N900WN
Service difficulty reports · 251
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 = 'N900WN' 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 = 'N900WN' 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 SWAA2021081804880Strip · corrodedAFT CARGO FLOOR PANEL TRANSITION STRIP; UPPER SURFACE CORRODED AT NUT PLATE. DOT 15/234 ; / [01] REMOVED CORROSION IAW SRM 51-10-02-0G-0; USING 10X MAG. VERIFIED MATERIAL LOSS ORIGINAL T .063' LOSS .020' REMAINING MATERIAL .043' OUT OF LIMITS IAW SRM 53-00-53-SDR SWAA2021081803084Seat Track · corrodedA45-12 - PASSENGER CABIN SEAT TRACK UPPER CROWN AREA HAS LIGHT CORROSION; WL 207; RBL 47; STA 706 TO 727A. ; / [01] STARTED REMOVING CORROSION FROM SEAT TRACK AT STA 706 TO 727A. REMOVED . 045' FROM BOTTOM INSIDE CROWN OF SEAT TRACK. FOUND SEAT TRACK TO BE OUTSDR SWAA2021081800580Stiffener · crackedA22-01; RIGHT HORIZ STAB; INSPAR RIB AT STA 129.5; 2ND FROM FWD STIFFENER IS CRACKED JUST ABOVE THE RIB LWR FLANGE; MRK'D. ; / [01] CUT AND REMOVED DAMAGED SECTION OF VERTICAL STIFFENER OF THE RIB IAW SRM 55-10-09-2R-4 REPAIR 4; [02] PERFORMED VISUAL INSPECTIOSDR SWAA2021081899590Floor Panel · debondedAFT CARGO FLOOR PANEL 140BF; HAS PREVIOUS REPAIR DISBONDING. DOT NO.4/234 ; / [01] VERIFIED MATERIAL AS A90RG1W. IAW AMM 25-52-01-201-801. A-TAG # A51996.; [02] VERIFIED STEP 1.; [03] FABRICATED REPLACEMENT AFT CARGO FLOOR PANEL 140BF; VERIFIED MATERIAL AS A90SDR SWAA2021081899596Gusset · crackedFWD CARGO COMPARTMENT; GUSSET CRACKED AT STA 500D; S-19L ; / [01] REMOVED CRACKED GUSSET AT S-19L IAW SRM 51-40-02-0G-0; [02] VERIFIED NEW GUSSET AS PN 143A9481-6 A-TAG A69533 IAW BOEING DWG 143A9481 ID 2 REV A.; [03] DRILLED UP NEW GUSSET IAW SRM 51-40-05-0G-SDR SWAA2021081899597Gusset · crackedFWD CARGO COMPARTMENT; GUSSET CRACKED AT STA 500D; S-19R ; / [01] REMOVED GUSSET AT STA 500D S-19R IAW SRM 51-40-02; [02] LOCATED AND DRILLED UP HOLED IN NEW GUSSET(P#143A9481-5 ATAG A69522) IAW SRM 51-40-02 AND DWG #413A7902 REV E; [03] VERIFIED STEP 2.<BR>OKSDR SWAA2021081800553Intercostal · corrodedA22-13; FWD PIT STA 500-500A; LBL 24; WL158; FLOOR SUPPORT INNER COSTAL HAS CORROSION; MRK'D. ; CORRECTION; SHOULD BE DOT 16 / [01] REMOVED CORROSION IAW SRM 51-10-02-0G-0. USED 10X MAG. EVALUATED MATERIAL LOSS ORIGINAL 'T' .020'; LOSS .004'; REMAINING MATERIASDR SWAA2021081800559Splice Plate · corrodedAFT CARGO COMP.FLOOR SPLICE PLATE CORRODED STA 727D WL 158 LBL 23-RBL 23' DOT 185-005 ; / [01] SPLICE PLATE AT STA 727D IS OUT OF LIMITS AT 100% MATERIAL LOSS. VERIFIED NEW PART TO BE 146A9401-8; A TAG# A72427.; [02] VERIFIED STEP 1.; [03] AFT CARGO COMPARTMENSDR SWAA2021081800560Intercostal · corrodedAFT CARGO COMP.RH INTERCOSTAL CORRODED STA.747-767 WL 158 RBL 25' DOT 185-007 ; / [01] STARTED REMOVING CORROSION FROM INTERCOSTAL STA747-767. ORG. THICKNESS . 032' ; REMAINING . 025' LOSS .007' . LOSS OF 22%. MAX ALLOWABLE IS 10%. FOUND INTERCOSTAL TO BE OUT SDR SWAA2021081800558Angle · corrodedAFT CARGO COMP.RH Z-ANGLE CORRODE 794-807 RBL 25' WL 158 DOT 185-004 ; / [01] AFT CARGO COMPARTMENT RH Z-ANGLE BS 727-767 WAS FABRICATED IAW SRM 53-00-53-2R-5; AND ALL WORK ACCOMPLISHED ON TTG8Q005ZF8U.; [02] REPLACEMENT OF Z-ANGLE FROM BS 727 + 4' -767; ARE TSDR SWAA2021081800565Shield · corrodedAFT CARGO COMP.FWD FLOOR SHIELD CORRODED STA.767-787 WL 158 RBL 25' ; NUMBER 185-002 / [01] REMOVED CORROSION IAW SRM 51-10-02-0G-0. USED 10X MAG. VERIFIED MATERIAL LOSS AS ORIGINAL 'T' .050' LOSS .010'; REMAINING MATERIAL .040'; OUT OF LIMITS IAW SRM 53-60-15SDR SWAA2021081800567Angle · corrodedAFT CARGO COMP.LH Z-ANGLE CORRODED STA.852-882 WL 158 LBL 25' DOT 185-006 ; / [01] REMOVED CORROSION AND VERIFIED LIMITS; ORIGINAL THICKNESS .040'; LOSS .010'; REMAINING .030' OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIGURE 103 DETAIL D.<BR>TOOL# AAR-27213 CAL DUE SDR SWAA2021081800566Angle · corrodedAFT CARGO COMP.RH Z-ANGLE CORRODED STA.837-867 RBL 25' WL 158 ; NUMBER 185-003 / [01] REMOVED CORROSION IAW SRM 53-00-50-1A-1. USED 10X MAG. VERIFIED MATERIAL LOSS ORIGINAL 'T' .040' LOSS .020' REMAINING MATERIAL .020'; OUT OF LIMITS IAW SRM 53-00-53-1A-2. AARSDR SWAA2021081800569Nut Plate · missingAFT CARGO COMP.FLOOR PANEL FASTNER NUT PLATE MISSING STA.727+5 BL 0 ; / [01] INSTALLED NUT PLATE IN AFT CARGO PIT ON FLOOR RAIL AT BS 727 + 5' AT BL '0' IAW SRM 51-40-02-0G-0.SDR SWAA2021081800568Frame Angle · crackedAFT CARGO COMP.LH FRAME ANGLE CRACKED STA 867 LBL 20' FWD AND INBD OF LAV TANK ; / [01] REMOVED CRACKED FRAME ATTACH ANGLE FROM AIRCRAFT. VERIFIED NEW ATTACH ANGLE TO BE P/N149A-8109U114; ISSUE TAG A32883. LOCATED AND DRILLED NEW ATTACH ANGLE IAW SRM 51-40-02-SDR SWAA2021081800575Pan · displacedAFT CARGO DOOR OUTER HANDLE OVER CENTERS ; / [01] DISPLACE INNER AFT CARGO DOOR CLOTH LINER AND REMOVED INNER PANEL 822BZ FOR F.O.M IAW SRM 51-40-02-0G-0; [02] REMOVED AFT CARGO DOOR HANDLE PAN ASSY. IAW SRM 51-40-02-0G-0; [03] LOCATED AND DRILLED NEW HANDLE PSDR SWAA2021081800561Nut Plate · missingAFT CARGO COMP.FLOOR PANEL FASTNER NUT PLATE MISSING STA.937 RBL 12' ; / [01] REPLACE MISSING NUT PLATE IN AFT CARGO COMPARTMENT AT BS 937 RBL 12 IAW SRM 51-40-02-0G-0.; [02] INSPECTION CW. AUDIT CWSDR SWAA2021081800562Nut Plate · missingAFT CARGO COMP.FLOOR PANEL FASTNER NUT PLATE MISSING STA.727E BL 0 ; / [01] REPLACE MISSING NUT PLATE AFT CARGO COMPARTMENT AT BS 727E BL'0' WL 156 IAW SRM 51-40-02-0G.; [02] INSPECTION CW. AUDIT CWSDR SWAA2021081899582Floor Panel · corrodedAFT CARGO; METAL FLOOR PANEL 140CF HAS CORROSION AROUND FASTENER HOLES; UPPER AND LOWER SURFACES. STATION 800-850 RBL 21; WL156. DOT NO.1/234. ; / [01] VERIFIED MATERIAL AS 2024 T3; .071 IAW AMM 25-52-01-201-801. A-TAG # A49494.; [02] INSPECTION CW STEP 1; [03SDR SWAA2021081898997Scuff Plate · crackedAFT CARGO DOOR CUTOUT FWD CORNER SCUFF PLATE CRACKED ; / [01] AFT CARGO DOOR CUTOUT FWD LOWER CORNER SCUFF PLATE WELDED FOR CRACK IAW SRM 53-60-15-2R-1. AAR WORK ORDER 42497-1600-0002.; [02] VERIFIED STEP 1.<BR>AUDIT C/WSDR SWAA2021081898998Scuff Plate · crackedAFT CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED ; / [01] AFT CARGO DOOR CUTOUT AFT LOWER CORNER SCUFF PLATE WELDED FOR CRACK IAW SRM 53-60-15-2R-1. AAR WORK ORDER 42497-1600-0001.; [02] VERIFIED STEP 1.<BR>AUDIT C/WSDR SWAA2021031554583Light · looseOH CEILING EMERGENCY EXIT LIGHT LOOSE @ ROW 11. / SECURED OH CEILING EMERGENCY EXIT LIGHT @ ROW 11 PER MM 33-51-01SDR SWAA2020022841942Sign · looseOVERHEAD EXIT SIGN IN AFT GALLEY WAS LOOSE. / R&R SIGN ASSEMBLY REF MM.SDR SWAA2019090336507Sign · brokenAFT GALLEY EXIT SIGN BROKEN OFF CEILING. REINSTALLED SIGN PER MM.SDR SWAA2019082736312Light · missingL2 DOOR AFT WALL EMERGENCY EXIT LIGHT MISSING. REINSTALLED LIGHT PER AMM.SDR SWAA2019082736337Battery Pack · dischargedR/H EXTERIOR EMERGENCY LIGHTS AT POSITION AFT OF R/H WING OT BODY FAIRING INOP. RECHARGED BATTERY PACK PER AMM.SDR SWAA2019082736336Battery Pack · dischargedR/H EXTERIOR EMERGENCY LIGHTS AT POSITION R2 DOOR INOP. RECHARGED BATTERY PACK PER AMM.SDR SWAA2019082736293Battery Pack · inoperativeR/H EXTERIOR EMERGENCY LIGHTS AT POSITION R/H OVERWING INOP. RECHARGED BATTERY PACK PER AMM.SDR SWAA2019081435883Floorbeam · crackedFLOOR SUPPORT ANGLE CRACKED AT L-1 DOOR CUTOUT FORWARD FRAME FLOOR LEVEL AT BS. 303.9, LBL 57. / R&R FLOOR SUPPORT ANGLE PER SRM AND DWG.SDR SWAA2022031456113Floor Panel · crackedCABIN FLOOR PNL 231YF HAS 1' CRACK. / REMOVED DAMAGE PANEL 231YF AT MAIN CABIN AND INSTALLED SERVICEABLE PANEL PER REF B737 AMM 53-21-00-400-801SDR SWAA2019082736292Rib · crackedCRACKED AT FASTENER HOLE LOCATED OUTBOARD OF LOWER CHORD OF THE L/H HORIZONTAL STABILIZER BOX RIB #4 AT STIFFENER. REPAIRED #4 RIB PER EA.SDR SWAA2019081335835Stiffener · crackedR/H HORIZONTAL STABILIZER BOX #4 RIB, #4 STIFFENER CRACKED AT LOWER CHORD INBOARD DIRECTION, STA. 120.3. / REPAIRED #4 STIFFENER IAW SRM.SDR SWAA2019080535618Rib · crackedRT HORIZONTAL STABILIZER RIB #5 STA. 129.5, FORWARD END LOWER CHORD INBOARD SIDE CRACKED. / REPAIRED #5 RIB PER SRM.SDR SWAA2022031456112Stiffener · out of toleranceLT HORI STAB RIB #4 LWR FLANGE IB FASTER HOLE # 8 FROM AFT END HAS HOLE OUT OF ROUND. / FABRICATED LOCATED DRILLED & INSTALLED REPAIR PARTS AT RIB #4 LWR FLANGE STIFFNER #4 IAW B737 SRM 55-10-09-2R-5; CUT OUT DAMAGE AREA AT RIB #4 LWR FLANGE I/B FASTENER HOLE SDR SWAA2019082736291Rib · crackedL/H HORIZONTAL STABILIZER #4 RIB CRACKED AT FORWARD END AT UPPER FLANGE ON OUTBOARD SIDE. REPAIRED #4 RIB IAW EA.SDR SWAA2019082736290Rib · crackedL/H HORIZONTAL STABILIZER #4 RIB CRACKED AT FORWARD END AT UPPER FLANGE ON INBOARD SIDE. REPAIRED #4 RIB IAW EA.SDR SWAA2019081335806Rib · crackedL/H HORIZONTAL STABILIZER #4 RIB CRACKED AT FORWARD END AT LOWER FLANGE ON OUTBOARD SIDES. / REPAIRED RIB PER SRM.SDR SWAA2019080535617Strap · corrodedR1 DOOR LOWER CUT OUT CHORD VERTICAL ANGLE CORRODED AT BS. 294.5+3, WL 208.1. R & R ANGLE STRAP PER SRM AND DWG.SDR SWAA2022031456104Angle · crackedNO.1 ENGINE IB FAN COWL INTERIOR DOOR FRAME SUPPORT ANGLE CRACKED / REMOVED AND REPLACED SUPPORT ANGLE AT # 4 ENG I/B FAN COWL INTERIOR DOOR FRAME PER REFERENCE IB737-700 SRM 51-40-02-OG-OSDR SWAA2022031456083Support · corrodedFWD CARGO LT FLOOR SIDE PLATE STA 500B HAS CORROSION AT DRILLED HOLE / REMOVED AND REPLACED AT L/H SIDE PLATE CHANNEL SUPPORT AT FWD CARGO COMP IN REF B737-700 SRM 51-40-02-0G-0SDR SWAA2019082236199Scuff Plate · corrodedAFT CARGO DOOR LOWER SURFACE AREA OF SCUFF PLATE UPPER COMPLETE SECTION CORRODED. R&R WEB PER SRM AND DWG.SDR SWAA2022031456065Intercostal · crackedCABIN FLOOR INTERCOSTAL CRACKED AT SCREW HOLE LBL 46 BS 321. / REMOVED DAMAGED INTERCOSTAL AT CABIN FLOOR LBL 46 BS 321 IAW B737-700 SRM 51-40-02-0G-0 INSTALLED NEW INTERCOSTAL PER REF B737 SRM 51-40-02-0G-0 AND DWG 141A5400SDR SWAA2022031456072Angle · crackedCABIN FLOOR SUPPORT ANGLES 2 EACH CRACKED AT STA 540 BL 1RT / REMOVED AND REPLACED NEW ANGLE SUPPORT CABIN FLOOR STA 540 BL 1RT AS PER B737 SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0. INSTALLATION DWG 143A0060SDR SWAA2019082236198Floorbeam · corrodedL/H SIDE CABIN FLOOR BEAM CORRODED AT BS. 987, LBL 44. / REPAIRED FLOOR BEAM PER SRM & DWG.SDR SWAA2019081335834Door Sill · corrodedR2 DOOR JUST INBOARD OF SILL INNER CHORD CORRODED BETWEEN BS. 947 TO BS. 987. R&R INNER CHORD PER SRM.SDR SWAA2019072935378Intercostal · crackedCABIN FLOOR INTERCOSTAL CRACKED AT BS. 316, RBL 31. R&R INTERCOSTAL IAW SRM.SDR SWAA2019072935377Intercostal · crackedFLOOR INTERCOSTAL CRACKED AT BS. 285, BL 0, SCREW HOLE. R&R INTERCOSTAL IAW SRM.SDR SWAA2022031456061Stiffener · crackedRT HORIZONTAL STABILIZER BOX RIB 4 2ND STIFNER {FACING FWD TO AFT }LOWER EDGE AREA CRACKED.MKD 126-002 / AT RIB #4; STIFNER #2 CUTOUT AREA DAMAGED PER B737 SRM 55-10-09-2R-4; AFTER REWORK NDT CHECK AREA NO CRACK FOUND; LOCATED AND DRILLED REPAIR KIT #55100003-SDR SWAA2019082736289Rib · crackedL/H HORIZONTAL STABILIZER BOX RIB 4, INBOARD FACE 2ND STIFFENER FROM FORWARD TO AFT LOWER EDGE AREA CRACKED. REPAIRED RIB 4 PER EA.SDR SWAA2019081435923Stiffener · crackedL/H HORIZONTAL STABILIZER BOX #4 RIB, INBOARD FACE AFT STIFFENER FROM FORWARD TO AFT LOWER EDGE AREA CRACKED. REPAIRED STIFFENER IAW SRM.
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