N831AL, cancelled Oct 16, 2007

Service difficulty reports · 298

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 = 'N831AL' AND deregistration_id = 'N831AL-2007-10-16'
  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 RRXA010056Pad · failedON 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 INDIJun 27, 2001 · N831AL · Doug DC873F · Landing Gear Brake SystemSDR RRXA010019Inu · failedNR 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 D9Mar 13, 2001 · N831AL · Doug DC873F · Inertial Guidance SystemSDR RRXA010018Tire · blownON 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 INSTAMar 11, 2001 · N831AL · Doug DC873F · TireSDR RRXA001043Bracket · brokenAT 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. MOTAug 11, 2000 · N831AL · Doug DC873F · Engine Oil Storage (Airframe Furnished)SDR RRXA001009A/C Pack · malfunctionedAIRCRAFT 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.Jul 4, 2000 · N831AL · Doug DC873F · Cabin Pressure Control SystemSDR RRXA001000Pump · leakingLOST ALL HYDRAULIC QUANTITY TO STAND PIPE. FOUND LEAK AT STBY RUDDER HYD PUMP. REMOVED AND REPLACED PUMP PER MM 27-42, NO LEAKS NOTED.Jun 17, 2000 · N831AL · Doug DC873F · Hydraulic System, AuxiliarySDR RRXA000262Transducer · inoperativeON 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.Apr 18, 2000 · N831AL · Doug DC873F · Brake Anti-Skid SectionSDR RRXA000618Longeron · corrodedDURING 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.Apr 10, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000617Skin · corrodedDURING 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-Apr 10, 2000 · N831AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA000685Door Frame · crackedDURING 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.Apr 5, 2000 · N831AL · Doug DC873F · Fuselage Main, StructureSDR RRXA000611Cargo Track · corrodedDURING 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. (CORROSIONApr 3, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000718Fitting · damagedDURING 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 DSKMar 31, 2000 · N831AL · Doug DC873F · Trailing Edge FlapsSDR RRXA000609Skin · corrodedDURING 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. (CORROSMar 31, 2000 · N831AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003392Seat Track · corrodedDURING 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.Mar 30, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000716Fitting · crackedDURING 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 #47Mar 29, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000607Longeron · corrodedDURING 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-Mar 26, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA003405Floorboard · corrodedDURING 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.Mar 23, 2000 · N831AL · Doug DC873F · Fuselage Floor PanelSDR RRXA000604Longeron · corrodedDURING 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. (CORROSIOMar 21, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000603Longeron · corrodedDURING 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. Mar 21, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000715Skin · damagedDURING 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 51-1-2Mar 16, 2000 · N831AL · Doug DC873F · Cargo/Baggage DoorsSDR RRXA000714Frame · crackedDURING 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.Mar 16, 2000 · N831AL · Doug DC873F · Fuselage Main, FrameSDR RRXA000598Keelbeam · corrodedDURING 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 DAMAMar 16, 2000 · N831AL · Doug DC873F · Fuselage Main, KeelSDR RRXA000597Frame · corrodedDURING 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 SRMMar 16, 2000 · N831AL · Doug DC873F · Fuselage Main, FrameSDR RRXA000712Web · crackedDURING 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 Mar 15, 2000 · N831AL · Doug DC873F · Fuselage Main, StructureSDR RRXA000600Attach Fitting · corrodedDURING 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 Mar 15, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA000599Attach Fitting · corrodedDURING 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 DMar 15, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA000595Frame · corrodedDURING 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 DACMar 15, 2000 · N831AL · Doug DC873F · Fuselage Main, FrameSDR RRXA000592Skin · corrodedDURING 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 SRMMar 15, 2000 · N831AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA000591Longeron · corrodedDURING 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 Mar 15, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000713Fitting · crackedDURING 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.Mar 14, 2000 · N831AL · Doug DC873F · Fuselage Structure (General)SDR RRXA000593Attach Fitting · corrodedDURING 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 DMar 14, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA000590Angle · corrodedDURING 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 Mar 14, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000589Web · corrodedDURING 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 51-1-20Mar 14, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000711Fitting · crackedDURING 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 51-1-2Mar 13, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000710Bracket · crackedDURING 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 IAWMar 13, 2000 · N831AL · Doug DC873F · Air Conditioning DoorsSDR RRXA000709Splice · crackedDURING 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.Mar 13, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000585Fitting · corrodedDURING 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 Mar 13, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000584Floorboard · corrodedDURING 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. (CORROSMar 13, 2000 · N831AL · Doug DC873F · Fuselage Floor PanelSDR RRXA000610Seat Track · corrodedDURING 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. (COMar 12, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000706Plate · gougedDURING 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 53Mar 11, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000705Web · crackedDURING 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.Mar 10, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000704Tip Cap · crackedDURING 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 WICMar 10, 2000 · N831AL · Doug DC873F · Wing, Control SurfacesSDR RXAA000588Seat Track · corrodedDURING 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 TRMar 10, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000580Floorboard · corrodedDURING 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 INSTALLEMar 10, 2000 · N831AL · Doug DC873F · Fuselage Floor PanelSDR RRXA000579Floorboard · corrodedDURING 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 Mar 10, 2000 · N831AL · Doug DC873F · Fuselage Floor PanelSDR RRXA003368Support · corrodedDURING 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 PAMar 9, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000708Fitting · crackedDURING 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 DMar 9, 2000 · N831AL · Doug DC873F · Wing Miscellaneous StructureSDR RRXA000702Angle · crackedDURING 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 51Mar 9, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000701Channel · crackedDURING 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 Mar 9, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000700Bracket · brokenDURING 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.Mar 9, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous Structure
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