N995CF

Service difficulty reports · 505

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 = 'N995CF' AND registry_match = 'registration'
  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 RRXA000123Floorbeam · misdrilledDURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES, FUSELAGE, MISDRILLED HOLES, FUSELAGE, FLOORBEAM AT STA 1420 CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.Jan 26, 2000 · N995CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA000122Floorbeam · misdrilledDURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES, FUSELAGE, FLOORBEAM AT STA 1440 CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.Jan 26, 2000 · N995CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA000121Intercostal · crackedDURING A MAINTENANCE VISIT FOUND CRACK, FUSELAGE, INTERCOSTAL GOUGED/CRACKED OUT HOLES BETWEEN STA 1420 AND STA 1400 RT, BETWEEN LONGERON 2 RIGHT AND LONGERON 3 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.Jan 26, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000120Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK, FUSELAGE, ATTACH ANGLE FRAME AT STA 1480 RT AT LONGERON 2 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.Jan 26, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA991475Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BL 36 LEFT BETWEEN STA 640 AND STA 720. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER REPAIR IAW DC8 SRM 51-1-Mar 6, 1999 · N995CF · Doug DC862 · Fuselage Floor PanelSDR RRXA98561O-Ring · leakingLOSS OF HYDRAULIC QUANTITY AND HYDRAULIC PRESSURE. PERFORMED CHECK LISTS TO LOWER FLAPS. FOUND FITTING ON LT GEAR TRIM FITTING LEAKING. REMOVED FITTING, REPLACED O-RING, REINSTALLED FITTING, SERVICED HYD RES. PERFORMED GROUND RUN ON NR 2 AND NR 3 ENGINES, Nov 10, 1998 · N995CF · Doug DC862 · Landing Gear Retraction/Extension SystemSDR RRXA98557Floorbeam · misdrilledDURING MAINTENANCE VISIT, FOUND FLOOR SUPPORT AT FS 660 WITH MISDRILLED HOLES IN THE UPPER FLANGE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED NEW T-CAP IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R51, DC-8 SRM 51-1-21 AND TREATED AREA IAW DC-8 SRM Nov 7, 1998 · N995CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA98556Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 920 WITH MISDRILLED HOLES AT LONGERON 16 LEFT. PLUGGED HOLES, FABRICATED AND INSTALLED REPAIR STRAP IAW FAA APPROVED ACMI SKETCH SK98242, DC-8 SRM 51-1-20D AND TREATED AREA IAW DC-8 SRM 51-1-8.Nov 7, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98555Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 640 CRACKED BETWEEN LONGERONS 9 AND 10 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW FAA APPROVED ACMI SKETCH SK98500, DC-8 SRM 51-1-20D, 51-1-21 AND TREATED AREA IAW DC-8 SRM 51-1-8.Nov 7, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98554Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 822 WITH MISDRILLED HOLE AT LONGERON 3 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED ACMI SKETCH SK98298, DC-8 SRM 51-1-20D AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 7, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98553Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 759 WITH MISDRILLED HOLE AT LONGERON 15 LEFT. FABRICATED AND INSTALLED REPAIR STRAPS AND CLIPS IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R87, DC-8 SRM 51-1-20D, 51-1-21 AND TREATED IAW DC-8 SRM 51-1-8.Nov 7, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98552Frame · misdrilledDURING MAINTENANCE VISIT, FOUND 540 WITH MISDRILLED HOLE AT LT CUSP. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE, FILLER AND SHIM IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R67 AND DC-8 SRM 51-1-1A.Nov 7, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98551Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 940 WITH MISDRILLED HOLE AT LONGERON 14 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE AND STRAPS IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R109, DC-8 SRM 51-1-1, 51-1-20D AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 7, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98550Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 280 WITH MISDRILLED HOLE AT LONGERON 5 RIGHT. FABRICATED AND INSTALLED REPAIR DOUBLER, TIE CLIPS AND SHIMS IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R31, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98549Frame · misdrilledDURING MAINTENANCE VISIT, FOUND THE FACE OF FRAME 960 GOUGED AND MISDRILLED HOLE AT LONGERON 9 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE, STRAP AND FILLER IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R94, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRNov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98548Scuff Plate · corrodedDURING MAINTENANCE VISIT, FOUND C-PIT DOOR THRESHOLD SCUFF PLATE BULGING AND SEVERAL PULLED FASTENERS. REMOVED DAMAGED SKIN AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R15, DC-8 SRM 51-1-20D, 51-Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA98547Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 560 WITH MISDRILLED HOLE BETWEEN LONGERONS 7 AND 8 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIMS IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R93, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98546Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 880 WITH MISDRILLED HOLE AT LONGERON 6 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED ACMI SKETCH SK98301, DC-8 SRM 51-1-1, 51-1-20D AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98545Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 920 WITH MISDRILLED HOLE AT LONGERON 11 LEFT. PLUGGED HOLE, FABRICATED AND INSTALLED REPAIR STRAP IAW FAA APPROVED ACMI SKETCH SK98302, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98544Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 880 WITH MISDRILLED HOLE AT LONGERON 3 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED ACMI SKETCH SK98300, DC-8 SRM 51-1-20D AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98543Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 600 WITH MISDRILLED HOLE AT LT CUSP. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE AND STRAP IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R69, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98542Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 540 WITH DRILL DAMAGE AT LONGERON 13 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED ACMI SKETCH SK98484, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98541Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 1120 WITH MISDRILLED HOLE AT LONGERON 13 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW FAA APPROVED ACMI SKETCH SK98376, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98540Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 1320 WITH MISDRILLED HOLE BETWEEN LONGERONS 9 AND 10 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIM IAW FAA APPROVED ACMI SKETCH SK98482, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98539Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 1360 WITH MISDRILLED HOLES AT LONGERON 9 RIGHT. REMOVED GUSSET, REMOVED DAMAGED AREA, FABRICATED AND INSTALLED NEW SPLICE, STRAPS AND GUSSET IAW FAA APPROVED ACMI SKETCH SK98390, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98538Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 1380 WITH MISDRILLED HOLE BETWEEN LONGERONS 11 AND 12 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE, STRAPS AND FILLERS IAW FAA APPROVED ACMI SKETCH SK 98393, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98537Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 1060 WITH MISDRILLED HOLE BETWEEN LONGERONS 7 AND 8 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE, STRAPS AND SHIMS IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R98, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98536Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 1180 WITH MISDRILLED HOLE AT LONGERON 13 RIGHT. FABRICATED AND INSTALLED NEW INTERCOSTAL CLIP AND REPAIR STRAPS IAW FAA APPROVED ACMI SKETCH SK98379, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98535Skin · corrodedDURING MAINTENANCE VISIT, FOUND CORROSION ON INTERNAL UPPER SKIN AT STA XE282 TO 291 OF LT HORIZONTAL STABILIZER. REMOVED PANEL, FABRICATED AND INSTALLED NEW SKIN PANEL IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R89, DC-8 SRM 51-1-21 AND TREATED IAW DNov 6, 1998 · N995CF · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR RRXA98534Skin · corrodedDURING MAINTENANCE VISIT, FOUND CORROSION ON INTERNAL UPPER SKIN AT STA XE224 TO 260 OF LT HORIZONTAL STABILIZER. REMOVED PANEL, FABRICATED AND INSTALLED NEW SKIN PANEL IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R90, DC-8 SRM 51-1-21 AND TREATED IAW DNov 6, 1998 · N995CF · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR RRXA98533Skin · corrodedDURING MAINTENANCE VISIT, FOUND CORROSION ON INTERNAL UPPER SKIN AT STA XE167 TO 221 OF LT HORIZONTAL STABILIZER. REMOVED PANEL, FABRICATED AND INSTALLED NEW SKIN PANEL IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R91, DC-8 SRM 51-1-21 AND TREATED IAW DNov 6, 1998 · N995CF · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR RRXA98532Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 700 WITH MISDRILLED HOLE BETWEEN LONGERONS 11 AND 12 LEFT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R65, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98531Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 640 WITH MISDRILLED HOLE AT LONGERON 12 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND STRAP IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R40, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98530Skin · corrodedDURING MAINTENANCE VISIT, FOUND CORROSION ON INTERNAL UPPER SKIN AT STA XE185 OF RT HORIZONTAL STABILIZER. REMOVED PANEL, FABRICATED AND INSTALLED NEW SKIN PANEL IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R91, DC-8 SRM 51-1-21 AND TREATED IAW DC-8 SRMNov 6, 1998 · N995CF · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR RRXA98529Frame · damagedDURING MAINTENANCE VISIT, FOUND FRAME 255 NICKED IN RADIUS BETWEEN LONGERONS 12 AND 13 RIGHT. FABRICATED AND INSTALLED REPAIR STRAP IAW FAA APPROVED ACMI SKETCH SK98364. HEAT TREATED IAW DC-8 SRM 51-1-1 AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98528Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 1080 WITH MISDRILLED HOLE BETWEEN LONGERONS 7 AND 8 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R97. HEAT TREATED ANGLE IAW DC-8 SRM 51-1-1 AND AREA TREATED IANov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98527Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 1260 WITH MISDRILLED HOLE AT LONGERON 20 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R21, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98526Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 1380 WITH MISDRILLED HOLE AT LONGERON 9 RIGHT. PLUGGED HOLE IN FRAME, FABRICATED AND INSTALLED REPAIR STRAPS IAW FAA APPROVED ACMI SKETCH SK98392, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98525Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 1300 WITH MISDRILLED HOLES AT LONGERON 13 RIGHT. FABRICATED AND INSTALLED REPAIR STRAPS AND INTERCOSTAL CLIPS IAW FAA APPROVED ACMI SKETCH SK98384, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98524Skin · corrodedDURING MAINTENANCE VISIT, FOUND CORROSION ON LOWER SURFACE OF RT HORIZONTAL STABILIZER SKIN PANEL AT STA XE270 TO 310. REMOVED CORROSION AND FOUND TO BE BEYOND LIMITS. FABRICATED AND INSTALLED NEW SKIN PANEL IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-Nov 6, 1998 · N995CF · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR RRXA98523Frame · misdrilledDURING MAINTENANCE VISIT FOUND FRAME 660 WITH MISDRILLED HOLE AT LT CUSP. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R69.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98522Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 1440 WITH MISDRILLED HOLE AT LONGERON 12 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R35, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98521Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 1320 WITH MISDRILLED HOLE BETWEEN LONGERONS 7 AND 8 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND STRAP IAW FAA APPROVED ACMI SKETCH SK98385, DC-8 SRM 51-1-21 AND TREATED IAW DC-8 SRM 51-1-8.Nov 5, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98520Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 440 WITH MISDRILLED HOLE BETWEEN LONGERONS 7 AND 9 RIGHT. FABRICATED AND INSTALLED REPAIR STRAPS IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R36, DC-8 SRM 51-1-21 AND TREATED AREA IAW DC-8 SRM 51-1-8.Nov 5, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98519Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 560 WITH MISDRILLED HOLES AT LONGERONS 19 AND 20 RIGHT. PLUGGED MISDRILLED HOLES IAW DC-8 SRM 51-1-21, FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R45 AND TREATED AREA IAW DC-8Nov 5, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98518Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 1420 WITH MISDRILLED HOLES AT LONGERONS 5, 7 AND 8 LEFT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R41.Nov 5, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98517Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 1240 WITH MISDRILLED HOLE AT LONGERON 8 LEFT. BLENDED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R44, DC-8 SRM 51-1-21 AND TREATED AREA IAW DC-8 SRM 51-1-8.Nov 5, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98516Floorbeam · misdrilledDURING MAINTENANCE VISIT, FOUND FLOORBEAM AT FS 880 WITH MISDRILLED HOLES. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLES, FILLER AND STRAP IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R54, DC-8 SRM 51-1-21, 51-1-20D AND TREATED AREA IAW DNov 5, 1998 · N995CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA98515Floorbeam · crackedDURING MAINTENANCE VISIT, FOUND FLOORBEAM AT FS 1480 LEFT CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA APPROVED ACMI SKETCH SK98463, DC-8 SRM 51-1-20D AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 5, 1998 · N995CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA98514Floorbeam · crackedDURING MAINTENANCE VISIT, FOUND FLOORBEAM AT FS 1500 LEFT CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER AND SHIM IAW FAA APPROVED ACMI SKETCH SK98464, DC-8 SRM 51-1-20D AND TREATED AREA IAW DC-8 SRM 51-1-8.Nov 5, 1998 · N995CF · Doug DC862 · Fuselage Main, Floor Beam
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