Rolls-Royce RB-211 series

Service difficulty reports · 353

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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 = 'RB211'
  ORDER BY difficulty_date DESC"

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SDR FDEA201010154077Seat Track · gougedMAIN DECK SEAT TRACK STA 440- 680 LBL 45.5 GOUGED & CORRODED. REMOVED GOUGES AND CORROSION PER SRM 51-10-02. BLENDED AREA ; L=13.0",W=1.0",D=.030". OUT OF LIMITS, EXCEEDS THE MAX DEPTH OF .020", GIVEN IN SRM 53-00- 52, FIG.101, DETAIL 1. FABRICATED NEW SEOct 15, 2010 · N943FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010101400468Fcu · failedETOPS SIGNIFICANT SYS - UNSUCCESSFUL INFLT APU START. REPAIRED CLASS 1 FCU FLOW DIVIDER. BITE CHECK AND CLASS 1 FAULT CLEARED.Oct 14, 2010 · N381HA · Airbus A330243 · APU Engine Fuel and ControlSDR FDEA201010134039Seat Track · gougedBS 418-440, LBL 24, SEAT TRACK IS GOUGED. REMOVED GOUGE IAW SRM 51-10-02. AFTER REWORK, FOUND OUT OF LIMITS IAW SRM 53-00- 52, FIG.101, DETAIL 7; L=1.5",W=1.0",D=.019". FABRICATED NEW SEAT TRACK, MATL ID BAC 1520-792, BATCH 1891618. INSTALLED NEW SEAT TRACK Oct 13, 2010 · N943FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010134041Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER CHORD HAS CORROSION ENTIRE LENGTH BS 1660 CHECKED LIMITS STA 1660 FLOORBEAM AT LBL 55 TO RBL 59. L=6.0 W = 2.0 AND D =.038, FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-51 . R & R STA 1660 FLOORBEAM IAW SRM 51-40-Oct 13, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201009283773Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER TEE HAS CORROSION BS 363.25. BLENDED DAMAGED AREAS IAW SRM 51-10-01. AREAS OUT OF LIMITS IAW SRM 53-00-51, FIG.101, DETAIL 3. R & R UPPER TEE AT RBL 18-60, BS 363.25, IAW SRM 53-00-51, FIG 201, AND SRM 51-40-02. INSTSep 28, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201009223619Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER CHORD CORRODED AROUND HOLES BS 480. FLOORBEAM WITHIN LIMITS AND CONSIDERED A MINOR REPAIR.Sep 22, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201009223645Intercostal · corrodedMAIN CARGO COMPARTMENT INTERCOSTAL HAS CORROSION AROUND HOLES BS 324 TO 340 RBL 25.75. ( ELONGATED HOLES )Sep 22, 2010 · N943FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201009213603Stringer · corrodedCORROSION FOUND AT STRINGER 3R BETWEEN STA 310.5-324. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA L=4",W=1",D=.020". ORIGINAL MATL.050", REMAINING MATL. .030". FOUND OUT OF LIMITS IAW SRM 53-00-03, FIG 101, DETAIL REPAIRED S4R, AT BS 310.5-324, IAW SRM Sep 21, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Longeron/StringerSDR FDEA201009203560Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER CHORD HAS CHAFED MARK AND CORRODED AROUND HOLES BS 740, RBL 42. REMOVED CORRSION IAW SRM 51-10-02 , CHECKED LIMITS OF BLENDED AREA L=3.01' W= 2.00', D = .015 ORIGINAL MATERIAL .125 , REMAINING. 110, OUT OF LIMITS IAWSep 20, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201009203571Frame · corrodedMAIN CARGO COMPARTMENT BULKHEAD UPPER CHORD HAS CORROSION BS 324 ENTIRE LENGTH. REMOVED CORROSION UPPER CHORD IAW SRM 51-10-02 . BLENDED AREA L= 44" W=3.0 " D=.039, ORIG MAT .125 REMAINING . 086 OUT OF LIMITS IAW SRM 53-10-08, FIG 101, DET 9. R & R UPPESep 20, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, FrameSDR FDEA201009143370Web · damagedTHIS NON ROUTINE FOR TIME AND REPAIR TRACKING. W/C MAE MOD (43607420001 / 118350499EZ2R01). REWORK REQUIRED AT LBL 29. FLOORBEAM WEBS AT FS 1620, 1640, AND 1661. STRUCTURES MECH MIS-READ DWG 657N3374, SHT 1, AND DRILLED / CUT A2" HOLE AT LBL 29 IN FLOORBEASep 14, 2010 · N902FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR 2010FA0001000Slide · activatedTHE R2 DOOR SLIDE WAS DEPLOYED WHEN DOOR WAS OPEN BY THE CREW IN THE ARMED POSITION AND DEPLOYED. ACFT INSPECTED AND NO DAMAGE FOUND EXCEPT SLIDE DEPLOYED. SERVICEABLE SLIDE INSTALLED AND ACFT RETURNED SERVICE.Sep 10, 2010 · N757SS · Boeing 757236 · Escape SlideSDR HALA2010081200362Computer · faultedETOPS SIGNIFICANT SYS - BTB - F/CTL AIL SERVO FAULT. REPLACED FCPC1 IAW 27-93-400-801, PG 400, ALL INDICATIONS NORMAL, ACFT OK FOR SERVICE.Aug 12, 2010 · N381HA · Airbus A330243 · Flight Management Computing Hardware SystemSDR HALA2010081200363Computer · malfunctionedETOPS SIGNIFICANT SYS - BTB - ECAM (AMBER) WARNING - FLT CONTROL AIL FAULT LIGHT. CHECKED SV SIGNAL WIRING FROM FCPC1 AD/12J, 12K TO SERVO CTL (8CS1) A /E,F AND SV CTL WIRING FROM FCPC-1 AD/12G, 12H TO AB/1J, 1K CONTINUITY CHECKS GOOD, NO SHORTS TO GND. SHAKAug 12, 2010 · N381HA · Airbus A330243 · Flight Management Computing Hardware SystemSDR IPXA10561723Flap System · malfunctionedAS FLAPS WERE IN TRANSIT FROM 1 TO UP SAW MOMENTARY INCREASE IN AIRSPEED TO 250 KNOTS. AFTER FLAPS UP AIRSPEED RAPIDLY DECREASED TO 235 KNOTS TS. FLAP INDICATOR WAS AT .5 POSITION. NR 431740 ASSIGNED. C/W PHASE 1 OVERSPEED INSP L/E FLAPS IAW AMM 05-51-08-2. Aug 11, 2010 · N451UP · Boeing 75724APF · Trailing Edge Flap Control SystemSDR CALA2010081000386Unknown · odorSTRONG INTERMITTENT ODOR IN COCKPIT AND CABIN FROM FWD CABIN TO ROW 8. NOTICE ONCE AT CRUISE AND AGAIN AT 10,000 FT. ALMOST SMELLS ELECTRICAL NO VISIBLE SMOKE. A/C MM TASK 05- 51-58-201 (SMOKE IN THE CABIN/ FLT DECK) AND FOUND NO DISCREPANCIES.Aug 10, 2010 · N14120 · Boeing 757224 · Air Distribution SystemSDR FDEA201007312743Seat Track · gougedSEAT TRACK STA 418-440, RBL 45 IS GOUGED. BLENDED DAMAGED AREA ORIG MAT .080, AFTER BLEND, L-2.00, W-.900, D-.022, REMAINING MAT .058. FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52, FIG 101, DET VII, FAB NEW SEAT TRACK OF PN 60-6549/24 BATCH NR 1541987 IAW SRMJul 31, 2010 · N902FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201007312745Crease Beam · corrodedMAIN CABIN STA 1440-1460, RT SIDE CREASE BEAM WEB HAS CORROSION. REMOVED CORROSION AT MAIN CABIN STA 1440-1460 RT SIDE CREASE BEAM IAW SRM 51-10-02. BLENDED AREA L= 1.75",W=1.45",D=.008" ORIGINAL MAT. .040". MAT REMAINING .032" FOUND OUT LIMITS IAW SRM 53-00-Jul 31, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, StructureSDR HALA2010072400328Warning Light · false activationETOPS SIGNIFICANT SYS - BTB, ECAM MESSAGE FLT CONTROL SEC 2 PITCH FAULT AFTER ENGINE START. COMPLIED WITH FCSC OPS TEST IAW AMM 27-94-00-710-801, OPS TEST OK, NO FAULT NOTED. OK FOR SERVICE.Jul 24, 2010 · N380HA · Airbus A330243 · Central WarningSDR AALA20100713TUL13Gearbox · faultyYYC - INFLIGHT DFW-NRT. CREW REPORTED LEFT ENGINE LOST OIL PRESSURE. LEFT ENGINE WAS SHUTDOWN SINGLE ENGINE TIME 20 MINUTES. EMERGENCY DECLARED DIVERTED YYC LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FLIGHT WAS FERRIED TO DFW FOR REPAIRS. REJul 13, 2010 · N797AN · Boeing 777223 · Turbine Engine Accessory DriveSDR CA100705007Pump · leakingDURING ROUTINE CHECK OF THE INBD STAND-BY FUEL PUMP LOCATION 5112 QA1 A FUEL LEAK AND ASSOCIATED FAULT MESSAGE WERE DETECTED. DURING REMOVAL OF THE FUEL PUMP, IT WAS NOTED THAT THERE WAS FUEL BEHIND THE VOID OF THE ELECTRICAL CONNECTOR, SEEPING THROUGH THE PIJul 1, 2010 · Airbus A330* · Fuel Boost PumpSDR FDEA201006152015Retainer · corrodedFWD CARGO COMPARTMENT, CARGO DOOR SURROUND STRUCTURE LOWER SILL SCUFF PLATE RETAINER PLATE AT STA 560 TO STA 620 FOUND WITH CORROSION. EVALUATE AND RECTIFY. FWD CARGO DOOR SURROUND STRUCTURE LOWER SILL SCUFF PLATE CORRODED. RETAINER PLATE REMOVED FROM STAJun 15, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, StructureSDR FDEA201006101921Access Panel · corrodedRIGHT WING FUEL TANK ACCESS PANEL NR 641LB, CORROSION FOUND IN THE LOWER SURFACE AREA. BLEND AND CHECK LIMIT. RT WING FUEL TANK ACCESS PANEL NO. 641LB REPAIRED IAW EA NR F-2810-135858-FUEL SYS-TANKS-RT WING LOWER SURFACE FUEL TANK ACCESS COVER CORROSION DAMJun 10, 2010 · N937FD · Boeing 7572T7 · Wing, Plate/SkinSDR FDEA201006101922Access Panel · corrodedRT WING FUEL TANK ACCESS PANEL NR 642AB, CORROSION FOUND IN LOWER SURFACE OF THE PANEL. BLEND AND CHECK THE LIMIT. RT WING FUEL TANK ACCESS PANEL NR 642AB REPAIRED IAW EA NR F-2810-135858-FUEL SYS-TANKS-RT WING LOWER SURFACE FUEL TANK ACCESS COVER CORROSION Jun 10, 2010 · N937FD · Boeing 7572T7 · Wing, Plate/SkinSDR FDEA201006101923Access Panel · corrodedRT WING FUEL TANK ACCESS PANEL NR 641GB, CORROSION FOUND IN THE LOWER SURFACE AND ITS SIDE. BLEND AND CHECK THE LIMITS. RT WING FUEL TANK ACCESS PANEL NR 641GB REPAIRED IAW E.A. F-2810-135858. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.Jun 10, 2010 · N937FD · Boeing 7572T7 · Wing, Plate/SkinSDR FDEA201006101924Access Panel · corrodedRT WING FUEL TANK ACCESS PANEL NR 641FB, CORROSION FOUND IN THE LOWER SURFACE AND ITS SIDE. BLEND AND CHECK THE LIMITS. RT WING FUEL TANK ACCESS PANEL NR 641FB REPAIRED IAW E.A. NR F-2810-135858. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.Jun 10, 2010 · N937FD · Boeing 7572T7 · Wing, Plate/SkinSDR FDEA201006101925Access Panel · corrodedRT WING FUEL TANK ACCESS PANELS NR 643AB, CORROSION FOUND IN THE LOWER SURFACE AND ITS SIDE. BLEND AND CHECK LIMITS. RT WING FUEL TANK ACCESS PANEL NR 643AB REPAIRED IAW E.A. F-2810-135858. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.Jun 10, 2010 · N937FD · Boeing 7572T7 · Wing, Plate/SkinSDR FDEA201006101927Access Panel · corrodedRT WING FUEL TANK ACCESS PANEL NR 641MB, CORROSION FOUND IN THE LOWER SURFACE AND ITS SIDE. BLEND AND CHECK LIMIT. RT WING FUEL TANK ACCESS PANEL NR 641MB REPAIRED IAW E.A. NR F-2810-135858. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.Jun 10, 2010 · N937FD · Boeing 7572T7 · Wing, Plate/SkinSDR FDEA201006101928Access Panel · corrodedRT WING FUEL TANK ACCESS PANEL NR 642BB, CORROSION FOUND IN THE LOWER SURFACE AND ITS SIDE. BLEND AND CHECK LIMITS. RT WING FUEL TANK ACCESS PANEL NR 642BB REPAIRED IAW E.A. NR F-2810-135858-FUEL SYS-TANKS-RT WING LOWER SURFACE FUEL TANK ACCESS COVER CORROJun 10, 2010 · N937FD · Boeing 7572T7 · Wing, Plate/SkinSDR FDEA201006071854Access Panel · corrodedLT WING FUEL TANK ACCESS PANEL NR 541GB, CORROSION FOUND IN THE LOWER SURFACE AND ITS SIDE. CORROSION ON PANEL NR 541GB REPAIRED IAW EA NR F-2810-135857. (LT WING LOWER SURFACE FUEL TANK ACCESS COVER CORROSION DAMAGE REWORK.) REPAIR IS CLASSIFIED AS MAJOR IJun 7, 2010 · N937FD · Boeing 7572T7 · Wing, Plate/SkinSDR FDEA201006011753Fitting · crackedDURING ACCOPLISHMENT OF EO F-5450-7-5006 PT1, AT NR 1 ENGINE PYLON FOUND 1 EA HOLE CRACK ON BULKHEAD FITTING HORIZ FLANGE LOWER FWD OTBD. NR 1 ENG PYLON BULKHEAD HOLE REPAIR CARRIED OUT IAW EA NR F-5450-135851 (LT PYLON AFT BULKHEAD FITTING CRACK REPAIR). REJun 1, 2010 · N937FD · Boeing 7572T7 · Nacelle/Pylon Miscellaneous StructureSDR FDEA201006011754Skin · crackedNR 1 ENGINE NACELLE STRUT AT FAIRING, LOWER AFT SECTION RT SIDE WITH CRACK. NR 1 ENGINE NACELLE STRUT AFT FAIRING SKIN R & R IAW SRM 51-40-02, REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Jun 1, 2010 · N937FD · Boeing 7572T7 · Nacelle/Pylon, Plate/SkinSDR FDEA201005281699Splice · damagedBS 700, LBL 45.5, FITTING PN 140N2504U1, IF DRILLED, A VARIETY OF FASTENERS WILL LAND IN RADIUS OF FITTING, ON HORZ. AND VERT FLANGES AT BS 700, LBL 45.5, AN ALTERATION WAD ACCOMPLISHED, DUE TO THE DISCREPANCY EFFECTING THE PTF CONVERSION, ON STAM MOD W/C 1183May 28, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA201005181564Skin · corrodedRT WING REAR SPAR UPPER SKIN LOWER SURFACE AT WS 190 FOUND WITH CORROSION. CORROSION ON RT WING UPPER SKIN LOWER SURFACE AT WS 190 REPAIRED IAW EA F-5730-138545 ( RT UPPER SKIN LOWER SURFACE CORROSION REPAIR AT WS 204.50). REPAIR IS CLASSIFIED AS MINOR IAW GMMay 18, 2010 · N937FD · Boeing 7572T7 · Wing, Plate/SkinSDR FDEA201005171562Support Bracket · crackedCEILING SUPPORT BRACKET IS CRACKED AT STA 365, STRINGER 3R. CRACKED BRACKET AT STA 365, STR 3R, R & R IAW SRM 51-40-02 REV.99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.May 17, 2010 · N937FD · Boeing 7572T7 · Fuselage Miscellaneous StructureSDR IPXA0560644Shear Web · damagedINSPECTION TYPE:C1, WHILE WORKING CUSTOMER CARD 860401, FOUND FIG 8 HOLE AT BS 336, LBL 61, WL 208. REPAIRED IAW ATS ER NR 10-2816.May 17, 2010 · N437UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR FDEA201005161551Frame · dentedFWD CARGO COMPT RT FRAME FLANGE AT STA 800, S-23R FOUND WITH DENT. DENTED FRAME FLANGE AT STA 800, S-23R REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 5, DETAIL 1, REV 99. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.May 16, 2010 · N937FD · Boeing 7572T7 · Fuselage Main, FrameSDR IPXA0560645Shear Web · corrodedINSPECTION TYPE:C1, FOUND CORROSION ON SHEAR WEB AT STA 355, LBL-48. REPAIRED IAW ATS ER 10-2816.May 14, 2010 · N437UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR FDEA201003250994Sill · corrodedL3 DOOR LOWER SILL IS CORRODED.Mar 25, 2010 · N904FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA201003250995Crease Beam · corrodedR1 DOOR CREASE BEAM IS CORRODED AT BS 350, RBL 58.Mar 25, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA201003250997Seat Track · gougedSEAT TRACK AT BS 780-879, RBL 24, IS BROKEN AND GOUGED. R & R SEAT TRACK, PN 1520-792, FROM BS 780-879, RBL 24.75, PER SRM 53-00-52, AND SRM 51-40-02. DAMAGE TO SEAT TRACK OUT OF LIMITS IAW SRM 53-00-52, DETAIL 1. MAJOR REPAIR.Mar 25, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003250998Seat Track · gougedSEAT TRACK AT BS 640-780, RBL 24, IS GOUGED.Mar 25, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003250999Seat Track · damagedSEAT TRACK AT BS 575, RBL 24, HAS BROKEN FLANGE. BLENDED AREA IAW SRM 51-10-02. SEAT TRACK DAMAGE AT BS 575, RBL 24 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 2 AND 3; L=6",W=1.3",D=.100". R & R SEAT TRACK AT BS 440-640, RBL 24.75, IAW SRM 5Mar 25, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003251001Frame · gougedFUSELAGE FRAME AT BS 1280, S10R-S11R, FLANGE IS GOUGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL 2, P.103. REMOVED AND INSTALLED NEW FRAME SECTION, AND 2EA. CHANNELS, AT BS 1280, S10R TO S11R IAW SRM 51-40-02 / 53-00-07, FIG 202, P.201-206Mar 25, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, FrameSDR FDEA201003251003Seat Track · gougedSEAT TRACK GOUGED AND WORN AT STA 879TO 900 RBL24 BLENDED AREA, CHECK LIMITS FOUND OUT IAW SRM 53-00-52 FIG 101 DETAIL 1, ORIG MAT .225 AFTER REWORK .213 MAT LOSS OF .12 EXCEEDS MAX MAT WEAR OF .004 . REMOVED SEAT TRACK CROWN STA 879 - 900 RBL 24 IAW SRM 51-Mar 25, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003251004Seat Track · gougedSEAT TRACK GOUGED AND WORN AT STA 879 TO 900 RBL 45 BLENDED AERA , CHECKED LIMITS, FOUND OUT IAW SRM 53-00-52 FIG 101 DETAIL 1, ORIG MAT 225 , AFTER REWORK .203, EXCEEDS MAX MAT LOSS OF .004 , REMOVED SEAT TRACK CROWN STA 879 TO 900 RBL 45 IAW SRM 51-40-02, Mar 25, 2010 · N904FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR CA100118004Windshield · arced(CAN) F CREW- ON DESCENT, PASSING THROUGH 7000FT, THE CAPTS MAIN FWD WINDSCREEN CRACKED WITH SOME ARCING OCCURING. NORMAL APPROACH CARRIED OUT. MX- WINDSHIELD CHANGE RECORDS SHOW THE WINDSHIELD HAD BEEN INSTALLED FOR 32907 HOURS.Jan 14, 2010 · Airbus A330342 · Flight Compartment WindowsSDR CA100119005Line · chafed(CAN) LT ENGINE, LT FAN COWL AFT LATCH NR4 AND ATTACH BOLT (2EA) ARE CHAFING AGAINST MAIN ENGINE FUEL SUPPLY TUBE AT 6 O`CLOCK POSITION. MOST WORN BOLT HAS LOST 2 TREADS DUE TO WEAR. THE FUEL TUBE HAS 2 CIRCULAR CHAFE MARKS. THE INNER MARK IS A 0.003 DEEP ON TJan 6, 2010 · Airbus A330243 · Engine Fuel DistributionSDR DL777091735Plug · missingFOUND DURING WALK AROUND ON ARRIVAL - NR 1 ENGINE AFT EXHAUST PLUG MISSING. SCREWS STILL ATTACHED TO FWD PLUG SECTION. NO DAMAGE FOUND TO AIRCRAFT. REPLACING FWD AND AFT EXHAUST PLUGS. FOUND INSULATION BLANKET ENG COVER DAMAGED. REMOVED AND REPLACED INSULNov 6, 2009 · N860DA · Boeing 777232 · Engine Collector/Tailpipe/NozzleSDR CA090915002Duct · ruptured(CAN) 2 ENGINES FAILED TO START DUE INSUFFICIENT DUCT PRESSURE. INVESTIGATION DISCOVERED RUPTURED STARTER DUCT ASSY ON INSIDE RADIUS OF ELBOW. REPLACEMENT CARRIED OUT. (TC# 20090915002)Sep 13, 2009 · Airbus A330243 · Engine Starter
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