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 USAA050838Stiffener · corrodedCLT - FOUND STIFFENER CORRODED 2 INCHES, STATION 227.8, BL 0 ON VERTICAL STIFFENER. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW EA 69945. (M)Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050839Beam · crackedCLT - FOUND BEAM CRACKED 1.25 INCH, AFT OF RIGHT AILERON AT TRAILING EDGE. INSTALLED A NEW BEAM IAW SRM 57-51-02. (M)Jul 7, 2005 · N526AU · Boeing 7373B7 · AileronsSDR USAA050840Angle · corrodedCLT - FOUND TRANSITION ANGLE CORRODED, TRANSITION ANGLE IN AFT CARGO BETWEEN STATION 727C AND STATION 827. REMOVED DAMAGE, INSTALLED TRANSITION ANGLE IAW SRM 51-10-02. (M)Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050841Floorbeam · corrodedCLT - FOUND FLOORBEAM TEE CAP CORRODED 1 INCH, AT BS 986.5, LBL 31. REMOVED AND REPLACED UPPER T-CAP OF FLOORBEAM IAW TYPICAL REPAIR 53-10-05, SRM 53-00-51. (M)Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050842Intercostal · crackedCLT - FOUND INTERCOSTAL SUPPORT CRACKED 1.4 INCHES, FS 295 AT STRINGER S16L. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 53-10-15M SRM 51-10-02. (M)Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050843Stiffener · corrodedCLT - FOUND STIFFENER CORRODED 2 INCHES, STATION 227.8, BL 0 ON VERTICAL STIFFENER. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW EA 69945. (M)Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050844Angle · corrodedFOUND CHORD ANGLE CORRODED .8 INCHES, LOWER CHORD ANGLE AT BS 227.8. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW EA 96645 AND BOEING DWG 69-38740. (M)Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050845Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED 6 INCHES, AFT OF FORWARD E/E DOOR AT BL 0, BS 219.8 TO 227.8. REMOVED CORRODED INTERCOSTAL. FABRICATED AND INSTALLED NEW PART IAW EA 96645 AND BOEING DWG 69-38740. (M)Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050846Skin · delaminatedCLT - FOUND ELEVATOR TOP SKIN CRACKED 3 INCHES TOP SURFACE. MAJOR, COMPOSITE REPAIR IAW EA 96681. (M)Jul 7, 2005 · N526AU · Boeing 7373B7 · Elevator, Plate/SkinSDR USAA050847Skin · crackedCLT - FOUND SKIN CRACKED 3 INCHES, FUSELAGE AT STATION 727E AT STRINGER 25R. INSTALLED DOUBLER AND TRIPLER IAW SRM 53-00-01. (M)Jul 7, 2005 · N505AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA050832Stringer · corrodedCLT - FOUND STRINGER CORRODED 12 INCHES, CARGO FLOOR STRINGERS AT STATION 773. REPLACED OUT OF LIMITS STRINGER SECTIONS IAW SRM 53-60-53 AND TR 53-10-06B. (M)Jul 5, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA050833Angle · corrodedCLT - FOUND TRANSITION ANGLE CORRODED 8 INCHES, IN AFT CARGO BETWEEN STATION 727C AND STATION 827. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-10-02. (M)Jul 5, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050834Web · corrodedCLT - FOUND WEB CORRODED 10 INCHES, UNDER STRAP AT THE AFT CARGO COMPARTMENT DOOR OPENING. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW PART IAW BOEING DWG 65-47957 AND SRM 51-10-02. (M)Jul 5, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050835Stringer · corrodedCLT - FOUND STRINGERS CORRODED 12 INCHES, CARGO FLOOR STRINGERS AT STATION 773. REPLACE OUT OF LIMITS STRINGER SECTION IAW SRM 53-60-53 AND TR 53-10-06B. (M)Jul 5, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR SB05079Indicator · failedCLT FLT 1417 AFTER TAKEOFF FROM CLT ENROUTE TO PBI, CREW REPORTED THE FLAPS LOCKED DURING RETRACTION DUE TO AN ASYMMETRY CONDITON. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD AT CLT WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPEJul 3, 2005 · N374US · Boeing 7373B7 · Trailing Flap Position Indicating SystemSDR SB05078Seal · leakingCREW REPORTED A LOSS OF CABIN PRESSURIZATION. CREW ACCOMPLISHED AN EMERGENCY DESCENT, DECLARED AN EMERGENCY AND DIVERTED TO RIC WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO OXYGEN MASKS WERE DEPLOYED. MAINTENANCE FOUND AND RESECURED LOOSE POTABLE WAJul 2, 2005 · N397US · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA050823Skin · dentedPIT - FOUND SKIN DENTED 2 INCHES BY 2 INCHES, DENT ONE BS 500-500A, S20R-S21R, DENT 2 AND 3 AT BS 500A-500B S19R-S20R. CUT OUT THREE DENTS, FABRICATED TRIPLERS, SIZE OF REPAIR IS 44.5 INCH BY 23 AT 10.22 LBS IAW SRM 53-00-01. (M)Jul 1, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA050819Angle · corrodedCLT - FOUND TRANSITION ANGLE CORRODED 8 INCHES, IN AFT CARGO BETWEEN STATION 727C AND AND STATION 827. REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE IAW SRM 51-10-02. (M)Jun 30, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050820Web · corrodedCLT - FOUND WEB CORRODED 10 INCHES, WEB UNDER STRAP AT THE AFT CARGO COMPARTMENT DOOR OPENING. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW PART IAW BOEING DWG 65-47957 AND SRM 51-10-02. (M)Jun 30, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR SB05077Charger · inoperativeMAINTENANCE REPORTED THE EMERGENCY EXIT SIGN BETWEEN THE AFT LAVATORIES, OVER THE R2 DOOR AND OUTSIDE OF THE L2 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY ALONG WITH THE BATTERY PACK. OPERATIONAL CHECK GOOD.Jun 30, 2005 · N519AU · Boeing 7373B7 · Emergency LightingSDR USAA050812Support Angle · crackedCLT - Q2 - SUPPORT ANGLE, 1 INCH, CRACK, STA 540 AND STR 22R. FABRICATED AND INSTALLED REPAIR PART. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050811Bracket · wornCLT - Q2 - ANGLE BRACKET, 2 INCHES X 3 INCHES, WORN AND CHAFED AREA, LWR WING PANEL OB OF NR 2 FLAP TRACK. FABRICATED AND INSTALLED NEW ANGLE IAW SRM. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Wing, Attach FittingsSDR USAA050810Skate Angle · wornCLT - Q2 - SKATE ANGLE, 2 INCHES X 4 INCHES, WORN AREA, AFT END OF THE RT SKATE ANGLE AT THE BASE OF THE VERTICAL FIN TO FUSELAGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage, Stabilizer Attach FittingsSDR USAA050809Angle · corrodedCLT - Q2 - L-ANGLE, 6 INCH FRETTING, L-ANGLE AT BS 1016 FORWARD OF THE RT FWD VERTICAL FIN MOUNT. FABRICATED AND REPLACED NEW L ANGLE. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050808Angle · crackedCLT - Q2 - HORIZONTAL ANGLE, 1 INCH CRACK, STA 695 LT OF BL0. REMOVED FABRICATED AND INSTALLED NEW L ANGLE IAW DWG. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050807Floor Support · crackedCLT - Q2 - FLOOR SUPPORT, 1 INCH CRACK, FLOOR SUPPORT AT STA 500D IN A/C DISTRIBUTION BAY. REMOVED DAMAGED WEB, FABRICATED NEW WEB IAW SRM. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050806Intercostal · dentedCLT - Q2 - INTERCOSTAL, 2 INCHES X 1 INCH, DENT, STR 25L BETWEEN FRAMES 440 AND 420. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DRWG. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050805Mount · corrodedCLT - Q2 - LAV MOUNT, 1 INCH X 3 INCHES, CORROSION, LT AFT LAV OB MOUNT. FABRICATED AND INSTALLED NEW MOUNT IAW WITH DRWG. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA050804Threshold · corrodedCLT - Q2 - WEB, 48 INCHES, CORROSION FWD ENTRY DOORWAY THRESHOLD WEB. FABRICATED WEB AND ASSOCIATED REPAIR PARTS AND INSTALLED DRWG IAW SRM. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050803Stringer · corrodedCLT - Q2 - CARGO FLOOR STRINGER, 6 INCH, CORROSION, AFT CARGO FLOOR STRINGERS AT STA 736 FROM LBBL 17.2 TO RBBL 13.8. REMOVED AND TREATED CORROSION IAW SRM. (K)Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA200506004Skin · cracked2.25 INCH CRACK FOUND AT 727E, S25R ON SKIN. INSTALLED DOUBLER IAW SRM 53-00-01 FIG. 229.Jun 29, 2005 · N511AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR SB05075Shutoff Valve · leakingPHL FLT 1085 AFTER TAKEOFF AND GEAR RETRACTION, CREW REPORTED A SUBSTANTIAL DROP IN THE A-HYDRAULIC SYSTEM QUANTITY. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FLIGHT CONTROL SHUTOJun 28, 2005 · N393US · Boeing 7373B7 · Hydraulic System, MainSDR AWXA200500765Stiffener · corrodedDURING C-13 CHECK FOUND CORROSION PRESENT ON STIFFENER CHANNEL LOCATED AT AFT PRESSURE BULKHEAD FORWARD SIDE AT BS 1016, WL 155, BL 0. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW BOEING 737-300 SRM 53-80-08-1 FIG 101. MAINTENANCE REMOVED CORROSION ON STIFFJun 28, 2005 · N328AW · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA050782Skin · crackedCLT - FOUND SKIN CRACKED 2.25 INCH, BS 727D AT S23R RT SIDE. INSTALLED DOUBLER IAW 53-00-01 FIG 229. (M)Jun 21, 2005 · N532AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA050781Splice · crackedCLT - FOUND STRINGER SPLICE CRACKED, .4 INCH AND .3 INCH, STATION 908, S4L. REMOVED OLD STRINGER SPLICE, INSTALL NEW SPLICE IAW SRM 53-00-01 FIG 229. (M)Jun 20, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050780Channel · wornCLT - FOUND L-CHANNEL FRETTING WEAR .5 INCH BY 3 INCHES, FORWARD OF THE LEFT FORWARD VERTICAL FIN MOUNT AT BS 1016 NR 2412. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 53-20-05. (M)Jun 20, 2005 · N526AU · Boeing 7373B7 · Fuselage, Stabilizer Attach FittingsSDR USAA050779Tear Strap · debondedCLT - FOUND TEAR STRAP DISBOND 15 INCHES, BS 867-887, S17-19 RT. INSTALLED RIVETS THROUGH SKIN AND STRAPS AS REQUIRED IAW SRM 53-00-01 FIG 225. (M)Jun 20, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA050778Tear Strap · debondedCLT - FOUND TEAR STRAP DISBOND 8 INCHES, BS 857, S16R-S17R. INSTALLED RIVETS TO SECURE IAW SRM 53-00-01, FIG 225 DET 3. (M)Jun 20, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA050777Tear Strap · debondedCLT - FOUND DEBONDED TEAR STRAP 11 INCHES, BS 877, S16R-17R. ADDED RIVETS IAW SRM 53-00-01 FIG 225 DET 3. (M)Jun 20, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA050775Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 827 STRINGER 9L. CUT OUT CRACK, INSTALLED NEW REPAIR ANGLES IAW 53-10-20B. (M)Jun 20, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, FrameSDR AWXA200500730Threshold · corrodedDURING C-13 CHECK, FOUND CORROSION IN FORWARD CARGO PIT ON 20 NUT PLATES LOCATED ON THRESHOLD WEB FROM STA 450 TO STA 490. MX FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-30-15-1 FIG 101. REMOVED THRESHOLD WEB FROM STA 450 TO STA 490 AND FABJun 17, 2005 · N328AW · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR SB05072Seal · out of trackCABIN ALTITUDE WARNING HORN ACTIVATED AS ACFT BEGAN A SLOW UNCONTROLLABLE CLIMB IN CABIN PRESSURE. OUTFLOW VALVE REPORTED TO BE CLOSED ENTIRE TIME. CREW DESCENDED FLIGHT TO 14,000 FT WHERE PRESSURE STABILIZED. O-2 MASKS DEPLOYED AS A PRECAUTION. FLT LANDEDJun 17, 2005 · N532AU · Boeing 7373B7 · Cargo/Baggage DoorsSDR USAA050774Floorbeam · corrodedFOUND FLOORBEAM CORRODED 3 INCHES, BS 967, LBL 43. FABRICATED NEW T-CAP FOR FLOORBEAM PER SRM 53-00-51, SAME AS PREVIOUS REPAIR. (M)Jun 16, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050773Skin · gougedCLT - FOUND SKIN GOUGED .125 INCH BY 1 INCH BY .060 INCH, LEADING EDGE RADIUS OF LEFT FOR FLAP .22 INCH FROM INBOARD END. REMOVED DAMAGED AREA, 2.5 INCH BY 1 INCH, INSTALLED EXTERNAL DOUBLER 7.5 INCH BY 6 INCHES IAW SRM 57-53-01 FIG 201. (M)Jun 16, 2005 · N526AU · Boeing 7373B7 · Trailing Edge FlapsSDR USAA050772Angle · corrodedCLT - FOUND TRANSITIONAL ANGLE CORRODED 2 SQUARE INCHES, UNDERSIDE OF NUTPLATE OF RIGHT TRANSITION ANGLE AT DOOR FRAME BS 496. REMOVED DAMAGE, FABRICATED REPAIR AND REPLACEMENT PART INSTALLED IAW 737 SRM 51-10-02. (M)Jun 16, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050771Angle · corrodedCLT - FOUND TRANSITION ANGLE CORRODED 3 INCHES, RT TRANSITION ANGLE AT BS 492.4. REMOVED DAMAGED PART. FABRICATED AND INSTALLED NEW PART IAW 737 SRM 51-10-02. (M)Jun 16, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050770Support Angle · crackedCLT - FOUND SUPPORT ANGLE CRACKED 1 INCH, LOWER EDGE OF INTERCOSTAL AT FORWARD SIDE OF STATION 328, RBL 32. REMOVED DAMAGED STIFFENER, FABRICATED REPLACEMENT PART, AND INSTALLED. (M)Jun 16, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050769Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH, AT BS 986.5, LBL 31. REMOVED AND REPLACED UPPER T-CAP OF FLOORBEAM IAW TYPICAL REPAIR 53-10-05 AND SRM 53-00-51. (M)Jun 16, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR AWXA200500754Intercostal · crackedDURING C-13 CHECK FOUND INTERCOSTAL CRACKED, .25 INCHES IN LENGTH INSIDE FORWARD CARGO DOOR AT CENTER OF DOOR, 20 IN FROM LOWER EDGE OF DOOR AT BS 470, WL 176, STRINGER 23R. MAINTENANCE REMOVED INTERCOSTAL AT FORWARD CARGO DOOR AT CENTER OF DOOR, 20 IN FROM LJun 16, 2005 · N328AW · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR SB05071Light · shortedCLT MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT ROW 22 WAS SHORTED. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AND THE FUSE IN THE EMERGENCY LIGHT BATTERY PACK BETWEEN AFT GALLEYS. OPERATIONAL CHECK GOOD.Jun 16, 2005 · N511AU · Boeing 7373B7 · Emergency Lighting
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