Boeing 757-224

Service difficulty reports · 3,824

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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 = '757224'
  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 CALA2022042501059Frame · misrepairedSUPPORT TASK, MAIN CABIN STA 760 L/H FUSELAGE FRAME AT FLOORBEAM HAS A DRILL START, TRANSCRIBED FROM HAECO GSO NRC 9285440 REPAIRED DRILL START ON MAIN CABIN STA 760 L/H FUSELAGE FRAME AT FLOORBEAM IAW UAL ECRA 5332-01026 AND HAECO REO-G23725, HAECO G SO MECH Apr 23, 2022 · N12125 · Boeing 757224 · Fuselage Main, Floor BeamSDR CALA2022042501058Skin · dentedFOUND DENT IN FUSELAGE 2FT AFT OF L1 DOOR APPROX STATION 399 STRINGER S16 DENT APPROX DIMENSIONS 2IN WIDE 3IN HIGH AND 1/8IN DEEP. DENT MEASURSES 1.9 X 2.7 IN WITH DEPTH OF 0.120". LOCATED 6.5 IN REQUESTING QC DO A SKIN THICKNESS INSPECTION AT BLENDED AREA OF Apr 22, 2022 · N34137 · Boeing 757224 · Fuselage Structure (General)SDR CALA2022042101050Stringer · dentedSTRINGER 16L HAS DENT 7" AFT OF STA 395 C/W RII FOR REMOVAL OF DAMAGED SECTION OF STRINGER 16L PER SRM 53-00-03-2R-1 REPAIR 1 STEP 1 PERFORMED HFEC INSPECTION OF INITIAL FASTENER HOLES IAW NDT PT REMOVED DAMAGE SECTION OF STRINGE 16L PER SRM 53-00-03-2R-1 6, 5Apr 21, 2022 · N34137 · Boeing 757224 · Fuselage Structure (General)SDR CALA2022042101037Wire · chafedREF AMES NR 143879-0200-0211 WIRES ABOVE LAV A HAVE EVIDENCE OF SMOKE AND HEAT DAMAGE. REF AMES NR 143879-0200-0211 00 OPS CHECK GOOD. SEE BACK FOR WORK ACCOMPLISHED. REPLACED LAV REPLACED LAV A DOOR SWITCH WIRING AND LAV A CALL RESET SWITCH WI A CALL RESET SWApr 20, 2022 · N12114 · Boeing 757224 · LavatoriesSDR CALA2022041801003Shear Web · noneSUPPORT TASK-- MAIN CABIN SHEAR WEB STA 700-720 RBL25 REQUIRES F ABRICATION. TRANSCRIBED FROM HAECO GSO NRC 9285902 REMOVED AND REPLACED -4 SHEAR WEB IAW B757-200 SRM 51-40-02 AND BOEING DWG 143N5140 REV B. HAECO GSO MECH V917499 INSP QC302Apr 14, 2022 · N12125 · Boeing 757224 · Fuselage Main, StructureSDR CALA2022041801002Deck Plate · corroded(SUPPORT TASK) MAIN CABIN DECK PLATE STA 1716 RBL50 HAS CORROSIO N ON WEB, TRANSCRIBED FROM HAECO GSO NRC 9285434 REMOVED CORROSION ON THE AFT DECK PLATE AT STA 1716 RBL50. REMAI INSP QC302 NING THICKNESS FOUND TO BE .027, REMOVED .044, ORIG .071 PER B75 7-200Apr 14, 2022 · N12125 · Boeing 757224 · Fuselage Main, StructureSDR CALA2022041801000Beam · corrodedSUPPORT TASK MAIN CABIN FLOOR BEAM 1681 CORRODED UNDER AFT DECK PRESSURE PLATE BETWEEN BL 0 AND LBL 54, TRANSCRIBED FROM HAECO G SO NR 9283143 TRANSCRIBED FROM HAECO LP 9283143. REPAIRED IAW ECRA 5365-01097.Apr 14, 2022 · N57111 · Boeing 757224 · Fuselage Structure (General)SDR CALA2022041800997Skin · corroded(SUPPORT TASK) EMPENNAGE INTERIOR FUSELAGE SKIN HAS CORROSION BE TWEEN BS1838 AND BS1850 LBL10 TO LBL15 STREAMER ATTACH. TRANSCRI BED FROM HAECO GSO NR 9282270 TRANSCRIBED FROM HAECO LP 9282270. FABRICATED REPAIR FILLER AND DOUBLER AND STRAP; INSTALLED REPAIR Apr 14, 2022 · N57111 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2022040800911Skin · stainedFLOOR SUPPORT STRUCTURE BELOW AFT R/H LAV HAS BLUE WATER RESUIDU E AT STA 1620-1681 S29R - S29L. CLEANED FLOOR SUPPORT STRUCTURE BELOW RH LAV STA 1620-1681 S29R- 29L IAW SOPM 20-30-03 AND ECRA 2011-01000.Apr 6, 2022 · N29124 · Boeing 757224 · Fuselage Main, StructureSDR CALA2022021800437Hydraulic Line · leakingCOMPLETE LOSS OF LEFT HYD QTY ON SHORT FINAL. NO NOSEWHEEL STRNG AND BROUGHT THE AIRCRAFT TO A STOP AND SHUT DOWN THE ELECTRIC PUMPS, (HYD QTY WAS AT 1.6), STARTED APU AND SHUT DOWN #2 ENGINE. CALLED FOR TOW TO GATE. INFO ONLY PER CREW: ON SHORT FINAL AFTER GEFeb 17, 2022 · N17139 · Boeing 757224 · Hydraulic Power Accumulator, MainSDR CALA2022021800420Skin · cracked(SUPPORT TASK} L-4 DOOR INNER SKIN LOWER HINGE ARM LIGHTENING HO LE IS CRACKED. TRANSCRIBED FROM HAECO GSO TASK CARD 9283246Feb 17, 2022 · N57111 · Boeing 757224 · Passenger/Crew DoorsSDR CALA2022021600392Fitting · corrodedSHEAR TIE CORRODED AT STA 28L FWD OF STA 1560. REMOVED AND REPLACED SHEAR TIE AT STA 1560 S-28L IAW B757 SRM 51 -40-02 PARA 4. WORK PERFORMED BY V936267, V933877 SEE REF AMES NR142726-0100-0082 FOR INSPECTION RII SIGN OFF BY INSPECTOR V933877Feb 14, 2022 · N14107 · Boeing 757224 · Fuselage Structure (General)SDR CALA2022020700338Engine · vibrationNO 1 ENG VIBE 2.6-3.0 NO VIBE FELT 2.6-3.0 HIGHEST IND FL390 PER PREVIOUS UPDATE CODE B7 ON AVM CHECKED WIREING SECURITY AT ENGINE 1 TRANDUCER, FOUND ALL SECURE THIS LOG HAS BEEN LOCKED BY THE TOMC MGR DUE TO EMERGENCY UNLOCKED FOR MX UPDATE DECLARATION. L AVMFeb 7, 2022 · N17139 · Boeing 757224 · Engine Ignition AnalyzerSDR CALA2022020700323Skin · dentedB757-06-3-0270 LH ELEVATOR LOWER SURFACE HAS 2 EACH DENTS BETWEE N ELE STA 200 AND ELE STA 312.673 MARKED, TRANSCRIBED FROM HAECO GSO NON ROUTINE 9282300 REPAIRED DENTS ON LH ELEVATOR LOWER SURFACE IAW B757 SRM 55-20-0 1-2R-1 AND 51-70-17-0G-0. HAECO GSO MECH Feb 4, 2022 · N57111 · Boeing 757224 · Elevator Control SystemSDR CALA2022011800168Seat Track · crackedSEAT TRACK AT STA 1540 LBL 44 FOUND CRACKED REPORTED BY V921297 REMOVED AND REPLACED SEAT TRACK @ STA 1540 LBL 44 IAW UAL EC/RA 5300-02793, B757 SRM 51-40-02 PARA 7, AND BOEING B757 DWG 146N51 20 & REA 47485FAB01 REF NR 142974-0200-0060 FOR DETAILSJan 17, 2022 · N13113 · Boeing 757224 · Fuselage Structure (General)SDR CALA2022011700166Support · damagedSDR REQUIRED, FOR REPAIR AT STATION 1380 FRAME INNER CHROD AT S-27R REQUIRES REPAIR. SDR REQUIRED, REF LOG PAGE 7591125. TRANSCRIBED FROM HAECO LP 9287333. AT STA 1320 S-27R, REMOVED SUPPORT STRUCTURE FOR INNER CHORD AND RESTORED PROTECTIVE FINISH SUPPORT STRUJan 16, 2022 · N33103 · Boeing 757224 · Fuselage Structure (General)SDR CALA2022011700155Support · damagedTRANSCRIBED FROM HAECO GSO NR LP 9287333 B757-06-3-0244 STATION 1380 FRAME INNER CHROD AT S-27R REQUIRES REPAIR PER ECRA 5360-01624: "PERFORM AN INSPECTION PER THE LATEST REVIS ION OF ECRA 5360-01624 PART 2 ON OR BEFORE 22-MAY-2023" DIP INITIATED, PERFORM INSPJan 14, 2022 · N33103 · Boeing 757224 · Fuselage Main, FrameSDR CALA2022010300013Fuel Control · nonePER FLT CREW: AFTER ENCOUNTERING MILD TURBULENCE, LEFT ENG FUEL VALVE LIGHT ILLUMINATED WITH ASSOCIATED EICAS MSG AND HAS REMAINED ON, NO DISRUPTION OF ENG PARAMETERS. ENGINE OPERATION NORMAL. ACP LEFT ENGINE RUN AND FUEL CONTROL ENGINE VALVE INDICATION CHK PIJan 3, 2022 · N14115 · Boeing 757224 · Fuel Control/Turbine EnginesSDR CALA2021112202155Door · damagedR/H APU DOOR HAS HEAT DAMAGE FROM TAIL PIPE AND DRAIN MAST FIRE. DAMAGE (1) IS 2" ABOVE DRAIN MAST MEASURING 6" X 6" AND IS .125" DEEP. DAMAGE AREA (2) IS 3" AFT OF DRAIN MAST MEASURING 5" X 11" AND IS .125" DEEP. DAMAGE (3) IS 2" BELOW DRAIN MAST AND MEASURINNov 21, 2021 · N13138 · Boeing 757224 · Auxiliary Power Unit (APU) DoorsSDR CALA2021110102006Doubler · damagedSUPPORT TASK: O/B L/H AFT FLAPMID FLAP BULLNOSE HAS 2EA. DENTS IN AREA FO #1 SPO,IER& BEAR METAL WING STA 615. MEASURED DMAGE AREA AND FOUND IT TO BE 5.5"X THE DEPTH OF THE DAMAGE IS .047" OVERALL. THE A OVER Y IS 117 THE DMG IS WITH IN LIMITS REF SRM57-53-01 Oct 29, 2021 · N34137 · Boeing 757224 · Wing StructureSDR CALA2021102601976Skin · noneSUPPORT TASK: EXISTING MAJOR REPAIR INSTALLED AT BS620 STRINGER 18L NOT LISTED FOR INSP FROM AIRCRAFT RECORDS REVIEW. REPAIR IS INSTALLED ADJACENT AND BELOW MAJOR REPAIR BETWEEN BS620-640 AND BETWEEN STRINGERS 16L-17L. REPAIR IS NOTED IN ECRA 5330-05371. T RANOct 26, 2021 · N19141 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2021102601975Intercostal · corrodedTRANSCRIBED FROM HAECO GSO NRC# 9287163- (B757-53-3-0480) MAIN C ABIN FLOOR STRUCTURE, INTERCOSTAL HAS CORROSION AT UPPER SURFACE BETWEEN BS 680 AND BS 700 APPROX RBL 56, MARKED. REMOVED AND REPLACED CORRODED PART #143N5434-1 IAW B757-200 SRM 51-40-02 AND SRM Oct 25, 2021 · N33103 · Boeing 757224 · Fuselage Main, StructureSDR CALA2021102001928None · noneTRANSCRIBED FROM ECRA 5311-02651 HAECO GSO NR 9284641. PLANNING TO CONTACT ENGINEERING AFTER 15-JAN-2023 BUT BEFORE 15-FEB-2023 AND REQUEST THAT UPDATED INSPECTION INSTRUCTIONS BE PROVIDED FOR ECRA 5311-02651. PLANNING TO CONTACT ENGINEERING AFTER 15-JAN-2023 Oct 19, 2021 · N19141 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2021101101849Flap System · malfunctionedTE FLAP ASYM LANDED F15 ITEM LOCKED BY TOMC MGR DUE TO FLT CREW DECLARING AN EMERGENCY FOR LANDING CYCLE ALT FLAP AND SLAT SWITCH TO OPERATE FLAP HYDRAULICALLY. PERFORM TEST OF THE FSEU''S 1,2,3 AND NO FAULT FOUND. CREW INDICATED AT ONE POINT THE FLAP INDICATIOct 11, 2021 · N19117 · Boeing 757224 · Trailing Edge Flap Control SystemSDR CALA2021101101842Skin · corrodedTRANSCRIBED FROM HAECO GSO NR LP 9288730 (SUPPORT TASK) #1 PYLON PANEL 433JR CUTOUT INNER SKIN CORRODED REPAIRED SKIN PER HAECO REO G-23376 REV IR AND UAL EC/RA 5451-01 348 REV IR HAECO GSO MECH V899890 INSP QC340Oct 9, 2021 · N34137 · Boeing 757224 · Nacelle/Pylon, Plate/SkinSDR CALA2021100601802Skin · crackedGENERATING ITEM: EA 5210-01364 REV G OP 003 /// SUPPORT TASK: L4 DOOR INTERNAL SKIN AT UPPER HINGE CRACKED. CLEANED R1 DOOR DRAIN AREA. SEE J/C 136989-0800-0060 STEP 52Oct 6, 2021 · N17122 · Boeing 757224 · DoorsSDR CALA2021100601800Skin · damagedPER CREW, POSSIBLE TAIL STRIKE ON LANDING. ATTACHED PICTURES OF DMAGED AREAS PERFORMED VISUAL INSPECTIONS STEPS 4&5 REF AVO# PERFORMED DETAIL VISUAL INSPECTION REF AVO ESC210928-0125-1 STEP ESC210928-0125-1. 4. NO INTERNAL STRUCTURE DAMAGE NOTED ON THE INTERIOOct 6, 2021 · N12125 · Boeing 757224 · Fuselage Structure (General)SDR CALA2021100601799Skin · gougedFUSELAGE SKIN WORN AND GOUGED AT AND BETWEEN STA.1720 - STA.1712 AT S-29RT AND S-29LT FWD OF APB ( REF. L/P 7137422 ) C/W RII INSP OF INSURANCE CUT REF DISPOSITION A.2 STEP 1 AVO ESC 210928-0125-3. TRIMMED OUT DAMAGE SKIN AT STA. 1713 TO 1720, BETWEEN S29L & POct 6, 2021 · N12125 · Boeing 757224 · Fuselage Structure (General)SDR CALA2021100601811Warning Message · illuminatedDURING APPCH FROM FLAPS UP TO FLAPS 1 TE FLAP DISAGREE EICAS MISSIONS AND ACCOMPL CORRECTIVE ACTION AS NECESSARY. SO FAR, THE LEFT WING MOST INBOARD FLAP TRANSMISSION #4 OVERLOAD IND IS POP PED. ABOVE LP IS CORRECT AND CONFIRMED THAT THE FLAP NEVER MOVED UPONOct 6, 2021 · N17126 · Boeing 757224 · Trailing Edge Flap Control SystemSDR CALA2021100601807Flap System · faultedTE FLAP DISAGREE EICAS WHEN FLAP HANDLE MOVED TO FLAPS 1 POSIT ION. QRH PROCEDURE RUN PERFORMED OPS TEST OF TE FLAP SYSTEM REF AMM 27-51-00-715-001, LE AND TE FLAPS OPERATE NORMAL. PERFORMED BITE OF FSEU 1,2,AND 3. BITE SHOW NO FAULTS REF 27-51 FAULT TREOct 6, 2021 · N17126 · Boeing 757224 · Trailing Flap Position Indicating SystemSDR CALA2021100601777Actuator · trippedLE SLAT DISAGREE DEBRIEF FROM CREW WHEN HE SELECTED FLAPS 1 THE FLAP INDICATOR RETURNED FLAPS TO NORMAL CONFIG AND PERFORMED FSEU BITE. ON CYCLED FLAPS UP AND DOWN SEVERAL TIMES WITH NO FAULTS. CHECKED STOPPED AT 1/2 AND A LEADING EDGE SLAT DISAGREE MSG CAME OOct 3, 2021 · N17126 · Boeing 757224 · Trailing Edge Flap ActuatorSDR CALA2021091301561Floorbeam · corrodedREF AMES N/R 0870 UPPER AFT PASSENGER CABIN. FOUND CORROSION IN AREAS OF THE BS 1640 FLOOR BEAM AND THE R4 DOO R INTERCOSTAL BLENDED, DAMAGE FOUND TO BE OUT OF LIMITS, REPAIRED IAW B757 SRM 53-00-51-02 ON 1640 FLOOR BEAM / R4 DOOR. SEE BACK AND PWS 1-4 FOR PARSep 11, 2021 · N34131 · Boeing 757224 · Fuselage Main, Floor BeamSDR CALA2021091301560Flange · corroded(B757-49-3-8084) THE INTERIOR FLANGE IS CORRODED AND CRACKED, FOR THE APU AIR INLET DOOR ASSY., AT THE FWD O/B EDGE AND THE O/B AFT EDGE, VIEWED SITTING ON TOP OF THE HOR. STAB. CENTER BOX, LO OKING UP.Sep 11, 2021 · N17122 · Boeing 757224 · APU Core EngineSDR CALA2021091301558Floor Support · corrodedREF AMES NR 0499 CORROSION FOUND ON FLOOR SUPPORT NEXT TO SEAT TRACK AT STA 720 RBL 33 UNDER FLOOR PNL 232LF. REMOVED FLOOR SUPPORT BY SEAT TRACK AT STA 720, RBL 33 FOUND TO BE OUT OF LIMITS, FABRICATED NEW FLOOR SUPPORT USING 7075-T6-071 PO # 0179415 IAW B757Sep 10, 2021 · N34131 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2021091001553Floorbeam · corrodedREF AMES N/R 0870 UPPER AFT PASSENGER CABIN. FOUND CORROSION IN AREAS OF THE BS 1640 FLOOR BEAM AND THE R4 DOO R INTERCOSTAL BLENDED, DAMAGE FOUND TO BE OUT OF LIMITS, REPAIRED IAW B757 SRM 53-00-51-02 ON 1640 FLOOR BEAM / R4 DOOR. SEE BACK AND PWS 1-4 FOR PARSep 10, 2021 · N34131 · Boeing 757224 · Fuselage Main, Floor BeamSDR CALA2021091001552Floor Support · corrodedREF AMES N/R 0498 CORROSION ON FLOOR SUPPORT AT BL 0 STA 1681. BLENDED, FOUND TO BE OUT OF LIMITS, REPAIRED IAW B757 BOEING DWG # 146N5249 ON FLOOR SUPPORT BLO STA1681, IAW B757 SRM 51-40-02 PARA 7 SEE BACKAND PWS 1-2 FOR WORK ACCOMPLISHED. ADD EMP:V921265Sep 10, 2021 · N34131 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2021091001551Structure · corrodedPERFORM AN INSPECTION PER PART 2 OF THE LASTEST REVISION OF ECRA 5383-01003 ON OR BEFORE 50000 TOTAL AIRCRAFT FLIGHT CYCLES. PERFORM AN INSPECTION PER PART 2 OF THE LASTEST REVISION OF ECRA 5383-01003 ON OR BEFORE 50000 TOTAL AIRCRAFT FLIGHT CYCLES. REF LP 701Sep 10, 2021 · N17122 · Boeing 757224 · Empennage StructureSDR CALA2021091001550Computer · inoperativeAUTOPILOT/FLIGHT DIRECTOR WARNING MODE CONTROL PANEL PROBLEM WAS ENCOUNTERED BY THE FLIGHT CREW WHICH IS NOT COVERED IN THE FAUL T CODE DIAGRAM RPL MODE CONTROL PANEL MM22-11-02-402-007. DUE LOG PAGE 6827661 RPL RIGHT FLIGHT CONTROL COMPUTER MM22-11-01-404-011Sep 10, 2021 · N48127 · Boeing 757224 · Autopilot SystemSDR CALA2021091001541Structure · corroded(B757-53-3-0591) THERE IS CORROSION ON THE UPPER CHORD, THAT CON NECTS THE SHELF TO THE FWD SIDE OF THE 1862.70 BULKHEAD, LOCATED ABOVE THE ELEVATOR MECHANISM, VIEWED SITTING ON TOP OF THE HOR. STAB. CENTER BOX, LOOKING AFT, FROM RBL8 TO RBL22 REMOVED CORROSIOSep 8, 2021 · N17122 · Boeing 757224 · Fuselage Main, BulkheadSDR CALA2021090601510Floorbeam · corrodedB757-53-3-0571 FLOOR BEAM AT STA 1640 BL0 IS CORRODED.Sep 4, 2021 · N17122 · Boeing 757224 · Fuselage Main, Floor BeamSDR CALA2021090101486Floorbeam · corrodedREF AMES NR 0499 CORROSION FOUND ON FLOOR SUPPORT NEXT TO SEAT T RACK AT STA 720 RBL 33 UNDER FLOOR PNL 232LF. REMOVED FLOOR SUPPORT BY SEAT TRACK AT STA 720, RBL 33 FOUND TO BE OUT OF LIMITS, FABRICATED NEW FLOOR SUPPORT USING 7075-T6-071 PO # 0179415 IAW B75Sep 1, 2021 · N34131 · Boeing 757224 · Fuselage Main, Floor BeamSDR CALA2021083001458Floor Support · cracked"SUPPORT TASK": DURING OK TO CLOSE FOUND FLOOR SUPPORT BETWEEN STA. 1320 AND 1340 BL0 CRACKED ON UPPER FLANGE. REMOVE AND REPLACED UPPER ANGLE BETWEEN STA1320 I.A.W B757-200 SRM 51-40-02 PARA 4, PARA 7 SEE PARTIAL WORK ACCOMPLISHED.Aug 30, 2021 · N34131 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2021083001457Attach Angle · corrodedATTACH ANGLES FOR WEB AND CARGO TIE DOWN AT STA 1380 S27R FOUND TO BE CORRODED. WORK WITH N/R 0641. MARINE V931857 REMOVED CORROSION ON ATTACH ANGLES FOR WEB AND CARGO TIE DOWN AT STA 138 S27R. SEE PARTIAL WORKSHEET 1 AND 2 FOR WORK ACCOMPLISH ED. ALSO SEE N/Aug 30, 2021 · N34131 · Boeing 757224 · Fuselage Main, Attach FittingsSDR CALA2021082701440Rib · damagedSUPPORT TASK-LEFT ELEVATOR OUTBD, RIB P/N 183N2505-31 AFT VERTIC AL EDGE HAS DAMAGE. REPAIRED L/H ELEVATOR OBD RIB IAW B757-200 SRM 55-20-02, SRM 51- 70-04, DWG 183N2505Aug 26, 2021 · N19141 · Boeing 757224 · Elevator, Spar/RibSDR CALA2021082501432Rib · bentREF AMES NR 0407 SUPPORT TASK B757-06-3-0356. CAP RIB BENT AT FW D LOWER CORNER AREA OF CARGO DOOR REMOVED AND REPLACE RIB ON AFT CARGO DOOR AN REAPPLIED LEVELING COMPOUND I.A.W B757-200 SRM 51-40-02 PARA 4, PARA 7, CMM 52-35-1 4 SEE PARTIAL WORK ACCOMPLISHED Aug 25, 2021 · N34131 · Boeing 757224 · Cargo/Baggage DoorsSDR CALA2021082001385Lavatory · overflowWASTE DISPOSAL MIDLAVG -LAVATORY WASTE SYSTEM PROBLEM WAS ENCOUNTERED BY FLIGHTCREW WHICH IS NOT COVERED IN FAULT CODE DIAGRAMS MULTIPLE LAVS OVERFLOWIN G. 2 OPERABLE LAVS ARA ALMOST FULL LOCKING TO VERIFY POSITIVE FIX. UNLOCKING FOR UPDATE. DEBRIEFED FLIGHT AAug 20, 2021 · N14115 · Boeing 757224 · Waste Disposal SystemSDR CALA2021082001377Shear Web · corrodedREFERENCE AMES NR 0547 LH CABIN FLOOR SHEAR WEB HAS MULTIPLE ARE AS OF CORROSION AT LFS 1680 TO LFS 1720, BL 0 TO BL43 (M REPAIRED L/H CABIN FLOOR SHEAR WEB IAW B-757 SRM 53-60-51. SEE P ARTIAL WORK ON ABCK AND PWS 1 AND 2. ADD EMP:V931869Aug 18, 2021 · N34131 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2021081801358Shear Web · corrodedREFERENCE N/R 0548 RH CABIN FLOOR SHEER WEB HAS MULTIPLE AREAS O F CORROSION FROM RFS 1680 TO RFS 1720, BL 0 T O BL 43 REPAIRED IAW B757 SRM 53-60-51 FIG 201 DETAIL I. SEE BACK OF R24 U AND R19A PG.3 AND 4. ADD EMP:V921495Aug 17, 2021 · N34131 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2021080901309Warning Message · false activationEMERGENCY DECLARED ON APPROACH AFTER SETTING FLAPS FROM 5 TO 20 WE HAD AN ASSYMETRY LEFT INDICATION 7 AND RIGHT INDCATION 20. PERFORM BITE FSEU PER FIM 27-51-00 NO FAULT NOTED AND RECYCLE FLAP NO EICAS MESSAGES OR FAULT NOTED.Aug 9, 2021 · N19130 · Boeing 757224 · Trailing Flap Position Indicating SystemSDR CALA2021072601193Radio · inoperativeHF RADIOS TRANSMIT NO RECEIVE..NO STATIC AT ALL...NO SIDE TONE ON RIGHT HF AT ALL R HF TRANSCEIVER R&R PER AMM 23-11-03-401 & TEST PASS. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1615423 SN OFF 6630 TRANSCEIVER, HF OFF 99-2310-9-0001 6630 ON 29-2311-9-001Jul 26, 2021 · N14106 · Boeing 757224 · HF Communications System
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