# Service difficulty reports: Boeing 757-2G5 A list on [Boeing 757-2G5](https://openairdocs.org/model/boeing-757-2g5.md). Newest first. General aviation reporting is voluntary. Page 1 of 12 · 556 reports - [SDR FDEA202610121559](https://openairdocs.org/sdr/FDEA202610121559.md): Skin · corroded · Oct 12, 2026 · N943FD · Boeing 7572G5 · Trailing Edge Flaps > LEFT WING INBD FLAP UPPER SURFACE O/B SIDE EXTERNAL SKIN SOME AREA WITH CORROSION. LT WING I/B FLAP UPPER SURFACE O/B SIDE WAS REPAIRED IAW B757 SRM 57-53-01-2R REPAIR 1 FIGURE 201 DETAIL I (SHEET 2) AND SRM 51-70-10-2R - [SDR FDEA202610091536](https://openairdocs.org/sdr/FDEA202610091536.md): Floorbeam · corroded · Oct 9, 2026 · N943FD · Boeing 7572G5 · Fuselage Main, Floor Beam > MAIN CARGO COMPARTMENT FLOORBEAM BS 1200 BETWEEN 24LBL TO 0BL SOME AREAS WITH CORROSION. AREA OUT OF LIMITS WAS REPAIRED AT MAIN CARGO COMPARTMENT FLOORBEAM BS 1200 BETWEEN 26LBL TO 13LBL IAW SRM 53-00-51-2R, REPAIR.1. - [SDR FDEA202610051478](https://openairdocs.org/sdr/FDEA202610051478.md): Skin · delaminated · Oct 5, 2026 · N943FD · Boeing 7572G5 · Elevator, Plate/Skin > TWO INDICATIONS OF DISBOND WERE FOUND OVER TWO DENTS ON THE UPPER SKIN OF THE LEFT ELEVATOR: ONE AT ELEV STA 107.360, 1.800 INCHES IN DIAMETER AND 13.5 INCHES FROM THE TRAILING EDGE; AND THE OTHER AT ELEV STA 109.430,1.300 INCHES IN DIAMETER AND 14.5 INC - [SDR FDEA202607220987](https://openairdocs.org/sdr/FDEA202607220987.md): Fitting · cracked · Jul 22, 2026 · N962FD · Boeing 7572G5 · Nacelle/Pylon Miscellaneous Structure > CRACK FOUND ON #2 ENGINE LOWER OUTBD MIDSPAR BULKHEAD FITTING. REPAIRED OUTBD MIDSPAR BULKHEAD FITTNG IAW EA F-5450-T0387823 PT1, NACELLS / PYLON - WING PYLON / STRUT - #2 PYLON - PP STA 174.30 MID BULKHEAD - RH FITTING CRACKED AT LOWER VERTICAL FLANGE. M - [SDR FDEA202607030828](https://openairdocs.org/sdr/FDEA202607030828.md): Door · unsecure · Jul 3, 2026 · N943FD · Boeing 7572G5 · Service Doors > COULD NOT GET R1 DOOR SLIDE LIGHT TO ILLUMINATE WHEN CLOSING DOOR. WHILE APPROACHING AIRCRAFT NOTED R1 DOOR NOT COMPLETELY CLOSED. CYCLED DOOR AND ARMED SLIDE, OPS CHECK NORMAL PER AMM 52-11-00-0. - [SDR IXXA20260501001](https://openairdocs.org/sdr/IXXA20260501001.md): Skin · corroded · May 6, 2026 · N752CX · Boeing 7572G5 · Wing, Plate/Skin > CORROSION ON THE LOWER SURFACE OF THE RIGHT WING LOWER SKIN - [SDR IXXA20260424001](https://openairdocs.org/sdr/IXXA20260424001.md): Bracket · corroded · Apr 21, 2026 · N752CX · Boeing 7572G5 · Wing Miscellaneous Structure > LEFT WHEEL WELL ON THE H BEAM IS A HYDRAULIC LINE B NUT THATS SITTING RIGHT IN FRONT OF THE CUSHION CLAMP AND BRACKET, AND THE BRACKET IS CORRODED. - [SDR IXXA202604080002](https://openairdocs.org/sdr/IXXA202604080002.md): Support Fitting · corroded · Apr 8, 2026 · N752CX · Boeing 7572G5 · Fuselage Main, Attach Fittings > CORROSION AROUND SUPPORT FITTING FASTENER AT STA 1180 RBL 28 - [SDR IXXA2026040600001](https://openairdocs.org/sdr/IXXA2026040600001.md): Support Angle · corroded · Apr 6, 2026 · N752CX · Boeing 7572G5 · Wing Miscellaneous Structure > CORROSION ON SUPPORT ANGLE IN LWW FOR STRUT DOOR CUTOUT - [SDR IXXA20260403002](https://openairdocs.org/sdr/IXXA20260403002.md): Pad · gouged · Apr 3, 2026 · N752CX · Boeing 7572G5 · Wing Main, Frame Structure > WHILE SERVICING MAIN LANDING GEAR STRUTS, THE AIRCRAFT TILTED TO THE LEFT CAUSING LEFT MAIN GEAR JACK TO COME INTO CONTACT LOWER WING AT JACKING PAD. - [SDR IXXA20260403001](https://openairdocs.org/sdr/IXXA20260403001.md): Pad · gouged · Apr 3, 2026 · N752CX · Boeing 7572G5 · Wing Main, Frame Structure > WHILE DRILLING OUT FASTENER IN THE LEFT-WING JACK PAD DOUBLER, THE DRILL CONTACTED THE OUTER PERIMETER OF HOLE IN THE WING SKIN - [SDR IXXA20260329002](https://openairdocs.org/sdr/IXXA20260329002.md): Keelbeam · corroded · Mar 29, 2026 · N752CX · Boeing 7572G5 · Fuselage Main, Keel > CORROSION AT THE HYD TUBING PASS THRU AT THE KEEL WALL IN THE LWW BS 1171-1180. - [SDR IXXA20260329001](https://openairdocs.org/sdr/IXXA20260329001.md): Support Beam · corroded · Mar 29, 2026 · N752CX · Boeing 7572G5 · Wing Miscellaneous Structure > LEFT WING UPPER FIXED WING SKIN PANEL SUPPORT BEAM CORRODED IN SEVERAL PLACES - [SDR IXXA20260316001](https://openairdocs.org/sdr/IXXA20260316001.md): Bracket · corroded · Mar 16, 2026 · N752CX · Boeing 7572G5 · Wing, Attach Fittings > LEFT WING T/E INBD. OF DEFUEL VALVE HAS CABLE GUIDE BRACKET CORRODED - [SDR IXXA20260315002](https://openairdocs.org/sdr/IXXA20260315002.md): Retainer · broken · Mar 15, 2026 · N752CX · Boeing 7572G5 · Fuselage Main, Structure > SEAL RETAINER SUPPORT STRUCTURE BROKEN IN RWW MLG DOOR CUTOUT - [SDR IXXA20260315001](https://openairdocs.org/sdr/IXXA20260315001.md): Skin · corroded · Mar 15, 2026 · N752CX · Boeing 7572G5 · Fuselage Main, Plate/Skin > FOUND SKIN CORROSION COMMON TO RT FILLET PANEL @ STA 793, 805, 825 ALL ON SKIN PANEL 143N3561-4 - [SDR IXXA04062026CC01](https://openairdocs.org/sdr/IXXA04062026CC01.md): Bracket · cracked · Mar 13, 2026 · N752CX · Boeing 7572G5 · Engine (Turbine/Turboprop) > NR 1 ENGINE COMPRESSOR BOOST FRAME FLANGE BRACKET BENT AND CRACKED AT THE ENGINE 11 O'CLOCK POSITION. - [SDR IXXA2026031301](https://openairdocs.org/sdr/IXXA2026031301.md): Skin Panel · damaged · Mar 13, 2026 · N752CX · Boeing 7572G5 · Wing, Plate/Skin > REPAIRED CORRODED LEFT WING REAR SPAR UPPER PANEL SUPPORT LIP AND SKIN. - [SDR IXXA20260311001](https://openairdocs.org/sdr/IXXA20260311001.md): Skin · corroded · Mar 11, 2026 · N752CX · Boeing 7572G5 · Fuselage Main, Plate/Skin > FUSELAGE SKIN IS CORRODED AT LOWER FWD WING TO BODY ATTACHMENT. STA 740-781, S18L- 18R. OTHER PN +143N3521-9,143N359-1/2 - [SDR IXXA20260310001](https://openairdocs.org/sdr/IXXA20260310001.md): Skin · corroded · Mar 10, 2026 · N752CX · Boeing 7572G5 · Fuselage Main, Plate/Skin > FUSEELAGE LEFT SIDE STA 785-855 LEVEL 2 CORROSION2 BODY TO WING PANELS - [SDR IXXA20260304001](https://openairdocs.org/sdr/IXXA20260304001.md): Skin Panel · corroded · Mar 4, 2026 · N752CX · Boeing 7572G5 · Fuselage Main, Plate/Skin > RIGHT FUSELAGE CLOSEOUT FAIRING PANEL AFT OF MAIN CARGO DOOR FOUND CORROSION AT UPPER AND LOWER DOOR CORNERS NO PART NUMBERS FOUND ON REMOVE PANEL. FABRICATED NEW CLOSEOUT FAIRING PANEL, ASSIGNED NEW P/N 47696FAB01 - [SDR IXXA20260302001](https://openairdocs.org/sdr/IXXA20260302001.md): Support Bracket · broken · Mar 2, 2026 · N752CX · Boeing 7572G5 · Compressor Bleed Valve > NR 1 ENGINE REMOVED AND REPAIRED HP2 VALVE CASE BRACKET DUE TO BROKEN SUPPORT BRACKET NR 187303-0400-0178, AND AMES 47170REA622 - [SDR IXXA20260223001](https://openairdocs.org/sdr/IXXA20260223001.md): Support Bracket · corroded · Feb 23, 2026 · N752CX · Boeing 7572G5 · Wing Miscellaneous Structure > REAR SPAR HYD BLOCK CLAMP SUPPORT BRACKET CORRODED.PN 271N6114-22 - [SDR IXXA20260222002](https://openairdocs.org/sdr/IXXA20260222002.md): Pressure Deck · corroded · Feb 22, 2026 · N752CX · Boeing 7572G5 · Fuselage Main, Structure > RIGHT WHEEL WELL PRESSURE DECK CORRODED STA1160 RBL3 P/N 144N8142-10 - [SDR IXXA20260222001](https://openairdocs.org/sdr/IXXA20260222001.md): Support Web · corroded · Feb 22, 2026 · N752CX · Boeing 7572G5 · Wing Miscellaneous Structure > LW FUEL BOOST PUMP CUTOUT CORROSION IRSS 183 - [SDR IXXA2026021901](https://openairdocs.org/sdr/IXXA2026021901.md): Bracket · corroded · Feb 19, 2026 · N752CX · Boeing 7572G5 · Wing Miscellaneous Structure > LEADING EDGE JUST ABOVE PYLON HAS CORROSION AROUND NUT PLATE - [SDR IXXA20260218001](https://openairdocs.org/sdr/IXXA20260218001.md): Bracket · corroded · Feb 18, 2026 · N752CX · Boeing 7572G5 · Wing Miscellaneous Structure > LEFT LANDING GEAR ELECTICAL CONNECTOR BRACKET CORRODED - [SDR IXXA2026020702](https://openairdocs.org/sdr/IXXA2026020702.md): Door · gouged · Feb 7, 2026 · N752CX · Boeing 7572G5 · Landing Gear Doors > RIGHT MLG DOOR IS GOUGED NEAR NO STEP PLACARD. - [SDR IXXA2026020701](https://openairdocs.org/sdr/IXXA2026020701.md): Web · corroded · Feb 7, 2026 · N752CX · Boeing 7572G5 · Wing Miscellaneous Structure > REAR SPAR FUEL BOOST PUMP CUTOUT TO BE CORRRODED - [SDR IXXA2026020605](https://openairdocs.org/sdr/IXXA2026020605.md): Skin · corroded · Feb 6, 2026 · N752CX · Boeing 7572G5 · Wing, Plate/Skin > CORROSION ON THE UPPER EXTERIOR SURFACE OF THE RIGHT WING UPPER SKIN, LOCATED FWD OF THE RIGHT AILERON. - [SDR FDEA202602060138](https://openairdocs.org/sdr/FDEA202602060138.md): Bulb · failed · Feb 6, 2026 · N943FD · Boeing 7572G5 · Emergency Lighting > FOUND L1 OVERHEAD EMERGENCY LIGHT DIM DURING MX PRE-FLIGHT CHECK. AMM: 33-51-01-2 REMOVED AND REPLACED 11 FAULTY BULBS AT THE L1 EMERGENCY EXIT SIGN AS PER ABOVE REF. OPS CHECK GOOD. - [SDR IXXA2026020603](https://openairdocs.org/sdr/IXXA2026020603.md): Skin · corroded · Feb 6, 2026 · N752CX · Boeing 7572G5 · Fuselage Main, Plate/Skin > FOUND AREA OF LW LOWER SKIN CORRODED JUST O/B OF BBL 70.50, JUST FWD OF STR L-10 ON THE EXTERNAL SURFACE - [SDR IXXA2026020602](https://openairdocs.org/sdr/IXXA2026020602.md): Support · corroded · Feb 6, 2026 · N752CX · Boeing 7572G5 · Fuselage Miscellaneous Structure > CORROSION ON PANEL SUPPORT ATTACHED TO THE AFT WALL IN THE LWW, FROM LBL7 TO LBL34 - [SDR IXXA2026020601](https://openairdocs.org/sdr/IXXA2026020601.md): Skin · damaged · Feb 6, 2026 · N752CX · Boeing 7572G5 · Fuselage Main, Plate/Skin > DURING REPAIR ON NR 187303-0100-0192 IT WAS DISCOVERED THAT THERE IS A SCRIBE JUST FWD OF THE REPAIR AREA AT STA 740 STR 19L COMMON TO THE SKIN LAP. - [SDR IXXA20260205002](https://openairdocs.org/sdr/IXXA20260205002.md): Stop Fitting · damaged · Feb 5, 2026 · N752CX · Boeing 7572G5 · Passenger/Crew Doors > L1 FWD DOOR STOP FITTING DAMAGE WAS REMOVED BY BLEND. THIS DAMAGE EXCEEDS ALLOWABLE LIMITS. - [SDR IXXA2026020404](https://openairdocs.org/sdr/IXXA2026020404.md): Bracket · corroded · Feb 4, 2026 · N752CX · Boeing 7572G5 · Wing Miscellaneous Structure > LEFT WING T/E FRONT SECTION OF LANDING GEAR SUPPORT BEAM HAS CORRODED PANEL SUPPORT BRACKET - [SDR IXXA2026020403](https://openairdocs.org/sdr/IXXA2026020403.md): Bracket · corroded · Feb 4, 2026 · N752CX · Boeing 7572G5 · Aerodynamic Fairings > LOWER FUSELAGE WING TO BODY PANEL SUPPORT BRACKET HAS CORROSION AT WIRING CLAMP HOOKUP BETWEEN LEFT WHEEL WELL AND GEAR - [SDR IXXA20260111002](https://openairdocs.org/sdr/IXXA20260111002.md): Bracket · corroded · Jan 11, 2026 · N752CX · Boeing 7572G5 · Fuselage Main, Attach Fittings > EDIT (NEW CONTROL NUMBER) FROM DUPLIACATE CONTROL NUMBER IXXA20260111001 - FOUND CORROSION ON THE BLOCK SUPPORT TUBING IN THE OUTBOARD UPPER AREA OF THE LEFT WHEEL WELL OUTBOARD OF THE ANTISKID VALVES. - [SDR IXX2026F00000](https://openairdocs.org/sdr/IXX2026F00000.md): Bracket · corroded · Jan 11, 2026 · N752CX · Boeing 7572G5 · Fuselage Main, Attach Fittings > FOUND CORROSION ON THE BLOCK SUPPORT TUBING IN THE OUTBOARD UPPER AREA OF THE LEFT WHEEL WELL OUTBOARD OF THE ANTISKID VALVES. - [SDR IXXA20260205001](https://openairdocs.org/sdr/IXXA20260205001.md): Bearing · galled · Jan 7, 2026 · N752CX · Boeing 7572G5 · Nacelle/Pylon, Main Frame > GALLING, LIGHT CORROSION AND GOUGE AROUND BEARING FACE - [SDR IXXA20260112002](https://openairdocs.org/sdr/IXXA20260112002.md): Support Beam · corroded · Jan 6, 2026 · N752CX · Boeing 7572G5 · Landing Gear Doors > RMLG STRUT DOOR SUPPORT BEAM IS CORRODED IN MULTIPLE AREAS - [SDR FDEA202601060010](https://openairdocs.org/sdr/FDEA202601060010.md): Bulb · failed · Jan 6, 2026 · N962FD · Boeing 7572G5 · Emergency Lighting > DURING MX PRE-FLIGHT, FOUND R1 EMERGENCY EXIT SIGN DIM. AMM: 33-51-01-2 FOUND R1 EMERGENCY EXIT SIGN HAS 9 BULBS OUT. REMOVED AND REPLACED 9 FAULTY BULBS AS PER ABOVE REF. PART NUMBER 0L3071BPEGPL. OPS CHECK GOOD. A/C OK FOR SERVICE. - [SDR FDEA202601060009](https://openairdocs.org/sdr/FDEA202601060009.md): Bulb · failed · Jan 6, 2026 · N962FD · Boeing 7572G5 · Emergency Lighting > DURING MX PRE-FLIGHT, FOUND L1 EMERGENCY EXIT SIGN DIM. AMM 33-51-01-2 FOUND L1 EMERGENCY EXIT SIGN HAS 7 BULBS OUT. REMOVED AND REPLACED 7 FAULTY BULBS AS PER ABOVE OPS CHECK GOOD. A/C OK FOR SERVICE. - [SDR IXXA20260112001](https://openairdocs.org/sdr/IXXA20260112001.md): Channel · corroded · Dec 30, 2025 · N752CX · Boeing 7572G5 · Fuselage Miscellaneous Structure > CORROSION ON THE INSIDE OF THE U CHANNEL THAT SUPPORTS THE HYD ISOLATION VALVE, LOCATED ON THE BACK WALL IN THE LEFT WHEEL WELL STA 1180 - [SDR IXXA20251222001](https://openairdocs.org/sdr/IXXA20251222001.md): Skin · corroded · Dec 22, 2025 · N752CX · Boeing 7572G5 · Wing, Plate/Skin > .CORROSION OF THE UPPER EXTERIOR SURFACE OFTHE RIGHT WING UPPER SKIN FWD OF THE AILERON - [SDR IXXA04022026CC01](https://openairdocs.org/sdr/IXXA04022026CC01.md): Fitting · deformed · Dec 18, 2025 · N752CX · Boeing 7572G5 · Wing, Attach Fittings > REMOVED FOR ACCESS THE RW SIDE LINK ATTACH FITTING "MICKEY MOUSE FITTING" FOR SIDE LOAD FITTING ALIGHNMENT. DURING REMOVAL FOUND DAMAGED FREEZE PLUG/BUSHING IN HOLE. - [SDR IXXA20260111001](https://openairdocs.org/sdr/IXXA20260111001.md): Support Channel · corroded · Dec 18, 2025 · N752CX · Boeing 7572G5 · Fuselage Miscellaneous Structure > RH AFT LOWER WING TO BODY FAIRING FRAME BS 1037 IS CORRODED - [SDR IXXA121820250001](https://openairdocs.org/sdr/IXXA121820250001.md): Rub Block · cracked · Dec 18, 2025 · N752CX · Boeing 7572G5 · Trailing Edge Flaps > RIGHT WING INBD FLAP T/E FAIRING 671BB HAD A CRACKED RUB BLOCK AT FAIRING AFT ATTACH ARM. - [SDR IXXA03292026CC01](https://openairdocs.org/sdr/IXXA03292026CC01.md): Support · corroded · Dec 9, 2025 · N752CX · Boeing 7572G5 · Wing Miscellaneous Structure > LEFT WING UNDER PANEL 551 AT SEVERAL AREA AROUND NUTPLATES ARE CORRODED. - [SDR IXXA03092026CC01](https://openairdocs.org/sdr/IXXA03092026CC01.md): Beam · worn · Nov 21, 2025 · N752CX · Boeing 7572G5 · Landing Gear Doors > RIGHT MLG STRUT DOOR SUPPORT BEAM IS HEAVILY WORN ALONG THE EDGE JUST FWD OF DRAG STRUT. Next page: https://openairdocs.org/model/boeing-757-2g5/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = '7572G5' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/boeing-757-2g5/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.