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 DHL2005802510Floor Support · corrodedAFT ACCY COMPT. FLOOR SUPPORT ANGLE CORRODED, STA 1710.000 RBL 19. REMOVED CORROSION FROM SUPPORT ANGLE IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG. 2P. FABRICATED REINFORCING ANGLE IAW SRM 53-7-3 FIG. 5A, SRM 53-2-0 PG. 2E/2F. CLEANED, TRESDR DHL2005802515Longeron · crackedFWD CARGO COMPT. CROSS SLIDE DOOR AREA L-35L CRACKED 1.000 STA 300.000-310.000 MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 1B. REMOVED FASTENERS IAW SRM 51-1-20D PG. 21. PERFORMED STOP HOLE IAW SRM 53-2-0 FIG. 1B SHEET 3. PERFORMED NDT INSP IAW DCSDR DHL2005802513Longeron · crackedFWD CARGO COMPT CROSS SLIDE DOOR AREA L-35L CRACKED STA 280.000-300.000 MAJOR REPAIR. CORR.: PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 1B. REMOVED FASTENERS IAW SRM 51-1-20D PG. 21. PERFORMED STOP HOLE IAW SRM 53-2-0 FIG. 1B (SHEET 3). PERFORMED NDT INSPECTIOSDR DHL2005802507Stiffener · crackedITEM REF. NR 030753: FWD ACCESSORY COMPT. FWD PRESSURE BULKHEAD STIFFENER CRACK 2.000 STA 8.000 LBL 20. REMOVED CRACKED STIFFENER IAW SRM 51-1-21 PG.1. FABRICATED NEW STIFFENER IAW SRM 53-3-3 FIG. 3. HEAT TREATED IAW SRM 51-1-1 PG. 1,13,17. INSTALLED NEW STIFFSDR DHL2005802506Stiffener · crackedITEM REF. NR. 030754: FWD ACCESSORY COMPT. FWD PRESSURE BULKHEAD STIFFENER CRACK 1.500" STA 8.000 RBL 20. CORR.: REMOVED CRACKED STIFFENER IAW SRM 51-1-21 PG.1. FABRICATED NEW STIFFENER IAW SRM 53-3-3 FIG. 3 ITEM A. HEAT TREATED STIFFENER IAW SRM 51-1-1 PG. 1,SDR DHL2005802508Fitting · crackedAFT CARGO COMPT. INTERCOSTAL FITTING 2.000 CRACK STA 1300.000 L-33R. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG. 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PG. 9. TORQUED IAW SRM 51-3-1 PG. 2A.SDR DHL2005802505Doubler · crackedRT OUTER WING INBD L/E LWR DOUBLER CRACKED 0.250. REMOVED CRACKED DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED DOUBLER (AL7075T6 0.050) IAW SRM 57-3-3. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG SDR DHL2005802504Cargo Track · brokenUPPER CARGO COMPT NR 6 TRACK LUGS BROKEN STA 310.000 - 370.000. CUT OUT NR 6 TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG 49-50 FIG 14. FABRICATED SPLICES IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED AREA AND APLICES IAW SRM 51-1-8B. INSTALLED NESDR DHL2005802503Drive Link · crackedRT OUTBD FLAP DRIVE LINK ASSY CRACKED 0.500 INCH LENGTH AT POINT J STA XF 219.498. REMOVED AND REPLACED RH OUTBD FLAP DRIVE LINK ASSY AT STA XF 219.498 IAW MM 27-51-4 PG. 201-204. REFER TO NR 030703 FOR OPS CHECK.SDR DHL2005802502Skin · crackedRT OUTBD FLAP UPPER SKIN CRACKED 0.500 APPROX. AT STA XF 304.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 57-7-1 FIG. 4, TR 57-94. REMOVED CRACKED PLATING IAW SRM 51-1-21 PG.1. FABRICATED NEW PLATING IAW SRM 57-7-1 FIG. 4, TR 57-94 ITESDR DHL2005802501Skin · damagedRT INBD FLAP UPPER EXTERNAL SKIN INTERIM REPAIR, STA XW 104.000-110.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 57-7-1 FIG. 1. REMOVED PLATING WITH EXISTING INTERIM REPAIR IAW SRM 51-1-21 PG.1. FABRICATED NEW PLATING (AL2024Y3 0.040) ISDR DHL2005802500Cargo Track · corrodedUPPER CARGO COMPT NR 2 TRACK CORRODED, STA 780.000 - 786.000. REMOVED CORROSION FROM TRACK NR 2 IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-3 FIG. 12. CUT OUT NR 2 TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG. 49-50 FIG. 14. FABRICATED SPLICES IAW SDR DHL2005802007Control Panel · malfunctionedNR 1 BUS FAILED ON ENGINE START. DEFERRED NR 1 GEN AND CSD REF MEL 24-1-1A DMI NR 20731 ASSIGNED PLACARD INSTALLED MPEREZ 8427. REF DMI 20731 NR 1 BUSS FAILED ON ENGINE START. REMOVED AND REPLACED BUSS PROTECTION PANEL IAW 24-20-7. OPS CHECKS OK IAW JRH ENSDR DHL2005802006Wire · shortedLEFT GEAR DOOR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. JACKED PLANE PER DACO M/M 7-11-0. PERFORMED GEAR DOOR CHECKOUT PER DACO M/M 32-31-4. FOUND SHORTED POWER WIRE PIN 1 JUST FWD OF DOOR SWITCH. REPAIRED PER DACO M/M 20-50-1. DOOR CHECKS SERV.SDR DHL2005802005Connector · dirtyDOORS NOT LATCHED AND LEFT DOOR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTED LIGHT WENT OUT APPROX ONE 1/2 MINUTES AFTER RETRACTION. CLEANED AND RESECURED CONNECTOR ON LT DOOR SW. OPS CK GOOD PER MM 32-60-0.SDR DHL2005802004Uplock · out of adjustDOOR NOT LATCHES LIGHT ILLUMINATED AFTER TAKEOFF. PERFORMED ABNORMAL PROCEDURE. LEFT AND RIGHT DOOR UNSAFE LIGHT ILLUMINATED. PERFORMED ADJUSTED/TET AT MAIN GEAR DOOR UPLATCH MECHANISM IAW 32-21-4, OPS CKD NORMAL.SDR DHL2005802003Elec Connector · failedUPON RETRACTING LANDING GEAR DOORS NOT LATCHED LIGHT CAME ON, AS WELL AS LEFT DOOR UNSAFE ON S/O PANEL. ABNORMAL PROCEDURE GEAR OR DOOR NOT LATCHED LIGHT ILLUMINATED WAS PERFORMED, DOORS NOT LATCHED LIGHT CAME BACK ON AS WELL AS THE RIGHT DOOR UNSAFE LIGHT ONSDR DHL2005802002Wire · brokenON CLIMB OUT LEFT DOOR UNSAFE LIGHT ILLUMINATED. RAN APPROPRIATE PROCEDURE. AFTER PROCEDURE, LEFT AND RIGHT DOOR UNSAFE LIGHTS ILLUMINATED. FOUND BROKEN WIRE AT THE LEFT GEAR DOOR UP SWITCH, REPAIRED SAME ALSO FOUND CONNECTOR FULL OF DEICING FLUID CLEANED. SDR DHL2005802001Actuator · leakingON GEAR RETRACTION LOST HYDRAULIC FLUID TO AUX LEVEL. FOUND LT GEAR ACTUATOR LEAKING. REPLACED LT GEAR ACTUATOR PER DC-8 M/M 32-32-2 OPS CHECKS NORMALSDR DHL2004802008Uplock Switch · failed"DOORS NOT LATCHED" AND "RIGHT DOOR UNSAFE" LIGHTS ILLUMINATED EN ROUTE. ABNORMAL PROCEDURE COMPLETED. REMOVED AND REPLACED LEFT GEAR DOOR UPLATCH SWITCH AND CLEANED AND RESEATED RT SIDE SWITCH IAW DC-8 M/M 32-31-4 AND 32-10-0. CK'S NORMAL. P/N: H20-24B.SDR DHL2004802007Uplock Switch · malfunctionedDURING LEVEL OFF AND FL 250 DOOR NOT LATCHED LIGHT ILLUMINATED RAN ABNORMAL PROCEDURES DOOR NOT LATCHED LIGHT REMAINED ILLUMINATED. RESTRICTED TO 230 KTS S/O PANEL RT GEAR DOOR UNSAFE LIGHT ALSO ILLUMINATED. REMOVED AND REPLACED LT MLG DOOR UPLATCH SWITCH PESDR DHL2004802006Battery Pack · inoperativeEMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK ASSY WITH SERVICABLE UNIT IAW MM 33-50-1. OPS CHECK, P/N OFF 5708458-505, S/N ID6303, P/N ON 5708458-505, S/N 117J.SDR DHL2004802005Bracket · crackedINBOARD SLOT, RT WING BRACKET ASSEMBLY CRACKED AT MOUNTING AREA. INSTALLED BRACKET ASSEMBLY P/N: 3770292-1 (I/B AT WING SLOT) IAW DC-8 M/M 22-80-1.SDR DHL2004802004Fitting · crackedLT X3 WING TO FUSELAGE FITTING CRACKED. REMOVED AND REPLACED LT STA. X3 WING TO FUSELAGE FITTING IAW DOUGLAS DRAWING 589477 AND DC-8 SRM 51-1-20.SDR DHL2004802003Flange · damagedSTA 966 INBOARD VERTICAL FLANGE OF SUPPORT, THERE IS A CRACK 2.5 INCHES LONG, FORWARD OF AFT BOLT. ACCOMPLISHMENT OF PERMANENT REPAIR REQUIRED BY 30 APR 04. STA. 966 XW3 THE INBOARD VERTICAL FLANGE OF THE SUPPORT, THERE IS A CRACK 2.5 INCH LONG, FORWARD OF ASDR DHL2004802002Fuel Filter · contaminatedFUEL BYPASS LIGHT ILLUMINATED ON NR 1 ENGINE. PERFORMED ABNORMAL PROCEDURE, LIGHT DID NOT EXTINGUISH. ENGINE PARAMETERS NORMAL. CLEARED DESCENDING THRU 15,000. INSPECTED NR 1 ENGINE FUEL FILTER. FOUND SMALL NON-METALLIC DEBRIS. REMOVED AND REPLACED NR 1 SDR DHL2004802001Fuel Filter · contaminatedDURING CRUISE FLIGHT AT FL 350, NR 4 ENGINE FLAMED OUT. SEVERAL ATTEMPTS TO RESTART, THE LAST AT FL 250 AT 300 KIAS WERE UNSUCCESSFUL. REMOVED AND REPLACED NR 4 ENGINE FUEL FILTER DUE TO CONTAMINATION IAW DC-8 M/M 73-11-10. PERFORMED VISUAL INSPECTION OF BOSDR DHL2003802015Bleed Valve · malfunctionedENGINE NR 3 AND 4 OVER PRESSURE LIGHTS ILLUMINATED AFTER BRAKE RELEASE DURING TAKEOFF ROLL. RTO PERFORMED. CONFERRED WITH MX AFTER LIGHTS EXTINGUISHED AND CONTINUED FLIGHT. NOTED BY MX NO REJECTED T/O INSPECTION REQUIRED DUE TO ZERO AIRSPEED AND MINIMAL BRSDR DHL2003802564Skin · delaminatedRIGHT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED STA XW 5.000 - XW 33.000. REMOVED AND REPLACED RIGHT WING T/E UPPER PANEL (STA XW 5.000 - XW 33.000) IAW SRM 51-3-0 PG 1.SDR DHL2003802567Skin · brokenLEFT INBD FLAP UPPER AFT SKIN BROKEN STA XW 2.000 CANT (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU38-7, DWG U38-R07. REMOVED DAMAGED SKIN SEGMENT IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN SEGMENT IAW ED EDU38-7, DWG U38-R07. COUNTERSUNK NEW SKIN SEGMSDR DHL2003802565Skin · wornLEFT OUTBD FLAP L/E PLATING WORN STA XF 163.000- 213.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU38-8, DWG U38-R08. REMOVED DAMAGED PLATING, RUB STRIPS AND RIBS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, ED EDU38-8, DWG U38-R08. HEAT TREATED IAW SRM 51SDR DHL2003802578Mechanism · crackedRIGHT WING INBD AILERON MANUAL REVERSION MECHANISM CRACKED. REMOVED AND REPLACED MANUAL REVERSION MECHANISM AT RIGHT WING INBD AILERON IAW MM 27-11-8 PG 401-404. PERFORMED ADJUSTMENT TEST, GOOD IAW MM 27-10-0 PAGES 510 THRU 515. SEE NR 1456 FOR OPS CHECK.SDR DHL2003802566Fitting · crackedAFT CARGO COMPT FITTING WITH 0.500 CRACK AT STA 1280.000 L-35L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IN AFT CARGO SDR DHL2003802576Hinge Fitting · crackedNR 6 LEFT AILERON HINGE FITTING CRACK. REMOVED NR 6 LEFT AILERON HINGE FITTING IAW MM 20-16-0 PG 208. REFER TO JC 8-27-11-026 FOR NEW NR 6 LEFT AILERON HINGE FITTING INSTALLATION.SDR DHL2003802573Skin Panel · delaminatedLEFT WING TO FUSELAGE NR 706 PANEL EXTERNAL SKIN DELAMINATED STA 912.000 - STA 980.000. REMOVED DELAMINATED PANEL IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED LPS3 IAW SRM 51-1-8 PG 35-36. INSTALLED NEW PANEL ASSY ON LEFT SDR DHL2003802553Skin · delaminatedRIGHT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED, STA XW 5.000 - XW 47.000. REMOVED AND REPLACED PANEL ON RIGHT WING T/E STA XW 5.000 - XW 47.000 IAW SRM 51-3-0 PG 1.SDR DHL2003802577Hinge Fitting · crackedNR 4 LT AILERON HINGE FITTING CRACK. REMOVED AND REPLACED NR 4 LT AILERON HINGE FITTING IAW MM 20-16-0 PG 208.SDR DHL2003802571Skin · delaminatedRIGHT WING CENTERWING 723 PANEL LOWER SKIN DELAMINATED STA 742.000. REMOVED AND REPLACED NR 723 PANEL ASSY ON RIGHT WING CENTERWING, STA 742.000 IAW SRM 51-3-0 PG 1.SDR DHL2003802563Fitting · crackedAFT CARGO COMPT T-BOLT FITTING CRACKED 0.500 AT STA 1240.000. REMOVED CRACKED T-BOLT FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW T-BOLT FITTING IAW SRM 51-1-20D PG 9.SDR DHL2003802568Door · crackedRIGHT WING OTBD SLOT UPPER DOOR CRACKED 3.000. REMOVED AND REPLACED UPPER DOOR ON RIGHT WING OTBD SLOT IAW MM 27-80-2 PG 201-203, SRM 51-3-0 PG 1, SRM 51-3-1 PG 2A. FOR OPS CHECK SEE NR 1456.SDR DHL2003802572Door Frame · wornWEAR DAMAGE TO THE RIGHT FUSELAGE FWD CTR SECTION LOWER CARGO COMPARTMENT DOOR JAMB AROUND STA 324.000, L-32R (MAJOR REPAIR). REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART O6,10-01.001. CLEANED, TREATED AND SDR DHL2003802555Skin · damagedLT OUTER WING CENTER EXTENDED L/E SLOT LWR PLATING ELONGATED HOLES AROUND STA XFS 526.000 (MAJOR REPAIR). REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA IAW ED EDU38-2 AND DWG U38-R02. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06,10-01-001. CLEANSDR DHL2003802570Skin · corrodedRIGHT MLG DOOR INTERNAL SKIN AFT PART CORRODED, STA 960.000. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 52-2-0 PG 20. TRIMMED OUT CORRODED AREA IAW SRM 52-2-0 PG 18. FABRICATED INTERNAL DOUBLER, FILLER IAW SRM 52-2-0 PG 18. CLESDR DHL2003802556Skin · damagedRIGHT WING EXTENDED L/E INBD VANE FWD OUTER PLATING ELONGATED HOLES AROUND STA XS 247.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU38-3 AND DWG U38-R03. REMOVED FASTENERS, TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATESDR DHL2003802554Skin · damagedELONGATED HOLES IN RT WING EXTENDED L/E INBD VANE FORWARD PLATING AROUND STA XILD 7095 (MAJOR REPAIR). REMOVED FASTENERS. TRIMMED OUT THE DAMAGED SKIN AREA. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA. FABRICATED AND EXTERNAL REPAIR DOUBLERSDR DHL2003802575Panel · crackedRIGHT ELEVATOR UPPER PANEL CRACK 0.250, STA XE 65.156 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-4-1 PG 1, 2. REMOVED CRACKED UPPER PANEL FROM RT ELEVATOR STA XE 65.156 IAW SRM 51-1-21 PG 1, SRM 51-1-21A PG 1, 4. CLEANED, TREATED ANDSDR DHL2003802574Rib · damagedRIGHT OUTBD STUB WING RIB HOLES ELONGATED STA XOLDO 67.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, ATM 201846, DWG 9753297. REMOVED DAMAGED RIB IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED RIB IAW ATM 201846, DWGSDR DHL2003802549Angle · crackedRIGHT OUTBD STUB WING WEB REINFORCING ANGLE CRACK 2.000, STA XS 503.000. REMOVED CRACK REINFORCING ANGLE IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-SDR DHL2003802544Door Frame · damagedFWD PASSENGER DOOR JAMB UPPER FWD CORNER INTERIM REPAIR, STA 25.000 L-9L TO L-10L (MAJOR REPAIR). PERFORMED MAJOR REPAIR, SERVICE REWORK DWG SRO 8530021, DWG 5750776. REMOVED INTERIM REPAIR. TRIMMED OUT AFFECTED AREA IAW SRM 53-2-0 FIG 15, SERVICE REWORK DWSDR DHL2003802540Door Frame · damagedAFT PASSENGER DOOR JAMB LWR FWD CORNER INTERIM REPAIR, STA 1620.000 L-21L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 18, SERVICE REWORK DWG SR08530021, DWG 5750776. REMOVED INTERIM REPAIR IAW SRM 51-1-20D PG 21. FABRICATED DOUBLER AND TRIPLER
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