N803DH
Service difficulty reports · 573
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 = 'N803DH' 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 = 'N803DH' 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 DHL2001803548Skin · damagedLT WING L/E SKIN EXHAUST GATE BROKEN APPROX 1.5 INCH. REMOVED DAMAGED SKIN PER SRM 51-1-21 PG 1. FABRICATED SKIN (2024-T3 0.032) PER SRM 57-2-1 FIG 1. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED NEW SKIN PER SRM 51-1-21 PG 1.SDR DHL2001803503Rib · brokenAT C CK; LH WING-CLOSING RIB BROKEN ON INBOARD AILERON RH LATERAL PART. REMOVED FASTNERS IAW SRM 51-1-21A, PG 1, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-1, PAR. 1, SRM 51-1-21A, PG 1. REF: N/R 0616. SDR CLSDR DHL2001803502Angle · crackedAT C CK; FWD CARGO COMPT.- RH SHROUD ANGLE WITH 1/2" CRACK ON DOOR. REMOVED CRACKED ANGLE IAW SRM 51-1-21 PG 1, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-1-21, PG 1. REF. N/R 1362. SDR CLOSED.SDR DHL2001803546Keelbeam · crackedRT MAIN LANDING GEAR WHEEL WELL KEEL BEAM INNER RIB SHOWS 1 INCH CRACK AT STA 920.SDR DHL2001803509Skin · crackedFUSELAGE EXTERNAL SKIN SHOWS CRACK (0.500 IN LENGTH) AT STA -13.000, L-1DR. CUT OUT DAMAGED SKIN PER SRM 53-2-1 FIG 7 SHEET 4.5. INSTALLED FILLER AND DOUBLER AND NEW FASTENERS PER SRM 51-20-20D PG 9.SDR DHL2001803507Structure · crackedTAIL CONE-RT ELEVATOR BRUSH COVER INNER STRUCTURE CRACKED 1.25. PERFORMED STOP HOLE PER SRM 53-2-0 FIG 1B. FABRICATED DOUBLER WITH ALCLAD (2420T3 0.025) PER SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED PER SRM 51-1-8, INSTALLED DOUBLER PER SRM 53-20 FIG 1SDR DHL2001803506Cover · crackedAT C CK; RH HORIZONTAL STAB. CLOSING REAR SPAR COVER SHOWS 2", 1 1/2",2" AND 1" CRACKS FROM STA. XRS 179 TO XRS 221. REMOVED DAMAGED COVER IAW SRM 55-2-0 FIG 6, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, INSTALLED NEW COVER IAW SRM 55-2-0 FIG 6. REF: N/RSDR DHL2001803504Doubler · corrodedAT C CK; COCKPIT- FINGER DOUBLER SHOWS CORROSION STA. 8.000 THRU STA. 20.000, LBL 60, L-22L. REMOVED FASTNERS IAW SRM 51-1-21, PG 7, REMOVED CORROSION AT FINGER DOUBLER IAW SRM 51-1-8, PG 17-18, FOUND OUT OF LIMITS IAW SRM 53-2-0, PG 2, CLEANED,TREATED AND PRISDR DHL2001803505Door · crackedAT C CK; FWD CARGO COMPT.-AFT DOOR FWD UPPER CORNER CRACKED 1/4" AT STA. 520.000. CUTOUT DAMAGED AREA IAW SRM 53-2-0, FIG 20, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 53-2-0, FIG 20, PG 141 & SRM 51-1SDR DHL2001803547Seat Track · wornMAIN CARGO COMPT - LUGS WORN ON CENTRAL TRACK AT STA 163.00 TO STA 62.000.REMOVED DAMAGED CTR TRACK (STA 62-163)PER SRM 51-3-0 PG 1.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW TRACK PER SRM 57-3-0 PG 1 AND 51-3-1 PG 1SDR DHL2001803530Angle · brokenFWD CARGO COMPT- LINING SUPPORT ANGLE BROKEN AT STA 440, L-27L.SDR DHL2001803527Angle · crackedFWD CARGO COMPT - LINING SUPPORT ANGLE CRACKED (.25 INCH) AT STA 600, L-31L.SDR DHL2001803526Angle · crackedFWD CARGO COMPT- LINING SUPPORT ANGLE CRACKED 1 INCH AT STA 620, L-31R.SDR DHL2001803525Floor Support · crackedFWD CARGO COMPT- FLOOR SUPPORT ANGLE CRACKED 1.5 INCH AT STA 580, L-34R.SDR DHL2001803521Angle · crackedFWD CARGO LINING SUPPORT ANGLE SHOWS 2 EA 1.5 IN CRACKS BETWEEN L-33 TO L34 RT STA 480.000.SDR DHL2001803518Angle · crackedFWD CARGO COMPT-LINING SUPPORT ANGLE CRACKED (3/4 IN) AT STA 360.000 L-33L.SDR DHL2001803517Angle · crackedFWD CARGO COMPT LINING SUPPORT ANGLE CRACKED (1/2 IN) AT STA 100.00 L-31L.SDR DHL2001803516Floor Support · crackedFWD CARGO COMPT, FLOOR SUPPORT ANGLE CRACKED (O/B) 1.5 IN AT STA 560.00 L-35L TO L-35R.SDR DHL2001803515Floor Support · crackedFWD CARGO COMPT-FLOOR SUPPORT ANGLE CRACKED 1 IN AT STA 500.000 L-34W.SDR DHL2001803514Angle · crackedFWD CARGO COMPT LINING SUPPORT ANGLE CRACKED .375 IN AT STA 620.000 L-29R.SDR DHL2001803513Floor Support · crackedFWD CARGO COMPT FLOOR SUPPORT ANGLE CRACKED (1/4 IN) AT STA 5000.000.SDR DHL2001803512Angle · crackedFWD CARGO COMPT LINING SUPPORT ANGLE CRACKED .25 IN AT STA 460.000, L31L.SDR DHL2001803511Angle · crackedFWD CARGO COMPT LINING SUPPORT ANGLE CRACKED .25 IN AT STA 460.000, L31L.SDR DHL2001803529Angle · crackedFWD CARGO COMPT- LINING SUPPORT ANGLE CRACKED (.5 INCH) AT STA 460, L-29L.SDR DHL2001803528Angle · crackedFWD CARGO COMPT- LINING SUPPORT ANGLE CRACKED (1.5 INCH) AT STA 460, L-31R.SDR DHL2001803524Angle · crackedFWD CARGO COMPT- LINING SUPPORT ANGLE CRACKED 1.5 IN AT STA 600, L31R.SDR DHL2001803523Seat Track · wornMAIN CARGO COMPT - LUGS WORN ON L/H # 1 TRACK AT STA 1570-1710.CUR OUT DAMAGED TRACK AT MAIN CARGO COMPT, STA 1530.000 - 1710.000 PER SRM 53-2-3 PG 1&2.CLEANED , TREATED AND PRIMED AREA PER SRN 51-1-8B.INSTALLED NEW TRACK PER SRM 53-2-3 PG 1 & 2SDR DHL2001803522Angle · crackedFWD CARGO LINING SUPPORT ANGLE WITH .5 IN CRACK AT L 32 LT AT STA 80.000.SDR DHL2001803510Angle · crackedFWD CARGO LINING SUPPORT ANGLE SHOWS .25 IN CRACK L-31 RT STA 480.000.SDR DHL2001803531Angle · crackedRT FUSELAGE WALL EXT VERTICAL ANGLE SHOWS .5 INCH CRACK AT STA 980.SDR DHL2001803519Fitting · crackedRT MLG TRAPEZOIDAL LWR END, STOP DRILLED CRACK (6.125 IN ) CONTINUES .5 IN BEYOND STOP DRILL AT STA 896.12. STOP DRILLED CRACK (.375 DIA), INSPECTED WITH NDT, CRACK DOES NOT CONTINUE PER SEQ-LIM 0100070H 06-20-01.SDR DHL2001803508Skin · dentedVERTICAL STABILIZER L/E SHOWS 3.52 IN DENT AT ZFS 123.500. CUT OUT DAMAGED AREA PER SRM 55-2-1 PG 17. FABRICATED FILLER (ALCLAD 7075 T6,0.050) PER SRM 55-2-1. FABRICATED DOUBLER (ALCLAD 7075-T6 0.050) PER SRM 55-2-1 PG 17. CLEANED, TREATED AND PRIMED PER SSDR DHL2001803520Angle · crackedFWD CARGO COMPT - LINING SUPPORT ANGLE CRACKED (.25 IN) AT STA 400.00 L-31L.SDR DHL2001803536Fairing · crackedAT C-CK, RT WING TO FUSELAGE UPPER FAIRING SHOWS 1 INCH BREAK AT STA 834.SDR DHL2001803535Skin · crackedAT C-CK, NR 2 ENGINE - RT THRUST REVERSER INTERNAL SKIN CRACKED 2 INCHES AT 3 O'CLOCK POSITION.SDR DHL2001803532Skin · crackedAT C-CK, ENGINE NR 3 HAD 1.5 INCH CRACK ON EXTERNAL SKIN OF TRANSLATING COWL LT (UPPER BORDER) AT 11 O'CLOCK.SDR DHL2001803534Angle · crackedAT C CK, RT WING - WING TO FUSELAGE FILLET SUPPORT ANGLE CRACKED (2 INCHES) AT XW 908-XCW 69.5.SDR DHL2001803533Doubler · brokenAT C-CK, RT WING- EXT PATCH ON OUTBOARD FLAP UPPER SKIN NEAR STA XW 219.00 SHOWS .3125 INCH BREAK APPROX.SDR DHL2001803537Radome · crackedAT C-CK, RADOME- 2 (EA) .25 INCH CRACKS ON RADOME LOWER LIP (INNER PART). PERFORMED STOP HOLE IAW SRM 53-2-0 FIG 1B, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B.SDR DHL2001803006Plug · unsecureNR 2 ENG FIRE WARNING. BOTH A & B LOOP. EMERGENCY CHECKLIST RUN - AFT FIRE BOTTLE DISCHARGED. FOUND COMBUSTER BORESCOPE PLUGS, 1 AND 3 O'CLOCK, IMPROPERLY SECURED. RESECURED 2 BORESCOPE PLUGS PER CFM M/M 72-42-00. PERFORMED VISUAL INSPECTION OF ENGINE ANDSDR DHL2001803005Indicator · faultyAUTOPILOT WHEN IN HEADING SELECT MODE DIVERGES IN ROLL. FOUND ON STEP 7A & 7B AT ROLL COMPUTER BITE CHECK, MM 22-12-0 PG 101-107, FAILED FULL SCALE RIGHT STOP WHEN SELECTING CAPT''S NAVIGATION INFO VIA NAV SELECT BUTTON. AUTOPILOT CONTROL PANEL ROLL COMPUTER BSDR DHL2001803004Control Unit · malfunctionedRUDDER CONTROL CHECK DID NOT HAVE INDICATION ON HYD SYS GAUGE. INSPECTED AND OPS CHECK RUDDER HYD SYS PER MM 27-21-6. NO DEFECTS NOTED. INSPECTED FLAP PRESS REDUCER VALVE AND LINKAGE PER MM 27-21-7. NO DEFECTS NOTED. PERFORMED RUDDER CONTROL CHECK AND OBSSDR DHL2001803003Powerpack · lack of lubeDURING CONTROL CHECK, NO DROP IN PRESSURE WHEN RUDDER WAS CHECKED. INSPECTED AND LUBED RUDDER POWER PACK. SYSTEM OPS CHECKS NORMAL PER MM 27-21-6.SDR DHL2001803001Wire · brokenF/O HEADSET JACK INOP ON TAXI OUT. REPAIRED BROKEN WIRE AT F/O CONSOLE. OPS OK PER M/M 23-40-0.SDR DHL2001803002Control Box · malfunctionedNOSE WHEEL STEERING UNRESPONSIVE DURING START OF TAKEOFF ROLL. REJECTED T/O. INSPECTED NOSE AND MAIN GEAR, NO DISCREPANCIES FOUND. OPERATED NOSE WHEEL STEERING, OPS CHECKS OK IAW 32-50-0. SUSPECT RUNWAY CONDITIONS. A/C OK FOR SERVICE.SDR DHL2001803140Tab · out of rigNO NOSE DOWN PITCH AT 80 KNOT ELEVATOR CHECK. FOUND ELEVATOR TABS OUT OF RIG. ADJUSTED ELEVATOR CONTROL TABS PER M/M 27-30-0. PRFORMED ACCEPTANCE FLT.SDR DHL2000803139Fuse · unserviceableNO SPOILER PRESS DURING TAXI OUT RAN ALT PROCEDURE BUT NO CHANGE.R&R SPOILER PUMP CURRENT LIMITER OPS NORMAL PER M/M 27-62-00.SDR DHLA200072201Static Wick · failedCOM NR 1 & 2 WEAK AND HAS CONSIDERABLE STATIC IN PRECIPITATION AND SQUEALS. LOST COMS FOR UP TO 1 MINUTE SEVERAL TIMES. REPLACED SEVERAL STATIC WICKS ON WINGS AND HORIZONTAL STAB. SYSTEMS OPS CHECKED GOOD IAW MM 23-20-0SDR DHL200080301Engine · failedAT FLT LEVEL 390 AT LEVEL OFF, NR 3 ENG FAILED, LESS THAN 2 MINS LATER NR 4 ENG FAILED. ALL ENG PARAMETERS PRIOR TO ENG FAIL WERE NORMAL. ENG''S RESTARTED BELOW F/L 220 AND PERFORMED NORMALLY. REMOVED AND REPLACED FUEL FILTERS ON ENG 3 AND 4 AS PRECAUTION, SDR DHL200080373CTrim Tab · delaminatedAT C-CHECK, LT WING I/B AILERON TRIM TAB UPPER SKIN DELAMINATED. REMOVED AND REPLACED TRIM CONTROL TAB IAW MM 27-13-1, OPERATIONAL CHECK GOOD IAW MM 27-10-0. N/R 1007
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