N892AT

Service difficulty reports · 110

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 = 'N892AT' 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 DALA2016021701092Cusp Web · corrodedRIGHT CUSP WEB CORRODED AT CUSP TEE BS 427-446 BOTTOM SIDE. REMOVED CORROSION IAW SRM 55-00-55, PG 101, ITEM 4 FOUND TO BE OUT OF LIMITS. INSTALLED NEW CUSP WEB AT BS 389 TO 503, RBL 45 TO RBL 54 IAW SRM 51-40-08 AND 51-40-02. REINSTALLED SEAT TRACKS AT RBLFeb 16, 2016 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016021601052Skin · damagedVERTICAL STABILIZER L/E WRAP AROUND SKIN PANEL JUST BELOW REMOVABLE PANELS 370DL 370GR HAS SEVERAL LOOSE SMOKING FASTENERS PULLING THROUGH SKIN. INSTALLED FABRICATED REPAIR DOUBLER AT VERTICAL STABILIZER WRAP AROUND SKIN PANEL IAW SRM 53-30-01, REPAIR (7) ANDFeb 15, 2016 · N892AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2016022001267Skin · crackedRIGHT AFT FUSELAGE SKIN IS CRACKED AROUND FASTENER, BS 1155 JUST ABOVE LONGERON 2R NEAR VERTICAL STABILIZER REPAIRED RT AFT FUSELAGE SKIN CRACK BS 1155 ABOVE L2R AS MARKED IAW ER/A 542364-14, REV ORIGINAL. ASSOCIATED ER/A 54-236514 ADDED FOR AC 9552.Feb 12, 2016 · N892AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016021301044Shear Tie · crackedCRACKED SHEAR TIE W/W SRM 53-30-08, REPAIR 8. REMOVED VERTICAL STIFFENER AT BS 1152, S2R FOR ACCESS IAW SRM 51-40-02, PG 1, PER 1 A. REPLACED SHEAR TIE AT BS 1152 S2R IAW SRM 51-40-02, PG 1, PAR 1 A, 51-40-08, PAR 3 AND 51-40-05, FIG 1 AND FIG 2. RE-INSTALLFeb 11, 2016 · N892AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2016102707770Angle · corrodedANGLE CORRODED S18R, BS 579. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02, 53-00-55 REPAIR 1 AND DWG 82912047.Feb 9, 2016 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016021000959Attach Fitting · crackedLEFT FLOORBEAM TO WEB VERTICAL ATTACH FITTING AT APPROXIMATELY LBL 45, FS 737, IS CRACKED IN 2 PLACES AT BOTTOM END. REMOVED ATTACH FITTING FOR REPLACEMENT IAW SRM 51-41-02, PAGE 40. INSTALLED NEW FITTING ON 3925812-1 IAW SRM 5141-05, PAGE 1.Feb 9, 2016 · N892AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2016020400866Fitting · corrodedCORROSION ON GIRT BAR FITTING BS 157, 18R. REPLACED GIRT BAR FITTINGIAW SRM 51-41-01, PG 17.Feb 3, 2016 · N892AT · Boeing 717200 · Entrance StairsSDR DALA2016020200817Frame · crackedCRACK ON OTBD END OF FORMER IN RT SIDE CANTED KEEL AREA AT BS 696, ASSOCIATED HI-LOCS MARKED ON EXTERIOR SURFACE, CRACK CHECKED BY EDDY CURENT, M62937-0100-0091. REPLACED FORMER IN THE RT CANTED KEEL AREA AT BS 696 IAW SRM 51-41-02, PG 1, PARA 4 AND 51-41-05,Feb 2, 2016 · N892AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016021301049Skin · damagedL1 DOOR SKIN LOWER EDGE IS WAVY AND CHAFED ALONG THE BOTTOM IN SEVERAL PLACES. TRIM/BLEND AND CHECK LIMITS. INSPECTED AND FOUND SKIN TO BE OIL CANNED AT LWR AFT CORNER OUT OF LIMITS IAW SRM 53-01-01, ALLOWABLE DAMAGE 1. FABRICATED REPAIR DOUBLER AND FILTER IJan 29, 2016 · N892AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016013000748Cusp Web · corrodedBS 526, RBL 57, CUSP WEB UPPER & LOWER SURFACE CORRODED. REF ORNRC 62937-0200-0126 REMOVED CORROSION IAW SRM 53-00-00 PG 105, FIG 103. ORIGINAL THICKNESS .020" MATERIAL REMOVED .005" MATERIAL REMAINING, .015" GAUGE TAG 10371. DAMAGE OUT OF LIMITS IAW SRM 5Jan 29, 2016 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016013000747Cusp Web · corrodedBS 545, RBL 57, CUSP WEB UPPER & LOWER SURFACE CORRODED & BS 550 LWR SURFACE CORRODED. REF ORNRC 62937-0200-0125. REMOVED CORROSION IAW SRM 53-00-00, PG 105, FIG 103. ORIGINAL THICKNESS .020" MATERIAL REMOVED .014" MATERIAL REMAINING .006". GAUGE TAG NR 103Jan 29, 2016 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016021301045Frame · crackedFRAME CRACKED, REPAIRED THE FRAME SECTION IAW SRM 51-41-02, PG 1, STEP 4.Jan 28, 2016 · N892AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016012900705Attach Fitting · crackedRIGHT FLOORBEAM TO WEB VERTICAL ATTACH FITTING AT APPROXIMATELY RBL 45, FS 713 IS CRACKED WITH FASTENER HEADS SHEARED OFF AND RIGHT FLOORBEAM TO WEB VERTICAL ATTACH FITTING AT APPROXIMATELY RBL 45, FS 737 IS CRACKED IN 2 PLACES AT BOTTOM END. BOTH FITTINGS MARJan 28, 2016 · N892AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2016012900704Cusp Web · corrodedRIGHT CUSP WEB HAS CORROSION AROUND FWD LIGHTING HOLE BETWEEN BS 446-465. BLENDED AREA IAW SRM 53-00-55, PG 101. FOUND TO BE OUT OF LIMITS. CUSP WEB REPLACED.Jan 28, 2016 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016012900703Cusp Web · corrodedRT CUSP WEB HAS CORROSION AROUND SEVERAL FASTENERS BETWEEN BS 408-427. BLENDED AREA IAW SRM 53-00-55, PG 101, PAR 4A. FOUND TO BE OUT OF LIMITS. CUSP WEB REPLACED.Jan 28, 2016 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016021801165Cusp Web · corrodedBS 670, RBL 58 CUSP WEB LOWER SURFACE CORRODED. REMOVED CORROSION AS MARKED IAW SRM 53-00-00, PG. 105, FIG 103 ORIGINAL THICKNESS =.020" MATERIAL REMOVED = .004" OUT OF LIMITS, IAW SRM 53-00-55, PG 101, PAR 4, A CUSP WEB WILL BE REPLACED ON NR 0111. GUAGE TAGJan 27, 2016 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016021801164Cusp Web · corrodedBS 692, RBL 58, CUSP WEB LOWER SURFACE CORRODED. REMOVED CORROSION AS MARKED IAW SRM 53-00-00, PG 105, FIG 103. ORIGINAL THICKNESS =.020" MATERIAL REMOVED =.004" OUT OF LIMITS IAW SRM 53-00-55, PG 101, PAR 4, A, CUSP WEB WILL BE REPLACED ON NR 0111. GUAGE TJan 27, 2016 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016021801163Cusp Web · corrodedRIGHT CUSP WEB LOWER SURFACE HAS CORROSION AROUND 2 FASTENERS JUST FWD OF MAIN FRAME AT FS 713 APPROXIMATELY, RBL 62, MARKED. REMOVED CORROSION AS MARKED IAW SRM 53-00-00, PG 105, FIG 103. ORIGINAL THICKNESS=.020", MATERIAL REMOVED=.004". OUT OF LIMITS IAWJan 27, 2016 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016021301048Cusp Web · corrodedRIGHT CUSP WEB LOWER SURFACE IS CORRODED AROUND A FASTENER AT APPROXIMATELY RBL 62 AT FRAME BS 674. CLEAN, BLEND CHECK LIMITS 53-00-55. REMOVED 6 FASTNERS IAW SRM 51-40-02, PG 1, PARA 1A FOR ACCESS. REMOVED CORROSION AS MARKED IAW SRM 53-00-00, PG 105 FIG 1Jan 27, 2016 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016021301047Cusp Web · corrodedBS 700, RBL 58 CUSP WEB LWR SURFACE CORRODED. CLEAN, BLEND CHECK LIMITS 53-00-55. REMOVED 3 FASTENERS IAW SRM 51-40-02, PG 1, PAR 1, A FOR ACCESS. REMOVED CORROSION AS MARKED IAW SRM 53-00-00, PG 105, FIG 103. ORIGINAL THICKNESS=.020". MATERIAL REMOVED = .Jan 27, 2016 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016021301046Pan · corrodedPAN AT LOWER ALC DOOR CUTOUT CORRODED. REPLACE PAN. REPLACED, AND INSTALLED LOWER AFT CARGO DOOR PAN AT DOOR CUTOUT. ALL WORK DONE IAW SRM 53-20-15, REPAIR NR 7, 51-41-02, 51-41-05, AND AMM 20-20-23-911-801, AND AMM 25-58-01-400-804.Jan 27, 2016 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016012500593Angle · corrodedRT SIDEWALL FUSELAGE BS 900, S18R CORRODED AT FLOOR SUPPORT ANGLE TO FUSELAGE SKIN. REPLACED SPLICE PLATE AT BS 900, STR 18R IAW SRM 51-41-05.Jan 22, 2016 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015090705477Longeron · crackedBS 225, LONGERON 17L CRACKED . REPLACED THE LONGERON IAW SRM 51-00-07.Sep 6, 2015 · N892AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2015043003037Frame · crackedDURING SPECIAL VISIT FOR THE OVERWING FRAME INSPECTION, GVI AND HFEC CONFIRMED CRACK IN THE LT FRAME AT FS 715. FRAME WAS REPLACED IAW AMDS WC 5310-01436-03A. LP 1926584.Apr 30, 2015 · N892AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2015043003013Cusp Web · crackedDURING OVERWING FRAME INSPECTION VISIT, NOTED CUSP WEB MEMBRANE IS CRACKED AT FS 674 UNDER MID SEAT TRACK. REPLACED CUSP WEB MEMBRANE IAW SRM 51-40-02. LP 1925089.Apr 29, 2015 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015043003012Attach Angle · crackedDURING OVERWING FRAME INSPECTION, NOTED WEB ATTACH ANGLE AT FS 715 BELOW LT CENTER SEAT TRACK CRACKED. REPLACED WEB ATTACH ANGLE IAW SRM 51-40-02. LP 1926102.Apr 29, 2015 · N892AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2015011700363Cusp Web · crackedPASSENGER CABIN BS 655, LBL 54, CUSP WEB CRACKED. REPAIRED IAW SRM 53-00-55, FIG 203.Jan 16, 2015 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015011700362Cusp Web · crackedPASSENGER CABIN BS 655, RBL 54 CUSP WEB CRACKED. REPAIRED IAW SRM 53-00-55, REPAIR 4, FIG 203.Jan 16, 2015 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2014012424524Sign · crackedFWD CEILING EMERGENCY EXIT SIGN LIGHT CRACKED. R & R SIGN IAW MM.Jan 18, 2014 · N892AT · Boeing 717200 · Emergency LightingSDR SWAA2014010823885Wire · brokenCEILING PANEL 222JC EMERGENCY EXIT LIGHT WIRE BROKEN. REPAIRED WIRE IAW MM.Dec 14, 2013 · N892AT · Boeing 717200 · Light System WiringSDR SWAA2013012311742Battery · dischargedFWD CABIN LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FORWARD CABIN LOWER EMERGENCY FLASHLIGHT BATTERY IAW AM/M . THIS CLEARS MDDR 238669.Jan 23, 2013 · N892AT · Boeing 717200 · Emergency EquipmentSDR SWAA2013012411761Seal · missingAFT EMERGENCY EXIT DOOR HANDLE MISSING SILVER SEALS. REPLACED SEAL AT REQUIED IAW AMM.Jan 11, 2013 · N892AT · Boeing 717200 · Emergency ExitsSDR SWAA2012120310178Holder · brokenR1 GIRT BAR HOLDER BROKEN. REMOVED AND REPLACED R1 DOOR GIRT BAR HOLDER PER MM.Dec 2, 2012 · N892AT · Boeing 717200 · Emergency EquipmentSDR SWAA2012120310127Holder · brokenR1 GIRT BAR HOLDER BROKEN. REMOVED AND REPLACED R1 DOOR GIRT BAR HOLDER PER M/M.Dec 2, 2012 · N892AT · Boeing 717200 · Emergency EquipmentSDR SWAA2012082807110Cover · missingAFT OVERHEAD EMERGENCY EXIT COVER MISSING. INSTALLED COVER PER AMM.Aug 28, 2012 · N892AT · Boeing 717200 · Emergency LightingSDR SWAA2012091707651Sign · looseEMERGENCY EXIT SIGN LOOSE NEAR ROW 1. SECURED SIGN PER AMM.Jul 15, 2012 · N892AT · Boeing 717200 · Emergency LightingSDR SWAA2012052104228Lanyard · frayedL1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LANYARD FRAYED. REMOVED AND REPLACED LANYARD PER MM.May 18, 2012 · N892AT · Boeing 717200 · Emergency EquipmentSDR SWAA2012051003919Cover · brokenAFT EEPLS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.May 10, 2012 · N892AT · Boeing 717200 · Emergency LightingSDR SWAA2012050903857Light · inoperativeFWD EEPLS SECTION INOP. RELAMPED EEPLS PER MM.May 8, 2012 · N892AT · Boeing 717200 · Emergency LightingSDR SWAA2012042703488Floor Support · corrodedFLOOR SUPPORT CORRODED AT BS 178, LBL 5. REPAIRED SUPPORT PER SRM.Apr 25, 2012 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2012042703487Web · corrodedFLOOR WEB CORRODED BETWEEN BS 220 TO BS 209, BL 0. REPAIRED WEB PER SRM.Apr 25, 2012 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2012042703484Floor Support · corrodedFLOOR SUPPORT CORRODED AT BS 220, BETWEEN LBL 29 TO LBL 17. REPAIRED SUPPORT PER SRM.Apr 25, 2012 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2012042703483Stringer · corrodedSTRINGER CORRODED AT BS 954, STR 29L. REPAIRED STRINGER PER SRM.Apr 25, 2012 · N892AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR SWAA2012042703482Frame · corrodedFRAME CORRODED AT BS 927, BETWEEN STR 30R TO STR 29R. REPAIRED FRAME PER SRM.Apr 25, 2012 · N892AT · Boeing 717200 · Fuselage Main, FrameSDR SWAA2012042703479Floor Support · corrodedFLOOR SUPPORT CORRODED BETWEEN BS 198 TO BS 220, RBL 45. REMOVED AND REPLACED SUPPORT IAW SRM.Apr 25, 2012 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2012042703478Floor Support · corrodedFLOOR SUPPORT CORRODED AT BS 220, BETWEEN BL 0 TO LBL 6. REMOVED AND REPLACED SUPPORT IAW SRM.Apr 25, 2012 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2012042703477Floor Support · corrodedFLOOR SUPPORT CORRODED AT BS 220, BETWEEN RBL 9 TO RBL 38. REMOVED AND REPLACED SUPPORT IAW SRM.Apr 25, 2012 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2012042703476Frame · corrodedFRAME CORRODED AT BS 954, RBL 2. REPAIRED FRAME PER SRM.Apr 25, 2012 · N892AT · Boeing 717200 · Fuselage Main, FrameSDR SWAA2012042703475Floor Support · corrodedFLOOR SUPPORT CORRODED AT BS 218, LBL 45. REMOVED AND REPLACED SUPPORT IAW SRM.Apr 25, 2012 · N892AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2012042703474Frame · corrodedFRAME CORRODED AT BS 927, BETWEEN STR 29L TO STR 29R. REPAIRED FRAME PER SRM.Apr 25, 2012 · N892AT · Boeing 717200 · Fuselage Main, Frame
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