# Service difficulty reports: N831AL, cancelled Oct 16, 2007 A list on [N831AL, cancelled Oct 16, 2007](https://openairdocs.org/deregistered/N831AL-2007-10-16.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 6 · 298 reports - [SDR RRXA010056](https://openairdocs.org/sdr/RRXA010056.md): Pad · failed · Jun 27, 2001 · N831AL · Doug DC873F · Landing Gear Brake System > ON DEPARTURE GEAR HANDLE UP NOSE GEAR HAD EXTREME NO ISE AS IF NOSE WHEELS WERE SPINNING AND RUBBING. ALSO HAD EXTREME VIBRATION, GEAR HANDLE PUT BACK DOWN, VIBRATION CONTINUED WITH GEAR DOWN, WHEN ACFT BANKED IN FLT NOSE GEAR HAD LOUD BANG. BOTH GEAR UP INDI - [SDR RRXA010019](https://openairdocs.org/sdr/RRXA010019.md): Inu · failed · Mar 13, 2001 · N831AL · Doug DC873F · Inertial Guidance System > NR 1 INS FAILED WENT ATT MODE. TRANSFERRED TO DMI LIST AS CONTROL D-9272201-1175 CAT: D MEL 3420 ATA 3410 DUE DATE 11JUL01 PLACARD INSTALLED. REMOVED AND REPLACED NR 1 INU PERFORMED OPERATIONAL CHECK IAW SUPPLEMENTAL MANUAL CHECK GOOD. THIS CLEARS DMI D9 - [SDR RRXA010018](https://openairdocs.org/sdr/RRXA010018.md): Tire · blown · Mar 11, 2001 · N831AL · Doug DC873F · Tire > ON LANDING, TOWER REPORTED SMOKE OF RIGHT MLG NR 8 TIRE BLEW, NR 3 TIRE DAMAGED UPON LANDING. NO SECONDARY CAUTION LIGHT OR ANTI SKID LIGHT ILLUMINATED. TRANSFERRED TO DMI LIST AS CONTROL C-9272181-1171 CAT: C MEL 3101 ATA 3245 DUE DATE 23MAR01 PLACARD INSTA - [SDR RRXA001043](https://openairdocs.org/sdr/RRXA001043.md): Bracket · broken · Aug 11, 2000 · N831AL · Doug DC873F · Engine Oil Storage (Airframe Furnished) > AT FL 370 CRUISE PWR NR 4 OIL PSI DECREASE TO APPROX 20 PSI NR 4 OIL TEMP 150 DEGREE NR 4 OIL QTY NORMAL. PRECAUTIONARY SHUT DOWN NR 4 (0213Z). REMOVED AND REPLACED OIL PROBES XMITTER IAW CH 79-32-1. REMOVED AND REPLACED OIL TEMP SENOR IAW CH 79-54-1. MOT - [SDR RRXA001009](https://openairdocs.org/sdr/RRXA001009.md): A/C Pack · malfunctioned · Jul 4, 2000 · N831AL · Doug DC873F · Cabin Pressure Control System > AIRCRAFT WILL NOT PRESSURIZE. RIGHT PACK INOPERATIVE. PRESSURIZED AIRCRAFT TO 8.8 TO 9 PSID-NO LEAKS NOTED 21-10-00-RT PACK OPERATIONAL CK''S GOOD ON GROUND AT THIS TIME. - [SDR RRXA001000](https://openairdocs.org/sdr/RRXA001000.md): Pump · leaking · Jun 17, 2000 · N831AL · Doug DC873F · Hydraulic System, Auxiliary > LOST ALL HYDRAULIC QUANTITY TO STAND PIPE. FOUND LEAK AT STBY RUDDER HYD PUMP. REMOVED AND REPLACED PUMP PER MM 27-42, NO LEAKS NOTED. - [SDR RRXA000262](https://openairdocs.org/sdr/RRXA000262.md): Transducer · inoperative · Apr 18, 2000 · N831AL · Doug DC873F · Brake Anti-Skid Section > ON LANDING ANTI-SKID FAILED. FOUND RFO TRANSDUCER TO BE INOP. REMOVED AND REPLACED RFO TRANSDUCER IAW DC-8 MM CH 32-43. PERFORMED SPIN UP ANTI-SKID, OPS CHECKS GOOD, NO DEFECTS NOTED. - [SDR RRXA000618](https://openairdocs.org/sdr/RRXA000618.md): Longeron · corroded · Apr 10, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LONGERON AT STA 665 AND LONGERON 31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED AND INSTALLED IAW DEE HOWARD AIRCRAFT MAINTENANCE SK 837-451. - [SDR RRXA000617](https://openairdocs.org/sdr/RRXA000617.md): Skin · corroded · Apr 10, 2000 · N831AL · Doug DC873F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO RT CENTER L/E LOWER SKIN AROUND O/B FUEL CAP AND EVIDENCE OF CRACK 8-18 INCHES FWD OF FRONT SPAR AT STA 385 TO 391.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51- - [SDR RRXA000685](https://openairdocs.org/sdr/RRXA000685.md): Door Frame · cracked · Apr 5, 2000 · N831AL · Doug DC873F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO DOOR 62 DOOR JAMB L/H FWD CORNER AND R/H CENTER AREA, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIRED PART AND INSTALLED IAW DC-8 SRM 53-2-0. - [SDR RRXA000611](https://openairdocs.org/sdr/RRXA000611.md): Cargo Track · corroded · Apr 3, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT, FOUND CORROSION TO THE LT AFT CARGO TRACK AT STA 1020 TO 1120, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 51-3-0 AND 53-2-3 FIG 6N. (CORROSION - [SDR RRXA000718](https://openairdocs.org/sdr/RRXA000718.md): Fitting · damaged · Mar 31, 2000 · N831AL · Doug DC873F · Trailing Edge Flaps > DURING A MAINTENANCE VISIT FOUND THE ALIGNMENT OUT OF TOLERANCE AT THE RT FLAP FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW FLAP SUPPORT FITTING IAW DC-8 SRM 27-51-12 AND DSK - [SDR RRXA000609](https://openairdocs.org/sdr/RRXA000609.md): Skin · corroded · Mar 31, 2000 · N831AL · Doug DC873F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE SKIN AT STA 1648 TO 1653 AND LONGERON 22R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED PART AND INSTALLED IAW DC-8 SRM 53-2-0 FIG 16. (CORROS - [SDR RRXA003392](https://openairdocs.org/sdr/RRXA003392.md): Seat Track · corroded · Mar 30, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT AFT CARGO TRACK AT FS 1020 TO 1120, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-3-0 AND DWG 5754223. - [SDR RRXA000716](https://openairdocs.org/sdr/RRXA000716.md): Fitting · cracked · Mar 29, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO A CABIN SPLICE FITTING AT STA'S 300 TO 320 AND LONGERON 6L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 51-1-20D AND DAC DWG #47 - [SDR RRXA000607](https://openairdocs.org/sdr/RRXA000607.md): Longeron · corroded · Mar 26, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LONGERON AT STA 155 AND ''X'' LONGERON 35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 51-1-20D, 5-1-21 AND 53-2- - [SDR RRXA003405](https://openairdocs.org/sdr/RRXA003405.md): Floorboard · corroded · Mar 23, 2000 · N831AL · Doug DC873F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR BOARD AT STA'S 55 TO 100 AND X60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-7-3 AND DWG 5759394. - [SDR RRXA000604](https://openairdocs.org/sdr/RRXA000604.md): Longeron · corroded · Mar 21, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/Stringer > DURING A MAINTENACE VISIT, FOUND CORROSION DAMAGE TO LONGERON 34R AT STA 190 TO 310, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 51-1-20D AND DAC DWG NR 9754913. (CORROSIO - [SDR RRXA000603](https://openairdocs.org/sdr/RRXA000603.md): Longeron · corroded · Mar 21, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LONGERON AT 35R BETWEEN STA 190 TO 310, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 51-1-20D AND DAC DWG 9754913. - [SDR RRXA000715](https://openairdocs.org/sdr/RRXA000715.md): Skin · damaged · Mar 16, 2000 · N831AL · Doug DC873F · Cargo/Baggage Doors > DURING A MAINTENANCE VISIT FOUND 3 TEMPERARY REPAIRS AT THE C-PIT DOOR FLOOR COVER HINGED SECTION SKIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPLACEMENT SKIN IAW DC-8 SRM 51-1-2 - [SDR RRXA000714](https://openairdocs.org/sdr/RRXA000714.md): Frame · cracked · Mar 16, 2000 · N831AL · Doug DC873F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND A CRACK TO C-PIT DOOR FLOOR COVER HINGED SECTION FRAME, EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED FRAME, REINSTALLED NEW FRAME IAW DC-8 SRM 51-1-21. - [SDR RRXA000598](https://openairdocs.org/sdr/RRXA000598.md): Keelbeam · corroded · Mar 16, 2000 · N831AL · Doug DC873F · Fuselage Main, Keel > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO KEEL BEAM AT STA 660 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED PER DEE HOWARD AIRCRAFT MAINTENANCE SK 831-363. (CORROSION DAMA - [SDR RRXA000597](https://openairdocs.org/sdr/RRXA000597.md): Frame · corroded · Mar 16, 2000 · N831AL · Doug DC873F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO AFT FUSE FRAME AT STA 1793 AND LONGERON 30L AND 30R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RE-INSTALLED FASTENERS AND BRACKETS IAW DC-8 SRM - [SDR RRXA000712](https://openairdocs.org/sdr/RRXA000712.md): Web · cracked · Mar 15, 2000 · N831AL · Doug DC873F · Fuselage Main, Structure > DURING A MAINTENANCE VISIT FOUND A CRACK ON THE WEB AT STA 1160 LONGERON 33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED DOUBLER AND FILLER IAW - [SDR RRXA000600](https://openairdocs.org/sdr/RRXA000600.md): Attach Fitting · corroded · Mar 15, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO BATH TUB FITTING AT STA 1220 BETWEEN LONGERONS 33R AND 34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED FITTING IAW DC-8 SRM 53-2-0 FIG 2G AND DAC - [SDR RRXA000599](https://openairdocs.org/sdr/RRXA000599.md): Attach Fitting · corroded · Mar 15, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO BATH TUB FITTING AT STA 1220 BETWEEN LONGERONS 33R TO 32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED FITTING IAW DC-8 SRM 53-2-0 FIG 2D AND DAC D - [SDR RRXA000595](https://openairdocs.org/sdr/RRXA000595.md): Frame · corroded · Mar 15, 2000 · N831AL · Doug DC873F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE UNDER NUT PLATES AT STA 1000 AND LONGERON L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED, REPAIRED AND INSTALLED IAW DC-8 SRM 53-2-0 FIG 2 AND DAC - [SDR RRXA000592](https://openairdocs.org/sdr/RRXA000592.md): Skin · corroded · Mar 15, 2000 · N831AL · Doug DC873F · Fuselage Main, Plate/Skin > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LT UPPER WING SKIN AT STA 354 TO 366 STR 5 TO 8, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 57-2-1 FIG 29 AND SRM - [SDR RRXA000591](https://openairdocs.org/sdr/RRXA000591.md): Longeron · corroded · Mar 15, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO 21 WASHERS AND NUTS AT STA 680 TO 660 AND LONGERON 31 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. INSTALLED WASHERS AND NUTS IAW DC-8 SRM - [SDR RRXA000713](https://openairdocs.org/sdr/RRXA000713.md): Fitting · cracked · Mar 14, 2000 · N831AL · Doug DC873F · Fuselage Structure (General) > DURING A MAINTENANCE VISIT FOUND A CRACK ON THE ATTACH FITTING AT STA 1160 AND LONGERON 33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC-8 SRM 51-1-20D. - [SDR RRXA000593](https://openairdocs.org/sdr/RRXA000593.md): Attach Fitting · corroded · Mar 14, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach Fittings > DURING A MAINTENANCE VISIT, FOUND DAMAGE TO BULKHEAD FITTING ON O/B SIDE AT STA 8 AND LONGERON 33 LEFT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED FITTING AND INSTALLED IAW DC-8 SRM 51-1-20D AND DAC D - [SDR RRXA000590](https://openairdocs.org/sdr/RRXA000590.md): Angle · corroded · Mar 14, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SUB FLOOR SUPPORT ANGLE AT STA 80 TO 100 AND BL-R 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SUB FLOOR SUPPORT ANGLE IAW DC-8 - [SDR RRXA000589](https://openairdocs.org/sdr/RRXA000589.md): Web · corroded · Mar 14, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SUB FLOOR WEB AT STA 80 TO 100 AND LONGERON BL-R 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SUB FLOOR WEB IAW DC-8 SRM 51-1-20 - [SDR RRXA000711](https://openairdocs.org/sdr/RRXA000711.md): Fitting · cracked · Mar 13, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE C-PIT FWD JAMB FITTING AT STA 1150 AND LONGERON 32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC-8 SRM 53-1-0 AND 51-1-2 - [SDR RRXA000710](https://openairdocs.org/sdr/RRXA000710.md): Bracket · cracked · Mar 13, 2000 · N831AL · Doug DC873F · Air Conditioning Doors > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BRACKET ON THE A/C COMPARTMENT DOOR #12 DOOR SWITCH, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED BRACKET IAW - [SDR RRXA000709](https://openairdocs.org/sdr/RRXA000709.md): Splice · cracked · Mar 13, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK AT A SPLICE FITTING AT STA 390 AND LONGERON 31L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED OUT AND REINSTALLED FITTING. - [SDR RRXA000585](https://openairdocs.org/sdr/RRXA000585.md): Fitting · corroded · Mar 13, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO BATH TUB FITTING AT STA 1152 AND LONGERON L33 RIGHT TO L34 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED SPLICES AND FITTINGS AND INSTALLED - [SDR RRXA000584](https://openairdocs.org/sdr/RRXA000584.md): Floorboard · corroded · Mar 13, 2000 · N831AL · Doug DC873F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBOARD AT STA 1020 TO 1300 AND LONGERON BL-0 AND BL-R 10, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED HEAVY EXFOLIATION CORROSION, ALODINED, PRIMED AREA AND REPLACED IAW DC-8 SRM 51-1-8. (CORROS - [SDR RRXA000610](https://openairdocs.org/sdr/RRXA000610.md): Seat Track · corroded · Mar 12, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE MAIN DECK SEAT TRACK AT STA 680 TO 820 AND RBL 60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 53-2-3 FIG 8A. (CO - [SDR RRXA000706](https://openairdocs.org/sdr/RRXA000706.md): Plate · gouged · Mar 11, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A GOUGE AT THE FWD ENTRY DOOR LOWER FWD DOOR JAMB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED, PRIMED AND ALODINED AREA IAW DC-8 SRM 51-1-8. REBLENDED GOUGE AND FOUND TO BE WITHIN LIMITS IAW DC-8 SRM 53 - [SDR RRXA000705](https://openairdocs.org/sdr/RRXA000705.md): Web · cracked · Mar 10, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK ON LT TOP SIDE OF NOSE RADOME AREA CANTED WEB ABOVE GLIDESLOPE ANTENNA, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED DOUBLER AND FILLER. - [SDR RRXA000704](https://openairdocs.org/sdr/RRXA000704.md): Tip Cap · cracked · Mar 10, 2000 · N831AL · Doug DC873F · Wing, Control Surfaces > DURING A MAINTENANCE VISIT FOUND A BARE STATIC WICK AND A DOUBLER MISSING AT THE T/E AT STA XW 773, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED, FABRICATED AND INSTALLED DOUBLER AND REPLACED STATIC WIC - [SDR RXAA000588](https://openairdocs.org/sdr/RXAA000588.md): Seat Track · corroded · Mar 10, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CABIN SEAT TRACK BETWEEN STA 1260 TO 1370 AND LONGERON BL-R 60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED MAIN CABIN SEAT TR - [SDR RRXA000580](https://openairdocs.org/sdr/RRXA000580.md): Floorboard · corroded · Mar 10, 2000 · N831AL · Doug DC873F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CABIN FLOORBOARD AT STA 280 TO 415 AND LONGERON RBL 58 TO 63, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED MAIN CABIN FLOORBOARD AND INSTALLE - [SDR RRXA000579](https://openairdocs.org/sdr/RRXA000579.md): Floorboard · corroded · Mar 10, 2000 · N831AL · Doug DC873F · Fuselage Floor Panel > DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CABIN FLOORBOARD AT STA 200 AND LONGERON RBL 12, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED, REPAIRED DOUBLER AND FILLER AND INSTALLED IAW - [SDR RRXA003368](https://openairdocs.org/sdr/RRXA003368.md): Support · corroded · Mar 9, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE GILINGER SUPPORT BRACKET AT BOTTOM OF FLOOR FRAME AT STA 520-640 X-48 AND +48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8S RM. REMOVED DAMAGE, ALODINED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PA - [SDR RRXA000708](https://openairdocs.org/sdr/RRXA000708.md): Fitting · cracked · Mar 9, 2000 · N831AL · Doug DC873F · Wing Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK ON THE LT WING L/E INTERNALLY 28 1/2 INCHES FWD OF WING SPAR UPPER CORD AT XILD.7095, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTING IAW D - [SDR RRXA000702](https://openairdocs.org/sdr/RRXA000702.md): Angle · cracked · Mar 9, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE WEB ANGLE AT STA 357, AND XFS -60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE IAW DC-8 SRM 53-3-3 FIG 1, 51-1-8 AND 51 - [SDR RRXA000701](https://openairdocs.org/sdr/RRXA000701.md): Channel · cracked · Mar 9, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE SUPPORT CHANNEL IN 'B' PIT AT STA 620 AND LONGERON 27L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW DC-8 - [SDR RRXA000700](https://openairdocs.org/sdr/RRXA000700.md): Bracket · broken · Mar 9, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND A BROKEN BRACKET FOR WINE CLAMP AT STA 70 AND LONGERON 31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW BRACKET AND INSTALLED IAW DC-8 SRM 51-1-8. Next page: https://openairdocs.org/deregistered/N831AL-2007-10-16/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 = 'N831AL' AND deregistration_id = 'N831AL-2007-10-16' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N831AL-2007-10-16/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.