GE CF6-80 series

Service difficulty reports · 1,092

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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 engine_model_key = 'CF680'
  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 HALA2009122400602Circuit Card · unserviceableETOPS SIGNIFICANT SYS - WHILE PERFORMING ENG TEST3 GRD IDLE TEST, LT ENG WOULD NOT RETURN TO GRD IDLE. CHK'D FOR 28VDC AT SOLENOID ON LT ENG MEC, NONE FOUND. CHK'D FOR 28VDC AT PIN 32 ON EEC DISCRETE CARD NONE FOUND. CONFIRMED 28VDC AT INPUT TO CARD AT PIN 62Dec 24, 2009 · N597HA · Boeing 767332 · Fuel Controlling SystemSDR DL76G092028Apu · failedAPU FAILED ON PUSHBACK WITH A FAULT LIGHT ILLUMAINATED. AFTER SYS RESET TEST PERFORMED WITH PNEUMATIC LOAD APPLIED. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.Dec 22, 2009 · N1602 · Boeing 767332 · Airborne Auxiliary Power Unit (APU) SystemSDR HALA2009120800575Engine · malfunctionedETOPS SIGNIFICANT SYS - ENG NR 1 EPR 106.1; N1 97.6; EGT 723; N2 96.9; FF 4.8 FUEL FLOW IN NR 1 ENG 3-4 HUNDRED LBS HIGHER. ENG NR 2 EPR 106.1; N1 95.5; EGT 706; N2 95.9;FF 4.5. INSP THROTTLES FOR BINDING, PLAY OR OTHER DEFECTS. NONE NOTED. PERF HIGH POWER Dec 8, 2009 · N596HA · Boeing 767332 · Engine (Turbine/Turboprop)SDR DL764091864Start Valve · inoperativeNR 2 ENG WILL NOT START. NO ROTATION. FWD TO MCO PER MEL 80-00-02 AND PLACARD. RTN TO REMOTE PAD. NOT A RTB. RT ENGINE START VALVE OPS CHECK NORMAL. FOUND NR 1 ENGINE LT ST VALVE INOP, REPLACED START VALVE PER M/M. OPS CHECK GOOD MCO/PLA REMOVED.Nov 28, 2009 · N835MH · Boeing 767432ER · Engine Start Valves/ControlsSDR IPXA10659479Floor Panel · crackedREF D413411, 4 IN CRACK/ DENT IN MAIN CARGO FLOOR POSITION 8R OTBD PANE PANEL. STA835 RBL85. ACCOMPLISHED MAJOR REPAIR IAW EO B767-5320-9693-G, REF N/R 398499.Nov 21, 2009 · N317UP · Boeing 76734AF · Fuselage Floor PanelSDR AALA20091116MIA01Fuel Control · failedLEFT ENGINE WOULD NOT DECELERATE BELOW 69 PERCENT N1 ON DESCENT. CREW TURNED OFF BOTH ELECTRONIC ENGINE CONTROLS AND POWER SURGED TO 79 PERCENT N1. LANDED MIA WITHOUT INCIDENT. REPLACED MAIN ENGINE FUEL CONTROL FOR NUMBER ONE ENGINE. SYSTEM GROUND CHECKED Nov 16, 2009 · N397AN · Boeing 767323 · Fuel Control/Turbine EnginesSDR HALA2009111400527Throttle · lack of lubeETOP SIGNIFICANT SYS - RT ENG THROTTLE STICK/BINDS. CLEANED AND LUBED THRUST LEVER (RT ENG) MECHANISM AT LEVER QUADRANT AND CLUTCH PACK ASSY OPS CKS NORMAL REF AMM 76-11-00, NO DEFECTS NOTED.Nov 14, 2009 · N596HA · Boeing 767332 · Power LeverSDR HALA2009111300526Bypass Switch · malfunctionedETOPS SIGNIFICANT SYS - STATUS MSG "R OIL FILTER" DISPLAYED, NO EICAS ADVISORY MSG. ALL ENG. PARAMETERS NORM. INSPECTED RT ENG IAW FIM 79-21-00. CHANGED RT ENGINE OIL FILTER BYPASS SWITCH IAW MM 79-35-01. OPS AND LEAK CHECK OK. NO LEAKS NOTED ON MAIN OIL Nov 13, 2009 · N594HA · Boeing 767332 · Turbine Engine Oil SystemSDR HALA2009092300436Liner · damagedETOPS SIGNIFICANT SYS -DURING OVERTEMP INSP FOUND INBD LINER FOR OUTLET GUIDE VANE AT 11 O'CLOCK POS LOOKING FROM FWD LOOKING AFT LIFTING, DUE TO DAMAGE AROUND FASTENERS. RMVD INBD LINER AND OGV AND FAIRINGS IAW AMM 72-33-03. INSTLD ACCOUSTICAL LINER SEGMENTSep 23, 2009 · N596HA · Boeing 767332 · Engine (Turbine/Turboprop)SDR TAMF20090039SFailsafe · corrodedDURING (SC3) CHECK INSP, WAS FOUND FUSELAGE SECTION 43 CARGO SURROUND STRUCTURE WITH CORROSION, FWD LARGE CARGO DOOR STRUCTURE MAIN STILL FAILSAFE STRAP, REPAIR ACCOMPLISHED IAW EWO 767-53-026, SR 1-225221220.Sep 16, 2009 · N770QT · Boeing 767241 · Cargo/Baggage DoorsSDR TAMF20090040SStructure · corrodedDURING (SC3) CHECK INSP WAS FOUND LARGE CARGO DOOR LATCH FITTING BORE WITH CORROSION STA 478-618, REPAIR ACCOMPLISHED IAW EWO 767-53-097 SR 1-1417346043.Sep 8, 2009 · N770QT · Boeing 767241 · Cargo/Baggage DoorsSDR DL764091451Warning System · activatedDURING RT ENG START WHEN AIR LOAD APPLIED APU FAULT LIGHT ILLUMINATED AND APU SHUTDOWN. ENGINE START ON STAND FAILED WITH RESULTING STATUS MSG. APU FUEL CONTROL. APU FWD TO MCO AS PER MEL 49-11-01B WITH DISPATCH APPROVAL. PLACARD INSTALLED. A/C OK FOR SERVSep 3, 2009 · N833MH · Boeing 767432ER · APU Indicating SystemSDR FDEA200908313171Seat Track · damagedMAIN CABIN SEAT TRACK SCALLOP IS BROKEN BETWEEN FR 63 AND FR 64; RT BUTTLINE 37 INCHES FROM CTR. REMOVED DAMAGED AREA REF SRM 71-73-10, PARA F. MATERIAL LOSS ALLOWED 0.016. MATERIAL REMOVED 0.155; FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16; PG 105. INSTAug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200908313172Floorboard · puncturedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 251 UH IS PUNCTURED AND CRUSHED FROM FRAME 62 TO FRAME 63. DAMAGED FLOOR PANEL REMOVED. NEW PANEL (251 UH) FABRICATED AND INSTALLED IAW AMM 53-10-23-4 AND DWG SRZ 25-005, REV "H".Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313173Floorboard · puncturedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 252 UH IS PUNCTURED AND CRUSHED FROM FRAME 62 TO FRAME 63. DAMAGED FLOOR PANEL (252 UH) REMOVED. NEW PANEL (252 UH) FABRICATED AND INSTALLED IAW AMM 53-10-23-4 AND DWG SRZ 25-005, REV "H".Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313174Floorboard · puncturedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 251 PH IS PUNCTURED AND CRUSHED FROM FRAME 58 TO FRAME 60. DAMAGED FLOOR PANEL 252 PH REMOVED. NEW PANEL 252 PH FABRICATED AND INSTALLED IAW AMM 53-10-23-4 AND DWG SRZ 25-005, REV "H".Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313175Floorboard · puncturedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 EK IS PUNCTURED AND CRUSHED FROM FRAME 51 TO FRAME 54. REMOVED DAMAGED FLOOR PANEL 242 EK. FABRICATED NEW FLOOR PANEL 242 EK, IAW DWG SRZ 25-005, REV "H". INSTALLED PANEL IAW AMM 53-10-23-4.Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313176Floorboard · puncturedMAIN CABIN FLOORBOARD 242 ZJ IS PUNCTURED AND CRUSHED FROM FRAME 47 TO FRAME 51. FABRICATED FLOORBOARD IAW (DWG SRZ 25-005, REV "H"). PART MARKED FLOORBOARD IAW GMM 7-0-1000.Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313177Floorboard · puncturedMAIN CABIN FLOORBOARD 242 AJ IS PUNCTURED AND CRUSHED FROM FRAME 47 TO FRAME 51. LOCATED FASTENER HOLES AND PREPED EDGE FOR POTTING IAW (DWG SRZ 25-005, REV "H"). PART MARKED IAW GMM 7-0-1000.Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313178Floorboard · puncturedMAIN CABIN FLOORBOARD 241 AJ IS PUNCTURED AND CRUSHED FROM FRAME 47 TO FRAME 51. FABRICATED FLOORBOARD IAW (DWG SRZ 25-005, REV "H"). PART MARKED FLOORBOARD IAW GMM 7-0-1000.Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313179Floor Panel · puncturedMAIN CABIN FLOORBOARD 242 UJ IS PUNCTURED AND CRUSHED FROM FRAME 43 TO FRAME 47. REMOVED DAMAGED FLOOR PANEL 242 UJ. FABRICATED NEW FLOOR PANEL 242 UJ, IAW DWG SRZ 25-005, REV "H". INSTALLED PANEL IAW AMM 53-10-23-4.Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313180Floorboard · puncturedMAIN CABIN FLOORBOARD 242 QJ IS PUNCTURED AND CRUSHED FROM FRAME 40 TO FRAME 43. FABRICATED NEW PANEL IAW (DWG SRZ 25-005, REV "H"). PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL IAW AMM 53-10-23-4.Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313181Floorboard · puncturedMAIN CABIN FLOORBOARD 242 TH IS PUNCTURED AND CRUSHED FROM FRAME 40 TO FRAME 43. FABRICATED NEW FLOOR PANEL 241TH IAW DWG SRZ 25-005, REV "H". INSTALLED PANEL IAW AMM 53-10-23-4.Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313182Floorboard · puncturedMAIN CABIN FLOORBOARD 232 YG IS PUNCTURED AND CRUSHED FROM FRAME 28 TO FRAME 30. REMOVED PANEL (232 YG) AMM 53-10-23-4. FABRICATED NEW PANEL IAW (DWG SRZ 25-005, REV "H"). PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL AMM 53-10-23-4.Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313183Floorboard · puncturedMAIN CABIN FLOORBOARD 242 BF IS PUNCTURED AND CRUSHED FROM FRAME 31 TO FRAME 34. REMOVED PANEL 242 BF REF AMM 53-10-23-4. FABRICATED NEW PANEL IAW DWG SRZ 25-005, REV "H". PART MARKED PANEL IAW GMM 7-0-1000. INSTALLED PANEL REF AMM 53-10-23-4.Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313184Floorboard · puncturedMAIN CABIN FLOORBOARD 242 GF IS PUNCTURED AND CRUSHED FROM FRAME 34 TO FRAME 37. REMOVED PANEL (242 GF) AMM 53-10-23-4. FABRICATED NEW PANEL IAW (DWG SRZ 25-005, REV "H"). PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL IAW AMM 53-10-23-4.Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313189Seat Track · damagedMAIN CABIN SEAT TRACK SCALLOP IS BROKEN AT BS 4140 - BS 4120; LBL Y 440 - LBL Y 440. CHECKED DAMAGED SCALLOP 0.170 REMAINING. SCALLOP WORN BEYOND MINIMUM ALLOWABLE LIMITS OF 0.260 IAW SRM 53-10-16, PG 105. REMOVED SEAT TRACK SECTION IAW SRM 53-10-156, PG 2Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR HALA2009082500384Engine · vibrationETOPS SIGNIFICANT SYS - VIBRATION ON RT ENG LPT=5.0 DURING CLIMB LPT=3.6 DURING CRUISE. ON LANDING FOUND METAL PIECES IN EXHAUST DUCTING, ALSO FOUND DAMAGE TO TURBINE BLADES. REMOVED AND REPLACED NR 2 ENG. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.Aug 25, 2009 · N598HA · Boeing 767332 · Engine (Turbine/Turboprop)SDR HALA2009082200378Anti-Ice Valve · failedETOPS SIGNIFICANT SYS - SELECTED LT ENG ANTI-ICE SWITCH TO ON. LT ENG ANTI-ICE EICAS MESSAGE ILLUMINATED. REMOVED AND REPLACED LT ENG ANTI-ICE VALVE IAW AMM 30-21-03. ALL CK NML.Aug 22, 2009 · N596HA · Boeing 767332 · Engine Anti-Icing SystemSDR HALA2009082000375Fmc · malfunctionedETOPS SIGNIFICANT SYS - LT AND RT FMC STUCK ON CROSSLOAD MODE. RELOADED CURRENT SOFTWARE ON LT FMC IAW AMM 34-61-00. REMOVED AND REPLACED RT FMC IAW AMM 34-61-00. ACCOMPLISHED CURRENT NAVIGATION DATABASE UPLOAD. FMC SYS OPS NORMAL.Aug 20, 2009 · N594HA · Boeing 767332 · Flight Management Computing Software SystemSDR HALA2009082000376Heater · malfunctionedETOPS SIGNIFICANT SYS - BTB - AFTER START, EICAS MESSAGE "PROBE HEAT" OVERHEAD CAPTS PITOT, LAOA, R AUX PITOT HEAT. MAINT FOUND L-17 AND L-18 AND K-14,15,16, 17 PULLED. THESE BREAKER WERE PULLED TO PERFORM MX IAW TASK CARD 767-3-HAL005. ALSO VERIFIED ALL OTAug 20, 2009 · N596HA · Boeing 767332 · Pitot/Static Anti-Ice SystemSDR HALA2009081900368Control Valve · malfunctionedETOPS SIGNIFICANT SYS - BTB - LT PACK OFF LIGHT AND PACK INOP EICAS MESSAGE DO NOT COME ON WHEN LT PACK IS OFF. CHECKED WIRING IAW WDM 21-51-11 REPLACED LT PACK FLOW CONTROL VALVE IAW AMM 21-51-61. OPS AND LEAK CK OK.Aug 19, 2009 · N594HA · Boeing 767332 · Cabin Cooling SystemSDR UIEA201000163Insulation · damagedUPON REMOVAL OF THE NR 2 ENGINE FOR REPLACEMENT PURPOSES THE NR 2 STRUT LOWER WEB INSULATION BLANKET ("HEAT SHIELD") WAS FOUND DAMAGED WITH MISSING MATERIAL. "DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR BY INSTALLING A REPAIR DOUBLER MADE FROM SS 301Aug 15, 2009 · N418MC · Boeing 74747UF · Nacelle/Pylon Miscellaneous StructureSDR UIEA200900049Seat Track · crackedMAIN DECK SIDE DOOR AREA AT LT, FS 1806.95 TO 1809.95, LBL99 SEAT TRACK CROWN LUG HAS A 3.0 INCH CRACK. PERMANENT REPAIR ACCOMPLISHED IAW SRM 53-00-52-2R-6 REPAIR 6 AND EO 4453A271.Aug 14, 2009 · N496MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR HALA2009081400369Eec · malfunctionedETOPS SIGNIFICANT SYS - IN CLIMB, CRUISE AND DESCENT RT THROTTLE ONE KNOB DIFFERENCE FROM LT -(1 KNOB IN FRONT OF RT TO LINE UP N1'S). REMOVED AND REPLACED NR 1 ENG EEC (PMC) ON LT ENG IAW AMM 73-21-07-404-009-600. ALSO PERFORMED GROUND TEST EEC IAW AMM 73-2Aug 14, 2009 · N596HA · Boeing 767332 · Fuel Controlling SystemSDR WRLA20090813197Engine · oil consumptionEN ROUTE TO ATL, AIR SYSTEM PRODUCED OILY SMELL. SHUT DOWN PACK NR 1 AND SMELL WENT AWAY. OIL QUANTITY OF NR 1 ENGINE DECREASED FROM 16 TO 3 QUARTS DURING 13 HOURS OF FLIGHT. REPLACED NR 1 ENGINE.Aug 13, 2009 · N270WA · Doug MD11 · Engine (Turbine/Turboprop)SDR UIEA200900048Warning Message · intermittentENROUTE EICAS STARTER CUTOUT ENG 3 ON/OFF INTERMITTENTLY. ACCOMPLISHED PROCEDURES IAW FIM 80-03-11-00. MESSAGE CLEARED. NO LATCHED FAULTS.Aug 12, 2009 · N412MC · Boeing 74747UF · Central WarningSDR DL76G091961Frame · crackedSTA 1809.5 BULKHEAD FWD CHORD, CRACKED APPROX 1" IN RADIUS AT STR 5R. REPAIRED DAMAGE IAW SRM 53-80-08, REPAIR 9.Aug 12, 2009 · N1501P · Boeing 7673P6 · Fuselage Main, FrameSDR HALA2009080900358Circuit Card · malfunctionedETOPS SIGNIFICANT SYS - WITH L PACK SELECTED OFF, PACK OFF LIGHT AND PACK OFF MSG INTERMITTENTLY NOT DISPLAYED. IAW FIM 21-51-00 FOUND LT FLOW CONTROL CARD NO GOOD. REMOVED AND REPLACED LT PACK FLOW CONTROL CARD ASSY IAW AMM 21-51-09. OPS CHECK GOOD. OK FOAug 9, 2009 · N594HA · Boeing 767332 · Cabin Cooling SystemSDR HALA2009072900337Mec · malfunctionedETOPS SIGNIFICANT SYS - DURING CRUISE L ENG EEC AND AUTOTHROTTLE DISCONNECT LIGHT ON EICAS. PERFORMED QRH AND L ENG EEC LIGHT WENT OUT. BITE OF MONITOR LT EEC MEC AMPS RANGE. T/S IAW FIM 71 EECM MESSAGE INDEX TABLE 101. EEC PREVIOUSLY REPLACED. CKD CIRCUIT BJul 29, 2009 · N597HA · Boeing 767332 · Engine ControlsSDR UIEA201000164Skin · damagedDURING MX WALKAROUND FOUND DAMAGE TO THE NR 1 ENG. THRUST REVERSER TRANSLATING COWL, EXTERNAL SKIN AT APPROX. 9:00 POSITION. THE DAMAGE IS APPROXIMATELY 12.5" LONG AND 3" WIDE (REF FIG 1). DISPOSITION IS TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1Jul 19, 2009 · N418MC · Boeing 74747UF · Engine Thrust ReverserSDR UIEA201000160Skin · gougedLT T/E INBD MID FLAP - INBD L/E SKIN PANEL - WBL 137.55 WITH A GOUGE HOLE/DAMAGE. (ONE FACE SKIN AND HONEYCOMB DAMAGE WITHOUT INTERNAL SKIN DAMAGE). MEASURING 1.0 IN X 10.0 IN. "EA4457A195: DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN Jun 23, 2009 · N412MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000161Structure · brokenTHE CORNER AT OTBD AFT L/E WING FLAP WAS BROKEN. (0.5" X 0.5"). 1. "REMOVED THE DAMAGE AS SRM 51-70-17. 2. "LAY-UP REPAIRED THE DAMAGE WITH EA9390A/B RESIN BM 59-3 TYH-2. FABRIC AS SRM 51-70-17. CURED UNDER VACUUM. 3. "SANDED SMOOTH THE REPAIR AREA AS SRM 51-Jun 23, 2009 · N412MC · Boeing 74747UF · Leading Edge DevicesSDR UIEA201000162Tray · crackedTRAY CRACKED AT STA 1800 IN AFT CARGO COMPT RT SIDE. "DRILL 0.25 DIA STOP HOLE. MAKE 2 REPAIR PLATES WITH 0.071 7075 = TE CLAD SHEET. INSTALL REPAIR PLATES IAW SRM 53-00-53/206."Jun 23, 2009 · N412MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR FDEA200906052009Support Bracket · crackedNR 1 ENGINE INBD T/R HALF FWD LATCH PULL CABLE SUPPORT BRACKET IS CRACKED. REMOVED NR 1 ENG. INBD SUPPORT BRACKET REF CMM 78-32-00, WELDED BRACKET REF SPM 70-41-00, INSTALLED BRACKET REF CMM 78-32-00.Jun 5, 2009 · N683FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA200905281818Valve · malfunctionedDURING T/O ROLL AT APPROX 70K ECAM SHOWED "GROUND SPOILERS NOT RETRACTED" AND SPOILER PANEL 3 AND 2 FAULT. REJECTED T/O - ATTEMPTED RESET OF SPOILER PANEL WITH NO LUCK. ECAM SHOWS PANEL NR 2 EXTENDED. ACFT RELEASED FOR SERVICE IAW MEL/CDL: 27-61-01-B. TROMay 28, 2009 · N443FE · Airbus A310203 · Drag Control SystemSDR UIEA201000165Skin · dentedDURING WALKAROUND INSP DAMAGE WAS FOUND TO THE FUSELAGE SKIN RT BS 1765, S34 (LAP SPLICE) DENT DAMAGE MEASURING 1.5 IN LONG, 0.500 IN. WIDTH AND 0.045 DEPTH. (REF FIGURE 1). LOCATED 15.0 IN. FWD OF CARGO DOOR CUTOUT AND 7.0 IN ABOVE CARGO DOOR SWITCH CUTOUT. "May 27, 2009 · N418MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR DL76G090784Starter · failedAPU FAILED TO START. FOUND APU STARTER INOP. REMOVED AND REPLACED APU STARTED PER MM. OPS NORMAL.Apr 29, 2009 · N1608 · Boeing 767332 · APU Start/Ignition SystemSDR WRLA2009095Wheel · missingFLT 1457/17 AGT-SCL UPON POST FLIGHT INSPECTION FOUND LEFT NOSE WHEEL MISSING FROM AIRCRAFT.Apr 17, 2009 · N384WA · Doug MD11F · Wheel/Ski/FloatSDR FDEA200903130913Engine · failedON TAKEOFF HEAVY VIBRATION WITH NOISE AND ECAM ADVISORY FOR NR 1 ENGINE N1. NR 1 ENGINE N1 SHOWED MAX OF 3.6. N2 VIB NR 1 ENG 0.6. ALL OTHER ENGINE PARAMETERS NORMAL. COMPLETED INSTALLATION OF FIRST STAGE FAN BLADES ACCORDING TO AMM 72-21-00-4. REINMar 13, 2009 · N689FE · Airbus A300F4605R · Engine (Turbine/Turboprop)
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