N794CP
Service difficulty reports · 35
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 = 'N794CP' 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SROM20260402002Spinner · wornUPON 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 FASDR SROM202404160001Ditching Dam · stiffDITCHING 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 SROM202312220001Wire Harness · misroutedPILOT 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 CRSDR SROM2023100200023Unknown · crackedCRACK DAMAGE TO UPPER CHANNEL OF RH WING TO FUSELAGE (ARMPIT) FAIRING SUPPORT STRUCTURE AT STA X400 AND Z173.0.SDR SROM20221130001Selector Valve · stuckMANUAL 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 HSDR SROM110220223None · chafedCHAFING DAMAGE ON RH INBOARD FLAP, OUTBOARD WING TANK CAN (P/N 85714630-004. DAMAGE IS BEYOND MANUFACTURES LIMITS; PART REQUIRES REPLACEMENT.SDR SROM110220222None · crackedLH NACELLE EXHAUST SHROUD SPRING CLIPS CRACKED AT 2 LOCATIONS (P/N 8Z9029-103). CRACKS ARE OUTSIDE OF MANUFACTURES LIMITS REQUIRING PART REPLACEMENT.SDR SROM110220221Stringer Fitting · corrodedSTRINGER FITTING WITH CORROSION DAMAGE AND HOLE ELONGATION BEYOND MANUFACTURES PUBLISHED LIMITS.SDR SROM2022101002Frame · corrodedCORROSION 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 SROM101020221Intercostal · corrodedCORROSION DAMAGE ON STRINGER INTERCOSTAL AT STATION X100.800 - X116.00 STRINGER 24S. DAMAGE BEYOND MANUFACTURES PUBLISHED LIMITS.SDR SROM09272022Door Frame · damagedSCORING DAMAGE O THE FORWARD BAGGAGE DOOR AFT FRAME THAT IS BEYOND MANUFACTURES LIMITATIONS.SDR SROM091801Support · corrodedCORROSION 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 SROM0918202202None · corrodedCORROSION DAMAGE BEYOND MANUFACTURER’S PUBLISHED LIMITS. CORROSION DAMAGE ON FUSELAGE FRAME UPPER WEB AND CAP. PN: 85329152-103(LH) AND 85329256-101(RH).SDR SROM091220223None · corrodedGOUGE DAMAGE PAST MANUFACTURER LIMITS ON LOWER RH FUSELAGE SKIN PN 85337133-109.SDR SROM0912202202None · corrodedCORROSION DAMAGE BEYOND MANUFACTURES PUBLISHED LIMITS. RH LOWER FRAME AND SILL.SDR SROM020201300020Floor Support · corrodedREFERENCE 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 SROM2020120020Stringer Splice · corrodedREFERENCE 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 SROM202001302005Fuel Line · out of positionFUEL 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 SROM20200130205Mount Fitting · crackedCRACKED 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 SROM20200130204Bracket · crackedREFERENCE 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 SROM202001302003Structure · corrodedCORROSION 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 SROM202001302002Stringer Clip · corrodedSTRINGER 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 SROM202001302001Bracket · corrodedREFERENCE 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 SROM2020013020Bracket · crackedREPLACE 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 SROM202001292004Support · corrodedCORROSION 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. 19SDR SROM20200129203Scuff Plate · corrodedFWD 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 SROM20200129003Fitting · corrodedEXFOLIATION 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 SROM20200129002Scuff Plate · corrodedCORROSION 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 SROM20200128001Support · corrodedCORROSION 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 SROM2020012620Seat Track · corrodedSEAT 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 SROM2019121305Stiffener · crackedCRACKS 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 SROM2019121241644Seat Track · corrodedLIGHT 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 SROM2019121241643Scuff Plate · corrodedCORROSION UNDER DOOR SCUFF PLATE L2 DOOR STA. 697.600 STR. 23 ON MULTIPLE FASTENENR HOLES. CORROSION BEYOND SRM LIMITS, REPLACEMENT REQUIRED.SDR SROM2019121146402Angle · corrodedCORROSION ON FLOOR STRUCTURE STA 783 LBL 20 AFT CARGO PIT. PART REPLACEMENT REQUIRED.SDR SROM201912114164Stiffener · crackedCRACKS ON STIFFENERS EXTENDING FROM END FASTENERS ON FUSELAGE TO BODY ACESS PANEL 262HT.
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