N8675A
Service difficulty reports · 130
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 = 'N8675A' 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 = 'N8675A' 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 SWAA2022011353817Shield · corrodedDOT 050-009 AFT CARGO COMPARTMENT STA 767 TO STA 794 RBL 22 WL 156 SHIELD HAS CORROSION ; / [01] BLENDED CORROSION ON RH SHIELD STA 767-794; ORIGINAL .050'; REMAINING .030; LOSS OF .020' WITH NO PUBLISHED SRM LIMITS REQUIRES REPLACEMENT IAW SRM 51-10-02-0G-0; SDR SWAA2022011353818Angle · corrodedDOT 050-011 AFT CARGO COMPARTMENT L/H SIDE ZEE ANGLE STA 727J TO STA 847 LBL 20 WL 156 IS CORRODED ; / [01] BLENDED CORROSION ON LH ZEE ANGLE STA 727J-847. FOUND STA 727J-787+10' OUT OF LIMITS WITH ORIGINAL .040'; REMAINING .030'; LOSS OF .010' IAW SRM 53-00-5SDR SWAA2022011353819Angle · corrodedDOT 050-012 AFT CARGO COMPARTMENT L/H SIDE ZEE ANGLE STA 727F TO STA 727J LBL 20 WL 156 IS CORRODED ; / [01] BLENDED CORROSION ON LH ZEE ANGLE STA 727F-727J. FOUND STA 727G+10'-727J OUT OF LIMITS WITH ORIGINAL .040'; REMAINING .023'; LOSS OF .017' IAW SRM 53-0SDR SWAA2022011353824Angle · crackedLEFT HAND PACK BAY; HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT STATION 663 LBL 35 IS CRACKED AT FASTENER HOLE. ; / [01] HFEC IAW B737 NDT PART 6; 51-00-00 PROC 23. CRACK VERIFIED. TOOL#36303; DUE 13APR22; [02] REMOVED L/H O/B C CHANEL FOR ACCSDR SWAA2022011353823Angle · crackedRIGHT HAND PACK BAY; HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT STATION 663 RBL 10 IS CRACKED 3RD FASTENER OUTBOARD OF KEEL BEAM VERTICAL ANGLE. ; / [01] REMOVED DAMAGED ATTACHESD ANGLE IAW SRM 57-10-10-2R-5 STEP 4 B.; [19] REPAIRED R/H PACK SDR SWAA2022011753560Floor Panel · corrodedFWD CARGO COMPARTMENT FLOOR PNL # 120DF L/H ; R/H AND AFT SIDE EDGES OF PNL TOP SKIN SURFACE UNDER CAP STRIPS IS CORRODED AS MARKED LENGTH OF PNL ; / [01] REMOVED CORROSION IAW SRM 51-10-02 VERIFIED WITH 10X MAGNIFY CORROSION EXCEEDS THE MAXIMUM 20'THEREFORE TSDR SWAA2022011753556Floor Panel · corrodedFWD CARGO COMPARTMENT FLOOR PNL # 120CF FWD; L/H AND R/H SIDES TOP SKIN UNDER CAP STRIPS IS CORRODED THE LENGTH AND WIDTH OF PNL AS MARKED ; / [01] VERIFIED LIMITS; CORROSION LENGTH EXCEEDS 20' OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIGURE 102.; [02] VERIFIED MATSDR SWAA2022011353561Floor Panel · corrodedFWD CARGO COMPARTMENT FLOOR PNL 120BF L/H/S TOP SKIN UNDER CAP STRIPS LENGTH OF PNL IS CORRODED AS MARKED ; / [01] VERIFIED CORROSION IS OUT OF LIMITS DUE BEING GREATER THAN 20SQ INCHES INA SRM 53-00-53-1A-1; [02] VERIFIED MATERIAL FOR NEW PANEL TO BE 2024-T3 SDR SWAA2022011353548Angle · corrodedFWD CARGO COMPARTMENT FLOOR STRUCTURE STA 500B TO 500C; RBL 24; WL 156 R/H Z-ANGLE HAS CORROSION. A224-12 ; / [01] REMOVED CORROSION IAW SRM 51-10-02 VERIFIED WITH 10X MAGNIFY ORIGINAL THICKNESS .040 MATERIAL REMOVED .007 REMAINING MATERIAL .033 FOUND TO BE OUSDR SWAA2022011353543Angle · corrodedFWD CARGO COMPARTMENT FLOOR STRUCTURE STA 500B+18; LBL 24; WL 156 L/H Z-ANGLE HAS CORROSION. A224-005 ; / [01] REMOVED CORROSION IAW SRM 51-10-02 VERIFIED WITH 10X MAGNIFY ORIGINAL THICKNESS .040 MATERIAL REMOVED .006 REMAINING MATERIAL034 OUT OF LIMITS IAW SRSDR SWAA2022011353396Shield · corrodedFWD CARGO COMPARTMENT FLOOR STRUCTURE STA 500 TO 500A; RBL 24 AND WL 156 SHIELD HAS CORROSION. A224-001 ; / [01] REMOVED CORROSION IAW SRM 51-10-02 VERIFIED WITH 10X MAGNIFY ORIGINAL THICKNESS.040 MATERIAL REMOVED .007 MATERIAL REMAINING .033 OUT OF LIMITS IAWSDR SWAA2021123053799Strip · corrodedFWD CARGO COMPARTMENT R/H CAP STRIPS 2EA AS MARKED BOTTOM SKIN SURFACES ARE CORRODED ENTIRE LENGTH OF STRIP ; / [01] REMOVED CORROSION IAW SRM 51-10-02 VERIFIED WITH 10X MAGNIFY ORIGINAL THICKNESS.063 MATERIAL REMOVED .008 MATERIAL REMAINING .055 OUT OF LIMITSSDR SWAA2021123053800Strip · corrodedFWD CARGO COMPARTMENT L/H/S CAP STRIPS 2EA OUT OF 4 EA CAP STRIPS ARE CORRODED IN SEVERAL AREAS BOTTOM SKIN AS MARKED ; / [01] REMOVED CORROSION IAW SRM 51-10-02 ORIGINAL THICKNESS.063 MATERIAL REMOVED .008 MATERIAL REMAINING .055 OUT OF LIMITS. REPLACED -14 SDR SWAA2021123053555Angle · corrodedFWD CARGO COMPARTMENT FLOOR STRUCTURE STA 500E TO 500F; RBL 24; WL 156 R/H Z-ANGLE HAS CORROSION. A224-15 ; / [01] REMOVED CORROSION IAW SRM 51-10-02 VERIFIED WITH 10X MAGNIFY ORIGINAL THICKNESS .040 MATERIAL REMOVED .007 MATERIAL REMAINING .033 FOUND TO BE OUSDR SWAA2022011352782Angle · crackedLEFT WING; DEFLECTION CONTROL RIB; INBOARD ATTACH ANGLE TO WEB IS CRACKED AT FASTENER HOLES COMMON TO DEFLECTION CONTROL RIB. A045-005 ; / [01] REMOVED LH WING DEFLECTION CONTROL RIB ATTACH ANGLE IAW SRM 51-40-02; [02] VERIFIED NEW ANGLE TO BE MPN: 115A6260-1 SDR SWAA2022011352783Attach Angle · crackedRIGHT WING; DEFLECTION CONTROL RIB; INBOARD ATTACH ANGLE TO WEB IS CRACKED AT FASTENER HOLES COMMON TO DEFLECTION CONTROL RIB. A045-006 ; / [01] REMOVED AND REPLACED R/W DEFLECTION RIB INBD ATTCH ANGLE IAW DWG 115A6200 REV:A SRM 51-40-02-OG-O; [02] REMOVED ANDSDR SWAA2022011352784Web · crackedLEFT WING; JUST INBOARD OF CONTROL RIB; WEB IS CRACKED AT OUTBOARD FASTENER HOLE COMMON TO UPPER PANEL. A045-007 ; / [01] REMOVED LH WING IB OF CONTROL RIB WEB IAW SRM 51-40-02; [02] VERIFIED NEW WEB TO BE MPN: 115A2156U7 ATAG: A106439 IAW DWG: 115A2512 REV: -SDR SWAA2021121452612Sleeve · crackedAPPROXIMATELY 1/2' CRACK AND IMPRESSION #1 ENGINE THRUST REVERSER SLEEVE OUTBOARD ; / [01] COMPLIED WITH EA 21-154-03700SDR SWAA2021120249157Lens · missingOVERHEAD CABIN EMER. EXIT SIGN MISSING ; / [01] LOCACATED AND INSTALLED EXIT SIGN LENS. REF AMM 33-51-01SDR SWAA2021110941820Battery · inoperativeFWD ENTRY DOOR EMERGENCY EXIT INT LIGHTS AND FWD L/H ESCAPE SLIDE LIGHT INOP. ; / [01] R+R FWD ENTRY DOOR EMERGENCY BATTERY PER AMM 33-51-06 OPS CHECK IS GOOD; [02] ADDED ADDITIONAL LABOR ROW IN ERRORSDR SWAA2021080298565Lamp · inoperativeEXTERIOR EMERGENCY LIGHT NEXT TO AFT ENTRY DOOR INOP / RE-LAMPED EMERGENCY LIGHT PER AMM 33-51-04SDR SWAA2021032958385Stringer · damaged***DELAY PURPOSE ONLY*** AFT CARGO STRINGER DAMAGE / C/W EA 21-153-007700.SDR SWAA2021020245321Landing · crackedGROUND POWER DOOR LOWER FLANGE CRACKED / TRIMMED OUT DAMAGE ON GROUND POWER DOOR LOWER FLANGE PER SRM 53-10-15-2R-4. HFEC REQUIRED. C/W HFEC OF DAMAGE CUTOUT PER NDT PART 6 51-00-00 PROD 23. NO DEFECTS NOTED. (D127). COMPLETED REPAIR PER SRM 53-10-15-2R-4SDR SWAA2020072001103Floor Panel · damagedCENTER ISLE, POPPING SOUND BY ROW 16, PERFORMED A PERMANENT REPAIR BY REPLACING THE FLOOR PANEL OR RECTIFY IAW AMM 53-21-00/401.SDR SWAA2022030753043Floor Panel · damagedCENTER FLOOR AT ROW 17 IS OIL CANNINGCOMPLIED WITH EA 1-A53-31403. PERFORM GENERAL VISUAL EXAMINATION OF PANEL TO ENSURE PANEL IS FREE OF DEFECTS.(CRACKS; DENTS;PUNCTURES; ETC.) PERFORM PERMANENT REPAIR BY REPLACING PANEL OR RECTIFY PER AMM 53-21-00/401. INSPESDR SWAA2019011728563Slide · defectiveR1 DOOR SLIDE ASPIRATOR ORIENTATION INCORRECT. R&R SLIDE PER MT.SDR SWAA2018112127005Light · unsecureCENTER WING AISLE EMERGENCY EXIT OVERHEAD LIGHT FELL OFF. SECURED LIGHT IAW AMM.SDR SWAA2018041621228Sign · missingR2 DOOR EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER AMM.SDR SWAA2017031312455Lamp · inoperativeLEFT WING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW MM.SDR SWAA2016082455117Lens · looseAISLE OVERWING EXIT SIGN LENS LOOSE. SECURED LENS IAW MM.
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