Boeing 737-522

Service difficulty reports · 1,682

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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 = '737522'
  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 2006UALA00391Frame · crackedLT CABIN STA 927, FRAME IS CRACKED AT PSU RAIL ATTACHED BRACKET FASTENER BTWN STR 8 & STR 9. UPDATE REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED REF MM 53-11-99 AND SRM 53-00-07 REP.NR 2.Mar 4, 2006 · N928UA · Boeing 737522 · Fuselage Main, FrameSDR 2006UALA00390Attach Angle · crackedRT CABIN STA 291 JUST ABOVE STR 11 INTERCOSTAL ATTACHED ANGLE IS CRACKED AT FWD END. REMOVED AND REPLACED ANGLE REF SRM 51-40-02Mar 4, 2006 · N928UA · Boeing 737522 · Fuselage Main, Attach FittingsSDR 2006UALA00389Stringer Clip · crackedSTA 867 UPPER LOBE STR 10R, STRINGER CLIP IS CRACKED AT RADIUS. REMOVED AND REPLACED STRIN GER CLIP REF SRM 51-40-02Mar 4, 2006 · N928UA · Boeing 737522 · Fuselage Main, Attach FittingsSDR 2006UALA00388Attach Angle · crackedLH CABIN STA. 967 FRAME ATTACHED ANGLE CRACKED JUST ABOVE DOOR 2L. REMOVED DAMAGE AND FABRICATED AND INSTALLED SHEAR TIE, SHIM, AND FILLER REF SRM 53-00-07Mar 4, 2006 · N928UA · Boeing 737522 · Fuselage Main, Attach FittingsSDR 2006UALA00387Crease Beam · corrodedCABIN CREASE BEAM WEB FROM STA 727A TO 767 IS CORRODED RBL 71 TO RBL 71 REMOVED AND REPLACED THE CREASE BEAM WEBS REF SRM 51-40-02Mar 4, 2006 · N928UA · Boeing 737522 · Fuselage Main, StructureSDR 2006UALA00386Splice · crackedLT CABIN STA. 907 STR 4 SPLICE IS CRACKED AT CENTER FASTENER. REMOVED AND REPLACED STR. FOUR SPLICE REF SRM 51-40-02Mar 4, 2006 · N928UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA00385Door Frame · crackedR1 DOOR CUTOUT HAS CRACK IN LOWER FWD FRAME STRUCTURE. REMOVED & REPLACED LOWER FWD FRAME REF SRM 51-40-02Mar 4, 2006 · N927UA · Boeing 737522 · Fuselage Main, StructureSDR 2006UALA00384Clip · crackedFWD CABIN BS 277 STR 11L INTERCOSTAL UPPER U-SHAPE CLIP CRACKED IN INBD RADIUS. REMOVED CLIP, FABRICATED & INSTALLED REF BAC DWG66-14210 & SRM 51-40-02.Mar 4, 2006 · N927UA · Boeing 737522 · Fuselage Main, Attach FittingsSDR 2006UALA00383Angle · crackedFWD CABIN BS 277 STR 11L INTERCOSTAL LOWER ANGLE CRACKED AT IB RADIUS. REPLACED ANGLE. FABRICATED AND INSTALLED REF SRM 51-20-02.Mar 4, 2006 · N927UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA00381Crease Beam · corrodedCREASE BEAM INNER CHORD CORRODED BS 941 TO 998 AT WL 208 DOOR THRESHOLD AREA.REMOVED & REPLACED CREASE BEAM REF SRM 51-40-02.Mar 3, 2006 · N928UA · Boeing 737522 · Fuselage Main, StructureSDR 2006UALA00380Attach Angle · crackedSTA 305 AT STR 9R WEB TO SKIN ATTACH ANGLE IS CRACKED. ANGLE REF SRM 51- 40-02.Mar 3, 2006 · N927UA · Boeing 737522 · Fuselage Main, Attach FittingsSDR 2006UALA00368Clip · crackedFOUND CRACKED SHEAR CLIP IN LOWER RADIUS JUST ABOVE DOOR L2 UPPER SILL, STA 967. FABRICATED CLIP PER 53-00- 07 AND INSTALLED PER SRM 51-40-02Mar 2, 2006 · N927UA · Boeing 737522 · Fuselage Main, Attach FittingsSDR 2006UALA00367Pin · damagedFOUND RT MLG TRUNNION LINK PIN HAS PLATING MISSING IN SHANK AREA. PIN REPLACED ON JC I3576 WO NR 11070-7500-0009. BY AAR-IND MECH 11708 AND INSP 050 ON AAR WO NR 11071-7500-0007.Mar 2, 2006 · N930UA · Boeing 737522 · Main Landing GearSDR 2006UALA00365Intercostal · crackedSTATION 305 STR 8R INTERCOSTAL WEB TO FUSELAGE SKIN ANGLE IS CRACKED IN THE RADIUS. REPLACED ANGLE PER SRM 51-40-02.Mar 1, 2006 · N927UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA00363Intercostal · crackedFOUND LT CABIN STA 312 INTERCOSTAL AT STR 4 IS CRACKED. REMOVED INTERCOSTAL REF SRM 51-40-02. PICKED UP FASTENER HOLES REF SRM 51-40-02, INSTALL REF SRM 51-40-02.Mar 1, 2006 · N928UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA00362Attach Angle · crackedFOUND RT CABIN STA 294, SILL CHORD ANGLE HAS CRACKED ATTACH ANGLE. REMOVED SILL ANGLE. DRILLED NEW ONE AND INSTALLED REF 51-40-02 SRM.Mar 1, 2006 · N928UA · Boeing 737522 · Fuselage Main, Attach FittingsSDR 2006UALA00361Door · dentedFOUND E/E DOOR DENT, OUT OF LIMITS. INSTALLED DOUBLER REPAIR PER SRM 52-00-01. NO FURTHER FINDINGS, O.K. FOR SERVICE.Feb 28, 2006 · N927UA · Boeing 737522 · Electrical/Electronic Compartment DoorsSDR 2006UALA00360Intercostal · crackedFOUND INTERCOSTAL WEB STR 16 BETWEEN STA 294.5 & 303.9 IS CRACKED. FABRICATED NEW WEB PER SRM 51-30-01, INSTALLED WEB PER SRM51-40-02.Feb 28, 2006 · N927UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA00359Splice · crackedFOUND STRINGER SPLICE CRACKED AT STA 907 L4 AT 2 FASTENERS. REPLACED SPLICE PER SRM 51-40-02.Feb 28, 2006 · N927UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA00358Attach Angle · crackedFOUND FWD CABIN BS 305 STR 10R WEB TO SKIN ATTACH ANGLE CRACKED IN RADIUS. MANUFACTURED AND INSTALLED NEW ANGLE PER SRM 51-40-02.Feb 28, 2006 · N927UA · Boeing 737522 · Fuselage Internal Mounting StructureSDR 2006UALA00352Floorbeam · corrodedAFT CABIN FLOORBEAM CORRODED AROUND NUT CLIP HOLES BS 986.5 RBL 23-45 WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, INSTALLED REPAIR REF MM 53-10-95.Feb 28, 2006 · N928UA · Boeing 737522 · Fuselage Main, Floor BeamSDR CA060228008Line · chafedFLUID LEAK ON RT GEAR "UP" HYDRAULIC RETURN LINE NOTICED DURING OVERNIGHT CHECK. LINE WAS CHAFED THROUGH DUE TO RUBBING ON A BRACKET. LINE REPLACED,GEAR SWING CARRIED OUT AND AIRCRAFT RETURNED TO SERVICE. TT-37255:17 TC-22887.Feb 27, 2006 · Boeing 737522 · Hydraulic System, MainSDR 2006UALA00581Fire Warning · illuminatedRETURNED TO THE BLOCKS DUE TO NR 2 ENGINE FIRE INDICATION.Feb 27, 2006 · N941UA · Boeing 737522 · Fire DetectionSDR 2006UALA00351Shear Tie · crackedFOUND STA 360 STR 14R SHEAR TIE IS CRACKED. REPLACED SHEAR TIE PER SRM 53-00-07.Feb 27, 2006 · N927UA · Boeing 737522 · Fuselage Internal Mounting StructureSDR 2006UALA00342Skin · dentedTWO DENTS FOUND IN FUSELAGE SKIN JUST AFT OF LT UPPER PITOT TUBE. CUT -OUT DAMAGE AND INSTALLED DOUBLER REPAIR PER FIG 201 DETAIL V,Feb 24, 2006 · N927UA · Boeing 737522 · Fuselage Main, Plate/SkinSDR 2006UALA00318Skin · dentedFWD CARGO DOOR HAS A SCRATCH IN PAINT WITH A SMALL DENT, APPROX 1 IN X 1-16TH, AT ABOUT EYE LEVEL FWD OF HANDLE ABOUT 18 IN. DENT IS FREE FROM CRACKS AND NO FASTENERS AFFECTED BUT LESS THAN 30 TO 1 RATIO, SCRATCH IS IN PAINT TO PRIMER DENT TO BE CHECKED AT EAFeb 20, 2006 · N924UA · Boeing 737522 · Cargo/Baggage DoorsSDR 2006UALA00317Skin · dentedFWD CARGO DOOR EXTERNAL SKIN IS DENTED 9.75 INCHES FROM BOTTOM EDGE, 14.75 INCHES FROM FWD EDGE. SHARP GOUGE WITH DENT, 2 INCHES IN LENGTH. INSTALLED REPAIR DOUBLER REF SRM 52-30-01 & SRM 51-40-02. BY AAR-IND MECH 11335 AND INSP 54 ON AAR WO 11014-8100-0014Feb 20, 2006 · N924UA · Boeing 737522 · Cargo/Baggage DoorsSDR 2006UALA00298Skin · gougedLOWER FUSELAGE EXT SKIN IS GOUGED AT STA 421 BETWEEN S26R & S27R. *S/D* REPAIRED REF SRM 53-00-01 REPAIR NR 32 PROCEDURE II.Feb 20, 2006 · N924UA · Boeing 737522 · Fuselage Main, Plate/SkinSDR 2006UALA00350Compressor · stalledCOMPRESSOR STALL DESCENDING OUT OF FL370. RECOVERED INSTANTLY. NO FLUXUATIONS IN ANY ENG PARAMETERS,ONLY AN AUDIBLE REPORT. :ACP STEPS 1 THRU 7 OF COMPRESSOR STALL TROUBLESHOOTING MANUAL REF 71-00-92 INCLUDING BOROSCOPE STEP 3 REF MM 72-00-41. NO LIMITING DEFeb 19, 2006 · N918UA · Boeing 737522 · Turbine Engine Compressor SectionSDR 2006UALA00319Intercostal · crackedFWD CABIN AT DOOR 1L INTERCOSTAL WEB IS CRACKED AT AFT SIDE STA 294.5 STR 18L. *S/D* REMOVED DAMAGED AREA, FABRICATED INTERCOSTAL WEB AND INSTALLED WEB REF 51-40-02.Feb 18, 2006 · N924UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA00297Support Fitting · crackedAFT CABIN FRAME SUPPORT FITTING HAS CRACK AT STA 727 STR 14R. *S/D* REMOVED DAMAGE, FABRICATED, DRILLED AND INSTALLED REPAIR PARTS REF EA NR I060081.Feb 18, 2006 · N924UA · Boeing 737522 · Fuselage Main, Attach FittingsSDR 2006UALA00296Support Fitting · crackedAFT CABIN FRAME SUPPORT FITTING HAS CRACK AT STA 727 STR 14L. *S/D* REMOVED DAMAGE, FABRICATED, DRILLED AND INSTALLED REPAIR PARTS REF EA NR I060082.Feb 18, 2006 · N924UA · Boeing 737522 · Fuselage Main, Attach FittingsSDR 2006UALA00295Frame · crackedMID CABIN STA 663 FRAME CRACKED AT STR 2R & 1R. *S/D* REMOVED CRACKS ACCOMPLISHED HFEC INSPECTION VERIFIED DAMAGE REMOVED, FABRICATED REPAIR ANGLE AND STRINGER STRAPS AND INSTALLED PER SRM 53-00-07.Feb 18, 2006 · N924UA · Boeing 737522 · Fuselage Main, FrameSDR 2006UALA00294Intercostal · crackedFWD CABIN DOOR CUTOUT 1-R INTERCOSTAL WEBS OUTER L-ANGLE IS CRACKED STA 293 WL 249 RBL 57. *S/D* REMOVED DAMAGED ANGLE, DRILLED NEW ANGLE AND INSTALLED AS REQUIRED REF SRM 51-40-02.Feb 18, 2006 · N924UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA00293Intercostal · crackedFWD CABIN DOOR CUTOUT 1R INTERCOSTAL WEBS OUTER -L- ANGLE IS CRACKED AT STA 293 WL 259 RBL 56. REMOVED AND REPLACED ANGLE REF SRM 51-40-02.Feb 18, 2006 · N924UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA00291Strap · corrodedAFT CARGO DOOR CUTOUT LOWER SILL BEAM STRAP IS CORRODED AT BS STA 807 TO BS 847. *S/D* BLENDED CORROSION & FOUND OUT OF LIMITS. REMOVED & REPLACED LOWER SILL BEAM STRAP REF SRM 53-60-53 & SRM 51-10-02.Feb 16, 2006 · N924UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA00288Skin · crackedAFT CARGO DOOR HAS CRACK ON EXT SKIN AT AFT UPPER CORNER OF DOOR HANDLE CUTOUT TO FASTENER HOLE. MAJOR REPAIR ACP'D, INST'D REPAIR DOUBLER NO FURTHER FINDINGS, O.K. FOR SERVICE.Feb 15, 2006 · N924UA · Boeing 737522 · Cargo/Baggage DoorsSDR CA060214004Tire · deflated(CAN) WHEN MAINTENANCE ARRIVED AT THE GATE FOR THE DAY'S FIRST DEPARTURE, IT WAS NOTICED THAT THE LT NOSE TIRE WAS FLAT. UPON FURTHER INVESTIGATION IT WAS DISCOVERED THAT THE RT NOSE TIRE WAS ALSO FLAT. BOTH NOSE ASSEMBLIES REPLACED AND AIRCRAFT RETURNED TO SEFeb 14, 2006 · Boeing 737522 · TireSDR 2006UALA00271Rivet · crackedEXTERNAL FUSELAGE HAS CRACKED RIVETS IN MULTIPLE LOCATIONS. EXTERNAL FUSELAGE, 40 EA FASTENERS CRACKED AND 1 EA FASTENER WITH LIGHTNING STRIKE SURROUNDING NR 3R COCKPIT WINDOW. NDT VERIFIED NUMBER OF RIVETS CRACKED, FOUND 3 EA RIVETS TO BE CRACKED. REMOVED Feb 10, 2006 · N924UA · Boeing 737522 · Fuselage Main, Plate/SkinSDR 2006UALA00263Sill · crackedFWD CARGO DOOR LOWER SILL PLATE IS CRACKED ON LOWER SURFACE AT STA 430. *S/D* ACCOMPLISHED REPAIR AT FWD CARGO DOOR LOWER SILL PLATE STA 430, REF SRM 51-70-11. REMOVED DAMAGE AREA REF SRM 51-10-02. MADE NEW REPAIR PARTS REF SRM 51-70-11 PAGE 5 DETAIL I. TFeb 10, 2006 · N924UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA00249Intercostal · crackedFWD CABIN AT DOOR CUTOUT 1L, INTERCOSTAL WEB IS CRACKED IN RADIUS WHERE ATTACHES TO FRAME AT STA 294.5 STR 8L. INSTALLED REPAIR STA 294.5 STR 8L REF SRM 51-40-02 FABRICATED PART #65-17684 REF GNMM 1-0-0-023.Feb 8, 2006 · N924UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA00248Web · crackedFWD CABIN, J-SHAPED WEB HAS CRACK ABOVE STRAP BETWEEN STA 294.5 AND 312 (294.5+9 INCHES), STR 4L. REPLACED WEB AT FS 294.5 TO FS 312 STR 4L REF SRM 51-40-02 AND DWG 50-08261.Feb 8, 2006 · N924UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA00247Support · crackedCABIN BS 827 AFT SIDE OF FRAME IS CRACKED BETWEEN S8L & S9L AT PSU RAIL SUPPORT. INSTALLED REPAIR REF MM 53-10-84.Feb 8, 2006 · N924UA · Boeing 737522 · Fuselage Main, Attach FittingsSDR 2006UALA00246Frame · crackedFWD CABIN STA 440 FRAME IS CRACKED JUST BELOW STR 8R. REPAIR OF FRAME ACCOMPLISHED REF MM 53-10-84.Feb 8, 2006 · N924UA · Boeing 737522 · Fuselage Main, FrameSDR 2006UALA00240Floorbeam · crackedFLOORBEAM STA 639 LBL 47, BRACKET OUTBOARD & AFT BELOW SEAT TRACK CRACKED. REMOVED CRACKED ANGLE & REPLACED WITH NEW FABRICATED ANGLE REF SRM 51-4-02 BOEING DRAWING 65-46540 GNMM 1-0-0-023.Feb 7, 2006 · N924UA · Boeing 737522 · Fuselage Main, Floor BeamSDR 2006UALA00239Support · crackedCABIN STA 867 BETWEEN S8L & S9L AFT SIDE OF FRAME IS CRACKED AT PSU RAIL SUPPORT. ACCOMPLISHED REPAIR TO FRAME REF MM 53-10-84-FIG 803.Feb 7, 2006 · N924UA · Boeing 737522 · Fuselage Main, Attach FittingsSDR 2006UALA00238Intercostal · crackedCABIN BS 291 INTERCOSTAL BETWEEN S12R & S11R ANGLE ON LOWER SIDE IS CRACKED IN RADIUS. REMOVED AND REPLACED ANGLE BETWEEN S12R & S11R REF B737 SRM 53-40-02.Feb 7, 2006 · N924UA · Boeing 737522 · Fuselage Miscellaneous StructureSDR 2006UALA00237Stringer · crackedCABIN STA 908, STR 4L IS CRACKED AROUND 2 EA RIVETS JUST AFT OF STA 907 FRAME. REMOVED AND REPLACED STRINGER SPLICE CHANNEL AT STR 4L FIG 908 REF SRM 51-40-02.Feb 7, 2006 · N924UA · Boeing 737522 · Fuselage Main, Longeron/StringerSDR 2006UALA00236Crease Beam · corrodedFWD CABIN DOOR CUTOUT AT 1L, INNER CREASE BEAM HAS UPPER SURFACE CORROSION STA 307 TO 328 STR 17L TO 17L LBL 55 TO LBL 58. REMOVED AND REPLACED 1L INNER CREASE BEAM REF SRM 51-40-02.Feb 7, 2006 · N924UA · Boeing 737522 · Fuselage Main, StructureSDR 2006UALA00235Support · crackedCABIN BS 902 BETWEEN S8R & S9R AT PSU RAIL SUPPORT AFT SIDE OF FRAME IS CRACKED. REMOVED DAMAGE AT PSU RAIL SUPPORT, HFEC CUTOUT REF: 51-00-00 FIG 23 NO CRACK FOUND, INSURANCE CUT REF MM 53-10-84 REPAIR III DRILLED AND TRIMMED ANGLES , ALODINED AND PRIMED AFeb 7, 2006 · N924UA · Boeing 737522 · Fuselage Main, Attach Fittings
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