N216WR
Service difficulty reports · 301
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 = 'N216WR' 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 = 'N216WR' 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 SWAA2025031493986Flap · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP ON IB SIDE AT LT WING 2025-112824 <[01]. TOOL USED ON STEP 4: BONDTESTING UNIT; P/N: BONDMASTER 600M; S/N:220052310; CAL DUE DATE: 04-DEC-25; [02] TOOL USED HOT BONDER PN: HCS9200B; SN: 18185847; DUE DATE: 01/OCT/25.; [SDR SWAA2025031493769Girt Bar · out of adjustWEAR ON GIRT BAR FITTING HARDWARE AND PLATE ENTRY DOOR AT FWD GALLEY AREA. 2025-112760 <[01]. REPLACED GIRT BAR FITTING HARDWARE AND PLATE ENTRY DOOR AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801; TEST IS OK.; [02] TASK COMPLETED.SDR SWAA2025031493762Girt Bar · wornWEAR ON GIRT BAR FITTING HARDWARE AND PLATE SERVICE DOOR AT FWD GALLEY AREA. 2025-112763 <[01]. REPLACED GIRT BAR FITTING HARDWARE AND PLATE SERVICE DOOR AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801; TEST IS OK.; [02] TASK COMPLETED.SDR SWAA2025031493764Gusset · crackedCRACK GUSSET LOCATED BS500D AT LEVEL STR19L AT FWD CARGO COMPARTMENT 2025-112755 <[01]. REPLACED GUSSET AND FASTENERS LOCATED BS500D AT LEVEL STR19L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 143A7902 SHEET 209 REV-. SSDR SWAA2025031493768Gusset · crackedCRACK GUSSET LOCATED BS500D AT LEVEL STR21R AT FWD CARGO COMPARTMENT 2025-112758 <[01]. REPLACED GUSSET AND FASTENERS LOCATED BS500D AT LEVEL STR21R AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02-0G-0; DWG 143A7902 SHEET: 209 REV: - AND B737-700 SRM 51-SDR SWAA2025031493766Gusset · crackedCRACK GUSSET LOCATED BS500D AT LEVEL STR21L AT FWD CARGO COMPARTMENT 2025-112757 <[01]. REPLACED GUSSET LOCATED BS500D AT LEVEL STR21L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND 143A7902 SHEET: 209 REV - ; SEE INDIVIDUAL SIGNOSDR SWAA2025031493765Gusset · crackedCRACK GUSSET LOCATED BS500D AT LEVEL STR19R AT FWD CARGO COMPARTMENT 2025-112756 <[01]. REPLACED GUSSET AND FASTENERS LOCATED BS500D AT LEVEL STR19R AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-05 AND DWG 143A7902 SHEET 209 REV - SEESDR SWAA2025031203434Power Supply · inoperativeINOP BATTERY POWER SUPPLY BETWEEN STA 600 AND STA 620 LH SIDE AT PASSENGER CABIN 2025-112874 <[01]. REPLACED BATTERY POWER SUPPLY BETWEEN STA 600 AND STA 620 LH SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-806 SEE INDIVIDUALS SIGN OFF BELOW. TEST IS SDR SWAA2025031793275Handle · deterioratedDETERIORATED SERVICE DOORWAY LINING HANDLE NUTS AT AFT GALLEY AREA (2 EA) 2025-112704<[01] REPLACED SERVICE DOORWAY LINING HANDLE NUTS AT AFT GALLEY AREA (2 EA) IAW B737-700 AMM 25-21-25-420-801 STEP 3.B(5).;[02] REPLACED SERVICE DOORWAY LINING HANDLE NUTS AT SDR SWAA2025031793396Vapor Barrier · cracked(CUSTOMER REQUEST) CRACK ON VAPOR BARRIER LOCATED ON BS 663 RH SIDE AT WING CENTER SECTION 2025-112711<[01] FAULT RESOLVED ON OTHER FAULT DUE TO TASK IS DUPLICATED SEE TTG8Q00YHFF6;[02] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00YHFF6SDR SWAA2025031492827Floor Panel · crackedCRACK FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT 2025-112623 <[01]. FABRICATED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT I.A.W B737-700 AMM 25-52-01-201-801 AND DWG 453A1610 SHEET: 7 REV: C. MATERIAL USED: ALUMINUM SHEET P/N: 2024T3-071 P/O: 2025 103758.; [0SDR SWAA2025031492826Vapor Barrier · cracked(CUSTOMER REQUEST) CRACK ON VAPOR BARRIER LOCATED AT BS 663.75 BETWEEN RBL 25 TO RBL 40 RH SIDE WHEEL WELL COMPARTMENT. 2025-112628 <[01]. TOOL USED CALIPER P/N 500-196-30 S/N B21141537 DUE DATE 29 DEC 25; [02] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 1818584SDR SWAA2024112670920Transmitter · inoperativeON APPROACH FLAPS LOCKED OUT; LOWERED FLAPS USING ALTERNATE FLAPS EXTENTION.<[01] CW FIM TASK 27-51 TASK 802. R/R RH FLAP POSITION TRANSMITTER IAW AMM 27-58-01.;[02] CW FIM TASK 27-51 TASK 820. R/R RH FLAP POSITION TRANSMITTER IAW AMM 27-58-01.SDR SWAA2024101447192Battery Pack · no testBATTERY PACK M1672 FAILED CAPACITY TEST.<[01] R&R BATTERY PACK M1672 IAW AMM 33-51-06.SDR SWAA2024101447022Handle · looseAFT ENTRY DOOR L2 DOOR HANDLE CAM LOOSE<[01] RE-SECURED AFT ENTRY DOOR L2 DOOR HANDLE CAM REF AMM 20-50-11.SDR SWAA2024082327663Vapor Barrier · crackedVAPOR BARRIER WEB CRACKED AT BS 663 (WL 167) RBL 24 TO RBL 30<[01] 04 - REPAIRED PER [EA EA-GENERAL (EA ATTACHED TO AN AIRCRAFT FAULT)];[02] VERIFIED STEP 1<BR>AUDIT CW;[03] REPAIRED RH VAPOR BARRIER WEB CRACK AT BS 663 (WL 167) RBL 24 TO RBL 30 IAW EA M-21-15SDR SWAA2024080823896Battery Pack · inoperativeEMERGENCY LIGHTS INOP OVER L1 DOOR; OUTSIDE L1 DOOR; AND IN CABIN AT ROWS 1ABC AND 4ABC<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK ON POWER SUPPLY M1675 REF AMM 33-51-06; OPS CHECK GOOD.SDR SWAA2024011038999Battery · inoperativeAFT MEGAPHONE INOP<[01] REPLACED BATTERIES IN AFT CABIN MEGAPHONE IAW AMM 25-64-00. A/C OK FOR SERVICE.SDR SWAA2023120527133Bracket · out of adjustSCREW CAME OUT OF BRACKET THAT HOLDS SCAPE SLIDE.<[01] SECURED SCREW AT FWD ENTRY DOOR SLIDE PER AMM 25-66-01. OPS CHECK NORMAL.SDR SWAA2023101911862Light · inoperativeCABIN R/H OVERWING EXIT LIGHT IS INOPERATIVE.<[01] REMOVED AND REPLACED CABIN R/H OVER WING EXIT LIGHT IAW B737 AMM 33-51-01.SDR SWAA2023092604013Battery Pack · inoperativeEMERGENCY LIGHTS MID R/H CABIN INOP.<[01] R/R EMERGENCY LIGHTS BATTERY PACK (M1669) FOR MID SECTION R/H. REF AMM 33-51-06 OPS CHK GOOD.SDR SWAA2023080484534Flap System · lockedFLAP ASYMMETRY DISCOVERED DURING CRUISE BY SPLIT NEEDLES ON FLAP GAUGE. RT FLAP SHOWED FULL UP; LT FLAP WAS BETWEEN UP AND 1. VERIFIED ASYMMETRY BY CONFIGURING EARLY ON ARRIVAL. FLAPS DID NOT MOVE. PERFORMED A TRAILING FLAPS UP LANDING. VREF/VTARGET WAS 170/17SDR SWAA2023062872299Light · inoperativeG4 GALLEY MOUNTED EMERGENCY LIGHT HAS INOP BULBS<[01] REMOVED AND REPLACED G4 GALLEY MOUNTED EMERGENCY LIGHT IAW AMM 33-51-01.SDR SWAA2023050946651Slide · low pressureR2 DOOR ESCAPE SLIDE IN THE RED(LOW BOTTLE PRESSURE)<[01] R&R DOOR MOUNTED ESCAPE SLIDE ON AFT SVC DOOR PER MT 25-66-01 AND AMM 25-66-01.SDR SWAA2023031615136Bulb · inoperative*C/R* EMERGENCY SIGN AFT OF R-2 DOOR HAS 1 BULB INOPERATIVE.<[01] RELAMPED EMERGENCY SIGN AFT OF R-2 DOOR AS PER B737 AMM 33-51-04-960-801. TEST OK.SDR SWAA2023031615132Light · inoperativeR/H AFTER WING EXTERIOR EMERGENCY LIGHT INOPERATIVE.<[01] RELAMPED R/H AFTER WING EXTERIOR EMERGENCY LIGHT PER REF AMM 33-51-04-960-801. PERFORMED OPS CHECK AND FOUND NORMAL.;[02] VERIFIED / INSPECTED LITE .IS OPERATIONAL ;SDR SWAA2023032010698Structure · elongatedCOCKPIT DOOR SURROUND ATTACHMENT AT FRAME 277 BETWEEN STRINGER 1R-2R AFTER REMOVE BOLTS; FOUND ELONGATED HOLES AND GAUGES.<[01] INSTALLED PROTECTION EWIS AROUND FRAME 277 BETWEEN STRINGERS 1R-2R REF. BOEING 737 AMM 20-60-07-913-801;[02] REMOVED CHANEL AND ANGLSDR SWAA2023032010166Panel · elongatedACCESS PANEL 191HL COVER PLATE - FORWARD FAIRING HOLES ENLONGATED<[01] RECEIVED NEW PANEL 191HL. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00GXTW3;[02] STEP #1 ENTER IN ERROR; ACCESS PANEL 191HL WILL BE UNAVAILABLE AND ESR WAS SEND TO ENGINEER; SEE ASDR SWAA2023032009379Plate · crackedR/H AFT FUSELAGE FWD SEAL GUIDE PLATE FOR HORIZONTAL ACCESS PANEL 343AT CRACKED.<[01] REMOVED R/H AFT FUSELAGE FWD SEAL GUIDE PLATE FOR HORIZONTAL ACCESS PANEL 343AT AS PER B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1. OK TO INSTALL NEW SEAL GUIDE PLATE.;[SDR SWAA2023031609578Skirt · out of adjustPER CUSTOMER REQUEST: R1 DOOR SLIDE SKIRT IS TOUCHING CABIN FLOOR<[01] REMOVE AND RE-INSTAL R-1 DOOR SLIDE PER MT 725-61-06 T/C TTG8Q00JF208;[02] INSTALLED CORRECTLY PACKED SLIDE INTO THE COMPARTMENT ASSY PER DWG 416A2200. R-1 DOOR SLIDE SKIRT IS NOT TOUCHING SDR SWAA2023031603565Floor Panel · peelingAFT CABIN FLOOR PANEL 241UF UPPER SKIN SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 241 UF; P/N 146A5810-54; NEW FLOOR TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GXTVS;[02] VERIFIED STEP 1SDR SWAA2023031602641Scuff Plate · crackedFWD CARGO COMPARTMENT SCUFF PLATE FWD CORNER HAS CRACK<[01] RECEIVED SERVICEABLE FWD CORNER SCUFF PLATE AT FWD CARGO; WELDED BY J.L. WELDING P. O. # 413896; SERVICEABL SCUFF PLATE TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00HR48J;[02] VERIFIED STEP 1.SDR SWAA2023031602642Scuff Plate · crackedFWD CARGO COMPARTMENT SCUFF PLATE AFT CORNER HAS CRACK<[01] RECEIVED SERVICEABLE AFT CORNER SCUFF PLATE AT FWD CARGO; WELDED BY J.L. WELDING P. O. # 413894; SERVICEABLE SCUFF PLATE TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00HR48J;[02] VERIFIED STEP 1.SDR SWAA2023032002231Support Angle · corrodedCORROSION ** AT R-1 SERVICE DOOR CUTOUT LOWER SILL INNER SCUFF PLATES SUPPORT ANGLE<[01] REMOVED SURFACE CORROSION ON R-1 LOWER MAIN SILL I/B ANGLE ON UPPER SURFACE PER B737-700 SRM 51-10-02-0G-G.;[02] VERIFIED STEP1;[03] MEASUREMENTS FOR INNER CHORD; ORIGINALSDR SWAA2023031702311Cap · elongatedAFT CARGO COMPARTMENT L/H CAP STRIPS WITH HOLE ELONGATED<[01] RECEIVED NEW AFT CARGO CAP STRIPS P/NS; 453A2611-8; -10;-4;- AND -13; NEW CAP STRIPS TOB INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS7H9 AND TTG8Q00GS7HB;[02] VERIFIED STEP 1SDR SWAA2023032002086Intercostal · crackedFWD CABIN FLOOR INTERCOSTAL AT 312-328 RIGHT B/L 28 IS CRACKED<[01] REMOVED INTERCOSTAL AT FWD CABIN FLOR STA 312 TO 328 RIGHT BL 28 FOR CRACKED SRM 51-40-02 -0G-0;[02] VERIFIED STEP 1AND OK TO INSTALL NEW INTERCOSTAL;[03] RECEIVED NEW PART PO#2002351) INSTALLSDR SWAA2023032001780Structure · corrodedCORROSION....R/H AFT CABIN FLOOR @ STA 947.5 - STA 992.8 + 6 RBL 57 WL 208.1 INNER CORD HAS CORROSION. (18-41)<[01] FOUND EXFOLIATE CORROSION ON R/H INNER CHORD FROM STA. 947.5 TO STA. 992.8; OUT OF LIMITS PER SRM 53-70-15-1A-1REMOVED R 2 DOOR INNER CHORD; PERSDR SWAA2023032001767Structure · corrodedCORROSION....L/H AFT CABIN FLOOR @ STA 986.5 LBL 43 WL 208.1 T - CORD FASTENER HOLE HAS CORROSION. (18-46)<OUT OF LIMITS PER REF SRM 53-70-51-1A-1 CUT OUT DAMAGE SECTION ON FLOOR BEAM STA 986.5; LBL 43' PER REF SRM 53-70-51-2R-6;[07] VERIFIED STEP 6;[08] PERFOSDR SWAA2023032002083Intercostal · corrodedCABIN FLOOR SUPPORT INTERCOSTAL BETWEEN 294.5-312 LEFT B/L 12 IS CORODED<[01] INSTALLED EWIS AND FOD PROTECTION ON AREA AS PER AMM 20-60-07-913-801.;[02] PARTIALLY REMOVED DAMAGED CABIN FLOOR SUPPORT INTERCOSTAL BETWEEN 294.5-312 LEFT B/L 12 PER REF SRM 51-40-SDR SWAA2023032002082Structure · corrodedR-! DOOR THRESHOLD INTER CORD HAS CORROSION.<[01] REMOVED SURFACE CORROSION ON INNER CHORD UPPER SURFACE AROUND FASTENER HOLES PER B737-700 SRM 51-10-02-0G-G.;[02] VERIFIED STEP1;[03] MEASUREMENTS FOR INNER CHORD; ORIGINAL MATERIAL 0.80'; MATERIAL LOSS .016' ASDR SWAA2023031601989Floor Panel · corrodedCABIN FLOOR PANEL 221BF HAS CORRODED INSERTS<[01] RECEIVED NEW PANEL P/N 141A5810-56 INSTALLATION WILL BE ACCOMPLISH ON TTG8Q00GS734;[02] RECEIVED NEW PANEL P/N 141A5810-56 INSTALLATION WILL BE ACCOMPLISH ON TTG8Q00GS734SDR SWAA2023031601762Floor Panel · peelingAFT CABIN FLOOR PANEL 241XF UPPER SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 241 XF; NEW FLOOR PANEL TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS6T5;[02] VERIFIED STEP 1 RECEIVING FLOOR PANEL 241XF AND TO BE INSTALLED ON TTG8Q00GS6T5.SDR SWAA2023031601778Floor Panel · peelingAFT CABIN FLOOR PANEL 241YF UPPER SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 241 YF; P/N 147A5810-77; NEW FLOOR TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS6UA;[02] VERIFIED STEP 1 RECEIVING FLOOR PANEL 241YF AND TO BE INSTALLED ON TTG8Q00GS6UA.SDR SWAA2023031601777Floor Panel · peelingAFT CABIN FLOOR PANEL 241ZF UPPER SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 241 ZF; P/N 147A5810-98; NEW FLOOR TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS6TY;[02] VERIFIED STEP 1 RECEIVING FLOOR PANEL 241 ZF AND TO BE INSTALLED ON TTG8Q00GS6TY.SDR SWAA2023031601761Floor Panel · peelingAFT CABIN FLOOR PANEL 241ABF UPPER SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 241 ABF P/N 147A5810-88; NEW FLOOR TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS6TU;[02] VERIFIED STEP 1 RECEIVED PANEL AND TO BE INSTALLED ON T/C TTG8Q00GS6TU.SDR SWAA2023031601775Floor Panel · peelingAFT CABIN FLOOR PANEL 241AAF UPPER SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 241 AAF; P/N 147A5810-8; NEW FLOOR TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS6TW;[02] VERIFIED STEP 1SDR SWAA2023031601774Floor Panel · peelingAFT CABIN FLOOR PANEL 242UF UPPER SURFACE PEELING.<[01] RECEIVED NEW CABIN FLOOR PANEL 242 UF P/N 147A5810-95; NEW FLOOR TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS726;[02] VERIFIED STEP 1 RECEIVED PANEL AND TO BE INSTALLED ON T/C TTG8Q00GS726.SDR SWAA2023031601772Floor Panel · peelingAFT CABIN FLOOR PANEL 241ACF UPPER SURFACE PEELING.<[01] PREPARED DAMAGE AREA AND APPLIED THE GLASS FABRIC REPAIR PLIES AT AFT CABIN FLOOR PANEL 241ACF UPPER SURFACE. REF B737 SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPH 3. MATERIAL USED GLASS FABRIC PLIES PO#: 169454SDR SWAA2023031601770Panel · crackedAFT CABIN FLOOR PANEL 242VF UPPER SURFACE CRACKED.<[01] RECEIVED NEW CABIN FLOOR PANEL 242VF; P/N 147A5810-350; NEW FLOOR PANEL TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GS724;[02] VERIFIED STEP 1.SDR SWAA2023031601758Floor Panel · crackedAFT CABIN FLOOR PANEL 241AEF CRACKED.<[01] PREPARED FOR REPAIR DAMAGED AREA; AT AFT CABIN FLOOR PANEL#241AEF AS PER B737 SRM 53-00-50-2R-1;[02] REPAIRED DAMAGED AREA AT AFT ABIN FLOOR PANEL #241 AEF AS PER B737 SRM 53-00-50-2R-1 MATERIAL USED PO#1799598 PO#169
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