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 ASAA2014090709072Wire · misinstalledNR 2 ENGINE FIRE HANDLE DOES NOT ILLUMINATE DURING TEST IN NORMAL, BUT LIGHTS WHEN SELECTED TO A. ACFT GROUNDED. OPENED NR 2 ENGINE FAN AND DUCT COWLING. INSPECTED ALL B LOOP FIRE DETECTORS AND FOUND DETECTOR MW0326 AT LT SIDE ENGINE CORE WITH AN IMPROPER CSDR CALA2014090801212Connector · shortedWHEEL WELL FIRE AFTER TAKEOFF FOUND CONNECTOR D840 SHORTED. INSTALLED NEW CONNECTOR D84 IAW SWP 20-62-14. PERFORMED WW FIRE TEST, OPERATIONS CHECKED GOOD.SDR ASAA2014082408947Terminal · brokenFIRE TEST FAILED ON NR 1 ENGINE. ACFT GROUNDED. ACCOMPLISHED ENGINEERING REQUESTS, FOUND BROKEN TERMINAL AT MW0316, UPPER LT FAN FIRE DETECTOR. INSTALLED NEW TERMINAL LUG, OPS CK GOOD REF WDM 26-11-11.SDR ASAA2014072308662Terminal · brokenNR 1 ENGINE FIRE DETECTION LOOP "B" INOPERATIVE. ACFT GROUNDED. INSPECTED ALL ENGINE FIRE LOOPS. FOUND LT UPPER FAN TERMINAL BROKEN AT M1757. REPAIRED IAW 26-11-02/801. REINSTALLED HARNESS REF 26-11-02/401 RETURNED SYS TO NORMAL. PERFORMED SYS OPS TEST RSDR CA140723003Wire · out of position(CAN) RT ENGINE FIRE LIGHT ILLUMINATED ON TAXI TO RUNWAY. INSPECTION OF THE RT ENGINE FIRE DETECTION WIRING AND SENSORS WAS COMPLETED. DUE TO VIBRATION ON TAXI, THE TERMINAL OF THE SENSOR EVIDENTLY MADE CONTACT WITH THE COVER OF THE FCU, PROVIDING A GROUNSDR HALA2014070500103Wire · damagedRIGHT ENGINE FIRE LOOP 2 DISPLAYED ON EICAS. REPAIRED WIRE AT TS682 IAW WDM 26-11-2 & SWPM 20-30-11. OPS CHECKED OK IAW AMM 26-11-00.SDR CALA2014062700813Wire Harness · brokenAFTER TAKEOFF ENG 2 OVERHEAT LIGHT CAME ON. REPLACED LT & RT CORE LOOPS NO HELP. FOUND LOOP A HARNESS 29-261 1-3-0024 RESISTANCE BAD WHILE MOVING HARNESS IAW FIM 26-10-00-8 10-805, MM26-11-01-000-801 & MM26-11-01-400-801. B LOOP TESTED OK. PLACED ON MEL. RSDR REXA2014060900580Connector · disconnectedSMOKE DETECTOR IN LAVATORY NOT WORKING. UPON REMOVAL OF LAVATORY SMOKE DETECTOR, FOUND CONNECTOR DISCONNECTED. RECONNECTED CONNECTOR & PERFORMED OPERATIONS CHECK IAW AMM 26-16-01. OPERATIONS CHECKED GOOD. OK FOR SERVICE.SDR ASAA2014060808102Connector · dirtyNR 2 ENGINE OVERHEAT ILLUMINATED. ACFT GROUNDED. BITE CHECKED ENGINE/APU FIRE DETECTOR MODULE, NO FAULTS LOGGED. GVI ENGINE AND DUCT, NO DEFECTS NOTED. INSPECTED FIRE/OVERHEAT DETECTOR CONNECTIONS. FOUND LOWER AFT GROUND CONNECTION DIRTY. CLEANED AND SECURSDR JJBA20140606001Wire · chafedBAGGAGE SMOKE WARNING LIGHT ILLUMINATED DURING CLIMB THROUGH 9000 FT. WENT OUT ON DESCENT THEN CAME ON AGAIN AT 2000 FT. DISCONNECTED DETECTORS TO ISOLATE SYS & DEFERRED IAW MEL. REPAIRED CHAFED WIRE TO NR 2 SMOKE DETECTOR. OPERATIONS CHECKED GOOD.SDR SWIA201438004Connector · dirtyAFT CARGO SMOKE DETECTOR WILL NOT TEST. CLEANED ELECTRICAL CONNECTOR ON 2 SMOKE DETECTOR. OPS CHECK GOOD.SDR CA140522012Wire · broken(CAN) FIRE WARNING TEST DISPLAYED ALL 3 ZONES ON LT & RT ENGINES, NO WARNING HORN DETECTED. WIRE FROM A/C MAIN BUSS BAR, 28 VDC FOUND TO HAVE BREAK. NEW WIRE INSTALLED AND SYSTEM GROUND FUNCTION CHECKED OK.SDR ASOA20140519086Connector · dirtyACFT HAD MULTIPLE EICIAC MESSAGES THAT THE E2 FIRE DETECT FAIL. ACFT LANDED WITHOUT ISSUE AND MAINTENANCE REMOVED AND REINSTALLED FIRE DETECT PANEL TO FACILITATE CLEANING IAW AMM 26-00-01. REMOVED AND REINSTALLED ENGINE 2 FIRE DETECT CONNECTOR FOR CLEANING ISDR ASAA2014041907502Shield · separatedFOUND SHIELDING SEPERATED IN SEVERAL PLACES AND SHIELD TERMINAL LUG ON CORE B2 FIRE LOOP HARNESS. ACFT GROUNDED.SDR CA140418001Wire · damaged(CAN) ON GROUND, FLIGHT CREW REPORTED THAT NR 2 ENGINE FIRE DETECTION CIRCUIT BREAKER (CB) J7 ON THE RT ESSENTIAL CB PANEL, POPPED. AS THIS WAS A HARD FAULT, THE ACFT WAS REMOVED FROM SERVICE. DURING TROUBLESHOOTING, BURNED SHIELD SOLDER SLEEVES WERE FOUND ASDR R61A201404130535Wire · chafedPRIOR TO FL 240, CREW RECEIVED INTERMITTENT INDICATION ON NR 1 SIDE FOR CHECK FIRE DETECTOR E1 AND B FAULT LIGHTS WITH CIRCUIT BREAKER K7 TRIPPED ON CAPTAINS SIDE PANEL. ELECTED TO RETURN TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOSDR ASAA2014041107519Connector · damagedNR 2 ENGINE RT CORE FIRE DETECTOR B LOOP HAS TERMINAL LUG DAMAGE, MW0326, REF ASA T/C N8420001. ACFT GROUNDED. REMOVED AND INSTALLED NEW LUG REF MM 26-11-02. SYS OPS CKS NORMAL REF 26-11-00.SDR ASAA2014040707468Wire Harness · failedB SIDE FIRE LOOP FOR NR 2 ENG WILL NOT TEST. ACFT GROUNDED. R & R AND TESTED NR 2 ENGINE FIRE LOOP HARNESS IAW MM 26-11-02, TEST PASSED. OK FOR SERVICE.SDR ASAA2014032207263Wire · detachedFOUND FIRE LOOP "B" UPPER RT WIRE DETACHED FROM CONNECTOR. ACFT GROUNDED. REF WDM 26-11-21 AND WDM 26-11-11. REPLACED BOTH RING TERMINALS FOR MW0326 HARNESS CONNECTION TO M1760 ENGINE CORE RT FIRE DETECTOR ASSY IAW SWPM 20-30-11, PARAGRAPH O AND PERFORMED ENSDR CALA2014032490686Connector · dirtyRT ENG SQUIB TEST ONE FAILS TO TEST. CLEANED CONNECTOR ON SQUIB, TESTED OK TEN TIMES.SDR CALA2014031990646Connector · dirtyENG 2 SQUIB TEST USING TEST SW NR 2 DOES NOT ILLUMINATE GREEN SQUIB TEST LIGHT. CLEANED & RESEATED SQUIB CONNECTORS DM228B & DM229B IAW SSM26-21-02. SQUIB TESTED NORMAL IAW AMM26-21-00.SDR ERAA20140006Pin · backed outSMOKE WARNING LIGHT INTERMITTENT. FOUND PIN 9 ON CONTROL AMPLIFIER CONNECTOR 2612-P1 RECESSED. REINSERTED PIN IN CONNECTOR & GND TESTED GOOD IAW -8 MM 26-12-00.SDR 39LA2014030862Connector · dirtyDURING FLIGHT FROM JBAD TO OAIX THE NR 1 ENG FIRE WARNING LIGHT ILLUMINATED INTERMITTENTLY. CLEANED CONNECTOR FOR NR 1 ENG FIRE WARNING LIGHT, INSPECTED FOR EVIDENCE OF FIRE OR DAMAGE, NONE NOTED.SDR CALA2014022590438Connector · not seatedFWD CARGO DETECTION FAN MAINTENANCE MESSAGE ON LOWER EICAS. PULLED CB'S, RESEATED CONNECTOR ON BLOWER 1, CLOSED CB'S, OPERATIONS NORMAL.SDR CALA2014022190412Wire · damagedNR 2 PYLON ELEC CONDUIT CONVOLUTED TUBING FOR FIREX BOTTLES WIRING WAS DETERIORATED & WIRING DAMAGED. REPLACED CONVOLUTED TUBING & DAMAGED WIRING 2621-0002 TO CONNECTOR 6WEZA & BOTH WIRES TO 5WEZA. RANG OUT WIRES & ACP CHECK OF FIREX SYS, OPERATIONS CHECKED SDR HALA2014021700026Terminal · brokenLEFT ENGINE FIRE LOOP 2 STATUS MESSAGE ALSO RIGHT ENGINE FIRE LOOP 2, STATUS MESSAGE. REPLACED BROKEN TERMINALS AT NR 1 ENGINE AFT LOWER LOOP AND NR 2 ENGINE AFT UPPER LOOP IAW WDM 26-11-11 AND 26-11-21. ENGINE FIRE DETECTION LOOPS OPS CHECKED OK IAW AMM 26-SDR GTIA201402141170Connector · damagedCARGO COMPARTMENT FIRE EXTINGUISHER CHECK FIRING CIRCUIT CONTINUITY FAIL TEST ON CONNECTOR 4015WX-C, CIRCUIT BREAKER ON PANEL 122VU T-19 KEPT POPPING WHEN DISCHARGE BUTTON WAS PRESSED.SDR ERAA20140001Wire Harness · chafedSMOKE CAUTION LIGHT ILLUMINATED. REPAIRED CHAFFED WIRES AT NR 2 SMOKE DETECTOR & OPERATIONS CHECKED GOOD.SDR JJBA20140203002Connector · unsecureLAVATORY SMOKE DETECTOR WILL NOT TEST. SECURED LAVATORY SMOKE DETECTOR CONNECTOR.SDR ASAA2014012412477Wire Harness · damagedNR 1 ENGINE, WIRE HARNESS FOR LT & RT CORE FIRE DETECTOR, STAINLESS STEEL INSULATION DAMAGED AND MISSING. ACFT GROUNDED. REPLACED NR 1 ENGINE LT & RT CORE FIRE DETECTOR HARNESS MW0326, REF AMM 26-11-02. ETOPS SIGNIFICANT SYS GROUND VERIFICATION SUCCESSFUL.SDR CA140313015Squib · misinstalled(CAN) DURING FIRST EMMA INSPECTIONS, RT FIRE EXTINGUISHER SQUIB FOUND WIRED BACKWARD. DURING TEST PRESSING THE FIRE BOTTLE BUTTON ONLY RESULTED IN A BREAKER POPPING.SDR SIMA20140113002Wire Harness · chafedDURING TROUBLESHOOTING FOR, E 1 FIRE DETECT FAIL. FOUND E 1 PYLON FIRE DETECT HARNESS CHAFFED. IAW NRWC 637-DFW-01561 FOR FIRE LOOP REPLACEMENT, PREFORMED INSPECTION & REPAIR OF E 1 PYLON FIRE DETECT HARNESS AT CONNECTOR P0915 IAW SPWM 20-21-00. OPERATIONSSDR CA140113006Wire · broken(CAN) AIRCRAFT RETURNED TO BASE AFTER THE FLIGHT CREW RECEIVED A SMOKE MASTER WARNING INDICATION ON DEPARTURE. UPON RETURN, MX ACTION FOUND A BROKEN WIRE IN THE NR 1 SMOKE DETECTOR CONNECTOR 2612-P2. ALL WIRES IN CONNECTOR WERE SOLDERED & THE SYS WAS CHECKEDSDR CA140210005Module · intermittent(CAN) AIRCRAFT HAD AN ABORTED TAKEOFF AS THE RT FIRE LIGHT CAME ON. STOP AND FEATHER WAS PULLED AND PUSHED THE FIRE EXTINGUSER SWITCH ON THE DASH. THE LIGHT WAS VERY DIM YET IT WAS ON. THE FLIGHT CREW CHECKED THE ENGINE COMPARTMENT AFTER BEING CLEARED BY THSDR FXGA20140110002Wire · damagedSMOKE INDICATION IN MAIN CABIN, CREWMEMBER INSPECTED WHILE WEARING PBE. TURNED TOWARD NEAREST SUITABLE AIRPORT. AFTER INSPECTION NO SMOKE NO FIRE & PROCEEDED TOWARDS ANC. CLEANED & SECURED NR 3 SMOKE DETECTOR GND. R & R 3 WIRES AT FS 470 FWD OF DOME LIGHT SDR FXGA20140110001Wire · chafedSMOKE DETECTOR ACTIVATED IN FLIGHT. VISUAL INSPECTION OF CARGO COMPARTMENT SHOWED NO EVIDENCE OF SMOKE. ZONE NR 2 WOULD NOT TEST. REPAIRED CHAFFED WIRES AT NR 1 & NR 3 SMOKE DETECTOR. RELAMPED TEST LIGHT ON NR 2 SMOKE DETECTOR IAW DC6 MM 28-5-5 OPERATIONS CSDR FXGA20140108001Wire · damagedNR 3 MAIN CABIN SMOKE DETECTOR GAVE FAULTY INDICATION, DIVERTED TO GAL AT 0405Z. DEFERRED NR 3 SMOKE DETECTOR IAW MEL 26-7. OFF LOADED CARGO & PROCEEDED TO ANC. AIRCRAFT WAS REPAIRED AT ANC, NR 3 SMOKE DETECTOR CONNECTOR WAS FOUND TO HAVE A DAMAGED WIRE THASDR CALA2013122793983Wire · shortedPIN F REMOVED FROM 450VT2 FOR DF988. IAW WD 26 12 08, MEG WIRE TO GND SORTED, WILL NEED TO OPEN JUNCTION BOX. SUGGEST WE HAVE DUCKS REMOVED AT 12 O'CLOCK POSITION TO SEE IF WE CAN GET ACCESS TO J BOX.SDR CALA2013122693908Wire · damagedNR 2 ENG PYLON FWD FIRE EXTINGUISHING BOTTLE SQUIB 5WE2 CONDUIT TORN & MISSING SECTION WIRE INSULATION, WEARING ON METAL CLAMP. REPLACE WIRE 2621-0003- CF20 FROM CONNECTOR 5WE2A TO CONNECTOR 474VC IAW WDM 26-21-03 ESPM 20-44-16 & ESPM 20-32-22.SDR YYFA2013201317002Connector · dirtyMID CARGO FIRE DETECTION LOOP A COMES ON IN FLIGHT & STAYS ON AFTER QRH PROCEDURE. CLEANED CONNECTOR ON MID CARGO COMPARTMENT LOOP A DETECTOR, OPERATIONS CHECKED GOOD. AMM BITE TEST OPERATIONS CHECKED GOOD AMM 26-16-00.SDR CALA2013122093837Wire · damagedNR 1 ENG LOOP SQUIB TEST FAILED. NR 1 SQUIB LIGHT DOES NOT ILLUMINATE. FOUND WIRE PULLED OUT OF A SPLICE REPAIR 10 INCHES FROM CONNECTOR 5WE1-A. REPLACED WIRES 2621-20, 2621-19, 2621-73 & 2621-21 ALONG WITH CONDUITS. WORK ACCOMPLISHED ON OV WU W0976G, W099SDR ASOA20131212217Connector · dirtyTHE CREW REPORTED A CARGO SMOKE INDICATION IN FLIGHT. LANDED WITHOUT INCIDENT, MAINTENANCE INSPECTED AND CLEANED FWD CARGO BAY SMOKE DETECTOR CONNECTOR, OPS TESTED WITH NO DEFECTS, AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR HALA2013121100179Terminal · damagedDURING PDC CHECK, FOUND RT ENGINE FIRE LP2 MESSAGE ON EICAS PAGE. TROUBLESHOT IAW FIM 26-11 804. REPLACED TERMINAL LUGS FOR RT ENGINE FIRE DETECTOR TS683. OPS CHECKED OK.SDR CALA2013121393651Connector · looseFLIGHT ATTENDANT`S CIDS PANEL CAUTION ON. FOUND LAVATORY SMOKE SYSTEM FAULT. SECURED LOOSE CONNECTOR 7200VC BEHIND FWD LAVATORY A IAW WD 25-41-01. LAVATORY SMOKE SYS CHECKED OK IAW AMM TK 26-17-00-710-001 & 26-16-00-710-001.SDR 39LA2013120727Cable Assy · damagedNR 1 ENG FIRE WARNING LIGHT ILLUMINATED IN FLIGHT. TROUBLE SHOT SYS, FOUND DAMAGED LEAD, REPLACED WITH SERVICEABLE LEAD PN 35302-62, SN NA, WORK PERFORMED IAW S61N MM SA4045-80, CHP 26-00-00, OPERATIONS CHECKED GOOD 12/07/13.SDR CALA2013121193593Wire · brokenNR 1 PYLON FIRE EXTINGUISHER BOTTLES BAY. FWD BOTTLE DISCHARGE CARTRIDGE CONNECTOR WIRING CONDUIT IS BROKEN & WORN AT CLAMP AT RT SIDE AFT OF FWD BOTTLE BELOW HYD TUBE GANG CLAMP ASSEMBLY.SDR CALA2013112093130Connector · dirtyNR 4 ENG SQUIB TEST 1 FAILED. CLEANED DM230C CONNECTOR AT FIRE BOTTLE A IAW WDM26-21-12 PG1, GND TESTED OK.SDR IBUA2014F00048Sleeve · out of positionACFT WAS IN FLIGHT WHEN A FIRE WARNING LIGHT ILLUMINATED. PILOT ACTIVATED ENGINE EXTINGUISHER SYS AND WARNING LIGHT WENT OUT. DURING INSPECTION, FIRE SLEEVE PROTECTING ENGINE WIRE BUNDLE AFT OF ENGINE, ADJACENT TO INBD EXHAUST PIPE WAS FOUND TO BE TOUCHING SDR ASAA2013111296389Wire · brokenNR 1 ENG FIRELOOP NR 3 POSITION, AFT INBD AT HOT SECTION, WIRE BROKEN AT TERMINAL. ACFT GROUNDED. REMOVED, REPLACED, AND TESTED MW0326 HARNESS IAW MM 26-11-02-400-802. TEST PASSED, OK FOR SERVICE. ALTERNATE DEACTIVATION ACCOMPLISHED IAW CH5, TABLE 3, ITEM 1.SDR CALA2013111300833Wire Harness · damagedCLIMBING THRU F200 ENG 1 OVERHEAT LIGHT ILLUMINATED. LIGHT EXTINGUISHED AFTER THRUST LEVER WAS RESTARTED AFTER 4 MINUTES, LIGHT ILLUMINATED AT BLOCK IN. TROUBLE SHOT NR 1 ENG FIRE DETECTOR. FOUND CONNECTOR DJ2501 LOOP A1 PIN 2 HAS OPEN WIRE. IAW AMM 26-11-
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