N262WN
Service difficulty reports · 272
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 = 'N262WN' 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 = 'N262WN' 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 SWAA2018100925808Threshold · corrodedFORWARD CARGO BAY DOOR CUTOUT LOWER MAIN SILL THRESHOLD WEB ASSEMBLY CORRODED BETWEEN BS 440 TO BS 492, RBL 26. R&R WEB IAW SRM AND DWG.SDR SWAA2018101525989Door Sill · crackedL1 DOOR MOPSILL CRACKED AT BS 303, LBL 50. R&R MOPSILL IAW DWG AND SRM.SDR SWAA2018101525955Mount Bracket · corrodedL1 DOOR GIRT BAR MOUNT BRACKET CORRODED AT BS 312, LBL 59. R&R BRACKET IAW DWG AND SRM.SDR SWAA2018101525954Bracket · corrodedL1 DOOR GIRT BAR MOUNT BRACKET CORRODED AT BS 328, LBL 60. R&R BRACKET IAW DWG AND SRM.SDR SWAA2018100925795Floor Support · crackedFLOOR SUPPORT CRACKED BETWEEN BS 277 TO BS 294, BL 0. R&R SUPPORT IAW SRM AND DWG.SDR SWAA2018100925794Floor Support · crackedFLOOR SUPPORT CRACKED BETWEEN BS 312 TO BS 328, LBL 45. R&R SUPPORT IAW SRM AND DWG.SDR SWAA2018100925793Floor Support · crackedFLOOR SUPPORT CRACKED BETWEEN BS 312 TO BS 328, RBL 31. R&R SUPPORT IAW SRM AND DWG.SDR SWAA2022022319915Floor Panel · pulledSUPPLEMENTAL INFORMATION: AFT FLOOR PANEL 242TF UPPER SKIN HAS PULLED STRANDS ALONG AFT EDGE. (MARKED) / REPAIRED PULLED STRANDS DAMAGE ALONG AFT EDGE UPPER SKIN AND ADDITIONAL EDGE DAMAGE FOUND ON AFT FLOOR PANEL 242YF IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2SDR SWAA2022022319911Floor Panel · damagedSUPPLEMENTAL INFORMATION: AFT FLOOR PANEL 241AEF FWD EDGE OF LARGE CUT-OUT IS SOFT. (MARKED) / REPAIRED SOFT FWD EDGE OF LARGE CUTOUT AND ADDITIONAL EDGE DAMAGE ON AFT FLOOR PANEL 241AEF IAW SRM 53-00-50-2R-4 AND SRM 53-00-50-2R-1.SDR SWAA2022022319910Floor Panel · pulledSUPPLEMENTAL INFORMATION: AFT FLOOR PANEL 241ADF UPPER SKIN HAS PULLED STRANDS. (MARKED) / AFT FLOOR PANEL 241ADF WITH PULLED STRANDS HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1. 57543U 28.SEP.18.SDR SWAA2022022319909Floor Panel · pulledSUPPLEMENTAL INFORMATION: AFT FLOOR PANEL 241ACF UPPER SKIN HAS PULLED STRANDS. (MARKED) / REPAIRED PULLED STRANDS OF AFT FLOOR PANEL 241ACF IAW SRM 53-00-50-2R-1. 59175U 09-27-18.SDR SWAA2022022319908Floor Panel · pulledSUPPLEMENTAL INFORMATION: AFT FLOOR PANEL 241ABF UPPER SKIN HAS PULLED STRANDS. (MARKED) / AFT FLOOR PANEL 241ABF WITH PULLED STRANDS HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1. 57543U 28.SEP.18.SDR SWAA2022022319907Floor Panel · pulledSUPPLEMENTAL INFORMATION: AFT FLOOR PANEL 241AAF UPPER SKIN HAS PULLED STRANDS. (MARKED) / DUE TO THE EXTENT OF DAMAGE TO THE UPPER SKIN OF AFT FLOOR PANEL 241AAF; FABRICATED NEW PANEL USING BMS 4-17 TY 6 LOT # 1337939-1; INSTALLED INSERTS USING BMS 5-107 LOT SDR SWAA2022022319906Floor Panel · pulledSUPPLEMENTAL INFORMATION: FWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS. / FWD FLOOR PANEL 222DF WITH AREAS OF PULLED STRANDS ON UPPER SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE.SDR SWAA2022022319905Floor Panel · pulledSUPPLEMENTAL INFORMATION: FWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS. / FWD FLOOR PANEL 222CF WITH AREAS OF PULLED STRANDS ON UPPER SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE.SDR SWAA2022022319902Floor Panel · pulledFWD FLOOR PANEL 222AF UPPER SKIN HAS AREAS OF PULLED STRANDS. / FWD FLOOR PANEL 222AF WITH AREAS OF PULLED STRANDS ON UPPER SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE.SDR SWAA2022022319904Floor Panel · pulledFWD FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS. / DUE TO THE EXTENT OF DAMAGE TO UPPER SKIN ON FWD FLOOR PANEL 222BF; REPLACED PANEL WITH NEW PANEL IAW AIPC 53-21-00-50D ITEM 96 AND SRM 51-10-02-0G-0 PARA 9. 57066U 9/24/18SDR SWAA2022022319916Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS PULLED STRANDS ALONG FWD EDGE. (MARKED) / REPAIRED PULLED STRANDS DAMAGE ALONG FWD EDGE UPPER SKIN OF AFT FLOOR PANEL 242UF IAW SRM 53-00-50-2R-1.SDR SWAA2022022319900Floor Panel · pulledFWD FLOOR PANEL 221EF UPPER SKIN HAS PULLED STRANDS. (MARKED) / REPAIRED UPPER SKIN DAMAGE ON FWD FLOOR PANEL 221EF IAW SRM 53-00-50-2R-1. 59049U 9-28-18SDR SWAA2022021719898Floor Panel · pulledFWD FLOOR PANEL 221CF UPPER SKIN HAS PULLED STRANDS (MARKED) AND DAMAGED INSERTS. / REPAIRED UPPER SKIN ON FWD FLOOR PANEL 221CF AND REPLACED DAMAGED INSERTS IAW SRM 53-00-50-2R-1 AND BOEING DRAWING 141A5810 7062U 9-29-18SDR SWAA2022022219847Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 242DF IS DELAMINATED AT AFT INBOARD CORNER. / DUE TO THE EXTENT OF DELAMINATION AT AFT I/B CORNER OF PASSENGER CABIN FLOOR PANEL 242DF; FABRICATED NEW PANEL USING BMS 4-23TY2 LOT # 1339310-1 AND INSTALLED INSERTS USING BMS 5-107 LOTSDR SWAA2022022219889Seal · crackedLT HORIZ. STAB FWD UPPER SLIDE SEAL IS CRACKED. / REMOVED AND REPLACED L/HORIZONTAL STAB UPPER SLIDE SEAL IAW AMM 53-31-31-400-801; AMM 53-31-31-000-801 AND SRM 51-40-02-0G-0 55916U 22SEP18 FASTENERS USED FROM IPC 53-31-31-03 55916U 22SEP18SDR SWAA2022022219890Seal · crackedRT HORIZ. STAB FWD UPPER SLIDE SEAL IS CRACKED. / REMOVED AND REPLACED R/HORIZONTAL STAB UPPER SLIDE SEAL IAW AMM 53-31-31-000-801; AND AMM 53-31-31-400-801; AND SRM 51-40-02-0G-0 FASTENERS USED FROM IPC 53-31-31-03 55916U 22SEP18SDR SWAA2022022219891Seal · crackedRT HORIZ. STAB FWD LWR SLIDE SEAL IS CRACKED. / REMOVED CRACKED SLIDE SEAL AND INSTALLED NEW SLIDE SEAL ON R/HORIZONTAL FWD LOWER IAW AMM 53-31-31-000-803 4.E. AND AMM 53-31-31-400-803 C.-D. 55916U 26SEP18SDR SWAA2018100925843Stiffener · crackedLT HORIZONTAL STABILIZER LEADING EDGE STA 123.85 RIB 3RD, STIFFENER CRACKED. REPAIRED STIFFENER PER SRM.SDR SWAA2018100925842Stiffener · crackedLT HORIZONTAL STABILIZER LEADING EDGE STA 123.85 RIB 4TH, STIFFENER CRACKED. REPAIRED STIFFENER PER SRM.SDR SWAA2018100925786Stiffener · crackedLT HORIZONTAL STABILIZER LEADING EDGE STA 123.85 RIB 2ND, STIFFENER CRACKED. REPAIRED STIFFENER PER SRM.SDR SWAA2018101826057Lens · crackedFORWARD CARGO BAY 3RD LIGHT FROM THE FORWARD BULKHEAD LENS CRACKED. R&R LENS PER AMM.SDR SWAA2022021819799Support Web · crackedRIGHT WING FIXED TRAILING EDGE OUTBOARD OF #6 CANOE HAS A 1' CRACK LOCATED ON SUPPORT WEB. / REMOVED AND REPLACED SUPPORT WEB REF SRM 51-40-02.SDR SWAA2022021819790Scuff Plate · crackedFWD CARGO DOOR SCUFF PLATE HAS CRACK. CRACK 3' AFT OF FORWARD EDGE OF SCUFF PLATE. MEASURES APPROXIMATELY 1' LONG. / REMOVED AND REPLACED FWD CARGO DOOR CENTER SCUFF PLATE REF AMM 53-11-02.SDR SWAA2018070323294Beam · crackedR1 DOOR CRACKED ON BEAM IN RADIUS BELOW CAM BOX ASSEMBLY NEXT TO FORWARD INBOARD MOUNTING BOLT. R&R R1 DOOR IAW MM.SDR SWAA2022021019569Scuff Plate · crackedAFT CARGO CENTER SCUFF PLATE CRACKED WITH MULTIPLE DENTS; #1 CRACK LOCATED 2 3/8' FROM FWD EDGE OF SCUFF PLATE. CRAC IS Ï¿½' LONG 'A' DIM 3.06' 'B' DIM 2.75' / R&R'D AFT CARGO THRESHOLD CENTER SCUFF PLATE PER AMM 53-11-02SDR SWAA2018020819595Slide · out of adjustR2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.SDR SWAA2016111609732Skin · delaminatedRT WING INBOARD GROUND SPOILER DELAMINATED ON LOWER SKIN. R&R SPOILER PER SRM.SDR SWAA2016082955198Support Fitting · corrodedRIGHT MLG FORWARD TRUNNION SUPPORT FITTING LUG FACES CORRODED. R & R FITTING IAW EA.SDR SWAA2016082955197Support Fitting · corrodedLEFT MLG FORWARD TRUNNION SUPPORT FITTING LUG FACES CORRODED. R & R FITTING IAW EA.SDR SWAA2016081254752Battery · failedEMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1674. R & R BATTERY IAW DWG AND AMM.SDR SWAA2016081254751Battery · failedEMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1669. R & R BATTERY IAW DWG AND AMM.SDR SWAA2016081254759Battery · failedEMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1668. R & R BATTERY IAW DWG AND AMM.SDR SWAA2016081254756Attach Bracket · crackedFUSELAGE KEELBEAM PANEL 192E FORWARD RT AND LT ATTACH BRACKETS CRACKED. R & R BRACKETS IAW SRM.SDR SWAA2015122347404Battery · failedEMERGENCY LIGHT BATTERY PACK M1675 FAILED CAPACITY TEST. R & R BATTERY IAW MM.SDR SWAA2015122347403Floor Support · crackedCABIN FLOOR SUPPORT CRACKED AT STATION 540, APPROX RBL 1. R & R FLOOR SUPPORT IAW SRM.SDR SWAA2015060340314Lens · looseR1 DOOR EXIT LIGHT LENS LOOSE. SECURED LENS IAW EA.SDR SWAA2015060340313Lens · looseR1 DOOR LOWER EXIT LIGHT LENS LOOSE. SECURED LENS IAW MM.SDR Z6WR20150427002Panel · burnedREFERENCE CMM 78-31-37, 01 MAR 2015, REVISION 032, FIGURE 35, ITEM 40K FAA – AIRWORTHINESS DIRECTIVE 2012-05-02, EFFECTIVE DATE MAY 10, 2012. ALTHOUGH SERVICE BULLETIN 737-78-1079, REVISION 01 DATED 17 DEC 2007 WAS PREVIOUSLY INCORPORATED, THE 315A2101-165 BOSDR SWAA2014121034885Intercostal · crackedFORWARD ENTRY DOOR INTERCOSTAL CRACKED BETWEEN BS 312 TO 328, 19 INCHES INBD OF PANEL ATTACH POINT. R & R INTERCOSTAL IAW SRM & DWG.SDR SWAA2014120834744Insert · corrodedFLOORBOARD 221AF INSERT CORRODED. R & R INSERT IAW SRM.SDR SWAA2014121535015Seat Track · crackedSEAT TRACK FLANGE CRACKED AT BS 727B, LBL 45.5, AT ALL FOUR FASTENER HOLES. REPAIRED SEAT TRACK IAW EA.SDR SWAA2014121535014Seat Track · crackedSEAT TRACK FLANGE CRACKED AT BS 727B, LBL 24.75 AT BOTH INBD FASTENER HOLES & THE AFT OTBD FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.SDR SWAA2014121535013Seat Track · crackedSEAT TRACK FLANGE CRACKED AT BS 727B, RBL 24.75 AT BOTH OTBD FASTENER HOLES & THE FWD INBD FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.
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