N802DH
Service difficulty reports · 511
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 = 'N802DH' 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 = 'N802DH' 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 DHL9980258CSeat Track · wornC-CHECK, SEAT TRACK NR 4 BETWEEN STA 300-340 TRACK WORN. CUT OUT DAMAGED SECTION OF SEAT TRACK NR 4 BETWEEN STA 310-370 & PREPARED NEW SECTION FROM APPROPIATED MATCHING SECTION OF TRACK & FABRICATED SPLICES FROM 7075-T6 0.100 (1 X 13), 0.125 (1 X 7) 0.160 (1 SDR DHL9980253CSkin · delaminatedC-CHECK, LT WING NR 1 FLAP VANE HAS DELAMINATED AREA DOT 53901. REMOVED NR 1 FLAP VANE FROM I/H WING IAW DC-8 MM 27-51-14. SENT TO STOCKROOM. INSTALLED NR 1 FLAP VANE I/H WING IAW DC-8 M/M 27-51-14 PG 201, 203 PAR 2B. PENDING OPS CHK PERFORMED, OPS CHK NORSDR DHL9980250CPanel · delaminatedC-CHECK, LT WING I/B AREA PANEL BELOW NR 2 SPOILER IS DELAMINATED. REMOVED DELAMINATED PANEL AT LT WING 8/B AREA LOWER SURFACE BELOW SPOILER NR 2 IAW DC-8 SRM 51-1-21 PG F1 P1. SEND DELAMINATED PANEL OUT TO BE REPAIR DRILLED SERVICEABLE PANEL PER DC-8 SRM 51SDR DHL9980249CPanel · crackedC-CHECK, LT WING ABOUT STA 162.263 T/E PANEL BEHIND REAR SPAR HAS A CRACK DOT 382618. STOP DRILLED END CRACK .25 DIAMETER IAW DER NR MHA-312A. FABRICATED DOUBLER REPAIR 7.5 X 9.5 2024T3 .050IAW DER NR MHA 3124. TREATED & PRIMED PER DC-8 SRM 51-1-8 PG 16 & 1SDR DHL9980248CAngle · crackedC-CHECK, ABOUT XCW 46.00 BELOW LT WING IS CRACKED DOT 382627. REMOVED DAMAGED ANGLE AT LT WING XW 46.00 IAW DC-8 SRM 51-1-21 PG 1 PAR 1. FABRICATED NEW ANGLE .071 2024T3 12 X 6 IAW DC-8 SRM 51-1-4 PG 1 PAR 1. TREATED & PRIMED PER DC-8.SDR DHL9980246CAngle · crackedC-CHECK, ABOUT XTS 6.000 BELOW LT WING IS A CRACK SEE MARK DOT 38262. REMOVED CRACKED ANGLE FROM WING ABOUT STA XRS 6.000 IAW DC-8 SRM 51-1-21 PAR 1 FIG 32. FABRICATED NEW ANGLE SAME MATERIAL & THICKNESS 2024-T3 0.050 (20 X 11) IAW DC-8 SRM 57-3-1 FIG 25. SDR DHL9980245CSeat Track · corrodedC-CHECK, SEAT TRACK NR 7 BETWEEN STA 299.200 CORROSION SPUTS ON TRACK. CUT OUT DAMAGED SECTION OF TRACK NR 7 AT STA 273 & CLEANED AREA OF TRACK BETWEEN STA 299-200 IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1 THRU 3, 51-1-8 PAR 6A. TREATED & PRIMED REWORKED AREAS IAW SDR DHL9980244CCowl · crackedC-CHECK, NR 1 ENGINE NOSE COWL L/E INTERIOR AT 10 O'CLOCK POSITION INTERNAL LIP FLANGE IS CRACKED D20EN4. ACCOMPLISHED ENG NR 1 NOSE COWL ANTI-ICE DEFLECTOR REPAIR BY TRIMMING CRACKED SECTION IAW SB 71-105 FIG 2. TREATED AREA OF TRIMMED DEFECTOR PER DC-8 SRMSDR DHL9980243CSeat Track · wornC-CHECK, NONROUTINE SEAT TRACK NR 6 BTWN STA 220-260 TRACK HOLES WORN & SOME ELONGATED. CUT OUT DAMAGED SECTION OF TRACK NR 6 BETWEEN STA 170 TO 310 & PREPARED NEW SECTION FROM APPROPRIATE MATCHING SECTION OF TRACK & FABRICATED SPLICES FROM 7075-T6 0.100 (1 XSDR DHL9980242CSeat Track · wornC-CHECK, BETWEEN STA 1560-1600 SEAT TRACK NR 5 IS WORN. CUT OUT DAMAGES SECTION OF NR 5 SEAT TRACK AT STA 1563 IAW DC-8 SRM 53-2-3 FIG 6D SHEET 1 THRU 3. CLEANED REWORKED AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED REWORKED AREA IAW DC-8 SRM 51-1-8 PG 13, SDR DHL9980241CFrame · crackedC-CHECK, UPPER CARGO COMPT AT STA 1600 CIRCUMFERENTIAL FRAME AT CUSP LINE IS CRACKED RT SIDE. CUT OUT CRACKED SECTION OF FRAME AT FS 1580 RT CARGO CABIN IAW DC-8 SRM 53-2-0 FIG 2. FABRICATED NEW SECTION OF FRAME: 7075-0 0.080' (6 X 2.5) & SPLICE FROM 7075.0 SDR DHL9980240CSeat Track · wornC-CHECK, SEAT TRACK NR 6 BTWN STA 415 - 420 TRACK HOLES WORN. REMOVED (2) DAMAGED, FOUR HOLES CARGO TRACK REPAIR FROM NR 6 SEAT TRACK STA 415-420 IAW DC-8 SRM 51-3-0 PAR 1 & 2. CLEANED REPAIR AREA PER SRM 51-1-8 PAR 6A. TREATED & PRIMED AREA IAW DC-8 SRM 51SDR DHL9980239CFairing · crackedC-CHECK, RT WING FLAP HINGE FAIRING AT STA 340 CRACKED IN 2 PLACES, DOT 450 ON RACK E4. STOP DRILLED END CRACK AT RT WING FLAP HINGE FAIRING IAW DC-8 SRM 51-3-2 PG 1 PAR 1. FABRICATED DOUBLER REPAIR 2024 T3.063 4 X 2.5 IAW DC-8 SR 51-1-4 PG 1 PAR 1. TREATEDSDR DHL9980238CSeat Track · crackedC-CHECK, SEAT TRACK NR 1 BETWEEN STA 1280-1380 TRACK CORRODED. CUT OUT DAMAGED SECTION OF TRACK NR 1 BETWEEN STA 1350 TO 1370 & PREPARED NEW SECTION FROM APPROPRIATED MATCHING SECTION OF TRACK & FABRICATED SPLICES FROM 7075-T6 0.100 (1 X 13), 0.125 (1 X 7), 0SDR DHL9980213CBracket · crackedC-CHECK, BELOW LT WING ABOUT X 46.000 STA 880 BRACKET CRACKED. REMOVED CRACKED BRACKET FROM LT WING AT STA 880 IAW DC-8 SRM 51-1-20D & 51-1-21 PAR 1. FABRICATED NEW BRACKET SAME MATERIAL & THICKNESS 2024-T3 0.0063 DC-8 SRM 53-8-3 FIG 2. CLEANED BRACKET ARESDR DHL9980212CTr Cowl · crackedC-CHECK, NR 1 ENGINE PYLON LT AFT REVERSER COWL UPPER AFT AREA FOUND CRACK ON U-CHANNEL ANGLE. REMOVED CRACKED U-CHANNEL ANGLE AT ENG NR 1 LT AFT REVERSER COWL IAW DC-8 SRM 51-1-21A PG 1 PARA 1. FABRICATED NEW U ANGLE 5.5 X 1.375. 301 STAINLESS .25 HARD 0.20SDR DHL9980210CSpar · crackedC-CHECK, PYLON FAIRED AREA INBOARD NR 1 PYLON FWD SPAR CAP HAD TWO INCHES & PROGRESSING PREVIOIUSLY STOP HOLE. DOT 382844. REMOVED 2 FASTENERS FOR ACCESS TO NDT AT PYLON NR 1 FWD SPAR CAP IAW DC-8 SRM 51-3-0 FIG 52A. REMOVED NR 1 DC-8 SRM 51-1-20 PAR 8 MM 2SDR DHL9980207CFitting · crackedC-CHECK, RUDDER I/E INTERIOR, FITTING CRACKED. MARKED STA ZR 105 DOT 327. STOP DRILLED END CRACK 1/4 PR DC-8 SRM 55-2-0 PAGE 7 FIG 2. FABRICATED ANGLE REPAIR 063 2024T3 7 X 1 1/2 X 1/2 IAW DC-8 SRM 55-2-0. TREATED & PRIMED PER DC8 SRM 51-1-8 PAGE 16 AND 13 SDR DHL9980206CStiffener · crackedC-CHECK, RUDDER L/E INTERTIOR STIFFENER CRACKED, MARKED STA ZR DOT 3211. REMOVED STIFFENER FROM RUDDER L/E INTERIOR AT STA ZR 105 IAW. CLEANED DAMAGED AREA, NO CRACKS FOUND AFTER DYE PENETRANT TEST IAW NDT SPM PART 8. TREATED & PRIMED STIFFENER. OK TO INSTSDR DHL98802002Bolt · shearedON S/O PREFLIGHT, FOUND RT MAIN LANDING GEAR OVER CENTER ARM ATTACH FITTING SHEARED OFF AND MISSING. INSTALLED UNIVERSAL LINK BOLT PER DC-8 MM 32-11-1.SDR DHL98802001Ins · malfunctionedNR 1 INS DISPLAY FLASHING, ALL OTHER FUNCTIONS NORMAL. NR 2 INS DOES NOT RESPOND TO INPUTS. REALIGNED NR 1 AND NR 2 INS.SDR DHL97802009Door · out of adjustBELLY DOOR OPEN LIGHT ILLUMINATED IN FLIGHT. LIGHT WENT OUT WHEN DEPRESSURIZING AIRCRAFT TO CABIN ALT OF 4,500 FEET. REPRESSURIZING, LIGHT CAME BACK ON. RERIGGED DOOR PER M/M 52.SDR DHL97802008Inu · failedNR 1 INS DRIFTED OFF 20 MILES WITHIN 1 HOUR OF DEPARTURE. UPDATED WAS INITIATED WITHIN 5 MIN. BOTH INS BEGAN FLASHING, BOTH ALERT AND WARNING LIGHTS ILLUMINATED, THEN EXTINGUISHED. MALFUNCTION CODES WERE 8010301 AND 0001. REMOVED AND REPLACED NR 1 INU, OPSSDR DHL9780264CSkin · damagedAT C-CHECK, NR 1 ENGINE RT FAN COWLS OUTER SKIN DAMAGED AT LOWER CORNER. TRIMMED DAMAGED AREA AND FABRICATED REPAIR DOUBLER 31.5 X 1 PER DC-8 -70 SRM 71-2-8.SDR DHL9780258CTr Sleeve · wornAT C-CHECK, ENG NR 1 ON RT REV SLEEVE INTERIOR SKIN 30 AFT OF FWD TOP HOLE WORN THROUGH. CUT OUT DAMAGED AREA AND FABRICATED REPAIR PER CFM 56 MM 78-31-10. INSTALLED REPAIR PER SRM 51-1-21A, 3 X 3.SDR DHL9780250CVane · delaminatedAT C-CHECK, RT WING I/B FLAP VANE DELAMINATED. REMOVED VANE, REPAIRED AND REINSTALLED PER M/M 27-51-14.SDR DHL9780248CPanel · delaminatedAT C-CHECK, RIGHT WING LOWER SURFACE STA 130 TO 219 PANEL DELAMINATED. REMOVED, REPAIRED PANEL AND INSTALLED PER SRM 51-1-15.SDR DHL9780211CSkin · delaminatedAT C-CHECK, RT WING LOWER T/E O/B AILERON HINGE PANEL INNER SKIN DELAMINATED. INSTALLED REPAIRED PANEL PER SRM 51-1-15.SDR DHL9780208CSkin · dentedAT C-CHECK, RT WING I/B T/E PANEL AFT OF MLG OUTER SKIN HAS TEMP REPAIR, DENTS AND SKIN SURFACE CORR. REMOVED, REPAIRED AND INSTALLED PANEL PER SRM 56-1-21.SDR DHL9780206CPanel · delaminatedAT C-CHECK, LT WING T/E PANEL BETWEEN XRS 172 AND 255 HAS DELAMINATION AND LOWER SURFACE HAS INTERM REPAIR. REMOVED DAMAGED PANEL, REPAIRED AND INSTALLED PER SRM 51-3-0.SDR DHL9780260CSkin · damagedAT C-CHECK, LEFT WING UPPER T/E PANEL ABOVE AT I/B GROUND SPOILER HOLE. TRIMMED DAMAGED AREA OF SKIN AND FABRICATED REPAIR DOUBLER PER SRM 57-2-1, 7.2 X 5.0.SDR DHL9780247CPanel · delaminatedAT C-CHECK, RT WING T/E LOWER SURFACE DELAMINATED FROM STA 97 TO 130. REMOVED DELAMINATED PANEL AND REPAIRED PER SRM 51-3-0.SDR DHL9780210CWing · dentedAT C-CHECK, LT LOWER T/E PANEL AFT OF MLG HAS HEAVY DENTS THROUGH LOWER SURFACE. REMOVED PANELS AND REPAIRED PER SRM 56-1-21.SDR DHL9780262CBulkhead · crackedAT C-CHECK, MAIN CARGO COMPT REAR PRESSURE BULKHEAD LT AT STA 1760 5 FT ABOVE FLOOR SUPPORT INTERCOSTAL NR 6 FROM BOTTOM TO TOP HAS CRACK APPROX 1 INCH LONG. REMOVED DAMAGED SECTION OF PRESSURE BULKHEAD BY CUTTING AND FABRICATED REPAIR DOUBLER 24 X 13 PER SRSDR DHL9780261CBulkhead Web · crackedAT C-CHECK, MAIN CARGO COMPT REAR PRESSURE BULKHEAD RT AT STA 1760, 5 FT ABOVE FLOOR SUPPORT INTERCOSTAL NR 6 FROM BOTTOM TO TOP OUTBD OF STIFFENER HAS 1 INCH LONG CRACK. REMOVED DAMAGED SECTION OF PRESSURE BULKHEAD WEB, FABRICATED REPAIR DOUBLER 24 X 13 AND SDR DHL9780252CPanel · delaminatedAT C-CHECK, PANEL NR 1621 RIGHT HAND LOWER FUSE HAS DELAMINATION ONE CORNER. REBONDED PER SRM 51-1-19.SDR DHL9780209CPanel · delaminatedAT C-CHECK, RT LOWER T/E ACCESS PANEL 54G EXTERIOR HAS SEVERAL DENTS. REMOVED DAMAGED PANEL, REPAIRED AND INSTALLED PER SRM SRM 51-3-0.SDR DHL9780254CPanel · damagedAT C-CHECK, HORIZ STAB RIGHT HAND ELEVATOR L/E HINGE NR 2 LOWER COVER PANEL DAMAGED. FABRICATED NEW PANEL 12 X 6 PER SRM 55-2-1.SDR DHL9780253CCowl · crackedAT C-CHECK, ENGINE NR 2 NOSE COWL ANTI-ICE DEFLECTOR AT 1 O'CLOCK IS CRACKED. MODIFIED PER S/B 71-97.SDR DHL9780249CBracket · corrodedAT C-CHECK, INTERIOR CABIN, SUBFLOOR BRACKET HAS CORROSION STA 20. REMOVED DAMAGED BRACKET AND FABRICATED NEW BRACKET PER SRM 51-2-0.SDR DHL9780234CSeat Track · chippedAT C-CHECK, FS 500 LINE NR 4 FLOOR TRACK IS CHIPPED AND ELONGATED. REMOVED AND REPLACED TRACK FROM STA 490 TO 530 PER SRM 51-3-0.SDR DHL9780222CSeat Track · wornAT C-CHECK, MAIN CARGO COMPT FS 1300 LINE NR 2 THREE PLUGS IN 15 INCHES OF TRACK. CUT OUT DAMAGED SECTION 1290 TO 1350, FABRICATED REPAIR SPLICES AND NEW TRACK PER SRM 53-2-3.SDR DHL9780212CSkin · damagedAT C-CHECK, RT WING INBD FLAP UPPER SECTION INBOARD SIDE OF ICE BREAKER BADLY DAMAGED. CUT OUT DAMAGED SECTION, FABRICATED REPAIR DOUBLER, INSTALLED PER SRM 57-2-1, 5.2 X 24.4.SDR DHL9780265CBracket · crackedAT C-CHECK, RT O/B FLAP O/B ACTUATOR LOWER SUPPORT BRACKET CRACKED. STOP DRILLED AND FABRICATED REPAIR DOUBLER PER SRM 57-2-0.SDR DHL9780263CFloorbeam · corrodedAT C-CHECK, UPPER CARGO COMPT AT STA 1680 BETWEEN LINES 4 AND 5 FLOORBEAM HAS CORRSION. REMOVED CORRODED FLOOR SUPPORT ANGLE AND FABRICATED NEW, INSTALLED PER SRM 51-3-0.SDR DHL9780241CSeat Track · wornAT C-CHECK, FS 140 LINE 5 FLOOR TRACK WORN. CUT OUT DAMAGED FLOOR TRACK FORM 130 TO 170, FABRICATED REPAIR SPLICED PER SRM 53-2-3.SDR DHL9780235CFloor Panel · corrodedAT C-CHECK, FWD CARGO COMPT LT INBD AREA BETWEEN STA 140 AND 180 FOUND CORROSION ON FLOOR PANEL. FABRICATED REPAIR PART PER SRM 53-2-0 AND INSTALLED, AREA 6 X 12.SDR DHL9780238CSeat Track · wornAT C-CHECK, FS 150 NR 6 SEAT TRACK WORN. CUT OUT DAMAGED AREA FROM FS 130 TO 170, FABRICATED REPAIR AND INSTALLED REPAIR PER SRM 53-2-3.SDR DHL9780225CSeat Track · wornAT C-CHECK, MAIN CARGO COMPT FS 320 NR 1 FLOOR TRACK WORN AND DAMAGED. CUT OUT 60 INCHES OF TRACK, FABRICATED REPAIR SPLICE AND NEW TRACK PER SRM 53-2-3.SDR DHL9780242CSeat Track · wornAT C-CHECK, FS 680 NR 5 FLOOR TRACK WORN. CUT OUT 40 OF TRACK AND REPLACED PER SRM 53-2-3.
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