Boeing 737-890
Service difficulty reports · 23,033
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 ASAA2025020856829Skin · corrodedCORROSION ON SKIN AT STA1088 TO STA1104 AND STR12R 2PLACES. SRXR430X. GROUNDED - YES. ACCOMPLISHED MINOR PERMANENT REPAIR TO RH BODY TO HORIZONTAL STAB. SLIDING SEAL FWD PANEL P/N 181A8011-12 BETWEEN STA 1104-1088 ABOVE STGR 12R IAW EA 800-53EA-28280 REV 00. ASDR ASAA2025020856678Skin · corrodedBELOW THE VERTICAL AT STR 4R AND BETWEEN STA 985.5 AND STA 947 CORROSION ON SKIN SEVERAL PLACES SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR ON FUSELAGE SKIN P/N 147A3110-20 AT STR 4R BETWEEEN STA 947 AND 1006 IAW EA#800-53EA-2883 REV 00 SRSDR ASAA2025020756443Rib · crackedREQ'S ACCESS @ STA 111.10 FOR 4(EA) CRACKS IN RIB, REPAIR 11 REQUIRED. GROUNDED - YES. REMOVED EXISTING REPAIR CUTOUT HORIZONTAL SKIN FOR ACCESS, ACCOMPLISHED HFEC OF CUTOUT, CLEANED EXISTING REPAIR HOLES, ACCOMPLISHED OPEN HOLE HFEC, FABRICATED AND INSTALLED SDR ASAA2025020656091Rib · crackedRIGHT HAND HORIZONTAL STAB HAS A CRACKED RIB AT STA 129.50. GROUNDED - YES. CUT OUT DAMAGE AND REPAIRED RIB IAW B737-800 SRM 55-10-09-2R-5.SDR ASAA2025020655775Skin · corrodedPOSSIBLE CORROSION ON FUSELAGE SKIN BELOW R2 DOOR STATIC PORT FWD OF STA 986 SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY B MINOR REPAIR ON FUSELAGE SKIN BELOW R2 DOOR STATIC POR STA 967-986 STGR 20R-21R IAW EA# 800-53EA-28220 REV 00 SRXR430X.SDR ASAA2025020655769Skin · corrodedPOSSIBLE CORROSION AT FUSELAGE SKIN LOCATION STA 927 STGR 4L SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON FUSELAGE SKIN P/N 147A3110-1 STA 907-927 STGR 4L IAW EA 800-53EA-28239 REV 00 SRXR430X.SDR ASAA2025020655757Skin · corrodedPOSSIBLE CORROSION AT FUSELAGE SKIN AFT DRAIN MAST AFT OF STA 986 SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON FUSELAGE SKIN P/N 147A3400-4 AT AFT DRAIN MAST BETWEEN STA 986.5 AND STA 1016 STGR 24L -25L IAW EA# 800-53EA-28213 REV 00 SRXR43SDR ASAA2025020655756Skin · corrodedPOSSIBLE CORROSION STA 1088 BETWEEN STGR 15R-17R SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR TO FUSELAGE SKIN 148A3321-13 AT STA 1088 STGR 16R TO STGR 18R IAW EA# 800-53EA-28233 REV 00.SDR ASAA2025020556003Transition Panel · corrodedFWD PIT R/H TRANSITION IS PUNCTURED AND HAS SPOTS OF CORROSION STA 500A TO 500D. GROUNDED - YES. FOUND TO BE 100% MAT LOSS. REMOVED AND REPLACED DAMAGED SECTION OF TRANSITIONSTA 500A TO 500D IAW B737-800 SRM 51-40-02-0G-0 AND 53-00-53-2R-6W= 2 O= .040 R= 0 L= SDR ASAA2025020456545Floor Panel · damagedFLOOR PANEL PN 146A5810-466 REQUIRES 2 INSERTS,. GROUNDED - YES. REPAIRED FLOOR PANEL 146A5810-466 OF 2 INSERTS IAW B737-800 SRM 53-00-50-2R-0.SDR ASAA2025020456235Angle · corrodedFWD CARGO PIT, R/H FROM STA 500C TO 500I, TRANSITION ANGLE HAS CORROSION ON TOP SURFACE. GROUNDED - YES. EVALUATED & REMOVED DAMAGE ON FWD CARGO PIT R/H TRANSITION @ STA 500C -500I, ORIGINAL: .040 , REMOVED: .040, REMAINING: .000 AND FOUND TO BE OUT OF LIMITS SDR ASAA2025020456160Channel · corrodedFWD CARGO PIT, L/H AT STA 500C TO 500I, TRANSITION ANGLE HAS CORROSION ON TOP SURFACE AT FASTENER HOLES, MARKED. GROUNDED - YES. REMOVED CORROSION ORIGINAL THICKNESS .040, REMOVED .040, REMAINING .000. FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2. SDR ASAA2025020456159Angle · corrodedFWD CARGO PIT, STA 500I AT AFT BULKHEAD TO FLOOR PANEL ANGLE HAS CORROSION AT FASTENER HOLES FOR PANEL. GROUNDED - YES. EVALUATED ORIGINAL MATERIAL THICKNESS .071, REMOVED .071, REMAINING .000 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-30SDR ASAA2025020456154Door Sill · corrodedFWD CARGO PIT, CARGO DOOR SILL STRUCTURE ON TOP HAS CORROSION MARKED. GROUNDED - YES. EVALUATED AREA AND REMOVED DAMAGE, ORIGINAL: .045, REMOVED: .012, REMAINING: .033 & IS FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 51-60-15-1A-1. REMOVED DAMAGED THRESHOLD WEBSDR ASAA2025020456149Angle · corrodedFWD CARGO PIT, R/H AT STA 500A TO 500C, TRANSITION ANGLE HAS CORROSION AT FASTENER HOLES, MARKED. GROUNDED - YES. EVALUATED AND REMOVED DAMAGE ON FWD CARGO PIT R/H TRANSITION @ STA 500A-500C , ORIGINAL : .040 , REMOVED : .040, REMAINING: .000 AND FOUND TO BE OSDR ASAA2025020455755Skin · corrodedPOSSIBLE CORROSION ON FUSELAGE SKIN AT AFT JACK POINT STA 1088 STGR 24R- 25R SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON AFT FUSELAGE SKIN AT AFT JACK POINT P/N 148A3321 AT STA 1088 STGR 24R-25R IAW EA#800-53EA-28214 REV 01 SRXR430X.SDR ASAA2025020455728Skin · corrodedPOSSIBLE CORROSION APPROXIMATE LOCATION STA 360 STGR 24L SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON FUSELAGE SKIN P/N 143A3212-20/143A3232-28 AT LAP SEAM STGR 24L BETWEEN STA 360 -380 IAW EA 800-53EA-28215 REV 00 SRXR430X.SDR ASAA2025020356155Housing · gougedR2 DOOR, EXTERIOR HANDLE PAN INSIDE DIAMETER IS GOUGED AND CORRODED. GROUNDED - YES. REMOVED GOUGED SEAL PLATE IAW B737-800 SRM 51-40-02 AND INSTALLED NEW SEAL PLATE P/N: 149A6121-1; P.O. 1113263.1 IAW B737-800 SRM 51-40-02; AND REMOVED CORROSION AND FOUND WITSDR ASAA2025020256157Shield · corrodedAFT CARGO PIT FWD SHIELD HAS CORROSION. GROUNDED - YES. EVALUATED, REMOVED CORROSION, ORIGINAL MATERIAL THICKNESS .050, REMOVED .021 REMAINING .029, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-60-15-1A-1. REMOVED DAMAGED SHIELD, INSTALLED NEW AFT PIT FWD SHISDR ASAA2025020256156Web · corrodedAFT CARGO PIT THRESHOLD WEB HAS CORROSION. GROUNDED - YES. REMOVED CORROSION ON AFT CARGO THRESHOLD WEB, ORIGINAL MATERIAL THICKNESS .050, REMOVED .020, REMAINING .030, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-60-15-1A-1. REMOVED DAMAGED WEB, LOCATED AND SDR ASAA2025020255873Support · corrodedAFT CARGO PIT L/H TRANSITION HAS MULTIPLE SPOTS OF CORROSION FROM STATION 727-727D+15. GROUNDED - YES. REMOVED CORROSION ORIGINAL MATERIAL THICKNESS .040, REMOVED .040, REMAINING .000 FOUND TO BE OUT OF LIMITS DUE TO 100% MATERIAL LOSS IAW B737-800 SRM 53-00-5SDR ASAA2025020156158Floorbeam · corrodedFLOOR BEAM STA 344 HAS CORROSION @ LBL 11.10. GROUNDED - YES. DAMAGE REMOVED AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-10-51-0I-2 & SRM 53-10-51-1A-1 REF BAC 1518-1218 REV:-.ORIG:175". REMOVED 047", REMAINING .128". BLO STA344-360, LBL 11.10 STA 344-36SDR ASAA2025020156006Web · corrodedAFT PIT DOOR CUTOUT LOWER SILL WEB HAS SPOTS OF CORROSION. GROUNDED - YES. REMOVED CORROSION LOWER SILL WEB, FOUND OUT LIMITS IAW B737-800 SRM 53-60-15-1A-1. REMOVED AND RELACED IAW B737-800 SRM 51-40-02-0G-0W= 2" O-= 0.050" R= 0.044" L= 1.2" D= 0.006".SDR ASAA2025020156005Web · corrodedFWD PIT DOOR CUTOUT LOWER SILL WEB HAS SPOTS OF CORROSION. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-30-15-1A-1. REMOVED AND REPLACED SILL WEB IAW B737-800 SRM 51-40-02-0G-0W= 2.3" O= 0.045" R= 0.037" L= 3" D= 0.008".SDR ASAA2025020156004Transition Panel · corrodedFWD PIT R/H TRANSITION HAS SPOTS OF CORROSION STA 500H TO 500I. GROUNDED - YES. REPAIRED TRANSITION PANEL SUPPOR ON RH FWD CARGO COMPT. STA 500H TO 500I IAW B737-800 SRM 53-00-53-2R-5W= 1.5 O= 0.045" R= 0.037" L= 2" D= 0.008".SDR ASAA2025020155874Channel · corrodedAFT CARGO PIT R/H TRANSITION HAS MULTIPLE SPOTS OF CORROSION FROM 727 - 767. GROUNDED - YES. REMOVED CORROSION ORIGINAL THICKNESS .040, REMOVED .040 , REMAINING .000. FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-55-1A-2. REMOVED DAMAGED TRANSITION PANEL. FSDR ASAA2025013056109Floor Panel · delaminatedFLOOR PANEL PN 147A5810-23, HAS A DELAMINATION. GROUNDED - YES. PERFORMED PERMANENT REPAIRS ON FLOOR PANEL PN: 147A5810-23 IAW ASA B737-800 SRM 53-00-50-2R-0, ASA B737-800 SRM 53-00-50-2R-1, ASA B737-800 SRM 53-00-50-2R-7 & ASA B737-800 SRM 53-00-50-1A-1. NO FSDR ASAA2025013056069Web · corrodedAFT PIT LOWER DOOR SILL WEB HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED AND REPLACED AFT PIT LOWER DOOR SILL WEB IAW B737-800 SRM 51-40-02-05-0W= 1" O= .050" R= .041 L= 9" D=.009".SDR ASAA2025012956306Rib · crackedR/H HORIZONTAL STABILIZER INTERNAL, RIB AT SS 111.10 CRACKED 4 PLACES AT VERTICAL STIFFENERS GROUNDED - YES. REMOVED DAMAGE @ STA 92.70 RIB AT 4EA LOCATION. ACCOMPLISHED HFEC OF 4EA CUTOUTS, HEAT TREATED, FABRICATED, AND INSTALLED REPAIR PARTS PN: BAC1490-279SDR ASAA2025012855622Battery Pack · inoperativeREF T/C 78233008, EMERGENCY EXIT LIGHTS ON LOWER OVERHEAD STOW BINS FWD OF EMERGENCY EXIT DOOR R/H SIDE ARE INOP. GROUNDED - YES. REMOVED AND INSTALLED A NEW BATTERY PACK AT SEAT 8F BEHIND AIR RETURN GRILL REF AMM 33-51-06, OPS CK GOOD.SDR ASAA2025012756002Skin · corrodedEXTERIOR SKIN BS.887 TO BS.1016 STR.23L UPPER LAP SHOWS SIGNS OF CORROSION 17 AREA. (MARKED IN RED). GROUNDED - YES. REMOVED CORROSION 17(EA) ON ZONE B. DAMAGE AREAS FROM STA 887-STA 1016 STR 23L UPPER LAP ORG MAT THICK 0.063, REMOVED 0.004 REMAINING 0.059 FOUSDR ASAA2025012655932Skin · crackedDURING FUEL LEAK CHECKS FOUND RIGHT WING CRACKED AT WS578 LOWER SURFACE JUST FORWARD OF TANK ACCESS PANEL. GROUNDED - YES. REPAIRED CRACK IAW ASA EA # 800-57EA-28207. THIS IS A CATEGORY B REPAIR WITH STAGE 1 APPROVAL FOR STATIC STRENGTH ONLY. A NEW FAA FORM 81SDR ASAA2025012555569Power Supply · inoperativeFOUND SEVERAL MAIN CABIN EMER LIGHTS OUT. GROUNDED - YES. REMOVED, REPLACED AND OP TEST IS GOOD OF MAIN CABIN EMER LIGHTS, POWER SUPPLY AND POWER SULLY BATTERY PACK IAW B737-800 AMMS 33-51-06-960-805 33-51-06-960-806 AND 33-51-00-720-801.SDR ASAA2025012455527Housing · detachedEXIT SIGN BETWEEN AFT JUMPSEAT CAME OFF ON TAKEOFF, REPLACED SIGN, IT DOES NOT LOOK SECURE. GROUNDED - YES. R&R EXIT SIGN LIGHT ASSY IAW AMM 33-51-01-960-802. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.SDR ASAA2025012355528Lens · missingSEAT 17A LOWER EXIT SIGNAGE MISSING ACCORDING TO F/A. GROUNDED - YES. REPLACED COVER ON SEAT 17A LOWER EXIT SIGN, OPS CHECK GOOD.SDR ASAA2025012256514Skin · corrodedEXTERIOR SKIN UPPER LAPSEAM BS.727E+13 TO BS.887 STR.23L HAS 9 AREAS THAT SHOW SIGNS OF CORROSION. (MARKED IN RED). GROUNDED - YES. ACCOMPLISHED ASA EA 800-53EA-28299 REV:00 REV. DATE 3/10/2025. TITLE SECTION 46 LH FUSELAGE SKIN, BETWEEN STA 727E+13 AND STA.88SDR ASAA2025012155907Intercostal · corroded(LATE FIND) AFT PIT BILGE INTERCOSTAL AT STA 867 TO 887 LBL 10 IS CORRODED. GROUNDED - YES. UPON FURTHER EVALUATION THE AFT PIT INTERCOSTAL AT STA 867-887, LBL 10 IS FOUND TO HAVE 100% MAT LOSS NO ALLOWABLE DAMAGE LIMITS ARE GIVEN IN B737-800 SRM. REMOVED DAMASDR ASAA2025012155495Power Supply · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M1676 ARE INOP. GROUNDED - YES. REMOVED AND REPLACED POWER SUPPLY M1676 S/N 130677 IAW B737-NG AMM 33-51-960-806. OPS CHECK GOOD.SDR ASAA2025012155494Power Supply · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY M1670 ARE INOP. GROUNDED - YES. REMOVED AND REPLACED POWER SUPPLY M1670 S/N 33222 IAW B737-NG AMM 33-51-06-960-806. OPS CHECK GOOD.SDR ASAA2025012056708Skin · corrodedCORROSION ON SKIN AT STR 4L AND STA727C SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY B MAJOR REPAIR TO FUSELAGE SKIN PANELS 146A3131-9 AND BETEEEN STA 727C STRG 4L IAW EA 800-53EA-28407 REV00 (SUBMITTED EAR UNDER MIG-5 N/R SA042461) SRXR430X.SDR ASAA2025012055566Rib · crackedL/H STAB RIB STA. 144 CRACKED (MARKED). GROUNDED - YES. REPAIRED L/H STAB RIB STA. 144 IAW B737-800 SRM 55-10-09-2R-5.SDR ASAA2025012055393Receiver · damagedR1 DOOR DIFFICULT TO CLOSE/WON'T CLOSE FROM INSIDE. UPPER AND LOWER AFT ROLLER GUIDES HAVE GALLING AND METAL SHAVINGS. UPPER AND LOWER AFT ROLLERS ALSO HAVE METAL SHAVINGS. UPPER IS MORE DAMAGED. DOOR CLOSES WITH NO ISSUE FROM OUTSIDE. GROUNDED - YES. REMOVESDR ASAA2025011955356Skin · corrodedLH FUSELAGE SEC 44 BUTT JOINT STA 727 FROM STGR 1L TO STGR 4L HAS SIGNS OF CORROSION SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY B MINOR REPAIR TO FUSELAGE SKIN PANEL 144A3111-18 AT STA 727 BUTT JOINT BETWEEN STGR 1L-4L IAW EA 800-53EA-28139 REV 00 SRXR430SDR ASAA2025011955354Skin · corrodedRH FUSELAGE SKIN SEC 44 BUTT JOINT AT STA 727 STGR 2R HAS SIGNS OF CORROSION SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY B MINOR REPAIR TO FUSELAGE SKIN PANEL 144A3111-18 AT STA 727 BETWEEN STGR 2R-3R IAW EA 800-53EA-28131 REV 00 SRXR430X.SDR ASAA2025011955351Skin · corrodedL/H SEC 43 LAP SEAM STA 500D STR 14L HAS SIGNS OF CORROSION SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A REPAIR ON FUSELAGE SKIN P/N 143A3212-20 AT STGR 14L LAP JOINT BTW STA 500D AND STA 500E IAW EA#800-53EA-28115 REV 00 SRXR430X.SDR ASAA2025011955349Skin · corrodedR/H SEC 46 LAP JOINT STA 727 STR 10R HAS SIGNS OF CORROSION SRXR430X. GROUNDED - YES. CATEGORY A MINOR REPAIR ACCOMPLISHED ON SKIN PANELS 146A 3131-10 AND 146A 3151-94 STA 727 STGR-10R ON MIG-5 NR 042319 IAW EA 800-53EA-28141 REV00 SRXR430X.SDR ASAA2025011955344Skin · corrodedRH FUSELAGE SKIN SEC 44 LAP SEAM STA 706 TO STA 727 STGR 10R HAS SIGNS OF CORROSION SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON FUSELAGE SKIN PANEL P/N 144A3321-4 AT STA 706-727 STGR 10R LAP JOINT IAW EA 800-53EA-28146 REV 00 SRXR430X.SDR ASAA2025011955343Skin · corrodedRH FUSELAGE SKIN SEC 46 LAP JOINT BETWEEN STA 822-857 STGR 10R HAS SIGNS OF CORROSION SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON FUSELAGE SKIN PANELS P/N 146A3131-10 AND 146A3151-94 AT STA 822-857 STGR 10R IAW EA 800-53EA-28140 REV 00 SRSDR ASAA2025011955342Skin · corrodedLH FUSELAGE SEC 48 BUTT JOINT STA 1088 STGR 9L HAS SIGNS OF CORROSION SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON FUSELAGE SKIN PANEL P/N 148A3311-1 AT STA 1064-1088 STGR 9L IAW EA 800-53EA-28134 REV 00 SRXR430X.SDR ASAA2025011955341Skin · corrodedRH FUSELAGE SKIN SEC 46 LAP JOINT STA 727B STGR 10R HAS SIGNS OF CORROSION SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON FUSELAGE SKIN PANELS P/N 146A3131-10 AND 146A3151-94 AT STA 727-727G STGR 10R LAP IAW EA 800-53EA-28141 REV 00 SRXR430X
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