N207WN
Service difficulty reports · 380
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 = 'N207WN' 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 = 'N207WN' 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 SWAA2022111561836Floor Panel · delaminatedFLOOR PANEL 232DF HAS THREE SPOTS OF DELAMINATION (STA 430) / [01] MEASUREMENTS;[02] REPAIRED TOP SURFACE DAMAGE AS MARKED ON MAIN CABIN FLOOR PANEL 232DF AS PER B737 SRM 53-00-50-2R-1; MATERIALS USED PO#1778544 AND PO#1690463;[03] PERFORMED TAP TEST ON REPAIRSDR SWAA2022111561866Floor Panel · damagedCABIN FLOOR PANEL 242DF;FIBER GLASS IS PEELING (STA 680). / [01] MEASUREMENTS;[02] REPAIRED TOP SURFACE DAMAGE AS MARKED ON MAIN CABIN FLOOR PANEL 242DF AS PER B737 SRM 53-00-50-2R-1; MATERIALS USED PO#1778544 AND PO#1690463;[03] PERFORMED TAP TEST ON REPAIREDSDR SWAA2022111561869Floor Panel · damagedCABIN FLOOR PANEL 241AF;FIBER GLASS IS PELLING. / [01] MEASUREMENTS;[02] REPAIRED TOP SURFACE DAMAGE AS MARKED WITH A PERMANENT REPAIR ON MAIN CABIN FLOOR PANEL 241AF AS PER B737 SRM 53-00-50-2R-1; MATERIALS USED PO#1778544 AND PO#1690463;[03] PERFORMED TAP TESDR SWAA2022111561256Door Sill · crackedFWD CABIN L/H WET AREA L-1 DOOR LOWER SILL INNER CHORD HAS 3' CRACK @ STA 303.9 MKD DOT / [01] CRACK CONFIRMED IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK LENGTH : 2.25'<BR>[NORTEC 600 ; B/C 172389 ; CALIB.DUE- 3/23];[02] STARTED REMOVING FWD CABIN L/H WET ASDR SWAA2022111561257Floor Panel · damagedMAIN CABIN AFT WET AREA FLOOR PANEL #242UF TOP SKIN FIBERGLASS PEELING OFF SEVERAL AREAS / [01] FABRICATED MAIN CABIN AFT WET AREA FLOOR PANEL #242UF BY OUTSIDE VENDOR WITH R.O #1792601 REF.DRAWING #147A5810. AND AMM 53-21-00-400-801. PANEL ASSY WILL BE INSTALSDR SWAA2022111561262Floor Panel · damagedMAIN CABIN AFT WET AREA FLOOR PANEL #241ABF TOP SKIN FIBERGLASS PEELING OFF SEVERAL AREAS / [01] FABRICATED MAIN CABIN AFT WET AREA FLOOR PANEL #241ABF BY OUTSIDE VENDOR WITH R.O #1792603 REF.DRAWING #147A5810. AND AMM 53-21-00-400-801. PANEL ASSY WILL BE INSTSDR SWAA2022111660707Fitting · corrodedCORROSION AT L-1 DOOR LOWER SILL FWD SLIDE LATCH FITTING FASTENER HOLES. REMOVED CORROSION AT FWD SLIDE LATCH (GIRT BAR SUPPORT) AT L1 DOOR LOWER SILL AREA SRM 51-40-01-0G-0. AFTER REMOVED CORROSION ON MAIN CABIN FWD GIRT BAR SUPPORT FOUN OUT LIMITS IAW SRMSDR SWAA2022111660708Door Sill · corrodedL-1 DOOR. CUTOUT LOWER SILL INNER CHORD FROM BS 312 TO 344 CORRODED. L1 DOOR LOWER SILL INNER CHORD WAS REPLACED ON FAULT TTG8Q00FJNG5.SDR SWAA2022111660709Door Sill · corrodedCORROSION @ R-1 DOOR LOWER SILL INNER CHORD FROM STA 294.5 TO STA 328 MKD DOT / [01] REMOVED CORROSION AT R1 DOOR LOWER SILL INNER CHORD;STA 294.5 TO STA 328.PER B 737-700 SRM 51-10-02-0G-0.;[02] VERIFIED STEP #1;[03] PERFORMED UT THICKNESS ON REWORKED AREA ASSDR SWAA2022111660909Door Sill · corrodedCORROSION ON R2 DOOR SILL, BS 947.5-992.8. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW NDT PART 4 51-00-00, PROC 3. EVALUATED REWORKED AREA AND FOUND OUT OF LIMITS IAW SRM 53-70-15-1A-1. REMOVED THE DOOR SISDR SWAA2022111660900Door Sill · corrodedCORROSION ON LT SIDE WALL BS 344-360. L1 DOOR LOWER SILL WAS REPLACED ON TTG8Q00FJNG5.SDR SWAA2022111660915Web · corrodedCORROSION AFT CABIN WET AREA FLOOR SUPPORT WEB FROM BL-0 TO LBL17 STA 1016. EVALUATED CORRODED AREA, FOUND EXFOLIATING CORROSION OUT OF LIMITS IAW SRM 51-10-02-0G-0. REMOVED DAMAGE WEB IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED THE NEW WEB IAW SRM 51-40-05-0SDR SWAA2022111660916Strap · corrodedCORROSION AT AFT CABIN WET AREA GALLEY FLOOR WEB STRAP LBL 3, BS 1016. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW NDT P4 51-00-00, PROC 3. EVALUATED REWORKED AREA AND FOUND OUT OF LIMITS IAW 53-70-51-1A-1. RSDR SWAA2022111660918Floorbeam · corrodedCORROSION AT AFT CABIN WET AREA FLOORBEAM UPPER TEE BS 986.5, RBL 45. REMOVED CORROSION IAW SRM 51-10-02-0G-0. FABRICATED A NEW TEE IAW SRM 53-70-51-2R-4, AND EA 1-753-30838. INSTALLED REPAIR PARTS, TEE, SPLICES, & INTERCOSTAL IAW SRM 53-70-51-2R-4, AND ESDR SWAA2022111560901Floor Support · crackedFWD CABIN WET AREA FLOOR SUPPORT INTERCOAL UPPER CAP CRACKED @ RBL 10 BETWEEN STA 380 AND 400 MKD DOT / [01] REMOVED INTERCOSTAL FLOOR SUPPORT AT FWD CABIN BET. STA 380 TO STA 400;BL-0.PER B 737-700 SRM 51-40-02;[02] LOCARED AND DRILL NEW INTERCOASTAL AT STA 3SDR SWAA2022111560902Floor Support · crackedFWD CABIN WET AREA FLOOR SUPPORT INTERCOAL UPPER CAP CRACKED @ BL-0 BETWEEN STA 380 AND 400 MKD DOT / [01] REMOVED INTERCOASTAL FLOOR SUPPORT AT FWD CABIN WET AREA BET. STA 380 TO STA 400;BL-0.PER B 737-700 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILL NEW INTERCOSDR SWAA2022111560903Floor Support · crackedFWD CABIN WET AREA FLOOR SUPPORT INTERCOAL UPPER CAP CRACKED @ LBL 13 BETWEEN STA 380 AND 400 MKD DOT / [01] REMOVED FLOOR SUPPORT INTERCOSTAL AT FWD WET AREA;LBL 13' BETWEEN STA 380 TO STA 400;PER B 737-700 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILL NEW INTERCSDR SWAA2022111560914Floorbeam · corrodedCORROSION. @ FASTENER HOLE FLOOR BEAM STA 986.5 RBL-5 MKD DOT / [01] REMOVED CORROSION AT FASTENER HOLE FLOOR BEAM STA 986.5 RBL-5 AS PER REFERENCE B737-700 SRM 51-10-02-0G-0;[02] VERIFIED STEP 1.;[03] PERFORMED UT THICKNESS INSP. ON REWORKED AREA @ FASTENER HSDR SWAA2022111560917Floorbeam · corrodedCORROSION. AFT CABIN WET AREA FLOOR BEAM UPPER CAP STA 986.5 LBL 45 MKD DOT / [01] REMOVED CORROSION AT AFT CABIN WET AREA FLOOR BEAM UPPER CAP STA 986.5; LBL 45 AS PER REF SRM 51-10-02-0G-0;[02] VERIFIED STEP 1.;[03] PERFORMED UT THICKNESS INSP. ON REWORKED ASDR SWAA2022111660587Support Bracket · crackedLOWER FUS. CENTER WING L/H A/C BAY FWD INB CROSSOVER AIR DUCT SUPPORT BRACKET CRACKED. REMOVED & REPLACED AIR DUCT SUPPORT BRACKET IAW SRM 51-40-02-0G-0.SDR SWAA2022111560583Floor Support · crackedFWD CABIN WET AREA FLOOR STRUCTURE INTERCOSTAL CRACKED AT UPPER CAP BETWEEN STA 277 AND STA 294.5 BL-0 MKD DOT / [01] REMOVED INTERCOASTAL AT FWD WET AREA ;STA 277 TO STA 294.5;BL-0;PER B 737-700 SRM 51-40-01-0G-0.;[02] LOCATED AND DRILL INTERCOSTAL AT FWD WETSDR SWAA2022111560582Door Sill · crackedFWD CABIN FUSELAGE INTERNAL FRAME CUTOUT FLANGE CRACKED ABOVE L-1 DOOR CUTOUT UPPER SILL @ STA 312 MKD DOT / [01] ACCOMPLISHED REPAIR PER EA 22-153-01244 TTG8Q00FQNL3.;[02] VERIFIED STEP 1.;[03] C/WSDR SWAA2022111659748Bear Strap · cracked0.300' CRACK EXTENDING FWD OF FASTENER ON R1 BEAR STRAP INTERIOR SIDE . REMOVED RAIN GUTTERS (2EA) FROM REPAIR AREA IAW SRM 51-40-02-0G-0. FABRICATED TAPERED SHIM IAW EA 21-153-03542 STEP 10 FIG.1. COMPLETED FABRICATION OF REPAIR IAW EA 21-153-03542 STEPSDR SWAA2022111660018Rib · crackedLT HORIZONTAL STABILIZER NR 5 RIB CRACKED AT STIFFENER 3. TRIM OUT DAMAGE AREA IAW SRM 55-10-09-2R-4. PERFORMED HFEC AT CUT OUT IAW NDTM PART 6, 51-00-00, PROCEDURE 23, NO CRACKS NOTED. PERFORMED HFEC HOLE PROBE INSPECTION ON ALL REMOVED FASTENER LOCATISDR SWAA2022111660023Rib · crackedRT HORIZONTAL STABILIZER RIB 5 CRACKED AT STIFFENER 2. REMOVED DAMAGE FROM RIB IAW SRM 55-10-09-2R-4. PERFORMED HFEC INSP ON REWORKED AREA IAW NDT P6 51-00-00 PROC.23, CRACK CONFIRMED. PERFORMED ROTO INSP ON ALL EXISTING HOLES IAW NDT P6 51-00-00, PROCSDR SWAA2022111660024Rib · crackedRT HORIZONTAL STABILIZER RIB 5 CRACKED AT STIFFENER 3. REMOVED DAMAGE FROM RIB IAW SRM 55-10-09-2R-4. PERFORMED HFEC INSP ON REWORKED AREA IAW NDT P6 51-00-00, PROC.23. CRACK CONFIRMED. PERFORMED ROTO INSP ON ALL EXISTING HOLES IAW NDT P6 51-00-00, PROCSDR SWAA2022111659949Panel · elongatedRIGHT WING LOWER INBOARD FIXED T/E ACCESS PANEL #651GB INNER CENTER FITTING WITH ELONGATED HOLES / [01] REMOVED AND REPLACED FITTING AT RT WING LOWER I/B FIXED T/E ACCESS PANEL #651GB PER B737-700 SRM 51-40-02-0G-0. (PERFORMED BY KV 34707);[02] VERIFIED STEP 1SDR SWAA2022111660021Bracket · crackedLEFT WING UPPER SEAL SUPPORT OF DEFLECTOR PANEL IS CRACKED / [01] BRACKET WIL BE REPLACED IN THE ITEM TTG8Q00FFE2B;[02] VERIFIED STEP 1.SDR SWAA2022111659744Bracket · crackedLT WING T/E; DEFLECTION CONTROL RIB UPPER PANEL CENTER AFT SEAL BRACKET CRACKED. REMOVED BRACKET IAW SRM 51-40-02-0G-0. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G-0.SDR SWAA2022111659727Bracket · crackedLEFT WING LOWER INBOARD T/E ACCESS PANEL #551FB INNER FWD CENTER BRACKET CRACKED. AFTER REMOVED SEAL TO REPLACE BRACKET FOUND SEAL WORN OUT. REMOVED SEAL FOUND ON STEP 1 IAW SOPM 20-50-02. REMOVED AND REPLACED THE BRACKET IAW SRM-51-40-02-0G-0.SDR SWAA2022111659284Panel · damagedRT WING;LOWER MID TRAILING EDGE PANEL #661AB WITH ELONGATED HOLE AT O/B AREA / [01] PREPARED AREA FOR REPAIR FASTENER HOLE AT R/T WINGLOWER MID TRAILING EDGE PANEL#661AB PER B737 SRM 51-70-04-2R-9;[02] OK TO ACCOMPLISH REPAIR.;[03] REPAIRED PANEL AT ELONGATED SDR SWAA2022060613417Light · missingRIGHT HAND EMERGENCY EXIT WINDOW LOWER EXIT SIGN MISSING DIRECTIONAL ARROW. / [01] REMOVED AND REPLACED EXIT SIGN COVER REF AMM 33-51-01;[02] C/WSDR SWAA2022060613416Light · missingR1 DOOR LOWER EMERGENCY SIGN MISSING DIRECTIONAL ARROW / [01] REMOVED AND REPLACED EXIT SIGN COVER REF AMM 33-51-01;[02] C/WSDR SWAA2022051205633Bracket · looseFWD ENTRY DOOR STOWAGE BRACKET FOR GIRT BAR LOOSE. / [01] ADJUSTED FWD DOOR GIRT BAR BRACKET PER AMM 25-66-01SDR SWAA2022031783154Flashlight · inoperativeFWD GALLEY LOWER EMER FLASHLIGHT INOP / [01] R&R FWD GALLEY LOWER FLASHLIGHT REF CMM 25-60-02SDR SWAA2022013164122Light · inoperativeLH OVERWING EXIT SIDEWALL LIGHT INOP / [01] RELAMPED AND REMOVED & REPLACED FUSE IAW AMM 33-21-00. OPS CHECK GOOD. THIS CLEARS MEL.SDR SWAA2021101127215Panel · elongatedCENTER WHEEL WELL PANEL 193D HAS MULTIPLE WORN AND/OR ELONGATED HOLES. ; / [01] TSR 2021006242 SUBMITTED WITH PICS.; [02] EA 21-153-02953 ADDED TO FAULT.; [03] C/W EA 21-153-02953SDR SWAA2021062886370Lamp · burned outOVERWING EMERGENCY EXIT SIGNS HAVE BURNT OUT BULBS ; / [01] RELAMPED OVERWING EMERGENCY EXIT SIGNS AND PERFORMED A GOOD OPS TEST PER AMM 33-51-01-960-801; [02] VERIFIED RELAMPED OVERWING EMERGENCY EXIT SIGNS AND PERFORMED A GOOD OPS TEST PER AMM 33-51-01-960-8SDR SWAA2021062882160Floor Panel · corrodedCORROSION ON AFT CARGO BAY FLOOR PANEL SPLICE BS 887; RBL 20-LBL 8; WL 154 ; / [01] NO ALLOWABLE DAMAGE FOUND ON SRM FOR THIS PART... PART REQUIRED TO BE REMOVE AND REPLACE IAW SRM 51-10-02-OG-0 STEP 9.; [02] CONFIRMED; OK TO PROCEED; [03] RECEIVED AND REPLACESDR SWAA2021062882159Floor Panel · corrodedCORROSION ON AFT CARGO BAY FLOOR PANEL SPLICE BS 767; RBL 20-LBL 20; WL 154 ; / [01] UPON INVESTIGATION; NO ALLOWABLE DAMAGE LIMITS IN SRM FOR THIS PART. WILL BE REMOTED AN REPLACED; [02] CONFIRMED; OK TO PROCEED; [03] RECEIVED AND REPLACED NEW AFT CARGO BAY FSDR SWAA2021062882158Floor Panel · corrodedCORROSION ON AFT CARGO BAY FLOOR PANEL SPLICE BS 727D; RBL 20-LBL 20; WL 154 ; / [01] UPON INVESTIGATION; NO ALLOWABLE DAMAGE LIMITS IN SRM FOR THIS PART. WILL BE REMOVED AND REPLACED; [02] CONFIRMED; OK TO PROCEED; [03] CONFIRMED; OK TO PROCEED; [04] RECEIVEDSDR SWAA2021062879847Support · out of toleranceREJECTION FWD O/B HOLE OF 887-947 FLOOR TO SIDEWALL SUPPORT REPLACEMENT OUT OF ROUND ; / [01] LOCATED AND DRILLED NEW FLOOR TO SIDEWALL P/N 147A7501-17 AT BS 887-947 RBL 21 WL 164; IAW B 737-700 SRM 51-40-05-OG-0 DWG 147A7501; [02] VERIFIED APPLICABILITY OF SRSDR SWAA2021062877523Floor Panel · corrodedPANEL 140CF IS CORRODED; AFT CARGO BAY ; / [01] FABRICATED NEW ACB FLOOR PANEL 140CF FROM 080 2024T3; LOT# 1457312-1 PER AMM 25-52-01-201-801 AND DWG 453A2610; [02] UPDATED FAULT INFORMATION; [03] VERIFIED PER AMM 25-52-01-201-801 AND DWG 453A2610SDR SWAA2021062877519Panel · chafedPANEL 192DR HAS CHAFING DAMAGE AT I/B EDGE / [01] VERIFIED APPLICABILITY OF SRM 53-40-70-OI-1 FOR IDENTIFICATION AND SRM 53-40-70-1A-1 FOR ALLOWABLE DAMAGE; [02] DAMAGE FOUND ON PANEL 192DR ON WING TO BODY FAIRING AT I/B EDGE; 5'X0.6'X0.020'; ORIGINAL THICKNESSDR SWAA2021062876861Panel · chafedPANEL 192F HAS CHAFING DAMAGE AT L/E INNER SURFACE ; / [01] IDENTIFIED PANEL 192F MATERIAL IAW SRM 53-40-70-OI-1 TABLE 2 FIGURE 2 ITEM 15. DAMAGE AT DISCREPANT LOCATION EXCEEDS ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1 PAR 4B(2). DAMAGE IS REPAIRABLE PER 51-70-05SDR SWAA2021062876859Panel · chafedPANEL 194CR HAS CHAFING DAMAGE ON L/E AT I/B END ; / [01] IDENTIFIED PANEL/MATERIAL IAW SRM 53-60-70-0I-1 FIG.2. TABLE 2. ITEM (6). FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-60-70-1A-1 PAR 4. B. (6) (B). REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-05-2SDR SWAA2021062876857Panel · chafedPANEL 194CL HAS CHAFING DAMAGE AT FWD I/B CORNER INNER SURFACE. ; / [01] IDENTIFIED PANEL 194CL IAW SRM 53-60-70-0I-1 FIGURE 2. TABLE 2. ITEM 6. FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-60-70-1A-1 PARA. 4.B.(7). DAMAGE IS TO BE REPAIRED IAWSDR SWAA2021062876846Panel · chafedPANEL 192BR HAS CHAFFING DAMAGE AROUND ENTIRE PERIMETER OF INNER SURFACE ; / [01] IDENTIFIED MATERIAL ID IAW SRM 53-40-70-0I-1 FIGURE 2; SHEET 1; TABLE 2; ITEM 6. UPON INSPECTION OF PANEL FOUND DAMAGE TO BE LIMITED TO AFT I/B CORNER. DAMAGE IS OUT OF ALLOWABLESDR SWAA2021062876845Panel · chafedPANEL 194DL HAS CHAFFING DAMAGE AT INNER SURFACE AFT EDGE ; / [01] IDENTIFIED PANEL/MATERIAL IAW SRM 53-60-70-0I-1 FIG. 2. TABLE 2. ITEM (7). FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-60-70-1A-1 PARA4.B.(6)(B). REPAIR TO BE ACCOMPLISHED IAW SRM 51-SDR SWAA2021062876836Support · chafedFAIRING FORMER SUPPORT HAS CHAFING DAMAGE AT BS727A JUST ABOVE NO.5 FLAP TRACK. ; / [01] LOCATED AND DRILLED FAIRING FORMER SUPPORT AT BS 727A JUST ABOVE NO.5 FLAP TRACK PER SRM 51-40-05 & BOEING DWG: 149A7902; [02] OK TO INSTALL FAIRING FORMER SUPPORT; [03] O
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