N938AT

Service difficulty reports · 150

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 = 'N938AT' AND registry_match = 'registration'
  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 DALA2019110406425Cover · missingTHE CABIN CEILING EMERGENCY EXIT LIGHT IS MISSING AT ROW 22AB. FORWARDED TO MEL 33-51-01A AND THE PLACARD WAS INSTALLED. 06NOV19 LGA INSTALLED EMERGENCY EXIT LIGHT COVER AT ROW 22AB AS PER B717 AMM 33-51. CHECKS OK. MEL AND PLACARD REMOVED. (LP #5955947)Nov 4, 2019 · N938AT · Boeing 717200 · Emergency LightingSDR DALA2019101875974Door · missingPNEUMATIC AIR GROUND CONNECT DOOR MISSING. REPLACED BROKEN HINGE ON GROUND AIR DOOR PER AMM 52-47, REINSTALLED DOOR. (LP5416466)Oct 14, 2019 · N938AT · Boeing 717200 · Service DoorsSDR DALA2018052103461Power Supply · inoperativeLEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY EXIT LIGHT POWER SUPPLY IAW AMM 33-51. OPS CHECKED GOOD.May 21, 2018 · N938AT · Boeing 717200 · Emergency LightingSDR DALA2018031001598Fastener · shearedSHEARED FASTENER ON LONGERON 2L, BS 1153 AT AFT ACCESSORY. REPAIRED IAW ER/A 566637-14, REV ORIGINAL, AND ETI-17-18-044 REV 1.Mar 9, 2018 · N938AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018030901832Tab · dentedTHE RUDER CONTROL TAB WAS DENTED ON TRAILING EDGE UPPER SECTION. THE RUDDER CONTROL TAB TRAILING EDGE UPPER SECTION WAS REPAIRED PER SRM 51-70-02-0G.Mar 8, 2018 · N938AT · Boeing 717200 · Rudder, Tab StructureSDR DALA2018030801486Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 520GB. CORROSION LEVEL 2, DUE TO EXCESSIVE DAMAGE BY CORROSION ON FUEL ACCESS PLATE 520GB WAS REPLACED PER SRM 57-10-01 REPAIR 2 PAR 5 CONDITION II (A AND B) AND VERIFIED PER IPC 57-23-01Mar 7, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018030801484Beam · crackedCRACKED BEAM 1 STA Y=170 AT FWD SERVICE DOOR. BEAM 1 WAS REPLACED PER SRM 51-41-02-0G AND DWG 9911579 REV L.Mar 7, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030801473Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 520CB. CORROSION LEVEL 2, DUE TO EXCESSIVE DAMAGE BY CORROSION FUEL ACCESS PLATE 520CB WAS REPLACED AND VERIFIED PER IPC 57-23-01-01 ITEM 465J.Mar 7, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018030701457Access Panel · crackedA CRACK WAS CONFIRMED IAW NDTSPM PART 6, 06-10-01.001 ON ACCESS PANEL 620EB, RT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00. A LEAK CHECK WAS PERFORMED IAW AMM 28-00-00. NO LEAKS FOUND.Mar 7, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018030701455Skin · crackedCRACKED SKIN, BS 1087, BETWEEN LONGERONS 13 AND 14R. REPAIRED THE SKIN IAW ER/A 566384-14, REV ORIGINAL, AND ETI-17-014, REV 1.Mar 6, 2018 · N938AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018030601400Frame · crackedCRACK ON FRAME STA Y=1022 LONG 7R AT PASSENGER CABIN. DAMAGE AREA WAS REPAIRED PER ER/A 566385-14 REV ORIGINAL AND ETI-17-18-015 REV ORIGINAL. HFEC INSPECTION WAS ACCOMPLISHED ON FRAME STA Y=1022 LONG 7R AT PASSENGER CABIN AND 2EA CRACKS WERE DELIMITED WITH FOMar 5, 2018 · N938AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018030601397Skin · corrodedCORROSION ON CENTER FUEL TANK LOWER SKIN STA Y=747 X=-23 AT RT WHEEL WELL. CORROSION LEVEL 2, CORROSION WAS REWORKED PER ER/A 566336-14AD REV ORIGINAL AND ETI-17-18-018 REV 1. PER ER/A 566336-14AD REV ORIGINAL SECTION DTE.Mar 5, 2018 · N938AT · Boeing 717200 · Fuel StorageSDR DALA2018030501388Fitting · crackedCRACKED INTERNAL FITTING STA Y=994 BEAM 4, ALSO INTERNAL FITTING Y=954 BEAM 2 AT AFT CARGO COMPARTMENT DOOR. FITTINGS STA Y=994 AND Y=954 WERE REPLACED PER SRM 51-41-01-0G, 51-41-05-0G, AND DWG 9957665 REV R.Mar 4, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030301381Floor Support · corrodedCORROSION ON THE FLOOR SUPPORT. THE FLOOR SUPPORT WAS REPLACED IAW DWG #9957828, REV Y.Mar 2, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030301380Pan · corrodedCORROSION ON LOWER PAN OF THE LOWER DOOR FRAME IN THE AFT CARGO BAY, THE PAN WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND SRM 53-20-15-2R-7.Mar 2, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030101293Beam · crackedCRACK ON INNER PAN IN BEAM NR 1 STA Y=427 AT FWD CARGO COMPARTMENT DOOR (PTAS). INNER PAN IN BEAM NR 1 STA Y=427 WAS REPAIRED PER SRM 52-30-02-2R-1 FIG 201.Feb 28, 2018 · N938AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018030101292Beam · crackedCRACK ON INNER PAN IN BEAM NR 3 STA Y=370 AT FWD CARGO COMPARTMENT DOOR (PTAS). INNER PAN IN BEAM NR 3 STA Y=370 WAS REPAIRED PER SRM 52-30-02-2R-1 FIG 201.Feb 28, 2018 · N938AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018030101291Membrane · crackedCRACK ON MEMBRANE STA Y=674 X=-54 AT PASSENGER CABIN. DAMAGE AREA WAS REPAIRED PER SRM 53-00-55-2R FIG 223 (ET) HFEC INSPECTION WAS ACCOMPLISHED ON MEMBRANE STA Y=674 X=-54 AT PASSENGER CABIN AND NO CRACKS WERE FOUND AFTER TRIM OUT PER NDT SPM 06-10-01.001. EQFeb 28, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030101290Tee Fitting · crackedCRACK ON INTERNAL FITTING "T" STA Y=389 (LOWER EDGE) AT FWD CARGO COMPARTMENT DOOR (PTAS). FITTING "T" STA Y=389 WAS REPLACED PER SRM 51-41-01, 51-41-02, 51-41-05, AND DWG 3926046 REV D.Feb 28, 2018 · N938AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018030101289Beam · crackedCRACK ON INNER PAN IN BEAM NR 5 STA Y=427 AT FWD CARGO COMPARTMENT DOOR (PTAS). PAN IN BEAM NR 5 STA Y=427 WAS REPAIRED PER SRM 52-30-02-2R-1 FIG 201.Feb 28, 2018 · N938AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018030101288Beam · crackedCRACK ON INNER PAN IN BEAM NR 5 STA Y=370 AT FWD CARGO COMPARTMENT DOOR (PTAS). PAN IN BEAM NR 5 STA Y=370 WAS REPAIRED PER SRM 52-30-02-2R-1 FIG 201.Feb 28, 2018 · N938AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018030101287Beam · crackedCRACK ON INNER PAN IN BEAM NR 1 STA Y=370 AT FWD CARGO COMPARTMENT DOOR (PTAS). PAN IN BEAM NR 1 STA Y=370 WAS REPAIRED PER SRM 52-30-02-2R-1 FIG 201.Feb 28, 2018 · N938AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018022801273Floor Panel · crackedCRACKED CHANNELS ON FLOOR PANELS #221XF, 221TF, 222AFF, AND 222AJF AT PAX CABIN (CPAX). NRC 00438: CRACKED CHANNELS ON FLOOR PANELS #221XF, 221TF, 222AFF AT PAX CABIN WERE REPAIRED PER B717 SRM 53-00-00-1A FIG 101. AND CRACKED CHANNEL ON FLOOR PANEL 222AJF WAFeb 27, 2018 · N938AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2018022701202Cusp Web · corrodedCORROSION ON CUSP WEB BS 487 - 491, BETWEEN RBL 54 TO RBL 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 215.Feb 26, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018022701201Door Frame · crackedCRACKS FOUND ON THE LT & RT DOOR FRAME BS 46 AT NLG WHEEL WELL. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14 R2, FIG 201. HFEC INSPECTION WAS ACCOMPLISHED, AND NO CRACKS WERE FOUND AFTER CUT OUT IAW NDT SPM 06-10-01.001.Feb 26, 2018 · N938AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022601168Floor Panel · damagedPUNCTURED AND BROKEN ON FLOOR PANELS 211AQF, 211ALF, 221AF, 221BF, 221CF, 221EF, 221JF, AND 222PF AT PAX CABIN / COCKPIT. NRC 00473: FERRULES DAMAGES ON FLOOR PANEL 221EF, 222PF, 221BF, 221AF, AND 221JF WERE REPLACED PER B-717 SRM 53-20-50-2R PROCEDURE 3. FLOOFeb 25, 2018 · N938AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2018022601167Intercostal · crackedCRACKED INTERCOSTAL IN X=O BTW STA Y=1002-1022 AT PAX CABIN. INTERCOSTAL IN X=O BTW STA Y=1002-1022 AT PAX CABIN WAS REPLACED PER SRM 51-41-02-0G AND SRM 51-41-05-0G.Feb 25, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018022601166Fitting · crackedCRACK FRAME CLIPS BTW LONG 13L AND 14L STA Y=1022 AND LONG 13R TO 14R. FRAME CLIP REPLACED PER DWG 9912243 REV HG. HFEC INSPECTION WAS ACCOMPLISHED ON FRAME CLIPS BTW LONG 13L AND 14L AND LONG 13R TO 14R STA Y=1022. CRACK OF 0.375" LENGTH ON FRAME CLIP BTW LONFeb 25, 2018 · N938AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018022601165Floor Panel · brokenBROKEN FLOOR PANEL NR 211ANF OF COCKPIT. FLOOR PANEL 211ANF WAS FABRICATED, REPLACED. AND IDENTIFIED PER SRM 53-20-50-2R PROCEDURE 3. AND WAS INSTALLED WITH THE CARD JIC 2040-0058.Feb 25, 2018 · N938AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2018022601164Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 620CT. CORROSION LEVEL 2, FUEL ACCESS PLATE 620CT WAS REPLACED AND VERIFIED PER IPC 57-22-01. INSTALLATION IS ATTENDED WITH CARD 2040-0012.Feb 25, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022601163Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 620DT. CORROSION LEVEL 2, FUEL ACCESS PLATE 620DT WAS REPLACED AND VERIFIED PER IPC 57-23-01. INSTALLATION IS ATTENDED WITH CARD 2040-0012.Feb 25, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022601162Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 520DT. CORROSION LEVEL 2, FUEL ACCESS PLATE 520DT WAS REPLACED AND VERIFIED PER IPC 57-23-01. INSTALLATION IS ATTENDED WITH CARD 2040-0010.Feb 25, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022601161Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 620CB. CORROSION LEVEL 2, FUEL ACCESS PLATE 620CB WAS REPLACED AND VERIFIED PER IPC 57-23-01. INSTALLATION IS ATTENDED WITH CARD 2040-0012.Feb 25, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022601160Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 520CT. CORROSION LEVEL 2, FUEL ACCESS PLATE 520CT WAS REPLACED AND VERIFIED PER IPC 57-22-01. INSTALLATION IS ATTENDED WITH CARD 2040-0010.Feb 25, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022701263Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PANEL 520HB. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01, REPAIR 2, PAR. 5, CONDITION II.Feb 24, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022701262Floorbeam · corrodedCORROSION ON THE FLOORBEAM ANGLE BS 200 BETWEEN RBL 22 TO 44 AND BTW RBL 44 TO 56. THE FLOORBEAM ANGLE WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.Feb 24, 2018 · N938AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2018022501159Rib · crackedCRACK ON SLAT NR 5 CORNER EXTERNAL LOWER SIDE STA XW 536.861 APPROX AT LT WING. CRACKED RIB ON SLAT NR 5 WAS REPLACED PER SRM 51-41-02 AND 51-41-08.Feb 24, 2018 · N938AT · Boeing 717200 · Leading Edge DevicesSDR DALA2018022501158Former · crackedCRACKED FORMER LT/RT SIDE STA Y=694 AT CANTED KEEL INTERNAL STRUCTURE. FORMER LT/RT SIDE STA Y=694 AT CANTED KEEL INTERNAL STRUCTURE WAS REPAIRED PER SRM 51-70-11 REPAIR 1.Feb 24, 2018 · N938AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018022501157Former · crackedCRACKED FORMER LT/RT SIDE STA Y=679 AT CANTED KEEL INTERNAL STRUCTURE. FORMER LT/RT SIDE STA Y=679 AT CANTED KEEL INTERNAL STRUCTURE WAS REPAIRED PER SRM 51-70-11 REPAIR 1.Feb 24, 2018 · N938AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018022501156Retainer · wornWEAR ON LOWER RETAINER (FWD AND AFT SECTION) AT FWD CARGO DOOR BARRIER. LOWER RETAINER FWD AND AFT SECTION WAS REPAIRED PER ER/A NR 559579-14MA REV ORIGINAL.Feb 24, 2018 · N938AT · Boeing 717200 · Cargo CompartmentsSDR DALA2018022501155Former · crackedCRACKED FORMER RT SIDE STA Y=715 AT CANTED KEEL INTERNAL STRUCTURE. FORMER RT SIDE STA Y=715 AT CANTED KEEL INTERNAL STRUCTURE WAS REPAIRED PER SRM 51-70-11 REPAIR 1.Feb 24, 2018 · N938AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018022401154Cusp Web · corrodedCORROSION ON CUSP WEB FROM STA Y=515-519 BTW X=-54 TO X=-60 AT PAX CABIN IN REF NRC 00325 (5300-2020). CORROSION LEVEL 2, CUSP WEB FROM STA Y=515-519 BTW X=-54 TO X=-60 AT PAX CABIN WAS REPAIRED PER SRM 53-00-55-2R.Feb 23, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018022401153Cusp Web · corrodedCORROSION ON CUSP WEB FROM STA Y=449-457 BTW X=-54 TO X=-60 AT PAX CABIN IN REF NRC 00324 (5300-2020). CORROSION LEVEL 2, CUSP WEB FROM STA Y=449-457 BTW X=-54 TO X=-60 AT PAX CABIN WAS REPAIRED PER SRM 53-00-55-2R.Feb 23, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018022401152Cusp Web · corrodedCORROSION ON CUSP WEB FROM STA Y=467-475 BTW X=-54 TO X=-60 AT PAX CABIN IN REF NRC 00324 (5300-2020). CORROSION LEVEL 2, CORROSION ON CUSP WEB FROM STA Y=467-475 BTW X=-54 TO X=-60 AT PAX CABIN WAS REPAIRED PER SRM 53-00-55-2R.Feb 23, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018022401151Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 520EB. CORROSION LEVEL 2, DUE TO EXCESSIVE DAMAGE BY CORROSION ON COUNTERSINK AREAS, ACCESS PLATE 520EB WAS REPAIRED PER SRM 57-10-01 REPAIR 2 PAR 5 CONDITION II.Feb 23, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022401150Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 520DB. CORROSION LEVEL 2, FUEL ACCESS PLATE 520DB WAS REPLACED FOR NEW ACCESS PLATE PER SRM 57-10-01 REPAIR 2 PAR 5.Feb 23, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022401149Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 620AT. CORROSION LEVEL 2, FUEL ACCESS PLATE 620AT WAS REPLACED FOR NEW ACCESS PLATE PER SRM 57-10-01 REPAIR 2 PAR 5.Feb 23, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022301148Diaphragm · corrodedCORROSION ON DIAPHRAGM BTW STA Y=200-205 AND BTW X=-40 TO X=-50 AT PAX CABIN IN REF NRTC 00316 (5300-2010). CORROSION LEVEL 2, DIAPHRAGM BTW STA Y=200-205 AND BTW X=-40 TO X=-50 AT PAX CABIN WAS REPAIRED PER SRM 53-00-00-2R FIG 201.Feb 22, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018022301097Longeron · crackedCRACK LONGERON 6R, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.Feb 22, 2018 · N938AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018022301096Pan · crackedCRACK RING PAN ON LWR CORNER BS 889. THE RING PAN WAS REPAIRED IAW SRM 56-20-02-2R, FIG 202.Feb 22, 2018 · N938AT · Boeing 717200 · Fuselage Main, Structure
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