# Service difficulty reports: JASC 3212 A list on [JASC 3212](https://openairdocs.org/jasc/3212.md). Reports filed under 3212 · Emergency Flotation Section, newest first. Page 1 of 16 · 759 reports - [SDR YV3R2023042700562](https://openairdocs.org/sdr/YV3R2023042700562.md): Cylinder · defective · Apr 18, 2023 · Robsin R44RAVENII > CUSTOMER REPORTED CYLINDER ASSEMBLY P/N: D679-3 LEAKED BELOW ALLOWABLE INDICATION LIMIT. - [SDR YV3R2023042700557](https://openairdocs.org/sdr/YV3R2023042700557.md): Cylinder · defective · Apr 10, 2023 · N466HR · Robsin R66 > CUSTOMER REPORTED CYLINDER ASSEMBLY P/N: D679-3 PRESSURE GAGE INDICATES ZERO. - [SDR FDEA202204010810](https://openairdocs.org/sdr/FDEA202204010810.md): Skin · delaminated · Apr 1, 2022 · N949FD · Boeing 757200 > LANDING 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 H44R2019061000009](https://openairdocs.org/sdr/H44R2019061000009.md): Float · malfunctioned · Jun 1, 2019 · N408GG · Bell 407 > DURING 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 I - [SDR CA190510007](https://openairdocs.org/sdr/CA190510007.md): Cable · out of rig · May 9, 2019 · Bell 412EP > (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 EXTERIOR - [SDR 2017FA0000496](https://openairdocs.org/sdr/2017FA0000496.md): Switch · out of alignment · Jul 20, 2017 · N6977A · Snias AS350B3 > WHILE 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 REMAIN - [SDR H44R2017072000005](https://openairdocs.org/sdr/H44R2017072000005.md): Handle · sheared · Jul 20, 2017 · N945R · Bell 407 > DURING 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 INIT - [SDR CA140217026](https://openairdocs.org/sdr/CA140217026.md): Cable · failed · Feb 11, 2014 · Snias AS350B3 > (CAN) DURING 36 MONTH INSPECTION HANDLE WAS PULLED TO DEPLOY EMERGENCY FLOAT SYSTEM. SYS DID NOT DEPLOY. CABLE WAS REMOVED AND FOUND UNSERVICEABLE. - [SDR ALGA2012110729104](https://openairdocs.org/sdr/ALGA2012110729104.md): Float · failed · Nov 3, 2012 · N933BG · Skrsky S92A > SECONDARY FLOAT SYS WOULD NOT TEST. MX PERFORMED OPS CHECK AND FOUND GOOD. - [SDR CA110907008](https://openairdocs.org/sdr/CA110907008.md): Pin · loose · Jul 26, 2011 · Bell 429 > (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 FL - [SDR AC2A7HV07162011](https://openairdocs.org/sdr/AC2A7HV07162011.md): Cable · seized · Jul 16, 2011 · N427HV · Bell 427 > FLOAT DEPLOYMENT CABLE SEIZED TO SHEATH AND END FITTING SEPARATED AT CRIMP INSIDE FITTING PROTECTIVE BOOT. - [SDR FDEA201101300418](https://openairdocs.org/sdr/FDEA201101300418.md): Rib · corroded · Jan 30, 2011 · N423FE · Airbus A310203 > LT 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 FDEA201101300417](https://openairdocs.org/sdr/FDEA201101300417.md): Rib · corroded · Jan 30, 2011 · N423FE · Airbus A310203 > RT 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 2011FA0000079](https://openairdocs.org/sdr/2011FA0000079.md): Float · misrepaired · Jan 26, 2011 > RECEIVED 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 PATCH - [SDR YTRAN293CA4](https://openairdocs.org/sdr/YTRAN293CA4.md): Float · bent · Oct 15, 2010 · N293CA · Bell 412 > THE 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 T - [SDR YTRAN293CAJZ3](https://openairdocs.org/sdr/YTRAN293CAJZ3.md): Float · malfunctioned · Oct 15, 2010 · N293CA · Bell 412 > THE 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 T - [SDR YTRAN293CAJZ2](https://openairdocs.org/sdr/YTRAN293CAJZ2.md): Float · binding · Oct 15, 2010 · N293CA · Bell 412 > THE 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 TH - [SDR YTRAN293CAJZ1](https://openairdocs.org/sdr/YTRAN293CAJZ1.md): Cable · broken · Oct 15, 2010 · N293CA · Bell 412 > THE 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 FAILURE - [SDR ALGA013010457AL](https://openairdocs.org/sdr/ALGA013010457AL.md): Valve · seized · Jan 30, 2010 · N457AL · Bell 407 > DURING 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 QMLA2009121109047](https://openairdocs.org/sdr/QMLA2009121109047.md): Cable · corroded · Dec 11, 2009 · N541LN · Urocop EC135P2 > DURING 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 INSTALL - [SDR 2008UALA03463](https://openairdocs.org/sdr/2008UALA03463.md): Structure · cracked · Jun 19, 2008 · N226UA · Boeing 777222 > RT 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 CA080130002](https://openairdocs.org/sdr/CA080130002.md): Head · leaking · Jan 15, 2008 · Bolkms BO105S > (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 AC2A118583](https://openairdocs.org/sdr/AC2A118583.md): Float · leaking · Dec 20, 2007 · N6533U · Bell 206L3 > LEAKED DURING 6 MONTH INSPECTION. - [SDR CA070810001](https://openairdocs.org/sdr/CA070810001.md): Cover · damaged · Aug 9, 2007 · Dhav DHC2MK3 > (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 EN - [SDR HEEA115977](https://openairdocs.org/sdr/HEEA115977.md): Link · sheared · Jun 17, 2007 · N776P · Skrsky S76A > AFTER 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 07FDEA00147](https://openairdocs.org/sdr/07FDEA00147.md): Trunnion · corroded · Jan 20, 2007 · N590FE · Doug MD11 > CENTER 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 07FDEA00146](https://openairdocs.org/sdr/07FDEA00146.md): Trunnion · corroded · Jan 20, 2007 · N590FE · Doug MD11 > FOUND CENTER LANDING GEAR LT TRUNNION FWD HOLE FOUND CORROSION. - [SDR 07FDEA00100](https://openairdocs.org/sdr/07FDEA00100.md): Trunnion · corroded · Jan 15, 2007 · N590FE · Doug MD11 > CENTER 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 06FDEA04053](https://openairdocs.org/sdr/06FDEA04053.md): Fitting · corroded · Nov 20, 2006 · N628FE · Doug MD11 > CENTER 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 06FDEA04052](https://openairdocs.org/sdr/06FDEA04052.md): Fitting · corroded · Nov 20, 2006 · N628FE · Doug MD11 > CENTER 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 06FDEA04051](https://openairdocs.org/sdr/06FDEA04051.md): Fitting · corroded · Nov 20, 2006 · N628FE · Doug MD11 > CENTER 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 06FDEA04050](https://openairdocs.org/sdr/06FDEA04050.md): Fitting · corroded · Nov 20, 2006 · N628FE · Doug MD11 > CENTER 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 06FDEA04049](https://openairdocs.org/sdr/06FDEA04049.md): Fitting · corroded · Nov 20, 2006 · N628FE · Doug MD11 > CENTER 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 06FDEA04048](https://openairdocs.org/sdr/06FDEA04048.md): Support Fitting · dirty · Nov 20, 2006 · N628FE · Doug MD11 > CENTER 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 06FDEA04046](https://openairdocs.org/sdr/06FDEA04046.md): Trunnion · corroded · Nov 20, 2006 · N628FE · Doug MD11 > CENTER 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 = 0 - [SDR 06FDEA04045](https://openairdocs.org/sdr/06FDEA04045.md): Trunnion · corroded · Nov 20, 2006 · N628FE · Doug MD11 > CENTER 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 = 0 - [SDR AC2A110236](https://openairdocs.org/sdr/AC2A110236.md): Hose · misinstalled · Jul 10, 2006 · N139CW · Agusta AB139 > LINES WERE INSTALLED WRONG, CAUSING THEM TO BE KINKED. - [SDR AC2A110235](https://openairdocs.org/sdr/AC2A110235.md): Hose · misinstalled · Jul 10, 2006 · N139CW · Agusta AB139 > LINES WERE INSTALLED WRONG, CAUSING THEM TO BE KINKED. - [SDR 06FDEA1370](https://openairdocs.org/sdr/06FDEA1370.md): Block · corroded · Apr 11, 2006 · N582FE · Doug MD11F > CENTER 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 PER - [SDR CA050923011](https://openairdocs.org/sdr/CA050923011.md): Float · activated · Sep 22, 2005 · Snias AS350B3 > HAD 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 IN - [SDR ALG2005F00054](https://openairdocs.org/sdr/ALG2005F00054.md): Switch · failed · Jul 27, 2005 · N1078N · Cessna STC206C > DURING 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 ALG2005F00051](https://openairdocs.org/sdr/ALG2005F00051.md): Relay · faulty · Jul 23, 2005 · N1078Y · Bell 206B > DURING 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 14038052105](https://openairdocs.org/sdr/14038052105.md): Float · activated · May 21, 2005 · N316PD · Agusta A119 > DURING 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 2005FA0000979](https://openairdocs.org/sdr/2005FA0000979.md): Actuator · defective · May 2, 2005 · N3126D · Cessna 180 > LT 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 CA050214001](https://openairdocs.org/sdr/CA050214001.md): Valve · obstructed · Feb 11, 2005 · Bell 206L > (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 ERAA098194](https://openairdocs.org/sdr/ERAA098194.md): Float · delaminated · Sep 17, 2004 · N129EH · Bolkms BO105S > DELAMINATION 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 ERAA098192](https://openairdocs.org/sdr/ERAA098192.md): Float · leaking · Sep 10, 2004 · N294EH · Bolkms BO105S > HOLES IN AFT COMPARTMENT OF FLOAT BAG. FLOAT WAS INSPECTED AND REPAIRED IAW OHSS-100-1. C/W INSPECTION IAW BO105-25-60-95. - [SDR ERAA097527](https://openairdocs.org/sdr/ERAA097527.md): Float · leaking · Sep 4, 2004 · N294EH · Bolkms BO105S > FLOAT 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 ERAA097526](https://openairdocs.org/sdr/ERAA097526.md): Float · leaking · Aug 9, 2004 · N133EH · Bolkms BO105S > CYLINDER 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 A - [SDR ERAA097525](https://openairdocs.org/sdr/ERAA097525.md): Float · torn · Jul 24, 2004 · N294EH · Bolkms BO105S > INSPECTION 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. Next page: https://openairdocs.org/jasc/3212/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 = '3212' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/jasc/3212/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.