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"

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SDR WRLA20100907452Coalescer Bag · cloggedAFTER LANDING SMOKE IN COCKPIT. AFTER INVESTIGATION FOUND SYS NR 1,2, AND 3 AIR CONDITIONING COALESCER BAGS CLOGGED AND DIRTY, R & R SYS NR1,2, AND 3 COALESCER BAGS, OPS CK GOOD (NO SMOKE NOTED) IAW AMM 21-50. ACFT WAS INBOUND FLIGHT 8128, OUT BOUND FLT 8129Sep 7, 2010 · N270WA · Doug MD11 · Humidity Control SystemSDR IPXA10662571Floor Panel · damagedINSPECTION TYPE:C, MCD STA 685 TO 764, RBL 77" TO RBL 89" FLOOR PANEL FOUND 1 DAMAGE & 6 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Sep 7, 2010 · N331UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662637Skin · misrepairedINSPECTION TYPE:C, SURVEY SEQUENCE NR331-F1-02 THE EXISTING REPAIR PATCH DOES NOT CORRELATE TO A SRM JUST AT BS 446 TO 461 BETWEEN STR -23R AND STR 25R. FX SKIN REPAIRED IAW HX RS R53-31-36824 REV A & EO B767-5330-39678-A. JUST AT BS446-461 BTN STR 23R & 25RSep 7, 2010 · N331UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR FDEA201009063298Frame · crackedUPPER AFT FUSELAGE FRAME CLIP AT CANT STATION Y = 2069.44, CRACKED APPROX 1 INCH IN LENGTH. R & R IAW SRM 51-31-01, REV 44. THIS REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.Sep 6, 2010 · N595FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201009043275Unknown · odorAFTER 45 MINUTE GOT MAIN DECK LOOP FAULT AND ALMOST IMMEDIATELY MAIN CARGO SMOKE. DONNED O2 MASKS. AFTER A FEW SECONDS GOT AVIONICS SMOKE. ENROUTE WE HAD DETECTED WHAT SEEMED LIKE HOT AIR COMING FROM THE AIR CONDITIONING, EVEN THOUGH THE TEMPERATURES WERE SHOSep 4, 2010 · N684FE · Airbus A300F4605R · Air Distribution SystemSDR FDEA201009043274Web · crackedLOWER VERTICAL STABILIZER AT PANEL NR 363QL INTERIOR AREA, WEB FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 55-30-02 FIGURE 201 REPAIR 2, REVISION 44 AND EA 1-5530-143725, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 111.Sep 4, 2010 · N595FE · Doug MD11F · Vertical StabilizerSDR FDEA201009033253Stringer · corrodedIN FWD CARGO AT FRONT FACE OF PRESSURE BULKHEAD FR 39 ALL THE WAY TO BOTTOM AND 24 " LT OF BOTTOM CTR THERE IS CORROSION APPROX 8 SQ INCHES AT STRINGER 50L. REMOVED CORROSION AND DAMAGED AREA IAW SRM 53-15-17 PG 215-216 . REPAIRED AREA BY INSTALLING 1 EA DOUBSep 3, 2010 · N425FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201009023239Seat Track · corrodedRIGHT NR 1 SEAT TRACK CORROSION AT FR58 POSITION. REMOVED THE CORROSION TRACK. POSITION AND TRANSFER DRILL THE FASTENER HOLES. REINSTALL WITH FASTENER. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Sep 2, 2010 · N673FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009023249Floorbeam · crackedIN FWD CARGO MAIN DECK FLOORBEAM (FR 37) AT 27 INCHES RT OF CTR LINE. FWD FACE IS A CRACK IN THE UPPER SIDE OF THE BEAM APPROX .7500 INCH LONG REMOVED DAMAGE SECTION , INSTALLED NEW BEAM SECTION IAW SRM 53-10-15, FIG 201.Sep 2, 2010 · N425FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201009023250Beam · corrodedLONGITUDENAL BEAM Y953 BETWEEN FR 12A AND FR 14 HAS EXFOLIATION CORROSION IN THE MAIN DECK. REMOVED CORROSION IAW SRM 51-74-10, CHECKED, FOUND OUT OF LIMIT. FABRICATED NEW TEE CAP AND REPAIRED IAW SRM 53-12-15 AND DWG 12A536-10797.Sep 2, 2010 · N425FE · Airbus A310203 · Fuselage Main, StructureSDR HALA2010090100386Unknown · unknownETOPS SIGNIFICANT SYS - RAN PACKS AND TROUBLESHOT PACK SYS IAW FIM 21-51-00-1 ALL CHECKS WERE NORMAL-PACK TEMP CONTROLLER BITE HAD NO FAULTS-OK FOR SERVICE. RAN PACKS AND TROUBLESHOT PACK SYS IAW FIM 21-51-00-1. ALL CHECKS WERE NORMAL-PACK TEMP CONTROLLER BISep 1, 2010 · N596HA · Boeing 767332 · Standard Practices/StructuresSDR UIEA2010090100154Skin · damagedEO 4452A084 DURING WALKAROUND INSP, MX FOUND THE CARGO DOOR OUTER SKIN WITH DENT/SCRATCH DAMAGE, MEASURES: 2.0 IN LONG X 1.5 IN WIDE X 0.125 IN DEEP. THE DENT IS OUT OF LIMITS IAW THE SRM 52-30-01, FIG 101, DETAIL XI, ALLOWABLE DAMAGE 1. THE BULK CARGO DOOR OSep 1, 2010 · N499MC · Boeing 74747UF · Cargo/Baggage DoorsSDR IPXA10662335Pump · inoperativeCTR HYD SYS FLUID LOSS IN FLIGHT. CTR PUMP OUTPUT C1 3270 PSI OVER PRESS. NOT IN LIMITS. R & R C1 CTR HYD PUMP IAW AMM 29-11-02-4. OPS GOOD. NO LEAKS NOTED.Sep 1, 2010 · N322UP · Boeing 76734AF · Hydraulic Pump (Electric/Engine), MainSDR UIEA2010083100150Nose Cowl · damagedDURING WALK AROUND INSP, IN MX, FOUND THE NR 3 ENGINE INLET NOSE COWL L/E DENTED (SUSPECTED BIRD-STRIKE) AT APPROX 4 O' CLOCK POSITION MEASURING 5.5 INCHES IN LENGTH, 3.0 INCHES WIDTH AND 0.5 INCH DEPTH. AFTER DETAIL VISUAL INSP (10X MAGNIFYING GLASS) IT WAS VAug 31, 2010 · N408MC · Boeing 74747UF · Engine Air Intake SystemSDR UIEA2010083100152Skin · crackedDURING A-CHECK, GOUGES AND A CRACK WERE FOUND IN THE FUSELAGE BELLY SKIN BETWEEN BS 2585 AND 2587 AND S-47L AND -47R. REFER TO FIG 1 FOR DAMAGE LOCATION AND DESCRIPTION. (THE FUSELAGE SKIN AT THE DAMAGE LOCATION IF MADE FROM A 0.050 INCH THICK SKIN WITH A 0.04Aug 31, 2010 · N412MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR DALA1021651808Socket · intermittentEMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT 6D. LIGHT SOCKET IS INTERMITTENT. CURRENTLY ON MCO.Aug 31, 2010 · N832MH · Boeing 767432ER · Emergency LightingSDR UIEA201000206Seat Track · damagedDURING D-CHECK INSP OF DATUM ACFT, WORN DAMAGE WAS FOUND ON CROWN AREA OF MAIN DECK SEAT TRACK NEAR STA 1140, RBL 11.33. EGAT PERFORMED REPAIR IAW SRM 53-40-52, REPAIR 3 WITH DEVIATION ABOUT FASTENER PATTERN COMMON TO SEAT TRACK HORIZ FLANGE DUE TO EXISTING FAug 31, 2010 · N497MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA201000208Skin · dentedDURING D02, C03 CHECK OF DATUM ACFT AT EGAT, DENT WAS FOUND ON LT HORIZONTAL STAB L/E LOWER SKIN OUTER SURFACE AT STAB STA 147. THE DETAILED LOCATION IS SHOWN IN FIG 1. EGAT PROPOSED TO REPAIR SRM 55-10-01, REPAIR 5 SRM, BUT SINCE THE SRM REPAIR IS A CATEGORY Aug 31, 2010 · N497MC · Boeing 74747UF · Horizontal Stabilizer, Plate/SkinSDR FDEA201008303199Floor Support · corrodedMAIN DECK CARGO COMPT 10 IN AFT OF FR 14 , 57 IN. LT OF CTR LINE FLOOR SUPPORT CHANNEL HAS 4 SQ IN OF LEVEL 1 CORROSION ON UPPER SURFACE OF CHANNEL. REMOVED LEVEL 1 CORROSION. DURING CORROSION REMOVAL FOUND FLOOR SUPPORT CHANNEL OUT OF LIMITS. R & R FLOOR SAug 30, 2010 · N425FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR HALA2010083000384Sensor · malfunctionedEICAS MSG, T/E FLAP DISAGREE DISPLAYED AND T/E FLAP LIGHT ILLUMINATED WITH FLAP LEVER AND INDICATOR IN SAME POSITION. R & R FLAP LEVER POSITION RVDT M603 IAW AMM 27-51-26 GROUND CHECK GOOD. R & R OTBD L/E NR2 SENSOR IAW AMM 27-81-11. OPS CKS OK, NO FAULT OR MAug 30, 2010 · N598HA · Boeing 767332 · Trailing Edge Flap Control SystemSDR FDEA201008303202Skin · dentedRT WING - INBD FLAP LOWER SURFACE FOUND DENT AT XIFH 198. DENT AREA TRIMMED OUT AND FABRICATED NEW SKIN AND DOUBLER AS PER SRM 57-50-01, FIGURE 201 REPAIR 2, REVISION 44. NEW SKIN AND DOUBLER INSTALLED AS PER SRM 57-50-01 FIGURE 201, REVISION 44. REPAIRAug 30, 2010 · N595FE · Doug MD11F · Trailing Edge FlapsSDR HALA2010082800382Control Valve · failedETOPS SIGNIFICANT SYS - APU FAILED TO START (2X) APU FAULT. APU ECU BITE CK SHOWS "FIRE EMERG" & "REV FLOW" FAULTS WIRING CKS GOOD FROM RELAY K421 TO SHUTDOWN SW S484 REPL K421 FOR PRECAUTION IAW FIM 49-11-00, FIG 103. R & R SURGE CONTROL VALVE IAW AMM 49-53Aug 28, 2010 · N598HA · Boeing 767332 · APU Start/Ignition SystemSDR FDEA201008283167Seat Track · damagedMAIN FLOOR SUPPORT FLANGE UPPER SURFACE OF SEAT TRACK GOUGED .5 SQ IN. LOCATED 4 IN FWD OF FR 17 AND 37IN RT OF CTR LINE. BLENDED GOUGE IN MAIN FLOOR SUPPORT FLANGE 4IN FWD OF FR17 AND37IN RT OF CTR LINE IAW SRM 51-74-10. CHECK LIMITS FOUND OUT OF LIMIT IAug 28, 2010 · N425FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR UIEA201000209Intercostal · crackedTHE PURPOSE OF THIS EO IS TO DOCUMENT THE PERMANENT REMOVAL OF CRACK DAMAGE FROM AREAS OF 65B06165-49 INTERCOSTAL. REPAIR OF CRACK DAMAGE AT BS 2000 ON INTERCOSTAL AT BL 0 AS DOCUMENTED IAW EGAT NCR 609 WAS REPAIRED IAW EGAT EI T2010A53B-1876. THE DAMAGED INTEAug 28, 2010 · N497MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA201000210Intercostal · crackedTHE PURPOSE OF THIS EO IS TO DOCUMENT THE PERMANENT REMOVAL OF CRACK DAMAGE FROM AREAS OF INTERCOSTAL. REPAIR OF CRACK DAMAGE AT BS 2000 ON INTERCOSTAL AT RBL 7.5 AS DOCUMENTED IAW EGAT NCR 610 WAS REPAIRED IAW EGAT EI T2010A53B-1888. THE DAMAGED INTERCOSTAL WAug 28, 2010 · N497MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA201000211Intercostal · crackedREPAIR OF CRACK DAMAGE AT BS 2040 AND BS 2060 ON INTERCOSTAL AT RBL .625 AS DOCUMENTED PER EGAT NCR 612 & NCR 614 WERE REPAIRED IAW EGAT EI T2010A53B-1825. THE DAMAGED INTERCOSTAL WAS CUT AT BS 2070 AND THE DAMAGED SECTION OF THE INTERCOSTAL WAS REMOVED. A REAug 28, 2010 · N497MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA201000212Intercostal · crackedREPAIR OF CRACK DAMAGE AT BS 2000 ON INTERCOSTAL AT RBL 22.5 AS DOCUMENTED IAW EGAT NCR 611 WAS REPAIRED IAW EGAT EI T2010A53B-1889. DAMAGED INTERCOSTAL WAS R & R. REPLACEMENT INTERCOSTAL WAS MFG IAW DWG 65B06165 AS AUTHORIZED IAW MFG SMAL PO225769. THE REPLAAug 28, 2010 · N497MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA201000213Intercostal · crackedREPAIR OF CRACK DAMAGE AT BS 2040 AND BS 2060 ON INTERCOSTAL AT RBL 7.625 AS DOCUMENTED IAW EGAT NCR 613 & NCR 615 WERE REPAIRED IAW EGAT EI T2010A53B-1824. DAMAGED INTERCOSTAL WAS CUT AT BS 2070 AND THE DAMAGED SECTION OF THE INTERCOSTAL WAS REMOVED. A REPLAug 28, 2010 · N497MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA201000214Intercostal · damagedREPAIR OF CRACK DAMAGE AT BS 2100 ON INTERCOSTAL AT LBL 7.625 AS DOCUMENTED IAW EGAT NCR 616 WAS REPAIRED IAW EGAT EI T2010A53B-1810. DAMAGED INTERCOSTAL WAS CUT AT BS 2090 AND THE DAMAGED SECTION OF INTERCOSTAL WAS REMOVED. A REPLACEMENT SECTION OF 65B06165-Aug 28, 2010 · N497MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR FDEA201008273165Floor Support · corrodedMAIN DECK CARGO COMPARTMENT 10 IN AFT OF FR 14, 53 IN LT OF C/L FLOOR CHANNEL SUPPORT FOR COURIER SEAT HAS 3 SQ IN OF CORROSION AROUND ANCHOR NUTPLATES TOP SURFACE. REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED FLOOR SUPPORT (WEB) AND REPLACED WITH NEW PART BEAug 27, 2010 · N425FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201008263152Seat Track · damagedMAIN CARGO DECK FLOOR STRUCTURE FRAME 54.2 SEAT TRACK STRUCTURE 3R HAS 1 EA .1875" DRILL START (MISDRILL). R & R SEAT TRACK 3R IAW SRM 51-72-10 ON MAIN DECK FLOOR STRUCTURE FR54 TO FR 54.2Aug 26, 2010 · N425FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201008263154Floorbeam · crackedMAIN CARGO DECK FLOOR STRUCTURE FR 54.3 BETWEEN SEAT TRACKS 2R AND 3R HAS 1 EA, .25 " CRACK IN STRUCTURE CROSSBEAM. CUT OUT DAMAGED AREA OF CROSSBEAM IAW SRM 53-10-15, FIG 204. NDT VERIFIED CRACKED AREA. REMOVED IAW NTM 51-10-08. FABBED REPAIR PART AND INSTAug 26, 2010 · N425FE · Airbus A310203 · Fuselage Main, Floor BeamSDR IPXA10662347Rib · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT INBD NOSE SKIN SUPPORT RIB FOUND CRACKED JUST AT OSS 572.5, .0652" APPROX IN LENGTH. RT WING NR 9 SLAT INBD NOSE SKIN SUPT RIB REPAIRED WITH FREEZE PLUG & REPAIR STRAP INSTALL IAW RS R57-40-36815 & EO B767-5750-39486-A JUSAug 26, 2010 · N334UP · Boeing 76734AF · Leading Edge DevicesSDR FDEA201008253133Stringer · misrepairedPREVIOUS STRINGER REPAIR LOCATED IN AFT CABIN UNDER FLOOR BEHIND BULK CARGO ON STRINGER 39 LT BETWEEN FRAMES 73 TO 74, HAS 1 EACH REPAIR ANGLE SPLICE 12.6" LONG WITH A STRINGER CUTOUT OF 4.4" LONG. PREVIOUSLY INSTALLED REPAIR LOCATED AT AFT CABIN UNDERFLOOR BAug 25, 2010 · N425FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201008253130Relay · malfunctionedAT APPROX 400' AGL WHILE FLYING RNAV/GPS APP RWY 29. RECEIVED "TO LOW GEAR" CALL OUT. EXECUTED GO AROUND. SELECTED SYS NR 2 ON GEAR AND LANDED WITHOUT OTHER WARNINGS. PER TSM INSPECTED NLG MSW 79GB, NO DEFECTS NOTED. CLEANED AND RESEATED C/P ONAug 25, 2010 · N405FE · Airbus A310203 · Landing Gear Position and WarningSDR IPXA10662346Fairing · delaminatedINSPECTION TYPE:C, RT WING OTBD T/E FLAP L/E FAIRING FOUND DELAMINATION. HOT BOND REPAIR PERFORMED IAW SRM 51-70-05 PAR 5A (1) FIG 5, REV 47.Aug 25, 2010 · N334UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10662348Flap · misrepairedINSPECTION TYPE:C, RT WING INBD AFT FLAP INBD FWD CORNER NON-STANDARD REPAIR DOUBLER. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R. REPAIR 4, FIG 202, SHEET 1, REV 47.Aug 25, 2010 · N334UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10662349Panel · misrepairedINSPECTION TYPE:C, LT WING NR 4 SLAT CLOSURE PANEL NON-STANDARD REPAIR HOT BOND REPAIR PERFORMED IAW SRM 51-70-17, PAR 4K, FIG 16, REV 47.Aug 25, 2010 · N334UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10662288Skin · crackedINSPECTION TYPE:C, RT WING NR9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR9 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, JUST AT OSS572.5 ORG MATL 7075T6-0063" CRACK LENGTH 0.164" DAMAGE CUTOUT 8.75" X 7.125" THIS IS CLASSIFIED AS Aug 24, 2010 · N334UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10662310Floor Panel · damagedINSPECTION TYPE:C, MCD STA 977 TO 1119 LBL 11 TO RBL 11, FLOOR PANEL FOUND 1 DAMAGE & DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & REINSTALLED IAW AMM 53-01-01.Aug 23, 2010 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662312Floor Panel · dentedINSPECTION TYPE:C, MCD STA 930 TO 977, LBL 11 TO RBL 11 FLOOR PANEL FOUND 1 CRACK (5" LONG) & 4 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & REINSTALLED IAW AMM 53-01-01.Aug 23, 2010 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662313Floor Panel · damagedINSPECTION TYPE:C, MCD STA 830 TO 930 LBL 11 TO RBL 11 FLOOR PANEL FOUND 1 DAMAGE & 10 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & REINSTALLED IAW AMM 53-01-01.Aug 23, 2010 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662314Floor Panel · damagedINSPECTION TYPE:C, MCD STA 720 TO 830 LBL 11 TO RBL 11 FLOOR PANEL FOUND 2 DAMAGED & 9 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & REINSTALLED IAW AMM 53-01-01.Aug 23, 2010 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662324Floor Panel · damagedINSPECTION TYPE:C, MCD STA 830 TO 930 LBL 11 TO LBL 33, FLOOR PANEL FOUND 1 DAMAGED & 4 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & REINSTALLED IAW AMM 53-01-01.Aug 23, 2010 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR HALA2010082200375Apu · malfunctionedETOPS SIGNIFICANT SYS - APU FAILED TO START AFTER LANDING. HIGH EGT BUT LOW RPM APU FAULT EICAS MSG. BITE CHECK PC FIM 49-11-00, FIG 103 NO FAULT NOTED. STARTED APU 3X OPS CHECK GOOD. NO DEFECTS NORMAL. SECURITY CONDITION GOOD.Aug 22, 2010 · N598HA · Boeing 767332 · APU Core EngineSDR IPXA10M62072Battery Pack · dischargedEMER LIGHT BAT 1 LOW. T/S & FOUND BATTERY EMER LOW. R & R EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51- 01-4. TEST OK, IAW FIM 33-51-00-810-801. ACFT OK FOR SVC.Aug 22, 2010 · N252UP · Doug MD11F · Emergency LightingSDR FDEA201008223089Skin · dentedEXTERIOR SKIN JUST AFT OF AFT CARGO DOOR BETWEEN FRAMES 64 AND 65 AND STR 39R AND 44R HAS MULTIPLE DENTS. DEEPEST DENT MEASURED APROX .7500 IN WIDE,1IN LONG AND .027IN DEEP. NDT CHECK C/W NO CRACKS FOUND IAW NTM 51-10-08. REPAIRED EXTERIOR SKIN BY FABRICATIAug 22, 2010 · N425FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR HALA2010082200377Actuator · failedETOPS SIGNIFICANT SYS - APU FAULT ICAS AND APU AUTO SHUTDOWN. BITE CHECKED APU ECU AND FOUND "DOOR SYS" FAULT ON ECU. REPLACED RELAYS K547 AND K176 IAW FIM 49-11-00/101 FOR PRECAUTIONARY. R & R APU DOOR ACTUATOR MM 49-15-06 RR APU DOOR OPEN SWITCH IAW MM 49-1Aug 22, 2010 · N598HA · Boeing 767332 · APU Core EngineSDR DALA1019945525Floor Support · corrodedDURING M-CHECK, FOUND CORROSION ON FLOOR SUPPORT CHANNEL AT BS 377.7, BL0, WL 208. REPAIRED IAW SRM 51-40-05.Aug 20, 2010 · N525US · Boeing 757251 · Fuselage Miscellaneous StructureSDR HALA2010081800373Relay · malfunctionedETOPS SIGNIFICANT SYS - APU FAULT MSG DISPLAYED ON EICAS, APU DID NOT START, 3RD ATTEMPT. ACOMPLISHED FIM 49-01-00 FAULT CODE 34. REPLACED K117 RELAY IAW WDM 49-41-11AND SB 767-49-00368, AND EO49-05-02-72, REV B. OPS CHECK OK. ALSO FOUND OIL LEAK AT APU OIAug 18, 2010 · N598HA · Boeing 767332 · APU Core Engine
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