Lockheed 188A

Service difficulty reports · 98

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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 aircraft_model_key = '188A'
  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.

SDR CA150625003Actuator · malfunctioned(CAN) THE NR 2 ENG LOST POWER ON THE OVERSHOT FROM A BOMB RUN & WAS SHUTDOWN, RETURNED TO BASE. FOUND THE NR 2 PROPELLER ROTARY ACTUATOR TO BE OVER TRAVELLING. REPLACED U S ACTUATOR WITH A SERVICEABLE UNIT & RETURNED THE ACFT TO SERVICE.Jun 24, 2015 · Lkheed 188A · Propeller Controlling SystemSDR CA140707015Valve · malfunctioned(CAN) ON TAKEOFF LOW HORSEPOWER, HIGH FUEL FLOW, AND HIGH T.I.T. WERE OBSERVED. TAKEOFF WAS ABORTED PRIOR TO BRAKE RELEASE. MAINTENANCE FOUND SPEED SENSE VALVE NOT CLOSING 5TH AND 10TH STAGES. VALVE REPLACED.Jul 3, 2014 · Lkheed 188A · Compressor Bleed ControlSDR CA140702010Gasket · leaking(CAN) NR 2 HYD SYS LOST ALL FLUID QTY. ACFT RETURNED TO THE AIRPORT. INSPECTED NR 2 HYDRAULIC SYSTEM, LEAK FOUND AT FILTER HOUSING, LEAKING GASKET FOUND AND REPLACED.Jun 24, 2014 · Lkheed 188A · Hydraulic System, MainSDR CA130813004Controller · malfunctioned(CAN) NR 4 ENGINE RPM DECAYED TO BOTTOM OF NORMAL RANGE AT HIGH POWER DURING TAKEOFF, BOMBING BUT WAS NORMAL IN CLIMB AND CRUISE. AFTER TROUBLESHOOTING THE ROTARY ACTUATOR WAS REPLACED AND PROBLEM WAS FIXED.Aug 11, 2013 · Lkheed 188A · Propeller Controlling SystemSDR CA130729021Regulator · malfunctioned(CAN) PROPELLER FAILED TO GOVERN RPM IN FLIGHT. UPON ADVANCEMENT OF POWER FOR ASSOCIATED ENGINE FCU HAD TO LIMIT ENGINE RPM VIA FUEL TOPPING GOVERNOR. MAINTENANCE CREW REPLACED GOVERNOR VALVE OF PROPELLER AND COMPLETED A PITCH LOCK CHECK AND DETERMINED PROPEJul 26, 2013 · Lkheed 188A · Propeller Controlling SystemSDR CA130515013Fire Detector · malfunctioned(CAN) PILOTS REPORTED A ZONE 1 FIRE INDICATION APPROXIMATELY 20 MILES FROM THE AIRPORT WHILE INBOUND FOR LANDING. AFTER PULLING THE POWER BACK TO IDLE NO CHANGE. THEY E-HANDLED THE ENGINE AND THE INDICATION WENT OUT IMMEDIATELY. ON THE GROUND WE INSPECTED VIMay 14, 2013 · Lkheed 188A · Fire DetectionSDR CA130513023Transfer Tube · misinstalled(CAN) PROPELLER NOT REGULATING OIL PRESSURE IN FLIGHT. RPM WOULD SWING WITH POWER LEVER CHANGES. UPON INVESTIGATION IT WAS DISCOVERED THAT AN O-RING AND BACK-UP RING COMBINATION INSTALLED ON AN INTERNAL TRANSFER TUBE ASSY IN THE PROPELLER HUB WERE REVERSED CAMay 9, 2013 · Lkheed 188A · Propeller AssemblySDR CA110602005Pulley · brokenDURING INITIAL TAXI FOR A MX TEST FLIGHT, THE FLIGHT CREW RECEIVED A FLAP ASYMMETRIC WARNING. THE ACFT WAS RETURNED TO THE HANGAR WHERE UPON INITIAL INVESTIGATION IT WAS FOUND THAT THE RT FLAP ASYMMETRIC CABLE LOCATED IN THE RT FLAP BAY WAS BROKEN WITH SIGNS OJun 1, 2011 · Lkheed 188A · Trailing Edge Flap Control SystemSDR CA100531005Nut · brokenAFTER TAKEOFF FOR A FIRE DISPATCH , THE NR 1 FIRE LIGHT AND BELL SOUNDED. THE LIGHT AND BELL QUIT AFTER THE POWER WAS REDUCED FROM TAKEOFF POWER. AFTER LANDING , MX FOUND THAT THE POWER TURBINE ON THE NR 1 ENGINE HAD FAILED. THE NEXT DAY THE ACFT WAS FLOWN OMay 18, 2010 · Lkheed 188A · Turbine SectionSDR CA090727010Engine · power lossDISPATCHED FOR FIRE ACTION. AFTER RETARDANT DROP NR 2 RPM DROOPED TO 13,500. RPM BEGAN TO HUNT BETWEEN 13500, 13300 (13820 NORMAL). NR 2 ENGINE SHUTDOWN AND SECURED IAW COMPANY SOP. ONE ENG INOP LANDING CARRIED OUT. MX IS TROUBLESHOOTING.Jul 26, 2009 · Lkheed 188A · Engine (Turbine/Turboprop)SDR CA090615011Module · burned out(CAN) SEVEN MINUTES FROM AIRPORT, CREW NOTICED SMOKE COMING FROM ELECTRICAL BAY. WITH NO SYSTEMS FAILED, THE CREW RETURNED TO DEPARTURE WITH NO INCIDENTS. MX FOUND NR 1 PROP PHASE SYNC MODULE HAD BURNED OUT. ALL ACFT WIRES WERE CHECKED OUT TO BE OK, THE SYS Jun 13, 2009 · Lkheed 188A · Propeller Synchronizer SectionSDR CA080422003Coupler · unknown(CAN) DURING START SEQUENCE OF NR 4 ENGINE, IT WAS OBSERVED THAT RPM AND ACCELERATION CLIMBED TOO FAST, BEFORE LIGHT OFF, ENGINE START ABORTED AND FOUND ENGINE DECOUPLED FROM GEARBOX. SUSPECT TORQUE SHAFT COUPLER (TC NR 20080422003)Apr 20, 2008 · Lkheed 188A · Accessory GearboxesSDR CA070918002Panel · cracked(CAN) AFTER A (WATER - FIRE SUPPRESSION) BOMBING MISSION, FUEL WAS FOUND LEAKING FROM A CRACK THAT WAS COMING FROM AN OLD REPAIR. THE A/C WAS DOWN LOADED WITH WEIGHT AND THE A/C WAS FERRIED TO THE COMPANY MAINTENANCE STATION. (TC NR 20070918002)Sep 16, 2007 · Lkheed 188A · Wing, Plate/SkinSDR CA060613003Seal · leaking(CAN) AFTER A WATER BOMBING RUN CLIMB OUT NR 2 ENGINE WAS SHOWING TWO GALLONS LOW ON OIL. THERE WAS NO OTHER ABNORMAL INDICATIONS, THE CREW DID A PRECAUTIONARY SHUT DOWN. MAINTENANCE FOUND THE SCAVENGE PUMP SEAL TO BE LEAKING OIL BY, THE SEAL WAS REPLACED AND Jun 11, 2006 · Lkheed 188A · Turbine Engine Oil SystemSDR CA050908003Coupling · broken(CAN) THE A/C HAD FINISHED IT'S THIRD DROP ON A FIRE BOMBING PRACTICE, FLAPS WOULD NOT RETRACT AND THE FLAP ASYMMETRIC LIGHT WAS ON. THE FLAP ASYMMETRY CHECKLIST WAS COMPLETED AND THE A/C RETURNED TO BASE. MAINTENANCE FOUND A BROKEN TORQUE TUBE COUPLING, THESep 5, 2005 · Lkheed 188A · Trailing Edge Flap Control SystemSDR ZIAA04082Fire Loop · false indicationSHUTDOWN NR 3 ENGINE DUE TO ZONE 1 FIRE WARNING AT 2004Z. DISCHARGED FIRE BOTTLES. REMOVED AND REPLACED ZONE 1 FIRE LOOP IAW L188 MM 26-1-0. NO FIRE WARNING NOTED ON EXTENDED GROUND RUN AT 847 DEGREES.Sep 28, 2004 · N346HA · Lkheed 188A · Fire DetectionSDR ZIAA04067Control Handle · out of rigLANDING GEAR HANDLE APPEARS NOT TO GO TO THE FULL UP POSITION. RIGHT MAIN GEAR UNSAFE LIGHT STAYS ON. RIGGED RIGHT LANDING GEAR UPLOCK MECHANISM IAW L-188 MM 32-1-0. ZIAA (M)Aug 4, 2004 · N343HA · Lkheed 188A · Landing Gear SelectorSDR CA040720005Propeller · malfunctionedPROPELLER OVERSPEED ON DESCENT INTO XXXX, THE ENGINE WAS SHUT DOWN AND AIRCRAFT LANDED WITHOUT INCIDENT. PROP ASSEMBLY WAS CHANGED, GROUND RUN AND PITCH LOCK TESTED SERVICABLE. AIRCRAFT WAS RETURNED TO SERVICE.Jul 17, 2004 · Lkheed 188A · Propeller GovernorSDR ZIAA03005Panel · corrodedYIP - PLANK NR 3 JUST AFT OF 2-3 PLANK SEAM CORROSION BETWEEN RISERS AT BL61R, CENTER DRY BAY, LOWER SURFACE. REMOVED CORROSION AND TREATED AREA. REPAIRED PER LOCKHEED S/B 678 DWG 841795. (M)Nov 3, 2003 · N346HA · Lkheed 188A · Wing, Plate/SkinSDR ZIAA03004Panel · crackedCRACK NOTED IN CENTER DRY BAY RIGHT WING AT PLANK SEAM 5-6 AT BL37R. ROUTED OUT CRACK AND INSTALLED FILLET PER L-188 SRM 51-2-7. REPAIRED PER L-188 SRM 57-2-1 FIG 3 SHEET 15. (M)Nov 3, 2003 · N346HA · Lkheed 188A · Wing, Plate/SkinSDR ZIAA03003Relay · overheatedLANDED IN TORONTO DUE TO ELECTRICAL SMOKE COMING FROM BEHIND COCKPIT CIRCUIT BREAKER PANEL. REMOVED AND REPLACED NR 2 MAIN DC BUS REVERSE CURRENT CUTOUT RELAY IAW L-188 MM CPT 24-0. ALL SYSTEM CHECK NORMAL. (M)May 21, 2003 · N5512 · Lkheed 188A · AC Power Distribution SystemSDR ZIAA03002Skin · corrodedYIP - FOUND CORROSION ON LEFT WING LOWER SURFACE NR 4 WING PLANK TRAILING EDGE BETWEEN APPROXIMATE LWS 448 AND LWS 533. REMOVED CORRODED SECTION OF NR 4 WING PLANK TRAILING EDGE PER ZANTOP DWG S59-R01. (M)Feb 18, 2003 · N343HA · Lkheed 188A · Wing, Plate/SkinSDR CA020829006Structure · cracked(CAN) CRACK ALONG EXISTING PATH FOUND. AIRCRAFT RETURNED TO MAINTENANCE BASE. CRACK IS OUTBOARD OF BL-165 19 INCHESAug 8, 2002 · Lkheed 188A · Wing Main, Frame StructureSDR ZIA2002F00000Battery · dischargedIN CRUISE, EN-ROUTE, LOST (A) BUS IN FLIGHT. LOST ALL RADIOS BOTH COMMS AND BOTH NAVS. OVERWEIGHT LANDING. RESET ALL MAIN FEEDER C/BS OPS. CHECKED GOOD ON GROUND RUN-UP. REMOVED MAIN AC BATTERY AND REPAIRED BATTERY CONNECTOR, OPS CHECKED GOOD COMPLIED WITHMay 14, 2002 · N346HA · Lkheed 188A · Battery/Charger SystemSDR TM92002F00000Battery · discharged(LEAD ACID BATTERY) IN CRUISE, ENROUTE LOST (A) BUS IN FLIGHT. LOST ALL RADIOS, BOTH COMMS AND BOTH NAVS. OVERWEIGHT LANDING. RESET ALL MAIN FEEDER C/BS. OPS CHECKED GOOD ON GROUND RUN-UP. REMOVED AND REPLACED MAIN AIRCRAFT BATTERY CONNECTOR, OPS CHECKED May 14, 2002 · N436HA · Lkheed 188A · Battery/Charger SystemSDR ZIAA06001Plank · crackedNR 2 PLANK CRACKED. LEFT WING INBOARD OF CENTER RISER. (M)Jun 24, 2001 · N346HA · Lkheed 188A · Wing, Plate/SkinSDR ZIAA00017Panel · crackedYIP - LEFT DRY BAY UPPER SURFACE, CRACK INDICATION COMING FROM FASTENER HOLE BETWEEN RISERS 46-47 AT WS 200, APPROX 1.5 INCH IN LENGTH. CLEANED CRACK PER L-188 SRM 51-2-7 PAGE 2. REPAIRED PER ZANTOP DWG M16-R01. (M)Nov 4, 2000 · N346HA · Lkheed 188A · Wing, Plate/SkinSDR ZIAA00011Pump · leakingYIP - IN FLIGHT NR 1A PUMP LOW PRESSURE LIGHT CAME ON, TURNED OFF. REMOVED AND REPLACED NR 1A HYD PUMP PER CARD N29-01. OPS AND LEAK CHECKS GOOD ON GROUND. (M)Sep 30, 2000 · N346HA · Lkheed 188A · Hydraulic Pump (Electric/Engine), MainSDR ZIAA00012Stringer · corrodedYIP - LONGERON NR 29 ON RIGHT FUSELAGE STATION 416 FOUND CORRODED. REPAIRED LONGERON PER L-188 DRAWING NR L55-R01. (M)Sep 28, 2000 · N344HA · Lkheed 188A · Fuselage Main, Longeron/StringerSDR 20010112SG015Fitting · wornYIP - FORWARD CARGO DOOR, DOOR MOUNTED LINK ARM HAS EXCESS MOTION AT DOOR ATTACH POINT. REPAIRED FORWARD CARGO DOOR ATTACH POINTS IAW ZANTOP DRAWING NR L84-R01. REF ZIAA00013. (M)Sep 28, 2000 · N344HA · Lkheed 188A · Cargo/Baggage DoorsSDR ZIAA00013Fitting · wornYIP - FORWARD CARGO DOOR, DOOR MOUNTED LINK ARM HAS EXCESS MOTION AT DOOR ATTACH POINT. REPAIRED FORWARD CARGO DOOR ATTACH POINTS IAW ZANTOP DRAWING NR L84-R01. (M)Sep 28, 2000 · N344HA · Lkheed 188A · Cargo/Baggage DoorsSDR ZIAA00015Skin · corrodedYIP - EVIDENCE OF CORROSION ON SEVERAL AREAS OF SKIN BETWEEN FS 445-588 RIGHT SIDE. NUMEROUS AREAS OF SURFACE CORROSION ON STRINGERS UNDER SKIN. REMOVED SKIN SECTION, FOUND CORROSION TO BE BEYOND LIMITS. FABRIATED NEW SKIN PANEL. REPLACED SKIN PER L-188 SRSep 14, 2000 · N344HA · Lkheed 188A · Fuselage Main, Plate/SkinSDR ZIAA00014Stringer · crackedYIP - FOUND FUSELAGE STATION 549 BELOW STRINGER 51 CRACKED ON RIGHT SIDE. REPAIRED CRACKED STRINGER IAW L-188 53-2-3 SRM. (M)Sep 13, 2000 · N344HA · Lkheed 188A · Fuselage Main, Longeron/StringerSDR ZIAA00010Panel · crackedYIP - LEFT DRY BAY, UPPER SURFACE, CRACK INDICATION BETWEEN NR 45-46 RISERS AT LT WS 200, CRACK SIZE 1.25 BY .375. CLEANED OUT CRACK PER L-188 SRM 51-2-7 PAGE 2. REPAIRED PER L-188 SRM 57-2-1 PAGE 19. (M)Jul 27, 2000 · N5512 · Lkheed 188A · Wing, Plate/SkinSDR ZIAA00009Panel · crackedYIP - LEFT DRY BAY, UPPER SURFACE, CRACK INDICATION COMING FROM UNDER FASTENER BETWEEN NR 19 AND 20 RISERS AT LT WS 170, CRACK SIZE 1.25 BY .5. CLEANED OUT CRACK PER L-188 SRM 51-2-7 PAGE 2. REPAIRED PER ZANTOP DRAWING L33-R01. (M)Jul 27, 2000 · N5512 · Lkheed 188A · Wing, Plate/SkinSDR ZIAA00008Panel · crackedYIP - LEFT DRY BAY, UPPER SURFACE, CRACK INDICATION IN FORWARD RADIUS OF NR 19 RISER AT LT WS 170, CRACK SIZE 1X.375. CLEANED OUT CRACK PER L-188 SRM 51-2-7 PAGE 2. REPAIRED PER ZANTOP DWG L33-R01. (M)Jul 27, 2000 · N5512 · Lkheed 188A · Wing, Plate/SkinSDR ZIAA00007Panel · crackedYIP - LEFT DRY BAY, UPPER SURFACE, CRACK INDICATION COMING FROM UNDER FASTENER BETWEEN NR 17-18 RISERS AT LT WS 170, CRACK SIZE .75 INCH BY .375. CLEANED OUT CRACK PER L-188 SRM 51-2-7 PAGE 2. REPAIRED PER ZANTOP DWG L33-R01. (M)Jul 27, 2000 · N5512 · Lkheed 188A · Wing, Plate/SkinSDR ZIAA01001Generator · failedYIP - SHUTDOWN ENGINE BECAUSE OF GENERATOR DISENGAGE LIGHT. REMOVED AND REPLACED NR 1 GENERATOR IAW N24-10. (M)Apr 26, 2000 · N346HA · Lkheed 188A · AC Generator-AlternatorSDR ZIAA00005Panel · crackedYIP - CRACK IND NR 1 UPPER RISER FORWARD RADIUS AT APPROX LWS 197, DRY BAY, EIGHT INCH CRACK. REPAIRED RISER NR 1 PER ZANTOP DWG K41-R02. (M)Feb 25, 2000 · N5522 · Lkheed 188A · Wing, Plate/SkinSDR ZIAA00004Panel · crackedYIP - CRACK BETWEEN RISERS 19 AND 20, UPPER PLANK AT LWS 209. REPAIRED PER SB675 LOCKHEED DWG 842362. (M)Feb 25, 2000 · N5522 · Lkheed 188A · Wing, Plate/SkinSDR ZIAA00003Panel · crackedYIP - CRACK IN RADIUS OF NR 14 RISER, APPROX RWS 205 UPPER SURFACE, DRY BAY. REPAIRED RISER NR 14 PER ZANTOP DWG K41-R01. (M)Feb 15, 2000 · N5522 · Lkheed 188A · Wing, Plate/SkinSDR ZIAA00002Skin · corrodedYIP - RIGHT LOWER FUSELAGE, FORWARD OF WING FRONT BEAM CORRODED, FS 552-565. REMOVED CORRODED SECTION OF FUSELAGE SKIN. REPAIRED FUSELAGE SKIN AS PER L-188 SRM REF 53-2-1 FIG 2 SHEET 3. (M)Feb 7, 2000 · N5522 · Lkheed 188A · Fuselage Main, Plate/SkinSDR ZIAA98040Fire Loop · malfunctionedMEM - SHUTDOWN NR 4 ENGINE DUE TO FIRE WARNING IN ZONES 2/3 AT 1811Z. FIRED BOTTLE AND LIGHTS WENT OUT. AT 1838Z FIRE WARNING IN ZONES 2/3, ENGINE NR 4 CAME ON AGAIN. FIRED SECOND BOTTLE AND WARNING REMAINED ON. DIVERTED TO MEM. REMOVED AND REPLACED NR 3/Oct 23, 1998 · N5512 · Lkheed 188A · Fire DetectionSDR ZIAA98032Panel · crackedYIP - PER AD 66-04-02 INSPECTION, LEFT WING LOWER SURFACE DRY BAY, 2 INCH LONG SUBSRUFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 3 AT 2/3 PLANK JOINT, LWS 166-168. ROUTED OUT CRACKED AREA, LWS164 TO LWS168, PER SB620. FABRICATED AND INSTALLED REPAIR PER SAug 18, 1998 · N346HA · Lkheed 188A · Wing, Plate/SkinSDR ZIAA98031Panel · crackedYIP - PER AD 66-04-02 INSPECTION, LT WING UPPER SURFACE-DRY BAY, 7 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 2 AT 2/3 PLANK JOINT, LWS 172-179. ROUTED OUT CRACKED AREA, LWS 176 TO LWS 180, PER SB 620. REPAIRED PER ZIA DRAWING F25-R07. (Aug 18, 1998 · N346HA · Lkheed 188A · Wing, Plate/SkinSDR ZIAA98030Panel · crackedYIP - PER AD 66-04-02 INSPECTION, LEFT WING UPPER SURFACE-DRY BAY. 5 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 7 AT 6/7 PLANK JOINT, LWS 188-193. ROUTED OUT CRACKED AREA, LWS 188.5 TO LWS197.5, PER SB 620. FABRICATED AND INSTALLED REPAIAug 18, 1998 · N346HA · Lkheed 188A · Wing, Plate/SkinSDR ZIAA98029Panel · crackedYIP - PER AD 66-04-02 INSPECTION, LEFT WING UPPER SURFACE-DRY BAY. 2 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 1 AT 1/2 PLANK JOINT, LWS 181-183. ROUTED OUT CRACKED AREA, LWS176.5 TO LWS180.5, PER SB620. REPAIRED PER ZIA DRAWING F25-R07Aug 18, 1998 · N346HA · Lkheed 188A · Wing, Plate/SkinSDR ZIAA98028Panel · crackedYIP - PER AD 66-04-02 INSPECTION, LEFT WING UPPER SURFACE-DRY BAY. 2 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 1 AT 1/2 PLANK JOINT, LWS 196-198. ROUTED OUT CRACKED AREA, LWS194 TO LWS196.5, PER SB620. REPAIRED PER ZIA DRAWING F25-R07. Aug 18, 1998 · N346HA · Lkheed 188A · Wing, Plate/SkinSDR ZIAA98027Panel · crackedYIP - PER AD 66-04-02 INSPECTION, LEFT WING NR 2 FUEL TANK-LOWER SURFACE. 2 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 4 AT 3/4 PLANK JOINT, LWS 115-117. ROUTED OUT CRACKED AREA, LWS115 TO LWS119, PER SB620. REPAIRED PER ZIA DRAWING F25-Aug 18, 1998 · N346HA · Lkheed 188A · Wing, Plate/SkinSDR ZIAA98038Panel · crackedYIP - PER AD 66-04-02 INSPECTION, LEFT WING NR 2 FUEL TANK UPPER SURFACE. THREE INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 9 AT 8/9 JOINT, LWS 88-91. ROUTED OUT CRACKED AREA, WS 87 TO WS 90 PER SB620. INSTALLED REPAIR PER SB620 DRAWING 8Aug 17, 1998 · N346HA · Lkheed 188A · Wing, Plate/Skin
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