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 RRXA000361Skin · crackedDURING A MAINTENANCE VISIT FOUND RIGHT WING TOP TRAILING EDGE AT XRS 162 CRACKED AND EXCEEDED LIMITS IAW DC-8 SRM. STOP DRILLED CRACK IAW DER APPROVED EO 00-016. FABRICATED DOUBLERS AND INSTALLED IAW DC-8 SRM 51-1-21 AND EO 00-016.Feb 3, 2000 · N792FT · Doug DC873F · Trailing Edge FlapsSDR UPS00831516Frame · crackedINSPECTION TYPE:SP, STA 25 LT FRAME CRACKED AT LONG 17L APPROX 1 INCH ABOVE SNUBBER ATTACH POINT. REPAIRED PER SRM 53-2-0 FIG 2.Feb 3, 2000 · N880UP · Doug DC873F · Fuselage Main, FrameSDR RRXA003786Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO CABIN ATTACH FITTING AT STA 1140 AND L21R, 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 51-1-20Feb 2, 2000 · N792FT · Doug DC873F · Fuselage Main, BulkheadSDR RRXA000525Structure · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO AIR CONDITIONING SERVICE DOOR BETWEEN STA 30 TO STA 60 AND BETWEEN LONGERONS 26 RIGHT TO 31 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED ANFeb 2, 2000 · N831AL · Doug DC873F · Air Conditioning DoorsSDR DHLA200080102Seat Track · brokenSEAT TRACK BROKEN.Feb 2, 2000 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2000804001Garlock Seal · leakingNR 4 ENGINE LOST OIL QUANTITY. SHUT DOWN ENGINE PER AOM ABNORMAL PROCEDURES. REMOVED NR 4 STARTER TO INSPECT DRIVE SHAFT AREA FOR DAMAGE. FOUND GARLOCK SEAL LEAKING PAST INTERNAL SEAL. REMOVED AND REPLACED GARLOCK SEAL AND INTERNAL SPACER. RAN NR 4 ENGINEFeb 2, 2000 · N804DH · Doug DC873F · Turbine Engine Oil SystemSDR DHL200080380CBracket · crackedAT C-CHECK, RT WING L/E LWR PART NR 555L ACCESS DOOR SLOT ADJUSTMENT FRAME CRACKED 1 INCH. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER AND INSTALLED IAW EO NR DHL020301. N/R 1889Feb 2, 2000 · N803DH · Doug DC873F · Wing Miscellaneous StructureSDR RRXA002954Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOORBEAM BETWEEN STA 320 - 340 AT X-40 AND Z-50, 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. (CORFeb 1, 2000 · N792FT · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA002948Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE NR 2 SEAT TRACK BETWEEN STA 920 - 940 AT X-45, 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 53-2-3. (CORROSIFeb 1, 2000 · N792FT · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000641Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIGHT WING L/E RIB AT LOWER AFT FASTENER AT STA XFS 653.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-2-0Feb 1, 2000 · N831AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA000638Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT THE RIGHT WING L/E RIB AT THE AFT LOWER FASTENER AT STA XFS 616.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAAW DC-8 SRM 5Feb 1, 2000 · N831AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA000637Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIGHT WING L/E RIB AT THE AFT LOWER FASTENERS AT STA XFS 660.0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-Feb 1, 2000 · N831AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA000636Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIGHT WING L/E RIB AT THE AFT LOWER FASTENER AT STA XFS 622.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-2Feb 1, 2000 · N831AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA000577Tee Chord · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FWD A/C COMPARTMENT TEE CHORD AT STA 70 AND LONGERON L35 LEFT TO L32 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW TEE CHORD AND INSTALLEDFeb 1, 2000 · N831AL · Doug DC873F · Fuselage Main, StructureSDR DHL2000803107Angle · crackedAT C-CHECK, NR 3 CARGO DOOR SUPPORT ANGLE SHOWS 2 CRACKS OF 1.25 INCH AND 1.5 INCH APPROX BETWEEN FS 1210 AND FS 1230. STOP DRILLED CRACKS, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-3-0 PG 13. REF: N/R 5341.Feb 1, 2000 · N803DH · Doug DC873F · Cargo/Baggage DoorsSDR UPS00831473Circuit Breaker · trippedINSPECTION TYPE:N/A, INFLIGHT EMERGENCY COCKPIT LIGHTS ARE ILLUMINATED WHEN EMERGENCY LIGHT SWITCH WAS IN THE ARMED POSITION. INSPECTED SYSTEM AND DISCOVERED POPPED C/B. RESET BREAKER AND OPS CHECK EMERGENCY LIGHTING SYSTEM. SYSTEM OPERATES NORMAL.Feb 1, 2000 · N868UP · Doug DC873F · Emergency LightingSDR DHL200080303CSkin · damagedAT C-CHECK, RIGHT WING I/B FLAP UPPER SURFACE SKIN DEFORMED 2 BETWEEN XW 41 AND 70.5. REPLACED SKIN PER SRM 51-1-21.Feb 1, 2000 · N803DH · Doug DC873F · Trailing Edge FlapsSDR DHL200080358CAngle · corrodedAT C-CHECK, AFT CARGO COMPARTMENT CENTER WALL UPPER ANGLE SHOWS CORROSION AND NUTS RUSTED AT FS 1320. REMOVED LEVEL 1 CORROSION LESS THAN 3 PERCENT IAW SRM 51-1-8 PG 17, REMOVED AND REPLACED NUTS IAW SRM 51-3-0. N/R 5635Feb 1, 2000 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080326CSkin · dentedAT C-CHECK, RIGHT WING TIP T/E DENTED. FABRICATED AND INSTALLED DOUBLER PER SRM 57-2-1. N/R 1097Feb 1, 2000 · N803DH · Doug DC873F · Wing, Plate/SkinSDR DHL200080331CSkin · deformedAT C-CHECK, RIGHT WING I/B FLAP UPPER SURFACE SKIN DEFORMED 2 INCHES BETWEEN XW 41 AND 70.5. REMOVED DAMAGED SKIN, INSTALLED PER SRM 51-1-21. N/R 1340Feb 1, 2000 · N803DH · Doug DC873F · Trailing Edge FlapsSDR RRXA000293Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO OBSERVERS AFT SEAT TRACK AT STA -12 TO STA . DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW DC-8 SRM 51-3-0Jan 31, 2000 · N832AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000507Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 33 RIGHT BETWEEN STA 55 TO STA 70. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DAC DWG 3642838. Jan 31, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000500Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK BETWEEN STA 130 TO STA 200 AND BL 24 LEFT. 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 53-2-3 FIGUREJan 31, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000333Skin · corrodedDURING A MAINTENANCE VISIT FOUND LEFT WING L/E CORRODED, UPPER SURFACE FROM XFS 40 - XFS 100. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPLACEMENT PARTS IAW DC-8 SRM 51-1-20D AND DCJan 31, 2000 · N792FT · Doug DC873F · Leading Edge DevicesSDR UPS00832176Skin · crackedINSPECTION TYPE:C123 (P4735) RE-INSPECT CLASS II REPAIR AT SKIN AND RIVETS FS 1400 AFT BOTTOM RT FUS SKIN (PER SRM 51-5-5). REMOVED EXISTING DOUBLER. REMOVED CRACK AREA IN SKIN. FABRICATED FILLER, REPAIR DOUBLER, TRIPLER. ALODINED, PRIMED AND INSTALLED FILJan 31, 2000 · N804UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS00831464Battery Pack · dischargedEMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK.Jan 31, 2000 · N874UP · Doug DC873F · Emergency LightingSDR DHL200080385CPanel · crackedAT C-CHECK, NR 614 ACCESS DOOR CRACKED 1 INCH AND 8 LOOSE RIVETS ON RT - LT UPPER AND LOWER EDGE. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-21A PG 4 & SRM 51-1-21 PG 7. N/R 4291Jan 31, 2000 · N803DH · Doug DC873F · Nacelle/Pylon, Plate/SkinSDR DHL200080352CSkin · crackedAT C-CHECK, NR 3 CARGO DOOR INTERNAL SKIN CRACKED .5 AND .75 INCH APPROX BETWEEN FS 1225 AND 1235. STOP DRILLED CRACK IAW SRM 52-2-0, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-21, PG 72 & 73. N/R 5347Jan 31, 2000 · N803DH · Doug DC873F · Cargo/Baggage DoorsSDR DHL200080341CFairing · crackedAT C-CHECK, RT WING LOWER SKIN FAIRING SHOWS CRACK 1.25 INCH AT XW 90. FABRICATED DOUBLER IAW SRM 57-2-0 PG 8, INSTALLED DOUBLER IAW SRM 51-1-8 PG 11 AND 12. N/R 1159Jan 31, 2000 · N803DH · Doug DC873F · Aerodynamic FairingsSDR RRXA000644Fitting · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE FOOTSTOOL SUPPORT FITTING UPPER END NR 4 PYLON I/B SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 51-3-0 AND DAC DWG 357Jan 30, 2000 · N831AL · Doug DC873F · Nacelle/Pylon StructureSDR RRXA000634Attach Fitting · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE FRAME ATTACH FITTING AFT OF FRAME AT STA 680 LONGERON 11R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC-8 SRM 51-3-0.Jan 30, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL200080355CSkin · crackedAT C-CHECK, NR 3 CARGO DOOR INTERNAL SKIN CRACKED .5 INCH APPROX BETWEEN FS 1220 AND 1230. STOP DRILLED CRACK IAW SRM 52-2-0, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-21 PG 72 & 73. N/R 5366Jan 30, 2000 · N803DH · Doug DC873F · Cargo/Baggage DoorsSDR DHL200080354CSkin · crackedAT C-CHECK, NR 3 CARGO DOOR INTERNAL SKIN CRACKED 2 INCHES APPROX BETWEEN FS 1210 AND 1230. STOP DRILLED CRACK IAW SRM 52-2-0, PG 7, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-21 PG 72 & 73. N/R 5344Jan 30, 2000 · N803DH · Doug DC873F · Cargo/Baggage DoorsSDR RRXA000292Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 28 LEFT BETWEEN STA 1050 TO STA 1160. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW FAA DER APPROVEJan 29, 2000 · N832AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA002959Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR PANEL AT STA 40, 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 51-1-4. (CORROSION DAMAGE RECORDED IN EWJan 29, 2000 · N792FT · Doug DC873F · Fuselage Floor PanelSDR RRXA000499Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CENTER AUX TANK LOWER SKIN AT XFS 107.5. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED ENGINEERING SKETCHJan 29, 2000 · N831AL · Doug DC873F · Wing, Center BoxSDR DHL200080390CAccess Door · crackedAT C-CHECK, ELECTRONIC COMPARTMENT COCKPIT NR 614 ACCESS PANEL CRACKED 1 INCH RT - LT LOWER EDGE. PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW SRM 53-2-0 PAGE 2P. CLEANED, TREATED AND PRIMED INDICATED AREA IAW SRM 51-1-8 PAGE 11 & 12. INSTALLED DOUBLER WJan 29, 2000 · N803DH · Doug DC873F · Accessory Compartment DoorsSDR DHL200080390Access Door · crackedELECTRONIC COMPARTMENT COCKPIT NR 614 ACCESS PANEL CRACKED 1 INCH RT - LT LOWER EDGE. PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW SRM 53-2-0 PAGE 2P. CLEANED, TREATED AND PRIMED INDICATED AREA IAW SRM 51-1-8 PAGE 11 & 12. INSTALLED DOUBLER WITH SOLID RIJan 29, 2000 · N803DH · Doug DC873F · Accessory Compartment DoorsSDR DHL200080378CSkin · misrepairedAT C-CHECK, FUSELAGE UPPER AND LOWER SURFACE SHOWS REPAIR INAPPROPIATE AT FS 1705 CLOSE TO L-20 RT. REMOVED OLD REPAIR, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-1 PG 105-106. N/R 5452Jan 29, 2000 · N803DH · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA000291Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA 159 AND BL/L 48. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC-8 SRM 51-3-3.Jan 28, 2000 · N832AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000290Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CARGO SEAT TRACK AT STA 280 AND BL/L 55. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW FAA DER APPRVED ENGINEJan 28, 2000 · N832AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS00831399Battery Pack · dischargedEMERGENCY LIGHTS WILL NOT TEST. REPLACED BATTERY PACK.Jan 28, 2000 · N836UP · Doug DC873F · Emergency LightingSDR DHL200080391CFloor Support · crackedAT C-CHECK, FWD LOWER CARGO FLOOR SUPPORT FLANGE BETWEEN LONGERONS 31 AND 32 CRACKED 1 INCH. REMOVED AFFECTED AREA IAW SRM 51-1-21A PAGE 4. FABRICATED DOUBLER AND TREATED IAW SRM 53-2-0 PAGE 10 TO 12. INSTALLED DOUBLER WITH SOLID RIVETS ON FLOOR SUPPORT FLAJan 28, 2000 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080391Floor Support · crackedFWD LOWER CARGO FLOOR SUPPORT FLANGE BETWEEN LONGERONS 31 AND 32 CRACKED 1 INCH. REMOVED AFFECTED AREA IAW SRM 51-1-21A PAGE 4. FABRICATED DOUBLER AND TREATED IAW SRM 53-2-0 PAGE 10 TO 12. INSTALLED DOUBLER WITH SOLID RIVETS ON FLOOR SUPPORT FLANGE IAW SRM Jan 28, 2000 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080372CVane · delaminatedAT C-CHECK, RT WING NR 5 FLAP VANE UPPER SKIN DELAMINATED. REMOVED VANE AND REPAIRED IAW MM 27-51-14, INSTALLED VANE IAW MM 27-51-14 PG 201, 202 203. OPERATIONAL CHECK GOOD IAW MM 27-51-14 PG 202 & 203. N/R 1015Jan 28, 2000 · N803DH · Doug DC873F · Trailing Edge FlapsSDR DHL200080343CFloor Support · crackedAT C-CK, AFT BAGGAGE COMPARTMENT FLOOR SUPPORT ANGLE CRACKED 2INCHES AT STA 1300, L-3 RT. FABRICATED AND INSTALLED DOUBLER ON FLOOR SUPPORT ANGLE IAW SRM 53-2-0, PG 10 & 11, FIG 16, 2B. N/R 5582.Jan 28, 2000 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000363Panel · damagedDURING A MAINTENANCE VISIT FOUND RIGHT I/B SLOT STUB WING AT XS 260 RIVET SHEARED OFF. PLUGGED HOLE IAW EO 00-016.Jan 27, 2000 · N792FT · Doug DC873F · Wing, Plate/SkinSDR UPS00831396Valve · failedLOUD NOISE AFTER TAKEOFF. GEAR WOULD NOT COME UP UNTIL FLT RELEASE HANDLE LATCH WAS USED. WHEN FLAPS WERE RETRACTED HAD A WARNING HORN AND SLOT LIGHT. DUMPED FUEL AND RETURNED TO SDF. REMOVED AND REPLACED NOSEWHEEL STEERING SHUTOFF VALVE PER MM 32-52-0 8. Jan 27, 2000 · N866UP · Doug DC873F · Landing Gear Steering SystemSDR DHL200080327CDeflector · missingAT C-CHECK, NR 3 ENGINE INLET COWL ANTI-ICE DEFLECTOR MISSING 2 O''CLOCK. COMPLIED WITH S/B 71-97. N/R 7126Jan 27, 2000 · N803DH · Doug DC873F · Airfoil Anti/De-ice SystemSDR DHL200080325CDeflector · missingAT C-CHECK, NR 4 ENGINE INLET COWL ANTI -ICE DEFLECTOR MISSING AT 11 O''CLOCK POSTION. PERFORMED S/B 71-97. N/R 7127.Jan 27, 2000 · N803DH · Doug DC873F · Airfoil Anti/De-ice System
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