Douglas DC-8-73F

Service difficulty reports · 15,471

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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"

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SDR DHL2003873503Frame · crackedRT WING CENTER LE FORMER CRACKED 0.250 AT XFS 297.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. 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 ANJun 12, 2003 · N873SJ · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003873502Frame · crackedRT WING CENTER L/E FORMER CRACKED 0.250 AT XFS 316.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. 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. INTALLED REINFORCING ANJun 12, 2003 · N873SJ · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003873501Seat Track · damagedFLIGHT COMPT F/E FWD SEAT TRACK SHOWS HOLES ELONGATED. REMOVED AND REPLACED F/E FWD SEAT TRACK (FLIGHT COMPT) IAW SRM 51-3-0 PG 1.Jun 12, 2003 · N873SJ · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS03840911Skin · corrodedINSPECTION TYPE: C3, EXTERIOR FUSELAGE SKIN STA 670 ON CENTERLINE OF BELLY, SKIN AT ANTENNA MOUNT FOUND TO BE CORRODED. BLENDED CORROSION. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED DOUBLER AND FINGER DOUBLERS IAW DC8 SRM 53-2-1 AND 51-1-24. ALODINED Jun 12, 2003 · N851UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003604761Skin · dentedEXTERIOR SKIN WITH DENT AND WEAR OUT OF LIMITS BETWEEN STA. 120.000 AND STA. 210.000, L-20L TO L-22L. PERFORMED MAJOR REPAIR IAW EODHL-030528, ED-3316. REMOVED FASTENERS AND EXISTING REPAIR DOUBLER. BLENDED OUT AFFECTED AREA. PERFORMED EDDY CURRENT INSPECTIONJun 11, 2003 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003604763Attach Fitting · corrodedMAIN CARGO COMPT T-FITTING ATTACHING NR 4 TRACK TO FLOORBEAM AT STA 1704.000 CORRODED. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1 ATM NR P0201387, DWG 5755032. REMOVED CORRODED FITTING IAW SRM 51-3-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND Jun 11, 2003 · N604AL · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2003604711Skin · crackedFUSELAGE NOSE SECTION EXTERIOR SKIN CRACKED 0.825 AROUND AFT LOWER JAMB OF RAM AIR EXHAUST DOOR STA FS 12.000, L-27L. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END (0.250) DIA IAW EODHL-030548, ED-3383. PERFORMED EDDY CURRENT INSPJun 11, 2003 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003604654Skin · corrodedLT INNER WING CTR L/E LOWER PLATING SHOWS THREE INTERIM REPAIRS AND CORROSION AROUND STA XFS 304.000. REMOVED FASTENERS. REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT THE DAMAGED AREA, PERFORMED EDDY CURRENT INSPECTION. CLEANED, TREATED AND PRIMED ARJun 11, 2003 · N604AL · Doug DC873F · Wing, Plate/SkinSDR DHL2003604600Skin · corrodedLT RUDDER INTERNAL SKIN CORRODED, STA ZR 150.000 - ZR 178.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12. REMOVED DAMAGED SKIN PANEL IAW EODHL-030533, ED-3354. CLEANED, TREAJun 11, 2003 · N604AL · Doug DC873F · Rudder, Plate/SkinSDR DHL2003604588Frame · crackedTAIL CONE SECTION - FRAME CRACKED 1.000 STA. 1937.000 LH SIDE. STOP DRILLED CRACK AND FABRICATED DOUBLER (2024-T3 AL0.040) IAW SRM 53-2-0 FIG.2. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED NEW DOUBLER IAW SRM 51-1-21 PG.1, SRM 51-Jun 11, 2003 · N604AL · Doug DC873F · Aerodynamic FairingsSDR DHL2003604589Frame · crackedTAIL CONE SECTION FRAME CRACKED 1.000 STA 1923.000 RT SIDE. STOP DRILLED CRACK AND FABRICATED DOUBLER IAW SRM 53-2-0 FIG 2. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1.Jun 11, 2003 · N604AL · Doug DC873F · Aerodynamic FairingsSDR DHL2003604590Tie · crackedFUSELAGE TAIL CONE INTERIOR RT TIE 1.000 CRACKED AT STA 1923.000. STOP DRILLED CRACK AND FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1.Jun 11, 2003 · N604AL · Doug DC873F · Aerodynamic FairingsSDR DHL2003873507Frame · crackedLT WING OUTBD L/E FORMER CRACKED 0.250 AT XFS 882.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. 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 REINFORCING ANGLE IAW SRM 51-1-8B. INSTALJun 11, 2003 · N873SJ · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003873506Frame · crackedLT WING OUTBD L/E FORMER CRACKED 0.250 AT STA XFS 566.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. 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 REINFORCINJun 11, 2003 · N873SJ · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003806009Seal · leakingFUEL LEAK UNDER WING BETWEEN NR 3 & 4 PYLON. TORQUED GAMMA SEAL JUST OUTBOARD NR 3 PYLON LEAK CHECKED GOOD IAW M/M 28-21-14.Jun 11, 2003 · N806DH · Doug DC873F · Aircraft Fuel Distribution SystemSDR DHL2003801004Cylinder · out of adjustUPON LANDING GEAR RETRACTION DOORS NOT LATCHED AND LEFT DOOR UNSAFE LIGHTS ILLUMINATED APPROPRIATE ABNORMAL PROCEDURE PERFORMED LIGHTS REMAINED ON GEAR NOT LATCHED LIGHT ILLUMINATED IN CVG PATTERN RIGHT DOOR UNSAFE LIGHT ILLUMINATED. ADJUSTED LEFT GEAR DOOR AJun 11, 2003 · N801DH · Doug DC873F · Landing Gear Door Retract SectionSDR DHL2003604784Skin · delaminatedLT ELEVATOR CONTROL TAB UPPER SKIN DELAMINATED. REMOVED AND REPLACED LT ELEVATOR CONTOL TAB IAW MM 27-30-2 PG 201-204. REFER TO N/R 0531 FOR OPS CHECK.Jun 10, 2003 · N604AL · Doug DC873F · Elevator, Tab StructureSDR DHL2003604584Access Door · corrodedLT C/W AUX TANK - PERFORM ANTI-CORROSION TREATMENT TO LT 5056 ACCESS DOOR. REMOVED CORROSION ON LT 5056 ACCESS DOOR IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG.43. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DOUBLER (7075Jun 10, 2003 · N604AL · Doug DC873F · Wing, Center BoxSDR DHL2003604587Fitting · crackedRUDDER FITTING ASSY IN RUDDER INNER STRUCTURE CRACKED STA. 104.000 (WATER DRAIN) REMOVED CRACKED FITTING IAW SRM 51-1-21 PG.1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-21 PG.1Jun 10, 2003 · N604AL · Doug DC873F · Rudder StructureSDR DHL2003604583Access Panel · corrodedRT C/W AUX TANK, PERFORM ANTI-CORROSION TREATMENT TO RT UPPER ACCESS DOOR NR 5056. REMOVED CORROSION ON 5056 RT UPPER ACCESS DOOR IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 43. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED DJun 10, 2003 · N604AL · Doug DC873F · Aircraft Fuel Distribution SystemSDR DHL2003873508Frame · crackedLT WING CTR L/E FORMER CRACKED 0.250 AT STA XFS 379. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT XFS 379 IAW SRM 57-2-0 PG 9,10. FABRICATED REINFORCEMENT ANGLE IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED REINFORCEMENT ANGLE IAW SRJun 10, 2003 · N873SJ · Doug DC873F · Wing, Rib/BulkheadSDR DHL2003604730Door Frame · wornCARGO DOOR JAMB SHOWS WEAR OUT OF LIMITS AT STA.1440.000 L-29R - L30R. PERFORMED MAJOR REPAIR IAW EODHL-03557, ED-3317. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. BLENDED OUT DAMAGED AREA IAW EODHL-03557, ED-3317. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SJun 9, 2003 · N604AL · Doug DC873F · Fuselage Main, StructureSDR DHL2003604727Stiffener · crackedMAIN CARGO COMPT. FLOORBEAM INTERCOSTAL JOINT SHOWS STIFFENER CRACKED (1.000) STA.702.000 BL-0. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG.1, ATM P0201384, DWG.5773275. REMOVED CRACKED STIFFENER IAW SRM 51-1-20D PG.21, SRM 51-1-21 PG.1. FABRICATED NEW STIFFENEJun 9, 2003 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2003604585Frame · crackedLT. WING CENTER L/E FORMER CRACKED 3.000 AT STA. XOLDI 6.225. STOP DRILLED CRACK AT STA. XOLDI 6.225 AND FABRICATED REINFORCEMENT ANGLE (301 0.250H 0.032) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED REINFORCEMENT ANGLE Jun 9, 2003 · N604AL · Doug DC873F · Wing SparSDR DHL2003604607Skin · delaminatedLT WING NR 1 VANE FLAP INTERNAL SKIN DELAMIATED. REMOVED AND REPLACED NR 1 VANE FLAP ON LT WING IAW MM 27-51-14 PG 201, 202. FOR OPS CHECK SEE N/R.Jun 9, 2003 · N604AL · Doug DC873F · Trailing Edge FlapsSDR DHL2003604782Skin · corrodedUPPER EXTERNAL FUSELAGE SKIN CORRODED AT STA 680.000, L-2L - L-2R. PERFORMED MAJOR REPAIR IAW EODHL-030540, ED-3308. REMOVED FASTENERS, REMOVED CORROSION ON AFFECTED AREA , FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. BLENDED OUT AFFECTED AREA IAW EODHL-030540Jun 8, 2003 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003604740Frame · corrodedAFT CARGO COMPT FRAME ANGLE DOUBLER CORRODED AT STA 1040.000 L-33R - L-34R. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED CORROSION ON FRAME ANGLE DOUBLER IAW SRM 51-1-8 PG 17-18. FOUND OUTJun 8, 2003 · N604AL · Doug DC873F · Fuselage Main, FrameSDR DHL2003604717Skin · crackedFUSELAGE NOSE SECTION SKIN CRACKED 1.125, STA 12.000 L-27R AT STRUCTURAL MODIFICATION. PERFORMED MAJOR REPAIR IAW EODHL-030549, ED3384. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END USING A 0.250 DIA DRILL IAW EODHL-030549, ED-338Jun 8, 2003 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003604789Skin · crackedEXTERNAL FUSELAGE SKIN CRACKED 0.450, STA 1160.000 BETWEEN L-26R AND L-28R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL-030555, ED-3311. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW EODHL-030555, ED-3311. PERFORMED EDDY CURRENT Jun 8, 2003 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003604714Skin · corrodedLOWER FUSELAGE EXTERIOR SKIN SHOWS SEVERAL SPOTS OF CORROSION BETWEEN STA 510.000 AND 570.000, L-31R - L-34R. PERFORMED MAJOR REPAIR IAW EODHL-030541, ED-3310. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF Jun 8, 2003 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003604661Skin · corrodedRT WING CTR L/E LWR EXTERNAL SKIN SHOWS CORROSION, XFS 341.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED OUT DAMAGED SKIN SECTION IAW EODHL-030531, ED-3304. PERJun 8, 2003 · N604AL · Doug DC873F · Wing, Plate/SkinSDR UPS03840926Skin · damagedINSPECTION TYPE: C, COMPLY WITH MPI P 14035: IAW M REPAIR TO AIRSTART DOOR CUTOUT AT 100Y CYCLES OR 3 MONTHS WHICHEVER COMES FIRST IAW EO DC8-5330-0793, STATION 25 TO 55 LONG. 28L-30L AT DOOR CUTOUT REMOVED EXISTING FILLERS,NDT VERIFIED NO CRACKS AT EXIJun 8, 2003 · N807UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003604704Fitting · corrodedFWD CARGO COMPT END FITTING CORRODED, STA 70.000, L-27R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21 SRM 51-1-21 PG 1. REMOVED CORROSION FROM END FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-2-0 PG 2P. REMJun 7, 2003 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2003604712Skin · damagedC-CARGO DOOR EXTERNAL SKIN WITH INTERIM REPAIR AND DENTS AT SEVERAL SPOTS. PERFORMED MAJOR REPAIR IAW SRM 52-1-0 PG 1, SRM 52-4-1 FIG 2, BOEING MESSAGE DHL-CVG-0079H. REMOVED DAMAGED SKIN IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMEDJun 7, 2003 · N604AL · Doug DC873F · Cargo/Baggage DoorsSDR DHL2003604764Fitting · corrodedFWD CARGO COMPT END FITTING AT STA 70.000, L-27L CORRODED. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21, SRM 51-1-21 PG 1. REMOVED CORROSION FROM END FITTING IAW SRM 51-1-8 PG 17-18. FOUND OUT OF ALLOWABLE LIMITS IAW SRM 53-2-0 PG 21. Jun 7, 2003 · N604AL · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2003604677Skin · dentedLT HORIZ STAB L/E OUTER SKIN DENTED FROM STA XFS 91.250 - XFS 116.250. PERFORMED MAJOR REPAIR IAW EODHL-030515, ED-3270. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EODHL-030515, ED-3270. CLEANED, TREATED AND PRIMED AREJun 6, 2003 · N604AL · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR DHL2003604715Skin · crackedUPPER FUSELAGE EXTERIOR SKIN WITH 0.750 CRACK AT STA 1751.000 BETWEEN L-14L AND L-17L. PERFORMED MAJOR REPAIR IAW EODHL-030546, ED-3298. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED AREA IAW EODHL-030546, ED-3298. PERFORMED EDDY CURRENT INSPECTIJun 6, 2003 · N604AL · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003604662Skin · dentedLT HORZ STAB L/E HAS INTERIM REPAIR & SEVERAL DENTS BETWEEN STA XFS 47.500 AND XFS 91.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EO DHL 030505, ED 3270. REMOVED FASTENERS & EXISTING INTERIM REPAIR IAW SRM 51-1-21 PG 1, SRM 51-1-21A PG 4. CLEANED, TREATEJun 6, 2003 · N604AL · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR DHL2003604569Skin · crackedLT WING INBD FLAP PLATING CRACKED 2.000 STA XW 125.000 - XW 128.000. REMOVED CRACKED PLATING IAW SRM 51-1-21 PG 1. FABRICATED NEW PLATING IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 1. CLEANTED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLATING IAW SRJun 6, 2003 · N604AL · Doug DC873F · Trailing Edge FlapsSDR DHL2003604573Skin · crackedLT WING OTBD SKIN SEGMENT FLAP PLATING CRACKED 2.00, XW 160.000 - XW 169.000. CUT OUT DAMAGED AREA AND FABRICATED SPLICE AND NEW SKIN SEGMENT IAW SRM 57-2-0 FIG 4. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED SPLICE AND NEW SKIN SEGMENT IAW SJun 6, 2003 · N604AL · Doug DC873F · Wing, Plate/SkinSDR DHL2003604576Angle · crackedLT WING OUTBD FLAP (TEE) ANGLE CRACKED 2.000 AT STA XF.165.000. REMOVED DAMAGED (TEE) ANGLE AT STA XF.165.000 IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED ARE IAW SRM 51-1-8B. INSTALLED NEW (TEE) ANGLE IAW SRM 51-1-21 PG 1.Jun 6, 2003 · N604AL · Doug DC873F · Trailing Edge FlapsSDR UPS03840908Longeron · crackedINSPECTION TYPE: C3 AFT PIT FS 1350, LONGERON 35L IS CRACKED. REMOVED CRACKED LONG 35L FS 1270 TO 1350 IAW SRM 51-1-20D. LOCATED AND DRILLED UP NEW LONG IAW SRM 51-1-24. INSTALLED NEW LONG 3 5L FS 1270-1350 IAW SRM 51-1-20D AND 51-3-0.Jun 6, 2003 · N851UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2003806008Battery · inoperativeDURING PREFLIGHT EMERGENCY LIGHTS DID NOT WORK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PER M/M 33-50-0. OPS CHECKED GOOD.Jun 6, 2003 · N806DH · Doug DC873F · Emergency LightingSDR UPS03840907Skin · crackedINSPECTION TYPE:C3 LOWER FUSELAGE CENTER SECTION AT FS 1350 LONGERON 34L FUSELAGE SKIN IS CRACKED. REMOVED 2 EA EXISTING REPAIR DOUBLERS, TRIMMED OUT CRACK FS 1350 LONG 34L FABBED REPAIR DOUBLER COMBINING 2 EA EXISTING REPAIR DOUBLERS, FABBED SKIN FILLERS ANJun 5, 2003 · N851UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2003804003Light · burned outEMERGENCY LIGHTS ARMED LIGHT BURNED OUT. REPLACED ARMED LIGHT, OPS CHECKED GOOD PER DC8 M/M 33-50-2.Jun 5, 2003 · N804DH · Doug DC873F · Emergency LightingSDR DHL2003806007Battery · inoperativeEMERGENCY EXIT LIGHTS WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY UNIT. OPS CHECKED GOOD IAW M/M 33-50-1.Jun 5, 2003 · N806DH · Doug DC873F · Emergency LightingSDR DHL2003604732Fitting · corrodedMAIN CARGO COMPT FITTING CORRODED AT STA 1280.000, L-21R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, ATM PO201389, DWG 3755856. REMOVED CORRODED FITTING IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. Jun 4, 2003 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2003604695Attach Fitting · crackedLT MLG W/W FITTING ATTACHING LONGERON 24L AT STA. 940.000 WITH 5.000 CRACK IN IT. PERORMED MAJOR REPAIR IAW SRM 53-2-0 FIG.8. REMOVED DAMAGED FITTING IAW SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. CUT OUT NEW FITTING SRM 53-2-0 FIG.Jun 4, 2003 · N604AL · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2003604682Door Frame · damagedMAIN CARGO COMPT AFT PASSENGER DOOR JAMB AFT UPPER CORNER HAS INTERIM REPAIR. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 1. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-0 FIG 18 SHEET 3 TR 53-135, DWG SR 08530021, DWG 5750776. FABRICATED FILLER (Jun 4, 2003 · N604AL · Doug DC873F · Fuselage Main, StructureSDR DHL2003604658Skin · wornFUSELAGE NOSE SECTION EXTERNAL AC POWER RECEPTACLE COMPARTMENT OUTER SKIN WORN STA -39.000 L-31R TO L-33R (MAJOR REPAIR). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW EODHL-030551, ED-3295. CLEANED, TREATED AND PRIMED AREA IAW SRM 51Jun 4, 2003 · N604AL · Doug DC873F · Fuselage Main, Plate/Skin
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