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 SWAA2024052478157Floor Panel · crackedAFT WET AREA PANEL 241ADF AFT OUTBOARD EDGE IS CRACKED..<[01] RECIEVED NEW FLOOR PANEL 241ADF PO# 2059779 REF TASK CARD'TTG8Q00SGWZF' FOR INSTALLATION;[02] VERIFIED STEP 1.SDR SWAA2024052477964Floorbeam · corrodedAFT WET AREA FLOOR BEAM SUPPORT STA 986.5 RBL 35 TO RBL 45 HAS THREE SPOTS OF CORROSION EVIDENCE.<[01] ACCOMPLISHED REPAIR ON FLOOR BEAM STA 986.5 RBL 45 REF SRM 53-70-51-2R-6; ALTERNATIVE 4;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2024052478165Seat Track · corrodedCORROSION AT CABIN SEAT TRACK RBL 45.5 CROWN INNER AND UPPER SURFACE STA 767.<[01] SEE NEW FAULT TTG8Q00SWZZP / TTG8Q00SX001.SDR SWAA2024052477839Gusset · crackedFWD CARGO STA 500D AT S-19L GUSSET BRACKET CRACK.<[01] REMOVED AND REPLACED NEW GUSSET AT FWD CARGO COMPT FROM STA 500D AT S-19L; PER REFR SRM 51-40-02-0G-0.;[02] CORRECTION: REMOVED AND REPLACED NEW GUSSET AT FWD CARGO COMPT FROM STA 500D AT S-19L; PER REFR SSDR SWAA2024052477840Gusset · crackedFWD CARGO STA 500D AT S-24L GUSSET BRACKET CRACK.<[01] REMOVED AND REPLACED NEW GUSSET AT FWD CARGO COMPT FROM STA 500D AT S-24L PER REF SRM 51-40-02-0G-0.;[02] CORRECTION: REMOVED AND REPLACED NEW GUSSET AT FWD CARGO COMPT FROM STA 500D AT S-24L PER REF SRM 5SDR SWAA2024052477585Stiffener · crackedLH HORIZONTAL STABILIZER RIB # 9 STIFFENER # 3 CRACK.<[01] ACCOMPLISHED REAPIR AT LH HORIZONTAL STABILIZER RIB # 9 COMMON TO STIFFENER # 3 REF SRM 55-10-09-2R-4;[02] RII VERIFIED CORRECTIVE ACTION.SDR SWAA2024052477056Skin · delaminatedLH INB MAIN FLAP AFT EDGE OUTB SECTION 24 INCH LENGHT DELAMINATION.<[01] DUE TO DAMAGE FOUND OUT OF ALLOWABLE DAMAGE LIMITS; REMOVED AND INSTALLED A SERVICIABLE TE WEDGE ASSY AT LT I/B MAIN FLAP AS PER B737-700 SRM 51-40-02-0G-0 PARAGRAPH 9 AND BOEING DWG 113ASDR SWAA2024052378156Vapor Barrier · crackedRIGHT VAPOR BARRIER CRACKED AT APPROX RBL40 UPPER AREA.<[01] APPLIED REPAIR AT R/H VAPOR BARRIER STA 663 ON FWD AND AFT SIDE AS PER B737 SRM 57-10-10-2R-2 AND B737 SRM 51-70-04-2R-10 PARAG 4-F AND B737 SRM 51-70-04-2R-0 PARAG 4-N-2; MATERIAL USED: RESIN EY 380SDR SWAA2024052383782Deflector · damagedCHECK L/H WING DEFLECTOR RIB TO DEFLECTOR PANEL ATTACH SERRATED PLATES FOR CONDITION AND ELONGATED HOLES.<[01] VISUAL INSPECTION ACCOMPLISHED AT LT WING TE DEFLECTION RIB TO DEFLECTOR PANEL ATTACH SERRATED PLATES REF. SRM 51-10-04-0G-0 AND AMM 57-50-01-820-801SDR SWAA2024020749262Handle · looseFLIGHT ATTENDANTS REPORT FORWARD ENTRY DOOR HANDLE LOOSE<[01] TIGHTENED FE DOOR HANDLE REF MM 52-11-00SDR SWAA2024011140001Skirt · out of positionF/A REPORTED SLIDE SKIRT STICK OUT TOO FAR<[01] REPOSITION SKIRT BACK TO CASE;DID NOT OPEN CASE PER AM 27-66-00SDR SWAA2023113025476Panel · delaminated193 B PANEL HAS DELAM AND CHIP OUT AREA MISSING ON INNER MATERIAL EDGE ON THE SAME FORWARD LEFT HAND CORNER LEADING EDGE.<[01] VERIFIED REPLACEMENT OF 193 B PANEL IAW SRM 53-40-70.;[02] DRILLED AND INSTALLED NEW 193B PANEL; REF. SRM 51-40-02.SDR SWAA2023102312634Battery Pack · failedM1675 FAILED CAPACITY CHECK<[01] R/R 1675 BATTERY PACK PER AMM 33-51-06SDR SWAA2023102312636Battery · failedM1668 FAILED CAPACITY CHECK<[01] R/R M1668 EMERGENCY BATTERY PER AMM 33-51-06SDR SWAA2023102312631Girt Bar · out of adjustAFT ENTRY DOOR GIRT HANGING LOW<[01] REPACKED GIRT. REF TTG8Q00NV2AP FOR WORK PERFORMED.;[02] REPACKED GIRT. REF TTG8Q00NV2AP AND MT 725-61-06 FOR WORK PERFORMED.;[03] C/WSDR SWAA2023091198546Battery Pack · inoperativeOVER WING EMERGENCY LIGHTS INOP R/H<[01] R/R OVER WING R/H EMERGENCY LIGHT BATTERY PACK (M1669) REF AMM 33-51-06 OPS CHK GOODSDR SWAA2023042830578Indication Sys · faulty#1 ENGINE FUEL FLOW INDICATOR ERRATIC #1 ENGINE FUEL FLOW INDICATOR ERRATIC. REMOVED AND REPLACED #1 ENGINE FUEL FLOW TRANSMITTER PER AMM 73-31-01 OPS AND LEAK CHECK GOOD THIS CLEARS MEL 73-5-01SDR SWAA2023031313729Battery Pack · failedR/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.SDR SWAA2023031313728Battery Pack · failedL/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.SDR SWAA2023031313730Battery Pack · failedEMERGENCY LIGHTING BATTERY PACK AT L/H OVER WING EXIT FAILED CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.SDR SWAA2022122684891Sensor · faultedTRAILING EDGE FLAP ASYMMETRY OCCURED WHEN CONFIGURING FOR APPROACH. FLAPS STOPPED AT LESS THAN POSITION 1. PERFORMED QRH PROCEDURE FOR TRAILING EDGE ASYMMETRY AND TRAILING EDGE FLAPS UP LANDING. USED MAX AUTOBRAKE SETTING WITH 30 MINBRAKE COOLING PERIOD. BRAKESDR SWAA2022111771639Flap · dislodgedR1 DOOR SLIDE DRAGS ON FLOOR. SECURED R1 DOOR SLIDE GIRT BAR FLAP TO VELCRO STRIPS ON SLIDE COMPARTMENT IAW SIP.SDR SWAA2022080538803Bracket · looseFWD SERVICE DOOR GIRT BAR BRACKET LOOSE ON RIGHT SIDE / [01] INSTALLED RIVET ON FWD SERVICE DOOR GIRT BAR BRACKET PER ARM 51-40-02 & MT 725-61-06-FS;[02] INSTALLED RIVET ON FWD SERVICE DOOR GIRT BAR BRACKET PER SRM 51-40-02SDR SWAA2022051206370Handle · loosePAX CABIN L1 DOOR UPPER CLOSE ASSIST HANDLE LOOSE / [01] SECURED PAX CABIN L1 DOOR UPPER CLOSE ASSIST HANDLE AS PER B737 SRM 51-40-02-0G-0<BR>WORKED ACCOMPLISHED BY IVET DENIS EMP #32092;[02] VERIFIED 1SDR SWAA2022051206364Power Supply · inoperativeEMERGENCY LIGHTS INOP FOR BATTERY CHARGER M1669 & M1674 / [01] REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK AT POSITION M1674 AND TEST OF POWER SUPPLY AND BATTERY PACK AT POSITION M1674 AND M1669 FOUND NORMAL REF AMM 33-51-06-960-805/806;[02] VERIFIED STSDR SWAA2022051204731Strip · corrodedCORROSION' FWD CARGO COMPARTMENT L/H CAP STRIP MID SECTION SPOTS OF CORROSION( 19 EA) / [01] REMOVED CORROSION AT FWD CARGO COMPARTMENT L/H CAP STRIP MID SECTION AS PER B737-700 SRM 51-10-02-0G-0.;[02] EVALUATED AREA AT FWD CARGO COMP. L/H CAP STRIP MID SECTIOSDR SWAA2022051204733Strip · corrodedCORROSION' FWD CARGO COMPARTMENT R/H FWD CAP STRIP SPOTS OF CORROSION ( 6 EA) / [01] REMOVED CORROSION AT FWD CARGO COMPARTMENT R/H FWD CAP STRIP AS PER B737-700 SRM 51-10-02-0G-0.;[02] EVALUATED AREA AT FWD CARGO COMP. R/H CAP STRIP FWD SECTION; CORROSION PASSDR SWAA2022051204729Strip · corroded'CORROSION' FWD CARGO COMPARTMENT L/H SIDE AFT CAP STRIP HAS SPOTS OF CORROSION (10 EA) / [01] REMOVED CORROSION AT FWD CARGO COMPARTMENT L/H SIDE AFT CAP STRIP PER B737-700 SRM 51-10-02-0G-0.;[02] EVALUATED AREA AT FWD CARGO COMP. L/H SIDE AFT CAP STRIP; CORRSDR SWAA2022051201474Shield · corrodedAFT CARGO FWD SHIELD WITH CORROSION SPOTS / [01] REMOVED LIGHT CORROSION AS PER REF B737-700 SRM 51-10-02-0G-0;[02] VERIFIED 1;[03] EVALUATED AREA: ORIGINAL THICKNESS 0.050' . MATERIAL REMOVED 0.001' . REMAINING THICKNESS 0.049' FOUND TO BE WITHIN LIMITS AS PESDR SWAA2022051201476Splice Strap · corrodedAFT CARGO SPLICE STRAP #2 WITH SEVERAL POTS OF CORROSION / [01] REMOVED CORROSION AT AFT CARGO SPLICE #2 AS PER B737-700 SRM 51-10-02-0G;[02] EVALUATED AREA; CORROSION PASS THRU 100% MATERIAL LOST FOUND TO BE OUT OF LIMITS PER REF B737-700 SRM 53-00-53-1A-2. RSDR SWAA2022051800456Service Door · corroded'CORROSION' TOILET SERVICE DOOR PAN CORROSION AT AFT LWR EDGE / [01] REMOVED LIGHT CORROSION AT TOILET SERVICE DOOR PAN AFT LOWER EDGE. MATERIAL ORIGINAL 0.100'. MATERIAL REMOVED 0.001. MATERIL REMAIN 0.099. TOOL USED RPT.583848 ID#453020 CAL DUE. 12/17/2022 ISDR SWAA2022051797739Sign · missingCENTER R/H EMERGENCY EXIT SIGN MISSING / [01] REPLACED NEW CENTER R/H EXIT SING AS PER B737-700 AMM 33-51-01-960-801;[02] OPS CHECK OK;[03] VERIFIED; STEP # 1 AND 2.SDR SWAA2022051797740Sign · brokenR/H 2 EMERGENCY EXIT SIGN BROKEN ONLY LEN COVER FOR EMERGENCY EXIT SIGN BROKEN. REPLACE LEN COVER / [01] REMOVED AND REPLACED R/H 2 EMERGENCY EXIT SIGN AS PER B 737-700 AMM 33-51-01-960-801;[02] CORRECTION STEP 1.REMOVED AND REPLACED R/H 2 EMERGENCY EXIT SIGN SDR SWAA2022051298074Seat Track · damagedMAIN CABIN STA 723 RBL 24.75 SEAT TRACK MISSING PART / [01] EWIS PROTECTION AT STA.537.45 TO STA. 727B RBL. 24.75 AS PER B-737-700 AMM.20-60-07-913-801;[02] TRIMED THE DAMAGED SECTION OF THE SEAT TRACK AT STA 717 AND EXTENDED THE CUTOUT IN THE UPPER CHORD OF TSDR SWAA2022051897335Skin · crackedCRACK FOUND AT LH HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90; 17' FROM FRONT SPAR I/B ROW. CRACK LENGTH 1'. CRACK FOUND AT LH HORIONTAL STABILIER LOWER SKIN STAB STA 193.90 17' FROM FRONT SPAR I/B ROW. CRACK LENGTH 1'. / LOCATED AND DRILLED THE REPAIR HOSDR SWAA2022051897463Rib · crackedLT HORIZONTAL STABILIZER #4 RIB STIFFENER # 2 CRACKED / CUT AND REMOVED THE DAMAGE FROM THE WEB AT HORIZONTAL STABILIZER # 4 RIB STIFFENER #2 IN IAW SRM 51-10-02-0G-0 AND 55-10-09-2R-4 LOCATED AND DRILLED REPAIR PARTS PER B737-700 SRM 55-10-09-2R-4 REPAIR 4 ANSDR SWAA2022051897461Rib · crackedLT HORIZONTAL STABILIZER #4 RIB STIFFENER # 3 CRACKED. REMOVED DAMAGE AT LT HORIZONTAL STABILIZER #4 RIB STIFFENER #3 IAW SRM 51-10-02-0G-0 AND SRM 55-10-09-2R-4. VERIFIED STEP 1;PERFORMED HFEC INSP. ON RIB#4 STIFFENER #3 WEB IAW B737 NDT PART 6; 51-00-00; PROSDR SWAA2022051897462Rib · crackedLT HORIZONTAL STABILIZER #4 RIB STIFFENER # 4 CRACKED. REMOVED DAMAGE AT LT HORIZONTAL STABILIZER #4 RIB STIFFENER #4 IAW SRM 51-10-02-0G-0 AND SRM 55-10-09-2R-4. PERFORMED HFEC INSP. ON RIB#4 STIFFENER #2 WEB IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. CRACKSDR SWAA2022051297460Vapor Barrier · crackedL/H VAPOR BARRIER CRACKED THROUGH / [01] MEASUREMENT;[02] PREFERMENT VISUAL INSPECTION AND TAP TEST FOUND CRACK SIZE 15'' AND CONTAMINATION AT L\H VAPOR BARRIER PER B737NTM PART 1 51-05-01;[03] APPLIED DRY OUT AT VAPOR BARRIER ON DAMAGED AREA PER B737 SRM 51-7SDR SWAA2021121350991Vapor Barrier · crackedSUPPLEMENTAL INFORMATION: VAPOR BARRIER CRACKED IN LEFT MAIN WHEEL WELL BELOW ?A? HYD MODULE APPROX. 6 INCHES LONG. ; / [01] C/W INTERIM REPAIR TO VAPOR BARRIER 6IN CRACK ON LEFT MAIN WHEEL WELL BELOW A HYD MODULE REF SRM 57-10-10.; [02] CHANGE SELECT REFERANCSDR SWAA2021112346642Slide · lowSUPPLEMENTAL INFORMATION: R1 FORWARD SERVICE DOOR SLIDE GAUGE SHOWS LOW PSI ; / [01] REMOIVED AND REPLACED FWD SVC DOOR SLIDE IAW AMM 25-66-01 MT 725-61-06SDR SWAA2021101829984Sign · missingSUPPLEMENTAL INFORMATION: FWD ENTRY DOOR EXIT SIGN MISSING. LIGHTS OPERATE NORMALLY. ; / [01] INSTALLED AS PER AMM 33-51-02SDR SWAA2021100626593None · flamed outAPPROXIMATELY ONE MINUTE AFTER SHUTDOWN, FLAMES WERE SEEN FROM THE NUMBER 2 ENGINE. THE FLAMES WENT AWAY AFTER A FEW SECONDS AND NO ABNORMAL INDICATIONS WERE NOTED. / PERFORMED FIM TASK 671-05 TASK 811. NO DEFECTS FOUND.SDR SWAA2020111832846Window · out of positionCAPTAIN SIDE WINDOW (L2) CAME OFF TRACK ON TAKEOFF TOWER DECLARED EMERGENCY. R & R LT SLIDING WINDOW, IAW M/T 756-12-11 RAR NR 79280 LT PN OFF:141A4810-3EFB1025 SN OFF:YA184 PN ON:141A4810-24EFB1025 SN ON:WN0232.SDR SWAA2020062994020Sign · damagedPASSENGER CABIN, AFT LAVATORY EMERGENCY LIGHTED SIGN NEAR THE L2 DOOR WAS DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHTED SIGN IAW AMM 33-51-01-960-802. OPS CHECKED GOOD IAW AMM 33-51-01-960-802.SDR SWAA2020062989859Floorboard · damagedPASSENGER CABIN AFT WET AREA FLOORBOARD 242UF HAD PEELING FIBERS ON THE UPPER SURFACE. REPAIRED THE FLOORBOARD IAW SRM 53-00-50-2R-0, GENERAL REPAIR, AND SRM 53-00-50-2R-1, REPAIR 1.SDR SWAA2020062989500Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT, BS 520 - 540, BL 0 WAS CRACKED. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02-0G-0, AND DWG 143A0060 REV A.SDR SWAA2020062989009Floor Panel · puncturedPASSENGER CABIN AFT WET AREA FLOOR PANEL 241ADF HAD TWO PUNCTURES AT FWD SIDE NEXT TO INSERTS. REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R-0, GENERAL REPAIR, AND SRM 53-00-50-2R-1, REPAIR 1.SDR SWAA2020062988382Stub Frame · corrodedE/E COMPARTMENT BS 319, STRINGER 23L, STUB FRAME FWD LOWER END HAD CORROSION. REMOVED CORROSION, ORIG 'T' .040', REMAINING .033', LOSS OF .007' . FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED THE STUB FRAME. APPLIED CIC TO AREA IAW SRM 51-10-02-0G-0; 53-SDR SWAA2020062988383Stub Frame · corrodedE/E COMPARTMENT STA 319 S-23L L-CHORD HAS A SPOT OF CORROSION AT FWD SIDE OF STUB FRAME. REMOVED CORROSION FROM STR23L CHORD PN 141A8240-37 FOUND ORIG T .100' LOSS .042' REMAINING .058' TO BE OUT OF LIMITS IAW SRM 53-20-15-1A-1 REPAIRED CHORD IAW EA 200428 R
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