# Service difficulty reports: N801GP, cancelled May 16, 2006

A list on [N801GP, cancelled May 16, 2006](https://openairdocs.org/deregistered/N801GP-2006-05-16.md).

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

Page 1 of 3 · 111 reports

- [SDR RRXA011041](https://openairdocs.org/sdr/RRXA011041.md): Fire Loop · failed · Apr 30, 2001 · N801GP · Doug DC871F · Fire Detection
  > ENGINE 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. AL
- [SDR RRXA010029](https://openairdocs.org/sdr/RRXA010029.md): Skin · damaged · Mar 29, 2001 · N801GP · Doug DC871F · Fuselage Main, Plate/Skin
  > APPROX 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 CYCLES
- [SDR RRXA010028](https://openairdocs.org/sdr/RRXA010028.md): Outflow Valve · failed · Mar 24, 2001 · N801GP · Doug DC871F · Pressure Regulator/Outflow Valve
  > ON 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 BE
- [SDR RRXA10807](https://openairdocs.org/sdr/RRXA10807.md): Plate · cracked · Feb 21, 2001 · N801GP · Doug DC871F · Nacelle/Pylon, Main Frame
  > DURING 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
- [SDR RRXA10839](https://openairdocs.org/sdr/RRXA10839.md): Attach Angle · cracked · Feb 15, 2001 · N801GP · Doug DC871F · Fuselage Main, Bulkhead
  > DURING 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. FABRICATE
- [SDR RRXA10806](https://openairdocs.org/sdr/RRXA10806.md): Drive Link · gouged · Feb 15, 2001 · N801GP · Doug DC871F · Aileron Tabs
  > DURING 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.#01-0
- [SDR RRXA10805](https://openairdocs.org/sdr/RRXA10805.md): Attach Angle · cracked · Feb 15, 2001 · N801GP · Doug DC871F · Aileron Tabs
  > DURING 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-8
- [SDR RRXA10802](https://openairdocs.org/sdr/RRXA10802.md): Clip · cracked · Feb 15, 2001 · N801GP · Doug DC871F · Wing Miscellaneous Structure
  > DURING 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 A
- [SDR RRXA10781](https://openairdocs.org/sdr/RRXA10781.md): Fitting · gouged · Feb 15, 2001 · N801GP · Doug DC871F · Aileron Tabs
  > DURING 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 WIT
- [SDR RRXA10828](https://openairdocs.org/sdr/RRXA10828.md): Spar · damaged · Feb 14, 2001 · N801GP · Doug DC871F · Cargo/Baggage Doors
  > DURING 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
- [SDR RRXA10777](https://openairdocs.org/sdr/RRXA10777.md): Panel · delaminated · Feb 14, 2001 · N801GP · Doug DC871F · Leading Edge Devices
  > DURING 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-
- [SDR RRXA10819](https://openairdocs.org/sdr/RRXA10819.md): Door Frame · cracked · Feb 13, 2001 · N801GP · Doug DC871F · Cargo/Baggage Doors
  > DURING 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 FI
- [SDR RRXA10813](https://openairdocs.org/sdr/RRXA10813.md): Skin · damaged · Feb 13, 2001 · N801GP · Doug DC871F · Elevator, Tab Structure
  > DURING 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
- [SDR RRXA10809](https://openairdocs.org/sdr/RRXA10809.md): Panel · corroded · Feb 12, 2001 · N801GP · Doug DC871F · Fuselage Main, Bulkhead
  > DURING 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 INSTALLE
- [SDR RRXA10794](https://openairdocs.org/sdr/RRXA10794.md): Vane · delaminated · Feb 12, 2001 · N801GP · Doug DC871F · Aileron Tabs
  > DURING 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-
- [SDR RRXA10775](https://openairdocs.org/sdr/RRXA10775.md): Panel · delaminated · Feb 12, 2001 · N801GP · Doug DC871F · Leading Edge Devices
  > DURING 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 27-6
- [SDR RRXA10793](https://openairdocs.org/sdr/RRXA10793.md): Vane · delaminated · Feb 10, 2001 · N801GP · Doug DC871F · Aileron Tabs
  > DURING 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-
- [SDR RRXA10789](https://openairdocs.org/sdr/RRXA10789.md): Stringer · cracked · Feb 10, 2001 · N801GP · Doug DC871F · Fuselage Main, Bulkhead
  > DURING 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-
- [SDR RRXA10810](https://openairdocs.org/sdr/RRXA10810.md): Panel · corroded · Feb 9, 2001 · N801GP · Doug DC871F · Fuselage Main, Bulkhead
  > DURING 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 INSTALLE
- [SDR RRXA10799](https://openairdocs.org/sdr/RRXA10799.md): Skin · damaged · Feb 9, 2001 · N801GP · Doug DC871F · Wing, Plate/Skin
  > DURING 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 WI
- [SDR RRXA10798](https://openairdocs.org/sdr/RRXA10798.md): Angle · cracked · Feb 9, 2001 · N801GP · Doug DC871F · Wing Miscellaneous Structure
  > DURING 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
- [SDR RRXA10787](https://openairdocs.org/sdr/RRXA10787.md): Skin · cracked · Feb 9, 2001 · N801GP · Doug DC871F · Wing Miscellaneous Structure
  > DURING 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-8
- [SDR RRXA10784](https://openairdocs.org/sdr/RRXA10784.md): Skin · damaged · Feb 9, 2001 · N801GP · Doug DC871F · Wing, Plate/Skin
  > DURING 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 01/1
- [SDR RRXA10788](https://openairdocs.org/sdr/RRXA10788.md): Skin · dented · Feb 8, 2001 · N801GP · Doug DC871F · Aileron Tabs
  > DURING 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.01
- [SDR RRXA10859](https://openairdocs.org/sdr/RRXA10859.md): Floor Panel · delaminated · Feb 7, 2001 · N801GP · Doug DC871F · Fuselage Floor Panel
  > DURING 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 IAW
- [SDR RRXA10856](https://openairdocs.org/sdr/RRXA10856.md): Floor Panel · delaminated · Feb 7, 2001 · N801GP · Doug DC871F · Fuselage Floor Panel
  > DURING 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 AND
- [SDR RRXA10848](https://openairdocs.org/sdr/RRXA10848.md): Panel · delaminated · Feb 7, 2001 · N801GP · Doug DC871F · Wing, Plate/Skin
  > DURING 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 DC
- [SDR RRXA10847](https://openairdocs.org/sdr/RRXA10847.md): Panel · delaminated · Feb 7, 2001 · N801GP · Doug DC871F · Wing, Plate/Skin
  > DURING 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 & 5
- [SDR RRXA10841](https://openairdocs.org/sdr/RRXA10841.md): Panel · damaged · Feb 7, 2001 · N801GP · Doug DC871F · Nacelle/Pylon, Plate/Skin
  > DURING 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.
- [SDR RRXA10827](https://openairdocs.org/sdr/RRXA10827.md): Skin · cracked · Feb 7, 2001 · N801GP · Doug DC871F · Cargo/Baggage Doors
  > DURING 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.
- [SDR RRXA10804](https://openairdocs.org/sdr/RRXA10804.md): Support Fitting · gouged · Feb 7, 2001 · N801GP · Doug DC871F · Aileron Tabs
  > DURING 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 51
- [SDR RRXA10854](https://openairdocs.org/sdr/RRXA10854.md): Skin · delaminated · Feb 6, 2001 · N801GP · Doug DC871F · Landing Gear Doors
  > DURING 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.
- [SDR RRXA10849](https://openairdocs.org/sdr/RRXA10849.md): Panel · delaminated · Feb 6, 2001 · N801GP · Doug DC871F · Wing, Plate/Skin
  > DURING 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 IA
- [SDR RRXA10846](https://openairdocs.org/sdr/RRXA10846.md): Panel · delaminated · Feb 6, 2001 · N801GP · Doug DC871F · Wing, Plate/Skin
  > DURING 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.
- [SDR RRXA10845](https://openairdocs.org/sdr/RRXA10845.md): Panel · delaminated · Feb 6, 2001 · N801GP · Doug DC871F · Wing, Plate/Skin
  > DURING 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.
- [SDR RRXA10842](https://openairdocs.org/sdr/RRXA10842.md): Boss · corroded · Feb 6, 2001 · N801GP · Doug DC871F · Main Landing Gear
  > DURING 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-
- [SDR RRXA10785](https://openairdocs.org/sdr/RRXA10785.md): Panel · delaminated · Feb 6, 2001 · N801GP · Doug DC871F · Wing, Plate/Skin
  > DURING 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 2
- [SDR RRXA10851](https://openairdocs.org/sdr/RRXA10851.md): Panel · delaminated · Feb 5, 2001 · N801GP · Doug DC871F · Wing, Plate/Skin
  > DURING 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.
- [SDR RRXA10803](https://openairdocs.org/sdr/RRXA10803.md): Skin · torn · Feb 5, 2001 · N801GP · Doug DC871F · Aileron Tabs
  > DURING 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 57
- [SDR RRXA10853](https://openairdocs.org/sdr/RRXA10853.md): Panel · delaminated · Feb 3, 2001 · N801GP · Doug DC871F · Wing, Plate/Skin
  > DURING 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.
- [SDR RRXA10855](https://openairdocs.org/sdr/RRXA10855.md): Panel · cracked · Feb 2, 2001 · N801GP · Doug DC871F · Fuselage Floor Panel
  > DURING 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 RE
- [SDR RRXA10852](https://openairdocs.org/sdr/RRXA10852.md): Panel · cracked · Feb 2, 2001 · N801GP · Doug DC871F · Wing, Plate/Skin
  > DURING 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.
- [SDR RRXA10840](https://openairdocs.org/sdr/RRXA10840.md): Brace · cracked · Feb 2, 2001 · N801GP · Doug DC871F · Rudder Structure
  > DURING 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 DC
- [SDR RRXA10838](https://openairdocs.org/sdr/RRXA10838.md): Retainer · cracked · Feb 2, 2001 · N801GP · Doug DC871F · Cargo/Baggage Doors
  > DURING 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-8
- [SDR RRXA10837](https://openairdocs.org/sdr/RRXA10837.md): Longeron · corroded · Feb 2, 2001 · N801GP · Doug DC871F · Fuselage Main, Bulkhead
  > DURING 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 5
- [SDR RRXA10801](https://openairdocs.org/sdr/RRXA10801.md): Stringer · corroded · Feb 1, 2001 · N801GP · Doug DC871F · Fuselage Main, Bulkhead
  > DURING 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, TREAT
- [SDR RRXA10800](https://openairdocs.org/sdr/RRXA10800.md): Stringer · corroded · Feb 1, 2001 · N801GP · Doug DC871F · Fuselage Main, Bulkhead
  > DURING 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.
- [SDR RRXA10786](https://openairdocs.org/sdr/RRXA10786.md): Stringer · corroded · Feb 1, 2001 · N801GP · Doug DC871F · Fuselage Main, Bulkhead
  > DURING 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 DC
- [SDR RRXA10835](https://openairdocs.org/sdr/RRXA10835.md): Frame · cracked · Jan 31, 2001 · N801GP · Doug DC871F · Cargo/Baggage Doors
  > DURING 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.
- [SDR RRXA10817](https://openairdocs.org/sdr/RRXA10817.md): Plate · corroded · Jan 31, 2001 · N801GP · Doug DC871F · Fuselage Floor Panel
  > DURING 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 APPROVED

Next page: https://openairdocs.org/deregistered/N801GP-2006-05-16/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N801GP-2006-05-16/reports

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