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 SWAA2023121824189Angle · corrodedCORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT 767 + 4 ' APROX<[01] REMOVED TRANSITION ANGLE (SHIELD) PER SRM 51-40-02.;[02] REMOVED CORROSION PER SRM 53-60-15-1A-1 (0.046' REMAINING THICKNESS). TRANSITION ANGLE (SHIELD) IS OUT OF LIMITS PER SRSDR SWAA2023121824200Angle · corrodedCORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT 767 +2 ' APROX AT STA 767 +2 ' APROX [<[01] REMOVED TRANSITION ANGLE (SHIELD) PER SRM 51-40-02.;[02] REMOVED CORROSION PER SRM 53-60-15-1A-1 (0.046' REMAINING THICKNESS). TRANSITION ANGLE (SHIELD) SDR SWAA2023121824190Angle · corrodedCORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT 767 + 19 ' APROX<[01] REMOVED CORROSION PER SRM 53-60-15-1A-1 (0.046' REMAINING THICKNESS). TRANSITION ANGLE (SHIELD) IS OUT OF LIMITS PER SRM 53-60-15-1A-1. TRANSITION ANGLE (SHIELD) WILL BE REPLASDR SWAA2023121824191Angle · corrodedCORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT 767 + 12 ' APROX<[01] REMOVED CORROSION PER SRM 53-60-15-A-1 (0.046' REMAINING THICKNESS). TRANSITION ANGLE (SHIELD) IS OUT OF LIMITS PER SRM 53-60-15-1A-1. TRANSITION ANGLE (SHIELD) WILL BE REPLACSDR SWAA2023121824201Angle · corrodedCORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT BS 727 J + 4 ' APROX<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2. TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2. TRANSITION SDR SWAA2023121824202Angle · corrodedCORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT BS 727 J + 2 ' APROX<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.038' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] TRANSITION ANGLE IS OUT OF LIMITS PER SSDR SWAA2023121824204Angle · corrodedCORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT BS 727 J + 12 ' APROX<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] TRANSITION ANGLE IS OUT OF LIMITS PER SDR SWAA2023121824205Angle · corrodedCORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT BS 727 J + 14 ' APROX<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.038' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.<BR>TRANSITION ANGLE WILL BE REPLACED ON NONSDR SWAA2023121824206Floor Support · corrodedCORROSION ON AFT CARGO R/H TRANSITION ANGLE FLOORBOARD HOLE AT BS 727 J + 19 ' APROX<[01] REMOVED CORROSION PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). TRANSITION ANGLE IS OUT OF LIMITS PER SRM 53-00-53-1A-2. TRANSITION ANGLE WILL BE REPLACED ON NONROUSDR SWAA2023121524136Angle · corrodedFWD CARGO RIGHT TRANS-ANGLE CORRODED STA 500A TO 500E+10<[01] WORKED CORROSION ON RT ANGLE PER SRM 51-10-02; REMOVED .020 MATERIAL. REWORKED AREA OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] REMOVED R/H TRANSITION ANGLE ASSY PN 143A7501-188 PER AMM 51-40-02.;[03] SDR SWAA2023121524132Angle · corrodedFWD CARGO RIGHT TRANS-ANGLE CORRODED STA 500E+10 TO 500I<[01] WORKED CORROSION ON RT ANGLE PER SRM 51-10-02; REMOVED .020 MATERIAL; REWORK OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] COMPLIED WITH ON JOB CARD #TTG8Q00PUDNS (LINE # 1264).;[03] COMPLIED WITH ON JOBSDR SWAA2023121524139Angle · corrodedFWD CARGO LEFT TRANS-ANGLE CORRODED STA 500C+7 TO 500I<[01] WORKED CORROSION ON LT ANGLE PER SRM 51-10-02; REMOVED .025 MATERIAL. REWORK OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] REMOVED LH TRANS ANGLE PER SRM 51-40-02-0G-0.<BR>REMOVED L ANGLE AT AFT BULKHEAD TSDR SWAA2023121524153Angle · corrodedCORROSION ON AFT CARGO L/H TRANSITION ANGLE FLOORBOARD HOLE AT 727 C + 2 ' AT STA 727 C + 2 ' APROXIMATELY<[01] REMOVED CORROSION ON AFT CARGO L/H TRANSITION ANGLE AT STA 727C +2. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-005-53-1A-2. AFT CARGO L/H TRANSITIOSDR SWAA2023121524178Angle · corrodedCORROSION ON AFT CARGO L/H TRANSITION ANGLE FLOORBOARD HOLE AT 747 + 10 ' APROX AT STA 747 + 10 ' APROX<[01] REMOVED CORROSION ON AFT CARGO L/H TRANSITION ANGLE AT STA 747+10' LBL 21. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. TRANSITION ANGLE TO SDR SWAA2023121524179Strap · corrodedAFT CARGO BIN UNDER FLOOR STRAP STA 789 RBL 20 CORRODED.<[01] REMOVED AND REPLACED NUTPLATE STRAP PER SRM 51-40-02;[02] REMOVED AND REPLACED NUTPLATE STRAP PER SRM 51-40-02;[03] VERIFIED CORRECTIVE ACTION #1&2SDR SWAA2023121524172Web · corrodedAFT CARGO BIN WEB UNDER DOOR THRESHOLD CORRODED.<[01] FOUND CORROSION DAMAGE OUT OF LIMITS PER SRM 53-60-15-1A-1.REMOVED WEB PER SRM 51-40-02;[02] LOCATED AND DRILLED HOLES FOR NEW WEB PER SRM 51-40-05. LOCATED AND DRILLED HOLES FOR NEW WEB PER SRM 51-40-05;[SDR SWAA2023121524176Angle · corrodedAFT CARGO BIN LT TRANS ANGLE CORRODED STA 807 TO 847.<[01] REMOVE CORROSION ON AFT CARGO COMPARTMENT L/H TRANSITION ANGLE FROM STA 807 TO STA 847 LBL 21. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVE CORROSION ON AFT CARGO COMPARTMENT L/HSDR SWAA2023121524169Angle · corrodedAFT CARGO BIN RT TRANS ANGLE CORRODED STA 767 TO 787.<[01] REMOVED TRANSITION ANGLE (SHIELD) PER SRM 51-40-02.;[02] REMOVED CORROSION PER SRM 53-60-15-A-1 (0.046' REMAINING THICKNESS). TRANSITION ANGLE (SHIELD) IS OUT OF LIMITS PER SRM 53-60-15-1A-1;[03] REJECSDR SWAA2023112724159Angle · corrodedCORROSION ON AFT CARGO L/H TRANSITION ANGLE FLOORBOARD HOLE AT 727 G + 4 ' AT STA 727 G + 4 ' APROXIMATELY<[01] REMOVED CORROSION ON AFT CARGO L/H TRANSITION ANGLE AT STA 727G +4'. DAMAGE FOUND TO BE WITHIN LIMITS PER SRM 53-005-53-1A-2. AFT CARGO L/H TRANSITISDR SWAA2023121823665Seal · crackedL/H HORIZONTAL STAB UPPER FWD SLIDING SEAL CRACKED<[01] REMOVED L/H UPPER FWD SLIDING SEAL;[02] REMOVED AND REPLACED THE ATTACH BRACKET TO THE NEW L/H UPPER FWD SLIDING SEAL REF SRM 51-40-02;[03] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1 AND #2;[04] INSTALLESDR SWAA2023121823668Seal · crackedR/H HORIZONTAL STAB UPPER FWD SLIDING SEAL CRACKED<[01] REMOVED R/H UPPER FWD SLIDING SEAL;[02] REPLACED R/H HORIZONTAL SAB SEAL PER SRM 51-40-02;[03] VERIFIED CORRECTIVE ACTION #2;[04] ADDED STEP 2;[05] REJECT: <BR>WORK ENTRY ITEM #2: IMPROPER FASTENER INSTALSDR SWAA2023121523842Angle · corrodedFWD WET AREA; GALLEY DOOR ENTRY Z ANGLE HAS AN AREA OF BARE METAL BETWEEN STA 328-344 IN RADIUS.<[01] UPON PREPPING AREA FOR TREATMENT THE AREA WAS DETERMINED TO HAVE CORROSION. CORROSION WILL BE WORKED ON FAULT ID TTG8Q00PV04E;[02] VERIFIED CA#1 UPON PREPPINGSDR SWAA2023121523839Floorbeam · corrodedFLOOR BEAM CORRODED STA 947 AT RBL-50 DEEP PIT AT EDGE OF GALLEY FITTING<[01] REMOVED CORROSION PER SRM 51-10-02. THE REWORKED AREA IS OUT OF LIMIT PER SRM 53-70-51-1A-1 FIG 104 DETAIL N.;[15] INSTALLED ALL FASTENERS IN STA 947 SPLICE ANGLES PER SRM 53-70-51-2SDR SWAA2023121523841Floor Support · corrodedFLOOR SUPPORT CORRODED STA 950 RBL -51 AFT SIDE AROUNG GALLEY FITTING<[01] REMOVED CORROSION PER SRM 53-70-51-1A-1 (0.188' REMAINING THICKNESS). FLOOR SUPPORT (INTERCOSTAL) IS OUT OF LIMITS PER <BR>SRM 53-70-51-1A-1.;[02] REMOVED FLOOR SUPPORT (INTERCOSTAL) PESDR SWAA2023121523851Floorbeam · corrodedFLOOR BEAM CORRODED AT STA 947 LBL-50 AROUND GALLEY FITTING<[01] REMOVED CORROSION FROM STA 947 FLOOR BEAM THAT WAS UNDER PAD .FOUND TO BE IN LIMITS FLOOR BEAM ONLY PER SRM 53-70-51-1A-1;[02] CORROSION DAMAGE TO MACHINED INTERCOSTAL UNDER PAD OUT OF LIMITS PERSDR SWAA2023121523151Scuff Plate · crackedFWD B/B FWD CORNER SCUFF PLATE CRACKED<[01] REMOVED AND REPLACED FWD CARGO CORNER SCUFF PLATE PER SRM 53-11-02.;[02] C/W INSPECTION;[03] C/W INSPECTIONSDR SWAA2023121823147Tab · delaminatedLEFT HAND ELEVATOR TAB TRAILING EDGE CARBON FIBER DELAMINATED<[01] VERIFIED SERVICEABLE REPLACEMENT L/H ELEVATOR TAB WEIGHT OF 8.46 LBS AND 4EA TAB ADJUST WEIGHTS INSTALLED IN L/H ELEVATOR BAY 2 IAW SRM 51-61-06-0G-0 TABLE 1.;[02] VERIFIED SERVICEABLE REPLACEMSDR SWAA2023092604049Light · inoperativeAFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED AFT SERVICE DOOR EXTERIOR LIGHT IN REF AMM 33-51-04. OPS CHECK GOODSDR SWAA2023092604047Battery Pack · inoperativeMULTIPLE FWD INTERIOR AND FWD ENTRY EXTERIOR EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED POWER SUPPLY BATTERY FOR FWD ENTRY ADN FWD EMERGENCY LIGHTS IN REF TO AMM 33-51-06. OPS CHECK GOODSDR SWAA2023090797906Brake · fireWHILE AT GATE #1TIRE FUSE BLEW AND A MONETARY FIRE ON BRAKE<[01] REMOVED AND REPLACED #1 MAIN WHEEL ASSY REF AMM 32-45-11 TO FACILITATE AIRCRAFT MOVEMENT TO THE HANGAR. THE #1 WHEEL ASSY WILL BE REMOVED FOR OTHER MAINT AND INSP.;[02] REMOVED #1 MAIN TIRE ASSY SDR SWAA2023090596424Battery Pack · inoperativeRH AFT EXTERIOR OVER WING EMERGENCY EXIT LIGHTS INOP.<[01] R&R EMERGENCY EXIT LIGHT BATTERY PACK AT STATION 727C+13 RBL 52. REF AMM 33-51-51. OPS CHECK GOODSDR SWAA2023072682014Handle · brokenAFT SERVICE DOOR ASSIST HANDLE BROKEN OFF<[01] REPLACED AFT SERVICE DOOR ASSIST HANDLE REF AMM 25-21-25SDR SWAA2023060957160Battery Pack · inoperativeEMERGENCY LIGHTS AT ROW 6-7FED;10-11FED;12-14FED INOP.<[01] R+R BATTERY PACK @ 8FED IAW AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2023060957323Battery Pack · inoperativeEMERGENCY LIGHT ROW 27ABC AND LEFT AFT GALLEY EMERGENCY EXIT LIGHT INOP.<[01] R+R BATTERY PACK @ LEFT AFT M-1673 LOCATION IAW AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2023032017841Flap · delaminatedWORKING TASK CARD TTG8Q008U3R4 : R/H AFT OUTBOARD FLAP DELAMINATED AT I/B LOWER CORNER REQUIRES REPLACEMENT<[01] REMOVED AND REPLACED R/H AFT OUTBOARD FLAP PER AMM 27-51-22.;[02] INSPECTION VERIFIED CORRECTIVE ACTION STEP 1. RII WITHIN AMM 27-51-22 COMPLIED WISDR SWAA2023012795333Fairing · cracked#1 ENGINE AFT STRUT FAIRING AFT FITTING CRACKED<[01] MEASUREMENT FIELD COMPLETED.;[02] INSTALLED #1 ENG AFT STRUT FAIRING END CAP IAW SRM 51-40-02.;[03] COMPLIED WITH AFT STRUT FAIRING FITTING ASSY REMOVAL AND REPLACEMENT PER SRM 51-40-02. REMOVED AND REINSTALSDR SWAA2023012795336Skin · delaminatedRIGHT OUTBOARD AFT FLAP DELAMINATED AT BOTTOM INBOARD CORNER.<[01] ACCOMPLISHED WITH EA 23-157-00293. (TTG8Q00HG3ZA)SDR SWAA2022081140946Light · out of positionCEILING EMERGENCY EXIT SIGN COVER CAME OFF / [01] RESECURED CEILING EMERGENCY EXIT SIGN COVER PER SIP.SDR SWAA2022060915840Handle · inoperativeFORWARD SERVICE DOOR HANDLE COVER FELL OFF. OK TO CONTINUE PER MEL 25-10-01 SP1B. FOUND MISSING COVER AND INSTALLED ORIGINAL COVER BACK ONTO FWD SERVICE DOOR HANDLE. IAW AMM 52-11-31.SDR SWAA2022051807927Sign · missingEMERGENCY EXIT SIGN MISSING ON CENTER AISLE / [01] REPLACED EMERGENCY EXIT SIGN CENTER AISLE MID CABIN REF AMM 33-51-01. OPS CHECK GOODSDR SWAA2022011360792Lamp · inoperativeFWD R/H EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT IS INOP ; / [01] REPLACED FWD R/H EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT LAMP. OPS CHECKS GOOD IAW AMM 33-51-04-960-801; [02] ALL WORK C/W<BR>AUDIT C/WSDR SWAA2021123056728Doubler · crackedEXTERNAL POWER CUTOUT LOWER DOOR LATCH BLOCK ATTACH POINT CRACKED ; / [01] CUT-OUT DAMAGE AT EXTERNAL POWER CUTOUT LOWER DOOR LATCH BLOCK ATTACH POINT IAW SRM 53-10-15-2R-4 REPAIR 4 STEP(4); [02] VERIFIED NEW DOUBLER MATERIAL AS 2024-T3-.050/ ALSO VERIFIED NEWSDR SWAA2022011753981Floor Panel · corrodedA091-002 AFT CARGO COMPARTMENT FLOOR PN# 140BF CORRODED ALONG EDGES; UPPER AND LOWER SURFACES ; / [01] FABRICATED NEW FLOOR PANEL 140BF ON FAULT TTG8Q009V472; [02] VERIFIED STEP 1<BR>AUDIT CWSDR SWAA2022011753983Floor Panel · corrodedA091-005 AFT CARGO COMPARTMENT FLOOR PN# 140EF CORRODED ALONG EDGES UPPER AND LOWER SURFACES. ; / [01] EVALUATED CORROSION AND FOUND TO BE OUT OF LIMITS EXCEEDS 20' IAW B737 SRM 53-00-53-1A-1; [02] VERIFIED MATERIAL TO BE 2024-T3 .071' A TAG A105082 IAW B737 ASDR SWAA2022011753982Splice · corrodedA091-004 AFT CARGO COMPARTMENT FLOOR PN# 140BF TRANSITION STRIP CORRODED ; / [01] VERIFIED AND REPLACED AFT CARGO COMPARTMENT FLOOR PANEL SPLICE STRIP AT STA 727D+5.6' ON PARTS RACK IAW IPC 53-42-11-26 AND BOEING DWG PL 146A9401 REV:D; [02] VERIFIED STEP 1<BR>SDR SWAA2022011453979Floor Panel · corrodedA091-007 AFT CARGO COMPARTMENT FLOOR PN# 140AF CORRODED ALONG EDGES ON UPPER AND LOWER SURFACES ; / [01] EVALUATED CORROSION FOUND TO BE OUT OF LIMITS. EXCEEDS 20' IN LENGTH. IAW B737 SRM 53-00-53-1A-1; [02] VERIFIED NEW MATERIAL FOR PANEL TO BE 2024-T3 .071 ISDR SWAA2022011353822Support Angle · crackedDOT 050-017 AFT CARGO COMPARTMENT STA 867 LBL11 WL 165 ENCLOSURE SUPPORT ANGLE IS CRACKED ; / [01] REMOVED ENCLOSURE SUPPORT ANGLE IAW SRM 51-40-02; [02] VERIFIED NEW ANGLE TO BE MPN: 149A8109U114 ATAG: A94253 IAW DWG: 149A8102 REV: A; [03] LOCATED AND DRILLEDSDR SWAA2022011353816Floor Panel · corrodedDOT 050-016 AFT CARGO COMPARTMENT FLOOR PANEL SPLICE STA 887 LBL6 WL168 IS CORRODED ; / [01] REMOVED DAMAGED PANEL SPLICE AT STA 887 IAW SRM 51-40-02-0G-0 SECTION 9.; [02] VERIFIED NEW FLOOR PANEL SPLICE P/N 146A9401U39 IAW IPC 53-42-11-26 AND BOEING DWG PL 45SDR SWAA2022011353814Floor Panel · corrodedDOT 050-010 AFT CARGO COMPARTMENT STA 767+5 WL 156 LBL 20 TO RBL 20 FLOOR PANEL SPLICE IS CORRODED ; / [01] VERIFIED AND REPLACED AFT CARGO FLOOR PANEL SPLICE AT 767+5' ON PARTS RACK IAW IPC 53-42-11-26 AND BOEING DWG# 146A9401 ID:0002 REV:C; [02] ALL WORK C/WSDR SWAA2022011353815Angle · corrodedDOT 050-015 AFT CARGO COMPARTMENT R/H SIDE ZEE ANGLE STA 727I TO STA 767 RBL 20 WL 156 IS CORRODED ; / [01] BLENDED CORROSION ON RH ZEE ANGLE STA 727I-767. FOUND STA 727H+10'-767 OUT OF LIMITS WITH ORIGINAL .040'; REMAINING .026'; LOSS OF .014' IAW SRM 53-00-5
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