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 UPS02839249Skin · corrodedINSPECTION TYPE:C2 LEFT WING CENTER L/E UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 366.5. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 57-2-0 FIG 7, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-2- 1 FIG 38.Jul 30, 2002 · N806UP · Doug DC873F · Wing, Plate/SkinSDR UPS02839247Seat Track · damagedINSPECTION TYPE:C2 CABIN FLOOR SEAT TRACK IS WORN AND BROKEN AT LBL 45 STA 1590-1600. REMOVED DAMAGED SEAT TRACK STA 1590 TO 1680 LBL 45, FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK SECTION IAW SRM 53-2-3 FIG 8A.Jul 30, 2002 · N806UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS02839246Angle · crackedINSPECTION TYPE:C2 BULKHEAD FWD OF RT WHEEL WELL STA 851 RBL 50 L ANGLE FITTING IS CRACKED. NDT VERIFIED CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-2-0 FIG 2.Jul 29, 2002 · N806UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS02839245Skin · crackedINSPECTION TYPE:C2 REMOVE STAINLESS STEEL DOUBLER ON THE R1 DOOR LOWER AFT CORNER AND REPAIR PER DC8 SRM 53-2-0 FIG 14. REMOVED EXISTING REPAIR, NDT VERIFIED NO CRACKS AROUND EXISTING CUTOUT, FABRICATED AND INSTALLED DOUBLER, FILLER, AND TRIPLER IAW SRM 53-2-Jul 29, 2002 · N806UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS02839244Skin · crackedINSPECTION TYPE:C2 REMOVE STAINLESS STEEL DOUBLER ON THE L2 DOOR LOWER FWD CORNER AND REPAIR PER DC8 53-2-0 FIG 18. REMOVED EXISTING REPAIR, NDT VERIFIED NO CRACKS AT PREVIOUS CUTOUT, FABRICATED AND INSTALLED DOUBLER TRIPLER AND FILLER IAW SRM 53-2-0 FIG 18.Jul 29, 2002 · N806UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS02839242Skin · crackedINSPECTION TYPE:C2 REMOVE STAINLESS STEEL DOUBLER ON L1 DOOR UPPER FWD CORNER AND REPAIR PER DC8 SRM 53-2-0 FIG 15. REMOVED EXISTING REPAIR, CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 5Jul 29, 2002 · N806UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS02839241Skin · crackedINSPECTION TYPE:C2 LEFT WING L/E LOWER SKIN IS CRACKED AT DRAIN HOLE AT XFS 597.5. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5720-4087.Jul 29, 2002 · N806UP · Doug DC873F · Wing, Plate/SkinSDR UPS02839240Rib · crackedINSPECTION TYPE:C2 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 616.25. STOP DRILLED CRACK, NDT VERIFIED NO CRACKS AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2.Jul 29, 2002 · N806UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS02839238Skin · corrodedINSPECTION TYPE:C2 LEFT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION IB OF XFS 710. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 2H.Jul 29, 2002 · N806UP · Doug DC873F · Wing, Plate/SkinSDR DHL2002806535Rudder · wornN/R 2473 RUDDER OUTER PLATING AROUND ZR101.000 RH SIDE(MAJOR REPAIR)CORR: PERFORMED MAJOR REPAIR IAW EO DHL020626 , ED-3111, EO SEMAN 2002725. REMOVED FASTNERS WITHIN REPAIR AREA IAW SRM51-1-21 PG. 1, TRIMMED OUT DAAGED SHIMN AREA IAW EO DHL 020626, ED3111, EOJul 27, 2002 · N806DH · Doug DC873F · Rudder Control SystemSDR DHL2002806858Door · delaminatedITEM N/R 0072 LH MLG OUTER DOOR SKIN DELAMINATEDCORR:R/R LH MLG OUTER DOOR IAW MM 32-12-1 PG 401 OPS CHECKED GOOD IAW M/M 32-30-0 PG 201Jul 26, 2002 · N806DH · Doug DC873F · Landing Gear Door Retract SectionSDR DHL2002806855Skin · corrodedLT HORIZ STAB INBOARD L/E ELONGATED HOLES & CORRODED STA XFS 178.750. PERFORMED MAJOR REPAIRS. REMOVED CORROSION LT HORIZ STAB L/E AT STA XFS178.750. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12-14. TRIMMED OUT DAMAGED AREA. FABRICATED A REPAIR DOUBLER & TRIPJul 26, 2002 · N806DH · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR UPS02838913Skin · crackedINSPECTION TYPE:N/A CRACK AT PIT 34 UPPER FWD CORNER FUSELAGE SKIN. INSTALLED REPAIR DOUBLERS PER EO DC-8 53-10-17222-A.Jul 25, 2002 · N852UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS02838896Skin · crackedINSPECTION TYPE:PFLT SHEET METAL CRACK ON PIT 34 FWD UPPER DOOR CUTOUT AREA. A/C FERRIED TO SDF 9146. ACCOMPLISHED PERMANENT REPAIR PER SRM 53-2-0.Jul 24, 2002 · N852UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS02838890Battery · dischargedINSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED TEST BATTERY & RELAY UNIT MM 33-50-01.Jul 24, 2002 · N894UP · Doug DC873F · Emergency LightingSDR UPS02839237Skin · damagedINSPECTION TYPE:C2 COMPLY WITH MPI P 13516;PERM REPAIR TO DENT STA -80 TO -74 ON LEFT SIDE ABOVE CUSP ANGLE. REMOVED INTERIN REPAIR, NDT VERIFIED NO CRACKS AT CUTOUT AREA, FABRICATED AND INSTALLED DOUBLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7.Jul 23, 2002 · N806UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2002806857Panel · delaminatedLOWER FUS FILLET NR 742 LT EXTERNAL SKIN DELAMINATED. REMOVED FILLET NR 742 LT IAW SRM 51-3-0 PG 1. INSTALLED NEW FILLET PANEL IAW SRM 51-3-0 PG 1, SRM 51-3-1 PG 1.Jul 23, 2002 · N806DH · Doug DC873F · Aerodynamic FairingsSDR DHL2002806533Spar Cap · corrodedLT WING INBOARD LEADING EDGE UPPER CAP SHOWS CORROSION AND CRACK BETWEEN XFS 20.000 AND XFS 195.000. REMOVED CRACKED UPPER CAP IAW SRM 51-1-20D PAGE 21 AND SRM 51-1-21. INSTALLED NEW UPPER CAP IAW SRM 57-3-3 PAGE 5 DRAWING 9750482, SRM 51-1-21 PAGE 1, SRM 51Jul 23, 2002 · N806DH · Doug DC873F · Wing SparSDR DHL2002801014Battery Pack · dischargedSTANDBY EMERGENCY CHECK INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW 33-50-1 ,TESTED OK.Jul 23, 2002 · N801DH · Doug DC873F · Emergency LightingSDR DHL2002806859Skin · damagedPERFORMED MAJOR REPAIR IAW EO DHL 020621, ED-3095, EO SEMAN 2002684. BLENDED DAMAGED AREAS. FABRICATED REPAIR DOUBLER IAW EO DHL 020621, ED-3095, EO SEMANS 2002684. INSTALLED DOUBLER ON RT WING L/E LOWER SURFACE STA XFS710.000 IAW EO DHL 020621, ED-3095, EOJul 22, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2002806841Skin · corrodedLT WING CENTER L/E LWR SKIN SHOWS CORROSION XFS 420.000. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. TRIMMED OUT AFFECTED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER ON LT WING CENTER L/E LWR SKIN.Jul 21, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2002807010Connector · faultyNR 4 B-FIRE LOOP WILL NOT TEST. REPLACED B-LOOP CONNECTOR ON LT SIDE OF CORE LOOP. SYSTEM CHECKS OK IAW 26-10.Jul 19, 2002 · N807DH · Doug DC873F · Fire DetectionSDR UPS02838848Control Valve · malfunctionedINSPECTION TYPE:N/A ON TAXI OUT A/C FELT LIKE LEFT BRAKES WERE DRAGGING. REMOVED AND REPLACED WHEEL BRAKE CONTROL VALVES PER MM 32-42-02. PERFORMED ADJ /TEST OF SYSTEM, ALL BRAKES OPERATE NORMALLY. A/C OK TO SERVICE.Jul 19, 2002 · N803UP · Doug DC873F · Landing Gear Brake SystemSDR DHL2002806860Skin · damagedLT WING OUTBOARD LEADING EDGE UPPER SKIN HOLES ELONGATED XFS710.000. PERFORMED MAJOR REPAIR IAW EO DHL 020614, ED-3086, EO SEMAN 2002675. TRIMMED OUT DAMAGED SKIN AREA. FABRICATED A REPAIR DOUBLER, A TRIPLER AND A FILLER IAW EO DHL 020614, ED-3086, EO SEMANJul 18, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2002806854Skin Panel · corrodedITEM N/R 0762 RH WING CTR SPAR SKIN CORRODED AROUND STA. XRS 34.500CORR: PERFORMED MAJOR REPAIR IAW EO DHL020609 ED-3094, EO SEMAN 2002683 REMOVED CORROSION ON RH WING IAW SRM 51-1-8 PG. 17-18, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG. 16 REMOVED FASTNERS IAW SRMJul 18, 2002 · N806DH · Doug DC873F · Wing SparSDR DHL2002806537Skin · crackedLT WING STUB WING LEADING EDGE LWR SKIN CRACKED .5 INCH XFS 207.000. FABRICATED AND INSTALLED DOUBLER IAW EO DHL020622, ED-3100, EO SEMAN 2002688, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9.Jul 18, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2002806536Panel · corrodedLT WING T/E SKIN UPPER PANEL SHOWS POINTS OF CORROSION XW47.000 - XW75.312. REMOVED CORROSION IAW SRM 57-1-8 PG 17-18, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. REMOVED DAMAGED PANEL IAW SRM 51-3-0, INSTALLED NEW PANEL ON LT WING T/E UPPER SKIN IAW SRM 51-3-Jul 18, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2002806534Skin · corrodedRT WING L/E SHOWS SPOT OF CORROSION AT STA XW257. REMOVED CORROSION ON RT WING L/E, FOUND OUT LIMITS IAW SRM 57-2-0 PG 16. TRIMMED OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER IAW EO DHL 020615 , ED3091, EO SEMAN 2002678.Jul 17, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2002801015Inertia Reel · malfunctionedSECOND OFFICER'S SHOULDER STRAP STUCK. VERIFIED TO BE STUCK. REMOVED AND REPLACED INERTIA ASSY. OPS CHECKS GOOD IAW DC8 MM 25-11-2.Jul 17, 2002 · N801DH · Doug DC873F · Flight Compartment EquipmentSDR UPS02838812Battery Pack · dischargedINSPECTION TYPE:N/A AFTER ENG START, WENT DARK, EMERGENCY LIGHTS CAME ON, WENT TO DISARM, THEN DISARM CHECK, DISARM, THEN BACK TO ARM. LIGHTS CAME BACK ON. PULLED AND RESET EMERGENCY LIGHTS CONTROL CB AND EMERGENCY LIGHTS CB TO GET THEM TO WORK NORMALLY. REJul 17, 2002 · N852UP · Doug DC873F · Emergency LightingSDR DHL2002806843Skin · corrodedRT STUB WING UPPER SURFACE SKIN CORRODED AROUND XILD42.000 - 257.000. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT AFFECTED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW EO DHL 020613, ED-3083 & EO SEMAN 2002680 SRM51-1-21 PG 1, SJul 16, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2002806842Skin · corrodedRT STUB WING UPPER SURFACE SKIN CORRODED AROUND XILD42.000 - 257.000. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT AFFECTED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW EO DHL 020613, ED-3083 & EO SEMAN 2002680 SRM 51-1-21 PG 1, Jul 16, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR UPS02838815Slide · out of positionINSPECTION TYPE:N/A ESCAPE SLIDE GIRT BAR WOULD NOT ENGAGE. REPACKED AND INSTALLED EVACUATION SLIDE ON MAIN CABIN DOOR IAW DC8-MM 25-60-01.Jul 16, 2002 · N852UP · Doug DC873F · Escape SlideSDR DHL2002806840SkinN/R:2477 LH WING UPPER SURFACE SHIN SHOWS CORROSION STRINGER 9 XRS396.000 ( MAJOR REPAIR)CORR: PERFORMED MAJOR REPAIR IAW SRM 57-2-1 SHEET 1.BLENDED OUT LH WING UPPER SKIN FOUND OUT OF LIMITS IAW SRM57-2-0 PG. 16 CUT CORRODED AREA IAW SRM 57-2-1 FIG. 32 CLEANEJul 12, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2002806504Flange · brokenDURING C-CHECK, FOUND LT FWD AUX TANK UPPER CAP FLANGE 2 BROKEN AT STA XFS 20.000. FABRICATED DOUBLER PER SRM 57-2-0 FIG 2. INSTALLED DOUBLER PER SRM 57-2-0 FIG 2.Jul 10, 2002 · N806DH · Doug DC873F · Wing Miscellaneous StructureSDR UPS02838882Skin · crackedINSPECTION TYPE:C2 R1 AFT LOWER DOOR JAMB CORNER HAS CRACKED EXT FUSELAGE SKIN AT FASTENER HOLE FOUND BY EDDY CURRENT INSP. CUT OUT DAMAGE, PERFORMED EDDY CURRENT INSP AFTER DAMAGE REMOVAL IAW DOUGLAS NDT SPM 06-10-01.001, NO CRACKS NOTED. FABBED DOUBLER TRIJul 10, 2002 · N802UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS02838767Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS STAY ON WITH AC POWER ON GENERATORS. REMOVED EMERGENCY EXIT LIGHT BATTERY PACK, OPS OK.Jul 10, 2002 · N804UP · Doug DC873F · Emergency LightingSDR UPS02838881Clip · crackedINSPECTION TYPE:C2 FWD PIT STA 380 INTERCOSTAL ATTACH CLIP IS CRACKED L33L. REMOVED CLIP, FABBED CLIP IAW DAC DWG 5750726-93, AND INSTALLED CLIP IAW DC8 SRM 51-3-0.Jul 9, 2002 · N802UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2002806844Former · crackedN/R: 1696 RH WING OUTBD L/E UPPER PART FORMER CRACKED .250 XFS647.500CORR: 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 ANGLE IAW SRM57-2-0 Jul 6, 2002 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR IXXA0200043OGyro · defectiveEN ROUTE FROM TOL, THE FLIGHT CREW NOTICED THE PITCH AND ROLL FLAGS DISPLAYED ON THE CAPTAINS AND FIRST OFFICERS ELECTRONIC ATTITUDE DIRECTION INDICATOR. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE IJul 6, 2002 · N606AL · Doug DC873F · Directional Gyro and Indicating SystemSDR DHL2002806856Skin · corrodedLT WING OUTBOARD L/E UPPER SKIN CORRODED (STA 578.000-603.750, 628.750-653.750). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 PG 2 FIG 38. REMOVED CORROSION FROM LT OUTBOARD LEADING EDGE UPPER SKIN IAW SRM 51-1-8 PG 17-18 FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. Jul 5, 2002 · N806DH · Doug DC873F · Wing, Plate/SkinSDR DHL2002806852Former · crackedITEM N/R 2281 RH WING CTR L/E UPPER FORMER 1/2" CRACKED , STA XFS 316.000CORR: PERFORMED STOP DRILL IAW SRM 57-2-0 PG. 9-10 FABRICATED DOUBLER WITH 2024T3 AL O.063 IAW SRM57-2-0 PG9-10 , CLEANED , TREATED , AND PRIMED. IAW SRM51-1-8B , INSTALLED DOUBLER ON R/HJul 5, 2002 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL8062002847Former · crackedITEM N/R 1964 RH WING OUTBOARD LEADING EDGE UPPER PART FORMER CRACKED 3/4 " XFS616.250CORR: REMOVEED FASTNERS IAW SRM 51-1-21 PG1 PERFORMED STOP DRILL IAW SRM 57-2-0 PG 9-10 FABRICATED DOUBLER IAW 57-2-0 PG 9-10 CLEANED , TREATED , AND PRIMED IAW SRM 51-1-8B ,Jul 5, 2002 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2002806845Fitting · crackedLT WING INBOARD SLOT ZEE PAN FITTING CRACKED 2 INCHES XS 250.000. REMOVED ZEE PAN FITTING IAW SRM 51-1-20D PG 21, PERFORMED ANTI CORROSIVE TREATMENT AND PRIMED EFFECTED AREA IAW SRM 51-1-8B, INSTALLED ZEE PAN FITTING IAW SRM 51-1-20D PAGE 9.Jul 5, 2002 · N806DH · Doug DC873F · Leading Edge DevicesSDR DHL2002806851Former · crackedITEM REF N/R 2282 RH WING CTR LEADING EDGE UPPER FORMER .500 CRACK @ STA XFS 322.750CORR: REMOVED FASTNER IAW SRM 51-1-21 PG 1 , FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG. 9-10 CLEANED , TREATED , AND PRIMED IAW SRM 51-1-8B INSTALLED REINFORCING ANGLE ANDJul 4, 2002 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2002806850Former · crackedITEM REF. N/R RH WING CTR L/E FORMER .500 CRACKED XFS329.000CORR: STOP DRILLED CRACK ON RH WING CTR L/E UPPER FORMER , STA. XFS329.000 , IAW SRM57-2-0 PG. 9-10 FABRICATED DOUBLER IAW SRM 57-2-0 PG. 9-10 CLEANED , TREATED , AND PRIMED IAW SRM 51-1-8B, INSTALLEDJul 4, 2002 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2002806849Former · crackedITEM REF N/R 2286 RH WING CTR L/E LOWER FORMER 1" CRACK , STA. XFS360.250CORR: PERFORMED STOP DRILL ON 1" CRACK , STA XFS360.250 IAW SRM 57-2-0 PG. 9-10 FABRICATED DOUBLER IAW SRM 57-2-0 PG. 9-10 CLEANED , TREATED , AND PRIMED IAW SRM 51-1-8B INSTALLED DOUBLERJul 4, 2002 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2002806846Former · crackedITEM REF N/R 1317 LT. WING OUTBD L/E FORMER CRACKED AT STA. XFS691.000CORR: 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 AREA IAW SRM 51-1-8B INSTALLED REINFORCING ANGLE ON OUTBD Jul 4, 2002 · N806DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2002806853Angle · corrodedLT MLG W/W SUPPORT ANGLE CORRODED AT STA 857.000 LBL 42. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18, FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2. REMOVED FORMER ANGLE IAW SRM 53-2-0 FIG 1F, FABRICATED ANGLE IAW SRM 53-2-0 FIG 1F, INSTALLED FORMER ANGLE IAW SRM 53Jul 3, 2002 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2002806848Former · crackedITEM REF N/R 2233 LH WING CTR. LEADING EDGE LOWER SURFACE FORMER WITH 1" CRACK IN IT STA XFS 335.220 CORR: REMOVED FASTNERS IAW SRM 51-1-21 PG. 1 STOP DRILLED CRACK IAW SRM57-2-0 PG. 9-10FABRICATED REINFORCING ANGLE IAW SRM57-2-0 PG. 9-10 , CLEANED , TREATED ,Jul 3, 2002 · N806DH · Doug DC873F · Wing, Rib/Bulkhead
Back to Douglas DC-8-73F