N526AS

Service difficulty reports · 86

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 = 'N526AS' 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 ASAA2019082430500Floor Support · crackedMAIN CABIN FLOOR STRUCTURE INTERCOSTAL IS CRACK AT BS356 LBL11 AS MARK. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL AT LBL 11 STA 344 - STA 360 IAW DWG 141A5400 REV B AND B737-800 SRM 51-40-02.Aug 24, 2019 · N526AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2019082743499Floor Support · crackedMAIN CABIN FLOOR STRUCTURE INTERCOSTAL IS CRACK AT BS322 LBL46 AS MARK. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL AT LBL 46 STA 312-STA 328 IAW BOEING DWG141A5400 REV - AND B737-800 SRM 51-40-02.Aug 24, 2019 · N526AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2019083030541Web · corrodedAFT CARGO DOOR CUTOUT, LOWER WEB HAS CORROSION NUMEROUS SPOTS BETWEEN BS 794 AND BS 847. GROUNDED - YES. REMOVED DAMAGED LOWER WEB AT AFT CARGO DOOR CUTOUT AND REPLACED WITH NEW WEB IAW BOEING DWG #146A8340 REV-.Aug 23, 2019 · N526AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2019082130656Skin · crackedCRACK INBOARD OF RT STAB STA 175.50, LOWER SKIN, 10" FORWARD OF REARSPAR APPROX 1" IN LENGTH. MARKED. GROUNDED - YES. REMOVED LOWER SKIN AT CRACK LOCATION ON THE RIGHT HAND HORIZONTAL STABILIZER AT STAB STA 175.50, 10" FORWARD OF THE REAR SPAR IAW SRM 51-10-02Aug 21, 2019 · N526AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2019062649822Display · odorFLIGHT DECK HAS STRONG ELECTRICAL BURNING SMELL. ACFT GROUNDED. FOUND CAPTAIN'S FMCS CONTROL UNIT TO BE THE SOURCE OF ELECTRICAL SMELL. PULLED AND TAGGED 1 C/B. REMOVED AND REPLACED #1 FMCS CDU. RESET 1 C/B. OPS TEST GOOD. SOFTWARE CONFIRMED APPLICABLE. REF B7Jun 24, 2019 · N526AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2017082721744Lens · missing17A EXIT SIGN LENS MISSING. ACFT GROUNDED. REPLACED THE LENS, OPS NORMAL.Aug 27, 2017 · N526AS · Boeing 737890 · Emergency LightingSDR ASAA2017080921592Transition Panel · crackedAFT CARGO TRANSITION PANEL HAS TWO CRACKS AT BS 727H+15 - 727I+3, STRINGERS 25L - 26L. ACFT GROUNDED. REPAIRED THE TRANSITION PANEL IAW SRM 51-10-02, SRM 53-00-53-2R-S, SRM 51-40-02, AND DWG 146A7500 REV.Aug 9, 2017 · N526AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2017080321593Skin · crackedCRACK INDICATION FOUND ON THE LT HORIZONTAL STAB LOWER SKIN. ACFT GROUNDED. CUT OUT THE DAMAGED AREA AND FABRICATED REPAIR FILLERS AND DOUBLER AND INSTALLED IAW SRM 55-10-01-2R-11.Aug 3, 2017 · N526AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2017080321527Skin · crackedCRACK INDICATION FOUND ON THE LEFT HORIZONTAL STAB LOWER SKIN. LOCATED INBD OF ROW OF FASTENERS HSS 157.10, 8.5 INCHES FWD OF T/E SPAR, .980" LONG. ACFT GROUNDED. REPAIRED THE LOWER SKIN IAW SRM 55-10-01-2R-11, AND SRM 51-40-02. ALODINED IAW SRM 51-20-01, Aug 3, 2017 · N526AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2017041020426Lens · detachedVERTICAL EXIT SIGN AT 17A FOUND DETACHED. ACFT GROUNDED. REINSTALLED LIGHT COVER ON ROW 17A. OPS CHECKED OK.Apr 10, 2017 · N526AS · Boeing 737890 · Emergency LightingSDR ASAA2017031120126Battery Pack · dischargedEMERGENCY BATTERY PACK FAILED TO OPERATE FOR THE 15 MINUTE INTERVAL FOR OVERWING EXIT CENTER AISLE CEILING EXIT LOCATION SIGN AND RIGHT OVERWING EXIT LOCATION SIGN LIGHTS. ACFT GROUNDED. REPLACED BATTERY PACK AT SEATS 15, 16ABC IAW AMM 33-51-06-960-805 OPS CHMar 11, 2017 · N526AS · Boeing 737890 · Emergency LightingSDR ASAA2016072617542Warning System · false activationAPU FAULT LIGHT CAME ON AFTER APU START. FAULT LIGHT WENT OUT AND APU RESTART HAD FAULT LIGHT ON AGAIN. ACFT GROUNDED. PERFORMED SEVERAL STARTS OF APU, WAS UNABLE TO REPLICATE FAULT, REF FIM TASK 49-40-00. OPS CHECK GOOD.Jul 26, 2016 · N526AS · Boeing 737890 · APU Indicating SystemSDR ASAA2016031015878Power Supply · failedEMERGENCY LIGHTS FAIL DEEP CYCLE AFT OF OVERWING EXITS BOTH SIDES & L2 DOOR. ACFT GROUNDED. R & R BATTERY PACKS, OPS CHECK GOOD.Mar 10, 2016 · N526AS · Boeing 737890 · Emergency LightingSDR ASAA2015100213498Floor Support · crackedFWD CARGO COMPARTMENT, RT FLOOR SUPPORT BAFFLE BETWEEN BS 500F AND 500G IS CRACKED AT UPPER AFT CORNER. ACFT GROUNDED. R & R FWD CARGO COMPARTMENT RT FLOOR SUPPORT BAFFLE BS 500F TO 500G IAW SRM 51-10-02, PARA 9 BAC DWG 143A7505, REV AND EA 800-53EA-15949 ANOct 2, 2015 · N526AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015092913497Stop Fitting · gougedAFT CARGO DOOR FWD SIDE NR 4 DOOR STOP FITTING HAS MINOR EDGE DAMAGE. AIRCRAFT GROUNDED. R & R AFT CARGO DOOR NR 4 STOP AND FASTENERS AS REQUIRED IAW SRM 51-40-02 AND BAC DWG 146A6110, REV B AND 146A617, REV A. INSTALLED AND ADJUSTED STOP PIN AT BEAM D, FWD SSep 29, 2015 · N526AS · Boeing 737890 · Cargo/Baggage DoorsSDR ASAA2015092913450Angle · crackedFWD CARGO BS 500H RT TRANSITION PANEL INTERCOSTAL ANGLE CRACKED. ACFT GROUNDED. R & R THE ANGLE IAW SRM 51-40-02 AND 51-10-02, PARA 9, AND DWG 143A7505, REV.Sep 29, 2015 · N526AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015092913449Angle · crackedFWD PIT BS 500G RT TRANSITION PANEL INTERCOSTAL ANGLE CRACKED. ACFT GROUNDED. R & R THE ANGLE IAW SRM 51-40-02 AND 51-10-02, PARA 9 AND BAC DWG 143A7505, REV.Sep 29, 2015 · N526AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015092813448Skin · crackedLEFT LOWER HORIZONTAL SKIN PANEL CRACKED AT STABILIZER, BS 120.30 17 FORWARD OF REAR SPAR APPROXIMATELY 1" IN LENGTH. ACFT GROUNDED. ACCOMPLISHED EXTERNAL DOUBLER REPAIR IAW SRM 55-10-01-2R-11.Sep 28, 2015 · N526AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2015092813447Skin · crackedLEFT LOWER HORIZONTAL SKIN PANEL CRACKED AT STAB STATION 129.50 21 FORWARD OF REAR SPAR APPROXIMATELY 1" IN LENGTH. ACFT GROUNDED. ACCOMPLISHED EXTERNAL DOUBLER REPAIR IAW IAW SRM 55-10-01-2R-11.Sep 28, 2015 · N526AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2015092613337Floor Panel · puncturedPARTS RACK, AFT CARGO COMPARTMENT, FLOOR PANEL 140BF IS PUNCTURED. ACFT GROUNDED. FABRICATED PANEL IAW DWG NR 453A2610, REMOVED DOT. PANEL WILL BE INSTALLED ON OPS 9900. ALODINED PANEL IAW SRM 51-20-01. PRIMED PANEL IAW SOPM 20-43-02.Sep 26, 2015 · N526AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2015052311889Bulkhead · crackedDURING A/C WALK AROUND FOUND POSSIBLE CRACK RT W/W UPPER FWD BULKHEAD APPROXIMATELY RBL 40.00 TO RBL 45.64. ACFT GROUNDED. REPAIRED CRACK ON FWD BULKHEAD ON RT SIDE OF MLG RBL 40 - 45.64 IAW SRM 57-10-10-2R-3, ALTERNATIVE 2.May 23, 2015 · N526AS · Boeing 737890 · Fuselage Main, BulkheadSDR ASAA2015020110520Skin · crackedRT HORIZONTAL STAB, LOWER SKIN, APPROXIMATE STA 165 .7500 CRACK FOUND AT APPROXIMATE STAB STA 177. ACFT GROUNDED. REMOVED DAMAGE FABBED LOCATED DRILLED DEBURRED AND COUNTERSUNK DOUBLER AND FILLER IAW SRM 55-10-01-2R-11 ALODINED DOUBLER AND FILLER IAW SRM 51-Feb 1, 2015 · N526AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2015020110518Skin · crackedLEFT HORIZONTAL STAB, LOWER SKIN, .7500" CRACK FOUND AT APPROXIMATELY STAB STA 177. ACFT GROUNDED. REMOVED DAMAGE FABRICATED DRILLED COUNTERSUNK REPAIR PARTS AND INSTALLED IAW SRM 55-10-01-2R-11, REPAIR 11 ALODINED IAW SRM 51-20-01 PRIMED IAW AMM 51-21-72-370Feb 1, 2015 · N526AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2014052708095Angle · corrodedAFT CARGO RT TRANSITION PANEL ANGLE HAS CORROSION, BS 787-807, S25-26R. ACFT GROUNDED. REMOVED CORROSION AND OUT OF LIMITS IAW SRM 53-60-53. R & R IAW SRM 51-40-02.May 27, 2014 · N526AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2014052708094Angle · corrodedAFT CARGO BAY, RT TRANSITION PANEL ANGLE HAS CORROSION, BS 727E-747, S25-26R. AIRCRAFT GROUNDED. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS AND REPAIRED AS REQUIRED IAW SRM 53-00-53-1A-2.May 27, 2014 · N526AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2014052708036Angle · corrodedAFT CARGO BAY LT TRANSITION PANEL HAS CORROSION, BS 727C-727J, S25-26L. ACFT GROUNDED. REMOVED CORROSION FROM AFT BAY LT TRANSITION PANEL FROM STA 727C-787, ALL AREAS FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53-1A-2 MATERIAL LOSS OUT OF LIMITS FROM STA 727-7May 27, 2014 · N526AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2014052707994Structure · gougedFORWARD GALLEY SERVICE DOOR, BACKSIDE OF CAM PLATE ON HANDLE BOX GOUGED BY CONTACT WITH FASTENER HEADS ON DOOR INTERIOR SKIN BELOW HANDLE BOX. ACFT GROUNDED. REMOVED CAM PLATE ON HANDLE BOX REF AMM 52-41-11 AND REINSTALLED CAM PLATE IAW REF BCMM 52-41-05. T/WMay 27, 2014 · N526AS · Boeing 737890 · Service DoorsSDR ASAA2014052707993Transition Panel · corrodedFWD CARGO BAY RT TRANSITION PANEL CORRODED BS 500A-500D, RBL 22-RBL 26. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2, FIG 103. R & R SECTION OF TRANSITION PANEL IAW SRM 53-00-53-2R-5, REPAIR 5.May 27, 2014 · N526AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2014052408210Floor Support · crackedPASSENGER CABIN FLOOR SPLICE STRAP BS 727B AFT OTBD HOLE CRACKED AT LBL 45.50. ACFT GROUNDED. REPLACED CABIN FLOOR SPLICE STRAP IAW EA SB737-53-1296-NG-113 AND REO-G17505.May 24, 2014 · N526AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2014052408209Floor Support · crackedPASSENGER CABIN FLOORS SPLICE STRAP BS 727B AFT INBD AND OTBD HOLES CRACKED AT LBL 24.75. ACFT GROUNDED. REPAIRED CABIN FLOOR SPLICE STRAP IAW EA SB737-53-1296-NG-113, REV NEW AND REO-G17505, REV C.May 24, 2014 · N526AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2014052408208Floor Support · crackedFUSELAGE PASSENGER CABIN FLOORS SPLICE STRAP BS 727B AFT INBD HOLE CRACKED AT RBL 24.75. ACFT GROUNDED. REPAIRED CABIN FLOOR SPLICE STRAP IAW EA SB737-53-1296-NG-113, REV NEW AND REO-G17505, REV C.May 24, 2014 · N526AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2014052408207Floor Support · crackedFUSELAGE PASSENGER CABIN FLOOR BS 727B SPLICE STRAP AFT INBD AND OTBD HOLES CRACKED AT RBL45.50. ACFT GROUNDED. REPAIRED CABIN FLOOR SPLICE STRAP AFT INBD AND OTBD HOLES AT STA RBL 45.50 IAW ASA EA SB 737-53-1296-NG-113, REV NEW AND REO-G17505 REV C.May 24, 2014 · N526AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2014042707590Lens · missingEXIT AT ROW 17 SEAT MISSING LENS. ACFT GROUNDED. INSTALLED NEW LENS COVER.Apr 27, 2014 · N526AS · Boeing 737890 · Emergency LightingSDR ASAA2014040107449Skin · crackedTWO CRACKS FOUND ON RT HORIZONTAL STABILIZER LOWER SURFACE. ACFT GROUNDED. CONFIRMED END OF CRACKS IAW DT MAN PART 6, 51-00-00, PROC 23 57120 4-1-14, FIRST CRACK LOCATED RT STABILIZER STA 101.9 38" AFT OF FRONT SPAR. REPAIRED CRACK.Apr 1, 2014 · N526AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2014020406782Engine · oscillatesNR 2 ENGINE N1, FUEL FLOW, AND EGT BEGAN TO OSCILLATE AT NEAR TOP OF CLIMB AFTER CENTER TANK FUEL USED. N1 OSCILLATED +/- 10 PERCENT. RAN QRH FOR ENGINE STALL - SURGE. REDUCED THRUST, ENGINE CONTINUED TO OSCILLATE. AUTOTHROTTLE OFF. AFTER SEVERAL MINUTES, OFeb 4, 2014 · N526AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2012100693025Display · failedNR 1 FMC SCREEN WENT BLANK FOLLOWED BY A LARGE PUFF OF ELECTRICAL SMOKE. THE SCREEN DISPLAY CAME BACK ON IN 15 SECONDS AND NO FURTHER SMOKE WAS SEEN. R & R LT MCDU IAW MM 34-61-01-000-802 /MM 34-61-01-400-802. PERFORMED CDU INSTALLATION TEST IAW MM 34-61-01-4Oct 6, 2012 · N526AS · Boeing 737890 · Central Display
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