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 UIEA2020052001086Wire · damagedRIGHT ENGINE LOOP 2 INOPERATIVE. REPAIRED DAMAGED WIRE INSULATION AT LOWER FORWARD LOOP 2 AND TESTED IAW SWPM 20-10-13 AND AMM 26-11-00.SDR DALA2020051102381Connector · brokenSHIP 7003 - IFSD - PASSING 10K FEET ON CLIMB OUT, LEFT ENGINE OVERHEAT EICAS MESSAGE APPEARED. THE FLIGHT CREW FOLLOWED QRH PROCEDURE AND SHUT THE LEFT ENGINE DOWN. THE FLIGHT CONTINUED TO ATL. CORRECTIVE ACTION: FOUND BROKEN CONNECTOR END ON #1 ENGINE RIGHT CSDR IPXA2020050154828Pin · looseINSPECTION TYPE:N/A DIVERSION, EMERGENCY DECLARED, LANDED UNEVENTFUL. CLIMBING THROUGH 33,000 RECEIVED EICAS MESSAGE L ENG OVERHEAT AND LIGHT RAN QRH REDUCED POWER ON LEFT HACKED THE CLOCK WAITED 2 MIN MESSAGE AND LIGHT DID NOT GO OUT SHUT ENGINE DOWN DIVERTEDSDR UIEA2020042870847Terminal · brokenRIGHT ENGINE FIRE LOOP 1 INOPERATIVE. REMOVED AND REPLACED THE CARD ASSY FIRE DETECTOR ENGINE 2 LOOP IAW AMM 26-11-01. FAULT COULD NOT BE DUPLICATED. FOUND LOWER AFT FIRE DETECTOR WITH A BROKEN TERMINAL, REPLACED THE TERMINAL AT TS 682 IAW WDM 26-11-21 AND SDR CALA2020032700737Wire · brokenWING-BODY OVERHEAT LIGHT LIGHT ON THIS IS A REPEAT WRITEUP BITE ON WING BODY OVERHEAT CTL. SHOWED CODE 44, AFT CARGO OVERHEAT ALARM. PERFORMED CONTINUITY CHECK OF CARGO BIN LOOPS WAS BAD PER TABLE 301 FIM TASK 26-18-00 P 301. NEED TO ISOLATE WHICH LOOP IS BAD SDR JIKA202003181601Connector · contaminatedWHILE ENROUTE TO KVIS FROM KONT ABOUT 30-40 MINUTES INTO THE FLIGHT THE LEFT FIRE T HANDLE ILLUMINATED. CREW COMPLETED THE “ENGINE FIRE WARNING IN FLIGHT” MEMORY ITEMS. AFTER 10 SECONDS OR SO THE LIGHT FLICKERED AGAIN, THE CREW CONTINUED TO PERFORM THE CHECK OSDR UIEA2020031300444Connector · looseRH ENGINE FIRE LOOP 2 STATUS MESSAGE (ENGINE FIRE DETECTION SYSTEMS, DETECTION LOOPS (ER RESTRICTED 120)).(<P>TRANSFERRED TO MDDR #125715 IAW MEL 26-11-01-01, CAT "C", DUE DATE 23MARCH20. PLACARD INSTALLED. NOTE: RESTRICTED TO ETOPS 120, DISP : DD @ 0013Z.</PSDR ASOA2020030654002Connector · looseMLU - FLIGHT 446, THE CREW REPORTED A LAV SMOKE WARNING ON SHORT FINAL. THE CREW RAN THE QRH, AND THE FA CONFIRMED NO SMOKE PRESENT IN THE LAV. THE AIRCRAFT LANDED AT MLU WITH NO INCIDENT WHERE THE SMOKE DETECTOR WAS PLACED ON MEL 26-14-00 CAT C. THE AIRCRAFT SDR ASAA2020030532354Wire Harness · damagedWHILE PERFORMING #2 ENGINE HARNESS GVI (T/C # N8420001), FOUND MW326 FIRE DETECTOR DAMAGED. GROUNDED - YES. #2 ENGINE HARNESS MW326 REMOVED AND REPLACED REF B737-900 AMM 26-11-01. OPERATIONAL CHECK GOOD AND GROUND VERIFICATION SUCCESSFUL.SDR ASAA2020030932353Wire Harness · broken#1 ENG "A" LOOP INOP. GROUNDED - YES. CONFIRMED FAULT, #1 ENGINE A-LOOP WILL NOT TEST. FOUND R/T CORE FIRE DETECTOR HARNESS (MW0315) TERMINAL LUG BROKEN AT THE DETECTOR, TOO SHORT TO REPAIR WIRING. REMOVED & REPLACED MW0315 CORE FIRE DETECTION HARNESS (A-LOOP)SDR ASAA2020030532352Wire Harness · brokenENG FIRE SWITCH HANDLE LIGHT LOOP B INOP. GROUNDED - YES. VERIFIED, FOUND HERMETICAL SEAL BROKEN AT RIGHT CORE. REMOVED AND REPLACED #2 ENG FIRE DETECTOR WIRE HARNESS PER B737-800 AMM 26-11-02 OPS CHECK GOOD.SDR ASAA2020030332327Wire Harness · chafedDETAILED VISUAL INSPECTION OF #1 ENG LOOP "B" FIRE DETECTION HARNESS MW0316 FOUND CHAFING AT THE 12 O'CLOCK POSITION, NEAR OUTBOARD COWLING HINGE. GROUNDED - YES. REMOVED & REPLACED ENG #1 FAN FIRE DETECTION HARNESS PER B737-800 AMM 26-11-02 ACCOMPLISHED OPS SDR ASAA2020022732326Wire · separatedFLT CREW REPORTS #2 ENGINE FIRE DETECTION DOES NOT TEST. GROUNDED - YES. PERFORMED ENGINE FIRE DETECTION RESISTANCE TEST PER B737-800 AMM 26-11-00-730-801. FAILED RIGHT CORE LOOP. DISCOVERED WIRES SEPARATED FROM TERMINAL LUGS. REPAIRED WIRES SEPARATED FROM TERSDR VE7A2020022740001Connector · shortedDURING CLIMB FROM 2000FT TO 3000FT IN RAINING CONDITIONS, THE #2 ENGINE FIRE LIGHT AND AUDIO ALARM ACTIVATED. #2 ENGINE DECK FITTING AT AIRFRAME BULKHEAD WAS FOUND WITH A SIZEABLE AMOUNT OF WATER INTRUDING ON PINS. (EVENT HAPPENED DURING HARD RAIN.)SDR RAIA2020012860001Wire · failedBAG SMOKE EICAS MSG, BAG BOTTLES DISCHARGED---R&R BOTH BAGGAGE FIRE BOTTLES(HIGH RATE AND METERING). ADDITIONAL MX- REPLACED WIRING FROM SG4313 TO SMOKE DETECTORS 1 AND 2 DUE TO WIRES READING 200 OHMS( TEST RESULT WHEM WIRES MEGGERED) PERFORMED BAGG SMOKE TESTSDR UIEA2020012400117Wire · looseLEFT ENG BLEED EICAS MSG DISPLAYED WHEN LEFT ENG ANTI-ICE SELECTED.(<P>PERFORMED BITE CHECK FOR FAMV, FOUND L FAV, FAS LIGHT ON. OPENED T/R ON LEFT ENG AND FOUND TWO LOOSE WIRES. TIGHTENED WIRES, RAN ENG, NO MESSAGES PRESENT AT THIS TIME. VERIFIED BITE ON FAMVSDR DUFA20200116002Terminal · damagedON JANUARY 14TH, 2020, DAKOTA 1024 DEPARTED THIEF RIVER FALLS (KTVF) AIRPORT AT
1844 AND CLIMBED TO 17,000 FEET MSL. WHILE APPROACHING THE GOLLF INTERSECTION ON
THE GOPHER ONE ARRIVAL, ARTCC ASSIGNED DESCEND AND MAINTAIN 10,000 FEET MSL. AT
APPROXIMATELY 11SDR ASAA2020011331831Wire · brokenNR 1 ENG A LOOP INOP. GROUNDED - YES. ACCOMPLISHED FIRE DETECTION CONTROL MODULE BITE TEST PER FIM 26-10 TASK 801. PERFORMED VISUAL INSPECTION OF FIRE LOOPS AND HARNESSES FOUND RT CORE A LOOP WIRE BROKEN AT TERMINAL LUG. REPLACED TERMINAL PER AMM 26-11-002-960SDR ASAA20191231735Wire Harness · brokenNR 1 ENGINE B LOOP DID NOT ILLUMINATE ON TEST PRIOR TO FLIGHT. GROUNDED - YES. HIGH RESISTANCE ON THE B LOOP FROM M279 BOX. RESISTANCE FLUCTUATES DURING SHAKE DOWN CORE MW0326, FOUND THE TERMINAL BROKE AT RT CORE DUE TO CORROSION. REPLACED MW0326 B LOOP CORSDR ASAA2019122091657Wire Harness · damagedWHILE ACCOMPLISHING TC N8420000, FOUND DAMAGE ON #1 ENGINE CORE FIRE DETECTOR HARNESS MW0325. GROUNDED - YES. REMOVED AND REPLACED #1 ENGINE CORE FIRE DETECTOR HARNESS MW0325. INSTALLATION TEST ACCOMPLISHED WITH NO FAULTS NOTED, REF B737 - 900 AMM 26-11-02. OPSDR UIEA2019121986105Terminal · brokenRIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE. FOUND A BROKEN TERMINAL LOG ON RIGHT ENGINE LOWER FWD FIRE LOOP 1. REPAIRED IAW SWPM 20-30-00. OPS CHECKED GOOD IAW AMM 26-11-00,SDR HALA2019121700518Connector · looseETOPS SIGNIFICANT SYSTEM - ENG 1 FIRE LOOP A FAULT, REPEAT WRITE-UP // INSPECTED ENG 1 FIRE LOOP, FOUND LOOSE CONNECTOR @ ENG 1 FIRE LOOP. RE-TORQUED CONNECTOR AS REQUIRED. PERFORMED FDU BITE CHECKED, PER AMM 26-12-00. TEST PASSED NO FAULTS NOTED. OK TO CONTINSDR ASAA2019121653607Wire Harness · damagedWHILE PERFORMING T/C N8420001 (RH ENG HARNESS GVI), FOUND HARNESS MW0325 SHIELDING DAMAGED. GROUNDED - YES. MW0325 FIRE DETECTOR HARNESS ON ENG #2 REMOVED AND REPLACED REF B737-900 AMM 26-11-01. OPERATIONAL CHECK GOOD AND GROUND VERIFICATION SUCCESSFUL.SDR HALA2019121600514Connector · looseETOPS - ENG 1 FIRE LOOP A FAULT, REPEAT WRITE-UP // INSPECTED ENG 1 FIRE LOOP, FOUND LOOSE CONNECTOR @ ENG 1 FIRE LOOP A. RETORQED CONNECTOR AS REQUIRED. PERFORMED FDU BITE CHECKED, PER AMM 26-12-00. TEST PASSED NO FAULTS NOTED.SDR ASAA2019121633606Wire Harness · damagedFOUND MW0326 CORE FIRE DETECTION HARNESS DAMAGE WHILE PERFORMING TASK CARD N8420001. GROUNDED - YES. REMOVED AND REPLACED CORE FIRE DETECTION HARNESS MW0326 IAW B737-800 AMM 26-11-02-000-802 / 26-11-02-400-802. ACCOMPLISHED ENGINE FIRE DETECTION OPC REF AMM 26SDR UIEA2019112545953Circuit Card · malfunctionedDURING CREW PRE-FLIGHT, STATUS MESSAGE "APU FIRE LOOP 1". (<P>TRANSFERRED TO DMI 121097 IAW MEL 26-15-01-01, CAT 'C', DUE DATE: 04-DEC-19.</P><P>LP 1223654 - M6: REMOVED AND REPLACED APU LOOP 1 PRINTED CIRCUIT CARD 685T, OPS CHECK GOOD. THIS CLEARS DMI 121097SDR VNAA20191122102Connector · dirtyENG BOTTLE 2 LO MESSAGE. APPROX. FL 340 WAS ON AND OFF FOR 4 MINUTES. RAN QRH AND LANDED AT NEAREST SUITABLE AIRPORT. REMOVED, CLEANED, & RE-SECURED CANNON PLUG ON #2 ENG FIRE BOTTLE IAW CRJ 700 AMM. OPS CHECK GOOD.SDR 120B201911200001Wire Harness · brokenRH ENGINE FIRE LOOP 1 DISPLAYED ON EICAS ON PREFLIGHT CHECK. TROUBLESHOT PER BOEING 767 FIM, FOUND A TERMINAL ON THE WIRE HARNESS WAS BROKEN. REMOVED AND REPLACED TERMINAL ON WIRE 5534-001R-16. COMPLIED WITH FIRE DETECTION OPERATIONAL CHECK IN ACCORDANCE WITH SDR ASAA2019111821320Connector · damagedON THE CARGO FIRE DETECTION PANEL, THE RED FWD LIGHT ON THE FWD SQUIB ARM BUTTON DOES NOT COME ON DURING THE SYSTEM TEST. GROUNDED - YES. PERFORMED CARGO ELECTRONIC UNIT (CEU) BITE CHECK REF FIM 26-16 TASK 801 DETECTOR A1 FAULT FOUND. INSPECTED D13844 CONNECTOSDR ASAA2019111501335Wire Harness · chafedDURING PREFLIGHT, ENGINE #2 FIRE LOOP WILL NOT TEST. GROUNDED - YES. PERFORMED B737-900 FIM 26-10 801 AND FOUND "#2 ENGINE LOOP "B" LOW DET RESISTANCE CLEAN CONNECTIONS" FAULT. ALL DETECTOR RESISTANCE VALUES ARE WITHIN LIMITS. UPON INSPECTION FOUND ISOLATOR CHSDR UIEA2019111315884Connector · damagedDURING POST-FLIGHT INSPECTION, DISCOVERED "APU FIRE LP 1" STATUS MESSAGE. (<P>TRANSFERRED TO DMI #120417 PER MEL CH 26-15-01-01, CAT "C".</P><P>LP 0994698 - M9: PERFORMED RESISTANCE CHECK 3.2 OHMS. NO TIME TO CHECK UPPER LOOPS, MDDR #120417 REMAINS OPEN PER FISDR ASAA2019102853122Wire Harness · damagedDURING TC N8420001 INSPECTION FOUND MW0326 HARNESS WITH DAMAGED BRAIDING. GROUNDED - YES. REMOVED AND REPLACED MW0326 HARNESS PER B737-900 AMM 26-11-02. PERFORMED GOOD OPS TEST OF R/H ENGINE FIRE DETECTION SYSTEM PER AMM 26-11-02-400-802.SDR ASAA2019102103055Wire Harness · damagedWHILE ACCOMPLISHING TASK CARD N8420000 FOUND HARNESS MW0326 DAMAGED BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED MW0326 REF B737-800 AMM TASK 26-11-02-000-802/400-801. PERFORMED OPS CHECK REF AMM 26-11-00-710-801. CHECKS GOOD. NO FURTHER DEFECTS NOTED.SDR ASAA2019101651020Wire Harness · damagedFOUND DAMAGE TO BRAIDING OF MW0325 AND MW0326 CORE FIRE DETECTION HARNESSES. GROUNDED - YES. REMOVED AND REPLACED MW0325 AND MW0326 CORE FIRE DETECTION HARNESSES, INSTALLATION TEST OK, REF AMM 26-11-02. OPENED, TAGGED, AND RESET 2CB'S. ETOPS SIGNIFICANT SYSTEMSDR ASAA2019092130763Wire Harness · brokenWHILE PERFORMING #1 ENGINE HARNESS INSPECTION PER TASK CARD N8420000 ON WO 1004707, FOUND BROKEN GROUND TERMINAL LUG ON WIRE HARNESS MW0326 FOR THE UPPER CORE FIRE DETECTION LOOP. GROUNDED - YES. REMOVED AND REPLACED MW0326 WIRE HARNESS IN REFERENCE TO AMM TASSDR UIEA2019091605508Wire · brokenRIGHT ENGINE FIRE LOOP #2 EICAS MESSAGE. TRANSFERRED TO MDDR 117744 IAW MEL 26-11-01-01, CAT 'C'. LP 841015 - M7: FOUND BROKEN WIRE AT TERMINAL TO FWD LOWER LOOP. REPLACED TERMINAL AS PER SWPM 20-30-00. OPS CHECK GOOD AS PER AMM 26-11-00. THIS CLEARS DMI #1177SDR ASAA2019090630635Wire Harness · damagedDURING REPLACEMENT OF #2 ENGINE IGNITER PLUGS, FOUND MISSING BRAIDING IN TWO LOCATION ON THE CORE FIRE DETECTION WIRE HARNESS, LWR HARNESS MW0325. GROUNDED - YES. REMOVED CORE FIRE DETECTOR HARNESS MW0325 PER AMM 26-11-02-000-802. INSTALLED HARNESS PER AMM 26-SDR FDEA201908282036Wire · damagedCARGO FIRE EXTINGUISHER BOTTLE 1 DOES NOT TEST. DOES ILLUMINATE WITH ANNUNCIATOR LIGHT TEST. REPAIRED WIRE AT 5WM-C PLUG IAW ESPM, WDM 26-23-02 AND AMM 26-23-12-04 . SYSTEM OPS CK NORMAL IAW AMM 26-23-12-04.SDR 2WAA201908263001Wire · brokenLT ENGINE LOOP A AND FIRE HANDLE INTERMITTENT ILLUMINATION DURING APPROACH WITHOUT FIRE BELL FOR THE ENGINE FIRE AND NO CAWS ALERT. OPS CHECK LT ENGINE FIRE DETECTION LOOP A FOUND TO BE NORMAL IAW AMM 26-10-00. DURING APPROACH, THE LT ENGINE DETECTION LOOP A NSDR UIEA2019081505188Connector · disconnectedMAIN CARGO LOOP 1 MESSAGE SHOWS ON LOWER EICAS DISPLAY. CONNECTED THE SMOKE DETECTOR M12213 1A2D ELECTRICAL PLUG IAW SWPM 20-60-06 SHT. PERFORMED SATISFACTORY MAIN CARGO SMOKE DET OPS CHECK IAW SMPM 26-14-00.SDR UIEA2019081635127Diode · failedFOUND PII-5 C766, & PII-4 C772 CIRCUIT BREAKER TRIPPED. REPLACED THE CIRCUIT BREAKERS C766 & C772, RELATED DIODES R203 & R204 PER WDM 26-16-11 REV55 AND CONDITION CHK NORMAL, PFM LOWER CARGO COMPARTMENT SMOKE DETECTION SYSTEM OPERATIONAL TEST IAW AMM 26-16-00SDR CALA2019081001345Wire Harness · damagedNR 2 ENGINE OVERHEAT LIGHT ILLUMINATED DURING FLIGHT. SHUTDOWN ENGINE AND LANDED. REPLACED THE NR 2 ENGINE LOOP B FIRE DETECTOR. FOUND LOOP A WIRE HARNESS DAMAGED AT TOP LUG. REMOVED & REPLACED CORE FIRE DETECTION HARNESS IAW MM. BITE TESTED GOOD. RAN SDR DALA2019081504771Connector · looseRIGHT ENGINE BOTTLE DISCHARGE LIGHT ILLUMINATED AT 34,000 PRIOR TO DESCENT. RIGHT ENGINE APPEARED TO BE OPERATING NORMALLY. LIGHT EXTINGUISHED AFTER LANDING . REMOVED PANEL X FOUND CONNECTOR LOOSE, RE-SECURED CONNECTOR. OPS CK GOOD. RT ENG BOTTLE DISCHARGE LSDR HCMA2019072900001Wire · looseDURING A TOUR FLIGHT FIRE LIGHT ILLUMINATED AND PILOT PERFORMED A PRECAUTIONARY LANDING. UPON INSPECTION OF FIRE DETECTION SYSTEM, FOUND LOOSE WIRE TO LOWER FIRE DETECTOR. WIRE WAS ADJUSTED AND RE-SECURED TO FIRE DETECTOR AND NO FURTHER PROBLEMS WERE FOUND.SDR ASAA2019072130139Connector · dirtyDURING FIRE TEST LOOP A ON ENGINE #1 DID NOT TEST. GROUNDED - YES. REF FIM 26-10 TASK 801. CLEANED LOOP A CONNECTIONS AND RE-SECURED THEM. OPS CHECK NORMAL AT THIS TIME.SDR ASAA2019071730111Wire Harness · failedNR 2 ENGINE FIRE SWITCH DOES NOT ILLUMINATE WHEN OVERHEAT/FIRE POSITION IS SELECTED WITH THE TEST SWITCH. GROUNDED - YES. REMOVED & REPLACED FIRE DETECTION HARNESS, MW0326, REF AMM 26-11-02-400-802. ACCOMPLISHED ENGINE FIRE DETECTION OPERATIONAL TEST REF AMM 2SDR ASAA2019071430027Wire Harness · failedFOLLOW UP TO HISTORY OF #2 ENGINE FIRE LOOP A FAULTS GROUNDED - YES. PERFORMED FIM 26-10 TASK 805 AND COULD RESISTANCE TO FLUCTUATE ON D998 PINS 24-25 FRIN 2.5 OHMS TO 7 OHMS BY MANIPULATING MW0315 HARNESS. REPLACED HARNESS IN REF TO AMM 26-11-02.SDR ASAA2019070129906Wire · broken#1 ENG "A" LOOP INTERMITTENTLY INOP. PRIOR TO TAXI #1 FIRE HANDLE DID NOT ILLUMINATE DURING TEST. AFTER TAXI TEST WAS NORMAL. GROUNDED - YES. WHILE PERFORMING GVI OF CORE FIRE DETECTION HARNESS MW0325 FOUND BROKEN WIRE AT HEAT DETECTOR M1759 REF WDM 26-11-11 PSDR ASAA2019063029905Wire Harness · brokenFIRE DETECTION FAULT NOTED ON PREFLIGHT. GROUNDED - YES. FOUND #2 ENGINE OVERHEAT LIGHT AND HANDLE LIGHT NOT ILLUMINATING DURING TEST. CYCLE A/C POWER REF AMM 20-60-99. A LOOP TEST NORMAL. B LOOP INOP. ENGINE APU FIRE BITE SHOWS #2 ENGINE LOOP B RIGHT CORE FASDR ASAA2019062929865Connector · dirtyDURING PREFLIGHT #2 FIRE HANDLE LIGHT DOES NOT ILLUMINATE DURING FIRE/OVERHEAT TEST. GROUNDED - YES. REFERENCE FIM 26-10 TASK 810, INSPECTED AND CLEANED # 2 ENGINE FIRE LOOP DETECTOR CONNECTIONS. RE-ACCOMPLISHED FIRE WARNING TESTS, TEST PASSED.
Back to JASC 2697