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.

SDR UPS02838770Door Frame · crackedINSPECTION TYPE:C2 R3 DOOR UPPER AFT CORNER HAS CRACK INDICATION FOUND BY RADIOGRAPHIC INSPECTION. REPAIRED DOOR JAMB CORNER IAW DC8 SRM 53-2-0 FIG 16.Jun 25, 2002 · N802UP · Doug DC873F · Fuselage Main, StructureSDR UPS02838769Door Frame · crackedINSPECTION TYPE:C2 R3 DOOR LOWER FORWARD CORNER HAS CRACK INDICATION FOUND BY RADIOGRAPHIC INSPECTION. REPAIRED DOOR JAMB CORNER IAW DC8 SRM 53-2-0 FIG 17.Jun 25, 2002 · N802UP · Doug DC873F · Fuselage Main, StructureSDR DHL2002806511Panel · delaminatedDURING C-CHECK FOUND RT WING T/E LWR PANEL INNER AND EXTERNAL SKIN DELAMINATED BETWEEN XW 5.000 TO XW 33.000. REMOVED AND REPLACED DELAMINATED PANEL PER SRM 51-3-0 PG 7 AND SRM 51-31 PG 1.Jun 24, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2002806509Panel · delaminatedDURING C-CHECK FOUND FUSELAGE LWR FILLET 728 RT EXTERNAL SKIN DELAMINATED. REMOVED DELAMINATED FILLET PANEL PER SRM 51-3-0 PG 1. INSTALLED NEW FILLET PANEL PER SRM 51-3-0 PG 1.Jun 24, 2002 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2002806505FilletDURING C CHK FOUND LWR FUESLAGE SIN FILLET # 741 EXTERNAL SKIN DELAMINATED (STA.1080.000-1100.000)REMOVED FILLET# 741 PER SRM 51-3-0 PG 1.CLEANED TREATED AND PRIMED AREA PER SRM 51-18B.INSTALLED NEW FILLET PER SRM 51-3-0 PG7 AND SRM 51-3-1 PG7.Jun 24, 2002 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS02838912Skin · crackedINSPECTION TYPE:C2 FUSELAGE EXTERIOR SKIN CRACKED FS 1724 L15R. REPAIRED AREA IAW DC8 SRM 53-2-1.Jun 23, 2002 · N802UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS02838771Door Frame · damagedINSPECTION TYPE:C2 L1 DOOR CORNER UPPER FWD DOUBLER DOES NOT MEET SRM REQUIREMENTS. REPAIRED DOOR JAMB CORNER IAW DC8 SRM 53-2-0 FIG 15.Jun 22, 2002 · N802UP · Doug DC873F · Fuselage Main, StructureSDR UPS02838684Fitting · looseINSPECTION TYPE:N/A, AT 1 HOUR AND 35 MIN AFTER TAKEOFF, NR 3 ENGINE FLAMED OUT IN MODERATE TURBULENCE AND RAIN. FLAME-OUT OCCURRED AT 35,000 FEET AND MUCH .80. ATTEMPTED INFLIGHT ENGINE START AT 35,000, WAS UNSUCCESSFUL. PERFORMED FLAME-OUT INSP PER M/M 71Jun 19, 2002 · N818UP · Doug DC873F · Engine Fuel DistributionSDR 2003F00055Floorbeam · corrodedFOUND DURING DOUGLAS D-CHECK INSPECTION, AT STATION 1600 LBL 42 INCH FLOORBEAM UPPER FLANGE LOWER SURFACE HAS 1 INCH BY 2 INCH CORRODED BEYOND LIMITS. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLER, FILLER IAW EO NR 02-039. TREATED, PRIMEDJun 17, 2002 · N961R · Doug DC873F · Fuselage Main, Floor BeamSDR UPS02838679Skin · crackedINSPECTION TYPE:C1, L1 DOOR UPPER FWD DOOR JAMB CORNER CRACKED, FOUND BY X-RAY INSPECTION. ROUTED OUT CRACKED SKIN IAW DC8 SRM 53-2-0 FIG 15. VERIFIED CRACK REMOVAL IAW HFEC WPM 06-10-01.001. REMOVED EXISTING DOUBLER, TRIPLER DOOR SILL, OVERHEAD WEB AND DOOJun 15, 2002 · N803UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS02838676Longeron · corrodedINSPECTION TYPE:C1 L31L STA 620-650 HAS EXFOL CORROSION. FABBED NEW LONGERON IAW DAC DWG 3750575. FABBED LONGERON CLIP IAW DAC DWG 5610416. LOCATE NEW SPLICE FITTING, DRILLED EXISTING FASTENER HOLES, INSTALLED NEW LONGERON SPLICE FITTING.Jun 14, 2002 · N803UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS02838642Light · malfunctionedINSPECTION TYPE:PFLT COCKPIT EMERGENCY LIGHTS ILLUMINATED BUT UNABLE TO EXTINGUISH AFTER RESET AND ARMED. PERFORMED OPERATIONAL CHECK PER MM 33-50-01 OPS CHECKS OK.Jun 14, 2002 · N852UP · Doug DC873F · Emergency LightingSDR UPS02838678Doubler · corrodedINSPECTION TYPE:C1 AC COMPT FS 24 L35R STRAP UNDER SHEAR TIE SKIN UNDER STRAP IS CORRODED. REMOVED AND REPLACED DOUBLER 2 SHEAR TIES STRAP LONGERONS L36, L35 AND L35R IAW DC8 SRM 53-2-1 PG 113, 51-1-21, 51-1-20D.Jun 12, 2002 · N803UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS02838655Skin · crackedINSPECTION TYPE:C1 R1 DOOR AFT DOOR JAMB CRACKED AT FASTENER HOLE APPROX LENGTH .375 INCH LONG ON FUSELAGE SKIN. ROUTED OUT CRACK IN EXTERIOR SKIN VERIFIED CRACK REMOVAL IAW HFEC NDT SPM 06-16-01-001. FABBED FILLER DOUBLER AND TRIPLER IAW DC8 SRM 53-2-0 FIG Jun 12, 2002 · N803UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2002804008Connector1) ENG #2 SHORT CIRCUIT FIRE WARNING LOOP "B" LIGHT ON. LOOP "A" OK LOOP "B" SHORT INTERMITTENT2) CHECKED WIRING AS PER WDM 26-01-01, ALL FOUND OK. ITEM TRANSF TO DMI 9566 IAW MEL 26-3-23) REF DMI 9566 ENGÑ2 SHORT CIRCUIT FIRE WARNING LOOP B LIGHT ON. LOOPJun 12, 2002 · N804DH · Doug DC873F · Fire Protection System WiringSDR 2002F01102Web · crackedFOUND DURING DOUGLAS D-CHECK INSPECTION, RIGHT INBOARD FLAP INBOARD WEB HAS PREVIOUS REPAIR CRACK EXTENDS TO NEW STOP DRILL AT END OF CRACK BEYOND REPAIR DOUBLER. STOP DRILLED END OF CRACK IAW DC-8 SRM 57-2-0. FABRICATED DOUBLER IAW DC-8 SRM 57-2-0, FIG 2. Jun 11, 2002 · N961R · Doug DC873F · Trailing Edge FlapsSDR 2002F01101Spar Cap · crackedFOUND DURING DOUGLAS D-CHECK INSPECTION, RIGHT WING LOWER FRONT SPAR CAP FORWARD TANG APPROXIMATELY STATION 520 SPAR CAP HAS CRACK. REMOVED INTERNAL REPAIR ANGLE FOR EVALUATION IAW DC-8 SRM 51-1-20D. REPAIR IS ACCEPTABLE AS TEMP REPAIR PER BOEING LETTER TEK-Jun 11, 2002 · N961R · Doug DC873F · Wing SparSDR 2002F01100Longeron · crackedFOUND DURING DOUGLAS D-CHECK INSPECTION, REPAIR AT STATION 55 LEFT LONGERON 31 HAS NO SUPPORTING DOCUMENTATION. REMOVED DOUBLER IAW DC-8 SRM 51-1-21. CRACK HAD EXTENDED .5 BEYOND STOP DRILL. STOP DRILLED CRACK IAW DC-8 SRM 53-2-0. FABRICATED REPAIR DOUBLERJun 11, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS02838587Battery Pack · dischargedINSPECTION TYPE:IN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01, OPS CHECK NORMAL.Jun 11, 2002 · N851UP · Doug DC873F · Emergency LightingSDR DHL2002801013Bulb1) MAIN DECK CARGO COMPT. DETECTOR #6 WONT TEST2) ENTERED ON DMI # 9542 IAW DHL MEL 26-6 CAT C PLACARD INSTALLED MARTIN 211513) REFER DMI #9542 MAIN DECK CARGO COMPT DETECTOR #6 WONT TEST4) RELAMPED #6 SMOKE DETECTOR BEACON TEST BULBS OPS CHECK NORMAL IAW Jun 9, 2002 · N801DH · Doug DC873F · Smoke DetectionSDR 2002FA0000724Longeron · damaged(LONGERON 24/ FITTING) FOUND DURING (D) CHECK INSPECTION, STA 960 AND LONGERON 24L HOLES ELONGATED IN FITTING AND LONGERON 24 TWO FORWARD.Jun 8, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/StringerSDR 2002FA0000723Panel · corroded(BULKHEAD PANELS) FOUND DURING (D) CHECK INSPECTION. RIGHT W/W STA. 980 CNAT BULKHEAD PANELS HAVE CORROSION SPOTS FROM LONG 24R TO LONGERON 25R.Jun 8, 2002 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2002805049Connector1) #2 ENG "B" SYS LOOP (FIRE) WILL NOT TEST2) R&R FIRE LOOP CONNECTOR PER DC8 WDM 26-01-01 & STANDARD WIRE PRACTICES CHAPT 20. OPS CK SERVICABLE.Jun 8, 2002 · N805DH · Doug DC873F · Fire Protection System WiringSDR 2002F01098Fitting · corrodedFOUND DURING DOUGLAS D-CHECK INSPECTION, RIGHT LONGERON AND BATHTUB FITTING STATION 960 AFT SIDE HAS SPOT OF SURFACE CORROSION. REMOVED CORROSION FROM LONGERON 24R AND BATHTUB FITTING IAW DC-8 SRM 51-1-8. LONGERON 24 REPAIRED. REMOVED AND REPLACED BATHTUB FJun 7, 2002 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2002806517Former · crackedDURING C-CHECK, FOUND LT WING O/B LEADING EDGE FORMER CRACKED .5 INCH. STOP DRILLED CRACK PER SRM 57-2-0 PG 9-10. FABRICATED DOUBLER PER SRM 57-2-0 PG 9-10. INSTALLED DOUBLER WITH NEW FASTENERS PER SRM 57-2-0 PG 9-10 AND SRM 51-1-21 PG 1.Jun 7, 2002 · N806DH · Doug DC873F · Wing Main, Frame StructureSDR UPS02838674Door Frame · damagedINSPECTION TYPE:C1 RT FWD DOOR UPPER FWD ELONGATED HOLE ON FRAME. FABBED DOUBLER IAW DAC DWG 5615762 AND INSTALLED SAME IAW DC8 SRM 51-1-21.Jun 7, 2002 · N803UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS02838652Fitting · crackedINSPECTION TYPE:C1 STA 940 RT FRAME FITTING AT PRESSURE WEB IS CRACKED. REMOVED INTERCOSTAL AND FITTING L21 LOCATED & DRILLED NEW FITTING IAW DAC DWG 5751966 INSTALLED END FITTING AND INTERCOSTAL IAW DC8 SRM 51-1-20D.Jun 7, 2002 · N803UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02838596Intercostal · crackedINSPECTION TYPE:C1 R1 DOOR FWD TORQUE BOX INTERCOSTAL JUST ABOVE LOWER CLEAR HINGE IS CRACKED. REMOVED INTERCOSTAL, FAB INTERCOSTAL IAW DAC DWG 5615700, ALODINED & PRIMED IAW DC8 SRM 51-1-21 & 511-20D.Jun 7, 2002 · N803UP · Doug DC873F · Service DoorsSDR DHL2002804007Smoke Detector · inoperativeNR 5 SMOKE DETECTOR WILL NOT TEST. RELAMPED NR 5 SMOKE DETECTOR IAW MM REF 26-10-1, GROUND OP CHECK GOOD.Jun 7, 2002 · N804DH · Doug DC873F · Smoke DetectionSDR 2002F01104Skin · damagedFOUND DURING DOUGLAS D-CHECK INSPECTION, REPAIR AT STATION 275 RIGHT 31 AND 32 HAS NO SUPPORTING DOCUMENTATION. REMOVED REPAIR IAW DC-8 SRM 51-1-20D. FABRICATED FILLER, DOUBLER. TREATED AND PRIMED AND INSTALLED REPAIR PER EO NR 02-039, WITH APPROVED 8110-3 Jun 5, 2002 · N961R · Doug DC873F · Fuselage Main, Plate/SkinSDR 2002F01103Longeron · crackedFOUND DURING DOUGLAS D-CHECK INSPECTION, REPAIR AT STATION 300 RIGHT LONGERON 33 HAS NO SUPPORT DOCUMENTATION. REMOVED DOUBLER IAW DC-8 SRM 51-1-21. IT IS ACCEPTABLE TO USE EXISTING FILLER. FABRICATED NEW DOUBLER. TREATED AND PRIMED ALL PARTS AND INSTALLED Jun 5, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/StringerSDR 2002F01105Frame · corrodedFOUND DURING DOUGLAS D-CHECK INSPECTION, STATION 460 HAS CORROSION ON FRAME BETWEEN STRINGERS 2/3 LEFT. REMOVED CORROSION. FOUND OUT OF LIMITS. FABRICATED REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-4, 53-2-0 AND 53-2-0, FIG 1F.Jun 4, 2002 · N961R · Doug DC873F · Fuselage Main, FrameSDR 2002F01095Fitting · corrodedFOUND DURING DOUGLAS D-CHECK INSPECTION, LONGERON 24L SURFACE CORROSION ON BOTH SIDES OF BATHTUB FITTING STATION 940 AT LONGERON ATTACH. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED AND REPLACED BATHTUB FITTING STATION 940 IAW DC-8 SRM 51-1-24, 51-3-0. Jun 3, 2002 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR 2002F01094Skin · corrodedFOUND DURING DOUGLAS D-CHECK INSPECTION, LIGHT SURFACE CORROSION ON LOWER CENTER FUSELAGE AREA BETWEEN CENTER WING STRINGERS 67 AND 68 5 INCHES RIGHT OF ECWO. CORROSION OUT OF LIMITS STATION 759-768, 6 INCHES RIGHT OF CENTER LINE, ITEM 4 ON FORM 84. REMOVED Jun 3, 2002 · N961R · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS02838578Attach Angle · corrodedINSPECTION TYPE:C1 AFT LWR ATTACH STRUCTURE FOR RADIO RACK CLOSEOUT PANEL HAS LIGHT CORROSION AND BARE METAL ON INTERNAL AND EXTERNAL SIDES. REMOVED ANGLE IAW DC8 SRM 53-2-9 AND IAW DAC DWG 564057 1. FABBED IAW DAC DWG 5640571, INSTALLED CHANNEL IAW DC8 SRM Jun 3, 2002 · N803UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02838675Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN 680 S11L LONGERON FITTING CRACKED. REMOVED FITTING, ALODINED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 51-1-20D, 51-1-24.Jun 2, 2002 · N803UP · Doug DC873F · Fuselage Miscellaneous StructureSDR 2002FA0000720Longeron · corroded(LONGERON/BATHTUB FITTING) FOUND DURING (D) CHECK INSPECTION, LEFT LONGERON, LEFT LONGERON, 24 STA. 960.Jun 2, 2002 · N961R · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS02838594Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN 680 S11L LONGERON FITTING CRACKED. REMOVED FITTING, ALODINED, PRIMED & INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 51-1-20D & 51-1-24.Jun 2, 2002 · N803UP · Doug DC873F · Fuselage Miscellaneous StructureSDR COOSDR02104Panel · delaminatedLEFT WING, OUTER WING TRAILING EDGE, UPPER FIXED PANEL DELAMINATED.Jun 1, 2002 · N605AL · Doug DC873F · Wing, Plate/SkinSDR COOSDR02103Skin · damagedHORIZONTAL STABILIZER RIGHT ELEVATOR GEAR TAB SKIN, INTERNAL DOUBLERS AND HONEY COMB CORE DAMAGE.Jun 1, 2002 · N605AL · Doug DC873F · Elevator, Tab StructureSDR COOSDR02095Fitting · corrodedAFT CARGO COMPARTMENT, AT STA 1445 LONGERON 34R LEVEL, SUPPORT FITTING HEAVY CORROSION.Jun 1, 2002 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR COOSDR020089Flap · damagedRIGHT WING INBOARD FLAP BAKELITE, DAMAGED.Jun 1, 2002 · N605AL · Doug DC873F · Trailing Edge FlapsSDR COOSDR020088Fitting · corrodedAFT LOWER CARGO COMPARTMENT, FITTING CORRODED.Jun 1, 2002 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR COOSDR020087Fitting · crackedAFT LOWER CARGO COMPARTMENT, FITTING CRACKED.Jun 1, 2002 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR COOSDR020086Stiffener · crackedLEFT WING TRAILING EDGE FIXED PANEL STIFFENER, CRACKED.Jun 1, 2002 · N605AL · Doug DC873F · Wing Miscellaneous StructureSDR COOSDR020085Angle · crackedAFT CARGO COMPARTMENT SUPPORT ANGLE CRACKED.Jun 1, 2002 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR COOSDR020084Fitting · corrodedMAIN CARGO CABIN FITTING, CORRODED.Jun 1, 2002 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR COOSDR020083Fitting · crackedAFT CARGO COMPARTMENT FITTING, CRACKED.Jun 1, 2002 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR COOSDR020082Fitting · crackedAFT CARGO COMPARTMENT FITTING, CRACKED.Jun 1, 2002 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR COOSDR020081Fitting · corrodedMAIN CARGO CABIN FITTING, CORRODED.Jun 1, 2002 · N605AL · Doug DC873F · Fuselage Miscellaneous Structure
Back to Douglas DC-8-73F