# Service difficulty reports: N752CX

A list on [N752CX](https://openairdocs.org/aircraft/N752CX.md).

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

Page 1 of 5 · 226 reports

- [SDR IXXA20260831077](https://openairdocs.org/sdr/IXXA20260831077.md): Insulation · melted · Aug 31, 2026 · N752CX · Boeing 757200 · Cabin Equipment/Furnishings
  > DURING CRUISE ELECTRICAL BURNING ODOR, FIRST OFFICER'S SIDE WAS THE STRONGEST FOR ABOUT 3 MINS. NO EMERGENCY DECLARED. ACFT LANDED WITHOUT INCIDENT. ACCOMPLISHED SMOKE/FUMES CONDITIONAL INSPECTION IAW AMM 05-51-56. FOUND & REMOVED METAL SHAVINGS & MELTED IN
- [SDR IXXA20260812069](https://openairdocs.org/sdr/IXXA20260812069.md): Light · inoperative · Aug 12, 2026 · N752CX · Boeing 757200 · Emergency Lighting
  > ROW 8 EMERGENCY LIGHT WILL NOT STAY ON PAST 4 SECONDS. PLACED ON DEFERRAL 75954 MINIMUM EQUIPMENT LIST CATEGORY C PER ATI-33-51-01-01. DUE 22 AUGUST 2026. TROUBLESHOT IN ACCORDANCE WITH B757 FIM 33-51 FAULT TRE 802 AND B757 WDM 33-51-15. EXAMINED PLUG D78. N
- [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 IXXA2026020604](https://openairdocs.org/sdr/IXXA2026020604.md): Web · corroded · Feb 6, 2026 · N752CX · Boeing 757200 · Fuselage Main, Keel
  > CORROSION ON THE KEEL WEB, AROUND THE HYD. TUBE FEEDTHROUGH, AT STA.1111, 47 INCHES UP FROM THE KEEL BEAM, IN THE LWW
- [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 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.
- [SDR IXXA03142026CC01](https://openairdocs.org/sdr/IXXA03142026CC01.md): Frame · corroded · Nov 19, 2025 · N752CX · Boeing 7572G5 · Aerodynamic Fairings
  > RH AFT WING TO BODY FAIRING ATTACH FRAME AT STA 1220 IS CORRODED.
- [SDR IXXA20262026003](https://openairdocs.org/sdr/IXXA20262026003.md): Door · gouged · Nov 19, 2025 · N752CX · Boeing 7572G5 · Landing Gear Doors
  > LEFT MLG DOOR GOUGED.
- [SDR IXXA04082026CC01](https://openairdocs.org/sdr/IXXA04082026CC01.md): Angle · corroded · Nov 17, 2025 · N752CX · Boeing 7572G5 · Aerodynamic Fairings
  > RH AFT LOWER WING TO BODY FAIRING FRAME STA 1050 IS CORRODED.
- [SDR IXXA20262026002](https://openairdocs.org/sdr/IXXA20262026002.md): Support Bracket · corroded · Nov 17, 2025 · N752CX · Boeing 7572G5 · Aerodynamic Fairings
  > LEFT LOWER WING - BODY FAIRING SUPPORT BRACKET STA 958 IS CORRODED.
- [SDR IXXA20262026001](https://openairdocs.org/sdr/IXXA20262026001.md): Skin · corroded · Nov 17, 2025 · N752CX · Boeing 7572G5 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN IS CORRODED AT LAP SEAM S-20L BS 1718.

Next page: https://openairdocs.org/aircraft/N752CX/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 n_number = 'N752CX' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N752CX/reports

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