N998AT

Service difficulty reports · 213

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 = 'N998AT' 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 DALA2018022201061Skin · corrodedCORROSION TYPE EXFOLIATION AT CENTER WING TANK UPPER SKIN AT LT MLG WHEEL WELL AREA BELOW SLANT PRESSURE PANELS. THIS NRC WAS ATTENDED WITH ETI-17-18-009 REV 5 AND ER/A 565972-14 REV ORIG. ASSOCIATED ER/A 00-565972.Feb 21, 2018 · N998AT · Boeing 717200 · Fuel StorageSDR DALA2018021800983Skin · crackedCRACK ON THE FUSELAGE SKIN, BS 1037, LONGERONS 13R AND 14R. THE SKIN WAS REPAIRED IAW ETI-17-18-003, REV 4, AND ER/A 565867-14, REV ORIGINAL.Feb 17, 2018 · N998AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018021800982Fitting · crackedCRACK ON FUSELAGE FITTING LONGERON 22R, BS 661. THE FITTING WAS REPAIRED ETI-17-18-004, REV 1, AND ER/A 565939-14, REV ORIGINAL.Feb 17, 2018 · N998AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2018021800981Skin · crackedCRACK ON THE SKIN AT BS 1076 BETWEEN LONGERONS 13L AND 14L. THE SKIN WAS REPAIRED IAW ETI-17-18-002, REV 2 AND ER/A 565871-14, REV ORIGINAL. HFEC INSPECTION WAS PERFORMED THE CRACK WAS FOUND OF 0.110" OF LENGTH IAW NDT SPM 06-10-01.001.Feb 17, 2018 · N998AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018021700980Frame · crackedCRACK OF 0.250 INCH IN LENGTH APROXIMATELY ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT BS 696 RT. THE FRAME WAS REPLACED IAW 5310-01436-03B.Feb 16, 2018 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018021600941Frame · corrodedCORRODED FRAME BS 1037, BETWEEN LONGERONS 28L AND 28R IN THE AFT CARGO COMPARTMENT. THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R, FIG 201.Feb 15, 2018 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018021600940Door · corrodedCORROSION ON LOWER INNER EDGE OF THE FWD AIR STAIRWELL DOOR. THE STAIRWELL DOOR WAS REPLACED IAW AMM 52-63-01.Feb 15, 2018 · N998AT · Boeing 717200 · DoorsSDR DALA2018021500904Frame Angle · crackedCRACKED FRAME ANGLE AT BS 1022, LONGERON 7L. THE FRAME ANGLE WAS REPAIRED IAW ETI-17-18-008, REV 1, AND ER/A 565874-14, REV ORIGINAL.Feb 14, 2018 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018021100860Frame Angle · crackedCRACK ON THE FRAME ANGLE BS 1022, BETWEEN LONGERONS 16L TO 17L. CRACK WAS FOUND TO BE 0.750 INCH IN LENGTH. REPLACED THE FRAME ANGLE IAW DWG 9912243, REV JS, SRM 51-41-02, AND 51-41-05.Feb 10, 2018 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018021600979Grill · corrodedCORROSION ON FRAME GRILL R1. THE FRAME GRILL WAS REPAIRED IAW SRM 53-00-00-2R-1, FIG.201.Feb 9, 2018 · N998AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018021000859Frame Angle · crackedCRACK FOUND ON THE ON THE FRAME ANGLE BS 1022 BETWEEN LONGERONS 13R TO 14R. THE CRACK IS 0.250" LONG. REPAIRED IAW SRM 53-00-06-2R-2, FIG 201.Feb 9, 2018 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018020900791Access Panel · corrodedCORROSION ON THE ACCESS PANEL. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION III.Feb 8, 2018 · N998AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018020900790Rub Strip · corrodedCORRODED RUB STRIP ON THE RT WING. REPLACED THE RUB STRIP IAW SRM 57-10-01-2R, REP 3, PAR 6.Feb 8, 2018 · N998AT · Boeing 717200 · Wing Miscellaneous StructureSDR DALA2018020700729Access Panel · corrodedCORROSION ON THE ACCESS PANEL. REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.Feb 6, 2018 · N998AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018020700728Access Panel · corrodedCORROSION IN THE COUNTERSINK OF THE ACCESS PANEL 520DB. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.Feb 6, 2018 · N998AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018020700727Access Panel · corrodedCORROSION ON THE ACCESS PANEL 520HB. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.Feb 6, 2018 · N998AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018020700726Rub Strip · corrodedCORROSION POINTS ON FUEL ACCESS PANEL RUB STRIP, LT WING. REPLACED IAW SRM 57-10-01.Feb 6, 2018 · N998AT · Boeing 717200 · Wing Miscellaneous StructureSDR DALA2018020700725Cusp Web · crackedCRACKED CUSP WEB, BS 665 TO 684, LBL 44 TO 54. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 222.Feb 6, 2018 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018020500649Access Panel · corrodedCORROSION IN THE COUNTERSINK OF THE ACCESS PANEL 520FT. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5,Feb 4, 2018 · N998AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018020500648Access Panel · corrodedCORROSION ON THE COUNTERSINK OF THE FUEL ACCESS PANEL 620EB. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01, REPAIR 2, PAR 5.Feb 4, 2018 · N998AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018020500647Floor Panel · delaminatedDELAMINATED FLOOR PANEL 211ANF. A NEW FLOOR PANEL WAS FABRICATED, AND INSTALLED IAW SRM 53-20-50-2R-3.Feb 4, 2018 · N998AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2018020400644Pan · crackedCRACK ON RING PAN AFT LOWER CORNER BS 908. THE PAN WAS REPAIRED IAW SRM 56-20-02-2R-1, FIG 202.Feb 3, 2018 · N998AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018020400643Pan · crackedCRACK ON RING PAN FWD LOWER CORNER BS 446 . REPAIRED PER B717 SRM 56-20-02-2R-1 FIG 202 . LONG CRACK 0.100" INCH. (LP #0410120)Feb 3, 2018 · N998AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018020400642Former · crackedCRACKED EGDE FORMER BS 694 IN THE KEEL BEAM AREA. THE FORMER WAS REPAIRED IAW SRM 51-70-11, REP 1.Feb 3, 2018 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018020400641Former · crackedCRACKED RT EGDE FORMER BS 679 AT THE KEEL BEAM AREA REPAIRED IAW SRM 51-70-11, REP 1.Feb 3, 2018 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018020300639Floor Support · corrodedCORROSION ON FLOOR SUPPORTS Y=150 TO 200 X=-44, Y=150 X=-32 TO X=-44 AND Y=150 X=-44 TO X=-50 PAX CABIN IS OUT OF LIMITS (W1) (AMDS 5300-2010). NRC 00453: LEVEL CORROSION 2, FLOOR SUPPORTS Y=150 TO 200 X=-44, Y=150 X=-32 TO X=-44 AND Y=150 X=-44 TO X=-50 WERE Feb 2, 2018 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018020300637Frame · crackedCRACKED NOSE LANDING GEAR WHEEL WELL FRAME. REPAIRED IAW SRM 53-10-14-2R, REP 2, FIGURE 201.Feb 2, 2018 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018020200607Pan · crackedCRACKED PAN 5 BEAM POSITION, ON AFT CUTOUT AT FWD CARGO DOOR INNER STRUCTURE. PAN 5 BEAM POSITION ON AFT CUTOUT AT FWD CARGO DOOR INNER STRUCTURE WAS REPAIRED PER SRM 52-30-02 FIG 201.Feb 1, 2018 · N998AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018020100606Cusp Web · corrodedCORROSION ON CUSP WEB BTW STA Y=465 TO Y=446 AND X=-54 TO X=-60 AT CAB PAX (CPAX). CORROSION LEVEL 2. CUSP WEB BTW STA Y=465 TO Y=446 AND X=-54 TO X=-60 WAS REPAIRED PER SRM 53-00-55-2R-4.Feb 1, 2018 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018020100587Pan · crackedCRACKED PAN NR 5 BEAM POSITION, ON FWD CUTOUT AT FWD CARGO DOOR INNER STRUCTURE. CRACKED PAN NR 5 BEAM POSITION, ON FWD CUTOUT WAS REPAIRED PER SRM 52-30-02-2R REPAIR 1 FIG 201.Jan 31, 2018 · N998AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018013100526Cusp Web · crackedCRACK ON CUSP WEB BTW STA Y=655 TO Y=674 AND X=54 TO X=60 AT CAB PAX (CPAX). CUSP WEB WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 206. HFEC INSPECTION WAS PERFORMED ON CUSP WEB AFT CUT OUT. NO CRACKS WERE FOUND PER NDT SPM 06-10-01.001.Jan 30, 2018 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018013100525Cusp Web · puncturedPUNCTURE ON CUSP WEB STA Y=696 AND X=-54 AT CAB PAX (CPAX). CUSP WEB WAS REPAIRED PER SRM 53-00-55-2-4 FIG 203. (HFEC) WAS ACCOMPLISHED ON CUSP WEB AT CAB PAX, NO CRACKS WERE FOUND AFTER TRIM OUT PER NDTSPM PART 6, 06-10-01.001.Jan 30, 2018 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018013100524Angle · crackedCRACK ON ANGLE AT BEAM 1 AND STA 197 APPROX AT FWD PASSENGER DOOR INT STRUCTURE. BEAM 1 AT FWD PASSENGER DOOR PAN WAS REPAIRED PER SRM 52-10-02-2R PROCEDURE 7 FIG 201.Jan 30, 2018 · N998AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2018013100523Cusp Web · crackedCRACK ON CUSP WEB AT STA Y=256 AND X=-54 AT CAB PAX (CPAX). CUSP WEB WAS REPAIRED PER SRM 53-00-55-2R-4- FIG 221. HFEC WAS ACCOMPLISHED ON CUSP WEB, TRIM OUT AREA WAS FOUND AT STA Y=256 AND X=-49 AT CAB PAX AND NO CRACK INDICATION WAS FOUND PER NDTSPM PART 6. Jan 30, 2018 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018013100522Beam · crackedCRACKED PAN 3 BEAM POSITION, ON FWD CUTOUT AT FWD CARGO DOOR INNER STRUCTURE (PTAS). CRACKED PAN #3 BEAM POSITION, ON FWD CUTOUT AT FWD CARGO DOOR INNER STRUCTURE WAS REPAIRED PER SRM 52-30-02-2R REPAIR 1 FIG 201.Jan 30, 2018 · N998AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018013100521Intercostal · crackedCRACK ON INTERCOSTAL BTW BEAM 4/5 AND STA 185.0 APROX (L1). INTERCOSTAL WAS REPLACED PER SRM 51-41-02-0G AND DWG 9955763 REV L.Jan 30, 2018 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017111408093Battery Pack · dischargedEMERGENCY EXIT SIGN L2-791 IS INOPERATIVE. TROUBLE SHOT PER WDM 33-51-12 AND FOUND BATTERY PACK AT B5-259 FOR THE EMERGENCY LIGHTS BAD. REPLACED THE SAME PER AMM 33-51. OPERATIONAL CHECK IS GOOD.Nov 13, 2017 · N998AT · Boeing 717200 · Emergency LightingSDR DALA2017101807617Battery Pack · inoperativeWHILE PERFORMING SERVICE CHECK, FOUND BOTH EXTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. INSTALLED A NEW BATTERY IN THE POWER SUPPLY AND FUNCTIONAL CHECKED GOOD.Oct 18, 2017 · N998AT · Boeing 717200 · Emergency LightingSDR DALA2016072105471Battery · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT THE OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND THE OPS CHECK WAS GOOD.Jul 21, 2016 · N998AT · Boeing 717200 · Emergency LightingSDR 2016F00094Skin · delaminatedDURING NON ROUTINE MAINTENANCE, CHECK SPOILER FOUND DELAMINATED.Mar 30, 2016 · N998AT · Boeing 717200 · SpoilersSDR DALA1704899547Spar Cap · not reportedSTABILIZER / VERTICAL / RT SPAR CAP FORWARD FLANGE,ZFS = 49-50 REPAIRED IAW ERA 543293-14.Feb 24, 2016 · N998AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2016022501439Slide · unserviceableINSPECTION DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE IN THE TAILCONE WAS NO LONGER IN AN ACCEPTABLE CONFIGURATION. THE SLIDE BECAME UNRAVELED INSIDE THE COVER. AN OUT OF POSITION, MISRIGGED, POOR CONDITION, OR ILL-ARRANGED SLIDE ASSEMBLY COULD PREVENT PROPEFeb 24, 2016 · N998AT · Boeing 717200 · Escape SlideSDR DALA2016022401395Skin · crackedAFT FUSELAGE SKIN IS CRACKED, 1.0" AT STA 1133 BETWEEN STR 2RT AND STR 3RT, HFEC -M-. SEE NR FOR ADDITIONAL INFORMATION 001-0219:0593-2005, 012 00102. REPAIRED BY CUTOUT AND INSTALLATION OF DOUBLER. STA LOCATION IAW ENGINEERING IS ACTUALLY BS 1152 NOT BS 1133Feb 23, 2016 · N998AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016010500036Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT BOTH OF THE EXTERIOR EMERGENCY FLOOD LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.Jan 2, 2016 · N998AT · Boeing 717200 · Emergency LightingSDR DALA2015070904198Battery Pack · inoperativeDURING SERVICE CHECK, FOUND AFT EMERGENCY LIGHT BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK.Jul 9, 2015 · N998AT · Boeing 717200 · Emergency LightingSDR DALA2014070703876Power Supply · inoperativeWHILE PERFORMING JC 3351-2001, FOUND OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY INOPERATIVE. REPLACED IAW WC 3351-2001. OPS CHECKED GOOD.Jul 3, 2014 · N998AT · Boeing 717200 · Emergency LightingSDR SWAA2014030325679Frame · corrodedFRAME CORRODED AT BS 889, BETWEEN LONGERON 29L TO LONGERON 19R. REPAIRED FRAME IAW SRM.Feb 26, 2014 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR SWAA2014022625588Lens · crackedL1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. R & R LENS IAW AMM.Feb 22, 2014 · N998AT · Boeing 717200 · Emergency LightingSDR SWAA2014022625587Lens · crackedR1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. R & R LENS IAW AMM.Feb 22, 2014 · N998AT · Boeing 717200 · Emergency LightingSDR SWAA2014020624923Frame · corrodedAFT CARGO COMPARTMENT FRAME CORRODED AT BS 908, BETWEEN LONGERON 25L TO LONGERON 25R. REPAIRED FRAME IAW SRM.Feb 3, 2014 · N998AT · Boeing 717200 · Fuselage Main, Frame
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