N8606C
Service difficulty reports · 204
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 = 'N8606C' 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 = 'N8606C' 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 SWAA2026083189225Light · unsecureFLOOR LIGHTING STRIP AT 16D RAISED FROM FLOOR. SECURED FLOOR LIGHTING STRIP WITH DOUBLE SIDED TAPE PER S.I.P AND CONDITION CHK GOODSDR SWAA2026022473519Lens · wrong partAFT LAV EMERGENCY EXIT LIGHT LENS NEEDS TO BE BLANK. REPLACED LENS IAW CMM 25-48-25. NO OPERATIONAL CHECK REQUIRED. REPLACED LENS IAW CMM 25-48-25. NO OPS CHECKED REQUIRED.SDR SWAA2026022472339Girt Bar · unsecureL2 DOOR AFT GIRT BAR FITTING NEEDS SECURED. SECURED L2 DOOR AFT GIRT BAR FITTING IAW AMM 25-66-02-400-801-NG. (SDR SWAA2026022472342Handle · unsecureL1 DOOR ASSIST HANDLE NEEDS TO BE SECURED. SECURED THE DOOR ASSIST HANDLE AMM 25-21-31-420-802.SDR SWAA2026022472341Handle · unsecureL2 DOOR ASSIST HANDLE NEEDS TO BE SECURED. SECURED THE ASSIST HANDLE IAW AMM 25-21-31-420-802.SDR SWAA2026022472340Handle · unsecureR2 DOOR ASSIST HANDLE NEEDS TO BE SECURED. SECURED THE DOOR ASSIST HANDLE IAW AMM 25-21-31-420-802.SDR SWAA2026022472343Handle · unsecureR1 DOOR ASSIST HANDLE NEEDS TO BE SECURED. SECURED THE DOOR ASSIST HANDLE IAW AMM 25-21-31-420-802.SDR SWAA2026011360923Fan Cowl · crackedAN APPROX 7 INCH CRACK FOUND ON THE NR 2 ENGINE COWLING OTBD, AT THE 4 O`CLOCK POSITION. R & R OTBD NR 2 ENG FAN COWL IAW 71-11-02.SDR SWAA2025100621588Sign · unsecureISLE EXIT SIGN WONT STAY UP. R & R CENTER ISLE EXIT SIGN IAW AMM 33-51-02.SDR SWAA2025081400110Skin · delaminatedLEFT TRAILING EDGE OTBD AFT FLAP HAS DELAMINATION AND DAMAGE ON I/B AFT EDGE. THE DELAMINATION AREA OF THE LOWER SKIN IS APPROX. 11.5' BY 14'. INCLUDING 5 FASTENER HOLES COMPLETELY PULLED THROUGH. THE MISSING MATERIAL TO THE LOWER SKIN IS ROUGHLY 5.5' X 2.0'. SDR SWAA2025012887176Light · brokenFOUND ASSY - EXIT EMERGENCY LIGHTS L1208 AND L1189 BROKEN<[01] REMOVED AND REPLACED EXIT EMERGENCY LIGHTS L1208 AND L1189 AND PERFORMED GOOD TEST IAW AMM 33-51-01-960-802.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2025012890460Light · brokenFOUND ASSY - EXIT EMERGENCY LIGHTS L1208 AND L1189 BROKEN<[01] REMOVED AND REPLACED EXIT EMERGENCY LIGHTS L1208 AND L1189 AND PERFORMED GOOD TEST IAW AMM 33-51-01-960-802.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2025012887175Tray · out of adjustSEATS ROW 14 ABC; ROW 14 DEF DON'T HAVE THE PRESENCE OF ONE-WAY TRAY TABLE LATCHES ON THE BACK OF THE EMERGENCY EXIT SEATS. <[01] ALL STEPS COMPLETED REMOVED AND REPLACED SEAT ROW 14 E&F WITH ONE-WAY TRAY TABLE LACHES PAR CMM 25-21-45 REMOVED AND REPLACED SEASDR SWAA2025012886392Battery Pack · inoperativeALL EMERGENCY LIGHT ASSOCIATED WITH BATTERY PACK WITH M1672 STAT 952 WL 291 AND RBL 14 ARE INOP<[01] REMOVED AND REPLACED BATTERY PACK M1672 AND PERFORMED GOOD EMERGENCY LIGHTS TEST IAW AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2025012886393Battery Pack · inoperativeALL EMERGENCY LIGHTS ASSOCIATED WITH M1673 BATTERY PACK AT STA 952 WL 290 LBL 14 ARE INOP<[01] REMOVED AND REPLACED BATTERY PACK M1673 AND PERFORMED GOOD EMERGENCY LIGHTS TEST IAW AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2025012883294Lens · crackedFWD LAV EMERGENCY LIGHT IS DAMAGED<[01] UPON FURTHER INVESTIGATION; FOUND LENS CRACKED ON FWD LAV EMERGENCY LIGHT ASSEMBLY; REMOVED LENS PER AMM 33-51-01-960-802 STEP 3.C.(5).(D) AND INSTALLED SERVICEABLE LENS PER AMM 33-51-01-960-802 STEP 3.C.(10); NO OPERATISDR SWAA2025012882026Skin Panel · delaminatedAREA OF DELAMINATION APPROX. 1.9' X 1.8'ON DORSAL FIN L/H SIDE SKIN 23.9' FROM LOWER EDGE; 37.3' FROM AFT EDGE.<[01] AREA OF DELAMINATION APPROX. 1.9' X 1.8' ON DORSAL FIN AT L/H SIDE SKIN 23.9' FROM LOWER EDGE; 37.3' FROM AFT EDGE WAS REPAIRED IAW SRM 51-70-0SDR SWAA2025012980128Intercostal · crackedCRACKED INTERCOSTAL ANGLE BETWEEN BS 380-400; LBL13; WL208. <[01] ALL STEPS COMPLETED VERIFIED THAT SRM 51-10-02 IS APPLICABLE TO THIS AIRCRAFT. PART FOUND TO BE OUT OF LIMITS DUE TO NO REPAIR REFERENCE PART WILL BE REPLACED. COMPLETED MEASURMENT TABLE. REMOVESDR SWAA2025012879551Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231LF HAS DELAMINATION<[01] REPLACED PASSENGER CABIN FLOOR PANEL 231LF WITH SERVICEABLE PART IAW SRM 51-10-02-0G-0 PARA 9.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2025012879550Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 232HF HAS DELAMINATION<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED PASSENGER CABIN FLOOR PANEL 232HF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-58B ITEM 345.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2025012879155Fairing · delaminated#1 CANOE FAIRING PANEL544BB DELAMINATED AREA ON OUTERM SKIN I/B SIDE 12.5' FROM FWD. END AND 4.4' FROM UPPER END.<[01] RECIEVED NEW FAIRING; INSTALLATION OF FAIRING TO BE ACCOMPLISHED ON FAULT TTG8Q00X5HUNSDR SWAA2025013083096Bracket · deformed#1 ENGINE HAS A DEFORMED AFT FIRE SEAL BRACKET ON THE UNDERSIDE OF THE PYLON (ONE PIECE) <[01]. UPDATED STEP 1 AND 2; [02] UPDATED STEP 1;2 AND 3.; [03] UPDATED STEP 1.; [04] UPDATED STEP 1 AND 3; [05] UPDATED STEP 1 AND 3.; [06] REPLACED AFT FIRE SEAL IAW SRMSDR SWAA2025012978172Floorbeam · corrodedCORROSION ON STA 986 BEAM UPPER SURFACE AT RBL 43; RBL 38; AND LBL 43; WL 208.1<[01] REPAIRED CORROSION ON STA 986 BEAM UPPER SURFACE AT RBL 43; RBL 38; AND LBL 43; WL 208.1 IAW SRM 53-70-51-2R-6 REP. 6. ALT. 3 AND SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1.SDR SWAA2025012878728Intercostal · crackedINTERCOSTAL CRACKED IN PASSENGER CABIN FLOOR STRUCTURE AT BS500I+6 WL208 LBL2.<[01] CARD COMPLETED;[02] REMOVED & REPLACED INTERCOSTAL PASSENGER CABIN FLOOR STRUCTURE AT BS 500I+6' LBL 2 WL 208 AS PER SRM 51-40-02 & DWG 143A5400 REV A.<BR>CARD COMPLETED;[03] VSDR SWAA2025012878732Intercostal · crackedTHERE IS CRACKED INTERCOSTAL IN PASSENGER CABIN FLOOR STRUCTURE AT BS380+10 WL208 LBL53.<[01] PARTIAL STEP 1;[02] REMOVED AND REPLACED INTERCOSTAL AT BS380 TO BS400 WL208 LBL53 PER SRM 51-40-02-0G-0 AND BOEING DWG 143A5400 REV -.;[03] VERIFIED CORRECTIVE ACTIOSDR SWAA2025012878731Intercostal · crackedTHERE IS CRACKED INTERCOSTAL IN PASSENGER CABIN FLOOR STRUCTURE AT BS380+14 WL208 LBL3.<[01] PARTIAL STEP 1;[02] CORRECTED FASTENER HOLE SIZE REFERENCE IN STEP 1;[03] REMOVED AND REPLACED INTERCOSTAL AT BS380 TO BS400 WL208 LBL3 IAW SRM 51-40-02-0G-0 AND BOEINSDR SWAA2025012878730Intercostal · crackedTHERE IS CRACKED INTERCOSTAL IN PASSENGER CABIN FLOOR STRUCTURE AT BS360+4 WL208 LBL19. THERE IS CRACKED INTERCOSTAL IN PASSENGER CABIN FLOOR STRUCTURE AT BS360-6 WL208 LBL11.<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 344 TO BS 360 LBL 11 WL 208 PER SRM 51-4SDR SWAA2025012878535Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231KF HAS DELAMINATION ON UPPER SURFACE (MARKED)<[01] PASSENGER CABIN FLOOR PANEL 231KF WAS REPLACED DUE TO EXCESSIVE UPPER SURFACE DELAMINATION IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND AIPC 53-21-51-58B ITEM #370.;[02] VERIFIED JOB COSDR SWAA2025012878171Strap · corrodedCORROSION ON AFT PAX CABIN FLOOR STRAP AT STA 1016+4; RBL 2; WL 208.2.<[01] ALL STEPS COMPLETED VERIFIED THAT SRM 51-10-02-0G-0 IS APPLICABLE TO THIS AIRCRAFT AND SUPPORT ANGLE IS OUT OF LIMITS DUE TO NO REPAIR REFERENCE TO SUPPORT CORROSION REMOVAL. PART WILLSDR SWAA2025012878169Support Angle · corrodedCORROSION ON GALLEY SUPPORT ANGLE AT STA 986+7; LBL 43 AND LBL 37; WL 208.2.<[01] ALL STEPS COMPLETED VERIFIED THAT SRM 51-10-02-0G-0 IS APPLICABLE TO THIS AIRCRAFT AND SUPPORT ANGLE IS OUT OF LIMITS DUE TO NO REPAIR REFERENCE TO SUPPORT CORROSION REMOVAL. PARSDR SWAA2025012878165Support Angle · corrodedCORROSION ON GALLEY SUPPORT ANGLE UPPER FLANGE AT STA 986+6; LBL 32; WL 208.5.<[01] ALL STEPS COMPLETED VERIFIED THAT SRM 51-10-02-0G-0 IS APPLICABLE TO THIS AIRCRAFT AND SUPPORT ANGLE IS OUT OF LIMITS DUE TO NO REPAIR REFERENCE TO SUPPORT CORROSION REMOVAL. PSDR SWAA2025012778532Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231NF HAS UPPER SURFACE DAMAGE (MARKED)<[01] PASSENGER CABIN FLOOR PANEL 231NF WAS REPLACED DUE TO EXCESSIVE UPPER SURFACE DELAMINATION IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND AIPC 53-21-51-58B ITEM #495.;[02] VERIFIED JOB COMPLETESDR SWAA2025012778530Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231TF HAS UPPER SURFACE DAMAGE (MARKED)<[01] PASSENGER CABIN FLOOR PANEL 231TF WAS REPLACED DUE TO EXCESSIVE UPPER SURFACE DELAMINATION IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND AIPC 53-21-51-58B ITEM #655.;[02] VERIFIED JOB COMPLETESDR SWAA2025012778537Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 232JF HAS UPPER SURFACE DAMAGE (MARKED)<[01] PASSENGER CABIN FLOOR PANEL 232JF WAS REPLACED DUE TO EXCESSIVE UPPER SURFACE DELAMINATION IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND AIPC 53-21-51-58B ITEM #295.;[02] VERIFIED JOB COMPLETESDR SWAA2025011578134Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 222DF HAS UPPER SURFACE DAMAGE (MARKED)<[01] PANEL 222DF WAS REPLACED DUE TO EXTENSIVE UPPER SURFACE DELAMINATION IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND AIPC 53-21-51-22B ITEM 270.;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COSDR SWAA2025012877501Angle · crackedCRACK ON ANGLE LH WING TRAILING EDGE ORSS-281 APROX. MARKED WITH RED TAPE. [01] REMOVED; REPLACED; AND INSTALLED A NEW ANGLE AT LH WING; TRAILING EDGE; ORSS-281 IAW SRM 51-40-02 AND IPC 57-45-51-03.; [02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2025013177369Intercostal · crackedINTERCOSTAL CRACKED IN PAX CABIN FLOOR STRUCTURE AT BS312+6 RBL35 WL208<[01]. REMOVED AND REPLACED INTERCOSTAL BS312-BS328 RBL35 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 REV -; [02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2025013177370Intercostal · crackedINTERCOSTAL CRACKED IN PAX CABIN FLOOR STRUCTURE AT BS277+14 BL0 WL208.<[01] REMOVED; REPLACED; AND INSTALLED A NEW INTERCOSTAL PAX CABIN FLOOR STRUCTURE AT BS277+14; BL0; WL208 IAW SRM 51-40-02; AND BOEING DWG 141A5400.SDR SWAA2025013177494Intercostal · corrodedCORROSION ON CABIN FLOOR STRUCTURE SUPPORT FRAME AT BS328+8 LBL25 WL208.<[01] REMOVED AND REPLACED FLOOR SUPPORT INTERCOSTAL I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A5730 REV:A;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; CARD COMPLETE.SDR SWAA2025012977497Attach Angle · corrodedCORROSION ON FSD CUTOUT SURROUND STRUCTURE MOPSILL FROM BS294.5+8 TO BS328 WL208 RBL60.<[01] EVALUATED DAMAGE ON FSD MOPSILL ATTACH ANGLE BS298-BS331 RBL60 AND FOUND TO BE OUT LIMITS REMOVED; LOCATED; DRILLED; INSTALLED ALL I.A.W SRM 53-10-15-1A-2 ALLOWABLE DASDR SWAA2025012977499Frame · crackedCRACK ON UPPER CHORD FRAME ASSEMBLY ON FED CUTOUT SURROUND AT BS312; BETWEEN S-5L AND S-6L WL283.<[01] ACOMPLISHED REPAIR I.A.W M-22-153-01244 (737-NG - SWA - BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L) RECORD ON CCN TTG8Q00XN7SS;[02SDR SWAA2025020379148Structure · debondedUNBONDED CAP STRIP FWD SIDE LOWER CORNER ON PANEL 844AW ASD DOOR LINER (MARKED)<[01] REMOVED AND REPLACED CAP STRIP ON FWD SIDE LOWER CORNER OF PANEL 844AW ASD DOOR LINER IAW BOEING DWG# 411A2114-41B SHEETS 1 AND 3; DWG# 411A2114 SHEET 20 FRAME 1; AND DWG# 411SDR SWAA2025012977156Baffle · corrodedCORROSION ON BAFFLE BS500C TO BS500D WL156 RBL25<[01] REMOVED AND REPLACED NEW BAFFLE BS500C TO BS500D WL156 RBL25 IAW SRM 51-40-02-0G-0. AND DWG 143A7505 REV:A.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.SDR SWAA2025012977157Baffle · corrodedCORROSION ON BAFFLE CLIPS BS500H AND BS500F FWD SIDE OF FRAME WL156 LBL25<[01] REMOVED BAFFLE CLIPS BS500H AND BS500F FWD SIDE OF FRAME WL156 LBL25 IAW SRM 51-40-02-0G-0 AND LOCATED; DRILLED AND REPLACED NEW BAFFLE CLIPS BS500H AND BS500F FWD SIDE OF FRAME WL1SDR SWAA2025011577161Baffle · corrodedCORROSION FWD CARGO 3EA BAFFLES FROM BS500D TO BS 500H WL156 RBL25<[01] REMOVED AND REPLACED FWD CARGO 3EA BAFFLES FROM BS500D TO BS 500H WL156 RBL25 IAW SRM 51-40-02-0G-0 AND DWG 143A7505 REV:A.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.SDR SWAA2025011577160Baffle · corrodedCORROSION FWD CARGO BAY 2EA BAFFLE CLIPS BS500G AND BS500H FWD SIDE OF FRAME WL156 RBL25<[01] REMOVED AND REPLACED FWD CARGO BAY 2EA BAFFLE CLIPS BS500G AND BS500H FWD SIDE OF FRAME WL156 RBL25 IAW SRM 51-40-02-0G-0 AND DWG 143A7505 REV: B.;[02] VERIFIED CORRESDR SWAA2025011577162Baffle · corrodedCORROSION FWD CARGO BAY ON BAFFLE CLIP BS500H AFT SIDE OF FRAME WL156 RBL25<[01] REMOVED AND REPLACED FWD CARGO BAY ON BAFFLE CLIP BS500H AFT SIDE OF FRAME WL156 RBL25 IAW SRM 51-40-02-0G-0 AND DWG 143A7505 REV:-.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD CSDR SWAA2025012976316Threshold · crackedAFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED<[01]. REPAIRED AFT CARGO BAY AFT CORNER THRESHOLD PER SRM 5360-15-2R-1; [02] VERIFIED.SDR SWAA2025012976577Web · corrodedCORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS794 TO BS847 RBL 26 WL156<[01]. REMOVED DAMAGED AFT CARGO BAY SUB THRESHOLD WEB IAW SRM 51-40-02-0G-0 AND LOCATED; DRILLED; INSTALLED NEW AFT CARGO BAY SUB THRESHOLD WEB BS794 TOSDR SWAA2025011576580Support Plate · corrodedCORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] CORROSION ON AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE; FOUND TO BE OUT OF LIMITS. REMOVED; REPLACED AND INSTALLED NE
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