N546AS

Service difficulty reports · 126

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 = 'N546AS' 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 ASAA2016081817760Light · inoperativeLT FWD OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. RELAMPED LT FWD OVERWING EMERGENCY LIGHT, REF AMM 33-51-04. OPS CHECK GOOD.Aug 18, 2016 · N546AS · Boeing 737890 · Emergency LightingSDR ASAA2016050216600Light · unsecureROW 12 EMERGENCY LIGHT BUCKLED. ACFT GROUNDED. SECURED THE LIGHT IAW AMM 33-51-15-960-801.May 2, 2016 · N546AS · Boeing 737890 · Emergency LightingSDR ASAA2016032616125Bulkhead Web · crackedPOSSIBLE CRACK ON RT WHEEL WELL FORWARD BULKHEAD, NEAR THE TOP, IT IS LOCATED JUST ABOVE THE SPOILER HYD CONTROL VALVE. ACFT GROUNDED. REMOVED DAMAGE AND ACCOMPLISHED REPAIR IAW SRM 57-10-10-2R-3, REPAIR 3. REPAIR IS A CATEGORY B REPAIR. THRESHOLD IS AT 56Mar 26, 2016 · N546AS · Boeing 737890 · Fuselage Main, BulkheadSDR ASAA2016030515821Floorbeam · crackedFWD CARGO COMPARTMENT, LT FLOOR SUPPORT BAFFLE CLIP AT AFT SIDE OF BS 500H FRAME IS CRACKED. ACFT GROUNDED. R & R LT FLOOR SUPPORT BAFFLE CLIP AT AFT SIDE OF BS 500H AND DISPLACED AND REINSTALLED LT BAFFLE BS 500H TO 500I IAW SRM 51-40-02, 51-10-02, PARA 9 , Mar 5, 2016 · N546AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2016030515820Floorbeam · crackedFORWARD CARGO COMPARTMENT, LT FLOOR SUPPORT BAFFLE CLIP AT FORWARD SIDE OF BS 500H FRAME IS CRACKED. ACFT GROUNDED. R & R LT FLOOR SUPPORT BADDLE CLIP AT FORWARD SIDE OF BS 500H FRAME AND REMOVED AND REINSTALLED LT BAFFLE BS 500G TO 500H IAW SRM 51-40-02, 51-Mar 5, 2016 · N546AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2016030415819Floorbeam · crackedFORWARD CARGO COMPARTMENT, LT FLOOR SUPPORT BAFFLE CLIP AT AFT SIDE OF BS 500G FRAME IS CRACKED. ACFT GROUNDED. R & R LT FLOOR SUPPORT BAFFLE CLIP AT AFT SIDE OF BS 500G FRAME IAW SRM 51-10-02 AND 51-10-02, PARA 9 AND BAC DWG 143A7505, REV B .Mar 4, 2016 · N546AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2016030415818Floorbeam · crackedFORWARD CARGO COMPARTMENT, LT FLOOR SUPPORT BAFFLE CLIP AT FORWARD SIDE OF BS 500G FRAME IS CRACKED. ACFT GROUNDED. R & R LT FLOOR SUPPORT BAFFLE CLIP AT FORWARD SIDE OF BS 500G FRAME AND DISPLACED AND REINSTALLED LT BAFFLE BS 500F TO 500G IAW SRM 51-40-02 AMar 4, 2016 · N546AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2016022615828Web · crackedAFT CABIN FLOOR, GALLEY 4B SUPPORT, LT WEB IS CRACKED. ACFT GROUNDED. R & R WEB IAW SRM 51-10-02, SRM 57-40-02 AND DWG 147A5700.Feb 26, 2016 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016022615816Intercostal · crackedMAIN CABIN FLOOR FORWARD WET AREA, STABILIZATION INTERCOSTAL AT BL 0, BS 277-294 IS CRACKED. ACFT GROUNDED. R & R MAIN CABIN FLOOR FORWARD WET AREA STABILIZATION INTERCOSTAL AT BL 0, STA 277-294 IAW SRM 51-40-02 AND SRM 53-10-51-01-2, DWG 141A5400, REV A. REFeb 26, 2016 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016022415813Web · corrodedL2 DOOR SURROUND LOWER AUXILIARY SILL WEB IS CORRODED AT APPROXIMATELY BS 990, AT GROUND BLOCK LOCATION. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-70-15-1A-1, ORIGINAL MATERIAL THICKNESS IS 0.040", REMOVED 0.006 ", REMAIFeb 24, 2016 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016022315827Web · crackedWHILE ACCOMPLISHING STRUCTURE, OPEN UP FOR BS986.5 FLOORBEAM REPAIR: FOUND SHEAR WEB AT BS 986 TO 1016, RBL 45-60, CORRODED AND CRACKED. ACFT GROUNDED. R & R RT G4 GALLEY SUPPORT WEB IAW SRM 51-10-02, PARA 9, 51-40-02, AND BAC DWG 147A5700, REV B. NO CORROFeb 23, 2016 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016021715858Floorbeam · gougedMAIN CABIN, FLOORBEAM DOUBLER GOUGED FS 540-RBL 26-43. ACFT GROUNDED. REMOVED GOUGED FLOORBEAM DOUBLER AND REPLACED WITH NEW DOUBLER IAW SRM 51-40-02 AND 143A5240, REV B. REMOVED DOT.Feb 17, 2016 · N546AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2016021615823Floorbeam · corrodedMAIN CABIN FLOORBEAM HAS CORROSION AT FASTENER HOLES BS 986.5-RBL 30, RBL 43. ACFT GROUNDED. CUT AND REMOVED LT AND RT DAMAGE FLANGE IAW SRM 53-70-51-2R-4, MATERIAL ID FOR ITEM SHEAR TIE BAC1506-4480, FOR ITEM NR 1 T-CHORD. BAC 1505-101474, FOR ITEM 5 IS BAC Feb 16, 2016 · N546AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2016021615805Shield · corrodedAFT PIT TRANSITION WEB AT BS 767-787, RT SIDE CORRODED TOP AND BOTTOM. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02, ORIGINAL MATERIAL .050 IAW SRM 53-60-15 MATERIAL REMOVED .023, REMAINING .027 OUT OF LIMITS IAW SRM 53-60-15, UT GAGE NR T8225S. R &Feb 16, 2016 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016021515859Floorbeam · corrodedCORROSION ON TOP AND BOTTOM OF FLOORBEAM, BS 896, LBL 30. ACFT GROUNDED. PERMANENT REPAIR HAS BEEN ACCOMPLISHED IN JC G642737, OPS 28714. REMOVED DOT. REMOVED CORROSION, ORIGINAL MATERIAL 0150 THICK, REMOVED .031 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51.Feb 15, 2016 · N546AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2016021515856Structure · crackedINTERCOSTAL BETWEEN FLOOR SUPPORTS BS 311-329, RBL 32 CRACKED AT 2 UPPER FLOORBOARD ATTACH HOLES. ACFT GROUNDED. R & R 141A5410-12 INTERCOSTAL IAW SRM 51-40-02 AND SRM 51-40-05.Feb 15, 2016 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016021515807Floor Support · corrodedFLOOR SUPPORT BS 312-320, LBL 12 HAS LIGHT SURFACE CORROSION. ACFT GROUNDED. REMOVED AND THE FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 141A5400, REV.Feb 15, 2016 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016021315732Rib · crackedRIGHT HORIZONTAL STABILIZER IN-SPAR RIB STIFFENER, 2 EA, CRACKED DOT ATTACHED, HSS 92 - HSS 92.7. ACFT GROUNDED. REMOVED DAMAGE AT 2 EA STIFFENERS ON RT HORIZONTAL STABILIZER IN-SPAR RIB AT STABILIZER BS 92.7 AND ACCOMPLISHED PERMANENT REPAIRS IAW SRM 55-10Feb 13, 2016 · N546AS · Boeing 737890 · Horizontal Stabilizer, Spar/RibSDR ASAA2016021215826Strip · corrodedPARTS RACK, AFT CARGO COMPARTMENT CAPSTRIP, PN 453A2611-4 IS CORRODED, 4 LT. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2, ORIGINAL MATERIAL THICKNESS IS 0.063", REMAINING THICKNESS IS 0.055", REMOVED 0.008". REPLAFeb 12, 2016 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016021215825Strip · corrodedPARTS RACK, AFT CARGO COMPARTMENT CAPSTRIP, PN 453A2611-11 IS CORRODED, NR 3 RT. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2, ORIGINAL MATERIAL THICKNESS IS 0.063", REMAINING THICKNESS IS 0.054", REMOVED 0.009". REFeb 12, 2016 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016021215822Strip · corrodedAFT CARGO COMPARTMENT CAPSTRIP, PN 453A2611-10 IS CORRODED, NR 3 LT . ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2, REPLACED CAPSTRIP IAW SRM 51-10-02, PARA 9.Feb 12, 2016 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016021015719Skin · crackedCRACK INDICATION ON RT HORIZONTAL STABILIZER LOWER SKIN, BS 101.9, 4" FWD OF EXISTING REPAIR ON AFT SPAR, APPROXIMATELY .5" IN LENGTH. ACFT GROUNDED. REMOVED DAMAGED AREA & ACCOMPLISH REPAIR IAW SRM 55-10-01-2R-11.Feb 10, 2016 · N546AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2015021210686Skin · crackedFOUND CRACK ON LT HORIZONTAL STAB LOWER SKIN AT STAB, STA 101.9 37' FROM THE L/E. ACFT GROUNDED. REPAIR INCORPORATED INTO CUSTOMER CARD NR G450012, OPS 42012. ALL WORK ACCOMPLISHED ON CUSTOMER CARD NR G450012.Feb 12, 2015 · N546AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2015021210677Skin · crackedFOUND CRACK ON LT HORIZONTAL STAB LOWER SKIN AT STAB STA 101.9 19' FROM THE L/E. ACFT GROUNDED. REPAIRED CRACKED SKIN IAW SRM 55-10-01.Feb 12, 2015 · N546AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2015021210666Skin · crackedTWO .7500" CRACKS FOUND ON LT HORIZONTAL STAB LOWER SKIN AT STAB STA 101.9 APPROXIMATELY 19" FROM L/E AND AT STAB STA 101.9 APPROXIMATELY 37" FROM L/E. ACFT GROUNDED. REPAIRED CRACKED SKIN IAW SRM 55-10-01-2R-11.Feb 12, 2015 · N546AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2014120309855Lens · brokenEMERGENCY LIGHT EXIT LOCATOR SIGN ADJACENT TO RT FORWARD OVERWING EXIT HAS BROKEN LENS. ACFT GROUNDED. REPLACED LENS AND TESTED, MM 33-51-01-960-801, OPS NORMAL.Dec 3, 2014 · N546AS · Boeing 737890 · Emergency LightingSDR ASAA2014101809423Sign · missingEXIT SIGN AT 16F MISSING. ACFT GROUNDED. INSTALLED THE EXIT SIGN IAW AMM TASK 33-51-01-960-801.Oct 18, 2014 · N546AS · Boeing 737890 · Emergency LightingSDR ASAA2014072415621Skin · dentedDENT ON FUSELAGE SKIN ON STR S22R AT APPROXIMATELY FS 306, RT SIDE. ACFT GROUNDED. RESOLVED ON W/O: 254932, TASKCARD: N/R-00003. REMOVED AND REINSTALL AIR DUCT FROM ELECTRONIC EQUIPMENT COMPARTMENT TO GET ACCESS IAW SRM 51-40-02 SWPM 20-10-12. REPAIR VERIFIJul 24, 2014 · N546AS · Boeing 737890 · Fuselage Main, Plate/SkinSDR ASAA2014072415620Skin · dentedDENT ON FUSELAGE SKIN ON STR S22R AT APPROXIMATELY FS 306, RT SIDE. ACFT GROUNDED. RESOLVED ON W/O: 254932, TASKCARD: N/R-00003. REMOVED AND RE-INSTALL AIR DUCT FROM ELECTRONIC EQUIPMENT COMPARTMENT TO GET ACCESS IAW SRM 51-40-02, SWPM 20-10-12. REPAIR VERIJul 24, 2014 · N546AS · Boeing 737890 · Fuselage Main, Plate/SkinSDR ASAA2014051207947Channel · corrodedAFT PIT, RT TRANSITION PANEL CORRODED AT FASTENER HOLES INCLUDING HOLES UNDER SIDEWALL PANELS, FS 272-792. ACFT GROUNDED. REMOVED AFT CARGO PIT RT TRANSITION PANEL IAW SRM 51-40-02. MATERIAL ID FOR CHANNEL, SIDE PLATE AND SPLICE BAC1496-377 7075 T62 IAW SRMMay 12, 2014 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2014051207956Transition Panel · corrodedFWD CARGO BAY RT TRANSITION PANEL HAS KNIFE MARKS ENTIRE LENGTH OF PIT. ACFT GROUNDED. BLENDED KNIFE MARKS AND CORROSION, ORIGINAL MATERIAL .040" MAT LOSS .009 REMAINING .031 IAW SRM 53-30-53 & 53-00-53 FOUND OUT OF LIMITS TOOL T8225M. REMOVED TRANSITION PANMay 12, 2014 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2014051207954Transition Panel · corrodedAFT PIT, LT TRANSITION PANEL CORRODED AT FASTENER HOLES INCLUDING HOLES UNDER SIDEWALL PANELS. FS 272-849. ACFT GROUNDED. R & R AFT PIT LT TRANSITION PANEL IAW SRM 53-00-53-2R-5 AND SRM 51-40-02.May 12, 2014 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2014051207944Skin · crackedFOUND CRACK ON RT HORIZONTAL STAB LOWER SURFACE APPROX 2.125' LONG, JUST FORWARD OF THE AFT SPAR BETWEEN STABILIZER STA 92.7 AND STABILIZER STA 101.9. AREA MARKED IN RED. ACFT GROUNDED. REPAIRED RT HORIZONTAL STAB LOWER SKIN IAW SRM 55-10-01-2R-11. REMOVED RMay 12, 2014 · N546AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2014051207943Skin · crackedFOUND CRACK ON LT HORIZONTAL STAB LOWER SURFACE APPROX 0.75' LONG, 18' FORWARD OF THE AFT SPAR JUST INBD OF STAB STA 101.9. AREA MARKED IN RED. ACFT GROUNDED. REPAIRED LT HORIZONTAL STAB LOWER KSIN IAW SRM 55-10-01-2R-11. REMOVED RED MARKS.May 12, 2014 · N546AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2014050807948Web · corrodedFWD CARGO BAY LOWER DOOR SILL WEB IS CORRODED. ACFT GROUNDED. R & R LOWER DOOR SILL WEB IAW SRM 51-40-02, REF DWG BAC 143A8120, REV D.May 8, 2014 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2014050807734Web · corrodedAFT CARGO DOOR LOWER SILL WEB IS CORRODED. ACFT GROUNDED. REMOVED CORROSION IAW SRM 53-60-15-1A-1 AND FOUND WITHIN ALLOWABLE LIMITS. ALODINED IAW SRM 51-20-01. PRIMED IAW SOPM 20-41-02. APPLIED TOPCOAT IAW SRM 51-20-01 MARKED CORROSION AREA IAW AMM 51-05-01.May 8, 2014 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2014050607972Power Supply · no testEMERGENCY LIGHT POWER SUPPLY M1675 FAILS DEEP CYCLE TEST. ACFT GROUNDED. R & R EMERGENCY LIGHT POWER SUPPLY M1674 IAW AMM 33-51-06. POWER SUPPLY OPS CHECK GOOD IAW AMM 33-51-06, ITEM 5.May 6, 2014 · N546AS · Boeing 737890 · Emergency LightingSDR ASAA2014040807484Hinge · lack of lubeL2 DOOR STUCK HALF WAY OPEN. ACFT GROUNDED. PERFORMED AFT ENTRY DOOR CHECK IAW MM 52-13-00. LUBED AFT UPPER HINGE IAW AMM 12-25-12. DOOR OPENS AND CLOSES NORMALLY. NO FURTHER DEFECTS NOTED.Apr 8, 2014 · N546AS · Boeing 737890 · Fuselage, Door HingeSDR ASAA11510254Skin · damagedAPPROX 3' HOLE IN AIRCRAFT SKIN APPROXIMATELY 4FT DWD OF L1 DOOR ON GREEN STRIPE. REPAIRED AREA BY ROUTING OUT DAMAGED AREA AND APPLYING FILLER AND EXTERNAL DOUBLER IAW TIMCO REO G13981 REV A DATED 08 17 2011 AND ASA EA800 53 06101.Aug 14, 2011 · N546AS · Boeing 737890 · Fuselage Main, Plate/SkinSDR ASAA1058472Intercostal · crackedINTERCOSTAL CRACKED ON UPPER FLANGE FS 312. REMOVED AND REPLACED INTERCOSTAL.Oct 21, 2010 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA1058015Bearing · lack of lubeDURING MANEUVERING FOR LANDING ON SHORT FINAL WHILE APPLYING AILERON TO ROLL LEFT YOKE MOMENTARY LOCKED AND REQUIRED EXCESSIVE FORCE TO OBTAIN DESIRED ROLL INPUT F/O HAND FLYING DURING FAULT. ISOLATION/TROUBLESHOOTING FOUND SIGNIFICANT NOISE CLICKING COMING FJun 28, 2010 · N546AS · Boeing 737890 · Aileron Control SystemSDR ASAA0954804Floor Panel · corrodedAFT CARGO BAY NR 5 FLOOR PANEL CORROSION. REMOVED AND REPLACED WITH NEW FABRICATED FLOOR PANEL.Mar 18, 2009 · N546AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA0954806Floor Panel · corrodedAFT CARGO BAY NR 3 FLOOR PANEL CORROSION. REMOVED AND REPLACED WITH NEW FABRICATED FLOOR PANEL.Mar 18, 2009 · N546AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA0954805Floor Panel · corrodedAFT CARGO BAY NR 4 FLOOR PANEL CORROSION. REMOVED AND REPLACED WITH NEW FABRICATED FLOOR PANEL.Mar 18, 2009 · N546AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA0954803Floor Panel · corrodedAFT CARGO BAY NR 2 FLOOR PANEL CORROSION. REMOVED AND REPLACED WITH FABRICATED NEW FLOOR PANEL.Mar 18, 2009 · N546AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA0954802Floor Panel · corrodedAFT CARGO BAY NR 1 FLOOR PANEL CORROSION. REMOVED AND REPLACED WITH NEW FABRICATED FLOOR PANEL.Mar 18, 2009 · N546AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA0954762Threshold · crackedFWD CARGO BAY DOOR CUTOUT FWD CORNER THRESHOLD IS CRACKED. REMOVED AND REPLACED WD CARGO BAY DOOR CUTOUT FWD CORNER.Mar 16, 2009 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA0954761Threshold · crackedFWD CARGO BAY DOOR CUTOUT AFT CORNER THRESHOLD IS CRACKED. REMOVED AND REPLACED FWD CARGO BAY DOOR CUTOUT AFT CORNER THRESHOLD.Mar 16, 2009 · N546AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA0954764Floorbeam · corrodedAFT CARGO FLOORBEAM AT BS 727I+4 RBL 8. REPAIRED AFT CARGO FLOOR BEAM AT BS 727I+4 RBL 8Mar 16, 2009 · N546AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA0954767Floorbeam · corrodedAFT CARGO FLOORBEAM CORRODED AT BS 767+4 LBL 12. REPAIRED AFT CARGO FLOOR BEAM AT BS 767+4 LBL 12Mar 16, 2009 · N546AS · Boeing 737890 · Fuselage Main, Floor Beam
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