N8308K
Service difficulty reports · 180
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 = 'N8308K' 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 = 'N8308K' 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 SWAA2023102501891Sidewall Support · corrodedAFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 727I+5; LBL 22; WL 162<[01] STEP 1;[02] WORK WILL BE ACCOMPLISH ON CUSTOMER CARD NBR: TTG8QOONH4KV;[03] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLESDR SWAA2023102501892Sidewall Support · corrodedAFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 727I+4 - 747+19; RBL 22; WL 162<[01] STEP 1;[02] REMOVED AND EVALUATED CORROSION AT AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 727I+4 - 747+19; RBL 22; WL 162 FOUND TO BE OUT OF LIMITS IAW SRM SRM SDR SWAA2023102501900Shield · corrodedAFT CARGO FWD SHIELD HAS CORROSION AT BS 767+3 - 787; RBL 22; WL 163<[01] UPDATED STEP 1 AND 2;[02] UPDATED STEP 3 AND 4;[03] UPDATED STEP 3;[04] UPDATED MEASUREMENTS TABLE;[05] UPDATED STEP 5;[06] REMOVED ACB FWD SHIELD IAW SRM 51-40-02-0G-0<BR><BR>RECEIVED NSDR SWAA2023102501901Sidewall Support · corrodedAFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 747+4; LBL 22; WL 162<[01] STEP 1;[02] PART WILL BE REPLACED AT CUSTOMER CARD# TTG8Q00NH4KV DUE TO COMMON AREAS OUT OF LIMITS.;[03] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLESDR SWAA2023102501902Sidewall Support · corrodedAFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 747+11 - 767+15; LBL 22; WL 163<[01] STEP 1;[02] WORK WILL BE ACCOMPLISH ON CUSTOMER CARD NBR: TTG8QOONH4KV;[03] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLESDR SWAA2023102501904Sidewall Support · corrodedAFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CORROSION AT BS 787+7; LBL 22; WL 164<[01] STEP 1;[02] WORK WILL BE ACCOMPLISH ON CUSTOMER CARD NBR: TTG8QOONH4KV;[03] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLESDR SWAA2023102601355Bracket · crackedLEFT WING-TO-BODY FAIRING - CRACKED BRACKET ASSY-DUCT SUPPORT; L/H PACK BAY (MARKED)<[01] LH PACK BAY SUPPORT BRACKET CRACKED NO ALLOWABLE DAMAGE NOTED ON SRM. PART TO BE REPAIR BY REPLACEMENT. PN 212A1116-1. IAW SRM 51-10-02-0G-0 PARA 9.;[02] REMOVED AND REPLSDR SWAA2023102601341Rib · crackedLH HORIZONTAL STAB REMOVABLE L/E 331B INNER RIB #9 IS CRACKED<[01] UPDATED MEASURMENT TABLE;[02] REMOVED AND REPLACED L/H HORIZONTAL STAB REMOVABLE L/E 331B INNER RIB # 9; LE STA 151.75.;[03] ADDED REFERENCE FOR CORRECTIVE ACTION. 2. : REMOVED AND REPLACED L/HSDR SWAA2023102601326Gusset · crackedFWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500I S-19R WL193. MARKED<[01] UPDATED STEP 1;[02] UPDATED STEP 2;[03] UPDATED MEASUREMENT TABLE.;[04] UPDATED STEPS 4-5.;[05] UPDATED STEP 2.;[06] UPDATED STEP 3.;[07] UPDATED STEP 6;[08] EDITED MEASUREMENSDR SWAA2023102601321Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500G AFT SIDE RBL25 WL155.<[01] UPDATED STEP#1;2;3;[02] UPON FURTHER INVESTIGATION CRACKED INTERCOSTAL ATTACH ANGLE IS LOCATED AT FCB BS500G FWD SIDE RBL25 WL155;[03] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FCSDR SWAA2023102601328Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500I FWD SIDE RBL25 WL155. CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500H FWD SIDE RBL25 WL155<[01] UPDATE STEP #1;2;3;[02] UPON FURTHER INVESTIGATION CRACKED INTERCOSTAL ATTACH ANGLE IS LOCATED AT FCB BS500H FWD SIDE SDR SWAA2023102601329Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500I AFT SIDE RBL25 WL155.<[01] UPON FURTHER INVESTIGATION CRACKED INTERCOSTAL ATTACH ANGLE WAS FOUND TO BE AT BS 500H AFT SIDE RBL 25 WL 155.;[02] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FCB BS500H AFT SIDE RSDR SWAA2023102601322Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500I FWD SIDE LBL25 WL155.<[01] RECEIVED NEW ATTACH ANGLE<BR>ITEM# : 143A7502U159<BR>PO# : 938941/1<BR><BR>REMOVED AND REPLACED NEW ATTACH ANGEL IAW SRM 51-40-02-0G-0 AND DWG 143A7505 ID:0109 REV:-;[02] VERIFIED STEPS SDR SWAA2023102601323Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500I AFT SIDE LBL25 WL155.<[01] REMOVED AND REPLACED NEW ATTACH ANGEL IAW SRM 51-40-02-0G-0 AND DWG 143A7505 ID:0109 REV:-;[02] VERIFIED STEPS 1;2;3; COMPLETE AND MEASUREMENT TABLE; CARD COMPLETE.SDR SWAA2023102601330Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500F FWD SIDE RBL25 WL155.<[01] UPON FURTHER INVESTIGATION INTERCOSTAL ATTACH ANGLE AT FCB BS500E FWD SIDE RBL25 WL155 FOUND NOT TO BE CRACKED. CLEANED AREA IAW SOPM 20-30-03;[02] VERIFIED MEASUREMENT TABLE<BR><BR>VERISDR SWAA2023102601324Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500E FWD SIDE RBL25 WL155.<[01] UPON FURTHER INVESTIGATION INTERCOSTAL ATTACH ANGLE AT FCB BS500E FWD SIDE RBL25 WL155 FOUND NOT TO BE CRACKED. CLEANED AREA IAW SOPM 20-30-03;[02] VERIFIED JOB COMPLETE;[03] RII STEP ENSDR SWAA2023102601325Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500G FWD SIDE LBL25 WL155.<[01] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FCB BS500G FWD SIDE LBL25 WL155 IAW BOEING DWG 143A7505 AND SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTION 1.;[03] TASK COMPLETESDR SWAA2023102601327Support Angle · corrodedCORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FCB BS500I LBL23 TO RBL23 WL156.<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF FCB ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE 500I LBL 23 RBL 23 WL 156 IAW SRM 53-30-08-1A-1;[02] SRM 53-30-08-1A-1 ISSDR SWAA2023102601317Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT BS500B+11 - BS500E; BS500G - BS500H RBL23 WL156.<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF FCB FLOOR TO SIDEWALL SUPPORT BS 500B+11-BS 500E;BS 500G-500H RBL 23 WL 156 IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGSDR SWAA2023102601332Strap · corrodedCORROSION ON TENSION STRAP AT AFT WET AREA BS1016+12 LBL17 WL208.<[01] EDITED STATUS FROM PENDING TO PARTIAL;;[02] UPDATED MEASUREMENT TABLE;[03] REMOVED CORROSION FROM AFT WET AREA ON TENSION STRAP BS1016+12; LBL17; WL208; THE FINAL REPAIR PROCESS WILL BE ACCSDR SWAA2023102601333Intercostal · corrodedCORROSION AROUND FASTENERS ON FLOOR SUPPORT AT AFT WET AREA BS947+4 LBL24 WL208.<[01] UPDATED STEP 1;[02] REMOVED AND REPLACED INTERCOSTAL AT BS 947.5 TO 967; LBL 24; WL 208 PER SRM 51-40-02-0G-0 AND BOEING DWG 147A5650.;[03] VERIFIED CORRECTIVE ACTION 2.<BR>VSDR SWAA2023102601334Channel · corrodedCORROSION ON AED MOP SILL BS947+4 LBL54 WL208.<[01] UPDATED STEP 1;[02] UPDATED STEP 2. ADDED ORIGINAL MATERIAL THICKNESS.;[03] REMOVED CORROSION FROM AED MOP SILL BS947+4 LBL54 WL208 FOUND TO BE WITHIN LIMITS PER RM 53-70-15-1A-1; PAR. 4.D.(2). (A). FIG. 103;SDR SWAA2023102601335Channel · corrodedCORROSION ON ASD MOP SILL BS947 - BS991 RBL54 WL208.<[01] UPDATED STEP 1;[02] UPDATED STEP 2. ADDED ORIGINAL MATERIAL THICKNESS.;[03] REMOVED CORROSION FROM ASD MOP SILL BS947 - BS991 RBL54 WL208; FOUND TO BE WITHIN LIMITS PER SRM 53-70-15-1A-1; PAR. 4.D.(2). SDR SWAA2023102510436Flap · delaminatedR/H OUTBOARD AFT FLAP LOWER SKIN IS DELAMINATED AT THE I/B EDGE. (MARKED)<[01] VERIFIED STEP 2 IN PARTIAL.;[02] REMOVED AND REINSTALLED R/H O/B AFT FLAP IAW AMM27-51-22-400-801.;[03] REMOVED AND REPLACED R/W O/B AFT FLAP IAW AMM 27-51-22;[04] COMPLETED MEASURESDR SWAA2023102501320Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500G FWD SIDE RBL25 WL155.<[01] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FCB BS500G FWD SIDE RBL25 WL155 IAW BOEING DWG143A7505 AND SRM 51-40-02;[02] WORK WAS ACCOMPLISHED ON CUSTOMER CARD #TTG8Q00NFNQX;[03] VESDR SWAA2023102501331Gusset · crackedFWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500I S-21L WL177. MARKED<[01] UPDATED STEPS 1-2.;[02] UPDATED MEASUREMENT TABLE.;[03] UPDATED STEP 3.;[04] UPDATED STEP 4.;[05] UPDATED STEP 3.;[06] UPDATED STEP 3;[07] UPDATED STEP 2.;[08] UPDATED STEP 5.SDR SWAA2023102500693Holder · brokenPANEL 843CZ AFT RH EMERGENCY ESCAPE HATCH ASSIST STRAP HOLDER IS BROKEN<[01] REMOVED AND REPLACED AFT RH EMERGENCY ESCAPE HATCH ASSIST STRAP HOLDER IAW SOPM 20-50-01;[02] VERIFIED;[03] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLESDR SWAA2023102500253Panel · corrodedFORWARD CARGO DOOR PANEL 821BR HAS CORROSION ON EXTERIOR SURFACE.<[01] REMOVED CORROSION DAMAGE IN A 3.9L X 3.2W AREA; AND 9 DAMAGE FASTENERS; EVALUATED BLEND AREA AND FOUND THE BLEND 0.024 OF 0.040 TO BE (OUT OF LIMITS). REPAIR BY REPLACEMENT. RECEIVED NEW PASDR SWAA2023102600237Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] UPDATED STEP 10;[02] SCUFF PLATE WAS FOUND CRACKED UPON REMOVAL. IT WAS SENT OUT FOR REPAIR. RECEIVED REPAIRED PART AND REINSTALLED IAW AMM 53-11-02; SOPM 20-50-19; SRM 53-30-15-2R-1; SRM 51-20-01; SOPM 20-2SDR SWAA2023102600244Attach Angle · crackedRH WING; O/B UPPER FIXED TRAILING EDGE PANEL; O/B ATTACH ANGLE IS CRACKED O/B TRANSVERSE WEB ATTACH ANGLE CRACKED<[01] REMOVED AND REPLACED RH WING O/B UPPER FIXED T/E PANEL O/B ATTACH ANGLE IAW SRM 51-40-02-0G-0 PARA. 4.;[02] VERIFIED CORRECTIVE ACTION STEP 1SDR SWAA2023102699717Fitting · crackedPANEL 621GB O/B CTR LATCH FITTING IS BROKEN<[01] REMOVED AND REPLACED PANEL 621GB O/B CTR LATCH FITTING PER AMM 20-50-11910-801 <BR>CAL TOOL: ATS1731 DUE: 07/2024;[02] UPDATED PARTS;[03] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.SDR SWAA2023102699558Slat · debonded#1 SLAT LOWER O/B SURFACE IS DISBONDED; (MARKED)<[01] REPAIRED AND REINSTALLED SLAT IAW AMM 27-81-21-400-801 AND CSD WORK ORDER #563768;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE.SDR SWAA2023102699096Panel · delaminatedLEFT WING L/E PANEL 521KB DELAMINATED AT CUTOUT CORNERS<[01] LEFT WING L/E PANEL 521KB WAS DELAMINATED AT CUTOUT CORNERS AND REPAIRED IAW SRM 51-70-05-2R-6. FINAL FINSIH WILL BE ACCOMPLISHED ON FAULT: TTG8Q00NQTZ;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2023032018041Flashlight · failedCREW REPORTS: LED NOT FLASHING ON FLASHLIGHT IN AFT GALLEY<[01] REPLACED BATTERY. ALL GOOD. REF AMM 25-64-00SDR SWAA2023012493993Light · out of adjustEMERGENCY PATH AISLE LIGHTING STRIP(AIRCRAFT RIGHT) LOOSE AT ROW 12<[01] INSTALLED NEW CARPET. TAPE AS REQUIRED PER S.I.PSDR SWAA2022100555825None · looseROW 11DEF FLOOR EGRESS LIGHT STRIP LOOSE / [01] SECURED FLOOR EGRESS LIGHTS IAW AMM 33-51-15SDR SWAA2022080237081Lens · looseMID CABIN OVERHEAD EMERGENCY EXIT SIGN BASE COVER FELL OFF EXIT SIGN LENS AND FU MID CABIN OVERHEAD EMERGENCY EXIT SIGN BASE COVER FELL OFF EXIT SIGN LENS AND FUNCTION NORMAL.MX... IF UNABLE TO FIX PLEASE GET PN SO WE CAN ORDER WHAT IS REQUIRED TO FIX THIS... SDR SWAA2022061418248Seal · crackedLH HORIZONTAL STABILIZER UPPER SLIDING SEAL IS CRACKED / [01] R&R LH HORIZONTAL STABILIZER UPPER SLIDING SEAL PER MM REF 53-31-31SDR SWAA2022061418249Seal · crackedRH HORIZONTAL STABILIZER UPPER SLIDING SEAL IS CRACKED / [01] R&R RH HORIZONTAL STABILIZER UPPER SLIDING SEAL PER AMM 53-31-31.SDR SWAA2022041192287Light · inoperativeR/H AFT OVER WING EMERGENCY LIGHT INOP. / [01] RELAMPED R/H AFT OVER WING EMERGENCY EXIT LIGHT & OPS CHECK GOOD REF AMM 33-51-04SDR SWAA2022011059272Light · looseEMERGENCY LIGHTING STRIP ON FLOOR-ROW 11 CAPTAIN\LEFT SIDE IS LOOSE ; / [01] RESECURED PER SIPSDR SWAA2021120148299Battery · poppedON PREFLIGHT CIRCUIT BREAKER P18-3 A-10 POPPED.(LIGHTING EMER CHGR L-AFT) ; / [01] REPLACED BATTERY PACK AND CHARGER ASSY PER AMM 33-51-06.SDR SWAA2021120149191Charger · poppedON PREFLIGHT CIRCUIT BREAKER P18-3 A-10 POPPED.(LIGHTING EMER CHGR L-AFT) ; / [01] REPLACED BATTERY PACK AND CHARGER ASSY PER AMM 33-51-06.SDR SWAA2021112446511Battery Pack · inoperativeRT SIDE EMERGENCY EXIT ROW SIGNS INOP ; / [01] R&R EMERGENCY LIGHT BATTERY PACK AT STATION 565RT. OPS CK GOOD. PER AMM 33-51-06SDR SWAA2021101126568Rib · crackedWEB I/B OF L/H WING DEFLECTION CONTROL RIB IS CRACKED. / REMOVED AND REPLACED WEB PER SRM 51-40-02SA-M 326 A1362027INSP D142SDR SWAA2021100826053Battery Pack · inoperativeFWD EMER LIGHTS OFF M 1675 BATTERY PACK INOP / REMOVED & REPLACED EMER EXIT LT BATTERY PACK M 1675 PER AMM 33-51-06. TEST GOOD.SDR SWAA2021101121274Rib · crackedR/H WING T/E DEFLECTION CONTROL RIB I/B SUPPORT ANGLE FOR UPPER SHELF PANEL IS CRACKED ; MRKD / REMOVED AND REPLACED ANGLE PER SRM 51-40-02.SDR SWAA2021101121275None · crackedR/H WING T/E WAFFLE PLATE CRACKED AT RIVET HOLE APPROX. IRSS 220. MRKD / REMOVED AND REPLACED WAFFLE PLATE PER SRM 51-10-02; INSTALLED FASTENERS PER SRM 51-40-02SDR SWAA2021070288383Structure · crackedEXTERNAL POWER DOOR LOWER CORNER CRACKED / C/W NDT OF CUTOUT AREA IAW 737 NDT PART 6; 51-00-00 PROD 23 NO DEFECT NOTED E75437 REPAIRED PER SRM 53-10-15-2E-4 REPAIR 4 ALTERNATIVE 2SDR SWAA2021062887214Megaphone · weakMEGA PHONE VOLUME WEAK / REPLACED FWD MEGAPHONE. AMM 25-64-00.
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