JASC 3600

Service difficulty reports · 508

Reports filed under 3600 · Pneumatic 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 = '3600'
  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.

SDR TSAA0436037Regulator · failedNR 2 ENGINE BLEED GIVES NO DUCT PRESSURE WITH ISOLATION VALVE IN AUTO OR CLOSED. RETURNED TO DEPARTURE AIRPORT, EXECUTED LOW SINK RATE LANDING. REMOVED AND REPLACED NR 2 ENGINE BLEED AIR REGULATOR IAW AMM 36-11-03-4. ENGINE NR 2 BLEED SYSTEM OPS CHECKS NORMAApr 14, 2004 · N746AL · Boeing 73776NSDR 03FDEA02175Pressure Switch · failedRECEIVED NR 1 MANIFOLD FAIL ALERT AT FL350. COULD NOT MAINTAIN CABIN PRESSURE. RAN RED TABS AND DIVERTED TO DEN. FOUND LEFT WING PRESSURE SWITCH FAULT BALL NO LEAKS NOTED. PERFORMED DECAY CHECK PER MD-10 MM 36-00-01-5 DECAY CHECK WITHIN LIMITS. REMOVED ANDec 8, 2003 · N364FE · Doug DC1010SDR IXXA0300072OPrecooler · crackedDURING CLIMB FROM KGSO TO KTOL NR 2 ENGINE PNEUMATIC SYSTEM OVERHEATS WITH LOW OR HIGH STAGE BLEED WITH CLIMB POWER SET AND LT PACK AT MIN FLOW. CREW RETURNED TO KGSO AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 2 PRECOOLER CONTROL VALVE Nov 8, 2003 · N822BX · Doug DC871FSDR USAASA03063Check Valve · failedAT APPROX FL260, DURING DESCENT, NR 2 ENG STALLED & LOST POWER. FELT A VIBRATION AS N1 DECREASED FROM 90 TO 50 PERCENT. THROTTLE PULL BACK STOPPED VIBRATION. COMMAND INDICATED APPROX 40 PERCENT, BUT ENGINE THRUST INDICATED 20 PERCENT. THROTTLE ADVANCED SLOWJun 12, 2003 · N705UW · Airbus A319112SDR 2003F00306Gasket · wornCREW REPORTED NR 3 STRUT OVERHEAT LIGHT CAME ON IMMEDIATELY AFTER LIFT OFF. CAPTAIN FOLLOWED AMERIJET NORMAL PROCEDURES AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND LEAK AT 13TH STAGE INBOARD DUCT. REMOVED AND REPLACED GASKETS. IN ADDITION, OFUNDApr 28, 2003 · N598AJ · Boeing 727212SDR AMTA200300546Pilot Valve · failedRIGHT ENGINE HIGH STAGE EICAS MESSAGE. REMOVED AND REPLACED HIGH STAGE PILOT PER FIM 36-10-00-1 FIG 111. OPS CHECKS GOOD. REF MM 36-11-08-4. (M)Apr 22, 2003 · N553TZ · Boeing 75733NSDR 200301Regulator · bindingDURING CRUISE FLIGHT, PILOT NOTICED A BURN ODOR IN COCKPIT. PILOT THEN NOTED THAT DOOR POST TRIM PANEL WAS DISCOLORED. RETURNED TO AIRPORT AND NOTIFIED MECHANIC. MECHANIC FOUND THE PRESSURE REGULATOR TO BE FAULTY. FURTHER INVESTIGATION LED TO REPLACEMENT OJan 15, 2003 · N95NA · Cessna 208BSDR SIMA200300601Connector · dirtyDFW - FLT 3873 - SHORTLY AFTER TAKEOFF CREW REPORTED A NR 1 BLEED LEAK WARNING. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS RETURNED TO DFW AND LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. A LEAK CHECK ON THE BLEED DUCTS FOUJan 3, 2003 · N504AE · Cndair CL6002C10SDR VNAA0211030Bleed Valve · failedDURING TAKE OFF, THE CREW RECEIVED A BLEED SHUT OFF VALVE CAS MESSAGE AND ABORTED TAKE OFF. WHILE THE AIRCRAFT WAS CLEARING THE RUNWAY THE MESSAGE CLEARED. THE CREW WAS THEN NOTIFIED THAT THERE WAS TWO PASSENGERS THAT WERE ON THE WRONG FLIGHT AND WANTED TO GNov 26, 2002 · N433JS · Dorner DO328100SDR VNAA0211029Bleed Valve · failedDURING TAKE OFF, THE CREW RECEIVED A BLEED SHUT OFF VALVE CAS MESSAGE AND ABORTED TAKE OFF. AFTER THE AIRCRAFT CLEARED THE RUNWAY, THE CREW CYCLED THE BLEED VALVE AND THE MESSAGE CLEARED. FLIGHT 9424 WAS THEN CLEARED FOR ANOTHER TAKE OFF ATTEMPT AND FLIGHT 9Nov 26, 2002 · N459PS · Dorner DO328100SDR CA021117001Duct · chafed(CAN) IN HANGAR, AT ENGINE INSTALLATION DURING RE CONNECTION OF THE INTERMEDIATE PRESSURE, (IP) DUCT INSIDE THE PYLON NR 3 AREA IT WAS NOTICED THAT THE FLEXIBLE SECTION OF THE PIPE SECTION FOR THE ANTI-ICE TAP-OFF OF THE IP DUCT WAS CHAFED THROUGH. DAMAGE OCCNov 16, 2002 · Lkheed 10113853SDR FL3A200200389Check Valve · inoperativeDURING CLIMB OUT, THE FLIGHT CREW NOTED AN ILLUMINATED WING/BODY OVERHEAT LIGHT WHICH WOULD NOT EXTINGUISH WHEN QUICK REFERENCE HANDBOOK ITEMS WERE ACCOMPLISHED. THE AIRCRAFT RETURNED TO THE DEPARTURE AIRPORT.MAINTENANCE REMOVED AND REPLACED THE START MANIFOLNov 16, 2002 · N118RW · Boeing 7372Y5SDR DL733021289Seal · tornAFTER LEVELING AT FL350 MASTER CAUTION W/OVERHEAD ON THE MASTER CAUTION PANEL ILL. PASS. O2 LIGHT ON THEOVERHEAD WASILL. CABIN ALT. WAS AT 15,000FEET. FA CONFIRMED MASKS HAD DROPPED. AUTO FAIL LIGHT WAS ILL. BUT NO ALT. ALERT HORN HADSOUNDED. ALT. CONT. Nov 1, 2002 · N947WP · Boeing 7373B7SDR C2XA02CL204Line · brokenCLE FLIGHT#3296 THE CREW REPORTED AFTER TAKEOFF THEY RECEIVED A #1 BLEED LEAK MESSAGE ON THE EICAS AND THE OVERHEAD PANEL.THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE #1 ENGINE DIRRERENTIAL PRESSURE SEOct 16, 2002 · N19554 · Emb EMB145LRSDR VJ32002F00077Pump · failedDURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM. SUSPECT PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP.Sep 20, 2002 · N5544A · Beech F33ASDR VJ32002F00076Pump · failedDURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM. SUSPECT PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP.Sep 20, 2002 · N8268T · Beech F33ASDR WVE2002F00017Duct · damagedDURING 300 HOUR INSPECTION, THE UPPER COWLING WAS REMOVED FOR MINOR INSPECTION. DAMAGE WAS NOTED TO THE UPPER BYPASS DUCT. DURING FURTHER INVESTIGATION, DAMAGE WAS ALSO NOTED ON THE RIGHT AND LEFT INNER CORE COWLS. TO BE EVALUATED BY MFG.Aug 19, 2002 · N229FX · Lear 60LEARSDR VJ32002F00049Pump · failedDURING GROUND RUN UP, OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT 800 RPM. RAN AIRCRAFT UP TO 1600 RPM BEFORE PRESSURE READ 4.5. CHECKED PRESSURE SYSTEM FOR LEAKS AND CHECKED REGULATOR ALL CHECKED WELL.Jul 3, 2002 · N5585Y · Beech F33ASDR ASOA02324Wire · brokenDURING CLIMB OUT, AT APPROXIMATELY 19,000 FEET, CAPTAIN REPORTED THAT DUCT LEAK WARNING WAS RECEIVED WITH CORRESPONDING LEFT DUCT LEAK LIGHT ILLUMINATING. CAPTAIN RAN CHECKLIST. WITH APU BLEED CLOSED THE WARNING INDICATION WENT OUT BRIEFLY THEN RETURNED. WJun 10, 2002 · N502AS · Emb EMB120ERSDR VJ32002F00045Pump · failedIN FLIGHT THE INSTRUMENT VACUUM SYSTEM FAIL. THE AIRCRAFT RETURNED TO MAINTENANCE AND AN INSPECTION OF THE SYSTEM FOUNDED THAT THE ROTOR HAD FROZEN UP AND THE SHAFT HAD SHEARED. PUMP WAS REMOVED AND A NEW PUMP INSTALLED. OPERATIONAL CHECK OF THE SYSTEM CHEMay 21, 2002 · N864AF · Grob G120ASDR VJ32002F00038Pump · failedIN FLIGHT, THE INSTRUMENT VACUUM SYSTEM FAILED. THE AIRCRAFT RETURNED TO MAINTENANCE AND AN INSPECTION OF THE SYSTEM FOUNDED THAT THE ROTOR HAD FROZEN UP AND THE SHAFT HAD SHEARED. PUMP WAS REMOVED AND A NEW PUMP INSTALLED. OPERATIONAL CHECK OF THE SYSTEM CMay 16, 2002 · N865AF · Grob G120ASDR VJ32002F00032Pump · shearedMETAL SHAFT SHEARED IN PUMP. REMOVED AND INSTALLED NEW PUMP, SYSTEM OPERATIONAL CHECKED NORMAL. PUMP SENT IN FOR WARRANTY.May 7, 2002 · N862AF · Grob G120ASDR DLM88020498Clamp · looseTAIL COMPT HIGH WARNING DURING CLIMBOUT CA FOUND RT CROSSBLEED VALVE CLAMP LEAKING TIGHTENED CLAMPLK CKS GOOD.May 2, 2002 · N928DL · Doug MD88SDR VJ32002F00028Pump · inoperativeLOW OUT PUT FROM PUMP TO AIRCRAFT, REMOVED PUMP AND INSTALLED NEW PUMP OPERATION WAS NORMAL. PUMP SENT IN FOR WARRANTY.Apr 26, 2002 · N1565A · Beech F33ASDR WVE2002F00008Sleeve · missingAIRCRAFT ARRIVED FOR 600/1200 INSPECTION WITH FAIL SAFE SLEEVE MISSING FROM BLEED AIR MANIFOLD, PN 6019060-8 AS SHOWN IN IPC 36-10-09. PROBABLE CAUSE: MECHANIC FAILED TO INSTALL SLEEVE, POSSIBLY DUE TO ERROR IN THE PROCEDURE FOR BLEED AIR COUPLING INSTALLATIApr 4, 2002 · N216FX · Lear 60LEARSDR 2002FA0000473Pump · inoperativeLOW OUT PUT FROM PUMP TO AIRCRAFT, REMOVED PUMP AND INSTALLED NEW PUMP, OPERATION WAS NORMAL. PUMP SENT IN FOR WARRANTY.Apr 2, 2002 · N5609S · Beech F33ASDR 2002FA0000478Pump · damagedMETAL SHAFT SHEARED IN PUMP. REMOVED AND INSTALLED NEW PUMP, SYSTEM OPERATIONAL CHECKED NORMAL. PUMP SENT IN FOR WARRANTY.Apr 1, 2002 · N861AF · Grob G102ASTIRSDR C1HA200293003Flow Valve · inoperativeDuring climbout, unable to pressurize cabin above 1 PSI diff. Action Taken: Removed and replaced right flow control valve. Ops and leak check good on ground IAW MM 36-10-02.Mar 22, 2002 · N293AS · Boeing 727212SDR ZKG2002F00001Cooler · crackedPRECOOLER CRACKED ON RIGHT ENGINE INBOARD AFT. THIS IS THE 2ND AC WITH THE SAME TROUBLE IN LESS THAN ONE WEEK.Mar 11, 2002 · N550CJ · Beech 1900CSDR 2002F00378Pilot Valve · inoperativeDURNG TAXI, LEFT DUCT PRESSURE FLUCTUATES. AIRCRAFT RETURNED TO GATES. MAINTENANCE REPLACED THE HIGH STAGE PILOT. (M)Feb 26, 2002 · N528AT · Boeing 75723NSDR 2002F00380Shutoff Valve · inoperativeDURING CRUISE EICAS MESSAGE LEFT ENGINE HIGH STAGE DISPLAYED, L HIGH STAGE LGT ILLUMINATED, DUCT PRESSURE NORMAL. AIRCRAFT LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED HPSOV PER MM 36-11-07. (M)Feb 19, 2002 · N519AT · Boeing 75723NSDR AALA20020061Duct · defectiveBOS - FLT 1229 - BOS-ORD - AFTER TAKEOFF, TAIL COMPARTMENT HIGH TEMP LIGHT ILLUMINATED. LANDED BOS WITHOUT INCIDENT. REPLACED RUPTURED DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Jan 19, 2002 · N474 · Doug DC982SDR VNAA0112017Bleed Valve · failedDURING TAKE OFF THE CREW RECEIVED A BLEED VALVE SHUTOFF FAIL MESSAGE AND ABORTED TAKE OFF. THE CREW CALLED MAINTENANCE CONTROL AND RESET THE SYSTEM. FLIGHT 4062 WAS CLEARED FOR ANOTHER TAKE OFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS.Dec 23, 2001 · N424JS · Dorner DO328100SDR VNAA0108020Valve · failedDURING CLIMB THE LEFT BLEED VALVE NEVER OPENED. AFTER TROUBLESHOOTING WITH MAINTENANCE CONTROL THE CREW WAS ASKED TO RETURN TO PIT. UPON ARRIVAL AT PIT, MAINTENANCE INSPECTED AND REPLACED THE FLOW CONTROL SHUT OFF VALVE IN ACCORDANCE WITH DORNIER MAINTENANCEAug 30, 2001 · N438JS · Dorner DO328100SDR C2XA01CL193Hose · blownCLE FLIGHT#3860 THE CREW SHUT DOWN THE #1 ENGINE ON LANDING INTO CLEVELAND DUE TO A #1 ENGINE BLEED LEAK WARNING AND PRESSURIZATION PROBLEM.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND THE BLEED DUCT HOSE HAD BLOWN OFF BETWEEN TAug 18, 2001 · N17928 · Emb EMB145ERSDR COMA0160423Valve · leakingR/H 14TH STAGE DUCT WARNING MESSAGE AND ANTI-ICE DUCT WARNING.FOUND 14TH STAGE BLEED VALVE LEAKING, REMOVED AND REINISTALLED VALVE.Jun 28, 2001 · N982CA · Cndair CL6002B19SDR DL738010957Controller · failedIRR/ NBR 1 ENG BLEED TRIP OFF LIGHT ILLUMINATED AS A/C LEVELED OF FL350. REPLACED BLEED AIR CONTROLLERJun 12, 2001 · N394DA · Boeing 737832SDR AALA20011198ClampDFW - FLT 552 - EN ROUTE DFW-PIT, DETECTED TAIL HIGH TEMPERATURE LIGHT ILLUMINATE IN COCKPIT. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. RE-SECURED CLAMP AT LEFT SIDE ACY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Jun 11, 2001 · N70401 · Doug DC982SDR AALA20011182Sensor · defectiveDFW - FLT 1612 - EN ROUTE DFW-LIT, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED TAIL COMPARTMENT HIGH TEMPERATURE SENSORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)May 30, 2001 · N477AA · Doug DC982SDR AALA20011183Clamp · defectiveLAX - FLT 335 - EN ROUTE LAX-SJD - SHORTLY AFTER TAKEOFF TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. RETURNED LAX AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE AUGMENTATION VALVE CLAMP. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERMay 30, 2001 · N228AA · Doug DC982SDR SIMA200114809O-Ring · wornORD - FLT 4112 - CREW REPORTED ENGINE TWO BLEED LEAK LIGHT CAME ON AFTER TAKEOFF. CREW RETURNED AIRCRAFT TO ORD. MAINTENANCE REPLACED O-RINGS AT COUPLING UNDER AFT PASSENGER SEAT NEAR THE LAVATORY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (May 28, 2001 · N609AE · Emb EMB145LRSDR AALA20011125ClampDFW - FLT 1580 - EN ROUTE DFW-DCA, TAIL HIGH TEMP LIGHT ILLUMINATED. RETURNED DFW LANDED WITHOUT INCIDENT. REPOSITIONED CLAMP ON LEFT PACK ANTI-ICE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)May 23, 2001 · N465A · Doug DC982SDR AAL20011035DuctORD - FLT 1666 - EN ROUTE ORD-ALB, TAIL COMPARTMENT HIGH TEMP LIGHT ILLUMINATED DURING CLIMB-OUT AT 24,000 FEET. RETURNED AND LANDED ORD WITHOUT INCIDENT. REPLACED UPPER RETURN SYSTEM AIR CONDITIONING DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)May 15, 2001 · N572AA · Doug DC983SDR DL76L010540Engine · malfunctionedON T/O GOT RT HP BLEED AND FOLLOWED POM. RETURNED TO CVG. REPLACED NBR 2 ENG HPSO VALVE PER MM 36-11-07-4-03 NO FURTHER FAULTS.Apr 2, 2001 · N178DN · Boeing 767332SDR DHL2001366008Control Box · failedDURING BEFORE T/O CHECKLIST, PRESSED MWP RECALL BUTTON. PNEU LIGHT ILLUMINATED WITH NO CHIME, ALL SYS NORMAL. REMOVED AND REPLACED PRESS SEQ BOX IAW 21-31-00, OPS NORMAL.Feb 6, 2001 · N366DH · Airbus A300B4203SDR DHL2001366007Controller · malfunctionedRETURNED TO BLOCK ON TAXI OUT. PNEUMATIC LIGHT ON MWP AND CHIME SOUNDED. ALL SYSTEMS APPEAR NORMAL. LIGHT WOULD NOT EXTINGUISH. SWAPPED PNEUMATIC CONTROLLERS FOR TROUBLESHOOTING. PERFORMED BITE CHECK. BOTH CHECK NORMAL IAW 36-10-01.Feb 6, 2001 · N366DH · Airbus A300B4203SDR 2001UALA00082Smoke · detectedSMOKE IN THE COCKPIT. *S/D* THREE WIRE SOCKETS IN CONNECTOR D96 BROKE OFF AND SHORTED TOGETHER. REPLACED THE SOCKETS.Feb 5, 2001 · N991UA · Boeing 737291SDR C2XA00CL099Duct · crackedCLE: CREW REPORTED NR 1 BLEED LEAK INDICATION AFTER TAKEOFF IN CLEVELAND. A/C RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND THE BLEED DUCT CRACKED ON LEFT SIDE IN THE AFT AVIONICS COMPARTMENT. DUCT WAS REPLACED IAW 36-12-02 & 36-11-09.Nov 27, 2000 · N16502 · Emb EMB135ERSDR VNAA0011006Bleed Valve · failedDAY - FLT 4026 - AFTER TAKING THE RUNWAY AND AS POWER WAS ADVANCED THE PUT BLEED SHUTOFF VALVE FAILED. MAINTENANCE REPLACED THE RIGHT LP BLEED VALVE. THE AIRCRAFT DEPARTED WITH FURTHER INCIDENTS. (M)Nov 10, 2000 · N436JS · Dorner DO328100SDR HALA0000341Controller · failedPDX - FLT 25 - NR 3 MANIFOLD FAIL LIGHT CAME ON DURING FLIGHT. FOLLOWED CHECKLIST AND TURNED OFF NR 3 PNEU AND NR 3 PACK. PRESSURIZED PNEU SYSTEM 3. INSPECTED ALL DUCTING FOR LEAKS. NONE FOUND. INSPECTED WIRING TO DETECTORS IN WING, RES SWITCH AND LOOPS. Oct 11, 2000 · N125AA · Doug DC1010
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