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 EE4Y2020020210596Fitting · wornSECTION 46 RH STRUT SUPPORT FITTING AFT LUG AT BS 685 WITH WEAR. THE PART WAS REPAIRED IAW BOEING ID #3-4617944374 UNDER 8100-9 FORM AND COOPESA EO COO-EO-2020-10578 R01SDR EE4Y2020020210594Stringer · corrodedAFT CARGO COMPART. STRINGER 26R WITH EXISTING REPAIR LOCATED BTWN S-787 / S-807. THE STRINGER WAS REPAIRED IAW AEI TICKET 10188.SDR EE4Y202002010593Tripler · corrodedAFT CARGO COMPT. DOOR CUT OUT WITH INTERNAL TRIPLER CORRODED LOCATED BTWN STA787 / STA 794.3 AND BTWN S-25R / S-26R. THE MENTIONED PART WAS REPAIRED IAW FROM AEI REF. TICKET 10188.SDR EE4Y202002010590Structure · corrodedLOWER FUSELAGE AFT CARGO COMPT. AT BS 727F BTWN S-27L AND S-27R WITH LOWER SECTION CLIPS CORRODED. THE MENTIONED CLIPS WERE REPLACED.SDR EE4Y202002010589Shear Tie · corrodedLOWER FUSELAGE AFT CARGO COMPT. AT BS 727F BTWN S-27L AND S-26R WITH LOWER SECTION CORRODED. THE MENTIONED PART WAS REPAIRED IAW B737-400 SRM 53-00-07-2R-17 REPAIR 17 FIG. 202 DETAIL V.SDR EE4Y202002010588Shear Tie · corrodedLOWER FUSELAGE AFT CARGO COMPT. AT BS 887 BTWN S-27L AND S-27L WITH LOWER SECTION CORRODED. THE MENTIONED PART WAS REPAIRED IAW B737-400 SRM 53-00-07-2R-17 REPAIR 17 FIG. 202 DETAIL VI.SDR EE4Y202002010585Skin · wornLH WING O/B MID FLAP LOWER SURFACE WITH WEAR AT WBL 255. THE MENTIONED PART WAS REPAIRED IAW BOEING ID #3-4620339317 AND COOPESA E.O. COO-EO-2020-10540-R01SDR I5EA2020021104Battery Pack · inoperativeRIGHT AFT SERVICE DOOR EMERGENCY LIGHT EXTERIOR AND INTERIOR INOP. ITEM M1137 STA975RSDR I5EA20191030904Battery · no testFT CABIN EMERGENCY LIGHT BATTERY M1197 HAS SHORT ON CYCLES TIME.SDR I5EA201910231002Power Supply · inoperativeR/H EMERGENCY LIGHT INOP R2 DOOR.SDR I5EA201910110906Power Supply · inoperativeBULLNOSE EMERGENCY LIGHT INOP AT SEAT ROW 14DF, 16DF, AND 18DF.SDR I5EA2019070900002Slide · unwanted deployDISCREPANCY: L1 DOOR SLIDE INADVERTANLY DEPLOYED. CORRECTIVE ACTION: LOGPAGE # 34538 REMOVED AND REPLACED L1 DOOR SLIDE IAW AMM 25-61-35. INSPECTED NO DEFECTS NOTED.SDR Q2SA20190522418Control Panel · shortedAIRCRAFT GROUNDED. ELECTRICAL SMOKE SMELL @ FL 340. MCP FAILED VNAV AND LNAV. ALL INDICATIONS FAILED TO INPUTS. MCP REMOVED AND REPLACED MCP 22-11-34-004-003 AND -004. DFCS MCP BITE TEST GOOD IAW AMM 22-11-34-745-001. ACFT OK FOR SERVICE. PILOT STATED THAT SMSDR I5EA2019052100032Toilet · overflowDISCREPANCY: AIR RETURN TO MDSD DUE TO LT AFT TOLIET OVER FLOWING INTO GALLEY AREA. CORRECTIVE ACTION: CLEANED AFT LT LAV AND GALLEY AREA. PERFORMED CONDITIONAL INSPECTION FOR TOLIET OVERSERVICING AND OVERWEIGHT LANDING IAW AMM 05-51-12 AND 05-51-74.SDR CA190422021Module · installed(CAN) LOSS OF HYDRAULIC SYSTEM B FLUID WHILE ENROUTE TO YEG. FLIGHT AND CABIN CREW ACTIONED APPROPRIATE CHECKLISTS, BRIEFED ALL PASSENGERS OF THE ABNORMAL CONDITION AND THAT EMERGENCY VEHICLES WOULD BE ON STANDBY, THEN COMPLETED PREPARATION OF THE AIRCRAFT FORSDR I5EA201904220003Battery Pack · dischargedDURING DAILY CHECKK FOUND L-2 DOOR EMERGANCY EXIT SIGN LIGHTS NOT WORKING. FOUND M1197 POWER SUPPLY BATTERY AT FAULT, REMOVED AND REPLACED BATTERY ASSEMBLY PER B-737 AMM 33-51-51. EMERGANCY EXIT LIGHT OPS OKAY.SDR UIEA2019F00131Flap System · malfunctionedRH INBOARD FORE-FLAP FAIL TO PROPERLY DEPLOY DURING TEST FLIGHT. CAUSING EMERGENCY LANDING (POSSIBLE DUPLICATE ENTRY)SDR UIEA201902270133Flap System · damagedRIGHT HAND OUTBOARD FORE-FLAP FAIL TO FULLY EXTEND DURING TEST FLIGHT. PILOT REQUESTED EMERGENCY EQUIPMENT BE PRESENT DURING LANDING AFTER TEST FLIGHT.SDR I5EA201812261204Ballast · inoperativeRH FWD OVERWING SIDEWALL LIGHT FOUND INOPERATIVE. REMOVED AND REPLACE RH OVERWING SIDEWALL LIGHT BALLAST IAW B737-400 AMM 33-21-32, OPERATION TESTS GOOD IAW B737-400 AMM 33-21-32DSDR A8ZR20181218001Cable · lack of lubeDURING TAKEOFF THE LANDING GEAR HANDLE WAS UNABLE TO GO INTO THE UP POSITION AND THE LANDING GEAR WERE UNABLE TO RETRACT. BOTH MLG AND NLG WERE CHANGED FOR TIME AT AERSALE IN ROSWELL, NM. AFTER THE AIRCRAFT LANDED SAFELY AND BROUGHT BACK INTO THE HANGAR AT AERSDR A8ZR20181211001Stop Fitting · not reportedACCOMPLISHED REPLACEMENT OF FUSELAGE FRAME P/N 65-20722U76 AT STA 440 AND S14R TO S28R FOR CRACK AT DOOR STOP #5. REF B737-400 SRM 51-40-02 REV 100 AND BOEING SB 737-53A1228 ORIG REV DTD JULY 10, 2003.SDR Q2SA20181114409Skin · chafedAIRCRAFT GROUNDED. LT WING OUTBD MID FLAP LOWER SKIN IS CHAFED NEAR INBD FLAP TRACK CUTOUT. REPLACED LT OUTBD MID FLAP. INSTALL AND ADJUSTMENTS TO BE ACCOMPLISHED ON CARD 8017551.SDR Q2SA20181114407Flap · dentedAIRCRAFT GROUNDED. RT INBD MID FLAP DENTED, 18Ï¿½ IN FROM EXHAUST GATE AND 5 Ï¿½ INCHES FROM THE T/E. OK TO INSTALL. REPAIRED R/H INBD MID FLAP IAW SRM 51-70-102R-2. SEE ATTACHED SHOP FOR WORK ACCOMPLISHED.SDR Q2SA201902275043Skin · chafedLH WING OB MID FLAP LOWER SKIN IS CHAFFED NEAR IB FLAP TRACK CUTOUT. FLAP REPLACED WITH P/N 65C26320-17, S/N 1953.SDR Q2SA201902273025Skin · delaminatedLH ELEVATOR DAMAGED AT STA 121.59SDR Q2SA201022796074Skin · dentedRH INBD MID FLAP DENTED, 18.0" FROM EXHAUST GATE AND 5.5" FROM TE.SDR Q2SA201902286073Skin · dentedRH IB AFT FLAP DENTED 10.0" IN FROM EXHAUST GATE 1.5" FROM TE.SDR Q2SA20181109412Light · inoperativeAIRCRAFT GROUNDED. LT FWD EMERGENCY SLIDE WHEN DEPLOYED DID NOT TRIGGER THE INTEGRAL LIGHTS. INSTALLED LT FWD DOOR SLIDE IAW AMM 25-61-35 TOOL# 346 DUE 23 MAR 19.SDR Q2SA20181109411Slide · defectiveAIRCRAFT GROUNDED. RT EMERGENCY FWD ESCAPE SLIDE FAILED TO DEPLOY CORRECTLY. REMOVED AND REPLACED R1 EMERGENCY SLIDE IAW AMM 25-61-35.SDR Q2SA201902278029Slide · no testLH FWD EMERGENCY SLIDE WHEN DEPLOYED DID NOT TRIGGER THE INTEGRAL LIGHTS. REPLACED WITH P/N 101660-107, S/N PAB626.SDR Q2SA201902278028Slide · no testRIGHT EMERGENCY FWD ESCAPE SLIDE FAILED TO DEPLOY CORRECTLY. REPLACED WITH P/N 10166-107, S/N PAB630.SDR Q2SA20181107410Battery · dischargedAIRCRAFT GROUNDED. ALL BATTERY PACKS FOR THE EMERGENCY LIGHTS FAILED DURING THE TESTS. REF TASK 3500444 2000-0105. REMOVED AND REPLACED ALL BATTERIES FOR THE EMERGENCY LIGHTING. REF TASK 33-51-51-962-015. OPS CHECKS PERFORMED - PASSED. REF TASK STEP 3E (4).SDR Q2SA2019022700105Battery Pack · no testBATTERY PACKS FOR THE EMERGENCY LIGHTS FAILED DURING THE TEST. PACKS REPLACED WITH P/N 2013-1A (9EA).SDR Q2SA20181105404Flap · gougedAIRCRAFT GROUNDED. FLAP 2 BY STATION 235 HAS DEEP GOUGE BY MOUNT BRACKET LT INBD FORE FLAP. SEE EA180602 IR FOR REPAIR PROCESS AND SHOP FOR ANY ADDITIONAL WORK STEPS COMPLETED.SDR Q2SA2019022700011Structure · gougedFLAP 2 BY STATION 235 HAS DEEP GOUGE BY MOUNT BRACKET L/H INBD FORE FLAP.SDR Q2SA20181031405Strap · not reportedAIRCRAFT GROUNDED. LOCATE AND FABRICATE AND DRILL UP, TREAT AND PRIME AND TOPCOAT NEW REPAIR STRAPS FOR SEAT TRACK LINK ASSEMBLIES. FABRICATED AND INSTALLED STRAPS ON CABIN DECK STA 520 TO 540 RBL 24.75, RBL 45.5, LBL 24.75, LBL 45.5 IAW EA180595 & EO 3753A156SDR Q2SA20181025413Floor Support · corrodedAIRCRAFT GROUNDED. CORROSION AT FLOOR SUPPORT IN SEVERAL AREAS ON UPPER JUST FWD OF CARGO DOOR ENTRANCE. REMOVED AND REPLACED FLOOR SUPPORT ON RT B2 787-807 PER 737-400-51-40-02.SDR Q2SA201902271679Floor Support · corrodedCORROSION AT FLOOR SUPPORT IN SEVERAL AREAS ON UPPER FLANGE, JUST FWD OF CARGO DOOR ENTRANCE.SDR Q2SA20181016403Shear Web · corrodedAIRCRAFT GROUNDED. CORROSION FOUND. SHEAR WEB JUST INBD AFT OF R2 DOOR AT BS 986.5 Ï¿½ BS 1016. REMOVED AND REPLACED WEB ON INBD AFT R2 DOOR AT BS 986.5 BS1016 IAW SRM 51-40-02.SDR Q2SA2019222700118Shear Web · corrodedCORROSION FOUND ON SHEAR WEB JUST INBD AND AFT OF R2 DOOR AT BS 986.5 TO 1016.SDR I5EA20180702Battery Pack · dischargedRT AND LT CABIN AFT OVERHEAD BIN EMERGENCY LIGHTS INOP FROM BS727 AFT. REMOVED AND REPLACED EMERGENCY BATTERY PACKS M1137 AT STA 975R, S/N 50962, AND M1197 AT STA 969L, S/N 41487. OPS CHECK GOOD IAW AMM 33-51-51.SDR I5EA2018071701Downlock Sensor · contaminatedUPON GEAR EXTENSION FOR LANDING, GOT GREEN LIGHTS FOR MAIN GEAR, GOT RED LIGHT FOR NOSE WITH NO GREEN LIGHT. FOLLOWED QRH WITH MANUAL EXTENSION, NO CHANGE. LANDED WITHOUT INCIDENT, STOPPED ON TAXIWAY, HAD ANOTHER SWIFT PILOT PIN NOSE GEAR. TROUBLE SHOT AND SDR EE4Y2018070906891Skin · crackedDURING THE CURRENT MAINTENANCE PROCESS IT WAS FOUND AT FWD ENTRY DOOR AREA, THE FUSELAGE SKIN WITH CRACK AT THE SILL LOWER AFT CORNER. DUE TO THIS SITUATION THE SKIN WAS REPAIRED AS PER SRM 53-10-01 REPAIR 12 FIGURE 201.SDR EE4Y2018070906892Attach Angle · crackedDURING THE CURRENT MAINTENANCE PROCESS IT WAS FOUND AT THE EMPENNAGE, VERTICAL STABILIZER TO FUSELAGE LEFT ATTACHMENT SUPPORT ANGLE CRACKED AT THE BS 1121 FIN WL 0.0. DUE TO THIS SITUATION THE AFFECTED SUPPORT ANGLE WAS REPAIRED AS PER SRM 53-80-71 REPAIR 1, FSDR EE4Y2018070906884Stringer · corrodedDURING THE CURRENT MAINTENANCE PROCESS IT WAS FOUND AT RT WING THE UPPER VENT STRINGERS S9U-S10U WITH CORROSION ON THE CHANNEL AREA INTERNAL SURFACE AT WS 557. THE CORROSION WAS COMPLETELY REMOVED AS PER SRM 51-10-02 PARAGRAPH 14A AND IT WAS FOUND OUT OF LIMITSDR FOTR20180324004Bear Strap · crackedFWD ENTRY DOOR LWR HINGE CUTOUT BS 303 STR 13L HAS CRACK INDICATION AT BEARSTRAP FASTENER HOLE.SDR FOTR20180324003Door Frame · corrodedCORROSION ON FWD FRAME AFT CARGO DOOR CUT OUT STR 27 26 25 24 RIGHT BS 787.SDR FOTR20180324001Skin · corrodedAD RELATED, INTERNAL FUSELAGE SKIN AROUND AFT DRAIN MAST HAS CORROSION BETWEEN STR 24L AND STR 25L AT APPROX FS990.SDR FOTR20180315001Frame · corrodedCORROSSION ON THE FRAME AT BS 847, RBL 16.SDR FOTR20171130177Frame · corrodedCORROSION ON FRAME BS 847, RBL 16.
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