N286WN
Service difficulty reports · 295
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 = 'N286WN' 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 = 'N286WN' 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 SWAA2022061401844Floor Panel · deterioratedAFT CARGO COMPARTMENT FLOOR PANEL #141DF; SURFACE WORN/DETERIORATED. (DOT-001). AFT CARGO COMPARTMENT FLOOR PANEL #140DF SURFACE WORN/DETERIORATED. / [01] FABRICATED AFT CARGO PANEL #140DF IAW B737 AMM 25-52-01-201-801 .MATERIAL USED: A90RG1W.;[02] FINAL INSPESDR SWAA2022061401842Bulkhead · deterioratedAFT CARGO COMPARTMENT FWD BULKHEAD PANEL #140BF; SURFACE WORN/DETERIORATED. (DOT-004). AFT CARGO COMPARTMENT FLOOR PANEL #140BF SURFACE WORN/DETERIORATED. / [01] FABRICATED AFT CARGO PANEL #140BF IAW B737AMM 25-52-01-201-801 MATERIAL USED: A90RG1W;[02] FINAL ISDR SWAA2022061401849Bulkhead · deterioratedAFT CARGO COMPARTMENT FWD BULKHEAD PANEL #140AF; SURFACE WORN/DETERIORATED. (DOT-005). / [01] FABRICATED AFT CARGO PANEL #140AF IAW B737AMM 25-52-01-201-801 MATERIAL USED: A90RG1W;[02] FINAL INSPECTION; PANEL FABRICATED.SDR SWAA2022061407519Stiffener · crackedL/H WING AFT SPAR STIFFENER JUST I/B OF AFT BOOST PUMP UPPER ATTACH ANGLE IS CRACKED. / [01] REMOVED AND REPLACED ANGLE AT L/W WING AFT SPAR STIFFENER JUST I/B OF AFT BOOST PUMP UPPER ATTACH AS PER B737 SRM 51-40-02-0G-0;[02] VERIFIED 1.SDR SWAA2022061401992Bear Strap · crackedCRACK FOUND AT R1 DOOR BEAR STRAP EMANATING FROM FASTENER OPPOSITE FITTING LATCH AT STA 294.5 BETWEEN STR-8R AND STR-9R. CRACK LENGTH : 0.968. / PERFORMED 0.040 IN. INSURANCE CUT AT R1-BEARSTRAP. REF.B737-7. SRM-53-10-01-2R-6. STEP 4-D(1).FABRICATED REPAIR DOUSDR SWAA2022061401993Stub Frame · crackedR-1 DOOR CUT-OUT FWD UPPER STUB FRAME FOUND CRACKED. 124-009 / [01] REMOVED DAMAGE STUB FRAME PER REF B737 SRM 51-40-02-0G-0;[02] RECEIVED NEW STUB FRAME. P.O# 1728471. LOCATED AND DRILLED STUB FRAME. REF. B-737-7 SRM-51-40-05-0G;[03] VERIFIED STEP 1 AND 2.;[0SDR SWAA2022061401678Skin · crackedCRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90 ;17.5' FROM REAR SPAR ;I/B FASTENER ROW.CRACK LENGTH = 0.843' CRACK FOUND AT RIGHT HORIONTAL STABILIER LOWER SKIN STAB STA 193.90 17.5' FROM REAR SPAR I/B FASTENER ROW.CRACK LENGTH = 0.843' SDR SWAA2022061401477Scuff Plate · damagedR2 DOOR FWD UPPER SCUFF PLATE AREA LEAKING. / [01] R2 DOOR SCUFF PLATE INSTALLATION WILL BE COMPLETED ON TASK CARD: TTG8Q003DJH3. LEAK CHECK WILL BE PERFORMED ON TASK CARD: TTG8Q003EP8A.;[02] FINAL INSPECTION; R2 DOOR SCUFF PLATE INSTALLATION WILL BE COMPLETEDSDR SWAA2022061401478Scuff Plate · damagedL2 DOOR AFT SCUFF PLATE LEAKING. / [01] L2 DOOR AFT SCUFF PLATE INSTALLATION WILL BE COMPLETED ON TASK CARD: TTG8Q003DJH3. LEAK CHECK WILL BE ACCOMPLISHED ON TASK CARD: TTG8Q003EP8A.;[02] FINAL INSPECTION; L2 DOOR AFT SCUFF PLATE INSTALLATION WILL BE COMPLETEDSDR SWAA2022061401480Scuff Plate · damagedL1 DOOR FWD LWR AREA SCUFF PLATE LEAKING. / [01] L1 DOOR SCUFF PLATE INSTALLATION WILL BE COMPLETED ON TASK CARD: TTG8Q003DJK5. LEAK CHECK WILL BE ACCOMPLISHED ON TASK CARD: TTG8Q003EP8A.;[02] FINAL INSPECTION; L1 DOOR SCUFF PLATE INSTALLATION WILL BE COMPLETESDR SWAA2022061401677Skin · crackedCRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90 ;9.5' FROM REAR SPAR ;I/B FASTENER ROW.CRACK LENGTH = 0.781' CRACK FOUND AT RIGHT HORIONTAL STABILIER LOWER SKIN STAB STA 193.90 9.5' FROM REAR SPAR I/B FASTENER ROW.CRACK LENGTH = 0.781' / SDR SWAA2022061401676Skin · crackedCRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90 ;17' FROM FRONT SPAR ;I/B FASTENER ROW.CRACK LENGTH = 1.234' CRACK FOUND AT LEFT HORIONTAL STABILIER LOWER SKIN STAB STA 193.90 17' FROM FRONT SPAR I/B FASTENER ROW.CRACK LENGTH = 1.234' / [0SDR SWAA2022061401125Floor Panel · deterioratedFWD CARGO FLOOR PNL 120AF DETERIORATED. / [01] FABRICATED FWD CARGO FLOOR PANEL 120AF. AMM 25-52-01-201-801. MATERIAL USED: A90RG1W4X12.;[02] FINAL INSPECTION; FLOOR PANEL FABRICATED.SDR SWAA2022061401126Floor Panel · deterioratedFWD CARGO FLOOR PNL 120CF DETERIORATED. / [01] FABRICATED AFT CARGO PANEL 120CF IAW AMM 25-52-01-201-801. MATERIAL USED: A90RG1W48144.;[02] FINAL INSPECTION; PANEL FABRICATED.SDR SWAA2022061401321Slat · crackedRT WING #6 SLAT LWR SURFACE HAS A CRACK AT AFT FASTENER SLAT STA 202.45. 8-8 / [01] PERFORMED HFEC AT SUSPECTED CRACK IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK CONFIRMED AT AFT FASTENER. CRACK LENGTH:0.984'<BR>[NORTEC 600 ; B/C 166317 ; CALIB.DUE-10/22];04SDR SWAA2022061401322Slat · crackedRT WING #8 SLAT LWR SURFACE HAS A SUSPECTED CRACK AT I/B HILOCK 2ND FROM FWD FASTENER SLAT STA 451.50. 8-9 / [01] PERFORMED HFEC AT SUSPECTED CRACK IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK CONFIRMED EMANATING FROM I/B AFT FASTENER. CRACK LENGTH : 0.748';[SDR SWAA2022061401323Slat · crackedRT WING #7 SLAT LWR SURFACE HAS A SUSPECTED CRACK AT I/B AFT HILOCK SLAT STA 322. 8-10 / [01] PERFORMED HFEC AT SUSPECTED CRACK IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK CONFIRMED EMANATING FROM I/B FURTHEST AFT FASTENER. CRACK LENGTH: 0.118';[02] REMOVED SDR SWAA2021111743089Limiter · failedHYD 'B' SYSTEM FAILURE; B QTY READS 0 ; / [01] FOUND FLAP FLOW LIMITER FITTING CRACKED; REMOVED & REPLACED FLAP FLOW LIMITER IAW AMM 27-51-67. REMOVED & REPLACED EDP & EMP CASE DRAIN FILTERS IAW AMM 29-11-51. NO CONTAMINATION FOUND. SERVICED B SYS IAW AMM 12-1SDR SWAA2021111745257Filter · failedHYD 'B' SYSTEM FAILURE; B QTY READS 0 ; / [01] FOUND FLAP FLOW LIMITER FITTING CRACKED; REMOVED & REPLACED FLAP FLOW LIMITER IAW AMM 27-51-67. REMOVED & REPLACED EDP & EMP CASE DRAIN FILTERS IAW AMM 29-11-51. NO CONTAMINATION FOUND. SERVICED B SYS IAW AMM 12-1SDR SWAA2021083012471Tail Cone · crackedRAMP REPORTS CRACK ON L/H #3 CANOE FAIRING TAILCONE. OK TO CONTINUE PER CDL 57-10-4. REMOVED AND REPLACED #3 AFT CANOE FAIRING PER 27-51-18 AMM.SDR SWAA2021051470951Lens · missingEMERGENCY LIGHT LENS CAP MISSING FROM BOTTOM LIGHT ON MID CABIN EXIT ROW F.O. SIDE. ; / REPLACED MISSING LENS IAW AMM 33-51-03SDR SWAA2020111730752Cover · brokenEMERGENCY EXIT LT COVER AT EMERGENCY EXIT ROW ON RT SIDE BROKEN. R & R COVER, PER SIP.SDR SWAA2020111630273Lens · looseCREW REPORTED: LEFT OVERWING LOWER EXIT LIGHT LENSE LOOSE. SECURED LEFT OVERWING LOWER SIDEWALL EXIT LIGHT LENSE, PER AMM 33-51-01.SDR SWAA2020071600134Sign · brokenCREW REPORTS EMERGENCY EXIT SIGN BROKEN AT RT OVERWING EXIT KICK PANEL. REPLACED LIGHT ASSY & OPS CHECK GOOD IAW MM 33-51-01.SDR SWAA2020062994466Lens · detachedMID CABIN OVERHEAD EMERGENCY LIGHT LENS POPPED OFF. REINSTALLED THE SIGN LENS IAW AMM 33-51-01.SDR SWAA2020061591456Sign · looseG4 GALLEY EMERGENCY EXIT LIGHT 50% BURNT. RESECURED LOOSE LAMP AT THE G4 GALLEY EMERGENCY EXIT SIGN IAW AMM 33-51-01--960-802 PERFORMED OPS-CHECK IAW AMM 33-51-00-720-801; TEST FOUND NORMALSDR SWAA2020061590949Connector · disconnectedR/H CABIN EMERGENCY EXIT DOOR AFT SIDE LIGHT INOP. RESECURED R/H CABIN EMERGENCY EXIT DOOR AFT SIDE LIGHT ASSY CONNECTOR D12394 PER B737 AMM 33-51-01-960-801SDR SWAA2021062990244Scuff Plate · crackedAFT CARGO CENTER SCUFF PLATE P/N 146A8342-7; CRACKED 2.5 INCHES AT I/B SIDE. / WELDED AFT CARGO COMPARTMENT CENTER SCUFF PLATE BY J.L. WELDING W/O 15903SDR SWAA2021040890243Baffle · crackedFORWARD CARGO BAFFLE CRACKED BELOW Z CHANNEL BETWEEN STA.500 AND 500A; LBL21;WL155; STR26L / REMOVED AND REPLACED BATTLE AT FWD CARGO COMPARTMENT BETWEEN FS 500 AND FS 500A LBL 21' WL 155. STRINGER 26L IN REF B737-700 SRM 51-40-02-0G-0 AND DRAWING # 143A7510SDR SWAA2021062989874Scuff Plate · crackedAFT CARGO COMPARTMENT AFT SCUFF PLATE CORNER CRACK AT LOWER SIDE. / WELDED AFT CARGO COMPARTMENT AFT SCUFF PLATE CORNER BY J.L. WELDING W/O 15903SDR SWAA2021081388681Stiffener · crackedLT W/W STA 663 BULKHEAD LBL 28 JUST O/B OF RAM AIR EXHAUST LOWER ANGLE BRACKET IS CRACKED AT LOWER END. [DOT 124-036] / REMOVED RAM AIR DUCT FOR ACCESS PER REF. B737 AMM 21-51-24-400-801; REMOVED DAMAGED STIFFENER FROM LT W/W STA. 663' BULKHEAD; LBL 288; JUST SDR SWAA2021071690055Baffle · brokenFWD CARGO HAS A BROKEN BAFFEL AT BS 500B-500C BETWEEN STRINGER 26 27 LEFT / REMOVED AND REPLACED BAFFLE AT FWD CARGO AT BS 500C BETWEEN STRINGER 26-27 LEFT IN REF B737-700 SRM 51-40-02-0G-0SDR SWAA2021072987917Fitting · corrodedVERTICAL STABILIZER R/H AFT SPAR FITTING I/B BOLT SHOWING STRESS CORROSION. / RECEIVED NEW SERVICABLE VERTICAL STABILIZER R/H AFT SPAR FITTING I/B BOLT P/N 170A1611-4 TO BE INSTALLED ON CUSTOMER CARD J753-480-00-00SDR SWAA2021072987916Bolt · corrodedVERTICAL STABILIZER AFT RIGHT SPAR FITTING O/B BOLT SHOWING STRESS CORROSION. / RECEIVED NEW SERVICABLE VERTICAL STABILIZER AT RIGHT SPAR FITTING O/B BOLT P/N 170A1611-1 TO BE INSTALLED ON CUSTOMER CARD J753-480-00-00SDR SWAA2020061587918Channel · corroded*** CORROSION*** FLIGHT DECK BETWEEN STA 259.5 AND STA 270 ; WL 208 ; LBL2 TO RBL2 INTERCOSTAL SUPPORT CHANNEL HAS CORROSION. REMOVED AND INSTALLED NEW INTERCOSTAL UPPER CHANNEL ON FLIGHT DECK BETWEEN STA259.5 AND STA 270 WL 208; LBL 2 RBL2 AS PER B737-700 SSDR SWAA2021052681881Gusset · crackedLEFT WING TRAILING EDGE ; ABOVE THE FIXED PANEL (BETWEEN SPOILERS #5 AND #6) GUSSET CRACKED AT LWR FASTENER HOLE / REMOVED AND REPLACED GUSSET AT L/W T/E BETWEEN SPOILER #5 AND #6 AS PER SRM 51-40-02-0G-0 AND DRAWING 115A2982SDR SWAA2021082580766Floor Support · corrodedCORROSION FOUND AT AFT CARGO COMPARTMENT. L/ H SIDE FLOOR SUPPORT Z CHANNEL AT S-25L FROM STA 727D TO STA 847. MKD DOT 60-010 LBL 21' AND W.L. 153.5 / REMOVED CORROSION ON AFT CARGO COMP L/H SIDE Z CHANNEL FROM STA 727E TO 847'PER REF B737 SRM 51-10-02-0G-0; OSDR SWAA2021081780762Floor Support · corroded*** CORROSION *** FLOOR SUPPORT ANGLE SURFACE CORROSION AT FASTENER HOLES INB. OF AFT CARGO COMPMT. LOWER SILL WEB CHORD BETWEEN STA 787 & STA 807 MKD DOT 60-009. RBL-20; WL-155.5 / REMOVED AND REPLACED FLOOR SUPPORT STRAP AT AFT CARGO COMP RBL 20 FROM STR 772SDR SWAA2021071580765Rail · corrodedCORROSION; ON SEVERAL SPOTS AT AFT CARGO COMP BILGE AREA FLOOR PANEL SUPPORT ANGLE FROM BS 944.5 TO BS 887 RBL-3 MKD 126-005. WL 155.5 / REMOVED CORROSION ON AFT CARGO COMP BILGE AREA; FLOOR RAIL SUPPORT; FROM STA 887 TO 944.5' RBL-3 PER REF B737 SRM 51-10-02-SDR SWAA2021061580768Fairing · delaminatedLOWER FUSELAGE BODY FAIRING PANEL # 194DL HAS SPOT DELAMINATION 31/2 INCHES FROM EDGE UPPER SURFACE SKIN / CLEANED & REPAIRED 3.4 DIA SPOT DELAMINATION ON LOWER FUSEAGE BODY FAIRING PANEL #194DL AS PER B737-700 SRM 51-70-04-2R-1 MATERIAL USED PO# 1480720 & PO#SDR SWAA2020061680980Support · corrodedCORROSION ON A SMALL SPOT AT THE FRAME SUPPORT AFT FACE LOWER EDGE AT BS 1006, BL 0.SDR SWAA2020061580609Beam · crackedCRACK INDICATION FOUND AT FWD SERVICE DOOR INTERNAL LWR BEAM #4 UPPER FILLET REGION. / REMOVED AND REPLACED BEAM AT FWD SERVICE DOOR INTERNAL LOWER AS PER B737-7 SRM 51-40-02-0G-0 DRAWING # 141A6535SDR SWAA2020061580767Cargo Track · corrodedCORROSION; SMALL SPOT AT AFT CARGO COMP BILGE AREA JUST BEHIND OF AFT BULKHEAD; FLOOR PANEL SUPPORT T ANGLE BS 947 RBL-13.8 MKD 126-006. WL 153.8 / REMOVED CORRODED TRACK AND INSTALLED NEW TRACK AFT CARGO COMPOARTMENT FROM STA 887 TO STA 947.5; RBL 13.8; PER RSDR SWAA2020061580771Fitting · corrodedL-1 DOOR AFT GIRT BAR FITTING STA 344 LBL 59 HAS CORROSION. [DOT 124-034] / REMOVED AND REPLACED L-DOOR AFT GIRT BAR FITTING STA 344 LBL 59 AS PER REF B737-700 SRM 51-40-02-0G-0 JS 5083 6/2/20SDR SWAA2020061580758Channel · corrodedFOUND AFT CARGO COMPARTMENT.RT SIDE Z CHANNEL FLOOR SUPPORT S-25R BETWEEN STA 727E AND STA 747 RBL 21' AND W.L. 153.5. EVALUATED CORROSION ON AFT CARGO COMP R/H Z CHANNEL BETWEEN STA 727E AND 747; FOUND EXFOLIATED CORROSION, AREA OUT OF LIMITS PER REF B737 SSDR SWAA2020061580981Fitting · corrodedL-1 DOOR FWD GIRT BAR FLOOR FITTING STA 312 LBL 55 HAS CORROSION. [DOT 124-035] / REMOVED AND REPLACED L-1 DOOR FWD GIRT BAR FITTING STA 312 LBL 55.SDR SWAA2021081380596Bracket · crackedFWD CARGO COMPARTMENT AT BS 500C AND STR26L ANGLE ATTACH BRACKET FROM FRAME TO Z CHZNNEL SUPPORT IS CRACKED. [200-008] / REMOVED AND REPLACED BRACKET AT FWD CARGO COMP AT BS 500C STR 26L IN REF B737-700 SRM 51-40-02-0G-0SDR SWAA2021072780590Attach Fitting · corroded***CORROSION*** LT WING T/E PANEL 561BB ATTACH SUPPORT STRUCTURE HAS CORROSION AT SEVERAL SCREW HOLES. [200-001] / BURNISHED AREA AT L/WING T/E PANEL 561BB SUPPORT STRUCTURE NO DAMAGE NOTED REF B737-700 SRM 51-10-02-0G-0SDR SWAA2021052680594Gusset · crackedFWD CARGO COMPARTMENT AFT BULKHEAD SUPPORT ANGLE AT BS 500D AND STR21L IS CRACKED. [200-006] / REMOVED AND REPLACED GUSSET AT FWD CARGO COMPARTMENT AFT BULKHEAD STA 500D STR21L REF B737-7 SRM 51-40-02-0G-0 DRAWING # 143A7902 MD 32785 05/31/2020SDR SWAA2021052680595Gusset · crackedFWD CARGO COMPARTMENT AFT BULKHEAD GUSSET AT BS 500D AND S-19R IS CRACKED. [200-007] / REPLACED CRACKED GUSSET @ FWD CARGO COMPARTMENT AFT BULKHEAD @ BS 500D SND STR 19R AS PER B737-700SRM 51-40-02-0G-0 AND BOEING DWG 143A7902
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