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 DHL2007802524Skin · delaminatedNR 5 LT SPOILER PANEL DELAMINATED. REMOVED AND REPLACED NR 5 LT SPOILER PANEL IAW MM 27-61-1 PG 201-206. REFER TO NR 071624 FOR OPS CHECK.SDR DHL2007802516Frame · brokenFOUND LT WING CTR L/E UPPER INTERNAL FORMER BROKEN 1" STA XS 521.000. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED DOUBLER (AL7075"0" 0.063") IAW SRM 57-3-3 FIG 4. HEAT TREATED FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED ASDR DHL2007802519Rib · crackedLT INBD FLAP RIB HAS FOUR CRACKS OF 1" AND 1.500" STA XW 125.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 2 PG 6 (SHEET 4). REMOVED CRACKED RIV IAW SRM 57-1-0 PG.1, SRM 51-1-21, SRM 51-1-20D. FABRICATED RIB (AL2024"0" 0.050") IAW SRM 57-7-1SDR DHL2007802517Frame · crackedFOUND LT OTBD FLAP FORMER 1.500" CRACKED STA XF 165.000. REMOVED CRACKED FORMER IAW SRM 51-1-21. FABRICATED NEW FORMER (AL7075"0" 0.050") IAW SRM 57-2-0 PG 1. HEAT TREATED FORMER FROM 7075"0" TO 7075T6 IAW SRM 51-1-1 PG 13-17. CLEANED, TREATED AND PRIMED FSDR DHL2007802518Door · crackedR2 DOOR AFT UPPER CORNER CRACKED 1.250" LENGTH. PERFORMED MAJOR REPAIR IAW AD200-20-08 S/B DC8 53-075, DOUGLAS DWG SR08530021 AND 5750776. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION IAW DOUGLAS DWG SR08530021. PERFORMED NDT INSPECTION IAW NSDR DHL2007802514Skin · misrepairedNR 4 RT STUB WING LWR SURFACE HAS A NON STANDARD REPAIR AT STA XFS 562.500. PERFORMED MAJOR REPAIR IAW SRM 57-2-1A FIG 1 PG 3. REMOVED NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED EXT REPAIR DOUBLER (AL7075T6 0.080") AND INTERNAL DOUBLER (ASDR DHL2007802511Splice · crackedRT WING CTR LE UPPER INTERNAL SPLICE 2" CRACK STA XOLD 6.2246. REMOVED CRACKED SPLICE IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. FABRICATED SPLICE (AL7075T6 0.080") IAW BOEING MSG NR 1-275396206-21 DATED JAN 23,2007. CLEANED, TREATED AND PRIMED AREA AND SPLSDR DHL2007802504Seat Track · wornMAIN CARGO COMPT NR 4 TRACK LUG WORN (STA 1670.000 - 1705.000). CUT OUT NR 4 TRACK DAMAGED SEGMENT AND FABRICATED (3EA) SPLICES (AL7075T6 0.100"/0.125"/0.160") IAW SRM 53-2-3 PG 49-50. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. INSTALLED SDR DHL2007802513Angle · crackedLT OTBD FLAP "T" ANGLE CRACKED 1" STA XF 165.000. REMOVED CRACKED T ANGLE IAW SRM 51-1-21. FABRICATED NEW T-ANGLE (EXTRUSION P/N 1243286) IAW SRM 57-7-0 FIG 3, SRM 51-2-0 FIG 50. CLEANED, TREATED AND PRIMED AREA AND T-ANGLE IAW SRM 51-1-8B. INSTALLED T-ANGSDR DHL2007802512Angle · crackedRT OUTBD FLAP SHOWS "T" ANGLE WITH CRACK 1" AT STA XT 165.000. REMOVED CRACKED T-ANGLE IAW SRM 51-1-21. FABRICATED NEW T-ANGLE (EXTRUSION P/N 1213286) IAW SRM 57-7-0 FIG 3, SRM 51-2-0 FIG 50. CLEANED, TREATED AND PRIMED AREA AND T-ANGLE IAW SRM 51-1-8B. INSDR DHL2007802509Skin · crackedRT WING UPPER SKIN 0.750" CRACKED STA XRS 74.000 S-14R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 10 SHEET 1. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2-1 FIG 10 SHEET 1. PERFORMED NDT INSP IAW DC8 NDT SPM PART SDR DHL2007802508Rib · crackedRT INBD FLAP RIB 1" CRACK STA XW 125.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED RIB IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 57-7-1 FIG 2 SHEET 4, SRM 51-1-21, SRM 51-SDR DHL2007802510Skin · crackedLT WING UPPER SKIN CRACKED 1" S-9 AT STA XRS 74.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR ON LT WING UPPER SKIN STA XRS 74.000 S-9 IAW SRM 57-2-1 FIG 17 PG 87-88. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2-1 FIG 17 PG 87-88. SDR DHL2007802507Door Frame · unknownPERFORM REPAIR/MODIFICATION OF FWD PAX DOOR UPPER AFT JAMB CORNER IAW AD2000-20-08, DWG SR08530021 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2000-20-08, S/B DC8 53-075, DOUGLAS DWG SR08530021, 5750776. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. PERSDR DHL2007802506Door Frame · unknownPERFORM REPAIR/MODIFICATION OF FWD PAX DOOR LWR FWD JAMB CORNER IAW AD2000-20-08, DWG SR08530021 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2000-20-08, S/B DC8 53-075, DOUGLAS DWG NR SR08530021, 5750776. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. PESDR DHL2007802515Angle · crackedFOUND LT INBD FLAP T/E ANGLE 1.500" CRACK STA XW 129.000. REMOVED CRACKED REINFORCING ANGLE IAW SRM 51-1-21. FABRICATED NEW REINFORCING ANGLE (AL2024"0" 0.050") IAW SRM 57-7-1 FIG 2 SHEET 1. HEAT TREATED FROM "0" TO AL2024T4 IAW SRM 51-1-1 PG 1-13-17. CLEASDR DHL2007802505Angle · crackedAFT CARGO COMPT CRACKED ANGLE AT STA 1420.000 BL 0". REMOVED CRACKED ANGLE IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21.SDR DHL2007802503Frame · crackedRT WING CTR L/E FORMER 0.500" CRACK STA XFS 291.500. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED (2) ANGLE DOUBLER (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTASDR DHL2007802502Floor Support · wornMAIN CARGO COMPT NR 5 TRACK LUGS WORN (STA 132.000 - 175.000). REMOVED DAMAGED TRACK SEGMENT AND SPLICES IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND REINSTALLED SPLICES IAW SRM 53-2-3 PG 49-5SDR DHL2007802501Seat Track · wornMAIN CARGO COMPT NR 7 TRACK LUG WORN STA 786.000. CUT OUT NR 7 TRACK DAMAGED SECTION IAW SRM 53-2-3 PG 17 FIG 6D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG AND CHANNEL IAW SRM 53-2-3 PG 17 FIG 6D, SRM 51-3-0, SRM 51-3-1.SDR DHL2007802500Seat Track · wornMAIN CARGO COMPT NR 1 TRACK PLUG LUG WORN STA 340.000. REMOVED WORN TRACK PLUG IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK PLUG IAW SRM 51-3-0, SRM 51-3-1 PG 3.SDR DHL2007802523Heat Exchanger · crackedRT PRIMARY HEAT EXCHANGER FWD LWR CORNER REPAIR DOUBLER 0.250" CRACKED, STA -32.000 L-27R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-30-07, DWG NR AC62-53-103 REV IR DATED 01-17-07. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGEDSDR DHL2006802002Strut · underservicedDURING INITIAL T/O ROLL, UNABLE TO MAINTAIN DIRECTIONAL CONTROL WITH FULL RUDDER PLUS TILLER INPUT. ALL ENG'S INDICATED EQUAL N1. CLOCKS RECORDED 7 SEC OF FLT. TIME INDICATING NOSE STRUT EXTENSION. ATIS WIND REPORTED AT 050 7 KTS RUNWAY 04L WAS USED. SERSDR DHL2006802001Stator Vane · out of adjustENCOUNTERED MAJOR UPDRAFT AT FL 410 ENGNE NR 3 FLAMED OUT PERFORMED INFLIGHT ENGINE START ABNORMAL PROCEDURE NORMAL SYSTEM OPERATION NR 3 RESTARTED. C/W ROUGH AIR INSPECTION PER DC-8 M/M 05-51-0. A/C FOUND SERV. NO DEFECTS. PERFORMED FAULT CODE 50 PER DC-SDR DHL2005802011Bulb · inoperativeEMERGENCY LIGHTS DISARM LIGHT INOP. REMOVED AND REPLACED EMER LIGHTS DISARM BULB. OPS CHECK OK IAW MM 33-50-0. P/N 313.SDR DHL2005802010Door · damagedFOUND L1 DOOR DAMAGED BY STAIRS. REMOVED DAMAGED AREA FROM BTM FWD LWR AREA OF DOOR STRUCTURE. FABRICATED DOOR FRAME SEGMENT DOUBLER FROM 2024-T3, .070. INSTALLED REPAIR USING EXSISTING RIVET SPACING AND SECOND ROW SPACING PER SRM.SDR DHL2005802009Fire Detector · malfunctionedAT FL 320 NR 2 ENGINE HAD INTERMITTENT FIRE WARNING. COMPLETED PHASE 1 OF ENGINE FIRE CHECKLIST, NO INDICATION OF FIRE, COMPLETED CHECKLIST. CHECKED BOTH LOOP A AND B. FIRE BOTTLE WAS NOT DISCHARGED. PLACED FIRE DETECTION LOOP A ON NR 2 ENGINE ON MEL 26-2-SDR DHL2005802008Fire Loop · failedENROUTE AT FL 370 WE HAD AN INTERMITTENT NR 2 FIRE INDICATION. AFTER BOTH BOTTLES WERE FIRED THE FIRE INDICATION REMAINED CONSTANT FOR APPROX 10 MIN AND WAS INTERMITTENT THROUGH REMAINDER OF FLT. LOOP-A FAILED TO TEST FOR FIRE WARNING, SHORT TEST GOOD.SDR DHL2005802542Support Bracket · crackedRUDDER TAB HINGE SUPPORT BRACKET CRACKED. REMOVED RUDDER TAB IAW MM 27-21-2 PG. 201. REMOVED CRACKED BRACKET IAW SRM 51-1-21. FABRICATED BRACKET IAW JC EA55100013-001-D, DWG DOUGLAS 4701452 AND BOEING COMPANY MSG 1-109638692-2. PERFORMED NDT INSP IAW DC8 NDT SSDR DHL2005802538Skin · corrodedITEM REF. NR. 045009: FWD ACCY COMPT. FUSELAGE INTERNAL SKIN CORRODED, STA 20.000 L-31R TO L-32R (STA 20.000-70.000) MAJOR REPAIR. CORR.: PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-18-05 DWG Z20-R14 REV IR DATED 06-24-05. REMOVED EXISTING REPAIR IAW SSDR DHL2005802533Fitting · brokenFWD ACCY COMPT. FITTING BROKEN 0.500 STA 70.000 L-31R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG. 1. REMOVED DAMAGED FITTING IAW SRM 51-1-20D PG. 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-SDR DHL2005802544Frame · crackedCARGO COMPT. FRAME 3.000 CRACK STA 278.000 L-20L (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 27 JUN 05, BOEING MSG 1-105552361-2, 1-105552361-3 DATED 27 JUN 05. REMOVED SUB FLOOR IAW SRM 51-1-21A PG. 1-4. REMOVED FITTING IAW SRM 51-SDR DHL2005802543Frame · crackedRT MLG WW FRAME CRACK 5.000 STA 868.000 RBL 50 (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 2 SHEET 3,6. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. CUT OUT DAMAGED FRAME SEGMENT IAW SRM 53-2-0 FIG. 2 SHEET 3. PERFORMED DSDR DHL2005802541Web · crackedRUDDER L/E FRONT SPAR FWD NOSE RIB WEB CRACK 1.500 STA ZR 71.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DOUGLAS DWG 5700556, JC EA55100012-001-D. REMOVED DAMAGED RIB IAW SRM 51-1-21 PG. 1. FABRICATED NEW RIB (AL2024"O" 0.063) IAW DWG 5700556, EA SEMAN 2005SDR DHL2005802539Skin · corrodedFUSELAGE INTERNAL SKIN CORRODED STA 220.000 L-35L TO L-36 (FWD CARGO COMPT. BILGE) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-15-05 DWG Z20-R06 REV. IR DATED 06-24-05. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. REMOVEDSDR DHL2005802535Doubler · brokenEXTERIOR FUSELAGE NR 2 ACCESS DOOR INTERNAL DOUBLER BROKEN STA -165.000 TO -156.000 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-15-05 DWG Z20-R15 REV IR DATED 06-24-05. REMOVED INTERNAL REPAIR DOUBLER AND EXTERNAL PLATING IAW SRM 51-1-21 SDR DHL2005802523Fitting · crackedMAIN TANK INTERIOR LWR SECTION INBD AFT FITTING CRACK STA XRS 74.689 S-61. PERFORMED MAJOR RELPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. CLEANED AND APPLIED TOP COATING MATERIAL TO AREA IAW SRM 51-1-12 PG 7. SDR DHL2005802545Door Frame · crackedCARGO DOOR AFT LWR JAMB CORNER 0.500 CRACKED STA 1440.000 L-32R TO L-33R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 BOEING MESSAGE 1-106666113-2, 1-106666113-3 DATED 07-01-03. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. CUT OUSDR DHL2005802540Frame · crackedRT UPPER CUSP EXTRUSION FRAME FWD FLANGE CRACK 0.750 STA 240.000 L-20R TO L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 2 SHEET 1,2,6, SRM 53-2-0 FIG. 2 SHEET 7-8, TR 53-110, SRM 53-2-0 FIG. 2 SHEET 1, SRM 53-4-1 FIG. 40 SHEET 7-9, SRM 51-2SDR DHL2005802525Skin · crackedFUSELAGE EXTERNAL SKIN AFT OF HOLD OPEN HOOK PIN CRACKED 0.375 STA 1610.000 L-14L TO L-15L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-11-05, DWG Z20-R04 REV IR DATED 06-24-05. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 2SDR DHL2005802524Fitting · crackedLT STUB WING INTERIOR FITTING CRACKED 2.000 (MAJOR REPAIR)STA XOLDO 67.750 PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED SEALANT TO FAYINGSDR DHL2005802520Fitting · crackedFUSELAGE TAIL SECTION L-17R FITTING CRACKED 0.250 STA 1766.000-1782.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLSDR DHL2005802516Panel · delaminatedLT WING T/E UPPER PANEL DELAMINATED (STA XW 5.000 - 47.000). REMOVED AND REPLACED LT WING TE UPPER PANEL (STA XW 5.000-47.000) IAW SRM 51-3-0 PG. 1. TORQUED IAW3 SRM 51-3-1.SDR DHL2005802536Fitting · crackedNR 2 MAIN TANK INTERIOR OUTBD FWD FITTING CRACKED STA XRS 74.869 S-61 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG. 21. CLEANED AND APPLIED TOP COATING MATERIAL TO AREA IAW SRM 51-1-SDR DHL2005802532Doubler · crackedEXTERIOR FUSELAGE NOSE SECTION STRUCTURAL MODIFICATION DOUBLER (ACS) CRACKED 0.750 AT AFT LWR CORNER OF RT PRIMARY HEAT EXCHANGER STA -12.000 L-27R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-13-05, DWG Z20-R01 REV. IR DATED 06-24-05. SDR DHL2005802530Fitting · crackedNR 2 MAIN TANK INTERIOR LWR SECTION OUTBD AFT FITTING CRACKED STA XRS 74.869 S-61 (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG. 21. CLEANED AND APPLIED TOP COATING MATERIAL TO AREA IAW SRM 51-1-SDR DHL2005802527Fitting · crackedNR 2 MAIN TANK INTERIOR LOWER SECTION INBD FWD FITTING CRACK, STA XRS 74.869 S-61 (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG. 21. CLEANED AND APPLIED TOP COATING MATERIAL TO AREA IAW SRM 51-1-SDR DHL2005802526Doubler · crackedEXTERIOR FUSELAGE NOSE SECTION ESTRUCTURAL MODIFICATION DOUBLER (ACS) CRACKED 0.250 AT AFT UPPER CORNER OF PRIMARY HEAT EXCHANGER STA -12.000 L-24L (MAJOR REPAIR). CORR.: PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-11-05, DWG Z20-R02 REV. IR DATED 06-2SDR DHL2005802531Longeron · crackedFUSELAGE TAIL SECTION L-17L CRACKED 2.000 (STA 1766.000-1786.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG.1, SRM 53-5-3 PG. 16 FIG. 5. REMOVED CRACKED LONGERON IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. FABRICATED NEW LONGERON P/N S1616757 IASDR DHL2005802509Angle · corrodedMAIN CARGO COMPT. PNEU. DUCT COVER SUPPORT ANGLE CORRODED STA 8.000 - 17.000, RBL 59. REMOVED CORROSION FRON SUPPORT ANGLE IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-3 PG. 2P. FABRICATED NEW SUPPORT ANGLE IAW SRM 53-2-0 PG.1. CLEANED, TREATED
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