N597AS
Service difficulty reports · 401
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 = 'N597AS' 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.
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 = 'N597AS' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ASAA2026062367063Skin · crackedCRACK INDICATION FOUND, NR 1 RT HORZONTAL STAB LOWER SKIN STAB. STA.157.10 .900"L INBD OF INBD ROW OF FASTENERS, 22.75" AFT OF FWD SPAR. GROUNDED - YES. REPLACED THE RT HORIZONTAL STAB LOWER SKIN STAB STA 157.10 IAW SRM 55-10-01-2R-11. REPAIR IS A CAT "B" INSDR ASAA2026062367062Skin · crackedCRACK INDICATION FOUND, NR 3 RT HORZONTAL STAB LOWER SKIN STAB. STA.129.50 .500"L INBD OF INBD ROW OF FASTENERS, 33.25" AFT OF FWD SPAR. GROUNDED - YES. REPAIRED THE RT HORIZONTAL STAB LOWER SKIN STAB STA 129.50 IAW SRM 55-10-01-2R-11. REPAIR IS A CAT "B" INSSDR ASAA2026042165876Mount · corrodedPASSENGER CABIN STA 916.5 LBL 51.55 DUAL FLOOR MOUNT ATTACHING INTERCOSTAL HAS CORROSION AROUND MOUNT. GROUNDED - YES. REMOVED AND REPLACED 147A5690-8 INTERCOSTAL IAW BAC DWG 147A5680 REV - AND B737-800 SRM 51-40-02. ALLOWABLE LIMITS IN SRM FOUND DEEMED OUT OFSDR ASAA2025110162010Door · no discrepancyFA REPORTS L1 DOOR DIFFICULT TO CLOSE, REQUIRING MORE FORCE THAN NORMAL. ALSO REPORTED A TAPPING NOISE EMANATING FROM UPPER RIGHT SECTION OF L1 DURING DESCENT, LANDING. DURING TAXI-IN. GROUNDED - YES. INSPECTED FWD L1 DOOR FRAME/SILL AND DOOR ASSY IAW AMM 52-SDR ASAA2025090260530Elec Connector · unsecureEMERGENCY AISLE / AREA LIGHT ABOVE 6 ABC INOPERATIVE. GROUNDED - YES. SECURED D11344 CONNECTOR WDM 33-51-12-6, LIGHT L1065 NOW OPERATING NORMALLY.SDR ASAA2025090260531Battery Pack · inoperativeWHILE WORKING TC 78233001 THE FOLLOWING DEFECTS NOTED: 1) RH FWD OWE GROUND ILLUMINATION LIGHT INOP. 2) L2 OVERDOOR & ASSOCIATED LIGHTS INOP. 3) 21-24 DEF EMERGENCY AISLE LIGHTS INOP. 4) LH OWE GROUND ILLUMINATION & ESCAPE LT INOP. 5) 18-22 ABC EMERGENCY AISLESDR ASAA2024081952258Rib · cracked(LATE FIND) WHILE INSPECTING FOR AN "OK TO INSTALL" L/H LEADING EDGE, FOUND TWO INTERNAL CRACKS AT STA LES 105.26 VERTICAL, SEGMENTS 3 AND 4. GROUNDED - YES. REPAIRED THE L/H HORIZ STAB AT STA 92.70 3EA LOCATIONS USING MAT BAC1505-100962 T-SECTION, BAC 1490-2SDR ASAA2024081952175Rib · cracked(LATE FIND) WHILE INSPECTING FOR AN "OK TO INSTALL" R/H HORIZONTAL LEADING EDGE. FOUND INTERNAL CRACK AT STA LES 123.85 3 VERTICAL SEGMENTS AFT STREAMER ATTACHED AT OPENING. GROUNDED - YES. REPAIRED THE RIGHT HORIZ STAB RIB AT LE STA 123.85 USING MAT BAC 1505-SDR ASAA2024071851458Baffle · crackedFWD PIT R/H BAFFLE BETWEEN STA 500E AND 500F CORNER BROKEN OFF. GROUNDED - YES. REMOVED AND REPLACED FWD PIT R/H BAFFLE BETWEEN STA 500E AND 500F PN:143A7510-22 PO: 1096771.4 IAW B737-800 SRM 51-40-02 AND SRM 51-40-05.SDR ASAA2024071552006Intercostal · corrodedMAIN CABIN INTERCOSTAL UPPER SURFACE HAS CORROSION AT BS307 LBL12 AS MARK. GROUNDED - YES. REMOVED CORROSION IAW B737-800 51-10-02. ORIG THICK 0.125, REMOVED 0.060, REMAINING THICK 0.065 OUT OF LIMITS IAW B737-800 SRM 53-10-51. REMOVED INTERCOSTAL IAW B737-800SDR ASAA2024071551579Floor Support · corrodedCABIN AFT WET AREA APRROX. STA. 952, RBL 24-48 LATERAL FLOOR SUPPORT CORRODED AROUND FASTENER HOLES (2EA) AS MARKED. GROUNDED - YES. REMOVED AND REPLACED FLOOR SUPPORT IAW B737-800 SRM 51-40-02 AND BOEING DWG 147A5650 REV A. ORIG THICKNESS IS 0.075" REMOVED 0.SDR ASAA2024071551513Floor Support · corrodedCABIN AFT WET AREA FLOOR STRUCTURE BETWEEN GALLEY FITTINGS APPROX. STA. 1014 AND LBL 32,FLOOR PANEL LONGITUDINAL SUPPORT CORRODED AS MARKED. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02,100% MAT LOSS,NO LIMITS NOTED NO ORIG THICKNESS NOTED,FOUNDSDR ASAA2024071551193Floorbeam · corrodedMAIN CABIN FLOORBOARD SUPPORT HAS CORROSION AT BS270 BETWEEN RBL0 AND RBL7 AS MARK. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02, ORIG THICKNESS FOR TOP SURFACE .100 REMOVED .007 REMAINING MAT .093 FOUND TO BE IN LIMITS IAW B737-800 SRM 53-10-51SDR ASAA2024071551465Floor Support · corrodedCABIN WET AFT AREA APPROX. STA. 952, LBL 16-24 LATERAL FLOOR SUPPORT CORRODED AROUND FASTENER HOLES AS MARKED. GROUNDED - YES. REMOVED DAMAGE IAW B737-800 SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW B737-800 B737-800 SRM 53-42-51, NO LIMITS NOTED, ORIG THICKNESDR ASAA2024071551464Floor Support · corrodedCABIN AFT WET AREA APPROX. STA. 952,LBL 24-48 LATERAL FLOOR SUPPORT CORRODED AROUND FASTENER HOLES AS MARKED. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02, 100% MAT LOSS OUT OF LIMITS IAW B737-800 SRM 53-70-51, NO ORIG THICKNESS NOTED, NO LIMITSSDR ASAA2024071551463Floor Support · corrodedCABIN AFT WET AREA APPROX. STA. 952,LBL 24 LONGITUDINAL FLOOR SUPPORT CORRODED AROUND (1EA)FASTENER HOLE AS MARKED. GROUNDED - YES. REMOVED DAMAGE IAW B737-800 SRM 51-10-02, FOUND TO BE OUT OF LIMITS NO ORIG THICKNESS NOTED, NO LIMITS NOTED. REMOVED AND REPLACSDR ASAA2024071551462Web · corrodedCABIN AFT WET AREA APPROX. STA. 988, RBL 32 GALLEY FLOOR SUPPORT PLATE TOP SURFACE CORRODED AS MARKED. GROUNDED - YES. BLENDED OUT CORROSION IAW B737-800 SRM 51-10-02. WEB ORIGINAL THICKNESS 0.040 IAW BAC DWG 147A5712 REV B, REMAINING THICKNESS 0.028, REMOVED SDR ASAA2024071551461Support · corrodedCABIN AFT WET AREA APPROX. STA. 993 AND RBL 34,GALLEY SUPPORT PLATE ATTACH ANGLE HAS DRILLED OUT ELONGATED HOLES(2EA) AS MARKED. GROUNDED - YES. SUPPORT HAS 100% MATERIAL LOSS. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW SUPPORT IAW B737-8SDR ASAA2024071551460Floor Support · corrodedCABIN AFT WET AREA FLOOR STRUCTURE BETWEEN GALLEY FITTINGS APPROX. STA. 1015 AND RBL 32, FLOOR SUPPORT AFT END CORNER CORRODED AS MARKED. GROUNDED - YES. SUPPORT HAS 100% MATERIAL LOSS AND OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW SUPPOSDR ASAA2024071551459Floor Support · corrodedCABIN AFT WET AREA APPROX. STA. 958,LBL 48 LONGITUDUNAL FLOOR SUPPORT UPPER SURFACE CORRODED AROUND (2EA)FASTENER HOLES AS MARKED. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02, 100% MAT LOSS OUT OF LIMITS IAW B37-800 SRM 53-70-51. REMOVED AND RSDR ASAA2024071551334Floor Support · crackedMAIN CABIN FLOOR STRUCTURE INTERCOSTAL IS CRACK AT BS312 RBL28 AS MARK. GROUNDED - YES. REMOVED AND REPLACED 1 CABIN FLOOR STRUCTURE INTERCOSTAL (P/N- 141A5410U12) P.O. 1096573.1 IAW B737-800- ETOP- SRM-51-40-02 AND BOEING DOCUMENT- 141A5400 REV:-SDR ASAA2024071451400Floorboard · delaminatedMAIN CABIN AFT WET AREA FLOORBOARD DELAME P/N 147A5810-136. GROUNDED - YES. EVALUATED AND REPAIRED MAIN CABIN AFT WET FLOORBOARD P/N 147A5810-136 AND REPLACED 55 INSERTS IAW B737-800 SRM 53-00-50-2R-0.SDR ASAA2024071451399Floorboard · delaminatedMAIN CABIN AFT WET AREA FLOORBOARD DELAME P/N 147A5810-28. GROUNDED - YES. REPAIRED MAIN CABIN AFT WET AREA FLOOR BOARD P/N 147A5810-28 DELAM WITH FIBERGLASS DOUBLER REPAIR I.A.W B737-800 SRM 53-00-50-2R-0, 53-00-50-2R-1.SDR ASAA2024071451398Floorboard · delaminatedMAIN CABIN AFT WET AREA FLOORBOARD DELAME P/N 147A5810-27. GROUNDED - YES. REPAIRED MAIN CABIN AFT WET AREA FLOOR BOARD P/N 147A5810-27 DELAM WITH FIBERGLASS DOUBLER REPAIR I.A.W B737-800 SRM 53-00-50-2R-0, 53-00-50-2R-1.SDR ASAA2024071451333Floorboard · delaminatedMAIN CABIN AFT WET AREA FLOORBOARD DELAME P/N 147A5810-23. GROUNDED - YES. REPAIRED MAIN CABIN AFT WET AREA FLOOR BOARD P/N 147A5810-23 DELAM WITH FIBERGLASS DOUBLER REPAIR I.A.W B737-800 SRM 53-00-50-2R-0, 53-00-50-2R-7.SDR ASAA2024071451332Floor Panel · delaminatedMAIN CABIN FWD WET AREA FLOOR PANEL DELAME P/N 141A5810-454. GROUNDED - YES. PERFORMED PERMANENT REPAIRS ON MAIN CABIN FWD WET AREA FLOOR PANEL P/N: 141A5810-454 IAW ASA B737-800 SRM 53-00-50-2R-7 & ASA B737-800 SRM 53-00-50-2R-1, ASA B737-800 SRM 53-00-50-2R-SDR ASAA2024071451331Floor Panel · delaminatedMAIN CABIN FWD WET AREA FLOOR PANEL DELAME P/N 141A5810-755. GROUNDED - YES. PERFORMED PERMANENT REPAIRS ON MAIN CABIN FWD WET AREA FLOOR PANEL P/N: 141A5810-755 IAW ASA B737-800 SRM 53-00-50-2R-7 & ASA B737-800 SRM 53-00-50-2R-0. NO FURTHER ACTION REQUIRED.SDR ASAA2024071451330Floorboard · delaminatedMAIN CABIN AFT WET AREA FLOORBOARD DELAME P/N 147A5810-137. GROUNDED - YES. REPAIRED MAIN CABIN AFT WET AREA FLOOR BOARD P/N 147A5810-137 DELAM WITH FIBERGLASS DOUBLER REPAIR I.A.W B737-800 SRM 53-00-50-2R-0, 53-00-50-2R-1.SDR ASAA2024071451203Floor Panel · delaminatedMAIN CABIN FWD WET AREA FLOOR PANEL DELAME P/N 141A5810-157. GROUNDED - YES. EVALUATED PANEL. REPAIRED DELAMINATION IAW B737-800 ER SRM 53-00-50.SDR ASAA2024071451202Floor Panel · delaminatedMAIN CABIN FWD WET AREA FLOOR PANEL DELAME P/N 141A5810-155. GROUNDED - YES. EVALUATED PANEL. REPAIRED DELAMINATION IAW B737-800 ER SRM 53-00-50.SDR ASAA2024071451201Floor Panel · delaminatedMAIN CABIN FWD WET AREA FLOOR PANEL DELAME P/N 141A5810-763. GROUNDED - YES. EVALUATED PANEL. REPAIRED DELAMINATION IAW B737-800 ER SRM 53-00-50.SDR ASAA2024071451200Floor Panel · delaminatedMAIN CABIN FWD WET AREA FLOOR PANEL DELAME P/N 141A5810-236. GROUNDED - YES. COMPLETED WET LAY UP REPAIR AND REMOVE/REPLACE INSERTS ON MAIN CABIN FWD FLOOR PANEL P/N 141A5810-236 IAW B737-800 SRM 53-00-50-2R-1.SDR ASAA2024071451199Floor Panel · delaminatedMAIN CABIN FWD WET AREA FLOOR PANEL DELAME P/N 141A5810-728. GROUNDED - YES. COMPLETED WET LAY UP REPAIR AND REMOVE/REPLACE INSERTS ON MAIN CABIN FWD FLOOR PANEL P/N 141A5810-728 IAW B737-800 SRM 53-00-50-2R-1.SDR ASAA2024071451198Floor Panel · delaminatedMAIN CABIN FWD WET AREA FLOOR PANEL DELAME P/N 141A5810-765. GROUNDED - YES. COMPLETED WET LAY UP REPAIR AND REMOVE/REPLACE INSERTS ON MAIN CABIN FWD FLOOR PANEL P/N 141A5810-765 IAW B737-800 SRM 53-00-50-2R-1.SDR ASAA2024071351514Strap · corrodedAFT PIT LOWER DOOR SILL STRAP HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT LOWER DOOR SILL STRAP IAW B737-800 SRM 53-60-15-1A-1 ORIG THICKNESS IS .100" IAW B737-800 SRM 53-60-15-01-1. REMOVED .016". REMAINING THICKNESS IS .084" AND IS FOUND TOSDR ASAA2024071351466Shield · corrodedAFT PIT FWD SHIELD HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT FWD SHIELD IAW B737-800 SRM 53-60-15-1A-1 ORIG'L MATERIAL THICKNESS WAS .050 IAW B737-800 SRM 53-60-15-01-1,MAT REMOVED .025 REMAINING IS .025 FOUND TO BE OUT OF LIMITS IAW B737-8SDR ASAA2024071351403Attach Angle · corrodedAFT PIT,FWD SHIELD ATTACH ANGLE HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT FWD SHIELD ATTACH ANGLE IAW B737-800 SRM 53-60-15-1A-1 ORIGNL THICKNESS WAS .050 IAW B737-800 SRM 53-60-15-01-1.REMOVED .025 REMAINING THICKNESS IS .025 FOUND TO BE OSDR ASAA2024071351402Support · corrodedFWD PIT,AFT BULKHEAD R/H SUPPORT IS CORRODED. GROUNDED - YES. REMOVED CORROSION FROM THE FWD PIT R/H AFT BULKHEAD SUPPORT IAW B737-800 SRM 53-30-08-1A-1.2.C. AND IS FOUND TO HAVE 100% MATERIAL LOSS IAW B737-800 SRM 53-30-08-1A-1.4.(2). REMOVED AND REPLACED FWDSDR ASAA2024071351337Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL STA 727 TO 727E+12 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT L/H TRANSITION PANEL AT STA 727 TO 727E+12 IAW B737-800 SRM 53-00-53-1A-2, ORIGNL MATERIAL WAS .040 IAW B757-800 SRM 53-60-53-01-2 100% MATERIAL LOST SDR ASAA2024071351336Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL STA 727E+12 TO 738 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT L/H TRANSITION PANEL AT STA 727E+12 TO 738 IAW B737-800 SRM 53-00-53-1A-2, ORIGN'L MATERIAL WAS .040 IAW B737-800 SRM 53-60-53-01-2 REMOVED .020. REMASDR ASAA2024071351335Shield · corrodedAFT PIT, AFT SHIELD HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT, AFT SHIELD IAW B737-800 SRM 53-60-15-1A-1. ORIG. THICKNESS IS .050" IAW B737-800 SRM 53-60-15-01-1. REMOVED .025" REMAINING THICKNESS IS .025" AND IS FOUND TO BE OUT OF LIMITS ISDR ASAA2024071351288Support · corrodedFWD PIT, AFT BULKHEAD LOWER SUPPORT IS CORRODED. GROUNDED - YES. REMOVED CORROSION FROM THE FWD PIT, AFT BULKHEAD LOWER SUPPORT IAW B737-800 SRM 53-30-08-1A-1.2.C AND IS FOUND TO HAVE 100% MATERIAL LOSS IAW B737-800 SRM 53-30-08-1A-1.4.(2). REMOVED AND REPLACESDR ASAA2024071351287Transition Panel · corrodedAFT PIT R/H TRANSITION PANEL STA 727 TO 727F+11 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT R/H TRANSITION PANEL AT STA 727 TO 727F+11 IAW B737-800 SRM 53-00-53-1A-2. ORIG. THICKNESS IS .040" IAW B737-800 SRM 53-60-53-01-2. REMOVED .020" REMASDR ASAA2024071351286Transition Panel · corrodedAFT PIT R/H TRANSISTION PANEL STA 727F+11 TO 767 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT R/H TRANSITION PANEL AT STA 727F+11 TO 767 IAW B737-800 SRM 53-00-53-1A-2. ORIG. THICKNESS IS .040" IAW B737-800 SRM 53-60-53-01-2. REMOVED .020" REMSDR ASAA2024071351285Transition Panel · corrodedFWD PIT R/H TRANSITION PANEL STA 500C+15 TO 500I IS CORRODED. GROUNDED - YES. REMOVED THE CORROSION FROM THE FWD PIT R/H TRANSITION PANEL AT STA 500C+15 -500I IAW B737-800 SRM 53-00-53-1A-2.2.D. ORIG THICKNESS IS .040" IAW B737- 800 SRM 53-30-53-1A-2. TABLE 2.SDR ASAA2024071051401Stop Fitting · wornMAIN CABIN L1 DOOR, AFT LOWER STOP PIN FITTINGS IS WORN ON SIDE. GROUNDED - YES. CHECKED LIMITS ON WORN AREA ON STOP FITTING, OUT OF LIMITS IAW B737-800 SRM 52-10-90-1A-4. MAT. REMOVAL LIMITS .030 IN ZONE 2 LUG SURFACE .035 REMOVED USED TOOL E1555B DUE 25JAN25SDR ASAA2024071051431Stop Fitting · wornMAIN CABIN L1 DOOR, AFT LOWER STOP PIN FITTINGS IS WORN ON SIDE. GROUNDED - YES. CHECKED LIMITS ON WORN AREA ON STOP FITTING, OUT OF LIMITS IAW B737-800 SRM 52-10-90-1A-4. MAT. REMOVAL LIMITS .030 IN ZONE 2 LUG SURFACE .035 REMOVED USED TOOL E1555B DUE 25JAN25SDR ASAA2024033048744Lens · missingFA REPORTS PLASTIC LIGHT COVER FOR EXIT ROW LIGHTING MISSING AT SEAT 16F. GROUNDED - YES. REPLACED L/H ROW 16F LOWER LIGHT COVER (EMERG). OPS GOOD.SDR ASAA2023100645510Unknown · unknownSINGLE FMC OPERATION MESSAGE ON CDU DURING TAXI IN. GROUNDED - YES. PERFORMED SYSTEM TEST OF FMC , NO FAULTS NOTED.SDR ASAA2023092245472Valve · malfunctionedCFM DIAGNOSTICS REPORTS #2 ENGINE HAS INCREASE IN DELTA EGT, FUEL FLOW AND DECREASE IN CORE SPEED. HPTACC MALFUNCTION IS SUSPECTED. (#PRI2/ETOPS) CNR 20230922006. GROUNDED - YES. (RESOLVED ON W/O: 1970765 TASKCARD: N/R-00001 ) ACCOMPLISHED REMOVALOF HPTACC REF
Back to N597AS