Pratt & Whitney JT8D-17

Service difficulty reports · 1,680

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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 = 'JT8D17'
  ORDER BY difficulty_date DESC"

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SDR CA121023009Connector · failed(CAN) DURING FLIGHT, THE ACFT EXPERIENCED A STICK SHAKER WITH NORMAL AIRSPEED DISPLAYED, FLIGHT CREW RESPONSE, AFFECTED CIRCUIT BREAKER PULLED, AS WELL AS INTERMITTENT AUTO PILOT RESPONSE AND INDICATION OF FORWARD POSITION OF THE TRIM. THE INDICATED TRIM POSITOct 19, 2012 · Boeing 7372S2C · Flight Control System WiringSDR CA121019006Flap System · false indication(CAN) DURING NORMAL APPROACH THE FLAPS HAD BEEN SELECTED IN SEQUENCE. AT FLAP POSITION 5, A FLAP DISAGREEMENT SIGNAL HAD BEEN DETECTED. THE FLAP SYS IS DISABLED IAW DESIGN TO INHIBIT FLAP OPERATION AND A POTENTIAL SPLIT FLAP CONFIGURATION WITH AN, INDICATIOOct 17, 2012 · Boeing 7372S2C · Trailing Flap Position Indicating SystemSDR FDEA201209293512Hinge · damagedLOUD SQUEL COMING FROM AREA UPPER FRONT SIDE OF COCKPIT NEXT TO S/O PANEL. CLOSING CARGO OUTFLOW VALVE HAS NO EFFECT. STARTED DURING CLIMB AROUND 250. WENT AWAY AT LEVEL OFF AT 350 THEN IMMEDIATELY CAME BACK. CONTINUED TO 370. ALL PRESSURIZATION INDICATISep 29, 2012 · N204FE · Boeing 7272S2F · Passenger/Crew DoorsSDR CA120906004Actuator · cracked(CAN) AFTER LANDING, CREW WAS TAXING TO THE GATE, THE CREW NOTICED THE STEERING AS NOT RESPONSIVE. THE ACFT WAS STOPPED AND IT WAS DISCOVERED TO HAVE A PUDDLE OF HYDRAULIC FLUID UNDER THE L/T WING. INSPECTION REVEALED THAT THE LT OTBD SPOILER ACTUATOR WAS CRASep 5, 2012 · Boeing 737200 · Drag Control ActuatorSDR FDEA201208042837Guide · out of adjustON BLOCK-IN, CAPTAIN OPENED SLIDING WINDOW TO TALK TO GROUND CREW. UNABLE TO CLOSE. TROUBLESHOT DOWN TO FWD AND AFT GLIDES. ADJUSTED AND TESTED L2 CAPT'S SLIDING WINDOW IAW MM56-12-011-5. OPS NORMAL.Aug 4, 2012 · N211FE · Boeing 7272S2F · Flight Compartment WindowsSDR FDEA201207282729Bottle · dischargedLEFT "BOTTLE DISCHARGED" LIGHT ILLUMINATED ON OVERHEAD PANEL. R & R LT ENGINE FIRE EXTINGUISHER BOTTLE IAW MM 26-21-001-4 AND PERFORMED INSPECTION CHECK IAW MM26-21-001-6. OPS NORMAL.Jul 28, 2012 · N204FE · Boeing 7272S2F · Extinguishing SystemSDR FDEA201207282730Pin · out of adjustON PREFLIGHT, CAPTAIN`S SLIDING WINDOW WILL NOT CLOSE. ADJUSTED GUIDE PIN IAW MM 56-12-011-5. OPS CHECKED NORMAL.Jul 28, 2012 · N211FE · Boeing 7272S2F · Flight Compartment WindowsSDR PCSA2012060501Engine · power lossDURING CLIMBOUT THE NR 2 ENGINE LOSS POWER.Jun 3, 2012 · N794AJ · Boeing 727227 · Engine (Turbine/Turboprop)SDR SROM201203200005Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 767 S22L.Mar 16, 2012 · N733PA · Boeing 737205 · Fuselage Main, Attach FittingsSDR CA120127010Blades · damaged(CAN) SERVERE VIBRATION ON NR 2 ENGINE WHEN ENGINE SELECTED TO IN-FLIGHT IDLE AT TOP OF DECENT. ENGINE VIBRATION GUAGE AT FULL MAXIMUM IN "TURBINE POSITION". FLIGHT CREW PERFORMED AN INFLIGHT SHUTDOWN AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL EXAMINov 10, 2011 · Boeing 737275C · Turbine SectionSDR SPAA1100004Bearing · frozenTUS-CYLW INTO C8 MAINTENANCE CHECK. ON APPROACH AND LANDING INTO CYLW, ELEVATOR CONTROLS STIFF. FOUND ELEVATOR INPUT TORQUE TUBE BEARINGS FROZEN/STIFF TO MOVE. REMOVED TORQUE TUBE ASSY, REPLACED AFFECTED BEARINGS, AND REINSTALLED ASSEMBLY AND RIGGED PER CMOct 17, 2011 · N703S · Boeing 7372T4 · Elevator Control SystemSDR CA111025006Engine · failed(CAN) ON CLIMB OUT, CREW EXPERIENCED A "BANG" AND VIBRATION FROM THE NR 3 ENGINE. CREW SECURED THE ENGINE AND RETURNED TO BASE. MX DISCOVERED THE NR 3 ENGINE HAD EXPERIENCED A CATASTROPHIC INTERNAL FAILURE. THE ENGINE WAS REPLACED AND ACFT RETURNED TO SERVICEOct 17, 2011 · Boeing 727200 · Engine (Turbine/Turboprop)SDR CA111012011Spindle · sheared(CAN) ACFT WAS ON FINAL APPROACH, WHEN THE FLIGHT CREW SELECTED INCREASING FLAP ANGLES, THEY NOTICED THE ACFT TENDED TO ROLL TO THE LT AND RUDDER TRIM WAS REQUIRED TO STABILIZE THE ROLL. WITH FLAPS SELECTED TO 40, 3 UNITS OF RUDDER TRIM WERE REQUIRED TO COMPEOct 8, 2011 · Boeing 737275C · Trailing Edge FlapsSDR EE4Y20111005007Skin · scratchedUPPER FUSELAGE SKIN WITH SCRATCH AT BS 846 BETWEEN S3-2R. A PERMANENT REPAIR IS REQUIRED IAW MFG REPAIR GUIDLINES UNDER WO Z10226, ITEM 2-153.Oct 5, 2011 · N733TW · Boeing 7372H4 · Fuselage Main, Plate/SkinSDR DALA1147039881Fan Blade · brokenDURING TAKEOFF ROLL JUST ABOVE 80 KNOTS A LOUD BANG WAS HEARD FOLLOWED BY AIRCRAFT SHIMMY. FLIGHT CREW ABORTED TAKEOFF AND NOTICED ENGINE NR 2 VIBRATION. ENGINE NR 2 WAS SHUTDOWN. MAINTENANCE FOUND FAN BLADES DAMAGED AND 1 BLADE BROKEN OFF AT THE BLADE ROOTAug 6, 2011 · N676MC · Doug DC951 · Turbine Engine Compressor SectionSDR CA110520002Window · brokenDURING CRUISE, THE FLIGHT CREW REPORTED THAT THE OUTER PANE OF THE L-1 WINDOW HAD SHATTERED. THE ACFT RETURNED TO POINT OF DEPARTURE, WHERE THE WINDOW WAS REPLACED.May 17, 2011 · Boeing 737217 · Flight Compartment WindowsSDR DALA1127639875Web · crackedAFT CABIN LT STA 1100-1110, LBL 44-LBL 56 SUB FLOOR WEB IS CRACKED. FABRICATED 2 EA DOUBLERS AND 1 EA FILLER. INSTALLED 2 EA DOUBLERS AND FILLERS 1 EA AT AFT CABIN LT STA 1100-1110, LBL 44 TO LBL 56 IAW SRM 51-30-2 PG:1-2 AND 51-30-05 PG:1-3 INSTALLED FITApr 20, 2011 · N784NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1125839871Wedge · crackedLT ELEVATOR OTBD T/E WEDGE CRACKED. FOUND ON REMOVAL OF STATIC WICK BASE DOUBLER. REMOVED T/E WEDGE IAW SRM 51-30-2. REPAIRED USING REPAIR KIT IAW SRM 51-70-1. INSTALLED IAW SRM 51-30-2. WEIGHT AND BALANCE TO BE ACCOMPLISHED.Apr 13, 2011 · N780NC · Doug DC951 · Elevator, Plate/SkinSDR DALA1125569871Floorbeam · corrodedFLOORBEAM AT STA 389, RBL 52 CORRODED AND CRACKED AT NUTPLATE. CUT OUT DAMAGED AREA 1" X 2". DAMAGE CONTAINED IAW NDT 06-01-10. 001. FABRICATED REPAIR ANGLE FROM MATERIAL ID 60-377707376571. MILLED ANGLE ON NR 2504NO1510. INSTALLED REPAIR ANGLE IAW SRM 51-3Apr 12, 2011 · N780NC · Doug DC951 · Fuselage Main, Floor BeamSDR TSAA1156003Window · crackedNON-ETOPS FLIGHT 54 HNL-ITO. ON DESCENT, THE CAPTAIN’S NR 2 WINDOW OUTER PANE CRACKED. GLASS REMAINED INTACT AND THERE WAS NO LOSS OF PRESSURIZATION. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX R & R THE CAPTAIN’S NR 2 WINDOW IAW AMM 56-12-11 ANApr 3, 2011 · N841AL · Boeing 7372X6C · Flight Compartment WindowsSDR DALA1123439871Floor Support · damagedFRAME STA 465, TITANIUM FLOOR SUPPORT HAS HOLE DRILLED IN RADIUS LT. REMOVED FLOOR SUPPORT STA 465, L22L TO L30 IAW SRM 51-30-2 & 51-30-2. PART RECEIVED FROM WELD ON TRAVELER 2504NO1006. WELDED HOLE IAW NWA SRP DC-9 A-51-71-03-801-663A-A. INSTALLED FLOOR SMar 31, 2011 · N780NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1116309878Frame · crackedAFT ACCESSORY CANTED FRAME, STA 1245, STIFFENER CRACKED AT L6R. REMOVED FASTENERS TO GET ACCESS AT CRACKED STIFFENER IAW SRM 51-30-2 STOP DRILLED ENDS OF CRACK IAW SRM 53-01, FIG 2. FABRICATED 2EA REPAIR ANGLES IAW SRM 53-01, FIG 2. INSTALLED REPAIR ANGLES Mar 8, 2011 · N787NC · Doug DC951 · Fuselage Main, FrameSDR DALA1115519877Structure · crackedOVERSIZED RIVNUT HOLE ON AFT SIDE OF FWD CARGO DOOR IS MISSING RIVNUT AND HOLE IS CRACKED. FABRICATED REPAIR DOUBLER IAW SRM 52-03, FIG 1. ALODINED REPAIR DOUBLER IAW SRM 51-10-3, PARA 21. PRIMED REPAIR DOUBLER IAW SRM 51-10-3B, PARA 2 F . INSTALLED REPAIR Mar 6, 2011 · N786NC · Doug DC951 · Fuselage Main, StructureSDR DALA1116329870Cusp Web · crackedMAIN CABIN STA 734, LBL-50 LT SIDE CUSP WEB CRACKED APPROX 1 IN. STOP DRILLED CRACK IAW SRM 53-10-16. REMOVED 1 FASTENER IAW 51-30-2. REQUESTED NDT, NDT REPORTS CRACK CONTAINED. RECEIVED LOCATED, DRILLED, FIT, TRIMMED, AND DEBURRED REPAIR DOUBLER IAW SRM 5Mar 3, 2011 · N779NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1115289870Floorbeam · corrodedMAIN CABIN STA 200, RBL 24 TO 43 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-3. ORIGINAL THICKNESS WAS .060 IAW SRM 53-13-1, FIG 11, AFTER BLEND MATERIAL THICKNESS IS .010 OUT OF LIMITS IAW SRM 53-01. REMOVED SUPPORT IAW SRM 51-30-5. FABRIMar 1, 2011 · N779NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1111439877Skin · dentedRT WING FWD MOVEABLE FLAP VANE UPPER SURFACE HAS A DENT AT XF STA 85.5 REPAIRED IAW SRM 51-70-02. PREPARED CORE, PLUGS AND DOUBLERS IAW SRM 51-70-02, PARA 10D, PG 43, CURED IAW SRM 51-70-02. SEALED IAW SRM 51-70-02. INSTALLED FASTENERS IAW SRM 51-70-02.Feb 16, 2011 · N786NC · Doug DC951 · Trailing Edge FlapsSDR DALA1115609877Floor Panel · crackedFLOOR PANEL NR 63 HAS CRACKS ON THE EDGE OF FLOOR PANEL. REMOVED 2 EA CRACKS IN FLOOR IAW SRM 53-01. FABRICATED 2 EA REPAIR DOUBLERS IAW SRM 53-23-0. TREATED & PRIMED IAW SRM 51-10-3, PG 3. INSTALLED REPAIR DOUBLER IAW SRM 5 3-01. DETECTED NO CRACKS AT 2 Feb 16, 2011 · N786NC · Doug DC951 · Fuselage Floor PanelSDR 2011FA0000029Light · inoperativeEXIT LIGHT INOP ABOVE L2 DOOR.Jan 18, 2011 · N727NK · Boeing 737212 · Emergency LightingSDR TSAA1132001Lock · lack of lubeLANDING GEAR LEVER WILL NOT MOVE UP AFTER TAKEOFF. CLEANED AND LUBED LANDING GEAR LOCK MECHANISM. OPS CK OK IAW AMM 32-31-31. ACFT RETURNED TO SERVICE.Jan 7, 2011 · N840AL · Boeing 7372X6C · Landing Gear Retraction/Extension SystemSDR DALA1100949860Lamp · inoperativeDURING LINE CHECK, MX FOUND THE RT OVERWING EMERGENCY EXIT SIGN WAS INOPERATIVE. MX REPLACED THE ASSOCIATED BALLAST AND INSTALLED A NEW LAMP. OPS CHECK WAS GOOD.Jan 6, 2011 · N769NC · Doug DC951 · Emergency LightingSDR DALA1100799864Intercostal · crackedMAIN PASSENGER CABIN BETWEEN STA 148-160 RT INTERCOSTAL IS CRACKED. TAGGED REPAIR DOUBLER IAW DPS 900-5-1. HFEC INSPECTED IAW NDT SPM 06-10-01.001 TO LOCATE CRACK IN INTERCOSTAL. INSTALLED IAW SRM 51-10-4, 51-10-3, 53-05 FIG 100, 53-30-0. REQUIRED INSP COMJan 4, 2011 · N773NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1100919855Doubler · crackedMAIN CABIN BETWEEN STA 674-693 LT WINDOW FRAME DOUBLER CRACKED. CUTOUT DAMAGED AREA NDT VERIFIED DAMAGE. REMOVED IAW NDT SPM 06-10-01. FABRICATED AND INSTALLED REPAIR IAW SRM 53-05.Jan 4, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1100929855Doubler · crackedMAIN CABIN-FS. 693 WINDOW DOUBLER IS CRACKED AT TOP FORWARDCORNER. CUTOUT DAMAGED AREA NDT VERIFIED DAMAGE REMOVED IAW NDT SPM 06-10-01. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 53-05.Jan 4, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1100939855Doubler · crackedMAIN CABIN BETWEEN STA 794-813 RT WINDOW FRAME DOUBLER CRACKED AT FWD UPPER CORNER. CUTOUT DAMAGED AREA NDT VERIFIED DAMAGE. REMOVED IAW NDT SPM 06-10-01. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-05, FIG 122, P205. REQUIRED INSP COMPLETED BY Q 971Jan 4, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1100959855Doubler · crackedMAIN PASSENGER CABIN, STA 351 WINDOW DOUBLER TOP AFT CORNER CRACKED. REMOVED IAW NDT SPM 06-10-01. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 53-05.Jan 4, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1100969855Doubler · crackedMAIN CABIN BETWEEN STA 693-712 RT WINDOW FRAME DOUBLER CRACKED AT LOWER FWD CORNER. CUTOUT DAMAGED AREA NDT. VERIFIED DAMAGE, REMOVED IAW NDT SPM 06-10-01. FABRICATED ANDINSTALLED REPAIR IAW SRM 53-05, FIG 122, P 205. REQUIRED INSPECTION COMPLETED.Jan 4, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1100979855Doubler · crackedMAIN CABIN STA 693-712 LT WINDOW FRAME DOUBLER CRACKED AT FWD UPPER CORNER, CUTOUT DAMAGED AREA. NDT VERIFIED DAMAGE REMOVED IAW NDT SPM 06-10-01. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-05.Jan 4, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1100999855Doubler · crackedMAIN CABIN BETWEEN STA 693-712 RT WINDOW FRAME DOUBLER CRACKED AT FWD UPPER CORNER. CUTOUT DAMAGED AREA. NDT VERIFIED DAMAGE, REMOVED IAW NDT SPM 06-10-01. FABRICATED ANDINSTALLED REPAIR DOUBLER IAW DC-9 53-05.Jan 4, 2011 · N764NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1101009864Angle · crackedNLG STA 37, RBL 12 PREVIOUS REPAIR ANGLE CRACKED. REMOVED REPAIR DOUBLER AT STA 37, RBL 12 NOT NECCESARY TO REINSTALL WEB BEING REPLACED IAW SRM 51-30-5.Jan 4, 2011 · N773NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1101039864Hinge Bracket · crackedLT WING T/E FLAP NR4 HINGE BRACKET CRACKED INBD AT MOUNT HOLE FLAP SIDE. REMOVED ANGLES FROM INBD SIDE OF FITTING IAW SRM 51-30-2 AND DWG 5910134-0. NEW HINGE BRACKET LOCATED AND DRILLED IAW SRM 51-10-4. INSTALLED ANGLES AND HINGE BRACKET IAW SRM 51-30-2 AND Jan 4, 2011 · N773NC · Doug DC951 · Trailing Edge FlapsSDR FDEA201012304785Indicator · failedREJECTED T/O AT 80 KNOTS. NR 1 EPR GUAGE INOP. RELEASED FOR SERVICE IAW MEL: 77-01-01, "MEL 77-01-01: NR 1 ENGINE EPR INDICATOR - INOP." ACFT OK FOR SERVICE. TO TROUBLSHOOT, FURTHER TROUBLESHOOTING REQUIRED. CODE 'A' ITEM DUE ON OR BEFORE 2-JAN-2011. ACDec 30, 2010 · N207FE · Boeing 7272S2F · Engine Pressure Ratio (EPR)SDR DALA1036669864Web · mismanufacturedDURING M-CHECK, FOUND MAIN PASSENGER CABIN LT SIDE BETWEEN BS 712 AND BS 693 BATH TUB FITTING ENCOMPASS WEB HAS SEVERAL DOUBLE DRILLED FASTENER HOLES. FABRICATED WEB IAW DWG 9923410-3 AND MATCH DRILLED IAW SRM 51-10-4.Dec 23, 2010 · N773NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1036679864Tie Down · crackedDURING M-CHECK FOUND FWD CARGO COMPARTMENT, STA 294 RT TIE DOWN RACK CRACKED. REMOVED TIE DOWN TRACK IAW SRM 51-30-1. FABRICATED THE SHAPE FUSELAGE TIE DOWN TRACK DRILLED IAW SRM 51-10-4. SCALLOPED TIE TRAVELER 2311N0251. TREATED, PRIMED IAW SRM 51-10-3. RDec 23, 2010 · N773NC · Doug DC951 · Fuselage Main, Attach FittingsSDR DALA1036689864Floorbeam · chafedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 237 BL 0- LBL 22 FLOORBEAM IS CHAFED, BLENDED CHAFE. REMAINING WAS OUT OF LIMITS IAW SRM 53-01, FIG 1, FABRICATED PARTS AND COMPLETED REPAIRS IAW SRM 53-05, FIG 20A AND SRM 51-30-5.Dec 23, 2010 · N773NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1036659864Seat Track · corrodedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 237, LBL 22 SEAT TRACK HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-3, FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. REMOVED SEAT TRACK IAW SRM 51-30-1 AND 51-30-5. LOCATED, DRILLED IAW SRM 51-10-4 ALODINEDDec 22, 2010 · N773NC · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1036309855Strut · crackedDURING M-CHECK FOUND FWD CARGO STA 275 LT STRUT CRACKED AT LOWER END. STOP DRILLED CRACK IAW SRM 53-01, FIG 2. VERIFIED CRACK CONTAINED IAW SPM 06-10-01.001. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-01, FIG 2, SHEET 4, 53-13-2, FIG 4, SHT 1&2, 51-10-3, 53Dec 21, 2010 · N764NC · Doug DC951 · Fuselage Main, StructureSDR DALA1036319855Strut · crackedDURING M-CHECK FOUND FWD CARGO STA 237 LT STRUT CRACKED AT LOWER END. STOPPED DRILLED CRACK IAW SRM 53-01, FIG 2. VERIFIED CRACK CONTAINED IAW SPM 06-10-01.001 FABRICATED AND INSTALLED DOUBLER IAW SRM 53-01, FIG 2, SHEET 4, 53-13-2, FIG 4, SHT 1&2, 51-10-3, 5Dec 21, 2010 · N764NC · Doug DC951 · Fuselage Main, StructureSDR DALA1036329855Strut · crackedDURING M-CHECK FOUND FWD CARGO STA 256 LT STRUT CRACKED AT LOWER END. STOP DRILLED CRACK IAW SRM 53-01, FIG 2. CRACK DETERMINED TO BE CONTAINED IAW SPM 06-10-01.001. FABRICATED AND DRILLED 2EA DOUBLERS IAW SRM 53-01, FIG 2 AND 53-13-2 FIG 4. TREATED, PRIMEDDec 21, 2010 · N764NC · Doug DC951 · Fuselage Main, StructureSDR DALA1036429855Floor Panel · corrodedDURING M-CHECK FOUND FLOOR PANEL 26, CORROSION AT AFT BOTTOM SECTION. PANEL CORRODED BEYOND LIMITS IAW SRM 53-01, FIG 1. REPAIRED PANEL IAW SRM 53-05, FIG 1. CUTOUT DAMAGE 4.25" X 1.25" HFEC NDT SRM 06-10-01 NO CRACK FOUND.Dec 21, 2010 · N764NC · Doug DC951 · Fuselage Floor PanelSDR FDEA201012214734Fire Loop · dirtyRECEIVED NR 1 ENGINE FIRE INDICATION ON FINAL APPROACH WITH POWER AT IDLE. SYS TESTED OK & ENGINE WAS SHUTDOWN AND BOTTLE DISCHARGED IAW CHECKLIST. FIRE WARNING SYS STILL DID NOT SILENCE UNTIL ON THE GROUND & NR 1 ENGINE DET "B" CB PULLED. EMERGENCY VEHICLEDec 21, 2010 · N204FE · Boeing 7272S2F · Fire Detection
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