# Service difficulty reports: N792CP

A list on [N792CP](https://openairdocs.org/aircraft/N792CP.md).

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

- [SDR SROM2025120479202](https://openairdocs.org/sdr/SROM2025120479202.md): Tire · separated · Nov 25, 2025 · N792CP · Bombdr DHC8402 · Tire
  > DURING TAKEOFF THE NR 1 MAIN LANDING GEAR TIRE TREAD SEPARATED FROM THE TIRE CASING IN SEVERAL LARGE PIECES AND WAS LEFT ON THE RUNWAY. WHEN THE TIRE TREAD SEPARATED IT CAUSED MINOR DAMAGE (DENTS) TO TWO OF THE SHOCK STRUT FAIRINGS REQUIRING THEM TO BE REPLAC
- [SDR SROM202311210001](https://openairdocs.org/sdr/SROM202311210001.md): Threshold · corroded · Oct 2, 2023 · N792CP · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > MED THRESHOLD MEMBER PN: 85329539 CORRODED AT SCREW HOLES AND BEYOND MANUFACTURES LIMITS. PART REPLACEMENT IS REQUIRED.
- [SDR SROM09122022](https://openairdocs.org/sdr/SROM09122022.md): Bracket · loose · Sep 8, 2022 · N792CP · Bombdr DHC8402 · Landing Gear Door Retract Section
  > THE THIRD OCCURRENCE OF N. DOOR GEAR DOOR ADVISORY LIGHT ILLUMINATED AFTER NORMAL GEAR EXTENSION OR RETRACTION. THE FOLLOWING TROUBLESHOOTING AND COMPONENT REPLACEMENTS/MAINTENANCE ACTIONS WERE TAKEN. FIRST OCCURRENCE; FOUND NOSE GEAR CLOSED PROXIMITY SENSOR
- [SDR SROM0523202204](https://openairdocs.org/sdr/SROM0523202204.md): Cleat · corroded · Jun 28, 2022 · N792CP · Bombdr DHC8402 · Fuselage Main, Longeron/Stringer
  > FUSELAGE FRAME UNDERFLOOR FS X156.00 STR. 24P CORROSION ON UPPER AND LOWER SURFACES OF BRACKET. CORROSION BEYOND MANUFACTURES LIMITS, PART REPLACEMENT REQUIRED. NOTE: RESUBMITTING THIS SDR DUE TO A CORRECTED PN. PN 85328131-120 WAS LISTED ON ORIGINAL SDR A
- [SDR SROM06222022](https://openairdocs.org/sdr/SROM06222022.md): Cleat · corroded · Jun 22, 2022 · N792CP · Bombdr DHC8402 · Fuselage Main, Structure
  > FUSELAGE FRAME UNDERFLOOR FS X236.00 STR. 27P, LIGHT CORROSION FOUND ON BRACKET SURFACE. POSSIBLE CORROSION UNDER FASTENER. DISASSEMBLY MAY BE REQUIRED. AFTER DISASSEMBLY, IT WAS DETERMINED THAT CLEAT PN 85328131-164 NEEDED TO BE REPLACED DUE TO CORROSION.
- [SDR SROM06142202](https://openairdocs.org/sdr/SROM06142202.md): Bracket · corroded · Jun 14, 2022 · N792CP · Bombdr DHC8402 · Trailing Edge Flap Control System
  > LH OUTBD FLAP, AFT FAIRING 526AB ATTACHMENT BRACKET INBD LUG HAS CHAFFING MARK, BOLTS FOUND LOOSE. AREA 1. DAMAGE DEPTH 0.003", LENGTH 0.570", WIDTH 0.200". AREA 2. DAMAGE DEPTH 0.015", LENGTH 0.100", WIDTH 0.400". AREA 3. DAMAGE DEPTH 0.025", LENGTH 1.300"
- [SDR SROM06142201](https://openairdocs.org/sdr/SROM06142201.md): Hinge · corroded · Jun 14, 2022 · N792CP · Bombdr DHC8402 · Spoilers
  > RH INBD SPOILER, INBD HINGE, CHAFING WEAR ON BOTH AIRCRAFT FITTING AND SPOILER FITTING. DAMAGE MAX DEPTH IS 0.018", MAX WIDTH IS 0.600" AND DAMAGE LENGTH IS 1.700".
- [SDR SROM060820221](https://openairdocs.org/sdr/SROM060820221.md): Skin · corroded · Jun 8, 2022 · N792CP · Bombdr DHC8402 · Fuselage Structure (General)
  > UPPER FUSELAGE OUTER SKIN AT FS X469 TO FS X553 BETWEEN STR. 12S AND 3S CHAFED ALONG WITH TO FUSELAGE FAIRING SEAL (AFT RG WING TO FUSELAGE FAIRING).
- [SDR SROM060720223](https://openairdocs.org/sdr/SROM060720223.md): Hinge Bracket · corroded · Jun 7, 2022 · N792CP · Bombdr DHC8402 · Rudder/Tab, Attach Fittings
  > CHAFING DAMAGE ON LOWER HINGE BRACKET OF RUDDER FITTING OF AIRCRAFT (LOWER FITTING).
- [SDR SROM060720222](https://openairdocs.org/sdr/SROM060720222.md): Skin · corroded · Jun 7, 2022 · N792CP · Bombdr DHC8402 · Fuselage Structure (General)
  > UPPER FUSELAGE OUTER SKIN AT FS X321 TO FS X373 AND STR 12P AND 12S CHAFED.
- [SDR SROM060720221](https://openairdocs.org/sdr/SROM060720221.md): Skin Panel · corroded · Jun 7, 2022 · N792CP · Bombdr DHC8402 · Fuselage Structure (General)
  > UPPER FUSELAGE OUTER SKIN AT FSX69 TO FSX553 AND STR12P TO STR3P CHAFED ALONG WING TO FUSELAGE FAIRING SEAL (AFT LH WING TO FUSE FAIRING).
- [SDR SROM06012022](https://openairdocs.org/sdr/SROM06012022.md): Intercostal · corroded · Jun 1, 2022 · N792CP · Bombdr DHC8402 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON FLOOR PANEL SUPPORT INTERCOSTAL STA. X1.000 AND LBL33. CORROSION OUT OF LIMITS AND REQUIRES AN RD TO SPLICE A REPLACEMENT SECTION.
- [SDR SROM0523202208](https://openairdocs.org/sdr/SROM0523202208.md): Bracket · corroded · May 23, 2022 · N792CP · Bombdr DHC8402 · Fuselage Main, Longeron/Stringer
  > FUSELAGE FRAME FS X216.00, STRINGER Y24P FLOORBOARD BRACKET MOUNT HOLE CORROSION DAMAGE. CORROSION BEYOND MANUFACTURES LIMITS, REPLACEMENT REQUIRED.
- [SDR SROM0523202207](https://openairdocs.org/sdr/SROM0523202207.md): Cleat · corroded · May 23, 2022 · N792CP · Bombdr DHC8402 · Fuselage Main, Longeron/Stringer
  > FUSELAGE FRAME UNDERFLOOR FS X236.00 CORROSION ON BRACKET SURFACE UNDER FASTENER AT STR. 24S, 25S, AND STR. 26S. CORROSION BEYOND MANUFACTURES LIMITS, PART REPLACEMENT REQUIRED.
- [SDR SROM0523202206](https://openairdocs.org/sdr/SROM0523202206.md): Cleat · corroded · May 23, 2022 · N792CP · Bombdr DHC8402 · Fuselage Main, Longeron/Stringer
  > FUSELAGE FRAME FS X 216.00, STR. 24P, CORROSION BETWEEN CLEAT AND STR. 24P. CORROSION BEYOND MANUFACTURES LIMITS, PART REPLACEMENT REQUIRED.
- [SDR SROM0523202205](https://openairdocs.org/sdr/SROM0523202205.md): Cleat · corroded · May 23, 2022 · N792CP · Bombdr DHC8402 · Fuselage Main, Longeron/Stringer
  > FUSELAGE FRAME UNDERFLOOR FS X156.0 STR. 24S CORROSION ON LOWER SURFACE OF BRACKET. CORROSION BEYOND MANUFACTURES LIMITS, REPLACEMENT REQUIRED.
- [SDR SROM0523202203](https://openairdocs.org/sdr/SROM0523202203.md): Cleat · corroded · May 23, 2022 · N792CP · Bombdr DHC8402 · Fuselage Main, Longeron/Stringer
  > FUSELAGE FRAME UNDERFLOOR FS X136.00 STR. 24P CORROSION ON UNDERSIDE OF BRACKET. CORROSION BEYOND MANUFACTURES LIMITS, PART REPLACEMENT REQUIRED.
- [SDR SROM0523202202](https://openairdocs.org/sdr/SROM0523202202.md): Cleat · corroded · May 23, 2022 · N792CP · Bombdr DHC8402 · Fuselage Main, Longeron/Stringer
  > FUSELAGE FRAME UNDERFLOOR FS X236.00, STR. 25P, CORROSION FOUND ON SURFACE OF BRACKET. CORROSION OUT OF MFG. LIMITS, REPLACEMENT REQUIRED.
- [SDR SROM051220223](https://openairdocs.org/sdr/SROM051220223.md): Shear Web · corroded · May 12, 2022 · N792CP · Bombdr DHC8402 · Fuselage Main, Structure
  > BAGGAGE COMPARTMENT AFT SHEAR WEB PN: 85339527-107SP CORRODED AT FS STA. X707 AND LBL 35. THIS CORROSION FALLS OUTSIDE THE ALLOWABLE BLEND AREA OF SRM 53-40-43. REPLACEMENT IS REQUIRED.
- [SDR SROM051220222](https://openairdocs.org/sdr/SROM051220222.md): Shear Web · corroded · May 12, 2022 · N792CP · Bombdr DHC8402 · Fuselage Main, Structure
  > BAGGAGE COMPARTMENT AFT SHEAR WEB PN: 85339627-111 CORRODED AT MULTIPLE SPOTS BETWEEN FS STA. X712 - X788. SRM 53-40-43 ALLOWS SOME BLENDING BUT DOES NOT ALLOW BLENDING AROUND THE RADIUS OF A LIGHTNING HOLE. CORROSION AT STA. X771 IS IN THE STAY-OUT AREA OF
- [SDR SROM05122022](https://openairdocs.org/sdr/SROM05122022.md): Threshold · corroded · May 12, 2022 · N792CP · Bombdr DHC8402 · Passenger/Crew Doors
  > PASSENGER MAIN ENTRANCE DOOR THRESHOLD SUPPORT CHANNEL PN: 85329540-001 CORRODED ON UPPER AND LOWER SURFACE. SRM 53-20-23-02-01 ONLY ALLOWS BLENDING OF THE UPPER SURFACE, REPLACEMENT REQUIRED.
- [SDR SROM042722](https://openairdocs.org/sdr/SROM042722.md): None · corroded · Apr 27, 2022 · N792CP · Bombdr DHC8402 · Fuselage Main, Floor Beam
  > LH AFT SEAT FLOOR RAIL P/N: 85338210-111 CORRODED AT AFT TIE DOWN RING IN AFT BAGGAGE COMPARTMENT. MEASURED AT 0.060" BEFORE BLENDING AND LIMIT IS 0.040" PER SRM 53-40-49. NEW REPLACEMENT FLOOR RAIL WILL BE INSTALLED.
- [SDR SROM03022022](https://openairdocs.org/sdr/SROM03022022.md): Power Supply · failed · Mar 2, 2022 · N792CP · Bombdr DHC8402 · Emergency Lighting
  > LEFT AFT PAX DOOR EMERGENCY EXIT SIGN INOP. CORRECTION: REPLACED EMERGENCY LIGHTS POWER SUPPLY IAW Q400 AMM 33-51-01-400-801. OPERATIONAL CHECK GOOD.
- [SDR SROM020200718201](https://openairdocs.org/sdr/SROM020200718201.md): I/O Module · malfunctioned · Jul 16, 2020 · N792CP · Bombdr DHC8402 · Overheat Detection
  > RIGHT FUEL TANK TEMP INDICATED +99°C WITH FIRE BELL. REMOVED AND REPLACED THE RT FUEL HEATER THERMAL ACTUATOR INAW DHC-8-400 AMM 73-11-05 (FOR THE FUEL OVERHEAT). SWAPPED INPUT/OUTPUT MODULE (IOM) POSITIONS IAW Q400 AMM 31-41-11 (FOR TROUBLE SHOOTING THE F

## 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 = 'N792CP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N792CP/reports

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