JASC 2997
Service difficulty reports · 343
Reports filed under 2997 · Hydraulic Power 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 = '2997' 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 = '2997' 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 SWIA201023859Wire Harness · burnedHYDRAULIC PUMP 3A WIRE HARNESS WIRES BURNT. (FLT 4527) REPLACED WIRING HARNESS.SDR 2010F00064Power Cable · brokenTHE ELECTRICAL POWER FEEDER CABLE OF NR 4 HYD AUX PUMP IN THE MEC WAS BROKEN, THE MAIN DECK FLOOR BEAM NEXT TO THE BROKEN CABLE WAS DISCOLORED AND HEAT DAMAGED. PERFORMED INSPECTION AND STRUCTURE REPAIR TO MAIN DECK FLOOR BEAM, SPLICE REPAIR ELECTRICAL POWER SDR UALA2010020100414Connector · burnedCTR HYD PUMP NR1 EICAS MESSAGE AND LOW PRESSURE LIGHT ON WITH MOVEMENT OF FLAPS AND FLIGHT CONTROL MESSAGE. FOUND BURNED SOCKET ON CONNECTOR D482. CONTACT POSITION IS C. REPLACED CONNECTOR D482 IAW WDM. R & R PUMP DUE TO BURNED PIN ON MAIN AC CONNECTOR, LEAK CSDR USAA20100119BB002Connector · failedCLT FLT 1041, DURING THE FLIGHT, MULTIPLE CREW MEMBERS EXPERIENCED SYMPTOMS OF POSSIBLE AEROSOLIZED FUMES FROM CABIN AIR. SUSPECT THE RIGHT RESERVOIR WAS OVER SERVICED DUE TO POSSIBLE BAD CONNECTOR (D60) SHORT (SHIELDING DAMAGE). REPLACED CONNECTOR AND SERVSDR HNAA2010012200011Connector · failedNR 2 ENG HYD PUMP CAUTION LIGHT ILLUMINATED WITH NO MAIN PRESSURE, QUANTITY IS GOOD. R & R NR 2 PRESSURE TRANSMITTER CONNECTOR PLUG. GROUND RAN ,OPS CKD GOOD.SDR UALA2009112303648Wire · shortedLEFT SYSTEM AND LEFT DEMAND PUMP LOW PRESSURE LIGHT ILLUMINATED WITH PUMP ON AND EICAS SHOWING 3000 PSI. ISOLATED M925 TIME DELAY MODULE AND CHECK RESISTANCE FROM M925 TO LOW PRESS CONNECTOR. METER SHOWED 1.6 OR WIRE GROUNDED. ISOLATED GROUND IN WIRE BUNDLESDR UALA2009102003269Connector · defectiveHYD PUMP PRI C1 LOW CENTER HYDRAULIC PRIMARY PUMP NR 1 PRESSURE WHEN COMMANDED ON, OR CENTER PRIMARY PUMP NR 1 OVERHEAT. STATUS MSG-2912015 LATCHD ER MODE. REPLACED CONNECTOR PER BOEING STANDARD ELECTRICAL PRACTICES. RE-ACTIVATED PUMP. HYD C1 PUMP WORKS NOSDR UALA2009092102970Wire · shortedL HYD PRESS & RUD RATIO EICAS, ABORTED TAKEOFF. ACP INSPECTION. ENERGY LEVELS FOUND TO BE IN THE NO SPECIAL PROCEDURE RANGE. ACP VISUAL INSPECTION OF WHEELS AND BRAKES, WITH NO DEFECTS NOTED. FAULT RECURRED 5 SEGMENTS LATER. FOUND WIRE SHORTING TO GRD AT SDR 2009FA0000730Connector · deformedCONNECTOR PLUG ADAPTER ON BACK OF SWITCH DEFORMS UNDER PRESSURE, O-RING DISPLACES, AND HYD FLUID LEAKS BY. LOSS OF HYD FLUID LED TO COMPLETE HYDRAULIC FAILURE. PILOTS FREEFALLED NOSE GEAR DOWN. (4) SIMILAR SWITCHES IN ACFT. MFG IS WORKING ON SB TO REPLACEDSDR HNAA2009061700177Wire · brokenNR 2 ENGINE HYD CAUTION LIGHT ILLUMINATED FOR APROX 30 SECONDS THEN EXTINGUISHED FOLLOWED BY NR 2 MAIN HYD PRESSURE GOING TO 0 PSI. FOUND BROKEN WIRE AT TRANSMITTER CONNECTOR PLUG REPAIRED IAW SMP GROUND RAN. OPS CHECK GOOD.SDR DXTA2009060403677Circuit Board · inoperativeWHILE ON APPROACH, FLAPS WERE SELECTED TO 15(DEG). FLAP INDICATOR DID NOT MOVE & STAB MISCOMP ANNUNCIATOR ILLUMINATED. WHEN MLG SELECTED DOWN, THEY DID NOT MOVE. APPROXIMATELY 30 SECONDS AFTER MLG WAS SELECTED DOWN, FLAPS MOVED, MLG MOVED & STAB MISCOMP ANNSDR UALA2009052701519Wire · damagedNR 1 PYLON HYD BAY HARNESS WIRE W398-201R-18 FOR L ENG HYD PUMP HAS AN IMPROPER SPLICE INSTALLED. REPAIRED WIRING REF BSWPM 20-00-13, 20-61-11 AND B767 WDM 29-11-12. RE-ASSEMBLED PLUG 0916 AND JACK D4280J TO INSTALL NEW SECTION OF WIRING.SDR HNAA2009050100141Wire · burnedNR 2 STANDBY HYD PUMP C/B POPPED DURING TAXI. REMOVED AND REPLACED NR 2 STANDBY HYD PUMP, NO FIX. FOUND BURNT WIRES BELOW 2921-P5 CONNECTOR AND REPAIRED WIRING TO 2921P5 CONNECTOR, OPS CHECKED GOOD.SDR CA090414001Connector · shorted(CAN) CIRCUIT BREAKER B250 (HYD 2 INDICATION) POPPED. WIRE DB1F22 AT CONNECTOR PLUG P12DM (NR 2 PRESSURE TRANSMITTER) SHORTED TO BACKSHELL.SDR IXXA090014OWire · defectiveDURING CRUISE FROM KPHL, BOTH AILERON AND RUDDER MANUAL LIGHTS CAME ON, HYDRAULIC SYSTEM PRESSURE INDICATED ZERO, HYDRAULIC QUANTITY SHOWS FULL. THE CREW ACCOMPLISHED LOSS OF HYDRAULICS CHECKLIST IN DC-8 QRH. THE CREW LANDED IN KTOL WITHOUT FURTHER INCIDENT.SDR UALA2009020400386Feeder Cable · faultyCTR HYD SYSTEM ELECTRIC PUMP C2 INOP. NEW P200 PANEL IS INSTALLED. AWAITING CONNECTOR. FOUND BURNED POWER FEEDER CABLES IN FWD PIT CEILING AT STA 972. REPAIRED AS PER GNMM STANDARD ELEC PRACTICES. C2 ELEC PUMP CK'S NORMAL.SDR DL75E081741Wire · brokenON TAXI OUT CREW REPORTED A PTU XFER STATUS MSG. A/C RTB. T/S SYSTEM FOUND WIRE W1260-0407-22 BROKEN ON THE X1 LEG OF RELAY K10337. MSG ONLY SHOWS WITH BOTH ENGINES RUNNING. PERFORMED CHECK OF PTU PER MM TEST OK. REPLACED LT AND RT RELAYS K10398 LEF K1044SDR ASAA0853873Connector · dirtyWHILE ACCOMPLISHING OPS CHECK OF NR 2 ENGINE AFTER ENGINE CHANGE NOTED ENGINE DRIVEN PUMP WILL NOT SHUT OFF CLEANED CONNECTOR PER SWPM 20-60-01. OPS CK GOOD. VERIFIED HYD PUMP SHUTS OFF DURING GROUND RUN REF AMM 29-11-11-710-015-002.SDR UALA2008112006586Wire · chafedWIRE BUNDLES AND COAX HAVE CHAFING, 1 EA BROKEN WIRE, NOT SECURED UNDER MAIN CABIN FLOOR STA 996 TO 1180, LBL 48. SECURED WIRE BUNDLES AND COAX UNDER MAIN CABIN FLOOR AT BS 996-1180, LBL 48 PER BSWPM 20-10-42. OPS CHECK OF HYDRAULIC RESERVOIR TEMP GOOD AND OSDR UALA2008111806570Connector · damagedCREW REPORT AIR DEMAND PUMP OVERHEAT LIGHT ILLUMINATED. LIGHT STAYED ON WITH PUMP SWITCHED OFF. CREW REPORT THAT C HYD DEM PUMP EICAS MSG FINALLY APPEARED 5 HOURS AFTER TURNING THE SWITCH ON. ALSO OVHT LIGHT STILL ON. FOUND DAMAGED CONNECTOR (D2216) TO TEMSDR HALA2008111700854Connector · looseETOPS SIGNIFICANT SYSTEM, RT HYD PRIME PUMP ANNUNCIATED ON EICAS ASSOC SWITCHED LIGHT (PRESS) ILLUMINATED BTB. C/W FIM 29-11-00, SECURED RT ENG HYD PUMP CONNECTOR D10980, OPERATED RT ENG PER MM 71-00-00, R ENG PRIMARY PRESS LIGHT EXTINGUISHED, NO MESSAGE ON ESDR UALA2008111306413Wire · faultyLT HYD QTY "LOW" PRESSURE DISPLAYED ON HYDRAULIC PAGE ALONG WITH OVERHEAD "RSVR" LIGHT ILLUMINATED. FOUND LEAKING CAP AT PRESSURIZATION MODULE. REPLACED CAP, LEAK CHECK GOOD WITH APU BLEED AND ENG BLEED. REPLACED LEFT SIDE HYDRAULIC RESERVOIR. OPS OKAY. FSDR 2008UALA06413Wire · faultyLT HYD QTY "LOW" PRESSURE DISPLAYED ON HYDRAULIC PAGE ALONG WITH OVERHEAD "RSVR" LIGHT ILLUMINATED. FOUND LEAKING CAP AT PRESSURIZATION MODULE. REPLACED CAP, LEAK CHECK GOOD WITH APU BLEED AND ENG BLEED. REPLACED LEFT SIDE HYDRAULIC RESERVOIR. OPS OKAY. FSDR CA090125006Wire · brokenACCUMULATOR IS THE ORIGINAL ONE (FLT HRS: 8880.5 AND CYCLES: 6991), THE CREW WAS ONBOARD (NO PASSENGERS) PERFORMING THE PRE FLIGHT AND WHEN SELECTING THE HYDRAULIC THEY HEARD A LOUD BANG. THE EVENT DID HAPPEN AROUND 13:30 AT DETROIT INTERNATIONAL AND THE AIRCSDR 2008UALA05919Connector · arcedCENTER SYS NR 1 ACMP CONNECTOR D482 SHOWS SIGNS OF ARCHING AND HAS A RECESSED PIN. REPLACED CONNECTOR D482P. OPS CHECKS GOOD.SDR 2008UALA05618Connector · damagedRIGHT ACMP CONNECTOR D486P, PIN 'B' IS BURNED, SHOWS SIGNS OF ARCING. REPLACED RIGHT ACMP CONNECTOR D486P PIN "B". OPS CHKS NORMAL.SDR RYN2008F00008Ground Wire · damagedLT HYDRAULIC LOW PRESSURE LIGHT AND PTU STATUS MESSAGE APPEARED ON EICAS SCREEN. REPAIRED GROUND WIRE AT THE DISCONNECT (D6240) LEFT PYLON AREA, SYSTEM OPS CHECKED NORMAL. (A)SDR 072208N523CS2Wire · damagedAFTER T/O FROM KSTP MASTER CAUTION AND STAB TRIM WARNING LIGHTS ILLUMINATED. WHILE FOLLOWING CHECKLIST HYDRAULIC CONTROL CIRCUIT BREAKER EXTENDED. AIRCRAFT DIVERTED TO KMSP AND AN EMERGENCY WAS DECLARED. LANDING GEAR WAS EXTENDED USING THE EMER SYSTEM AS PESDR UALA2008111303691Clamp · missingNR 1 ENG PYLON HYD BAY CONNECTOR D02134 SADDLE CLAMP IS MISSING. REPLACED CONNECTOR DO2134P SADDLE CLAMP. OPS CHECKS OF NR 1 ENG HYD PRESSURE INDICATION CHECKS NORMAL.SDR UALA2008111303690Connector · deterioratedNR 1 ENG HYD BAY (PYLON) CONNECTOR D00916 HAS DETERIORATED INSULATOR. REPLACED CONNECTOR D00916. OPS CHECKED AND NO DEFECTS NOTED.SDR UALA2008111303688Wire · chafedNR 1 ENG PYLON HYD BAY WIRE W390-082-18 IS CHAFED. REPLACED WIRE. OPS CHECKS GOOD.SDR UALA2008111303687Socket · damagedNR 1 ENG PYLON HYD BAY CONNECTOR D02118 HAS DAMAGED SOCKET. REPLACED SOCKET AT CONNECTOR D02118P PER BSWPM 20-60-09 AND WDM 78-34-11. OPS CHECKS GOOD. AC OK FOR SERVICE.SDR 2008UALA03691Connector · damagedNR 1 ENG PYLON HYD BAY CONNECTOR D02134 SADDLE CLAMP IS MISSING.SDR 2008UALA03682Ground Wire · chafedNR 1 HYD PUMP WIRE IS CHAFED DOWN TO PRIMARY CONDUCTOR. REPLACED GROUND WIRE PER B 767 WDM 29-11-12, SWPM 20-10-11, AND 20-20-12. OPS CHECKED ELECT HYD PUMP PER MM29-11-00, OP CHECK GOOD. AC OK FOR SERVICE.SDR COMA0860311Circuit Breaker · trippedRECEIVED A GEAR DISAGREE AND HYDRAULIC PUMP 3B WARNING DURING CLIMBOUT OF JFK, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. RESET CIRCUIT BREAKER FOR HYDRAULIC PUMP 3B AND PERFORMED GEAR SWINGS, NO DEFECTS NOTED. (S)SDR UIE2008F00014Wire · chafedDURING CRUISE, EICAS ADVISORY "HYD PRESS ENGINE 1" ON HYD SYNOPTIC. NR EDP AND DEMAND PUMPS RUNNING. THEN NOTED EDP INTERMITTENT AND IAW CHECKLIST EDP SWITCH OFF, BUT PUMP DID NOT SWITCH OFF. (EDP CONTINUED RUNNING INTERMITTENTLY AND DEMAND PUMP RUNNING). LASDR CA080611001Wire · damaged(CAN) WHILE RUNNING ACFT HYDRAULIC SYS IN HANGAR FOR CONTROL SYS FUNCTIONAL CHECKS, AN AUDIBLE BANG WAS HEARD FROM THE BACK OF THE CABIN, ALONG WITH A FLASH. (INTERIOR IS REMOVED). CIRCUIT BREAKER FOR HYDRAULIC SYS NR1 (B161) POPPED SHORTLY AFTER THIS OCCURRENSDR 2008UALA02925Connector · dirtyRIGHT HYDRAULIC SYSTEM PRESSURE FAILURE. RT HYD SYS PRESS LIGHT & RT HYD SYS ELEC DEMAND PUMP PRESS LIGHT ALONG WITH BRAKE SOURCE LIGHT ALL. VERBAL REPORT FROM FLT CREW. EVERYTHING NORMAL ON REST OF FLT. MOTORED RT ENG & OPERATED RT ELEC HYD PUMP. UNABLE TOSDR QXEA200800458Connector · corrodedPDX- FLIGHT 2187 (PDX-RDM) RETURNED TO THE FIELD FOR A HYDRAULIC PRESSURE FLUCTUATION AFTER TAKEOFF AND GEAR RETRACTION. LANDING UNEVENTFUL. MAINTENANCE WAS ABLE TO DUPLICATE AND FOUND CORROSION ON THE PINS FOR THE CONNECTOR FOR THE NR 2 TRANSDUCER. CLEANEDSDR CA080625002Connector · loose(CAN) HYDR FLUID NOTED LEAKING FROM MANUAL HYDR HAND PUMP UPON POST-TAKEOFF GEAR RETRACTION. ATTEMPT TO RE-EXTEND GEAR WITH STANDARD SYS OR MANUAL HAND PUMP FAILED. CO2 EMERGENCY DEPLOYED, GEAR EXTENSION UNSUCCESSFUL. S-PIN ON BACK OF PRIORITY VALVE REMOVED BYSDR HNAA0800137Wire · brokenAFTER TAKEOFF NR 1 ENGINE HYD PUMP C/L CAME ON AND WOULD NOT RESET, QTY AND PRESS NORMAL. SBY MX MET A/C, FOUND BROKEN WIRE AT HYD PRESSURE SWITCH CONNECTOR. REPAIRED BROKEN WIRE IAW CHAPTER 20 STANDARD MTN PRACTICES.SDR IXXA080014OWire · brokenDURING CRUISE FROM KLRD TO KDFW ,THE CREW OBSERVED ONE OF THE MAIN HYDRAULIC PUMPS WOULD NOT BYPASS. THE CREW DIVERTED TO KIAH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE MAIN HYDRAULIC PUMP SYSTEM AND FOUND A BROKEN WIRE ON THE NUMBER TWO MAIN HYSDR 45357033108Connector · crackedRED STAB OVERHEAT CAS MSG ILLUMINATED. PERFORMED CHECKLIST AND LIGHT WENT OUT AFTER SEVERAL MINUTES. IFE DECLARED BY ATC. AIR DIVERSION WITH UNEVENTFUL LANDING AND TAXI. PERFORMED GROUND RUNS WITH BOTH ENGINES AT VARIOUS POWER SETTING, CHECKED CONNECTORS AT SDR 2008UALA01267Connector · damagedLEFT HYDRAULIC SUPPLY SHUTOFF VALVE DOES NOT CYCLE (MOVE) WHEN ENGINE FIRE HANDLE IS PULLED. FOUND CONNECTOR D44045 DAMAGED SUSPECT IMPROPERLY INSTALLED. REPLACED CONNECTOR OPS CHECKED GOOD IAW MM 29-11-06. AC OK FOR SERVICE.SDR DL76L080290Wire · disconnectedON TAXI OUT, EICAS CAUTION L HYD SYS PRESS ILLUMINATED. SELECTED DEMAND PUMP TO ON. LIGHT REMAINED ILLUMINATED. ON ARRIVAL LIGHT EXTINGUISHED. VERIFY LT PUMP WORKS BOTH IN AUTO AND IN ON. SUSPECT INTERMITTENT PRESS SWITCH. FWD TO MCO AND PLAC PER MEL 29-SDR HNAA0800007Connector · dirtyDURING APPROACH, LANDING GEAR WAS SELECTED DOWN AND PILOTS OBSERVED THREE RED LIGHTS ON THE LANDING GEAR SELECTOR PANEL AND ILLUMINATION OF THE NR 2 HYDRAULIC ISOLATION VALVE CAUTION LIGHT. HYDRAULIC QUANTITIES AND PRESSURES REMAINED STEADY. PILOTS DECLARED SDR CA071221001Wire · incorrect(CAN) DURING AN AC CONVERSION IAW SB 01.00.50 THE HYD CONTROL WIRE WAS FOUND NOT CRIMPED PROPERLY IN SPLICE CONNECTOR. WIRE DH5E PULLED OUT OF SPLICE DURING HANDLING. WIRE CONNECTOR SHOW NO SIGN OF PROPER CRIMP. THE INSTALLATION OF THIS SPLICE IS MANDATED BSDR 2007UALA03678Connector · damagedHYD PUMP DEM C2 LOW CENTER HYDRAULIC DEMAND PUMP NR 2 PRESSURE WHEN COMMANDED ON, OR CENTER DEMAND PUMP NR 2 OVERHEATED. 10-05-07 AFTER TROUBLESHOOTING & HISTORY REVIEW, DETERMINED THAT NR 2 CONTROL HYD PUMP OPERATED OK FOR SEVERAL LEGS AFTER PIN D7716B (SDR CA070914018Wire Harness · shorted(CAN) DEFECT - BLUE HYDRALULIC PUMP U/S. RECTIFICATION, AC WILD BLUE PUMP WIRING SHORTED AND BURNED IN HYDRAULIC BAY DURING TROUBLESHOOTING OF UNSERVICEABLE BLUE HYDRAULIC PUMP. (TCNR 20070914018)SDR QXEA200701391Socket · damagedSEA FLIGHT NR 2262: ELEVATOR PRESSURE CAUTION ILLUMINATED AT ROTATION ON TAKEOFF. C/W EMERGENCY ABNORMAL CHECKLIST. CAUTION LIGHT EXTINGUISHED ON TOUCHDOWN. MAINTENANCE REPAIRED SOCKET FOR NR 1 SYSTEM PRESS SWITCH. C/W FUNCTIONAL TEST OF NR 3 SYSTEM. HYD
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