N894AT

Service difficulty reports · 119

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 = 'N894AT' 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 DALA2016031101835Cusp Web · corrodedRT CUSP SECTION, BS 389-503, UPPER AND LOWER SURFACES, HAS SEVERAL AREAS OF CORROSION. INSTALLED RT CUSP WEB AT FS 389-503 IAW SRM 51-41-02, SRM 51-41-01 AND SRM 51-41-05.Mar 3, 2016 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016030701684Floor Support · corrodedWEB FLOOR SUPPORT FWD OF R1 DOOR AND WATER LINE PAN IS CORRODED, M ON REPAIR RACK. BLEND & CHECK LIMITS. REF ORNRC 64480-0200-0140. CORRODED BEYOND LIMITS IAW SRM 53-00-00. REPLACED FLOOR SUPPORT MATCH DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-08, PG 1 TO BE INFeb 29, 2016 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016022701483Skin · crackedBS 1153, 3" INBD OF STR 3R, SKIN HAS .2500" CRACK AT SHEAR TIE FASTENER LOCATION. HFEC VERIFIED IAW NDT SPM 06-10-01. 001 PROCEDURE 1, REF: ORNRC 64480-0300-0006. REPAIRED DAMAGE AREA AT BS 1153 3" INBD OF STR 3R IAW ER/A 543583-14. AMDS CONTINUATION FORM PFeb 26, 2016 · N894AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016022601444Longeron · crackedLEFT PYLON APRON, FRAME BS 1076 UPPER LONGERON REPAIR CRACKED AT UPPER COWLING HINGE FITTING CUTOUT. INSTALLED FABED NEW DOUBLER FROM 2024-T3- .071 QQ-A- 250/S. 2024-T3 IS A PERMITTED SUBSTITUTION FOR 2024-T42 IAW SRM 51-30-08, FIG 1, TABLE A IAW SRM 54-50-02Feb 25, 2016 · N894AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016022501397Bulkhead · crackedUPPER CABIN LT ENGINE PYLON SUPPORT BULKHEAD, BS 1022 IS CRACKED ON AFT SIDE AT LONGERON 7L. MARKED, VERIFIED WITH EDDY CURRENT. CUT OUT DAMAGE AS MARKED BS 1022 L7L IAW SRM 51-70-11, FIG 201. HFEC OF CUTOUT SHOWED NO DEFECTS IAW NOT SPM 06-10-01. 001 TAG 678Feb 24, 2016 · N894AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2016022401364Cusp Web · corrodedLH OUTER CUSP WEB HAS CORROSION AROUND SEVERAL FASTENER HEADS BETWEEN BS 813 & 832. REPAIRED LT OUTER CUSP WEB AT BS 813 TO 832 IAW SRM 53-00-55, PG 101, 102 AND 104, AND FIG 216, REPAIR 4.Feb 23, 2016 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016022401363Cusp Web · corrodedLEFT OUTER CUSP WEB HAS CORRODED LAP JOINT AT ATTACH ANGLE AT BS 589. MARKED. BLENDED CORROSION ON LEFT UPPER CUSP ANGLE SPLICE AT BS 589 AND FOUND TO BE OUT OF LIMITS. ORIGINAL 0.080", REMAINING 0.055". REMOVED UPPER CUSP ANGLE SPLICE AND FABRICATED NEW CUSFeb 23, 2016 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016022401362Cusp Web · corrodedLEFT OUTER CUSP WEB HAS CORRODED LAP JOINT AT ATTACH ANGLE, BS 635. MARKED. BLENDED CORROSION ON LT UPPER CUSP ANGLE SPLICE AT BS 635 AND FOUND TO BE OUT OF LIMITS. ORIGINAL 0.080", REMAINING 0.060". FABRICATED NEW UPPER CUSP ANGLE SPLICE AND HEAT TREATED Feb 23, 2016 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102807815Cusp Web · corrodedLEFT OUTER CUSP WEB HAS TWO SPOTS OF CORROSION BETWEEN BS 794 - 813. BLENDED CORRODED AREAS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55 PG 101 & 102 FIG 101. FABRICATED & INSTALLED A REPAIR DOUBLER IAW SRM 53-00-55 REPAIR 4 FIG 216.Feb 22, 2016 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102807814Cusp Web · corrodedLEFT OUTER CUSP WEB CORRODED AT BS 544. CORRISION BLENDED BEYOND ALLOWABLE LIMITS. REPAIRED THE CUSP WEB IAW SRM 53-00-55 ALLOWABLE DAMAGE 1 AND 53-00-55 REPAIR 4.Feb 22, 2016 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016022301310Drain Mast · corrodedELECTRONIC EQUIPMENT COMPARTMENT A LOWER DRAIN MAST IS CORRODED, FWD OF 218 BULKHEAD BETWEEN S27-S28R. VERIFIED DRAIN MAST DOUBLER WAS OUT OF LIMITS BY VISUAL INSPECTION. ZERO THICKNESS REMAINING. REMOVED 2 EA INTERCOSTALS TO GAIN ACCESS REMOVED DRAIN MAST ANFeb 21, 2016 · N894AT · Boeing 717200 · Water Line Anti-Ice SystemSDR DALA2016022101270Attach Angle · crackedBOTH LOWER ATTACH ANGLES FOR PANEL 370AL, LT AND RT SIDES ARE CRACKED. REPLACED CRACKED ATTACH ANGLES 2 IAW SRM 51-41-02, SECTION 4, SRM 51-41-05, SECTION 8 AND ERA 510501-14MA.Feb 20, 2016 · N894AT · Boeing 717200 · Wing, Attach FittingsSDR DALA2016022901486Beam · crackedLOWER BEAM CRACKED ON R-1 SERVICE DOOR AT LOWER END BELOW BEAM ATTACH FITTING REPAIR, REPLACE BEAM REF ORNRC 64480-0800-0029. REMOVED AND INSTALLED NEW Z FRAME IAW SRM 51-40-02, PAR 6 AND DWG 591084.Feb 18, 2016 · N894AT · Boeing 717200 · Service DoorsSDR DALA2016022101269Structure · crackedR1 DOOR AFT SUBFLOOR IS CRACKED AND HAS CORROSION. REPLACE SUBFLOOR IAW OR NRC 64480-0200-0145. FABRICATED NEW SUB FLOOR IAW DWG 9936535. APPLIED ALODINE IAW AMM 51-10-00-370-803. PRIMED AS REQUIRED IAW AMM 51-10-00-370-803. APPLIED TOP COAT IAW AMM 51-10-Feb 18, 2016 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016011100197Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Jan 10, 2016 · N894AT · Boeing 717200 · Emergency LightingSDR DALA2016102607663Scuff Plate · corrodedSCUFFPLATE AFT CARGO BIN HAS CORROSION. OPENED UP AFT CARGO DOOR JAMS AND REMOVED CORRODED FRAME SECTION TO FOM. ITEM TRANSFERRED TO NR 02 FOR COMPLETION.Dec 29, 2015 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015123007777Structure · corrodedAFT CARGO DOOR CUTOUT CORRODED. C/W PRI 542549-14, REV 0, REV 1, REV 2. FINAL ERA 542549-14 REV ORIGINAL C/W AND MATCHES.Dec 29, 2015 · N894AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2015123007776Stringer · corrodedSTRINGER 30L CORRODED AT BS 954. FABRICATED REPAIR AND INSTALLED IAW SRM 53-20-05, REPAIR 1. STRINGER INSTALLATION OK IAW SRM 53-20-05.Dec 29, 2015 · N894AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2015123007775Frame · corrodedSECOND FRAME AFT UNDER INTERIOR SCUFF PLATE AFT CARGO BIN HAS CORROSION. OPENED UP AFT CARGO DOOR JAMB AND REMOVED CORRODED FRAME SECT TO FORM. REPLACED FRAME IAW DWG 995822T.Dec 29, 2015 · N894AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2015080304786Handle · stiffDURING SCHEDULED CHECK OF THE TAILCONE DEPLOYMENT, IT WAS NOTED THAT THE FORCE REQUIRED TO PULL THE INTERNAL RELEASE HANDLE EXCEEDED TEST LIMITS. COMPLIED WITH REPAIR ON NON-ROUTINE WC OF WO 9554 07/31/15.Aug 1, 2015 · N894AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2015022501630None · noneREMOVED OTBD RT SEAT TRACK FROM STA 589 TO STA 746 TO FACILITATE OVERWING FRAME REPLACEMENT DUE TO AD MANDATED OVERWING FRAME INSPECTION FINDINGS.Feb 24, 2015 · N894AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2015022501629Frame · crackedDURING SPECIAL VISIT IN MSP, FOUND CRACK INDICATION ON RT SIDE FRAME 715 WITH EDDY CURRENT. REPLACED OVERWING FRAME AT STA 715 RT IAW AMDS WC 5310-01436-03B.Feb 24, 2015 · N894AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2015022501628Frame · crackedDURING FRAME INSPECTION IN MSP, FOUND CRACK INDICATION ON RT SIDE FRAME 674 WITH EDDY CURRENT. REPLACED OVERWING FRAME AT STA 675 RT IAW AMDS WC 5310-01436-03B.Feb 24, 2015 · N894AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2015022501627Cusp Web · unknownREMOVED CUSP WEB FROM STA 655 TO STA 715 RT SIDE. REPLACED CUSP WEB IAW SRM 51-41. WEB WAS REMOVED TO PERFORM OVERWING FRAME REPLACEMENT DUE TO AD MANDATED INSPECTION FINDINGS.Feb 24, 2015 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015022301548Stringer · noneDURING SPECIAL VISIT FOR OVERWING FRAME INSPECTION, IT WAS NECESSARY TO CUT AND SPLICE STR 11 RT STA 655-674 FOR REMOVAL OF FRAME 674 RT. INSTALLED REPAIR SPLICE IAW ER/A 530437-14MA.Feb 22, 2015 · N894AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2015011500316Floorbeam · crackedFLOORBEAM BS 737 LT BETWEEN LBL 54 AND LBL 50, CRACKED. REPLACED THE FLOORBEAM ANGLE LBL 19 TO LBL 60 IAW SRM 51-40-08, 51-41-05 AND DWG 5930561, REV AC.Jan 13, 2015 · N894AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2015011500315Floorbeam · corrodedRT FLOORBEAM CRACKED AT RADIUS. BS 737, RBL 54. REPLACED CRACKED FLOORBEAM TEE RBL 19 TO RBL 60 IAW SRM 51-40-08, 51-41-05 AND DWG 5930561, REV AC.Jan 13, 2015 · N894AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2015011300258Vertical Support · crackedVERTICAL SUPPORT ANGLE AT STA 737, LBL 44 WAS FOUND TO BE CRACKED. REPLACED VERTICAL SUPPORT IAW SRM 51-40-08, DWG 5940863, REV N AND DWG 9923417, REV B.Jan 12, 2015 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015011300257Vertical Support · crackedVERTICAL SUPPORT ANGLE AT BS 737, RBL 44 WAS FOUND TO BE CRACKED. REPLACED CRACKED VERTICLE SUPPORT PN 3925812U2 AT STA 737 RBL 44 IAW SRM 51-40-08 AND DWG 5940863, REV N AND DWG 9923417, REV B.Jan 11, 2015 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015011300256Tee Fitting · crackedDURING INSPECTION, THE TEE ANGLE AT BS 715, LBL 44 WAS FOUND TO BE CRACKED. REPLACED TEE ANGLE IAW DWG 9923417.Jan 11, 2015 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015011400312Seat Track · damagedSEAT TRACK DAMAGED BS 737 LBL 44. REPAIRED IAW ER/A 531461-14.Jan 10, 2015 · N894AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2014021225094Light · inoperativeRT FWD OVERWING DOOR EMERGENCY LIGHT BULB INOPERATIVE. REPAIRED BULB IAW MM.Feb 11, 2014 · N894AT · Boeing 717200 · Emergency LightingSDR SWAA2014021225093Light · inoperativeTAIL COMPARTMENT AFT EMERGENCY EXIT LIGHT BULB INOPERATIVE. REPAIRED BULB IAW MM.Feb 11, 2014 · N894AT · Boeing 717200 · Emergency LightingSDR SWAA2014020424853Skin · damagedRT WING FLAP OTBD UPPER SKIN SECTION DAMAGED. REPAIRED SKIN IAW SRM & DRAWING.Feb 3, 2014 · N894AT · Boeing 717200 · Trailing Edge FlapsSDR SWAA2014020424852Rib · damagedRT WING FLAP NR 4 RIB DAMAGED. REPAIRED NR 4 RIB IAW SRM & DRAWING.Feb 3, 2014 · N894AT · Boeing 717200 · Trailing Edge FlapsSDR SWAA2014020624922Skin · delaminatedRT WING FLAP INBD FIXED VANE UPPER SKIN SURFACE DELAMINATED. REPAIRED SKIN IAW SRM.Feb 1, 2014 · N894AT · Boeing 717200 · Trailing Edge FlapsSDR SWAA2014020424850Light · missingAFT CABIN EMERGENCY EXIT LIGHT ASSEMBLY ABOVE AFT ACCESSORY COMPARTMENT DOOR MISSING. INSTALLED LIGHT IAW AMM.Jan 24, 2014 · N894AT · Boeing 717200 · Emergency LightingSDR SWAA2014011424090Doubler · crackedMAIN CABIN DOUBLER CUSP WEB CRACKED AT BS 674 LBL 44. REPAIRED DOUBLER IAW SRM.Jan 10, 2014 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2014011324076Doubler · crackedMAIN CABIN DOUBLER CUSP WEB CRACKED AT BS 674 RBL 44. REPAIRED DOUBLER IAW SRM.Jan 10, 2014 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2014020424849Stringer · crackedSTRINGER CRACKED AT BS 1133, LONGERON 2L. REPAIRED STRINGER IAW SRM.Jan 4, 2014 · N894AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR SWAA2014020424844Shear Tie · crackedSHEAR TIE CRACKED AT BS 1144, STRINGER 2R. R & R SHEAR TIE IAW SRM.Jan 3, 2014 · N894AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR SWAA2014010723823Fitting · crackedLT WING NR 5 SLAT OTBD END FITTING CRACKED, R & R FITTING IAW SRM & DRAWING.Jan 3, 2014 · N894AT · Boeing 717200 · Leading Edge DevicesSDR SWAA2014021024931Skin · corrodedLT WING FWD BULKHEAD CTR WING UPPER SKIN CORRODED ALONG THE EDGES. REPAIRED SKIN IAW SRM.Dec 29, 2013 · N894AT · Boeing 717200 · Wing, Plate/SkinSDR SWAA2014020424843Pan · corrodedFWD CARGO DOOR JAMB PAN CORRODED. R & R PAN IAW SRM.Dec 29, 2013 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2014012024201Light · brokenAFT LT LAVATORY EMERGENCY LIGHT BROKEN. R & R LIGHT IAW AMM.Dec 29, 2013 · N894AT · Boeing 717200 · Emergency LightingSDR SWAA2014020424842Frame · crackedFRAME CRACKED AT BS 522, BETWEEN LONGERON 24L TO LONGERON 26L. REPAIRED FRAME IAW SRM.Dec 28, 2013 · N894AT · Boeing 717200 · Fuselage Main, FrameSDR SWAA2014020624916Skin · crackedSKIN CRACKED BETWEEN BS 514 TO BS 541, BETWEEN LONGERON 24L TO STRINGER 25L. REPAIRED SKIN IAW SRM.Dec 24, 2013 · N894AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR SWAA2014012024232Frame · corrodedFRAME CORRODED AT BS 889 BETWEEN LONGERON 27L TO LONGERON 27R. REPAIRED FRAME IAW SRM.Dec 18, 2013 · N894AT · Boeing 717200 · Fuselage Main, FrameSDR SWAA2014012024230Frame · corrodedFRAME CORRODED AT BS 927 BETWEEN LONGERON 27L TO LONGERON 27R. REPAIRED FRAME IAW SRM.Dec 18, 2013 · N894AT · Boeing 717200 · Fuselage Main, FrameSDR SWAA2014012024229Frame · corrodedFRAME CORRODED AT BS 908 BETWEEN LONGERON 27L TO LONGERON 27R. REPAIRED FRAME IAW SRM.Dec 18, 2013 · N894AT · Boeing 717200 · Fuselage Main, Frame
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