N870BX, cancelled May 22, 2017

Service difficulty reports · 109

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 = 'N870BX' AND deregistration_id = 'N870BX-2017-05-22'
  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 IXXA0000037Panel · defectiveEN ROUTE FROM LRD TO BRO, DURING DESCENT LOST OF ALL GENERATOR ELECTRICAL POWER WAS EXPERIENCED. THE FLT CREW FOLLOWED COMPANY PROCEDURES AND ALL ELECTRICAL POWER WAS RESTORED. ALL GENERATOR OPERATING PARAMETERS WERE NORMAL. SEVERAL MINUTES LATER ELECTRICALOct 28, 2000 · N870BX · Doug DC863F · AC Generation SystemSDR IXXA0000012Unknown · odorFLT 823 - MKE-TOL, AN ODOR WAS SENSED IN THE COCKPIT WHEN THE CENTER PEDESTAL LIGHTING FUSE ILLUMINATED, THEN SUBSIDED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE PLACED THE CENTER PEDESTAL LIGHTING SYSTEM ON DEFERRAL. THE AIRCRAFT WMar 29, 2000 · N870BX · Doug DC863F · Air Distribution SystemSDR CKSA98259Transformer · malfunctionON LANDING F/E'S PANEL BEHIND LIGHT SWITCH'S BEGAN TO ARC AND SMOKE. ON INSPECTION OF LIGHT SWITCHES FOUND DAMAGE ON FLOOD LIGHT SWITCHES PULLED BREAKERS AS REQUIRED AND TIED OFF CONTINUE DMI NR 8230998 IAW DC8 MM 33-1. REMOVED AND REPLACED RHEOSTAT TRANSFORApr 14, 1998 · N870BX · Doug DC863F · Flight Compartment LightingSDR CKSA98201Skin · corrodedDURING ROUTINE C-2 CHECK INSPECTION, FOUND B-PIT DOOR HAS CORROSION ON LOWER SEAL CHANNEL FWD LOWER TO AFT LOWER. REMOVED MINOR SURFACE CORROSION ON LOWER AFT CORNER AND AREA BETWEEN FWD AND AFT CORNER. .002 METAL REMOVED IS WITHIN LIMITS IAW DC8 SRM 52-2-0 Feb 28, 1998 · N870BX · Doug DC863F · Cargo/Baggage DoorsSDR CKSA98200Frame · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION ON FWD FACE OF FRAME AT FS Y180 ABOVE LONGERON 34R. CORROSION REMOVAL BEYOND DC8 SRM LIMITS IAW DC8 SRM 51-1-8 AND 53-2-0 FIG 7. HEAT TREATED AND AGED DOUBLER IAW DC8 SRM 51-1-1. LOCATED ANFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, FrameSDR CKSA98199Fitting · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. NR 1 T-BOLT BACK-UP FITTING CORRODED STA Y288. REMOVED NR 1 T BOLT BACK UP FITTING AT STA Y288. CLEANED AND PRIMED AREA IAW DC8 SRM 51-1-8. DRILLED NEW FITTING AND FABRICATED REPAIR SPLICES IAW DC8 SFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous StructureSDR CKSA98198Fitting · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION ON FITTING AT FS 340 BETWEEN LONGERON 34R AND 35R. CORROSION IS OUT OF LIMITS. REMOVED FITTING FROM STA 340 BETWEEN L34R AND 35R. CUT NEW FITTING, FABRICATED SPLICES IAW DC8 SRM 53-2-0 FIG 2Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous StructureSDR CKSA98197Fitting · corrodedDURING ROUTINE CPCP INSPECTION, FOUND CORROSION ON FRAME TO SPAR FITTING CENTER WING UPPER SKIN UNDER CUSP RIGHT SIDE STA680 X=-64. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. REMOVED FITTING AND REPLACED WITH NFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous StructureSDR CKSA98196Seat Track · corrodedDURING ROUTINE C-2 CHECK INSPECTION, FOUND COCKPIT FLOOR TRACK SECOND OBSERVERS SEAT AFT TRACK HAS CORROSION AROUND FASTENERS. REMOVED AND REPLACED AFT FLOOR TRACK AT SECOND OBSERVERS SEAT IAW DC8 SRM 51-1-21. SEAT TRACK DRILLED IAW DAC DWG NR 3657504. PRIMFeb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach FittingsSDR CKSA98195Seat Track · corrodedDURING ROUTINE C-2 CHECK INSPECTION, FOUND COCKPIT FLOOR TRACK SECOND OBSERVERS SEAT FWD TRACK HAS CORROSION AROUND FASTENERS. REMOVED AND REPLACED FWD FLOOR TRACK AT SECOND OBSERVERS SEAT IAW DC8 SRM 51-1-21. SEAT TRACK DRILLED IAW DAC DWG NR 3657504. PRIMFeb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach FittingsSDR CKSA98194Frame · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION OF FLOOR FRAME STA 240 ABOVE LONGERON 35L A PIT. AFTER REMOVAL OF CORROSION FLOOR FRAME OUT OF LIMITS. FABRICATED REPAIR FILLER AND DOUBLERS IAW DC8 SRM 53-2-0 FIG 2. HEAT TREATED AND AGED Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, FrameSDR CKSA98193Fitting · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION ON UPPER CUSP FITTING AT FS 580 LT. REMOVED UPPER CUSP FITTING AT STA 580 LT. CORROSION EVALUATION BEYOND LIMITS IAW DC8 SRM 53-2-0. TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8. INSTALLED NFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous StructureSDR CKSA98192Fitting · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION AND GOUGE MARK ON LT UPPER CUSP FITTING AT FS 1000. REMOVED OLD FITTING IAW DC8 SRM 53-1-0. DRILLED UP NEW FITTING ON LT UPPER CUSP AT FS 1000 IAW DC8 SRM 51-1-20D. INSTALLED NEW FITTING ATFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous StructureSDR CKSA98191Longeron · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION SPOT ON LT SIDE OF LONG 34 RT AT FS Y298 INSIDE DOOR CUT OUT. CORROSION REMOVAL IS BEYOND LIMITS OF DC8 SRM 53-2-0 FIG 1F. REMOVED SECTION OF LONG 34R FROM FS 285 TO 315 INSIDE DOOR CUTOUT. Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Longeron/StringerSDR CKSA98190Bulkhead Web · puncturedDURING ROUTINE C-2 CHECK INSPECTION, FOUND NUMEROUS PUNCTURES ON LOWER END OF 9G BULKHEAD. FABRICATED REPAIR DOUBLERS TO REPAIR PUNCTURES ON LOWER END OF 9G BULKHEAD, DRILLED AND DEBURRED DOUBLERS AND BULKHEAD, TREATED, PRIMED AND INSTALLED DOUBLERS IAW DC8 SFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, BulkheadSDR CKSA98189Bulkhead Angle · brokenDURING ROUTINE CPCP INSPECTION, FOUND BULKHEAD ATTACH ANGLE RT SIDE BETWEEN C AND D PITS FS 1320 HAS AREA BROKEN OUT AT TWO HOLES WHERE ATTACH ANGLE ATTACHES TO FRAME. REPAIRED BROKEN BULKHEAD ATTACH ANGLE RT SIDE BETWEEN C AND D PITS IAW DC8 SRM 53-2-0 FIG 1Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, BulkheadSDR CKSA98188Seat Track · wornDURING ROUTINE C-2 CHECK INSPECTION, FOUND CAPT'S UPPER SEAT TRACKS WORN. REMOVED AND REPLACED BOTH FWD SEAT TRACK T'S AT CAPT'S POSITION IAW DC8 SRM 53-1-0 AND 51-1-20D. INSTALLATION OK. AFTER CAPT'S SEAT INSTALLATION SEAT TRACK AND SEAT OPERATES GOOD AT AFeb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach FittingsSDR CKSA98187Skin · damagedDURING ROUTINE CPCP INSPECTION, FOUND SKIN TORN DAMAGE TOP OF DOOR CUT OUT BOX FS 320 TO 330 ABOVE LONGERON 35 RT. ROUTED OUT DAMAGED AREA AT FS 320 TO 330 LONGERON 35 RT. FABRICATED FILLER AND REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 1D. TREATED AND PRIMED PAFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Plate/SkinSDR CKSA98186Flange · crackedDURING ROUTINE CPCP INSPECTION, FOUND FRAME FLANGE CRACKED STA Y420 ABOVE LONGERON 36. REMOVED INTERCOSTAL AT FS 420 TO ACCESS DAMAGE AREA FROM LONGERON 35 TO 36RT. REMOVED DAMAGE, FABRICATED PLUG AND 2 REPAIR DOUBLERS IAW DC8 SRM 53-2-0 FIG 2. HEAT TREATEDFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, FrameSDR CKSA98185Skin · corrodedDURING ROUTINE C-2 CHECK INSPECTION, FOUND LEFT WHEEL WELL BARE METAL WITH SLIGHT CORROSION ON TOP OF LONGERON 24 STA 980 AROUND 2 AFT BOLT HEADS. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND CRACK AT FS 980 ON LONGERON. STOP DRILLED CRACK, FABRICATED REPAIRFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Plate/SkinSDR CKSA98184Fitting · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND HOLES DRILLED INTO RT UPPER CUSP FITTING AT FS 1000. REMOVED AND REPLACED CUSP FITTING AT FS 1000 IAW DC8 SRM 51-1-20D AND 51-3-0. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04793 TASK NR Y1252.Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous StructureSDR CKSA98183Frame · crackedDURING ROUTINE CPCP INSPECTION, FOUND LT FRAME CRACKED AT FS 1560. REMOVED CUSP FITTING AND CUT OUT CRACKED FRAME SEGMENT ON LT FRAME STA 1560. FABRICATED NEW FRAME SEGMENT AND DOUBLERS AND FILLERS IAW DC8 SRM 53-2-0 FIG 2 SHEET 4 VIEW J. HEAT TREATED 7075-Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, FrameSDR CKSA98182Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 480, 5.5 ABOVE UPPER CUSP AREA. PLUGGED HOLES, FABED SHIM, ANGLE AND DRILLED RT FRAME AT FS 480 IAW COTNEY DWG NR D93-R15 AND DC8 SRM 51-1-21 AND 51-1-8. CORROSION TASK CARD NUMBFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, FrameSDR CKSA98181Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 560, 5.5 ABOVE UPPER CUSP AREA. FABRICATED REPAIR ANGLE IAW COTNEY DWG NR D93-R02. HEAT TREATED AND AGED IAW DC8 SRM 51-1-1. PERFORMED CONDUCTIVITY TEST ON HEAT TREATED ANGLE ITFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, FrameSDR CKSA98180Skin · damagedDURING ROUTINE C-2 CHECK INSPECTION, FOUND RT WING L/E STA XFS710 LOWER SEAM SCREW HEADS PULLED THROUGH L/E SKIN. FABRICATED FILLER PLATE FROM 7075-T6 .063 IAW SRM 57-2-1 FIG 2H PG 15 AND INSTALLED REPAIR ON RT WING L/E STA XFS710 LOWER SEAM SCREWS IAW SRM 57Feb 28, 1998 · N870BX · Doug DC863F · Wing, Plate/SkinSDR CKSA98179Fitting · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND LT UPPER CUSP FITTING AT FS 600 DRILLED INTO. REMOVED LT UPPER CUSP FITTING AT FS 600. POSITION AND FITTED NEW CUSP FITTING IAW DC8 SRM 53-1-0. INSTALLED FITTING IAW DC8 SRM 51-3-0 AND 51-1-20D. CORROSION TASK CARD NUMFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous StructureSDR CKSA98178Fitting · crackedDURING ROUTINE CPCP INSPECTION, FOUND FITTING CRACKED ON STA 857 FRAME RT SIDE 20 INCHES ABOVE CUSP. REMOVED FITTING FROM STA 857 FRAME, FABRICATED FITTING IAW DAC DWG NR 3779498. LOCATE AND PICKED UP ALL ATTACHMENT LOCATIONS IAW DC8 SRM 51-1-20D. TREATED AFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous StructureSDR CKSA98177Fitting · crackedDURING ROUTINE CPCP INSPECTION, FOUND FITTING CRACKED ON STA 902 FRAME RT SIDE 20 INCHES ABOVE CUSP. REMOVED DAMAGED FITTING, FABRICATED NEW FITTING IAW DAC DWG NR 3779498. DRILLED UP NEW FITTING PER DC8 SRM 53-1-0 AND 51-1-20D. TREATED AND PRIMED IAW DC8 SFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous StructureSDR CKSA98176Skin · crackedDURING ROUTINE C-2 CHECK INSPECTION, FOUND A PIT DOOR INNER SKIN CRACKED 2 PLACES UPPER FWD CORNER. STOP DRILLED CRACK AND FABRICATED, HEAT-TREATED, TREATED AND PRIMED AND INSTALLED DOUBLER ON CRACK A-PIT DOOR INNER SKIN IAW DC8 SRM 51-1-1, 51-1-21, 52-4-1 PGFeb 28, 1998 · N870BX · Doug DC863F · Cargo/Baggage DoorsSDR CKSA98175Seat Track · wornDURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 1400, BL 45RT. CUT OUT DAMAGED AREA 2 PLACES FOR PLUG REPAIR AT STA 1400 BL 45RT IAW DC8 SRM 53-2-3. TREATED AND PRIMED AREA OF REPAIR IAW DC8 SRM 51-1-8. INSTALLED PLUG REPAIRS IAW DC8 SRM 51-Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach FittingsSDR CKSA98174Seat Track · wornDURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 860, BL 45RT. REMOVED THE DAMAGED CARGO TRACK AT STA 860, BL 45RT. CORROSION TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED CHANNELS AND PLUGS ON CARGO TRACK AT STA 860 BL 45RT IAW DC8 SRM 53Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach FittingsSDR CKSA98173Seat Track · wornDURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 770 BL 24RT. CUT WORN OUT SEAT TRACK AT STA 770, BL 24RT. INSTALLED CHANNELS AND SEAT TRACK IAW DC8 SRM 53-2-3 FIG DG. C-CHECK WORK CARD NUMBER 0060. NON-ROUTINE NR 04472 TASK NR Y1583.Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach FittingsSDR CKSA98172Seat Track · wornDURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 1130, BL 24RT. CUT THE DAMAGED SEAT TRACK AT STA 1130 BL 24RT TO FIT PLUGS AND CHANNELS. INSTALLED THE PLUGS AND CHANNELS FIT IN TRACK STA 1130, BL 24RT IAW DC8 SRM 53-2-3 FIG 6D. C-CHECK WORK Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach FittingsSDR CKSA98171Seat Track · brokenDURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK LUGS BROKEN AT BEAR TRAP POSITION BETWEEN COMP 1 AND 2 BL 24RT. ROUTED OUT BROKEN LUGS AT BEAR STRAP BETWEEN COMP 1 AND 2 BL24RT TO INSTALL PLUGS. INSTALLED PLUGS WITH SCREWS IAW SRM 53-2-3 FIG 6D AND DC8Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach FittingsSDR CKSA98170Seat Track · wornDURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 1220 BL 45 LT. REMOVED DAMAGE FROM SEAT TRACK TO FLT TRACK PLUGGED IAW DC8 SRM 53-2-3 FIG 6D. PRIMED AND INSTALLED IAW DC8 SRM 53-2-3 FIG 6D. C-CHECK WORK CARD NUMBER 0060. NON-ROUTINE NR 0447Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach FittingsSDR CKSA98169Seat Track · wornDURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 680, BL 0. REMOVED 2 SECTIONS OF WORN SEAT TRACK, STA 680, BL 0. INSTALLED TWO TRACK PLUGS IAW DC8 SRM 53-2-3 FIG 6D SHEET 1 AND DC8 SRM 51-3-0. C-CHECK WORK CARD NUMBER 0060. NON-ROUTINE NR 0Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach FittingsSDR CKSA98168Seat Track · wornDURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 870, BL 0. CUT OUT DAMAGED AREA OF SEAT TRACK 2 PLACES FOR PLUG REPAIR IAW DC8 SRM 53-2-3. TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8. INSTALLED PLUG REPAIRS IAW DC8 SRM 53-2-3 AT STA 870. C-CFeb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach FittingsSDR CKSA98167Seat Track · wornDURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 1310, BL 24RT. REMOVED DAMAGED CARGO TRACK AT STA 1310, BL 24RT TO FIT PLUGS. CORROSION TREATED, PRIMED IAW DC8 SRM 51-1-8. INSTALLED CHANNELS AND PLUGS ON TRACK STA 1310, BL 24RT IAW DC8 SRM 5Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach FittingsSDR CKSA98166Splice · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION ON DOUBLER FS 1050 LONG 31LT. CLEANED CORROSION ON SPLICE PLATE IAW DC8 SRM 51-1-8. CORROSION REMOVAL OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. REMOVED SPLICE PLATE IAW DC8 SRM 51-1-20D AND Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous StructureSDR CKSA98165Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND HOLE DRILLED INTO LT FRAME RADIUS AT FS 580, 12 ABOVE UPPER CUSP AREA. PLUGGED MISDRILLED HOLES FABRICATED SHIM AND REPAIR STRAP, FITTED, DRILLED AND DEBURRED STRAPS, SHIM AND FRAME. TREATED AND PRIMED BARE METAL, SEALEDFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, FrameSDR CKSA98164Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND HOLE DRILLED INTO LT FRAME RADIUS AT FS 480, 20 ABOVE UPPER CUSP AREA AND GOUGE AT 12 ABOVE UPPER CUSP AREA. FABRICATED REPAIR ANGLE AND SHIMS, LOCATED, DRILLED ATTACHMENTS LOCATIONS IAW COTNEY DWG NR D93-R12. HEAT TREATFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, FrameSDR CKSA98163Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME RADIUS AT FS 1540, 5 ABOVE UPPER CUSP AREA. FABRICATED AND INSTALLED NEW ANGLE FOR FRAME REPAIR AT FS 1540 LT, 5 ABOVE UPPER CUSP AREA PER COTNEY DRAWING D93-R72. FABRICATED, HEAT AND Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, FrameSDR CKSA98162Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED IN LT FRAME RADIUS AT FS 1520, 5 ABOVE UPPER CUSP AREA. INSTALLED RIVET IN MISDRILLED HOLE IN RADIUS IAW DC8 SRM 51-1-21, FABRICATED DOUBLER AND SHIM IAW COTNEY DRAWING NR D93-R51, PRIME AND TREATED Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, FrameSDR CKSA98161Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1500 5 ABOVE UPPER CUSP AREA. REMOVED DAMAGED AREA OF FRAME OF LT FRAME FS 1500 5 ABOVE UPPER CUSP. FAB REPAIR STRAP AND SHIM, FITTED, DRILLED, AND DEBURRED FRAME, SHIM AND STRAPFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, FrameSDR CKSA98160Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1480, 5 ABOVE UPPER CUSP AREA AND ON LT FRAME RADIUS FROM 9 TO 44 ABOVE UPPER CUSP AREA. DEEP GOUGE ON LT FRAME AT FS 1480, 5 ABOVE UPPER CUSP AREA. ROUTED OUT DAMAGED AREA, DID Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, FrameSDR CKSA98159Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1460, 5 ABOVE UPPER CUSP AREA. FAB 2 REPAIRS IAW COTNEY DWG NBR D93-R33. HEAT TREATED AND AGED REPAIR ANGLES, INSTALLED REPAIRS IAW DC8 SRM 51-1-1, 51-1-8, 51-1-21, 51-1-20D. COFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, FrameSDR CKSA98158Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1440, 5 ABOVE UPPER CUSP AREA. FABRICATED REPAIR PARTS FOR STA 1440 LT SIDE, 5 ABOVE CUSP AREA. DRILLED UP PARTS. TREATED AND PRIMED PARTS, INSTALLED -3 SHIM -2 ANGLE -4 SHIM -1 Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, FrameSDR CKSA98157Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1420, 5 ABOVE UPPER CUSP AREA AND LT FRAME RADIUS AT 31 AND 40 ABOVE UPPER CUSP AREA. FABRICATED 2 REPAIR FROM 7075.0 HEAT TREATED TO 7075-T6 .071 DRILL TO FIT FRAME 2 SHIM. INSFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, FrameSDR CKSA98156Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1380, 5 ABOVE UPPER CUSP AREA. FABRICATED, DRILLED, HEAT-TREATED, TREATED AND PRIMED AND INSTALLED FILLER AND SHIM ON LT FRAME AT FS 1380 IAW COTNEY DRAWING D93-R40 AND DC8 SRM 51Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, FrameSDR CKSA98155Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1360, 5 ABOVE UPPER CUSP AREA. FABRICATED REPAIRS DRILLED TO FIT FRAME AT STA 1360 2 REPAIRS. PRIMED AND TREATED. INSTALLED REPAIR IAW COTNEY DRAWING D93-R34, DC8 SRM 51-1-1 ANDFeb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Frame
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