N936DL, cancelled Feb 12, 2021

Service difficulty reports · 130

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 = 'N936DL' AND deregistration_id = 'N936DL-2021-02-12'
  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 DALA2018082105162Fuse · failedDURING A SERVICE CHECK, FOUND SEAT EMERGENCY LIGHTS, ROWS 30 TO AFT INOPERATIVE. TROUBLESHOT IAW WDM 33-51-14. FOUND TWO BAD FUSES ON CHARGER B5-212, AND LOOSE CONNECTOR AT PAX SEAT 33E. REPLACED FUSES IAW CMM 25-60-03, AND RECONNECTED THE PLUG, IAW AMM 3Aug 19, 2018 · N936DL · Doug MD88 · Emergency LightingSDR DALA2018070304329Wire · brokenSEAT MOUNTED EMERGENCY LIGHT INOP FROM ROW 31 TO 36. FOUND BAD FUSE ON BATTERY PACK, REMOVED AND REPLACED- NO HELP, AFTER INSPECTION OF WIRES FOUND BROKEN WIRE TO BATTERY PACK. REPAIRED WIRE/SPLICE IAW SPM 20-50 AND WDM 33-21. OPS CHECK GOOD.Jun 29, 2018 · N936DL · Doug MD88 · Light System WiringSDR DALA2018062304165Support Fitting · crackedRT WW TRAPEZOIDAL AND FLAP ACTUATOR SUPPORT FITTING MID-SECTION CRACKED. REMOVED AND REPLACED RT MLG W/W FLAP ACTUATOR SUPPORT FITTING IAW DRAWING 9910155 REV ED, REV DY, 5936030 REV AV, AND SRM 51-30-5. CRACK DIM 2.0".Jun 21, 2018 · N936DL · Doug MD88 · Trailing Edge FlapsSDR DALA2018062004116Skin · dentedLT WING NR 1 FLAP VANE LWR SURFACE HAS DENTS. ACCOMPLISHED PERMANENT REPAIR ON LT WING NR 1 FLAP VANE LWR SURFACE IAW SRM 57-03 AND SRM 51-70-2 PAR 18 B.Jun 19, 2018 · N936DL · Doug MD88 · Trailing Edge FlapsSDR DALA2018110106390Floorbeam · corrodedCORRODED CEILING ANGLE IN E&E STA 160 APPROX RBL 30. CORROSION DAMAGE ON MAIN CABIN FLOORBEAM STA 160 RBL 30 FOUND OUT OF LIMITS DUE TO 100% MAT LOSS, ORIG THICKNESS .078" IAW SRM 53-01. ACCOMPLISHED A PERMANENT REPAIR TO AREA IAW ER/A 569009-14 REV ORIGINAL.Jun 18, 2018 · N936DL · Doug MD88 · Fuselage Main, Floor BeamSDR DALA2018061504021Skin · corrodedLT AFT FUSELAGE LAV SERVICE ACCESS DOOR LOWER CUTOUT IS CORRODED AT APPROX STA 1312. IN WORK REPAIR.Jun 14, 2018 · N936DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2018061403996Doubler · corrodedAFT FRAME 1338 LOWER CHORD AFT SIDE TO APB STA 1361 HAS CORROSION IN BILGE APPROX LBL 10 - RBL 10. CORROSION DAMAGE ON AFT JACK PAD DOUBLER STA 1338 BL0 FOUND TO BE OUT OF LIMITS DUE TO 100% MAT LOSS, ORIG THICKNESS .100" IAW SRM 53-01 AND DRAWING 9915561 REV Jun 13, 2018 · N936DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2018052503605Engine · making metalFLT 1668 DIVERTED TO CAE DUE TO A RIGHT ENGINE COMPRESSOR STALL ON CLIMB OUT AND ERRATIC ENGINE INDICATIONS. THE FLIGHT CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE ENGINE WAS NOT SHUT DOWN. MAINTENANCE FOUND METAL IN THE TAIL PIPE AND THE 3RD &May 25, 2018 · N936DL · Doug MD88 · Engine (Turbine/Turboprop)SDR DALA2018042502809Cable · disconnectedCREW REPORTED THAT THE RT ENGINE WAS UNRESPONSIVE ON APPROACH. SHUT THE ENGINE DOWN AT 20K DURING DECENT. THE RIGHT ENGINE DID NOT RESPOND. ENGINE WAS STUCK AT IDLE. THE ENGINE BEGAN CREEPING UP TO 1.4 EPR, WHICH WAS TOO MUCH FOR LANDING. THE FLIGHT CREW ELEApr 25, 2018 · N936DL · Doug MD88 · Power LeverSDR DALA2018040202049Csd · failedRIGHT CSD OIL PRESSURE LOW MESSAGE ILLUMINATED DURING FLIGHT & APU WOULD NOT START. DIVERTED. MAINTENANCE FOUND NO OIL IN RIGHT CSD WITH FLUID AROUND FILTER AND SERVICE PORT. REPLACED THE CSD, GENERATOR, AND COOLER IAW AMM. BLED FUEL LINE TO APU AND STARTED Apr 2, 2018 · N936DL · Doug MD88 · AC Generator-AlternatorSDR DALA2017111608160Engine · making metalDECLARED AN EMERGENCY DUE TO A RIGHT ENGINE OIL STRAINER CLOG MESSAGE. FOUND METAL IN THE OIL FILTER AND ON MCD. RT ENGINE CHANGED.Nov 15, 2017 · N936DL · Doug MD88 · Engine (Turbine/Turboprop)SDR DALA2017110808005Light · inoperativeSEAT 19DEF EMERGENCY LIGHT INOPERATIVE. REPLACED THE LIGHT ASSY IAW AMM 33-53.Nov 8, 2017 · N936DL · Doug MD88 · Emergency LightingSDR DALA2017022301492Skin · corrodedFUSELAGE SKIN AND INTERNAL DOUBLER BS 750 - 759, LONGERON 29L - 29R CORRODED. REPAIRED IAW ERA 555617-14 ISSUED.Feb 22, 2017 · N936DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2016120509608Battery Pack · inoperativeAFT OVERWING EXIT LIGHTS INOPERATIVE. TROUBLESHOT TO THE BATTERY PACK B5105. R & R BATTERY PACK IAW WDM 33-51.Dec 4, 2016 · N936DL · Doug MD88 · Emergency LightingSDR DALA2016120509607Fuse · failedFIRST CLASS EMERGENCY LIGHTS INOPERATIVE. FOUND A BAD FUSE AT BATTERY CHARGER BASE. REPLACED THE FUSE IAW AMM 33-51. LIGHTS CHECKED OK.Dec 3, 2016 · N936DL · Doug MD88 · Emergency LightingSDR DALA2016101907380Fuse · blownEMERGENCY EXIT LIGHTING IN FIRST CLASS INOP. REPLACED FUSE NR 1 ON RT F/C EMERGENCY LIGHT BATTERY PACK, NOW OPS NORMAL. OK FOR SERVICE.Oct 18, 2016 · N936DL · Doug MD88 · Emergency LightingSDR DALA2016060204322Pan · crackedRIGHT AFT OVERWING EXIT DOOR PAN CRACKED AT FWD UPPER DOOR STOP. R & R DOOR IAW AMM 52-21-00. LEAK CHECKED GOOD.Jun 1, 2016 · N936DL · Doug MD88 · Fuselage Main, StructureSDR DALA2016060104269Tail Cone · out of rigVAULT DOOR FORCE REQUIRED TO DROP TAIL CONE EXCEEDED 20 LBS TENSION. ADJUSTED TAIL CONE RIG IAW AMM 53-53-00 AND AMDS 5350-01077-0101.May 31, 2016 · N936DL · Doug MD88 · Aerodynamic FairingsSDR DALA2016060104267Skin · crackedA/C SKIN HAS .3750" LONG CRACK EXTENDING INBD FROM FASTENER HOLE AT BS 1418, 1.5" OTBD OF L2R. ACCOMPLISHED SEC I IAW ERA 547264-14AD. SEC II MONITOR AMOC REQUIRED BY 25 MAY 17. ESTABLISHED ON LOG PAGE 2505537.May 31, 2016 · N936DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2016060104265Skin · corrodedPOPPED RIVET AND PILLOWING SKIN CORROSION ON BELLY AT BS 217 STR 30. COMPLETED SEC I IAW ERA 546984-14, REV O. SECTION II MONITOR TO BE ACCOMPLISHED AT 8000 CYCLE INTERVALS ESTABLISHED ON LOG PAGE 2509314.May 31, 2016 · N936DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2016053004219Door Frame · corrodedFWD CARGO DOOR FRAME UNDER ENTRY SCUFF PLATE CORRODED. DOOR FRAME OF SRM LIMITS. REMOVED AND REINSTALLED NEW LOWER PAN. REPAIRED IAW SRM 53-05, FIG 44A.May 27, 2016 · N936DL · Doug MD88 · Fuselage Main, StructureSDR DALA2016052604152Attach Fitting · brokenDUCT JOINT LOWER ATTACH TAB IS BROKEN, AFT OF LT GROUND BLOWER. WELDED TAB IAW ER/A 494638-14MA, REV B.May 25, 2016 · N936DL · Doug MD88 · Fuselage Main, Attach FittingsSDR DALA2016041502937Battery Pack · inoperativeMAINTENANCE FOUND THE AFT CABIN EMERGENCY LIGHTS INOPERATIVE. BATTERY PACK WAS REPLACED AND THE LIGHTS CHECKED OK.Apr 15, 2016 · N936DL · Doug MD88 · Emergency LightingSDR DALA2015113007264Wire Harness · damagedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 22D IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.Nov 25, 2015 · N936DL · Doug MD88 · Light System WiringSDR DALA2015102306402Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE VENTRAL STAIRWAY ARE VERY DIM. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Oct 22, 2015 · N936DL · Doug MD88 · Emergency LightingSDR DALA2015082005095Angle · crackedSTABILIZER SUPPORT STRUCTURE LT ANGLE CRACKED. REMOVED ANGLE, REPLACEMENT ANGLE WAS FABRICATED FROM .090, 7075-0, HEAT TREATED TO T6 CONDITION. ON RO 702799 IAW DWG 9911808, DRILL AND TRIMMED ANGLE. TREATED AND PAINTED. INSTALLED NEW ANGLE ALL FASTENERS SECAug 18, 2015 · N936DL · Doug MD88 · Vertical StabilizerSDR DALA2015082005094Angle · crackedDURING JACKSCREW INSPECTION FOUND VERTICAL STABILIZER SUPPORT STRUCTURE RT ANGLE CRACKED. ANGLE WAS FABRICATED FROM .090 7075-0 AND HEAT TREATED TO T6 ON RO 702799 IAW DWG 9911808. TREATED AND PAINTED. INSTALLED NEW ANGLE ALL FASTNERS SECURED REF SRM 51-30-Aug 18, 2015 · N936DL · Doug MD88 · Vertical StabilizerSDR DALA2015062403973Wire Harness · damagedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FROM THE EXIT ROWS TO THE AFT CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS DUE TO THE WIRES BEING RIPPED FROM THE PINS AT THE CONNECTOR AT AFT CABIN LAST ROW. THE SYSTEJun 23, 2015 · N936DL · Doug MD88 · Light System WiringSDR DALA2015010800154Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS ABOVE THE AFT OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.Jan 8, 2015 · N936DL · Doug MD88 · Emergency LightingSDR DALA14024500936Release Cable · out of toleranceDURING THE TAILCONE RELEASE SYS FUNCTIONAL CHECK, MAINTENANCE FOUND THAT THERE WAS EXCESSIVE TENSION ABOVE 25 LBS IN THE RELEASE CABLE SYSTEM. THE CABLE RELEASE MECHANISM WAS ADJUSTED AND THE SYSTEM WAS RIGGED TO PULL AT 19 LBS. THE RII STEPS WERE COMPLETED AApr 17, 2014 · N936DL · Doug MD88 · Aerodynamic FairingsSDR DALA14024520936Catwalk · crackedMAINTENANCE DISCOVERED THAT THE TAILCONE CATWALK OVER THE VENTRAL STAIRWAY HAD STRUCTURAL CRACKS IN 3 PLACES. THIS IS CONSIDERED A DEFECT IN THE EMERGENCY ESCAPE SYSTEM AND COULD HAVE AN ADVERSE AFFECT ON THE EVACUATION ROUTE. THE CATWALK WAS REPAIRED IAW ER/Apr 16, 2014 · N936DL · Doug MD88 · Fuselage Main, StructureSDR DALA13071130936Wire Harness · inoperativeDURING LINE CHECK, NOTED THE SEAT MOUNTED EMERGENCY LIGHT AT 22DE INOPERATIVE. REPLACED HARNESS AT 22DE IAW AMM 33-52 AND OPERATION THEN CHECKED GOOD.Dec 23, 2013 · N936DL · Doug MD88 · Light System WiringSDR DALA13063500936Cabin Pressure · malfunctionedPERFORMED AN AIR TURN BACK DUE TO ACFT CABIN WOULD NOT PRESSURIZE DURING CLIMB OUT. FLOW LIGHT ILLUMINATED. NO FAULTS ON EITHER CABIN PRESSURE CONTROLLERS. OUTFLOW VALVE OPERATION CHECKED GOOD. PRESSURIZED ACFT ON EACH PACK WITH NO EXTERNAL LEAKS FOUND. NONov 22, 2013 · N936DL · Doug MD88 · Cabin Pressure Control SystemSDR DALA13049090936Ballast · burnedDURING CLIMBOUT, AN ACRID ODOR BEGAN ISSUING FROM AIR CONDITIONING DUCTS. THE ENGINE ANTI-ICE WAS ON AND NORMAL PNEUMATIC CONFIGURATION. SELECTED A COLDER TEMP ON PACKS AND FUMES EVENTUALLY DISSIPATED. FOUND INOPERATIVE LIGHTING BALLAST AT ROW 33ABC. BALLSep 20, 2013 · N936DL · Doug MD88 · Passenger Compartment LightingSDR DALA13011990936Wire · disconnectedDURING OVERNIGHT MX, THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT ROW 31 WAS FOUND TO BE INOPERATIVE. MX FOUND A WIRE PULLED FROM THE CONNECTOR AT ROW 31. THE CONNECTOR WAS REPLACED IAW STANDARD WIRING PRACTICES MANUAL CHAPTER 20. OPERATION CHECKED GOOD.Mar 14, 2013 · N936DL · Doug MD88 · Light System WiringSDR DALA13001020936Wire Harness · inoperativeDURING LINE CHECK, MX FOUND THAT THE EMERGENCY LIGHTING AT SEATS 22 AND 28DE INOPERATIVE. MX REPLACED WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.Jan 12, 2013 · N936DL · Doug MD88 · Light System WiringSDR DALA12016860936Seat Track · corrodedAFT CABIN, SEAT TRACK CORRODED AND GOUGED, BS 1226 TO 1250, RBL 22. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REPLACED SEAT TRACK IAW SRM 51-30-1.Dec 19, 2012 · N936DL · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA12016810936Seat Track · corrodedCORROSION AND GOUGES ON MAIN CABIN SEAT TRACK AT LBL 45.5 FROM FS 484 TO 493. REMOVED SEAT TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 51-30-5 AND SRM 51-30-1.Dec 19, 2012 · N936DL · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA12016800936Longeron · damagedCORROSION ON DOME NUT IN MAIN CABIN BS 250 L1. REPLACED LONGERON 2L SECTION AND SPLICE. REPLACED TWO ATTACH ANGLE FWD AND AFT DOME NUTS BETWEEN BS 227 AND 290. PERFORMED TCAS SELF TEST FOR UPPER TCAS ANTENNA. ALL WORK ACCOMPLISHED IAW SRM 51-30-5, 51-30-2,Dec 19, 2012 · N936DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA12016760936Channel · damagedE & E BAY BS 218, LONGERON 30 & 29 LT HAS DAMAGE TO LONGERON FLANGE ON BOTH SIDES OF LONGERON HAT CHANNEL. REMOVED DAMAGE ON E/E BAY STA 218, LONGERON 30 AND 29L ON LONGERON FLANGE IAW SRM 51-03, FIG 1. FOUND TO BE WITHIN LIMITS. HFEC INSP DETECTED 1 EA CRACKDec 17, 2012 · N936DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA12016750936Doubler · corrodedFS 594 BETWEEN L30-L29R, POTABLE WATER BELLY DRAIN DOUBLER CORRODED. REMOVED CORROSION FROM DOUBLER FS 594 L30-29R MID CARGO IAW SRM 51-10-3. FOUND TO BE OUT OF LIMITS. FABRICATED, TREATED, AND INSTALLED POTABLE WATER FITTING HOSE AND INTERNAL RING DOUBLER Dec 17, 2012 · N936DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA12016740936Attach Angle · crackedVERTICAL STAB TO FUSELAGE LT SKATE ANGLE AND FASTENERS ARE CRACKED STA 1474 CANT. CUT OUT CRACKED AREA AT VERTICAL STAB TO FUSELAGE LT SKATE ANGLE STA 1474 CANT. FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE IAW SRM 53-05, FIG 23 THE CRACKED FASTENER WAS Dec 17, 2012 · N936DL · Doug MD88 · Vertical Stabilizer, Attach FittingsSDR DALA12016730936Skin · crackedDURING NDT INSPECTION, FWD SERVICE DOOR JAMB CORNER, FOUND ONE CRACK ON UPPER FWD CORNER ON OUTER LAYER OF SKIN. CUT OUT DAMAGE AREA AND REPAIRED IAW SRM 53-05, FIG 112, VIEW D AND ER/A 45.Dec 17, 2012 · N936DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA12016480936Skin · damagedCORROSION ON CUTOUT AND AROUND FASTENERS, FWD CARGO BAY BS 370 L26R. REPAIRED DAMAGED IAW SRM 51-70-4, PG 1-4.Dec 16, 2012 · N936DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA12016080936Fairing · crackedON INSTALLATION OF VERTICAL STAB TIP FAIRING, FOUND A CRACK ON RT SIDE, EMINATING FROM A RADIUS OF UPPER SKIN. REMOVED FITTING ON RT STAB FAIRING BY ACCESS TO CRACK. NDT VERIFIED END OF CRACK, CHECK STOP DRILL, AND OPEN HOLES. FABRICATED, PRIMERED, TREATED, Dec 13, 2012 · N936DL · Doug MD88 · Vertical StabilizerSDR DALA12015370936Bulkhead · crackedFS 1007, LBL 18 MLG WW AFT PRESSURE BULKHEAD AFT FACE (ACCESS FROM AFT CARGO BIN) SUSPECTED CRACK NEXT TO U CHANNEL STIFFENER APPROX 2 INCHES FROM TOP OF BULKHEAD (064-68) COMPLIED WITH FINAL ER/A 508338-14 REV ORIGINAL.Dec 6, 2012 · N936DL · Doug MD88 · Fuselage Main, BulkheadSDR DALA12015360936Bulkhead · crackedFS 1007, RBL18, MLG WW AFT PRESSURE BULKHEAD AFT FACE (ACCESS FROM AFT CARGO BIN) SUSPECTED CRACK NEXT TO U-CHANNEL STIFFENER APPROX 2" FROM TOP OF BULKHEAD (064-69). COMPLIED WITH PRI 508338-14, REV 0, COMPLIED WITH PRI 508338-14 REV 1, COMPLIED WITH FINAL EDec 6, 2012 · N936DL · Doug MD88 · Fuselage Main, BulkheadSDR DALA12014850936Longeron · damagedLONGERON 4R CRACKED AT ST 522 AND ST 541 UNDER SUPPORT MOUNT (204-111&112). REMOVED INTERCOSTAL BETWEEN STA 522-541 AT L4R. REMOVED DAMAGE LONGERON AT STA 513 TO 550 AT L4R. HFEC INSPECTION NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED LONGERON AND SPLICES Dec 5, 2012 · N936DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA12014840936Cusp Web · corrodedCORROSION ON CUSP WEB FLOOR PANEL, AFT LT CORNER ST 199L AT BL 44L (204-151). CUTOUT CORROSION AND REPAIRED CUSP WEB FLOOR PANEL STA 199 LBL44 IAW SRM 53-01, FIG 4, SHEET 4. COMPLETED AND INSPECTED.Dec 5, 2012 · N936DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA12014830936Skin · corrodedON REMOVAL OF POTABLE WATER BELLY DRAIN AT FS 594 BETWEEN L30-L29R, EXTERNAL FUSELAGE FOUND CORROSION ON DRAIN CUTOUT AND INTERNAL SKIN. COMPLIED WITH ER/A 508946-14 REV ORIGINAL. COMPLETED AND INSPECTED. ASSOCIATED ER/A 14-508946 ADDED FOR AC 0936.Dec 5, 2012 · N936DL · Doug MD88 · Fuselage Main, Plate/Skin
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