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 SWAA2026091602212Stiffener · crackedCRACKED INTERNAL STRUCTURE STIFFENER LOCATED BTW BS 907 TO BS 927 AND BTW STRG 25R TO STRG 27R FWD POSITION AT AFT CARGO COMPARTMENT. REPLACED THE STIFFENER & FASTENERS IAW SRM 51-40-02 AND DWG 147A7221, SHEET 17 REV D.SDR SWAA2026091661779Stiffener · crackedCRACK INTERNAL STRUCTURE STIFFENER LOCATED BTW BS 907 TO BS 927 AND BTW STRG 25R TO STRG 27R AFT POSITION AT AFT CARGO COMPARTMENT 2026-505555 REPLACED STIFFENER & FASTENERS LOCATED BTW BS 907 TO BS 927 AND BTW STRINGER 25R TO STRINGER 27R AFT POSITION AT AFT SDR SWAA2026091199190Handle · deterioratedDETERIORATED HANDLE NUT, & YELLOW STRAP ON AFT ENTRY DOOR LINING AT AFT GALLEY AREA. REPLACED HANDLE NUT & YELLOW STRAP ON AFT ENTRY DOOR LINING AT AFT GALLEY AREA IAW AMM 25-21-25-420-801, STEP 3.B (5), AND DWG 411A2500, SH-5, REV C.SDR SWAA2026091438273Bracket · crackedCRACK BRACKET TRAILING EDGE LOCATED IRSS 210 APROX AT RT WING. REPLACED BRACKET IAW SRM 51-40-02, SRM 51-10-02, AND DWG 115A2001, SHEET 24, REV A.SDR SWAA2026091654020Strap · crackedCRACK INDICATION FOUND AT BS 616, LBL 45.57 STUB BEAM TRAPS AREA. (FWD FASTENER HOLE). REPLACED STUB BEAM STRAP IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 144A1714, SHEET 9, REV -, DWG 112A3301, SHEET 16, REV -, & DWG 144A1704, SHEET 8, REV -.SDR SWAA2026091671091Light · deterioratedDETERIORATED PHOTOLUMINESCENT LIGHT ALONG PASSENGER CABIN. REPLACED THE PHOTOLUMINESCENT LIGHT IAW AMM 33-51-15-400-802.SDR SWAA2026091417259Web · corrodedCORROSION ON UPPER MAIN SILL WEB LOCATED BTW BS 440 TO BS 492.4 RBL 68 WL 200 AT FWD CARGO BAY. REPLACED UPPER MAIN SILL WEB AND FASTENERS LOCATED BTW BS 440 TO BS 492.4 RBL 68 WL 200 AT FWD CARGO BAY IAW BOEING SRM 51-40-02 DWG 143A8111 SHEET 1 REV -. AND DWSDR SWAA2026091480621Skin · debondedDEBONDED LOWER SKIN ON OTBD AFT FLAP RT WING. REPAIRED OTBD AFT FLAP RT WING IAW SRM 57-53-01-2R-4, REPAIR 4, & SRM 51-70-10-2R-4, REPAIR 4.SDR SWAA2026091420796Skin · debondedDEBONDED LOWER SKIN ON OTBD AFT FLAP, LT WING. PERFORMED INTERIM REPAIR ON OTBD AFT FLAP AT LT WING IAW SRM 57-53-01-2R-16 REPAIR 16. PERFORMED TAP TEST INSPECTION EVERY 6875 FLIGHT CYCLES OR 30 MONTHS WICHEVER COMES FIRST.SDR SWAA2026091605216Access Panel · leakingFUEL LEAK ON ACCESS PANEL 632HB AT RT WING. REMOVED AND REINSTALLED ACCESS PANEL 632HB IAW AMM 28-11-11-000-801 AND AMM 28-11-11-400-801.SDR SWAA2026091462607Support Angle · crackedCRACKED SUPPORT ANGLE, ACCESS PANEL 651FB, RT WING. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, DWG 115A2710, SHEET 5, REV A, & DWG 287A9152, SHEET 3, REV A.SDR SWAA2026091463270Rib · crackedCRACKED LEADING EDGE RIB ACCESS PANEL 331B LE HSS 114.55 AT LT HORIZONTAL STAB. REPLACED LEADING EDGE RIB & FASTENERS ON ACCESS PANEL 331B LE HSS 114.55 IAW SRM 51-40-02 AND DWG 186A1001, SHEET 10, REV A.SDR SWAA2026091453396Access Panel · crackedCRACKED BLADE, ACCESS PANEL 333AT AT LT HORIZONTAL STAB. REPLACED BLADE ON ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW SRM 51-10-02 AND SRM 51-40-02.SDR SWAA2026091439784Panel · debondedDEBONDED WEDGE PANEL ON RT INBOARD FLAP AT RT WING. PERFORMED INTERIM REPAIR ON WEDGE PANEL ON RT INBD FLAP AT RT WING IAW SRM 57-53-01-2R-18, REPAIR 18. PERFORMED TAP TEST INSPECTION EVERY 6875 FLIGHT CYCLES OR 30 MONTHS WICHEVER COMES FIRST.SDR SWAA2026091435509Angle · crackedCRACK ANGLE, ACCESS PANEL 651GB AT RT WING. REPLACED ANGLE LOCATED ON ACCESS PANEL 651GB AT RT WING IAW SRM 51-40-02, & SRM 51-10-02-0G-0. INSPECTION AND REMOVAL OF DAMAGE.SDR SWAA2026091430002Rib · crackedCRACK LEADING EDGE RIB ACCESS PANEL 331B LE STA 86.66 AT LT HORIZONTAL STAB. REPLACED LEADING EDGE RIB AND FASTENERS ON ACCESS PANEL 331B LE STA 86.66 AT LT HORIZONTAL STAB IAW SRM 51-40-02, AND DWG 186A1001, SHEET 10, REV A.SDR SWAA2026091475041Access Panel · delaminatedACCESS PANEL 192HL - DENTED & DELAMINATED. REPAIRED THE ACCESS PANEL 192HL IAW SRM 51-70-05-2R-2, REPAIR 2.SDR SWAA2026091493968Access Panel · delaminatedACCESS PANEL 551AT DENTED WITH DELAMINATION. REPAIRED ACCESS PANEL 551AT IAW SRM 51-70-05-2R-2 REPAIR 2.SDR SWAA2026091689932Seat Track · corrodedCORROSION ON SEAT TRACK (TOP SURFACE) LOCATED BS 639 PLUS 23 INCH RBL 45.50 AT PASSENGER CABIN REFER TO FAULT TTG8Q01DUFY3 WHERE 26-153-02366-WIP1 WAS ADDED AS A SUBTASK.SDR SWAA2026091672764Seat Track · corrodedCORROSION ON SEAT TRACK (TOP SURFACE) LOCATED BS 639 PLUS 12 INCH RBL 45.50 AT PASSENGER . REPAIRED SEAT TRACK BTW BSTA 639 & BSTA 706 AT RBL 45.50 AT PASSENGER CABIN IAW EA 26-153-02366 AND EA 26-153-02366-WIP1.SDR SWAA2026091689594Seat Track · corrodedCORROSION ON SEAT TRACK (TOP AND BOTTOM SURFACE) LOCATED BTW BS 685 TO BS 706 RBL 45.50 AT PASSENGER CABIN.SDR SWAA2026091621561Skin · corrodedCORROSION EXTERNAL SKIN WATER SERVICE CUT OUT BTW BS 907 TO BS 927 AND BTW STRG 26R TO STRG 27R AT LOWER FUSELAGE. REPAIRED EXTERNAL SKIN WATER SERVICE CUT OUT BTW BS 907 TO BS 927 AND BTW STRG 26R TO STRG 27R AT LOWER FUSELAGE IAW EA 26-153-02413 SUMMARY EA SDR SWAA2026091613651Seat Track · corrodedCORROSION ON SEAT TRACK (TOP SURFACE) LOCATED BTW BS 663 TO BS 685 RBL 45.50 AT PASSENGER CABIN 2026-505409 REFER TO FAULT TTG8Q01DUFY3 WHERE 26-153-02366-WIP1 WAS ADDED AS A SUBTASK..SDR SWAA2026091478011Crossbeam · crackedCRACKED BRAKE PANEL, BS 540, BTWN BL 0 - RBL 24.75. REPLACED THE BRAKE PANEL IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, & DWG 143A0060, SHEET 64, REV-.SDR SWAA2026091100263Angle · crackedCRACK ON ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN. REPLACED ANGLE AND FASTENERS IAW SRM 51-40-02 AND DWG 273A9110, SHEET 6, REV A.SDR SWAA2026091682161Seat Track · corrodedCORROSION SEAT TRACK LOC. ON BS 807 PLUS 6 INCHES AND WL 208 ON TOP SURFACE AT LBL 45.5 AT PASSENGER CABIN REPAIRED SEAT TRACK LOC. ON BS 807 PLUS 6 INCHES AND WL 208 ON TOP SURFACE AT LBL 45.5 AT PASSENGER CABIN IAW EA 26-153-02367 AND EA 26-153-02367-WIP1.SDR SWAA2026091433998Frame · crackedCRACKED FRAME, BS 312 BTW STR 5L - 6L. PERFORMED TRIM OUT OF FRAME UPPER ANGLE IAW EA M-22-153-01244, REV B.SDR SWAA2026091411280Strap · crackedCRACK STRAP LOCATED ON ACCESS PANEL 142KW AT AFT CARGO BAY. TOOK MEASURES OF CRACK ON STRAP LOCATED ON ACCESS PANEL 142KW AT AFT CARGO COMPARTMENT DUE TO NO FOUND ALLOWABLE DAMAGE ON SRM-52-30-01-1A-1 ALLOWABLE DAMAGE 1 STRAP WAS REPLACED AND WILL BE INSTALLSDR SWAA2026091483813Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 671CB TRAILING EDGE, RT WING. PERFORMED VISUAL INSPECTION ON REPORTED AREA AND NOT FOUND ELONGATED HOLE ONLY FOUND BURN PAINT AROUND THE HOLE IAW SRM 51-00-06-OG-0. RESTORED PAINT IAW AMM 51-21-99-300-801.SDR SWAA2026091465029Access Panel · elongatedELONGATED HOLE ACCESS PANEL 561BB ON LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026091482156Access Panel · elongatedELONGATED HOLE ACCESS PANEL 561CB AT LT WING. REPAIRED ACCESS PANEL 561CB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026091139224Skin · crackedCRACK EXTERNAL GROUND ELECTRICAL POWER CUTOUT LOWER AREA AT LOWER FUSELAGE. REPAIRED EXTERNAL GROUND ELECTRICAL POWER DOOR CUTOUT LOWER AREA AT LOWER FUSELAGE IAW SRM 53-10-15-2R-4, REPAIR 4.SDR SWAA2026091100219Scuff Plate · crackedCRACK ON AFT CORNER SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED THE AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4. B, STEPS (2 TO 7) FIGURE 203.SDR SWAA2026072831243Screw · missingFWD GALLEY SERVICE DOOR SLIDE IS GETTING CAUGHT ON FLOOR METAL COVER PLATE. INSTALLED MISSING SCREW ON FLOOR METAL COVER PLATE BY FWD GALLEY SERVICE DOOR SLIDE IAW AMM 20-50-11.SDR SWAA2026072034663Lens · missingFORWARD OVERWING EXIT SIGN IS MISSING. REPLACED LENS COVER PER SIP.SDR SWAA2026051197064Bolt · looseSEAT 15D WILL NOT LOCK IN UPRIGHT POSITION<[01] OK TO CONTINUE PER MEL 25-6-01 SP 1B. FOUND LOOSE & STRIPPED BOLT REPLACED BOLT PER CMM 25-21-42SDR SWAA2025112639129Light · detachedFORWARD GALLEY EMERGENCY EXIT LIGHT COVER FELL OFF. R & R FWD GALLEY EMERGENCY LIGHT ASSY IAW AMM 33-51-01-960-802-NG, OPS CHECKED NORMAL.SDR SWAA2025110530947Sign · inoperativeAFT SERVICE DOOR, BOTH RT AND LT OVER WING EMERGENCY EXIT SIGNS LIGHTS MISSING BULBS. REPLACED THE BULBS IN THE SIGNS AND PERFORMED GOOD TEST IAW AMM 33-51-01-960-801.SDR SWAA2025092518029Girt Bar · unpackedL2 DOOR ESCAPE SLIDE GIRT REQUIRES REPACK. REPACKED L2 DOOR ESCAPE SLIDE GIRT IAW AMM 25-66-01-000-804-NG.SDR SWAA2025092518027Girt Bar · unpackedR2 DOOR ESCAPE SLIDE GIRT REQUIRES REPACK. REPACKED R2 DOOR ESCAPE SLIDE GIRT IAW AMM 25-66-01-000-804-NG.SDR SWAA2025081199344Lens · detachedCREW REPORTS F.O. SIDE OVERWING EXIT LIGHT LENS COVER DEATTACHED. SECURED WITH TAPE. OK TO CONT. PER EA# MT M-21-133-00720.SDR SWAA2025052774702Lamp · inoperativeRH EMERGENCY EXIT DOOR LIGHT INOP. RELAMPED RH EXIT DOOR LAMP REF AMM 33-51-01.OPS CHECKED GOOD.SDR SWAA2025050565193Seal · crackedL/H STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL CRACKED<[01] REMOVED AND REPLACED L/H STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL IN ACCORDANCE WITH AMM 53-31-31. OPS CHECK GOOD.SDR SWAA2024111156197Light · missingMAIN CABIN EPL STRIPS MISSING AT ROWS 10ABC AND 18DEF.<[01] INSTALLED MAIN CABIN EPL STRIPS AT ROWS 10ABC AND 18DEF AS PER B737 AMM 33-51-15-400-802;[02] VERIFIED STEP 1.SDR SWAA2024111156196Handle · missingL-1 DOOR AFT ASSISTED HANDLE AND SAFETY STRAP MISSING.<[01] INSTALLED L1 DOOR AFT ASSISTED HANDLE AND SAFETY STRAP AS PER B737 AMM 25-21-25-420-801;[02] VERIFIED STEP 1.SDR SWAA2024111155286Battery Pack · inoperativeINTERIOR/EXTERIOR EMERGENCY EXIT LIGHTS INOP<[01] PERFORMED TROUBLESHOOTING AS PER BOEING 737 WDM 33-51-13; FOUND M1670 EMERGENCY EXIT LIGHT BATTERY PACK DEFECTIVE. REMOVED AND REPLACED M1670 EMERGENCY EXIT LIGHT BATTERY PACK AS PER B737 AMM 33-51-06-960-805. SDR SWAA2024110854620Sign · brokenL-1 DOOR EXIT SIGN INDICATOR BROKEN.<[01] ITEM ENTER IN ERROR;[02] ITEM ENTERED ON ERROR WILL BE ACCOMPLISHED TTG8Q004Z0B5;[03] VERIFIED STEPS 1 AND 2SDR SWAA2024110848216Seat Track · crackedF/O I/B FORWARD SEAT TRACK HAS CRACK FWD END<[01] RECEIVED NEW SEAT TRACK P/N 1A226-0204ATSMRO P.O. 2074280 PER B737-700 AMM 25-11-01-200-802. FOR SEAT TRACK INSTALLATION SEE TASK CARD TTG8QOO3JJ4A.;[02] VERIFIED RECEIVED.<BR>CORRECTION CARD TTG8Q003JJ4JSDR SWAA2024111145898Scuff Plate · crackedAFT CARGO COMPARTMENT DOOR CUTOUT LOWER SILL FWD SCUFF PLATE CRACKED MKD DOT<[01] RECIEVED AFT CARGO COMPARTMENT DOOR CUTOUT LOWER SILL FWD SCUFF PLATE REF INSTALLATION TO TASK CARD# TTG8Q005JAU3.;[02] VERIFIED STEP 1;[03] VERIFIED STEP 1SDR SWAA2024111146262Support · corrodedCORROSION, RIGHT MAIN W/W CUTOUT AFT ALL BLADE SEAL SUPPORTS TOP SURFACE. REMOVED CORROSION AT RIGHT MAIN W/W CUTOUT AFT SEAL TOP SURFACE AS PER B-737 SRM 51-10-02-0G<BR>'EVALUATED REWORKED AREA OF CUTOUT AFT BLADE SEAL TOP SURFACE'<BR>ORIGINAL MATERIAL: 0.06
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