Boeing 737-76N
Service difficulty reports · 4,807
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '73776N' 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 aircraft_model_key = '73776N' 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 SWAA2024020539669Support Angle · crackedFWD CABIN FLOOR STRUCTURE BETWEEN STA 380 AND 400 LBL 13 WL 208.1 INTERCOSTAL UPPER FLOOR SUPPORT ANGLE IS CRACKED. 124-053<[01] REMOVED AND INSTALLED NEW ANGLE SUPPORT UPPER INTERCOSTAL AT FWD CABIN FLOOR STRUCTURE BETWEEN STA. 380 TO 400 LBL. 13' WL 208.1 RESDR SWAA2024020539812Support Angle · crackedFWD CABIN FLOOR STRUCTURE BETWEEN STA 380 AND 400 RBL 8.5 WL 208.1 INTERCOSTAL UPPER FLOOR SUPPORT ANGLE IS CRACKED. 124-054<[01] REMOVED AND REPLACED NEW INTERCOSTAL UPPER ANGLE AT MAIN CABIN BETWEEN STA 380 TO 400 RBL 8.5 WL 208.1 MIXED TIME SEALANT 10:00AM SDR SWAA2024012339784Sign · brokenMAIN CABIN AFT LOWERED CEILING PANEL EXIT LIGHT SINGS BROKEN.<[01] REMOVED AND REPLACED MAIN CABIN AFT LOWERED CEILING PANEL EXIT LIGHT SIGN AS PER AMM 33-51-01-960-802.;[02] REMOVED AND REPLACED MAIN CABIN AFT LOWERED CEILING PANEL EXIT LIGHT SIGN AS PER AMM SDR SWAA2024012439148Seat Track · corrodedMAIN CABIN SEAT TRACK AT STA 380 TO STA 390 LBL 48 DIRTY MAIN CABIN SEAT TRACK AT STA 380 TO STA 390 LBL 45.5 DIRTY AND CORRODED.<[01] REMOVED AND INSTALLED NEW SEAT TRACK AT MAIN CABIN FROM STA 360 TO STA 480 LBL 45.50 PER SRM 51-40-02-0G-0 AND DWG 143A5300;[SDR SWAA2024020538521Floor Panel · peelingMAIN CABIN AFT WET AREA FLOOR PNL 241ABF UPPER SURFACE DELAMINATED<[01] RECEIVED NEW AFT WET AREA FLOOR PANEL 241ABF; PANEL WILL BE INSTALLED ON TTG8Q00PGLTN.;[02] VERIFIED STEP 1SDR SWAA2024020537081Door Sill · crackedFOUND CRACK AT LH INNER CHORD L-1 DOOR SILL AREA STA 303.9<[01] REMOVED AND REPLACED INNER CHORD AT L1 DOOR BETWEEN STA 277 TO 360 SRM 51-40-02-0G-0 AND DWG 141A8110;[02] VERIFIED STEP 1SDR SWAA2024013136056Floor Panel · delaminatedCABIN FLOOR PANEL 232QF UPPER SKIN AFT EDGE DENTED/DELAMINATED 1' SQUARE APPROX.<[01] INSTALLED FLOOR PANEL 232QF AS PER B737 AMM 53-21-00-400-801.;[02] CORRECTION: RECEIVED AND INSTALLED NEW PANEL 232QF.<BR>P/N: 143A5810-110. PO#2051706 AS PER B737 AMM 53-21-SDR SWAA2023122735613Transmitter · incorrectTRAILING EDGE FLAPS DISAGREE ON APPROACH. TRAILING EDGE FLAPS INDICATE 13 DEGREES WITH FLAP HANDLE AT 30 DEGREES.<[01] R&R'D L/H FLAP POSITION X-MITTER PER AMM 27-58-01. OPS CHK NORMALSDR SWAA2024020535400Seal · damagedR/H HORIZONTAL STAB. UPPER ACCESS PANEL # 343AT HAS 2 EA RUBBER SEAL WITH ELONGATED HOLES<[01] REMOVED AND REPLACED R/H HORIZONTAL STAB. UPPER ACCESS PANEL # 343AT BOTH RUBBER SEAL AS BER 51-40-02-0G-0;[02] CORRECTION TO STEP ONE SHOULD READ;<BR>REMOVED AND RESDR SWAA2024020535396Floor Support · corrodedAFT CARGO FLOOR SUPPORT AT B/S 887 22' RIGHT TO 8' LEFT IS CORRODED.<[01] REMOVED AND REPLACED TEE ASSY (PN: 146A9401U39 PO: 1728471) AT AFT CARGO COMPT STA 887; LBL 8 TO RBL 22; PER REF SRM 51-40-02-0G-0 AND DWG #146A7500;[02] VERIFIED STEP 1SDR SWAA2024020535398Web · corrodedAFT CARGO THRESHOLD WEB HAS LIGHT CORROSION<[01] REMOVED CORROSION AT AFT CARGO COMPT THRESHOLD WEB FROM STA 794.37 TO STA 847; RBL 23 TO RBL 28; PER REF SRM 51-10-02-0G-0.EVALUATED REWORKED AREA. ORIGINAL MATERIAL THICKNESS: 0.050'; MATERIAL LOST: 0.007; REMASDR SWAA2024020535466Door · corroded***CORROSION*** AT LH INNER CORE FROM STA 312 TO 344; SEVERAL SPOTS OF CORROSION. DOT 82-010.<[01] THE DISCREPANCY WAS COMPLETED IN THE [TTG8Q00QNCTV] SRM 51-40-02-0G-0 AND DWG 141A8110;[02] CORRECTIVE ACTION WAS RESOLVED ON TTG8Q00QNCTVSDR SWAA2024020535110Frame · corrodedCORROSION....R/H CABIN FLOOR FRAME @ STA 1016 RBL 34 WL 208.1 FASTENER HOLE HAS CORROSION. (18-021)<[01] ACCOMPLISHED REPAIR AT RT. CABIN FLOOR FRAME STA 1016 RBL 34 WL 208.1; PER EA24-153-00155-WIP1; EA24-153-00155-WIP2; AND EA24-153-00155-WIP3;[02] VERIFIED SDR SWAA2024020535104Skin · crackedCRACK FOUND AT LT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90; CRACK LENGTH 0.750'; I/B OF I/B FASTENER ROW; 16.5' FROM L/E. CRACK FOUND AT LT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90 CRACK LENGTH 0.750' I/B OF I/B FASTENER ROW 16.5' FROM L/E.<[01SDR SWAA2024020239482Support Bracket · crackedPNEUMATIC CROSSOVER DUCT R/H SUPPORT BRACKET CRACKED<[01] REMOVED AND REPLACED PNEUMATIC CROSSOVER DUCT R/H SUPPORT BRACKET IN REF TO B737 SRM 51-40-02-0G-0.;[02] VERIFIED REPLACEMENT OF BRACKET.SDR SWAA2024013135042Support Bracket · crackedPNEUMATIC CROSSOVER DUCT L/H SUPPORT BRACKET CRACKED<[01] REMOVED AND REPLACED PNEUMATIC CROSSOVER DUCT L/H SUPPORT BRACKET IN REF TO B737 SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2024020534834Floor Panel · peelingMAIN CABIN FLOOR PANEL 241UF UPPER SURFACE HAS PEELED FIBERS (017)<[01] FLOOR PANEL 241UF WILL BE ACCOMPLISHED ON TTG8Q00QKN94.;[02] STEP 1: ENTER IN ERROR.<BR>FLOOR PANEL 241UF WILL BE ACCOMPLISHED ON TTG8Q00QGLV7.;[03] VERIFIED CORRECTIVE ACTION; STEP 2.SDR SWAA2024020534825Floor Panel · peelingMAIN CABIN FLOOR PANEL 241ACF UPPER SURFACE HAS PEELED FIBERS (014)<[01] RECEIVED NEW FLOOR PANEL 241ACF; P/N D104MM0003-311.<BR>PO# 2052116.<BR>PANEL 241ACF WILL BE INSTALLED ON TTG8Q00PGLTL.;[02] VERIFIED STEP 1SDR SWAA2024020534838Floor Panel · peelingMAIN CABIN FLOOR PANEL 242UF UPPER SURFACE HAS PEELED FIBERS (015)<[01] RECEIVED AFT WET AREA FLOOR PANEL 242UF; PANEL WILL BE INSTALLED ON TTG8Q00PGM33.;[02] VERIFIED STEP 1SDR SWAA2024020534832Floor Panel · peelingMAIN CABIN FLOOR PANEL 241AAF UPPER SURFACE HAS PEELED FIBERS (016)<[01] RECEIVED AFT WET AREA FLOOR PANEL 241AAF; PANEL WILL BE INSTALLED ON TTG8Q00PGLTQ.;[02] VERIFIED STEP 1SDR SWAA2024020534835Floor Panel · corrodedMAIN CABIN FLOOR PANEL 241C HAS CORRODED INSERTS (011)<[01] REMOVED AND REPLACED BROKEN INSERTS AT MAIN CABIN FLOOR PANEL 241C REF. SRM. 53-00-50-2R-0;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2024020534823Floor Panel · corrodedMAIN CABIN FLOOR PANEL 242VF HAS CORRODED INSERTS (004)<[01] REMOVED AND REPLACED. INSERTS BROKEN AT MAIN CABIN FLOOR PANEL 242VF. REF. SRM. 53-00-50-2R-0;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2024020534824Floor Panel · corrodedMAIN CABIN FLOOR PANEL 241ACF HAS CORRODED INSERTS (005)<[01] THIS ITEM WILL BE ACCOMPLISHED ON TTG8Q00QGLT3; RECEIVED NEW FLOOR PANEL 241ACF.;[02] VERIFIED STEP 1SDR SWAA2024020534837Floor Panel · corrodedMAIN CABIN FLOOR PANEL 241ADF HAS CORRODED INSERTS (006)<[01] REMOVED AND REPLACED BROKEN INSERTS AT MAIN CABIN FLOOR PANEL 241ADF REF.SRM. 53-00-50-2R-0;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2024020534827Floor Panel · corrodedMAIN CABIN FLOOR PANEL 242UF HAS CORRODED INSERTS (003)<[01] PANEL 242UF WILL BE REPLACED ON TTG8Q00QGN40;[02] VERIFIED STEP 1SDR SWAA2024020534829Floor Panel · corrodedMAIN CABIN FLOOR PANEL 242B HAS CORRODED INSERTS (001)<[01] REMOVED AND REPLACED INSERTS BROKEN AT MAIN CABIN FLOOR PANEL 242B. REF. SRM. 53-00-50-2R-0;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2024020534830Floor Panel · corrodedMAIN CABIN FLOOR PANEL 241ABF HAS CORRODED INSERTS (009)<[01] PANNEL ASSY 241ABF WILL BE RE PLACED ON ITEM TTG8Q00QSA0K;[02] VERIFIED STEP 1SDR SWAA2024020534839Floor Panel · corrodedMAIN CABIN FLOOR PANEL 241AAF HAS CORRODED INSERTS (008)<[01] THIS ITEM WILL BE ACCOMPLISHED ON TTG8Q00QGLV0.;[02] VERIFIED STEP 1SDR SWAA2024020534392Support Frame · crackedFWD CABIN WET AREA FUSELAGE SUPPORT FRAME CRACKED @ CUTOUT ABOVE L-1 DOOR FWD STA 312 MKD DOT<[01] ACCOMPLISHED REPAIR FOR EA NO:M-22-153-01244;[02] VERIFIED REPAIR ACCOMPLISHED PER EA NO: M-22-153-01244;[03] VERIFIED REPAIR ACCOMPLISHED PER EA NO: M-22-153-01SDR SWAA2024020534397Floor Panel · peelingCABIN FLOOR PANEL 231BF HAS PEELED UPPER SURFACE FIBERS. 124-028<[01] RECEIVED FLOOR PANEL #231BF WITH P/N: 141A5810-168. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00PGM3P;[02] VERIFIED STEP 1.SDR SWAA2024020534626Floor Panel · peelingCABIN FLOOR PANEL 231AF HAS PEELED UPPER SURFACE FIBERS. 124-030<[01] RECEIVED CABIN FLOOR PANEL 231AF WILL BE INSTALLATION WILL BE ACCOMPLISHED ON TTG8Q00PGM3R;[02] RECEIVED CABIN FLOOR PANEL 231AF WILL BE INSTALLED ON TTG8Q00PGM3R;[03] VERIFIED STEP 2 (CORRESDR SWAA2024020534627Floor Panel · peelingCABIN FLOOR PANEL 222BF HAS PEELED UPPER SURFACE FIBERS. 124-024<[01] RECEIVED FLOOR PANEL #222BF; WITH P/N:141A5810-507. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00PGLLD.;[02] VERIFIED STEP 1.SDR SWAA2024020534618Floor Panel · peelingCABIN FLOOR PANEL 221EF HAS PEELED UPPER SURFACE FIBERS. 124-027<[01] RECEIVED PANEL: 221EF P/N: 141A5810-526 INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD: 'TTG8Q00PGM44';[02] VERIFIED STEP 1.SDR SWAA2024020534628Floor Panel · peelingCABIN FLOOR PANEL 221BF HAS PEELED UPPER SURFACE FIBERS. 124-032<[01] RECEIVED FLOOR PANEL #221BF WITH P/N: 141A5810-56. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00PGM4B;[02] VERIFIED STEP 1.SDR SWAA2024020534625Floor Panel · peelingCABIN FLOOR PANEL 222A HAS PEELED UPPER SURFACE FIBERS. 124-031 CABIN FLOOR PANEL 222AF HAS PEELED UPPER SURFACE FIBERS. 124-031<[01] RECEIVED CABIN FLOOR PANEL 222A WILL BE INSTALLATION WILL BE ACCOMPLISHED ON TTG8Q00PGLLF;[02] RECEIVED CABIN FLOOR PANEL 222ASDR SWAA2024020534633Floor Panel · peelingCABIN FLOOR PANEL 222CF HAS PEELED UPPER SURFACE FIBERS. 124-025<[01] RECEIVED CABIN FLOOR PANEL 222DF WILL BE INSTALLED ON TTG8Q00PGM3W;[02] RECEIVED CABIN FLOOR PANEL 222CF WILL BE INSTALLED ON TTG8Q00PGM3W;[03] VERIFIED STEP 2 (CORRECTION FOR STEP 1)SDR SWAA2024020534395Support Angle · corrodedCORROSION AT AFT CABIN GALLEY DOOR R-2 CUTOUT LOWER SILL SCUFF PLATES SUPPORT ANGLE MKD DOT<[01] REF TASK CARD TTG8Q00QHCG5 FOR REMOVAL OF CORROSION AT R/H MAIN CABIN INNER CHORD.;[02] MEASUREMENTS WILL BE RECORDED ON TTG8Q00QHCG5;[03] VERIFIED STEPS 1 AND 2;[SDR SWAA2024020534617Floor Panel · corrodedCABIN FLOOR PANEL 221DF HAS CORRODED INSERTS. 124-023<[01] RECEIVED NEW FLOOR PANEL 221DF; PANEL WILL BE INSTALLED ON <BR>TTG8Q00PGM47.;[02] VERIFIED STEP 1SDR SWAA2024020534619Floor Panel · corrodedCABIN FLOOR PANEL 221CF HAS CORRODED INSERTS. 124-022<[01] RECEIVED NEW FLOOR PANEL 221CF; PANEL WILL BE INSTALLED ON TTG8Q00PGM49.;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2024020534383Fitting · damagedR/W REAR SPAR T/E LOWER WIGGLE FITTING HAS SHEARED RIVETS AND ELONGATED HOLE O/B OF FLAP TRACK # 6 MKD DOT<[01] REMOVED AND REPLACED WIGGLE FITTING AT R/W REAR SPAR T/E LOWER SRM 51-40-92-0G-0 AND DWM 115A2781;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2024020534218Support Angle · crackedLH DEFLECTION CONTROL RIB AND SUPPORT BEAM HAS UPPER MIDDLE SUPPORT BULB SEAL CRACKED.<[01] REMOVED AND REAPLACED SUPPORT ANGLE AT L/H DEFLECTION CONTROL RIB PER REF SRM 51-40-02-0G-0 SRM 51-40-05-0G-0;[02] CW;[03] VERIFIED CORRECTIVE ACTION.SDR SWAA2024012433390Frame · crackedSTA. 312 FRAME CRACKED ABOVE L1 DOOR FWD CORNER.<[01] ACCOMPLISHED REPAIR AT STA 312 ABOVE L1 DOOR PER M-22-153-01244;[02] VERIFIED REPAIR PER M-22-153-01244SDR SWAA2024012433202Floor Support · corrodedAFT CARGO FLOOR SUPPORT AT B/S 767-787 IS CORRODED 23' RIGHT OF CENTER LINE.<[01] REMOVED AND REPLACE AFT CARGO FLOOR SUPPORT STRAP AT B/S 767-787 (P/N:146A9401U21) REF. SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2024012932494Rib · crackedRH WING T/E RIGHT ABOVE #2 ENGINE AFT FAIRING TIP THERE IS A RIB CRACKED AT THE BOTTOM BOLT ATTACHMENT HOLE. DOT 82-002.<[01] THIS N/R WAS ACCOMPLISHED ON N/R: TTG8Q00Q7JM0.;[02] VERIFIED STEP 1SDR SWAA2024012632192Stiffener · crackedRH HORIZ. STAB RIB 4 STIFFNER 4 SUSPECT CRACK RH HORIZ. STAB RIB 4 STIFFNER 4 CRACKED<[01] ACCOMPLISHED REPAIR AT RH HORIZ. STAB RIB 4 STIFFNER 4 AS PER SRM 55-10-09-2R-5 REPAIR 5.;[02] VERIFIED REPAIR INSTALLATION AT RH HORIZ. STAB RIB 4 STIFFNER 4.SDR SWAA2024012532386Strap · corroded***CORROSION*** AFT WET AREA AT STA 1016+8' RBL20 WL 208.1. DOT 82-012.<[01] REMOVED AND INSTALLED NEW STRAP AT AFT WET AREA STA.1016+8 RBL20 ASPER REF. B737-SRM 51-40-02-0G-0 AND DWG# 147A5700;[02] RII -- VERIFIED 1.SDR SWAA2024012532387Strap · corroded***CORROSION*** AFT WET AREA AT STA 1016 RBL3 WL 208.1. DOT 82-013.<[01] REMOVED AND REPLACE STRAP AT AFT WET AREA AT STA 1016 RBL3 WL 208.1<BR>AS PER REF. B737.700- SRM-51-40-02-0G-0 AND DWG- 147A5600.;[02] VERIFIED STRAP REPLACEDSDR SWAA2024012432376Floor Support · crackedFWD CABIN BETWEEN STA 277 AND STA 294.5 AT BL-0 WL 208.1 INTRCOSTAL CRACKED. DOT 124-001<[01] REMOVED AND INSTALLED NEW INTERCOSTAL P/N 141A5410-3 PO# 2028887 AT FWD CABIN BETWEEN STA 277 AND STA 294.5 AT BL-0 WL 208.1 AS PER SRM-51-40-02-0G-0 AND DWG #141A541SDR SWAA2024012432377Floor Support · crackedFWD CABIN BETWEEN STA 312 AND STA 328 RBL 31 WL 208.1 INTERCOSTAL CRACKED 124-003<[01] REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 312 AND STA 328 RBL 31 WL 208.1 AS PER SRM 51-40-02-0G-0 DWG 141A5400;[02] VERIFIED NEW INTERCOSTAL INSTALLEDSDR SWAA2024012432380Floor Support · crackedFWD CABIN BETWEEN STA 380 AND STA 400 BL-0 WL 208.1 INTERCOSTAL CRACKED 124-009<[01] INSTALLED NEW INTEWRCOSTAL AT ABIN BETWEEN STA 380 AND STA 400 BL-0 WL 208.1 PER SRM 51-40-02-0G-0 DWG 143A5400;[02] CORRECTING STEP 1: INSTALLED NEW INTERCOSTAL AT FWD CABIN
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