N955DL, cancelled Apr 25, 2022

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 = 'N955DL' AND deregistration_id = 'N955DL-2022-04-25'
  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 DALA2019080604590Turbine · damagedRETURNED TO DEPARTURE FOR ENGINE FAILURE. CREW REPORTED AT 3800' HEARD A COMPRESSOR STALL AND RIGHT ENGINE PARAMETERS ROLLED BACK AND EGT CLIMBED. FOLLOWED THE QRH AND SHUT DOWN THE RIGHT ENGINE. EMERGENCY DECLARED. MAINTENANCE FOUND TURBINE DAMAGE AND THE RIGAug 5, 2019 · N955DL · Doug MD88 · Turbine SectionSDR DALA2019070303994Door · damagedE/E DOOR HAS 9 1/2" CREASE IN IT. RT EDGE OFF DOOR IS CATCHING AIRCRAFT SKIN WHEN OPENING AND CLOSING. R/R E/E DOOR PER AMM 52-43. NO DAMAGE ON AIRCRAFT SKIN. (LP5926825)Jul 3, 2019 · N955DL · Doug MD88 · Electrical/Electronic Compartment DoorsSDR DALA2019040302117Battery Pack · inoperativeFWD OVERWING EXIT LIGHT ABOVE LT TRT OVERWING EXITS INOP. REPLACED BATTERIES FOR THE FWD OVER EXIT SIGNS PER MD88 AMM 35-53. CKS GOOD. (LP5797649)Apr 3, 2019 · N955DL · Doug MD88 · Emergency LightingSDR DALA2019030601487Connector · defective16D EMERGENCY LIGHT INOP. R/R LIGHT CONNECTOR AT 16D PER SWPM 20-31. OPS CHECK GOOD OK FOR SVC. R/R LIGHT CONNECTOR AT 16D PER SWPM 20-31. OPS CHECK GOOD OK FOR SVC. (LP5741945)Mar 6, 2019 · N955DL · Doug MD88 · Light System WiringSDR DALA2019010700054Fitting · crackedLWR LEFT FRAME CLIP CRACKED 7:00 POSITION CANTED FRAME 1510. R/R DAMAGE CLIP. (LP0892190)Jan 5, 2019 · N955DL · Doug MD88 · Fuselage Main, FrameSDR DALA2019010700053Frame · crackedAFT FRAME 1510 NALIGHMENT PIN HOLES CRACKED/MISSING MATERIAL LWR RIGHT FRAME 4 PLACES 5:30, 5:00, 3:30, 2:30. REMOVED BOTTOM LOWER RIGHT FRAME, DRILLED AND BEGAN INSTALLATION OF NEW FRAME PER BAC DWG 5966769 FINISHED INSTALL OF FRAME PER BAC DWG 5966769. (LP08Jan 5, 2019 · N955DL · Doug MD88 · Fuselage Main, FrameSDR DALA2019010700052Frame · crackedUPPER FRAME POWERPACK MOUNT CANTED FRAME CRACKED LWR I/B BOLT 2 OCLOCK POSITION FRAME 1510. REMOVED DAMAGE UPPER CANTED FRAME AT STA 1510. DRILLED UP NEW CANTED FRAME PER BAC DWG 5966768 INSTALLED CANTED FRAME PER BAC DWG 5966768. (LP0892161)Jan 5, 2019 · N955DL · Doug MD88 · Fuselage Main, FrameSDR DALA2019010300017Battery · dischargedAFT OVER WING EXIT SIGN LIGHTS ON BOTH LEFT AND RIGHT SIDE ARE INOP. FOUND NO VOLTAGE AT BATTERY PACK IN OVERHEAD BIN 25E,D. REPLACED BATTERY IN BATTERY PACK. PER AMM 33-53. BOTH LEFT AND RIGHT EXIT SIGNS WORK GOOD. LP5057498)Jan 3, 2019 · N955DL · Doug MD88 · Emergency LightingSDR DALA2018110106378Skin · corrodedFUSELAGE/SKIN/STA 464 / BETWEEN L-29L AND L-30 / CORROSION. ER/A 561921-14 REV B - PERMANENT REPAIR RESTRICTION = REPAIR MUST BE REACCOMPLISHED PER SECTION II. INSTRUCTIONS NOT MORE THAN 24 MONTHS OF SERVICE AFTER SECTION I REPAIR. APPROVAL IS LIMITED TO 24 MOOct 30, 2018 · N955DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2018082205194Slide · low pressureFOUND L2 DOOR SLIDE PRESSURE WAS BELOW LIMITS. REMOVED AND REPLACED THE SLIDE IAW WORK CARD 2561-4002, AND AMDS 2561-4002 440684.Aug 21, 2018 · N955DL · Doug MD88 · Escape SlideSDR DALA2018031701738Channel · crackedRT FWD MLG WELL CHANNEL CRACKED FOUND ON SVC CHECK. FND CRACKS IN RT WHEEL WELL 1", 3.5" &3" CORNER CHANNEL BY SERVICING DOOR. REF TOP PARA XB2- ENGINEERING HAS EVALUATED & FINDS ACCEPTABLE FOR FERRY FLIGHT, PER ENGINEERING STOPPED DRILLED CRACKED. A/C TO FERMar 17, 2018 · N955DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2018021600964Battery Pack · inoperativeCEILING EMERGENCY LIGHTS ROWS 22 TO 26 INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK B5104 IAW AMM 33-53.Feb 16, 2018 · N955DL · Doug MD88 · Emergency LightingSDR DALA2017092307055Skin · damagedPER MAINTENANCE REQUEST FOUND SKIN DAMAGE AT LONGERON 30 AND STATION 465 IN FRONT OF THE VHF ANTENNA. SEVERAL RIVET HEADS ARE MISSING. AREA LOOKS LIKE LIGHTNING STRIKE. C/W PRI 561921-14 REV O MATCHES ERA 561921-14.Sep 22, 2017 · N955DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2018110106376Skin · not reportedPER ERA 561921-14 DTE IS REQUIRED ON THE FUSELAGE SKIN AT FS 464 BETWEEN L-30 AND L29L DUE TO A SKIN REPAIR. REF LOG PAGE 0807279 FOR ERA561921-14 REV B TRACKING. LOGPAGE TERMINATED, PERMANENT REPAIR REQUIRED ON DIFFERENT LOGPAGE PER ER/A 561921-14 REV B. (LP0Sep 20, 2017 · N955DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2017021701325Coffeemaker · smokeNR 2 COFFEEMAKER SMOKING WHEN ON, BUT NOT BREWING; TURNED OFF, SMOKE STOPPED. REPLACED THE COFFEEMAKER.Feb 16, 2017 · N955DL · Doug MD88 · Buffet/GalleysSDR DALA2017013100763Actuator · failedON APPROACH INTO BHM WHEN GEAR SELECTED DOWN, THE NLG FAILED TO EXTEND. CREW ACCOMPLISHED QRH PROCEDURE AND PERFORMED AN ALTERNATE GEAR EXTENSION. NLG EXTENDED NORMALLY WITH GREEN DOWN/LOCKED INDICATION, CREW STOWED ALTERNATE EXTENSION LEVEL AND LANDED NORMALLJan 30, 2017 · N955DL · Doug MD88 · Landing Gear ActuatorSDR DALA2016071805385Intercostal · crackedINTERCOSTAL FOUND CRACKED 2 OCLOCK POSITION. REMOVED INTERCOSTAL AND ATTATCHING PARTS. DRILLED UP NEW INTERCOSTAL IAW DWG 9911875. INSTALLED IAW DWG 9911875.Jul 17, 2016 · N955DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA2015110306654Light · 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.Nov 3, 2015 · N955DL · Doug MD88 · Emergency LightingSDR DALA2015091605669Skin · crackedACFT HAS SKIN PROTRUDING AND CRACKED AT BS 241, STRINGER 29L. REPAIRED IAW PRI 539193-14, REV 7.Sep 15, 2015 · N955DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2015091605668Structure · crackedAFT LT EMPENNAGE, JUST ABOVE NR 1 PYLON. PACK EXIT FLANGE IS CRACKED. REPAIRED IAW ERA 539229-14, REV ORIGINAL.Sep 15, 2015 · N955DL · Doug MD88 · Empennage StructureSDR DALA2015091405613Skin · corrodedSKIN HAS AN AREA OF CORROSION, BS 578, STRINGER 29L. REPAIRED IAW SRM 53-04, FIG 12C, VIEW H.Sep 13, 2015 · N955DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2016091209445Skin · damagedMTC REPORTED CORROSION, CRACKED SKIN, AND THREE PLUGS UNDER THE TCAS ANTENNA DOUBLER LOCATED BETWEEN FS 229-255 AND L-28L TO L-29R. ER/A 539193-14 WAS ISSUED TO REPAIR THE DAMAGE.Sep 12, 2015 · N955DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA2015091405616Skin · corrodedBELLY SKIN BULGED, FASTENERS PULLED THROUGH BS 555 STRINGER 29R. REPAIRED IAW SRM 53-04, FIG 12C.Sep 12, 2015 · N955DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA13055560955Door Frame · corrodedCORROSION ON FWD & AFT CARGO BAY DOOR FRAME BEAM. CORROSION REMOVED IAW SRM 51-10-3, PAR 26A. FOUND OUT OF LIMITS IAW SRM 53-05, FIG 123A. REPAIRED IAW ER/A 519124-14, REV ORIGINAL. REPAIR INSPECTED IAW ER/A 5109124-14 RE, ORIG AND SRM 53-05, FIG 123A.Oct 27, 2013 · N955DL · Doug MD88 · Fuselage Main, StructureSDR DALA13055540955Tee Fitting · damagedSCRATCHES ON TEE ANGLE OF PRESSURE DOME LOWER AREA Y=1338 X=25 TO 23, X=6 TO 4, X=-35 TO 33. DAMAGED TEE SECTION AND STRUCTURE PARTS WERE REMOVED IAW SRM 53-03, FIG 37. NEW TEE SECTION FABRICATED AND INSTALLED IAW SRM 53-03, FIG 37, 51-30-2 AND 51-30-5.Oct 24, 2013 · N955DL · Doug MD88 · Fuselage Main, BulkheadSDR DALA13053890955Finger Doubler · damagedDAMAGE ON FINGER DOUBLER FASTENER PROTUDING LOWER AFT CORNER, BS 617, S20-21R. DOUBLER WAS REPLACED IAW ER/A 239715-14, REV D.Oct 20, 2013 · N955DL · Doug MD88 · Wing, Plate/SkinSDR DALA13053450955Skin · damagedCORROSION ON FUSELAGE SKIN BELOW FILLET PANEL RUBSTRIP AREA ON BS 807 BETWEEN LONGERONS 28-29R. SKIN REPAIRED IAW SRM 53-04, FIG 57, 51-30-5, 51-30-1.Oct 18, 2013 · N955DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA13053310955Tab · damagedLIGHTING STRIKE ON T/E CONTROL TAB. REPAIRED IAW SRM 55-04 PH3.Oct 17, 2013 · N955DL · Doug MD88 · Elevator StructureSDR DALA13053330955Skin · damagedDAMAGED METALLIZED SURFACE ON RUDDER. REPAIRED IAW SRM 51-70-IA.Oct 16, 2013 · N955DL · Doug MD88 · Rudder, Plate/SkinSDR DALA13053320955Longeron · corrodedCORROSION ON LONGERON 26L BETWEEN, BS 1287 AND 1309, AFT CARGO BAY. CORROSION REMOVED, OUT OF LIMITS. LONGERON REMOVED AND NEW LONGERON SECTION INSTALLED IAW SRM 51-10-3 PAR. 26-21-14 53-02 FIG. 18.Oct 16, 2013 · N955DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA13052650955Structure · corrodedDURING SCHEDULED CHECK, CORROSION WAS FOUND ON PREVIOUS REPAIR DOUBLERS BETWEEN BS 731 & 750 IN THE CABIN FLOOR STRUCTURE. DOUBLERS WERE REMOVED AND NEW REPAIR DOUBLERS INSTALLED IAW SRM 53-05, FIGURE 131A.Oct 14, 2013 · N955DL · Doug MD88 · Fuselage Main, StructureSDR DALA13052660955Doubler · corrodedDURING SCHEDULED HEAVY CHECK, CORROSION WAS NOTED AT ALL 4 RADIO ALTIMETER TO SKIN FAYING SURFACES. CORROSION WAS REMOVED AND NEW DOUBLERS WERE INSTALLED IAW SRM 51-30-2 AND 51-10-3.Oct 13, 2013 · N955DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA13052430955Seat Track · corrodedCORROSION ON RT SEAT TRACK, X=-54, STA Y=480-482 AT CABIN FLOOR STRUCTURE. REPAIRED PLUG, INSTALLED PLUG IAW SRM 53-05, FIG 4A.Oct 11, 2013 · N955DL · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13052440955Seat Track · corrodedCORROSION ON LT SEAT TRACK X=54 BETWEEN STA Y=423-425 AT CABIN FLOOR STRUCTURE. DAMAGE WAS REMOVED AND REPAIR PLUG WAS INSTALLED IAW SRM 53-05, FIG 4A.Oct 10, 2013 · N955DL · Doug MD88 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13051820955Frame · corrodedCORROSION ON FRAME AT STA Y=127 AND BETWEEN LONGERONS 17 AND 18R COCKPIT STRUCTURE. FRAME WAS REPLACED IAW SRM 51-30-5 , 51-30-2 AND DWG 9911511, REV "B".Oct 10, 2013 · N955DL · Doug MD88 · Fuselage Main, FrameSDR DALA13051800955Access Panel · corrodedCORROSION ON ACCESS PLATE NR 1464C AND SCREW HOLES OF RT MAIN FUEL TANK. REPLACED PLATE 1464C IAW SRM 51-22-2A.Oct 10, 2013 · N955DL · Doug MD88 · Wing, Plate/SkinSDR DALA13051790955Access Panel · corrodedCORROSION ON ACCESS PLATE NR 1462C AND SCREW HOLES OF RT MAIN FUEL TANK. ACCESS PLATE NR 1462C. REPLACED IAW SRM 51-22-2A.Oct 10, 2013 · N955DL · Doug MD88 · Wing, Plate/SkinSDR DALA13051740955Longeron · crackedCRACKED LONGERON 12L AT BS 1437. REPAIRED IAW SRM 53-02, FIG 18.Oct 10, 2013 · N955DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA13053920955Skin · corrodedCORROSION ON FUSELAGE SKIN BENEATH RUBSTRIP FROM BS 769 TO 771 AND BETWEEN LONGERONS 27-28R . REPAIR DOUBLER WAS FABRICATED AND REPAIR WASHERS, AND REPAIR DOUBLER WERE INSTALLED IAW SRM 53-0 4 FIG. 57.Oct 9, 2013 · N955DL · Doug MD88 · Fuselage Main, Plate/SkinSDR DALA13051430955Door Frame · crackedCRACK ON INTERNAL DOUBLER AT THE LOWER AFT DOOR FRAME CORNER, BS 423.5 BETWEEN LONGERONS 27-28R AT THE FWD CARGO BAY. FASTENERS WERE REMOVED AND DAMAGE REMOVED IAW SRM 51-30-2 AND 51-30-5 AND 53-05, FIG 105. DOUBLERS AND FILLERS WERE FABRICATED IAW SRM 53-05Oct 9, 2013 · N955DL · Doug MD88 · Fuselage Main, StructureSDR DALA13051410955Bushing · damagedELONGATED BUSHINGS TO ATTACH RT HEATER BLANKET AFT EDGE NR 3,4,5, AND 9 AT RT WING. BUSHINGS TO ATTACH RT HEATER BLANKET AFT EDGE NR 3,4,5, AND 9 AT RT WING WERE R & R IAW EA 09-070683-03, AD REV L AND SRM 51-30-10; RII COMPLETED.Oct 8, 2013 · N955DL · Doug MD88 · Wing Miscellaneous StructureSDR DALA13050170955Frame · corrodedCORROSION ON FRAME BS 1380 FROM X=-25 TO X=25. FRAME REPLACED IAW SRM 51-30-2 AND 51-30-5, DWG 9912246, REV CE.Oct 6, 2013 · N955DL · Doug MD88 · Fuselage Main, FrameSDR DALA13050140955Longeron · crackedCRACK LONGERON 10R, BS 1431, SECTION OF LONGERON DAMAGE WAS REMOVED. NEW SECTION AND SPLICE INSTALLED IAW SRM 53-02, FIG 18, 51-30-2, 51-30-5, 51-20-0.Oct 6, 2013 · N955DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA13049500955Skin · wornWORN PREVIOUS REPAIR DOUBLER ON L/E STA XFS=110 RT WING. PREVIOUS REPAIR REMOVED, NEW DOUBLER WAS FABRICATED, TREATED, PAINTED, INSTALLED AND IDENTIFIED IAW ER/A N 378819-14, REV A.Oct 3, 2013 · N955DL · Doug MD88 · Wing, Plate/SkinSDR DALA13049080955Cusp Web · corrodedCORROSION ON LT CUSP WEB UPPER AND LOWER SURFACE BETWEEN STA Y=1003 TO Y=1022 AND BETWEEN X=54 TO X=60 AT PAX CABIN. DAMAGE WAS REMOVED, REPAIR PARTS WERE FABRICATED, TREATED, PAINTED, INSTALLED, IDENTIFIED, AND CIC WAS APLICATED IAW SRM 53-05 FIG 131A, 51-10Oct 2, 2013 · N955DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA13049070955Cusp Web · corrodedCORROSION ON LT CUSP WEB UPPER AND LOWER SURFACE BETWEEN STA Y=1022 TO 1041 AND BETWEEN X=54 TO X=60 AT PAX CABIN REF NRC (T0 294284) OR NC 193 ZONE 58, REF (T0 295304). DAMAGE WAS REMOVED IAW SRM 53-05, FIG 131A. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIGOct 2, 2013 · N955DL · Doug MD88 · Fuselage Miscellaneous StructureSDR DALA13048820955Longeron · crackedCRACK ON LONGERON 2LT AT BS 160. SECTION OF LONGERON WAS REMOVED AND NEW SECTION LONGERON AND SPLICE WERE INSTALLED IAW SRM 53-02, FIG 18.Oct 1, 2013 · N955DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA13055550955Longeron · corrodedCORROSION ON LONGERON 23LT FROM BS 1271 - 1322 IN AFT CARGO BAY LT TUNNEL. CORROSION REMOVED. REWORKED AREA FOUND OUT OF LIMITS IAW SRM 53-01, FIG 1., DAMAGE LONGERON SECTION REMOVED, AND A NEW SECTION LONGERON INSTALLED.Sep 26, 2013 · N955DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA13053860955Longeron · wornWORN LONGERON 19 LEFT BS 1375 . DAMAGE BLENDED AND LONGERON SECTION REMOVED. NEW SECTION INSTALLED IAW SRM 53-01, FIG 1, 51-30-2, 51-30-5,53-02, FIG 18, 51-10-3 PAR 21 AND 14, AND PS 900-5-1.Sep 24, 2013 · N955DL · Doug MD88 · Fuselage Main, Longeron/StringerSDR DALA13057730955Skin · crackedCRACKS FOUND ON FUSELAGE SKIN BS 1418 BETWEEN LONGERONS 2-3L. REPAIRED IAW ER/A 519129-14AD REV. ORIG.Sep 17, 2013 · N955DL · Doug MD88 · Fuselage Main, Plate/Skin
Back to N955DL, cancelled Apr 25, 2022