Boeing 737-4Q8

Service difficulty reports · 6,250

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 = '7374Q8'
  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 ASAA2015081613120Crease Beam · corrodedRIGHT CREASE BEAM WEB IS CORRODED, BS 727E-727F. ACFT GROUNDED. R & R RT CREASE BEAM WEB BS 727E-727F IAW SRM 51-40-02-0G-0, W 1.5", O .032", R .023", L1, D .009".Aug 16, 2015 · N769AS · Boeing 7374Q8 · Fuselage Main, StructureSDR ASAA2015081612979Crease Beam · corrodedRT CREASE BEAM WEB IS CORRODED BS 496. ACFT GROUNDED. REMOVED CORROSION ON CREASE BEAM WEB BS 496-500 IAW SRM 51-10-02, W 2.50", O .036, R .023, L 3.70, D .013, MATERIAL LOSS OUT OF LIMITS IAW SRM 53-31-13, DETAIL II. NEW WEB FABRICATED ON MIG 5 OK 5289. RAug 16, 2015 · N769AS · Boeing 7374Q8 · Fuselage Main, StructureSDR ASAA2015081612976Crease Beam · corrodedRIGHT CREASE BEAM WEB IS CORRODED, BS 727F-727G. ACFT GROUNDED. R & R RT CREASE BEAM WEB BS 727F-727G IAW SRM 51-490-02-0G-0, W 3, O .032, R .026, L 2, D .006.Aug 16, 2015 · N769AS · Boeing 7374Q8 · Fuselage Main, StructureSDR ASAA2015081612975Crease Beam · corrodedRIGHT CREASE BEAM WEB IS CORRODED, BS 747-767. ACFT GROUNDED. CORROSION FOUND TO BE OUT OF LIMITS. R & R WEB IAW SRM 51-40-02-0G-0, W 2, O .032, R .027, L 1, D .005.Aug 16, 2015 · N769AS · Boeing 7374Q8 · Fuselage Main, StructureSDR ASAA2015081612974Crease Beam · corrodedRIGHT CREASE BEAM WEB IS CORRODED, BS 727C-727D. ACFT GROUNDED. R & R RT CREASE BEAM WEB BS 727C -BS 727D IAW SRM 51-40-02-0G-0, W .5, O .032, R .019, L 3.0, D .013.Aug 16, 2015 · N769AS · Boeing 7374Q8 · Fuselage Main, StructureSDR ASAA2015081612973Crease Beam · corrodedRIGHT CREASE BEAM WEB IS CORRODED BS 767-787. ACFT GROUNDED. R & R RT CREASE BEAM IAW SRM 51-40-02-0G-0, W 4, O .032, R .012, L 2.75, D .020.Aug 16, 2015 · N769AS · Boeing 7374Q8 · Fuselage Main, StructureSDR ASAA2015081513078Frame · corrodedAFT CARGO BAY FRAME BS 887 IS CORRODED ON AFT SIDE AT LBL2. ACFT GROUNDED. REMOVED CORROSION, WAS FOUND OUT OF LIMITS. REPAIRED FRAME IAW EA 400, 53EA 15774.Aug 15, 2015 · N769AS · Boeing 7374Q8 · Fuselage Main, FrameSDR ASAA2015081513036Transition Panel · corrodedAFT CARGO LT TRANSITION PANEL HAS SPOTS OF CORROSION, BS 767 TO BS 787. ACFT GROUNDED. REMOVED CORROSION WAS FOUND OUT OF LIMITS, REPAIRED TRANSITION IAW SRM 53-60-53-2R-4, W 1.5, O .080, R .034, L 1.2, D .006.Aug 15, 2015 · N769AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2015081512978Failsafe · corrodedAFT PIT FRAME BS 827 FAILSAFE ANGLE IS CORRODED BS 25L TO 23L. ACFT GROUNDED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-A-1 DETAIL II. R & R FAILSAFE ANGLE IAW SRM 51-40-02-0G-0, W 1", O .045", R .038:", L 2.00", D .007".Aug 15, 2015 · N769AS · Boeing 7374Q8 · Fuselage Main, StructureSDR ASAA2015081413118Stringer Clip · crackedAFT CARGO BAY STRINGER CLIP, BS 727B, STR 25L IS CRACKED. ACFT GROUNDED. R & R STRINGER CLIP, BS 727B, STR 25L IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0.Aug 14, 2015 · N769AS · Boeing 7374Q8 · Fuselage Main, Attach FittingsSDR ASAA2015081313000Floor Panel · corrodedFWD CARGO NR 4 FLOOR PANEL IS CORRODED. ACFT GROUNDED. FABRICATED NEW FLOOR PANEL IAW SRM 51-40-05-0G-0.Aug 13, 2015 · N769AS · Boeing 7374Q8 · Fuselage Floor PanelSDR ASAA2015081312999Skin · crackedL2 DOOR CUTOUT FWD LWR CORNER FUSE SKIN IS CRACKED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN IAW SRM 53-00-01-2R-32, DETAIL IV THIS IS A CATEGORY B REPAIR INITIAL THRESHOLD IS SET AT 66,000 CYCLES INTERVALS SET AT 24,000 CYCLES, SRM 53-00-01-212-32, TABLE IX FOAug 13, 2015 · N769AS · Boeing 7374Q8 · Fuselage Main, Plate/SkinSDR ASAA2015081212910Torque Box · crackedAPU TORQUE BOX RT SIDE INLET DUCT CORRODED AROUND THE FASTENER HOLES TOP STRAP. ACFT GROUNDED.Aug 12, 2015 · N769AS · Boeing 7374Q8 · Fuselage Main, StructureSDR ASAA2015080314491Stringer · corrodedAPU TORQUE BOX CENTER STRINGER, AFT OF MAIN CUTOUT HAS A CORROSION. ACFT GROUNDED. APU TORQUE BOX CENTER STRINGER AFT OF MAIN CUTOUT, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-1A-1 AND R & R IAW SRM 51-40-02.Aug 3, 2015 · N764AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2015073012831Skin · crackedAFT ENTRY DOOR CUTOUT FWD LWR CORNER IS CRACKED. ACFT GROUNDED. REPAIRED SKIN ASSY IAW SRM 53-00-01-2R-32. THIS IS A CAT B REPAIR WITH A INTERVAL OF 24,000 CYCLES AND A THRESHOLD OF 66000 CYCLES AT TIME OF REPAIR 45,218.Jul 30, 2015 · N764AS · Boeing 7374Q8 · Fuselage Main, Plate/SkinSDR ASAA2015072812627Door · lack of lubeL1 DOOR VERY STIFF TO CLOSED. ACFT GROUNDED. PERFORMED OPS CHECK OF DOOR. FOUND NO DEFECT. LUBED PINS AND GUIDE AS PRECAUTIONARY. ACFT OK FOR SERVICE, REF AMM 52-11-00 AND AMM 52-11-11.Jul 28, 2015 · N756AS · Boeing 7374Q8 · Passenger/Crew DoorsSDR ASAA2015071012554Shear Tie · crackedSKIN ATTACH FRAME, P/N 007-00420-10 AT FS 500B BETWEEN STRS 2 AND 3 LT IS CRACKED AT FASTENER HOLE. ACFT GROUNDED. R & R SHEAR TIE IAW SRM 51-40-02-0G-0 PARA 4.Jul 10, 2015 · N765AS · Boeing 7374Q8 · Fuselage Internal Mounting StructureSDR ASAA2015070912566Rib · crackedLT WBL 135 RIB CHORD FOUND CRACKED WHILE ACCESSING FASTENERS ON NR 00021, UPPER WING AFT PYLON FAIRING. ACFT GROUNDED. REPAIRED LT WING RIB CHORD AT WBL 135 IAW EA 400, 57 EA 15473.Jul 9, 2015 · N765AS · Boeing 7374Q8 · Wing, Rib/BulkheadSDR ASAA2015070912565Rib · crackedRIGHT WBL 135, RIB CHORD FOUND CRACKED WHILE ACCESSING FASTENERS ON NR-00021 UPPER WING AFT PYLON FAIRING. ACFT GROUNDED. REPAIRED RT WING RIB CHORD AT WBL 135 IAW EA 400, 57 EA 15473.Jul 9, 2015 · N765AS · Boeing 7374Q8 · Wing, Rib/BulkheadSDR ASAA2015070614344Skin · crackedL2 DOOR CUTOUT FWD LOWER CORNER HAS CRACK INDICATION. REMOVAL OF MARKED FASTENER IS REQUIRED TO VERIFY USING BHEC INSPECTION. ACFT GROUNDED. REPAIRED L2 DOOR CUTOUT FWD LOWER SKIN IAW SRM 53-00-01-2R-32, REPAIR 32. THIS IS A CATEGORY B REPAIR WITH A THRESHOLJul 6, 2015 · N765AS · Boeing 7374Q8 · Fuselage Main, Plate/SkinSDR ASAA2015070612529Skin · crackedL2 DOOR CUTOUT FWD LOWER CORNER HAS CRACK INDICATION. REMOVAL OF MARKED FASTENER IS REQUIRED TO VERIFY USING BHEC INSPECTION. GROUNDED - YES. REPAIRED L2 DOOR CUTOUT FWD LWER SKIN IAW SRM 53 00 01 2R 32 REPAIR 32.Jul 6, 2015 · N765AS · Boeing 7374Q8 · Fuselage Main, Plate/SkinSDR ASAA2015070612448Skin · crackedAFT GALLEY R2 SERVICE DOOR, CUT OUT LOWER FORWARD CORNER IS CRACKED FROM CORNER EXTENDING THROUGH 3 FASTENERS AND IS APPROXIMATELY 3" LONG. ACFT GROUNDED. REPAIRED THE SKIN IAW SRM 53-00-01-2R-32.Jul 6, 2015 · N765AS · Boeing 7374Q8 · Fuselage Main, Plate/SkinSDR ASAA2015070612405Frame · crackedFRAME 500F LT HAS A CRACK .25" LONG EXTENDING INBD AT 9:00 POSITION FROM 1" WIRE PENETRATION HOLE. ACFT GROUNDED. REPAIRED FRAME IAW SRM 53-00-07-2R-13.Jul 6, 2015 · N765AS · Boeing 7374Q8 · Fuselage Main, FrameSDR ASAA2015070512372Skin · crackedRIGHT HORIZONTAL STABILIZER REAR SPAR LOWER SKIN BETWEEN RIBS 5 AND 6 STAB STA 120.30-129.50 HAS .2500" CRACK IN LENGTH. ACFT GROUNDED. REPAIRED RT HORIZONTAL STABILIZER LWR SKIN BETWEEN RIB 5 AND 6, STABILIZER BS 120.30- BS 129 .50, CRACKED IAW SRM 55-10-01-Jul 5, 2015 · N765AS · Boeing 7374Q8 · Horizontal Stabilizer, Plate/SkinSDR ASAA2015070214493Web · crackedAFT CARGO DOOR CROSSBEAM AND WEB ARE CRACKED AT FWD END. ACFT GROUNDED. REPAIRED AFT CARGO DOOR CROSSBEAM AND WEB IAW ATTACHED WO 300444, AD20131312-400-52-5.Jul 2, 2015 · N765AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2015070212562Web · crackedAFT CARGO DOOR CROSSBEAM AND WEB ARE CRACKED AT FWD END. ACFT GROUNDED. REPAIRED AFT CARGO DOOR CROSSBEAM AND WEB IAW ATTACHED WO 300444, AD20131312-400-52-5.Jul 2, 2015 · N765AS · Boeing 7374Q8 · Cargo/Baggage DoorsSDR ASAA2015070212528Beam · crackedAFT CARGO DOOR CROSSBEAM E ON AFT END IS CRACKED. ACFT GROUNDED. REPAIRED AFT CARGO DOOR AFT END IAW ATTACHED WO 300444, AD 20131312-400-52-6.Jul 2, 2015 · N765AS · Boeing 7374Q8 · Cargo/Baggage DoorsSDR ASAA2015062712244Cover · detachedL1 DOOR EMERGENCY EXIT SIGN COVER FELL OFF. ACFT GROUNDED. REPLACED L1 DOOR EMERGENCY EXIT LIGHT ASSY IAW WDM 33-51-12. OPS TEST NORMAL.Jun 27, 2015 · N760AS · Boeing 7374Q8 · Emergency LightingSDR ASAA2015061412168Stiffener · corrodedRIGHT LONGITUDINAL BEAM ANGLE ABOVE AFT HEAT EXCHANGER CUTOUT IS CORRODED AT BS 619. ACFT GROUNDED. REMOVED CORROSION, MATERIAL LOSS FOUND TO BE OUT OF LIMITS. R & R ANGLE IAW SRM 51-40-02-0G-0.Jun 14, 2015 · N763AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2015061212204Strap · crackedWHILE CLOSING FWD CARGO BAY, FOUND MAIN CARGO DOOR LOWER FRAME INNER SKIN STRAP AT BS 480 CRACKED. ACFT GROUNDED. R & R STRAP IAW SRM 51-40-02.Jun 12, 2015 · N763AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2015061112205Web · corrodedAFTER REMOVAL OF RT RAM AIR DUCT FOUND CORROSION ON CENTER WING BOX RT SUPPORT BEAM WEB. ACFT GROUNDED. REPAIRED UNDERWING LONGITUDINAL BEAM WEB STA 576-585 AND 637, RBL 40.875 IAW EA'S 400, 53EA, 15279 AND 400, 53EA, 15288.Jun 11, 2015 · N763AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2015061112189Web · corrodedAFTER REMOVAL OF RT RAM AIR DUCT, FOUND CORROSION ON CENTER WING BOX RT SUPPORT BEAM WEB. ACFT GROUNDED. REPAIRED UNDERWING LONGITUDINAL BEAM, WEB BS 576-585 AND BS 637, RBL 40.875 IAW EA 400, 53EA 15279 AND 400, 53EA 15288, W 3, O .060, R .015, L 16.0, D .0Jun 11, 2015 · N763AS · Boeing 7374Q8 · Wing Miscellaneous StructureSDR ASAA2015060312033Lock · brokenFLOOR PALLET LOCK BROKEN , NR 1 POSITION FAR RT INBD SIDE, FWD. ACFT GROUNDED. REMOVED DAMAGED TRACK MATERIAL IN POSITION NR 1, REF SRM 53-00-52, REPAIR OPTION NR 1. DRILLED FASTENER HOLES ON NEW SEAT TRACK EXTRUSION PIECE REF SRM 53-00-52. REPAIR OPTION NR Jun 3, 2015 · N762AS · Boeing 7374Q8 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2015051912022Link · corrodedAFTER REMOVING EXPANSION LINK TO REPLACE PIVOT FOUND EXFOLIATING CORROSION ON EXPANSION LINK AT LBL 24, BS 520. ACFT GROUNDED. REMOVED DAMAGED EXPANSION LINK AND REPLACED WITH NEW EXPANSION LINK IAW BSOPM 20-50-01 AND SRM 51-40-05-0G-0.May 19, 2015 · N763AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2015051912020Link · corrodedAFTER REMOVING EXPANSION LINK TO REPLACE PIVOT, FOUND EXFOLIATING CORROSION ON EXPANSION LINK AT LBL 45, BS 520. ACFT GROUNDED. REMOVED DAMAGED EXPANSION LINK AND REPLACED WITH NEW EXPANSION LINK IAW BSOPM 20-50-01 AND SRM 51-40-05-0G-0.May 19, 2015 · N763AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2015051811971Fitting · corrodedRT INBD FLAP, EB RIB TORQUE TUBE FITTING HAS PITTING , DISCOVERED AFTER REMOVING TORQUE TUBE. ACFT GROUNDED. REMOVED DAMAGE, FOUND TO BE ACCEPTABLE FOR CONTINUED SERVICE IAW SAS EA 400, 57EA, 15179, REV. NEW DATED 04JUN15. THIS IS A CATEGORY B REPAIR STAGEMay 18, 2015 · N763AS · Boeing 7374Q8 · Trailing Edge Flap Control SystemSDR ASAA2015051612092Floorbeam · corrodedBS 500C FLOORBEAM LOWER FLANGE IS CORRODED AT LBL 10. ACFT GROUNDED. REMOVED CORROSION, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-51-1A-1, REPAIRED IAW 53EA-15206.May 16, 2015 · N763AS · Boeing 7374Q8 · Fuselage Main, Floor BeamSDR ASAA2015051514492Skin · gougedLEFT FUSELAGE SKIN AT GROUND A/C DOOR CUTOUT IS GOUGED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN AT AC DOOR CUTOUT IAW SRM 53-30-01-2R-2. THIS IS A CATEGORY B REPAIR WITH INSPECTION THRESHOLD OF 30,000 FLT CYCLES, FLT CYCLES AFTER REPAIR WITH INSPECTION INTERVAMay 15, 2015 · N760AS · Boeing 7374Q8 · Fuselage Main, Plate/SkinSDR ASAA2015051511870Angle · corrodedKEEL BEAM INTERIOR AFT ANGLE CORRODED, FWD ACCESS AREA AFT OF ROTATING BEACON. ACFT GROUNDED. REMOVED CORRODED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-12-1A-1 DETAIL 7. REMOVED ANGLE FABRICATED NEW ANGLE AND INSTALLED IAW SRM 51-40-05-0G-0 AND 51-40-02-May 15, 2015 · N760AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2015051511869Skin · gougedLT FUSELAGE SKIN AT GROUND, ACFT DOOR CUTOUT IS GOUGED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN AT ACFT DOOR CUTOUT IAW SRM 53-30-01-2R-2. THIS IS A CATEGORY B REPAIR WITH INSPECTION THRESHOLD OF 30,000 FLT CYCLES, FLT CYCLES AFTER REPAIR WITH INSPECTION INTEMay 15, 2015 · N760AS · Boeing 7374Q8 · Fuselage Main, Plate/SkinSDR ASAA2015051511868Doubler · corrodedLOWER ROTATING BEACON ATTACH DOUBLER CORRODED, INSIDE KEEL BEAM FWD ACCESS AREA. ACFT GROUNDED. REMOVED CORRODED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-12-1A-1, DETAIL 7. REMOVED DOUBLER FABRICATED NEW DOUBLER AND INSTALLED IAW SRM 51-40-05-0G-0 AND 51-May 15, 2015 · N760AS · Boeing 7374Q8 · Fuselage Main, Plate/SkinSDR ASAA2015051411886Skin · crackedR2 DOOR CRACKED IN SKIN FWD LWR CORNER NDT VERIFIED. ACFT GROUNDED. REPAIRED R2 CRACKED FWD LOWER SKIN IAW SRM 53-00-01-2R-32, REPAIR 32. THIS REPAIR IS A CATEGORY B REPAIR AND REG INSPECTION WITH THRESHOLD OF 66000 AND INTERVAL OF 24000 FLIGHT CYCLES CURREMay 14, 2015 · N760AS · Boeing 7374Q8 · Service DoorsSDR ASAA2015051411872Floorbeam · crackedFOUR CRACKS IN BBL 0.07 FLOORBEAM WEB LT SIDE AT BS 710.1. ACFT GROUNDED. REPAIRED BBL 0.07 FLOORBEAM WEB LT SIDE AT BS 710 IAW ASA T/C AD20080421-400-57-6.May 14, 2015 · N760AS · Boeing 7374Q8 · Fuselage Main, Floor BeamSDR ASAA2015051411871Channel · corrodedAFT WASTE WATER DRAIN MAST CHANNEL IS CORRODED. ACFT GROUNDED. REPAIRED THE AFT WASTE WATER DRAIN MAST CHANNEL IAW EA 400, 53EA, 15136.May 14, 2015 · N760AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2015051312193Rib · crackedRIGHT WING RIB AT WBL 135 LOWER RIB CHORD BETWEEN STR 2 AND 3 IS CRACKED. ACFT GROUNDED. REPAIRED DAMAGE TO RT WING LWR RIB CHORD, WBL 135 IAW EA 400, 57EA 15246.May 13, 2015 · N763AS · Boeing 7374Q8 · Wing, Rib/BulkheadSDR ASAA2015051312192Rib · crackedLT WING RIB AT WBL 135, LOWER RIB CHORD BETWEEN STR 2 AND 3 IS CRACKED. ACFT GROUNDED. REPAIRED DAMAGE TO LT WING LWR RIB CHORD, WBL 135 IAW EA 400, 57EA 15246.May 13, 2015 · N763AS · Boeing 7374Q8 · Wing, Rib/BulkheadSDR ASAA2015051312031Shear Tie · corrodedAFT CARGO FRAME AT BS 887 BETWEEN STR 25 AND 26 RT HAS CORROSION. ACFT GROUNDED. CORROSION BEYOND LIMITS.May 13, 2015 · N763AS · Boeing 7374Q8 · Fuselage Internal Mounting StructureSDR ASAA2015051312018Floorbeam · crackedFLOORBEAM BS 661 BL 0 UPPER TEE IS CRACKED OUT OF FLOOR PANEL ATTACH HOLE AT . ACFT GROUNDED. REPAIRED THE FLOORBEAM IAW T/C AD20080421, 400-57-5, REV 0.May 13, 2015 · N763AS · Boeing 7374Q8 · Fuselage Main, Floor BeamSDR ASAA2015051312016Floor Support · corrodedAFT CARGO FLOOR SUPPORT ANGLE JUST INBD OF STR 27LT IS CORRODED AT FS 747. ACFT GROUNDED. REPAIRED AFT CARGO FLOOR SUPPORT IAW SRM 53-00-53-2 R 1, REPAIR 1.May 13, 2015 · N763AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2015051212194Stringer · corrodedAPU TORQUE BOX INLET UPPER STRINGER IS CORRODED. ACFT GROUNDED. R & R STRINGER IAW SRM 51-40-02-0G-0-1 1.0, O .065, R .045, L 12, D .020.May 12, 2015 · N763AS · Boeing 7374Q8 · Fuselage Main, Structure
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