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 ASAA2014021006953Frame · crackedLEFT FRAME IS CRACKED AT INBD HOLE OF THE ATTACH POINT. ACFT GROUNDED. CUT OUT DAMAGE AREA FABRICATED, LOCATED, DRILLED AND INSTALLED TWO REPAIR ANGLES AT LT FRAME IAW T/C AD 20062609-400-53-1-760.Feb 10, 2014 · N760AS · Boeing 7374Q8 · Fuselage Main, FrameSDR ASAA2014021006950Skin · delaminatedRT INBD FOREFLAP UPPER SURFACE EXISTING DOUBLER IS DELAMINATED. ACFT GROUNDED. REPAIRED RT INBD FOREFLAP UPPER SURFACE EXISTING DOUBLER IAW SRM 51-70-10-2R-4, REPAIR 4.Feb 10, 2014 · N760AS · Boeing 7374Q8 · Trailing Edge FlapsSDR ASAA2014021006911Attach Fitting · crackedINTERCOSTAL ATTACH FITTING IS CRACKED AT BS 360, S9L. ACFT GROUNDED. R & R FITTING IAW SRM 51-40-02-0G-0.Feb 10, 2014 · N760AS · Boeing 7374Q8 · Fuselage Main, Attach FittingsSDR ASAA2014020907214Stringer Clip · crackedBS 400 STRINGER CLIP 8R IS CRACKED. ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G0.Feb 9, 2014 · N760AS · Boeing 7374Q8 · Fuselage Main, Attach FittingsSDR ASAA2014020907087Hinge Fitting · crackedINBD OF SKATE ANGLE ON VERTICAL STAB LT SIDE, AFT OF THE HINGE FITTING IS CRACKED. ACFT GROUNDED. PERFORMED EDGEBLEND OF FREE FLANGE OF DAMAGED AREA, FOUND TO BE WITHIN LIMITS IAW SRM 55-30-10-1A-1.Feb 9, 2014 · N760AS · Boeing 7374Q8 · Vertical StabilizerSDR ASAA2014020906970Frame · crackedFRAME AT BS 360 CRACKED BETWEEN STR 8-9L. ACFT GROUNDED. REPAIRED FRAME IAW ASA T/C AD20062609-400-53-1-760.Feb 9, 2014 · N760AS · Boeing 7374Q8 · Fuselage Main, FrameSDR ASAA2014020806805Door · out of rigF/A REPORTS L2 DOOR DIFFICULT TO CLOSE. ACFT GROUNDED. FOUND L-2 DOOR OUT OF RIG. ACCOMPLISHED RIG ON L-2 DOOR HORIZONTAL ROD, GUIDE ARM & STOP PINS IAW AMM 52-13-00-705-001 & OTHER RIG CHECKS CHECKED GOOD IAW AMM 52-13-00-705-001. ACCOMPLISHED LUBRICATION Feb 8, 2014 · N762AS · Boeing 7374Q8 · Passenger/Crew DoorsSDR ASAA2014020507230Frame · crackedFWD CARGO AFT SIDE FRAME BS 500 LOWER CORNER CLOSE OUT PANEL CRACKED. ACFT GROUNDED. R & R DOUBLER ON FWD CARGO AFT SIDE FS 500 LOWER CLOSE OUT PANEL IAW SRM 51-40-02.Feb 5, 2014 · N760AS · Boeing 7374Q8 · Fuselage Main, FrameSDR ASAA2014020507149Web · damagedAFT CARGO BAY DOORWAY FWD FRAME REVEAL WEB IS GOUGED AND CREASED OVER FRAME ON LOWER END. ACFT GROUNDED. FABRICATED NEW FRAME REVEAL WEB IAW SRM 51-40 05, TABLE I.Feb 5, 2014 · N760AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2014020507057Door Frame · crackedFWD CARGO BAY DOOR CUT OUT AFT FRAME CRACKED AT LWR AND UPPER STOP FITTINGS. ACFT GROUNDED. R & R CRACKED FRAME IAW SRM 51-40-02-0G-0.Feb 5, 2014 · N760AS · Boeing 7374Q8 · Fuselage Main, StructureSDR ASAA2014020506994Anchor Fitting · corrodedAFT CARGO BAY FWD ANCHOR PLATE TORN AND CORRODED ON MATING SURFACE. ACFT GROUNDED. RECEIVED NEW PART LOCATED AND DRILLED FASTENER HOLES ON NEW PART FOR AFT CARGO FWD ANCHOR PLATE IAW SRM 51-40-05-0G-0, FIG 2 DETAIL I, REMOVED CORROSION WAS FOUND TO BE OUT OFFeb 5, 2014 · N760AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2014012806749Stiffener · corrodedLOWER NOSE COMPARTMENT VERTICAL STIFFENER CORRODED AT BS 227.5 FWD SIDE OF BULKHEAD BL 0. ACFT GROUNDED. REMOVED CORRODED STIFFENER, FABRICATED, AND INSTALLED NEW STIFFNER IAW DWG 65-45801 AND SRM 51-40-02-0G-0.Jan 28, 2014 · N763AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2014012412488Guide · out of adjustF/A REPORTED R2 DOOR HARD TO OPEN & CLOSE. ACFT GROUNDED. ADJUSTED TOP HINGE GUIDE ARM DOOR. OPS AND CLOSES NORMAL IAW MM 52-13-00. OPS CHECKED GOOD IAW MM 52-13-00-705-003.Jan 24, 2014 · N764AS · Boeing 7374Q8 · Service DoorsSDR ASAA2014012112490Cargo Track · corrodedAFTER REMOVAL OF THE AFT CARGO BALLAST, THE AFT CARGO TRACK AT RBL 17.2 FOUND CORRODED. REPAIRED CARGO TRACK IAW SRM 53-00-53-2R-2.Jan 21, 2014 · N763AS · Boeing 7374Q8 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2014011812514Doubler · corrodedRIGHT FUSELAGE FWD OF BS 1088 AT TAILSKID DOUBLER HAS CORROSION. R & R TAILSKID DOUBLER IAW SRM 51-40-02-0G-0.Jan 18, 2014 · N779AS · Boeing 7374Q8 · Fuselage Main, Plate/SkinSDR ASAA2014011612445Structure · crackedCRACK AT LOWER LIGHTNING HOLE ON BOTTOM EDGE. BLENDED CRACK ON R2 DOOR LOWER LIGHTNING HOLE, FOUND TO BE OUT OF LIMITS, REPAIRED LIGHTNING HOLE IAW SRM 51-70-13-0G-0.Jan 16, 2014 · N763AS · Boeing 7374Q8 · Service DoorsSDR ASAA2014011612422Door · lack of lubeF/A REPORTS L1 DOOR VERY DIFFCUT TO LATCH CLOSED. ACFT GROUNDED. LUBED L1 DOOR, REF 12-25-21. PERFORMED FORWARD ENTRY DOOR TEST AMM REF 25-11-00. GVI PERFORMED AND DOOR FOUND SERVICEABLE. DOOR TORQUE TEST PERFORMED AND CHECK GOOD. AMM REF 25-11-00, DOORJan 16, 2014 · N756AS · Boeing 7374Q8 · Passenger/Crew DoorsSDR ASAA2014011212462Skin · crackedLEFT LOWER FUSELAGE EXTERNAL FWD A/C BAY GROUND SERVICE ACCESS DOOR CUTOUT FAIRING INBD SIDE SKIN IS BENT. ACFT GROUNDED. REMOVED DAMAGE IAW SRM 53-00-01-1A-1. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01-1A-1. FABRICATED -1, DOUBLER, -4 FILLERS, -5 TAPERED Jan 12, 2014 · N763AS · Boeing 7374Q8 · Fuselage Main, Plate/SkinSDR ASAA2014011212434Skin · chafedNR 2 SLAT INNER SURFACE CHAFED AT INBD END. ACFT GROUNDED. REPAIRED NR 2 SLAT IAW SRM 51-70-10-2R-4, REPAIR 4.Jan 12, 2014 · N763AS · Boeing 7374Q8 · Leading Edge DevicesSDR ASAA2014010912489Doubler · gougedRIGHT FUSELAGE EXTERNAL POWER DOOR CUTOUT IS GOUGED AT LOWER LAND. AREA REPAIRED IAW EA 400-53EA.Jan 9, 2014 · N763AS · Boeing 7374Q8 · Fuselage Main, Plate/SkinSDR ASAA2014010912460Door Frame · crackedFWD CARGO DOOR FORWARD FRAME IS CRACKED AT LOWER STOP FITTING, ACFT GROUNDED. R & R FWD CARGO DOOR CUT OUT FWD FRAME IAW SRM 51-40-02-0G-0-PAR-7D.Jan 9, 2014 · N763AS · Boeing 7374Q8 · Fuselage Main, StructureSDR ASAA2014010912444Skin · delaminatedNR 4 SLAT OTBD LOWER CORNER HAS EVIDENCE OF DELAMINATION. REPAIRED NR 4 SLAT OTBD LOWER CORNER IAW SRM 51-70-10-2R 2 PARA. DJan 9, 2014 · N763AS · Boeing 7374Q8 · Leading Edge DevicesSDR ASAA2014010912443Skin · delaminatedNR 4 SLAT UPPER SURFACE HAS EVIDENCE OF DELAMINATION. REPAIRED SLAT IAW SRM 51-70-10-2R-4, REPAIR 4.Jan 9, 2014 · N763AS · Boeing 7374Q8 · Leading Edge DevicesSDR ASAA2014010806752Slide · no testL2 DOOR SLIDE FAILED DEPLOYMENT TEST. TWO INTEGRAL LIGHTS FAILED TO ILLUMINATE. ACFT GROUNDED. SLIDE REPLACED ON T/C 61621-469 PNC.Jan 8, 2014 · N763AS · Boeing 7374Q8 · Escape SlideSDR ASAA2014010812447Tee Fitting · corrodedLEFT ACFT BAY DOOR INBD LANDING TEE FITTING IS CORRODED SEVERAL PLACES FRONT TO BACK. R & R TEE FITTING IAW SRM 51-40-02-0G-0.Jan 8, 2014 · N763AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2014010812355Skin · crackedCRACK FOUND ON FUSELAGE SKIN STA 941 TO 944.2, BETWEEN STR 24R AND 25R. ACFT GROUNDED. REPAIRED SKIN IAW SRM 53-00-01-2R-31, CAT B REPAIR INSPECTION THRESHOLD 66,000, FOR METHOD AND INTERVAL REFER TO OPERATORS REPAIR ASSESSMENT PROGRAM.Jan 8, 2014 · N762AS · Boeing 7374Q8 · Fuselage Main, Plate/SkinSDR ASAA2014010712464Skin · crackedFOUND A CRACK AT BS 941 TO 944, 2.75 INCHES LONG BETWEEN STRINGERS 24 & 25R. ACFT GROUNDED. REPAIRED SKIN IAW SRM 53-00-01-2R-31, CAT B REPAIR.Jan 7, 2014 · N762AS · Boeing 7374Q8 · Fuselage Main, Plate/SkinSDR ASAA2014010512304Skin · crackedNR 3 L/E SLAT ACTUATOR CUTOUT CRACKED. ACFT GROUNDED. REPAIRED NR 3 L/E SLAT ACTUATOR CUTOUT IAW SRM 57-41-01-2R-7, REPAIR 4, PROCEDURE 1.Jan 5, 2014 · N778AS · Boeing 7374Q8 · Wing, Plate/SkinSDR ASAA2014010212316Cover · looseAFT EXIT LIGHT COVER LOOSE. ACFT GROUNDED. REPLACED AFT L2 DOOR EXIT LIGHT ASSY. OPTS CHECKED GOOD IAW AMM 33-51-11.Jan 2, 2014 · N762AS · Boeing 7374Q8 · Emergency LightingSDR ASAA2013122012208Engine · odorF/A REPORTED SMOKE IN CABIN DURING CLIMB THROUGH 12,000 FT, ACCOMPLISHED QRH ITEMS, SMOKE SUBSIDED. RETURNED FOR NORMAL LANDING. ACFT GROUNDED. DIVERSION TIME 7 MINUTES. COMPLETED CONDITIONAL INSP, REF MM 05-51-56-200-801 & 21-00-01-101. NO LEAKING FLUIDSDec 20, 2013 · N764AS · Boeing 7374Q8 · Engine (Turbine/Turboprop)SDR ASAA2013121812307Web · damagedSHEAR WEB AFT OF L1 DOOR IS DAMAGED. ACFT GROUNDED. DISSASSEMBLED SHEAR WEB AFT OF L2 DOOR, FABBED NEW WEB, RE-ASSEMBLED SHEAR WEB IAW SRM 51-40-02-0G-0, 4-51-30-01-0G-0, NR 8.Dec 18, 2013 · N778AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2013121812239Skin · chafedRIGHT OTBD MID FLAP OTBD L/E CORNER IS CHAFED. REPAIRED RT OTBD MID FLAP OTBD L/E CORNER IAW SRM 57-53-01-2R-8.Dec 18, 2013 · N778AS · Boeing 7374Q8 · Trailing Edge FlapsSDR ASAA2013121812238Skin · chafedLEFT WING OTBD MIDFLAP INBD L/E IS CHAFED. REPAIRED LT OTBD MIDFLAP INBD L/E IAW SRM 57-53-01-2R-8.Dec 18, 2013 · N778AS · Boeing 7374Q8 · Trailing Edge FlapsSDR ASAA2013121612301Attach Angle · corrodedAPU COMPARTMENT RT TORQUE BOX SUPPORT ANGLE LOCATED AFT OF AFT AIR INLET CUTOUT HAS MID ATTACH CLIP CORROSION AND TWO ATTACH FASTENERS MISSING. ACFT GROUNDED. R & R SUPPORT ANGLE IAW SRM 51-40-02.Dec 16, 2013 · N778AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2013121496866Hinge Fitting · lack of lubeL2 DOOR DIFFICULT TO OPEN. ACFT GROUNDED. LUBRICATED HINGE GUIDE PLATES IAW AMM 12-25-11-603-001, DOOR OPERATES NORMALLY.Dec 14, 2013 · N765AS · Boeing 7374Q8 · Passenger/Crew DoorsSDR ASAA2013121212232Stringer · corrodedAPU RT TORQUE BOX AREA, APU INLET CUTOUT LWR STRINGER IS CORRODED, ACFT GROUNDED. BLENDED DAMAGED AREA REMAINING MATERIAL FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED STRINGER AND INSTALLED NEW STRINGER IAW SRM 51-40-02-0G-0.Dec 12, 2013 · N778AS · Boeing 7374Q8 · Fuselage Main, Longeron/StringerSDR ASAA2013121112260Beam · crackedHORIZONTAL STABILIZER CENTER SECTION LT THRUST BEAM LOWER OTBD CORNER FITTING IS CRACKED ON HORIZONTAL FLANGE. COMPLIED WITH T/C SB737-55-1091-400-1 FOR LEFT SIDE THRUST BEAM CORNER FITTING REPLACEMENT ONLY IAW EA 400-55EA-11823.Dec 11, 2013 · N778AS · Boeing 7374Q8 · Horizontal Stabilizer StructureSDR ASAA2013121012221Support Angle · corrodedAFT CARGO BAY LT TRANSITION ANGLE HAS CORROSION FROM BS 767 TO 817. REMOVED CORROSION IAW SRM 53-60-53-1A-1. REPAIRED ANGLE IAW SRM 53-60-53-2R-4, REP 4.Dec 10, 2013 · N778AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2013120896688Lens · dislodgedEMERGENCY EXIT SIGN OVER ROWS 16-17, ACFT RT, FELL OFF AND IS TAPED IN PLACE, APPEARS TO BE MISSING A SCREW. ACFT GROUNDED. RE-INSTALLED EMERG. EXIT SIGN COVER ACFT RT ROWS 16 & 17.Dec 8, 2013 · N756AS · Boeing 7374Q8 · Emergency LightingSDR ASAA2013120796883Bullnose · crackedNR 2 SPOILER INBD HINGE BULLNOSE IS CRACKED, INBD OF HINGE ON TOP OF WING. ACFT GROUNDED. R & R NR 2 SPOILER INBD OF HINGE BULLNOSE PANEL IAW SRM 51-40-02 AND 51-40-05.Dec 7, 2013 · N754AS · Boeing 7374Q8 · SpoilersSDR ASAA2013120612306Structure · corrodedAPU BAY RT SIDE AFT AIR INLET DUCT CUTOUT SURROUND LANDING HAS MULTIPLE CORROSION AREAS. ACFT GROUNDED. REMOVED AND INSTALLED NEW TEE IAW SRM 51-40-02.Dec 6, 2013 · N778AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2013120612291Support Angle · corrodedAPU COMPARTMENT, RT AFT AIR INLET CUTOUT, AFT SUPPORT ANGLE CORRODED. ACFT GROUNDED . R & R SUPPORT ANGLE IAW SRM 51-40-02.Dec 6, 2013 · N778AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2013120612290Support Angle · corrodedAPU COMPARTMENT ON RT WEB ANGLE BETWEEN TWO CUTOUTS HAS CORROSION ON AFT END. ACFT GROUNDED. R & R SUPPORT ANGLE IAW SRM 51-40-02.Dec 6, 2013 · N778AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2013120612284Attach Angle · corrodedAPU COMPARTMENT RT TORQUE BOX WEB SUPPORT FRAME BS 1129, MID ATTACH ANGLE HAS CORROSION. ACFT GROUNDED. REMOVED AND INSTALLED NEW ATTACH ANGLE IAW SRM 51-40-02.Dec 6, 2013 · N778AS · Boeing 7374Q8 · Fuselage Main, Attach FittingsSDR ASAA2013120612176Tee Fitting · corrodedON BACK SIDE OF APU COMPARTMENT, RT WEB, THE SUPPORT FRAME FWD OF THE AFT CUTOUT HAS MID ATTACHMENT ANGLE CORRODED. ACFT GROUNDED. R & R TEE ANGLE IAW SRM 51-40-02, W .5", O .094, R .049", L .5", D .045".Dec 6, 2013 · N778AS · Boeing 7374Q8 · APU Cowling/ContainmentSDR ASAA2013120512171Doubler · corrodedANTENNA DOUBLER CORRODED BETWEEN FS 500A AND STR 27L AND 27R. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01-1A1. R & R VHF ANTENNA DOUBLER IAW SRM 51-40-02-0G-0, W 2", O .050", R .043", L 3", D .007.Dec 5, 2013 · N754AS · Boeing 7374Q8 · Fuselage Main, Plate/SkinSDR ASAA2013120596854Panel · crackedACCESS PANEL 5815 CRACKED. INSTALLED NEW ACCESS PANEL.Dec 5, 2013 · N754AS · Boeing 7374Q8 · Nacelle/Pylon, Main FrameSDR ASAA2013120596828Stiffener · crackedDURING DISASSEMBLING OF RT RAM AIR INLET LOWER DUCT WALL ASSY, FOUND LOWER WEB UPPER STIFFENER ANGLE RADIUS CRACKED. FABRICATED NEW STIFFENER IAW SRM 51-40-05-06-0.Dec 5, 2013 · N754AS · Boeing 7374Q8 · Fuselage Miscellaneous StructureSDR ASAA2013120596798Angle · corrodedAFT CARGO BAY BS 947, LOWER BULKHEAD SUPPORT ANGLE IS CORRODED LBL 20 TO RBL 20. REMOVED ANGLE IAW SRM 51-40-02. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-0I-1. INSTALLED NEW ANGLE IAW SRM 51-40-02.Dec 5, 2013 · N754AS · Boeing 7374Q8 · Fuselage Main, BulkheadSDR ASAA2013120596732Angle · corrodedAFT CARGO FLOOR STRUCTURE RT TRANSITION ZEE CORRODED IN MULTIPLE AREAS ON UPPER AND LWR SURFACES FROM BS 727 TO STA 727F. R & R TRANSITION ANGLE IAW SRM 51-40-02-0G-0.Dec 5, 2013 · N754AS · Boeing 7374Q8 · Fuselage Miscellaneous Structure
Back to Boeing 737-4Q8