# Service difficulty reports: N8087U, cancelled Feb 13, 2008 A list on [N8087U, cancelled Feb 13, 2008](https://openairdocs.org/deregistered/N8087U-2008-02-13.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 · 131 reports - [SDR RRXA001069](https://openairdocs.org/sdr/RRXA001069.md): Gyro · failed · Oct 17, 2000 · N8087U · Doug DC871F · Attitude Gyro and Indicating System > CO PILOTS ATT GYRO INOP ATTITUDE. FOUND SIX DEGREE SPILT BETWEEN PILOTS AND CO-PILOTS HSI. REMOVED AND REPLACED VG IAW DC-8 M/M 34-25-1. CHECK GOOD. REMOVED AND REPLACED DG IAW DC-8 M/M 34-21-1. OPS CHECK GOOD. - [SDR RRXA001011](https://openairdocs.org/sdr/RRXA001011.md): Fire Detector · shorted · Jul 7, 2000 · N8087U · Doug DC871F · Fire Detection > ENROUTE- ENGINE FIRE WARNING #1 ENG FIRED BOTH BOTTLES AND COULD NOT GET A TEST DIVERTED TO DENVER. FOUND FIRE LOOP DETECTOR ELEMENT ABOVE COMBUSTION SECTION SHORTED. REMOVED AND REPLACED SAME IAW DC8MM 26-11-16. ALSO REMOVED AND REPLACED BOTH FIRE EXTINGU - [SDR RRXA001006](https://openairdocs.org/sdr/RRXA001006.md): Warning Light · illuminated · Jun 29, 2000 · N8087U · Doug DC871F · Hydraulic Indicating System > ON CLIMBOUT HYD OVERTEMP LIGHT CAME ON. WHEN RUNNING QRH TEMP WOULD NOT COME DOWN AND ACFT KEPT GIVING STRONG AILERON INPUTS. HYD SYSTEM WAS DEPRESSED AND HYD PWR LEVERS OFF, FLIGHT CONTROLS WERE STILL GIVING STRONG AILERONS & RUDDER INPUTS. HYDRAULIC ZERO - [SDR RRXA991630](https://openairdocs.org/sdr/RRXA991630.md): Plank · corroded · Sep 21, 1999 · N8087U · Doug DC871F · Horizontal Stabilizer Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, HORIZONTAL STABILIZER, CENTER SECTION UPPER CENTER PLANK UPPER SURFACE AT RBL X30. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PLANK IAW SB 55- - [SDR RRXA991521](https://openairdocs.org/sdr/RRXA991521.md): Panel · corroded · Sep 21, 1999 · N8087U · Doug DC871F · Horizontal Stabilizer, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION, HORIZONTAL STAB, CENTER SECTION, UPPER CENTER PLANK, UPPER SURFACE AT BL -30 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PLANK IAW DC8 SB - [SDR RRXA991636](https://openairdocs.org/sdr/RRXA991636.md): Frame · corroded · Sep 1, 1999 · N8087U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE FRAME AT FLOORBEAM AT STA 1727, LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 53-2-0. (CORROSION - [SDR RRXA991635](https://openairdocs.org/sdr/RRXA991635.md): Floorbeam · corroded · Sep 1, 1999 · N8087U · Doug DC871F · Fuselage Main, Floor Beam > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOORBEAM AT STA 1727 AT FRAME R/S. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOORBEAM IAW FAA DER ENGINEERING SKETCH NR SK-087-316 - [SDR RRXA991471](https://openairdocs.org/sdr/RRXA991471.md): Frame · corroded · Sep 1, 1999 · N8087U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE FRAME, AT STA 1727, AT THE FLOORBEAM (LON L/R). DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 53-2-0. (CORROSION DAM - [SDR RRXA991435](https://openairdocs.org/sdr/RRXA991435.md): Floorbeam · corroded · Sep 1, 1999 · N8087U · Doug DC871F · Fuselage Main, Floor Beam > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR BEAM AT STA Y1727 AT FRAME. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOORBEAM SECTION IAW FAA APPROVED ENGINEERING SKETCH NR - [SDR RRXA991629](https://openairdocs.org/sdr/RRXA991629.md): Fitting · corroded · Aug 31, 1999 · N8087U · Doug DC871F · Wing Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, WING, RIGHT, RT OB FLAP AT STA X=410 FLAP SUPPORT FITTING LWR SURFACE UNDER FLAP TRACKS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW - [SDR RRXA991518](https://openairdocs.org/sdr/RRXA991518.md): Fitting · corroded · Aug 31, 1999 · N8087U · Doug DC871F · Wing Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND SPOTS OF CORROSION ON RT O/B FLAP AT STA X-410, FLAP SUPPORT FITTING LWR SURFACE UNDER FLAP TRACKS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW - [SDR RRXA991646](https://openairdocs.org/sdr/RRXA991646.md): Retract Pin · corroded · Aug 29, 1999 · N8087U · Doug DC871F · Landing Gear Retraction/Extension System > DURING A MAINTENANCE VISIT FOUND CORROSION, RT MLG, RETACT PIN BOSS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REBUSHED RT MLG CYL RETRACT PIN BOSS BORE IAW AAR FAA-99-417 AND EWA MA AI-3210-01:03. (CORROSION D - [SDR RRXA991645](https://openairdocs.org/sdr/RRXA991645.md): Retract Pin · corroded · Aug 29, 1999 · N8087U · Doug DC871F · Landing Gear Retraction/Extension System > DURING A MAINTENANCE VISIT FOUND CORROSION, LT MLG, RETRACT PIN BOSS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REBUSHED LT LMG RETRACT PIN BOSS BORE IAW AAR FAA 99-417 AND EWA MA AI-3210-01:03. - [SDR RRXA991473](https://openairdocs.org/sdr/RRXA991473.md): Retract Pin · corroded · Aug 29, 1999 · N8087U · Doug DC871F · Landing Gear Retraction/Extension System > DURING A MAINTENANCE VISIT FOUND CORROSION, LT MLG RETRACT PIN BOSS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REBUSHED LT MLG RETRACT PIN BOSS BORE IAW AAR FAA APPROVED DER ENGINEERING SKETCH NR 99-417 AND EMER - [SDR RRXA991472](https://openairdocs.org/sdr/RRXA991472.md): Retract Pin · corroded · Aug 29, 1999 · N8087U · Doug DC871F · Landing Gear Retraction/Extension System > DURING A MAINTENANCE VISIT FOUND CORROSION, MAIN LANDING GEAR, RIGHT MLG, RETRACT PIN BOSS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REBUSHED RIGHT MLG CYL RETRACT PIN BOSS BORE IAW ARR FAA APPROVED DER ENGINE - [SDR RRXA991625](https://openairdocs.org/sdr/RRXA991625.md): Skin · corroded · Aug 28, 1999 · N8087U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT, LE, UPPER SKIN BETWEEN XFS 341.50 AND XOLDI 6.225. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SKIN IAW FAA SKETCH NR 087-252. (CO - [SDR RRXA991465](https://openairdocs.org/sdr/RRXA991465.md): Skin · corrosion · Aug 28, 1999 · N8087U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, L/E UPPER SKIN BETWEEN STA XFS 341.50 VOID AND STA XFS 6.225. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SKIN IAW FAA APPROVED DER - [SDR RRXA991626](https://openairdocs.org/sdr/RRXA991626.md): Skin · corroded · Aug 25, 1999 · N8087U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT, OB, SLOT VANE, INNER DOUBLER AT XOLDI 6.225. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DAC DWG 5769933-21 AND DC8 SRM - [SDR RRXA991520](https://openairdocs.org/sdr/RRXA991520.md): Skin · corroded · Aug 25, 1999 · N8087U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION, LT O/B SLOT VANE INNER DOUBLER HAS HEAVY CORROSION AT STA XOLDI 6.225. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DAC DWG NR 576993 - [SDR RRXA991437](https://openairdocs.org/sdr/RRXA991437.md): Longeron · corroded · Aug 25, 1999 · N8087U · Doug DC871F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 31 LEFT BETWEEN STA Y660 AND STA Y680, UPPER FLANGE.. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED LONGERON SECTION IAW FAA APPROVED DER ENGIN - [SDR RRXA991634](https://openairdocs.org/sdr/RRXA991634.md): Frame · corroded · Aug 24, 1999 · N8087U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, AT STA 1120, BETWEEN LONGERONS 36 AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED FRAME IAW DC8 SRM - [SDR RRXA991440](https://openairdocs.org/sdr/RRXA991440.md): Skin · corroded · Aug 24, 1999 · N8087U · Doug DC871F · Trailing Edge Flaps > DURING A MAINTENANCE VISIT FOUND CORROSION, WING, RT INBD FLAP UPPER SKIN BETWEEN STA XW0 TO STA XW5, AT 5 TO 6 INCHES FWD OF THE T/E. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SKIN IAW - [SDR RRXA991432](https://openairdocs.org/sdr/RRXA991432.md): Frame · corroded · Aug 24, 1999 · N8087U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME AT FSY 1120, BETWEEN LONGERONS 36 AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED FRAME IAW DC8 SRM 53-2-0 FIG 2. (CORROSION - [SDR RRXA991627](https://openairdocs.org/sdr/RRXA991627.md): Skin · corrosion · Aug 22, 1999 · N8087U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT, AND BULGED SKIN AT FRONT SPAR, STA XS 250.089. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 57-2-0 FIG 2A. (CORRO - [SDR RRXA991516](https://openairdocs.org/sdr/RRXA991516.md): Skin · corroded · Aug 22, 1999 · N8087U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION, LT WING, L/E HAS BULGED SKIN AT FRONT SPAR AT STA XS 250.089. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 57-2-0, FIG 2A. ( - [SDR RRXA991467](https://openairdocs.org/sdr/RRXA991467.md): Skin · corroded · Aug 22, 1999 · N8087U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION, LT WING L/E HAS BULGED SKIN AT FRONT SPAR AT STA XS 250.089. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 57-2-0, FIG 2A. (CO - [SDR RRXA991662](https://openairdocs.org/sdr/RRXA991662.md): Rib · cracked · Aug 21, 1999 · N8087U · Doug DC871F · Wing, Rib/Bulkhead > DURING A MAINTENANCE VISIT FOUND CRACK, WING, LT CENTER L/E UPPER RIB CRACKED AT FASTENER END AT STA XFS 347.75, 354, AND 372.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC - [SDR RRXA991463](https://openairdocs.org/sdr/RRXA991463.md): Rib · cracked · Aug 21, 1999 · N8087U · Doug DC871F · Wing, Rib/Bulkhead > DURING A MAINTENANCE VISIT FOUND CRACK, LT CENTER L/E UPPER RIB AT FASTENER END, AT STA XFS 347.75, XFS 354, AND XFS 372.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR LT, L/E RIB - [SDR RRXA991661](https://openairdocs.org/sdr/RRXA991661.md): Skin · cracked · Aug 20, 1999 · N8087U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E UPPER SKIN AT STA XFS 423.25, CRACKED AT 2 RIVET HOLES, ALSO HAS 12 RIVET HEAT CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED R - [SDR RRXA991628](https://openairdocs.org/sdr/RRXA991628.md): Frame · corroded · Aug 20, 1999 · N8087U · Doug DC871F · Wing Spar > DURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT, LE, AUX TANK UPPER AFT MOUNTING CHORD BETWEEN STA XFS 7.50 AND XFS 20.0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED THE CHORD IAW D - [SDR RRXA991462](https://openairdocs.org/sdr/RRXA991462.md): Skin · cracked · Aug 20, 1999 · N8087U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E UPPER SKIN AT STA XFS 423.25 AT 2 RIVET HOLES, ALSO HAS 12 RIVET HEAT CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FA - [SDR RRXA991439](https://openairdocs.org/sdr/RRXA991439.md): Frame · corroded · Aug 20, 1999 · N8087U · Doug DC871F · Wing Spar > DURING A MAINTENANCE VISIT FOUND CORROSION, LT WING, L/E AUX TANK UPPER AFT MOUNTING CHORD BETWEEN STA XFS 7.50 AND XFS 20.0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED THE CHORD IAW DC8 - [SDR RRXA991436](https://openairdocs.org/sdr/RRXA991436.md): Web · corroded · Aug 20, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, NLG UPPER PRESSURE PANEL JUST AFT OF AIR CONDITIONING UNIT BETWEEN STA -32 AND STA -12, AND BETWEEN BL 5 RIGHT AND BL 10 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 S - [SDR RRXA991637](https://openairdocs.org/sdr/RRXA991637.md): Web · corroded · Aug 19, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, WEB, BETWEEN STA 920 AND STA 940, AT LONGERON 22 RIGHT AND RIGHT BL 60. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR WEB IAW FAA - [SDR RRXA991633](https://openairdocs.org/sdr/RRXA991633.md): Floorbeam · corroded · Aug 19, 1999 · N8087U · Doug DC871F · Fuselage Main, Floor Beam > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR SUPPORT AT STA 600, BETWEEN LONGERON 33 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOOR SUPPORT IAW DAC - [SDR RRXA991438](https://openairdocs.org/sdr/RRXA991438.md): Web · corroded · Aug 19, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, WEB, BETWEEN STA Y920 AND SAT Y940, AT LONGERON 22 RIGHT, BL 60 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED WEB IAW FAA APPROVED DER ENGI - [SDR RRXA991431](https://openairdocs.org/sdr/RRXA991431.md): Support · corroded · Aug 19, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, FLOOR SUPPORT, AT LOCATION Y600, BETWEEN LONGERONS 33 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOOR SUPPO - [SDR RRXA991666](https://openairdocs.org/sdr/RRXA991666.md): Fitting · cracked · Aug 17, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CRACK, FLOORBEAM SUPPORT STRUT LOWER FITTING CRACKED AT AFT SIDE OF TEE AT STA 1160, TOP OF LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED - [SDR RRXA991665](https://openairdocs.org/sdr/RRXA991665.md): Fitting · cracked · Aug 17, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CRACK, LONGERON SPLICE FITTING CRACKED AT LONGERON 31 LEFT, AT STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW MFG DWG 4753059 AND DC - [SDR RRXA991654](https://openairdocs.org/sdr/RRXA991654.md): Intercostal · cracked · Aug 17, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CRACK, INTERCOSTAL BETWEEN STA 580 AND STA 600 AT LONGERON 33 LEFT, 2 CRACKS FWD OF STA 600. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED INTERCOSTAL IAW MF - [SDR RRXA991632](https://openairdocs.org/sdr/RRXA991632.md): Skin · corroded · Aug 17, 1999 · N8087U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, INTERNAL DOUBLER AND INNER SUFRACE OF OUTER SKIN BETWEEN LONGERONS 31 LEFT AND LONGERON 31 RIGHT AND BETWEEN STA 350 AND STA 370. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC- - [SDR RRXA991631](https://openairdocs.org/sdr/RRXA991631.md): Finger Doubler · corroded · Aug 17, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FINGER DOUBLER AT LONGERON 31 RIGHT, AT STA 100. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLER IAW DAC DWG 5779917 AND DC - [SDR RRXA991519](https://openairdocs.org/sdr/RRXA991519.md): Fitting · cracked · Aug 17, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CRACK, FLOOR BEAM SUPPORT STRUT LOWER FITTING, CRACKED AT AFT SIDE OF TEE, AT STA 1160, TOP OF LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALL - [SDR RRXA991517](https://openairdocs.org/sdr/RRXA991517.md): Fitting · cracked · Aug 17, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CRACK, LONGERON SPLICE FITTING CRACKED AT LONGERON 31 LEFT, STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC DWG NR 470359 AND DC8 - [SDR RRXA991455](https://openairdocs.org/sdr/RRXA991455.md): Intercostal · cracked · Aug 17, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CRACK, INTERCOSTAL BETWEEN STA FS 580 AND FS 600 AT LONGERON 33 LEFT, FWD OF STA FS 600. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED INTERCOSTAL PER DAC DW - [SDR RRXA991434](https://openairdocs.org/sdr/RRXA991434.md): Skin · corroded · Aug 17, 1999 · N8087U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, INTERNAL DOUBLER AND INNER SURFACE OF OUTER SKIN, BETWEEN LONGERONS 31 LEFT AND LONGERON 31 RIGHT, AND BETWEEN STATIONS Y350 AND STA Y370. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED ARE - [SDR RRXA991433](https://openairdocs.org/sdr/RRXA991433.md): Finger Doubler · corroded · Aug 17, 1999 · N8087U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FINGER DOUBLER, AT STA Y100, LONGERON 31 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLER IAW DAC DWG NR 5779917 AND - [SDR RRXA991664](https://openairdocs.org/sdr/RRXA991664.md): Rib · cracked · Aug 16, 1999 · N8087U · Doug DC871F · Wing, Rib/Bulkhead > DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB AT STA XFS 163.75, CRACKED AT THE AFT LWR END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-0 FIG - [SDR RRXA991657](https://openairdocs.org/sdr/RRXA991657.md): Angle · cracked · Aug 16, 1999 · N8087U · Doug DC871F · Wing Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E AT STA XW 0.00, THE UPPER AFT L/E ATTACH ANGLE CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE IAW MFG DWG 5613646 AND DC - [SDR RRXA991656](https://openairdocs.org/sdr/RRXA991656.md): Skin · cracked · Aug 16, 1999 · N8087U · Doug DC871F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E LWR SKIN INTERNAL TRIPLER AT STA XFS 430 AT THE SPAR, CRACKED IN TWO. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. F8 REPAIR IAW MFG DWG 5769891 AND DC8 SRM 5 Next page: https://openairdocs.org/deregistered/N8087U-2008-02-13/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 = 'N8087U' AND deregistration_id = 'N8087U-2008-02-13' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N8087U-2008-02-13/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.