Boeing 737-3B7

Service difficulty reports · 4,722

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 = '7373B7'
  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 USAASB01004Circuit Board · faultyCLE - FLT 1515 - CREW REPORTED THAT DURING CLIMB-OUT FROM CLE, THE LANDING GEAR LEVER WOULD NOT MOVE TO THE UP POSITION. GEAR INDICATION SHOWED THREE RED AND THREE GREEN GEAR LIGHTS. FLIGHT REQUESTED WITH CEL TOWER TO STAY AT 3,000 FEET DUE TO GEAR INDICATIOJan 12, 2001 · N533AU · Boeing 7373B7 · Landing Gear Retraction/Extension SystemSDR USAA010162Crossbeam · corrodedPIT - FOUND ENGINE MOUNT CROSSBEAM CORRODED, BEARING BORE OF CROSS BEAM. CORROSION LEVEL 1. ENLARGED BORE .010 CHANFERED BORE, MPI ROTO PEEN. INSTALLED OVERSIZED BEARING PER TYP REP 54-50-09. (M)Jan 10, 2001 · N393US · Boeing 7373B7 · Engine Mount SectionSDR AWXA0001227Wire · brokenAFT SECTION OF EMERGENCY TRACK LIGHTING SYSTEM DOES NOT ILLUMINATE. FOUND BROKEN WIRE AT ROW 18; REPAIRED WIRE; EMERGENCY LIGHT OPS CHECK NORMAL.Jan 4, 2001 · N328AW · Boeing 7373B7 · Light System WiringSDR USAASB00363Circuit Breaker · faultyCLT - FLT 1775 - EN ROUTE FROM PHL-ORD - THE LEFT FORWARD WINDOW HEAT OVERHEAT LIGHT ILLUMINATED. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES BUT LIGHT REMAINED ILLUMINATED. ICE BEGAN TO FORM ON THE WINDSHIELD SO THE CREW DIVERTED TO CLT. FLIGHT LDec 30, 2000 · N385US · Boeing 7373B7 · Windshield/Door Rain/Ice RemovalSDR USAA002220Attach Angle · crackedCLT - FOUND WEB ATTACH ANGLE CRACKED 1 INCH, STATION 295, STRINGER 17R, WL 208. INSTALLED NEW ANGLE PER SRM 51-10-02. (M)Dec 29, 2000 · N523AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR AWXA0001142Skin · dentedAFT CARGO DOOR EXT SKIN DENTED BEYOND LIMITS (A/Y = 23.8). FABED REPAIR OUTER SKIN AND REPLACED DAMAGED SKIN IAW SRM 52-30-01 FIG 202Dec 29, 2000 · N328AW · Boeing 7373B7 · Cargo/Baggage DoorsSDR AWXA0001141Skin · dentedDENT ON LT HORIZONTAL STABILIZER LEADING EDGE AT APPROX STA 135. REPAIRED IAW ENG. REPAIR 03-5510-00356-552Dec 29, 2000 · N328AW · Boeing 7373B7 · Horizontal Stabilizer, Plate/SkinSDR AWXA0001140Skin Panel · dentedINSPECTION OF LOWER LOBE NOSE FUSELAGE FOUND DENT TO BE OUT OF LIMITS AT BS 211.8 STR 24R. REPAIRED IAW SRM 53-00-01, SKIN LAP JOINT REPAIRDec 29, 2000 · N328AW · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR AWXA0001139Door Frame · crackedAFT CARGO DOOR FWD PAN HAS CRACKS AT SPRING PULLEY BRACKET ATTACHMENTS (AT PAN SPLICE). STOP DRILLED CRACKS; INSTALLED INTERNAL FORMED SECTION REPAIR AND AN EXTERNAL WEB REPAIR IAW SRM 51-70-11 AND 51-70-13Dec 29, 2000 · N328AW · Boeing 7373B7 · Fuselage Main, StructureSDR AWXA0001138Intercostal · crackedDURING INSPECTION OF THE BS 178 BULKHEAD, FOUND ATTACHING INTERCOSTAL AT RBL 24 AND WL 195 ON THE AFT SIDE OF BULKHEAD TO BE CRACKED AT FLOOR BEAM ATTACHMENT FLANGE. CUTOUT DAMAGE AND INSTALLED REPAIR ANGLE IAW SRM 53-10-08 FIG 207Dec 29, 2000 · N328AW · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002202Support Fitting · crackedCLT - FOUND MLG BEAM OUTBOARD SUPPORT CRACKED .5 INCH, RT WING AFT SPAR AT WBL 157. REPAIRED PER EA 68723 AND EA 68767. (M)Dec 28, 2000 · N523AU · Boeing 7373B7 · Wing, Landing Gear Attach FittingsSDR USAA002212Web · crackedCLT - FOUND WEB CRACKED .25 INCH, STRINGER 7L WEB STATION 294.5. FABRICATED NEW WEB AND INSTALLED PER SRM 51-10-2. (M)Dec 27, 2000 · N520AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002213Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, STATION 867 BETWEEN STRINGER 8/9. INSTALLED DOUBLER PER TR 53-10-14. (M)Dec 27, 2000 · N520AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA002205Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, STATION 827 BETWEEN STRINGER 8/9R. INSTALLED FILLER AND DOUBLER PER TR 53-10-14. (M)Dec 27, 2000 · N520AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA002206Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, STATION 787 BETWEEN STRINGER 8 AND 9R. REMOVED DAMAGE AND INSTALLED DOUBLER PER TR 53-10-14. (M)Dec 27, 2000 · N520AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA002207Floorbeam · corrodedCLT - FOUND BEAM CORRODED 36 INCHES, FLOORBEAM UPPER CHORD RIGHT SPLICE 986. REPLACED DAMAGED SECTION PER TR 53-10-05A. (M)Dec 27, 2000 · N520AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA002201Angle · crackedCLT - FOUND VERTICAL CHORD ANGLE CRACKED .25 INCH, BS 178, LBL 5.7, WL 184. INSTALLED REPAIR PER SRM 53-10-08. (M)Dec 26, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA002203Attach Fitting · crackedCLT - FOUND ATTACH FITTING CRACKED .25 INCH, LT MLG SUPPORT BEAM ATTACH FITTING. REMOVED CRACK PER TR 57-40-13. REMOVED CRACK PER TR 57-40-13. (M)Dec 26, 2000 · N523AU · Boeing 7373B7 · Wing, Landing Gear Attach FittingsSDR USAASB00356Relay · intermittentMCO - FLT 82 - AIRCRAFT WAS TAXIING OUT FROM MCO WHEN THE CREW REALIZED THAT THE STABILIZER TRIM WAS NOT WORKING. CAPTAIN RESET THE CIRCUIT BREAKERS AND THE STABILIZER TRIM BEGAN WORKING FINE. DURING CLIMB-OUT, CAPTAIN TRIED TO TRIM STABILIZER ELECTRICALLY, Dec 25, 2000 · N387US · Boeing 7373B7 · Stabilizer Control SystemSDR USAASB00357Controller · failedPIT - FLT 843 - SHORTLY AFTER TAKEOFF, BETWEEN 2,000 TO 3,000 FEET, THE PRESSURIZATION SYSTEM FAILED IN THE AUTO MODE. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CABINDec 25, 2000 · N511AU · Boeing 7373B7 · Cabin Pressure ControllerSDR USAASB00354Windshield · crackedPHL - FLT 1797 - ON CLIMB-OUT FROM PHL, EN ROUTE TO MCO, THE OUTER PANE ON THE CAPTAINS WINDSHIELD CRACKED. CAPTAIN REPORTED THAT THE LOWER LEFT CORNER ARCED AND GLOWED BEFORE CRACKING. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. ANDec 22, 2000 · N506AU · Boeing 7373B7 · Flight Compartment WindowsSDR USAA002195Skin · crackedCLT - FOUND SLAT SKIN .375 INCH, LOWER SKIN NR 3 L/E SLAT MID SPAN. INSTALLED DOUBLER PER TR 57-50-01 DRAWING 65C30133. (M)Dec 22, 2000 · N523AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA002187Floorbeam · corrodedCLT - FOUND BEAM CORRODED 1 INCH BY 1 INCH, STATION 986 UPPER CHORD BEAM. CORROSION LEVEL 1 C53-107-02. INSTALLED T-CAP AND SPLICE PE TR 53-10-05A AND SRM 53-60-51. (M)Dec 21, 2000 · N520AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA002188Crossbeam · corrodedPIT - CROSSBEAM FOUND WITH WEAR AND CORROSION IN BEARING BORE, .006 DEPTH. LEVEL 1 CORROSION. OPEN BORE UP FOR OVERSIZE BEARING RECHAMFER MPI ROTO PEEN. INSTALLED NEW BEARING, TYP REP 54-50-09. (M)Dec 21, 2000 · N384US · Boeing 7373B7 · Nacelle/Pylon StructureSDR USAA002181Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 1 INCH BY 1 INCH, UPPER FLANGE FLOORBEAM STATION 312, RBL 7 TO 8. CORROSION LEVEL 1 C53-107-01. INSTALLED NEW T-CAP PER SRM 53-10-51. (M)Dec 20, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA002174Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, STATION 747 BETWEEN STRINGER 8L AND 9L. ATTACHED ANGLE REPAIR PER SRM 51-40-2. (M)Dec 20, 2000 · N520AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA002179Frame · crackedCLT - FOUND SIDE CHORD CRACKED .125 INCH, BS 178, WL 207, RBL 26. SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M)Dec 20, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA002180Door Frame · crackedCLT - FOUND DOOR SURROUND FRAME CRACKED .125 INCH, FORWARD SERVICE DOOR FRAME AT FORWARD UPPER DOOR STOP FITTING. REMOVED AND REPLACED SURROUND FRAME PER SRM 51-10-2. (M)Dec 20, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA002170Bulkhead · crackedCLT - FOUND WEB BULKHEAD CRACKED .25 INCH AND .5 INCH CRACKS, LBL.5, RBL .5, WL 188, BS 178. INSTALLED REPAIR DOUBLER PER EA 68706. (M)Dec 19, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA002171Bulkhead · crackedCLT - FOUND WEB BULKHEAD CRACKED .25 INCH, RBL, WL 206, BS 178. INSTALLED REPAIR DOUBLER PER EA 68706. (M)Dec 19, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA002172Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED .5 INCH, STATION 178, WL 211, RBL 7. INSTALLED REPAIR DOUBLER PER EA 68706. (M)Dec 19, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA002173Bulkhead · crackedCLT - FOUND WEB BULKHEAD CRACKED .5 INCH, STATION 178, WL 213, LBL 7. INSTALLED REPAIR DOUBLER PER EA 68706. (M)Dec 19, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA002164Skin · crackedCLT - FOUND SKIN CRACKED .25 INCH, AFT END OF COOLING DUCT CUTOUT FASTENER HOLE. INSTALLED DOUBLER PER TR 53-30-07. (M)Dec 18, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA002165Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 440, STRINGER 14R. INSTALLED NEW PART PER SRM 51-10-2. (M)Dec 18, 2000 · N523AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002166Angle · crackedCLT - FOUND ANGLE CRACKED .250 INCH, BS 287 ABOVE STRINGER 10L ATTACH ANGLE. INSTALLED NEW PART PER SRM 51-10-2. (M)Dec 18, 2000 · N523AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002167Attach Angle · crackedCLT - F0UND ATTACH ANGLE .125 INCH, BS 289 STRINGER 11R INTERCOSTAL ATTACH ANGLE. INSTALLED NEW PART PER SRM 51-10-2. (M)Dec 18, 2000 · N523AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002168Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED 2 INCHES, STATION 706, STRINGER 2L. INSTALLED FABRICATED STRINGER TIE CLIP PER EA 68676. (M)Dec 18, 2000 · N523AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAASB00349Sealant · looseCLT - FLT 1607 - EN ROUTE FROM PHL-CUN, A LOUD NOISE WAS HEARD FROM THE MID CABIN, LEFT SIDE, ALONG WITH AN AIRFRAME VIBRATION. ALL ENGINE PARAMETERS WERE NORMAL. SELECTING SYSTEM ''A'' ELECTRIC HYDRAULIC PUMP OFF HAD NO EFFECT. FLIGHT DIVERTED TO CLT AND LDec 16, 2000 · N383US · Boeing 7373B7 · Aerodynamic FairingsSDR USAA002159Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 685, STRINGER 2L. FABRICATED AND INSTALLED NEW TIE CLIP PER EA 68676. (M)Dec 15, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA002153Attach Angle · crackedCLT - FOUND ATTACH ANGLE CRACKED .25 INCH, BS 294, STRINGER 7L. FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 51-70-11 FIG 1. (M)Dec 14, 2000 · N523AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002154Attach Angle · crackedCLT - FOUND ATTACH ANGLE CRACKED .25 INCH, BS 294, STRINGER 11L. FABRICATED REPAIR ANGLE PER SRM 51-70-11 FIG 1. (M)Dec 14, 2000 · N523AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002155Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .25 INCH, BS 294, STRINGER 12L. FABRICATED AND INSTALLED NEW PART PER SRM 51-70-11 FIG 1. (M)Dec 14, 2000 · N523AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002133Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 400 FRAME JUST ABOVE STRINGER 9L. INSTALLED DOBLER PER TR 53-10-14A. (M)Dec 13, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA002134Floorbeam · corrodedCLT - FOUND T-CAP CORRODED .250 INCH BY .250 INCH, BS 328 LBL 31, RBL 17, RBL 24. REPAIRED PER EA 68697. (M)Dec 13, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA002096Bulkhead · crackedCLT - FOUND WEB CRACKED 1 INCH, 1 INCH AFT OF STATION 178 BULKHEAD, RBL 28, WL 207. INSTALLED UPGRADED WEB PER SRM 51-10-02. (M)Dec 11, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA002097Intercostal · crackedCLT - FOUND UPPER FLANGE CRACKED 1.5 ICH, INTERCOSTAL STATION 539, BL 0 UPPER FLANGE. INSTALLED DOUBLER PER SRM 51-70-11, 51-20-01 AND 51-10-02. (M)Dec 11, 2000 · N523AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002098Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH THREE PLACES, STATION 400, STRINGER 4L. REPLACED CLIP PER SRM 51-10-2 AND 51-40-00. (M)Dec 11, 2000 · N523AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002099Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 480, STRINGER 9R. INSTALLED DOUBLER PER TR 53-10-14A. (M)Dec 11, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA002100Web · crackedCLT - FOUND WEB CRACKED 1 INCH, UPPER FORWARD CORNER INTERCOSTAL STATION 500D PLUS 1, BL 0. FABRICATED AND INSTALLED NEW WEB PER SRM 53-30-51 AND 51-10-02. (M)Dec 11, 2000 · N523AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002101Angle · crackedCLT - FOUND ANGLE CRACKED 2 INCHES IN TWO PLACES, INTERCOSTAL UPPER FLANGE STATION 500D TO 520, LBL 0. REPLACED UPPER FLANGE WEB ANGLE PER SRM 51-10-02. (M)Dec 11, 2000 · N523AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
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