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 UPS00833238Battery Pack · inoperativeEMERGENCY EXIT LIGHT INOPERATIVE. R&R BATTERY PACK CHKS GOODJul 7, 2000 · N819UP · Doug DC873F · Emergency LightingSDR RRXA002784Skin · dentedDURING A MAINTENANCE VISIT FOUND 3 DENTS ON THE RIGHT I/B FLAP UPPER SURFACE, 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 SRM 57-2-1 AND 51-1-21.Jul 6, 2000 · N602AL · Doug DC873F · Trailing Edge FlapsSDR RRXA002783Brace · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LEFT WING FLAP CANOE SIDE BRACE AT STA 98 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-186 WITH APPROVED 81Jul 6, 2000 · N602AL · Doug DC873F · Trailing Edge Flap Control SystemSDR RRXA002782Link · gougedDURING A MAINTENANCE VISIT FOUND A GOUGE TO THE LEFT O/B FLAP AFT LINK AT STA 410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-186 WITH APPROVED 8110-3 DATEJul 6, 2000 · N602AL · Doug DC873F · Trailing Edge Flap Control SystemSDR RRXA002787Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE, PITTING AND SMALL AREA OF GOUGING ON THE RT WING FLAP LWR MOUNT AT STA 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLEJul 5, 2000 · N602AL · Doug DC873F · Trailing Edge FlapsSDR RRXA002786Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE, PITTING AND SMALL AREA OF GOUGING ON THE RT WING FLAP LWR MOUNT AT STA 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLEJul 5, 2000 · N602AL · Doug DC873F · Trailing Edge FlapsSDR RRXA002785Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE, PITTING AND SMALL AREAS OF GOUGING TO THE RT WING FLAP LWR MOUNT AT STA 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLEJul 5, 2000 · N602AL · Doug DC873F · Trailing Edge FlapsSDR RRXA002781Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE, PITTING AND SMALL AREAS OF GOUGING ON THE LT FLAP LWR MOUNT AT STA 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAJul 5, 2000 · N602AL · Doug DC873F · Trailing Edge FlapsSDR RRXA002780Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE, PITTING AND SMALL AREAS OF GOUGING ON THE LT FLAP LWR MOUNT AT STA 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAJul 5, 2000 · N602AL · Doug DC873F · Trailing Edge FlapsSDR RRXA002779Fitting · gougedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE, PITTING AND SMALL AREAS OF GOUGING TO THE LT FLAP LWR MOUNT AT STA 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAWJul 5, 2000 · N602AL · Doug DC873F · Trailing Edge FlapsSDR RRXA001009A/C Pack · malfunctionedAIRCRAFT WILL NOT PRESSURIZE. RIGHT PACK INOPERATIVE. PRESSURIZED AIRCRAFT TO 8.8 TO 9 PSID-NO LEAKS NOTED 21-10-00-RT PACK OPERATIONAL CK''S GOOD ON GROUND AT THIS TIME.Jul 4, 2000 · N831AL · Doug DC873F · Cabin Pressure Control SystemSDR RRXA003730Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RIGHT AFT LOWER STAB WIPER PANEL AT STA 1723-1849, L15R, 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 51-1-4 , Jul 3, 2000 · N961R · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA002789Link · gougedDURING A MAINTENANCE VISIT FOUND A GOUGE TO THE LT WING O/B FLAP FWD LINK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-186 WITH APPROVED 8110-3 DATED 7-3-00Jul 3, 2000 · N602AL · Doug DC873F · Trailing Edge Flap Control SystemSDR DHLA200072201Static Wick · failedCOM NR 1 & 2 WEAK AND HAS CONSIDERABLE STATIC IN PRECIPITATION AND SQUEALS. LOST COMS FOR UP TO 1 MINUTE SEVERAL TIMES. REPLACED SEVERAL STATIC WICKS ON WINGS AND HORIZONTAL STAB. SYSTEMS OPS CHECKED GOOD IAW MM 23-20-0Jul 2, 2000 · N803DH · Doug DC873F · Static Discharge SystemSDR RRXA001007Fitting · crackedDURING A PRE-FLIGHT, FOUND LT WING OUTBOARD FLAP SUPPORT FITTING CRACKED, AT XFS 219. REMOVED CRACKED SUPPORT FITTING. RECEIVED NEW FITTING AND INSTALLED IAW DC-8 MAINTENANCE MANUAL AND SB 27-249. OPERATIONS CHECK PREFORMED SERVICEABLE.Jun 30, 2000 · N873SJ · Doug DC873F · Trailing Edge FlapsSDR UPS00833082Connector · looseON CLIMBOUT, EMERGENCY LIGHTING ILLUMINATED. ALL ELECTRICAL BUSSES VOLTS / FREQS WERE NORMAL, BATTERY VOLTAGE NORMAL. FOUND EMERGENCY EXIT LIGHTING CONTROL CB POPPED. RESET WITHOUT FURTHER PROBLEMS.(DC BUS 1) FOUND EMERGENCY LIGHT BATTERY PACK ELECTRICAL CJun 30, 2000 · N874UP · Doug DC873F · Emergency LightingSDR UPS00833080Switch · inoperativeRIGHT MAIN LANDING GEAR INDICATED UNSAFE. CHANGED LIGHT BULBS, NO JOY. CKD FLAPS 35, NO HORN. FLY BY TOWER INDICATING GEAR WAS DOWN. LANDED STRAIGHT AHEAD - GEARS PINNED. T/S IN WORK NOW. MAYBE BAD SWITCH RIGHT GEAR DOWN. ***SUPPLEMENTAL M RR*** REMOVED Jun 29, 2000 · N866UP · Doug DC873F · Landing Gear Position and WarningSDR DHL2000801103Skin · wornAT C CK; LT WING IB TRAILING EDGE, OB FLAP LE WORN FROM XW 240.00 TO XW 280.00. REMOVED DAMAGED FILLET IAW SRM 51-1-21A, PAGE 4, CLEANED AND PRIMED AREA IAW SRM 51-1-8B, PAGE 1-2, FABRICATED AND INSTALLED NEW FILLET IAW SRM 51-1-21A, PAGE 3. REF: N/R 1092.Jun 23, 2000 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL2000801102Skin · deformedAT C CK; LT IB WING, TE OB FLAP DEFORMED AT XW 255.00. REMOVED DEFORMED T/E IAW SRM 51-1-21 PAGE 1, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PAGE 1-2, FABRICATED AND INSTALLED TE SECTION IAW SRM 51-7-21 PAGE 1. REF: N/R 1090.Jun 23, 2000 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL2000801100Skin · deformedAT C CK; RT WING, IB FLAP TE DEFORMED AT XWS 120.00 AND 135.00. REMOVED FASTNERS IAW SRM 51-1-21 PAGE1, CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B, PAGE 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-21, PAGE 1. REF: N/R 1099.Jun 23, 2000 · N801DH · Doug DC873F · Trailing Edge FlapsSDR RRXA003414Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AT FWD LAV AREA BETWEEN STA'S 35.000 AND 55.000 AND X-44 AND -66, 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 SRM 51-20-01 Jun 22, 2000 · N796FT · Doug DC873F · Fuselage Floor PanelSDR DHL200080199CCargo Track · wornAT C CK; MAIN CARGO COMPARTMENT 3 RT TRACK WORN AND CORRODED FROM STA. 1490.0 TO 1540.0. REMOVED DAMAGED TRACK IAW SRM 51-3-0 PAGE 1, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PAGE 1-2, INSTALLED NEW TRACK IAW SRM 51-3-0. REF: N/R 1619.Jun 22, 2000 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS00833025Flange · misdrilledINSPECTION TYPE: C2 R-2 DOOR SEAL DEPRESSOR, LWR SECTION HAS BAD HOLES. LOCATED & DRILLED NEW SEAL DREPRESSOR IAW DC8 SRM 51-1-24. ALODINE & PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SEAL DEPRESSOR IAW DC8 S RM 51-1-20D & 51-1-21.Jun 22, 2000 · N803UP · Doug DC873F · Passenger/Crew DoorsSDR UPS00832977Light · inoperativeINSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP. REPLACED B5-55 EMERGENCY LIGHTS, OP CHECKS NORMAL.Jun 22, 2000 · N866UP · Doug DC873F · Emergency LightingSDR UPS00832960Skin · crackedINSPECTION TYPE:C2, FUSELAGE SKIN CRACKED AT R2 DOOR, FWD LWR CORNER. ROUTED OUT CRACK IAW DC8 SRM 53-2-0 FIG 16. FABBED AND INSTALLED REPAIR DOUBLERS AND FILLERS IAW DC8 SRM 53-2-0 FIG 16 AND 51-1-20D AND 5 1-3-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.Jun 22, 2000 · N803UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL200080195CFitting · crackedAT C CK; MAIN CARGO COMPARTMENT, BATHTUB FITTING CRACKED (2 INCHES) STA. 680.00, L-4 LT. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, PAGE 9-21. REF: N/R 1080.Jun 21, 2000 · N801DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL200080188CAngle · crackedAT C CK; FWD CARGO COMPARTMENT, LINING SUPPORT ANGLE LWR PART CRACKED 1INCH STA. 640.00 BETWEEN L-30L AND L-31LT. PERFORMED STOP DRILL IAW SRM 53-2-5 FIG 8B-1, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-5 FIG 8B-1. REF: N/R 1930.Jun 21, 2000 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080186CFitting · crackedAT C CK; MAIN CARGO COMPARTMENT BATH TUB FITTING CRACKED 4 INCHES AT STA. 680.0 L-5 RT. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D PAGE 21-9. REF: N/R 2222.Jun 21, 2000 · N801DH · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS00833042Light · inoperativeON PREFLIGHT EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE. R & R EMERGENCY EXIT LIGHT BATTERY PACK. OPS CHECK OK P/N ON 5708458-503 SN ON NC 2624 P/N OFF 60-1223-5 SN OFF 348Jun 21, 2000 · N805UP · Doug DC873F · Emergency LightingSDR DHL2000801118Cargo Track · corrodedMAIN CARGO COMPT FLOOR TRACK 3 LT SHOWS CORROSION AT STA 1460.000. CUT OUT DAMAGED AREA PER SRM 53-2-3. FABRICATED CHANNEL AND PLUG PER SRM 53-2-3. CLEANED, TREATED AND PRIMED PER 51-1-8B. INSTALLED CHANNEL AND PLUG PER SRM 53-2-3.Jun 20, 2000 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL200080194CFitting · crackedAT C CK; MAIN CARGO COMPARTMENT, FRAME FITTING CRACKED 4 INCHES AT STA. 680.00, L-11 RT, UPPER PART. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, PAGE 21-9. REF: N/R 1177.Jun 20, 2000 · N801DH · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL200080193CFitting · corrodedAT C CK; AFT ACCESSORY COMPARTMENT, FITTING SHOWS CORROSION AT STA. 1690.0, L-30 RT. REMOVED DAMAGED FITTING IAW SRM 51-1-20D, PAGE 24, PERFORMED ANTI-CORROSION TREATMENT AND PRIMED AREA IAW SRM 51-1-8B, PAGE 1-2, INSTALLED NEW FITTING IAW SRM 51-1-20D, PAGE Jun 20, 2000 · N801DH · Doug DC873F · Fuselage, Equipment Attach FittingsSDR DHL200080192CFitting · crackedAT C CK; AFT ACCESSORY COMPARTMENT, FITTING SHOWS CORROSION AT STA. 1690.0, L-32 RT. REMOVED DAMAGED FITTING IAW SRM 51-1-20D, PAGE 21, PERFORMED ANTI-CORROSION TREATMENT AND PRIMED IAW SRM 51-1-8B, PAGE 1-2, INSTALLED NEW FITTING IAW SRM 51-1-20D, PAGE 9. REFJun 20, 2000 · N801DH · Doug DC873F · Fuselage, Equipment Attach FittingsSDR DHL200080191CFitting · corrodedAT C CK; AFT ACCESSORY COMPARTMENT, FITTING SHOWS CORROSION AT STA. 1690.00, L-27LT. REMOVED DAMAGED FITTING IAW SRM 51-2-20D, PAGE 21, PERFORMED ANTI-CORROSION TREATMENT AND PRIMED AREA IAW SRM 51-1-8B, PAGE 1-2, INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 9.Jun 20, 2000 · N801DH · Doug DC873F · Fuselage, Equipment Attach FittingsSDR DHL200080196CCargo Track · wornAT C CK; MAIN CARGO COMPARTMENT 1 LT TRACK LUGS WORN AT STA. 680. CUTOUT DAMAGED AREA IAW SRM 53-2-3 PAGE 17, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PAGE 1-2, INSTALLED CHANNEL AND PLUG IAW SRM 53-2-3.Jun 20, 2000 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001002Structure · crackedLT GEAR DOOR CRACKED IN TWO PLACES (MAIN LANDING). PERFORMED PLATING REPAIR IAW DC-8 SRM CHAP 52-2-0 FIG 2.Jun 20, 2000 · N961R · Doug DC873F · Landing Gear DoorsSDR DHL200080146CSkin · dentedAT C CK; LT HORIZONTAL STABILIZER ELEVATOR UPPER PART DENTED 2 INCHES AT XE. 66.250. CUTOUT DAMAGED SKIN IAW SRM 51-1-21A, FABRICATED AND INSTALLED FILLER AND NEW SKIN IAW SRM 51-1-21A PAGE 3. REF: N/R 2116.Jun 19, 2000 · N801DH · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR DHL200080143CSkin · canningAT C CK; LT HORIZONTAL STABLIZER ELEVATOR UPPER SKIN SHOWS OIL CANNING AT XS. 272.00. REMOVED DAMAGED SKIN IAW SRM 51-1-21 PAGE 1, FABRICATED AND INSTALLED NEW SKIN IAW SRM 55-2-1 PAGE 6. REF: N/R 2119.Jun 19, 2000 · N801DH · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR DHL200080163CAngle · crackedAT C CK; LT WING TO FUSELAGE UPPER FAIRING SUPPORT ANGLE CRACKED 1/4 INCH AT STA. 920. PERFORMED STOP DRILL IAW SRM 53-2-0, FABRICATED AND INSTALLED ANGLE IAW SRM 53-2-0. REF: N/R 1437.Jun 19, 2000 · N801DH · Doug DC873F · Aerodynamic FairingsSDR DHL200080160CSupport Bracket · crackedAT C CK; FWD CARGO COMPARTMENT-LINING SUPPORT SHOWS 1&1/2 INCH. REMOVED CRACKED LINING, WELDED CRACKED AREA IAW DPS 10-225, REINSTALLED REPAIRED LINING SUPPORT.Jun 19, 2000 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2000801110Rib · crackedLT WING LEADING EDGE RIB CRACKED 1/45 IN AT STA XFS 650.000. STOP DRILLED PER SRM 57-2-0. FABRICATED REINFORCING ANGLE PER SRM 57-2-0. CLEANED, TREATED AND PRIMED PER SRM 51-1-8B. INSTALLED ANGLE PER SRM 57-2-0 FIG 2.Jun 18, 2000 · N801DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2000801108Rib · crackedLT WING LEADING EDGE RIB CRACKED .25 INCH. STOP DRILLED PER SRM 57-2-0. FABRICATED DOUBLER PER SRM 57-2-0. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED DOUBLER PER SRM 51-2-0.Jun 18, 2000 · N801DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL200080145CSkin · dentedAT C CK; RT OB FLAP TE DENTED AT STA. 410.000. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-2-0. REF: N/R 1900.Jun 18, 2000 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL200080144CSkin · dentedAT C CK; LT HORIZONTAL STABLIZER ELEVATOR UPPER SKIN SHOWS DENTS FROM XS. 99.241 REMOVED DAMAGED SKIN IAW SRM 51-1-21 PAGE 1. FABRICATED AND INSTALLED NEW SKIN IAW SRM 51-1-21. REF: N/R 2118.Jun 18, 2000 · N801DH · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR DHL200080159CCargo Track · wornAT C CK; MAIN CARGO COMPARTMENT FLOOR TRACK 1RH LUGS WORN STA. 781.000. CUTOUT DAMAGED AREA IAW SRM 53-2-3, FABRICATED AND INSTALLED CHANNEL IAW SRM 51-1-8B. REF:N/R 1758.Jun 18, 2000 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL200080158CFloor Support · misrepairedAT C CK; MAIN CARGO COMPARTMENT RT FLOOR SHOWS AN IMPROPER REPAIR AT STA. 165.0. CUTOUT IMPROPER REPAIR IAW SRM 53-2-3 PAGE 1, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 53-2-3 PAGE 1. REF: N/R 2158.Jun 18, 2000 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080157CSupport Bracket · crackedAT C CK; FWD CARGO COMPARTMENT LINING SUPPORT CRACKED 3/4 INCH AND 1/4 INCH AT STA. 240 BETWEEN L-35 - L36LT. REMOVED CRACKED SUPPORT IAW SRM 51-1-21 PAGE 1, WELDED CRACKED AREA IAW DPS 10.225, REINSTALLED IAW SRM 51-1-21 PAGE 1. REF: N/R 0936.Jun 18, 2000 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2000801105Rib · crackedAT C CK; LT WING LEADING EDGE RIB CRACKED 1/2 INCH. STA. XFS. 725.000. PERFORMED STOP DRILL IAW SRM 57-2-0, PAGE 12, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B, PAGE 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0, PAGE 12. REF: N/R 0443.Jun 17, 2000 · N801DH · Doug DC873F · Leading Edge DevicesSDR DHL2000801104Rib · crackedAT C CK; LT WING LEADING EDGE RIB CRACKED 1/4 INCH, STA. XFS. 730.000. PERFORMED STOP DRILL IAW SRM 57-2-0 PAGE 12, CLEANED,TREATED AND PRIMED AREA IAW SRM 51-1-8B,PAGE 1-2, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0, PAGE 12. REF: N/R 0442.Jun 17, 2000 · N801DH · Doug DC873F · Leading Edge DevicesSDR DHL200080137CRib · crackedAT C CK; LT WING LEADING EDGE (2EA) RIBS CRACKED 1/4 INCH STA. XFS. 750.000. PERFORMED STOP DRILL IAW SRM 57-2-0 PAGE 12, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0 PAGE 12. REF: N/R 0440.Jun 17, 2000 · N801DH · Doug DC873F · Leading Edge Devices
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