N891AT

Service difficulty reports · 140

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 = 'N891AT' 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 DALA2023033102473Unknown · unknownAIRCRAFT 9551, INITIAL INSPECTION: CRACK ON INNER FITTING OF BEAM # 2 IN FWD EDGE AND BEAM # 3 ON FWD EDGE APPROX BTW STA Y=954 AND STA Y=964 AT AFT CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: INNER FITTING OF BEAM # 2 IN FWD EDGE AFT CARGO COMPARTMENT DOOR WASMar 29, 2023 · N891AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023032302264Unknown · unknownAIRCRAFT 9551, INITIAL INSPECTION: CRACK ON BEAM NO. 2 STA Y=157 AT PASSENGER FWD ENTRANCE DOOR (L1). CORRECTIVE ACTION: BEAM NO. 2 STA Y=157 AT PASSENGER FWD ENTRANCE DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 8 REPAIR 8. (LP 2683386)Mar 22, 2023 · N891AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2023032302263Unknown · unknownAIRCRAFT 9551, INITIAL INSPECTION: CRACK ON UPPER BEAM NO. 1 STA Y=157 AND STA Y=194 AT PASSENGER DOOR (L1). CORRECTIVE ACTION: UPPER BEAM NO. 1 STA Y=157 AND STA Y=194 AT PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP 26828Mar 22, 2023 · N891AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2020123104352Power Supply · inoperativeMAINTENANCE NOTED THAT THE OVERHEAD EMERGENCY EXIT LIGHT (INTERIOR) AT THE OVERWING EMERGENCY EXIT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY, B5-120, PER B717 AMM 33-51.Dec 21, 2020 · N891AT · Boeing 717200 · Emergency LightingSDR DALA2019120206970Light · inoperativeTHE EMERGENCY LIGHTS IN THE FIRST CLASS SECTION ARE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY PER B-717 AMM 33-51. ALL EEPL CHECK GOOD NOW. (LP #6630556)Nov 27, 2019 · N891AT · Boeing 717200 · Emergency LightingSDR DALA2019102806189Frame · crackedRH OVERWING EXIT FRAME STA 674 CRACKED AT UPPER RADIUS OF FRAME TAB. CRACK IS CONDITION 3 (GREATER THAN 0.125 INCHES). NRC 025-0004:5310-01439-01D/001 00052: C/W AMDS WORK CARD 54310-01436-03B. (LP #1334164)Oct 27, 2019 · N891AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023012400526Skin · damagedERA 564482-14AD REVISED TO REV 'A'. SECTION I ORIGINALLY ISSUED FOR DAMAGE TO V STAB FRONT SPAR CAP SKIN. DAMAGE TOLERANCE EVALUATION COMPLETE. FOLLOW ON ACTION REQUIRED. ACCOMPLISH SECTION II INSPECTION PRIOR TO 5100 FLIGHT CYCLES FROM SECTION I ACCOMPLISHMENJul 22, 2019 · N891AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2019050302819Power Supply · inoperativeTHE RIGHT & LEFT AFT OVERWING EMERGENCY EXIT IDENTIFIERS L2-837, L2-836 WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THAT THERE WAS NOT ANY POWER AT PIN 9 ON THE POWER SUPPLY B5-119. THE POWER SUPPLY WAS REPLACED PER AMM 33-51-03 400-802. CHECK WAS GOOD. (LMay 3, 2019 · N891AT · Boeing 717200 · Emergency LightingSDR DALA2019050302818Light · inoperativeTHE EMERGENCY LIGHTS L2-786, L2-771, AND L2-772 ARE INOPERATIVE. MAINTENANCE FOUND THE GROUNDS 5238D AND 5239D TO BE LOOSE. THE GROUNDS WERE RE-INSTALLED PER WDM 33-51-12 AND ALL CHECKS WERE GOOD. (LP #5691118)May 3, 2019 · N891AT · Boeing 717200 · Emergency LightingSDR DALA2023012400531Skin · crackedVERTICAL STAB LE INDICATES CRACKING AT 4EA HOLES OF DOUBLER REPAIR STRAP. COMPLIED WITH ERA 564482-14AD REV ORIG.Jan 17, 2019 · N891AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2023012400530Skin · crackedDURING INSPECTIONS PER WORKCARD 5530-01048-01 & AD 2016-09-05, MTC FOUND A CRACK INDICATION COMMON TO THE VERTICAL SPLICE BETWEEN LOWER DORSAL ASSEMBLY SKIN & FRONT SPAR FORWARD CAP ON LT OF STAB. WORKCARD DOES NOT GIVE INSTRUCTIONS IF A CRACK IND IS FOUND. EJan 16, 2019 · N891AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2018080604876Skin · damagedFUSELAGE SKIN AT BS 1110, LONGERON 24R WAS DAMAGED. REPAIRED THE SKIN IAW ER/A 569013-14, REV ORIGINAL.Aug 5, 2018 · N891AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018080604875Skin · damagedFUSELAGE SKIN DAMAGED BETWEEN BS 1116 - 1140, LONGERON 23R - 25R. REPAIRED THE SKIN IAW ER/A 569014-14, REV ORIGINAL.Aug 5, 2018 · N891AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018080604874Doubler · damagedTHE FUSELAGE SKIN BUTTSPLICE DOUBLER WAS DAMAGED AT BS 1116 BETWEEN LONGERONS 24R AND 23R. REMOVED, FABRICATED, AND INSTALLED A NEW BUTTSPLICE DOUBLER IAW SRM 51-40-02, AND DWG 5911429, REV DZ.Aug 5, 2018 · N891AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018080604873Longeron · damagedLONGERON 23R, BS 1110 WAS DAMAGED. CUT OUT DAMAGED SECTION OF THE LONGERON AND REPAIRED IAW SRM 53-00-05, REPAIR 2.Aug 5, 2018 · N891AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018080604872Longeron · damagedLONGERON 24R, BS 1110 WAS DAMAGED. CUT OUT THE DAMAGED SECTION AND REPAIRED THE LONGERON IAW SRM 53-00-05, REPAIR 2.Aug 5, 2018 · N891AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018080604871Frame · damagedFRAME BS 1116, BETWEEN LONGERONS 23R AND 24R WAS DAMAGED. REMOVED, FABRICATED, AND INSTALLED A NEW FRAME IAW SRM 51-40-02, AND DWG 9915559, REV AB.Aug 5, 2018 · N891AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018080604870Frame · damagedFRAME BS 1116, LONGERON 24R WAS DAMAGED. REPLACED THE FRAME SECTION IAW SRM 51-40-02, AND DWG 5913596, REV AN.Aug 5, 2018 · N891AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018011200245Skin · corrodedDURING A C CHECK, FOUND CORROSION THE LT WING UPPER SKIN. THE CORROSION WAS BEYOND THE LIMITS IAW SRM 57-10-01 ALLOWABLE DAMAGE 1. THE CORROSION WAS BLENDED IAW SRM 51-10-02 AND PERFORMED A UT THICKNESS INSPECTION IAW NDT SPM 04-00-00. THE SKIN WAS REPLACEJan 11, 2018 · N891AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017122909003Angle · corrodedAN ANGLE IS CORRODED AT C2 BB LOWER DOOR CUT OUT, FWD SIDE TO AFT OF MIDDLE FITTING. REPAIRED IAW SRM 53-20-15, REPAIR 7.Dec 22, 2017 · N891AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016111608848Lens · crackedTHE PILOT DISCOVERED THAT AN EMERGENCY EXIT SIGN DIFFUSER COVER WAS CRACKED. MAINTENANCE REPLACED THE LENS/COVER AND THE OPERATIONAL CHECK WAS GOOD.Nov 15, 2016 · N891AT · Boeing 717200 · Emergency LightingSDR DALA2016081205958Wire Harness · disconnectedDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING IN THE CENTER SECTION OF THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND THE WIRE HARNESS DISCONNECTED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.Aug 12, 2016 · N891AT · Boeing 717200 · Light System WiringSDR DALA2016012600597Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN THE CEILING BETWEEN ROWS 1-16 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT SEAT ROW 10 AND THE OPERATIONAL CHECK WAS GOOD.Jan 26, 2016 · N891AT · Boeing 717200 · Emergency LightingSDR DALA2015121707645Skin · crackedEMPENNAGE SKIN CRACKED AT SHEAR TIE FASTENER BETWEEN STR 2R & 3R. REPAIRED SKIN AT STRINGERS 2 - 3R BS 1155 IAW ER/A 541025-14, INSTRUCTIONS 1-11.Dec 16, 2015 · N891AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2015121707644Skin · crackedLEFT BS 1155, EMPENNAGE SKIN CRACKED AT SHEAR TIE FASTENER BETWEEN STR 2L & 3L. REPAIRED SKIN CRACK AT STR 2L AND NR LT SHEAR TIE AT LT F/S 1155 IAW ER/A 541025-14 INSTRUCTIONS 1-11.Dec 16, 2015 · N891AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2015121607634Pan · chafedSERVICE DOOR LOWER PAN IS CHAFED. R & R SERVICE DOOR LOWER PAN IAW SRM 51-41-02, PARA 4 & 51-41-05, PARA 8.Dec 12, 2015 · N891AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015121107520Floor Panel · corrodedCORROSION ON UPPER SURFACE OF SUBFLOOR, UNDER FWD CABIN FLOOR PANEL 221MF. BLENDED CORROSION REMOVE .010 MATERIAL ORGINAL THICKNESS .020 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55. FABRICATED NEW CUSP IAW DWG 9936535 INSTALLED IAW SRM 51-41-02, PG 1 PARA4, 5Dec 10, 2015 · N891AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2015121007491Longeron Splice · corroded30 LONGERON SPLICE AND SHIMS ARE CORRODED, M PARTS LOCATED ON REPAIR RACK. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, PG 105, FIG 103. BLENDED SHIMS AND FOUND TO BE OUT OF LIMITS IAW SRM PG 105, FIG 103, FABRICATED SHIMS IAW SRM 53-20-Dec 9, 2015 · N891AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2015120507416Anchor · crackedFLOOR ANCHOR IS CRACKED & CORRODED IN THE CORNER RADIUS, ON REPAIR RACK. REPLACED CRACKED AND CORRODED ALC FLOOR ANCHOR, INTERCOSTAL, IAW SRM 51-41-02 AND 51-41-05 JOB COMPLETE.Dec 4, 2015 · N891AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2015120807455Structure · corrodedCORROSION IN POCKET JUST AFT OF R-1 SERVICE DOOR LOWER AFT CORNER. BLENDED CORROSION NOMINAL .071 REMAINING .090 FOUND TO BE OF LIMITS IAW SRM 53-00-00, FIG 103, PG 105. REPLACED UPPER CUSP IAW SRM 51-41-05, PARA 8, JOB COMPLETE.Dec 3, 2015 · N891AT · Boeing 717200 · Service DoorsSDR DALA2015120407387Door Sill · corrodedFWD LOWER CARGO DOOR CUTOUT LOWER SILL AREA HAS CORROSION AROUND SEVERAL FASTENERS ALONG ENTIRE LENGTH OF CUTOUT. REPAIRED IAW SRM 53-20-15, FIG 201, SHT 4-6.Dec 3, 2015 · N891AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015120407386Cusp Web · crackedCUSP MEMBRANE CRACKED BS 674 AT LT OTBD SEAT TRACK FWD OF SEAT TRACK ATTACH POINT, BELOW FLOOR. REPAIRED CRACKED CUSP MEMBRANE AT BS 674 IAW SRM 53-00-55, REPAIR 4.Dec 3, 2015 · N891AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015120807457Frame · crackedRIGHT OVERWING FRAME AT BS 715.000 CRACKED BELOW FLOOR FROM TAB INTO POCKET. CONDITION 3, CRACK GREATER THAN 0.125, REF: CARD 5310-01436-01C, FIG 2, SH 1 FOR LOCATION. RIGHT OVERWING FRAME AT BS Y=715.000 WAS REPLACED ON JOB CARD 5310-01436-03B.Dec 1, 2015 · N891AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2015120507414Frame · corrodedFRAME CORRODED AT STRINGER 30. REPAIRED FRAME AT BS 1037, STR 30 IAW SRM 53-20-07, REPAIR 3.Nov 30, 2015 · N891AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2015120807456Structure · damagedVERTICAL STABILIZER HAS NUMEROUS WORKING/SMOKING FASTENERS IN THE L/E. REPAIRED VERTICAL STABILIZER BY REMOVING DAMAGED AREA IAW SRM 55-30-01, REPAIR 7. FABRICATED REPAIR PART AND INSTALLED REPAIR PARTS IAW SRM 55-30-01, REPAIR 7.Nov 27, 2015 · N891AT · Boeing 717200 · Vertical StabilizerSDR DALA2015120507415Stringer · corrodedSTRINGER 30R AND FRAME AT BS 954 CORRODED. STRINGER 30 REPLACED FROM BS 935 - 1012 IAW SRM 53-20-05, REPAIR NR 1.Nov 27, 2015 · N891AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2015120607418Stringer · corrodedSTR 30 CORROSION IN BETWEEN BS 908 - 927. REPLACED THE STR IAW SRM 51-40-02, PAGES 1 THRU 4 AND 51-40-05, PAGES 1 THRU 5.Nov 25, 2015 · N891AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2015120607417Window Frame · crackedLEFT CABIN WINDOW INTERNAL FRAME AT APPROXIMATELY BS 795 HAS A CRACK APPROXIMATELY .1250" LONG ON THE FWD LOWER CORNER. VERIFIED CRACK AND MARKED END OF CRACK USING HFEC WITH MODEL NORTEC 500D, TAG 6782, SN N500D000D030. REPAIRED LT CABIN WINDOW INTERNAL FRANov 24, 2015 · N891AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2015121107566Slide · damagedMAINTENANCE DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE AT DOOR 1L WAS DAMAGED, NOT SPECIFIED. THE DOOR SLIDE WAS REPLACED.Nov 2, 2015 · N891AT · Boeing 717200 · Escape SlideSDR DALA2015092805848Bulb · inoperativeTWO BULBS INOPERATIVE IN AFT EMERGENCY EXIT IDENTIFIER LIGHT. REPLACED THE BULBS IAW AMM 33-51.Sep 27, 2015 · N891AT · Boeing 717200 · Emergency LightingSDR DALA2015071704450Structure · damagedRAMP CREW REPORTED A TEAR ON THE L/E OF THE FWD CARGO DOOR. DAMAGE IS 2", TEAR 20" FROM LOWER THRESHOLD RT SIDE. REPAIRED IAW SRM 53-20-15, REPAIR 11. REQUIRED INSPECTION COMPLETED.Jul 17, 2015 · N891AT · Boeing 717200 · Cargo/Baggage DoorsSDR 2015F00086Skin · delaminatedTHE SUBJECT FLIGHT SPOILER IS TYPICALLY FOUND WITH DISBONDS & DELAMINATION’S ALONG THE UPPER & LOWER SURFACES. THE UPPER & LOWER SKINS ARE ORIGINALLY MANUFACTURED FROM 0.032” 2024-T81CLAD SHEET & THE UNDERLYING DOUBLERS ARE MANUFACTURED FROM 0.020” 2024-T81 CJun 11, 2015 · N891AT · Boeing 717200 · SpoilersSDR DALA2015010700121Seat Track · damagedONE FASTENER MISSING AT BS 312 RBL 54 SEAT TRACK. REPAIRED IAW ER/A 95-531456-14.Jan 3, 2015 · N891AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA14001219551Cover · out of positionDURING CONFORMITY INSPECTION, THE TAIL CONE SLIDE PRESSURE INDICATOR WAS NOTED TO BE UNREADABLE. MAINTENANCE ADJUSTED THE COVER TO ENABLE PROPER READING.Jan 6, 2014 · N891AT · Boeing 717200 · Escape SlideSDR SWAA2013121823490Sign · crackedCEILING EMERGENCY EXIT SIGN AT ROW 1 CRACKED. R & R SIGN IAW AMM.Dec 15, 2013 · N891AT · Boeing 717200 · Emergency LightingSDR SWAA2013120523052Floor Panel · damagedMAIN CABIN FLOOR PANEL 222ADF METAL COVERS DAMAGED. R & R PANEL IAW SRM & DRAWING.Nov 20, 2013 · N891AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013120523046Floor Panel · damagedMAIN CABIN FLOOR PANEL 2224F METAL COVERS DAMAGED. R & R PANEL IAW SRM & DRAWING.Nov 20, 2013 · N891AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2013121123147Skin Panel · crackedRT WING INBD BUTTE DOOR LOWER SKIN INBD END CRACKED. R & R SKIN IAW SRM & DRAWING.Nov 19, 2013 · N891AT · Boeing 717200 · Wing, Plate/SkinSDR SWAA2013120322921Hinge · crackedRT WING CENTER BUTTE DOOR INBD SIDE OF HINGE CRACKED. R & R HINGE IAW SRM & DRAWING.Nov 19, 2013 · N891AT · Boeing 717200 · Wing Miscellaneous StructureSDR SWAA2013120523045Bracket · crackedRT WW FWD BULKHEAD OTBD SIDE HYD LINES SUPPORT CLAMP CRACKED. R & R BRACKET IAW SRM & DRAWING.Nov 18, 2013 · N891AT · Boeing 717200 · Fuselage Miscellaneous Structure
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