# Service difficulty reports: N8177U, cancelled May 16, 2006 A list on [N8177U, cancelled May 16, 2006](https://openairdocs.org/deregistered/N8177U-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 2 · 95 reports - [SDR RRXA010010](https://openairdocs.org/sdr/RRXA010010.md): Servo · malfunctioned · Feb 12, 2001 · N8177U · Doug DC871F · Autopilot Main Servo > AUTOPILOT PORPOISING IN VERTICAL SPEED AND PITCH DUMP MODES (ROUGH PORPOISING). PROBLEM DUPLICATED, REPLACED A/P ELEVATOR SERVO IAW DC-8 M/M 22-12-02 AND A/P PITCH CHANNEL COMPUTER IAW DC-8 M/M 22-10-39, SYS OPS CHECK GOOD. - [SDR RRXA000447](https://openairdocs.org/sdr/RRXA000447.md): Fitting · corroded · May 1, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO Z FITTING AT STA 1160 AND LONGERON 36L - 35L. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED Z FITTING IAW DC8 SRM 53-1-2 FIG 1. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION DAMAGE RECORDED - [SDR RRXA000415](https://openairdocs.org/sdr/RRXA000415.md): Fitting · corroded · May 1, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FWD CARGO DOOR FRAME FITTING AND FASTENER AT STA 315 AND STR 32L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED CORRODED FITTING IAW DC8 SRM 53-1-02 AND MM 20-16-0 FIG 1. TREATED AREA IAW - [SDR RRXA000412](https://openairdocs.org/sdr/RRXA000412.md): Frame · corroded · May 1, 2000 · N8177U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FWD CARGO FRAME AT STA 120 AND STR 30R AND 27R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED DAMAGED FRAME, TREATED AREA IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 53-2-0 FIG 1. CORROSION - [SDR RRXA000411](https://openairdocs.org/sdr/RRXA000411.md): Frame · corroded · May 1, 2000 · N8177U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME, FWD CARGO AT STA 100 AND STR 35L - 35R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, RECEIVED PART AND INSTALLED IAW DC8 SRM 53-1-2. CORROSION DAMAGE RE - [SDR RRXA000397](https://openairdocs.org/sdr/RRXA000397.md): Frame · corroded · May 1, 2000 · N8177U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MID CARGO AT STA 607 AND STR 34L AND 35R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE DOUBLER, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATE PART AND INSTALLED IAW DC8 SRM DC8 SRM 51-1-9 & SRM 5 - [SDR RRXA000441](https://openairdocs.org/sdr/RRXA000441.md): Fitting · corroded · Apr 27, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO ''Z'' FITTING AFT BAGGAGE AT STA 1220 AND LONGERON 36R - 35R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED FITTING IAW DC8 SRM 53-2-0 FIG 2D. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION - [SDR RRXA000433](https://openairdocs.org/sdr/RRXA000433.md): Cargo Track · corroded · Apr 27, 2000 · N8177U · Doug DC871F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO RT CARGO TIE DOWN AT STA 365 AND LONGERON 33R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED TRACK IAW DC8 SRM 51-1-24, 51-1-8, 51-3-2, 53-2-3 FIG 12. TREATED AREA IAW DC8 SRM 51-1-8. COR - [SDR RRXA000428](https://openairdocs.org/sdr/RRXA000428.md): Longeron · corroded · Apr 27, 2000 · N8177U · Doug DC871F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON AT STA 216 - 220 AND LONGERON STR 36, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED LONGERON IAW DC8 SRM 53-2-2 FIG 4A & 52-2-0 FIG 1F. TREATED AREA IAW DC8 SRM 51-1-8. CORROSIO - [SDR RRXA000426](https://openairdocs.org/sdr/RRXA000426.md): Skin · corroded · Apr 27, 2000 · N8177U · Doug DC871F · Cargo/Baggage Doors > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO INNER SKIN FWD, BELOW AND AFT OF NR 1 CARGO DOOR. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGED DOUBLER, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATE PART AND INSTALLED IAW DC8 SRM 51-1-20 & 53-2 - [SDR RRXA000424](https://openairdocs.org/sdr/RRXA000424.md): Fitting · corroded · Apr 27, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 420 AND LONGERON 33R - 34R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED FITTING IAW DC8 SRM 53-01-0, 53-2-0 FIG 2A, 53-02-0 FIG 1F. TREATED AREA IAW DC8 SRM 51-1-8. CORR - [SDR RRXA000414](https://openairdocs.org/sdr/RRXA000414.md): Fitting · corroded · Apr 27, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO DOOR FRAME FITTING FWD CARGO AT STA 320 AND STR 32R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED DOOR FRAME FITTING IAW DC8 SRM 53-2-0 FIG 1F, TREATED AREA IAW DC8 SRM 51-1-8. CORROSION - [SDR RRXA000410](https://openairdocs.org/sdr/RRXA000410.md): Cap · corroded · Apr 27, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FWD CARGO END CAP AT STA 60 AND STR 36, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGED END CAP, TREATED AREA IAW DC8 SRM 51-1-8, RECEIVED PART AND INSTALLED IAW DC8 SRM 53-01-0 AND 53-2-0 FIG 1F - [SDR RRXA000403](https://openairdocs.org/sdr/RRXA000403.md): Angle · corroded · Apr 27, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOOR SUPPORT ANGLE AT STA 25 - 55 AND LONGERON RBL 62, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGED SUPPORT ANGLE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATE PART AND INSTALLED IAW DC8 SRM 53- - [SDR RRXA000402](https://openairdocs.org/sdr/RRXA000402.md): Plate · corroded · Apr 27, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SUPPORT PLATE FOR TOILET DRAINS AT STA 35 & 50 AND LONGERON RBL 50, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGED SUPPORT PLATE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATE PART AND INSTALLED IA - [SDR RRXA000399](https://openairdocs.org/sdr/RRXA000399.md): Angle · corroded · Apr 27, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO CUSP ANGLE AT STA 25 - 55 AND LONGERON RBL 62, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATED PART AND INSTALLED IAW DC8 SRM 51-1-1, 51-1-8, 51-1-20D - [SDR RRXA000454](https://openairdocs.org/sdr/RRXA000454.md): Splice · corroded · Apr 26, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SPLICE AT STA 1050 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED SPLICE IAW DC8 SRM 53-2-0 AND 53-2-2 FIG 10. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION DAMAGE RECORDED I - [SDR RRXA000451](https://openairdocs.org/sdr/RRXA000451.md): Fitting · corroded · Apr 26, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO Z FITTING AT STA 1220 AND LONGERON 36R - 35R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED Z FITTING IAW DC8 SRM 53-2-0 FIG 2D. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION DAMAGE RECORDED - [SDR RRXA000449](https://openairdocs.org/sdr/RRXA000449.md): Longeron · corroded · Apr 26, 2000 · N8177U · Doug DC871F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON AT STA 1380 AND LONGERON 36L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATED PART AND INSTALLED IAW DC8 SRM 51-1-8 & 53-2-2 FIG 11. CORROSIO - [SDR RRXA000446](https://openairdocs.org/sdr/RRXA000446.md): Fitting · corroded · Apr 26, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO Z FITTING AFT BAGGAGE AT STA 1160 AND LONGERON 35R-34R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED Z FITTING IAW DC8 SRM 53-2-0 FIG 2D. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION DAMAG - [SDR RRXA000443](https://openairdocs.org/sdr/RRXA000443.md): Fitting · corroded · Apr 26, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO Z FITTING AFT BAGGAGE AT STA 1200 AND LONGERON 36L-35L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED Z FITTING IAW DC8 SRM 53-2-0 FIG 2D. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION DAMAG - [SDR RRXA000439](https://openairdocs.org/sdr/RRXA000439.md): Clip · corroded · Apr 26, 2000 · N8177U · Doug DC871F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO AFT CARGO SKIN CLIP AT STA 1240 AND LONGERON 34L TO 33R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATED PART AND INSTALLED IAW DC8 SRM 53-4-0 FIG 7 & - [SDR RRXA000438](https://openairdocs.org/sdr/RRXA000438.md): Clip · corroded · Apr 26, 2000 · N8177U · Doug DC871F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO AFT CARGO SKIN CLIP AT STA 1260 AND LONGERON 36L - 35L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATED PART AND INSTALLED IAW DC8 SRM 51-1-4 AND 51-1- - [SDR RRXA000434](https://openairdocs.org/sdr/RRXA000434.md): Pressure Panel · corroded · Apr 26, 2000 · N8177U · Doug DC871F · Fuselage Main, Bulkhead > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CABIN SHEAR WEB AND PRESSURE PANEL AT STA 848 AND LONGERON LEFT BL 44, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, REPLACED DOUBLER AND ANGLES IAW DC8 SRM - [SDR RRXA000420](https://openairdocs.org/sdr/RRXA000420.md): Stiffener · corroded · Apr 26, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO PRESSURE PANEL STIFFENER AT STA 960 - 980. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATE PART AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-2 AND 53-2-0 FIG - [SDR RRXA000452](https://openairdocs.org/sdr/RRXA000452.md): Bracket · corroded · Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO Z BRACKET AT STA 1220 AND LONGERON 36L-35L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED Z BRACKET IAW DC8 SRM 53-2-0 FIG 2D. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION DAMAGE RECORDED - [SDR RRXA000448](https://openairdocs.org/sdr/RRXA000448.md): Clip · corroded · Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SKIN CLIP AT STA 1260 AND LONGERON 36R - 35R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATE PART AND INSTALLED IAW DC8 SRM 51-1-4 & 51-1-8 FIG 7 & 8. - [SDR RRXA000442](https://openairdocs.org/sdr/RRXA000442.md): Fitting · corroded · Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO Z FITTING AT STA 1180 AND LONGERON 36L - 35L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED Z FITTING IAW DC8 SRM 51-1-24, 51-1-8 AND 53-2-0 FIG 2D. TREATED AREA IAW DC8 SRM 51-1-8. CORRO - [SDR RRXA000440](https://openairdocs.org/sdr/RRXA000440.md): Structure · corroded · Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO AFT CARGO RIB AT STA 1400 AND LONGERON 35L TO 35R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATE PART AND INSTALLED IAW DC8 SRM 53-04-1 AND 51-1-4 FIG - [SDR RRXA000429](https://openairdocs.org/sdr/RRXA000429.md): Longeron · corroded · Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON AT STA 343 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED LONGERON IAW DC8 SRM 53-2-0 FIG 1F. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION DAMAGE RECORDED IN EWA C - [SDR RRXA000427](https://openairdocs.org/sdr/RRXA000427.md): Finger Doubler · corroded · Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FINGER DOUBLER AT STA 190 - 220 AND 240 - 450 AND LONGERON 31L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATE PART AND INSTALLED IAW DC8 SRM 51-1-20 - [SDR RRXA000425](https://openairdocs.org/sdr/RRXA000425.md): Finger Doubler · corroded · Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FINGER DOUBLER AT SKIN SPLICE AT STA 190 AND LONGERON 30R TO 31R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED DOUBLER IAW DC8 SRM 53-4-0 AND 51-1-21. TREATED AREA IAW DC8 SRM 51-1-8. CO - [SDR RRXA000423](https://openairdocs.org/sdr/RRXA000423.md): Strap · corroded · Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO TIE STRAP AND FITTINGS AT STA 190 - 224 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-2, 53-2-2 FIG 4C, 51-1-20 FIG 2D, AND 53-2-0 FIG 1F. TREATED - [SDR RRXA000419](https://openairdocs.org/sdr/RRXA000419.md): Finger Doubler · corroded · Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FINGER DOUBLER AT STA 190 - 220, 240 - 450 AND LONGERON 31L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED DOUBLER IAW DC8 SRM 51-1-20 AND 53-2-1 FIG 7 & 8. TREATED AREA IAW DC8 SRM 51-1-8 - [SDR RRXA000417](https://openairdocs.org/sdr/RRXA000417.md): Fitting · corroded · Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, Attach Fittings > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME FITTING AT STA 260 AND STR 35L AND 36L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED FITTING IAW DC8 SRM 53-2-0 FIG 2D, TREATED AREA IAW DC8 SRM 51-1-8. CORROSION DAMAGE RECORDED IN - [SDR RRXA000413](https://openairdocs.org/sdr/RRXA000413.md): Finger Doubler · corroded · Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FINGER DOUBLER AT SKIN SPLICE FWD CARGO COMP AT STA 180 - 220 AND STR 31R TO 27R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED DOUBLER AND SPLICE IAW SRM 51-1-0, 51-1-21 AND 53-2-1 FIG 7 & - [SDR RRXA000400](https://openairdocs.org/sdr/RRXA000400.md): Splice · corroded · Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SKIN SPLICE AT STA 1340 & 1360 AND LONGERON 35L & 35R, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATED PART AND INSTALLED IAW DC8 SRM 53-2-2 AND 53-2-1 - [SDR RRXA000396](https://openairdocs.org/sdr/RRXA000396.md): Finger Doubler · corroded · Apr 25, 2000 · N8177U · Doug DC871F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FINGER DOUBLER IN SKIN SPLICE AT STA 1500 - 1520 AND LONGERON 27L TO 31L, DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REPLACED DOUBLER IAW DC8 SRM 53-2-0 AND 53-04-1 FIG 7 & 8. CORROSION DAMAGE RECORDED IN E - [SDR RRXA000453](https://openairdocs.org/sdr/RRXA000453.md): Skin · corroded · Apr 20, 2000 · N8177U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO AFT CARGO COMP SKIN AT STA 1050 TO 1130 AND LONGERON 36. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED SKIN IAW DC8 SRM 53-4-0, 51-1-2 AND EAPD 01-53-029. TREATED AREA IAW DC8 SRM 51-1-8. - [SDR RRXA000405](https://openairdocs.org/sdr/RRXA000405.md): Frame · corroded · Apr 20, 2000 · N8177U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO TOP OF FRAME AT STA 1140 AND LONGERON 35L - 32R. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGED FRAME, TREATED AREA IAW DC8 SRM 51-1-8, AND INSTALLED IAW DC8 SRM 53-4-0, 51-1-21 FIG PD08-53-036. - [SDR RRXA000432](https://openairdocs.org/sdr/RRXA000432.md): Door Frame · corroded · Mar 6, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO R1 SERVICE DOOR LOWER FRAME SILL AT STA 55.000 AND LONGERON. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATED PART AND INSTALLED IAW DC8 SRM 51-1-21, 51 - [SDR RRXA000395](https://openairdocs.org/sdr/RRXA000395.md): Skin · corroded · Feb 19, 2000 · N8177U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO AIRCRAFT BELLY SKIN AT STA 190 TO STA 450. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. - [SDR RRXA000394](https://openairdocs.org/sdr/RRXA000394.md): Skin · corroded · Feb 19, 2000 · N8177U · Doug DC871F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INNER SKIN FWD, BELOW AND AFT OF NR 1 CARGO DOOR AT STA 220 - 400 AND STR 35L TO 31R. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. - [SDR RRXA000435](https://openairdocs.org/sdr/RRXA000435.md): Fitting · corroded · Feb 8, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO Z FITTING AFT BAGGAGE AT STA 1120 - 1150 AND STR 36 AND 35L - 35R. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED 2 Z-FITTINGS IAW DC8 SRM 53-2-0. TREATED AREA IAW DC8 SRM 51-1-8. CORROSIO - [SDR RRXA000457](https://openairdocs.org/sdr/RRXA000457.md): Floor Support · corroded · Feb 7, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR SUPPORT AT STA 1120 - 1140. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED FLOOR SUPPORT IAW DC8 SRM 53-2-0 FIG 1F. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION DAMAGE RECORDED IN EWA - [SDR RRXA000456](https://openairdocs.org/sdr/RRXA000456.md): Intercostal · corroded · Feb 6, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERCOSTAL AT STA 1100 - 1120 AND LONGERON 35L. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED INTERCOSTAL IAW DC8 SRM 53-4-0 AND 51-1-8 FIG 1. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION D - [SDR RRXA000455](https://openairdocs.org/sdr/RRXA000455.md): Fitting · cracked · Feb 6, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FRAME FITTING AT STA 1140 AND LONGERON 35R. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED AFT CARGO BAY FRAME FITTING IAW DC8 SRM 51-1-24, 51-1-8, 53-2-0 FIG 1F. TREATED AREA IAW DC8 SRM 51-1- - [SDR RRXA000431](https://openairdocs.org/sdr/RRXA000431.md): Fitting · corroded · Jan 19, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SHEAR TIE FITTING FWD BAGGAGE AT STA 420 AND LONGERON 35L - 36L. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGED FITTING, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATED PART AND INSTALLED IAW DC8 SRM - [SDR RRXA000430](https://openairdocs.org/sdr/RRXA000430.md): Fitting · corroded · Jan 19, 2000 · N8177U · Doug DC871F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FWD BAGGAGE AT STA 340 AND LONGERON 32, 33, & 34. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED AND REPLACED FITTINGS IAW DC8 SRM 53-2-0 AND 53-1-02 FIG 1F. TREATED AREA IAW DC8 SRM 51-1-8. CORROSION - [SDR RRXA000450](https://openairdocs.org/sdr/RRXA000450.md): Frame · corroded · Jan 18, 2000 · N8177U · Doug DC871F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO AFT CARGO COMP RIB AT STA 1120 AND LONGERON 34L - 32R. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8, FABRICATED PART AND INSTALLED IAW DC8 SRM 53-20 AND EAPD08-5 Next page: https://openairdocs.org/deregistered/N8177U-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 = 'N8177U' AND deregistration_id = 'N8177U-2006-05-16' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N8177U-2006-05-16/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.