JASC 2130
Service difficulty reports · 3,458
Reports filed under 2130 · Cabin Pressure Control 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 = '2130' 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 = '2130' 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 UIEA2018123102971Status Message · false activationCABIN ALT AUTO #2 STATUS MESSAGE(<P>BITE CHECK CABIN ALT 2 CONTROLLER IAW B767 AMM 21-31-00, BITE & OPS CHECKED GOOD</P>)SDR AALA2018123189009Clamp · brokenPASSING FL280 IN CLIMB, THE CABIN ALTITUDE ALERT ACTIVATED, CLIMBING THROUGH 9000 FT, STARTED DESCENT AS CABIN REACHED 10,000 FT. DECLARED EMERGENCY FOR DESCENT. CREW VERBALLY REPORTED THAT THEIR CABIN PRESSURE PAGE SHOWED SKIN AIR VALVE, EXTRACT AND SAFETSDR ASAA2018122437508Warning Light · false activationAUTO FAIL AND ALTN LIGHTS ARE ILLUMINATED ON PRESSURIZATION PANEL WITH AUTO POSITION SELECTED. GROUNDED - YES. MOVED PRESSURIZATION MODE SELECTOR TO "MAN" AND BACK TO "AUTO", LIGHT REMAINS EXTINGUISHED. THIS CORRECTS FAULT.SDR ASAA2018122617545Control Panel · malfunctionedFOLLOW-UP TO HISTORY OF PRESSURIZATION PANEL (P5-6) NOT DIMMING ISSUES. GROUNDED - YES. ENGINEERING REQUEST - REMOVED/REPLACED CABIN PRESSURE CONTROL MODULE REF B737-900 AMM 21-31-02. ALL REQUIRED TESTS PER SAME MM OPS NML. GROUND VERIFICATION TESTS GOOD REF SSDR GTIA2018122103034Cabin Pressure · overpressuredCAB PR EXCESS CAB ALT-PER TSM 21-31-00-810-806-A. OPS TEST WERE PERFORMED IAW AMM 21-31-00-710-002-A OPS TEST OF PRESSURE CONTROL & MONITORING, AMM 21-31-00-710-003-A OPS TEST OF MAN MODE SELC & MAN MODE PRESS CONT & FUNC TEST OF MAN MODE CAB ALT/FLOW VALVE POSDR MASA2018121911599Pseu · inoperativeMIS-RTF/EMER DECLARED CABIN ALT CAUTION/ALT WARN. REPLACED PSEU.SDR ASAA2018122087477Warning Light · false activationPRESSURIZATION AUTO FAIL AMBER LIGHT ILLUMINATED. GROUNDED - YES. PERFORMED AUTO FAIL LIGHT "ON" FAULT ISOLATION REF B737-800 FIM 21-31 TASK 827, C/W ETOPS GROUND SYSTEM OPERATIONAL VERIFICATION PERFORMED ON BOTH #1 & 2 CONTROLLERS, NO FAULTS NOTED.SDR UIEA2018121702858Warning System · false activationCABIN AUTO INOP EICAS MESSAGE ILLUMINATED DURING CRUISE, FOLLOWED QRH PROCEDURE. ACCOMPLISHED CABIN PRESS CONTROLLER BITE TEST PROCEDURE FIM 21-31 FT 803, MSG CLEARED. OPS CHECK NORMAL.SDR ANCF201812271501Warning Light · false activationDURING INITIAL CLIMB, ADV ON CABIN PRESS CAME ON, SYS RESET WAS PERFORMED SUCCESFULLY. THEN JUST PRIOR TO T.O.D, ADV ON CABIN PRESS MAME ON AGAIN, SYS RESET WAS PERFORMED AGAIN, BUT EXCESS CABIN ALT ECAM CAME ON. EMERG DESCENT WAS PERFORMED // CORRECTIVE ACTIOSDR ASAA2018121527402Warning System · false activationCABIN DIFFERENTIAL MASTER WARNING AT GATE GROUNDED - YES. PERFORMED CABIN PRESS CONTROLLER 1 AND 2 TEST. TEST OK. PERFORMED AMM 21-63-00-05 AND AMM 31-32-00-860-002-A. BOTH TEST OK.SDR Y2PA201812184048Unknown · malfunctionedCREW REPORTED – AIRCRAFT DECOMPRESSED AND LOST ALL CABIN PRESSURE. CREW ON O2. CABIN ALTITUDE CLIMBED TO 15,000 FEET. DECLARED EMERGENCY/RETURNED TO KYIP. USA JET MAINTENANCE AT KYIP PRESSURIZED AIRCRAFT I/A/W DA-20 MM 21-30-05. OPS CHECK WAS GOOD. NO DEFSDR SIMA20181212001Outflow Valve · malfunctionedA/C DID NOT PRESSURIZATION / PRESSURIZE. RETURNED TO DFW. NO EICAS ALERTS, LANDED AT APPROX 39,000 LBS. DEFERRED AUTOMATIC PRESSURIZATION MODE .C/W MAINT ACTION. PERFORMED MANUAL PRESSURIZATION & FOUND WORKING PROPERLY IAW MM 21-31-00. C/W "M" PROCEDURES AND SDR SIMA20181212003Not Reported · malfunctionedAIRCRAFT WOULD NOT PRESSURIZE AFTER TAKE OFF. ON DESCENT COMING THROUGH 10,000 FEET AIRCRAFT APPEARED TO BEGIN PRESSURIZING NORMALLY. PERFORMED FUNCTIONAL TEST OF PRESSURIZATION CONTROL SYSTEM IN AUTOMATIC MODE IAW AMM 21-31-00-700-802-A. FUNCTIONAL TEST GOODSDR ASAA201812117307Light · inoperativePRESSURIZATION PANEL BACKLIGHTING INOP, OUTFLOW VALVE INDICATOR INOP, LCP ALTITUDE DISPLAYS DO NOT DIM. GROUNDED - YES. CYCLED ELEC PWR PER B737-800 AMM 20-60-99 AND ALL INDICATIONS RETURNED TO NML. BACKGROUND / LCD DISPLAYS AND OUTFLOW VALVE INDICATE AND OPS SDR CALA2018121102552Control Module · failedAUTO PRESSIZATION FAILED DUE TO SWITCH REPLACED CABIN PRESSURE CONTROL MODULE IAW AMM 21-31-02-400-801 ADD EMP:U029666 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1950071 SN OFF 5515 PANEL, PRESS, C OFF 29-2131-9-0006 5515 ON 29-2131-9-0006 1738SDR ASAA2018121197306Light · malfunctionedAT TOP OF DESCENT THE PRESSURIZATION PANEL LIGHTING WENT DARK AND THE NUMBERS BECAME EXTREMELY DIM AND HARD TO READ. GROUNDED - YES. PERFORMED B737-900 FIM 21-31 TASK 803. AFTER RESET OF BREAKERS LIGHTING RETURNED TO NORMAL AND NO OTHER DEFECTS NOTED AT THIS TSDR UIEA2018121202825Status Message · false activationCABIN AU AUB STATUS MSG DECENDING THROUGH FL 200. PERFORMED CK ON CABIN PRESS AMM 21-32-00 AC MOTOR FAULT RESET, NO FAULT. STATUS MSG CLEARED.SDR IEYAN201812100001Unknown · pressure lossLOUD 'BANG FOLLOWED BY PRESSURIZATION LOSS AT 3000 - 4000 FPM. NO ASSOCIATED ANNUNCIATOR LIGHTS. OCCURRED AT 35,000'. AIRCRAFT WILL BE FERRIED TO GULFSTREAM DALLAS FOR REPAIR.SDR UIEA2018120602787Warning System · false activationCABIN ALT AUTO 2 STATUS MESSAGE. PERFORMED BITE TEST OF AUTO CABIN PRESSURE CONTROLLERS IAW AMM 21-31-00. BITE TEST GOOD, NO FURTHER DEFECTS NOTED. MSG CLEARED.SDR DALA2018120306970Regulator Valve · malfunctionedSHIP 951- PRESS - FLOW LIGHT IN CRUISE. DURING DESCENT PRESSURIZATION COULD NOT KEEP UP. AT 10,000 FEET AIRCRAFT WAS COMPLETELY DEPRESSURIZED UNTIL LANDING. CORRECTIVE ACTION: REPLACED LEFT PRESSURE REGULATING VALVE AND LEFT A/C PILOT PRESSURE REGULATOR. (LP48SDR ASAA2018120397169Warning Light · false activationDURING TAXI IN AUTOFAIL/ALTN LIGHT ILLUMINATED. GROUNDED - YES. ACCOMPLISHED DCPC BITE PROCEDURE REF B737-900 FIM 21-31 TASK 801. NO. 1 DCPC SHOWS 1 FAULT CODE 011 OFV LRU FAULT. PERFORMED FAULT ISOLATION REF B737-900 FIM 21-31 TASK 802, OPS CK NML.SDR DJFA201812210001Dcu · malfunctioned"PRESN AUTO FAIL" CAS MESSAGE ILLUMINATED IN FLIGHT ALONG WITH "AP FAIL" AND "YD FAIL". R&R GSD41 1 (DCU1). OPS CHECK GOOD. MESSAGE CLEARED.SDR ASAA2018112107022Control Panel · dimPRESSURIZATION PANEL DISPLAY LIGHTS VERY DIM. GROUNDED - YES. CYCLED SYSTEM POWER. DISPLAYS RETURNED TO NORMAL #1 CONTROLLER LOGGED 016, SEL PANEL LRU FAIL. PRESSURIZATION CONTROLLER BITE CK NORMAL. REF B737-800 FIM 21-31 TASK 801.SDR ASAA2018111976896Annunciator · false indicationRESIDUAL CABIN PRESSURE AT GATE WITH APU BLEED ON. DOOR 1R ANNUNICIATED GROUNDED - YES. PFR SHOWS NO FAILURE OR WARNING. PER TSM 21-30-00-810-845-A PERFORMED OPS TEST OF CPC 1 / 2. TEST OK. NO FAULTS NOTED AT THIS TIMESDR AALA201811139027Duct · disconnectedAIRCRAFT WOULD NOT MAINTAIN PRESSURE. INTIALLY PACK PRESSURE OFF WITH A PACK INOPERATIVE LIGHT. FOLLOWED QRH PROCEDURES, DECENDED TO 31,000 FEET, CABIN ALTITUDE WAS SLOWLY CLIMBING. CONTINUED DECENT TO 24,000 FEET, COULD NOT CONTROL THE CABIN ALTITUDE, TRIESDR UIEA2018111102565Warning System · activatedCABIN ALT AUTO NR 1 STATUS MSG. PERFORMED CABIN PRESS CONTROLLER BITE TEST AS PER FIM PROCEDURE 21-31-00 FIG 103 TEST PASS MSG CLEARED.SDR FXGA2019031200000Unknown · malfunctionedLOSS OF PRESSURIZATION @ FL250 RIGHT PACK WAS DMI. FOLLOWED QRH EMERGENCY CHECK LIST INSTRUCTIONS TO 10,000 FEET. DESCENDED PER QRH TO 10,000 FEET.SDR UIEA2018110902555Warning System · false activationSTATUS MSG CABIN ALT AUTO 2 (OUTFLOW VALVE DID NOT OPEN ON LANDING). PERFORMED BITE ON CABIN PRESSURE CONTROLLER AS PER AMM 21-31-02, TEST PASSED NO MESSAGES.SDR I5EA2018111202Warning Horn · false activationDISCREPANCY: CABIN WARNING HORN SOUNDED AT FL370. PERFORMED EMERGENCY DESCENT TO FL290. CORRECTIVE ACTIONS: PERFORMED OPS CHECK OF CABIN PRESSURE CONTROL PANEL SYSTEMS, OPS CHECK GOOD IAW BOEING AMM 21-33-00.SDR JJBA201811075001Clamp · leakingLOST PRESSURIZATION INFLIGHT PACK 1&2 VALVE FAIL MESSAGE DISPLAYED BLEED 1 OVERTEMP EICAS MESSAGE DISPLAYED TEMPORARILY TROUBLESHOT PACK 1 VALVE, FOUND NUMEROUS CLAMPS LEAKING. TIGHTEN CLAMPS AS REQUIRED NO FURTHER LEAKS REF. TROUBLESHOT BLEED 1 OVERTEMP - FOUSDR AALA2018110659051Pressure Switch · failedCABIN PRESSURE LIGHT FLASHED WHEN DOOR DISARMED. CABIN DEPRESSURIZED WITH COCKPIT WINDOW. REPLACED PRESSURE SWITCH. ACCOMPLISHED OPERATIONS CHECK OF THE SYSTEM PER AMM 52-73-12-A, AND LOW RANGE LEAK CHECK IAW AMM 34-21-00.SDR ASAA2018110126708Control Module · intermittentFLT ALT SELECTOR KNOB INTERMITTENTLY SELECTS DESIRED ALTITUDE. GROUNDED - YES. REMOVED AND REPLACED CABIN PRESSURE CONTROL MODULE, OPS CK GOOD REF B737-800 AMM 21-31-02.SDR R61A201811011106Switch · pilot errorCABIN ALTITUDE WAS HIGH ON EICAS. DECLARED AN EMERGENCY, AND RETURNED TO FIELD, LANDED WITHOUT INCIDENT. FOUND PRESSURIZATION MODE IN MANUAL MODE. SWAPPED TO AUTO MODE. PERFORMED CPCS CONTROLLER CHANNELS FUNCTIONAL TEST IAW AMM 21-30-00, OPS CHECK GOOD. NOT SDR UIEA2018102702381Control Unit · malfunctionedCABIN ALTITUDE AUTO 1 STATUS MESSAGE. REMOVED AND REPLACED THE NR 1 AUTO PRESSURE UNIT IAW AMM 23-31-00. OPS CHECKED OKSDR K11A2018102900002Control Panel · faultyON DEPATURE AIRCRAFT WOULD NOT PRESSURIZE, CABIN WOULD NOT HOLD PRESSURE IN AUTO OR MANUAL MODES, RETURNED TO KPHX FOR UNSCHEDULED LANDING.SDR I5EA2018102600011Unknown · malfunctionedDISCREPANCY: AIRCRAFT WILL NOT PRESSURIZE AUTO/STANDBY OR MANUAL CORRECTIVE ACTION: PERFORMED DETAILS VISUAL INSP OF CABIN OUTFLOW VALVE, PRESSURE CONTROLLER AND RACK CONNECTORS. VERIFIED AIR/GROUND LOGIC AND PERFORMED SATISFACTORY PRESSURIZATION OPS CHECKSDR ASAA2018101726508Warning System · false activationAT CRUISE THE AUTO FAIL AND ALTN LIGHTS ILLUMINATED COMPLIED WITH QRH. NORMAL OPS. GROUNDED - YES. FAULT HISTORY SHOWS OFV LRU FAIL ON NR 2 CONTROLLER. PERFORMED SYSTEM TESTS ON BOTH CONTROLLERS- SYS TESTS OKAY REF FIM 21-31-TASK 801.SDR ASAA2018101726507Warning System · false activationIN CRUISE FLIGHT AT FL 350, PRESSURIZATION "AUTO FAIL" AND "ALTN" LIGHTS ILLUMINATED. ACCOMPLISHED CHECKLIST. OPS OK WITH ALTN MODE. GROUNDED - YES. ACCOMPLISHED FIM 21-31 TASK 827. AUTO FAIL RECOVERED. REPAIR CONFIRMATION TEST GOOD REF FIM 21-31 TASK 801 DCPCSDR ASAA2018101626509Control Module · failedPRESSURIZATION MODE CONTROL LAND ALT DIGITS FAILING. GROUNDED - YES. REMOVED AND REPLACED CABIN PRESSURE CONTROL MODULE, CABIN PRESSURE CONTROL SYSTEM OPS CK GOOD REF AMM TASK 21-31-00.SDR UIEA2018101102246Status Message · false activationCABIN ALT AUTO 1 STATUS MESSAGE. PERFORMED TEST OF CABIN ALT AUTO 1 IAW AMM 21-31-00, OPS CHECK GOOD AT THIS TIME.SDR ASAA2018101026428Control Module · faultyIN FLIGHT, NOTICED THAT THE INDICATOR LIGHTS IN THE PRESSURIZATION CONTROL PANEL WERE ALL BLANK. PRESSURIZATION WORKED NORMAL- NO ISSUES. GROUNDED - YES. DIVERSION TIME 66 MINUTES. REPLACED CABIN PRESS CONT MODULE REF AMM 21-31-02-400-801. OPS CK OK OF PRESS SSDR ASAA2018101026427Control Module · defectiveFLT ALT WINDOW IS INTERMITTENT. NOT ABLE TO CHANGE DISPLAYED WITH FLIGHT ALT KNOB. GROUNDED - YES. REMOVED AND REPLACED CABIN PRESSURE CONTROL MODULE PER AMM 21-31-02. OPS CHECKED NORMAL.SDR QXEA2018100900362Unknown · malfunctionedDURING CLIMBOUT AT APPROXIMATELY 2000 FEET MSL THERE WAS A LOUD THUMP AND OUR EARS POPPED. DURING CLIMBOUT THE PLANE WOULD NOT PRESSURIZE. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. PLACED PRESSURIZATION SYSTEM ON MEL 21-30-5A. RETURNED TO SESDR GTIA2018100802879Unknown · malfunctionedA/C NOT PRESSURING NO ECAM MESSAGES ON SYS DISPLAY-PERFORMED ENGINE RUN AND PRESSURING SYS. IAW AMM 05-53-00. OPS CHECK NORMAL. A/C OK FOR SERVICESDR ASAA2018100826387Unknown · malfunctionedPRESSURIZATION CONTROL PANEL AUTO DISPLAY BLANK. GROUNDED - YES. RESET A/C POWER ACCOMPLISHED FIM 21-31 TASK 803 NO DEFECTS NOTED. PERFORMED (DCPC) BITE CHECK, SYSTEM OK NO FAULTS GENERATED REF FIM 21-31 TASK 801.SDR ASAA2018100226357Warning System · false activationPRESSURIZATION "AUTO FAIL" ILLUMINATED AFTER LANDING. GROUNDED - YES. RESET AUTO FAIL REF FIM TASK 21-31-827 & BITE CK OF NR 1 & NR 2 DCPC OK REF. FIM TASK 21-31 TSK 801. OPS CK OK.SDR ASAA2018092426207Control Module · defectiveCABIN PRESSURE PANEL LIGHTS PULSE IT IS WORST IN DIM SETTING. GROUNDED - YES. REMOVED AND REPLACED CABIN PRESSURE CONTROL SELECTOR MODULE REF AMM 21-31-02. CABIN PRESSURIZATION OPERATIONAL GROUND TEST AND MANUAL MODE TEST CHECKED NORMAL REF AMM 21-31-00.SDR AALA201809219014Warning Light · false activationR2 DOOR CABIN PRESSURE LIGHT WAS FLASHING ON DESCENT. PERFORMED AN OPERATIONAL TEST OF CABIN OVERPRESSURE WARNING SYSTEM IAW 52-73-00. OPS CHECKED GOOD.SDR FDEA201809202632Warning System · activatedALT FL350 CABIN ALTITUDE LEVEL 3 ALERT. FASE 1S TO QRH. REF FIM 21-33-00-2 FIG 103 CHECKED BOTH CPC'S FOR BLOCKAGE AND NONE FOUND. CFDS FAULTS ACC1 WITH PK 1 RAD ACT IN LAST LEG BUT NO CURENT FAULTS. DEFERED PACK NR 1 RAM AIR ACTUATOR WRI 21-52-1583. PERFORMESDR UIEA2018091801993Indication Sys · faultyDESENDING THRU FL200 WE SAW THE CABIN ALT INDICATOR INDICATED 0, DIFF PREESSURE AND RATE APPEARED NORMAL. PERFORMED OPS CHECK ON CABIN ALT PRESS SYSTEM IAW AMM 21-31-00. OPS CHECK GOOD AT THIS TIME.
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