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.

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 Apr 29, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 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 NORApr 29, 1999 · N802DH · Doug DC873F · Trailing Edge FlapsSDR 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 51Apr 29, 1999 · N802DH · Doug DC873F · Wing, Plate/SkinSDR 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 & 1Apr 29, 1999 · N802DH · Doug DC873F · Wing, Plate/SkinSDR 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.Apr 29, 1999 · N802DH · Doug DC873F · Wing Miscellaneous StructureSDR 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. Apr 29, 1999 · N802DH · Doug DC873F · Wing Miscellaneous StructureSDR 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 Apr 29, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 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 SRMApr 29, 1999 · N802DH · Doug DC873F · Engine Cowling SystemSDR 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 XApr 29, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 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, Apr 29, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 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 Apr 29, 1999 · N802DH · Doug DC873F · Fuselage Main, FrameSDR 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 51Apr 29, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 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. TREATEDApr 29, 1999 · N802DH · Doug DC873F · Trailing Edge FlapsSDR 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), 0Apr 29, 1999 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 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 AREApr 29, 1999 · N802DH · Doug DC873F · Wing Miscellaneous StructureSDR 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 0.20Apr 29, 1999 · N802DH · Doug DC873F · Engine Thrust ReverserSDR 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 2Apr 29, 1999 · N802DH · Doug DC873F · Nacelle/Pylon StructureSDR 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 Apr 29, 1999 · N802DH · Doug DC873F · Rudder StructureSDR 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 INSTApr 29, 1999 · N802DH · Doug DC873F · Rudder StructureSDR 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.Sep 26, 1998 · N802DH · Doug DC873F · Landing Gear Retraction/Extension SystemSDR 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.Jul 25, 1998 · N802DH · Doug DC873F · Inertial Guidance SystemSDR 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.Dec 3, 1997 · N802DH · Doug DC873F · Electrical/Electronic Compartment DoorsSDR 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, OPSDec 3, 1997 · N802DH · Doug DC873F · Inertial Guidance SystemSDR 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.Nov 17, 1997 · N802DH · Doug DC873F · Engine Cowling SystemSDR 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.Nov 17, 1997 · N802DH · Doug DC873F · Engine Thrust ReverserSDR DHL9780250CVane · delaminatedAT C-CHECK, RT WING I/B FLAP VANE DELAMINATED. REMOVED VANE, REPAIRED AND REINSTALLED PER M/M 27-51-14.Nov 17, 1997 · N802DH · Doug DC873F · Trailing Edge FlapsSDR DHL9780248CPanel · delaminatedAT C-CHECK, RIGHT WING LOWER SURFACE STA 130 TO 219 PANEL DELAMINATED. REMOVED, REPAIRED PANEL AND INSTALLED PER SRM 51-1-15.Nov 17, 1997 · N802DH · Doug DC873F · Wing, Plate/SkinSDR 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.Nov 17, 1997 · N802DH · Doug DC873F · Wing, Plate/SkinSDR 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.Nov 17, 1997 · N802DH · Doug DC873F · Wing, Plate/SkinSDR 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.Nov 17, 1997 · N802DH · Doug DC873F · Fuselage Main, Plate/SkinSDR 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.Nov 16, 1997 · N802DH · Doug DC873F · Wing, Plate/SkinSDR 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.Nov 15, 1997 · N802DH · Doug DC873F · Wing, Plate/SkinSDR 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.Nov 15, 1997 · N802DH · Doug DC873F · Wing, Plate/SkinSDR 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 SRNov 14, 1997 · N802DH · Doug DC873F · Fuselage Main, BulkheadSDR 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 Nov 14, 1997 · N802DH · Doug DC873F · Fuselage Main, BulkheadSDR DHL9780252CPanel · delaminatedAT C-CHECK, PANEL NR 1621 RIGHT HAND LOWER FUSE HAS DELAMINATION ONE CORNER. REBONDED PER SRM 51-1-19.Nov 14, 1997 · N802DH · Doug DC873F · Fuselage Main, Plate/SkinSDR 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.Nov 14, 1997 · N802DH · Doug DC873F · Wing, Plate/SkinSDR 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.Nov 13, 1997 · N802DH · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR DHL9780253CCowl · crackedAT C-CHECK, ENGINE NR 2 NOSE COWL ANTI-ICE DEFLECTOR AT 1 O'CLOCK IS CRACKED. MODIFIED PER S/B 71-97.Nov 13, 1997 · N802DH · Doug DC873F · Engine Cowling SystemSDR DHL9780249CBracket · corrodedAT C-CHECK, INTERIOR CABIN, SUBFLOOR BRACKET HAS CORROSION STA 20. REMOVED DAMAGED BRACKET AND FABRICATED NEW BRACKET PER SRM 51-2-0.Nov 13, 1997 · N802DH · Doug DC873F · Fuselage Miscellaneous StructureSDR 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.Nov 13, 1997 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 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.Nov 13, 1997 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 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.Nov 13, 1997 · N802DH · Doug DC873F · Wing, Plate/SkinSDR 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.Nov 12, 1997 · N802DH · Doug DC873F · Trailing Edge Flap ActuatorSDR 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.Nov 12, 1997 · N802DH · Doug DC873F · Fuselage Main, Floor BeamSDR 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.Nov 12, 1997 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 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.Nov 12, 1997 · N802DH · Doug DC873F · Fuselage Floor PanelSDR 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.Nov 11, 1997 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 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.Nov 11, 1997 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9780242CSeat Track · wornAT C-CHECK, FS 680 NR 5 FLOOR TRACK WORN. CUT OUT 40 OF TRACK AND REPLACED PER SRM 53-2-3.Nov 10, 1997 · N802DH · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
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