# Service difficulty reports: N794CP

A list on [N794CP](https://openairdocs.org/aircraft/N794CP.md).

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

- [SDR SROM20260402002](https://openairdocs.org/sdr/SROM20260402002.md): Spinner · worn · Apr 2, 2026 · N794CP · Bombdr DHC8402 · Propeller Spinner Section
  > UPON APPROACH INTO PAKU IT WAS IDENTIFIED BY THE FLIGHT MECHANIC ONBOARD THAT THE NR 2 SPINNER SEEMED OFF OF CENTER AND HAD MORE MOVEMENT DURING ROTATION THAN TYPICAL. AFTER LANDING THE MECH INVESTIGATED FURTHER & FOUND WHAT APPEARED TO BE LOOSE SLEEVE NUT FA
- [SDR SROM202404160001](https://openairdocs.org/sdr/SROM202404160001.md): Ditching Dam · stiff · Apr 16, 2024 · N794CP · Bombdr DHC8402 · Cabin Equipment/Furnishings
  > DITCHING DAM AT FORWARD PASSENGER DOOR IS DIFFICULT TO DEPLOY. AFT EDGE OF DAM CATCHES ON OVERHEAD BIN. ADJUSTED END CAP OF OVERHEAD BIN BEHIND DITCHING DAM TO CREATE MORE CLEARANCE FOR OPERATION OF DAM. OPS CHECKS GOOD.
- [SDR SROM202312220001](https://openairdocs.org/sdr/SROM202312220001.md): Wire Harness · misrouted · Dec 22, 2023 · N794CP · Bombdr DHC8402 · Fuselage Main, Bulkhead Fuselage wiring
  > PILOT WAS UNABLE TO MAKE LEFT RUDDER INPUT DURING TAXI FOR DEPARTURE. AIRCRAFT RETURNED TO GATE FOR MAINTENANCE. MAINTENANCE PERFORMED INSPECTION OF THE PILOT AND COPILOT'S RUDDER CONTROL CABLES/HARDWARE. FOUND COPILOTS LH RUDDER PEDAL PUSH RODS AND BELL CR
- [SDR SROM2023100200023](https://openairdocs.org/sdr/SROM2023100200023.md): Unknown · cracked · Oct 2, 2023 · N794CP · Bombdr DHC8402 · Fuselage Structure (General)
  > CRACK DAMAGE TO UPPER CHANNEL OF RH WING TO FUSELAGE (ARMPIT) FAIRING SUPPORT STRUCTURE AT STA X400 AND Z173.0.
- [SDR SROM20221130001](https://openairdocs.org/sdr/SROM20221130001.md): Selector Valve · stuck · Nov 30, 2022 · N794CP · Bombdr DHC8402 · Landing Gear Retraction/Extension System
  > MANUAL GEAR EXTENSION DOOR WILL NOT FULLY OPEN. CLEANED AND LUBRICATED EXPOSED SURFACE OF THE SELECTOR VALVE. OPS CHECKS GOOD. NOTE THE OAT WHEN THIS HAPPED WAS 6 DEGREES FAHRENHEIT, SO COULD ALSO BE COLD RELATED SINCE THE AIRCRAFT WAS MOVED INTO A HEATED H
- [SDR SROM110220223](https://openairdocs.org/sdr/SROM110220223.md): None · chafed · Nov 2, 2022 · N794CP · Bombdr DHC8402 · Wing, Center Box
  > CHAFING DAMAGE ON RH INBOARD FLAP, OUTBOARD WING TANK CAN (P/N 85714630-004. DAMAGE IS BEYOND MANUFACTURES LIMITS; PART REQUIRES REPLACEMENT.
- [SDR SROM110220222](https://openairdocs.org/sdr/SROM110220222.md): None · cracked · Nov 2, 2022 · N794CP · Bombdr DHC8402 · Engine Exhaust System
  > LH NACELLE EXHAUST SHROUD SPRING CLIPS CRACKED AT 2 LOCATIONS (P/N 8Z9029-103). CRACKS ARE OUTSIDE OF MANUFACTURES LIMITS REQUIRING PART REPLACEMENT.
- [SDR SROM110220221](https://openairdocs.org/sdr/SROM110220221.md): Stringer Fitting · corroded · Nov 2, 2022 · N794CP · Bombdr DHC8402 · Fuselage Main, Structure
  > STRINGER FITTING WITH CORROSION DAMAGE AND HOLE ELONGATION BEYOND MANUFACTURES PUBLISHED LIMITS.
- [SDR SROM2022101002](https://openairdocs.org/sdr/SROM2022101002.md): Frame · corroded · Oct 10, 2022 · N794CP · Bombdr DHC8402 · Fuselage Main, Frame
  > CORROSION DAMAGE ON FUSELAGE FRAME UPPER WEB AND CAP. DAMAGE IS BEYOND MANUFACTURES PUBLISHED LIMITS. DAMAGE AT STA. X32.400 STRINGERS 30P AND 30S. PART NUMBERS ARE 85329152-103 (LH) / 85329256-101 (RH)
- [SDR SROM101020221](https://openairdocs.org/sdr/SROM101020221.md): Intercostal · corroded · Oct 10, 2022 · N794CP · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > CORROSION DAMAGE ON STRINGER INTERCOSTAL AT STATION X100.800 - X116.00 STRINGER 24S. DAMAGE BEYOND MANUFACTURES PUBLISHED LIMITS.
- [SDR SROM09272022](https://openairdocs.org/sdr/SROM09272022.md): Door Frame · damaged · Sep 27, 2022 · N794CP · Bombdr DHC8402 · Cargo/Baggage Doors
  > SCORING DAMAGE O THE FORWARD BAGGAGE DOOR AFT FRAME THAT IS BEYOND MANUFACTURES LIMITATIONS.
- [SDR SROM091801](https://openairdocs.org/sdr/SROM091801.md): Support · corroded · Sep 20, 2022 · N794CP · Bombdr DHC8402 · Fuselage Structure (General)
  > CORROSION DAMAGE BEYOND MANUFACTURES PUBLISHED LIMITS. CORROSION ON FORWARD WARDROBE SUPPORT STRUCTURE. 11.4" AFT OF STA. -18.250 AND 2.85" FORWARD OF STA. 1.0.
- [SDR SROM0918202202](https://openairdocs.org/sdr/SROM0918202202.md): None · corroded · Sep 19, 2022 · N794CP · Bombdr DHC8402 · Fuselage Structure (General)
  > CORROSION DAMAGE BEYOND MANUFACTURER’S PUBLISHED LIMITS. CORROSION DAMAGE ON FUSELAGE FRAME UPPER WEB AND CAP. PN: 85329152-103(LH) AND 85329256-101(RH).
- [SDR SROM091220223](https://openairdocs.org/sdr/SROM091220223.md): None · corroded · Sep 12, 2022 · N794CP · Bombdr DHC8402 · Fuselage Structure (General)
  > GOUGE DAMAGE PAST MANUFACTURER LIMITS ON LOWER RH FUSELAGE SKIN PN 85337133-109.
- [SDR SROM0912202202](https://openairdocs.org/sdr/SROM0912202202.md): None · corroded · Sep 12, 2022 · N794CP · Bombdr DHC8402 · Fuselage Main, Frame
  > CORROSION DAMAGE BEYOND MANUFACTURES PUBLISHED LIMITS. RH LOWER FRAME AND SILL.
- [SDR SROM020201300020](https://openairdocs.org/sdr/SROM020201300020.md): Floor Support · corroded · Feb 13, 2020 · N794CP · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > REFERENCE KF AERO WO. 1000072826. FLOOR RAIL AT STA. X-39.00 TO 10.5 STR. 23 RBL 8 CORRODED BEYOND LIMITS. FLOOR RAIL WAS REPLACED WITH NEW PURCHASED PART IAW Q400 SRM 53-20-49 REV. 19. FLOOR RAIL P/N 85328210-121.
- [SDR SROM2020120020](https://openairdocs.org/sdr/SROM2020120020.md): Stringer Splice · corroded · Feb 12, 2020 · N794CP · Bombdr DHC8402 · Fuselage Main, Longeron/Stringer
  > REFERENCE KF AERO WO. 1000074504. STRINGER SPLICE AT STA. X32 – X47 LH STR. 31 IS CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED NEW STRINGER SPLICE IAW DHC-8-400 SRM 51-42-05 REV. 19.
- [SDR SROM202001302005](https://openairdocs.org/sdr/SROM202001302005.md): Fuel Line · out of position · Jan 30, 2020 · N794CP · Bombdr DHC8402 · Aircraft Fuel Distribution System
  > FUEL PIPE TOO CLOSE TO STRUCTURE AT 2 PLACES, LT YW 8.68 AND 25.265 IAW AMM PART 2, PSM 1-84-2 SECTION, 28-10-00-280-811, SUBTASK 28-10-00-210-019 (B). FUEL LINE ADJUSTED CLAMPS TO ALLOW FOR PROPER CLEARANCE IAW Q400 AMM 28-11-06 REV. 67.
- [SDR SROM20200130205](https://openairdocs.org/sdr/SROM20200130205.md): Mount Fitting · cracked · Jan 30, 2020 · N794CP · Bombdr DHC8402 · Passenger/Crew Doors
  > CRACKED DOOR SHELL MOUNT FITTING ON L1 DOOR STAIRS. FITTING REPLACED WITH NEW IAW SRM 51-10-00, PARAGRAPH 2, SECTION 3, REV 19, AND SRM 51-41-05.
- [SDR SROM20200130204](https://openairdocs.org/sdr/SROM20200130204.md): Bracket · cracked · Jan 30, 2020 · N794CP · Bombdr DHC8402 · Nacelle/Pylon Structure
  > REFERENCE WO. 1000078407. REPLACED BROKEN/CRACKED RH PYLON BRACKET FORWARD OF O/B LUG FITTING IN ACCORDANCE WITH DHC-8-400 SRM 51-10-00 PARAGRAPH 2 SECTION 3 REV. 19 AND SRM 51-42-05-02-01 REV. 19 PART REPLACED WITH NEW BRACKET PART NUMBER 82454318-102.
- [SDR SROM202001302003](https://openairdocs.org/sdr/SROM202001302003.md): Structure · corroded · Jan 30, 2020 · N794CP · Bombdr DHC8402 · Fuselage Main, Structure
  > CORROSION ON Z SECTION AT STA. X32 LBL 38 UNDER FLOOR US BEYOND LIMITS. Z SECTION REPLACED WITH MANUFACTURED PART IAW DHC-8-400 SRM 53-20-43, ITEM 211, AND 51-24-35 REV. 19. INSTALLED Z SECTION FOLLOWING SRM REV. 19 SECTION 51-42-05.
- [SDR SROM202001302002](https://openairdocs.org/sdr/SROM202001302002.md): Stringer Clip · corroded · Jan 30, 2020 · N794CP · Bombdr DHC8402 · Fuselage Main, Attach Fittings
  > STRINGER CLIP AT BS 47 STRINGER 30L BELOW FLOOR WAS CORRODED. THE STRINGER CLIP WAS REPLACED IAW SRM 51-10-00-00-01, SECTION 2, SUB SECTION 3, RE. 19.
- [SDR SROM202001302001](https://openairdocs.org/sdr/SROM202001302001.md): Bracket · corroded · Jan 30, 2020 · N794CP · Bombdr DHC8402 · Passenger/Crew Doors
  > REFERENCE WO. 1000076529. CORRODED MOUNT BRACKET REQUIRES REPLACEMENT AT FORWARD SIDE OF STAIRS L1 DOOR. BRACKET PN: 85217097-101 REPLACED IAW DHC-8-400 SRM 51-10-00 PARAGRAPH 2 SECTION 3 REV. 19 AND SRM 51-41-05.
- [SDR SROM2020013020](https://openairdocs.org/sdr/SROM2020013020.md): Bracket · cracked · Jan 30, 2020 · N794CP · Bombdr DHC8402 · Nacelle/Pylon Miscellaneous Structure
  > REPLACE BROKEN AND CRACKED LT PYLON BRACKET FWD OF O/B LUG FITTING YW STA. 155.20. REPLACED WITH NEW IAW DRAWING NO. 85404001 REV. A AND SRM 51-42-05 REV. 19.
- [SDR SROM202001292004](https://openairdocs.org/sdr/SROM202001292004.md): Support · corroded · Jan 29, 2020 · N794CP · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > CORROSION BEYOND ALLOWABLE LIMITS ON AFT CARGO SILL PIECE CONNTECTED TO AFT 1 FRAME STA. X783.102 STR. 24. FABRICATED AND INSTALLED REPLACMENT PART FOLLOWING Q400 SRM 51-15-00 PARA B. REV. 19
- [SDR SROM20200129203](https://openairdocs.org/sdr/SROM20200129203.md): Scuff Plate · corroded · Jan 29, 2020 · N794CP · Bombdr DHC8402 · Cargo/Baggage Doors
  > FWD BAGGAGE DOOR HAS CORROSION IN SILL AREA THAT IS BEYOND MANUFACTURES LIMITS. FABRICATED AND INSTALLED REPLACEMENT PART AT STA. 32 - 41 RH SIDE FOLLOWING BOMBARDIER DRAWING #85329381 REV. C.
- [SDR SROM20200129003](https://openairdocs.org/sdr/SROM20200129003.md): Fitting · corroded · Jan 29, 2020 · N794CP · Bombdr DHC8402 · Fuselage Main, Attach Fittings
  > EXFOLIATION CORROSION ON FWD LAV FLOOR AT DOOR ENTRYWAY (SILL PLATE FLOOR FITTING). REPLACED EXTRUSION ON FLOOR AT DOOR ENTRYWAY. PART NUMBER 9701029-5. WORK ACCOMPLISHED IAW Q400 SRM 51-41-00 REV. 19.
- [SDR SROM20200129002](https://openairdocs.org/sdr/SROM20200129002.md): Scuff Plate · corroded · Jan 29, 2020 · N794CP · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > CORROSION UNDER DOOR SCUFF PLATE L2 DOOR STA. 697.600 STR. 23. REMOVED CORROSION AND REMAINING THISCKNESS IS BEYOND LIMITS IN SRM. SCUFF PLATE REPALACED WITH NEW MANUFACTURED PN: 85339540.
- [SDR SROM20200128001](https://openairdocs.org/sdr/SROM20200128001.md): Support · corroded · Jan 28, 2020 · N794CP · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON FLOOR STRUCTURE BS 783, LBL 20, IN THE AFT CARGO BAY, WAS FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM. INSTALLED NEW PARTS IAW SRM REV. 19 51-41-00-00-01 AND 51-42-02-01.
- [SDR SROM2020012620](https://openairdocs.org/sdr/SROM2020012620.md): Seat Track · corroded · Jan 26, 2020 · N794CP · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK IN THE MAIN CABIN BS 216 +10 - 584.5 +10, LBL 9.25 WAS FOUND CORRODED OUT OF SRM LIMITS. REPAIRED IAW SRM 51-40-10, 51-40-15, AND 51-42-05, REV. 19.
- [SDR SROM2019121305](https://openairdocs.org/sdr/SROM2019121305.md): Stiffener · cracked · Dec 13, 2019 · N794CP · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > CRACKS ON STIFFENERS (X3) ON BODY ACCESS PANEL #262AT. REPLACED WITH NEW FABRICATED PARTS IAW Q400 SRM 51-42-05 AND 51-24-35 REV. 19 AND DHC DWG. # 85357339 REV. A.
- [SDR SROM2019121241644](https://openairdocs.org/sdr/SROM2019121241644.md): Seat Track · corroded · Dec 12, 2019 · N794CP · Bombdr DHC8402 · Fuselage, Seat/Cargo Attach Fittings
  > LIGHT CORROSION ON SEAT TRACK RAIL (FLOOR RAIL) FS 10.5 TO FS 102.5 RBL 9.25. FOUND CORROSION BEYOND LIMITS IAW Q400 SRM. REPLACED FLOOR RAIL WITH NEW PART.
- [SDR SROM2019121241643](https://openairdocs.org/sdr/SROM2019121241643.md): Scuff Plate · corroded · Dec 12, 2019 · N794CP · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > CORROSION UNDER DOOR SCUFF PLATE L2 DOOR STA. 697.600 STR. 23 ON MULTIPLE FASTENENR HOLES. CORROSION BEYOND SRM LIMITS, REPLACEMENT REQUIRED.
- [SDR SROM2019121146402](https://openairdocs.org/sdr/SROM2019121146402.md): Angle · corroded · Dec 11, 2019 · N794CP · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR STRUCTURE STA 783 LBL 20 AFT CARGO PIT. PART REPLACEMENT REQUIRED.
- [SDR SROM201912114164](https://openairdocs.org/sdr/SROM201912114164.md): Stiffener · cracked · Dec 11, 2019 · N794CP · Bombdr DHC8402 · Fuselage Miscellaneous Structure
  > CRACKS ON STIFFENERS EXTENDING FROM END FASTENERS ON FUSELAGE TO BODY ACESS PANEL 262HT.

## 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 = 'N794CP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N794CP/reports

---
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