N801GP, cancelled May 16, 2006

Service difficulty reports · 111

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N801GP' AND deregistration_id = 'N801GP-2006-05-16'
  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 RRXA011041Fire Loop · failedENGINE NR 1 ON TAKEOFF INTERMITTENT FIRE WARNING. AS PER QRH, ENG WAS SHUT DOWN AND FIRE LOOP TESTED. IT DID NOT RESET. DISCHARGED BOTTLE NR 1, WAITED 30 SEC, FIRE LOOP TESTED. IT DID NOT RESET, DISCHARGED BOTTLE NR 2, WAITED 30 SEC, LOOP DID NOT TEST. ALApr 30, 2001 · N801GP · Doug DC871F · Fire DetectionSDR RRXA010029Skin · damagedAPPROX 3 INCH TEAR IN FUSELAGE SKIN AT FWD LOWER CORNER BELOW CARGO DOOR DURING FWD DOOR GUARD INSTALLATION. REPAIRED DAMAGED AREA AT LOWER FORWARD CORNER OF MCD JAMB IAW GUIDELINES OF EWA ENGINEERING MEMO ML329011 THIS TEMPORARY REPAIR LIMITED TO 1000 CYCLESMar 29, 2001 · N801GP · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA010028Outflow Valve · failedON DESCENT, CABIN BEGAN TO CLIMB. WENT TO MAX RATE ON AUTO CONTROLLER AND MAX FLOW ON PACKS, WOULD NOT STOP CLIMB, CABIN COULD NOT BE CONTROLLED MANUALLY EITHER. ANY ATTEMPT TO MANUALLY CONTROL PRESSURE CAUSED CABIN TO CLIMB HIGHER, MANUAL LEVER COULD NOT BEMar 24, 2001 · N801GP · Doug DC871F · Pressure Regulator/Outflow ValveSDR RRXA10807Plate · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO WING L/E SHIM PLATE AT I/B NR3 ENG. PYLON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-006 WITH APPROVED 8110-3 DATED Feb 21, 2001 · N801GP · Doug DC871F · Nacelle/Pylon, Main FrameSDR RRXA10839Attach Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO AFT LWR CARGO COMPARTMENT BULKHEAD DIVIDERS ATTACH ANLGE AT STA Y+14, Z-7, X-24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATEFeb 15, 2001 · N801GP · Doug DC871F · Fuselage Main, BulkheadSDR RRXA10806Drive Link · gougedDURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO R/H O/B FLAP CENTER DRIVE LINK AT STA. 319, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-0Feb 15, 2001 · N801GP · Doug DC871F · Aileron TabsSDR RRXA10805Attach Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT. WING REAR SPAR FLAP ATTACH FITTING AT STA. XRS98, 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-8Feb 15, 2001 · N801GP · Doug DC871F · Aileron TabsSDR RRXA10802Clip · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO ATTACH CLIP AT STA. 252 CAN'T AND R/H WING #4 MAIN INSIDE TANK THRU ACCESS HOLE 505D AND BETWEEN STRINGER 68 & 69, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AFeb 15, 2001 · N801GP · Doug DC871F · Wing Miscellaneous StructureSDR RRXA10781Fitting · gougedDURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO LT. WING FLAP IN FITTING AT STA. 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-006 WITFeb 15, 2001 · N801GP · Doug DC871F · Aileron TabsSDR RRXA10828Spar · damagedDURING A MAINTENANCE VISIT FOUND ROUTED OUT DAMAGE TO C-PIT DOOR SPAR AT RT SPAR, 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 AND DC-8 SRM 51-1-20D AND DC-8 SRM Feb 14, 2001 · N801GP · Doug DC871F · Cargo/Baggage DoorsSDR RRXA10777Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO L/H WING #3 SPOILER PANEL AT #3 SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED ARE IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 27-Feb 14, 2001 · N801GP · Doug DC871F · Leading Edge DevicesSDR RRXA10819Door Frame · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L-2 DOOR FRAME AT UPPER AFT CORNER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 FIFeb 13, 2001 · N801GP · Doug DC871F · Cargo/Baggage DoorsSDR RRXA10813Skin · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE TO RT. ELEVATOR CONTROL TAB AT O/B CORNER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-006 WITH APPROVED 8110-3 DATED 02/01/01 Feb 13, 2001 · N801GP · Doug DC871F · Elevator, Tab StructureSDR RRXA10809Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO L/H KEEL BEAM STRESS PANEL AT STA. 690-779 AND L35L-L33L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLEFeb 12, 2001 · N801GP · Doug DC871F · Fuselage Main, BulkheadSDR RRXA10794Vane · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO RT. WING #4 FLAP VANE AT #4 RT. WING FLAP VANE, 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-Feb 12, 2001 · N801GP · Doug DC871F · Aileron TabsSDR RRXA10775Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING #2 SPOILER PANEL AT #2 PANEL, 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 MM 27-6Feb 12, 2001 · N801GP · Doug DC871F · Leading Edge DevicesSDR RRXA10793Vane · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO RT. WING I/B FLAP VANE AT RT. I/B FLAP, 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 MM 27-Feb 10, 2001 · N801GP · Doug DC871F · Aileron TabsSDR RRXA10789Stringer · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LOWER STRINGER #55 AT STA. 495 CAN'T AND 508 CAN'T, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIRAND INSTALLED IAW DC-Feb 10, 2001 · N801GP · Doug DC871F · Fuselage Main, BulkheadSDR RRXA10810Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO R/H KEEL BEAM ACCESS COVER AT STA. 742-749 AND L33R-L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLEFeb 9, 2001 · N801GP · Doug DC871F · Fuselage Main, BulkheadSDR RRXA10799Skin · damagedDURING A MAINTENANCE VISIT FOUND ELONGATION DAMAGE TO NR 4 STUB WING L/E AT FWD OF SLOT PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-20A AND E.O. 01-006 WIFeb 9, 2001 · N801GP · Doug DC871F · Wing, Plate/SkinSDR RRXA10798Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO #3 PYLON WING L/E BULLNOSE AT STA. XS220, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-4 AND DC-8 SRM 51-1-24 AND DC-8 SRM 51-1-21 AND Feb 9, 2001 · N801GP · Doug DC871F · Wing Miscellaneous StructureSDR RRXA10787Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT. WING L/E AT STA. XW485.0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-4 AND DC-8Feb 9, 2001 · N801GP · Doug DC871F · Wing Miscellaneous StructureSDR RRXA10784Skin · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLE DAMAGE TO WING L/E AT NR 3 ENGINE PYLON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O 01-006 WITH APPROVED 8110-3 DATED 01/1Feb 9, 2001 · N801GP · Doug DC871F · Wing, Plate/SkinSDR RRXA10788Skin · dentedDURING A MAINTENANCE VISIT FOUND DENT DAMAGE TO L/H I/B FLAP AT STA.XW62.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW NDT SPM 08-00-06 AND E.O.01Feb 8, 2001 · N801GP · Doug DC871F · Aileron TabsSDR RRXA10859Floor Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO FLOOR PANEL BETWEEN TRACKS 1 & 2 AT STA. 480-560, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAWFeb 7, 2001 · N801GP · Doug DC871F · Fuselage Floor PanelSDR RRXA10856Floor Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO UPPER CARGO COMPT. FLOOR PANEL AT STA. 580-590 X=45-55, 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 51-3-0 ANDFeb 7, 2001 · N801GP · Doug DC871F · Fuselage Floor PanelSDR RRXA10848Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING UPPER SURFACE T/E PANEL OVER MAIN LANDING GEAR AT STA XW5 TO XW 47, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DCFeb 7, 2001 · N801GP · Doug DC871F · Wing, Plate/SkinSDR RRXA10847Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING T/E PANEL LWR. SURFACE AT STA. XRS 170, 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 51-1-21 & 51-1-24 & 5Feb 7, 2001 · N801GP · Doug DC871F · Wing, Plate/SkinSDR RRXA10841Panel · damagedDURING A MAINTENANCE VISIT FOUND HOLE ELONGATED DAMAGE TO NR 3 PYLON PANEL AT PANEL 392A, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PARTS AND INSTALLED IAW DC-8 SRM 51-1-21.Feb 7, 2001 · N801GP · Doug DC871F · Nacelle/Pylon, Plate/SkinSDR RRXA10827Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO A-PIT DOOR SKIN AT FWD. CENTER SECTION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-20D.Feb 7, 2001 · N801GP · Doug DC871F · Cargo/Baggage DoorsSDR RRXA10804Support Fitting · gougedDURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO RT. WING FLAP SUPPORT FITTING AT STA. 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51Feb 7, 2001 · N801GP · Doug DC871F · Aileron TabsSDR RRXA10854Skin · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO R/H MLG UPPER O/B DOOR, 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 MM 32-12-1 AND DC-8 SRM 51-3-0.Feb 6, 2001 · N801GP · Doug DC871F · Landing Gear DoorsSDR RRXA10849Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING UPPER SURFACE UX-SPAR PANEL OVER MAIN LANDING GEAR AT STA. XW5 TO XW33, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAFeb 6, 2001 · N801GP · Doug DC871F · Wing, Plate/SkinSDR RRXA10846Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING T/E PANEL LWR. SURFACE AT STA. XW350, 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 MM 57-30-0.Feb 6, 2001 · N801GP · Doug DC871F · Wing, Plate/SkinSDR RRXA10845Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LT. WING T/E PANEL LWR. SURFACE AT STA. XW106, 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 MM 57-30-0.Feb 6, 2001 · N801GP · Doug DC871F · Wing, Plate/SkinSDR RRXA10842Boss · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RETRACT PIN BOSS AT MLG SHOCK STRUT ASSSEMBLY, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-006 WITH APPROVED 8110-Feb 6, 2001 · N801GP · Doug DC871F · Main Landing GearSDR RRXA10785Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO RT. WING SCISSORS PANEL AT FLAP SCISSORS, 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 MM 2Feb 6, 2001 · N801GP · Doug DC871F · Wing, Plate/SkinSDR RRXA10851Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LWR. WING PANEL AT RT AUX. SPAR, 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 51-3-0.Feb 5, 2001 · N801GP · Doug DC871F · Wing, Plate/SkinSDR RRXA10803Skin · tornDURING A MAINTENANCE VISIT FOUND TORN DAMAGE TO FLAP SKIN AT SAT. 219 AND I/B FWD. SECTION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57Feb 5, 2001 · N801GP · Doug DC871F · Aileron TabsSDR RRXA10853Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO RT LWR. T/E PANEL AT STA XRS 219 TO XRS 340, 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 51-3-0.Feb 3, 2001 · N801GP · Doug DC871F · Wing, Plate/SkinSDR RRXA10855Panel · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO CENTER FLOOR PANEL BEHIND CENTER PADISTAL EDGE BENT & CRACKED AT SCREW HOLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REFeb 2, 2001 · N801GP · Doug DC871F · Fuselage Floor PanelSDR RRXA10852Panel · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO UPPER T/E PANEL HINGE FOR SPOILER AT STA. 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 & 57-2-0.Feb 2, 2001 · N801GP · Doug DC871F · Wing, Plate/SkinSDR RRXA10840Brace · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RUDDER LOAD FEEL UNIT SUPPORT SIDE BRACE AT UPPER AND LOWER, 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 51-1-21 AND DCFeb 2, 2001 · N801GP · Doug DC871F · Rudder StructureSDR RRXA10838Retainer · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO D-PIT DOOR AT LWR. AFT DOOR RETAINER, 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 51-1-21 AND DC-8SRM 51-1-20D AND DC-8Feb 2, 2001 · N801GP · Doug DC871F · Cargo/Baggage DoorsSDR RRXA10837Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON FITTING L34L AT STA 1260 AND C-PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVE DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 5Feb 2, 2001 · N801GP · Doug DC871F · Fuselage Main, BulkheadSDR RRXA10801Stringer · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO STRINGER #75 AND FWD SIDE STRINGER SPLICE AT STA. XCW 23 X=0 AND INSIDE R/H CENTER TANK THRU MID SPAR ACCESS 560E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATFeb 1, 2001 · N801GP · Doug DC871F · Fuselage Main, BulkheadSDR RRXA10800Stringer · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LWR STRINGER#76 AT STA. XCW47&23 AND INSIDE R/H CENTER TANK THRU MID SPAR ACCESS 560E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.Feb 1, 2001 · N801GP · Doug DC871F · Fuselage Main, BulkheadSDR RRXA10786Stringer · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO STRINGER #76 AT STA. XCW23 AND XCW46 AND INSIDE L/H CENTER WING TANK THRU MID SPAR ACCESS HOLE 560E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DCFeb 1, 2001 · N801GP · Doug DC871F · Fuselage Main, BulkheadSDR RRXA10835Frame · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO D-PIT DOOR FRAME DOUBLER AT AFT TOP CORNER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21.Jan 31, 2001 · N801GP · Doug DC871F · Cargo/Baggage DoorsSDR RRXA10817Plate · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO D-PIT KICK PLATE AT D-PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.#01-006 WITH APPROVEDJan 31, 2001 · N801GP · Doug DC871F · Fuselage Floor Panel
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