Boeing MD-11F

Service difficulty reports · 31,320

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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 aircraft_model_key = 'MD11F'
  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 FDEA201607132429Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR ATTACH INBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.221", FINAL HOLE DIA: 1.225", MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRICATED AJul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132428Hinge · corrodedRT WING, OTBD FLAP, OTBD FWD HINGE UPPER MOUNT INBD BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 0.880", FINAL HOLE: DIA 0.953", MAXIMUM ALLOWABLE HOLE: DIA 0.944". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5Jul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132427Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE UPPER MOUNT OTBD BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT CMM 57-44-09. EXISTING HOLE: DIA 0.880". FINAL HOLE: DIA 0.953". MAXIMUM ALLOWABLE HOLE: DIA 0.944", REPAIR BUSHING FABRICATED AND INSTALLED IAW EA NR 1-575Jul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132426Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE UPPER MOUNT, INBD BORE SURFACE AREA CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.715", MATERIAL REMOVED: 0.003", REMAINING THICK: 0.712". MINIMUM ALLOWABLE THICKNESS: 0.720". REPAJul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132425Hinge · corrodedRT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT OTBD BORE SURFACE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.709", MATERIAL REMOVED: 0.003", REMAINING THICKNESS: 0.706". MINIMUM ALLOWABLE THICKNESS:Jul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132424Hinge · corrodedRT WING, OTBD FLAP, OTBD FWD HINGE LOWER MOUNT INBD CORRODED. REWORKED AND FOUND, EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 0.521", FINAL HOLE: DIA 0.613", MAXIMUM ALLOWABLE HOLE: DIA 0.584". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA NR 1-5750Jul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132423Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER MOUNT OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 0.581", FINAL HOLE: DIA 0.613", MAXIMUM ALLOWABLE HOLE: DIA 0.584". REPAIR BUSHING FABRICATED AND Jul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132422Hinge · corrodedRT WING, OTBD FLAP, OTBD FORWARD HINGE LOWER MOUNT INBD BORE SURFACE AREA CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.414", MATERIAL REMOVED: 0.008", REMAINING THICKNESS: 0.406", MINIMUM ALLOWABLE, THICKNESS: 0.408", RJul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132421Hinge · corrodedRT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD BORE SURFACE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.387", MATERIAL REMOVED: 0.008", REMAINING THICKNESS: 0.379", MINIMUM ALLOWABLE THICKNESS: Jul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132420Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER BOLT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.380", FINAL HOLE DIA: 0.407", MAXIMUM ALLOWABLE HOLE DIA: 0.391". REPAIR BUSHING FABRICATED Jul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132419Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER BOLT HOLE FOUND CORROSION. CORROSION AT RT WING, OTBD FLAP, OTBD FORWARD HINGE, WING SIDE, BARREL NUT LOWER BOLT HOLE, NR 7 HOLE, REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOJul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132418Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.662", FINAL HOLE DIA: 0.699", MAXIMUM ALLOWABLE HOLE DIA: 0.667". REPAIR BUSHING FABRICATED AND INSTALLJul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132417Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD HINGE, WING SIDE, INBD ACTUATOR ATTACH BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 1.220", FINAL HOLE: DIA 1.224", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED AND INSTALJul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132416Hinge · corrodedRT WING, OTBD FLAP, OTBD HINGE, WING SIDE, OTBD ACTUATOR ATTACH BORE, CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-09. EXISTING HOLE: DIA 1.220", FINAL HOLE: DIA 1.224", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED AND INSTALLJul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132415Hinge · corrodedLT WING, INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.188", FINAL HOLE DIA: 1.235" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED AND IJul 13, 2016 · N582FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201607132413Hinge · corrodedLEFT WING, INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT INBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.188", FINAL HOLE DIA: 1.235" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED ANDJul 13, 2016 · N582FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201607132411Hinge · corrodedLEFT WING, OTBD FLAP, INBD FORWARD HINGE, WING SIDE, ACTUATOR ATTACH OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.218", FINAL HOLE DIA: 1.224", MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRIJul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132409Hinge · corrodedLEFT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR ATTACH INBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08 EXISTING HOLE DIA: 1.225", FINAL HOLE DIA: 1.231", MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRICATED AND Jul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132406Hinge · corrodedLT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, PIVOT BORE FOUND, CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 2.311", FINAL HOLE DIA: 2.316" AND MAXIMUM ALLOWABLE HOLE DIA: 2.3135". NEW REPAIR BUSHING FABRICATED AND INSTAJul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132403Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.618", FINAL HOLE DIA: 0.645" AND MAXIMUM ALLOWABLE HOLE DIA: 0.584". NEW REPAIR BUSHING FABRICATJul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132401Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER BOLT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.391", FINAL HOLE DIA: 0.407" AND MAXIMUM ALLOWABLE HOLE DIA: 0.391". NEW REPAIR BUSHING FAJul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132399Hinge · corrodedLEFT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER BOLT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA, 0.390", FINAL HOLE DIA: 0.407" AND MAXIMUM ALLOWABLE HOLE DIA: 0.391". NEW REPAIR BUSHING FABRJul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132397Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.674", FINAL HOLE DIA: 0.691" AND MAXIMUM ALLOWABLE HOLE DIA: 0.667". NEW REPAIR BUSHING, FABRICATED ANJul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132395Hinge · corrodedLEFT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, ACTUATOR ATTACH INBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 1.238", FINAL HOLE DIA: 1.244" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRIJul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201607132393Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR ATTACH OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 1.247", FINAL HOLE DIA: 1.252" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRJul 13, 2016 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR IPXA2016071405849Indicator · inoperativeINSPECTION TYPE: RI, DOOR EVAC SLIDE REMOTE PRESSURE PRESS TO TEST INOPERATIVE. R & R R1 DOOR REMOTE PRESS INDICATOR ASSY IAW AMM 25-61-04. OPS CK GOOD, EFF SOURCE REF 25-61-05-01.Jul 13, 2016 · N254UP · Doug MD11F · Emergency EquipmentSDR FDEA201607122366Spring · brokenL-1 DOOR UPPER LINING SLIDING CLOSEOUT PANEL SPRING BROKEN AND PANEL DAMAGED. NO RESTRICTION, IAW 25-23-23-2 L1 DOOR UPPER LINING SLIDING CLOSEOUT PANEL SPRING BROKEN AND PANEL DAMAGED. REMOVED L1 DOOR SLIDING CEILING AND EXIT LIGHT PANEL ASSY IAW MM 25-23-Jul 12, 2016 · N615FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201607122361Seal · cut35 MINS INTO FLIGHT FO'S WINDOW HAD LOUD SQUEAL SOUND. UNABLE TO COMMUNICATE IN COCKPIT, IT IS TOO LOUD. T/S AS PER FIM 56-12-05, FOUND FO`S SLIDING WINDOW INNER SEAL CUT AT THE UPPER AFT CORNER. F/O SLIDING WINDOW RUBBER SEAL COMPLETELY CURED. PERFORMED Jul 12, 2016 · N587FE · Doug MD11F · Flight Compartment WindowsSDR IPXA2016072306199Floor Panel · damagedINSPECTION TYPE: 2C, MAIN CABIN FLOOR PANEL 232EF UPPER SURFACE MULTIPLE DAMAGED. REMOVED, FABRICATED AND INSTALLED A REPLACEMENT FLOOR PANEL IAW DWG WSP0845.Jul 12, 2016 · N292UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2016072306197Floor Panel · damagedINSPECTION TYPE: 2C, MAIN CABIN FLOOR PANEL 232DF UPPER SURFACE HAD MULTIPLE DAMAGE. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT FLOOR PANEL IAW DWG WSP0822.Jul 12, 2016 · N292UP · Doug MD11F · Fuselage Floor PanelSDR FDEA201607122368Terminal · overheatedFUME EVENT, CAPTAIN AND BOTH JUMPSEATING PILOTS SMELLED STRONG ELECTRICAL BURNING ODOR ON ARRIVAL AT AIRCRAFT. 3RD WRITE-UP OLD DISCREPANCY: 615-24-00-0003950. ACCOMPLISHED GVI OF FLIGHT DECK WINDOWS, FOUND L1 WINDOW UPPER CTR TERMINAL STRIP HAS EVIDENCE OFJul 12, 2016 · N615FE · Doug MD11F · Windshield/Door Rain/Ice RemovalSDR IPXA2016072306196Attach Angle · crackedINSPECTION TYPE: 2C, FRAME ATTACH ANGLE CRACKED IN LOWER AUX TANK BAY, BS 1278. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT ANGLE IAW DWG AYB7035 AND SRM 51-33-01.Jul 11, 2016 · N292UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2016072106119Attach Angle · crackedINSPECTION TYPE: 2C, FRAME ATTACH ANGLE BROKEN IN LOWER AUX TANK COMPT, RT SIDE, BS 1278. REMOVED FABRICATED AND INSTALLED REPLACEMENT ATTACH ANGLE IAW DWG AYB7035 AND SRM 51-33-01.Jul 11, 2016 · N292UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2016071505914Skin · crackedINSPECTION TYPE: 3C, LT NR 5 SPOILER UPPER SKIN DENTED WITH CRACKED. REPAIRED THE DENT IAW SRM 51-71-00 REPAIR GENERAL, PARA. 19.B. MAJOR REPAIR.Jul 11, 2016 · N285UP · Doug MD11F · SpoilersSDR IPXA2016071105734Girt Bar · out of adjustPILOT REPORTED R 1 DOOR SLIDE FAILED TO ARM. ADJUSTED GIRT BAR IAW MM 25-61-01. OPS CHECKED NORMALJul 11, 2016 · N291UP · Doug MD11F · Emergency EquipmentSDR FDEA201607112355Contact · burnedLEFT UPPER STROBE INOPERATIVE. FOUND BURNED INTERNAL CONTACT IAW AMM 33-47-01-2.Jul 11, 2016 · N599FE · Doug MD11F · Exterior LightingSDR FDEA201607112352Seat Track · crackedON REMOVAL OF MAIN DECK FLOOR PANEL 243CF, FOUND SEAT TRACK CRACKED AT BS 755 X -27.5. REPAIR CARRIED OUT BY SECTIONAL REPLACEMENT FROM STA 745 TO STA 765, X=-27.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Jul 11, 2016 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607112351Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 770 FOUND CRACKED. BEADED DOUBLER REPAIRED IAW SRM 57-40-02-2R, REPAIR 15, FIGURE 203. REPAIR CLASSIFIED AS MAJOR AS IAW GMM 6-2-100.Jul 11, 2016 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201607112350Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 664 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, REPAIR 15, FIG 203. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 11, 2016 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201607112349Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 749 FOUND CRACKED. BEADED DOUBLER REPLACED IAW SRM 57-40-02-2R, REPAIR 15, FIGURE 203. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 11, 2016 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201607112346Floor Support · corrodedFWD CABIN MAIN DECK CARGO FLOOR SUPPORT CORRODED AT BS 494, X -57.0. FWD CABIN, MAIN DECK CARGO COMPARTMENT. CORRODED FLOOR SUPPORT AT RT STA 494, X= -57.0. R & R NEW FLOOR SUPPORT FROM STA 459 TO STA 515 X=-57.0 IAW SRM 51-31-01-0G. NEW FLOOR SUPPORT FABJul 11, 2016 · N602FE · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016072906467Stanchion · corrodedINSPECTION TYPE: 2C, FWD CARGO BAY AT STA 6-70 X 57, STANCHION IS CORRODED. REPAIRED IAW EA 011-5310-01-A6368-IR AND EO MD11-5310-61326-A.Jul 10, 2016 · N292UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016071105638Skin · damagedL1 DOOR FWD UPPER CORNER SKIN DAMAGED. REPAIRED THE SKIN IAW EO MD11-5210-61239-A ACTION 6,A, STEPS (1)-(5) & (7)-(10). COMPLIED WITH HFEC OF DOOR SKIN NO CRACKS WERE DETECTED IAW NTM 51-10-0 PP.Jul 10, 2016 · N273UP · Doug MD11F · Passenger/Crew DoorsSDR FDEA201607102343Fire Loop · faultedPASSING 11,000 FT ON DESCENT, RECEIVED A MOMENTARY FIRE INDICATION ON NR 3 ENGINE LASTED 2 SECONDS AND WENT AWAY. NO OTHER INDICATIONS LEFT ENGINE AT IDLE AND LANDED WITHOUT SHUTTING IT DOWN. PERFORMED FDCU-3 FAULT REVIEW, LOOP B FAULTED, UPPER RIGHT FIRE DJul 10, 2016 · N593FE · Doug MD11F · Fire DetectionSDR IPXA2016072806420Stringer · crackedINSPECTION TYPE:2C, CENTER AUXILIARY TANK STR 46 CRACKED AT XCW 17. REPAIRED IAW EA 011-5710-01-A6358, REV IR AND EO MD11-5710-61382-A.Jul 9, 2016 · N292UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2016072206159Stringer · crackedINSPECTION TYPE: 2C, STRINGER 49 IS CRACKED. REPAIRED IAW SRM 57-10-03 REPAIR 1 FIG. 201 (MAJOR).Jul 9, 2016 · N292UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2016072206158Stringer · crackedINSPECTION TYPE :2C, CENTER WING TANK STRINGER 48 IS CRACKED AT STA. XCW=17.REPAIRED CRACKED CENTER WING TANK STRINGER #48 AT STA. XCW=18 IAW MD-11 SRM 57-10-03 REPAIR1 FIG. 201 (MAJOR).Jul 9, 2016 · N292UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2016072206160Stringer · crackedINSPECTION TYPE: 2C, CENTER WING TANK STRINGER 47 IS CRACKED IN 3 PLACES AT XCW=17, XCW=56.5, XCW=-17. REPAIRED THE STRINGER IAW SRM 57-10-03 REPAIR 1 FIG. 201. (MAJOR)Jul 9, 2016 · N292UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2016071305817Tire · leakingLEFT NOSE TIRE HAD LOW PRESSURE. EMERGENCY DECLARED. R & R LEFT NOSE WHEEL ASSY IAW AMM 32-42-01-401Jul 9, 2016 · N282UP · Doug MD11F · TireSDR FDEA201607092339Start Valve · failedTHE START VALVE LIGHT CAME ON DURING ENGINE START WHEN THE START VALVE WAS MANUALLY OPEN AND THE START VALVE LIGHT WENT OUT WHEN THE START VALVE WAS MANUALLY CLOSED AFTER ENGINE START. DURING CLIMBOUT AFTER TAKEOFF, THE START VALVE LIGHT CAME ON STEADY ANJul 9, 2016 · N590FE · Doug MD11F · Engine Start Valves/Controls
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