N506AS
Service difficulty reports · 490
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 = 'N506AS' 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 = 'N506AS' 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 ASAA2026062867053Battery Pack · inoperativeREF TASK CARD 78233001 FOUND LH AFT EMERGENCY LIGHTS DID NOT PASS TEST. GROUNDED - YES. REMOVED AND REPLACED AFT LT EMERGENCY BATTERY M1672 REF AMM 33-51-06, NEW BATTERY PASSED TEST.SDR ASAA2026051666171Gcu · faultedGEN CONTROL UNIT A/C LEFT IN E+E BAY HAS BTB FAULT LIGHT ILLUMINATED. GROUNDED - YES. RESET GCU REF AMM 24-21-81-400-801 NO FAULTS NOTED.SDR ASAA2026051166100Skin · crackedFOUND 1 EA CRACK INDICATION LOWER SKIN L/H STAB 138.70 AND S147.90 16 INCH LENGTH APROX AS MARK. GROUNDED - YES. REPAIRED THE L/H HORIZ. STAB LOWER SKIN STA 138.70 AND 147.90 USING MAT .071 2024-T3 AND .100 2024-T3 PER B737-80 SRM 55-10-01-2R-11. REPAIR IS A CSDR ASAA2026020164080Battery Pack · failedLEFT & RIGHT MAIN CABIN EMERGENCY LIGHTS INOPERATIVE. GROUNDED - YES. R & R THREE EMERGENCY BATTERIES, LT & RT ROW 23 & LT SEAT ROW 7. PERFORMED AN OPS CHECK, TESTED GOOD IAW AMM 33-31-06-960-805.SDR ASAA2026020164079Battery Pack · failedLEFT & RIGHT MAIN CABIN EMERGENCY LIGHTS INOPERATIVE. GROUNDED - YES. R & R THREE EMERGENCY BATTERIES LT & RT ROW 23 & LT SEAT ROW 7 & PERFORMED AN OPS CHECK, TESTED GOOD IAW AMM 33-31-06-960-805.SDR ASAA2026020164078Battery Pack · failedLEFT & RIGHT MAIN CABIN EMERGENCY LIGHTS INOPERATIVE. GROUNDED - YES. R & R THREE EMERGENCY BATTERIES LT & RT ROW 23 AND LT SEAT ROW 7 & PERFORMED AN OPS CHECK, TESTED GOOD IAW AMM 33-31-06-960-805.SDR ASAA2024090452430Skin · corrodedREF DEFECT # 300011333 N/R-00004 LAV WASTE VENT SKIN IS OUT OF LIMITS AND REQUIRES REPAIR. GROUNDED - YES. REPAIRED LAV WASTE VENT SKIN IAW 737-800 SRM 53-70-01-2R-3W= .5" O= .125" R= .096" L= 1" D= .029".SDR ASAA2024062750724Power Supply · inoperativeLIGHTS ASSOCIATED WITH M1674 POWER SUPPLY ARE INOP. GROUNDED - YES. REMOVED AND REPLACED M1674 POWER SUPPLY IAW B737-800 AMM 33-51-06-960-806 TEST GOOD.SDR ASAA2024060350503Floor Support · corrodedMAIN CABIN SUPPORT P/N 147A5676-16 STA 927 - STA 947 LBL16 CORRODED. GROUNDED - YES. BLENDED CORROSION SUPPORT HAS 100% MAT LOSS FOUND OUT OF LIMITS ALLOWABLE DAMAGE IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW SUPPORT IAW B737-800 SRM 51-40-05 AND BAC DSDR ASAA2024060350502Floorbeam · corrodedMAIN CABIN SUPPORT P/N 147A5676-5 STA 947 LBL 25 - LBL 50 CORRODED. GROUNDED - YES. CORROSION IS AROUND SEVERAL FASTENERS HOLE FOUND OUT OF LIMITS ALLOWABLE DAMAGE IAW B737-800 SRM 53-70-51-1A-1 100% MATERIAL LOSS. DRILLED NEW SUPPORT IAW B737-800 SRM 51-40-05SDR ASAA2024060350501Floor Support · corrodedMAIN CABIN INTERCOSTAL P/N 147A5676-13 STA 947.5 TO 967 CORRODED. GROUNDED - YES. CORROSION IS AROUND SEVERAL FASTENERS HOLE FOUND OUT OF LIMITS ALLOWABLE DAMAGE IAW B737-800 SRM 53-70-51-1A-1, 100% MAT LOSS. DRILLED NEW SUPPORT IAW B737-800 SRM 51-40-05 AN BASDR ASAA2024060350431Floorbeam · corrodedMAIN CABIN STA 990 RBL 32-43 CORRODED SUPPORT. GROUNDED - YES. CORROSION AT FASTENER HOLES 100% MATERIAL LOSS. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW SUPPORT IAW B737-800 SRM 51-40-05 AND BAC DWG 147A5700 REV.- SUPPORT INSTALLED ON N/SDR ASAA2024060350430Sidewall Support · corrodedMAIN CABIN WALL SUPPORT STA 990 - 1016 LBL 32 CORRODED. GROUNDED - YES. CORROSION IS AROUND SEVERAL FASTENER HOLES, 100% MATERIAL LOSS. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW SUPPORT IAW B737-800 SRM 51-40-05 AND BAC DWG 147A5700 REV.SDR ASAA2024060350429Support · corrodedMAIN CABIN SUPPORT STA 990 - 1016 RBL 32 CORRODED. GROUNDED - YES. BLENDED OUT CORROSION. SUPPORT HAS 100% MATERIAL LOSS. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW SUPPORT IAW B737-800 SRM 51-40-05 AND BAC DWG 147A5700 REV.- SUPPORT INSTSDR ASAA2024060250427Floorbeam · corrodedMAIN CABIN AFT WET AREA FLOOR STRUCTURE AT STA 951 R/H HAS CORROSION AT FASTENER HOLES UNDERSIDE. GROUNDED - YES. REMOVED AND REPLACED SUPPORT FRAME IAW B737-800 SRM 51-40-02 AND IAW REF'S AIPC 53-42-51.SDR ASAA2024053150499Rib · crackedRIGHT HORZ. STAB INTERNAL APPROX. SS 120 BETWEEN FRONT SPAR AND REAR RIB CRACKED. GROUNDED - YES. REPAIRED THE RIGHT HORIZ. STAB RIB AT APPROX SS 120 USING MAT BAC1505-100962 T-SECTION, BAC1490-2793 ANGLE, 0.12 7075-T6 SHIMS PER B737-800 SRM 55-10-09-2R-4.SDR ASAA2024052950500Floor Support · corrodedMAIN CABIN FLOOR SUPPORT INTERCOSTAL AT STA 947 CORRODED. GROUNDED - YES. BLENDED CORROSION INTERCOSTAL HAS 100% MATERIAL LOSS FOUND OUT OF LIMITS ALLOWABLE DAMAGE IAW B737-800 STM 53-70-51-1A-1 AT STA 242.5 LBL 24.5, DRILLED FIT NEW INTERCOSTAL IAW B737-800 SSDR ASAA2024052950418Angle · crackedFWD PIT, L/H BAFFLE CLIP AT STA 500H FWD SIDE IS CRACKED. GROUNDED - YES. REMOVED & REPLACED FWD PIT L/H BAFFLE CLIP AT STA 500H PN:143A7502-155 IAW B737-800 SRM 51-40-02 & SRM 51-40-05.SDR ASAA2024052950230Baffle · crackedFWD PIT, L/H BAFFLE CLIP AT STA 500G AFT SIDE IS CRACKED. GROUNDED - YES. REMOVED & REPLACED FWD PIT, L/H BAFFLE CLIP AT AT STA 500G WITH PN: 143A 7502-159 PO: 1092414.1 IAW B737-800 SRM 51-40-02 & SRM 51-40-05.SDR ASAA2024052950090Transition Panel · corrodedFWD PIT R/H TRANSITION PANEL STA 500E+10 TO 500I HAS CORROSION. GROUNDED - YES. REMOVED THE CORROSION FROM THE FWD PIT R/H TRANSITION PANEL AT STA 500E+10 TO 500I IAW B737-800 SRM 53-00-53-1A-2.2.D. ORIG THICKNESS IS .040" IAW B737-800 SRM 53-30-53-01-2 TABLE SDR ASAA2024052950089Transition Panel · corrodedFWD CARGO LT TRANSITION PANEL STA 500G+2 TO 500I HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM THE FWD PIT L/H TRANSITION PANEL AT STA 500G+2 TO 500I IAW B737-800 SRM 53-00-53-1A-2.2.D ORIG THICKNESS IS .040 IAW B737-800 SRM 53-30-53-01-2 TABLE 2. REMOSDR ASAA2024052850723Bracket · wornE/E COMPT. AFT DOOR PIN RECEPTICLE BRACKET IS WORN. GROUNDED - YES. REMOVED AND REPLACED RECEPTICLE BRACKET IAW B737-800 SRM 51-40-02 AND BOEING DWG # 141A3501 REV: - ADJUSTMENT CHECK GOOD.SDR ASAA2024052850504Floorbeam · corrodedAFT WET AREA STA 947 T-CAP HAS CORROSION AT MOUNT FITTING. GROUNDED - YES. REMOVED CORROSION, ORIGINAL THICK 0.1800 IAW B737-800 SRM 53-70-51-1A-1 AND FLOOR BEAM BAC 1518-1212 REMAINING THICK 0.154 AT RBL 53, 0.026" REMOVE MAT, REMAINING THICK 0.158 AT LBL 4, SDR ASAA2024052850428Floorbeam · corrodedAFT WET STA 986 HAS CORRODED FASTENER HOLES FLOOR BEAM. GROUNDED - YES. REMOVED CORROSION. ORIGINAL THICKNESS 0.150 IAW B737-800 SRM 53-70-51-0I-1 AND BAC 1518-1211. REMAINING THICKNESS AT RBL 34- 0.100, REMOVED 0.050. REMAINING THICK AT LBL43 0.095, REMOVED 0SDR ASAA2024052850426Floor Support · corrodedFWD WET AREA STA 328 - 344 LBL11 FLOOR STIFFNER HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM FWD WET AREA, STA 328-344, LBL 11 FLOOR STIFFENER (PANEL BREAK) REF B737-800 SRM 53-10-51-0I-2. TABLE 3. ITEM 8 PER. B737-800 SRM 53-10-51-1A-A. PAR 4.F,(2) OSDR ASAA2024052850425Floor Support · corrodedFWD WET AREA STA 312 - 328 LBL 11 FLOOR STIFFNER HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM FWD WET AREA, STA 312-328, LBL 11 FLOOR STIFFENER (PANEL BREAK) REF B737-800 SRM 53-10-51-OI-2, TABLE 3 ITEM (8)PER B737-800 SRM 53-10-51-1A-1, PAR. 4.F (2) SDR ASAA2024052550417Skin · dentedR2 DOOR OUTER HANDLE PAN HAS LIGHT CORROSION. GROUNDED - YES. REMOVED WORN HANDLE PAN & INSTALLED NEW HANDLE PAN, REFERENCE BAC DWG#147A6502 REV B, UPON FURTHER INSPECTION FOUND DENT & FOUND HANDLE PAN TO BE OUT OF LIMITS , REFERENCE B737-800 SRM 52-10-02-1A-4SDR ASAA2024052550416Skin · dentedR1 DOOR OUTER HANDLE PAN HAS LIGHT CORROSION. GROUNDED - YES. REMOVED DAMAGED PAN ASSY & INSTALLED NEW 141A6554Y1 PAN ASSY IAW B737-800 SRM 51-40-2 & BAC DWG 141A6516 REV.A UPON FURTHER INSPECTION FOUND DENT AND HANDLE PAN TO BE OUT OF LIMITS IAW B737-800 SRM SDR ASAA2024052550232Pan · dentedL2 DOOR OUTER HANDLE PAN HAS LIGHT CORROSION. GROUNDED - YES. REMOVED WORN HANDLE PAN & INSTALLED NEW HANDLE PAN REFERANCE BACDWG #147A6116 REV-, UPON FURTHER INSPECTION FOUND DENT & FOUND TO BE OUT OF LIMITS, REFERENCE B737-80 SRM 52-10-02-1A-3.SDR ASAA2024052450721Floor Support · corrodedAFT PIT FLOOR SUPPORT HAS CORROSION BETWEEN STA 794-807 RBL 13.84. GROUNDED - YES. REMOVED THE CORROSION FROM THE AFT PIT FLOOR SUPPORT AT STA 794-807, RBL 13.84 IAW B737-800 SRM 53-00-53-1A-2.2.0 ORIG THICKNESS IS .070" IAW B737-800 SRM 53-60-53-01-2 TABLE 2.SDR ASAA2024052450424Shield · corrodedAFT PIT, DOOR SURROUND FWD SHIELD IS CORRODED. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT DOOR SURROUND FWD SHIELD IAW B737-800 SRM 53-60-15-1A-1, ORIGIN'L MATERIAL WAS .050 IAW B737-800 SRM 53-60-15-01-1 100% MATERIAL LOSS. FOUND TO BE OUT OF LIMITS IAW B737SDR ASAA2024052450423Floor Support · corrodedAFT PIT FLOOR SUPPORT HAS CORROSION BETWEEN STA 727 AND 727B RBL 13.84. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT FLOOR SUPPORT BETWEEN STA 727 TO 727B RBL 13.84 IAW B737-800 SRM 53-00-53-1A-2 ORIG. THICKNESS IS .070" IAW B737-800 SRM 53-60-53-01-2 TABLE SDR ASAA2024052450422Transition Panel · corrodedAFT PIT R/H TRANSITION PANEL HAS CORROSION BETWEEN STA 727 AND 727F+11. 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 53-60-53-10-2 TABLE 2. RESDR ASAA2024052450421Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL CORROSION BETWEEN STA 727 AND 727F+11 GROUNDED - YES. REMOVED CORROSION FROM AFT PIT L/H TRANSITION PANEL AT STA 727 TO 727 F+11 IAW B737-800 SRM 53-00-53-1A-2-0, 100% MATERIAL LOSS, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-0SDR ASAA2024052450420Web · corrodedAFT PIT DOOR THRESHOLD WEB IS CORRODED. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT THRESHOLD WEB IAW ASA B737-800 SRM 53-60-15-1A-1 ORIGINAL MATL THKS .050 PER ASA B737-800 SRM 53-60-15-OI-1 TABLE ITEM 2 REMOVED .009 MATL .041 REMAINING MATL FOUND TO BE OUT OSDR ASAA2024052450231Strap · corrodedAFT PIT, DOOR SURROUND LOWER MAIN SILL STRAP IS CORRODED BETWEEN STA 767 AND 787. GROUNDED - YES. REMOVED DAMAGE FROM LOWER MAIN SILL STRAP IAW B737-800 SRM 53-60-15-1A-1. ORIG. THICKNESS .080 PER B737-800 SRM 53-60-15-0I-1.REMOVED .037. REMAINING THICKNESS ISSDR ASAA2024052450225Attach Angle · corrodedAFT PIT, DOOR SURROUND FWD SHIELD ATTACH ANGLE IS CORRODED. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT FWD SHIELD ATTACH ANGLE IAW B737-800 SRM 53-60-15-1A-1. ORIGN'L MATERIAL WAS .050 IAW B737-800 SRM 53-60-15-01-1. REMOVED .020, REMAINING IS .030. FOUND TO SDR ASAA2024052350419Floor Support · crackedMAIN CABIN UNDER FLOOR STA 540 PANEL SUPPORT CRACKED AT RBL 0 - RBL 10. GROUNDED - YES. REMOVED PANEL SUPPORT IAW B737-800 SRM 51-40-02. NEW PLATE PART . DRILLED TO FIT IAW B737-800 SRM 51-40-05. INSTALLED PANEL SUPPORT IAW B737-800 SRM 51-40-02 REF AIPC. 53-SDR ASAA2024052350415Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR BOARD DELAME P/N 147A5810-136. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOOR BOARD DELAMINATION PN 147A5810-136 IAW B737-800-SRM-53-00-50-2R-1 AND 53-00-50-2R-4.SDR ASAA2024052350410Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR BOARD DELAME P/N 147A5810-28. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOOR BOARD DELAMINATION P/N 147A5810-28 IAW B737-800-SRM-53-00-50-2R-1 AND 53-00-50-2R-4.SDR ASAA2024052350409Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOORBOARD DELAME P/N 147A5810-27. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOOR BOARD DELAMINATION PN 147A5810-27 IAW B737-800-SRM-53-00-50-2R-1 AND 53-00-50-2R-4.SDR ASAA2024052350395Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR BOARD DELAME P/N 147A5810-23. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOOR BOARD DELAMINATION P/N 147A5810-23 IAW B737-800-SRM-53-00-50-2R-1 AND 53-00-50-2R-4.SDR ASAA2024052350394Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR BOARD DELAME P/N 147A5810-137. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF MAIN CABIN AFT WET AREA FLOORBOARD DELAMINATION PN 147A5810-137 IAW B737-800-SRM-53-00-50-2R-1 AND 53-00-50-2R-4.SDR ASAA2024052350086Floorboard · delaminatedMAIN CABIN AFT WET AREA FLOOR BOARD DELAME P/N 147A5810-90. GROUNDED - YES. REPAIRED MAIN CABIN AFT WET AREA FLOOR BOARD NOTED DAMAGE BY PREFORMING PERMANENT WET LAY UP REPAIR IAW B737 SRM 53-00-50-2R-0, 53-00-50-2R-1.SDR ASAA2024052150393Floor Panel · delaminatedFLOOR PANEL DELAME FWD WET AREA P/N 141A5810-763. GROUNDED - YES. COMPLETED PERMANENT REPAIR OF FLOOR PANEL DELAMINATION ON FWD WET AREA PANEL PN 141A5810-763 IAW B737-800-SRM-53-00-50-2R-1 AND 53-00-50-2R-4.SDR ASAA2024052150085Floor Panel · delaminatedMAIN CABIN FLOOR PANEL DELAME P/N 141A5810-236. GROUNDED - YES. REPAIRED FLOOR PANEL P/N 141A5810-236 NOTED DAMAGE BY PREFORMING PERMANENT WET LAY UP REPAIR IAW B737 SRM 53-00-50-2R-1, 53-00-50-2R-0.SDR ASAA2024052150080Floor Panel · delaminatedFLOOR PANEL DELAME FWD WET AREA P/N 141A5810-728. GROUNDED - YES. REPAIRED FLOOR PANEL P/N 141A5810-728 NOTED DAMAGE BY PREFORMING PERMANENT WET LAY UP REPAIR IAW B737 SRM 53-00-50-2R-1, 53-00-50-2R-0.SDR ASAA2024042249193Lens · brokenF.A. REPORTS: L-1 FLOOR LEVEL EMERGENCY LIGHT COVER FELL OFF. GLASS BROKEN. GROUNDED - YES. REMOVED & REPLACED LOWER THRESHOLD LIGHT ASSEMBLY COVER IAW AMM 33-14-00.SDR ASAA2024041549080Lamp · inoperativeROW 17 EXIT LIGHTING DIM. GROUNDED - YES. RE-LAMPED ROW 17 EXIT LIGHT, OPS GOOD.SDR ASAA2024033048710Door · noisyFA REPORTS L1 DOOR MAKES UNUSUAL NOISE AND HAS GREATER THAN NORMAL RESISTANCE DURING OPENING AND CLOSING. GROUNDED - YES. LUBRICATED L1 DOOR UPPER AND LOWER HINGES, GUST LOCK, AND OPS CK NORMAL. DOOR OPENS AND CLOSES NORMALLY.
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