Douglas DC-8-73F

Service difficulty reports · 15,471

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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 UPS01835778Engine · flamed outAPPROX 2 MIN AFTER LEVEL OFF AT FL350 + 273IAS, NR 4 ENG FLAMES OUT. I MMEDIATE X-FEED DID NOT RE-LIGHT IT. 2 NORMAL AIRSTART ATTEMPTS WERE TRIED IAW CHECKLIST PROCEDURES. BOTH UNSUCCESSFUL. PERFORMED IDLE CHECK, POWER ASSURANCE CHECK, PMC DROPCHECK ACCELERMay 1, 2001 · N801UP · Doug DC873F · Powerplant SystemSDR RRXA11028Skin · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LH WING LWR TE PANEL IB OF FLAP HINGE 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 Apr 30, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR RRXA11027Structure · crackedDURING A MAINTENANCE VISIT FOUND CRACKED DAMAGE TO DOOR AT LT OB SLOT UPPER CENTER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 27-80-01.Apr 30, 2001 · N602AL · Doug DC873F · Leading Edge Slat Control SystemSDR UPS01836007Bulkhead · crackedINSPECTION TYPE:C1,3 STA 683 PRESSURE BULKHEAD IS CRACKED RBL 6-24. REMOVED AND REPLACED BULKHEAD IAW DWG 9753751, AND SRM 53-1-0, 51-1-20D, 51-1-21.Apr 30, 2001 · N880UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS01836002Skin · corrodedINSPECTION TYPE:C1,3 STA 270 - 370 LONG 28R - 33R FUSELAGE SKIN IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SKIN SECTION IAW 8110-3 APPROVED DH SK 880-334.Apr 30, 2001 · N880UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS01835880Fitting · crackedINSPECTION TYPE:C1,3 STA 660-680 L11R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5750540 AND SRM 51-1-20D, 51-1-23Apr 30, 2001 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835870Fitting · corrodedINSPECTION TYPE:C1,3 STA 70 L21R CUSP JOINT ATTACH FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3610130 AND SRM 51-1-20D, 51-1-21Apr 30, 2001 · N880UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835826Skin · corrodedINSPECTION TYPE: C1, 3. LEFT WING L/E. LOWER SKIN IS CORRODED BEYOND LIMITS AT XFS 635 ***CPCP*** REPAIRED SKIN I.A.W. E.O. DC8-5720-4087-B APPX. CApr 30, 2001 · N880UP · Doug DC873F · Wing, Plate/SkinSDR UPS01835824Skin · corrodedINSPECTION TYPE: C1, 3. LEFT WING OB. L/E. LOWER SKIN HAS INTERGRANULAR CORROSION BETWEEN XFS 710-716.25 ***CPCP*** REPAIRED SKIN I.A.W. E.O. DC8-5720-4087,AND SRM. 51-1-20D,51-1-21Apr 30, 2001 · N880UP · Doug DC873F · Wing, Plate/SkinSDR UPS01835955Skin · crackedINSPECTION TYPE:C1 SKIN BELOW CUTOUT FOR AFT LT ENTRANCE DOOR CRACKED LWR FWD CORNER. REPAIRED AREA IAW REO G08018.Apr 29, 2001 · N819UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS01835896Intercostal · crackedINSPECTION TYPE:C1 FWD PIT - STN 90 - S33R - INTERCOSTAL UNDER CARGO TRACK IS BENT AND CRACKED. REMOVED AND FABBED NEW INTERCOSTAL P/N 5750726-70. ALODINED, PRIMED AND INSTALLED INTERCOSTAL CARGO TRACK IAW DC8 SRM 51-3-0 AND 51-1-21.Apr 29, 2001 · N819UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806001Computer · malfunctionedAUTOPILOT WILL NOT BANK GREATER THAN 10 DEGREE WITH GPS 1 OR 2 IN AUX NAV. ALL LATERAL MODES FUNCTION NORMALLY. R&R ROLL CHANNEL COMPUTER PER DC8 M/M REF 22-12-1. OPS CKS SERVICABLE. P/N OFF 2588788-905, S/N OFF 1180385. P/N ON 2588788-905, S/N ON 1070200.Apr 28, 2001 · N806DH · Doug DC873F · Autopilot ComputerSDR RRXA11022Spar Cap · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RH AUX TANK UPPER SPAR CAP AT XFS32.5 AND XFS1117, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW Apr 27, 2001 · N602AL · Doug DC873F · Wing Main, Frame StructureSDR RRXA11021Strut · brokenDURING A MAINTENANCE VISIT FOUND BROKEN DAMAGE TO LT MLG STRUT ASSY GEAR AT LT WW, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 32-11-1.Apr 26, 2001 · N602AL · Doug DC873F · Main Landing Gear Strut/Axle/TruckSDR DHL2001804006Computer · malfunctionedAUTOPILOT ELEVATOR SERVO TRIM METER OSCILLATES FULL DEFLECTION UP AND DOWN WHILE AIRCRAFT IS LEVEL FLIGHT. RERACKED PITCH CHANNEL COMPUTER. SYSTEM OP CHECKS NORMAL PER MM 22-13-1.Apr 26, 2001 · N804DH · Doug DC873F · Autopilot SystemSDR DHL2001804005Computer · defectiveIN LEVEL FLIGHT AT CRUISE ALTITUDE THE AUTOPILOT ROWS THE AIRCRAFT 2 DEG LEFT AND RIGHT CONTINUOUSLY. REMOVED AND REPLACED ROLL CHANNEL COMPUTER PER MM 22-12-1. OPS NORMAL.Apr 26, 2001 · N804DH · Doug DC873F · Autopilot SystemSDR DHL2001802005Fire Warning · false activationNR 4 ENG FIRE LIGHT AND BELL CAME ON. PERFORMED PHASE ONE ITEMS. FIRE LIGHT WENT OUT. SHORT TEST INDICATED GOOD. INSPECTED NR 4 ENG FIRE LOOPS. NO DEFECTS NOTED. DUE TO HISTORY DEFFERED NR 4 ENG A LOOP FIRE DETECTION PER MEL 26-2-3. DMI 5331. PERFORMEDApr 25, 2001 · N802DH · Doug DC873F · Fire DetectionSDR RRXA11017Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO N/W/W AFT LWR BLKD FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-3-0, DWG#464011Apr 24, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA11016Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO PANEL AT LH WING LWR PANEL FWD OF MLG, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM Apr 24, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR RRXA11015Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA 1577-1600 AND RBL45, 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 DC-8 SRM 53-2-Apr 24, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA11014Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FITTING AT L33R AND STA 1230, 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 DC-8 SRM 51-1-20D, DWG#4758Apr 24, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA11013Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO BATHTUB FITTING AT STA 340 AND L35L TO L36L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-Apr 24, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA11012Tab · debondedDURING A MAINTENANCE VISIT FOUND DEBONDED DAMAGE TO LH ELEVATOR IB CORNER OF GEARED TAB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-9A, DC-8 MM 27-30-3.Apr 23, 2001 · N602AL · Doug DC873F · Vertical StabilizerSDR UPS01835684Bracket · crackedINSPECTION TYPE:C2 LT WING LE SECTION BETWEEN NR 1 & 2 ENGINE SLOT DOOR ACTUATOR ATTACH BRACKET IS CRACKED APPROX 50 INCHES FROM OTBD LWR SIDE RMVD OB SECTION OF LT OB SLOT, SETAINER & SEAL FABBED NEW ATTACH BRA CKET FITTING IAW DAC DWG 4770278 INSTALLED Apr 23, 2001 · N805UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS02838365Skin · corrodedINSPECTION TYPE:C13 LT EXT FUS SKIN HAS BULGES WITH SURFACE CORROSION L27L APPROX STA 1640-1670 AT FASTENERS. REMOVED CORROSION PER DC8 SRM 51-1-8, OUT OF LIMITS. FABBED REPAIR DOUBLERS, FINGER DOUBLERS, AND FILLER PER DC8 SRM 53-2-1 FIG 7. INSTALLED PER DCApr 22, 2001 · N818UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2001801004Pulley Bracket · defectiveON POST FLIGHT FOUND A SPOILER ON RT WING EXTENDED AND WILL NOT RETRACT. REMOVED AND REPLACED SPOILER PULLEY BRACKET RT W/W IAW MM 20-16-0. COMPLIED WITH FUNCTIONAL TESTS IAW DC-8 MM 27-60-0, 27-63-0, 32-43-0 WITH NO DEFECTS NOTED. RIG CHECK ACCOMPLISHED PEApr 22, 2001 · N801DH · Doug DC873F · Drag Control SystemSDR RRXA11018Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LH WING LWR TE PANEL AT FLAP HINGE 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0, 51-1-9A.Apr 21, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR DHL2001804004Adc · malfunctionedAFTER AIRSPEED INDICATORS DECREASED TO ZERO THE A/C BEGAN TO OSCILLATE IN PITCH (+/- 150FT) ALT HOLD REMAINED INOP. PITCH DUMP MODE OK. NAV SELECT OK. AUTO PILOT OK BELOW 1800 FT. REPLACED DADC AND TESTED PER SMM 34-11-31. PITOT STATIC LEAK TEST FAILED. Apr 21, 2001 · N804DH · Doug DC873F · Air Data ComputerSDR RRXA11010Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR BEAM LOWER FLANGE AT STA 902 AND LBL48-53, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DHSK602-708. (CORROSION DAMAGEApr 20, 2001 · N602AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA11009Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RH WING INTERCOSTAL FITTING AT STA XW98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 57-1-0, 5Apr 19, 2001 · N602AL · Doug DC873F · Wing Main, Frame StructureSDR RRXA11008Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CABIN SEAT TRACK AT STA 1400 AND LBL48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-3 FIG8A.Apr 19, 2001 · N602AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA11007Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA 1160 AND L35L TO L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM Apr 19, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA11006Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT A-PIT DOOR FRAME LWR #4 LATCH, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2Apr 19, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA11005Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LH WING LE SKIN AT STA X5520, 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 DC-8 SRM 57-1-0, 51-1-21, 5Apr 19, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR RRXA11004Seat Track · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 610-1000 AND RBL24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-21-03, 53-Apr 19, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA11003Web · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO BULKHEAD AT STA 70 AND RBL28, 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 DC-8 SRM 53-2-0 FIG23.Apr 19, 2001 · N602AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA11002Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA. 960 AND LBL60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0FIG8, 51-Apr 19, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA11001Frame · damagedDURING A MAINTENANCE VISIT FOUND BLEND OUT DAMAGE TO FRAME AT STA 1280 AND L34L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 FIG2, 51-1-20D.Apr 19, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA11000Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LH LWR WING SKIN AT STA XFS422-75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 51Apr 19, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR RRXA10999Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 940 AND LBL60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0Apr 19, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA10998Skin · gougedDURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO RT WING UPPER LE AT STA XFS257-500, 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 DC-8 SRM 51-1-20D, 5Apr 19, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR DHL2001806632Fitting · crackedC-CHECK, LT WING FLAP HINGE SUPPORT FITTING SHOWS 0.750 INCH CRACK AT STA 409. REMOVED CRACKED FITTING AT STA 409 IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED, AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 21.Apr 19, 2001 · N806DH · Doug DC873F · Trailing Edge FlapsSDR RRXA10997Intercostal · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMGE TO C-PIT FLOOR SUPPORT STRAP AT STA. 1300 AND RBL33, 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 DC-8 SRMApr 18, 2001 · N602AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA10996Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT SAT 1120 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DHSK 602-260. (CORROSIONApr 18, 2001 · N602AL · Doug DC873F · Fuselage Main, StructureSDR RRXA10995Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LH WING LE LWR SKIN AT STA. XOL D16-225, 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 DC-8 SRM 51-Apr 18, 2001 · N602AL · Doug DC873F · Wing, Plate/SkinSDR RRXA10994Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO SUPPORT ANGLE AT STA 860 AND LBL55, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D, 53-1-0 AND DWG 564533Apr 18, 2001 · N602AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA10993Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO R/H VERT STAB SKIN AT STA ZR45 TO ZR74, 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 DC-8 SRM 51-3Apr 18, 2001 · N602AL · Doug DC873F · Empennage StructureSDR RRXA10992Aileron · bentDURING A MAINTENANCE VISIT FOUND BENT DAMAGE TO R/H OUTBOARD AILERON OUTBOARD TRAILING EDGE, 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 DC-8 SRM 51-1Apr 18, 2001 · N602AL · Doug DC873F · Aileron Control SystemSDR RRXA10725Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 32R AT STA 100, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Apr 18, 2001 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS01835629Smoke Detector · inoperativeCREW-PREFLIGHT MULTIPLE SMOKE DETECTORS INOP IN PIT 34. R&R BATT CLEARED DEFERRALApr 18, 2001 · N818UP · Doug DC873F · Smoke Detection
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