N8313F
Service difficulty reports · 177
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 = 'N8313F' 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 = 'N8313F' 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 SWAA2024012930852Support · corrodedFWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 500E - 500A; RBL 24; WL 156<[01] REJECTED FOR DOCUMENTATION ONLY; SUB TASK EA INSTRUCTION IS NOT COMPLIED WITH FOR DOCUMENTATION AND SIGN-OFF REQUIREMENTS OF THIS FAULT.;[02] ' THE DAMAGE WAS SDR SWAA2024012530523Floorbeam · corrodedCORROSION ON BS 947.5 FLOOR BEAM LBL 52 WL 208<[01] EDITED CORRODED P/N;[02] UPDATED STEP 14;[03] PARTIAL STEP 14;[04] PARTIAL STEP 14;[05] PARTIAL STEP 16-17-18;[06] PARTIAL UPDATE STEP 15;[07] PARTIAL UPDATE STEP 19;[08] PARTIAL UPDATE STEP 20;[09] COMPLETEDSDR SWAA2024012530524Floor Support · corrodedCORROSION ON FLOOR SUPPORT BS 947.5+2 LBL 26 WL 208<[01] UPDATED MEASUREMENT TABLE.;[02] REMOVED AND REPLACED FLOOR SUPPORT BS 947-967; LBL 25; WL 208 PER SRM 51-40-02-0G-0 AND BOEING DWG 147A5660.;[03] VERIFIED CORRECTIVE ACTION 2.<BR>VERIFIED MEASUREMENTS TASDR SWAA2024012530840Floorbeam · corrodedUPON REMOVING LAV D HARDPOINT FITTING; FOUND CORROSION ON BS 947.5 FLOOR BEAM AT LBL 26 WL 208.<[01] UPDATED MEASUREMENT TABLE.;[02] BLENDED CORROSION ON BS 947.5 FLOOR BEAM AT LBL 26 WL 208 <BR>1'X1'X.030' AREA; ORIGINAL THICKNESS .180 FOUND TO BE OUT OF LIMISDR SWAA2024012530844Shield · corrodedFWD CARGO COMPARTMENT AFT SHIELD HAS CORROSION AT BS 480+16; RBL 24; WL 156<[01] VERIFIED ALL STEP COMPLETED;[02] VERIFIED RII REQUIREMENTS COMPLETE;[03] VERIFIED CORRECTIVE ACTION ITEMS COMPLETE; AND MEASUREMENT TABLE; CARD COMPLETE.SDR SWAA2024012530850Sidewall Support · corrodedFWD CARGO COMPARTMENT AFT SIDEWALL BULKHEAD SUPPORT HAS CORROSION AT BS 500I; RBL 25; WL 156<[01] FAULT TTG8Q00Q7TQG COMPLETED;[02] VERIFIED JOB COMPLETE<BR><BR>VERIFIED MEASUREMENT TABLESDR SWAA2024012530847Sidewall Support · corrodedFWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 500I - 500E+14; RBL 24; WL 156<[01] TASK COMPLETE;[02] MEASUREMENT FIELD'S ITEM 1 AND 2 INCORRECT; NO RII MAINTENANCE IS PERFORMED ON THIS CARD. NO MAJOR REPAIR ACTION ON THIS CARD.;[03] TASK SDR SWAA2024011730026Handle · brokenFWD ENTRY DOOR UPPER ASSIST HANDLE BRACKET UPPER FORWARD NUT PLATE IS BROKEN.<[01] REMOVED AND REPLACED DAMAGED NUTPLATE PER SRM 51-40-02-0G-0 PARAGRAPH 4;[02] VERIFIED CORRECTIVE ACTION STEP 1; VERIFIED MEASUREMENTS TABLE AND TASK CARD COMPLETE.SDR SWAA2024011730258Floor Panel · pulledCABIN FLOOR PANEL 242E HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] CABIN FLOOR PANEL 242E WITH NUMEROUS PULLED FIBERGLASS STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVSDR SWAA2024011730259Floor Panel · pulledCABIN FLOOR PANEL 242D HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] CABIN FLOOR PANEL 242D WITH NUMEROUS PULLED FIBERGLASS STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVSDR SWAA2024011730260Floor Panel · pulledCABIN FLOOR PANEL 242SF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] CABIN FLOOR PANEL 242SF WITH NUMEROUS PULLED FIBERGLASS STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED ACTION SDR SWAA2024011730271Floor Panel · pulledCABIN FLOOR PANEL 242UF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] CABIN FLOOR PANEL 242UF WITH NUMEROUS PULLED FIBERGLASS STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTSDR SWAA2024011730272Floor Panel · pulledCABIN FLOOR PANEL 242RF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] CABIN FLOOR PANEL 242RF WITH NUMEROUS PULLED FIBERGLASS STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED ACTION SDR SWAA2024011730261Floor Panel · pulledCABIN FLOOR PANEL 241ABF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] CABIN FLOOR PANEL 241ABF WITH NUMEROUS PULLED FIBERGLASS STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRESDR SWAA2024011730273Floor Panel · pulledCABIN FLOOR PANEL 241AAF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE FABRICATED NEW FLOOR PANEL 241AAF USING BMS4-17 TYIV LOT#1544951-1 AND INSTALLED INSERTS USING BMS5-107 LOT#AK3BA2380A/A THEN PART MARKED AND APPLIED TAPE IAW SRMSDR SWAA2024011730262Floor Panel · pulledCABIN FLOOR PANEL 241YF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] CABIN FLOOR PANEL 241YF WITH NUMEROUS PULLED FIBERGLASS STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED ACTION SDR SWAA2024011730263Floor Panel · pulledCABIN FLOOR PANEL 241ZF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] CABIN FLOOR PANEL 241ZF WITH NUMEROUS PULLED FIBERGLASS STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED ACTION SDR SWAA2024011730264Floor Panel · pulledCABIN FLOOR PANEL 241XF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] CABIN FLOOR PANEL 241XF WITH NUMEROUS PULLED FIBERGLASS STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED ACTION SDR SWAA2024011730265Floor Panel · pulledCABIN FLOOR PANEL 241F HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] CABIN FLOOR PANEL 241F WITH NUMEROUS PULLED FIBERGLASS STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED ACTION 1 SDR SWAA2024011730266Floor Panel · pulledCABIN FLOOR PANEL 241D HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] CABIN FLOOR PANEL 241D WITH NUMEROUS PULLED FIBERGLASS STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVSDR SWAA2024011730267Floor Panel · pulledCABIN FLOOR PANEL 222BF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] NUMEROUS PULLED FIBERGLASS STRANDS ON CABIN FLOOR PANEL 222BF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2024011730274Floor Panel · pulledCABIN FLOOR PANEL 222DF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] CABIN FLOOR PANEL 222DF WITH NUMEROUS PULLED FIBERGLASS STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTSDR SWAA2024011730275Floor Panel · pulledCABIN FLOOR PANEL 222CF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] CABIN FLOOR PANEL 222CF WITH NUMEROUS PULLED FIBERGLASS STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTSDR SWAA2024011730268Floor Panel · pulledCABIN FLOOR PANEL 222GF HAS NUMEROUS PULLED FIBERGLASS STRANDS. CABIN FLOOR PANEL 221GF HAS NUMEROUS PULLED FIBERGLASS STRANDS. THE CORRECT PANEL NUMBER REQUIRING REPAIR IS 221GF.<[01] CABIN FLOOR PANEL 221GF WITH NUMEROUS PULLED FIBERGLASS STRANDS WAS REPLACESDR SWAA2024011730276Floor Panel · pulledCABIN FLOOR PANEL 221FF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] CABIN FLOOR PANEL 221FF WITH NUMEROUS PULLED FIBERGLASS STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED ACTION SDR SWAA2024011730277Floor Panel · pulledCABIN FLOOR PANEL 221EF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] CABIN FLOOR PANEL 221EF WITH NUMEROUS PULLED FIBERGLASS STRANDS WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED RII STEPS COMPLETE;[03] VERIFIED JOB COMPLETE AND CURE SHEETSSDR SWAA2024011730269Floor Panel · pulledCABIN FLOOR PANEL 221DF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] NUMBER PULLED FIBERGLASS STRANDS ON UPPER SURFACE OF CABIN FLOOR PANEL 221DF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2024011730270Floor Panel · pulledCABIN FLOOR PANEL 221CF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] FLOORBOARD 221CF PULLED FIBERGLASS STRANDS HAVE BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED REPAIR COMPLETE;[03] VERIFIED JOB COMPLETE AND CUSDR SWAA2024011730278Floor Panel · pulledCABIN FLOOR PANEL 221AF HAS NUMEROUS PULLED FIBERGLASS STRANDS.<[01] CABIN FLOOR PANEL 221AF WITH NUMEROUS PULLED FIBERGLASS STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED ACTION SDR SWAA2024012929283Skin · corroded#2 SLAT O/B UPPER AFT CORNER IS CORRODED.<[01] DISREGARD INSP ITEM DALE; MICHAEL STEPS 1;3;[02] STEP 2 PARTIAL ADJUSTMENT.;[03] COMPLETED STEP 4;[04] CERTIFIED;[05] CERTIFIED;[06] UPDATED RII;[07] CERTIFIED;[08] REMOVED AND REINSTALLED #2 SLAT PER AMM 27-81-21SDR SWAA2024011729688Scuff Plate · crackedFWD CARGO BAY FWD CORNER SCUFF PLATE CRACKED<[01] FWD CARGO BAY FWD CORNER SCUFF PLATE GOING TO BE INSTALL ON TASK CARD TTG8R0058GK;[02] WELDED THE CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-30-15-2R-1 PARAGRAPH 4.B.(4) AND BAC597SDR SWAA2024011729285Flap · delaminatedR/W O/B AFT FLAP LOWER I/B END IS DELAMINATED REQUIRING REPAIR<[01] PARTIALED STEP 1;[02] VERIFIED STEP 1 IN PARTIAL.;[03] REMOVED AND REINSTALLED IAW AMM 27-51-22/401;[04] UPDATED RII;[05] VERIFIED STEPS 1;2 COMPLETE; ADJUSTMENT CHECK DUE.;[06] REMOVED AND RESDR SWAA2024012929008Angle · crackedRIGHT WING UPPER TRAILING EDGE PANEL ATTACHMENT ANGLE JUST I/B SIDE OF DEFLECTION CONTROL RIB IS CRACKED<[01] REMOVED AND REPLACED R/W UPPER TRAILING EDGE PANEL ATTACHMENT ANGLE P/N 115A6260-2; JUST I/B SIDE OF DEFLECTION CONTROL RIB IAW SRM 51-40-02-0G-0 AND SDR SWAA2024012632747Rib · looseRIGHT WING DEFLECTION CONTROL RIB IS LOOSE<[01] REPAIRED RIGHT WING DEFLECTION CONTROL RIB AND PANEL SUPPORT IAW SRM 57-51-02-2R-1; SRM 57-51-02-2R-4;[02] VERIFIED COMPLETE STEP 9; MEASUREMENTS TABLE OK; CARD COMPLETE.SDR SWAA2024012428719Cover Plate · missingWHILE REMOVING G4 GALLEY FOUND LOWER ATTACH FITTING'S COVER PLATES AT FLOOR MISSING MINUS AFT L/H.<[01] REPLACED AND SEALED MISSING G4 GALLEY LOWER ATTACH FITING'S COVER PLATES AT FLOOR MINUS AFT L/H PER AMM 25-31-41-400-801-005 STEP 3.G.13;[02] VERIFIED CORRESDR SWAA2023110919037Cover · missingEMER EXIT ROW LIGHT COVER MISSING ROW 14 AIRCRAFT RIGHT / [01] INSTALLED MISSING COVER PER AMM 33-51-01SDR SWAA2023071777383Seal · crackedRH HORIZONTAL STABILIZER UPPER SLIDING SEAL IS CRACKED<[01] R&R RH HORIZONTAL STABILIZER UPPER SLIDING SEAL. IAW AMM 53-31-31SDR SWAA2023061358131Slide · looseAFT RIGHT SIDE DOOR SLIDE FELL OUT CASE<[01] REPACKED Z-FOLD OF R2 DOOR SLIDE. REF AMM 25-66-01SDR SWAA2022092283101None · damagedFORWARD F.O. SIDE PHOTOLMINESCENT AISLE STRIP DIM / [01] CLEANED IAW M/M 33-51-15SDR SWAA2022012763883Fairing · cracked#3 CANOE FAIRING CENTER HAS CRACK ON THE INSIDE OF FAIRING (CENTER AFT ) ; / [01] REMOVED DAMAGE TO #3 CANOE IAW SRM 51-70-05-2R-0. DAMAGE LIMITED TO INNER PLIES. NO HONEYCOMB DAMAGE NOTED. APPLIED REPAIR AS PER SRM 51-70-05-2R-0; SEALED PER SRM 51-70-08.SDR SWAA2022020363423Skin · delaminatedLH O/B AFT FLAP LOWER SURFACE HAS DELAMINATION SPOT AT LOWER SURFACE INBD CORNER. ; / [01] REMOVED L/H O/B AFT FLAP; [02] INSTALLED NEW L/H O/B AFT FLAP ASSY PER A.M.M. 27-51-22.; [03] C/W RII INSPECTION INSTALLED NEW L/H O/B AFT FLAP ASSY PER A.M.M. 27-51-22.SDR SWAA2022020961777Bracket · cracked90 DEGREE ANGLE BRACKET ON PANEL 651FB IS CRACKED AT THE BEND RADIUS. ; / [01] REMOVED THE BRACKET PER SRM 51-40-02.; [02] INSTALLED NEW BRACKET PER SRM 51-40-02.; [03] INSTALLED NEW BRACKET PER SRM 51-40-02.SDR SWAA2022020961104Bracket · crackedRIGHT WING; BULB SEAL SUPPORT ANGLE BRACKET CRACKED; OUTBOARD END @ DEFLECTION CONTROL RIB; FORWARD OF SEAL; (MARKED; PICTURE) ; / [01] REMOVED AND REPLACED SUPPORT ANGLE BRACKET P/N 115A6260-1 PER SRM 51-40-02.; [02] INSPECTED AS REQUIRED.SDR SWAA2022020961102Support · crackedCABIN FLOOR SUPPORT IS CRACKED AT STA 540 RBL 1 ; / [01] REMOVED AND REPLACED CABIN SUPPORT ANGLE AT STA 540 PER SRM 51-40-02.; [02] C/W INSPECTIONSDR SWAA2022020961101Support · crackedCABIN FLOOR SUPPORT IS CRACKED AT STA 540 LBL 1 ; / [01] REMOVED FLOOR SUPPORT FOR REPLACEMENT PER SRM 51-40-02. AWAITING PART 143A5240-35; [02] LOCATED NEW FLOOR SUPPORT PER SRM 51-40-05 AND INSTALLED NEW FLOOR SUPPORT PER SRM 51-40-02SDR SWAA2022020960159Angle · corrodedIN THE G4 GALLEY; THE LOWER ATTACH ANGLE IN COMPARTMENT 4B-09 HAS EVIDENCE OF CORROSION. ; / [01] REMOVED AND REPLACED LOWER ATTACH ANGLE IN GALLEY COMPACTMENT G4B-09 PER CMM 25-31-68.; [02] REMOVED AND REPLACED LOWER ATTACH ANGLE IN GALLEY COMPARTMENT G4B-09 SDR SWAA2022020960161Angle · corrodedIN THE G4 GALLEY; THE LOWER ATTACH ANGLE IN COMPARTMENT 4B-01 HAS EVIDENCE OF CORROSION. ; / [01] REMOVED AND REPLACED LOWER ATTACH ANGLE FROM GALLEY COMPARTMENT G4B-01 PER CMM 25-31-68.; [02] REMOVED AND REPLACED LOWER ATTACH ANGLE IN GALLEY COMPARTMENT G4B-0SDR SWAA2021111142276Battery Pack · inoperativeOVERWING EMERGENCY LIGHT WOULD NOT OPERATE ; / [01] R&R EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06SDR SWAA2021111141318Lens · missingDUE TO CDL APPLIED MEL 33-14-01 SP1 ; DUE TO CDL APPLIED FOR MISSING EXTERIOR EMERGENCY LIGHT LENS MEL 33-14-01 ALSO APPLIED SP1 / [01] R&R L/H EXIT OVERWING LENS IAW AMM 33-51-04.SDR SWAA2021111141317Lens · missingEMERGENCY EXIT LIGHT COVER MISSING CAPTAIN OVERWING (LH) / [01] INSTALLED NEW LENS LANYARD PER SRM 51-40-02; [02] R&R L/H EXIT OVERWING LENS IAW AMM 33-51-04.
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