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 UPS01836628Pressure Panel · crackedINSPECTION TYPE:C1,3 RIGHT MLG WHEEL WELL IB. BULKHEAD SUPPORT WEB IS CRACKED STA 879 RBL 4. REPAIRED WEB IAW SRM 53-2-0 FIG 1B.Aug 1, 2001 · N809UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS01836627Fitting · crackedINSPECTION TYPE:C1,3 LEFT WING T/E SUPPORT FITTING IS CRACKED OUTBOARD SIDE OF FLAP HINGE 410 CANOE FITTING. REMOVED AND REPLACED FITTING IAW DWG 4649597, AND SRM 51-1-20D, 51-3-0.Aug 1, 2001 · N809UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS01836602Skin · crackedINSPECTION TYPE:C1,3 LEFT WING L/E LOWER SKIN IS CRACKED AT XFS 635. REPAIRED SKIN IAW DC8-5720-4087-B.Aug 1, 2001 · N809UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836594Skin · damagedINSPECTION TYPE:C1,3 LEFT WING L/E UPPER SKIN HAS SCREWS PULLING THRU SKIN AT XFS 883. REPAIRED SKIN IAW SRM 57-2-1 FIG 2H.Aug 1, 2001 · N809UP · Doug DC873F · Wing, Plate/SkinSDR UPS01836585Skin · crackedINSPECTION TYPE:C1,3 LEFT WING L/E. LOWER SKIN IS CRACKED AT XFS 572.5. REPAIRED SKIN IAW DC8-5720-4087-B.Aug 1, 2001 · N809UP · Doug DC873F · Wing, Plate/SkinSDR DHL2001806006Plank · crackedLEFT WING OUTBOARD FLAP INBOARD HINGE BASE OUTBOARD PLANK CRACKED. NR1301 REMOVED & INSTALLED LT O/B FLAP AS PER DC-8 M/M 27-51-2 OPS CHECKS OK AS PER DC-8 M/M 27-50-0.Aug 1, 2001 · N806DH · Doug DC873F · Trailing Edge FlapsSDR DHL2001806007Plank · crackedON LINE CHECK, LEFT WING OUTBOARD FLAP INBD HINGE BASE OUTBOARD PLANK CRACKED. REMOVED AND REPLACED FLAP AS PER DC8 MAINTENANCE MANUAL 27-51-2.3) OPS CHECK L/H O/B FLAP AS PER DC8 M/M 27-50-0 OPS CHECK OKAug 1, 2001 · N806DH · Doug DC873F · Trailing Edge FlapsSDR UPS03841017Door · leakingIN CLIMB OUT, KEPT INCREASING FLOW TO MAINTAIN DESIRED CAB PRESS FOR F L330. APPROX 5 MIN AFTER REACHING FL330 WE LOSSED CONTROL OF BOTH AUTO AND MANUAL CAB CONTROL. CABIN REACHED FL230 RAN CHECKLIST AND DESEN DED TO FL230. FOUND AIR LEAK AT THE NR 3 PIT DOJul 31, 2001 · N868UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS02839252Skin · crackedINSPECTION TYPE:C2 LEFT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGERS 9,10,12. REMOVED EXISTING DOUBLER, CUTOUT DAMAGE AT XRS 74 STRINGERS 9,10,12, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW UPS ENGINEERING FILE NUMBJul 31, 2001 · N806UP · Doug DC873F · Wing, Plate/SkinSDR RRXA11444Web · crackedDURING A MAINTENANCE VISIT FOUND AT FS 70 WEB ON TORQUE BOX AFT SIDE OF FWD ENTRY DOOR CRACKED. *** CORRECTIVE ACTION *** REMOVED WEB, FABRICATED AND INSTALLED WEB AND DOUBLER IAW SRM 51-1-20D, 53-2-0, 51-1-21 AND DWG 5642063Jul 31, 2001 · N873SJ · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA11434Panel · crackedDURING A MAINTENANCE VISIT FOUND LT ELEVATOR LEADING EDGE PANEL 73 CRACKED. REPLACED PANEL REF DC8 MM 20-15-0Jul 31, 2001 · N873SJ · Doug DC873F · Elevator StructureSDR DHL2001805016Uplock · out of adjAFTER T/O UPLATCH CHECK FAIL GEAR NOT LATCH LIGHT AND LT GEAR UNSAFE LIGHT ILLUM W/AURAL WIND SOUND ACCOMPANYING LIGHTS. SOUNDS OF GEAR IN WIND PERFORMED ABNORMAL PROCEDURE - ON HELP.ACCOMPLISHED T/SHOOTING AND FOUND MAIN GEAR UPLATCH MECH INTERMITTENTLY ON LJul 31, 2001 · N805DH · Doug DC873F · Landing Gear Retraction/Extension SystemSDR DHL2001801009Autopilot Sys · malfunctionedAUTOPILOT DOES UNCOMMANDED DISENGAGE, WILL NOSE DOWN WITH ATTEMPTED REENGAGE. TRIM NORMAL AFTER DISENGAGE. REPLACED AUTOPILOT PITCH CHANNEL OPS CHECKS GOOD IAW DC8 MM 22-13-1 PN ON 2588789-901 S/N ON 0180236.Jul 31, 2001 · N801DH · Doug DC873F · Autopilot SystemSDR RRXA11443Link · chafedDURING A MAINTENANCE VISIT FOUND RT FLAP FWD LINK HINGE WITH EXCESSIVE CHAFED DAMAGE AT STA 340. REPLACED RH FLAP FWD LINK HINGE AT STA 340.Jul 30, 2001 · N873SJ · Doug DC873F · Trailing Edge FlapsSDR RRXA11442Web · crackedDURING A MAINTENANCE VISIT FOUND WEB CRACKED AT STA 280 L21L TO L20L. *** CORRECTIVE ACTION *** FABRICATED AND INSTALLED REPLACEMENT PART PER DHSK 873948.Jul 30, 2001 · N873SJ · Doug DC873F · Fuselage Structure (General)SDR RRXA11441Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACKED FITTING AT STA 1200 L33R - L34R. *** CORRECTIVE ACTION *** REPLACED CRACKED FITTING AT STA 1200 L33R TO L34R PER DC8 SRM 53-2-0 FIG 20Jul 30, 2001 · N873SJ · Doug DC873F · Fuselage Structure (General)SDR RRXA11440Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION ON FRAME AT STA 70 BELOW CUSP FROM L21L TO L21R. *** CORRECTIVE ACTION *** REPLACED STA 70 FRAME BELOW CUSP FROM L21L TO L21R DUE TO CORROSION, REF DC8 SRM 51-1-21, 51-1-21D, 51-3-0, 51-9-0, 51-1-11, 53-2-5 AND SRO 8Jul 30, 2001 · N873SJ · Doug DC873F · Fuselage Structure (General)SDR RRXA11439Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION ON SEAT TRACK AT STA 46-330 LBL63. *** CORRECTIVE ACTION *** REPLACED CORRODED SEAT TRACK AT STA 160 LBL63 PER DC8 SRM 53-7-1 FIG 9 AND SRM 53-2-3 FIG 8A.Jul 30, 2001 · N873SJ · Doug DC873F · Fuselage Structure (General)SDR RRXA11438Frame · damagedDURING A MAINTENANCE VISIT FOUND FRAME AT STA 1140 L31L TO L34R WITH NUMEROUS MISDRILLED HOLES. *** CORRECTIVE ACTION *** REPLACED FRAME AT STA 1140 L31L TO L34R DUE TO MUMEROUS MISDRILLED HOLES PER DHSK 873-816Jul 30, 2001 · N873SJ · Doug DC873F · Fuselage Structure (General)SDR RRXA11437Fitting · crackedDURING A MAINTENANCE VISIT FOUND LT W/W TRAPAZOID FITTING CRACKED. REPLACED PER DAC DWG 5750127, DC8 SRM 51-1-21, 51-1-20D AND OHM 13-1-6Jul 30, 2001 · N873SJ · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA11436Web · damagedDURING A MAINTENANCE VISIT FOUND TORQUE BOX WEB IN C-PIT HAS LITE SURFACE CORROSION AND IS MIS DRILLED. *** CORRECTIVE ACTION *** FABRICATED REPLACEMENT PER DAC DWG 9754948 AND INSTALLED PER DC8 SRM 51-1-21 AND 51-1-20D STA 1180 L31RJul 30, 2001 · N873SJ · Doug DC873F · Fuselage Structure (General)SDR RRXA11428Fitting · crackedDURING A MAINTENANCE VISIT FOUND BAHTUB FITTING IS CRACKED AT STA 1180 BETWEEN L35R AND L34R. *** CORRECTIVE ATION *** REMOVED AND REPLACED BATH TUB FITTING IAW DC8 SRM 53-2-0 FIG 20 AND DWG 63755843Jul 29, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA11432Longeron · corrodedDURING A MAINTENANCE VISIT FOUND L31L CORRODED BEYOND LIMITS AT STA 450-520. REPLACED SECTION PER DHSK 873-508Jul 29, 2001 · N873SJ · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA11431Frame · corrodedDURING A MAINTENANCE VISIT FOUND FRAME AT STA 70 CORRODED SEVERAL SPOTS FROM L21L TO L21R. REPLACED PER DC8 SRM 53-2-0 FIG 2Jul 29, 2001 · N873SJ · Doug DC873F · Fuselage Main, FrameSDR RRXA11430Frame · corrodedDURING A MAINTENANCE VISIT FOUND FRAME AT FS 1120 HAS HEAVY CORROSION BETWEEN LONGERONS 35L - 35R. *** CORRECTIVE ACTION *** CUT OUT DAMAGED AREA OF FRAME IAW SRM 53-2-0 FIG2. FRABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW SRM 53-2-0 FIG 2Jul 29, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA11429Fitting · corrodedDURING A MAINTENANCE VISIT FOUND LONGERON TIE FITTING AT FS 70 AND L22R HAS EXFOLIATION CORROSION. *** CORRECTIVE ACTION *** REMOVED AND REPLACED LONGERON TIE FITTING IAW DC8 SRM 51-1-21, 51-1-20D,51-3-0 AND DWG 464067NJul 29, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA11427Longeron · corrodedDURING A MAINTENANCE VISIT FOUND STABLONGERONS (2 EACH) AT STA 58-70, L35L AND L35R HAVE HEAVY CORROSION. *** CORRECTIVE ACTION *** LONGERONS FOUND OUT OF LIMITS PER SRM 53-2-0 FIG 1F AND SRM 53-3-3. FABRICATED 2EA REPLACEMENT LONGERONS PER DWG 3702969 AND IJul 29, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA11426Frame · corrodedDURING A MAINTENANCE VISIT FOUND FRAME AT STA 580 HAS CORROSION BETWEEN L35L - L35R. *** CORRECTIVE ACTION *** REMOVED AND REPLACED FRAME SECTION IAW DC8 SRM 53-2-0 FIG 2, FABBED SPLICE ANGLES AND STRAPS IAW DC8 SRM 53-2-0 FIG 2. INSTALLED SPLICE ANGLES ANDJul 29, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA11424Plate · corrodedDURING A MAINTENANCE VISIT FOUND LONGERON AND SKIN CORRODED AT L24 R TO L22R AT STA 574 AT APU BLANKING PLATE. MADE REPAIR BY BLENDING OUT AREA, FABRICATING REPAIR PART AND INSTALLING IAW DHSK 873-536Jul 29, 2001 · N873SJ · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA11425Former · crackedDURING A MAINTENANCE VISIT FOUND F/S 64 LBL 55 FORMER FOR L1 DOOR HAS A 1 3/4" CRACK AT L22L. *** CORRECTIVE ACTION *** STOP DRILLED CRACK IAW SRM 53-2-0 FIG 1B. FABRICATED REPAIR ANGLES IAW SRM 53-2-0 FIG 1B, INSTALLED REPAIR ANGLES IAW SRM 51-1-20DJul 28, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA11423Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION ON INTERNAL DOUBLER STA 35-55 L26R TO L30R. REPLACED INTERNAL DOUBLER STA 35-55 L26R TO L30R DUE TO CORROSION. REF DC8 SRM 51-1-21,51-1-20D, 53-1-0 AND DWG5649028Jul 26, 2001 · N873SJ · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA11422Longeron · crackedDURING A MAINTENANCE VISIT FOUND LONGERON 30R CRACKED AND CORRODED BETWEEN STA 8-70. REPLACED LONGERON 30R DUE TO CRACK AND CORROSION FROM STA 8 - 70 PER DC8 SRM 51-1-21, 51-1-20D AND DWG 3648667Jul 26, 2001 · N873SJ · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA1136Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LOWER BELLY SKIN AT STA. 600-680 AND L33R-L34L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED SKIN REPAIR AND INSTALLED IAJul 26, 2001 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA11337Door · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO R/H KEEL PRESSURE PANEL AT STA. 705, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORRJul 26, 2001 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA11421Structure · crackedDURING A MAINTENANCE VISIT FOUND NR 3 ENGINE RT INLET STRAKE LWR MOUNTBRACKET CRACKED. REMOVED DAMAGED BRACKET, FABRICATED AND INSTALLED NEW BRACKET IAW DWG D51B11810 AND SRM 51-1-21Jul 24, 2001 · N873SJ · Doug DC873F · Engine Air Intake SystemSDR DHL2001806005Smoke Detector · malfunctionedDURING SMOKE DETECTION CHECK APPEARS MESSAGE "AC6781 FALSE ALARM" ON CDU. R&R SMOKE DETECTOR UNIT IAW MM26-15-05. TESTED SMOKE DETECTION SYSTEM OK NOW.Jul 24, 2001 · N806DH · Doug DC873F · Smoke DetectionSDR RRXA11420Fitting · corrodedDURING A MAINTENANCE VISIT FOUND AT STA 70 L23R LONGERON TIE FITTING CORRODED BEYOND LIMITS. *** CORRECTIVE ACTION *** REMOVED AND REPLACED PER DC8 SRM 51-1-21, 51-1-21D, 51-3-0 AND DWG 6464067Jul 20, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA11419Fitting · corrodedDURING A MAINTENANCE VISIT FOUND LONGERON TIE FITTING CORRODED BEYOND LIMITS AT STA 70 L34R. *** CORRECTIVE ACTION *** REMOVED AND REPLACED PER DC8 SRM 51-1-21,51-1-21D, 51-3-0 AND DWG 4611067Jul 20, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR UPS01836384Light · inoperativeINSPECTION TYPE:N/A, LIGHT INOP IN EMERGENCY LIGHT ASSY AT ENTRY DOOR. RELAMPED AS REQ, EMERGENCY LIGHTS CK GOOD.Jul 20, 2001 · N811UP · Doug DC873F · Emergency LightingSDR RRXA11433Seat Track · damagedDURING A MAINTENANCE VISIT FOUND CABIN SEAT TRACK DAMAGED AT FS1030 TO FS 1040 RBL 24. *** CORRECTIVE ACTION *** REMOVED, FABRICATED AND REPLACED SEAT TRACK FS 990 - FS1210 RBL24 IAW SRM 53-2-2A, 53-2-3 FIG 14, 51-1-8, 51-3-0 AND 51-1-20D.Jul 19, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR DHL2001804014Smoke Detector1) NO 5 SMOKE DETECTOR INOP2) MAY BE INOP PER MEL 26-6-1 DMI #6439 PLACARD INSATALLEDSTATUS: CLOSEJul 19, 2001 · N804DH · Doug DC873F · Smoke DetectionSDR DHL2001806019Window · lack of lubeCAPT'S/LEFT SLIDING WINDOW REQUIRES AT LEAST 20 LBS PULL FORCE TO OVERCOME BINDING RESISTANCE TO HOOK UNLATCHING PART OF WINDOW MECHANISM. LUBED CAPT'S SLIDING WINDOW, CLEARED TAPE FROM UPPER EDGE. OPS CHECK OK IAW MM 56-10-3.Jul 18, 2001 · N806DH · Doug DC873F · Flight Compartment WindowsSDR RRXA11418Door · crackedDURING A MAINTENANCE VISIT FOUND R/H I/B SLOT UPPER PANEL CRACKED. *** CORRECTIVE ATION *** NDT MARKED END OF CRACK REF NDT SPM 06-10-01001. OPENED SLOT DOOR IAW MM 27-80-1, STOP DRILLED CRACK PER DHSK 873-943. FABRICATED DOUBLER IAW DHSK 873-943, INSTALLEDJul 18, 2001 · N873SJ · Doug DC873F · Leading Edge Slat Control SystemSDR DHL2001804013Smoke Detector1) #5 SMOKE DETECTOR INOP2) RELAMPED SMOKE DETECTOR OPS CHECKED GOOD PER MM 26-10-5STATUS: CLOSEDJul 18, 2001 · N804DH · Doug DC873F · Smoke DetectionSDR RRXA11417Angle · corrodedDURING A MAINTENANCE VISIT FOUND LWR CARGO COMPT C-PIT ATTACH ANGLE CORRODED AT STA 1040 L36. *** CORRECTIVE ACTION *** REPAIRED FRAME IAW 8110-3 APPROVED DHSK 873-510Jul 17, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA010058HoseON LANDING ROLL LOST HYD PRESS AND QTY *** CORRECTIVE ACTION *** FOUND HOSE ON R/H BOGIE TRIM CYL HAD SEPARATED FROM FITTING- R AND R HOSE IAW 20-12-0 LK CK GOODJul 17, 2001 · N602AL · Doug DC873F · Main Landing Gear Strut/Axle/TruckSDR UPS01836441Splice · crackedINSPECTION TYPE:C1 STA 440-460 LONG 14L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3887799,AND SRM. 51-1-20D, 51-1-21Jul 17, 2001 · N874UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA11335Splice Plate · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO AFT ACCY COMPARTMENT SPLICE PLATE AT STA.1580-1600 AND LBL46, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAJul 17, 2001 · N606AL · Doug DC873F · Fuselage Main, StructureSDR RRXA11334Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BELLY SKIN AT STA.-21TO70 AND L31L-L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DHSK 606-485Jul 17, 2001 · N606AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA11416Fitting · corrodedDURING A MAINTENANCE VISIT FOUND LWR CARGO COMPARTMENT C-PIT LONG SPLICE FITTING CORRODED AT STA 1050 L31R *** CORRECTIVE ACTION *** REMOVED AND REPLACED FITTING IAW DC8 SRM 53-1-0, 51-1-20D AND DWG 3750257Jul 16, 2001 · N873SJ · Doug DC873F · Fuselage Main, Structure
Back to Douglas DC-8-73F