N928WN
Service difficulty reports · 238
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 = 'N928WN' 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 = 'N928WN' 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 SWAA2020062988361Door · abnormalFWD ENTRY DOOR IS SAGGING. REMOVED FWD ENTRY DOOR IAW AMM 52-11-00-000-802. REMOVED AND REPLACED UPPER AND LOWER TORQUE TUBE BEARINGS IAW SOPM 20-50-03. REMOVED AND REPLACED UPPER AND LOWER TORQUE TUBE SPIGOTS IAW AMM 52-11-41-400-802 AND DWG 141A6270, REV ASDR SWAA2020062988363Door · abnormalR1 DOOR WAS SAGGING. REMOVED THE R1 DOOR IAW AMM 52-41-00-00-801, REPLACED THE GUIDE ARM IAW AMM 52-41-21-400-801, REPLACED UPPER AND LOWER BEARING PLATES IAW SRM 51-40-02-0G-0, INSTALLED R1 DOOR IAW AMM 52-41-00-400-801, AND ACCOMPLISHED ADJUSTMENT IAW ASDR SWAA2020062988336Intercostal · corrodedE&E BAY, BS 328 - 333, STRINGER 23L INTERCOSTAL WAS CORRODED. REMOVED THE CORROSION, ORIG 'T' .063', REMOVED .043, LOSS OF .020'. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-10-02-0G-0, 53-00-04-1A-1, AND AMM 51-21-91-620SDR SWAA2020062988337Intercostal · corrodedE&E BAY, BS.344 - 351, STRINGER 23L INTERCOSTAL WAS CORRODED. REMOVED CORROSION, ORIG 'T' .063', REMAINING .025', LOSS OF .038', FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-10-02-0G-0, 53-00-04-1A-1, AND AMM 51-21-91-620SDR SWAA2020062988333Intercostal · corrodedE&E BAY, BS 294 - 302, STRINGER 23L. THE INTERCOSTAL WAS CORRODED, LBL 33, WL 165. REMOVED THE CORROSION, ORIG 'T' .050', REMOVED .035', LOSS OF .015'. FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED THE INTERCOSTAL.SDR SWAA2020062988367Intercostal · corrodedNOSE GEAR BAY, LEFT AFT ACCESS HOLE, 3 INCHES FWD OF BS 294, STRINGER 23L, WL 165, INTERCOSTAL HAD CORROSION ON UPPER FACE. REMOVED CORROSION, ORIG 'T' .050', REMAINING .036', LOSS OF .014'. FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED THE INTERCOSTSDR SWAA2020062988364Floor Panel · damagedPASSENGER CABIN FLOOR PANEL 232HF HAD FIBERS PULLING LOOSE. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0, GENERAL REPAIR, AND SRM 53-00-50-2R-1, REPAIR 1.SDR SWAA2020062988366Baffle · crackedFWD CARGO COMPARTMENT RT BAFFLE WAS CRACKED, BS 500A - 500B, WL 155. REMOVED THE BAFFLE, RECEIVED A NEW BAFFLE AND INSTALLED A -2 REPAIR DOUBLER ON NEW BAFFLE. ALODINED; PRIMED AND APPLIED CIC TO BAFFLE AND -2 REPAIR DOUBLER. DOUBLER INSTALLED IAW SRM 53-30SDR SWAA2020062988368Floorboard · damagedPASSENGER CABIN FWD WET AREA FLOORBOARD 221AF UPPER SURFACE HAD FIBERS PEELING. REPAIRED THE FLOORBOARD IAW SRM 53-00-50-2R-1, AND SRM 53-00-50-2R-0.SDR SWAA2020062988369Floor Panel · damagedCABIN FLOOR PANEL 242QF AFT INBD EDGE IS DAMAGED. REMOVED THE FLOOR PANEL IAW SRM 53-00-50-2R-1, REV 70, AND SRM 53-00-50-2R-0, REV 70.SDR SWAA2020062988375Floorboard · damagedPASSENGER CABIN FWD WET AREA FLOORBOARD 221CF UPPER SURFACE HAD FIBERS PEELING. REPAIRED THE FLOORBOARD IAW SRM 53-00-50-2R-1, PARA 3, AND SRM 53-00-50-2R-0.SDR SWAA2020062988378Floorboard · peelingPASSENGER CABIN FWD WET AREA FLOORBOARD 221EF UPPER SURFACE HAD FIBERS PEELING. REPAIRED THE FLOORBOARD IAW SRM 53-00-50-2R-1, PARA 3, AND SRM 53-00-50-2R-0.SDR SWAA2020062988381Floorboard · damagedPASSENGER CABIN FWD WET AREA FLOORBOARD 221GF UPPER SURFACE HAD FIBERS PEELING. REPAIRED THE FLOORBOARD IAW SRM 53-00-50-2R-1, REV 70, AND SRM 53-00-50-2R-0, REV 70.SDR SWAA2020062988356Floorboard · damagedPASSENGER CABIN FWD WET AREA FLOORBOARD 222DF, UPPER SURFACE HAD FIBERS PEELING. REPAIRED THE FLOORBOARD IAW SRM 53-00-50-2R-1, REPAIR 1, REV 70, AND SRM 53-00-50-2R-0, REPAIR GENERAL, REV 70.SDR SWAA2020062988354Floorboard · damagedPASSENGER CABIN FWD WET AREA FLOORBOARD 222CF, UPPER SURFACE HAD FIBERS PEELING. REPAIRED THE FLOORBOARD IAW SRM 53-00-50-2R-1, REPAIR 1, REV 70, AND SRM 53-00-50-2R-0, REPAIR GENERAL, REV 70.SDR SWAA2020062988352Floorboard · damagedPASSENGER CABIN FWD WET AREA FLOORBOARD 222BF, UPPER SURFACE HAD FIBERS PEELING. THE FLOORBOARD WAS REPAIRED IAW SRM 53-00-50-2R-1.SDR SWAA2020062988351Floor Panel · damagedPASSENGER CABIN FWD WET AREA FLOORBOARD 222AF, UPPER SURFACE HAD FIBERS PEELING. REPAIRED THE FLOOR PNAEL IAW SRM 53-00-50-2R-0, GENERAL REPAIR, AND SRM 53-00-50-2R-1, REPAIR 1.SDR SWAA2020062988345Floor Panel · damagedPASSENGER CABIN FLOOR PANEL 231CF HAD FIBERS PULLING LOOSE. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0, GENERAL REPAIR. AND SRM 53-00-50-2R-1, REPAIR 1.SDR SWAA2020062988343Floor Panel · damagedPASSENGER CABIN FLOOR PANEL 231AF HAD FIBERS PULLING LOOSE. REPAIRED THE FLOOR PANEL IAW SRM 53-0-0-50-2R-0, GENERAL REPAIR, AND SRM 53-00-50-2R-1, REPAIR 1.SDR SWAA2020062988380Floorboard · damagedPASSENGER CABIN, FWD WET AREA FLOORBOARD 221FF, UPPER SURFACE HAS FIBERS PEELING. REPAIRED THE FLOORBOARD UPPER SURFACE IAW SRM 53-00-50-2R-1, REV 70, AND SRM 53-00-50-2R-0, REV 70.SDR SWAA2020062988349Floor Panel · damagedPASSENGER CABIN FLOOR PANEL 231GF HAD FIBERS PULLING LOOSE. REPLACED BY FABRICATING A NEW FLOOR PANELE IAW SRM 53-00-50-2R-0, REV GENERAL, AIPC 53-21-51-81, INSTALLED IAW SEC 43 DWG 143A5810 BAC5085.SDR SWAA2020062988365Floor Panel · loosePASSENGER CABIN FLOOR PANEL 231KF HAD FIBERS PULLING LOOSE. FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-30-2R-0, REV 70, STEP 1 & STEP 4, IAW DRAWING 143A5810 ID 0580, REV -, & BAC5085 PG 21-23 STEP 8.4.2.SDR SWAA2020062988376Floor Panel · loosePASSENGER CABIN FLOOR PANEL 231DF HAD FIBERS PULLING LOOSE. FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-50-2R-0, REV 70, STEP 1A, AND STEP 4. IAW DWG 143A5810, REV A, AND BAC5085 PG 21-23 STEP 8.4.2.SDR SWAA2020062988335Intercostal · corrodedE&E COMP BS 320 - 326 STRINGER 23L INTERCOSTAL CORRODED LBL 39' WL165 / REMOVED CORROSION E+E COMP. STA 320 - 326 L/H STR 23 LBL 39' WL 165. ORIG 'T' .063' REMAINING 'T' .050' LOSS OF .013' FOUND TO BE OUT OF LIMITS. REMOVED + REPLACED INTERCOSTAL. APPLIED CISDR SWAA2021081587760Floorbeam · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE STA. 947.5 FRAME; LBL 10.5 IS CORRODED. / REMOVED CORROSION FROM STA 947.5 CARGO COMPARTMENT FLOOR FRAME 100% MATERIAL LOSS. REMOVED AND REPLACED FRAME IAW SRM 51-40-02-0G-0 AND DWG 147A1047. P/N 147A1047U48SDR SWAA2021071587787Support · corrodedAFT CARGO COMPARTMENT AFT BULKHEAD LOWER SUPPORT ANGLE AT STA 947; WL 179; RBL 21 TO LBL 2; HAS AREAS OF CORROSION; MARKED. / REMOVED CORROSION FROM AFT CARGO AFT BULKHEAD LOWER SUPPORT ANGLE STA 947.5 0.003' LOSS NO PUBLISHED ALLOWABLE LIMITS. REMOVED AND REPSDR SWAA2021060887776Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE STA 847 TO 867; S-25R; FLOOR SHIELD HAS VARIOUS AREAS OF CORROSION. / REMOVED CORROSION FOUND 100% MATERIAL LOSS FOUND OUT OF LIMIT IAW SRM 53-00-53-1A-1 VERIFIED MATERIAL P/N 146A8127-10 IAW B737-700 DWG #146A0081 REV A ASDR SWAA2021052687769Gusset · crackedFWD CARGO PIT LH SIDEWALL BODY FRAME GUSSET IS CRACKED AT BS 500D; STR 22L. / REMOVED AND REPLACED GUSSET AT B.S. 500D; STRINGER 22 LEFT I/A/W SRM 51-40-02-0G; DRAWING 143A9483 REV B; SOPM 20-20-02; SRM 51-40-05-0G; AMM 51-21-72-370; AMM 51-00-58-201 AND AMM 5SDR SWAA2021052687768Gusset · crackedFWD CARGO PIT LH SIDEWALL BODY FRAME GUSSET IS CRACKED AT BS 500D; STR 21L. / REMOVED CRACKED BODY FRAME GUSSET STA 500D STR. 21 L/H AND INSTALLED NEW GUSSET ALL IAW SRM 51-40-02-0G-0 AND DWG # 143A7902 REV -. ATAG A59194SDR SWAA2021052687767Gusset · crackedFWD CARGO PIT LH SIDEWALL BODY FRAME GUSSET IS CRACKED AT BS 500D; STR 19L. / REMOVED AND REPLACED CRACKED GUSSET IN FWD CARGO COMPARTMENT AT STA 500D; STR 19L IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A7902 ID: 0174 REV - ATAG A59199SDR SWAA2021052687766Gusset · crackedFWD CARGO PIT RH SIDEWALL BODY FRAME GUSSET IS CRACKED AT BS 500D; STR 19R. / REMOVED AND REPLACED GUSSET IN FWD CARGO COMPARTMENT AT STA 500D STR 19R IAW SRM 51-40-02-0G-0 AND BOEING DWG # 143A7902 ID 0174 REV - A59193SDR SWAA2020062987809Crease Beam · corrodedCORROSION ON L1 CREASE BEAM VERTICAL FLANGE AT BS 303.9, LBL 56, WL 209. REMOVED AND REPLACED L1 CREASE BEAM FROM BS 270 - 360 IAW SRM 53-10-15-01, SRM 51-10-02-0G, SRM 53-10-15-1A, SRM 51-40-02-0G, DRAWING 141A8110, REV A, SRM 51-40-05-0G, AMM 51-21-9SDR SWAA2020062987780Floorbeam · crackedPASSENGER CABIN FLOORBEAM BS 540, BL 0 - RBL 24 WAS CRACKED. THE FLOORBEAM WAS REPLACED IAW SRM 51-40-02-0G-0, AND DWG 143A0060 REV A.SDR SWAA2020062987781Floorbeam · crackedPASSENGER CABIN FLOORBEAM BS 540, BL 0 - LBL 24 CRACKED. THE FLOORBEAM WAS REPLACED IAW SRM 51-40-02-0G-0, AND DWG 143A0060, REV A.SDR SWAA2020062987777Angle · crackedRIGHT WING I/B LEADING EDGE. SUPPORT ANGLE FOR L/E WING TO BODY FAIRING STRUCTURE CRACKED AT STATION 500D. MARKED. / REPLACED R/H WING INBOARD L/E SUPPORT ANGLE FOR WING TO BODY FAIRING STRUCTURE AT STA 500D IAW SRM 51-40-02-0G-0 AND BOEING DRAWING 116A3110 RESDR SWAA2020062987751Floor Panel · damagedPASSENGER CABIN FLOOR PANEL 242VF TOP COVERING FIBERS PEELING. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-1, AND SRM 53-00-50-2R-0.SDR SWAA2020062990039Seat Track · wornCABIN SEAT TRACK, BS 520, LBL45 HAD WEAR ON THE UPPER AND LOWER SURFACES. REMOVED THE DAMAGE ON THE SEAT TRACK UPPER SURFACE IAW SRM 53-00-52-1A-1. REMOVED .028' MATERIAL, MAX. CLEAN UP WAS .020' AND OUT OF LIMITS IAW SRM 53-00-52-1A-1, FIG 103. REMOVED THSDR SWAA2020062990038Seat Track · gougedCABIN SEAT TRACK BS 500D+7, LBL45 WAS GOUGED ON THE UPPER SURFACE. REMOVED AND REPLACED THE SEAT TRACK, BS 500C + 10 - 521.5, LBL 45.SDR SWAA2020062987793Seat Track · corrodedPASSENGER CABIN SEAT TRACK UPPER CROWN HAD DEEP WEAR, BS 500D+13, RBL 45. REMOVED CORROSION IAW SRM 51-10-02-0G-0, ITEM 15. MATERIAL LOSS TO BE .032 ALLOWED TO REMOVE I .020', FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1, CUT OUT DAMAGED AREA FABRICATEDSDR SWAA2020062987788Floorbeam · corrodedCORROSION ON TOP OF FLOORBEAM, BS 312, LBL 20, WL 207. REMOVED THE CORROSION AND FOUND MATERIAL LOSS TO BE .047, OUT OF LIMITS IAW SRM 53-10-51-1A-1, REPAIRED THE FLOORBEAM IAW SRM 53-10-51-2R-15, STEP 4.SDR SWAA2020062987758Floor Panel · crackedPASSENGER CABIN FLOOR PANEL 242XF WAS CRACKED IN TWO PIECES. REPLACED THE FLOOR PANEL.SDR SWAA2020062987756Floor Panel · damagedPASSENGER CABIN FLOOR PANEL 242VF INSERT DAMAGED, AFT INBD EDGE. REPLACED THE FLOOR PANEL INSERT IAW SRM 53-00-50-2R-0 GENRAL REPAIR, STEP 5 (5), TAB 205, AND DRWG 147A5810-ID0350 REV -.SDR SWAA2020062987753Floor Panel · peelingPASSENGER CABIN FLOOR; PANEL 241ABF TOP COVERING FIBERS PEELING. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R- GENERAL REPAIR, AND SRM 53-00-50-2R-1, REPAIR 1.SDR SWAA2020062987752Floor Panel · peelingPASSENGER CABIN FLOOR; PANEL 241AAF TOP COVERING FIBERS PEELING. REPAIRED PASSENGER CABIN FLOOR PANEL IAW SRM 53-0-50-2R-0, GENERAL REPAIR, AND SRM 53-00-50-2R-1, REPAIR 1.SDR SWAA2021082587169Nut Plate · brokenFWD CARGO PIT FLOOR RH Z-ANGLE CAPTIVE NUTPLATE STRAP IS BROKEN AT BS 440; RBL 24; WL 156. / FWD CARGO R/H Z ANGLE NUT PLATE STRAP BROKEN AT STA 440 REMOVED BROKEN NUT PLATE STRAP IAW SRM 51-40-02-0G-0 FABRICATED NEW NUT PLATE STRAP IAW SRM 51-40-05-0G-0 SRM 5SDR SWAA2021081687146Stiffener · damagedLEFT WING DEFLECTION RIB TAB AND TRAILING EDGE PANEL STIFFENER HAVE DAMAGE FROM ATTACH BOLTS. / REPAIRED LEFT WING DEFLECTION RIB AND T/E PANEL STIFFENER IAW SRM 57-51-02-2R-1 AND SRM 57-51-02-2R-4 A55799SDR SWAA2021081387164Shield · corrodedFWD CARGO PIT FLOOR RH Z-ANGLE IS CORRODED AT BS 492 TO 500A; RBL 24; WL 156. / FWD CARGO FLOOR Z-ANGLE SHIELD IS CORRODED AT BS 492 TO BS 500A RBL 24. BLENDED AND REMOVED CORROSION ON SHIELD I/A/W SRM 51-10-02-0G-0 CHECK WITH 10X MAG. MATERIAL THICKNESS IS .0SDR SWAA2021081387172Nut Plate · brokenFWD CARGO PIT DOOR OPENING AFT BODY FRAME WEB HAS TWO BROKEN NUT PLATES AT BS 492; STR 25R. / FWD CARGO AFT FRAME -2 QTY N/PS CENTERS BROKEN STA 492 FRAME. REPLACED 2 QTY NUT PLATES AT FWD CARGO AFT FRAME STA 492 I/A/W SRM 51-40-02-0G-0.SDR SWAA2021080393119Structure · erodedVERTICAL STAB. RUDDER ARM WEIGHT EDGES ARE ERODED / REMOVED AND INSTALLED NEW VERTICAL STAB. RUDDER ARM WEIGHT IAW B737 51-21-73-370-801; CMM 55-40-09; AMM 20-50-11-910-801; SRM 51-40-02-0G-0; AMM 27-21-11-400-801 SEAL GAP CHECK GOOD ATAG: WN0643SDR SWAA2021062487155Scuff Plate · crackedAFT CARGO DOOR AFT CORNER SCUFF PLATE CRACKED / WELD REPAIR ACCOMPLISHED IN BACK SHOP ON WO: 41023-8100-0001 AND INSTALLED ON WO: 753-140-00-02Y.
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