# Service difficulty reports: N870BX, cancelled May 22, 2017 A list on [N870BX, cancelled May 22, 2017](https://openairdocs.org/deregistered/N870BX-2017-05-22.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 · 109 reports - [SDR IXXA0000037](https://openairdocs.org/sdr/IXXA0000037.md): Panel · defective · Oct 28, 2000 · N870BX · Doug DC863F · AC Generation System > EN 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 ELECTRICAL - [SDR IXXA0000012](https://openairdocs.org/sdr/IXXA0000012.md): Unknown · odor · Mar 29, 2000 · N870BX · Doug DC863F · Air Distribution System > FLT 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 W - [SDR CKSA98259](https://openairdocs.org/sdr/CKSA98259.md): Transformer · malfunction · Apr 14, 1998 · N870BX · Doug DC863F · Flight Compartment Lighting > ON 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 TRANSFOR - [SDR CKSA98201](https://openairdocs.org/sdr/CKSA98201.md): Skin · corroded · Feb 28, 1998 · N870BX · Doug DC863F · Cargo/Baggage Doors > DURING 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 - [SDR CKSA98200](https://openairdocs.org/sdr/CKSA98200.md): Frame · corroded · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Frame > DURING 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 AN - [SDR CKSA98199](https://openairdocs.org/sdr/CKSA98199.md): Fitting · corroded · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous Structure > DURING 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 S - [SDR CKSA98198](https://openairdocs.org/sdr/CKSA98198.md): Fitting · corroded · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous Structure > DURING 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 2 - [SDR CKSA98197](https://openairdocs.org/sdr/CKSA98197.md): Fitting · corroded · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous Structure > DURING 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 N - [SDR CKSA98196](https://openairdocs.org/sdr/CKSA98196.md): Seat Track · corroded · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings > DURING 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. PRIM - [SDR CKSA98195](https://openairdocs.org/sdr/CKSA98195.md): Seat Track · corroded · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings > DURING 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. PRIM - [SDR CKSA98194](https://openairdocs.org/sdr/CKSA98194.md): Frame · corroded · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Frame > DURING 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 - [SDR CKSA98193](https://openairdocs.org/sdr/CKSA98193.md): Fitting · corroded · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous Structure > DURING 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 N - [SDR CKSA98192](https://openairdocs.org/sdr/CKSA98192.md): Fitting · corroded · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous Structure > DURING 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 AT - [SDR CKSA98191](https://openairdocs.org/sdr/CKSA98191.md): Longeron · corroded · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Longeron/Stringer > DURING 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. - [SDR CKSA98190](https://openairdocs.org/sdr/CKSA98190.md): Bulkhead Web · punctured · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Bulkhead > DURING 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 S - [SDR CKSA98189](https://openairdocs.org/sdr/CKSA98189.md): Bulkhead Angle · broken · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Bulkhead > DURING 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 1 - [SDR CKSA98188](https://openairdocs.org/sdr/CKSA98188.md): Seat Track · worn · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings > DURING 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 A - [SDR CKSA98187](https://openairdocs.org/sdr/CKSA98187.md): Skin · damaged · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Plate/Skin > DURING 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 PA - [SDR CKSA98186](https://openairdocs.org/sdr/CKSA98186.md): Flange · cracked · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Frame > DURING 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 TREATED - [SDR CKSA98185](https://openairdocs.org/sdr/CKSA98185.md): Skin · corroded · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Plate/Skin > DURING 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 REPAIR - [SDR CKSA98184](https://openairdocs.org/sdr/CKSA98184.md): Fitting · misdrilled · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous Structure > DURING 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. - [SDR CKSA98183](https://openairdocs.org/sdr/CKSA98183.md): Frame · cracked · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Frame > DURING 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- - [SDR CKSA98182](https://openairdocs.org/sdr/CKSA98182.md): Frame · misdrilled · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Frame > DURING 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 NUMB - [SDR CKSA98181](https://openairdocs.org/sdr/CKSA98181.md): Frame · misdrilled · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Frame > DURING 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 IT - [SDR CKSA98180](https://openairdocs.org/sdr/CKSA98180.md): Skin · damaged · Feb 28, 1998 · N870BX · Doug DC863F · Wing, Plate/Skin > DURING 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 57 - [SDR CKSA98179](https://openairdocs.org/sdr/CKSA98179.md): Fitting · misdrilled · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous Structure > DURING 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 NUM - [SDR CKSA98178](https://openairdocs.org/sdr/CKSA98178.md): Fitting · cracked · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous Structure > DURING 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 A - [SDR CKSA98177](https://openairdocs.org/sdr/CKSA98177.md): Fitting · cracked · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous Structure > DURING 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 S - [SDR CKSA98176](https://openairdocs.org/sdr/CKSA98176.md): Skin · cracked · Feb 28, 1998 · N870BX · Doug DC863F · Cargo/Baggage Doors > DURING 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 PG - [SDR CKSA98175](https://openairdocs.org/sdr/CKSA98175.md): Seat Track · worn · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings > DURING 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- - [SDR CKSA98174](https://openairdocs.org/sdr/CKSA98174.md): Seat Track · worn · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings > DURING 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 53 - [SDR CKSA98173](https://openairdocs.org/sdr/CKSA98173.md): Seat Track · worn · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings > DURING 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. - [SDR CKSA98172](https://openairdocs.org/sdr/CKSA98172.md): Seat Track · worn · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings > DURING 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 - [SDR CKSA98171](https://openairdocs.org/sdr/CKSA98171.md): Seat Track · broken · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings > DURING 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 DC8 - [SDR CKSA98170](https://openairdocs.org/sdr/CKSA98170.md): Seat Track · worn · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings > DURING 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 0447 - [SDR CKSA98169](https://openairdocs.org/sdr/CKSA98169.md): Seat Track · worn · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings > DURING 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 0 - [SDR CKSA98168](https://openairdocs.org/sdr/CKSA98168.md): Seat Track · worn · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings > DURING 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-C - [SDR CKSA98167](https://openairdocs.org/sdr/CKSA98167.md): Seat Track · worn · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage, Seat/Cargo Attach Fittings > DURING 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 5 - [SDR CKSA98166](https://openairdocs.org/sdr/CKSA98166.md): Splice · corroded · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Miscellaneous Structure > DURING 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 - [SDR CKSA98165](https://openairdocs.org/sdr/CKSA98165.md): Frame · misdrilled · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Frame > DURING 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, SEALED - [SDR CKSA98164](https://openairdocs.org/sdr/CKSA98164.md): Frame · misdrilled · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Frame > DURING 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 TREAT - [SDR CKSA98163](https://openairdocs.org/sdr/CKSA98163.md): Frame · misdrilled · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Frame > DURING 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 - [SDR CKSA98162](https://openairdocs.org/sdr/CKSA98162.md): Frame · misdrilled · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Frame > DURING 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 - [SDR CKSA98161](https://openairdocs.org/sdr/CKSA98161.md): Frame · misdrilled · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Frame > DURING 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 STRAP - [SDR CKSA98160](https://openairdocs.org/sdr/CKSA98160.md): Frame · misdrilled · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Frame > DURING 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 - [SDR CKSA98159](https://openairdocs.org/sdr/CKSA98159.md): Frame · misdrilled · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Frame > DURING 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. CO - [SDR CKSA98158](https://openairdocs.org/sdr/CKSA98158.md): Frame · misdrilled · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Frame > DURING 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 - [SDR CKSA98157](https://openairdocs.org/sdr/CKSA98157.md): Frame · misdrilled · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Frame > DURING 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. INS - [SDR CKSA98156](https://openairdocs.org/sdr/CKSA98156.md): Frame · misdrilled · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Frame > DURING 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 51 - [SDR CKSA98155](https://openairdocs.org/sdr/CKSA98155.md): Frame · misdrilled · Feb 28, 1998 · N870BX · Doug DC863F · Fuselage Main, Frame > DURING 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 AND Next page: https://openairdocs.org/deregistered/N870BX-2017-05-22/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 = 'N870BX' AND deregistration_id = 'N870BX-2017-05-22' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N870BX-2017-05-22/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.