Boeing 757-2Y0

Service difficulty reports · 830

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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 = '7572Y0'
  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 6PMR2020082900397Pressure Deck · corrodedAIRBORNE/PEMCO NON-ROUTINE 2867N258 DISCREPANCY: RMWW UPPER PRESSURE DECK HAS CORROSION BETWEEN STA 1148 QND STA 1180 FROM RBL 16 TO RBL 45. CORRECTIVE ACTION: REMOVED CORROSION ON RT W/W PRESSURE DECK AREA FOUND TO BE ACCEPTABLE AS IS, TREATED AND PRIMED I/AJul 15, 2020 · N753CX · Boeing 7572Y0 · Fuselage Main, StructureSDR 6PMR2020082600383Pressure Blkhd · corrodedAIRBORNE/PEMCO NON-ROUTINE 2867N280 DISCREPANCY: LT W/W PRESSURE DECK HAS CORRODED WEB STRAP NEAR FASTENERS AT BS 1110 LBL 53-59. CORRECTIVE ACTION: EVALUATED PRESSURE DECK WEB STRAP AT BS 1110 LBL 53-59, ALL (21) AREAS FOUND TO BE ACCEPTABLE, AS IS PER EO# 2Jul 15, 2020 · N753CX · Boeing 7572Y0 · Fuselage Main, BulkheadSDR 6PMR202008250367Keelbeam · corrodedAIRBORNE/PEMCO NON-ROUTINE 2867N279 DISCREPANCY: LT W/W INNER BULKHEAD WEB CORRODED AT PASS THRU BS 1175 LBL 0. CORRECTIVE ACTION: CLEANED AND EVALUATED LT WW INNER BULKHEAD WEB ORIGINAL MATERIAL .130", MATERIAL LOSS .040", MATERIAL REMAINING .090", FOUND TO Jul 15, 2020 · N753CX · Boeing 7572Y0 · Fuselage Main, KeelSDR 2020F00360Keelbeam · corrodedAIRBORNE/PEMCO NON-ROUTINE 2867N279 DISCREPANCY: LH W/W INNER BULKHEAD WEB CORRODED AT PASS-THRU BS 1175 LBL0 CORRECTIVE ACTION: CLEANED AND EVALUATED L/H WW INNER BULKHEAD WEB ORIGINAL MATERIAL .130", MATERIAL LOSS .040", MATERIAL REMAINING .090" FOUND TO BE Jul 15, 2020 · N753CX · Boeing 7572Y0 · Fuselage Main, Attach FittingsSDR FDEA2020040630685Intercostal · crackedAFT CARGO COMPT. AFT BULKHEAD INTERCOSTAL BETWEEN FLOOR BEAMS BS. 1681.8 AND BS. 1701, IS CRACKED AT FWD SIDE ON RADIOUS AT BS. 1681.8 BL-0. REMOVED INTERCOASTAL CHANNEL STA 1681.8 TO 1701 BL0 IAW B757 SRM 51-40-02. FABRICATED, LOCATED, DRILLED AND INSTALLApr 3, 2020 · N930FD · Boeing 7572Y0 · Fuselage Miscellaneous StructureSDR FDEA2020040320659Strap · missingAFT CARGO COMPT. AFT BULKHEAD FLOOR BEAM BETWEEN BS 1681.8 AND BS 1701,FLOOR BEAM IS MISSING STABILIZER STRAP ON INTERCOSTAL WEB LOWER FLANGE AT BL-0. FABRICATED, LOCATED, DRILLED AND INSTALLED STABILIZER STRAP STA 1681.8 TO 1701 BL0 IAW BOEING DWG 146N519Apr 2, 2020 · N930FD · Boeing 7572Y0 · Fuselage Main, Floor BeamSDR FDEA2020031210534Collar · brokenL1 DOOR HOLD OPEN LOCK COLLAR BROKEN. REMOVED PANEL 221AL TO GET ACCESS TO COLLAR AS PER MM 52-11-08-4. INSTALLED COLLAR AND CATCH ASSY AS PER AMM 52-11-08-8. OPS CHECK OK. STILL NEED TO INSTALL THE 221AL PANEL WHICH STILL IN LEAD OFFICE. INSTALLED PANEL Mar 11, 2020 · N974FD · Boeing 7572Y0 · Passenger/Crew DoorsSDR FDEA2020030970502Unknown · odorFUMES IN COCKPIT ON TAKEOFF ROLL TILL ABOUT 5K FT. REQUIRED CREW TO DON O2 MASK IMMEDIATELY AFTER TAKEOFF. ODOR OF BURNT RUBBER/ENG SMELL MAINLY ON CAPTAINS SIDE. FO DID NOT DETECT ODOR. ODOR CLEARED BEFORE CREW COULD SECURE ANY EQUIPMENT. NO FURTHER OCCMar 7, 2020 · N961FD · Boeing 7572Y0 · Air Distribution SystemSDR FDEA2020021420331Line · leakingAFTER TAKEOFF, RAISED GEAR HANDLE TO UP. RECEIVED A GEAR DOORS EICAS AND DOORS LIGHT. COMPLED WITH QRH. NO OTHER ASSOCIATED PROBLEMS. PERFORMED B757 FIM 32-09 FT804, PSEU BITE TEST, NO HISTORY FAULTS STORED OR CURRENT FAULTS PRESENT AT THIS TIME. FAULTFeb 12, 2020 · N930FD · Boeing 7572Y0 · Hydraulic System, MainSDR FDEA201912063197Power Supply · inoperativeLT PASSENGER DOOR EXTERNAL EMERGENCY LIGHT L25 INOP. POWER SUPPLY M731 REPLACED.Dec 6, 2019 · N974FD · Boeing 7572Y0 · Emergency LightingSDR IXXA20191029019Cabin Pressure · malfunctionedIN CRUISE AT FL360, EICAS MSGS CABIN ALT AND CAB AUTO INOP. CREW REPORTS CABIN ALTITUDE AROUND 12,000 PLUS FEET, WITH AN ESTIMATED RATE OF PLUS 300 TO 400 INCREASE. CREW NOTED SLIGHT PRESSURIZATION LEAK, DONNED 02 MASKS AND PERFORMED QRH PROCEDURES. BOTH AUTO Oct 24, 2019 · N753CX · Boeing 7572Y0 · Cabin Pressure Control SystemSDR IXXA20191024017Battery Pack · inoperativePILOT REPORT: R1 DOOR EMERGENCY EXIT LIGHT AND EXTERNAL LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY IAW AMM 33-51-07. OPERATIONAL CHECK SATISFACTORY. FAULT NOT DUPLICATED. AIRCRAFT RELEASED TO SERVICE.Oct 22, 2019 · N754CX · Boeing 7572Y0 · Emergency LightingSDR IXXA20191024016Battery Pack · inoperativePRE DEPARTURE CHECK: R-4 EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY IAW AMM 33-51-07. OPERATIONAL CHECK SATISFACTORY. FAULT NOT DUPLICATED. AIRCRAFT RELEASED TO SERVICE.Oct 21, 2019 · N754CX · Boeing 7572Y0 · Emergency LightingSDR FDEA201909102200Shutoff Valve · inoperativePDIS 974 36-10 5902 10SEP19 CDG OPEN U LOGPAGES:3010680 REJECTED TAKEOFF FOR " L ENG BLEED OFF " AFTER ENGINE REDUCED IDLE EICAS MESSAGE REMOVED. GOT EICAS MESSAGE ON SECOND TAKEOFF AND AFTER AIRBORNE RAN QRH AND SELECTED LEFT ENGINE BLEED AIR Sep 10, 2019 · N974FD · Boeing 7572Y0 · Pneumatic Distribution SystemSDR FDEA2019083092040Skin · delaminatedRH I/B FLAP, LOWER SURFACE REPAIR 52" FORM O/B EDGE AND 13" FORM T/E. REPAIR FOUND TO BE UNSERVICABLE PLEASE PERFORM REPAIR IAW SRM 57-53-01-0I IDENT 1, SRM 57-53-01- 2R REPAIR 1, AND SRM 51-70-10-2R. RH I/B MAIN TRAILING EDGE FLAP REPLACED IAW AMM 27-51-02Aug 29, 2019 · N974FD · Boeing 7572Y0 · Trailing Edge FlapsSDR FDEA2019082191948Panel · corrodedNR 2 ENG I/B C-DUCT UPPER BIFURICATION PANEL DAMAGE UPPER BIFURICATION UPPER TRACK BEAM SUPPORT PANEL EVALUATED AND FOUND TO BE CORROSION. CORROSION OUT OF LIMITS AS PER EM 78-31-28-300-085 REPLACED THE THRUST REVERSER ASSY IAW W/O:00074899 WRI:78305814 ANDAug 19, 2019 · N974FD · Boeing 7572Y0 · Engine Thrust ReverserSDR FDEA2019082191940Skin · damagedUPON EVALUATION OF AGING AIRCRAFT INSPECTION OF EXISTING DOUBLER AND TRIPLER REPAIR @ BSTA 620-624, STR21R - STR24R DAMAGED FASTENER HOLE FOUND ON INTERNAL SKIN WORK INSTRUCTIONS CARRIED OUT IAW FEDEX E.A.#F-5330-T0348760 TITLE: AD 2006-11-11 - FUSELAGE - Aug 19, 2019 · N974FD · Boeing 7572Y0 · Fuselage Main, Plate/SkinSDR FDEA2019082181930Nozzle · crackedNR 1 ENGINE CNA HAS CRACKS AT THE 3 O'CLOCK AND 9 O'CLOCK POSITIONS. CRACKS REMOVED IAW EM 78-11-04 AND CRACKS REPAIR IAW E.A. F-7810-T0348465.Aug 18, 2019 · N974FD · Boeing 7572Y0 · Engine Collector/Tailpipe/NozzleSDR FDEA2019082181931Panel · crackedSLAT #6 IN/B T/E SKIRT (FLEX PANEL) IS CRACKED. REPAIRED CRACK IAW SRM 51-70-17 GENERAL & E.A. F-5750-T0348677Aug 18, 2019 · N974FD · Boeing 7572Y0 · Leading Edge DevicesSDR FDEA2019081541877Skin · dentedDENT OUTSIDE PERMITTED LIMITS IAW SRM 53-00-01 ALLOWABLE DAMAGE FIG101 DETAIL III @ B/S 580-597 STR 25L REAPIRED DENT IAW FEDEX EA# F-5300-T0348400 (P1) AND SRM 51-00-01 REPAIR 28 FIG 1Aug 14, 2019 · N974FD · Boeing 7572Y0 · Fuselage Main, Plate/SkinSDR FDEA2019081531854Stringer Clip · crackedSTRINGER CLIP ' B/S 1500 STR2 WAS FOUND DAMAGED AND CRACKED . REPLACED STRINGER CLIP IAW SRM 51-40-02Aug 13, 2019 · N974FD · Boeing 7572Y0 · Fuselage Main, Attach FittingsSDR FDEA201908121843Seat Track · corrodedSEAT TRACK B/S 364 RBL 47-51 CORRODED BEYOND PERMITTED LIMITS. REPAIRED IAW FEDEX EA F-5310-T0348507(P1).Aug 12, 2019 · N974FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201908071844Floor Support · noneEXISTING REPAIR FOUND ON FLOOR SUPPORT STRUCTURE BS 570 APPROX. LBL 10. REPAIR REQUIRES EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA EVALUATION CARRIED OUT OF EXISTING REPAIR ON FLOOR SUPPORT STRUCTURE AT BSAug 7, 2019 · N974FD · Boeing 7572Y0 · Standard Practices/StructuresSDR FDEA2019080211788Strap · crackedSTRAP CRACKED FWD GALLEY FLOOR BS 367 ,LBL 24 FABRICATED NEW STRAP AND REPLACED OLD PART IAW EA F-5310-T034848 PART 1, SRM 53-00-5-2R, REPAIR 13, AND GMM. 7-0-1001.Aug 1, 2019 · N974FD · Boeing 7572Y0 · Fuselage Miscellaneous StructureSDR FDEA2019080211787Floor Panel · delaminatedFLOOR PANEL DAMAGED @ DOORWAY #1R OUTSIDE PERMITTED LIMITS IAW SRM53-00-50-1A REPAIRED FLOOR PANEL IAW SRM 53-00-50-2RAug 1, 2019 · N974FD · Boeing 7572Y0 · Fuselage Floor PanelSDR FDEA2019080211786Floor Panel · delaminatedFLOORBOARD @ 1L DOORWAY DAMAGED OUTSIDE PERMITTED LIMITS IAW SRM 53-00-50-1A. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2RAug 1, 2019 · N974FD · Boeing 7572Y0 · Fuselage Floor PanelSDR FDEA201907281732Seat Track · corrodedSEAT TRACK HAS EVIDENCE OF CORROSION @ B/S-344-356 AND 367-374. REMOVED SEAT TRACK SECTION IAW SRM 51-40-02. REMOVED CORROSION FROM SEAT TRACK SECTION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A FIG101 DETAIL 1. MATERIAL REMOVED 0.060" MAX ALLOWABLE 0Jul 28, 2019 · N974FD · Boeing 7572Y0 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201907251689Cargo · fumesDURING CLIMBOUT HAD STRONG UNKNOWN FUMES IN COCKPIT FOR 2-3 MINUTES. THAN SEEMED TO BE DISSAPPATING, BUT AT LEVEL OFF AT FL 380 STARTED COMING BACK. DECLARED AN EMERGENCY AND DIVERTED. PER B757 FIM 21-00-01-3 VERIFIED ALL ENG OIL AND HYD NOT OVER SERVICED.Jul 25, 2019 · N930FD · Boeing 7572Y0 · Air Distribution SystemSDR FDEA201907081504Warning System · false activationPDIS 974 27-50 5786 08JUL19 TLV OPEN U LOGPAGES:3010096 TE FLAP ASYM INDICATED WHEN FLAPS SELECTED TO "1". FOLLOWED QRH PROCEDURES TO LANDING. TOUCHDOWN SPEED WAS APPROX 170 KIAS. FIM 27-51 TREE 805 PERFOMED NO FINDINGS, FLAPS SYS OPER TEST PERFORJul 8, 2019 · N974FD · Boeing 7572Y0 · Trailing Flap Position Indicating SystemSDR IXXA201908310001Structure · corrodedLEFT MAIN LANDING GEAR HAS CORROSION ON CEILING AFT OF THE LEFT HYDRAULIC RESERVOIR. CORROSION OUT OF LIMITS. ORIGINAL MATERIAL 140", MATERIAL REMOVED .040, MATERIAL REMAINING .100. ALL REPAIRS PER FVCI ENGINEERING ORDER 19158.Jun 19, 2019 · N754CX · Boeing 7572Y0 · Fuselage Main, StructureSDR IXXA2019062029012Skin · corrodedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE C-17. IN COMPLIANCE OF GENERAL VISUAL INSPECTION-CORROSION PREVENTION TASK CARD 53-800-10-01, THE FOLLOWING FINDINGS WERE NOTED: BULGED SKIN AT STA 1400 BETWEEN STRINGER 26L AND 27L. WORK IN PROGRESS. REPAIRED BULGED SKIJun 9, 2019 · N754CX · Boeing 7572Y0 · Fuselage Main, Plate/SkinSDR FDEA201905121036Control Valve · malfunctionedDURING CLIMB RECEIVED CABIN ALTITUDE EICAS MESSAGE. DONNED OXYGEN MASKS AND DESCENDED BELOW 10,000 FT. NOTICED OUTFLOW VALVE IN FULL CLOSED POSITION WITH RIGHT PACK OPERATIVE WHICH SHOULD HAVE PRESSURIZED THE AIRCRAFT WITH NO PROBLEM. DM REMOVED AND REPLACMay 12, 2019 · N930FD · Boeing 7572Y0 · Cabin Cooling SystemSDR FDEA201905101022Shutoff Valve · failedPDIS 930 21-30 7416 10MAY19 MEM OPEN U LOGPAGES:3112369 DURING CLIMB RECEIVED CABIN ALTITUDE EICAS MESSAGE. DONNED OXYGEN MASKS AND DESCENDED BELOW 10,000 FT. NOTICED OUTFLOW VALVE IN FULL CLOSED POSITION WITH RIGHT PACK OPERATIVE WHICH SHOULDMay 10, 2019 · N930FD · Boeing 7572Y0 · Cabin Cooling SystemSDR FDEA2019020530254Pressure Deck · wornMAIN CABIN AFT PRESSURE DECK HAS 4 EA BLEND OUTS THAT ARE OUT OF LIMITS AT APPROX. LBL.50 APPROX. STA.1684 TO STA. 1690. INSTALLED DOUBLER REPAIR ON MAIN CABIN AFT DECK PLATE AT STA. 1684 TO STA. 1690 LBL. 50 IAW B757 SRM 53-60-51-2R REPAIR 2 ALTERNATIVE IFeb 3, 2019 · N973FD · Boeing 7572Y0 · Fuselage Main, StructureSDR FDEA201902030253Bulb · inoperativeEMERGENCY SLIDE LIGHT L1 NO LIGHT FACT 03FEB19 11:23 CPH EMERGENCY SLIDE LIGHT L1 BULP REPLACED AMM 33-51-06-2-1 REV 123.4 Feb 3, 2019 · N974FD · Boeing 7572Y0 · Emergency LightingSDR FDEA201901300229Pressure Deck · chafedAFT PRESSURE DECK HAS BLENDS OUT AT STA 1702 RBL 25 TO RBL 33. INSTALLED DOUBLER REPAIR ON AFT DECK IN MAIN CABIN STA. 1702 RBL.25 TO RBL 33 IAW B757 SRM 53-60-51-2R REPAIR 2 ALTERNATIVE I.Jan 30, 2019 · N973FD · Boeing 7572Y0 · Fuselage Main, BulkheadSDR FDEA201901300228Pressure Deck · chafedMAIN CABIN AFT PRESSURE DECK HAS 1 EA BLEND OUT, OUT OF LIMITS AT STA 1708 LBL 25. INSTALLED DOUBLER REPAIR ON MAIN CABIN AFT DECK STA.1708 LBL.25, IAW B757 SRM 53-60 60-51-2R REPAIR 2 ALTERNATIVE I.Jan 30, 2019 · N973FD · Boeing 7572Y0 · Fuselage Main, BulkheadSDR FDEA201901300227Pressure Deck · chafedMAIN CABIN AFT PRESSURE DECK HAS 3 EA BLEND OUTS, OUT OF LIMITS AT APPROX STA 1689 TO STA 1706, RBL 23 TO RBL 35. INSTALLED DOUBLER REPAIR ON MAIN CABIN AFT DECK AT STA.1689 TO STA. 1706, RBL 23 TO RBL 35 IAW B757 SRM 53-60-51-2R REPAIR 2 ALTERNATIVE I.Jan 30, 2019 · N973FD · Boeing 7572Y0 · Fuselage Main, BulkheadSDR FDEA201901110094Insert · unsecureFOUND L1 DOOR SLIDE COVER FWD UPPER LATCH, UNLATCHED. REPAIRED POTTED INSETS REF. AMM 25-00-00-8. REINSTALLED L-1 DOOR SLIDE COVER, DOOR OPS CHECKS NORMAL REF AMM 52-11-02-4.Jan 11, 2019 · N930FD · Boeing 7572Y0 · Passenger/Crew DoorsSDR FDEA2018120653433Actuator · failedPDIS 961 27-80 5336 05DEC18 LEVEL 10000 FT, 220 KIAS AND SLOWING, RECEIVED EICAS " LE SLAT DISAGREE" AND DISCRETE "LEADING EDGE" WHILE EXTENDING FLAPS 1. EMERGENCY DECLARED. COMPLETED INSTALLATION OF BAD ROTARY ACTUATORS IAW Dec 5, 2018 · N961FD · Boeing 7572Y0 · Leading Edge Slat ActuatorSDR FDEA201811283384Inlet · failed82081 APROX 1200 FT AGL EXPERIENCED WHAT WE THOUGHT WAS A LEFT ENG COMPRESSOR STALL. HEARD A LOUD BANG SURGE IN EGT. INSTRUMENTS RETURED TO NORMAL IN A SECOND. DECLARED AN EMERGENCY AND RETURNED TO MEM REMOVED AND REPLACED LEFT ENGINE PER 7180260-01-0Nov 28, 2018 · N973FD · Boeing 7572Y0 · Turbine Engine Air Inlet SectionSDR IXXA20181130043Socket · fodPRE-DEPARTURE CHECK FINDING, RH ENGINE #2 SQUIB LIGHT WILL NOT ILLUMINATE DURING TEST. CLEANED CONTAMINANTS FROM LAMP SOCKET IAW B757 AMM 20-00-00. INITIATED DEFERRAL MAINTENANCE ITEM IAW ATI MEL 26-20-02-01 CAT C NO FLY DATE 12/7/2018. GENERAL VISUAL INSPECTINov 26, 2018 · N753CX · Boeing 7572Y0 · Central WarningSDR FDEA201811173272Stringer · crackedMAIN CABIN STA 1505 STR 1 CRACKED. REMOVED DAMAGED SECTION DIM 12" STA 1500 IAW SRM 53-00-03-2R REPAIR 2 FIG 201 DET 1. REMOVED FWD SECTION ON STR 1 FROM STA 1492 TO EXISTING SPLICED STA 1460 IAW SRM 51-40-02-0G. FABRICATED NEW REPAIR STRINGER SECTION AND SPLINov 17, 2018 · N961FD · Boeing 7572Y0 · Fuselage Main, Longeron/StringerSDR FDEA201811093166Cover · damagedMDIS 973 52-10 4805 09NOV18 AFW OPEN U RAMP REPORTED THAT L1 ENTRY DOOR HAD RUBBER FLAP HANGING DOWN WHEN DOOR OPEN. MEL 09NOV18 06:24 AFW U RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B EXPIRATION : 12NOV18 "MEL 52-11-01-A: L1 Nov 9, 2018 · N973FD · Boeing 7572Y0 · Passenger/Crew DoorsSDR IXXA20181113888Hydraulic Line · damagedON APPROACH TO DESTINATION STATION WSAP, LOSS OF LEFT SYSTEM HYDRAULIC QUANTITY AND SYSTEM PRESSURE. LOSS WAS NOTED AFTER SELECTING LANDING DOWN FOR LANDING. FLAPS CONFIGURED TO 20 BEFORE LOSS OF PRESSURE. APPROACH WAS ABANDONED. HYDRAULIC SYSTEM PRESSURE (LEFNov 6, 2018 · N754CX · Boeing 7572Y0 · Hydraulic System, MainSDR IXXA20181125042Control Panel · faultyNON-REVENUE FLIGHT-REPOSITION-AT MAX POWER TAKE OFF, 1000 AGL SELECTED VNAV, DID NOT ARM/ENGAGE, AUTO THROTTLES DISENGAGED AND INTERMITTENT, RT ENG EGT EXCURSION IN THE ZONE A AREA. VNAV, FL CH, V/S LIGHTED AND ALL SPEED/ALT WINDOWS OPEN. AT LEVEL, MAIN CABIN Oct 10, 2018 · N753CX · Boeing 7572Y0 · Autopilot ComputerSDR FDEA201810092843Bottle · inoperativeON POST FLIGHT FOUND R1 DOOR EMERGENCY POWER RESERVOIR BOTTLE DEPLETED. REPLACED R1 DOOR EMERGENCY POWER RESERVOIR BOTTLE PER AMM 52-11-30-4. A/C OK FOR SERVICE.Oct 9, 2018 · N930FD · Boeing 7572Y0 · Passenger/Crew DoorsSDR IXXA20181008038Skin · corrodedAIRCRAFT GROUNDED FOR SCHEDULED MAINTENANCE. SURFACE CORROSION ON RT O/B HORIZ STAB UPPER SKIN PANEL BETWEEN STA 260- 272 OUT OF LIMITS DUE TO THE DEPTH AND NEARNESS OF THE TWO BLENDS, 9" BETWEEN THE 2 BLENDS. THE BLENDS ARE ON THE EDGE WHERE THE TWO ALUMINUM Aug 22, 2018 · N753CX · Boeing 7572Y0 · Horizontal Stabilizer, Plate/SkinSDR IXXA20181008039Skin · corrodedAIRCRAFT GROUNDED FOR SCHEDULED MAINTENANCE. CORROSION ON INNER AFT FUSELAGE BETWEEN STA 1825 TO AFT OF STA 1844 AT S-27L. FABRICATED REPAIR DOUBLER AFT FUSELAGE BETWEEN STA 1825 TO 1862 IAW EO 13902 AND EA 47279REA04. INSTALLED REPAIR AFT FUSELAGE STA 1825 TOJul 23, 2018 · N753CX · Boeing 7572Y0 · Fuselage Main, Plate/SkinSDR IXXA20181008040Structure · corrodedAIRCRAFT GROUNDED FOR SCHEDULED MAINTENANCE. NOSE WHEEL WELL LEFT LOWER CHORD HAS CORROSION JUST BELOW AFT DOOR AFT HINGE. REMOVED AND REPLACED NOSE WHEEL WELL LEFT LOWER CHORD JUST BELOW AFT DOOR AT HINGE IAW SRM 51-40-02, SRM 53-10-14 AND AMM 32-34-05, AND Jul 15, 2018 · N753CX · Boeing 7572Y0 · Fuselage Miscellaneous Structure
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