JASC 3212
Service difficulty reports · 759
Reports filed under 3212 · Emergency Flotation Section, 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 = '3212' 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 = '3212' 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 YV3R2023042700562Cylinder · defectiveCUSTOMER REPORTED CYLINDER ASSEMBLY P/N: D679-3 LEAKED BELOW ALLOWABLE INDICATION LIMIT.SDR YV3R2023042700557Cylinder · defectiveCUSTOMER REPORTED CYLINDER ASSEMBLY P/N: D679-3 PRESSURE GAGE INDICATES ZERO.SDR FDEA202204010810Skin · delaminatedLANDING GEAR - BODY GEAR AND DOORS - LH MLG DOOR LH HEAT SHIELD ASSY DELAMINATI COMPLY WITH E..A. F-3212-T0367771 REV NO. POS. P1. COMPLIED WITH EA F-3212-T0367771 P1 BY REPAIR ON PN 149N6023-7 HEAT SHIELD DELAMINATION ON SKIN.SDR H44R2019061000009Float · malfunctionedDURING ACCOMPLISHMENT OF THE APICAL LIGHTWEIGHT EMERGENCY FLOAT KIT (STC# SR01450LA) 3 YEAR INSPECTION THE SYSTEM IS ACTUATED AND THE EMERGENCY FLOATS ARE DEPLOYED. IT REQUIRED 3 ATTEMPTS TO ACTUATE THE SYSTEM. WE WERE UNABLE TO DETERMINE IF IT WAS A RIGGING ISDR CA190510007Cable · out of rig(CAN) AFTER A SUCCESSFUL FLOAT DEPLOYMENT AND INFLATION FROM COCKPIT DURING THE 36 MONTH INSPECTION, THE LIFE RAFT DEPLOYMENT HANDLE WAS CYCLED NUMEROUS TIMES BUT FAILED TO DEPLOY/INFLATE THE LIFE RAFTS. LIFE RAFTS WERE SUCCESSFULLY DEPLOYED USING THE EXTERIORSDR 2017FA0000496Switch · out of alignmentWHILE PERFORMING THE ICA CHECK ON THE ARM/FIRE CONTROL & INDICATOR CIRCUIT TEST PROCEDURE FOR THE EMERGENCY FLOATATION GEAR IAW MM SUPPLEMENT (ICA), DISCOVERED THAT THE PILOT’S CYCLIC MOUNTED SWITCH GUARD COULD BE IN THE CLOSED POSITION WITH THE SWITCH REMAINSDR H44R2017072000005Handle · shearedDURING A 3 YEAR INSPECTION OF THE EMERGENCY FLOAT GEAR SYSTEM THE INFLATION ACTUATION HANDLE BROKE, THE FLOATS DID NOT ACTUATE. TO CONTINUE THE INSPECTION THE ACTUATION CABLE WAS PULLED DIRECTLY, IT REQUIRED A LOT OF PULL TO INITIATE FLOAT INFLATION. ONCE INITSDR CA140217026Cable · failed(CAN) DURING 36 MONTH INSPECTION HANDLE WAS PULLED TO DEPLOY EMERGENCY FLOAT SYSTEM. SYS DID NOT DEPLOY. CABLE WAS REMOVED AND FOUND UNSERVICEABLE.SDR ALGA2012110729104Float · failedSECONDARY FLOAT SYS WOULD NOT TEST. MX PERFORMED OPS CHECK AND FOUND GOOD.SDR CA110907008Pin · loose(CAN) DURING REWORK MX, THE INTERFACE BETWEEN THE EXTERNAL PIN AND THE LEVER WAS FOUND TO BE NOT ROBUST ENOUGH AND WOULD ALLOW THE EXTERNAL PIN TO MOVE WITHIN THE LEVER. IF THE EXTERNAL PIN WAS TO MOVE COMPLETELY OUT OF THE LEVER, IT WOULD FALL OUT AND THE FLSDR AC2A7HV07162011Cable · seizedFLOAT DEPLOYMENT CABLE SEIZED TO SHEATH AND END FITTING SEPARATED AT CRIMP INSIDE FITTING PROTECTIVE BOOT.SDR FDEA201101300418Rib · corrodedLT WING RIB 5 FWD LUG HAS CORROSION. REPAIRED IAW EA 6-5710-145518 WING-AD 2008-17-02 - WING GEAR RIB 5 FWD LUG BORE REWORK (LT SIDE), SB A310-57-2090, EO 6-5710-7-5010.SDR FDEA201101300417Rib · corrodedRT WING, RIB 5, FWD LUG HAS CORROSION REPAIRED IAW EA 6-5710-145517, WING-AD2008-17-02, WING GEAR, RIB5 FWD LUG BORE REWORK (RT SIDE), SB A310-57-2090, EO 6-5710-7-5010.SDR 2011FA0000079Float · misrepairedRECEIVED SEVERAL EMERGENCY FLOATATION SYS USED ON THE HELICOPTERS. DURING INSP/ EVALUATION, UNAPPROVED REPAIRS WERE FOUND TO HAVE BEEN INCORPORATED ONTO THESE EMERGENCY FLOAT ASSEMBLIES. IAW COMPONENT (CMM 25-61-01) SEC 6, D REPAIRS "USE NO MORE THAN 3 PATCHSDR YTRAN293CA4Float · bentTHE ACFT WAS IN FOR THE FIRST ROUTINE SCHEDULED 24 MONTH ACTIVATION/ INSP REQUIRED FOR THE OEM EMERGENCY FLOATATION KIT THAT IS INSTALLED IN CONJUNCTION WITH STC’D MID BAG WITH LIFE RAFT FLOAT KIT. THE STC’D FLOAT STEP KIT WAS INSTALLED 24 MONTHS AGO DUE TO TSDR YTRAN293CAJZ3Float · malfunctionedTHE AIRCRAFT WAS IN FOR THE FIRST 24 MONTH ACTIVATION/ INSPECTION. THE KIT WAS INSTALLED NEW 24 MONTHS AGO AND ONE OF THE PREREQUISITES FOR INSTALLATION OF THE STC'D KIT IS REMOVING THE OEM STEPS AND INSTALLING THE STC'D OPTIONAL STEPS. OUR COMPANY ELECTED TSDR YTRAN293CAJZ2Float · bindingTHE ACFT WAS IN FOR THE FIRST 24 MONTH ACTIVATION/ INSP. THE KIT WAS INSTALLED NEW 24 MONTHS AGO AND 1 OF THE PREREQUISITES FOR INSTALLATION OF THE STC'D KIT IS REMOVING THE OEM STEPS AND INSTALLING THE STC'D OPTIONAL STEPS. OUR COMPANY ELECTED TO INSTALL THSDR YTRAN293CAJZ1Cable · brokenTHE ACFT IS EQUIPPED WITH STC'D EMERGENCY FLOAT BAGS WITH LIFE RAFT. THE EMERGENCY RAFT PULL CABLE TO ACTIVATE THE RAFT FAILED COMPLETELY DURING THE INITIAL 24 MONTH ROUNTINE INSP. THE CABLE IS MADE FROM INFERIOR NON-AVIATION GRADE MATERIALS AND THIS FAILURESDR ALGA013010457ALValve · seizedDURING 3 YR FLOAT SYS FUNCTION CHECK, PULL CABLE WAS ACTUATED AND PLUNGER CAME COMPLETELY OUT OF FLOAT VALVE BUT VALVE FAILED TO OPEN CAUSING TEST TO FAIL. MX REPLACED FLOAT BOTTLE.SDR QMLA2009121109047Cable · corrodedDURING 18 MONTH INSP OF EMERGENCY FLOAT SYS, FOUND CABLE FOR ACTUATING DEPLOYMENT OF FLOATS CORRODED COMPLETELY THRU. CABLE FOR FLOAT SYS IS PART OF STC NR SR01855LA. SYS WAS INSTALLED ON ACFT 08 MAY 2008. MECHANICS INSTALLING REPLACEMENT CABLE WILL INSTALLSDR 2008UALA03463Structure · crackedRT AFT NLG DOOR AFT LOWER CORNER CRACKED APPROX 3"X1" AREA. *S/D* SUSPECT NORMAL AC OPERATION. ACCOMPLISHED INTERIM REPAIR PER EVA-71532. ** MF2588 CREATED TO MONITOR ** AC OK FOR SERVICE.SDR CA080130002Head · leaking(CAN) DURING AN INSPECTION THE EMERGENCY FLOAT SYS WERE DEPLOYED ACCIDENTALLY. (2) REFURBISHED KITS (PN:28022969) WERE ORDERED. BOTH VALVE ASSY (PN: 105-E-0031) WERE REBUILDED INCLUDING SHEARHEAD ASSY. (PN:29022979) NITROGEN PRESSURE WAS BROUGHT UP TO 3200PSI SDR AC2A118583Float · leakingLEAKED DURING 6 MONTH INSPECTION.SDR CA070810001Cover · damaged(CAN) THIS TURBO OPERATING AMPH FLOATS WAS ON DESCENT TO LAND AT ITS HOME AIRPORT WHEN THERE WAS NO GEAR DOWN INDICATION ON RT MAIN WHEEL. PILOT ASKED PASSENGER IN THE RT SEAT TO LOOK AT THE TOP OF FLOATS TO CHECK TIE-DOWN ROPES, AND IT WAS NOTICED THAT THE ENSDR HEEA115977Link · shearedAFTER DEPARTURE, THE RED GEAR UNSAFE LIGHT STAYED ILLUMINATED WHEN THE GEAR HANDLE WAS PLACED IN THE UP POSITION. MAINTENANCE FOUND THE SHEAR PIN IN ONE EXPLOSIVE LINK SHEARED. REPLACED LINK ASSY.SDR 07FDEA00147Trunnion · corrodedCENTER LANDING GEAR LT TRUNNION FOUND CORROSION. CTR LANDING GEAR LT TRUNNION FITTING REMOVED & REPLACED AS PER DWG AEA7035 AND SRM 51-31- 01 VOL.II. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA00146Trunnion · corrodedFOUND CENTER LANDING GEAR LT TRUNNION FWD HOLE FOUND CORROSION.SDR 07FDEA00100Trunnion · corrodedCENTER LANDING GEAR RT TRUNNION AFT HOLE FOUND CORROSION. REPAIR CARRIED OUT AT CENTER LANDING GEAR RH TRUNNION AFT HOLE AS PER FEDEX EA 1-5340-105661, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 06FDEA04053Fitting · corrodedCENTER LANDING GEAR RT TRUNNION SUPPORT FITTING FWD BORE HOLE FOUND CORROSION. REPAIR CARRIED OUT AT CENTER LANDING GEAR RT TRUNNION SUPPORT FITTING BORE HOLE AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 06FDEA04052Fitting · corrodedCENTER LANDING GEAR RT TRUNNION SUPPORT FITTING CTR BORE HOLE FOUND CORROSION. REPAIR CARRIED OUT AT CENTER LANDING GEAR RT TRUNNION SUPPORT FITTING BORE HOLE AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 06FDEA04051Fitting · corrodedCENTER LANDING GEAR RT TRUNNION SUPPORT FITTING AFT BORE HOLE FOUND CORROSION. REPAIR CARRIED OUT AT CENTER LANDING GEAR RT TRUNNION SUPPORT FITTING BORE HOLE AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 06FDEA04050Fitting · corrodedCENTER LANDING GEAR LT TRUNNION SUPPORT FITTING AFT BORE HOLE FOUND CORROSION. REPAIR CARRIED OUT AT CENTER LANDING GEAR LT TRUNNION SUPPORT FITTING BORE HOLE AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 06FDEA04049Fitting · corrodedCENTER LANDING GEAR LT TRUNNION SUPPORT FITTING CTR BORE HOLE FOUND CORROSION. REPAIR CARRIED OUT AT CENTER LANDING GEAR LT TRUNNION SUPPORT FITTING BORE HOLE AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 06FDEA04048Support Fitting · dirtyCENTER LANDING GEAR LT TRUNNION SUPPORT FITTING FWD BORE HOLE FOUND STAIN. STAIN AT CENTER LANDING GEAR LT TRUNNION SUPPORT FITTING FWD BORE HOLE CLEANED UP AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 06FDEA04046Trunnion · corrodedCENTER LANDING GEAR RT TRUNNION MATING SURFACE FOUND CORRODED. CENTER LANDING GEAR RIGHT TRUNNION MATING SURFACE CORROSION REMOVED AND FOUND WITHIN LIMIT AS PER SRM 53-40-00 FIGURE 15 VOLUME I. FORWARD SIDE ORIGINAL THICKNESS = 2.477". REMOVED MATERIAL = 0SDR 06FDEA04045Trunnion · corrodedCENTER LANDING GEAR LT TRUNNION MATING SURFACE FOUND CORRODED. CENTER LANDING GEAR LEFT TRUNNION MATING SURFACE CORROSION REMOVED AND FOUND WITHIN LIMIT AS PER SRM 53-40-00 FIGURE 15 VOLUME I. FORWARD SIDE ORIGINAL THICKNESS = 2.485". REMOVED MATERIAL = 0SDR AC2A110236Hose · misinstalledLINES WERE INSTALLED WRONG, CAUSING THEM TO BE KINKED.SDR AC2A110235Hose · misinstalledLINES WERE INSTALLED WRONG, CAUSING THEM TO BE KINKED.SDR 06FDEA1370Block · corrodedCENTER LANDING GEAR REPLACEMENT, RIGHT PILLOW BLOCK ATTACHMENT BOTTOM MATING SURFACE FOUND CORRODED. RT PILLOW BLOCK ATTACHMENT BOTTOM MATING SURFACE CORROSION REMOVED AND REPAIR CARRIED OUT AS PER SRM 53-40-00 FIG 15 VOL I. REPAIR CLASSIFIED AS MINOR AS PERSDR CA050923011Float · activatedHAD JUST FINISHED TRACING, BALANCING AC, BEGAN REMOVING BALANCING EQUIP. A/C READY DEPARTURE, LT SIDE EMERGENCY FLOAT INFLATED. AC HAD JUST COMPLETED TRANSMISSION CHANGE, ENGINE REMOVAL/REPAIR/REISTALLATION. DURING MAINT, EMERGENCY FLOATS SAFETY PINS WERE INSDR ALG2005F00054Switch · failedDURING RUN UP THE FLOAT WOULD NOT ARM, THE PILOT SHUT THE AC DOWN AND NOTIFIED MAINTENANCE. THE MECHANIC REMOVED AND REPLACED THE FLOAT ARM SWITCH AND THE AC WAS RETURNED TO SERVICE UPON COMPLETION OF THE FUNCTION CHECKS. (K)SDR ALG2005F00051Relay · faultyDURING THE SECOND TOUCH DOWN OF THE DAY, FLOATS INFLATED WITHOUT ANY INPUT FROM THE PILOT. THE MECHANIC REMOVED AND REPLACED THE FAULTY RELAY AND THE AC WAS RETURNED TO SERVICE UPON COMPLETION OF SYSTEM CHECKS. (K)SDR 14038052105Float · activatedDURING MAINT, TECH ATTEMPTED TO INSTALL SAFETY PIN IN RESERVOIR ASSY, FLOATS DEPLOYED. IT WAS LATER DISCOVERED THAT ELEC ACT USED TO DEPLOY FLOATS HAD BEEN PARTIALLY DEPLOYED. CHECK OF SYS REVEALED THAT ACT ONLY ENERGIZES WHILE DEPLOYMENT BUTTON IS DEPRESSED.SDR 2005FA0000979Actuator · defectiveLT MAIN LANDING GEAR FAILED DOWN AND LOCKED POSITION, UPON INSPECTION, O-RING IN ACTUATOR PLUNGER ASSY, MS28775-214 WAS FOUND DEFECTIVE, REPLACED WITH SAME PN RE INSTALLED ACTUATO TO FLOAT ASSY. OPS CHECKED OK, NO DEFECTS NOTED. (AL05200502475) (K)SDR CA050214001Valve · obstructed(CAN) FLOAT BAGS WOULD NOT INFLATE DURING 3 YEAR OPERATIONAL CHECK, THE VALVE ASSY WAS ASSEMBLED WITH THE SHEARED PORTION OF THE SHEAR HEAD STILL IN THE VALVE OBSTRUCTING THE AIR FLOW TO THE BAGS.SDR ERAA098194Float · delaminatedDELAMINATION AT AFT COMPARTMENT TOPPING OFF VALVE FOUND LEAKING VALVE AND 2 HOLES. REPAIRED IN A/W AC 25-60-95. FOUND BAG TO BE SERVICEABLE.SDR ERAA098192Float · leakingHOLES IN AFT COMPARTMENT OF FLOAT BAG. FLOAT WAS INSPECTED AND REPAIRED IAW OHSS-100-1. C/W INSPECTION IAW BO105-25-60-95.SDR ERAA097527Float · leakingFLOAT ASSY DUE 6 MONTH ASSY. SQUIB ALE LEAKING AT VALVE/MANIFOLD JUNCTION FWD CHECK VALVE ON BAG NOT OPENING PROPERLY. FLOAT BAG HAS EXCESSIVE NUMBER OF HOLES AT AFT COMPARTMENT. FWD END CAP WORN AND TORN. REMOVED AND REPLACED 1 EA O-RING AND 1 EA BACK UP SDR ERAA097526Float · leakingCYLINDER LEAKING. CYLINDER SQUIB VALVE ASSY TO BE LEAKING. REMOVED SQUIB VALVE/MANIFOLD ASSY FROM CYLINDER. REMOVED AND REPLACED O-RING AND BACK UP RING. VALVE TO MANIFOLD JUNCTION AND RE-INSTALLED VALVE/MANIFOLD ASSY ONTO CYLINDER. RE-CHARGED CYLINDER ASDR ERAA097525Float · tornINSPECTION DUE ON FLOAT ASSY. FLOAT COVER AND FWD END CAP WORN AND TORN. SQUIB CHARGE (1) P/N 94455 (SN 1709) EXPIRES 12-04. ELBOW ON SQUIB VALVE CORRODED. BAD CHECK VALVE ON AFT COMPARTMENT OF FLOAT BAG. REMOVED AND REPLACED FWD END CAP AND FLOAT COVER.
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