N520AS

Service difficulty reports · 63

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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 = 'N520AS'
  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 ASAA2025030456607Skin · puncturedFUSELAGE SKIN STA 950 STR 23R-24R HAS PUNCTURE. GROUNDED - YES. CUT OUT PUNCTURE AND REMOVED DAMAGED SHEAR TIE AT STA 947.5 STR 23R-24R IAW B737-800 SRM 51-10-02, SRM 51-40-02. REPAIRED SKIN, FABRICATED NEW SHEAR TIE AND INSTALLED IAW ASA EA 800-53EA-28409 ANDMar 4, 2025 · N520AS · Boeing 737890 · Fuselage Main, Plate/SkinSDR ASAA2025021356543Floor Panel · mechanic errorFLOOR PANEL 241RF HAS MISALIGNED FASTENER HOLE. GROUNDED - YES. COMPLETED WET LAY UP REPAIR ON FLOOR PANEL 241RF IAW B737-800 SRM 53-00-50-2R-6. FLOOR PANEL 241RF ON CUSTOMER CARD G2103934.Feb 13, 2025 · N520AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2025020756443Rib · crackedREQ'S ACCESS @ STA 111.10 FOR 4(EA) CRACKS IN RIB, REPAIR 11 REQUIRED. GROUNDED - YES. REMOVED EXISTING REPAIR CUTOUT HORIZONTAL SKIN FOR ACCESS, ACCOMPLISHED HFEC OF CUTOUT, CLEANED EXISTING REPAIR HOLES, ACCOMPLISHED OPEN HOLE HFEC, FABRICATED AND INSTALLED Feb 7, 2025 · N520AS · Boeing 737890 · Horizontal Stabilizer, Spar/RibSDR ASAA2025020456545Floor Panel · damagedFLOOR PANEL PN 146A5810-466 REQUIRES 2 INSERTS,. GROUNDED - YES. REPAIRED FLOOR PANEL 146A5810-466 OF 2 INSERTS IAW B737-800 SRM 53-00-50-2R-0.Feb 4, 2025 · N520AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2025020456235Angle · corrodedFWD CARGO PIT, R/H FROM STA 500C TO 500I, TRANSITION ANGLE HAS CORROSION ON TOP SURFACE. GROUNDED - YES. EVALUATED & REMOVED DAMAGE ON FWD CARGO PIT R/H TRANSITION @ STA 500C -500I, ORIGINAL: .040 , REMOVED: .040, REMAINING: .000 AND FOUND TO BE OUT OF LIMITS Feb 4, 2025 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2025020456160Channel · corrodedFWD CARGO PIT, L/H AT STA 500C TO 500I, TRANSITION ANGLE HAS CORROSION ON TOP SURFACE AT FASTENER HOLES, MARKED. GROUNDED - YES. REMOVED CORROSION ORIGINAL THICKNESS .040, REMOVED .040, REMAINING .000. FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2. Feb 4, 2025 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2025020456159Angle · corrodedFWD CARGO PIT, STA 500I AT AFT BULKHEAD TO FLOOR PANEL ANGLE HAS CORROSION AT FASTENER HOLES FOR PANEL. GROUNDED - YES. EVALUATED ORIGINAL MATERIAL THICKNESS .071, REMOVED .071, REMAINING .000 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-30Feb 4, 2025 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2025020456154Door Sill · corrodedFWD CARGO PIT, CARGO DOOR SILL STRUCTURE ON TOP HAS CORROSION MARKED. GROUNDED - YES. EVALUATED AREA AND REMOVED DAMAGE, ORIGINAL: .045, REMOVED: .012, REMAINING: .033 & IS FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 51-60-15-1A-1. REMOVED DAMAGED THRESHOLD WEBFeb 4, 2025 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2025020456149Angle · corrodedFWD CARGO PIT, R/H AT STA 500A TO 500C, TRANSITION ANGLE HAS CORROSION AT FASTENER HOLES, MARKED. GROUNDED - YES. EVALUATED AND REMOVED DAMAGE ON FWD CARGO PIT R/H TRANSITION @ STA 500A-500C , ORIGINAL : .040 , REMOVED : .040, REMAINING: .000 AND FOUND TO BE OFeb 4, 2025 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2025020356155Housing · gougedR2 DOOR, EXTERIOR HANDLE PAN INSIDE DIAMETER IS GOUGED AND CORRODED. GROUNDED - YES. REMOVED GOUGED SEAL PLATE IAW B737-800 SRM 51-40-02 AND INSTALLED NEW SEAL PLATE P/N: 149A6121-1; P.O. 1113263.1 IAW B737-800 SRM 51-40-02; AND REMOVED CORROSION AND FOUND WITFeb 3, 2025 · N520AS · Boeing 737890 · Service DoorsSDR ASAA2025020256157Shield · corrodedAFT CARGO PIT FWD SHIELD HAS CORROSION. GROUNDED - YES. EVALUATED, REMOVED CORROSION, ORIGINAL MATERIAL THICKNESS .050, REMOVED .021 REMAINING .029, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-60-15-1A-1. REMOVED DAMAGED SHIELD, INSTALLED NEW AFT PIT FWD SHIFeb 2, 2025 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2025020256156Web · corrodedAFT CARGO PIT THRESHOLD WEB HAS CORROSION. GROUNDED - YES. REMOVED CORROSION ON AFT CARGO THRESHOLD WEB, ORIGINAL MATERIAL THICKNESS .050, REMOVED .020, REMAINING .030, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-60-15-1A-1. REMOVED DAMAGED WEB, LOCATED AND Feb 2, 2025 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2025020255873Support · corrodedAFT CARGO PIT L/H TRANSITION HAS MULTIPLE SPOTS OF CORROSION FROM STATION 727-727D+15. GROUNDED - YES. REMOVED CORROSION ORIGINAL MATERIAL THICKNESS .040, REMOVED .040, REMAINING .000 FOUND TO BE OUT OF LIMITS DUE TO 100% MATERIAL LOSS IAW B737-800 SRM 53-00-5Feb 2, 2025 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2025020156158Floorbeam · corrodedFLOOR BEAM STA 344 HAS CORROSION @ LBL 11.10. GROUNDED - YES. DAMAGE REMOVED AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-10-51-0I-2 & SRM 53-10-51-1A-1 REF BAC 1518-1218 REV:-.ORIG:175". REMOVED 047", REMAINING .128". BLO STA344-360, LBL 11.10 STA 344-36Feb 1, 2025 · N520AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2025020155874Channel · corrodedAFT CARGO PIT R/H TRANSITION HAS MULTIPLE SPOTS OF CORROSION FROM 727 - 767. GROUNDED - YES. REMOVED CORROSION ORIGINAL THICKNESS .040, REMOVED .040 , REMAINING .000. FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-55-1A-2. REMOVED DAMAGED TRANSITION PANEL. FFeb 1, 2025 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2025013056109Floor Panel · delaminatedFLOOR PANEL PN 147A5810-23, HAS A DELAMINATION. GROUNDED - YES. PERFORMED PERMANENT REPAIRS ON FLOOR PANEL PN: 147A5810-23 IAW ASA B737-800 SRM 53-00-50-2R-0, ASA B737-800 SRM 53-00-50-2R-1, ASA B737-800 SRM 53-00-50-2R-7 & ASA B737-800 SRM 53-00-50-1A-1. NO FJan 30, 2025 · N520AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2025012956306Rib · crackedR/H HORIZONTAL STABILIZER INTERNAL, RIB AT SS 111.10 CRACKED 4 PLACES AT VERTICAL STIFFENERS GROUNDED - YES. REMOVED DAMAGE @ STA 92.70 RIB AT 4EA LOCATION. ACCOMPLISHED HFEC OF 4EA CUTOUTS, HEAT TREATED, FABRICATED, AND INSTALLED REPAIR PARTS PN: BAC1490-279Jan 29, 2025 · N520AS · Boeing 737890 · Horizontal Stabilizer, Spar/RibSDR ASAA2024021977884Battery Pack · no testWHILE PERFORMING TC 78233001 FOUND 3 EMERGENCY LIGHT FAILED. GROUNDED - YES. REPLACED BATTERY PACKS IAW AMM 33-51-06. OPS CHECKS GOOD.Feb 17, 2024 · N520AS · Boeing 737890 · Emergency LightingSDR ASAA2023013141888Fitting · cracked# 2 ENG AFT PYLON FAIRING AFT FITTING CRACKED. GROUNDED - YES. REPAIRED IAW B737-800 SRM 54-50-70-2R-6.Jan 31, 2023 · N520AS · Boeing 737890 · Nacelle/Pylon, Main FrameSDR ASAA2023011311507Lamp · inoperativeEMERGENCY EXIT LIGHTS LEFT SIDE ROW 16 INOP. GROUNDED - YES. RELAMPED PER B737-800 AMM 33-51-01. LIGHT ILLUMINATES NORMALLY.Jan 11, 2023 · N520AS · Boeing 737890 · Emergency LightingSDR ASAA2021021234195Skin · crackedRH HORIZONTAL LOWER SKIN CRACKED AT REAR SPAR AND STA 97. GROUNDED - YES. REMOVED EXISTING REPAIR, CUTOUT DAMAGED,FABRICATED,LOCATED,DRILLED & INSTALLED NEW REPAIR PARTS IAW B737-800 SRM 55-10-01-2R-11 REPAIR 11 THIS IS A CAT B REPAIR WITH AN INTERVAL INSPECTIFeb 12, 2021 · N520AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2020011331844Light · inoperativeEMERGENCY LIGHT EXIT LOCATOR SIGN AT RIGHT FORWARD OVERWING EXIT HAS LAMPS INOP. GROUNDED - YES. RELAMPED AND TESTED PER AMM 33-51-01-960-801 - OPS NORMAL.Jan 12, 2020 · N520AS · Boeing 737890 · Emergency LightingSDR ASAA2019031828659Battery Pack · dischargedLT FWD OVERWING EMERGENCY EXIT LIGHT INOP. GROUNDED - YES. REMOVED AIR GRILLE AT STA 565 LBL68 IAW AMM 21-23-03-00-801, REMOVED AND REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY AND BATTERY PACK M1694 AND INSTALLATION TEST GOOD IAW AMM 33-51-06-960-805 AND AMM 33Mar 18, 2019 · N520AS · Boeing 737890 · Emergency LightingSDR ASAA2019031628623Power Supply · inoperativeMAIN CABIN FWD ENTRY CEILING AND L1 DOOR HEADER EXIT LIGHTS INOP. GROUNDED - YES. REPLACED POWER SUPPLY OPS CK GOOD IAW AMM 33-51-06.Mar 16, 2019 · N520AS · Boeing 737890 · Emergency LightingSDR ASAA2019022738366Floorbeam · wornMAIN CABIN FLOOR STRUCTURE, STA 520 FLOORBEAM UPPER T-CAP HAS DEEP WEAR MARK APPROX. RBL 10. GROUNDED - YES. REMOVED DAMAGE TO UPPER T CAP REF: B737-800 SRM 53-00-51-2R-1. ORIGINAL MATERIAL .125 MATERIAL REMOVED 100%, LOCATED AND DRILLED REPAIR ANGLES #1 AND #Feb 13, 2019 · N520AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2019020928605Transition Panel · corrodedFWD. CARGO COMPARTMENT RT TRANSITION PANEL HAS CORROSION STA.500F TO STA.500G LBL.24. MARKED IN RED. GROUNDED - YES. REMOVED CORROSION ON RT TRANSITION PNL ORG MAT .040 REMOVED .007 REMAINING .033 AND FOUND TO BE OUT OF LIMITS IAW DWG #BAC1496-444 AND SRM 51-1Feb 9, 2019 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2019020828580Transition Panel · corrodedAFT PIT, LT TRANSITION PANEL HAS CORROSION 4 PLACES BETWEEN STA 727I AND 727J. GROUNDED - YES. REMOVED CORROSION ORG THICKNESS .040 REMOVED .007 REMAINING .033 FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 AND DWG BAC1496-444 TOOL# T8225P. REMOVED TRANSITION PNL SFeb 8, 2019 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2018102126559Power Supply · inoperativeR1 DOOR INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP. GROUNDED - YES. REMOVED AND REPLACED FWD RIGHT EMERGENCY POWER SUPPLY REF AMM 33-51-06 OP CK GOOD.Oct 21, 2018 · N520AS · Boeing 737890 · Emergency LightingSDR ASAA2018012323275Light · inoperativeFOUND LT FWD (L1) EMERGENCY SLIDE LIGHT INOP. GROUNDED - YES. REMOVED AND REPLACED L1 EMERGENCY SLIDE LIGHT BULB REF AMM 33-51-04. OPS CHECK GOOD.Jan 23, 2018 · N520AS · Boeing 737890 · Emergency LightingSDR ASAA2017100822144Lens · missingAFT EMERGENCY SIGN LENS MISSING FROM BULKHEAD. ACFT GROUNDED. INSTALLED A NEW LENS AMM 33-51-14.Oct 8, 2017 · N520AS · Boeing 737890 · Emergency LightingSDR ASAA2017041320493Skin · crackedRT HORIZ STAB LOWER SKIN WAS FOUND TO HAVE A 1IN CRACK AT STA 101.90. GROUNDED - YES. REPAIRED RT HORIZ STAB LWR SKIN AT STA 101.90 IAW SRM 55 10 01 2R 11 REPAIR 11 THIS IS A CAT B REPAIR.Apr 13, 2017 · N520AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2017020121293Stop Fitting · crackedL1 DOOR HAS UPPER FWD STOP BEARING PLATE CRACKED/DAMAGED. GROUNDED - YES. REMOVED AND REPLACED L1 DOOR UPPER FWD STOP BEARING PLATE, REF AMM 52-11-01/401.Feb 1, 2017 · N520AS · Boeing 737890 · Passenger/Crew DoorsSDR ASAA2017011119328Battery Pack · failedEMERGENCY LIGHTING SWITCH OPERATIONAL CHECK AND BATTERY PACKS - FUNCTIONAL CHECKS ILLUMINATED. ALL EMERGENCY LIGHTS FROM AND INCLUDING OVERWING EMERGENCY EXIT ROWS AFT INCLUDING AFT GALLEY FAILED 15 MINUTE CHECK. ACFT GROUNDED. REMOVED AND REPLACED THE BATTJan 11, 2017 · N520AS · Boeing 737890 · Emergency LightingSDR ASAA2016032516101Power Supply · failed2 BATTERY PACKS FAILED EMERGENCY EXIT DEEP CYCLE TEST, FWD AND AFT. ACFT GROUNDED. R & R BATTERY PACKS M1673 AND M1675, REF WDM 33-51-11. OPS TEST NORMAL, REF AMM 33-51-00. ACCESS AREA CHECKED SECURED. INSTALLED TAMPER SEAL AFT ACCESS PANEL.Mar 25, 2016 · N520AS · Boeing 737890 · Emergency LightingSDR ASAA2016032516099Module · failedELECTRICAL ODOR IN CABIN. F/A'S TURNED OFF CABIN LIGHTS. NO C/B'S POPPED IN GALLEYS. NOTHING MELTING IN OVEN. RAN SMOKE/FUMES CHECKLIST. WITH LIGHTS OFF, IFF, PASSENGER AND CABIN UTIL POWER OFF, RECIRC FANS OFF, ODOR DISSIPATED. ACFT GROUNDED. DIVERSION -Mar 25, 2016 · N520AS · Boeing 737890 · Passenger Compartment LightingSDR ASAA2015072412580Lamp · inoperativeR1 EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMP IN THE R1 EXTERIOR EMERGENCY EXIT LIGHT AND LAMP TESTED GOOD IAW AMM 33-51-04-960-801.Jul 24, 2015 · N520AS · Boeing 737890 · Emergency LightingSDR ASAA2015070912445Intercostal · crackedFWD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 500C - 500D. ACFT GROUNDED. R & R THE INTERCOSTAL IAW SRM 51-40-02-OG-0 AND DWG 1437505, REV.Jul 9, 2015 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015070712492Intercostal · corrodedAFT CARGO BAY INTERCOSTAL AT RBL 21, BS 747 TO 767 IS CORRODED. ACFT GROUNDED. REMOVED CORROSION IAW SRM 53-60-15-1A-1, 4C, 2B. REMOVED INTERCOSTAL IAW SRM 51-40-02. FABRICATED A NEW INTERCOSTAL IAW DWG 146A7505, REV-, AND INSTALLED IAW SRM 51-40-02 & DWG Jul 7, 2015 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015070612398Floorbeam · crackedFLOORBEAM CRACKED, BS 540, RBL 3. ACFT GROUNDED. R & R IAW DWG 143A0060, REV A, SHEET 36.Jul 6, 2015 · N520AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2015070612397Floorbeam · crackedMAIN CABIN FLOORBEAM CRACKED, BS 540, LBL 3. ACFT GROUNDED. R & R IAW DWG 143A0060, REV A, SHEET 36.Jul 6, 2015 · N520AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2015070612370Floor Support · crackedFWD CABIN FLOOR SUPPORT CRACKED BS 312 - 328, RBL 31.5. ACFT GROUNDED. R & R THE FLOOR SUPPORT IAW DWG 141A5400, SHT 39, AND SRM 51-40-02.Jul 6, 2015 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015070612366Floor Support · crackedFWD CABIN FLOOR SUPPORT CRACKED, BS 344 - 360, BL 0. ACFT GROUNDED. R & R THE FLOOR SUPPORT IAW DWG 141A5400 SHT32, AND SRM 51-40-02.Jul 6, 2015 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015070612365Floor Support · crackedFWD CABIN FLOOR SUPPORT CRACKED BS 344 - 360, LBL 11.1. ACFT GROUNDED. R & R THE FLOOR SUPPORT IAW DWG 141A5400, SHT43, AND SRM 51-40-02.Jul 6, 2015 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015070612364Floor Support · crackedFWD CABIN FLOOR SUPPORT CRACKED BS 312 - 328, LBL 45.5. ACFT GROUNDED. R & R THE FLOOR SUPPORT IAW DWG 141A5400, SHT 26 AND IAW SRM 51-40-02. .Jul 6, 2015 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015070412510Transition Panel · corrodedAFT PIT LT TRANSITION PANEL HAS DOUBLE DRILLED HOLE BETWEEN BS 727C AND 727D. ACFT GROUNDED. LEFT TRANSITION PANEL HAD DOUBLE DRILLED HOLE AT STA 727G+10 AND CORROSION AT 727D, ORIGINAL MATERIAL = .040, REMOVED=.007, REMAINING=.033 BOTH FOUND OUT OF LIMITS IJul 4, 2015 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015070412491Transition Panel · crackedAFT CARGO BAY RT TRANSITION PANEL CRACKED AT BS 727J . ACFT GROUNDED. R & R AFT PIT RT REPAIR SECTION OF TRANSITION PANEL FROM BS 727I+10 TO 767 IAW SRM 53-00-53-2R-5.4.Jul 4, 2015 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015070412490Floor Support · corrodedAFT CARGO FLOOR SUPPORT HAS CORROSION BETWEEN BS 787 - 867, RBL 19. ACFT GROUNDED. REMOVED CORROSION, AND FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-10. R & R IAW DWG 146A0081, REV A, & SRM 51-40-02.Jul 4, 2015 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015070412407Transition Panel · crackedAFT CARGO BAY LT TRANSITION PANEL CRACKED AT BS 747. ACFT GROUNDED. REPAIRED THE TRANSTITION PANEL IAW SRM 53-00-53-2R-5.Jul 4, 2015 · N520AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015070312513Seat Track · crackedCRACK INDICATION AT 10 O'CLOCK POSITION ON OTBD AFT HOLE OF FORWARD SEAT TRACK RBL 24.75, STA 727B. ACFT GROUNDED. ALL WORK ACCOMPLISHED REF EA NR SB737-53-1296-NG-124, REV: NEW DATE 07/16/2015 AND REO-G19044, REV B, DATE 07/16/2015.Jul 3, 2015 · N520AS · Boeing 737890 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2015070312512Seat Track · crackedCRACK INDICATION AT 10 O'CLOCK POSITION ON INBD AFT HOLE OF FORWARD SEAT TRACK LBL45.50, STA 727B. ACFT GROUNDED. ALL WORK ACCOMPLISHED, REF EA SB737-53-1296-NG-124, REV: NEW DATE 07/16/2015 AND REO-G19044, REV B, DATE 07/16/2015.Jul 3, 2015 · N520AS · Boeing 737890 · Fuselage, Seat/Cargo Attach Fittings
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