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 USAA050356Attach Angle · wornPIT - Q4 - ATTACH ANGLE, 1 INCH X 2 INCH WEAR AREA, BS 1288 AT S2R. FABRICATED NEW ANGLE IAW TYP REP 53-20-05A. (K)SDR USAA050294Beam · crackedPIT - FOUND FORWARD ENTRY DOOR CRACKED .5 INCH, STOP CUTOUT AFT END NR 6 BEAM AFT LIP ON PAN. REMOVED DAMAGE, INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-16. (M)SDR USAA050293Skin · crackedPIT - FOUND FORWARD ENTRY DOOR CRACKED FOUR PLACES, .5 INCH EACH, INNER SKIN AFT EDGE AT BEAM 3, 4, 5, 6 STOP CUTOUTS. REMOVED DAMAGE, INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-16. (M)SDR USAA050331Shear Tie · crackedPIT - FOUND SHEAR TIE CRACKED .25 INCH, STRINGER 1 STATION 578. REMOVED AND REPLACED WITH NEW PART PR SRM 51-40-02. (M)SDR USAA050330Shear Tie · crackedPIT - FOUND SHEAR TIE CRACKED .5 INCH, STRINGER 2R STATION 578. REMOVED AND REPLACED WITH NEW PART PER SRM 51-40-02. (M)SDR USAA050292Skin · crackedPIT - FOUND AFT CARGO DOOR CRACKED .5 INCH, UPPER AFT CORNER OF HANDLE/FLAPPER CUTOUT TO RIVET. REMOVED DAMAGE, INSTALLED DOUBLER PER SRM 52-00-01 FIG 202. (M)SDR USAA050291Skin · crackedPIT - NR 1 SLAT WITH FIVE CRACKS .1875 INCH CRACKS, LOWER SKIN UNDER OUTBOARD SLAT FITTING, AFT RIVET ROW. INSTALLED DOUBLER PER SRM 57-43-01. (M)SDR USAA050290Skin · crackedPIT - FOUND SKIN CRACKED .5 INCH, RT WING LEADING EDGE WBL 204 AT LOWER WING SURFACE. REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER PER T/R 57-41-02. (M)SDR USAA050289Structure · crackedPIT - FOUND AFT CARGO DOOR WITH TWO .25 INCH CRACKS, LOCK FASTENER BOTTOM OUTBOARD T-CHORD AFT END. REMOVED AND REPLACED T-CHORD PER RM 51-40-02. (M)SDR USAA050237Skin · crackedPIT - FOUND HORIZ STAB CRACKED 2 INCHES, HORIZ STAB LOWER SKIN REAR SPAR STAB STATION 138.7. INSTALLED DOUBLER PER TYPICAL REPAIR 55-10-07 REV B. (M)SDR SB05025Battery · dischargedPIT - FOUND EMERGENCY AISLE LIGHTS AT ROWS 3, 4 AND 5 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY SUPPLY ASSEMBLY.SDR USAA050308Floor Support · corrodedPIT - FOUND FLOOR SUPPORT CORRODED .75 INCH DIAMETER, BETWEEN STRAP 500 AND 500A RBL 9. INSTALLED ANGLE DOUBLER PER TYPICAL REPAIR 53-10-06B. (M)SDR SB05024Battery · dischargedPIT - FOUND R1 DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK.SDR USAA050352Skin · delaminatedPIT - C5 - SLAT, 3 INCH LONG X 2.5 INCH WIDE - 2 AREAS, DELAMINATION. NR 5 SLAT TOP SURFACE IB AND OB T/E. INSTALED NEW CORE, TOP DOUBLERS, SEAL AND REFINISH IAW SRM. (K)SDR SB05021Power Supply · dischargedCLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS ON SEATS 24L AND 25L INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1137 EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK NORMAL.SDR SB05019Wire · brokenPIT - FLT1466 - CREW REPORTED THE FIRST OFFICER'S PITOT STATIC NR 2 AUX STATIC LIGHT ILLUMINATED. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A BROKEN WIRE ON PITOT STATIC PROBE CONNECTOR. REPAIRED SAME PER MM 30-3SDR USAA050215Cargo Track · crackedPIT - FOUND CARGO FLOOR TIE DOWN CRACKED .125 INCH, FLOOR TIE DOWN RBBL 13.88 STATION 767 IN RADIUS. REMOVED AND REPLACED CARGO FLOOR TIE DOWN TRACK PER SRM 51-40-02. (M)SDR USAA050216Skin Panel · crackedPIT - FOUND SKIN PANEL CRACKED 1 INCH, LEFT LEADING EDGE LOWER SKIN PANEL AT SLAT STATION 3.25. FILLER AND DOUBLER INSTALLED PER TYPICAL REPAIR 57-41-02. (M)SDR USAA050217Clip · corrodedPIT - FOUND CLIP CORRODED 1 INCH BY 3 INCH AREA, FRAME 795, STRINGER 27R. CORROSION LEVEL 1, TASK C53-208-01. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR PER EA 79752, SRM 53-00-07 FIG 207. (M)SDR USAA050188Bulkhead · crackedPIT - FOUND FORWARD BULKHEAD WEB CRACKED .25 INCH, WL 218 AND LBL 12. INSTALLED DOUBLER PER SRM 53-10-08. (M)SDR USAA050197Support Fitting · chafedPIT - FOUND SPOILER CHAFED .5 INCH, NR 4 GROUND SPOILER INBOARD SUPPORT FITTING. INSTALLED ANGLE PER TYP REPAIR 57-50-14. (M)SDR SB05008Outflow Valve · faultyRSW - FLT1052 - DURING CRUISE AT FL250, EN ROUTE FROM CLT TO RSW, A/C LOST PRESSURIZATION JUST SW OF JAX. CREW CAUGHT THE PROBLEM BEFORE THE CABIN PRESSURE DROPPED ENOUGH TO DEPLOY THE OXYGEN MASKS. CREW DESCENDED FLT TO 10,000 FT AND THEN LANDED AT RSW WITHSDR SB05007Fuse · blownPIT - MAINTENANCE REPORTED THE AFT SERVICE DOOR EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE 5 AMP FUSE (E-1) AT POWER SUPPLY M1137. OPERATIONAL CHECK GOOD.SDR USAA050193Web · corrodedPIT - FOUND WEB CRACKED 1 INCH BY 2 INCH AREA AROUND NUT PLATE, AFT CARGO THRESHOLD WEB STATION 800 TO 833 PLATE. CORROSION LEVEL 1. REMOVED WEB AND REPLACED WITH NEW WEB PER SRM 53-60-15, 51-40-02. (M)SDR SB05006Charger · inoperativeMCO - MAINTENANCE REPORTED THE EMERGENCY AISLE LIGHTS AT SEAT ROWS 10 AND 11 AND AT THE AFT LEFT OVERWING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CHARGER ASSEMBLY NR 3 AND THE BATTERY PACK. OPERATIONAL CHECK NORMAL.SDR USAA050196Angle · corrodedPIT - FOUND Z-ANGLE CORRODED 4 INCH BY 8 INCH AREA, AT NUT PLATE HOLES, RT Z-ANGLE AT AFT SERVICE DOOR BS 950-990. REMOVED AND REPLACED Z-ANGLE PER SRM 51-40-00. (M)SDR USAA050195Mount · corrodedPIT - FOUND MOUNT GALLEY AFT CORRODED 3 INCH BY 3 INCH AREA, LEFT AFT GALLEY MOUNT BS 990, BS 1016 LBL 32.10. REPLACED MOUNT LEFT AFT GALLEY PER SRM 51-40-00. (M)SDR USAA050204Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, BETWEEN STRINGER 8L AND 9L AT STATION 827. CUT OUT DAMAGE, HI FREQ, INSTALLED DOUBLER PER TR 53-10-20A. (M)SDR USAA050203Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, BETWEEN STRINGER 8L AND 9L AT STATION 867. CUT OUT DAMAGED AREA, HI FREQ INSTALLED DOUBLER PER TR 53-10-20A. (M)SDR USAA050200Support Beam · gougedPIT - Q3 - MLG SUPPORT BEAM, .025 DEEP .250 X .125 (4 EA) GOUGE; LT MLG SUPPORT BEAM, LOWER FLANGE AFT EDGE 37 INCHES OB OF IB EDGE. (K)SDR USAA050214Floorbeam · corrodedPIT - FOUND BEAM CORRODED 2 INCH BY 100 INCH AREA, BS 986.5 FLOORBEAM ENTIRE UPPER SURFACE. SPLICED IN NEW UPPER CAP PER TYPICAL REPAIR 53-60-01 REV A. (M)SDR USAA050207Frame · crackedPIT - FOUND FRAME CRACKED .125 INCH FROM RIVET, STATION 727D BETWEEN S8/59R. REPAIR ANGLE PER TYPICAL REPAIR 53-10-20A. (M)SDR USAA050202Stringer · crackedPIT - FOUND STRINGER CRACKED .25 INCH, STATION 907 STRINGER 4R. DOUBLER INSTALLED PER SRM 53-00-03 FIG 201. (M)SDR USAA050192Intercostal · corrodedPIT - FOUND INTERCOSTAL CORRODED 2 INCH BY 2 INCH AND 4 INCH BY 4 INCH, BS 947 TO 967 LBL 50. CORROSION LEVEL 1, TASK C53-107-102. REPLACED WITH BOEING PART PER SRM 51-40-04. (M)SDR USAA050023Skin · crackedCLT - FOUND SKIN 2.5 INCHES CRACK, STATION 727G STRINGER 22L. INSTALLED DOUBLER IAW SRM 53-00-1. (M)SDR SB05004Wire · brokenCREW REPORTED EXPOSED WIRES IN THE FORWARD COAT CLOSET. MAINTENANCE REPAIRED BROKEN WIRES, FOR EMERGENCY LIGHTS, IN FORWARD COAT CLOSET. OPERATIONAL CHECK GOOD.SDR USAA050044Skin · damagedPIT - FOUND SKIN OUT OF LIMITS 2 INCHES BY 1.6250 INCH BY .018 INCH, RT SIDE, STATION 420 STRINGER 14R. REMOVED DAMAGE, INSTALLED DOUBLER REPAIR PER SRM 53-00-01 FIG 231. (M)SDR USAA050209Skin Panel · crackedPIT - FOUND SKIN PANEL CRACKED .5 INCH LONG, OUTBOARD SIDE OF PYLON ABOVE MID SPAR FITTING LOWER SKIN PANEL SLAT STATION 3.25. STOP DRILLED, INSTALLED FILLER AND DOUBLER FREEZE PLUG PER TR 57-41-02, SRM 51-20-10 AND EA 79764. (M)SDR USAA041049Skin · damagedPIT - Q1 - RUDDER SKIN, .1250 INCH X .2500 INCH AREA, DAMAGE, LT SIDE 5.5 INCH FWD OF T/E 62.5 INCH UP FROM BOTTOM. PREPARED DAMAGED AREA, LIGHT SANDING, INSTALLED MULTI LAYERED REPAIR IAW SRM AND EA.SDR USAA050208Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED .5 INCH, 2 FASTENER HOLES STATION 500G TO 520 BL 0. INSTALLED INTERCOSTAL PER 53-30-51. (M)SDR USAA050210Frame · crackedPIT - FOUND FRAME CRACKED TWO PLACES .125 INCH LONG, STATION 500A BETWEEN STRINGER 8LT AND 9L OVERHEAD BIN LOWER ATTACH POINT. REINFORCED WITH PREFABRICATED DOUBLERS PER TYPICAL REPAIR 53-10-20A. (M)SDR USAA050213Mount · corrodedPIT - FOUND LAV FLOOR MOUNT CORRODED 2 INCH BY 2 INCH AREA, STATION 304, LBL 12. REPLACED FITTING PER 53-10-00. CORROSION LEVEL 1. (M)SDR USAA050191Floorbeam · corrodedPIT - FOUND UPPER CHORD CORRODED 8 INCH BY 2 INCH, STATION 312 LBL 8 TO RBL 7 FLOOR UPPER CHORD. REPLACED UPPER CHORD PER SRM 53-10-51 FIG 205. (M)SDR USAA050212Structure · crackedPIT - FOUND AFT CARGO DOOR CRACKED .25 INCH, LOWER T-CHORD AFT VERTICAL FLANGE. REMOVED AND REPLACED T-CHORD PER BOEING BLUEPRINT 65-47952. (M)SDR USAA050198Skin · delaminatedPIT - FOUND TOP SKIN CORE BOND DELAMINATED 2.5 INCH BY 1.5 INCH AREA, NR 3 SLAT TOP SURFACE OUTBOARD T/E. BONDED IN NEW CORE, BOND ON TOP DOUBLER PR SRM 51-70-10. (M)SDR USAA050101ASkin · crackedFOUND SKIN CRACKED 1.5 INCHES, STATION 727D STRINGER 23R. INSTALLED DOUBLER IAW SRM 53-00-01. (M)SDR USAA050199Intercostal · burnedPIT - Q3 - INTERCOSTAL UNK SIZE- ARC BURN DAMAGE; GROUND STUD GD 3252, STA 344-360, LBL60 WL 204. REPLACED INTERCOSTAL IAW EA. (K)SDR USAA050223Structure · crackedPIT - FOUND AILERON TAB CRACKED 2 INCHES, OUTBOARD TRAILING EDGE, OF LEFT AILERON TAB. REPLACED AILERON TAB PER MM 27-11-21. (M)SDR USAA050211Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED 1.75 INCH, STATION 384-386 IN RADIUS OF INTERCOSTAL BL 0. INSTALLED INTERCOSTAL PER 53-20-1/53-30-1. (M)SDR USAA050206Skin · crackedPIT - FOUND SLAT CRACKED .5 INCH, FORWARD OF INBOARD AUX TRACK LOWER SURFACE AFT FASTENER. INSTALLED DOUBLER PER SRM 57-43-01 FIG 206. (M)
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