Boeing 737-890
Service difficulty reports · 23,038
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 = '737890' 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 = '737890' 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 ASAA2024042849802Transition Panel · corrodedAFT CARGO PIT LH TRANSITION CORRODED FROM STA 727 TO STA 787 IN MULTIPLE AREAS. GROUNDED - YES. REMOVED DAMAGE FOUND OUT LIMITS, REPLACED TRANSITION IAW B737-800 SRM 53-00-53-2R-5.W= 1.2 O= .040 R= 0 L= 8 D= .040.SDR ASAA2024042849328Battery Pack · dischargedL/H FWD EMERGENCY LIGHT INOP. GROUNDED - YES. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK REF BOEING AMM TASK 33-51-06-960-805. ASSY M1675 AND M1694. OP TEST GOOD. NO FURTHER DEFECTS.SDR ASAA2024042749288Lamp · inoperativeRH AFT EMERGENCY EXIT DOOR EMERGENCY ILLUMINATION LIGHT (IN UNIT AFT) INOP. GROUNDED - YES. RELAMPED AS REQUIRED. OPS TEST GOOD.SDR ASAA2024042449242Light · looseGALLEY 4 (AIRCRAFT LEFT) EXIT SIGN IS LOOSE. GROUNDED - YES. REMOVED & REPLACED EXIT LIGHT ASSY REF AMM 33-51-01 OPS NORMAL.SDR ASAA2024042349843Attach Angle · corrodedUPON REMOVAL OF AFT PIT DOOR SURROUND FWD SHIELD, FOUND ATTACHING ANGLE UNDERNEATH TO HAVE MULTIPLE AREAS OF CORROSION. GROUNDED - YES. REMOVED CORR. FROM AFT PIT DOOR SURROUND FWD SHIELD ATTATCHED ANGLE ORIG THICKNESS .050. I.A.W. B737-800 SRM 53-60-15 MAT. LSDR ASAA2024042349216Cover · detachedF/A REPORTS: CEILING EXIT SIGN AT ROW 16 IS DAMAGED. GROUNDED - YES. FWD EMERGECNY LT ASSY COVER POPPED OFF ON CEILING LT ASSY AT ROW 16. RE-ATTACHED LT COVER. EMERGENCY LTS CHECK GOOD. NO OTHER DEFECTS NOTED.SDR ASAA2024042249819Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR PANEL 147A5810-30 HAS CORRODED INSERTS. GROUNDED - YES. EVALUATED AND REPAIRED IAW B737-800 SRM 53-00-50-2R-0, SRM 53-00-50-2R-1.SDR ASAA2024042249818Floor Panel · corrodedMAIN CABIN WET AREA FLOOR PANEL 147A5810-28 HAS CORRODED INSERTS. GROUNDED - YES. REMOVED AND REPLACED 62 EA INSERTS, REPAIRED PANEL 147A5810-28 WITH FIBERGLASS DOUBLERS IAW B737-800 SRM 53-70-50-2R-0, 53-00-50-2R-0 & 53-00-50-2R-1.SDR ASAA2024042249817Floor Panel · corrodedMAIN CABIN AFT WET AREA FLOOR PANEL 147A5810-27 HAS CORRODED INSERTS. GROUNDED - YES. REMOVED AND REPLACED 62 EA INSERTS, REPAIRED PANEL 147A5810-27 WITH FIBERGLASS DOUBLERS IAW B737-800 SRM 53-70-50-2R-0, 53-00-50-2R-0 & 53-00-50-2R-1.SDR ASAA2024042249816Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR PANEL 147A5810-137 HAS CORRODED INSERTS. GROUNDED - YES. REPAIRED FLOOR BOARD 147A5810-137 BY REPAIRING TOP SKIN AND REPLACING INSERTS IAW B737 SRM 53-00-50-2R-0; 53-00-50-2R-1.SDR ASAA2024042249815Floor Panel · delaminatedMAIN CABIN AFT WET AREA FLOOR PANEL 147A5810-123 HAS CORRODED INSERTS. GROUNDED - YES. REPLACED CORRODED INSERTS ON FLOOR PANEL 147A5810-123 IAW ASA B737-800 SRM 53-00-50-0I-1, SRM 53-00-50-1A-1, SRM 53-00-50-2R-0, SRM 53-00-50-2R-4, AIPC 53-21-51-56C.SDR ASAA2024042249814Floor Panel · delaminatedMAIN CABIN FWD WET FLOOR PANEL 141A5810-454 HAS CORRODED INSERTS. GROUNDED - YES. REPAIRED FLOOR PANEL 141A5810-454 BY REPAIRING TOP SKIN AND REPLACING INSERTS IAW B737 SRM 53-00-50-2R-0; 53-00-50-2R-1.SDR ASAA2024042249813Floor Panel · delaminatedMAIN CABIN FWD WET AREA FLOOR PANEL 141A5810-755 HAS DELAM & CORRODED INSERTS. GROUNDED - YES. REPAIRED IAW B737-800 SRM 53-00-50-2R-0, SRM 53-00-50-2R-1.SDR ASAA2024042249812Floor Panel · delaminatedMAIN CABIN FWD WET AREA FLOOR PANEL 141A5810-769 HAS PEELING FIBERS & CORRODED INSERTS. GROUNDED - YES. REPAIRED DAMAGED FIBERS AND REPLACED CORRODED INSERTS ON FLOOR PANEL 141A5810-769 IAW ASA B737-800 SRM 53-00-50-0I-1, SRM 53-00-50-1A-1, SRM 53-00-50-2R-0, SDR ASAA2024042249811Floorboard · delaminatedMAIN CABIN FWD WET AREA FLOOR PANEL 141A5810-763 HAS DELAM & CORRODED INSERTS. GROUNDED - YES. REPAIRED MAIN CABIN FWD WET AREA FLOOR PANEL 141A5810-763 HAS DELAM & CORRODED INSERTS IAW ASA B737-800 SRM 53-00-50.SDR ASAA2024042249193Lens · brokenF.A. REPORTS: L-1 FLOOR LEVEL EMERGENCY LIGHT COVER FELL OFF. GLASS BROKEN. GROUNDED - YES. REMOVED & REPLACED LOWER THRESHOLD LIGHT ASSEMBLY COVER IAW AMM 33-14-00.SDR ASAA2024042049134Lens · detachedFA REPORTS L2 EXIT IND ASSY COVER FALLEN OFF. GROUNDED - YES. REPLACED L2 DOOR EXIT IND ASSY OPS CHECKS GOOD.SDR ASAA2024041949891Skin · crackedRIGHT HORIZONTAL STABILIZER LOWER SKIN IS CRACKED AT STAB. STA. 101.90 RIB LOCATED 9" FROM THE REAR SPAR. APPROX. 1.250" IN LENGTH. (MARKED AND IDENTIFIED END OF CRACK). GROUNDED - YES. REPAIRED RIGHT HORIZONTAL STAB LOWER SKIN CRACKS 2EA. IAW B737-800 SRM 55-SDR ASAA2024041949163Lens · crackedFA REPORTS KNEE HIGH EXIT SIGN TO THE RIGHT SIDE OF R2 DOOR CRACKED. GROUNDED - YES. REMOVED &REPLACED R/H AFT EXIT SIGN R2 DOOR FLOOR LIGHT LENS REF AMM 33-51-01. NO FURTHER DEFECTS NOTED.SDR ASAA2024041849918Web · corrodedAFT PIT WEB HAS CORROSION. GROUNDED - YES. REMOVED CORR.FROM AFT PIT WEB ORIG. THICKNESS .045 I.A.W B737-800 SRM53-60-15. MAT LOSSED .040 REMAINING THICKNESS .005 FOUND TO BE OUT OFLIMITS I.A.W B737-800 SRM 53-60-15.TOOL#T8224K DUE 25/OCT/24.REMOVED AND REPLASDR ASAA2024041849917Transition Panel · corrodedAFT PIT TRANSITION PANEL @ STA727E+16 TO STA767 IS CORRODED. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT R/H TRANSITION PNL AT STA727E+16 TO ST767 ORIG THICK .040 I.A.W B737-800 SRM 53-60-53. AREA FOUND TO BE OUT OF LIMITS AND PUNCTURED I.A.W B737-800 SRM 53-0SDR ASAA2024041849842Shield · corrodedAFT PIT DOOR SURROUND FWD SHIELD HAS CORROSION. GROUNDED - YES. EVALUATED AFT PIT FWD SHIELD ORIG THICKNESS IS .050" IAW B737-800 SRM 53-60-15-0I-1 REMOVED .007" REMAINING .043" AND IS FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-60-15-1A-1 4.G.2 TOOL# T8224KSDR ASAA2024041849841Transition Panel · corrodedAFT PIT RH TRANSITION PANEL @ STA727 TO STA727E+15 IS CORRODED. GROUNDED - YES. REMOVED CORR. FROM AFT PIT R/H TRANSITON PNL AT STA.727 TO STA.727E+15 ORIG. THICKNESS .040 I.A.W B737-800 SRM 53-60-53 MAT. LOSSED .010 REMAIING THICKNESS .030 FOUND TO BE OUT OFSDR ASAA2024041849840Transition Panel · corrodedAFT PIT LH TRANSITION PANEL IS CORRODED @ STA727I+14 TO STA827. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT L/H TRANSITION PANEL @ STA 727I +14 TO STA 827 IAW B737-800 SRM 53-00-53-1A-2.2.D. ORIG. THICKNESS: .040 IAW B737-800 SRM 53-60-53-IO-2. 100% MAT LOSS ASDR ASAA2024041849839Transition Panel · corrodedAFT PIT LH TRANSITION PANEL IS CORRODED @ STA727C+7 TO STA727I+13. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT L/H TRANSITION @ STA727C+7 TO 727I+13 IAW B737-800 SRM 53-00-53-1A-2.R.D. ORIG. THICKNESS: .040 IAW B737-800 SRM 53-60-53-OI-1 REMOVED: .007, REMAINISDR ASAA2024041849838Transition Panel · corrodedAFT PIT LH TRANSITION PANEL IS CORRODED @ STA727 TO STA727C+6. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT L/H TRANSITION PANEL @ STA727 TO STA727C+6 IAW B737-800 SRM 53-00-55-1A-2. ORIG THICKNESS: .040 IAW B737-800 SRM 53-60-53-IO-2. 100% MAT LOSS AND IS FOUNSDR ASAA2024041849836Floorbeam · corrodedMAIN CABIN AFT WET AREA, FLOOR BEAM CORRODED ON UPPER SURFACE AT BS 947.5 BETWEEN LBL-30 AMD RBL-10. MARKED. GROUNDED - YES. CORROSION IS LOCATED ON A PREVIOUS T-CAP REPAIR. CORROSION FOUND TO BE OUT OF LIMITS DUE TO BEING LOCATED AT A HARD MOUNT ATTACHMENT LOSDR ASAA2024041549446Floor Support · corrodedMAIN CABIN FLOOR SUPPORT INTERCOSTAL STA 967 - STA 986 RBL 16 CORRODED. GROUNDED - YES. CORROSION IS AROUND NUTPLATE HOLE. OUT OF ALLOWABLE LIMITS IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW INTERCOSTAL IAW B737-800 SRM 51-40-05 AND BAC DWG 140A9870 REVSDR ASAA2024041549442Floorbeam · corrodedMAIN CABIN FLOOR SUPPORT STA 994 RBL 32 - RBL 44 CORRODED. GROUNDED - YES. CORROSION IS IN AND AROUND HOLE. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1 DRILLED TO FIT NEW FLOOR SUPPORT IAW B737-800 SRM 51-40-05 AND BAC DWG 147A5700 REV A. FLOOR SUPPORT INSTALSDR ASAA2024041549441Floor Support · corrodedMAIN CABIN FLOOR SUPPORT STA 992 - STA 1016 LBL 32 CORRODED. GROUNDED - YES. FLOOR SUPPORT HAS 100% MATERIAL LOSS AT CORRODED AREA. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW FLOOR SUPPORT IAW B737-800 SRM 51-40-05 AND BAC DWG 147A5700 RESDR ASAA2024041549440Floor Support · corrodedMAIN CABIN FLOOR SUPPORT STA 992 - STA 1016 RBL 32 CORRODED. GROUNDED - YES. FLOOR SUPPORT HAS 100% MATERIAL LOSS AT CORRODED AREA. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW FLOOR SUPPORT IAW B737-800 SRM 51-40-05 AND BAC DWG 147A5700 RESDR ASAA2024041549439Floor Support · corrodedMAIN CABIN FLOOR STRUCTURE MACHINED INTERCOSTAL STA 986-STA 1006 RBL32 CORRODED. GROUNDED - YES. REMOVED CORROSION. ORIGINAL THICKNESS 0.080. REMAINING THICKNESS 0.050, REMOVED 0.030 OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1 PARA 4A. DRILLED TO FIT NEW INTESDR ASAA2024041549080Lamp · inoperativeROW 17 EXIT LIGHTING DIM. GROUNDED - YES. RE-LAMPED ROW 17 EXIT LIGHT, OPS GOOD.SDR ASAA2024041449835Stop Fitting · gougedMAIN CABIN, L/H AFT ENTRY DOOR I/B TOP 'DOOR STOP FITTING' HAS BARE (METAL.GOUGE). DOT#Z211 STREAMER IIS ATTACHED. GROUNDED - YES. EVALUATED STOP FITTING AND FOUND DAMAGE TO THE BUSHING, DAMAGE TO BUSHING IS NOT PERMITTED AND FOUND TO BE OUT OF LIMITS IAW B737SDR ASAA2024041349372Web · corrodedFWD CARGO DOOR CUTOUT LWR CLOSE OUT WEB CORRODED. GROUNDED - YES. BLENDED CORR FOUND TO BE OUT OF LIMITS REMOVED & REPLACED LWR CLOSE OUT WEB IAW B737-800 SRM 51-40-02-0G-0 W 1, O ..045, R .038, L 2, D .007.SDR ASAA2024041349019Roller · stuckR2 AFT SERVICE DOOR FOUND OPEN WITH THE HANDLE IN THE FULL CLOSED POSITION. FA'S WERE UNABLE TO MOVE THE HANDLE. GROUNDED - YES. PRIOR TO GETTING R2 DOOR OPEN SAW BOTH DOOR UPPER ROLLERS WERE JAMMED UNDER THE GUIDE TRACK, FWD UPPER ROLLER GUIDE APPEARS TO BE GSDR ASAA2024041249041Battery Pack · no testWHILE PERFORMING T/C 78233001 FOUND EMERGENCY BATTERY PACK M1670, M1671,M1673,M1695 AND M1694 TO HAVE FAILED CAPACITY CHECK. GROUNDED - YES. REPLACED EMERGENCY BATTERY PACKS M1670, M1671, M1695 & M1694. BATTERY PACK CAPACITY CHECKED & ALL PACKS PASSED REF AMM SDR ASAA2024041149203Transition Panel · crackedDURING INSTALL OF R/H TRANSITION FOUND LOWER FRAME HOLE AT STA 500D TO BE CRACKED. GROUNDED - YES. REPAIRED LOWER FRAME HOLE AT STA 500D IAW EA 800-53EA-26889.SDR ASAA2024041148992Battery Pack · no testREF T/C 78233001, EMERG LIGHT CAP TEST M1671, M1672, M1673 & M1675 FAILED TEST. GROUNDED - YES. REMOVED & REPLACED EMERG LIGHT BATT PACKS M1671, M1672, M1673 & M1675 REF AMM 33-51-06, OPS CHECK GOOD.SDR ASAA2024040949000Web · gougedFOUND INTERCOSTAL WEB DAMAGED E&E BAY CUT OUT RBL 15.47, BS 338 & WL 152. GROUNDED - YES. DAMAGE LOCATED ON R/H INTERCOSTAL WEB UPPER EDGE IN E&E BAY DOOR SURROUND STRUCTURE. DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS REF SRM 53-10-15-1A-3. REPLACED WEB SECTION.SDR ASAA2024040849533Floor Support · corrodedL/H HORIZONTAL AFT SUPPORT STRUCTURE FOR PANEL 333CB HAS CORRODED DOUBLE DRILLED HOLE. GROUNDED - YES. REPAIRED L/H HORIZONTAL LOWER BEAM IAW EA# 800-55EA-26983 REV: 00.SDR ASAA2024040548985Skin · dentedFOUND DENT ON R/H SIDE OF FUS. AT STA 905 +9" 3" BELOW STR 17R GOUGE IN CENTER OF DENT. GROUNDED - YES. (RESOLVED ON W/O: 1996489 TASKCARD: N/R-00001 ) DENT ON R/H SIDE OF FUSELAGE AT STA 905+9" 3" BELOW STR 17R REPAIRED IAW EA 800-53EA-26862. THIS IS A CATEGOSDR ASAA2024040449507Transition Panel · corrodedAFT CARGO, R/H TRANSITION PANEL HAS AREAS OF CORROSION FROM STA 727F - 767. GROUNDED - YES. REMOVED CORROSION FROM THE AFT PIT R/H TRANSITION PANEL AT STA 727F TO 767 IAW B737-800 SRM 53-00-53-1A-2.2D ORIG THICKNESS IS .040" IAW B737 -800 SRM 53-60-53-01-2 TABSDR ASAA2024040449506Door Sill · corrodedMAIN CABIN AFT GALLEY SERVICE DOOR CUTOUT, LOWER SILL AREA AT FASTENER HOLES HAS CORROSION (MARKED). GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN AFT GALLEY SERVICE DOOR CUTOUT LOWER SILL IAW B737-800 SRM 51-40-02 AND IAW BAC DWG 147A8501 REV:-.SDR ASAA2024040449504Transition Panel · corrodedAFT CARGO, L/H TRANSITION PANEL HAS AREAS OF CORROSION FROM STA 777-847 GROUNDED - YES. REMOVED CORROSION FROM AFT PIT L/H TRANSITION PANEL AT STA 777-847 IAW B737-800 SRM 53-00-53-1A-2-2.D 100% MATERIAL LOSS AND IS FOUND TO BE OUT OF LIMITS PER B737-800 SRMSDR ASAA2024040449502Door Sill · corrodedMAIN CABIN AFT PASSENGER ENTRY DOOR CUTOUT, LOWER SILL AREA AT FWD CORNER HAS CORROSION. GROUNDED - YES. REMOVED CORROSION IAW B737-800 SRM 51-10-02. LOWER SEAL AREA ORIG THICK 0.080 REMOVED 0.002 REMAINING THICK 0.078 IN LIMITS IAW B737-800 SRM 53-70-15-1A-SDR ASAA2024040449501Door Sill · corrodedMAIN CABIN FORWARD PASSENGER ENTRY DOOR CUTOUT, LOWER SILL AREA AT FASTENER HOLES HAS CORROSION. GROUNDED - YES. REMOVED CORROSION AT MAIN CABIN FWD PASSENGER ENTRY DOOR CUTOUT, LWR SILL AREA AT FASTENER HOLES AS MARKED IAW B737-800 SRM 53-10-15-1A-1, FIG.108SDR ASAA2024040449500Web · corrodedR/H A/C PACK INLET DUCT FWD LOWER 4EA MOUNTING BOLT HOLES HAVE CORROSION. GROUNDED - YES. REMOVED CORROSION ON R/H A/C PACK INLET DUCT IAW B737-800 SRM 51-10-02 ORIG THICKNESS .100 IAW BAC DWG 111A7101 REV: B, REMOVED .008, REMAINING .092". FOUND TO BE INSDR ASAA2024040449497Door Sill · corrodedMAIN CABIN FORWARD GALLEY SERVICE DOOR CUTOUT, LOWER SILL AREA AT FASTENER HOLES HAS CORROSION (MARKED). GROUNDED - YES. REMOVED AND REPLACED R1 DOOR INNER CHORD IAW B737-800 SRM 51-40-02 AND BOEING DWG# 141A8310 REV B, 141A0631 REV B, 141A8310 REV-.SDR ASAA2024040349444Floorbeam · corrodedMAIN CABIN FLOOR BEAM STA 986 HAS MULTIPLE AREAS OF CORROSION. GROUNDED - YES. BLENDED CORROSION, ORIGINAL THICK 0.150 IAW B737-800 SRM 53-70-51-0I-1. REMAINING THICK AT RBL47 0.105, REMOVED 0.045. DOUBLE DRILLED HOLE AT LBL-38. OUT OF LIMITS IAW B737-800 SRM
Back to Boeing 737-890