Douglas DC-8-71F

Service difficulty reports · 8,938

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 = 'DC871F'
  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 UPS00833396Unknown · odorINSPECTION TYPE:N/A, COCKPIT ODOR - MX VERIFIED WHAT APPEARED TO BE AN ELECTRICAL PROBLEM ODOR. COULD NOT ISOLATE SOURCE.Jul 21, 2000 · N748UP · Doug DC871F · Air Distribution SystemSDR UPS00833394Lanyard · brokenINSPECTION TYPE:N/A, SLIDE COVER LANYARD BROKEN AT CABLE (SLIDE AT ENTRY DOOR). REPLACED MAIN ENTRY DOOR SLIDE COVER LANYARD AND SECURED SLIDE LANYARD INSTALLED PER IPC 25-62-00.Jul 21, 2000 · N779UP · Doug DC871F · Escape SlideSDR UPS00833397Transformer · overheatedINSPECTION TYPE:N/A, SMOKE IN COCKPIT. DIVERTED INTO KJAX. DECLARED EMERGENCY, OVER-WEIGHT LANDING. *S/D* REFERENCE UPS00833396, PERFORMED OVERWEIGHT/HARD LANDING INSPECTION. REMOVED AND REPLACED TRANSFORMER BALLAST FOR SUSPECTED OVERHEATING. REMOVED ANDJul 20, 2000 · N748UP · Doug DC871F · Flight Compartment LightingSDR RRXA003140Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FRAME LEG ON FWD SIDE AT FS 1200 AND L34R-L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0, 51-1-4 (Jul 18, 2000 · N8076U · Doug DC871F · Fuselage Main, FrameSDR IXXA0000028Actuator · out of adjEN ROUTE FROM PDX TO TOL, THE LANDING GEAR DOOR AND GEAR UNSAFE WARNING LIGHTS ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE GEAR, PERFORMED AN UNSUCCESSFUL GEAR UP LATCH CHECK, THE WARNING INDICATIONS REMAINING THE SAME. THE FLIGHT RETURNED Jul 18, 2000 · N825BX · Doug DC871F · Landing Gear ActuatorSDR RRXA001017Engine · flamed outAFTER ENCOUNTER WITH TURBULENCE AND RAIN AT FL390 NR 2 ENG FLAMED OUT. NOTICED NR 2 OIL PRESSURE LIGHT ON AND ENGINE WAS WINDMILLING, RAN CHECKLIST FROM QRH. OIL PRESSURE WAS BELOW 13 PSI SO PROCEEDED WITH IN-FLIGHT SHUTDOWN. ENGINE STARTED WINDMILLING 1448Jul 14, 2000 · N500MH · Doug DC871F · Engine (Turbine/Turboprop)SDR FWT2001F00003Actuator · inoperativeWING SLOT LIGHT ON AFTER TO, FLAPS UP, AND BUFFET. UNABLE TO COMPLETE WING SLOT LIGHT ON ABNORMAL PROCEDURE CONDITION NR 1. NOTE: FLAP INDICATOR REMAINS AT 0 FLAP HANDLE IS PLACED TO 0 DEGREE OR 25 DEGREE FLAP POSITION. CHANGED WING FLAP CONTROL VALVE IAW Jul 12, 2000 · N872SJ · Doug DC871F · Trailing Edge Flap ActuatorSDR FWT2001F00002Actuator · inoperativeWING SLOT LIGHT ON AFTER TO, FLAPS UP, AND BUFFET. UNABLE TO COMPLETE WING SLOT LIGHT ON ABNORMAL PROCEDURE CONDITION NR 1. NOTE: FLAP INDICATOR REMAINS AT 0 FLAP, WHEN FLAP HANDLE IS PLACED TO 0 DEGREE OR 25 DEGREE FLAP POSITION. CHANGED WING FLAP CONTROLJul 12, 2000 · N872SJ · Doug DC871F · Trailing Edge Flap ActuatorSDR RRXA003014Bracket · brokenDURING A MAINTENANCE VISIT FOUND A BROKEN BRACKET ON THE LT WING L/E WING LOWER L/E AT STA XFS 622, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DCJul 10, 2000 · N997GE · Doug DC871F · Wing Miscellaneous StructureSDR UPS00833241Duct · looseLOST CABIN PRESSURE ON CLIMB-OUT. FOUND 3 DUCTS PULLED APART ON LEFT PACK. RE ATTACHED DUCTS AND SECURED. OPS CHECKS OK.Jul 8, 2000 · N752UP · Doug DC871F · Cabin Pressure Control SystemSDR RRXA001011Fire Detector · shortedENROUTE- ENGINE FIRE WARNING #1 ENG FIRED BOTH BOTTLES AND COULD NOT GET A TEST DIVERTED TO DENVER. FOUND FIRE LOOP DETECTOR ELEMENT ABOVE COMBUSTION SECTION SHORTED. REMOVED AND REPLACED SAME IAW DC8MM 26-11-16. ALSO REMOVED AND REPLACED BOTH FIRE EXTINGUJul 7, 2000 · N8087U · Doug DC871F · Fire DetectionSDR RRXA001010Engine · flamed outNR 4 ENGINE FLAME OUT ON T/O MMMX. ON ENGINFLIGHT START CHECKLIST NR 4 ENG LIT OFF & STAGNATED AT APPROX 320DEG C. THEN FAMED OUT AGAIN. PERFORMED INFLIGHT SHUTDOWN CHECKLIST. NR 4 ENG. R&R'D BY G.E. ON-WING IAW MM 71-00-42. ENG. CHECKED GOOD , OPS. CHECKEJul 6, 2000 · N8091U · Doug DC871F · Engine (Turbine/Turboprop)SDR RRXA003010Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE SPLICE ON THE LT WING CTR L/E MIDDLE OF L/E RIB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8Jul 5, 2000 · N997GE · Doug DC871F · Wing, Rib/BulkheadSDR UPS00833346Longeron · corrodedINSPECTION TYPE:C123, AFT ACCESSORY COMPARTMENT FS 1600 AT L34L LONGERON EXFOLIATED UNDER FRAME. REMOVED DAMAGE SECTION OF LONGERON, LONGERON SPLICE AND LONGERON END FITTING IAW DC8 SRM 51-3-2. LOCATE NEW SECTION OF LONGERON, DRILL EXISTING HOLES, ALODINE ANJul 5, 2000 · N708UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA003015Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CTR L/E I/B BOTTOM SIDE NR 4 RIB I/B END, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-2-0 AND 51-1-20D.Jun 30, 2000 · N997GE · Doug DC871F · Wing, Rib/BulkheadSDR RRXA003013Clip · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE ATTACH CLIP ON THE LT WING CTR L/E MIDDLE OF L/E AT SPLICE TOP SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1Jun 30, 2000 · N997GE · Doug DC871F · Wing Miscellaneous StructureSDR RRXA003012Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CTR L/E 14TH RIB O/B TOP SIDE OF L/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, ALODINED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-20-0, 51-1-2Jun 30, 2000 · N997GE · Doug DC871F · Wing, Rib/BulkheadSDR RRXA003011Doubler · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE SPLICE ON THE LT WING CTR L/E MIDDLE OF L/E DOUBLER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW Jun 30, 2000 · N997GE · Doug DC871F · Wing Miscellaneous StructureSDR RRXA003009Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE O/B HOLE ON THE LT WING CTR L/E O/B END #2 RIB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 Jun 30, 2000 · N997GE · Doug DC871F · Wing, Rib/BulkheadSDR RRXA003008Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CTR L/E I/B BOTTOM SIDE NR 13 RIB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-1, 51-2-0 AND 51-1-20D.Jun 30, 2000 · N997GE · Doug DC871F · Wing, Rib/BulkheadSDR RRXA003007Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CTR L/E TOP SIDE I/B NR 7 RIB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0, 51-1-20D AND 51-1-21, FJun 30, 2000 · N997GE · Doug DC871F · Wing, Rib/BulkheadSDR RRXA003006Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CTR L/E TOP SIDE I/B #6 RIB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0,Jun 30, 2000 · N997GE · Doug DC871F · Wing, Rib/BulkheadSDR RRXA003005Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CTR L/E #4 RIB I/B BOTTOM OF L/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51Jun 30, 2000 · N997GE · Doug DC871F · Wing Miscellaneous StructureSDR RRXA003004Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CTR L/E I/B BOTTOM #5 RIB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-20D Jun 30, 2000 · N997GE · Doug DC871F · Wing SparSDR RRXA002749Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON FWD SIDE OF FRAME AT STA 20 AT CUSP LINE RT SIDE OF CABIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRJun 30, 2000 · N8084U · Doug DC871F · Fuselage Main, FrameSDR UPS00833151Engine · flamed outNR 1 ENGINE FLAMED OUT AT FL310 M80 CRUISE FLT WHEN ENGINEER OPENED NR 1 CROSSFEED THEN TURNED OFF NR 2 MAIN BOOST PUMP TO TRANSFER FUEL FROM NR 1 TO NR 2 MAIN CROSSFEEDS WERE OPENED AND START SWITCH TO ALL ENGINES BOTH, RESTARTED ENGINES ***SUPPLEMENTAL Jun 30, 2000 · N709UP · Doug DC871F · Engine (Turbine/Turboprop)SDR UPS00833149Regulator · stuckCAPTAINS O2 REGULATOR STUCK ON REMOVED AND REPLACED CAPTAINS REGULATORJun 30, 2000 · N798UP · Doug DC871F · Crew Oxygen SystemSDR RRXA002719Nut Plate · missingDURING A MAINTENANCE VISIT FOUND A BROKEN NUT PLATE ON THE RIGHT O/B SLOT UPPER SIDE SCREW AT STA XS 515, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW EO NR 00-107 WITH APPROVED 8Jun 29, 2000 · N8084U · Doug DC871F · Wing Miscellaneous StructureSDR UPS00833345Skin · corrodedINSPECTION TYPE:C123, LWR SKIN BETWEEN STA 360 TO 380 ANT MOUNTING PLATE CORRODED. FABBED MOUNTING PLATE IAW DAC DWG 3778019 AND SRM 51-1-21, OK TO ALODINE AND PRIME.Jun 29, 2000 · N708UP · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA001006Warning Light · illuminatedON CLIMBOUT HYD OVERTEMP LIGHT CAME ON. WHEN RUNNING QRH TEMP WOULD NOT COME DOWN AND ACFT KEPT GIVING STRONG AILERON INPUTS. HYD SYSTEM WAS DEPRESSED AND HYD PWR LEVERS OFF, FLIGHT CONTROLS WERE STILL GIVING STRONG AILERONS & RUDDER INPUTS. HYDRAULIC ZEROJun 29, 2000 · N8087U · Doug DC871F · Hydraulic Indicating SystemSDR UPS00833199Fitting · crackedINSPECTION TYPE: C1, STA 1690, LONG 26 LT, FWD SIDE END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG. 4641326,AND SRM. 51-1-21Jun 29, 2000 · N772UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833081Battery Pack · dischargedEMERGENCY EXIT LIGHTS FAILED OPS CHECK. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK.Jun 29, 2000 · N713UP · Doug DC871F · Emergency LightingSDR RRXA003016Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CHANNEL NUT PLATES ON THE LT L/E ABOVE NR 1 PYLON ANGLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, ALODINED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-Jun 28, 2000 · N997GE · Doug DC871F · Wing Miscellaneous StructureSDR RRXA003003Doubler · crackedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THE LT WING L/E O/B OF #2 PYLON L/E DOUBLER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGED, ALODINED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW Jun 28, 2000 · N997GE · Doug DC871F · Wing Miscellaneous StructureSDR RRXA003002Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN LOWER SPAR CAP, WEB AND SKIN LOWER ON LEFT WING AT STA XFS 576, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAJun 28, 2000 · N997GE · Doug DC871F · Wing Miscellaneous StructureSDR UPS00833220Fitting · crackedINSPECTION TYPE: C1, STA 958, WHEEL WELL KEELBEAM LOWER DOOR SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG. 5616306, AND SRM. 51-1-20D.Jun 28, 2000 · N772UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833451Bulkhead · crackedINSPECTION TYPE:C123, REMOVE EXISTING DOUBLER FROM FWD SIDE OF LT AFT PRESSURE BULKHEAD AND INSTALL DOUBLERS IAW DAC DWG SR08530007. REPAIRED AREA BY INSTALLATION OF REPAIR DOUBLERS IAW DAC DWG SR08530 07 AND REO G07477.Jun 27, 2000 · N708UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS00833313Frame · corrodedINSPECTION TYPE:C123, AFT PIT FS 1100 CORROSION UNDER NUT PLATE ON UPPER FRAME FLANGE LOWER SURFACE BETWEEN L36 AND L35L. REMOVED CORROSION MATERIAL, FOUND TO BE OUT OF LIMITS. PERFORMED REPAIR IAW UPS EO DC8 5310-11728B.Jun 27, 2000 · N708UP · Doug DC871F · Fuselage Main, FrameSDR UPS00833373Skin · crackedINSPECTION TYPE:C123, FWD PIT FS 180 LONG 36 SKIN HAS CRACK AT FASTENER HOLE. REMOVED CIRCULAR SECTION OF DAMAGED PLATING IAW DC8 SRM 53-2-1, FABBED EXTERNAL DOUBLER, FILLER, AND INTERNAL DOUBLERS IAW DC8 SRM 53-2-1, ALODINED AND PRIMED IAW SRM 51-1-8, INSTALJun 25, 2000 · N708UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS00833007Spar Cap · corrodedINSPECTION TYPE: C1 RT WING AUX. TANK SPAR UPPER CAP IS CORRODED BEYOND LIMITS BETWEEN XFS 107.5 AND XFS 126.25 REPAIRED SPAR CAP I.A.W. SRM. 57-2-1 FIG. 36.Jun 25, 2000 · N772UP · Doug DC871F · Wing SparSDR UPS00833078Floor Support · corrodedINSPECTION TYPE: C1. STA 1746 BL 0 TO LBL 30 FLOORBEAM SUPPORT CHANNEL IS CORRODED. REMOVED, FABRICATED, AND REPLACED CHANNEL I.A.W. DWG. 5755032,AND SRM. 51-1-20DJun 24, 2000 · N772UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833077Floor Support · corrodedINSPECTION TYPE: C1. STA 1746 BL 0 TO RBL 30 UPPER FLOORBEAM SUPPORT CHANNEL IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED CHANNEL I.A.W. DWG. 5755032,AND SRM. 51-1-20D ***CPCP***Jun 24, 2000 · N772UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA002720Link · damagedDURING A MAINTENANCE VISIT FOUND THAT THE FLAP LINK SUPPORT (CANOE FITTING) NEEDS TO BE REPLACED AT STA XW 219.498, 339.723 & 97.906 IAW DC-8 MM 27-51-12 RIGHT SIDE PER S/B 27-260, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-Jun 23, 2000 · N8084U · Doug DC871F · Trailing Edge FlapsSDR RRXA002718Retainer · misinstalledDURING A MAINTENANCE VISIT FOUND CANOE FITTING BOLT RETAINER INSTALLED ON WRONG SIDE OF FITTING AT STA 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR 00-107 WITH APPRJun 23, 2000 · N8084U · Doug DC871F · Wing, Attach FittingsSDR UPS00833203Channel · corrodedINSPECTION TYPE: C1, STA 1702 - 1723, RBL 30 FLOOR SUPPORT CHANNEL IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED CHANNEL IAW DWG. 5755032,AND SRM. 51-1-20D,51-1-21 ***CPCP***Jun 22, 2000 · N772UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833202Channel · corrodedINSPECTION TYPE: C1, STA 1764, RBL. 8 HAS FLOOR SUPPORT CHANNEL CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED CHANNEL IAW. DWG. 5755032, AND SRM. 51-1-20D ***CPCP***Jun 22, 2000 · N772UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833201Frame · crackedINSPECTION TYPE: C1, STA. -12, LONG 14 LT, FRAME IS CRACKED. REPAIRED FRAME IAW E.O.DC8-5310-11728-A,AND DC8-53A-011Jun 22, 2000 · N772UP · Doug DC871F · Fuselage Main, FrameSDR UPS00833047Fitting · crackedINSPECTION TYPE: C123. STA 1220, LONG 30 - 32 RT BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755847,AND SRM. 51-1-20DJun 22, 2000 · N715UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833045Floor Support · corrodedINSPECTION TYPE: C1. STA 1766, RBL 20 - 24 FLOORBOARD SUPPORT CHANNEL IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED CHANNEL I.A.W. DWG. 5755032,AND SRM. 51-1-20DJun 22, 2000 · N772UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833044Floor Support · corrodedINSPECTION TYPE: C1. STA 1766, LBL 20 - 23 FLOORBOARD SUPPORT CHANNEL IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED CHANNEL I.A.W. DWG.5755032,AND SRM. 51-3-0.Jun 22, 2000 · N772UP · Doug DC871F · Fuselage Miscellaneous Structure
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