N448WN
Service difficulty reports · 367
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 = 'N448WN' 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 = 'N448WN' 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 SWAA2026092891617Battery Pack · no testFWD LT EMERGENCY BATTERY PACK M1675 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.SDR SWAA2026092151509Transmitter · faultedWHEN SELECTING FLAPS TO 5 THEN 15, THE FLAP INDICATOR SHOWED A MINOR SPLIT OF THE FLAPS. ONE FLAP WAS IN UP POSITION OTHER BETWEEN UP AND 1. REPLACED OIL IN ALL FLAP TRANSMITIONS IAW AMM 12-22-51. REPLACED LT & RT FLAP POSITION TRANSMITTERS IAW AMM 27-58-01SDR SWAA2026090766008Sign · brokenL1 EMERGANCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED EMERGANCY EXIT SIGN IAW AMM 33-51-01, OPS CHECKED GOOD.SDR SWAA2026090366150Fastener · missing14C SEAT TRAY COMES OFF WHEN EXTENDED. INSTALLED FASTENER @T/T SEAT 14C PER SIP.SDR SWAA2026082516841Lens · missingRIGHT EMERGENCY EXIT LOWER EMERGENCY LIGHT LENS MISSING. REPLACED THE EMERGENCY LIGHT LENS IAW AMM 33-51-01. OPS CHECKED GOOD. NO DEFECTS NOTED.SDR SWAA2026070216990Bracket · unsecureFWD SERVICE DOOR AFT GIRT BAR BRACKET HAS ONE SHEARED RIVET. C/W EA M-23-125-01839.SDR SWAA2026042992778Fairing · crackedRT WING NR 6 FLAP TRACK AFT FAIRING CRACKED AT 6 OCLOCK POSITION AT AFT END. REMOVED AND REPLACED THE RT WING NR 6 FLAP TRACK FAIRING IAW AMM 27-51-18.SDR SWAA2026042992779Wedge · crackedLEFT INBOARD MAIN FLAP TRAILING EDGE HAS DEBOND, CRACK AND PUNCTURE DAMAGE. REMOVED TRAILING EDGE WEDGE; LOCATED AND DRILLED NEW WEDGE PER SRM 51-40-06, INSTALLED LT INBD MAIN FLAP WEDGE IAW SRM 51-40-02.SDR SWAA2026041789932Fairing · crackedFOUND #6 FLAP TRACK MID-CANOE FAIRING CRACKED AT 6OCLOCK POSITION AFT SIDE<[01] C/W EA 26-157-01040SDR SWAA2025092616871Scuff Plate · corrodedCORROSION ON CORNER PLATE (2EA) OF THRESHOLD SCUFF PLATE AT AFT CARGO COMPARTMENT. REPLACED CORNER PLATE (2EA) OF THRESHOLD SCUFF PLATE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; ITEM 9 AND DWG 453A2611; SHEET 1; REV C.SDR SWAA2025092612577Scuff Plate · crackedCRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED THE FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SDR SWAA2025092612579Threshold · crackedCRACK THRESHOLD AT FWD CARGO COMPARTMENT. REPLACED THRESHOLD AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G ITEM 9; SCUFF PLATE WILL BE INSTALLED ON TTG8Q014X931 AND TTG8Q00SFVBA.SDR SWAA2025092911544Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING . REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING IAW B737-700 SRM 51-10-02-0G ITEM 9; SRM 51-40-02-0G AND DWG: 115A2001; SHEET: 29; REV: -SDR SWAA2025092911541Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661CB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661CB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9.SDR SWAA2025092911540Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 661BB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-9 REPAIR 9.SDR SWAA2025092911543Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 661AB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661AB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-9 REPAIR 9.SDR SWAA2025092611539Scuff Plate · crackedCRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED THE FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.SDR SWAA2025092611931Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193B IAW SRM 51-70-05-2R-8 REPAIR 8.SDR SWAA2025092911530Plate · crackedCRACK CORRUGATED PLATE LOCATED ORSS290 TRAILING EDGE AT LT WING. REPLACED CORRUGATED PLATE LOCATED ORSS290 TRAILING EDGE AT LT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9.SDR SWAA2025092911306Support Angle · crackedCRACK ANGLE SUPPORT LOCATED ORSS269 TRAILING EDGE AT RT WING. REPLACED ANGLE SUPPORT LOCATED ORSS269 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET:8 REV:-.SDR SWAA2025092611310Nut · deterioratedDETERIORATED ASSIST HANDLE NUT SERVICE DOORWAY LINING AT AFT GALLEY AREA (2EA). REPLACED ASSIST HANDLE NUT SERVICE DOORWAY LINING AT AFT GALLEY AREA (2EA) IAW AMM 25-21-25-420-801 STEP 3.B.(5).SDR SWAA2025092611308Nut · deterioratedDETERIORATED ASSIST HANDLE NUT ENTRY DOORWAY LINING AT AFT GALLEY AREA (2EA). REPLACED ASSIST HANDLE NUT ENTRY DOORWAY LINING AT AFT GALLEY AREA (2EA) IAW AMM 25-21-25-420-801 STEP 3.B.(5).SDR SWAA2025092611307Nut · deterioratedDETERIORATED ASSISTLE HANDLE NUT ENTRY DOOR LINING AT AFT GALLEY AREA (2EA). REPLACED ASSIST HANDLE NUT ENTRY DOOR LINING AT AFT GALLEY AREA (2EA) IAW AMM 52-13-31-400-802 STEP 3.G.(2).SDR SWAA2025092611309Nut · deterioratedDETERIORATED ASSIST HANDLE NUT SERVICE DOOR LINING AT AFT GALLEY AREA (2EA) . REPLACED ASSIST HANDLE NUT SERVICE DOOR LINING AT AFT GALLEY AREA (2EA) IAW B737-700 AMM 52-13-31-400-802 STEP 3.G.(2).SDR SWAA2025092611304Angle · crackedCRACK ANGLE LOCATED ORSS282 TRAILING EDGE AT RT WING. REPLACED ANGLE LOCATED ORSS282 TRAILING EDGE AT RT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9 DWG:115A6200 SHEET:10 REV.-SDR SWAA2025092611531Beam · elongatedELONGATED HOLE ON BEAM LOCATED ORSS281 TRAILING EDGE AT LT WING 2025-549032<[01] REAMED HOLE ON BEAM LOCATED ORSS281 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-05-0G-0 FIGURE 4 SHEET 3 TABLE B.<BR>SEE INDIVIDUAL SIGNS OFF BELOW;[02] CERTIFIED ACTION 1; COSDR SWAA2025092611528Support Angle · crackedCRACK SUPPORT ANGLE LOCATED ORSS269 TRAILING EDGE AT LT WING. REPLACED SUPPORT ANGLE LOCATED ORSS269 TRAILING EDGE AT LT WING IAW SRM 51-40-02 AND #DWG: 115A2930 SHEET: 7 REV:-.SDR SWAA2025092611305Web · crackedCRACK WEB LOCATED ORSS269 TRAILING EDGE AT RT WING. REPLACED WEB LOCATED ORSS269 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-10-02-0G ITEM 9; SRM 51-40-02-0G AND DWG: 115A2982; SHEET: 4; REV: -.SDR SWAA2025092611529Web · crackedCRACK WEB LOCATED ORSS269 TRAILING EDGE AT LT WING. REPLACED WEB LOCATED ORSS269 TRAILING EDGE AT LT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9..SDR SWAA2025092611533Support Angle · crackedCRACK ON SUPPORT ANGLE ACCESS PANEL 323AL AT VERTICAL STABILIZER. REPLACED SUPPORT ANGLE ACCESS PANEL 323AL AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 DWG 172A6122 SHEET 1 REV B.SDR SWAA2025092911097Floorbeam · crackedCRACK FLOORBEAM, BS 540, LBL 1. REPLACED IAW SRM 51-40-02, AND DWG 143A0060, SHEET 64, REV -. VERIFIED CRACK LENGTH: L=0.955.SDR SWAA2025092911083Seat Track · corrodedCORRODED SEAT TRACK, BS 727B - 867, RBL 24.75, WL 208.1. REMOVED DAMAGE & EVALUATED REWORK AREA IAW SRM 53-00-52-1A-1, STEP 4 A, (2)(A), FIGURE 103, DETAIL A.SDR SWAA2025092911075Angle · corrodedCORRODED ANGLE, BS 695 + 3 INCHES, LBL 65, WL 208.1. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, & DWG 144A7713, SHEET 1, REV B.SDR SWAA2025092911072Angle · corrodedCORROSION ON ANGLE, LOCATED BS 706 + 8 INCHES, LBL 65, WL 208.1. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02-0G, AND DWG 144A7700, SHEET 130, REV A.SDR SWAA2025092911077Angle · corrodedCORROSION ANGLE LOCATED BS685 PLUS 9 INCHES RBL65 AND WL208.1 AT CENTER BOX. REPLACED ANGLE LOCATED BS685 PLUS 9 INCHES RBL65 AND WL208.1 AT CENTER BOX IAW SRM 51-40-02 AND DWG 144A7730; SHEET: 9 AND REV: ?.SDR SWAA2025092911084Angle · corrodedCORROSION ANGLE LOCATED BS685 PLUS 3 INCHES RBL65 WL208.1 AT CENTER BOX . REPLACED ANGLE LOCATED ON BS685 PLUS 3 INCHES RBL65 WL208.1 AT CENTER BOX IAW SRM 51-40-02-0G AND DWG 144A7730 SHEET 9 REV.-SDR SWAA2025092610919Crease Beam · corrodedCORROSION CREASE BEAM LOCATED BS639 LBL65 AND WL208.1 AT PASSENGER CABIN. REPLACED CREASE BEAM (INNER CHORD) LOCATED BETWEEN BS 627.5 TO BS 685 LBL 65 AND WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 5SDR SWAA2025092611085Angle · corrodedCORROSION ANGLE LOCATED BS695 PLUS 9 INCHES RBL65 AND WL208.1 AT CENTER BOX . REPLACED ANGLE LOCATED ON BS695 PLUS 9 INCHES RBL65 AND WL208.1 AT CENTER BOX IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02-0G AND DWG 144A7700 SHEET 130 REV. A.SDR SWAA2025092611095Crease Beam · corrodedCORROSION CREASE BEAM LOCATED BS639 RBL65 WL208.1 AT PASSENGER CABIN. REPLACED CREASE BEAM (INNER CHORD) LOCATED BTW BS 627.5 TO BS 663.75 + 10? RBL65 WL208.1 AT PASSENGER CABIN IAW SRM 51-10-02 ITEM 9 INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 DWG 144A59SDR SWAA2025092611089Angle · corrodedCORROSION ANGLE LOCATED BS716 PLUS 3 INCHES RBL65 AND WL208.1 AT CENTER BOX. REPLACED ANGLE LOCATED BS716 PLUS 3 INCHES RBL65 AND WL208.1 AT CENTER BOX IAW SENM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING # 144A7730; SHEET 6;SDR SWAA2025092611068Angle · corrodedCORRODED ANGLE LOCATED BS 716 PLUS 9 INCHES, LBL 65, AND WL 208.1. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 144A7700, SHEET 120, REV-.SDR SWAA2025092611073Angle · corrodedCORROSION ANGLE LOCATED BS706 PLUS 3 INCHES LBL65 AND WL208.1. REPLACED ANGLE LOCATED BS706 PLUS 3 INCHES LBL65 AND WL208.1 IAW SRM 51-10-02 ITEM 9 AND DWG 144A7730 SHEET 7 REV: -.SDR SWAA2025092611069Angle · corrodedCORROSION ANGLE LOCATED BS716 PLUS 3 INCHES LBL65 AND WL208.1. REPLACED ANGLE LOCATED BS716 PLUS 3 INCHES LBL65 AND WL208.1 IAW SRM 51-40-02 AND DWG 144A7730 SHEET 6 REV-..SDR SWAA2025092611087Angle · corrodedCORROSION ANGLE LOCATED BS706 PLUS 3 INCHES RBL65 AND WL208.1. REPLACED ANGLE AND FASTENERS LOCATED BS706 PLUS 3 INCHES RBL65 AND WL208.1 IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 144A7713 SHEET 1 REV B.SDR SWAA2025092611088Angle · corrodedCORROSION ANGLE LOCATED BS706 PLUS 9 INCHES RBL65 AND WL208.1. REPLACED ANGLE LOCATED BS706 PLUS 9 INCHES RBL65 AND WL208.1 IAW SRM 51-10-02 ITEM 9 AND DWG 144A7713 SHEET 1 REV B.SDR SWAA2025032406921Seal · crackedLEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED LH HORIZONTAL STAB FWD UPPER SLIDING SEAL IAW AMM 53-31-31SDR SWAA2025032406923Seal · delaminatedRIGHT HORIZONTAL STABILIZE LOWER FORWARD SLIDING SEAL TEFLON STRIP DELAMINATING.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-31-31-401 CONFIG 1-NG (STABILIZER TO BODY FRONT SPAR SLIDING SEAL - REMOVAL/INSTALLATION - PERMANENT)]SDR SWAA2025032406920Seal · delaminatedLEFT HORIZONTAL STABILIZER FORWARD LOWER SLIDING SEAL DELAMINATING.<[01] REMOVED AND REPLACED LH HORIZONTAL STAB FWD LOWER SLIDING SEAL IAW AMM 53-31-31SDR SWAA2024121878596Relay · failedSPEED TRIM TEMP FAIL THEN ELECTCTRIC TRIM FAIL<[01] R/R?D R64 RELAY AND STAB TRIM MOTOR REF AMM 27-41-71 AND FIM 27-41 TASK 804 OPS CHECK NORMAL. DFCS TESTS PASSED.SDR SWAA2024121878936Trim Motor · failedSPEED TRIM TEMP FAIL THEN ELECTCTRIC TRIM FAIL<[01] R/R?D R64 RELAY AND STAB TRIM MOTOR REF AMM 27-41-71 AND FIM 27-41 TASK 804 OPS CHECK NORMAL. DFCS TESTS PASSED.
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