N8677A
Service difficulty reports · 118
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 = 'N8677A' 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 = 'N8677A' 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 SWAA2022021462283Angle · crackedRIGHT HAND PACK BAY HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT STATION 663 RBL 34' IS CRACKED AT FASTENER. ; / [01] HFEC IAW B737 NDT PART 6; 51-00-00 PROC 23. CRACK VERIFIED. TOOL#36303; DUE 13APR22; [02] REMOVED 24 EACH FASTENERS COMMON TO SDR SWAA2022021462192Support · crackedCABIN FLOOR PANEL SUPPORT ANGLE AT STATION 540 LBL 1' CRACKED AT FASTENER HOLE. ; / [01] PART IS 143A5240-35 IAW BOEING DRAWING 143A0060 REV:-. ATAG WN 12485.; [02] REMOVED CABIN SUPPORT ANGLE BS 540 LBL 0 TO LBL 24 IAW SRM 51-40-02.; [03] DRILLED NEW FLOOR PASDR SWAA2022021461859Floor Panel · corrodedA125-24 - FORWARD CARGO BAY - FLOOR PANEL - 120CF - PERIMETER CORRODED ; / [01] VERIFIED DAMAGE ON FLOOR PNL # 120 CF ; FOUND OUT OF LIMITS DUE THE ACCUMULATED DAMAGE LENGTH IS MORE THAN 20 INCHES. IAW SRM 53-00-53-1A-1; [02] IDENTIFIED. MATERIAL FOR FLOOR PNLSDR SWAA2022021461857Floor Panel · corrodedA125-22 - FORWARD CARGO BAY - FLOOR PANEL - 120DF - PERIMETER CORRODED ; / [01] EVALUATED CORROSION FOUND OUT OF LIMITS EXCEEDS 20' IAW B737 SRM 53-00-53-1A-1; [02] VERIFIED ITEM 1; [03] VERIFIED MATERIAL TO BE 2024-T3 CLAD A TAG# A106990 PER B737 AMM 25-52-01SDR SWAA2022021462182Angle · corrodedA125-29 - AFT CARGO BAY - LH FLOOR Z-ANGLE - CORRODED - BS727G TO 807 - LBL 24 - WL 156 ; / [01] REMOVED CORROSION I.A.W SRM 53-00-53-1A-2; [02] VERIFIED MATERIAL LOSE ORIGINAL 0.040 REMOVED .006 REMAIN .036 ALLOWABLE TO REMOVE 10% MAX FOUND OUT OF LIMITS USEDSDR SWAA2022021462184Shield · corrodedA125-30 - AFT CARGO BAY - FLOOR SHIELD FWD OF DOOR - CORRODED ON UPPER AND LOWER SURFACES - BS767 TO 787 - RBL 24 - WL 156 ; / [01] REMOVED CORROSION EVALUATED AREA REMOVED .015 ORIGINAL .050 REMAIN .035 NO ALLOWABLE LIMITS FOUND IN SRM <BR>53-60-15-1A-1 SHIELSDR SWAA2022021462181Angle · corrodedA125-28 - AFT CARGO BAY - RH FLOOR Z-ANGLE - CORRODED - BS727H TO 767 - RBL 24 - WL 156 ; / [01] REMOVED CORROSION I.A.W SRM 53-00-53-1A-2; [02] VERIFIED MATERIAL LOSE ORIGINAL .040 REMOVED .007 REMAIN .033 ALLOWABLE 10% MAX FOUND OUT OF LIMITS USED <BR>AAR TOSDR SWAA2022021661843Fairing · crackedDOT A-24-008 NUMBER 3 FLAP TRACK AFT TAILCONE FAIRING 542EB HAS 2 INCH CRACK AT FORWARD END. / [01] REMOVED #3 FLAP TRACK AFT TAIL CONE 542EB FROM AFT FLAP TRACK FAIRING F.O.M. IAW BOEING SOPM 20-50-01.;[02] SUMMARY EA 22-157-00207 HAS BEEN APPROVED; ACTIVATEDSDR SWAA2022021461838Floor Panel · corrodedDOT A-24-002 AFT PIT FLOOR PANEL 140AF IS CORRODED ON UPPER SURFACE ALONG OUTBOARD EDGES. ; / [01] FLOOR PANEL 140AF IS 'OUT OF LIMITS' TOTAL LENGTH OF CORROSION IS BEYOND LIMITS (20') AS STATED IN SRM 53-00-53-1A-1 FIGURE 102 AD 1.; [02] VERIFY MATERIAL FOR FSDR SWAA2022021461840Floor Panel · corrodedDOT A-24-004 AFT PIT FLOOR PANEL 140CF IS CORRODED ON UPPER SURFACE ALONG OUTBOARD EDGES. ; / [01] MEASURED TOTAL ACCUMULATED LENGTH OF CORROSION DAMAGE TO BE = 37' LIMIT = 20'. FLOOR PANEL 140CF IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102.; [02] VERIFIED NSDR SWAA2022021461841Floor Panel · corrodedDOT A-24-006 AFT PIT FLOOR PANEL 140EF IS CORRODED ON UPPER SURFACE ALONG OUTBOARD EDGES. ; / [01] REMOVED CORROSION IAW SRM 51-10-02 10X MAGNIFY CORROSION EXCEEDED 20' OUT OF LIMITS IAW SRM 53-00-53-1A-1 .071 2024T3 ATAG A106987 AMM 25-52-01-201-801; [02] VERSDR SWAA2022021461837Floor Panel · corrodedDOT A-24-005 AFT PIT FLOOR PANEL 140DF IS CORRODED ON UPPER SURFACE ALONG OUTBOARD EDGES. ; / [01] EVALUATED CORRODED AREA FOUND CORROSION IS MORE THAN 20' <BR>PNL IS OUT OF LIMITS I.A.W SRM 53-00-53-1A-1; [02] VERIFIED MATERIAL FOR NEW PNL AS 2024T3 .071 I.A.SDR SWAA2022021461831Doubler · crackedPOWER RECEPTICAL CUTOUT LOWER LATCH DOUBLER IS CRACKED ; / [01] CUTOUT DAMAGE AT POWER DOOR LOWER LATCH DOUBLER IAW SRM 53-10-15-2R-4 REPAIR4; [02] VERIFIED STEP 1 COMPLETE<BR><BR>HFEC IAW B737 NDT P6 51-00-00 P23 TOOL 36303 DUE 13APR22 NO CRACKS NOTED; [03] VSDR SWAA2021091717225Support Bracket · brokenRH WING FIXED UPPER T/E SUPPORT BRACKET BROKEN JUST INBD OF DEFLECTION RIB BETWEEN #7 & #8 SPOILERS / REMOVED AND REPLACED R/H WING FIXED UPPPER T/E SUPPORT BRACKET PER SRM 51-40-02SDR SWAA2020122938707Skin · crackedGROUND POWER EXTERNAL POWER DOOR CUTOUT CRACKED. REPAIRED IAW SRM 53-10-15-2R-4 REPAIR 4 (SA-M 326 ATTACHED: A1156238).SDR SWAA2020111830925Lens · looseFLOOR EXIT SIGN COVER ROW 14 FED EXIT SEATS. REINSTALLED EXIT LIGHT LENS AT ROW 14DEF, IAW AMM 33-51-01.SDR SWAA2019060333298Hook And Loop · looseL1 DOOR SLIDE EXCESS GIRT BAR MATERIAL LOOSE. / REATTACHED VELCRO ON GIRT IAW AMM AND MT.SDR SWAA2017061414341Cover · looseLT AFT LAV DOOR EMERGENCY LENS COVER LOOSE. SECURED COVER PER MM.
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