JASC 3432
Service difficulty reports · 66
Reports filed under 3432 · Glide Slope System, newest first.
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 jasc_code = '3432' 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 jasc_code = '3432' 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 FDEA202607100898Glide Slope · malfunctionedON RNAV APPROACH RW 21, ON GLIDEPATH AND CONFIGURED FOR LANDING GOT GLIDESLOPE GLIDESLOPE REPEATEDLY STARTING AT 100 FEET UNTIL TOUCHDOWN.SDR DALA2026052603148Glide Slope · faultedDIV - TO SAV DUE TO GLIDE SLOPE NOT CAPTURING DURING THE APPROACH TO ATL IN IFR CONDITIONS. COULD NOT DUPLICATE. SWAPPED MMR NR 1 AND NR 2. AIRCRAFT RETURNED TO SERVICE. (LP: 8881250) AIRCRAFT WAS GROUNDED.SDR DALA2026030301468Glide Slope · failedSHIP 3044 - DIV - TO BHM DUE TO CAPTAINS GLIDE SLOPE FAILURE DURING THE APPROACH TO ATL. CORRECTIVE ACTION: REPLACED MMR #1. (LP 1472944, 1472661)SDR HNAA2025103100730Glide Slope · unknownRECIEVED FULL DEFLECTION OF 1.5 ON BOTH SIDE OF GLIDESLOPE IN EWN, DIVERTED TO ILM DEFLECTION HAPPENED 700 FT, AND RA WAS INTERMITTANT GOING INTO EWN. CAPTAIN DIVERTED TO ILM. PERFORMED OPS CHECK OF VOR & ILS SYSTEM IAW AMM 34-32-00-700-801-A. REF T30D TEST PSDR YENA2024101801379Glide Slope · faultedFLT#287, BOS-LAX. 'GS FAILED TO CAPTURE ON ILS APPROACH; PERFORMED BITE TEST OF MMR 1 AND 2 PER AMM 34-36-00-740-007-A. ILS AND GS PASSED, TEST OK,NO FAULTS NOTED.'SDR HNAA2020122100376Control Unit · malfunctionedGLIDESLOPE LEFT AND RIGHT SIDE DID NOT MATCH ON ILS APPROACH. FOR THE ENTIRE APPROACH. R & R RT NAV UNIT, IAW EMB AMM 34-32-01. OPERATIONS CHECK GOOD OK FOR SERVICE. PERFORMED ILS CHECK, IAW TIC BOX, NAV SENSITIVITY CHECK GOOD. CLEAR MEL 34-10 AND SIL 34-5SDR YBBA20181203001Glide Slope · false indicationPIC REPORTED #1 GLIDE SCOPE INTERMITTENT DURING DESCENT TO KAPA, DOM NOTIFIED. MX CALLED OUT TO LOCATION. UNIT MEL CAT "C" IAW FACILITY APPROVED MEL DATED 01/15/2018.SDR CA191205007Adapter · failed(CAN) LPV APPROACH ANOMALY: GLIDE SLOPE DEVIATION POINTER MOMENTARILY SCALLOPED UP FOR A SPLIT SECOND AT FINAL APPROACH FIX ON RNAV LPV APPROACH TO RUNWAY. THIS RESULTED IN THE AUTOPILOT MOMENTARILY PITCHING THE AIRCRAFT NOSE UP FOLLOWING THE GLIDE SLOPE SCALLSDR DALA2016110108052Access Panel · corrodedCORROSION ON ACCESS PANEL 370GR VOR/LOCALIZER ANTENNA PANEL. LOWER RT VOR/LOCALIZER ANTENNA PANEL WAS REPLACED IAW AMM 34-32-03 AND TEST WAS PERFORMED IAW AMM 34-35-01. TEST OK.SDR CA1912050006Adapter · failed(CAN) FINAL APPROACH CONDUCTING LPV APPROACH AIRCRAFT WAS FULLY CONFIGURED AND STABLE ON APPROACH WITH LOCALIZER AND GLIDE SLOPE CAPTURED. EXACTLY WHILE CROSSING FAF GLIDE SLOPE HAD A LARGE UPWARD DEVIATION AND AUTOPILOT RAPIDLY PITCHED AIRCRAFT NOSE UP. I IMMSDR CALA2014021790401Indicator · malfunctionedLOST BOTH FLIGHT DIRECTOR GLIDE SLOPE INDICATORS ON FINAL.SDR CA130809006Amplifier · misinstalled(CAN) THE AIRCRAFT EXPERIENCED AUDIO CONTROL ISSUES ON A ROUTINE FLIGHT FROM YEG TO YMM, MAINTENANCE WAS CALLED OUT AND VERIFIED THE AUDIO AMP HAD FAILED. THE AMP WAS REPLACED AND THE AUDIO SYSTEM WAS GROUND FUNCTION CHECKED SERVICEABLE. ON AUG 6, 2013 THE AISDR UALA2011120506672Circuit Card · malfunctionedAPU BATTERY OVERHEAT STATUS MESSAGE DISPLAYED ON EICAS. REPLACED APU BATTERY, NO HELP. SIGNAL CONDITIONING CARD REPLACED REF AMM & DIODE 405 POS-12 IN P310 REPLACED REF WDM 24-09-26 PG 1-SHT2, NO MESSAGES PRESENT AFTER 4 HRS OF ACFT POWER -ON-, WITH MULTIPLSDR ASAA1159413Battery · defectiveAUX BATTERY READING 2 AMPS DRAW. PERFORMED AUX BATTERY CHARGER OPERATIONAL TEST PER M/M 24 31 31 710 801 TESTS WITHIN LIMITS. AUX BATTERY STILL 27 VOLTS 2 AMP CHARGE. REPLACED AUX BATTERY REF M/M 24 31 11 TEST NORMAL. AFTER APPROX 20 MINUTES AUX BATTRY RESDR HNAA2010082600195Glide Slope · malfunctionedCREW REPORTED BOTH GLIDE SLOPES OPERATED NORMALLY AND LOCALIZERS SHOW ACFT LT OF RUNWAY. HAD TO USE WET COMPASS FOR HEADING DIRECTION. PERFORMED OPS CHECK OF BOTH ILS SYS WITH TEST EQUIPMENT, OPS NORMAL AT THIS TIME.SDR UALA2010071302516Battery · failedAPU FAULT - STATUS MSGS NEEDS BATTERY. REPLACED APU BATTERY PER MM. APU BATTERY CHARGE AND VOLTS GOOD.SDR 2010FA0000624Antenna · unknownCREW REPORTED THAT ON APPROACH, GLIDE SLOPE DEVIATED UP AND DOWN TO RUNWAY 18L. AUTOPILOT WAS ENGAGED AND COUPLED TO BOTH OF THE NAVIGATION RECEIVERS, WHICH CAUSED THE AIRPLANE TO PORPOISE UP AND DOWN. A/P DISCONNECTED BY CREW AND LANDING CONTINUED ON VISUALLSDR 2010FA0000267Transceiver · malfunctionedON 01/30/2010 POST INSTALLATION, EMI TESTING WAS CONDUCTED IAW APPENDIX B OF TDFM-136 INSTALLATION AND OPERATING INSTRUCTIONS TIL DOC NR 99RE255, REV D ISSUE 7, DATED APRIL 2004. AS A RESULT OF THOSE TESTS IT WAS DETERMINED THAT AN INTERFERENCE PROBLEM EXISTSSDR 2010FA0000266Transceiver · malfunctionedON 01/30/2010 POST INSTALLATION, EMI TESTING WAS CONDUCTED IAW APPENDIX B OF TDFM-136 INSTALLATION AND OPERATING INSTRUCTIONS TIL DOC NR 99RE255, REV D ISSUE 7, DATED APRIL 2004. AS A RESULT OF THOSE TESTS IT WAS DETERMINED THAT AN INTERFERENCE PROBLEM EXISTSSDR 2010FA0000265Transceiver · malfunctionedON 01/30/2010 POST INSTALLATION, EMI TESTING WAS CONDUCTED IAW APPENDIX B OF TDFM-136 INSTALLATION AND OPERATING INSTRUCTIONS TIL DOC NR 99RE255, REV D ISSUE 7, DATED APRIL 2004. AS A RESULT OF THOSE TESTS IT WAS DETERMINED THAT AN INTERFERENCE PROBLEM EXISTSSDR 2010FA0000264Transceiver · malfunctionedON 01/30/2010 POST INSTALLATION, EMI TESTING WAS CONDUCTED IAW APPENDIX B OF TDFM-136 INSTALLATION AND OPERATING INSTRUCTIONS TIL DOC NR 99RE255, REV D ISSUE 7, DATED APRIL 2004. AS A RESULT OF THOSE TESTS IT WAS DETERMINED THAT AN INTERFERENCE PROBLEM EXISTSSDR 2010FA0000263Transceiver · malfunctionedON 01/30/2010 POST INSTALLATION, EMI TESTING WAS CONDUCTED IAW APPENDIX B OF TDFM-136 INSTALLATION AND OPERATING INSTRUCTIONS TIL DOC NR 99RE255, REV D ISSUE 7, DATED APRIL 2004. AS A RESULT OF THOSE TESTS IT WAS DETERMINED THAT AN INTERFERENCE PROBLEM EXISTSSDR 2010FA0000262Transceiver · malfunctionedON 01/30/2010 POST INSTALLATION, EMI TESTING WAS CONDUCTED IAW APPENDIX B OF TDFM-136 INSTALLATION AND OPERATING INSTRUCTIONS TIL DOC NR 99RE255, REV D ISSUE 7, DATED APRIL 2004. AS A RESULT OF THOSE TESTS IT WAS DETERMINED THAT AN INTERFERENCE PROBLEM EXISTSSDR 2010FA0000261Transceiver · malfunctionedON 01/30/2010 POST INSTALLATION, EMI TESTING WAS CONDUCTED IAW APPENDIX B OF TDFM-136 INSTALLATION AND OPERATING INSTRUCTIONS TIL DOC NR 99RE255, REV D ISSUE 7, DATED APRIL 2004. AS A RESULT OF THOSE TESTS IT WAS DETERMINED THAT AN INTERFERENCE PROBLEM EXISTSSDR 2010FA0000260Transceiver · malfunctionedON 01/30/2010 POST INSTALLATION, EMI TESTING WAS CONDUCTED IAW APPENDIX B OF TDFM-136 INSTALLATION AND OPERATING INSTRUCTIONS TIL DOC NR 99RE255, REV D ISSUE 7, DATED APRIL 2004. AS A RESULT OF THOSE TESTS IT WAS DETERMINED THAT AN INTERFERENCE PROBLEM EXISTSSDR 2010FA0000259Transceiver · malfunctionedON 01/30/2010 POST INSTALLATION, EMI TESTING WAS CONDUCTED IAW APPENDIX B OF TDFM-136 INSTALLATION AND OPERATING INSTRUCTIONS TIL DOC NR 99RE255, REV D ISSUE 7, DATED APRIL 2004. AS A RESULT OF THOSE TESTS IT WAS DETERMINED THAT AN INTERFERENCE PROBLEM EXISTSSDR 2010FA0000258Transceiver · malfunctionedON 01/30/2010 POST INSTALLATION, EMI TESTING WAS CONDUCTED IAW APPENDIX B OF TDFM-136 INSTALLATION AND OPERATING INSTRUCTIONS TIL DOC NR 99RE255, REV D ISSUE 7, DATED APRIL 2004. AS A RESULT OF THOSE TESTS IT WAS DETERMINED THAT AN INTERFERENCE PROBLEM EXISTSSDR 2010F00070Transceiver · interferenceON 01/30/2010 POST INSTALLATION EMI TESTING WAS CONDUCTED IAW APPENDIX B OF TDFM-136 INSTALLATION AND OPERATING INSTRUCTIONS TIL DOCUMENT NR 99RE255, REV D ISSUE 7, DATED APRIL 2004. AS A RESULT OF THOSE TESTS IT WAS DETERMINED THAT AN INTERFERENCE PROBLEM EXISDR 2010F00069Transceiver · interferenceON 01/30/2010 POST INSTALLATION EMI TESTING WAS CONDUCTED IN ACCORDANCE WITH APPENDIX B OF TDFM-136 INSTALLATION AND OPERATING INSTRUCTIONS TIL DOC NR 99RE255, REV D ISSUE 7, DATED APRIL 2004. AS A RESULT OF THOSE TESTS IT WAS DETERMINED THAT AN INTERFERENCE SDR 2010F00068Transceiver · interferenceON 01/30/2010 POST INSTALLATION EMI TESTING WAS CONDUCTED IAW APPENDIX B OF TDFM-136 INSTALLATION AND OPERATING INSTRUCTIONS TIL DOC NR 99RE255, REV D ISSUE 7, DATED APRIL 2004. AS A RESULT OF THOSE TESTS IT WAS DETERMINED THAT AN INTERFERENCE PROBLEM EXISTS ASDR 2010FA0000234Transceiver · interferenceON 01/30/2010 POST INSTALLATION EMI TESTING WAS CONDUCTED IAW APPENDIX B OF TDFM-136. INSTALLATION AND OPERATING INSTRUCTIONS TIL DOC NR. 99RE255, REV D ISSUE 7, DATED APRIL 2004. AS A RESULT OF THOSE TESTS IT WAS DETERMINED THAT AN INTERFERENCE PROBLEM EXISTSDR A6WA200940141Antenna · erraticNAV 1 AND NAV 2 INDICATED ERRATIC GLIDE SLOPE INDICATIONS FOLLOWED BY ERRONEOUS INDICATION AND GLIDE SLOPE FLAG WHILE OTHER ACFT RECEIVED NAV-AID RECEPTION. REMOVED AND REPLACED GLIDE SLOPE ANTENNA IAW AMM 34-51-11. OPS CHECK GOOD. (K)SDR COMA2009012650070Antenna · failedON APPROACH INTO CVG, GLIDE SLOPE INDICATIONS ERRATIC FOLLOWED BY TOTAL LOSS OF GLIDE SLOPE INDICATOR. A/C LANDED SAFELY. REMOVED AND REPLACED GLIDE SLOPE ANTENNA. OPS CHECK GOOD.SDR MALA070204Antenna · malfunctionedON ILS APPROACH TO DTW, APPROACH MODE ARMED AT 4000 FT, SHOWING HIGH ON SLOPE. AUTO PILOT ON. UNCOMMANDED DESCENT TO 4000 FPM NOTED. AP OFF. AP REMAINED OFF FOR REMAINDER OF FLIGHT. UPON UNCOMMANDED DESCENT, AVIONICS LIGHT NOTED. YELLOW GS NOTED EADI. SSDR FDKA200709441Detector · malfunctionedABORTED T/O DUE TO F/O'S HEADING OFF 30 PERCENT. REMOVED AND REPLACED FLUX DETECTOR.SDR CA040908003Glide Slope · erratic(CAN) RT GLIDESLOPE INDICATION VERY ERRATIC AND NO WARNING FLAP IN VIEW TELLING PILOT SIGNAL INVALID. MEL'ED SYSTEM AND TROUBLESHOOTING IN PROGRESS.SDR 04FDEA01764Housing · crackedGLIDE SLOPE HOUSING MOUNTING BRACKET FOUND CRACKED. GLIDESLOPE HOUSING MOUNTING BRACKET REMOVED AND REPLACED AS PER AMM 32-21-34-4 AND GLIDESLOPE FUNCTIONAL TEST CARRIED OUT AS PER AMM 34-32-02-2, FOUND SATIS.SDR ASMF200406004Relay · failedAIRCRAFT RETURNED TO PLATFORM DURING ENGINE START, VHF NAV NR 1 FAILED. VHF NR 1 CONTROL PANEL, DFGC AND VOR RECEPTOR WERE REPLACED AND FAIL CONTINUE. ENGINE WAS SHUTDOWN AND HIGH FREQUENCY ON LT GENERATOR WAS DETECTED. LT GENERATOR WAS INOPERATIVE AND AIRCRASDR ASMF200404010Connector · damagedDURING TRANSIT CHECK, CAPTAIN REPORTED THAT THE LEFT VHF SYSTEM WAS OUT OF SERVICE. TECHNICAL PERSONNEL REPLACED RX VOR ILS AND CONTROL PANEL, BUT FAIL CONTINUED. WIRING WAS CHECKED DETECTING THE LINE 1RN11A22 OF THE CONNECTOR P10-407 (PIN H) DAMAGED. REPAISDR C1HA200476002Glide Slope · erraticBOTH GLIDE SLOPES ERRATIC CAUSING GO-AROUND. SUSPECT GROUND PROBLEM. PERFORMED TEST ON BOTH ILS SYSTEMS. NO DEFECT NOTED IAW MM 34-31-00.SDR COMA0460242Receiver · malfunctionedFLIGHT 5837 COPILOTS GLIDESLOPE FLAG ON APPROACH. REPLACED THE NR 2 NAV RECEIVER.SDR MEX2003468Receiver · failedAIRCRAFT RETURNED TO PLATFORM, DURING TAXING. VOR FLAGS ON RDMI INSIGHT IN BOTH INSTRUMENTS. TX RX VOR/ILS WAS REPLACED BUT FAIL CONTINUED. RETURN TO SERVICE TEST WAS PERFORMED SHOWING 375 FAILURE CODE (VOR/DFGC FAILURE). AIRCRAFT WAS SENT TO THE HANGAR WHSDR 2003FA0000237Indicator · inoperativeNEW AIRCRAFT, NEW HSI 345 HRS TTAF. GLIDESLOPE INOPERATIVE, FOUND GLIDESLOPE NEEDLE RESTRAINT (FROM TRANSPORT) STILL IN PLACE.SDR BAQA084698Controller · brokenBACK OF CONNECTOR ON HSI IS BROKEN. BROKEN AT TIME OF RECEIVING.SDR AUS20020197Connector · faulty(AUS) GLIDESLOPE RECEIVER CONNECTOR INPUT VOLTAGE PIN BENT.SDR ABXA010524Indicator · malfunctionedBOTH LEFT AND RIGHT GLIDE SLOPES WERE FLAGGED. MAINTENANCE PERFORMED B767 FIM 22-00-02, FIG 113. A CAT III EVALUATION APPROACH WAS COMPLETED WITH SATISFACTORY RESULTS.SDR HEEA072647Receiver · failedWILL NOT RECEIVE. PERFORMED PRELIMINARY INSPECTION. REPLACED OPEN FUSE F501. REPAIRED PROBLEM. ADJUSTED LOCALIZER DEVIATION. BENCH CHECK GOOD.SDR 2001UALA00046Receiver · inoperativeNR 1 NAVIGATION RECEIVER IS INOPERATIVE. *S/D* REPLACED NR 1 NAVIGATION RECEIVER. OPS CHECKED OK.SDR MALA000653Computer · malfunctionedAIR RETURN FOR STANDBY PITCH TRIM INOP (AIR ONLY). FROM DMR AFCS COMMANDED 7 PITCH UP JUST PRIOR TO GS CAPTURE. GS INDICATED LOW WHEN EVENT OCCURRED. MAINTENANCE REPLACED F1 CONTROL COMPUTER IAW HMM CHAP 34 P/N 622-7491-210, SN/OFF 1723, SN/ON 1548. OPS CHSDR SWIA971996Indicator · failedNUMBER TWO NAV SYSTEM FAILED INFLIGHT. ''''NAV'''' FLAG WITHOUT IDENT FEATURE ON ALL VOR AND ILS FREQUENCIES. RETURNED TO SLC. INSTALLED SERVICEABLE VIR-32 NAV BOX IAW MM 34-54-00. NUMBER TWO NAV SYSTEM OPS CHECKS GOOD. (S/N 14919) ON, (S/N 10605) OFF.
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