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.

SDR USAA067Frame · defectiveBS 639 FRAME AT OVERWING DOOR STOP LT SIDE DEFECTIVE. DEFECTIVE PART REPLACED WITH IDENTICAL PART: ORDERED T- ANGLE 1717710 STOCK,FAB REPLACED IAW DWG65-46450, DEFECT SIZE: 1.5 INCH BY 1.5 INCH MISSING T-ANGLE (MISSING SINCE MANUFACTURE).Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA066Frame · crackedBS 727F BETWEEN S-8R & S-9R AT AIR CONDITION ATTACH BRACKET CRACKED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE IAW TR 53-10-20C, DEFECT SIZE: APPROX .5 INCH CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA065Attach Angle · crackedBS 877; S-11L CRACKED. REMOVED CRACKED ANGLE. FABRICATED & INSTALLED NEW ANGLE IAW BOEING DRW 69-45156; SRM 51-10-02, DEFECT SIZE: APPROX .25 INCH CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA0612Angle · crackedBETWEEN STA 927 AND 947.5 AT BL 0 CRACKED. INSTALLED NEW ANGLE IAW SRM 51-40-02, DEFECT SIZE: 1 INCH CRACKED.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA0614Frame · crackedSTA 907, BELOW S-8L CRACKED. FAB FROM ANGLES 1133534 & 1133533, INSTALLED DOUBLERS IAW TR 53-10-20C, DEFECT SIZE: FRAME CRACKED 0.25 INCH.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA0615Stringer Clip · crackedS-4R, BS 727E CRACKED. INSTALLED NEW CLIP CC 1133482, INSTALLED IAW SRM 51-10-02, DEFECT SIZE: SHEETMETAL 5958 S-4R TIE CLIP CRACKED BS 727E.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA069Splice · crackedSTA 907, S-4L CRACKED. REMOVED AND REPLACED WITH NEW PART IAW SRM 51-10-02, DEFECT SIZE: .500 INCH CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA0616Floorbeam · corrodedCORROSION ON FLOORBEAM STA 328 RBL 21 CORROSION. INSTALLED DOUBLER IAW SRM 53-00-51 FIG 201, DEFECT SIZE: SHEETMETAL ITEM 1030M EVIDENCE OF CORROSION ON FLOORBEAM 1 X 2 INCH, STA 328 RBL 21.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA0610Floor Panel · crackedCOCKPIT ENTRY FLOOR CRACKED. REMOVED AND REPLACED WITH NEW PART/KIT IAW SRM 51-10-02, DEFECT SIZE: SHEETMETAL ITEM 1036, NOSE GEAR DOWNLOCK VIEW SUP STRUCTURE CRACKED ON FWD END.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Floor PanelSDR USAA0611Floorbeam · corrodedBS 986.5 CABIN FLOORBEAM LBL 18, 21, 24, 30 CORROSION. REPLACED T-CAP IAW TR 53-60-01A, DEFECT SIZE: SEVERAL 1 X 1 INCH CORRODED AREAS.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA058Frame · damagedBS 639 FRAME & OVERWING DOOR STOP RT SIDE. 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).Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA057Frame · damagedBS 639 FRAME AT OVERWING DOOR STOP LT SIDE. DEFECTIVE PART REPLACED WITH IDENTICAL PART: ORDERED T-ANGLE 1717710 STOCK, FAB REPLACED IAW DWG65-46450, DEFECT SIZE: 1.5 INCH BY 1.5 INCH MISSING T-ANGLE (MISSING SINCE MANUFACTURE).Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA056Frame · crackedBS 727F BETWEEN S-8R & S-9R (AT AIR CONDITION ATTACH BRACKET) CRACKED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE IAW TR 53-10-20C, DEFECT SIZE: APPROX .5 INCH CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA055Attach Angle · crackedBS 877; S-11L CRACKED. REMOVED CRACKED ANGLE. FABRICATED & INSTALLED NEW ANGLE IAW BOEING DRW 69-45156; SRM 51-10-02, DEFECT SIZE: APPROX .5 INCH CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA059Splice · crackedSTA 907, S-4L CRACKED. REMOVED AND REPLACED WITH NEW PART IAW SRM 51-10-02, DEFECT SIZE: .500 INCH CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA0510Floor Panel · crackedCOCKPIT ENTRY FLOOR CRACKED. REMOVED AND REPLACED WITH NEW PART/KIT IAW SRM 51-10-02, DEFECT SIZE: SHEETMETAL ITEM 1036, NOSE GEAR DOWNLOCK VIEW SUP STRUCTURE CRACKED ON FWD END.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Floor PanelSDR USAA0516Floorbeam · corrodedCORROSION 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 X 2 INCH, STA 328 RBL 21.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA0515Tie Clip · crackedSTR 4R, BS 727E CRACKED. INSTALLED NEW CLIP CC 1133482, INSTALLED IAW SRM 51-10-02, DEFECT SIZE: SHEETMETAL 5958 S-4R TIE CLIP CRACKED BS 727E.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA0514Frame · crackedSTA 907, BELOW S-8L CRACKED. FAB FROM ANGLES 1133534 & 1133533, INSTALLED DOUBLERS IAW TR 53-10-20C, DEFECT SIZE: FRAME CRACKED 0.25 INCH.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA0513Frame · crackedSTA 440, S-8L CRACKED. FABRICATED ANGLES FROM NR 1133534 AND 1133533, INSTALLED DOUBLERS IAW TR 53-10-20C, DEFECT SIZE: 0.25 INCH CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA0512Angle · crackedBETWEEN STA 927 AND 947.5 AT BL 0 CRACK. INSTALLED NEW ANGLE IAW SRM 51-40-02, DEFECT SIZE: 1 INCH CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Longeron/StringerSDR USAA0511Floorbeam · corrodedBS 986.5 CABIN FLOORBEAM LBL 18, 21, 24, 30 CORRODED. REPLACED T-CAP IAW TR 53-60-01A, DEFECT SIZE: SEVERAL 1INCH X 1INCH CORRODED AREAS.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR SB06001Clamp · looseEN ROUTE FL340 CABIN PRESS PROBLEMS, CABIN ALT CLIMBED TO 9,800 FT, 200 FT PER MINUTE. DESCENDED TO FL280, CABIN ALT DOWN TO 8,500 FT. CABIN STABILIZED FL240. COULD NOT LOWER CABIN ALT OR RATE IN AUTO OR STANDBY PRESSURIZATION MODES. FOUND COUPLING BOOTS OJan 7, 2006 · N781AU · Boeing 7374B7 · Air Distribution SystemSDR USAA051645Skin · damagedFOUND SKIN DAMAGE RT HORIZ STAB LEADING EDGE FASTENER HOLE 3 FT FROM I/B EDGE. REMOVED DAMAGED SKIN, INSTALLED FILLER AND DOUBLER PER EA 97189 DEFECT SIZE: 1/4".Dec 29, 2005 · N781AU · Boeing 7374B7 · Horizontal Stabilizer, Plate/SkinSDR USAA051646Clevis · corrodedFOUND CLEVIS R1 ON HORIZ STAB CORRODED. REMOVED CORROSION, REPLACED BUSHING PER SRM 55-10-10, DEFECT SIZE: 2".Dec 29, 2005 · N781AU · Boeing 7374B7 · Horizontal Stabilizer StructureSDR USAA051654Clevis · corrodedFOUND CORROSION CLEVIS R7, HORIZ STAB. REMOVED CORROSION, INSTALLED BUSHING PER SRM 55-10-10, DEFECT SIZE: 2".Dec 29, 2005 · N781AU · Boeing 7374B7 · Horizontal Stabilizer StructureSDR USAA051653Skin · dentedFOUND SKIN DENTED FUSELAGE STA 490, LONG 19L-20L . FABRICATED REPAIR AND INSTALLED IAW EA 97190, DEFECT SIZE: 1.250" BY 0.750" BY 0.250"D.Dec 29, 2005 · N781AU · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA051652Splice · crackedFOUND CRACK RT STA 907, STR 4R. REMOVED AND REPLACED WITH FABRICATED STR SPLICE PER SRM 51-40-02, DEFECT SIZE: .250".Dec 29, 2005 · N781AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051651Splice · crackedFOUND CRACK FUSELAGE STA 907 LT S4. REMOVED AND REPLACED WITH FABRICATED STRINGER SPLICE PER SRM 51-40-02, DEFECT SIZE: .125".Dec 29, 2005 · N781AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051650Attach Fitting · corrodedFOUND R2 ON HORIZ STAB. REMOVED CORROSION AND GOUGE, INSTALLED BUSHING PER SRM 55-10-10, DEFECT SIZE: 2".Dec 29, 2005 · N781AU · Boeing 7374B7 · Horizontal Stabilizer, Attach FittingsSDR USAA051649Clevis · corrodedFOUND CORROSION CLEVIS R13 ON HORIZ STAB. REMOVED CORROSION, INSTALLED BUSHING PER SRM 55-10-10, DEFECT SIZE: 2".Dec 29, 2005 · N781AU · Boeing 7374B7 · Horizontal Stabilizer StructureSDR USAA051648Clevis · gougedFOUND CORROSION CLEVIS R4 ON HORIZ STAB. REMOVED CORROSION; BLENDED GOUGES, REPLACED BUSHING PER SRM 55-10-10, DEFECT SIZE: 2" CORROSION; 1/4" GOUGES 3 EA.Dec 29, 2005 · N781AU · Boeing 7374B7 · Horizontal Stabilizer StructureSDR USAA051647Clevis · corrodedFOUND CORROSION CLEVIS R3 ON HORIZ STAB. REMOVED CORROSION; REPLACED BUSHING PER SRM 55-10-10, DEFECT SIZE: 2".Dec 29, 2005 · N781AU · Boeing 7374B7 · Horizontal Stabilizer StructureSDR USAA051642Frame · crackedSTA 663.75, S3L CRACKED. CUT OUT DAMAGE, INSTALLED FILLER, REPAIR ANGLE AND STRAPS IAW SRM 53-00-07-2R9, DEFECT SIZE: .25 INCH.Dec 23, 2005 · N783AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA051639Intercostal · crackedFOUND CORROSION STA 294.5-303.9 STR 16L. REMOVED AND REPLACED FABRICATED INTERCOSTAL PER SRM 51-40-02, DEFECT SIZE: 1.5".Dec 21, 2005 · N781AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051638Gate · corrodedFOUND CORROSION AFT ENTRANCE DOOR, LOWER GATE. REMOVED AND REPLACED PER SRM 52-10-02; 51-40-05; CORROSION LEV 1; TASK C5310701, DEFECT SIZE: 21"L X 0.250"W X 0.154"D.Dec 21, 2005 · N781AU · Boeing 7374B7 · Passenger/Crew DoorsSDR USAA051637Sill · corrodedFOUND CORROSION BET STA 290-360, LBL 48 (CABIN FLOOR). REMOVED AND REPLACED NEW DOOR SILL CHORD PER SRM 51-40-02; CORROSION LEVEL 1; TASK C5310701 DEFECT SIZE: 25"L X 1.5"W X .039"D.Dec 21, 2005 · N781AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051636Floor Support · corrodedFOUND CABIN FLOOR SUPPORT BETWEEN STA 967-986.5 LBL 16. REMOVED AND REPLACED NEW SUPPORT ANGLE PER SRM 51-40-02; CORROSION LEVEL 1; TASK C5310702, DEFECT SIZE: 2.125"L BY 2"W BY .069"D.Dec 21, 2005 · N781AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051635Skin · canningFOUND OIL CANNING STA 403, STR 14R-15R. FAB REPAIR DOUBLER/TRIPLER/FILLERS PER 53-00-01, 53-30-01, DEFECT SIZE: 1.85" X 1.80".Dec 21, 2005 · N781AU · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA051640Floorbeam · corrodedFOUND CORROSION FLOORBEAM STA 986.5, RBL 4-38. FABRICATED NEW PARTS PER TR 53-60-01 REV A, 53-15-01B; TASK NR C5310702; LEVEL 1, DEFECT SIZE: 46" BY 2.0" BY 0.055".Dec 21, 2005 · N781AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA051616Frame · corrodedFOUND CORROSION FRAME 794.3 AND JUST ABOVE S25R. MAJOR REPAIR REMOVED DAMAGED. INSTALL FILLER AND THREE STRAPS IAW SRM 51-70-12, DEFECT SIZE: 3.0".Dec 21, 2005 · N783AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA051597Frame · crackedFUSELAGE STA 600, BETWEEN S17L TO S18L CRACKED. INSTALLED FAB FILLER AND STIFFENER PER TYP REPAIR 53-62-01, SRM 51-40-02, DEFECT SIZE: .5 INCH CRACK.Dec 20, 2005 · N781AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA051592Panel · corrodedCORROSION ON WEB PANEL UNDER AFT CARGO DOOR SCUFF PLATE. PART REPLACED WITH IDENTICAL PART REPLACED WEB IAW SRM 53-60-51, DEFECT SIZE: SHEETMETAL 3999 CORROSION ON WEB PANEL UNDER SCUFF PLATE TOP & BOTTOM 2 X 1 INCH.Dec 20, 2005 · N783AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA051589Seat Track · crackedBS 727B, RBL 24.75 RIGHT I/B SEAT TRACK FLOORBEAM CRACKED. CUT OUT DAMAGED SECTION, FAB & INSTALLED NEW SECTION OF TRACK/BEAM & SPLICE PRTS IAW SRM 53-00-52 EA 97204, DEFECT SIZE: .250 INCH CRACK.Dec 20, 2005 · N783AU · Boeing 7374B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA051588Frame · crackedSTA 601 LEF TR SIDE ON INNER CORD ANGLE JUST BELOW CABIN FLOOR LEVEL CRACKED. REMOVED DAMAGED METAL, INSTALLED FILLER & REPAIR ANGLE IAW EA 97193, DEFECT SIZE: 1.5 INCH CRACK.Dec 20, 2005 · N783AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA051587Frame · crackedSTA 615 RT SIDE I/B UPPER CORD ANGLE JUST BELOW CABIN FLOOR CRACKED. REMOVED DAMAGE, FAB & INSTALLED FILLERS & DOUBLERS IAW TR 53062-01, DEFECT SIZE: 1.5 INCH CRACK IN THE FRAME.Dec 20, 2005 · N783AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA051586Frame · crackedSTA 601 RIGHT SIDE ON INNER CORD ANGLE JUST BELOW CABIN FLOOR LEVEL CRACKED. REMOVED DAMAGED MATERIAL, INSTALLED FILLER AND STIFFENER ANGLE IAW TR 53-62-01 & EA 97193, DEFECT SIZE: 1.5 INCH CRACK.Dec 20, 2005 · N783AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA051559Floorbeam · gougedFOUND GOUGE FWD SIDE OF FLOORBEAM STA 887 BELOW CREASE BEAM A/C RT. FABRICATED AND INSTALLED DOUBLER ISW SRM 51-70-12, DEFECT SIZE: GOUGES IN FWD SIDE OF FLOORBEAM STA 887, BELOW CREASE BEAM, A/C RT.Dec 15, 2005 · N783AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA051556Seat Track · crackedLOCATION: BS727B RBL 24.75 (RT IB SEAT TRACK FLOOR BEAM) ACTION: FABRICATED AND INSTALLED NEW SECTION OF TRACK/BEAM IAW SRM 53-00-52 EA 97204 DEFECT SIZE: .250 INCH.Dec 14, 2005 · N783AU · Boeing 7374B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA051555Seat Track · crackedLOCATION: BS 727B LBL 45.5 (LT OB SEAT TRACK/FLOORBEAM) ACTION: FABRICATED AND INSTALLED NEW TRACK SECTION IAW SRM 53-00-02 REPAIR 3 DEFECT SIZE: .375 INCH.Dec 14, 2005 · N783AU · Boeing 7374B7 · Fuselage, Seat/Cargo Attach Fittings
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