N17128

Service difficulty reports · 106

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N17128' AND registry_match = 'registration'
  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 CALA2026091419401Acm · faultySMOKE/ODOR IN CABIN ON CONDITION INSPECTION REQUIRES COMPLETION AMM 05-51-58-910-801-C1. SOURCE OF THE SMOKE SMELL IS BELIEVED TO BE THE R ACM WHICH WAS REPLACED AND OPS CHECKED, REMOVED AND REPLACED LT & RT RECIRCULATION FILTERS IAW MM 21-25-02-004-175. WILSep 7, 2026 · N17128 · Boeing 757224 · Cabin Cooling SystemSDR CALA2025121512130Lavatory · leakingBLUE JUICE LEAKED UNDER FWD LAV A FLOOR PAN. REQUIRES FURTHER CLEANING. NOT ENOUGH TIME TO CLEAN AT THIS TIME. WITHIN 7 DAYS ACCOMPLISH ECRA 2011-01000 LAV SPILL SEC 2 B, IN DEPTH CLEAN UP IN THE AREA AROUND LAV A. APPROX STA 310 TO 340. WL 208. STRINGERS18 TODec 12, 2025 · N17128 · Boeing 757224 · Waste Disposal SystemSDR CALA2025111711274Stiffener · corrodedEXFOLIATION DAMAGE ON THE LOWER END AFT SIDE OF THE BS 1180 WHEEL WELL BULKHEAD STIFFENER, LOCATED AT LBL 53.96. THE REPAIR INCORPORATED VIA ECRA 5340-02246 FUSELAGE BULKHEAD STATION 1180 WHEEL WELL STIFFENER. REMOVED THE AIRCRAFT FROM SERVICE.Nov 13, 2025 · N17128 · Boeing 757224 · Fuselage Main, StructureSDR CALA2025111711273Frame · dentedONE DENT ON THE BS 1560 FRAME BOTTOM, BETWEEN S26L & S27L. THE DENT MEASURES 0.750 INCH LONG, 0.600 INCH WIDE, AND 0.020 INCH DEEP. THIS DENT IS THE SUBJECT OF EA 5310-07582 AND ALSO AD 2020-05-25 PERFORM INSPECTIONS PER PART 2 OF THE LATEST REVISION OF ECRA Nov 12, 2025 · N17128 · Boeing 757224 · Fuselage Main, FrameSDR CALA2025111411216Inlet Door · corroded(SDR)(B757-MP-2000-53-1-0026) THROUGH ACCESS PANEL 311AL APU INL ET DOOR LOWER STRAP BETWEEN 1787 TO 1825 WITH EXFOLIATION DOT 07 -024. REF NR 134577. SFR REPORTING ONLY FABRICATED APU INLET DOOR STRAP IAW SRM 53-80-15-2R. REPLACED NE W INLET DOOR APU STRAP IANov 11, 2025 · N17128 · Boeing 757224 · APU Core EngineSDR CALA2025111111104Fuel Tank · corrodedDURKING OK TO INSTALL OF FLOOR PANEL, FOUND BETWEEN BS 984 - 996 BELOW ACCESS PANEL 242BF, EXFOLIATION IN THE LOWER SURFACE. REF NRC 135215. REMOVED CORROSION ON UPPER SURFACE OF FUEL TANK SKIN BETWEEN BS 989 - 996 IAW SRM 51-10-02, SRM 57-10-01, REPAIR APB-1Nov 10, 2025 · N17128 · Boeing 757224 · Fuel StorageSDR CALA2025111711272Fitting · crackedCRACK DAMAGE ON THE OTBD SIDE, FWD LOWER FLANGE OF MID BULKHEAD FITTING OF THE NR 2 STRUT ASSY AT PPS 174.30. THE CRACK EXTENDS FROM THE FWD EDGE OF FLANGE TO THE FWD FASTENER HOLE THROUGH ENTIRE MATERIAL THICKNESS.Nov 9, 2025 · N17128 · Boeing 757224 · Nacelle/Pylon, Main FrameSDR CALA2025111711271Frame · dentedONE DENT REPORTED DURING C CHECK ON THE LT BS 680 FRAME, BETWEEN S23L & S24L. THE DENT MEASURES 0.700 INCH LONG, 0.500 INCH WIDE, AND 0.015 INCH DEEP. INTERIM REPAIR PERFORMED AS PER ECRA 5330-07645 PART1.Nov 9, 2025 · N17128 · Boeing 757224 · Fuselage Main, FrameSDR CALA2025111711270Frame · dentedDURING C-CHECK, REPORTED ONE DENT ON BS 1280 FRAME BOTTOM, BETWEEN S26R AND S27R. THE DENT MEASURES 1.20 INCH LONG, 0.92 INCH WIDE, AND 0.024 INCH DEEP. INTERIM REPAIR PERFORMED AS PER ECRA 5360-02051 PART1.Nov 9, 2025 · N17128 · Boeing 757224 · Fuselage Main, FrameSDR CALA2025111711269Frame · crackedWHILE ACCOMPLISHING INSPECTION PER EA 5311-01827, NOTED CRACK ON THE LT BS 1640 FRAME BETWEEN S14L AND S15L. THE CRACK STARTS AT FREE FLANGE OF THE INBD CHORD AND PROPAGATES INTO THE WEB. PERFORMED INSPECTIONS PER PART 2 OF THE LATEST REVISION OF ECRA 5360-Nov 9, 2025 · N17128 · Boeing 757224 · Fuselage Main, FrameSDR CALA2025111211165Frame · dentedFWD CARGO BAY FRAME BS 680, DENTED. REPAIRED FWD CARGO FRAME AT BS 680, S23L IAW EC/RA 757-5330-13 -A4168.Nov 8, 2025 · N17128 · Boeing 757224 · Fuselage Main, FrameSDR CALA2025111211155Frame · dentedAFT CARGO BAY BS 1280 BETWEEN STRINGERS 26R TO 27R DENTED. REPAIRED THE FRAME BS 1280 S26R-27R IAW EA 757-5360-13- A4160.Nov 7, 2025 · N17128 · Boeing 757224 · Fuselage Main, FrameSDR CALA2025111211153Frame · dentedBULK CARGO BAY, FRAME HAS A DENT ON LOWER LOBE, BS 1560, LT SIDE, NEAR S26L. REPAIRED BULK CARGO IAW EA 757-5360-13- A4162.Nov 7, 2025 · N17128 · Boeing 757224 · Fuselage Main, FrameSDR CALA2025111011098Fitting · crackedNUMBER 2 PYLON OTBD SIDE THROUGH ACCESS PANEL 443CR, LOWER CORNER OF PP STA 174 WITH EVIDENCE OF A CRACK. REPAIRED THE PYLON OTBD SIDE BULKHEAD FITTING IAW EA 757-5450-13-A4151 AND EC/RA 5450-03064 REV-.Nov 7, 2025 · N17128 · Boeing 757224 · Nacelle/Pylon, Main FrameSDR CALA2025111011049Tee Angle · corrodedEXTERNAL LOWER FUSELAGE BS 900 TEE ANGLE LBL 6 WITH CORROSION. TEE ANGLE BS 900 WAS REPLACED IAW SRM 51-70-11- OG.Nov 6, 2025 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025111011047Fitting · crackedL4 DOOR UPPER FITTING CRACKED. REMOVED AND REPLACED UPPER FITTING ON L4 DOOR IAW SRM 51-40-02-06-0Nov 6, 2025 · N17128 · Boeing 757224 · Passenger/Crew DoorsSDR CALA2025111011036Bracket · crackedDURING REMOVAL OF TEE FITTING AT BS 900, FOUND ONE ANGLE BRACKET WITH A CRACK AT LBL 5. REMOVED AND REPLACED BRACKET (CLIP) ON TEE FITTING IAW SRM 51-40-02-OG AND DWG 149N7130.Nov 4, 2025 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025110610966Intercostal · corrodedFWD CARGO BAY BETWEEN BS 740 - 760, STR 28L-29L, INTERCOSTAL HAS EVIDENCE OF CORROSION. R & R THE INTERCOSTAL IAW SRM 51-40-02-06 & DWG 143N5355.Nov 4, 2025 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025110610960Skin · crackedLEFT WING, SLAT NR 1, INNER SURFACE, ABOVE INBD TRACK, CLOSE TO WS 735, SKIN CRACKED. REMOVED, FABRICATED, & INSTALLED LT WING INNER SKIN IAW SRM 51-40-02, REINSTALLED SLAT NR 1 IAW AMM 27-81-02-424-021.Nov 1, 2025 · N17128 · Boeing 757224 · Leading Edge DevicesSDR CALA2025110610958Skin · crackedLEFT WING, SLAT NR 2, INNER SURFACE, ABOVE OTBD TRACK, CLOSE TO WS 675, SKIN HAS A CRACK. REMOVED AND REPLACED THE INNER SKIN IAW SRM 51-40-02-0G-0. REINSTALLED THE NR 2 SLAT IAW AMM 27-81-02-024-001, & 27-81-02 424-021.Nov 1, 2025 · N17128 · Boeing 757224 · Leading Edge DevicesSDR CALA2025110610956Stiffener · corrodedAFT CARGO COMP, FWD BULKHEAD, REAR SIDE, STIFFENER BS 1180, LBL 53.96 HAS EXFOLIATION ON LOWER AREA. REPAIRED IAW EC/RA 5340-02246 AND EA 757-5340-13-A4169 REV-.Nov 1, 2025 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025110610954Skin · crackedLEFT WING, SLAT 3, INNER SURFACE, ABOVE INBD TRACK, SKIN CRACKED. REMOVED, FABRICATED & INSTALLED LH WING SLAT #3 INNER SURFACE SKIN IAW SRM 51-40-02, & MAE TRAVELER T25/1836170. REMOVED AND REINSTALLED THE SLAT IAW AMM 27-81-02-024-001, & 27-81-02-424-021Nov 1, 2025 · N17128 · Boeing 757224 · Leading Edge DevicesSDR CALA2025110210826Intercostal · corrodedFWD CARGO BAY, BETWEEN BS 740 - 760, S27L-28L, INTERCOSTAL HAS EVIDENCE OF CORROSION. REMOVED CORROSION IAW SRM 51-10-02-OG, EVALUATED DAMAGE (ORIGINAL THICKNESS 0.032") REMAING TH 0.022" FOUND TO BE OUT OF LIMITS IAW SRM 53-30-04-01-1 T88093, INTERCOSTAL ANDNov 1, 2025 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025111211139Strap · crackedEA 5311-01827 REV F - CRACK FOUND AT FLANGE RADIUS LOCATED AT THE INTERCOSTAL STRAP AT S14L AT FR 1640. ACCOMPLSIHED EC/RA 5360-02050 AND EA 757-5360-13 A4156 PRELIMINARY 1.Oct 28, 2025 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025102710576Floor Support · crackedE/E FLOOR STRUCTURE OF THE PASSENGER CABBIN BETWEEN BS 395 TO 418 CROSSBEAM 0, SUPPORT CHANNEL WITH EVIDENCE OF A CRACK. REMOVED AND REPLACED SUPPORT P/N141N5191-1 IAW SRM 51-4 0-02-0G, RESTORED SURFACE PROTECTION AT SUPPORT IAW AMM 51-21-15-370-801, & AMMOct 23, 2025 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025102310440Support Strap · corrodedAFT CARGO COMP, BEHIND RH SIDE PANEL, BTW STA 1360 AND STA 1380, STRAP SUPPORT HAS CORROSION AROUND NUTPLATES. REMOVED SUPPORT ANGLE BTW BS 1360 - 1380 IAW SRM 51-4 0-02. REMOVED FOR ACCESS TRANSITION PANEL IAW SRM 51-40-02. INSTALLED NEW PART IAW SRM 5 1Oct 21, 2025 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025102110328Bracket · corrodedAFTER THE SCUFF PLATE WAS REMOVED AT L4 PAX DOOR, AREA UNDER FOUND SPOTS WITH CORROSION. REMOVED AND REPLACED (3EA ANGLE) CLIP P/N 146N5246U61 BATCH 0004 433738 SUPPORT P/N 146N5246U5 BATCH 0004433522 AND BRACKET P/N U A1489-113 TRAVELER T25/1836788 ON LOWER Oct 16, 2025 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025102110327Intercostal · corrodedFWD CARGO BAY, BETWEEN BS 720-740 AND STR 27R-28R, INTERCOSTAL HAS EVIDENCE OF CORROSION. NR: 134672 COMPLETED SFR REPORTING ONLY REMOVED CORROSION ON FWD CARGO INTERCOSTAL STA 720-740 STR 27R-2 8R. IAW B757-300 SRM 51-10-02. FOUND OUT LIMITS ORIGINAL MAT 0.0 Oct 16, 2025 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025102110326Intercostal · corrodedFWD CARGO CMPT, BETWEEN STA 660-680 STR 28R, INTERCOSTAL HAS EVIDENCE OF CORROSION. COMPLETED SFR REPORTING ONLY REMOVED AND REPLACED INTERCOSTAL AT FWD CARGO COMPT BETWEEN STA 660-680 STR 28R.Oct 16, 2025 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025101610184Floor Support · crackedAFT CARGO COMPARTMENT FLOOR STRUCTURE OF PASSENGER CABIN BETWEEN 1320 TO 1340, CROSSBEAM WEB WITH CRACK. REMOVED AND REPLACED FLOOR SUPORT ANGLE FROM STA 1320-1340 BL0 IAW SRM 51-40-02.Oct 15, 2025 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025101610174Channel · crackedAFT CARGO COMP, RT SIDE, LOWER LOBE SIDEWALL SUPPORT IS BENT. REMOVED AND REPLACED SUPPORT CHANNEL P/N JA453N1801-22 AND TRAVELER T25/1834688 AT AFT CARGO COMP, RH SIDE, LOWER LOBE SIDE WALL SUPPORT, STA 0360. IAW B757-200 SRM 51-40-02.Oct 14, 2025 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025101610173Floor Support · crackedAFT CARGO COMPARTMENT FLOOR SUPPORT OF PASSENGER CABIN BETWEEN 1520 TO 1540 CROSSBEAM WEB WITH CRACK. REMOVED AND REPLACED FLOOR SUPPORT ANGLE BTW STA 1520-1540 BLO I AW B757-200 SRM 51-40-02-0G-0.Oct 14, 2025 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025101510130Wire Harness · chafedINSIDE HYD SERVICE COMPARTMENT NEXT TO HYD CENTRAL RESERVOIR, FOUND ELECTRICAL HARNESS WITH CHAFING. REMOVED AND REPLACED THE WIRING HARNESS W2412-1002-18 OF THE HYD RSVR IN HYD SERVICE BAY IAW SWPM 20-00-13, WDM 29-32-41 OK, PERFORMED OPS TEST OF HYD RSVR TEOct 14, 2025 · N17128 · Boeing 757224 · Hydraulic Power System WiringSDR CALA2025101410074Channel · crackedMAIN CABIN, AFTER REMOVED DOME N UTS FLOOR STRUCTURE, FOUND T-CHANNEL WITH A CRACK AT FR1180 LBL 0. REMOVED FLOOR PANEL SUPORT FROM FR1190 LBL 0 MAIN CABIN IAW SRM 51-40-02 FABRICATED LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-40-03-OG-0 AND DWG 144N8006 APPLOct 13, 2025 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025101510123Angle · crackedAFT CARGO COMPARTMENT FLOOR STRUCTURE OF PASSENGER CABIN BETWEEN 1200 TO 1220, CROSSBEAM 0, WEB CRACKED. EVALUATED SHEAR WEB AND ANGLE, CRACK OUT OF LIMITS IAW SRM 53-00-04-1A-1; INSTALLED NEW SHEAR WEB AND SLEEVE IAW SRM 51-40-02-0G-0.Oct 12, 2025 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025101510122Bracket · crackedAFT BULK CARGO, WATER SERVICE BOX HAS A BRACKET WITH A CRACK, NEAR BS 1681.8, S30. REMOVED AND REPLACED AFT BULKHEAD BRACKET NEAR BS 1581.8 S30 IAW SRM 51-10-02.Oct 12, 2025 · N17128 · Boeing 757224 · Fuselage Main, Attach FittingsSDR CALA2025101510121Channel · corrodedAFT CARGO BAY LT SIDE, LOWER LOBE SIDWALL SUPPORT IS BENT AND WITH EVIDENCE OF CORROSION, BS 1300. REMOVED CHANNEL IAW SRM 51-40-02-0G-0, AND INSTALLED IAW SRM 51-40-02-0G-0.Oct 12, 2025 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025101410065Support Strap · corrodedAFT CARGO COMP) BEHIND RH SIDE PA NEL, BTW STA1280 AND STA1300, STRAP SPPRT HAS CORROSION AROUND N UTPLATES. DOT 23-043 COMPLETED SFR REPORTING ONLY REMOVED AND REPLACED STRAP (CHORD). AT AFT CARGO COMP. BEHIND R/ H SIDE PANEL BTW B51280-B51300. P/N:146N5448-2Oct 12, 2025 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025101410064Stringer Clip · crackedAFT CARGO COMP, BS 1380, NEAR S-27R, FLOOR STR CLIP HAS A CRACK. DOT 23-065 COMPLETED SFR REPORTING ONLY REMOVED AND REPLACED STR CLIP AT OFF CARGO COMP. STA 1380 FLOOR STR 5-27R IAW B757-200 SRM 51-40-02, DWG. 146N5393 AND TRAVELER T25/1835297.Oct 12, 2025 · N17128 · Boeing 757224 · Fuselage Main, Attach FittingsSDR CALA2025081507837D-Ring · looseL4 DOOR D-RING INACESSABLE, REATTACHED D-RING AT L4 DOOR. OPS CHECKS NORMAL AT THIS TIME. OK TO CONTINUEAug 15, 2025 · N17128 · Boeing 757224 · Emergency EquipmentSDR CALA2025072306860Computer · unknownTCAS INOP, TCAS INOPERATIVE. TCAS FAIL BOTH TRANSPONDER COMPUTER, T/S IAW FIM 34-45 FAULT TREE 802. PERFORMED TCAS BITE PROCEDURE AND COULD NOT DUPLICATE FAULT. REMOVED AND REPLACED TCAS COMPUTER AS A PRECAUTION IAW AMM 34-45-01. OPS CHECK GOOD. NO FAULTS NOJul 21, 2025 · N17128 · Boeing 757224 · Air Collision Avoidance SystemSDR CALA2025043004336Flap · brokenLEFT AFT OVERWING EMERGENCY EXIT HATCH HANDLE FLAPPER, BROKEN.ACCOMPLISHED A DETAILED VISUAL INSPECTION OF LATCH AND TRIGGER, NO FAULTS. INSURED FASTNERS ARE INTACT AND DOOR ARMED NORMAL. REMOVED LEFT AFT OVERWING HATCH FOR EVALUATION PER AMM 25-66-09. FOUNDApr 25, 2025 · N17128 · Boeing 757224 · Emergency ExitsSDR CALA2024121201478Light · faultedEMERGENCY LIGHTS (USING CONTROL SWITCHES) OPERATIONAL CHECK {MULT-33-3-0001} - FOUND ROW30C EEL LITE ASSY STOWED AND NOT SECURED REPLACED ROW 30 C EEL LIGHT ASSEMBLY, OP CHECKS GOOD, REFERENCE AMM 33-51-11. PARTS USED: 42-2521-3-0092, QTY :1 42-2521-3-0084,QTDec 8, 2024 · N17128 · Boeing 757224 · Emergency LightingSDR CALA2024042401221Transition Panel · dentedDURING OK TO INSTALL AFT CARGO TRANSITION PANEL S26LH AND STA 14 00 UPPER SKIN FRAME WITH DENT. EVALUATED FRAME AT STA 1400 S26LH IAW B757-200 SRM 53-00-07-1A1, INSTALL NEW REPAIR SECTION AT STA1400 526 LA IAW B757-200 SRM 53 NO DENTS ALLOW ON FLANGE THEREFOREApr 22, 2024 · N17128 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2024041701115Skin · damagedNOSE FUSELAGE SKIN BETWEEN STA 333 TO STA 350 AND NEXT TO S23R WITH LIGHTNING STRIKE MARK. ACCOMPLISH PERMANENT REPAIR IAW B757-200 SRM 53-00-01-2R-28, REP AIR 28 FIG 202, NOSE FWD FUSELAGE SKIN, BETWEEN STA 333 TO STA S TA 350, AT S23R.Apr 16, 2024 · N17128 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2024011900138Warning Light · false activationREJECTED T/O DUE TO RIGHT ENG BLEED TRIP. LOW SPEED REJECT. TEST WITHIN LIMITS. LOCKED FOR MORE INFORMATION UNLOCKED EWR MM WORKING ITEM. F.O.B L 14.4 C 10.9 R 15.0 40.2 TOTAL CREW STATES THAT THE RIGHT BLEED OFF LIGHT CAME ON DURING TOMC REQUESTED TO CHECK FAJan 16, 2024 · N17128 · Boeing 757224 · Engine Bleed Air SystemSDR CALA2024010500038Pump · corrodedC HYD ELEC 1 ON CLB OUT AT FL280 DEFER PER MEL 2911D. C1 HYD ELETRIC PUMP INOPERATIVE AND DEACTIVATED COMPLIED WITH MEL 2911D MEL 2911D APPROVED CONNECTOR D2204 AT C1 PUMP CORRODED. REF WD29-11-31. WILL NEED CONNECTOR AND PUMP REPLACED. WILL NEED 14 MANHRS FORJan 3, 2024 · N17128 · Boeing 757224 · Hydraulic Pump (Electric/Engine), MainSDR CALA2023083002664Plug · leakingBOTH REAR LAVS LEAKING CONTINUOUSLY DURING FLIGHT BRADLEY NEIL PAUL TOMC APPROVES LAVATORY K & M TOILET FLUSH SYSTEM(S) INOPERATIVE AND DEACTIVATED. ASSOCIATED LAVATORY(IES) IS NOT USABLE PER MEL 3830C. BOTH TANKS DUMPED/DRAINED AND NO LEAKS DISPATCH DESK: 349Aug 26, 2023 · N17128 · Boeing 757224 · Water and Waste SystemSDR CALA2023080902467Control Valve · inoperativeLOW SPEED ABORT DUE TO R ENG BLEED EICAS R FAN AIR MODULATION VALVE LOCKED IN OPEN POSITION PER MEL 3612D. AMM 05-51-14 INSPECTION DUE TO ABORT, NO ISSUES NOTED MEL 3612D LHRMM WORKING ITEM REMOVED AND REPLACED NO.2 ENGINE FAN AIR MODULATING VALVE PER PARTS USAug 6, 2023 · N17128 · Boeing 757200 · Compressor Bleed ValveSDR 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 System
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