N927DA, cancelled Apr 8, 2019

Service difficulty reports · 180

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 = 'N927DA' AND deregistration_id = 'N927DA-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 DALA2018072304608Charger · inoperativeEMERGENCY PATH LIGHTING AT SEATS 13-23 INOP. R&R BATTERY CHAGER AT B5-211 PER 33-50 OPS CK NML.Jul 23, 2018 · N927DA · Doug MD88 · Emergency LightingSDR DALA2018011700260Reservoir · malfunctionedDURING CRUISE, RT HYD LOW PRESSURE MESSAGE ON OAP, RIGHT HYD QTY WENT UP TO 19 QTS. FOLLOWING QRH, REPRESSURIZED BELOW 10,000 FT. PRESSURE CAME UP TO 3000 PSI, QTY DOWN TO 10 QUARTS. PRESSURE WAS ZERO FOR 5 - 20 MINUTES. REPLACED THE RESERVOIR AND ENGINE DRIVJan 17, 2018 · N927DA · Doug MD88 · Hydraulic Reservoir, MainSDR DALA2017100207192Connector · disconnectedEMERGENCY LIGHTS INOPERATIVE SEATS 10D, 27D, AND 33D. CHECK LIGHTS AND WIRING. CONNECTED THE CONNECTORS. CHECKED GOOD.Sep 29, 2017 · N927DA · Doug MD88 · Light System WiringSDR DALA2017052104053Shutoff Valve · leakingDURING FLIGHT, CREW REPORTED RIGHT HYDRAULIC FLUID QUANTITY LOSS AND ACCOMPLISHED QRH PROCEDURE SECURING RIGHT HYDRAULIC SYSTEM PUMPS. ON APPROACH, ATTEMPTED TO RE-PRESSURIZE RIGHT HYDRAULIC SYSTEM PER QRH AND THE SYSTEM FAILED TO PRESSURIZE. ACCOMPLISHED ALTEMay 20, 2017 · N927DA · Doug MD88 · Rudder Control SystemSDR DALA2017032302348Battery · dischargedAIR STAIR EMER LIGHTS INOP. REPLACED BATTERIES AFT EMER LIGHT BATTERY PACK REF AMM 33-53.Mar 23, 2017 · N927DA · Doug MD88 · Emergency LightingSDR DALA2017030101645Pin · out of adjustTAILCONE RELEASE MECHANISM CAM ASSY. PIN IS IMPROPERLY INDEXED ON SPLINE. REINDEXED CAM RELEASE PIN PER MD88 AMM 53-53-02-201, O.K. FOR SERVICE.Feb 28, 2017 · N927DA · Doug MD88 · Aerodynamic FairingsSDR DALA2017021201145Valve · failedAFTER TAKEOFF AT 3000FT CABIN AND FLIGHT CREW NOTICED THAT AIRCRAFT WAS LOSING CABIN PRESSURE. AT 12,000FT MSL MAX CABIN ALTITUDE REACHED 10,500FT. CABIN ALTITUDE AND MASTER WARNING LIGHTS WERE ILLUMINATED ALONG WITH CABIN ALTITUDE WARNING HORN SOUNDING. ATB Feb 13, 2017 · N927DA · Doug MD88 · Cabin Pressure Control SystemSDR DALA2016121909973Slide · malfunctionedDOOR 1L OPENED BY FA WHILE ARMED. SLIDE DID NOT DEPLOY. INSPECTED SLIDE VERIFIED PARACHUTE PINS ARE INSTALLED. REINSTALLED SLIDE ON L1 DOOR PER AMDS CARD 2561-4964. OK FOR SERVICE.Dec 18, 2016 · N927DA · Doug MD88 · Escape SlideSDR DALA2016042403283Skin · damagedLIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN BS 1174 AND LONGERON 1. EXTERNAL FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04-1, PAR 6 D, 3, COND 3, AMM 25-28-00-201, AMM 21-00-00-401, ETI 88-16 -175, REV 5, ER/A 545136-14 MA, REV ORIGINAL, AND PS 900-5-1, NR 04. REPApr 23, 2016 · N927DA · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2016042303238Skin · corrodedCORROSION ON INNER PRODUCTION DOUBLER BS 1309, OUTFLOW VALVE AREA. DUE TO EXCESIVE CORROSION DOUBLER WAS REPLACED IAW SRM 51-10-4M, 51-10-3, PAR 21 AND 14, 51-30-2 AND 51-30-5, AND DWG 5936021.Apr 22, 2016 · N927DA · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2016042303237Skin · corrodedCORRODED PREVIOUS REPAIR DOUBLER BETWEEN BS 200 TO 218, LONGERON 29LT TO 30 AT ELECTRONIC EQUIPMENT COMPARTMENT. REPAIR WAS ACCOMPLISHED IAW ER/A 545129-14, REV ORIGINAL AND ERI -88-16-171, REV 1, SECTION 1.Apr 22, 2016 · N927DA · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2016042303236Skin · damagedEXPOSED MATERIAL ON LT, RT SIDE AT RUDDER. DAMAGE AREA BOTH SIDE WERE REPAIRED IAW ERA NR 092613-14MA, REV "A", SRM 51-70-01A, PAR 23 AND ERA NR 545122-14, REV ORIGINAL.Apr 22, 2016 · N927DA · Doug MD88 · Rudder, Plate/SkinSDR DALA2016042503249Skin · corrodedFUSELAGE, SKIN, FS 200-218, L29-30L AT MODE S ANTENNA CORROSION REPAIR. ACCOMPLISH ER/A 545129-14, SECTION II.Apr 21, 2016 · N927DA · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2016042203231Structure · damagedHINGE EDGE ON RUDDER LT/RT SIDE. EDGE ON RUDDER LT & RT SIDE WERE REPAIRED IAW SRM 51-70-4AD AND OPEN 2304653.Apr 21, 2016 · N927DA · Doug MD88 · Rudder StructureSDR DALA2016042103148Pan · crackedCRACKED PAN ON AFT UPPER AT R1 DOOR. PAN WAS REPAIRED IAW SRM 52-03D, FIG 3.Apr 20, 2016 · N927DA · Doug MD88 · Service DoorsSDR DALA2016042103147Beam · crackedCRACKED BEAM NR 1 AFT EDGE AT FWD SERVICE DOOR. BEAM WAS REPLACED IAW SRM 51-30-2.Apr 20, 2016 · N927DA · Doug MD88 · Service DoorsSDR DALA2016042103143Longeron · crackedCRACKED LONGERON 29L, BS 200. THE LONGERON WAS REPLACED IAW SRM 53-14-1, FIG 3, 51-30-2 AND 51-30.Apr 20, 2016 · N927DA · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016042003140Beam · crackedCRACKED BEAM NR 4 FWD EDGE AT FWD R1 DOOR. NR 4 BEAM WAS REPLACED IAW DWG 9911582, REV T, 51-30-1, 51-30-2, 51-30-4 AND 51-30-5.Apr 19, 2016 · N927DA · Doug MD88 · Service DoorsSDR DALA2016042003135Skin · damagedEXPOSED MATERIAL ON LT & RT SIDE AT RUDDER. LT & RT SIDE AT RUDDER WERE REPAIRED IAW ER/A 092613-14MA, REV A, ER/A 545141-14, REV ORIGINAL.Apr 19, 2016 · N927DA · Doug MD88 · Rudder, Plate/SkinSDR DALA2016042003134Skin · damagedASSESS DAMAGE ON FUSELAGE SKIN BS 484, BETWEEN LONGERON 23-24 RT, SPEED TAPE ID DATA. REPAIR WAS EVALUATED AND FOUND ACCOMPLISHED IAW INSTRUCTIONS OF SRM 53-04-2, FIG 2, SHEET 5, AS PERMANENT REPAIR.Apr 19, 2016 · N927DA · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2016042003131Beam · damagedCRACKED PAN ON FWD EDGE AT NR 4BEAM FWD R1 SERVICE DOOR. BEAM WAS REPAIRED IAW SRM 52-03, FIG 3.Apr 19, 2016 · N927DA · Doug MD88 · Service DoorsSDR DALA2016041903026Longeron · crackedCRACK ON LONGERON 4L BS 200. LONGERON WAS REPLACED IAW SRM 53-02, FIG 18, PAR 12, 51-30-5, AND CARD 5330-01204-02-03. Apr 18, 2016 · N927DA · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016041903024Longeron · crackedCRACKED LONGERON 29R BS 180. LONGERON WAS REPLACED IAW SRM 53-02, FIG 18, SHEET 2, 51-30-2, 51-10-4, 51-30-5, PAR 7, FIG 10, PAR 14, 21.Apr 18, 2016 · N927DA · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016041802991Longeron · crackedCRACKED LONGERON 29R BS 180 AT ELECTRONIC EQUIPMENT COMPARTMENT. LONGERON WAS REPLACED IAW SRM 53-02, FIG 18, SHEET 2, 51-30-2, 51-10-4, 51-30-5 PAR 7, FIG 10, PAR 14, 21.Apr 17, 2016 · N927DA · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016041802989Cargo Track · crackedCRACK ON LOWER SUPPORT OF TIE TRACK BETWEEN BS 1212 TO 1231 AND PROJECTION LONGERONS 28LT TO 27LT AT AFT CARGO COMPARTMENT. SUPPORT WAS REPLACED IAW SRM 53-05, FIG 4G, 51-10-3, PAR 21,14, 51-30-2, 51-30-5.Apr 17, 2016 · N927DA · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016041702971Rib · crackedCRACKED RIB ON RT WING FIXED L/E BS XRS 324. THE RIB WAS REPAIRED IAW SRM 57-06 B, D, FIG 18.Apr 15, 2016 · N927DA · Doug MD88 · Wing, Rib/BulkheadSDR DALA2016041602963Support Fitting · corrodedCORROSION ON MLG SUPPORT FITTING LOWER AREA BS XCW=98.500. AREA WAS REPAIRED IAW SRM 57-03, FIG 34, 51-10-3, P 14-21 AND 51-30-5.Apr 14, 2016 · N927DA · Doug MD88 · Fuselage, Landing Gear Attach FittingsSDR DALA2016041502929Skin · damagedFUSELAGE SKIN DAMAGED BETWEEN BS 1287- 1309, LONGERON 26L.Apr 14, 2016 · N927DA · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2016041402909Longeron · crackedAD 98-13-35, REV 1: CRACK ON LONGERON 2 LT BS 160, AT CPAX COMPLETE WC 5330-01204-0205. 1ST EVAL, LONGERON NR 2 WAS REPAIRED IAW SRM 51-30-2, 53-02, FIG 18, 51-10-4, 51-10-3 PAR 14 AND 21, 51-30-5.Apr 13, 2016 · N927DA · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016041302867Door Frame · corrodedCORROSION ON DOOR FRAME AT CARGO DOOR BS 650 - 690 LONGERON 28R. CORROSION WAS REMOVED AND REWORKED AREA WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 26, 21, 14. WITHIN LIMITS IAW SRM 53-05, FIG 123.Apr 12, 2016 · N927DA · Doug MD88 · Fuselage Main, StructureSDR DALA2016021501078Battery Pack · inoperativeMAINTENANCE FOUND THE AFT CEILING EMERGENCY LIGHTS INOPERATIVE. BATTERIES WERE REPLACED AND THE LIGHTS CHECKED GOOD.Feb 14, 2016 · N927DA · Doug MD88 · Emergency LightingSDR DALA14017360927Connector · disconnectedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEAT 27D/E IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYS.Mar 18, 2014 · N927DA · Doug MD88 · Light System WiringSDR DALA13051230927Toggle · failedACFT FAILED THE FUNCTIONAL CHECK OF TAILCONE RELEASE SYS WHEN A WORN TOGGLE ON THE SLIDE LANYARD PREVENTED THE SLIDE FROM DEPLOYING. THE TOGGLE WAS REPLACED, THE SYS WAS RETURNED OPERATIONAL STATUS, AND THE RII WAS COMPLETED.Oct 8, 2013 · N927DA · Doug MD88 · Escape SlideSDR DALA13046470927Battery Pack · inoperativeDURING LINE CHECK, MX FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE LT AND RT OVERWING DOORS WERE INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.Sep 21, 2013 · N927DA · Doug MD88 · Emergency LightingSDR DALA13046010927Connector · damagedDURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 19R IN THE CABIN WAS INOPERATIVE. MX FOUND A LOOSE PIN IN THE CONNECTOR AND RE-PINNED IT. THE SYS RETURNED TO NORMAL OPERATION.Sep 18, 2013 · N927DA · Doug MD88 · Light System WiringSDR DALA13044350927Power Supply · inoperativeDURING LINE CHECK, MX FOUND THAT MULTIPLE OVERHEAD EMERGENCY PATHWAY LIGHTS IN THE MID-CABIN WERE INOPERATIVE. MX REPLACED THE POWER SUPPLY AND RELAMPED AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.Sep 12, 2013 · N927DA · Doug MD88 · Emergency LightingSDR DALA13002440927Structure · crackedON BOLT HOLE INSPECTION OF VERTICAL STAB, FOUND OVERSIZED HOLE WITH CRACK INDICATION. FOUND HOLE TO BE LARGER THAN .202" ALLOWABLE HOLE SIZE. OVERSIZED HOLE WAS REPAIRED IAW FINAL ER/A 510507-14AD REV ORIG ASSOCIATED ER/A 14-510507 ADDED FOR AC 0927.Jan 16, 2013 · N927DA · Doug MD88 · Vertical StabilizerSDR DALA13002410927Release Mech · stuckMX DISCOVERED THAT THE TAILCONE RELEASE SYS CAM WAS STUCK, CAM AND BLOCKS FOR THE RELEASE CABLE WERE WORN AND OUT OF RIG BEYOND ALLOWABLE LIMITS. THE MATING FLANGE WAS CRACKED AT MULTIPLE ALIGNMENT PIN POSITIONS. THE CABLE CAMS AND BLOCKS WERE REPLACED ANDJan 12, 2013 · N927DA · Doug MD88 · Aerodynamic FairingsSDR DALA13002450927Structure · damagedON BOLT HOLE INSPECTION OF VERTICAL STAB, FOUND THREE HOLES DAMAGED. DAMAGE CLEAN-UP RESULTED IN OVERSIZING HOLES LARGER THAN ALLOWED SIZE. OVERSIZED HOLES WERE REPAIRED IAW ER/A 510499-14AD, REV ORIG ASSOCIATED ER/A 14-510499 ADDED FOR AC 0927.Jan 11, 2013 · N927DA · Doug MD88 · Vertical StabilizerSDR DALA13002430927Structure · crackedON BOLT HOLE EC INSPECTION OF RT SIDE VERTICAL, 3 HOLE DOWN FROM COLLAR, FAULT FOUND OVERSIZED HOLE WITH CRACK INDICATION, CLEAN UP OF HOLE, NO HELP. FURTHER CLEANUP OF SUSPECTED HOLE WITH CRACK AND FOUND HOLE TO BE LARGER THAN .202" ALLOWABLE HOLE SIZE. OVEJan 11, 2013 · N927DA · Doug MD88 · Vertical StabilizerSDR DALA13002420927Attach Fitting · damagedCOMPLETING BOLT HOLE EC OF VERTICAL STAB, FOUND 3 RT SIDE HOLES, THREAD CUT-DAMAGED INSIDE OF HOLES. REMOVED NUT PLATE CHANNEL & POLISHED HOLES. ACCOMPLISHED DVI OF REWORKED AREA, DAMAGE CONTAINED. ALL 3 HOLES ARE LARGER THAN THE .202" ALLOWABLE HOLE SIZE. Jan 11, 2013 · N927DA · Doug MD88 · Vertical Stabilizer, Attach FittingsSDR DALA1245510927Seat Track · corrodedSEAT TRACK STA 1155 LBL 22 HAS AREA OF CORROSION ON LT FLANGE AND BARE META. SEAT TRACK REPLACED ON NRC 7000098670001.Aug 13, 2012 · N927DA · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1245500927Seat Track · corrodedSEAT TRACK AT STA 1287-1309 LBL 22 HAS CORROSION ON TOP OF TRACK INSIDE CHANNEL IN 3 AREAS. SEAT TRACK REPLACED ON NRC7000098670001.Aug 13, 2012 · N927DA · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1245490927Seat Track · corrodedSEAT TRACK AT STA 1174-1193 LBL 22 HAS 2 AREAS OF CORROSION ON LT FLANGE AND BARE METAL. SEAT TRACK REPLACED ON NRC 7000098670001.Aug 13, 2012 · N927DA · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1245480927Seat Track · corrodedSEAT TRACK AT BS 1271-1287 HAS CORROSION ON TOP OF TRACK AND INSIDE CHANNEL. SEAT TRACK REPLACED ON NRC 7000098670001.Aug 13, 2012 · N927DA · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1245470927Seat Track · corrodedSEAT TRACK AT BS 1250-1271 HAS CORROSION ON TOP OF TRACK AND DOWN IN CHANNEL. REPAIRED PER MD-88 SRM 51-30-1.Aug 12, 2012 · N927DA · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1245460927Beam · corrodedMID CARGO LOWER BILGE BEAM HAS CORROSION AT BS 636 AND L29R. COMPLIED WITH ER/A 505651-14 REV ORIG.Aug 12, 2012 · N927DA · Doug MD88 · Fuselage Main, StructureSDR DALA1245450927Skin · dentedRT FUSELAGE STA 1375 L-7R HAS A DENT JUST BELOW SKIN OVERLAP. ACCOMPLISHED ER/A 505309-14 REV ORIG.Aug 12, 2012 · N927DA · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA1245430927Seat Track · corrodedCABIN SEAT TRACK SECTION LBL 54 FS 266-797 HAS PITTING CORROSION AT CTR CHANNEL AND LUGS FS 790-797. REPLACED SEAT TRACK IAW SRM 53-05.Aug 12, 2012 · N927DA · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1245420927Cusp Web · corrodedMAIN CABIN RT CUSP WEB LOWER SURFACE HAS CORROSION AT BS 933. WEB REPLACED ON NRC 210001.Aug 12, 2012 · N927DA · Doug MD88 · Fuselage Miscellaneous Structure
Back to N927DA, cancelled Apr 8, 2019