N951DL, cancelled Jan 24, 2020

Service difficulty reports · 102

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 = 'N951DL' AND deregistration_id = 'N951DL-2020-01-24'
  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 DALA2019010200018Position Switch · out of adjustSLAT DISAGREE AT FLAPS 15. T/S FLAP/SLAT HANDLE POS SEITCH REF AMM 22-80 FOUND SWITCH OUT OF ADJUSTMENT, REQUIRES MAINTENANCE. REMOVED AND REPLACED FLAP HANDLE SWITCH PACK ASSY PER AMM 27-80. PERFORMED NR 1 & NR 2 RTS BOTH "GO". SDR REPORTED DUE TO DECLARED EMJan 1, 2019 · N951DL · Doug MD88 · Leading Edge Slat Position Indicating SystemSDR DALA2018121877255Brake · odorAFTER LANDING BURNING RUBBER SMELL IN CABIN AND COCKPIT, NO HAZE. FOUND NBR 4 TIRE FLAT SPOT. R/R NBR 4 MLG WHEEL ASSY AND BRAKE ASSY PER MD88 AMM 32-40,32-42. T/S ANTISKID PER MD88 AMM 32-43. CKS GOOD. PERFORMED NO GO ODI PREVENTION SECTION 2172. C/W WC 2120-Dec 17, 2018 · N951DL · Doug MD88 · Landing Gear Brake SystemSDR DALA2018120306970Regulator Valve · malfunctionedSHIP 951- PRESS - FLOW LIGHT IN CRUISE. DURING DESCENT PRESSURIZATION COULD NOT KEEP UP. AT 10,000 FEET AIRCRAFT WAS COMPLETELY DEPRESSURIZED UNTIL LANDING. CORRECTIVE ACTION: REPLACED LEFT PRESSURE REGULATING VALVE AND LEFT A/C PILOT PRESSURE REGULATOR. (LP48Dec 2, 2018 · N951DL · Doug MD88 · Cabin Pressure Control SystemSDR DALA2018090705496Splice · defectiveEMERGENCY LIGHT INOP ROW 25 TO 28 SEATS. FOUND SPLICE BAD AT ROW 28 RT AND 25 RT. REPAIRED BOTH SPLICE IAW AMM 20-50 AND AMM WDM 33-51 OPS CHECK GOOD.Sep 5, 2018 · N951DL · Doug MD88 · Light System WiringSDR DALA2018052003452Frame · crackedWHILE WORKING RT HYD PRESSURE PROBLEM FOUND RT FWD WHEEL WELL FRAME CRACKED 4" BELOW PROX SENSOR. REMOVED DAMAGED FRAME AND BEGAN DRILLED NEW FRAME PER DWG 5930584. INSTALLED NEW FRAME PER DWG 5930584.May 19, 2018 · N951DL · Doug MD88 · Fuselage Main, FrameSDR DALA2018021700972Light · inoperativeEMERGENCY LIGHT 24ED INOPERATIVE. R & R THE LIGHT ASSY. OPS NORMAL IAW AMM 33-52.Feb 17, 2018 · N951DL · Doug MD88 · Emergency LightingSDR DALA2017112108256Pin · detachedL1 DOOR SLIDE PIN NOT ATTACHED. R & R THE DOOR SLIDE IAW JIC 5200-0652.Nov 20, 2017 · N951DL · Doug MD88 · Escape SlideSDR DALA2017100507316Pin · disengagedDURING INSPECTION OF THE L1 DOOR MOUNTED ESCAPE SLIDE PIN ENGAGEMENT, PIN NOT ENGAGED. REPLACED THE DOOR SLIDE IAW 2561-4964.Oct 5, 2017 · N951DL · Doug MD88 · Escape SlideSDR DALA2017071705511Slide · damagedFOUND SLIDE PACK UNFOLDING. REMOVED AND REPLACED THE TAILCONE SLIDE PACK.Jul 16, 2017 · N951DL · Doug MD88 · Escape SlideSDR DALA2017032402372Unknown · odorPASSING 6,000 MSL FLIGHT ATTENDANT CALLED TO REPORT A STRONG PLASTIC BURNING SMELL IN CABIN THAT GOT STRONGER FURTHER BACK IN CABIN. NO SMOKE OR HAZE OBSERVED. FAINT OILY SMELL OBSERVED IN FLIGHT DECK. RAN QRH PAGE 8.6 FOR SMOKE, FIRE OR FUMES. RETURNED TO CVGMar 23, 2017 · N951DL · Doug MD88 · Air Distribution SystemSDR DALA2017013100762Duct · disconnectedFLIGHT RETURNED TO ATL DUE TO ODOR AND VISIBLE HAZE IN FIRST CLASS GALLEY AREA. CREW REPORTED WHEN AIRFOIL ANTI-ICE WAS SELECTED ON, A LOUD NOISE WAS HEARD, FOLLOWED BY RUSHING AIR NOISE WITH ASSOCIATED SMOKE/ODOR. AIRFOIL ANTI-ICE WAS SELECTED OFF AND NOISE CJan 30, 2017 · N951DL · Doug MD88 · Airfoil Anti/De-ice SystemSDR DALA2017011800480Fitting · crackedDURING LUBRICATION OF GROUND SPOILER ACTUATORS, THE HINGE SUPPORT WAS FOUND CRACKED AT LT WING. HINGE SUPPORT FITTING. THE FITTING WAS REPLACED IAW AMM 20-30-01 AND DC9/MD80 SRM 51-30-1, 51-30-2 AND 51-30-5.Jan 17, 2017 · N951DL · Doug MD88 · SpoilersSDR DALA2017011700383Door Frame · corrodedMID CARGO BAY HAD CORROSION ON THE LOWER DOOR FRAME BS 636 - 693. THE DOOR FRAME WAS REPAIRED IAW SRM 53-05 PAR. 140 FIG. 123.Jan 16, 2017 · N951DL · Doug MD88 · Fuselage Main, StructureSDR DALA2017011600361Skin · crackedCRACKED SKIN AT FWD AIRSTAIR DOOR FRAME AT AFT LWR CORNER. THE SKIN WAS REPAIRED IAW DWG SR09530031 REV K.Jan 15, 2017 · N951DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2017011500359Door Frame · corrodedAFT CARGO BAY HAD CORROSION ON LOWER DOOR FRAME BS 1155 - 1212. THE DOOR FRAME WAS REPAIRED IAW SRM 53-05 PAR 140 FIG. 123.Jan 14, 2017 · N951DL · Doug MD88 · Fuselage Main, StructureSDR DALA2017011500358Stringer · crackedA CRACK WAS FOUND ON STRINGER 11 LT WING STA XRS =160. THE STRINGER WAS REPAIRED IAW DRAWING SR09570100.Jan 14, 2017 · N951DL · Doug MD88 · Wing, Longeron/StringerSDR DALA2017010900210Frame · crackedCRACK ON RT AFT WHEEL WELL FRAME. THE FRAME WAS REPLACED IAW SRM 51-30-2.Jan 8, 2017 · N951DL · Doug MD88 · Fuselage Main, FrameSDR DALA2016072905652Wire Harness · inoperativeDURING SERVICE CHECK, FOUND SEAT 15E EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY IAW CMM 33-50-63. OPS NORMAL.Jul 28, 2016 · N951DL · Doug MD88 · Light System WiringSDR DALA2016071605362Structure · crackedCRACK FOUND IN RT WING L/E AT NR 2 SLAT LOCATION. C/W ERA 548916-14 REV ORIGINAL ACCOMPLISHED SEC 1 TIME LIMITED REPAIR. SECTION 2 PERMANENT REPAIR DUE WITHIN 760 DAYS.Jul 15, 2016 · N951DL · Doug MD88 · Wing Miscellaneous StructureSDR DALA2016070305057Slide · malfunctionedCABIN SERVICE DEPLOYED TAIL CONE ASSY AND SLIDE DID NOT BLOW. REPLACED TAILCONE EVACUATION SLIDE IAW WC 5350-4287.Jul 2, 2016 · N951DL · Doug MD88 · Escape SlideSDR DALA2016061304603Lamp · inoperativeDURING SERVICE CHECK, LT OVERWING EMERGENCY LAMP WAS NOT ILLUMINATING. REPLACED THE LAMP AND OPS CHECKED NORMAL.Jun 12, 2016 · N951DL · Doug MD88 · Emergency LightingSDR DALA2016061304602Battery Pack · inoperativeDURING SERVICE CHECK, FOUND OVERWING EMERGENCY LIGHTS REMAINED ILLUMINATED AFTER EMERGENCY POWER REMOVED. REPLACED OVERWING EMERGENCY LIGHTS BATTERY PACK.Jun 12, 2016 · N951DL · Doug MD88 · Emergency LightingSDR DALA2016050903840Connector · disconnectedTHE CREW OF FLIGHT 2459, FOUND SEAT 14D EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RESEATED A PLUG PIN AND THE LIGHT CHECKED OK.May 9, 2016 · N951DL · Doug MD88 · Light System WiringSDR DALA2015102806541Light · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 19D IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.Oct 27, 2015 · N951DL · Doug MD88 · Emergency LightingSDR DALA2015010200009Intercostal · crackedCRACK ON INTERCOSTAL BETWEEN BS 1148 - 1153, LONGERONS 29 - 30R. THE INTERCOSTAL WAS REPLACED IAW DWG 5930483, REV AL, SRM 51-30-2, 51-30-5, AND 51-10-3 PAR 14 AND 21.Jan 1, 2015 · N951DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2015010200008Lanyard · frayedINSPECTION DISCOVERED THAT THE L1 DOOR EMERGENCY ESCAPE SLIDE LANYARD WAS FRAYED. THE SLIDE LANYARD WAS REPLACED.Jan 1, 2015 · N951DL · Doug MD88 · Escape SlideSDR DALA2014122606769Cusp Web · corrodedCORROSION ON LEFT CUSP WEB X 54 - 60, BETWEEN BS 859 - 864. CUSP WEB REPARED IAW SRM 51-10-3, PAR 14, 21, 26, 38. 53-05 FIG 131A-1 AND ER/A 511165-14 MA AND 51-30-2.Dec 25, 2014 · N951DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2014072404204Channel · brokenMAINTENANCE DISCOVERED THAT THE TAILCONE CATWALK OVER THE VENTRAL STAIRWAY HAD GOTTEN STUCK HALF WAY THROUGH TRANSITION WHEN LOWERING THE STAIRS. CAUSE OF BINDING WAS BROKEN CHANNEL EXTRUSION ON THE STAIR AREA SIDEWALL. THIS IS CONSIDERED A DEFECT IN THE EMEJul 17, 2014 · N951DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA14032320951Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT SEVERAL OF THE OVERHEAD EMERGENCY PATHWAY LIGHTS IN THE FWD CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.May 27, 2014 · N951DL · Doug MD88 · Emergency LightingSDR DALA14007810951Acm · odorDURING CLIMB, CREW BEGAN DETECTING FUMES. THE ODOR INCREASED AT CRUISE FLIGHT AND WAS WORSE IN THE REAR CABIN AREA. FLIGHT WAS DIVERTED, WHEN THE FUMES INFILTRATED COCKPIT TO SUCH A DEGREE THAT THE FLIGHT CREW DONNED MASKS. MAINTENANCE REPLACED THE LT AIR CYFeb 7, 2014 · N951DL · Doug MD88 · Cabin Cooling SystemSDR DALA13062890951Power Supply · inoperativeDURING LINE CHECK, CEILING EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 10-15. REPLACED POWER SUPPLY AND OPS CHECKED GOOD IAW AMM 33-53.Nov 22, 2013 · N951DL · Doug MD88 · Emergency LightingSDR DALA13036150951Skin · crackedCRACKED FUSELAGE SKIN BELOW RAM AIR SCOOP BS 1418 BETWEEN LONG 1 AND 2 RT. (VHS) (T0 286773). DAMAGE WAS REMOVED, FILLERS & DOUBLERS WERES FABRICATED, REPAIR PARTS WERE INSTALLED, REPAIR WAS IDENTIFIED, REPAIR WAS ACCOMPLISHED IAW ER/A 516239-14AD REV ORIG Jul 24, 2013 · N951DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA13036140951Heater Blanket · out of limitsDURING UT INSPECTION 1 VOID AREA 271 SQ " WAS FOUND ON LT HEATER BLANKET AND IS OUT OF LIMITS IAW CARD 5700-2232, JOB 001-0843, FIG 1, STEP 1(B) (LW) REF (T0 286220) (CARD 21, ZONE 13). LT HEATER BLANKET PANEL WAS REPLACED IAW AMM 30-80-02, PAGE BLOCK 401. RJul 23, 2013 · N951DL · Doug MD88 · Airfoil Anti/De-ice SystemSDR DALA2015011607845Skin · crackedDURING HMV4, A SID INSPECTION FOUND A TWO INCH CRACK AT BS 1418 BETWEEN L1 AND L2R. THE CRACK WAS REPAIRED. SID AD 2004-11-07 APPLIES. ACCOMPLISH ER/A 88-516239-14 SECTION II DTA REQUIREMENT WITHIN 18 MONTHS OF SECTION I ACCOMPLISHMENT. ASSOCIATED ER/A 88-Jul 22, 2013 · N951DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA13035110951Longeron · crackedCRACK ON LONGERON 2L AT BS 1418 IN AFT ACCESORY COMPARTMENT. CRACKED LONGERON WAS REMOVED AND A NEW LONGERON WAS INSTALLED WITH THE PREVIOUS REPAIR SPLICE, 53-02 FIG 18.Jul 17, 2013 · N951DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA13035100951Longeron · corrodedCORROSION ON LONGERON 29LT BETWEEN BS 1287 TO 1298 AT AFT CARGO COMPARTMENT. CORROSION REMOVED IAW SRM 51-10-3 PAR 26. AREA FOUND OUT OF LIMITS IAW SRM 53-01, FIG 1 (SHEET 3). DAMAGE AREA WAS REMOVED AND NEW LONGERON SECTION AND REPAIRS WERE INSTALLED IAW 5Jul 17, 2013 · N951DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2014102406956Skin · damagedDURING HMV 4 A LIGHTNING STRIKE WAS FOUND AND REPAIRED AT FS 906 AND L-3R. THIS REPAIR AFFECTS A PSE.Jul 16, 2013 · N951DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA13035650951Skin · damagedLIGHTING STRIKE ON OUTER FUSELAGE SKIN BETWEEN LONGERON 3-4R BS 693, DAMAGE WAS BLEND OUT AND WAS FOUND OUT OF LIMITS AND AREA WAS REPAIR IAW ER/A 516241-14, REV ORIG AND SRM 53-04-1, PAR 6 (UT) WAS ACCOMPLISHED.Jul 16, 2013 · N951DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA13034570951Longeron · crackedCRACK ON LONGERON 14LT BS 1380 IN AFT ACCESSORY COMPARTMENT. CRACKED LONGERON WAS REMOVED, NEW LONGERON SECTION AND SPLICE WERE INSTALLED. REPAIR LONGERON WAS IDENTIFIED, REPAIR WAS ACCOMPLISHED IAW SRM 53-02, FIG 18.Jul 14, 2013 · N951DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA13034560951Longeron · crackedCRACK ON LONGERON 11LT BS 1380, IN AFT ACCESSORY COMPARTMENT. LONGERON WAS REMOVED, NEW LONGERON AND SPLICE WERE INSTALLED, REPAIR LONGERON WAS IDENTIFIED, REPAIR WAS ACCOMPLISHED IAW SRM 53-02, FIG 18.Jul 14, 2013 · N951DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA13034410951Longeron · damagedCRACKED LONGERON 2R AT BS 693 AT CABIN FUSELAGE STRUCTURE. DAMAGE LONGERON REMOVED. NEW LONGERON INSTALLED IAW SRM 53-02 FIG 18.Jul 9, 2013 · N951DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA13034400951Longeron · crackedCRACK ON LONGERON 18 RT AT BS 1380 IN AFT ACCESSORY COMPARTMENT. LONGERON WAS REMOVED FROM BS 1370 TO 1395 SPLICES WERE FABRICATED AND INSTALLED. REPAIR WAS IDENTIFIED AND ACCOMPLISHED IAW SRM 53-02, FIG 18.Jul 9, 2013 · N951DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA13034390951Longeron · corrodedCORROSION ON LONGERON 27 LT BETWEEN BS 1287 TO 1309 AT AFT CARGO COMPARTMENT. DAMAGED LONGERON REMOVED IAW SRM 53-02, FIG 18. NEW SECTION LONGERON AND REPAIR SPLICE INSTALLED IAW SRM 53-02, FIG 18.Jul 9, 2013 · N951DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA13034010951Longeron · crackedCRACK AND INADEQUATE SCREW HOLES ON LONGERONS 1 AND 2 LT FROM STA Y=256 TO 275. (FCS) REF (T0 286313) (CARD 204 ZONE 58). LONGERONS 1 & 2 WERE REMOVED, NR 1 FROM STA 256 TO 320 AND NR 2 FROM STA 256 TO 275, NEW LONGERONS AND REPAIR SPLICES WERE INSTALLED IAW SJul 8, 2013 · N951DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA13034080951Lever · wornDURING A CHECK OF TAILCONE RELEASE SYS, MX FOUND THE LOCKPIN LEVER AND LATCH LEVER WERE WORN BEYOND ALLOWABLE LIMITS. MX REPLACED THE TAILCONE LOCK SYS. THE RII COMPLETED FOLLOWING MX.Jul 7, 2013 · N951DL · Doug MD88 · Aerodynamic FairingsSDR DALA13033990951Turnbuckle · corrodedMX DISCOVERED THAT THE EMERGENCY ESCAPE PATH TAILCONE RELEASE CABLE HAD CORRODED HARDWARE (TURNBUCKLES). 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 Jul 4, 2013 · N951DL · Doug MD88 · Aerodynamic FairingsSDR DALA13034100951Cam · wornMX DISCOVERED THAT THE TAILCONE RELEASE CAM BASE WAS WORN OUT OF ALLOWABLE LIMITS. THE CAM BASE WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE RII WAS SATISFACTORY.Jul 3, 2013 · N951DL · Doug MD88 · Aerodynamic FairingsSDR DALA13034020951Longeron · crackedCRACKED LONGERON NR 3LT AND 4LT, STA Y=160 OF FUSELAGE INTERNAL STRUCTURE. DAMAGED SECTION OF LONGERONS 4LT AND 3LT WERE REMOVED AND NEW SECTIONS OF LONGERONS WERE INSTALLED. REPAIRS WERE IDENTIFIED IAW SRM 53-02, FIG 18 AND 51-10-4. RII COMPLETED.Jul 1, 2013 · N951DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA13031880951Cusp Web · corrodedCORROSION ON RT CUSP WEB UPPER SURFACE BETWEEN BS 1136 AND 1231 X=-54 TO X=-60. CORROSION WAS REMOVED FROM BS 1155 AND 1174. FOUND OUT LIMITS IAW ER/A 511165-14 MA REV A.Jun 26, 2013 · N951DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA13035120951Skin · wornSTRUCTURE STA 953-958 AT RT MLG DOOR. PREVIOUS REPAIR DOUBLER WAS REMOVED IAW SRM 51-30-2. NEW DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, PAR 14, 21.Jun 22, 2013 · N951DL · Doug MD88 · Fuselage Main, Plate/Skin
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