Boeing 737-232
Service difficulty reports · 1,700
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 = '737232' 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 = '737232' 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 NACA2016081100051Flap Track · corrodedCORROSION ON THE NR 1 FLAP TRACK AT AFT SPAR ATTACH POINT. REPLACED THE NR 1 FLAP TRACK IAW AMM 27-51-151 REV 122.SDR NACA2016081100050Attach Bracket · crackedCRACKED LEFT WING TO BODY FAIRING BRACKET BS 540. REPAIRED THE BRACKET IAW SRM REV 112 SECTION 51-20-1 FIG 7.SDR NACA2016081100049Frame · crackedCRACKED FRAME WEB BS 328 BETWEEN STRINGER 20 - 21R. REPAIRED THE FRAME IAW SB 737-53A1323 REV 00.SDR NACA2016081100048Bulkhead Web · crackedAFT PRESSURE DOME CAP AT CENTER ON PRESSURE BULKHEAD CRACKED AT BS 1016, STRINGERS 7 AND 23R. REPAIRED PRESSURE BULKHEAD IAW DRAWING 4-3234689378SDR NACA2016081100047Frame · crackedCRACK INDICATION ON FRAME BS 727, STRINGER 18A LT. REPAIRED THE FRAME IAW SR 3-3621156580.SDR NACA2016081100046Attach Bracket · corrodedCORROSION ON STRINGER 25R, BS 540 STRINGER TO FRAME ATTACH BRACKET. CORROSION FOUND BEYOND LIMITS. ATTACH BRACKET REPLACED IAW SRM 51-25-01 PARA 7, FIG. 3, REV 110.SDR NACA2016081100045Angle · crackedCRACKED LEFT FUSELAGE TO FUEL TANK ANGLE BS 540, STRINGERS 20 - 21L, IN THE FORWARD CARGO BAY. REPAIRED THE ANGLE IAW DWG 65-45401 REV D AND DWG 65-45767 REV H AND REV D.SDR NACA2016081100044Floorbeam · corrodedCORRODED FLOORBEAM AT BS 520 LBL 26 AND RBL26. CHANNEL FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-10-1, REV 110. REPLACED THE CHANNEL IAW DWG 65-46803, REV E.SDR NACA2016081100043Frame · damagedDOUBLE DRILLED HOLES IN FRAME AT BS 344 STRINGERS 7 - 14L. REPLACED THE FRAME IAW DWG 65-17685.SDR NACA2016081100042Intercostal · crackedCRACK IN OUTER CHORD OF INTERCOSTAL BETWEEN STRINGERS 13-14R BS 290. REPLACED IAW SB 737-53A1241 REV 1.SDR NACA2016081100041Skin · crackedSKIN CRACKED AT RADIO ALTIMETER CUTOUT AT BS 410 BETWEEN STRINGERS 28L AND 28R. SKIN REPAIRED IAW SB 53-1230 FIG.10(A).SDR NACA2016081100040Beltframe · corrodedCORROSION ON BELTFRAME BS 1016 BETWEEN STRINGER 20 AND 21L. CORROSION FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-10-1, FIGURE 1, SHEET 11, REV 101. REPAIRED IAW SR 3-3612631720.SDR NACA2016081100039Stringer Clip · crackedCRACKED STRINGER CLIP IN UPPER FUSELAGE BS 663 STRINGER 10R. THE STRINGER CLIP WAS REPLACED IAW SB 53-1268 REV.00.SDR NACA2016081100038Floor Support · corrodedCORROSION ON FLOOR SUPPORT BS 986 - 1016 RBL 40 JUST AFT OF R2 DOOR. CORROSION FOUND TO BE BEYOND ALLOWABLE LIMITS. REPLACED IAW SRM REV.110 53-10-2, ITEM 62.SDR NACA2016081100037Keelbeam · corrodedCORROSION ON LEFT KEEL BEAM AND ADJOINING STRUCTURE BETWEEN BS 616 TO 639. REPAIRED AT C CHECK. REPAIRED LT KEEL BEAM AND ADJOINING STRUCTURE BETWEEN STA 616 TO 639 DWG R23092.1-053-016-001 REV B.SDR NACA2016081100036Keelbeam · corrodedCORROSION ON RIGHT KEEL BEAM AND ADJOINING STRUCTURE BETWEEN BS 598 TO 578. REPAIRED AT C CHECK. REPAIRED RT KEELBEAM AND ADJOINING STRUCTURE BETWEEN 598 TO 578 IAW DWG R23092.1-053-013-001 REV A.SDR NACA2016081100035Stringer Clip · crackedCRACK ON STRINGER CLIP BS 348.2, STRINGER 15L ATTACHED TO L1 DOOR FUSELAGE FRAME. REPLACED THE THE STRINGER CLIP IAW DWG 65-17685, AND SRM 51-30-2 REV 110.SDR NACA2016081100034Stringer Clip · crackedCRACKED STRINGER CLIP BS277, STRINGER 15R. THE STRINGER CLIP WAS REPLACED IAW DWG 65-45805 REV K.SDR NACA2016081100033Floorbeam · corrodedCORROSION ON UPPER AFT FLOORBEAM BS 480 BETWEEN RBL 24-45. REPAIRED THE FLOORBEAM IAW SRM REV 110 , AND 53-10-9 FIG 7.SDR NACA2016081100032Beltframe · crackedCRACK ON BELT FRAME BS 291 STRINGER 14R JUST FORWARD OF R1 DOOR. REPLACED BELTFRAME IAW DRAWING 65-45807 ID 0002 REV K.SDR NACA2016081100031Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER FLANGE LOWER BS 480 LBL 21. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG.7, REV 110.SDR NACA2016081100030Floorbeam · corrodedCORROSION ON LOWER FWD FLOORBEAM BS 500B LBL 23-20. FLOORBEAM REPLAIRED IAW SRM 53-10-09, REV 110.SDR NACA2016081100029Stiffener · crackedSTIFFENER FLANGES ON AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016 STRINGER 1, 8L, & 6R. REPAIRED THE STIFFENER IAW SERVICE REQUEST 4-3234689378, SERVICE BULLETIN 737-53A1214.SDR NACA2016081100028Stringer Clip · crackedCRACKED STRINGER CLIP AT BS 616 STRINGER 5L. THE STRINGER CLIP WAS REPLACED IAW SB737-53-1268 REV 00.SDR NACA2016081100027Beltframe · dentedDENT ON BELTFRAME UPPER FUSELAGE BS 500A STRINGER 8R. BELTFRAME REPAIRED IAW SRM 53-10-4 FIG. 1, REV 110.SDR NACA2016081100026Attach Angle · crackedCRACKED WING BOX ATTACH ANGLE BS 540-559 RBL 45-60 UNDER FLOOR. REPLACED THE ATTACH ANGLES IAW DWG 65-45401 REV K, AND SRM 51-30-2 PG 1, 3, 5 REV 110.SDR NACA2016081100025Attach Angle · crackedCRACKED WING BOX ATTACH ANGLE IN THE MAIN CABIN BS 540, LBL 32. REPLACED THE ATTACH ANGLE IAW DRAWING 65-45401 REV.KSDR NACA2016081100024Attach Angle · crackedCRACKED WING BOX ATTACH ANGLES IN THE MAIN CABIN BS 540 LBL 40. REPLACED THE ATTACH ANGLE IAW DRAWING 65-45401 REV.IC.SDR NACA2016081100023Bracket · crackedCRACKED BRACKET BS 639, STRINGER 17R, RBL 65. THE BRACKET WAS REPLACED IAW SRM 51-20-1 FIG.7, REV 110.SDR NACA2016081100022Bracket · crackedCRACKED BRACKET, MAIN CABIN BS 639, S17R, RBL 65 UNDER FLOOR. CRACKED BRACKET IN MAIN CABIN AT BS 639, S17R, RBL 65 UNDER FLOOR. SILL REPLACED WITH MADE REPAIR PART IAW SRM REV 110, SECTION 51-20-1, FIG 7.SDR NACA201608110022Beltframe · dentedDENT ON BELT FRAME IN UPPER FUSELAGE BS 500 S9R. DENT ON BELT FRAME IN UPPER FUSELAGE BS 500 S9R REPAIRED IAW SRM, REV 110, SECTION 53-10-4, FIG 1.SDR NACA2016081100021Beltframe · gougedGOUGED BELTFRAME IN UPPER FUSELAGE BS 480 BETWEEN STRINGERS 15 AND 16R. REPAIRED IAW DWG R23092.1-015-001.SDR NACA2016081100020Stiffener · corrodedCORRODED STIFFENER AT BS 553.75 RBL 39 INSIDE WHEEL WELL. THE STIFFENER WAS REPLACED IAW SRM 51-20-1, REV 110 AND 51-30-02, REV 110.SDR NACA2016081100019Mount · corrodedSURFACE CORROSION ON MARKER BEACON MOUNTING BASE, AND SEIZED HARDWARE. CORROSION FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-10-1 FIGURE 1, REV 110. REPLACED IAW DWG 65-45866 REV B, AND SRM 51-30-02, REV 110.SDR NACA2016081100018Beltframe · crackedCRACKED BELTFRAME BS 294.5 STRINGER 4L. REPAIRED THE BELTFRAME IAW SRM 53-10-4 PG 2B-2E, FIGURE 1, REV 110.SDR NACA2016081100017Strip · crackedCRACKED STABILIZER STRIP LBL 45, BS 328 UNDERFLOOR. REPAIRED CRACKED STABILIZER STRIP LBL 45, BS 328 UNDER FLOOR IAW SRM 53-10-9, PARA 4, REV 110.SDR NACA2016081100016Intercostal · crackedCRACKED FLOOR INTERCOSTAL BS344, LBL45 JUST FORWARD 9G BULKHEAD UNDER FLOOR. REPLACED FLOOR INTERCOSTAL BS 344, LBL45 JUST FWD 9G BULKHEAD UNDER FLOOR WITH MADE REPAIR PART IAW SRM, REV 110 MATERIAL IDENTIFIED IN SECTION 51-20-3, FIG 1 AND 2. FLAT PATTERN INSDR NACA2016081100015Strip · brokenBROKEN STABILIZER STRIP LBL12, BS344, UNDER FLOOR. REPAIRED BROKEN STABILIZER STRIP LBL12, BS344 UNDER FLOOR IAW SRM 53-10-9, FIG 4, REV 110.SDR NACA2016081100014Web · crackedAFT CARGO DOOR AFT CORNER WEB AND T-CHORD CRACKED. REPAIR IAW SB 52A1153, REMOVED AND REINSTALLED DOOR.SDR NACA2016081100013Skin · corrodedCORROSION ALONG LAP SEAM OF SKIN FROM STA 947 TO STA 1016 AT STR 25L. FOUND TO BE BEYOND LIMITS, SKIN MAT IDENTIFIED IAW SRM REV 112 ITEM 34. MADE REPAIR SKIN INSTALLED IAW DRAWING 65-45776 REV D. RII COMPLETED.SDR NACA2016081100012Stringer Clip · crackedCRACKED STR CLIPS IN AFT PIT RT STR 20 AND 22, BS 787. REPLACED STR CLIPS IN AFT PIT RT STR 20 AND 22, BS 787 WITH MADE REPAIR PART IAW DWG 69-353352, REV C.SDR NACA2016081100054Stringer Clip · corrodedCORRODED STRINGER CLIP AT BS 767, S20R. CORRODED STR CLIP AT BS 767 S20R. REPLACED WITH MADE REPAIR PART FABRICATED AND INSTALLED IAW SRM REV 110 51-20-01 AND 51-30-02.SDR NACA2016081100011Beltframe · corrodedCORROSION ON BELTFRAME BS 767, S20R IN AFT PIT. CORRODED BELTFRAME AT BS 767, S20R REPAIRED IAW SRM REV 110, 51-70-11, FIG 1.SDR NACA2016081100010Web · corrodedCORROSION ON FLOOR WEB IN AFT CARGO PIT BETWEEN BS 927 TO BS 907. MATERIAL ID, NEW FLOOR WEB FABRICATED AND INSTALLED AT AFT CARGO PIT BETWEEN BS 927-907, S17L IAW DWG 65-52878, REV C. MAINTENANCE PERFORMED AT C-CHECK.SDR NACA2016081100009Door Sill · corrodedCORROSION ON L2 ENTRY SILL BS847-BS986, S17L. CORROSION ON L2 ENTRY SILL BS 847-986, S17L, REPLACED PART WITH OEM PART IAW DWG 65-52878, REV B. MAINTENANCE PERFORMED AT
C-CHECK.SDR NACA2016081100008Door Sill · corrodedCORROSION ON THE DOOR SILL BETWEEN BS 967 - 986 RBL 56, R2 DOOR. THE DOOR SILL WAS REPLACED IAW DRAWING 65-52878 REV. B.SDR NACA2016081100007Skin · corrodedCORROSION LAP SEAM OF SKIN AT STA 900 TO STA 1016 STR 25R. FOUND TO BE BEYOND LIMITS. SKIN REPLACED STA 907 TO STA 1016 STR 20R TO STR 25 IAW DWG 65-45778 REV G.SDR NACA2016081100006Floorbeam · corrodedCORROSION ON LOWER FLANGE OF FLOORBEAM IN AFT CARGO BAY RBL 60 BS 787. REPAIRED IAW DWG 23092.1-053-015-001 REV A.SDR NACA20160711005Frame · crackedTHE BS 360 FRAME INSULATION BLANKET HOLE WAS DISCOVERED CRACKED AT S20R, DURING ACCOMPLISHMENT OF AD2015-28-03. FRAME REPAIR INSTALLED IAW MFG SERVICE REQUEST MESSAGE: NAC-NAC-16-0016-04B.SDR NACA201607110004Frame · crackedA PARTIALLY SEVERED FRAME WAS DISCOVERED AT BS 328, S20R-S21R, DURING THE ACCOMPLISHMENT OF AD2015-28-03. THE REPAIR/PREVENTIVE MODIFICATION ON THE BS 328 FRAME WAS ACCOMPLISHED IAW SB 737-53A1323.
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