Boeing 737-4Q8
Service difficulty reports · 6,249
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR Q2SA20161204296Strap · corrodedAFT CARGO BAY AT BS 727D, BETWEEN STRINGERS 25L AND 25R, FLOORBEAM STRAP CORRODED. REPLACED THE STRAP IAW SRM 51-10-01 PARA 8. AIRCRAFT GROUNDED.SDR ASAA2016120121270Threshold · corrodedAFT CARGO DOOR THRESHOLD AFT CORNER CRACKED. ACCOMPLISHED TEMP REPAIR PER EA 5310-01251. ACFT GROUNDED.SDR ASAA2016120119045Skin · crackedFUSELAGE SKIN HAS A CRACK AT CHEM MILL STEP STRINGER 1 BS 437 - 439. ACFT GROUNDED. ACCOMPLISHED REPAIR TO FUSELAGE SKIN ON T/C AD20121204-420-53-3.SDR ASAA2016120119043Skin · crackedFUSELAGE SKIN HAS A CRACK AT CHEM MILL STEP STR 1, BS 447 - 448.5. ACFT GROUNDED. ACCOMPLISHED REPAIR TO FUSELAGE SKIN ON T/C AD20121204-400-53-3.SDR Q2SA20161130367Skin · damagedAIRCRAFT GROUNDED. UPPER FUSELAGE EXTERIOR FUSELAGE AT BS778 BETWEEN STR3L AND STR4L SKIN SECTION WITH LIGHTNING STRIKE. REPAIRED FUSELAGE SKIN IAW SRM 53-00-01 REPAIR 19 FIG 201 SECTION II.SDR Q2SA20161130366Skin · damagedAIRCRAFT GROUNDED. UPPER FUSELAGE EXTERIOR FUSELAGE, AT BS737D+6IN BETWEEN STR3L AND STR4L SKIN SECTION WITH LIGHTNING STRIKE. REPAIRED FUSELAGE SKIN AT BS737D+6IN DUE TO LIGHTNING STRIKE IAW SRM 53-00-01 REPAIR 19 FIG 201 SECTION I.SDR Q2SA20161130365Skin · damagedAIRCRAFT GROUNDED. UPPER FUSELAGE EXTERIOR FUSELAGE, AT BS701 BETWEEN STR3L AND STR4L SKIN SECTION WITH LIGHTNING STRIKE. REPAIRED FUSELAGE SKIN AT BS701 BETWEEN STR3L AND STR4L DUE TO LIGHTNING STRIKE IAW SRM 53-00-01 REPAIR 19 FIG201 SECTION II.SDR Q2SA20161130364Skin · damagedAIRCRAFT GROUNDED. UPPER FUSELAGE EXTERIOR FUSELAGE, AT BS686 BETWEEN STR3L AND STR4L SKIN SECTION WITH LIGHTNING STRIKE. REPAIRED FUSELAGE SKIN AT BS686 BETWEEN STR3L AND STR4L DUE TO LIGHTNING STRIKE IAW SRM 53-00-01 REPAIR 19 FIG 201 SECTION II.SDR Q2SA20161130363Skin · damagedAIRCRAFT GROUNDED. UPPER FUSELAGE EXTERIOR FUSELAGE AT BS640 AT STR3L SKIN SECTION WITH LIGHTNING STRIKE. REPAIRED FUSELAGE SKIN AT BS640 AT STR3L DUE TO LIGHTNING STRIKE IAW SRM 53-00-01 REPAIR 19 FIG201 SECTION II.SDR Q2SA20161130362Skin · damagedAIRCRAFT GROUNDED. UPPER FUSELAGE EXTERIOR FUSELAGE AT BS622 BETWEEN STR3L AND STR4L SKIN SECTION WITH LIGHTNING STRIKE. REPAIRED FUSELAGE SKIN AT BS622 BETWEEN STR3L AND STR4L DUE TO LIGHTNING STRIKE IAW SRM 53-00-01 REPAIR 19 FIG201 SECTION I.SDR Q2SA20161130361Skin · damagedAIRCRAFT GROUNDED. UPPER FUSELAGE EXTERIOR AT BS610 AT STR3L SKIN SECTION WITH LIGHTNING STRIKE. REPAIRED FUSELAGE SKIN AT BS610 AT STR3L DUE TO LIGHTNING STRIKE IAW SRM 53-00-01 REPAIR 19 FIG 201 SECTION II.SDR Q2SA20161130360Skin · damagedAIRCRAFT GROUNDED. UPPER FUSELAGE EXTERIOR FUSELAGE AT BS580 AT STR3L SKIN SECTION WITH LIGHTNING STRIKE. REPAIRED FUSELAGE SKIN AT BS580 AT STR3L DUE TO LIGHTNING STRIKE IAW SRM 53-00-01 REPAIR 19 FIG 201 SECTION II.SDR ASAA2016113019037Bear Strap · corrodedFWD CARGO DOOR CUTOUT AFT SIDE INTERNAL BEARSTRAP HAS CORROSION UNDER SFT CORNER SCUFF PLATE LOCATION. ACFT GROUNDED. REPAIRED THE BEARSTRAP IAW EA 400-53EA-18213 REV 00.SDR ASAA2016113018974Frame · cracked1.04 WIRE PENETRATION HOLE ON FRAME CRACKED AT BS 500D ON AFT SIDE BETWEEN STRINGERS 20 AND 21L. ACFT GROUNDED. REPAIRED THE FRAME IAW SRM 53-00-07-2R-20.SDR ASAA2016113018965Stringer Clip · crackedFWD CARGO BAY BS 500C STRINGER CLIP AT 22R IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0.SDR ASAA2016112919014Bear Strap · crackedFWD ENTRY DOOR CUT OUT LOWER AFT CORNER HAS A CRACK ON BEAR STRAP. GROUNDED - YES. REPAIRED DAMAGE TO SKIN IAW B737 400 SRM 53 10 01 2R 12. THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 60,000 TOTAL FLIGHT CYCLES OR 12,000 FLT. CYCLES AFTER REPAISDR ASAA2016112318834Snubber · failedFA'S REPORTS L2 DOOR STIFF AND HARD TO OPEN/CLOSE. GROUNDED, YES. REMOVED & REPLACED SNUBBER REF AMM 52-13-71. OPS CK'S GOOD.SDR Q2SA2016120700263Shear Tie · corrodedAIRCRAFT GROUNDED. AFT CARGO COMPARTMENT AT BS 727C, BETWEEN STR 26L & 27L FRAME SHEAR TIE WITH CORROSION. REMOVED CORROSION. REWORKED AREA OUT OF ALLOWABLE DAMAGE LIMIT IAW B737-400 SRM 53-00-07. FABRICATED SHEAR TIE, SUPPORT AND FILLER IAW APPROVED SPECIFICASDR ASAA2016102318484O-Ring · damagedDURING TAXI, NR 2 ENGINE SHUTDOWN ON ITS OWN. ENGINE PARAMETERS WERE ALL WITHIN LIMITS. ACFT GROUNDED. STARTED NR 2 ENGINE, INDICATIONS FLUCTUATING, N1 21.9 TO 21.2, EGT 460 TO 450, N2 59.6 TO 59.0, FF 85-75, APPROX 3 MIN AFTER INITIAL ENGINE START, ALL ENGISDR 4AER20161102006Door · corrodedAFT CARGO DOOR REPLACED DUE TO EXCESSIVE CORROSION.SDR 4AER20161014010Spar · crackedRIGHT HAND WING REAR SPAR UPPER CHORD AND MAIN LANDING GEAR AFT SUPPORT FITTING, NUMBER 3 & 4 INBOARD HOLES HAVE CRACKS.SDR 4AER20161014009Spar · crackedLEFT HAND WING REAR SPAR UPPER CHORD AND MAIN LANDING GEAR AFT SUPPORT FITTING, FOUR INBOARD HOLES HAVE CRACKS.SDR 4AER20161103006Sink · corrodedNUMBER 1 GALLEY SINK AND FLOOR AREAS HAD CORROSION.SDR 4AER20161103002Door · corrodedFORWARD LAVATORY DOOR ASSEMBLY HAS CORROSION ON INNER SURFACE.SDR 4AER20161014005Angle · corrodedSTRINGER 27R KEEL ANGLE AT BS 727D=10.75" HAS CORROSIONSDR 4AER20161014004Angle · corrodedSTRINGER 27L KEEL BEAM ANGLE AT BS 727D+10.75" HAS CORROSION.SDR 4AER20161014003Skin · corrodedEXTERNAL FUSELAGE SKIN FROM BS 1006-1016 & STRINGER 27L-24R HAS CORROSIONSDR 4AER20161102005Door · corrodedRIGHT EMERGENCY EXIT DOOR AT BS 627.5 HAS BEEN REPLACED DUE TO EXCESSIVE CORROSION.SDR 4AER20161102004Door · corrodedLEFT EMERGENCY EXIT DOOR AT BS 627.5 HAS BEEN REPLACED DUE TO EXCESSIVE CORROSION.SDR 4AER20161102003Door · corrodedRIGHT EMERGENCY EXIT AT BS 589.5 HAS BEEN REPLACED DUE TO EXCESSIVE CORROSION.SDR 4AER20161102002Door · corrodedLEFT FORWARD EMERGENCY EXIT DOOR AT BS 589.5 HAS BEEN REPLACED DUE TO EXCESSIVE CORROSION.SDR 4AER20161103004Intercostal · corrodedINTERCOSTAL WEBBING AND FLANGE AT BS 727A TO 727A+10 CORRODED.SDR ASAA2016093018409Stringer · corrodedEND FITTING AT BS 540 STRINGER 22R IS CORRODED. ACFT GROUNDED. REMOVED AND REPLACED THE END FITTING IAW SRM 51-40-02-0G.SDR ASAA2016092818403Bear Strap · crackedL1 DOOR LOWER HINGE CUT OUT SHOWS CRACK INDICATION IN HOLE. GROUNDED, YES. CRACKS FOUND AT UPPER AND LOWER HINGE CUT OUTS REPAIR OF BOTH CRACKS TO BE REPAIRED ON MIG5 OK33947 W/O 1013489 2000/0110.SDR ASAA2016092818402Bear Strap · crackedL1 DOOR UPPER HINGE CUT OUT SHOWS CRACK INDICATION IN HOLE MARKED. GROUNDED, YES. REPAIRED CRACKS AT UPPER AND LOWER HINGE CUT OUTS IAW EA 400-53EA-17876. THIS IS A CATEGORY B REPAIR WITH STAGE 1 APPROVAL 2ND AND 3RD STAGE DT DATA TO DEMONSTRATE COMPLIANCE SDR 4AER20161014008Skin · corrodedEXTERNAL FUSELAGE SKIN FROM BS 907-1016 & STRINGERS 25L-25R HAS CORROSION.SDR 4AER20161103008Bracket · corrodedFLOOR BRACKET AT BS 998 & STRINGER 17R HAS CORROSIONSDR ASAA2016092118356Skin · crackedFUSELAGE SKIN CRACKED AT THE R1 DOOR LOWER AFT CORNER. ACFT GROUNDED. REPAIRED THE SKIN IAW SRM 53-10-01-2R 2 REP 2.SDR ASAA2016092118205Skin · crackedCRACK IN FUSELAGE SKIN BS 727E +3 BELOW STRINGER 22L. ACFT GROUNDED. REPAIRED THE SKIN IAW SRM 53-00-01 REP. 31.SDR ASAA2016092018364Frame · crackedFUSELAGE FRAME AT BS 360 INSULATION STAND OFF HOLE BETWEEN STRINGERS 19 AND 20R SHOWS CRACK INDICATION IAW T/C AD20152308-400-53-11. ACFT GROUNDED. REPAIRED THE DAMAGE IAW EA 400-53EA-17811.SDR 4AER20161102009Floor Panel · corrodedAFT CARGO COMPARTMENT FROM BS 727-727D FLOOR PANEL HAS EXCESSIVE CORROSION.SDR 4AER20161102007Frame · corrodedRIGHT HAND RUDDER UPPER AFT CORNER CONDUCTIVE FRAME AT RUDDER STATION 234.89 HAS CORROSION.SDR ASAA2016091518055Battery Pack · dischargedR2 DOOR INTERIOR EMERGENCY EXIT LIGHT ABOVE DOOR ONLY ILLUMINATES FOR 5-10 SECONDS. ACFT GROUNDED. REPLACED R2 DOOR EMERGENCY LIGHT BATTERY PACK, REF AMM 33-51-51. OPS NORMAL.SDR 4AER20161102010Pan · corrodedLEFT HAND WATER SERVICE PAN INNER SURFACE HAS CORROSION.SDR ASAA2016082817835Roller · out of positionCAPTAIN'S SLIDING WINDOW DIFFICULT TO OPEN AND CLOSE. ACFT GROUNDED. FOUND AFT LOWER ROLLER CAME OFF FROM AFT LOWER BELLCRANK, REF AMM 56-12-11-825-001. REPLACED LOWER AFT ROLLER & SHIMMED. ALSO UPPER ROLLER SHIMMED FOR PROPER ENGAGEMENT IAW AMM 56-12-11-4SDR 4AER20161017002Skin · corrodedSKIN PANEL FROM BS 727G TO 907 & STRINGER 25L TO 25R HAD CORROSION.SDR Q2SA20160816257Actuator · wornAIRCRAFT GROUNDED AFTER EMERGENCY LANDING DECLARED, LANDED WITH NO INCIDENT. LEADING EDGE FLAP IN-TRANSIT LIGHT REMAINED ON NR 1 LE DEVICE IS AMBER. MX REPLACED THE NR 1 KRUEGER FLAP ACTUATOR AND REPLACED THE FLAP/SLAT POSITION INDICATOR MODULE.SDR Q2SA20160816256Indicator · dirtyAIRCRAFT GROUNDED AFTER EMERGENCY LANDING DECLARED. LE FLAPS TRANSIT LIGHT AFTER SELECTING FLAP TO 1 DEG. LE DEVICES OVERHEAD PANEL LIGHT FLPAS 1 AMBER AND 2 WAS BLACK. REMOVED CLEANED AND REINSTALLED LE FLAP SLAT INDICATING MODULE PER AMM 27-88-41 BITE CHECK/SDR 4AER20161014007Skin · corrodedEXTERNAL FUSELAGE SKIN FROM BS 727G TO 907 & STRINGERS 20 TO 25R HAS CORROSION.SDR 4AER20161014006Bear Strap · corrodedAFT CARGO DOOR CUTOUT BEAR STRAP HAS CORROSION.
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