N922WN
Service difficulty reports · 296
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 = 'N922WN' 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 = 'N922WN' 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 SWAA2021071686889Access Panel · wornR/H WING; FUEL TANK ACCESS PANEL #632FB; PANEL ATTACH RING; AREAS OF LITE FRETTING ON TOP SIDE OF MOUNT RING; AREAS MARKED IN BLACK / EVALUATED RH WING FUEL TANK ACCESS PANEL 632FB PANEL ATTACH RING FRETTING IAW B737 SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 CIRCLESDR SWAA2021071686888Access Panel · wornR/H WING; FUEL TANK ACCESS PANEL #632CB; PANEL ATTACH RING; AREAS OF LITE FRETTING ON TOP SIDE OF MOUNT RING; AREAS MARKED IN BLACK / EVALUATED RH WING FUEL TANK ACCESS PANEL 632CB PANEL ATTACH RING FRETTING IAW B737 SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 CIRCLESDR SWAA2021071686886Access Panel · corrodedL/H WING; FUEL TANK ACCESS PANEL #53LB; PANEL ATTACH RING; AREAS OF LITE FRETTING ON TOP SIDE OF MOUNT RING; AREAS MARKED IN BLACK / EVALUATED LH WING FUEL TANK ACCESS PANEL 532LB PANEL ATTACH RING FRETTING IAW B737 SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 CIRCLE SDR SWAA2021071686887Access Panel · corrodedR/H WING; FUEL TANK ACCESS PANEL #631BB; PANEL ATTACH RING; AREAS OF LITE FRETTING ON TOP SIDE OF MOUNT RING; AREAS MARKED IN BLACK / EVALUATED RH WING FUEL TANK ACCESS PANEL 631BB PANEL ATTACH RING FRETTING IAW B737 SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 CIRCLESDR SWAA2021071686885Access Panel · corrodedL/H WING; FUEL TANK ACCESS PANEL #532JB; PANEL ATTACH RING; AREAS OF LITE FRETTING ON TOP SIDE OF MOUNT RING; AREAS MARKED IN BLACK / EVALUATED LH WING FUEL ACCESS PANEL 532JB PANEL ATTACH RING FRETTING IAW B737 SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 CIRCLE H. BSDR SWAA2021071686884Access Panel · corrodedL/H WING; FUEL TANK ACCESS PANEL #532FB; PANEL ATTACH RING; AREAS OF LITE FRETTING ON TOP SIDE OF MOUNT RING; AREAS MARKED IN BLACK / EVALUATED LH WING FUEL TANK ACCESS PANEL 532FB PANEL ATTACH RING FRETTING IAW B737 SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 CIRCLESDR SWAA2021071686882Access Panel · corrodedL/H WING; FUEL TANK ACCESS PANEL #532CB; PANEL ATTACH RING; AREAS OF LITE FRETTING ON TOP SIDE OF MOUNT RING; AREAS MARKED IN BLACK / EVALUATED LH WING FUEL TANK ACCESS PANEL 532CB PANEL ATTACH RING FRETTING IAW B737 SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 DIRCLESDR SWAA2021071686880Access Panel · corrodedL/H WING; FUEL TANK ACCESS PANEL #532MB; PANEL ATTACH RING; AREAS OF LITE FRETTING ON TOP SIDE OF MOUNT RING; AREAS MARKED IN BLACK / EVALUATED LH WING FUEL ACCESS PANEL 532MB PANEL ATTACH RING FRETTING IAW B737 SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 CIRCLE H. BSDR SWAA2021071686877Access Panel · corrodedL/H WING; FUEL TANK ACCESS PANEL #532AB; PANEL ATTACH RING; AREAS OF LITE FRETTING ON TOP SIDE OF MOUNT RING; AREAS MARKE IN BKACK / EVALUATED LH WING FUEL TANK ACCESS PANEL 532AB PANEL ATTACH RING FRETTING IAW B737 SRM 57-20-01-1A-1 FIGURE 104 SHEET 7 CIRCLE SDR SWAA2021050543969Seal · crackedRH HORIZONTAL STABILIZER ROOT FRONT SPAR UPPER SLIDING SEAL IS CRACKED AT TIE BAR CORNER PLATES. / REMOVED AND REPLACED R/H HORIZONTAL UPPER SLIDER SEAL IAW B737 AMM 53-31-31-400-802.SDR SWAA2021082786854Fairing · damagedLOWER WING TO BODY FAIRING 193AL; LEFT FWD. WHEEL WELL PANEL; INFOARD FASTENER HOLE ELONGATED/WORN THROUGH COMPOSITE. / REPAIRED FASTENER HOLE I/B EDGE OF FAIRING 193AL; WORK ACCOMPLISHED ON N/R #40847-1700-0021; (Y218619)SDR SWAA2021082743721Balance Weight · corrodedRIGHT AILERON; BALANCE BAY #1 CENTER WEIGHT HAS CORROSION / REMOVED CORRODED BALANCE WEIGHT FROM RH AILERON; BALANCE BAY #1; CENTER AND REPLACED WITH NEW WEIGHT IAW SOPM 20-50-01 AND AIPC 27-11-31-02 ITEM 55. NO CHANGE IN WEIGHT. ATAG: WN1223 TW 20071 07/22/20SDR SWAA2021082743722Balance Weight · corrodedRIGHT AILERON; BALANCE BAY #2 CENTER WEIGHT HAS CORROSION / REMOVED CORRODED WEIGHT FROM RH AILERON BALANCE BAY #2 AND INSTALLED NEW WEIGHT IAW AIPC 27-11-31-02 ITEM 55 AND SOPM 20-50-01. NO CHANGE IN WEIGHT. TW 20073 ATAG UP1656SDR SWAA2021081743737Strip · crackedL/H HORIZONTAL STAB PANEL 333CB T/E FAIRING STRIP HAS SEVERAL CRACKS AT FASTENER HOLES / REMOVED AND REPLACED LH HORIZONTAL STAB PANEL 333CB T/E FAIRING STRIP IAW SRM 51-4-02-0G-0. UP1637SDR SWAA2021081743738Strip · crackedL/H HORIZONTAL STAB PANEL 333DB T/E FAIRING STRIP HAS CRACK AT FASTENER HOLE / REMOVED AND INSTALLED NEW L/H HORIZONTAL STAB PANEL 333DB T/E FAIRING STRIP I/A/W SRM 51-40-02-0G-0 AND BOEING DWG 185A1702 REV:J A-TAG# UP1636SDR SWAA2020052643806Floor Panel · damagedPANEL 231XF FIBER DAMAGE. FABRICATED AND REPLACED PNL 231XF IAW SRM 53-00-50-2R-0 REV 70. DRAW 144A5810 ID:0126 REV:-. BAC 5085 REV E; IAW ORIGINAL PNL 231XF.SDR SWAA2020052643518Intercostal · crackedAFT CARGO RT INTERCOSTAL FOUND CRACKED AT STA 727A TO 727B RBL 13. REMOVED CRACKED INTERCOSTAL AT AFT CARGO RT STA 727B TO 727A RBL 13 IAW SRM 51-40-02-0G-0. FABRICATED NEW INTERCOSTAL IN BACKSHOP ON N/R 40849/1600/0001 IAW DWG 146A7505. DRILLED AND TRIMMED ISDR SWAA2020052643720Rib · crackedRT HORIZONTAL STABILIZER LEADING EDGE PANEL 341B RIB CHORD IS CRACKED ON LOWER AFT END AT LE STA 105.26. REMOVED CRACKED RIB IN RT STAB L/E AT LE STA 105.26 AND INSTALLED RIB 186A1304-2 IAW SRM 51-40-05-0G-0 51-40-02-0G-0 STEP 4; BAC DWG 186A1001 REV.SDR SWAA2021081743423Bracket · crackedL/H KEEL BEAM AT STA 540; CROSSOVER DUCT BRACKET IS CRACKED ON FWD SIDE. / REMOVED AND INSTALLED NEW L/H KEEL BEAM AT STA 540; CROSSOVER DUCT BRACKET I/A/W SRM 51-40-02-0G-0 AND BOEING DWG #212A1101REV:- A-TAG #A13588SDR SWAA2021081743428Floorboard · pulledCABIN FLOORBOARD 231DF UPPER SURFACE HAS PULLED FIBERS. / REPLACED BY FABIRCATED CABIN FLOORBOARD 251 DF IAW B737 SRM 53-0-50-2R-0 REV 70; BAC 5085 REV E; DWG 143A5810-513 REV A AND SAMPLE. WN5879; A18238; A30438.SDR SWAA2021081743431Floorboard · pulledCABIN FLOORBOARD 231GF UPPER SURFACE HAS PULLED FIBERS. / REPLACED BY FABRICATION CABIN FLOORBOARD 231GF IAW B737 SRM 53-00-50-2R-0 REV 70; DWG 143A5810-575 REV- AND BAC5085 REV (E). WN5879 A18238 A30438 3SDR SWAA2020052643515Floorboard · damagedCABIN FLOORBOARD 231KF UPPER SURFACE HAS PULLED FIBERS. FABRICATED AND REPLACED PNL 231KF IAW SRM 53-00-50-2R-0 REV 70; BAC 5085 REV E; IAW ORIGINAL PNL 231KF SAMPLE, DRAW 143A0850 REV -.SDR SWAA2020052643422Vapor Barrier · crackedCUSTOMER REQUEST (DW) BS 663 LT SIDE VAPOR BARRIER IS CRACKED. EVALUATED DAMAGE, VAPOR BARRIERS IS REPAIRABLE IAW SRM 57-10-10-2R-2. CLEANED, PREPPED REPAIR AREA AND BONDED REPAIR ON LT STA 663 VAPOR BARRIER IAW SRM 51-70-04-2R-0 AND SRM 51-70-04-2R-10.SDR SWAA2020052643426Floorboard · damagedCABIN FLOORBOARD 231BF UPPER SURFACE HAS PULLED FIBERS. REPAIRED CABIN FLOORBOARD 231BF OF UPPER SURFACE PULLED FIBERS (AS MARKED) IAW SRM 53-00-50-2R-0 REV 70 AND SRM 53-00-50-2R-1 REV 70.SDR SWAA2020052643427Floorboard · puncturedCABIN FLOORBOARD 231FF UPPER SURFACE HAS PUNCTURE. REPAIRED CABIN FLOORBOARD 231FF UPPER SURFACE PUNCTURE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0.SDR SWAA2020052643429Floorboard · damagedCABIN FLOORBOARD 232CF UPPER SURFACE HAS PULLED FIBERS. REPAIRED CABIN FLOORBOARD 232CF OF UPPER SURFACE PULLED FIBERS (AS MARKED) WITH NO DAMAGE TO COMPOSITE SUBSTRATE IAW SRM 53-00-50-2R-0 REV 70 AND SRM 53-00-50-2R-1 REV 70.SDR SWAA2020052643447Stiffener · crackedLEFT HORIZONTAL STABILIZER RIB STAB STA 129.50, 2ND STIFFENER IS CRACKED AT LOWER END. CUT OUT DAMAGED AREA LT HORIZONTAL STAB. RIB STA 129.50, 2ND STIFFENER AT LOWER END IAW SRM 55-10-09-2R-4 REPAIR 4. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 55-10-09-SDR SWAA2020052643448Stiffener · crackedLEFT HORIZONTAL STABILIZER RIB STAB STA 129.50, 4TH STIFFENER IS CRACKED AT LOWER END. CUT OUT DAMAGE AREA LT HORIZONTAL STABILIZER RIB STA 129.50 4TH STIFFENER LOWER END IAW SRM 55-10-09-2R-4 REPAIR 4. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 55-10-09-SDR SWAA2020052643450Stiffener · crackedRIGHT HORIZONTAL STAB INSPAR RIB ASSY 4 (STAB STA 120.30) STIFFENER 2 IS CRACKED NEAR LOWER SKIN. CUT OUT DAMAGED AREA AT RT HORIZONTAL STAB RIB ASSY 4, STA 120.30, STIFFENER 2 NEAR LOWER SKIN IAW SRM 55-10-09-2R-4 REPAIR 4. FABRICATED REPAIR PARTS AND INSTALSDR SWAA2020052643451Stiffener · crackedRIGHT HORIZONTAL STAB INSPAR RIB ASSY 4 (STAB STA 120.30) STIFFENER 3 IS CRACKED NEAR LOWER SKIN. CUTOUT DAMAGE AREA AT RIGHT HORIZONTAL STAB RIB 4 STA 120.30 STIFFNER 3 NEAR LOWER SKIN IAW SRM 55-10-09-2R-5 REPAIR 5. FABRICATED REPAIR PARTS AND INSTALLED IAWSDR SWAA2020052643516Floorboard · damagedCABIN FLOORBOARD 231UF UPPER SURFACE HAS PULLED FIBERS. REPAIRED PASSENGER CABIN FLOORBOARD 231UF UPPER SURFACE IAW SRM 53-00-50-2R-0 GENERAL REV 70; B737-SRM 53-00-50-2R-1 REV 70.SDR SWAA2020052643452Intercostal · corrodedAFT CARGO; INTERCOSTAL UNDER ZEE PLATE AT STATION 767; WL 157 AND RBL 20 HAS CORROSION AROUND FASTENER HOLES. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS. ORIG MATERIAL 0.032'; LOSS 0.005'; REMAINING MATERIAL 0.027'. OUT OF LIMITS IAW SRM 53-00-53-1A-2SDR SWAA2021082743072Support Bracket · crackedLEFT WING FIXED TRAILING EDGE O/B OF #6 SPOILER; AFT SUPPORT BRACKET; O/B UPPER CORNER IS CRACKED. / REPLACED LEFT WING FIXED TRAILING EDGE AFT SUPPORT BRACKET O/B OF #6 SPOILER IAW SRM 51-40-02-0G-0 AND BOEING DWG 115A2512 REV- ATAG A49092SDR SWAA2021082743097Balance Weight · corrodedLEFT WING AILERON I/B BAY; BALANCE WEIGHTS HAVE CORROSION. / REMOVED AND REPLACED LEFT WING AILERON I/B BAY FIXED WEIGHTS 113A7183-5 QTY 4 I/A/W B737-700 SRM 51-60-01-0G-0 STEP 4A4 A TAG WN0971 UP1634 UP1631SDR SWAA2021082743098Balance Weight · corrodedLEFT WING AILERON BALANCE BAY #4; WEIGHTS HAVE CORROSION. / REMOVED AND REPLACED LEFT WING AILERON BALANCE #4 WEIGHTS IAW SOPM 20-50-01; SRM 51-40-02-0G-0; AMM 20-50-11-910-801 TABLE 215 NO CHANGE IN WEIGHT TW 20073 DUE 06/03/20 A TAG: UP1649 UP1669SDR SWAA2021082743099Balance Weight · corrodedLEFT WING AILERON #2 BALANCE BAY; 2EA. BALANCE WEIGHTS HAVE CORROSION. / REMOVED AND INSTALLED 2EA NEW BALANCE WEIGHTS IN L/H WING AILERON BALANCE BAY #2 IAW B737 20-50-11-910-801 TABLE 215; SRM 51-40-02-0G-0; SOPM 20-50-01. NO CHANGE IN WEIGHT A TAG UP1648 TWSDR SWAA2021082743102Balance Weight · corrodedLEFT WING AILERON BALANCE BAY #1; 1EA. WEIGHTS HAS CORROSION. / REMOVED AND REPLACED LEFT WING AILERON BALANCE WEIGHT 1 EA. REF B737 SOPM 20-56-01 & AIPC 27-11-31-02 ITEM 55; NO WEIGHT CHANGE. A TAG WN1039 TW DUE 06/31/20 20073.SDR SWAA2021082303076Splice · brokenRT WING INBD OF LANDING LIGHT WING TO BODY SPLICE BROKEN / REMOVED ADN REPLACED FRAME SPLICE ON RT WING INBD OF LANDING LIGHT IAW SRM 51-40-02-0G-0 BOEING DWG 116A3110; 149A7101 AND 116A3010. A TAG A49468 PN 116A3118010.SDR SWAA2021071443109Floorbeam · crackedCABIN FLOOR STA 540 PANEL BREAK ASSY BL 0 TO LBL 24.75 IS CRACKED AT INBOARD END / REMOVED AND REPLACED PANEL BREAK ASSY BL 0 TO LBL 29.75 IAW SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 AND BOEING DWG-143A0060 ID 36 REV ASDR SWAA2020052643064Intercostal · crackedCABIN FLOOR STRUCTURE STA 312 TO 328, RBL 31 INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL IN CABIN FLOOR STRUCTURE STA 312 TO 328, RBL IAW DWG 141A5400 REV- AND SRM 51-40-02-0G-0. APPLIED CIC IAW AMM 51-21-91-620-802.SDR SWAA2020052643067Intercostal · crackedCABIN FLOOR STRUCTURE STA 344 TO 360, BL 0 HAS INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL STA 344 TO 360, BL 0 IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0 AND DWG 141A5400 ID 32 REV:-. P/N 141A5410-23.SDR SWAA2020052643071Intercostal · crackedCABIN FLOOR STRUCTURE STATION 312 TO 328, LBL 45 HAS INTERCOSTAL CRACKED. REMOVED AND REPLACED CABIN FLOOR STRUCTURE AT STA 312 TO 328, LBL 45 INTERCOSTAL IAW DWG 141A5400 REV- AND B737SRM 51-40-02-0G-0.SDR SWAA2020052643113Cargo Track · corrodedAFT CARGO COMPARTMENT, STA 927+18, RBL13, WL 177 TRACK HAS CORROSION AROUND FASTENER HOLE. REMOVED CORROSION AT AFT CARGO STA 927+18, RBL13, WL177 TRACK IAW SRM 51-10-02-0G-0. VERIFIED MATERIAL LOSS ORIGINAL .070 REMOVED, .015 REMAIN, .055 ALLOWABLE, 10% MAXSDR SWAA2020052643083Crease Beam · corrodedPASSENGER CABIN FLOOR; AFT GALLEY DOOR SURROUND CREASE BEAM OUTER ANGLE CORRODED STA.947-987 WL208. REMOVED CORROSION FROM CABIN FLOOR AFT GALLEY DOOR SURROUND CREASE BEAM OUTER ANGLE STA 947 - 987 WL208 RBL 66 IAW SRM 51-10-02-0G-0 AND INSPECTED W/ 10X MAG GSDR SWAA2020052643087Crease Beam · corrodedPASSENGER CABIN FLOOR, AFT ENTRY DOOR WAY CREASE BEAM STA 947-987 CORRODED AROUND FASTENER HOLES WL208 LBL 52. REMOVED CORROSION FROM AFT ENTRY DOOR WAY CREASE BEAM AT STA 947-987. ORIGINAL MATERIAL .080 LOSS OF .012 WITH .068 REMAINING IS OUT OF LIMITS IAW SDR SWAA2020052643415Crease Beam · corrodedCABIN FLOOR RIGHT CREASE BEAM WEB STA 727D+6' RBL 68.5 WL 208 LOWER SURFACE HAS CORROSION JUST OUTBOARD OF LIGHTNING HOLE. BLENDED CORROSION ON RT CREASE BEAM WEB PN 146A5925-24 AT STA 727D+6' RBL 68.5 WL208. LOWER SURFACE ORIGINAL THICKNESS .036', LOSS .005'SDR SWAA2020052643066Floorboard · damagedCABIN FLOOR FLOORBOARD 222BF UPPER SURFACE HAS PULLED FIBERS. BONDED UPPER SURFACE PLY ON FLOORBOARD 222 BF IAW SRM 53-00-50-2R-1 PG'S 1AND 2 STEPS 3 (A-M).SDR SWAA2020052643084Floorbeam · corrodedPASSENGER CABIN FLOOR AFT GALLEY DOOR WAY STA 987 FLOORBEAM CORRODED AROUND FASTENER HOLE WL 208 RBL 0 - 45. REMOVED CORROSION FROM CABIN FLOOR AFT GALLEY DOORWAY STA 987 FLOORBEAM WL 208 AROUND FASTENER HOLE IAW SRM 51-10-02-0G-0 AND INSPECTED W/ 10X MAG GLASDR SWAA2020052643107Intercostal · crackedBS 500D + 6'; STR-27R; WL 156; INTERCOSTAL FOR CABIN AIR RECIRC FAN COLLOCTOR(R2D2). FOUND CRACKED NEAR NUT PLATE AND INNER RADIUS / REMOVED AND REPLACED INTERCOSTAL AT STA 500D +6' STR 27R WL156 IAW SRM 51-40-02-0G-0 AND DWG 143A9805 SHEET 11.SDR SWAA2020052643070Angle · crackedCABIN FLOOR STRUCTURE L-1 DOOR Z-ANGLE AT STA 302 LBL 59 CRACKED. REMOVED AND REPLACED CABIN FLOOR STRUCTURE L-1 DOOR Z-ANGLE (CREASE BEAM) P/N 6540004-1073 IAW B737 SRM 51-40-02-0G-0 AND DWG 8110 REV.-
Back to N922WN