Boeing 737-4B7
Service difficulty reports · 5,757
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 = '7374B7' 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 = '7374B7' 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 USAA060062Support Angle · crackedFOUND SUPPORT ANGLE CRACKED STA 616, RBL 64.5. REMOVED DAMAGE, FAB AND INSTALLED DOUBLER PER TYPICAL REPAIR 53-62-01 FIG 2. DEFECT SIZE: CABIN AT EMERGENCY EXIT STA 616, RBL 64.5 SUPPORT ANGLE CRACKED, CRACK IS 0.25SDR USAA060063Stringer Clip · crackedFOUND STRINGER CLIP CRACKED 11R AT BS 500. REMOVED AND INSTALLED NEW FABRICATED TIE CLIP IAW BOEING DWG 69-45156 AND SRM 51-10-02, DEFECT SIZE: STRINGER 11R TIE CLIP CRACKED IN RADIUS, APPROX 0.250".SDR USAA060054Frame · tornFWD CARGO DOOR CUT-OUT FWD FRAME, FABRICATED WEB REPAIR PER SRM 51-70-13 FIG 1, DEFECT SIZE: .125.SDR USAA060065Frame · crackedFOUND FRAME CRACKED STA 440 AT RT PSU SUPPORT RAIL. INSTALLED FILLER AND DOUBLERS IAW TR 53-10-20C, DEFECT SIZE: .250" CRACK.SDR USAA060053Attach Angle · crackedFOUND ATTACH ANGLE CRACKED, STA 727B 0BL. FABRICATED NEW ANGLE AND INSTALLED SRM 51-10-02 DWG 65-45410, DEFECT SIZE: 1.00".SDR USAA060067Repair · unknownFOUND PREVIOUS REPAIR L/E 81" O/B OF I/B END. UPDATED SDA AS REQUIRED IAW SRM 55-10-01, DEFECT SIZE: PREVIOUS REPAIR FOR RT HORZIONTAL REMOVABLE L/E 81" O/B OF I/B END, FLUSH PATCH.SDR USAA060068Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR, L/E 38" O/B OF I/B END. MAJOR REPAIR, UPDATED SDA AS REQUIRED SRM 55-10-01. DEFECT SIZE: PREVIOUS REPAIR ON SDA FOR LEFT HORIZONTAL REMOVE L/E 38" O/B OF I/B END FLUSH PATCH.SDR USAA060069Skin · damagedABOVE RSS 140, 6" OUTBD OF FUSELAGE, UPPER WING SKIN, BLENDED DAMAGE OUT SHOT PEENED AND TREATED SKIN PER SRM 51-20-06 FIG 1, DEFECT SIZE: 7.0" BY 2.25" AREA, CHAFFED SKIN.SDR USAA060070Skin · gougedFOUND DEEP GOUGE AFT CARGO DOOR SKIN ABOVE HANDLE CUTOUT. REMOVED DAMAGED, INSTALLED FILLER AND DOUBLER IAW SRM 52-30-01, 52-00-01, DEFECT SIZE: 2.00" BY .016" DEEP GOUGE.SDR USAA060071Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR, OUTER DOOR SKIN. UPDATED SDA AS REQUIRED IAW SRM 52-30-01, DEFECT SIZE: 34" BY 43".SDR USAA060072Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR, 178 BULKHEAD. UPDATED SDA IAW EO 5300V153 DEFECT SIZE: UNKNOWN.SDR USAA060073Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR, I/B END LWR SURFACE. SDA UPDATED AS REQUIRED IAW TR 57-50-26A, DEFECT SIZE: UNKNOWN.SDR USAA060074Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR I/B END UPPER SURFACE. UPDATED SDA AS REQUIRED IAW TR 57050-26A, DEFECT SIZE: 10 BY 4.SDR USAA060075Repair · unknownFOUND SLAT SKIN WITH PREVIOUS REPAIR LWR SURFACE AT I/B AUX TRACK. SDA UPDATED AS REQUIRED IAW TR 54-43-01, DEFECT SIZE: 12" BY 4".SDR USAA060064Structure · crackedFOUND SLAT CRACKED OTBD END, LOWER SURFACE AT AFT FASTENER ROW, 3.5" BY 8" DOUBLER ON OUTBD END INSTALLED IAW SRM 57-43-01 AND 57-56-22, DEFECT SIZE: APPROX TOT ACCUMULATIVE LENGTH 0.375".SDR USAA060044Attach Angle · crackedFOUND ATTACH ANGLE CRACKED STA 737B 0BL. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 51-10-02 DWG 65-45410, DEFECT SIZE: 1.00".SDR USAA060033Frame · crackedFOUND FRAME CRACKED STA 787 FRAME BETWEEN S8L AND S9L. REPAIRED AND INSTALLED DOUBLER IAW TR 53-10-20C, DEFECT SIZE: .125".SDR USAA060034Frame · crackedFOUND FRAME CRACKED 827 S9R AT I/B PSU SUPPORT BRACKET RIVET. INSTALLED DOUBLER IAW 53-10-20-C, DEFECT SIZE: .500".SDR USAA060035Frame · crackedFOUND FRAME 787 CRACKED AT I/B PSU SUPPORT RIVET S9R. INSTALLED REPAIR ANGLES PER TR 52-10-20C, DEFECT SIZE: .500".SDR USAA060036Floorbeam · corrodedFOUND FLOORBEAM CORRODED AT BS 986.5 AND LBL 8 TO RBL 43. REMOVED DAMAGE AND INSTALLED FABRICATED T CAP FROM LBL 6 THRU RBL 30 IAW SRM 53-60-01A, DEFECT SIZE: 6".SDR USAA060037Wedge · unknownFABRICATED DOUBLER THAT MEASURES 3" BY 5" IAW 57-42-02, NR 2 SLAT UPPER O/B T/E WEDGE SURFACE, DEFECT SIZE: 3" BY 5".SDR USAA060038Skin · crackedFOUND SKIN CRACKED STA 179 BETWEEN S-16 AND S-15L. FABRICATED DOUBLER 3" BY 5" IAW EO 5300V157, DEFECT SIZE: 3" BY 5".SDR USAA060039Wedge · unknownUPPER I/B T/E WEDGE SURFACE, FABRICATED DOUBLER THAT MEASURES 3" BY 5" IAW 57-42-01, DEFECT SIZE: 3" BY 5".SDR USAA060040Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR STA 179 BETWEEN S16R AND S15R. SDA UPDATED AS REQUIRED IAW EO 5300V157, DEFECT SIZE: 3" BY 5".SDR USAA060041Repair · unknownFOUND NR 1 ENGINE NOSE COWL AT 4 O'CLOCK POSITION. UPDATED SDA AS REQUIRED IAW SRM 54-10-01, DEFECT SIZE: 5" BY 8".SDR USAA060055Skin · delaminatedFOUND DELAMINATION UPPER OTBD END OF T/E WEDGE. REMOVED DAMAGE INSTALLED CORE AND DOUBLER IAW SRM 51-70-10, DEFECT SIZE: 4.750" BY 5.250.SDR USAA060043Skin · crackedFOUND NR 1 SLAT CRACKED, FASTENER HOLES LOWER SURFACE T/E. INSTALLED EXTERNAL DOUBLER IAW BOEING SRM 57-43-01, DEFECT SIZE: .050".SDR USAA060032Stringer Clip · crackedFOUND TIE CLIP CRACKED AT BS 400 AND STRINGER 16R . REMOVED AND REPLACED WITH A FABRICATED TIE CLIP IAW SRM 51-10-02, DEFECT SIZE: 1".SDR USAA060045Support · corrodedFOUND SUPPORT CORRODED, STA 313-328 RBL 12. REMOVED AND REPLACE WITH NEW PART IAW SRM 51-10-02, DEFECT SIZE: 1.000".SDR USAA060046Floorbeam · corrodedFOUND FLOORBEAM CORRODED STA 312 FROM BLO 0 TO RBL 10.10" BY 2". INSTALLED T CAP IAW SRM 53-10-51 FIG 201, DEFECT SIZE: 10.10" BY 2".SDR USAA060047Floorbeam · corrodedFOUND FLOORBEAM CORRODED, BS 927 AND RBL 10. CUT OUT TO REMOVE DAMAGE AND INSTALLED REPAIR ANGLE PER SRM 53-60-51, DEFECT SIZE: UNKNOWN.SDR USAA060048Skin · crackedFOUND NR 1 SLAT CRACKED, FASTNER HOLE LOWER SURFACE T/E. INSTALLED EXTERNAL DOUBLER IAW SRM 57-43-01, DEFECT SIZE: .050".SDR USAA060049Shear Tie · crackedSHEAR TIE CRACKED BS 967 BETWEEN S-6L AND S7-L. REMOVED DAMAGED SECTION OF FRAME. FABRICATED AND INSTALLED REPAIR SHEAR TIE IAW SRM 53-00-07-2R-07, DEFECT SIZE: 1.5".SDR USAA060050Stringer Clip · crackedFOUND TIE CLIP CRACKED, BS 312 S-27L. FABRICATED AND INSTALLED NEW TIE CLIP IAW SRM 51-40-03 AND 02 AND BOEING DRW 69-37411, DEFECT SIZE: .25".SDR USAA060051Splice · crackedFOUND CRACK STA 908 STR 4 R. REPLACED SPLICE IAW SRM 51-10-02, DEFECT SIZE: .125".SDR USAA060052Splice · crackedFOUND CRACK BS 908 AND S41L. FABRICATED SPLICE AND INSTALLED STRINGER SPLICE AND NEW TIE CLIP PER SRM 51-10-02, DEFECT SIZE: .250".SDR USAA060042Repair · unknownPREVIOUS REPAIR UPPER IB T/E. UPDATED SDA AS REQUIRED IAW TR 57-42-02 DEFECT SIZE: 5" BY 5".SDR USAA060013Frame · crackedFOUND CRACK STA 440, S-8L. FABRICATED ANGLES FROM NR 1133534 AND 1133533, INST DOUBLERS IAW TR 53-10-20C, DEFECT SIZE: 0.25" CRACK.SDR USAA060007Frame · defectiveBS 639 FRAME AT OVERWING DOOR STOP LT SIDE, DEFECTIVE PART REPLACED WITH IDENTICAL PART:ORDERED "T" ANGLE 1717710 STOCK, FAB`D REPLACED IAW DWG65-46450, DEFECT SIZE: 1.5 INCH BY 1.5 INCH MISSING T-ANGLE (MISSING SINCE MANUFACTURE).SDR USAA060006Frame · crackedFOUND CRACK BS 727F BETWEEN S-8R AND S-9R AT AIRCONDITIONAL ATTACH BRACKET. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANLGE IAW TR 53-10-20C, DEFECT SIZE: APPROX 1/2" CRACK.SDR USAA060005Attach Angle · crackedFOUND ANGLE CRACKED BS 877; S-11L. REMOVED CRACKED ANGLE. FABRICATED AND INSTALLED NEW ANGLE IAW BOEING DRW 69-45156; SRM 51-10-02, DEFECT SIZE: APPROX 1/4" CRACK.SDR USAA060012Angle · crackedFOUND ANGLE CRACKED BETWEEN STA 927 AND 947.5 AT BL 0. INSTALLED NEW ANGLE IAW SRM 51-40-02, DEFECT SIZE: 1" CRACK.SDR USAA060014Frame · crackedFOUND FRAME CRACKED STA 907, BELOW S-8L. FAB`D FROM ANGLES NR 1133534 AND 1133533. INSTALLED DOUBLERS IAW TR 53-10-20C, DEFECT SIZE: FRAME CRACKED 0.25".SDR USAA060015Stringer Clip · crackedFOUND TIE CLIP CRACKED S-4R, BS 727E. INSTALLED NEW CLIP CC NR 1133482. INSTALLED IAW SRM 51-10-02, DEFECT SIZE: SHEETMETAL NR 5958 S-4R TIE CLIP CRACKED BS 727E.SDR USAA060009Splice · crackedFOUND STRINGER SPLICE CRACKED STA 907, S-4L. REMOVED AND REPLACED WITH NEW PART IAW SRM 51-10-02, DEFECT SIZE: .500" CRACK.SDR USAA060016Floorbeam · corrodedFOUND SHEET METAL CORRODED ON FLOORBEAM STA 328 RBL 21. INSTALLED DOUBLER IAW SRM 53-00-51 FIG 201, DEFECT SIZE: SHEETMETAL ITEM 1030M EVIDENCE OF CORROSION ON FLOORBEAM 1" BY 2", STA 328 RBL 21.SDR USAA060010Floor Panel · unknownLOCATION, COCKPIT ENTRY FLOOR, REMOVED AND REPLACED W/NEW PART KIT IAW SRM 51-10-02, DEFECT SIZE: SHEETMETAL ITEM 1036, NOSE GEAR DOWN LOCK VIEW SUP STRUCTURE CRACKED ON FWD END.SDR USAA060011Floorbeam · corrodedFOUND FLOORBEAM CORRODED BS 986.5 CABIN FLOORBEAM LBL 18, 21,24,30. REPLACED "T" CAP IAW TR 53-60-01A, DEFECT SIZE: SEVERAL 1" BY 1" CORRODED AREAS.SDR USAA0613Frame · crackedSTA 440, S-8L CRACKED. FABRICATED ANGLES FROM 1133534 & 1133533, INSTALLED DOUBLERS IAW TR 53-10-20C, DEFECT SIZE: 0.25 INCH CRACK.SDR USAA068Frame · defectiveBS 639 FRAME & OVERWING DOOR STOP RIGHT SIDE DEFECTIVE. PART REPLACED WITH IDENT PART: ORDERED T-ANGLE 1717710 STOCK FAB & INSTALLED PER DWG 65-46450, DEFECT SIZE: 1.5 INCH BY 1.5 INCH MISSING T-ANGLE (MISSING SINCE MANUFACTURE).
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