Douglas DC-8-73F

Service difficulty reports · 15,471

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 = '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 DHL2004873556Fairing · crackedLT MLG DOOR JAMB FAIRING CRACKED 1.500 AT XW 3.125 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 12-02-04 DWG W90-R12 REV IR DATED 11-18-04 DWG BOEING 5651221. REMOVED CRACKED FAIRING IAW SRM 51-1-21 PG 1. FABRICATED NEW FAIRING (AL2024 0Dec 3, 2004 · N873SJ · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2004873554Fitting · crackedMAIN CARGO COMPT FITTING ATTACHING TRACK NR 3 TO FLOORBEAM CRACKED 1.000 STA 798.000. REMOVED CRACKED FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0 PG 1, SRM 51-1-20D Dec 3, 2004 · N873SJ · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2004873547Frame · misdrilledMAIN CARGO COMPT FRAME HAS 2EA MISDRILLED HOLES AT STA 1380.000, L-11R TO L-12R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R17, REV IR DATED 11-22-04, FAA FORM 8110-3 DATED 12-2-04. CUT OUT MISDRILLED HOLE AREA IAW DWG W90-R17. CLEANED, TREATED AND Dec 3, 2004 · N873SJ · Doug DC873F · Fuselage Main, FrameSDR DHL2004873559Fairing · crackedRT MLG DOOR JAMB FAIRING CRACKED 0.875, XW 3.125 AFTER EXISTING REPAIR (MAJOR REPAIR). REMOVED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 12-02-04, DWG W90-R12 REV IR DATED 11-18-04 DWG BOEING 5651221. REMOVED CRACKED FAIRING IAW SRM 51-1-21 PG 1. FABRICATED NEDec 3, 2004 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR DHL2004873555Frame · misdrilledMAIN CARGO COMPT FRAME MISDRILLED HOLES AT STA 1300.000, L-11L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 12-02-04, DWG W90-R18 DATED 11-22-04. REMOVED 2EA FITTINGS IAW DWG W90-R18, SRM 51-1-21 PG 1, SRM 51-1-20C. TRIMMED OUT MISDRILLEDec 3, 2004 · N873SJ · Doug DC873F · Fuselage Main, FrameSDR DHL2004873550Frame · misdrilledMAIN CARGO COMPT FRAME HAS 3EA MISDRILLED HOLES AT STA 1400.000 L-11R TO L-12R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R17, REV IR DATED 11-22-04, FAA FORM 8110-3 DATED 12-02-04. CUT OUT MISDRILLED HOLE AREA IAW DWG W90-R17. CLEANED, TREATED AND Dec 3, 2004 · N873SJ · Doug DC873F · Fuselage Main, FrameSDR DHL2004873557Frame · damagedMAIN CARGO COMPT FRAME HAS 3 MISDRILLED HOLES STA 1300.000, L-10R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 12/02/04, DWG W90-R18 REV IR DATED 11/22/04. REMOVED 2 FITTINGS IAW DWG W90-R18, SRM 51-1-21 PG 1, SRM 51-1-20C. CUT OUT MISDRILLED HOLES AREDec 3, 2004 · N873SJ · Doug DC873F · Fuselage Main, FrameSDR DHL2004809010Battery · inoperativeON PREFLIGHT WHILE DOING BATTERY TEST, EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE. DURING SUBSEQUENT TESTS, EMERGENCY EXIT LIGHT DID ILLUMINATED, BUT FAILED WHEN IGNITION POWER WAS PLACED TO TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND A/C MAIN BATTEDec 3, 2004 · N809DH · Doug DC873F · Emergency LightingSDR DHL2004873543Frame · misdrilledMAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1600.000 L-20R. PERFORMED MAJOR REPAIR IAW DWG W90-R20, FAA FORM 8110-3 DATED NOV 29,2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RIDec 2, 2004 · N873SJ · Doug DC873F · Fuselage Main, FrameSDR DHL2004873544Beam · damagedMAIN CARGO COMPT AFT PRESSURE BULKHEAD VERTICAL BEAM HOLES MISDRILLED AT STA 1766.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R15 AND FAA FORM 8110-3 NOV 30,2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. PERFORMED NDT INDec 2, 2004 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR DHL2004873545Skin · crackedLT WING INBOARD L/E CRACKED 3.000 IN LWR SKIN SURFACE (STA XFS 622.500 - 628.725) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DWG W90-R14, REV: IR DATED 11-22-04, FAA FORM 8110-3 DATE 11-29-2004. REMOVED EXISTING REPAIR DOUBLER IAW DWG W90-R14, SRM 51-1-20D PG Dec 1, 2004 · N873SJ · Doug DC873F · Wing, Plate/SkinSDR DHL2004873542Frame · misdrilledMAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1600.000 L-20L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R20, FAA FORM 8110-3 DATED NOV 29, 2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILDec 1, 2004 · N873SJ · Doug DC873F · Fuselage Main, FrameSDR DHL2004873551Skin · corrodedRT VERTICAL STABILIZER L/E SKIN CORRODED, STA ZFS 140.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R16, REV IR DATED 11-18-04 FAA FORM 8110-3 DATED 11-30-04. REMOVED L/E SKIN PANEL AND REPAIR PARTS FROM INTERNAL STRUCTURE IAW DWG W90-R16, SRM 51-1-Dec 1, 2004 · N873SJ · Doug DC873F · Vertical Stabilizer, Plate/SkinSDR DHL2004873549Frame · misdrilledMAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1200.000, L-12R TO L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R19, REV:IR DATED 11-22-04 FAA FORM 8110-3 DATED 11-29-04. REMOVED EXISTING DAMAGED FRAME SPLICE PLATE AND FASTENERS IAW DWG W90-R19, SRDec 1, 2004 · N873SJ · Doug DC873F · Fuselage Main, FrameSDR DHL2004873539Frame · misdrilledMAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1600.000 L-17R. PERFORMED MAJOR REPAIR IAW DWG W90-R20, FAA FORM 8110-3 DATED NOV 29, 2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLED HOLE WITH RDec 1, 2004 · N873SJ · Doug DC873F · Fuselage Main, FrameSDR DHL2004873548Skin · dentedUPPER FUSELAGE SKIN DENTED BETWEEN STA 210.000 AND 220.000 (4.000 BELOW MAIN CARGO DOOR LWR JAMB) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW DWG W90-R09, REV:IR DATED 11-22-04, FAA FORM 8110-3 DATED 11-29-04. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-Dec 1, 2004 · N873SJ · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2004873538Frame · misdrilledMAIN CARGO COMPT MISDRILLED HOLES AT STA 1311.000 L-11 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R20, FAA FORM 8110-3 DATED 29-11,2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLES AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGINS MISDRILLED HOLDec 1, 2004 · N873SJ · Doug DC873F · Fuselage Main, FrameSDR DHL2004873536Frame · misdrilledMAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1540.000 L-19R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R20, FAA FORM 8110-3 DATED NOV 29, 2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILDec 1, 2004 · N873SJ · Doug DC873F · Fuselage Main, FrameSDR DHL2004873540Frame · misdrilledMAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1560.000 L-20R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R20 FAA FORM 8110-3 DATED NOV 29, 2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDRILLDec 1, 2004 · N873SJ · Doug DC873F · Fuselage Main, FrameSDR DHL2004873553Skin · crackedLT WING INBOARD L/E LWR SKIN CRACKED 0.500 AT XCW 69.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R01, REV IR DATED 11-08-04 FAA FOMR 8110-3 DATED 11-30-04. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. CUT OUT DAMAGED SECTION IAW DWG WDec 1, 2004 · N873SJ · Doug DC873F · Wing, Plate/SkinSDR DHL2004873541Frame · misdrilledMAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1080.000, L-15R TO L-14R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R20, FAA FORM 8110-3 DATED NOV 29, 2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGIDec 1, 2004 · N873SJ · Doug DC873F · Fuselage Main, FrameSDR DHL2004873535Frame · misdrilledMAIN CARGO COMPT FRAME MISDRILLED HOLE AT STA 1000.000 L-14R TO L-15R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R20 FAA FORM 8110-3 DATED NOV 29, 2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGINGDec 1, 2004 · N873SJ · Doug DC873F · Fuselage Main, FrameSDR DHL2004873546Skin · wornLT WING OUTBOARD FLAP L/E UPPER PART SKIN WORN BETWEEN XF 200.000 AND XF 213.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R03 REV: TR DATE 11/08/04 FAA FORM 8110-3 DATED 11-30-04. TRIMMED OUT PLATING SEGMENT (DAMAGED) IAW DWG W90-R03. PERFORMED NDDec 1, 2004 · N873SJ · Doug DC873F · Trailing Edge FlapsSDR DHL2004873537Frame · misdrilledMAIN CARGO COMPT FRAME MISDRILLED AT STA 1020.000, L-14R TO L-13R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W90-R20, FAA FORM 8110-3 DATED NOV 29,2004. CLEANED, TREATED AND PRIMED MISDRILLED HOLE AREA IAW SRM 51-1-8B. REPAIRED DAMAGED AREA PLUGGING MISDec 1, 2004 · N873SJ · Doug DC873F · Fuselage Main, FrameSDR DHL2004873526Floor Panel · deformedMAIN CARGO COMPT FLOOR PANEL NR 1D SKIN DEFORMED AND CRACKED 40.000 (STA 879.000-1000.000). REMOVED DEFORMED AND CRACKED FLOOR PANEL NR 1D (STA 879.000-1000.000) IAW SRM 53-1-0 PG 1, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND NEW FLOOR PANEL IAW SDec 1, 2004 · N873SJ · Doug DC873F · Fuselage Floor PanelSDR DHL2004873525Floor Panel · crackedMAIN CARGO COMPT FLOOR PANEL NR 1E SKIN DEFORMED AND CRACKED 20.000 (STA 688.000-729.000). REMOVED CRACKED AND DEFORMED FLOOR PANEL NR 1E (STA 688.000-729.000) IAW SRM 53-1-0 PG 1, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND NEW FLOOR PANEL IAW SRMDec 1, 2004 · N873SJ · Doug DC873F · Fuselage Floor PanelSDR DHL2004873524Floor Panel · crackedMAIN CARGO COMPT FLOOR PANEL NR 3E CRACKED 10.000 AND CORRODED ON SEVERAL AREAS OF SKIN SURFACE (STA 1300.000-1582.000). REMOVED CRACKED FLOOR PANEL NR 3E IAW SRM 53-1-0 PG 1, SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND NEW FLOOR PANEL IAW SRM 51-1Dec 1, 2004 · N873SJ · Doug DC873F · Fuselage Floor PanelSDR DHL2004805012Latch · brokenCOCKPIT DOOR LATCH BROKEN DOOR WILL NOT LATCH CLOSED. REMOVED AND REPLACED LATCH ASSY WITH SERVICEABLE LATCH ASSY. OPS CHECKS GOOD PER 52-51-1 P/N AR2529-1GRY1.Dec 1, 2004 · N805DH · Doug DC873F · Fixed Inner DoorsSDR DHL2004873552Angle · corrodedAFT FUSELAGE ATTACH ANGLE WITH VERTICAL STABILIZER CORRODED (BETWEEN FRONT SPAR AND CTR SPAR RT SIDE). PERFORMED MAJOR REPAIR. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 55-2-0 PG 12. TRIMMED OUT CORRODED AREA IAW SRM 53-2-5 FIGNov 30, 2004 · N873SJ · Doug DC873F · Fuselage, Stabilizer Attach FittingsSDR DHL2004873562Stiffener · corrodedAFT CARGO COMPT STIFFENER CORRODED, STA 980.000 L-27L. REMOVED CORROSION FROM STIFFENER STA 980.000 L-27L IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED STIFFENER IAW SRM 53-1-0 PG 1, SRM 51-1-21 PG 1, SRM 51-1-20D PG 21Nov 30, 2004 · N873SJ · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2004873558Frame · crackedMAIN CARGO COMPT FRAME FLANGE CRACKED 2.000 AND DENTED, STA 1580.000 L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2, TR 53-110. CUT OUT DAMAGED FRAME SEGMENT IAW SRM 53-2-0 FIG 2. FABRICATED NEW FRAME SEGMENT (7075"0" 0.080) AND 2EA SPLICNov 30, 2004 · N873SJ · Doug DC873F · Fuselage Main, FrameSDR DHL2004873528Angle · crackedRIGHT WING T/E MLG DOOR JAMB ZEE ANGLE CRACKED 2.000, STA XW 3.125. REMOVED CRACKED ZEE ANGLE IAW SRM 51-1-21 PG 1. FABRICATED ZEE ANGLE (AL2024 -0- 0.050) IAW DWG 5651221. HEAT TREATED IAW DADO DPS 7.00. CLEANED, TREATED AND PRIMED AREA AND ZEE ANGLE IAW Nov 30, 2004 · N873SJ · Doug DC873F · Landing Gear DoorsSDR DHL2004873527Floor Panel · crackedMAIN CARGO COMPT NR 3C FLOOR PANEL SKIN CORRODED AND CRACKED 1.000 (STA 1560.000-1580.000). REMOVED CORROSION FROM NR 3C FLOOR PANEL SKIN (STA 1560.000-1580.000) IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED SECTION AND Nov 30, 2004 · N873SJ · Doug DC873F · Fuselage Floor PanelSDR DHL2004873530Skin · damagedRIGHT WING OUTBOARD FLAP LWR FWD SKIN DAMAGED (BROKEN 1.000) AT XF 203.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-5 FIG 1 PG 3/4, 5/6. TRIMMED OUT DAMAGED AREA IAW SRM 57-2-5 FIG 1 PG 5-6. FABRICATED PLATING SEGMENT (AL2024-T3 0.032) SPLICE (ALNov 29, 2004 · N873SJ · Doug DC873F · Trailing Edge FlapsSDR DHL2004873534Skin · corrodedLEFT VERTICAL STABILIZER L/E SKIN CORRODED, STA ZFS 98.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-5-1 FIG 1. REMOVED CORROSION FROM LEFT VERTICAL STABILIZER, L/E STA ZFS 98.000 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRMNov 29, 2004 · N873SJ · Doug DC873F · Vertical Stabilizer, Plate/SkinSDR DHL2004873532Skin · corrodedRIGHT VERTICAL STABILIZER L/E LWR SKIN CORRODED, STA ZFS 80.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 55-1-0 PG 1, SRM 55-5-1 FIG 1. REMOVED CORROSION FROM RIGHT VERTICAL STABILIZER L/E LWR SKIN STA ZFS 80.000 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF Nov 29, 2004 · N873SJ · Doug DC873F · Vertical Stabilizer, Plate/SkinSDR DHL2004873533Longeron · corrodedAFT ACCY COMPT L-34R INTERNAL PART CORRODED AT FS 1660.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-4-1 FIG 43A. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED LONGERON IAW SRNov 28, 2004 · N873SJ · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL2004873560Angle · crackedAFT ACCY COMPT FRAME SPLICE ANGLE CRACKED 4.000 STA 1640.000 BETWEEN L-25 AND L-26R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-4-1 FIG 51. REMOVED CRACKED FRAME SPLICE ANGLE IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW FRNov 28, 2004 · N873SJ · Doug DC873F · Fuselage Main, FrameSDR DHL2004873561Floorbeam · crackedAFT CARGO COMPT FLOORBEAM CRACKED 0.500, STA 1160.000 L-26R TO L-27R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FLOORBEAM IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLEDNov 26, 2004 · N873SJ · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2004873520Door · crackedLEFT INBOARD SLOT UPPER DOOR CRACKED 1.000. REMOVED AND REPLACED INBOARD SLOT UPPER DOOR IAW SRM 51-3-0 PG 1.Nov 26, 2004 · N873SJ · Doug DC873F · Leading Edge DevicesSDR DHL2004873565Fitting · crackedAFT CARGO COMPT FITTING CRACKED 1.500 STA 1160.000 L-26R TO L-27R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 53-1-0 PG 1, DWG 3754025. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D PG 21. FABRICATED NEW FITTING (7075T651) IAW DWG 3754025. PERFORMED Nov 24, 2004 · N873SJ · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2004873521Cusp Web · crackedMAIN CARGO COMPT CUSP EXTRUSION CRACKED 2.000, STA 1080.000 L-21R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-5 FIG 15, TR 53-179. REMOVED FASTENERS IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. CUT OUT CUSP EXTRUSION DAMAGED SEGMENT IAW SRM 53-2-5 FIG Nov 23, 2004 · N873SJ · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS04843540Slide · deployedMAIN CABIN EXIT EMERGENCY SLIDE DEPLOYED. REPLACED SLIDE IAW 25-60-00 SECURITY CK GOOD, THIS CLEARS M291801.Nov 23, 2004 · N810UP · Doug DC873F · Escape SlideSDR DHL2004873523Doubler · corrodedEXT FUSELAGE FWD CARGO COMPT FWD DOOR JAMB DOUBLER REPAIR INTERNAL PART CORRODED AT STA 320.000 L-32R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW BOEING MESSAGE 1-SHTHH FAA FORM 8110-3 DATED 11-11-2004 SB DC8 53078 REV 1 SR08530019 AD2004-06-06 DWG SEMAN ED344Nov 22, 2004 · N873SJ · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2004873522Floorbeam · corrodedAFT CARGO COMPT FLOORBEAM FLANGE CORRODED AT STA FS 1360.000 LBL 47 TO LBL 50 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 1G TR 53-124. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. FABRICATED REPAIR ANNov 22, 2004 · N873SJ · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2004801014Transfer Valve · failedRUDDER INDICATOR WAS FULL LEFT. IT TOOK 5 1/2 UNITS TO MAINTAIN STRAIGHT AND LEVEL. WHEN THE RUDDER TRIM WAS MOVED TOWARD ZERO THE AIRCRAFT MADE AN AGGRESSIVE ROLL TO THE LEFT. DID NOT TRY TO FLY AIRCRAFT WITH YAW. REMOVED AND REPLACED ROLL SERVO DRIVE IANov 19, 2004 · N801DH · Doug DC873F · Autopilot SystemSDR DHL2004873518Floorbeam · corrodedMAIN CARGO COMPT UPPER FLOORBEAM FLANGE CORRODED, STA 1300.000 RBL 8 TO RBL 16 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 1G, TR 53-124. REMOVED CORROSION FROM UPPER FLOORBEAM FLANGE AT STA 1300.000 RBL 8 TO RBL 16 IAW SRM 51-1-8 PG 17-18. FONov 17, 2004 · N873SJ · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2004873529Skin · elongatedRT HORIZONTAL STABILIZER L/E ELONGATED HOLES IN UPPER SKIN (STA XFS 60.000-116.250) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW BOEING MSG 1-S23U2, 1-S32CQ, DWG SEMAN ED-3475. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. CUT OUTNov 16, 2004 · N873SJ · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR DHL2004873519Rib · damagedNR 1 LEFT STUB WING RIB HOLES ELONGATED, STA XS 520.168 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1. REMOVED NR 1 LEFT STUB WING RIB IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. Nov 14, 2004 · N873SJ · Doug DC873F · Wing, Rib/BulkheadSDR DHL2004873512Bracket · crackedNR 4 ALT TANK FWD BOOSTER PUMP BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON NR 1 ALT TANK FWD BOOSTER PUMP IAW SRM 51-1-20D PG 9-21.Nov 13, 2004 · N873SJ · Doug DC873F · Wing, Attach Fittings
Back to Douglas DC-8-73F