N929DL, cancelled Mar 19, 2019

Service difficulty reports · 93

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 = 'N929DL' AND deregistration_id = 'N929DL-2019-03-19'
  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 DALA2017122808938Pin · disengagedON SERVICE CHECK, FOUND THE L1 DOOR SLIDE ENGAGEMENT PINS NOT ENGAGED. REMOVED AND REPLACED THE L1 DOOR SLIDE ASSY IAW AMM 25-62-00.Dec 27, 2017 · N929DL · Doug MD88 · Escape SlideSDR DALA2017101607537Battery Pack · inoperativeOVERHEAD EMERGENCY LIGHTS INOPERATIVE FROM ROWS 16 - 20. REPLACED THE BATTERY PACK B5-102. CHECKED GOOD.Oct 16, 2017 · N929DL · Doug MD88 · Emergency LightingSDR DALA2017052604304Battery Pack · inoperativeEMERGENCY EXIT LIGHT INOPERATIVE AT SEAT ROW 24, BOTH SIDES. REMOVED AND REPLACED BATTERY PACK B5-103 IAW AMM 33-53.May 26, 2017 · N929DL · Doug MD88 · Emergency LightingSDR DALA2017020300906Bulb · inoperativeMULTIPLE EMERGENCY CEILING BULBS ARE OUT. REPLACED THE BULBS.Feb 3, 2017 · N929DL · Doug MD88 · Emergency LightingSDR DALA2017010700206Lever · corrodedCORROSION ON NOSE LANDING GEAR SHOCK STRUT LEVER ASSY. NOSE WHEEL STEERING CONTROL LEVER WAS REPLACED IAW AMM 32-52-06.Jan 6, 2017 · N929DL · Doug MD88 · Landing Gear Steering SystemSDR DALA2017010600135Pan · crackedHIDDEN DAMAGE, CRACK ON AFT EDGE INNER PAN AT BEAM NR 1 ON FWD SERVICE DOOR. SERVICE DOOR (R1) WAS REPAIRED PER ETI-88-16-496 REV 1 AND ER/A N 552897-14 REV ORIG.Jan 5, 2017 · N929DL · Doug MD88 · Service DoorsSDR DALA2017010400069Beam · crackedCRACKED AFT EDGE BEAM NR 1 ON FWD SERVICE DOOR. CRACKED BEAM NR 1 ON FWD SERVICE DOOR WAS REPLACED PER SRM 51-30-2, 51-30-5.Jan 4, 2017 · N929DL · Doug MD88 · Service DoorsSDR DALA2017010100017Angle · crackedCRACKED AFT ANGLE OVER BEAM NR 1 ON FWD SERVICE DOOR. THE ANGLE WAS REPLACED IAW SRM 51-30-5 AND DWG 9911579 REV L.Dec 31, 2016 · N929DL · Doug MD88 · Service DoorsSDR DALA2017010100016Access Panel · damagedLT WING:ELONGATED HOLE ON ACCESS PANEL 1363C. REPAIRED IAW SRM 51-22-2A PAR 6 CONDITION II.Dec 31, 2016 · N929DL · Doug MD88 · Wing, Plate/SkinSDR DALA2017010310181Angle · crackedCRACKED DOOR PAN ANGLE BTW BEAM 5 AND 6 AT MAIN ENTERANCE DOOR. SPLICE WAS REPLACED PER DC 9/MD80 SRM 51-30-02 AND DWG 5914121 REV. AV. (LP2828943)Dec 30, 2016 · N929DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2016123010141Skin · crackedRIGHT WING CRACKS AND SHEARED FASTENERS AT SLAT PANEL NR 3 INBD SKIN. REPAIRED IAW SRM 57-01, FIG. 5.Dec 29, 2016 · N929DL · Doug MD88 · Leading Edge DevicesSDR DALA2016122810099Door Frame · corrodedAFT CARGO DOOR FRAME CORRODED BS 1212 TO 1155. REPAIRED IAW SRM 53-05 FIG. 123 A.Dec 27, 2016 · N929DL · Doug MD88 · Fuselage Main, StructureSDR DALA2016122810097Longeron · crackedCRACKED LONGERON 3L ON BS 160. REPAIRED IAW SRM 53-02 FIG.18. Dec 27, 2016 · N929DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA2016122410059Fairing · crackedCRACK ON LT ELEVATOR CONTROL TAB FAIRING. ELEVATOR CONTROL TAB FAIRING WAS REPAIRED IAW SRM 55-01 FIG 2 (SHEET 2).Dec 23, 2016 · N929DL · Doug MD88 · Elevator, Tab StructureSDR DALA2016122310041Skin · crackedA CRACK ON THE FUSELAGE SKIN BS 1474 LONGERON 22L. THE SKIN WAS REPAIRED IAW SRM 53-01 FIG. 2 AND SRM 51-30-2.Dec 23, 2016 · N929DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2016121409851Spar Cap · crackedRIGHT WING REAR SPAR CAP XRS=164 CRACKED. REPAIRED IAW ER/A 530469-14AD, REV A.Dec 1, 2016 · N929DL · Doug MD88 · Wing SparSDR DALA2016101707293Connector · disconnectedEMERGENCY LIGHTS AT ROW 25 INOPERATIVE. CONNECTED THE CONNECTOR AND OPS CHECKED GOOD.Oct 15, 2016 · N929DL · Doug MD88 · Light System WiringSDR DALA2016072805628Wire · looseEMERGENCY LIGHT INOPERATIVE AT SEATS 17D AND 27D. CONNECTED A LOOSE CONNECTION. CHECKED GOOD.Jul 27, 2016 · N929DL · Doug MD88 · Light System WiringSDR DALA2016062304888Connector · damagedDURING LINE CHECK, FOUND CABIN EMERGENCY EXIT LIGHTS INOPERATIVE, ROW 15-23. REPAIRED CONNECTOR AT ROW 15. LIGHTS NOW OPERATE NORMAL.Jun 22, 2016 · N929DL · Doug MD88 · Light System WiringSDR DALA2016042503297Spring · brokenMAINTENANCE FOUND THE TAILCONE DEPLOYMENT MECHANISM SPRING BROKEN. THE SPRING WAS REPLACED IAW DWG 5910828.Apr 24, 2016 · N929DL · Doug MD88 · Aerodynamic FairingsSDR DALA2016012500572Connector · looseMAINTENANCE FOUND SEAT ROW 1 EMERGENCY LIGHT INOPERATIVE. A LOOSE CONNECTOR WAS FOUND AND RECONNECTED. THE LIGHT OPS CHECKED GOOD.Jan 24, 2016 · N929DL · Doug MD88 · Light System WiringSDR DALA2016012500571Wire · brokenMAINTENANCE FOUND THE EMERGENCY LIGHTING INOPERATIVE FROM SEAT ROWS 15 TO 23. A BROKEN WIRE WAS FOUND AT ROW 15 AND REPAIRED. THE LIGHTS CHECKED GOOD.Jan 24, 2016 · N929DL · Doug MD88 · Light System WiringSDR DALA2015122807741Inlet · crackedDURING SEVERE TURBULANCE INSPECTION, FOUND APPROXIMATELY 6" CRACK AT AIR INLET LT SIDE AT BASE OF VERTICAL. WELDED APU AIR INLET IAW ERA 382101-14MA. ACCOMPLISHED FPI OF WELDED AERA IAW PS 900-6-3, NR 2.Dec 28, 2015 · N929DL · Doug MD88 · APU Bleed Air SystemSDR DALA2015100505960Wire 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.Oct 3, 2015 · N929DL · Doug MD88 · Light System WiringSDR DALA2014121506534Spar Cap · crackedRT WING REAR SPAR LOWER CAP XRS 164, CRACKED 0.250 INCHES AT LOWER-INBD ATTACH BOLT. REPAIR THE SPAR IAW ER/A 530469-14 AD, REV 0.Dec 14, 2014 · N929DL · Doug MD88 · Wing SparSDR DALA2014121006499Frame · corrodedAFT CARGO BAY FRAME BS 1271 BETWEEN LONGERON 29-30R HAS LIGHT CORROSION ON LOWER SIDE OF FRAME ON BOTH SIDES. CUT DAMAGED AREA IAW SRM 53-03, FIG 2A. FABRICATED REPAIR PARTS IAW SRM 53-03, REV 2A. ALODINED AND PRIMED REPAIR PARTS IAW SRM 51-10-3. APPLIED TODec 9, 2014 · N929DL · Doug MD88 · Fuselage Main, FrameSDR DALA2014101705607Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS AT ROWS 21-30 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.Oct 16, 2014 · N929DL · Doug MD88 · Emergency LightingSDR DALA14021050929Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY EXIT SIGNS AT BOTH OF THE OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECKED GOOD.Apr 6, 2014 · N929DL · Doug MD88 · Emergency LightingSDR DALA13071140929Battery Pack · inoperativeDURING LINE CHECK, NOTED SEVERAL EMERGENCY LIGHTS INOPERATIVE IN FWD CABIN. REPLACED BATTERY PACKS IN FWD DROP DOWN PANEL AT LAV DOOR AND SEAT ROW 12DEF. OPS CHECKED GOOD.Dec 21, 2013 · N929DL · Doug MD88 · Emergency LightingSDR DALA13036930929Connector · looseDURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT INOPERATIVE. FOUND A CONNECTOR IN THE WIRE HARNESS LOOSE, CONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.Jul 28, 2013 · N929DL · Doug MD88 · Light System WiringSDR DALA13033730929Frame · crackedCANTED FRAME AT BS 1474, TAIL INTERIOR. CRACKED AT FASTENER 4:00 POSITION. REMOVED CRACKED SECTION. HFEC INSP CUTOUT 2" X 1.5" IAW NDT SPM 06-10-01.001, NO DEFECTS NOTED. INSTALLED DOUBLER IAW SRM 51-70-5. IDENTIFIED REPAIR "P" WITH TAG. JOB COMPLET. REQJul 2, 2013 · N929DL · Doug MD88 · Fuselage Main, FrameSDR DALA13033480929Bracket · looseMX DISCOVERED THAT THE TAILCONE RELEASE CABLE SPRING BRACKETS ARE LOOSE. THE BRACKETS HARDWARE WAS REPLACED, RESECURED, AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED AND THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.Jul 2, 2013 · N929DL · Doug MD88 · Aerodynamic FairingsSDR DALA13033470929Release Cable · frayedMX DISCOVERED THAT THE TAILCONE RELEASE CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYS WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.Jul 2, 2013 · N929DL · Doug MD88 · Aerodynamic FairingsSDR DALA13016550929Connector · disconnectedDURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 3D IN THE CABIN WAS INOPERATIVE. MX FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYS.Apr 13, 2013 · N929DL · Doug MD88 · Light System WiringSDR DALA1236480929Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW 24 ABCDE IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.Jun 11, 2012 · N929DL · Doug MD88 · Emergency LightingSDR DALA1228760929Mechanism · out of limitsAIRCRAFT FAILED STEP 7 OF THE TAILCONE RELEASE SYSTEM OPERATIONAL CHECK. THE RELEASE MECHANISM CAM EXCEEDED THE ALLOWABLE TORQUE LIMIT. THE SYSTEM WAS CLEANED, LUBRICATED, AND THE SPRING TENSION ADJUSTED PER MANUAL. THE RII STEPS WERE COMPLETED AND SIGNED OApr 21, 2012 · N929DL · Doug MD88 · Aerodynamic FairingsSDR DALA1228750929Release Cable · wornCHECK FAILED STEP 21 OF THE TAILCONE RELEASE SYSTEM OPERATIONAL CHECK. THE EXTERIOR RELEASE CABLE WAS OUT OF ALLOWABLE LIMITS AT THE CLAMP TO THE INTERNAL RELEASE CABLE. THE CLAMP ON THE CABLE WAS ADJUSTED AND THE SYSTEM WAS RIGGED BACK INTO SPECIFICATIONS. Apr 21, 2012 · N929DL · Doug MD88 · Aerodynamic FairingsSDR DALA1228740929Tail Cone · out of limitsAIRCRAFT FAILED THE FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM, DUE TO THE GAP BETWEEN PIN AND ROD WAS BEYOND ALLOWABLE LIMITS. THE PIN WAS ADJUSTED AND BROUGHT WITHIN LIMITS AND THE RII COMPLETED.Apr 21, 2012 · N929DL · Doug MD88 · Aerodynamic FairingsSDR DALA1200910929Cusp Web · damagedHIDDEN DAMAGE ELONGATED HOLES ON CUSP ANGLE STRAP BELOW PREVIOUS REPAIR. CUSP ANGLE WAS REPLACED PER ERA 498181-14 REV ORIGINAL.Jan 6, 2012 · N929DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA1170870929Skin · corrodedDURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN PREVIOUS REPAIR TRIPLER AT WING FILLET PANELS RUBSTRIP SETTLEMENT AREA STA Y=757-775 BETWEEN LONGERON 26RT-23RT. REF SRM 53-04D FIG 53 FOR REPAIR.Dec 24, 2011 · N929DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA1170920929Skin · damagedDURING HMV ELONGATED HOLES WERE FOUND ON VERTICAL STAB LEADING EDGE PREVIOUS REPAIR DOUBLER AND REPAIR STRAP STA ZFS=52.Dec 24, 2011 · N929DL · Doug MD88 · Vertical Stabilizer, Plate/SkinSDR DALA1170880929Finger Doubler · corrodedDURING HMV CORROSION WAS FOUND ON PRODUCTION FINGER DOUBLERS FROM STA Y=229-250 LONGERON 26RH, ALSO FROM STA Y=229-265 26LT REF SRM 53-04D FIG 12C FOR REPAIR.Dec 24, 2011 · N929DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA1170930929Skin · damagedDURING HMV ELONGATED REPAIR BUSHINGS WERE FOUND ON VERTICAL STAB REMOVABLE LEADING EDGE REPAIRED SKIN STA ZFS=52-55. WILL BE REPAIRED WITH ERA CLASSIFIED MAJOR.Dec 24, 2011 · N929DL · Doug MD88 · Vertical Stabilizer, Plate/SkinSDR DALA1170910929Strap · damagedDURING HMV ELONGATED HOLES AND CORROSION WERE FOUND ON VERTICAL STAB REMOVABLE LEADING EDGE PREVIOUS REPAIR EXTERNAL SPLICE STRAP STA ZFS=57. WILL BE REPAIED WITH AN ERA CLASSIFIED MAJOR.Dec 24, 2011 · N929DL · Doug MD88 · Vertical Stabilizer Miscellaneous StructureSDR DALA1170900929Doubler · damagedDURING HMV ELONGATED HOLES WERE FOUND ON VERTICAL STAB REMOVABLE LEADING EDGE PREVIOUS EXTERNAL REPAIR DOUBLER STA ZFS=53. REPAIRED WITH AN ERA CLASSIFIED MAJOR.Dec 24, 2011 · N929DL · Doug MD88 · Vertical Stabilizer, Plate/SkinSDR DALA1170890929Doubler · damagedDURING HMV ELONGATED HOLES WERE FOUND ON VERTICAL STAB LEADING EDGE PREVIOUS REPAIR EXTERNAL DOUBLER AND SKIN STA ZFS=50-52. WILL BE A ERA REPAIR CLASSIFIED MAJOR.Dec 24, 2011 · N929DL · Doug MD88 · Vertical Stabilizer, Plate/SkinSDR DALA1200580929Fitting · damagedHIDDEN DAMAGE ELONGATED HOLES ON FRAME CLIP STA 218 BTW LONGERONS 18-19 LT. REPAIRS WERE COMPLETED PER ERA 498181-14 REV ORG.Dec 22, 2011 · N929DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA1200140929Skin · corrodedCORROSION ON FUSELAGE SKIN RUB STRIP AREA STA 1079-1080. REPAIR ACCOMPLISHED IAW SRM 53-04D FIG 53.Dec 16, 2011 · N929DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA1200020929Rub Strip · corrodedCORROSION FUSE SKIN RUB STRIP AREA STA 1102-1106. DOUBLER REPAIR INSTALLED IAW DC9/MD80 SRM 53-04D FIG 53.Dec 16, 2011 · N929DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA1171470929Skin · corrodedCORROSION ON FUSELAGE SKIN BELOW RUB STRIP STA 1105. DOUBLER REPAIR WAS INSTALLED IAW DC9/MD80 SRM 53-04 FIG 53.Dec 16, 2011 · N929DL · Doug MD88 · Fuselage Main, Plate/Skin
Back to N929DL, cancelled Mar 19, 2019