Boeing 757-224

Service difficulty reports · 3,824

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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 aircraft_model_key = '757224'
  ORDER BY difficulty_date DESC"

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SDR CALA2023062101961Tat Probe · inoperativeTAT PROBE ANNCTR IN FLT UPDATING WITH INDICATED FAULTS. REPLACED THE TAT PROBE REF. MM 34-12-02. PROBE GROUND CHECKS GOOD. ADD EMP:404924Jun 21, 2023 · N57111 · Boeing 757224 · Navigation SystemSDR CALA2023062101959Control Unit · inoperativeA/C REQD 7 UNITS OF RT TRIM THRU FL340 AND 5 UNITS IN CRZ. L AIL LOOKS DEFLECTEDLEFT INBD AILERON PCA REQUIRES REPLACEMENT FOR PRECAUTIONARY REF. LOGPAGE 4909755. REMOVED LEFT INBD AILERON PCA PER AMM TASK 27-11-20-022-006 AND TASK PROGRESS SCREEN SHOTS ADDED Jun 19, 2023 · N19117 · Boeing 757224 · Flight Control SystemSDR CALA2023061901946Pressure Switch · unknownTE FLAP DISAGREE AT FLAPS 25.FLAPS FROZE AT 20-25 DEGREES UNABLE TO MOVE AFTER NOT DISAGREE AT ANY POINT AND NO UNCOMMANDED ROLL OR MOVEMENT TRANSMISSIONS FOUND TO BE OK, NOT TRIPPED. OCCURED. CREW DEBRIEF STATED WHEN ATTEMPTING TO MOVE FLAPS FROM 20 TO 25, PEJun 17, 2023 · N19130 · Boeing 757224 · Flight Control SystemSDR CALA2023061901947Downlock Sensor · out of limitsLDG GEAR MONITOR EICAS S "SYSTEM 1 AND SYSTEM 2 LANDING GEAR POSITION INDICATIONS DO NOT AGREE. ALL GEAR DOW N GEAR DISAGREE GEAR DOORS GEAR LEVER L(R) GEAR DOWN L(R) DRAG B RACE L(R) SIDE BRACE NOSE GEAR DOWN NOSE GEA NOTED AFTER TO ADJUSTED NOSE GEAR DOWNLOCJun 16, 2023 · N13138 · Boeing 757224 · Landing Gear SystemSDR CALA2023061901911A/C Pack · restrictedL PACK NO AIRFLOW OR TEMPERATURE CONTROL L ENG BLEED CLOSED WHEN PACK WAS TURNED OFF OPERATING NORMALLY. "FLT DECK TEMP" AUTO EVENT ON ECS PAGE. ALL BITE CHECK PASS, NO FAULTS. OPERATED REGULATION SYSTEM, THE COOLING SYSTEM AND THE REVERSE FLOW BOTH PACKS IN Jun 16, 2023 · N58101 · Boeing 757224 · Air Conditioning SystemSDR CALA2023061901907Door · damagedR1 DOOR HAS TOOLING DAMAGE ON LOWER AFT INSDE CORNER OF DOOR. THIS LOG PAGE IS INFORMATIONAL ONLY FOR ESFR INPUT. REFERENCE NR001332028. BLENDED OUT TOOLING DAMAGE AND INSTALLED DOUBLER PER ECRA 5211-01815.Jun 16, 2023 · N14115 · Boeing 757224 · Passenger/Crew DoorsSDR CALA2023061601893Indicator · inoperativeCREW REPORTS AT CRZ THE STANDBY ADI 28DEG RIGHT BANK AND PITCH 28DEG UP WHILST WINGS LEVEL AND PITCH AT LEVEL FLIGHT. REMOVED AND REPLACED STANDBY ATTITUDE INDICATOR REF AMM 34-24-01. OPS CHECK GOOD REF AMM TASK 34-24-00-715-001. NO NOTICABLE HISTORY A/C OK TJun 14, 2023 · N14118 · Boeing 757224 · Pneumatic SystemSDR CALA2023061601889Frame · crackedFRAME ATTACH BRACKET FOR OVERHEAD BIN IS CRACKED @ STA. 1120 L/H STRINGER 8. D. OSBORNE V921218 (M). FRAME ATTACH BRACKET FOR OVERHEAD BIN IS CRACKED @ STA. 1120 L/H STRINGER 8. D. OSBORNE V921218 (M). ADD EMP:V921218Jun 14, 2023 · N13113 · Boeing 757224 · Fuselage Structure (General)SDR CALA2023061601888Frame · crackedCRACK ON FRAME WEB ATTACH BRACKET FOR OVERHEAD BIN @ STA 760 L/H @ STRNGR 8. D. OSBORNE V921218 (M). CRACK ON FRAME WEB ATTACH BRACKET FOR OVERHEAD BIN @ STA 760 L/H @ STRNGR 8. D. OSBORNE V921218 (M). ADD EMP:V931845Jun 12, 2023 · N13113 · Boeing 757224 · Fuselage Structure (General)SDR CALA2023061601887Floorbeam · corrodedCORROSION FOUND ON TOP OF FLOOR BEAM AT STA 720 BL 20R. DOCUMENTED ON AMES NR 159536-0200-0147. CORROSION FOUND ON TOP OF FLOOR BEAM AT STA 720 BL 20R. DOCUMENTED ON AMES NR 159536-0200-0147. ADD EMP:V921493Jun 11, 2023 · N13113 · Boeing 757224 · Fuselage Main, Floor BeamSDR CALA2023061601886Frame · crackedCUSP WEB FORWARD LOWER FRAME CLIP CRACKED. LOCATED JUST AFT STA. 1120 LEFT SIDEWALL, FLOOR LEVEL, VIEW WITH MIRROR AND FLASHLIGHT UNDER CUSP WEB. (K. JONES V932161) CUSP WEB FORWARD LOWER FRAME CLIP CRACKED. LOCATED JUST AFT STA. 1120 LEFT SIDEWALL, FLOOR LEVEJun 9, 2023 · N19141 · Boeing 757224 · Fuselage Structure (General)SDR CALA2023061201815Unknown · gougedABOVE R4 DOOR, ON FRAME 1640, THERE IS A GOUGE IN THE FRAME. (SEE IMAGES) INTERIM REPAIR ACCOMPLISHED AT FUSELAGE STA 1640 FRAME AND S5R-S6R - ACCOMPLISH INITIAL INSPECTION REQUIREMENTS PER PART 2 OF THE LATEST REVISION OF EC/RA 5360-01713 ON OR BEFORE 22-NOV-Jun 9, 2023 · N14115 · Boeing 757224 · Fuselage Main, StructureSDR CALA2023060201732Frame · damagedAFT CARGO COMPARTMENT FRAME AT STA 1460 L/H STR 26 HAS AN EXISTI NG FRAME REPAIR WITHOUT SRM STANDARD. RESULTS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE THE A/C RECEIVED FINDING APPROVAL FOR DAMAGE TOLERANCE REQUIREMENTS FROM SVC ON OR BEFORE 26 NOV 2024 UNJun 1, 2023 · N19130 · Boeing 757224 · Fuselage Main, FrameSDR CALA2023053101722Stringer · damagedREF L/P4612658. STR24L BETWEEN STA680-700 DAMAGED CUT AND REMOVED STR24L FROM STA640-710 REF SRM53-00-03-2R-1 VERIFIED CUTOUT OF S24L STRINGER. PER AVO10784 REV A. C/W RR GMM PERFORMED HFEC PER AVO10784 REV A STEP 12. NO CRACKS INDICATION VERIFIED .040" INSURAMay 29, 2023 · N17105 · Boeing 757224 · Fuselage Main, Longeron/StringerSDR CALA2023053101721Skin · damagedLAV SERVICE VEHICLE MADE CONTACT WITH AIRCRAFT WHILE SERVICING LAVATORY. GROUND DAMAGE SUSTAINED. DAMAGE SUSTAINED AROUND AFT LAV SERVICE PANEL. CORRECTION, DAMAGE SUSTAINED AT FWD LAV SERVICE PANEL NOT AFT LAV SERVICE PANEL AS PREVIOUSLY REPORTED. THE DAMAGE May 29, 2023 · N17105 · Boeing 757224 · Fuselage Structure (General)SDR CALA2023052401635Skin · dentedUNDOCUMENTED DENT DISCOVERED AT BS 1480 + 19 BETWEEN S24R-S25R. DIMENSIONS: 5.00"L X 2.65"W X .125"D AND IS .5" FROM BS 1500 & S24R. PER SRM 53-00-01 ALLOWABLE DAMAGE 1 FIGURE 101 DETAIL III. DENT OUT OF LIMITS. UE DIP FOR INSPECTION REQUIREMENTS TABLE 206/REPMay 23, 2023 · N18119 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2023052401632Frame · gougedSPEC B757-06-3-0241 AFT CARGO COMPT FRAME HAS A GOUGE AT STA 1500 S24L PER SRM 53-00-07-2R-5 REP 5 TAB II ZONE 1M 37,500 FLT CY AFTER AND DETAILED INSP EVERY 12000 FLT CYCLES INSTALLATION OR 50,000 FLT CY WHICHEVER COMES FIRST. REPEAT HFEC REF ST PNS NR 62317 May 22, 2023 · N19130 · Boeing 757224 · Fuselage Main, FrameSDR CALA2023051901576Spar · loose#1 FLAP, O/B ATTACH POINT TO FLAP CARRIAGE IS LOOSE AND HAS THREE SHEARED/MISSING BOLTS/HI-LOCS. 5753-02106 REV. -. GENERATED 2 EA ELB LOG PAGES #''S 4615060 AND PAGE LIMITS PER STEP 19 ARE "ACCOMPLISH INITIAL INSPECTION PER CYCLES". 4615786 FOR DIP ENTRIES May 18, 2023 · N14115 · Boeing 757224 · Trailing Edge FlapsSDR CALA2023051701527Unknown · loose(B757-06-3-0328) RIGHT WING APPROX. FSS 228 UNDER #6 SLAT, VERTI CAL STIFFNER AT DUCT ATTACH BRACKET CHAFING DUE TO BRACKET BEING LOOSE AS MARKED. TRANSCRIBED FROM HAECO GSO NR 9280145. AND BOEING DWG 112N2038 REV-. INSTALLED NEW STIFFENER IAW REO-G2 4456, B75May 16, 2023 · N13138 · Boeing 757224 · Leading Edge DevicesSDR CALA2023051701526Skin · cracked2(EA) CRACK INDICATIONS FOUND: L/H UPPER WING SKIN & DRAG FITTIN G FASTENER HOLE #2, IN UPPER LAYER(SKIN) AT 3 & 9 ''OCLOCK POSITI ONS. FLIGHT CYCLES THEREAFTER." REPAIRED #2 HOLE AT L/H WING SKIN & I/B DRAG FITTING PER REO-G24 "ACCOMPLISH INITIAL INSPECTIONMay 16, 2023 · N13138 · Boeing 757224 · Wing, Plate/SkinSDR CALA2023051101455Frame · crackedCABIN FRAME IS CRACKED AT I/B FASTENER FOR PSU BRACKET STA.760 BETWEEN S-8LT & S-9LT. [MARKED AND VERIFIED WITH HFEC] INSPECTION THRESHOLD 12,000 FLIGHT CYCLE FROM THE REPAIR FIRST. REPEAT INSPECTIONS DVI AT INTERVAL 12,000 FLIGHT CYCLES. INSTALLATION OR 50,00May 10, 2023 · N14115 · Boeing 757224 · Fuselage Main, FrameSDR CALA2023050901430Skin · damagedTHE REPAIR INCORPORATED VIA ECRA 5331-03025 IS APPROVED AS TIME- LIMITED UNTIL 37,500 TOTAL AIRCRAFT CYCLES PENDING THE RESULTS OF A DAMAGE TOLERANCE ANALYSIS(DTA). REMOVE THE AIRCRAFT FROM SE RVICE ON OR BEFORE 37,500 TOTAL AIRCRAFT FLIGHT CYCLES, UNLESS A NMay 8, 2023 · N13138 · Boeing 757224 · Fuselage Structure (General)SDR CALA2023050901428Skin · unknownREFERENCE PREVIOUS LOGPAGE #9295835. THE REPAIR INCORPORATED VIA ECRA 5331-03026 IS APPROVED AS TIME-LIMITED UNTIL 39,750 TOTAL A IRCRAFT CYCLES PENDING THE RESULTS OF A DAMAGE TOLERANCE ANALYSI S (DTA). REMOVE THE AIRCRAFT FROM SERVICE ON OR BEFORE 39,750 TO May 8, 2023 · N13138 · Boeing 757224 · Fuselage Structure (General)SDR CALA2023050901427Frame · crackedCABIN FRAME CRACKED BETWEEN S8RT AND S9RT, AT I/B RIVET FOR PSU RAIL ATTACHMENT AT STA. 1240RT 001234528. INSPECTION REQUIREMENTS ZONE 3 INSPECTION THRESHOLD: AIRFRAME FLIGHT CYCLES, WHICHEVER COMES FIRST. REPEAT 12,000 FLIGHT CYCLES FROM REPAIR INSTALLATION, May 8, 2023 · N18119 · Boeing 757224 · Fuselage Structure (General)SDR CALA2023050801405Actuator · unknownRUDDER TRIM INOP REF FIM PROCEDURE 27-21 FAULT TREE 805 RUDDER TRIM PROBLEMS REPLACED RUDDER TRIM INDICATOR - NO HELP. REINSTALLED ORIGINAL SEE FIM 27-28 TASK 802. PLACED TRANSMITTER AND INDICATOR IN FLIGHT DECK F.O. SEAT. VERIFIED 28V PRESENT AT PIN 11 ON D17May 8, 2023 · N17128 · Boeing 757224 · Flight Control SystemSDR CALA2023050501360Skin · damagedL4 DOOR UPPER DOOR TORQUE TUBE CUTOUT DAMAGED REPAIRED L4 DOOR INNER SKIN DAMAGE STA 1656 BTW HINGE CTR LINE AND BEAM #3 REF ECRA 5210-03284 SEE NR 001262457 FOR ALL WORK PERFORMED. VERIFIED REPAIRED L4 DOOR INNER SKIN DAMAGE STA 1656 BTW HINGE CTR LINE AND BEMay 3, 2023 · N18119 · Boeing 757224 · Passenger/Crew DoorsSDR CALA2023050501359Frame · dentedAFT CARGO COMPARTMENT FRAME AT STA 1280 S-26R HAS A DENT ON THE UPPER FLANGE. REPORT (DTA). REMOVE AIRCRAFT FROM SERVICE ON OR BEFORE NOV 01, FOR DAMAGE TOLERANCE REQUIREMENTS. 2024, UNLESS ANOTHER 8110-3 FORM IS RECEIVED FINDING APPROVAL THE REPAIR INCORPORATMay 3, 2023 · N17122 · Boeing 757224 · Fuselage Main, FrameSDR CALA2023050501356Frame · crackedCABIN FRAME IS CRACKED AT I/B FASTENER FOR PSU BRACKET STA.1120 BETWEEN S-8LT & S-9LT. [MARKED AND VERIFIED WITH HFEC] INSPECTION REQUIREMENTS AS GIVEN IN TABLE 203/REPAIR 8 ZONE 1. INSTALLATION, OR 50,000 AIRFRAME FLIGHT CYCLES, WHICHEVER COMES FLIGHT CYCLES.May 3, 2023 · N14115 · Boeing 757224 · Fuselage Main, FrameSDR CALA2023013100274Knob · inoperativeAIRSPEED SELECTOR KNOB INOP REMOVED KNOB AND VERIFIED THAT THE SHAFT IS BROKEN. R&R MODE CONTROL PANEL PER AMM 22-11-02-022-001 AND 22-11-02-402-007. PERFORMED MCDP GROUND TEST 4 AND TEST 30PER AMM 22-00-02/201. ALL TESTS PASSED. AC REMAINS FULL CAPIBILITY. OJan 31, 2023 · N34137 · Boeing 757224 · Airspeed/Mach IndicatorSDR CALA2023013100273Knob · inoperativeAIRSPEED SELECTOR KNOB INOP REMOVED KNOB AND VERIFIED THAT THE SHAFT IS BROKEN. R&R MODE CONTROL PANEL PER AMM 22-11-02-022-001 AND 22-11-02-402-007. PERFORMED MCDP GROUND TEST 4 AND TEST 30PER AMM 22-00-02/201. ALL TESTS PASSED. AC REMAINS FULL CAPIBILITY. OJan 31, 2023 · N34137 · Boeing 757224 · Airspeed/Mach IndicatorSDR CALA2023013000238Intercostal · corroded(B757-06-3-0243) AFT PIT BILGE AREA, RH INTERCOSTAL HAS CORROSIO N ON LOWER FLANGE AND VERTICAL WEB FROM STA 1310-S28R (MARKED). STREAMER ATTACHED. TRANSCRIBED FROM TASK CARD HAECO GSO NR 9282 611. B757-200 SRM 51-40-02, RECEIVED NEW INTERCOSTAL P/N 146N5700UJan 27, 2023 · N17139 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2023012700229Fuse · inoperativeCABIN CEILING EMERGENCY LIGHT BETWEEN THE TWO OVER WING DOORS IS INOP. SUPPORT TASK NSA EMX N/R 00257. 33-51-07-962-071. DATA WAS TRANSCRIBED FROM NSA EMX N/R 00257. TROUBLE SHOT SYSTEM CHECKED POWER AND GND AT L48 DISCONNECT IAW B757-ALL SCM 33-51-01 DETECTEDJan 27, 2023 · N41135 · Boeing 757224 · Emergency LightingSDR CALA2023012500196Wedge · damaged(B757-06-3-0306) #3 SLAT WEDGE T/E PREVIOUS REPAIR SEPARATED 31" FROM INBD EDGE. TRANSCRIBED FROM HAECO NR 9282457. REPAIRED #3 SLAT WEDGE T/E IAW B757 SRM 57-43-02-2R-1, SRM 51-70 -10-2R-0 AND AMM 51-21-001/701. REMOVED HAECO DOT. TRANSCRIBED F ROM HAECO NR 9Jan 23, 2023 · N17139 · Boeing 757224 · Leading Edge DevicesSDR CALA2023012300185Slide · unknownDOOR-MOUNTED ESCAPE SYSTEM DOOR 1R - A EVACUATION SLIDE PROBLEM WAS ENCOUNTERED WHICH IS NOT COVERED IN THE FAULT CODE DIAGRAMS DOOR KNUCKLE KNOCKER REMAINS FLUSH DURING ARM 1R CYCLED DOOR. AND ARMED. COULD NOT DUPLICATE ERROR. OPS CHECK GOOD.Jan 23, 2023 · N29124 · Boeing 757224 · Escape SlideSDR CALA2023012300184Processor · faultedLEFT FUEL TANK FLUCTUATES BETWEEN 14.6 AND 13.0 EVERY 30 MIN OR SO LEFT TANK AT STICK 87 IS 4.2 WITH ROLL 0 AND PITCH -5. RIHJY TANK AT STICK 7 IS 5.1. REMOVED AND REPLACED FUEL QTY PROCESSOR. REMOVED AND REPLACED FUEL QTY PROCESSOR. PERFORMED TANK UNIT CAPACJan 23, 2023 · N58101 · Boeing 757224 · Fuel Indicating SystemSDR CALA2023012300179Angle · corrodedMAIN CABIN STA 720-740 RBL 61 R2 LOWER SILL CHORD UPPER SURFACE CORRODED. REMOVED AND REPLACED LOWER SILL CHORD IAW DRAWING 143N83 22 REV-, SRM 51-40-06, SRM 51-40-05. REMOVED ANDJan 21, 2023 · N17139 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2023012000162Battery Pack · inoperativeR&R EMERGENCY LIGHT BATERY PACK LOCATED IN GALLEY AREA LIGHT PANEL BETWEEN L3 AND R3 DOOR. BATTERY PACK DID NOT HOLD CHARGE REMOVED AND REPLACED EMERGENCY LIGHT BATERY PACK LOCATED IN GALLEY AREA LIGHT PANEL BETWEEN L3 AND R3 DOOR. IAW AMM 33-51-07 REV. 130Jan 19, 2023 · N18119 · Boeing 757224 · Emergency LightingSDR CALA2023012000161Battery Pack · inoperativeR&R EMERGENCY LIGHT BATERY PACK LOCATED AFT OF THE GALLEY AREA LIGHT PANEL BETWEEN L1 AND R1 DOOR. BATTERY PACK DID NOT HOLD CHARGE REMOVED AND REPLACED EMERGENCY LIGHT BATERY PACK LOCATED AFT OF THE GALLEY AREA LIGHT PANEL BETWEEN L1 AND R1 DOOR. IAW AMM 35-5Jan 19, 2023 · N18119 · Boeing 757224 · Emergency LightingSDR CALA2023011600129Bracket · crackedDURING FRAME REPAIR PER SRM 53-00-07-2R-8, REPAIR 8 - A/C BRKT LOCATION STA 1540 LT SIDE, A CRACK INDICATION WAS FOUND AT STR 9LT STR TIE I/B FASTENER LOCATION. AT THE STR 8LT STR TIE LOCATION, THE O/B FASTENER LOCATION WAS DRILLED IN ERROR TO .430. THIS LOG Jan 16, 2023 · N29129 · Boeing 757224 · Fuselage Main, Attach FittingsSDR CALA2023011300095Skin · damagedENTRY STAND BLEW WITH SEVERE WEATHER AND IMPACTED THE FUSELAGE FWD OF DOOR 2L REMOVAL OF EXSISTING DOUBLER LEFT SIDE FUESLAGE APPROX. STATION REMOVED 4 ROWS OF RIVETS AT BOTTOM OF DOUBLER. REMOVED ALL FASTENERS ON DOUBLER AND REMOVED DOUBLER. REMOVED FWD CARGOJan 11, 2023 · N14115 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2023011000077Skin · damagedDISCOVERED ADDITIONAL LEFT SIDE FUESLAGE DAMAGE BETWEEN WATER SYSTEM DRAIN AND LAV SERVICE DOOR BLENDED OUT DAMAGE MARKED 1 INCH GRID FOR NDT ATTACHED IMAGES HFEC NO CRACKS ULTRASOUND MATERIAL AFTER BLEND. SEE IMAGE FOR ACCOMPLISHED STEP 2 & 5 , REF AVO 102Jan 10, 2023 · N14115 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2023010600038Skin · damagedENTRY STAND BLEW WITH SEVERE WEATHER AND IMPACTED THE FUSELAGE FWD OF DOOR 2L REMOVAL OF EXSISTING DOUBLER LEFT SIDE FUESLAGE APPROX. STATION REMOVED 4 ROWS OF RIVETS AT BOTTOM OF DOUBLER. REMOVED ALL FASTENERS ON DOUBLER AND REMOVED DOUBLER. REMOVED FWD CARGOJan 6, 2023 · N14115 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2023010600049Floorbeam · corrodedL/P GENERATED FOR ESFR REPORTING-FWD WET AREA FLOOR BEAM CHORD HAS CORROSION STA 365.25 RBL61. SEE NR 001094009 FOR FLOOR BEAM CHORD REPAIR-REPAIRED FLOOR BEAM REF SRM 53-00-51-2R-8.Jan 5, 2023 · N29129 · Boeing 757224 · Fuselage Main, Floor BeamSDR CALA2023010600047Stringer · damagedUPON DAMAGE REMOVAL OF FUSELAGE SKIN SECTION REF. L/P: 3443028, BETWEEN STA. 620 - 640, STRINGER S9L ALSO FOUND DAMAGED COMPLIED WITH INSPECTION REQUIREMENTS FOR VERIFICATION OF MAT''L FOR HAT SECTION DOUBLER AND FILLER MAT''L PER SRM: 53-00-03-2R-1 STEP 3. CUJan 5, 2023 · N14106 · Boeing 757224 · Fuselage Main, Longeron/StringerSDR CALA2023010600046Skin · dentedDURING JETBRIDGE CONNECTION TO THE AIRCRAFT THE JETBRIGDE CONTACTED THE AIRCRAFT FUSELAGE FWD OF D2L . INSPECTED DENT REF SRM 53-00-01 SHEET 3 PARA B,F,I,J.. DENT IS OUT OF LIMITS BUT MEETS ALL CRITERIA LISTED IN PARAGRAPH "I". APPROVED FOR DIP PER THIS SRM WIJan 5, 2023 · N14106 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2023010400027Indicator · intermittentFO AIRSPEED INDICATOR READ SLOW WITH INTERMITTENT FLAG RPL FO MACH AIRSPEED INDICATOR MM34-13-02-404-004. INSPECTED ACFT FOR HIGH ENERGY STOP PER AMM TASK 05-51-14-212-001 FOUND NO DEFECTS ON ACFT.Jan 4, 2023 · N17133 · Boeing 757224 · Airspeed/Mach IndicatorSDR CALA2023010400030Seat Track · not reportedSEAT TRACK REPLACEMENT AT BS 1320 - 1540, LBL 45.50. REMOVED AND REPLACED SEAT TRACK SECTION IAW SRM 53-00-52, REPAIR 3.Jan 2, 2023 · N41135 · Boeing 757224 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2023010200010Toilet · leakingRIGHT AFT LAV LEAKING BLUE WATER.CARPETS SOAKED RH AFT LAV LEAK INSPECTED. NO ISSUES NOTED.Jan 2, 2023 · N14106 · Boeing 757224 · Waste Disposal SystemSDR CALA2023010200008Fuel Line · leaking50 MIN INTO FLT HAD FUEL DISAGREE-PROG PAGE 2. CONFIRM ED FUEL STREAMING FROM RT IAW CREW. FUEL STREAMING FROM RT ENGINE, FOUND O-RING AT HP INLET FLANGED CONNECTION OF GEAR DRIVEN FUEL PUMP DISPLACED ON NR 2 ENGINE. FOUND HP INLET AT FUEL PUMP FLANGE CONNJan 1, 2023 · N18112 · Boeing 757224 · Engine Fuel DistributionSDR CALA2022123003525Anti-Ice Valve · faultedRTO AT 90KTS FOR R ENG ANTI-ICE CAUTION RETURNED TO GATE. REMOVED & REPLACED PRESS REGULATOR ANTI-ICE SHUTOFF VALVE. OPS CHK GOOD.Dec 30, 2022 · N14106 · Boeing 757224 · Engine Anti-Icing System
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