N626AS
Service difficulty reports · 208
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 = 'N626AS' 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 = 'N626AS' 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 ASAA2022101240719Floorbeam · corrodedFLOOR SUPPORT AT STA 259.5 HAS AREAS OF CORROSION ON UPPER FLANGE BETWEEN LBL-10 TO RBL-10. GROUNDED - YES. REPAIRED FLOOR SUPPORT AT STA 259.5 IAW ASA EA# 700-53EA-24860. THIS IS A CATEGORY B REPAIR WITH FIRST STAGE APPROVAL FOR STATIC STRENGTH AND WILL REQUISDR ASAA2022101240610Seat Track · corrodedSEAT TRACK RBL 60.70 STA 500 TO STA 522 HAS MULTIPLE AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION DETERMIND TO BE OUT OF ALLOWABLE LIMITS IAW BOEING 737-700 SRM 53-00-52-1A-1, REMOVED AND REPLACED SEAT TRACK AT RBL 60.70 FROM STA 500 TO STA 522 W: 1" SDR ASAA2022101240609Seat Track · corrodedSEAT TRACK LBL 45.5 STA 727B TO STA 887 HAS MULTIPLE AREAS OF CORROSION. GROUNDED - YES. REMOVED CORROSION, DETERMIND TO BE OUT OF ALLOWABLE LIMITS IAW B737-700 SRM 53-00-52-1A-1, REMOVED AND REPLACED SEAT TRACK AT LBL 45.5 FROM STA 727B TO STA 887W 1" O .250 SDR ASAA2022101240608Seat Track · corrodedSEAT TRACK RBL 45.5 STA 727A+18 TO STA 887 HAS MULTIPLE AREAS OF CORR. GROUNDED - YES. SURFACE BLENDED CORR FOUND TO BE OUT OF LIMITS FROM STA 727A TO 887 RBL 45.5 REMOVED & REPLACED TRACK WITH NEW IAW B737-700 SRM 51-40-05-0G-0 51-40-02-0G-0.SDR ASAA2022101240607Seat Track · corrodedSEAT TRACK LBL 24.75 STA 380 TO STA 500 HAS MULITPLE AREAS OF CORR. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS IAW B737-700 SRM 53-0052-1A-1 REMOVED & REPLAED IAW B737-700 SRM 51-40-*02-0G-0.SDR ASAA2022101240602Seat Track · corrodedSEAT TRACK LBL 24.75 STA 727A+18 TO STA 887 HAS MULIPLE AREAS OF CORROSION. GROUNDED - YES. REMOVED CORR DETERMINED TO BE OUT OF ALLOWABLE LIMITS IAW B737-700 SRM 53-00-52-1A-1 REMOVED & REPLACED SEAT TRACK AT LBL 24.75 FPOM STA 727A+18 TO STA 887 IAW B737-700SDR ASAA2022101240598Shield · corrodedRH FWD TRANSITION SHEILD HAS CORR. GROUNDED - YES. REMOVED CORR & CK'D LIMITS FOUND SHEILD TO BE OUT OF LIMITS IAW B737-700 SRM 53-60-15-1A-1 REMOVED & REPLACED SHEILD IAW B737-700 SRM 51-40-02-0G-0.SDR ASAA2022101240597Transition Panel · corrodedLH TRANSTION PNL HAS CORR FROM STA 727A TO STA 847. GROUNDED - YES. REMOVED CORR & CK'D LIMTS FOUND TRANSITION PNL TO BE OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-2 REPAIRED TRANSITION PNL IAW B737-700 SRM 53-00-53-2R-5. W 2.0 O .040 R .032 L 12.0 D .008SDR ASAA2022101240593Transition Panel · corrodedRH TRANSITION HAS AREAS OF CORROSION FROM STA 727B TO STA 787. GROUNDED - YES. REMOVED CORR & CHECKED TRANSITION PNL FOUND TO BE OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-2 REPAIRED TRANSITON PNL IAW B737-700 SRM 53-00-53-2R-5.SDR ASAA2022101240503Floor Support · crackedSTA 330.62-348.2 LBL 45 INTERCOSTAL IS CRACKED AT ATTACH HOLE. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL AT STA 330.62 TO 348.2 LBL 45 IAW BOEING 737-700 SRM 51-40-02-0G-0.SDR ASAA2022101240501Seat Track · corrodedSEAT TRACK AT LBL -45.5 HAS MULTIPLE AREAS OF CORROSION BETWEEN STA 540 TO STA 727A+18. GROUNDED - YES. REMOVED AND REPLACED SEAT TRACK AT LBL 45.5 STA 540 TO 727A+18 IAW B737-700 SRM 51-40-02-0G-0.W= 1" O= 1.00 R= .942 L= 1" D= .058.SDR ASAA2022100740606Skin · crackedRH HOIRZ LWR SKIN CRACKED AT APPROX STA 94 & REAR SPAR. GROUNDED - YES. REPAIRED SKIN IAW B737-700 SRM 55-10-01-2R-11.SDR ASAA2022100740605Skin · crackedRH HORIZ LWR SKIN CRACKED AT STA 101 19 INCHES FWD OF REAR SPAR. GROUNDED - YES. REPAIRED SKIN IAW B737-700 SRM 55-10-01-2R-11.SDR ASAA2022100740604Skin · crackedRH HORIZ LWR SKIN CRACKED AT APPROX STA 124 & NEAR SPAR. GROUNDED - YES. REPAIRED SKIN IAW B737-700 SRM 55-10-01-2R-11.SDR ASAA2022100640722Skin · cracked#8 SLAT LOWER LEADING EDGE SKIN, LOOSE FASTENERS COMMON TO THE SLAT ACTUATOR ATTACH POINT, 1EA FASTENER HAS EVIDENCE OF A CRACK (MARKED IN GREASE PENCIL). GROUNDED - YES. REPAIRED #8 SLAT LOWER LEADING EDGE SKIN IAW B737-700 SRM 57-42-01-2R-8.SDR ASAA2022032637788Bulb · inoperativeEMERGENCY EXTERIOR LIGHTS L1 AND R1 DO NOT COME ON WHEN EMERGENCY LIGHT SWITCH ON OVERHEAD P5 PANEL IS TURNED ON. GROUNDED - YES. RELAMPED EMERGENCY EXTERIOR LIGHTS AT L1 AND R1 REF B737-700 AMM 33-51-04 OPS CHECK GOOD.SDR ASAA2021081135731Control Valve · failedON TAXI IN , SHORTLY AFTER PUTTING ELECTRICS ON APU BUSS, GOT A APU FIRE WARNING STOPPED AIRCRAFT , SET BRAKES AND PERFORMED APU FIRE QRC AND QRH. TAXIED TO GATE. DID BLOW ONE FIRE BOTTLE INTO APU. GROUNDED - YES. OIL SOAKED / LOW OIL IN TANK. SUSPECT APU INTESDR ASAA2021021334108Bushing · crackedON GEAR RETRACTION A LOUD THUD OCCURRED IN MAIN LANDING GEAR. CREW DEBRIEF: VERBAL FROM FLIGHT CREW "THUD" NOISE FROM RT MAIN GROUNDED - YES. REMOVED AND REPLACED BOTH RT AND LT MLG LANDING GEAR SUPPORT LINK ASSEMBLIES. PN 115A1500-14 (RT SIDE - CRACKED & SDR ASAA2019101020982Shear Tie · crackedPASSENGER CABIN OVERWING PRESSURE DECK SHEAR TIE IS CRACKED STA. 540 RBL 5. GROUNDED - YES. REMOVED AND REPLACED SHEAR TIE IAW B737-700 SRM 51-40-02-0G-0.SDR ASAA2019101092981Shear Tie · crackedPASSENGER CABIN CENTER WING SHEAR TIE IS CRACKED STA. 540 RBL 14. GROUNDED - YES. REMOVED AND REPLACED SHEARTIE IAW B737-700 SRM 51-40-02-0G-0.SDR ASAA2019101098980Shear Tie · crackedPASSENGER CABIN CENTER WING SHEAR TIE IS CRACKED STA. 540 LBL 40. GROUNDED - YES. REMOVED AND REPLACED SHEAR TIE IAW B737-700 SRM 51-40-02-0G-0.SDR ASAA2019100293877Floor Support · crackedFWD WET AREA INTERCOSTAL BETWEEN STA. 312 AND 328 LBL 44 IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED INTERCOSTAL FROM STA 312 TO 328 LBL 44 IAW B737-700 SRM 51-40-02-0G-0.SDR ASAA2019102493188Frame · crackedL/H VAPOR BARRIER STA 663.75 UPPER CHORD LBL 13 IS CRACKED AT FASTNER LOCATION. GROUNDED - YES. REPAIRED L/H VAPOR BARRIER STA 663.75 UPPER CHORD LBL 13 IAW B737-700 SRM 57-10-10-2R-5.SDR ASAA2019101526012Web · corrodedRIGID BARRIER FLOOR WEB AT STA. 907 RBL 44 HAS LIGHT CORROSION. GROUNDED - YES. NO ALLOWABLE LIMITS ON FLOOR WEB, OUT OF LIMITS IAW IAI SRM 53-70-54, REMOVED AND REPLACED FLOOR WEB IAW B737-700 SRM 51-40-04-0G-0 & 51-40-02-0G-0 W: 1 O: .071 R: 0 L: 6 D: .071.SDR ASAA2019101093979Crease Beam · corrodedR2 DOOR CREASE BEAM CORRODED AT PREVIOUS BLENDOUTS UPPER AND LOWER SURFACES MOSTLY AROUND NUTPLATES, MARKED. GROUNDED - YES. REMOVED CORROSION ON CREASE BEAM INNER CHORD AND FOUND TO BE OUT OF LIMITS IAW 737-700 SRM 53-70-15-1A-1. REMOVED CREASE BEAM INNER CHOSDR ASAA2019100496900Floor Support · corrodedFLOOR SUPPORT BETWEEN STA. 947 AND 967 LBL 46 IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED FLOOR SUPPORT AT SAT 947 TO 967 LBL 46 IAW B737-700 SRM 51-40-02-0G-0.SDR ASAA2019102295370Transition Panel · corrodedAFT PIT RH TRANSITION PANEL HAS SMALL AREAS OF COROSSIONS FRM STA. 727 TO 767. GROUNDED - YES. BLENDED CORROSION ON TRANSITION PANEL, REMAINING MATERIAL FOUND OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-2, REMOVED TRANSITION PANEL IAW B737-700 SRM 51-40-02-0G-0SDR ASAA2019100923962Web · corrodedAFT PIT DOOR CUR OUT LWR SILLWEB HAS AREA OF CORROSION. GROUNDED - YES. BLENDED CORROSION ON AFT CARGO DOOR CUT OUT LOWER SILLWEB, REMAINING MAT. FOUND OUT OF LIMITS IAW B737-700, SRM 53-60-15-1A-1, REMOVED & REPLACED SILLWEB IAW B737-700 SRM 51-40-02-0G-0, ITSDR ASAA2019100890948Baffle · corrodedAFT PIT RH STA. 747 BAFFLE HAS COROSSION ON LWR FLANGE. GROUNDED - YES. REMOVED CORROSION, ORIG "T" .032", LOSS OF .007", REMAINING "T" .025", FOUND TO BE OUT OF LIMITS IAW B737-700 SRM 53-60-53-1A-2. REMOVED DAMAGED BAFFLE IAW B737-700 SRM 51-40-02-0G-0. LOCASDR ASAA2019100893947Web · corrodedFWD CARGO DOOR CUT OUT LWR SILLWEB HAS SMALL AREAS OF LIGHT COROSSION. GROUNDED - YES. BLENDED CORROSION ON FWD CARGO DOOR CUT OUT LWR SILLWEB IAW B737-700 SRM 53-30-15-1A-1, ORIG. "T" .056", LOSS OF .013", REMAINING "T" .043", FOUND TO BE OUT OF LIMITS IAW B7SDR ASAA2018122477539Lamp · inoperativeEMERGENCY EXIT LIGHT ON MAIN CARGO DOOR OUT. GROUNDED - YES. RELAMPED EMERGENCY EXIT LIGHT ON MAIN CARGO DOOR OUT & OPS CHECKS GOOD IAW B737-700 AMM 33-51-04-960-801.SDR ASAA2018092876300Pin · shortedON APPROACH INTO JNU, FLAPS LOCKED OUT AT FLAPS 5 POSITION. FLAPS WOULD NOT GO DOWN OR UP WITH ANY FLAP LEVER SELECTION. TRAILING EDGE FLAP DISAGREE CHECKLIST COMPLETED. DIVERTED TO PASI. FLAPS EXTENDED TO 15 USING ALTERNATE FLAP EXTENSION. NORMAL LANDING PASISDR ASAA2018091026079Warning System · false activationWHILE CONFIGURING FOR LANDING AND SELECTING FLAPS 5, THE FLAP GAUGE INDICATED L-1.5, R 2.0 AND THE FLAPS FROZE. DURING A TURN IN HOLDING, THE LEFT FLAP INDICATION MOVED TO 2.0. FLAP HANDLE WAS AT FLAPS 1 PER QRH. FOLLOWED QRH. NO ROLL ENCOUNTERED. FLAP INDICATSDR ASAA2018010423284Window Frame · crackedLT NR 3 WINDOW FWD FRAME HAS CRACK AT 3RD FROM LOWER FASTENER HOLE. GROUNDED - YES. REPAIRED CRACK IAW EA 700 53EA 19750 THIS IS A CATEGORY B REPAIR WITH FIRST AND SECOND STAGE APPROVAL. A NEW FAA APPROVAL WHICH CONTAINS THE INSPECTION REQUIREMENTS MUST BE ISSSDR ASAA2018010223214Floor Support · corrodedFLT DECK FLOOR SUPPORT ANGLE CORRODED UNDER AFT CENTER FLOOR ACCESS PANEL. GROUNDED - YES. REPAIRED FLT DECK FLOOR SUPPORT ANGLE IAW EA 700 53EA 19749 W .90" O .050" R .033" L 3.5" D .017".SDR ASAA2017112622695Guide Arm · out of adjustRAMP REPORTED THE L1 DOOR WILL NOT CLOSE. ACFT GROUNDED. VERIFIED L1 DOOR DOES NOT CLOSE PARALLEL TO FUSELAGE ON FINAL STAGE AND HARD TO CLOSE FROM INSIDE, ADJUSTED THE L1 DOOR GUIDE ARM IAW AMM 52-11-00-820-801, STEP 2, PARA H. DOOR OPS CHECKED GOOD.SDR ASAA2017082222330Frame · crackedFOUND A CRACK ON THE FRAME AT BS 867 BETWEEN STRINGERS 8 & 9L. ACFT GROUNDED. ACCOMPLISHED A REPAIR IAW REA MF01088R0321.SDR ASAA2017082222329Frame · crackedFOUND A CRACK ON THE FRAME AT BS 787 BETWEEN STRINGERS 8 & 9R. ACFT GROUNDED. ACCOMPLISHED A REPAIR IAW REA MF01088R0321.SDR ASAA2017082222328Frame · crackedFOUND A CRACK ON THE FRAME AT BS 727D BETWEEN STRINGERS 8 & 9R. ACFT GROUNDED. ACCOMPLISHED A REPAIR IAW REA MF01088R0321.SDR ASAA2017082222325Frame · crackedFOUND A CRACK ON THE FRAME AT BS 480, BETWEEN STRINGERS 8 & 9R. ACFT GROUNDED. ACCOMPLISHED A REPAIR IAW IAI REA MF01088R0321, 700-53EA-19377SDR ASAA2017010519268Gust Lock · stuckL1 DOOR IS DIFFICULT TO CLOSE. ACFT GROUNDED. FOUND THE GUST LOCK STUCK. CLEANED, LUBED, AND EXERCISED THE GUST LOCK. OPS CHECKED GOOD.SDR ASAA2016120618963Light · inoperativeEMERGENCY LIGHT AREA LIGHT (AISLE LIGHT) INOP AT ROW 8 LEFT. GROUNDED - YES. RELAMPED AND TESTED PER AMM 33-51-03-960-801. OPS NORMAL.SDR ASAA2016072617528Lamp · failedEMERGENCY AISLE AREA LIGHT IS INOPERATIVE AT SEAT ROWS 24 AND 25ABC. ACFT GROUNDED. REPLACED THE LAMPS IAW AMM 33-51-03-960-801. OPS CHECKED GOOD.SDR ASAA2016042116498Support Bracket · unsecureLEFT FWD DOOR L1 ESCAPE SLIDE PACK LOWER SUPPORT FITTING FOUND OUT OF DOOR SUPPORT BRACKET. SLIDE OUT OF POSITION OFF OF THE DOOR RESULTING IN 33 PERCENT LOSS OF PACK RETENTION TO DOOR. POSSIBLE FAILURE OF CORRECT DEPLOYMENT. ACFT GROUNDED. FOUND BOTTOM BASDR ASAA2015121414484Transition Panel · corrodedAFT CARGO LT TRANSITION PANEL FROM BS 727 TO 787 HAS CORROSION NUMEROUS SPOTS. ACFT GROUNDED. REMOVED CORROSION ON AFT PIT LT TRANSITION PANEL IAW SRM 51-10-02. FROM BS 727- BS 747 ORIGINAL THICKNESS IS .040, REMOVED .010, REMAINING THICKNESS IS .030 OUT OF SDR ASAA2015121414403Transition Panel · corrodedAFT CARGO TRANSITION PANEL CORRODED BETWEEN BS 907 - 927. ACFT GROUNDED. REMOVED CORROSION ORIGINAL MATERIAL .040". REMOVED .001" REMAINING AMT .039" WHICH IS IN LIMITS IAW SRM 53-00-53, FIG 103, DET B. APPLIED ALODINE IAW AMM 51-21-41. APPLIED PRIMER IASDR ASAA2015121414301Transition Panel · corrodedAFT PIT LT TRANSITION PANEL FROM BS 727 TO BS 787 HAS CORROSION NUMEROUS SPOTS. ACFT GROUNDED. REMOVED CORROSION ON AFT PIT LT TRANSITION PANEL IAW SRM 51-10-02. FROM BS 727- BS 747 ORIGINAL THICKNESS IS .040, REMOVED .010, REMAINING THICKNESS IS .030 OUT OFSDR ASAA2015121114372Skin · corrodedLOWER EXTERNAL FUSELAGE, UHF/L NR 1 & NR 2 TELEPHONE ANTENNA MOUNTING AREA CORRODED AT BS 500+8 AND 500A+12. ACFT GROUNDED. REMOVED CORROSION AT BS 500+8 IAW SRM 53-00-01, ORIGINAL THICKNESS .063 IAW 53-30-01, REMAINING .058, REMOVED .005 AT BS 500A+12 ORISDR ASAA2015121014583Window Frame · crackedR3 WINDOW FRAME HAS CRACK AT EXTERNAL FASTENER LOCATED AT FWD LWR CORNER SECOND FROM BOTTOM. ACFT GROUNDED. REPAIRED R3 WINDOW FAME IAW EA 700-56EA-16327, REV. NEW AND REO-G19436, REV A. R & R R2 WINDOW IAW NG AMM 56-12-11. LEAK AND OPS CHECKS GOOD. COMPLSDR ASAA2015120714167Window Frame · crackedR1 WINDOW OTBD POST HAS POSSIBLE CRACK. ACFT GROUNDED. REPAIRED WINDOW POST IAW SB737-53-1336-NG-2.
Back to N626AS