# Service difficulty reports: JASC 3432

A list on [JASC 3432](https://openairdocs.org/jasc/3432.md).

Reports filed under 3432 · Glide Slope System, newest first.

Page 1 of 2 · 66 reports

- [SDR FDEA202607100898](https://openairdocs.org/sdr/FDEA202607100898.md): Glide Slope · malfunctioned · Jul 10, 2026 · N654FE · Airbus A300F4605R
  > ON RNAV APPROACH RW 21, ON GLIDEPATH AND CONFIGURED FOR LANDING GOT GLIDESLOPE GLIDESLOPE REPEATEDLY STARTING AT 100 FEET UNTIL TOUCHDOWN.
- [SDR DALA2026052603148](https://openairdocs.org/sdr/DALA2026052603148.md): Glide Slope · faulted · May 24, 2026 · N319NB · Airbus A319114
  > DIV - 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 DALA2026030301468](https://openairdocs.org/sdr/DALA2026030301468.md): Glide Slope · failed · Feb 28, 2026 · N344DN · Airbus A321213
  > SHIP 3044 - DIV - TO BHM DUE TO CAPTAINS GLIDE SLOPE FAILURE DURING THE APPROACH TO ATL. CORRECTIVE ACTION: REPLACED MMR #1. (LP 1472944, 1472661)
- [SDR HNAA2025103100730](https://openairdocs.org/sdr/HNAA2025103100730.md): Glide Slope · unknown · Oct 29, 2025 · N652RS · Emb EMB145LR
  > RECIEVED 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 P
- [SDR YENA2024101801379](https://openairdocs.org/sdr/YENA2024101801379.md): Glide Slope · faulted · Oct 16, 2024 · N2142J · Airbus A321271N
  > FLT#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 HNAA2020122100376](https://openairdocs.org/sdr/HNAA2020122100376.md): Control Unit · malfunctioned · Dec 20, 2020 · N658AE · Emb EMB145LR
  > GLIDESLOPE 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 34-5
- [SDR YBBA20181203001](https://openairdocs.org/sdr/YBBA20181203001.md): Glide Slope · false indication · Nov 30, 2018 · N111WH · Amd FALCON10
  > PIC 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 CA191205007](https://openairdocs.org/sdr/CA191205007.md): Adapter · failed · Jan 26, 2017 · Boeing 73736Q
  > (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 SCALL
- [SDR DALA2016110108052](https://openairdocs.org/sdr/DALA2016110108052.md): Access Panel · corroded · Aug 4, 2016 · N959AT · Boeing 717200
  > CORROSION 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 CA1912050006](https://openairdocs.org/sdr/CA1912050006.md): Adapter · failed · Jan 24, 2016 · Boeing 73736N
  > (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 IMM
- [SDR CALA2014021790401](https://openairdocs.org/sdr/CALA2014021790401.md): Indicator · malfunctioned · Feb 14, 2014 · N659UA · Boeing 767322
  > LOST BOTH FLIGHT DIRECTOR GLIDE SLOPE INDICATORS ON FINAL.
- [SDR CA130809006](https://openairdocs.org/sdr/CA130809006.md): Amplifier · misinstalled · Aug 4, 2013 · Beech B200
  > (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 AI
- [SDR UALA2011120506672](https://openairdocs.org/sdr/UALA2011120506672.md): Circuit Card · malfunctioned · Dec 5, 2011 · N783UA · Boeing 777222
  > APU 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 MULTIPL
- [SDR ASAA1159413](https://openairdocs.org/sdr/ASAA1159413.md): Battery · defective · Apr 10, 2011 · N566AS · Boeing 737890
  > AUX 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 RE
- [SDR HNAA2010082600195](https://openairdocs.org/sdr/HNAA2010082600195.md): Glide Slope · malfunctioned · Jul 29, 2010 · N808EX · Dhav DHC8102
  > CREW 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 UALA2010071302516](https://openairdocs.org/sdr/UALA2010071302516.md): Battery · failed · Jul 13, 2010 · N794UA · Boeing 777222
  > APU FAULT - STATUS MSGS NEEDS BATTERY. REPLACED APU BATTERY PER MM. APU BATTERY CHARGE AND VOLTS GOOD.
- [SDR 2010FA0000624](https://openairdocs.org/sdr/2010FA0000624.md): Antenna · unknown · May 4, 2010 · N779AZ · Cndair CL6002B16
  > CREW 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 VISUALL
- [SDR 2010FA0000267](https://openairdocs.org/sdr/2010FA0000267.md): Transceiver · malfunctioned · Mar 16, 2010
  > ON 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
- [SDR 2010FA0000266](https://openairdocs.org/sdr/2010FA0000266.md): Transceiver · malfunctioned · Mar 16, 2010
  > ON 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
- [SDR 2010FA0000265](https://openairdocs.org/sdr/2010FA0000265.md): Transceiver · malfunctioned · Mar 16, 2010
  > ON 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
- [SDR 2010FA0000264](https://openairdocs.org/sdr/2010FA0000264.md): Transceiver · malfunctioned · Mar 16, 2010
  > ON 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
- [SDR 2010FA0000263](https://openairdocs.org/sdr/2010FA0000263.md): Transceiver · malfunctioned · Mar 16, 2010
  > ON 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
- [SDR 2010FA0000262](https://openairdocs.org/sdr/2010FA0000262.md): Transceiver · malfunctioned · Mar 16, 2010
  > ON 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
- [SDR 2010FA0000261](https://openairdocs.org/sdr/2010FA0000261.md): Transceiver · malfunctioned · Mar 16, 2010
  > ON 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
- [SDR 2010FA0000260](https://openairdocs.org/sdr/2010FA0000260.md): Transceiver · malfunctioned · Mar 16, 2010
  > ON 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
- [SDR 2010FA0000259](https://openairdocs.org/sdr/2010FA0000259.md): Transceiver · malfunctioned · Mar 16, 2010
  > ON 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
- [SDR 2010FA0000258](https://openairdocs.org/sdr/2010FA0000258.md): Transceiver · malfunctioned · Mar 16, 2010
  > ON 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
- [SDR 2010F00070](https://openairdocs.org/sdr/2010F00070.md): Transceiver · interference · Jan 30, 2010
  > ON 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 EXI
- [SDR 2010F00069](https://openairdocs.org/sdr/2010F00069.md): Transceiver · interference · Jan 30, 2010
  > ON 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 2010F00068](https://openairdocs.org/sdr/2010F00068.md): Transceiver · interference · Jan 30, 2010
  > ON 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 A
- [SDR 2010FA0000234](https://openairdocs.org/sdr/2010FA0000234.md): Transceiver · interference · Jan 30, 2010
  > ON 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 EXIST
- [SDR A6WA200940141](https://openairdocs.org/sdr/A6WA200940141.md): Antenna · erratic · Mar 20, 2009 · N404AW · Cndair CL6002B19
  > NAV 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 COMA2009012650070](https://openairdocs.org/sdr/COMA2009012650070.md): Antenna · failed · Jan 25, 2009 · N810CA · Cndair CL6002B19
  > ON 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 MALA070204](https://openairdocs.org/sdr/MALA070204.md): Antenna · malfunctioned · Dec 28, 2007 · N415XJ · Saab 340B
  > ON 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. S
- [SDR FDKA200709441](https://openairdocs.org/sdr/FDKA200709441.md): Detector · malfunctioned · Sep 3, 2007 · N832MJ · Emb EMB145LR
  > ABORTED T/O DUE TO F/O'S HEADING OFF 30 PERCENT. REMOVED AND REPLACED FLUX DETECTOR.
- [SDR CA040908003](https://openairdocs.org/sdr/CA040908003.md): Glide Slope · erratic · Sep 7, 2004 · Beech B200
  > (CAN) RT GLIDESLOPE INDICATION VERY ERRATIC AND NO WARNING FLAP IN VIEW TELLING PILOT SIGNAL INVALID. MEL'ED SYSTEM AND TROUBLESHOOTING IN PROGRESS.
- [SDR 04FDEA01764](https://openairdocs.org/sdr/04FDEA01764.md): Housing · cracked · Jun 16, 2004 · N610FE · Doug MD11
  > GLIDE 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 ASMF200406004](https://openairdocs.org/sdr/ASMF200406004.md): Relay · failed · Jun 4, 2004 · N754RA · Doug DC987
  > AIRCRAFT 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 AIRCRA
- [SDR ASMF200404010](https://openairdocs.org/sdr/ASMF200404010.md): Connector · damaged · Apr 13, 2004 · N838AM · Doug DC983
  > DURING 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. REPAI
- [SDR C1HA200476002](https://openairdocs.org/sdr/C1HA200476002.md): Glide Slope · erratic · Apr 13, 2004 · N817EA · Boeing 727225
  > BOTH GLIDE SLOPES ERRATIC CAUSING GO-AROUND. SUSPECT GROUND PROBLEM. PERFORMED TEST ON BOTH ILS SYSTEMS. NO DEFECT NOTED IAW MM 34-31-00.
- [SDR COMA0460242](https://openairdocs.org/sdr/COMA0460242.md): Receiver · malfunctioned · Apr 1, 2004 · N710CA · Cndair CL6002B19
  > FLIGHT 5837 COPILOTS GLIDESLOPE FLAG ON APPROACH. REPLACED THE NR 2 NAV RECEIVER.
- [SDR MEX2003468](https://openairdocs.org/sdr/MEX2003468.md): Receiver · failed · Oct 6, 2003 · N751RA · Doug DC987
  > AIRCRAFT 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 WH
- [SDR 2003FA0000237](https://openairdocs.org/sdr/2003FA0000237.md): Indicator · inoperative · Feb 28, 2003 · N3535T · Cessna 206H
  > NEW AIRCRAFT, NEW HSI 345 HRS TTAF. GLIDESLOPE INOPERATIVE, FOUND GLIDESLOPE NEEDLE RESTRAINT (FROM TRANSPORT) STILL IN PLACE.
- [SDR BAQA084698](https://openairdocs.org/sdr/BAQA084698.md): Controller · broken · Feb 24, 2003 · N941MS · Aerosp AS355F2
  > BACK OF CONNECTOR ON HSI IS BROKEN. BROKEN AT TIME OF RECEIVING.
- [SDR AUS20020197](https://openairdocs.org/sdr/AUS20020197.md): Connector · faulty · Feb 23, 2002 · Cessna TR182
  > (AUS) GLIDESLOPE RECEIVER CONNECTOR INPUT VOLTAGE PIN BENT.
- [SDR ABXA010524](https://openairdocs.org/sdr/ABXA010524.md): Indicator · malfunctioned · Sep 26, 2001 · N787AX · Boeing 767281
  > BOTH 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 HEEA072647](https://openairdocs.org/sdr/HEEA072647.md): Receiver · failed · Apr 17, 2001 · N3911L · Bell 412
  > WILL NOT RECEIVE. PERFORMED PRELIMINARY INSPECTION. REPLACED OPEN FUSE F501. REPAIRED PROBLEM. ADJUSTED LOCALIZER DEVIATION. BENCH CHECK GOOD.
- [SDR 2001UALA00046](https://openairdocs.org/sdr/2001UALA00046.md): Receiver · inoperative · Jan 22, 2001 · N334UA · Boeing 737322
  > NR 1 NAVIGATION RECEIVER IS INOPERATIVE. *S/D* REPLACED NR 1 NAVIGATION RECEIVER. OPS CHECKED OK.
- [SDR MALA000653](https://openairdocs.org/sdr/MALA000653.md): Computer · malfunctioned · Oct 31, 2000 · N109XJ · Saab SF340A
  > AIR 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 CH
- [SDR SWIA971996](https://openairdocs.org/sdr/SWIA971996.md): Indicator · failed · Sep 23, 2000 · N212SW · Emb EMB120ER
  > NUMBER 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.

Next page: https://openairdocs.org/jasc/3432/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/jasc/3432/reports

---
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