Douglas DC-8-73F
Service difficulty reports · 15,471
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'DC873F' 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 aircraft_model_key = 'DC873F' 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 DHL2003873503Frame · crackedRT WING CENTER LE FORMER CRACKED 0.250 AT XFS 297.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9,10. FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANSDR DHL2003873502Frame · crackedRT WING CENTER L/E FORMER CRACKED 0.250 AT XFS 316.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9,10. FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INTALLED REINFORCING ANSDR DHL2003873501Seat Track · damagedFLIGHT COMPT F/E FWD SEAT TRACK SHOWS HOLES ELONGATED. REMOVED AND REPLACED F/E FWD SEAT TRACK (FLIGHT COMPT) IAW SRM 51-3-0 PG 1.SDR UPS03840911Skin · corrodedINSPECTION TYPE: C3, EXTERIOR FUSELAGE SKIN STA 670 ON CENTERLINE OF BELLY, SKIN AT ANTENNA MOUNT FOUND TO BE CORRODED. BLENDED CORROSION. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED DOUBLER AND FINGER DOUBLERS IAW DC8 SRM 53-2-1 AND 51-1-24. ALODINED SDR DHL2003604761Skin · dentedEXTERIOR SKIN WITH DENT AND WEAR OUT OF LIMITS BETWEEN STA. 120.000 AND STA. 210.000, L-20L TO L-22L. PERFORMED MAJOR REPAIR IAW EODHL-030528, ED-3316. REMOVED FASTENERS AND EXISTING REPAIR DOUBLER. BLENDED OUT AFFECTED AREA. PERFORMED EDDY CURRENT INSPECTIONSDR DHL2003604763Attach Fitting · corrodedMAIN CARGO COMPT T-FITTING ATTACHING NR 4 TRACK TO FLOORBEAM AT STA 1704.000 CORRODED. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1 ATM NR P0201387, DWG 5755032. REMOVED CORRODED FITTING IAW SRM 51-3-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND SDR DHL2003604711Skin · crackedFUSELAGE NOSE SECTION EXTERIOR SKIN CRACKED 0.825 AROUND AFT LOWER JAMB OF RAM AIR EXHAUST DOOR STA FS 12.000, L-27L. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END (0.250) DIA IAW EODHL-030548, ED-3383. PERFORMED EDDY CURRENT INSPSDR DHL2003604654Skin · corrodedLT INNER WING CTR L/E LOWER PLATING SHOWS THREE INTERIM REPAIRS AND CORROSION AROUND STA XFS 304.000. REMOVED FASTENERS. REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT THE DAMAGED AREA, PERFORMED EDDY CURRENT INSPECTION. CLEANED, TREATED AND PRIMED ARSDR DHL2003604600Skin · corrodedLT RUDDER INTERNAL SKIN CORRODED, STA ZR 150.000 - ZR 178.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12. REMOVED DAMAGED SKIN PANEL IAW EODHL-030533, ED-3354. CLEANED, TREASDR DHL2003604588Frame · crackedTAIL CONE SECTION - FRAME CRACKED 1.000 STA. 1937.000 LH SIDE. STOP DRILLED CRACK AND FABRICATED DOUBLER (2024-T3 AL0.040) IAW SRM 53-2-0 FIG.2. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED NEW DOUBLER IAW SRM 51-1-21 PG.1, SRM 51-SDR DHL2003604589Frame · crackedTAIL CONE SECTION FRAME CRACKED 1.000 STA 1923.000 RT SIDE. STOP DRILLED CRACK AND FABRICATED DOUBLER IAW SRM 53-2-0 FIG 2. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1.SDR DHL2003604590Tie · crackedFUSELAGE TAIL CONE INTERIOR RT TIE 1.000 CRACKED AT STA 1923.000. STOP DRILLED CRACK AND FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1.SDR DHL2003873507Frame · crackedLT WING OUTBD L/E FORMER CRACKED 0.250 AT XFS 882.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9,10. FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED REINFORCING ANGLE IAW SRM 51-1-8B. INSTALSDR DHL2003873506Frame · crackedLT WING OUTBD L/E FORMER CRACKED 0.250 AT STA XFS 566.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9,10. FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCINSDR DHL2003806009Seal · leakingFUEL LEAK UNDER WING BETWEEN NR 3 & 4 PYLON. TORQUED GAMMA SEAL JUST OUTBOARD NR 3 PYLON LEAK CHECKED GOOD IAW M/M 28-21-14.SDR DHL2003801004Cylinder · out of adjustUPON LANDING GEAR RETRACTION DOORS NOT LATCHED AND LEFT DOOR UNSAFE LIGHTS ILLUMINATED APPROPRIATE ABNORMAL PROCEDURE PERFORMED LIGHTS REMAINED ON GEAR NOT LATCHED LIGHT ILLUMINATED IN CVG PATTERN RIGHT DOOR UNSAFE LIGHT ILLUMINATED. ADJUSTED LEFT GEAR DOOR ASDR DHL2003604784Skin · delaminatedLT ELEVATOR CONTROL TAB UPPER SKIN DELAMINATED. REMOVED AND REPLACED LT ELEVATOR CONTOL TAB IAW MM 27-30-2 PG 201-204. REFER TO N/R 0531 FOR OPS CHECK.SDR DHL2003604584Access Door · corrodedLT C/W AUX TANK - PERFORM ANTI-CORROSION TREATMENT TO LT 5056 ACCESS DOOR. REMOVED CORROSION ON LT 5056 ACCESS DOOR IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG.43. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER (7075SDR DHL2003604587Fitting · crackedRUDDER FITTING ASSY IN RUDDER INNER STRUCTURE CRACKED STA. 104.000 (WATER DRAIN) REMOVED CRACKED FITTING IAW SRM 51-1-21 PG.1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-21 PG.1SDR DHL2003604583Access Panel · corrodedRT C/W AUX TANK, PERFORM ANTI-CORROSION TREATMENT TO RT UPPER ACCESS DOOR NR 5056. REMOVED CORROSION ON 5056 RT UPPER ACCESS DOOR IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 43. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DSDR DHL2003873508Frame · crackedLT WING CTR L/E FORMER CRACKED 0.250 AT STA XFS 379. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT XFS 379 IAW SRM 57-2-0 PG 9,10. FABRICATED REINFORCEMENT ANGLE IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED REINFORCEMENT ANGLE IAW SRSDR DHL2003604730Door Frame · wornCARGO DOOR JAMB SHOWS WEAR OUT OF LIMITS AT STA.1440.000 L-29R - L30R. PERFORMED MAJOR REPAIR IAW EODHL-03557, ED-3317. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. BLENDED OUT DAMAGED AREA IAW EODHL-03557, ED-3317. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SSDR DHL2003604727Stiffener · crackedMAIN CARGO COMPT. FLOORBEAM INTERCOSTAL JOINT SHOWS STIFFENER CRACKED (1.000) STA.702.000 BL-0. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG.1, ATM P0201384, DWG.5773275. REMOVED CRACKED STIFFENER IAW SRM 51-1-20D PG.21, SRM 51-1-21 PG.1. FABRICATED NEW STIFFENESDR DHL2003604585Frame · crackedLT. WING CENTER L/E FORMER CRACKED 3.000 AT STA. XOLDI 6.225. STOP DRILLED CRACK AT STA. XOLDI 6.225 AND FABRICATED REINFORCEMENT ANGLE (301 0.250H 0.032) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED REINFORCEMENT ANGLE SDR DHL2003604607Skin · delaminatedLT WING NR 1 VANE FLAP INTERNAL SKIN DELAMIATED. REMOVED AND REPLACED NR 1 VANE FLAP ON LT WING IAW MM 27-51-14 PG 201, 202. FOR OPS CHECK SEE N/R.SDR DHL2003604782Skin · corrodedUPPER EXTERNAL FUSELAGE SKIN CORRODED AT STA 680.000, L-2L - L-2R. PERFORMED MAJOR REPAIR IAW EODHL-030540, ED-3308. REMOVED FASTENERS, REMOVED CORROSION ON AFFECTED AREA , FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. BLENDED OUT AFFECTED AREA IAW EODHL-030540SDR DHL2003604740Frame · corrodedAFT CARGO COMPT FRAME ANGLE DOUBLER CORRODED AT STA 1040.000 L-33R - L-34R. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED CORROSION ON FRAME ANGLE DOUBLER IAW SRM 51-1-8 PG 17-18. FOUND OUTSDR DHL2003604717Skin · crackedFUSELAGE NOSE SECTION SKIN CRACKED 1.125, STA 12.000 L-27R AT STRUCTURAL MODIFICATION. PERFORMED MAJOR REPAIR IAW EODHL-030549, ED3384. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END USING A 0.250 DIA DRILL IAW EODHL-030549, ED-338SDR DHL2003604789Skin · crackedEXTERNAL FUSELAGE SKIN CRACKED 0.450, STA 1160.000 BETWEEN L-26R AND L-28R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030555, ED-3311. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW EODHL-030555, ED-3311. PERFORMED EDDY CURRENT SDR DHL2003604714Skin · corrodedLOWER FUSELAGE EXTERIOR SKIN SHOWS SEVERAL SPOTS OF CORROSION BETWEEN STA 510.000 AND 570.000, L-31R - L-34R. PERFORMED MAJOR REPAIR IAW EODHL-030541, ED-3310. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF SDR DHL2003604661Skin · corrodedRT WING CTR L/E LWR EXTERNAL SKIN SHOWS CORROSION, XFS 341.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED OUT DAMAGED SKIN SECTION IAW EODHL-030531, ED-3304. PERSDR UPS03840926Skin · damagedINSPECTION TYPE: C, COMPLY WITH MPI P 14035: IAW M REPAIR TO AIRSTART DOOR CUTOUT AT 100Y CYCLES OR 3 MONTHS WHICHEVER COMES FIRST IAW EO DC8-5330-0793, STATION 25 TO 55 LONG. 28L-30L AT DOOR CUTOUT REMOVED EXISTING FILLERS,NDT VERIFIED NO CRACKS AT EXISDR DHL2003604704Fitting · corrodedFWD CARGO COMPT END FITTING CORRODED, STA 70.000, L-27R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21 SRM 51-1-21 PG 1. REMOVED CORROSION FROM END FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-2-0 PG 2P. REMSDR DHL2003604712Skin · damagedC-CARGO DOOR EXTERNAL SKIN WITH INTERIM REPAIR AND DENTS AT SEVERAL SPOTS. PERFORMED MAJOR REPAIR IAW SRM 52-1-0 PG 1, SRM 52-4-1 FIG 2, BOEING MESSAGE DHL-CVG-0079H. REMOVED DAMAGED SKIN IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMEDSDR DHL2003604764Fitting · corrodedFWD CARGO COMPT END FITTING AT STA 70.000, L-27L CORRODED. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21, SRM 51-1-21 PG 1. REMOVED CORROSION FROM END FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-2-0 PG 21. SDR DHL2003604677Skin · dentedLT HORIZ STAB L/E OUTER SKIN DENTED FROM STA XFS 91.250 - XFS 116.250. PERFORMED MAJOR REPAIR IAW EODHL-030515, ED-3270. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EODHL-030515, ED-3270. CLEANED, TREATED AND PRIMED ARESDR DHL2003604715Skin · crackedUPPER FUSELAGE EXTERIOR SKIN WITH 0.750 CRACK AT STA 1751.000 BETWEEN L-14L AND L-17L. PERFORMED MAJOR REPAIR IAW EODHL-030546, ED-3298. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED AREA IAW EODHL-030546, ED-3298. PERFORMED EDDY CURRENT INSPECTISDR DHL2003604662Skin · dentedLT HORZ STAB L/E HAS INTERIM REPAIR & SEVERAL DENTS BETWEEN STA XFS 47.500 AND XFS 91.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EO DHL 030505, ED 3270. REMOVED FASTENERS & EXISTING INTERIM REPAIR IAW SRM 51-1-21 PG 1, SRM 51-1-21A PG 4. CLEANED, TREATESDR DHL2003604569Skin · crackedLT WING INBD FLAP PLATING CRACKED 2.000 STA XW 125.000 - XW 128.000. REMOVED CRACKED PLATING IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 1. CLEANTED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLATING IAW SRSDR DHL2003604573Skin · crackedLT WING OTBD SKIN SEGMENT FLAP PLATING CRACKED 2.00, XW 160.000 - XW 169.000. CUT OUT DAMAGED AREA AND FABRICATED SPLICE AND NEW SKIN SEGMENT IAW SRM 57-2-0 FIG 4. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED SPLICE AND NEW SKIN SEGMENT IAW SSDR DHL2003604576Angle · crackedLT WING OUTBD FLAP (TEE) ANGLE CRACKED 2.000 AT STA XF.165.000. REMOVED DAMAGED (TEE) ANGLE AT STA XF.165.000 IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED ARE IAW SRM 51-1-8B. INSTALLED NEW (TEE) ANGLE IAW SRM 51-1-21 PG 1.SDR UPS03840908Longeron · crackedINSPECTION TYPE: C3 AFT PIT FS 1350, LONGERON 35L IS CRACKED. REMOVED CRACKED LONG 35L FS 1270 TO 1350 IAW SRM 51-1-20D. LOCATED AND DRILLED UP NEW LONG IAW SRM 51-1-24. INSTALLED NEW LONG 3 5L FS 1270-1350 IAW SRM 51-1-20D AND 51-3-0.SDR DHL2003806008Battery · inoperativeDURING PREFLIGHT EMERGENCY LIGHTS DID NOT WORK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PER M/M 33-50-0. OPS CHECKED GOOD.SDR UPS03840907Skin · crackedINSPECTION TYPE:C3 LOWER FUSELAGE CENTER SECTION AT FS 1350 LONGERON 34L FUSELAGE SKIN IS CRACKED. REMOVED 2 EA EXISTING REPAIR DOUBLERS, TRIMMED OUT CRACK FS 1350 LONG 34L FABBED REPAIR DOUBLER COMBINING 2 EA EXISTING REPAIR DOUBLERS, FABBED SKIN FILLERS ANSDR DHL2003804003Light · burned outEMERGENCY LIGHTS ARMED LIGHT BURNED OUT. REPLACED ARMED LIGHT, OPS CHECKED GOOD PER DC8 M/M 33-50-2.SDR DHL2003806007Battery · inoperativeEMERGENCY EXIT LIGHTS WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY UNIT. OPS CHECKED GOOD IAW M/M 33-50-1.SDR DHL2003604732Fitting · corrodedMAIN CARGO COMPT FITTING CORRODED AT STA 1280.000, L-21R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, ATM PO201389, DWG 3755856. REMOVED CORRODED FITTING IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. SDR DHL2003604695Attach Fitting · crackedLT MLG W/W FITTING ATTACHING LONGERON 24L AT STA. 940.000 WITH 5.000 CRACK IN IT. PERORMED MAJOR REPAIR IAW SRM 53-2-0 FIG.8. REMOVED DAMAGED FITTING IAW SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. CUT OUT NEW FITTING SRM 53-2-0 FIG.SDR DHL2003604682Door Frame · damagedMAIN CARGO COMPT AFT PASSENGER DOOR JAMB AFT UPPER CORNER HAS INTERIM REPAIR. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 1. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-0 FIG 18 SHEET 3 TR 53-135, DWG SR 08530021, DWG 5750776. FABRICATED FILLER (SDR DHL2003604658Skin · wornFUSELAGE NOSE SECTION EXTERNAL AC POWER RECEPTACLE COMPARTMENT OUTER SKIN WORN STA -39.000 L-31R TO L-33R (MAJOR REPAIR). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW EODHL-030551, ED-3295. CLEANED, TREATED AND PRIMED AREA IAW SRM 51
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