASURED AND FOUND OUT OF LIMITS. REPLACED THE ACCESS PANEL IAW SRM 51-22-2A CONDITION II.Feb 23, 2017 · N923DL · Doug MD88 · Wing, Plate/SkinSDR DALA2017022401526Access Panel · corrodedCORROSION ON ACCESS PANEL. CORROSION MEASURED AND FOUND OUT OF LIMITS. REPLACED IAW SRM 51-22-2A CONDITION II.Feb 23, 2017 · N923DL · Doug MD88 · Wing, Plate/SkinSDR DALA2017022301493Support · crackedCRACKED CONNECTOR SUPPORT ON FIRE LOOP AT FLANGE "J" BTW 6 TO 7 HRS POSITION, RT NACELLE. FIRE DETECTOR LOOP SUPPORT ASSY WAS REMOVED IAW AMM 26-10-04 AND REPLACED IAW AMM 26-10-04. TESTED IAW AMM 26-00-00-201.Feb 22, 2017 · N923DL · Doug MD88 · Nacelle/Pylon Miscellaneous StructureSDR DALA2017022301489Doubler · wornWORN TITANIUM DOUBLER AT BS 1309 BETWEEN LONGERONS 18 & 23L. THE DOUBLER WAS REPLACED IAW ETI-88-17-067 R4 AND ER/A 554160-14 REV ORIGINAL.Feb 22, 2017 · N923DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2017022301487Doubler · corrodedCORROSION ON INTERNAL CUTOUT DOUBLER AT AFT LAVATORY SERVICE PANEL LOWER AFT CORNER. REPAIRED IAW ETI-88-17-067 REV.4 AND ER/A 554160-14 REV.ORIG.Feb 22, 2017 · N923DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2017022101364Frame · crackedAFT ACCESORIES COMPARTMENT. CRACKED FRAME BS 1474 BETWEEN LONGERONS 23 - 25R. THE FRAME WAS REPAIRED IAW SRM 53-01, FIG. 2, 51-30-2 ,AND 51-30-5.Feb 20, 2017 · N923DL · Doug MD88 · Fuselage Main, FrameSDR DALA2017022001360Frame · crackedAFT ACCESSORY BAY HAD CRACKS ON FRAME BS 1510. THE FRAME WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5, AND 51-30-8 .Feb 19, 2017 · N923DL · Doug MD88 · Fuselage Main, FrameSDR DALA2017021901354Skin · crackedVERTICAL STABILIZER CRACKED ON THE RAM AIR ACCESS CUTOUT 6301A. REPAIRED IAW SRM 55-05, PAR. 6, FIG. 3.Feb 18, 2017 · N923DL · Doug MD88 · Vertical Stabilizer, Plate/SkinSDR DALA2017021901358Angle · corrodedE& E BAY HAD CORROSION ON AN ANGLE, BS 150 AND LONGERON 28R. THE ANGLE WAS REPLACED IAW DWG 9911550 REV: E.Feb 17, 2017 · N923DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2017021701313Skin · damagedL1 DOOR SKIN BENDED THE SKIN WAS REPLACED IAW SRM 52-05, FIG 64.Feb 16, 2017 · N923DL · Doug MD88 · Passenger/Crew DoorsSDR DALA2017021701311Pan · crackedL1 DOOR HAS A CRACKED PAN AT FWD UPPER CORNER. THE PAN WAS REPAIRED IAW SRM 52-05, FIG 18A.Feb 16, 2017 · N923DL · Doug MD88 · Passenger/Crew DoorsSDR DALA2017021701309Angle · crackedL1 DOOR HAS A CRACKED TEE ANGLE AT FWD PASSENGER DOOR INTERNAL STRUCTURE BETWEEN BEAMS 4 AND 5 AND BS 168. THE TEE ANGLE WAS REPLACED IAW DWG 9955763 REV: K, SRM 51-30-2, AND 51-30-5.Feb 16, 2017 · N923DL · Doug MD88 · Passenger/Crew DoorsSDR DALA2017021601275Stringer · crackedPAX CABIN CRACKED LONG 3L ON STA Y=160. ACCOMPLISH WHIT WORK CARD 5330-01204-04. LONGERON 3L ON STA Y=160 WAS REPAIRED PER SRM 53-02 FIG18 AND 5330-01204-04 JOB 100-0001.Feb 15, 2017 · N923DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016060704399Wire · looseFLIGHT CREW REPORTED SMOKE IN THE COCKPIT ON APPROACH; DONNED O2 MASKS. SMOKE WAS COMING FROM UNDERNEATH THE CAPTAINS TAXI LIGHT CONTROL PANEL. AN EMERGENCY WAS DECLARED. MAINTENANCE FOUND A LOOSE TERMINAL WIRE AT THE LANDING LIGHT/GROUND FLOOD LIGHT SWITCH PJun 6, 2016 · N923DL · Doug MD88 · Light System WiringSDR DALA2015082005147Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROWS 2-10 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECKED GOOD.Aug 20, 2015 · N923DL · Doug MD88 · Emergency LightingSDR DALA2015071104299Skin · crackedCORROSION AND CRACKED BELLY SKIN AT BS 680, STRINGERS 29 - 30L, REPAIRED THE SKIN IAW ERA 537463-14, REV ORIG.Jul 10, 2015 · N923DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2015012200527Web · corrodedC-1 DOOR AFT CUTOUT WEB CORRODED APPROXIMATELY STA 27-434, LONGERONS L-27 AND L-25. BURNISHED AREA C-1 DOOR CUT-OUT WEB STA 427 TO 434, LONGERON L-27 TO L-25 AND ALODINED AREA. C/W UT OF AREA WITH ORIG 0.040 REM MAT 0.030 IAW NDTM P. 4 CA 04-00-07 A 9710. EVALJan 20, 2015 · N923DL · Doug MD88 · Fuselage Main, StructureSDR DALA2015011500337Pulley Bracket · wornLEFT PULLEY BRACKET, TAIL CONE RELEASE CABLE, GUARD PIN HOLE WORN. R & R PULLEYS BRACKET FOR TAIL CONE RELEASE CABLE AT LOWER LEFT IAW SRM 51-30-02 AND SRM 51-30-01.Jan 14, 2015 · N923DL · Doug MD88 · Aerodynamic FairingsSDR DALA2015012200539Frame · crackedDOOR FRAME CRACKED INSIDE L-1 DOOR AT UPPER AFT CORNER. REMOVED L-1 DOOR IAW AMM 52-11-00-401, STEP 1A-2A5. INSTALLED SERVICEABLE L1 DOOR IAW AMM 52-11-00-501. PERFORMED SATISFACTORY RIG & LEAK/PRESSURE CHECK IAW AMM 52-11-00.Jan 8, 2015 · N923DL · Doug MD88 · Passenger/Crew DoorsSDR DALA2015012600636Skin · damagedSKIN FOUND DENT AND SCRATCH AT BS 239 BELOW STRINGER 17L. REPAIRED IAW ERA 531743-14, REV A SEC III.Dec 27, 2014 · N923DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2014070203845Wire · brokenDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROW 6DEF WAS INOPERATIVE. MAINTENANCE FOUND WIRES BROKEN AT THE LIGHT RECEPTACLE. REPLACED THE LIGHT ASSEMBLY AND THE SYSTEM RETURNED TO NORMAL.Jul 1, 2014 · N923DL · Doug MD88 · Light System WiringSDR DALA2015031102095Skin · corrodedSIGNS OF CORROSION FOUND ON FUSELAGE LOWER SKIN AND INTERNAL C2 DOOR SURROUND DOUBLER. DAMAGE LOCATED AT STA 617-636 AND BETWEEN LONGERONS 29L AND 29R. DAMAGE CUT OUT AND REPAIRED IAW SECTION I OF ER/A 525291-14.Apr 30, 2014 · N923DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2015031102096Skin · corrodedCORROSION FOUND ON SKIN AT TCAS ANTENNA LOCATION. PERMANENT REPAIR ACCOMPLISHED IAW ER/A 525060-14.Apr 14, 2014 · N923DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA14010450923Light · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHT IN COCKPIT AND AT DOORS L1 & L2 WERE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLIES, REPLACED BULBS, AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.Feb 15, 2014 · N923DL · Doug MD88 · Emergency LightingSDR DALA13062390923Wire · shortedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT IN AFT CABIN. MAINTENANCE FOUND A SHORT IN THE WIRES IN THE TAIL AND REPAIRED WIRES.Nov 17, 2013 · N923DL · Doug MD88 · Light System WiringSDR DALA13042520923Bulkhead · crackedMX DISCOVERED THAT THE EMERGENCY ESCAPE PATH TAILCONE RELEASE ALIGNMENT PIN BULKHEAD SKIN WAS CRACKED. THIS IS CONSIDERED A DEFECT IN THE EMERGENCY ESCAPE SYS AND COULD HAVE AN ADVERSE AFFECT ON THE EVACUATION ROUTE IF IT PREVENTED PROPER DEPLOYMENT OF THE TAIAug 30, 2013 · N923DL · Doug MD88 · Fuselage Main, BulkheadSDR DALA13042500923Pin · wornMX DISCOVERED THAT THE RELEASE LATCH "TEE PIN" FOR THE TAILCONE WAS WORN OUT OF ALLOWABLE LIMITS. THE T-PINS WERE REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.Aug 30, 2013 · N923DL · Doug MD88 · Aerodynamic FairingsSDR DALA13042490923Release Cable · frayedMX DISCOVERED THAT THE TAILCONE KEVLAR RELEASE CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.Aug 30, 2013 · N923DL · Doug MD88 · Aerodynamic FairingsSDR DALA13042480923Spring · missingMX DISCOVERED THAT THE TEE PIN SPRINGS WERE MISSING AND REQUIRED REPLACEMENT.Aug 30, 2013 · N923DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA13042730923Release Cable · brokenMX DISCOVERED THAT THE EMERGENCY ESCAPE PATH TAILCONE RELEASE CABLE WAS BROKEN. THIS IS CONSIDERED A DEFECT IN THE EMERGENCY ESCAPE SYS AND COULD HAVE AN ADVERSE AFFECT ON THE EVACUATION ROUTE IF IT PREVENTED PROPER DEPLOYMENT OF THE TAILCONE. THIS NOT IN COMPAug 29, 2013 · N923DL · Doug MD88 · Aerodynamic FairingsSDR DALA13042510923Arm · out of rigMX DISCOVERED THAT THE TAILCONE RELEASE ARM WAS OUT OF ALLOWABLE RIG LIMITS. THE AFT TAILCONE RELEASE ARM WAS ADJUSTED TO GET PIN CLEARANCE FROM THE DOOR STOP AND THE SYSTEM WAS RIGGED BACK INTO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.Aug 29, 2013 · N923DL · Doug MD88 · Aerodynamic FairingsSDR DALA13040390923Connector · looseDURING LINE CHECK, MX FOUND EMERGENCY LIGHTS AT ROW 18D IN CABIN INOPERATIVE. FOUND CONNECTOR LOOSE, CONNECTED IT, AND FUNCTIONALLY CHECKED SYSTEM.Aug 20, 2013 · N923DL · Doug MD88 · Light System WiringSDR DALA13040380923Power Supply · inoperativeDURING LINE CHECK, MX FOUND OVERHEAD EMERGENCY PATHWAY LIGHTING FOR CATWALK IN TAIL WAS INOPERATIVE. MX REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.Aug 20, 2013 · N923DL · Doug MD88 · Emergency LightingSDR DALA13026850923Battery · inoperativeDURING LINE CHECK, MX FOUND THAT BOTH THE FWD AND THE AFT OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. MX REPLACED THE BATTERIES IN BOTH BATTERY PACKS AND THE LIGHTS RETURNED TO AN OPS CONDITION.Jun 3, 2013 · N923DL · Doug MD88 · Emergency LightingSDR DALA1213210923Longeron Splice · crackedLONGERON 29L SPLICE IS CRACKED AT STA 1193-1211. REMOVED SPLICE ON LONGERON 29L AT STA 1193-1211 IAW MD80 SRM 51-30-5 PG 12 AND 29. TP BE REPAIRED ON NRC 202495.Mar 4, 2012 · N923DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA1218500923Fitting · chafedNR 2 PYLON AT NAC 201 I/B LOWER SIDE BULKHEAD FITTING EXTERIOR CHAFED. BLENDED DAMGAED AREA, FOUND TO BE OUT OF LIMITS. REPAIR TO BE ACCOMPLISHED PER PRI 501029-14 REV 0 & 1.Feb 28, 2012 · N923DL · Doug MD88 · Nacelle/Pylon, Bulkhead/FirewallSDR DALA1216570923Frame · crackedMAIN CABIN STA 1117 LONGERON 7L FRAME IS CRACKED. CUT OUT DAMAGED AREA IAW MD80 SRM 53-03D FIG 4. FABRICATED REPAIR PART 2 EA ANGLE REPAIR AND FILLER REPAIR IAW MD80 SRM 53-03D FIG 4 AND INSTALLED PER MD80 SRM 51-30-2 PARA 1 PG 1, MD80 SRM 51-30-5 PARA 1 PG Feb 27, 2012 · N923DL · Doug MD88 · Fuselage Main, FrameSDR DALA1212910923Cusp Web · corrodedLT CUSP WEB AT STA 834 LBL 58 IN MAIN CABIN IS CORRODED. FOUND TO BE OUT OF LIMITS IAW MD80 SRM 53-01 PG 8 FIG 1. FABRICATED AND INSTALLED FILLER SPLICE DOUBLER AND RING DOUBLER PER MD80 SRM 51-30-2 PG 24 DURING HMV ON NRC 197383.Feb 27, 2012 · N923DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA1212520923Floor Support · corrodedCORROSION ON MAIN CABIN FLOOR SUPPORT ATTACH ANGLE STA 200 RBL 42. FOUND TO BE OUT OF LIMITS IAW MD80 SRM 53-01 PG 8 FIG 1. FABRICATED AND INSTALLED FLOOR SUPPORT ANGLE ON MAIN CABIN AT STA 200 RBL 42 IAW MD80 SRM 51-30-01 FIG 1 PGS 1, 2 AND 3 AT SAA DURING Feb 26, 2012 · N923DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA1215450923Longeron · crackedIN CABIN FUSELAGE LONGERON 3L IS CRACKED AT STA 160. BLENDED DAMAGE SECTION, FABRICATED AND INSTALLED LONGERON REPAIR AND SPLICE IAW DC9/MD80 SRM 53-02 DURING HMV.Feb 24, 2012 · N923DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA1212510923Floor Support · corrodedCORROSION ON MAIN CABIN FLOOR SUPPORT MOUNT TRACK STA 188 RBL 4. FOUND FLOOR SUPPORT STA 188 RBL 44 OUT OF LIMITS IAW MD80 SRM 53-01 FIG 1 SHEET 3 PG 8. FABRICATED AND INSTALLED FLOOR SUPPORT AT STA 188 RBL 44 IAW MD80 SRM 51-30-5 PG 12 AT DURING HMV ON.Feb 23, 2012 · N923DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA1213190923Cusp Web · corrodedMAIN CABIN RT CUSP WEB HAS CORROSION FROM STA 503-525 INCLUDING THE PREVIOUS REPAIR DOUBLER AT STA 511. REMOVED CORROSION CUSP WEB AREA FROM STA 503-525. MATERIAL LOST FOUND TO BE OUT OF LIMITS IAW MD80 SRM 53-01 FIG 1 SHEET 3. CUT OUT DAMAGE AREA IAW DWG SFeb 21, 2012 · N923DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA1212900923Seat Track · corrodedMAIN CABIN SEAT TRACK AT RBL 22 HAS CORROSION FROM SEAT TRACK PLUG AT STA 433-797. FOUND STA 498.5-499.5 AND STA 597-598 TO BE OUT OF LIMITS IAW MD80 SRM 51-10-01 FIG 26. INSTALLED NEW SECTION OF TRACK RBL 22 STA 493-609 AND 2 EA SPLICES AND REPAIR PLATES IAFeb 20, 2012 · N923DL · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1212870923Floor Support · gougedMAIN CABIN FLOOR SUPPORT STRUCTURE IS GOUGED AT STA 826 LBL 17-RBL 17. FOUND TO BE OUT OF LIMITS IAW DC9/MD80 SRM 53-01 FIG 1 PG 8. FABRICATED AND INSTALLED FLOOR SUPPORT IAW DC9/MD80 SRM 51-30-5 PARAGRAPH 7 ON NRC 202315. (NRC 202315)Feb 20, 2012 · N923DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA1212530923Seat Track · corrodedMAIN CABIN STA 1098-1088 BL22L SEAT TRACK HAS CORROSION. FOUND OUT OF LIMITS IAW MD80 SRM 53-05 FIG 4B 1 SECTION D-D SHEET 2 PG 28. REPAIR TO BE ACCOMPLISHED ON NRC 202469.Feb 19, 2012 · N923DL · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1210750923Seat Track · corrodedMAIN CABIN STA 454 TO 456 BL L22 SEAT TRACK HAS CORROSION. REMOVED CORROSION AT STA 454-456 L22 SEAT TRACK, FOUND TO BE OUT OF LIMITS.Feb 19, 2012 · N923DL · Doug MD88 · Fuselage, Seat/Cargo Attach Fittings
Back to N923DL, cancelled Apr 8, 2019