JASC 2697
Service difficulty reports · 1,399
Reports filed under 2697 · Fire Protection System Wiring, 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 = '2697' 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 = '2697' 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 UALA2013042302806Wire · shortedSTATUS MESSAGE, OVERHEAT CIRCUIT R1. ISOLATED NR 2 FIRE HARNESS. MEGGERED WIRE SHORTED TO GROUND. INSTALLED WIRES, NO MESSAGES. REPLACED WIRES W0656-1001R-16 AND W0656-1002R-16 IAW 26-11-21 SWPM 20-10-13.SDR FDEA201304200873Wire · damagedSHORTLY AFTER STARTING APU AUTO SHUTDOWN WITH FIRE HANDLE ILLUMINATED. NO AURAL WARNING. NO INDICATION OF ACTUAL FIRE. REPAIRED WIRING INSULATION IAW SWPM 20-10-01. OPS AND LEAK CHECKED GOOD. FIRE WARNING TEST OF APU GOOD.SDR ASAA2013041794526Connector · looseFWD CARGO FIRE LOOP A INOPERATIVE. FOUND FWD NR 1 SMOKE DETECTOR CONNECTOR LOOSE. RESECURED CONNECTOR, ALL OPS NORMAL. REF MM 28-16-00, 28-16-02.SDR UALA2013041502542Contact · dirtyAFT CARGO FIRE EXTINGUISHER ARM LIGHT DOES NOT ILLUMINATE DURING FIRE TEST. CLEANED AND RESEATED CONTACTS ON ARM LIGHT. OPS TESTED NORMAL.SDR UALA2013041202526Wire · damagedLEFT ENGINE FIRE LOOP 2 STATUS MESSAGE INTERMITTENTLY IN FLT. FOUND FIRE LOOP WIRES INSULATION AND BROKEN STRANDS DEFECTIVE. WIRE REPAIRED IAW MM 71-51-00. GROUND FUNCTIONAL TESTED GOOD.SDR UALA2013041202513Connector · contaminatedAPU IS INOPERATIVE DUE TO NO FIRE PROTECTION. FOUND CONNECTOR ON BOTTLE OILY. CLEANED CONNECTOR AND OPS CHECKED OK.SDR CA130412010Wire · chafed(CAN) IN THE MIDDLE OF COMPLETING TASKS FOR THE APPROACH, THE AMBER EXTINGUISHER DISCHARGE LIGHT BECAME STEADILY ILLUMINATED. IN THINKING IT WAS A ZONE FIRE LIGHT, ACTIONS WERE TAKEN TO COMPLETE THE ENGINE FIRE AFTER BSEC MEMORY ITEMS. THE ENGINE WAS SHUTDOWNSDR UALA2013041202509Connector · faultedWHEEL WELL FIRE LIGHT FAILED TO ILLUMINATE DURING TEST. RESEATED CONNECTOR M691, GROUND CHECKED OK IAW MM 26-17-00SDR FDEA201304090746Wire Harness · shortedLEVEL 3, FIRE WARNING NR 3 IN FLIGHT. USED BOTH FIRE EXTINGUISHING BOTTLES. LANDED UNEVENTFULLY. FOUND PYLON LOOP A HARNESS CREATING THE HIGH RESISTANCE READING. R & R WIRE HARNESS. ENGINE RUN OPS CHECKED NORMAL, RAN ENGINE TO HIGH POWER IAW JRH APROXIMASDR UALA2013032802003Connector · defectiveENGINE 1 FIRE LOOP B FAULT DISPLAYED. T/S PER TSM 26-12-00-810 804-A AND ASM 26-12-01 FOUND PUSHED BACK PIN ON CONNECTOR 4001WD2-A PIN A (BLUE WIRE) ATTEMPTED TO LOCK PIN IN BUT PIN WILL NOT LOCK IN PLACE NEEDS NEW CONNECTOR FIN 4001WD2-A.SDR CALA2013032900178Terminal · damagedFIRE PANEL FAULT LIGHT CAME ON DURING FLIGHT AND THEN WENT OUT. LIGHT CAME BACK ON AND NOW INDICATES "A" LOOP FAILURE ON NR 2 ENG. CONFIRMED NR 4 AFT LOOP A AND B TERM FAULTS. WIRES GENTLY PULLED FROM TERM BARREL. REPLACED THREE TERMINAL ENDS IAW AMM 26-11-SDR UALA2013032501839Smoke Detector · miswiredFOUND CB N8 AT P11 POPPED WHEN FIRST CLASS LAV DOOR LATCH SWITCH LOCKED. CONNECTOR D42 CHECKED NO DAMAGE FOUND. FOUND SMOKE DETECTOR WIRES IN FWD LAVATORY INSTALLED INCORRECTLY. INSTALLED AND SECURED WIRES REF WDM 26-14-11, OPS CHECKED GOOD.SDR R61A201303200299Connector · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE ENGINE NUMBER TWO FIRE BOTTLE SQUIB CONNECTOR CORRODED. MAINTENANCE REMOVED AND REPLACED THE CONNECTOR IAW EMB 170 SWPM 20-40. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR CA130208001Connector · failed(CAN) ANTI-ICE DUCT WARNING MESSAGE, WHILE ON DOWNWIND TO LANDING. SHORTLY AFTER, THE MESSAGE CHANGED TO, ANTI-ICE DUCT CAUTION MESSAGE AND THE ANTI-ICE PAGE SHOWED WING HEAT OFF. THE CREW REPORTED THAT THE ACFT WAS FLYING IN MODERATE TO SEVERE ICING CONDITIOSDR AALA20130129017Connector · faultyTPA - INFLIGHT DFW-SJU. CREW REPORTED SMOKE IN COCKPIT AND CABIN, FOLLOWED BY FORWARD EQUIPMENT OVERHEAT MESSAGE. EMERGENCY DECLARED FLIGHT DIVERTED TPA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CONNECTOR AT FLOW SENSOR D1574. SYSTESDR SWIA201332725Connector · looseGALLEY SMOKE ALARM IS ANNUNCIATING WITH NO VISABLE SIGNS OF SMOKE OR FLAMES PRESENT. (FLT 7386) FOUND CONNECTOR ON LAV SMOKE DETECTOR WAS LOOSE. RE-SECURED CONNECTOR. OPS CHECKS GOOD.SDR FDEA201301190148Wire Harness · damagedFORTY MINUTES INTO FLIGHT RECEIVED A LEVEL ONE "FIRE DET 1 FAULT" ALERT IT WAS FOLLOWED BY INTERMITTENT LEVEL THREE NR 1 FIRE ALERT AND "FIRE DET 1 FAIL" ALERTS. DECLARED EMERGENCY AND RETURNED TO DEPARTURE. CFDS SHOWS NOT CURRENT FAULTS FOR FDCU 1. LEG 1SDR UALA2013011700307Wire Harness · pinchedNR 2 ENGINE FIRE LOOP B FAULT. FOUND WIRES AT 10 O'CLOCK POSITION PINCHED UNDER FWD SIDE OF PRSOV. WIRE HARNESS FROM 4001WD 2 CORE DETECTOR TO PYLON, SHIELD AND BLUE WIRE DAMAGED. FOUND SECOND WIRE HAS HEAT DAMAGE AND CHAFED. NEED TO IDENTIFY AND MEGGER TOSDR UHLA2013011500086Connector · reversedENGINE FIRE EXTINGUISHING BOTTLE A CONNECTOR P0749 AND CONNECTOR P0751 ARE INSTALLED IN REVERSE PER AMM 26-21-03 FIGURE 401. INSTALLED FIRE BOTTLE WITH CORRECTORS, FIRE PROTECTION SYSTEM TESTING/CHECKING PERFORMED IAW AMM 26-00-0.SDR CA130125004Wire · damaged(CAN) BOTH NR 4 ENGINE FIRE DETECTION ELEMENTS FOUND TO HAVE CHAFE DAMAGE FROM CONTACT WITH AIRFRAME STRUCTURE CAUSING ACTIVATION OF THE FIRE WARNING. BOTH DETECTION ELEMENTS REPLACED, CHECKED SERVICEABLE.SDR UALA2013011400230Wire Harness · chafedLEFT ENGINE OVERHEAT DETECTION CIRCUIT 2 FAILED. MEASURED LEFT ENGINE LOOP 2 INDIVIDUAL ELEMENT CORE RESISTANCE AND MEGGER RESISTANCE TO GROUND, FOUND TO BE WITHIN LIMITS OF FIMMAN 26-11-810. FOUND CHAFED WIRE HARNESS AT RIGHT SIDE ENGINE, 2 FT FWD OF 'LWR ASDR UALA2013011400231Wire Harness · chafedNR 2 ENGINE FIRE DETECTION SYSTEM LOOP 2 FAILED. FOUND CHAFED WIRE HARNESS BETWEEN LWR FWD AND LWR AFT LOOPS. REPLACED FIRE LOOP HARNESS AND FIRE TESTED OK.SDR UALA2013010700077Wire Harness · shortedCREW HAD NR 2 ENGINE FIRE WARNING ON SHUTDOWN. FOUND SHORT BETWEEN BOTH LOOPS IN WIRE HARNESS W0656-1001R AND W0656-1002R REFERENCE WDM 26-11-21 PG 1 SHEET 2. REMOVED OLD HARNESS. NEW ON AOG (K0390). NEW HARNESS NEEDS TO BE INSTALLED AND TESTED. REPLACED SDR HSYA201212310001Wire · chafedON SHORT FINAL AT APPROX 1000 FT, CREW HEARD THE FIRE DETECTION WARNING HORN CHIRP AND THE FIRE DETECTION WARNING LIGHT WAS FLICKERING INTERMITTENTLY. THE CREW ADVISED ALL ENGINE PARAMETERS INDICATED NORMALLY AND NO EVIDENCE OF FIRE WAS DETECTED. NO EMERGENSDR HSYA20122412Wire · out of positionAFTER TAKEOFF, THE FIRE DETECTION WARNING HORN SOUNDED AND THE FIRE DETECTION WARNING LIGHT ILLUMINATED. CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE, LANDING AT 17:13 ZULU WITHOUT FURTHER INCIDENT. CREW REPORTED THAT THERE WAS NO INDICATION OF FIRE ASDR QMLA2012122212197Connector · dirtyDURING ENGINE STARTING CHECKS, ENGINE FIRE LIGHT ILLUMINATED. SHUTDOWN ACFT, NO SIGN OF FIRE IN ENGINE COMPARTMENT. ENGINE FIRE LIGHT REMAINED ILUMMINATED. INSPECTED AND CLEANED THE ACCESSIBLE ELECTRICAL CONNECTOR IN THE FIRE DECTECTION SYSTEM. AFTER CLEASDR UALA2012122107317Wire Harness · chafedNR 2 ENGINE FIRELOOP HARNESS IS CHAFED AT 3 O'CLOCK POS BY HEAT SHIELD. CLAMP REMOVED. REPLACED FIRE LOOP WIRING HARNESS FROM M26004 (A1-B2) TO M26005 (A1-B2).SDR V2JA20121218001Connector · dirtyRT ENGINE FIRE LIGHT ON SHORT FINAL. AFTER LANDING, SHUTDOWN ENGINE AND DISCHARGED FIRE BOTTLE. CONNECTOR ON FIRE LOOP DIRTY.SDR UALA2012120407030Connector · dirtyFWD CARGO DET 1 STATUS MSG NO CLEAR :NO TIME. CLEANED CONNECTOR AT FWD DETECTOR AND OPS NW NORMAL.SDR CA121129005Circuit Breaker · intermittent(CAN) DURING COMPLETION OF TASK 2620/04, CONTINUITY CHECK OF FIRE BOTTLE DISCHARGE CARTRIDGES, 1 YEAR INTERVAL, ENGINEER FOUND 7 AMPS CIRCUIT BREAKER G2 FIRE EXT 1 & 2 INTERMITTENT. CIRCUIT BREAKER REPLACED AND SYS TESTED SERVICEABLE.SDR UALA2012120406960Connector · faultyCARGO FIRE BTL DISCHARGE LIGHT DOES NOT TEST. REMOVED AND REINSTALLED CONNECTOR FROM LIGHT LENS FROM CARGO BOTTLE DISCHARGE LIGHT ASSY. LIGHT TEST NORMAL.SDR UALA2012112906854Connector · malfunctionedCARGO FIRE BTL DISCHARGE LIGHT DOES NOT TEST. DEFERRED DUE TIME COMPLIED WITH REQUIREMENTS CONTAINED IN MEL 2620G. REMOVED AND REINSTALLED CONNECTORS FROM LIGHT LENS FROM CARGO BOTTLE DISCHARGE LIGHT ASSY LIGHT TEST NORMAL.SDR RU3A20121113001Wire · brokenON TAKEOFF ROLL AT APPROX 60 KIAS, PNF OBSERVED DISCHARGED LIGHT ILLUMINATION ON LEFT FIRE BOTTLE. PNF CALLED OUT AN ABORT AND PF ABORTED TAKEOFF. CREW TAXIED AIRCRAFT TO HANGAR WITH NO FURTHER INCIDENT. FOUND BROKEN WIRE TO NR 1 FIRE BOTTLE. REPAIRED BROKSDR UALA2012110906447Wire Harness · damagedNR 2 ENGINE RIGHT STATUS MESSAGE. FOUND WIRES W0656-1001R-16 AND W0656-1002R-16 FROM M26005 LOWER AFT FIRE DETECTOR TO M26004 LOWER FORWARD WITH DAMAGED INSULATION BENEATH CLAMPS BEHIND EDP HYDRAULIC SUPPLY LINE HEATSHIELD AT 3 O'CLOCK POSITION. REPLACED FIRSDR UALA2012110906446Wire · damagedSTATUS MSG OVERHEAT CIRCUIT R2. FOUND WIRES W0656-1001R-16 AND W0656-1002R-16 FROM M26005 LWR AFT DETECTOR TO M26004 LOWER FWD WITH DAMAGED INSULATION BENEATH CLAMPS BEHIND EDP HYDRAULIC SUPPLY LINE HEATSHIELD AT THE 3 O'CLOCK POSITION. REPROTECTED INSULATIOSDR UALA2012110706387Wire · chafedRIGHT ENGINE FIRE LOOP 2 STATUS MESSAGE. FIRE LOOP 2 RIGHT ENGINE - FOUND WIRES W0656-1001R-16 CHAFED THROUGH SHIELD TO CENTER CONDUCTOR AND W0656-1002R-16 CHAFED THROUGH TO SHIELD. NEEDS APPROX 30FT OF BMS13-55T4C1G16. REF IPC71-00-01-751C ITEM 120 PCN 566SDR HEEA20121029000Connector · contaminatedDURING TRANSITION FROM HOVER TO FORWARD FLIGHT, THE NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED WITH A STEADY WARNING TONE. LIGHT/TONE EXTINGUISHED AFTER 2-3 SECONDS. LANDED AND RETURNED TO THE RAMP. MX CLEANED MOISTURE FROM CONNECTOR.SDR HALA2012101900222Terminal · damagedLT ENGINE FIRE LOOP L1 DISPLAYED ON EICAS AFTER PDC FIRE/ OVHT LOGIC TEST. REPAIRED TERMINAL ON UPPER AFT ELEMENT. OPS TEST OK IAW FIM 26-11-804, FIG 104.SDR HALA2012101700219Terminal · damagedLEFT ENGINE FIRE LOOP LP1 DISPLAYED ON EICAS AFTER PDC FIRE/OVHT LOGIC TEST. REPLACED TERMINAL LUG ON UPPER AFT ELEMENT OPS TEST OK IAW FIM 26-11-804, FIG 104.SDR HALA2012101000217Connector · dirtyICAS MESSAGE "LT ENG FIRE" LP1 DISPLAYED. CLEANED LUG ON LOWER AFT ENG FIRE DETECTOR CHANNEL A. FIRE OVERHEAT BITE TESTED OK. READINGS OK IAW FIM 26-11-804, FIG 104.SDR UIEA2012101000462Connector · damagedRIGHT BLEED DUCT LEAK EICAS MESSAGE ON INTERMITTENTLY 3 TIMES DURING CLIMBOUT. REMOVED CONNECTOR D10222 AND WIRES W062-786R-22, W062-801R-22, W062-100K-2, IAW WDM 91 HOOKUP LIST D10222 AND WDM 26-18-21 AND SWPM 20-00-00.SDR UALA2012100905722Connector · dirtyLEFT ENGINE FIRE LOOP 2 EICAS. PER TOMC DIRECTION CYC CB'S B21 AND B21, NO HELP, EICAS MSG REMAINS. CLEAN ALL FIRE LOOP CONNECTORS ON NR 1 ENGINE, LEFT ENGINE FIRE LOOP 2 MESSAGE GONE. FIRE TESTED NORMAL.SDR UALA2012090404975Wire · brokenNR 1 ENGINE, NR 1 FIRE BOTTLE. WHILE ACCOMPLISHING DL1057 FIRE BOTTLE AGENT DISCHARGE TEST, FOUND BOTH WIRES BROKEN UNDER CONDUIT BETWEEN CONNECTOR 473VC PINS 4 TO FIRE AGENT PRESSURE CONNECTOR PIN 2. ALSO GROUND WIRE FROM AGENT CONNECTOR PIN NR 3 TO GROUND,SDR UIEA2012090100371Terminal · looseEICAS MESSAGE FOR LT ENGINE FIRE LOOP ONE, DISPLAYED. FOUND LOWER AFT ENGINE FIRE DETECTOR TERMINAL LOOSE. CLEANED & AMP; INSTALLED IAW AMM 26-11-02/406. OPS CKS GOOD.SDR SWIA201231567Connector · looseRECEIVED MLG BAY OVERHEAT WARNING WITH ASSOCIATED TRIPLE CHIME AND AURAL WARNING. (FLT 2981) TIGHTENED LOOSE CONNECTOR AND TIGHTENED JAM NUT IN REFERENCE TO AMM.SDR CALA2012081500506Wire Harness · damagedON PUSH BACK AND START ENG NR 2 OVERHEAT LIGHT ILLUMINATED AND WENT OUT. AFTER TEST, ALL CHECKED GOOD AND CONTINUED AFTER TAKEOFF. 8000FT LIGHT ILLUMINATED, RAN QRH LIGHT WENT OUT. RETURNED TO DEPARTURE, INSPECTED NR 2 ENG FOR PNEUMATIC LEAKS, NONE FOUND, CSDR ASAA2012080992687Terminal · brokenFOUND FIRE DETECTION GROUND WIRE BROKEN AT GROUND TERMINAL LT CORE MW0326 HARNESS CONNECTIONS. ACFT GROUNDED. REPLACED TERMINAL LUG AND RESECURED GROUND WIRE OF MW0326, REF SWPM 20-30-11. OPS NML, REF MM 26-11-00.SDR HEEA20120808463Wire Harness · damagedNR 2 ENGINE FIRE WARNING LIGHT AND AURAL WARNING CAME ON IN CUISE FLIGHT. LANDING UNEVENTFUL. INSTALLED NEW FLAME DETECTOR AND HARNESS AND COMPLIED WITH SHRINK WRAP MODIFICATION.SDR UALA2012080304149Circuit Breaker · trippedAPU FIRE LOOP B FAULT, CIRCUIT BREAKER L44 APU FIRE AND OVERHEAT DET LOOP B FOUND TRIPPED. VERIFIED ON ASM 26-13-01 THAT CIRCUIT IS ISOLATED, CIRCUIT BREAKER PULLED AND CAPPED. GROUND CHECKED NORMAL REF AMM TASK 26-22-00-710-001.SDR QMLA2012080212125Connector · contaminatedDURING TAKEOFF, HAD A FLICKERING ENGINE FIRE LIGHT. REMOVED CONNECTOR ON ENGINE DECK, CLEANED WITH CONTACT CLEANER, SUSPECT MOISTURE, APPLIED STABILANT TO CONNECTOR REINSTALLED CONNECTOR. FIRE LIGHT FLICKED 2-3 TIMES AGAIN. APPLIED STABILANT TO CONNECTOR.
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