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 7AHR201308072119Web · puncturedVERTICAL STAB POWER CONTROL UNIT LOWER WEB PUNCTURED AND CRACKED. INSTALLED THE REPAIR IAW B73751-40-2 & 51-30-2.SDR 7AHR201308072123Skin · dentedLEFT HORIZONAL STAB HAS DENT OVER TOP OF EXISTING REPAIR ON L/E. INSTALLED REPAIR IAW SRM 55-10-03.SDR 7AHR201308072272Skin · corrodedNR 1 ENGINE OTB COWL HAS CORROSION. INSTALLED REPAIR IAW SRM 51-30-02.SDR 7AHR201308072194Skin · dentedLEFT INBD FOREFLAP IS DENTED 17"-30" FROM INBD END. INSTALLED REPAIR IAW SRM 51-40-20.SDR 7AHR201308072104Seal Depressor · damagedNR 2 ENGINE INLET COWL AFT LOWER SEAL DEPRESSOR IS DAMAGED IN SEVERAL AREAS. REPAIR WAS INSTALLED IAW SRM 54-10-3, FIG 4.SDR NACA201305230001Indicator · faultyABORTED TAKEOFF DUE TO INTERMITTENT EGT NR 1 GAUGE. REMOVED AND REPLACED INDICATOR.SDR NACA2013051000001Engine · failedNR 1 ENGINE FAILURE IN FLIGHT, ENGINE SHUT DOWN. REMOVED AND REPLACED ENGINE DUE TO TURBINE FAILURE.SDR NACA2013050100001Skin · crackedCRACK IN SKIN, LOWER FORWARD CORNER RADIUS OF L2 DOOR BS 958. CRACK IN LOWER FORWARD CORNER OF L2 DOOR REPAIRED IAW B737-200 SRM 53-30-3 FIG 24 DETAIL I.SDR NACA2013040900001Transmitter · faultyTAKEOFF WAS ABORTED AT 90KTS DUE TO EXCESSIVE FUEL FLOW INDICATION ON NR 2 ENGINE. REPLACED NR 2 ENGINE FUEL FLOW TRANSMITTER, REF: B737-200MM 73-31-11.SDR NACA2013032700001Oil Filter · dirtyABORTED TAKEOFF DUE TO NR 1 ENGINE OIL FILTER BY-PASS LIGHT ILLUMINATING DURING TAKEOFF ROLL. REPLACED MAIN OIL FILTER. RAN ENGINE, NO LEAKS NOTED. P&WMM 72-61-00-430-00.SDR NACA20130402015Shear Web · crackedINNER SKIN SHEAR WEB IS CRACKED (2) PLACES & HAD CORROSION STA 348.2 - 351.2 LT STR 15-17. REPLACEMENT OF INNER SKIN SHEAR WEB STA 348.2-351.2 LT STR 15-17 IAW B737-200 DWG 65-17685 REV N.SDR NACA2013053100001Skin · dentedDENT FOUND ON SKIN AT STATION 914, STRINGER 24 R. PERFORMED HFEC ON EXISTING HOLES COMMON TO REPAIR AND FUSELAGE SKIN, NO CRACKS FOUND. INSTALLED PERMANENT REPAIR FOR DENT IAW B737 SRM 53-30-3 FIGURE 48 REVISION 105.SDR NACA20130402014Seat Track · corrodedCORROSION ON SEAT TRACK STA 380-460 CORROSION ON SEAT TRACK STA 380-460 RBL 45 BEYOND ALLOWABLE LIMITS. SEAT TRACK REPAIRED IAW B737-200 SRM 53-10-5 FIG 2 REV 105.SDR NACA20130402013Intercostal · crackedCRACK IN INTERCOSTAL ANGLE STA 278 STR 9R-18R BETWEEN. REPLACED CRACKED INTERCOSTAL ANGLE STA 278 STR 9R-18R BETWEEN IAW B737 SRM 51-10-01 PARA 7 REV 105 AND B737 SRM 51-30-02 REV 105.SDR NACA20130402012Seat Track · corrodedCORROSION ON SEAT TRACK BS 400 - 470 LBL 25.SDR NACA20130402011Seat Track · corrodedCORROSION ON SEAT TRACK BS 360 - BS 470, LBL 45. CORROSION ON SEAT TRACK REPAIRED BY REPLACEMENT IAW B737-200 SRM 51-10-5 FIG 2 REV 105.SDR NACA20130402010Floor Support · crackedCORROSION ON FLOOR SUPPORT ANGLE BS 346 LBL 61 AT L1 DOOR ORIFICE.SDR NACA20130402009Floor Support · crackedNDT DETECTED CRACK DURING OPEN HOLE PROBE AS PER SB737-57-1296, LONGITUDINAL FLOORBEAM LOWER CHORD BS 663 LBL 24, AFT HOLE.SDR NACA20130402008Floor Support · crackedNDT DETECTED CRACK DURING OPEN HOLE PROBE AS PER SB737-57- 1296, LONGITUDINAL FLOORBEAM LOWER CHORD BS 663 RBL 24, AFT HOLE.SDR NACA20130402007Floorbeam · gougedGOUGE IN LOWER FLANGE FLOORBEAM BS 294.5 LBL 50 WL 203.SDR NACA20130402006Intercostal · crackedCRACK IN INTERCOSTAL BS 327 LBL 47. REPLACED CRACKED INTERCOSTAL STA 327 LBL 47 IAW BOEING DRAWING 65-45834 REV F AND BOEING 737 SRM 51-30-2 REV 105.SDR NACA20130402005Intercostal · crackedCRACK IN INTERCOSTAL BS 329 LBL 47. REPLACE CRACKED INTERCOSTAL STA 329 LBL 47 IAW BOEING DRAWING 65-45834 REV F AND B737 SRM 51-30-2 REV 105.SDR NACA20130402004Floor Support · crackedSEVEN CRACKS FOUND IN WEB OF LONGITUDINAL FLOORBEAM BS 706-716 LBL 24. REPAIRED WEB OF LONGITUDINAL FLOORBEAM STA 706-716 LBL 24 IAW B737 SB 737-57-1296 FIG 21 REV 1.SDR NACA20130402003Floor Support · crackedFOUR CRACKS FOUND IN WEB OF LONGITUDINAL FLOORBEAM BS 706 - BS 716 RBL 24. REPAIRED WEB OF LONGITUDINAL FLOORBEAM STA 706-716 RBL 24 IAW B737 SB 737-57-1296 FIG 22 REV 1.SDR NACA20130402002Door Frame · damagedHOLE DAMAGE TO BS 248.2 FRAME INNER CHORD & INTERCOSTALS & DOORSTOPS FROM S14 TO S7 L1 DOOR ORIFICE.SDR NACA20130402001Skin · crackedCRACK ON FUSELAGE SKIN S16R BS 520. REPAIRED CRACK ON FUSELAGE SKIN STR 16R STA 520 IAW B737-200 SRM 53-30-3 FIG 48 DETAIL VII SHT 29 REV 105.SDR NACA20130401007Skin · crackedCRACK IN FUSELAGE SKIN BS 788 S17L - S16L IN BETWEEN STRINGERS. REPAIRED CRACK IN FUSEALGE SKIN STA 788 STR 17L-16L IN BETWEEN STRINGERS IAW BOEING SB737-53-1065 FIG 54 REV 2.SDR NACA20130401006Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER "T" BS 328 BS 12-35. CORROSION ON FLOORBEAM UPPER "T" STA 328 RBL 12-35 BEYOND LIMITS IAW B737 SRM 53-10-1 FIG 1 REV 105. UPPER "T" REPLACED IAW BOEING DWG 65-45812 REV L AND B737 SRM 53-10-9 FIG 5 REV 105.SDR NACA20130401005Structure · corrodedCORROSION AROUND L1 ENTRY AFT DRAIN LINE UNDERSIDE.SDR NACA20130401004Shear Tie · corrodedCORROSION ON FITTING THAT ATTACHES BELT FRAME TO THE SKIN AT BS 986.5 BETWEEN S24R AND S25R. REPLACED CORRODED SHEAR TIE THAT ATTACHES BELTFRAME TO THE SKIN AT STA 986.5 BETWEEN STRINGERS 24R AND 25R IAW BOEING DWG 65-46564 REV AB.SDR NACA20130401003Stringer · corrodedCORROSION ON S27R IN AFT CARGO PIT EQUIPMENT BAY BS 947.5. STRINGER 27R IN AFT CARGO PIT EQUIPMENT BAY STA 947.5 REPAIRED IAW BOEING 737-200 SRM 53-10-3 FIG1 REV 105.SDR NACA20130401002Floorbeam · corrodedCORROSION ON FLOORBEAM CAP UNDER CLIP NUTS BS 480 LBL 47 - LBL 62.SDR NACA20130401001Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA 535 WL 208 HAVE BEEN BLENDED OUT IAW B737-200 SRM 53-10-01. MTL THICKNESS 0.040" MTL REMOVED 0.010" MTL REMAIN 0.030" AND FOUND BEYOND LIMITS. REPLACED FLOOR SUPPORT STA 535 LBL 45-LBL IAW B737-200 SRM 51-10-1 PAGE 9 & IAW B737SDR ABXA20130222409Intercostal · crackedINTERCOSTAL CRACKED AND CORRODED RIGHT SIDE OF LOWER CARGO FLOOR BETWEEN STA 1263 AND STA 1285. REMOVED AND REPLACED LOWER CARGO FLOOR INTERCOSTAL ON RIGHT SIDE STA 1263 AND STA 1285 IAW B767 SRM 51-40-02 STEP 7(D), ACFT WAS GROUNDED.SDR NACA20130221029Stringer Splice · corrodedSTRINGER SPLICE HAS CORROSION ON IT BETWEEN BS 907 - BS 927 S19R. REPLACED STRINGER SPLICE BETWEEN STA 907-927 STR 19 IAW B737 SRM REV 105 CHAPTER 51-10-1 PARAGRAPH 7 AND CHAPTER 51-30-02.SDR NACA20130221028Intercostal · crackedCRACKED UPPER FLANGE OF INTERCOSTAL BS 348 - BS 360 LBL10. REPLACED UPPER FLANGE OF INTERCOSTAL AT STA 348-360 LBL 10 IAW B737200 SRM 511001 PARA 7 REV 105, 513002 REV 105.SDR NACA20130221027Angle · damagedFAILSAFE ANGLE ON BELT FRAME DAMAGED AT BS 986.5 BETWEEN S24R - S25R. FAILSAFE ANGLE ON BELT FRAME AT FS 986.5 REPLACED IAW BOEING DWG 6546564 REV AB.SDR NACA20130221026Intercostal · crackedCRACKED UPPER FLANGE OF FLOOR INTERCOSTAL AT BS 344 RBL 24. REPLACED CRACKED UPPER FLANGE OF FLOOR INTERCOSTAL AT STA 344 RBL 24 WITH MADE REPAIR PART IAW B737200 SRM REV 105 51201 FIG 7 MATERIAL IDENTIFIED AS 7075T6 .040 IAW SRM REV 105 53102 FIG 7 SHT 7 BACSDR NACA20130221025Fitting · corrodedCORROSION ON STRINGER FITTING 27L AT BS 1016 IN AFT CARGO PIT EQUIPMENT BAY. CORROSION ON STRINGER FITTING 27L AT FS 1016, BEYOND ALLOWABLE LIMITS, NEW FITTING INSTALLED IAW BOEING DWG 6549574 REV D.SDR NACA20130221024Door Frame · crackedCRACK FOUND ON C1 ORIFICE STOP FRAME LOWER INBOARD HOLE AT BS 420 BETWEEN S20 - S21R. CRACK ON C1 ORFICE STOP FRAME LOWER I/B HOLE AT STA 420 BETWEEN STR 2021R REPAIRED IAW B737 SRM REV 105 51403 FIG 1 AND 53102 FIG 3 AND SB 73753A1228/ FASTENERS INSTALLED IASDR NACA20130221023Floorbeam · corrodedCORROSION ON TOP FLANGE OF FLOORBEAM BS 947 RIGHT RBL 48 AT FLOORBOARD FASTENER HOLE. CORROSION ON TOP FLANGE OF FLOORBEAM STA 947 RIGHT BL 48 RIGHT AT FLOORBOARD FASTENER HOLE IS BEYOND LIMITS. FLOORBEAM REPAIRED IAW B737 DWG 5310D1577 REV IR.SDR NACA20130221022Seat Track · corrodedLIGHT CORROSION IN SEAT TRACK AT VARIOUS LOCATIONS FROM BS 927 - BS 986.5, LBL 40. CORROSION ON SEAT TRACK STA 927-986.5 BL 40 LEFT FOUND BEYOND LIMITS, NEW SEAT TRACK INSTALLED IAW B737 SRM REV 105 51-10-1 PARA 7 AND 51-30-02.SDR NACA20130221021Seat Track · corrodedCORROSION ON SEAT TRACK FLANGE AND TRACK AT SEVERAL LOCATIONS BS 927 - BS 986.5 RBL 40. CORROSION ON SEAT TRACK FLANGE STA 927986.5 RIGHT BL 40 RIGHT IS BEYOND LIMITS. NEW SEAT TRACK INSTALLED, MTRL IDENTIFIED IAW B737 SRM CHPT 53102 REV 105. NEW SEAT TRACKSDR NACA20130221020Attach Angle · corrodedCORROSION ON BELT FRAME TO SKIN ATTACH ANGLE BS 344 S26R - S27R. CORROSION ON BELTFRAME SKIN ATTACH ANGLE STA 344 STR 26R27R BEYOND LIMITS, MADE LIKE REPAIR PART IAW B737 SRM REV 105 CHAPTER 51101 PG 910. INSTALLED IAW CHAPTER 51302.SDR NACA20130221019Beltframe · corrodedCORROSION ON BELT FRAME ATTACH BS 328 S27R. CORROSION ON BELTFRAME ATTACH STA 328 STR 27R REMOVED AND FOUND TO BE BEYOND LIMITS. REPAIRED IAW B737200 SRM 53104 FIGURE 6 PG 1315 REV 105.SDR NACA20130221018Support Angle · crackedCRACKED SUPPORT ANGLE AT UPPER HINGE INTERCOSTAL FOR RIGHT FORWARD SERVICE DOOR BS 298. REMOVED & RE-INSTALLED NEW SUPPORT ANGLE AT UPPER HINGE INTERCOSTAL FOR RT SERVICE DOOR STA 298 IAW BOEING 737200 SRM 51101 REV 105 & IAW BOEING 737200 SRM 5130 REV 105 & SDR NACA20130221017Floorbeam · corrodedCORROSION ON FLOORBEAM BS 312 LBL 12 ALSO ON INTERCOSTAL SAME LOCATION AND AROUND ANCHOR NUTS. CORROSION ON FLOORBEAM STA 312 LBL 12 AND ON INTERCOSTAL SAME LOCATION AND AROUND A/NUTS REMOVED IAW B737200 SRM 511006 REV 105, NOMINAL THICKNESS .080" REMOVED .01SDR NACA20130221016Floorbeam · corrodedCORROSION OF FLOORBEAM BS 348 RBL 14 - RBL 16 TOP SEVERAL LOCATIONS AND AROUND ANCHOR NUTS. CORROSION ON FLOORBEAM STA 348 RBL 14-16 TOP CHORD SEVERAL LOCATIONS & AROUND A/NUTS REMOVED IAW B737-200 SRM 51-10-06 REV 105. NOMINAL THICKNESS WAS .080 REMOVED .03SDR NACA20130221015Floorbeam · corrodedCORROSION ON FLOORBEAM. BS 328 RBL 12 - RBL 18 TOP VARIOUS LOCATIONS AND AROUND ANCHOR NUTS. REPLACED FLOORBEAM AT STA 328 RBL WITH REPLACEMENT OF PARTS & REPAIRED IAW B737200 SRM REV 105 53109 FIG 5 SHTS 14.SDR NACA20130221014Support Angle · crackedCRACKED INTERCOSTAL SUPPORT ANGLE AT BS 348 S15L LOWER SIDE UNDERNEATH. REPAIRED CRACKED INTERCOSTAL SUPPORT ANGLE STA 348 LEFT STR 15 LWR SIDE IAW BOEING 737200 SRM 511001 REV 105 & 737200 SRM 513002 REV 105 AND WITH BOEING SERVICE BULLETIN 73753A1240.
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