# Service difficulty reports: N832AL, cancelled Feb 21, 2006 A list on [N832AL, cancelled Feb 21, 2006](https://openairdocs.org/deregistered/N832AL-2006-02-21.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR RRXA001081](https://openairdocs.org/sdr/RRXA001081.md): Skin · damaged · Nov 10, 2000 · N832AL · Doug DC873F · Fuselage Main, Plate/Skin > 2 INCH HOLE IN BELLY OF ACFT AT 2 FT AFT OF AVIONICS COMPARTMENT. INSP HOLE AFTER REMOVAL OF FWD BUG BIN FWD CENTER PANEL. FOUND NO STRUCTURAL DAMAGE OTHER THAN 2.5 INCH X 4.38 MAC IN EXTERIOR SKIN. REMOVED DAMAGED PORTION OF SKIN FROM FS 105-F5111 BET - [SDR RRXA001054](https://openairdocs.org/sdr/RRXA001054.md): Wire · misinstalled · Sep 14, 2000 · N832AL · Doug DC873F · Ice/Rain Protection System Wiring > SMOKE IN COCKPIT WITH SPARKS COMING OUT OF BOTTOM OF BULKHEAD. UPON INSP FOUND QUESTIONABLE TERMINAL CONNECTIONS AND BROKEN WIRE ON LT WINDOW OVERHEAT MODIFICATION BREAKER. LOCATED BROKEN WIRE TERMINAL ON LT WINDSHIELD OVERHEAT CB (P/N 7M C41-217-90V), REPAI - [SDR RRXA000293](https://openairdocs.org/sdr/RRXA000293.md): Seat Track · corroded · Jan 31, 2000 · N832AL · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO OBSERVERS AFT SEAT TRACK AT STA -12 TO STA. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW DC-8 SRM 51-3-0 - [SDR RRXA000292](https://openairdocs.org/sdr/RRXA000292.md): Longeron · corroded · Jan 29, 2000 · N832AL · Doug DC873F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 28 LEFT BETWEEN STA 1050 TO STA 1160. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW FAA DER APPROVE - [SDR RRXA000291](https://openairdocs.org/sdr/RRXA000291.md): Seat Track · corroded · Jan 28, 2000 · N832AL · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA 159 AND BL/L 48. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC-8 SRM 51-3-3. - [SDR RRXA000290](https://openairdocs.org/sdr/RRXA000290.md): Seat Track · corroded · Jan 28, 2000 · N832AL · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CARGO SEAT TRACK AT STA 280 AND BL/L 55. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW FAA DER APPRVED ENGINE - [SDR RRXA001036](https://openairdocs.org/sdr/RRXA001036.md): Skin · corroded · Jan 24, 2000 · N832AL · Doug DC873F · Trailing Edge Flaps > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, FLAP EXTERNAL SKIN BETWEEN XW 2 TO XW 64. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-7- - [SDR RRXA000288](https://openairdocs.org/sdr/RRXA000288.md): Frame · corroded · Jan 20, 2000 · N832AL · Doug DC873F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO TORQUE BOX (FRAME) WEB AT STA 270 BETWEEN LONGERONS 33 RIGHT TO 34 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FRAME WEB - [SDR RRXA001038](https://openairdocs.org/sdr/RRXA001038.md): Vane · corroded · Jan 18, 2000 · N832AL · Doug DC873F · Trailing Edge Flaps > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, FLAP VANE BETWEEN XFS 383 TO XFS 386. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-7-1. - [SDR RRXA000289](https://openairdocs.org/sdr/RRXA000289.md): Skin · corroded · Jan 17, 2000 · N832AL · Doug DC873F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, LEADING EDGE, EXTERNAL SKIN BETWEEN XFS 885 TO XFS 892. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW D - [SDR RRXA001033](https://openairdocs.org/sdr/RRXA001033.md): Skin · corroded · Jan 16, 2000 · N832AL · Doug DC873F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, LEADING EDGE LOWER SKIN BETWEEN XFS 347 TO XFS 379. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 - [SDR RRXA001028](https://openairdocs.org/sdr/RRXA001028.md): Longeron · corroded · Jan 13, 2000 · N832AL · Doug DC873F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 34 LEFT BETWEEN STA 390 TO STA 410. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-2 FIGURE - [SDR RRXA001021](https://openairdocs.org/sdr/RRXA001021.md): Seat Track · corroded · Jan 13, 2000 · N832AL · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA 1590 AND BL48R TO WL 0. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW FAA DER AP - [SDR RRXA000286](https://openairdocs.org/sdr/RRXA000286.md): Skin · corroded · Jan 13, 2000 · N832AL · Doug DC873F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, LEADING EDGE, EXTERNAL SKIN AT XFS 710. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-1. - [SDR RRXA001027](https://openairdocs.org/sdr/RRXA001027.md): Frame · corroded · Jan 12, 2000 · N832AL · Doug DC873F · Fuselage Main, Frame > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 1040 AND LONGERON 35 RIGHT. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 FIGURE 2. - [SDR RRXA001035](https://openairdocs.org/sdr/RRXA001035.md): Vane · corroded · Jan 10, 2000 · N832AL · Doug DC873F · Trailing Edge Flaps > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, FLAP VANE AT XFS 225 TO XFS 322. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED FLAP VANE AND INSTALLED NEW VANE IAW DC-8 MM 27-51- - [SDR RRXA001030](https://openairdocs.org/sdr/RRXA001030.md): Longeron · corroded · Jan 10, 2000 · N832AL · Doug DC873F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 30 RIGHT BETWEEN STA 370 TO STA 410. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 SRM - [SDR RRXA001025](https://openairdocs.org/sdr/RRXA001025.md): Fitting · corroded · Jan 8, 2000 · N832AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACHMENT FITTING AT STA 960 TO STA 980 AND BL44R. CORROSION DAMAGE BEYOND 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 - [SDR RRXA001039](https://openairdocs.org/sdr/RRXA001039.md): Clip · corroded · Jan 4, 2000 · N832AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WHEEL WELL ATTACHMENT CLIP AT STA 902, BL59R AND WL 12. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ATTACHMENT CL - [SDR RRXA001026](https://openairdocs.org/sdr/RRXA001026.md): Fitting · corroded · Jan 4, 2000 · N832AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 1480 TO STA 1490 AND LONGERON 33 RIGHT. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC DWG - [SDR RRXA001022](https://openairdocs.org/sdr/RRXA001022.md): Longeron · corroded · Jan 4, 2000 · N832AL · Doug DC873F · Fuselage Main, Longeron/Stringer > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 21 RIGHT AT STA 1190. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-0 FIGURE 23. - [SDR RRXA001037](https://openairdocs.org/sdr/RRXA001037.md): Skin · corroded · Jan 3, 2000 · N832AL · Doug DC873F · Leading Edge Devices > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, OUTBOARD SLOT VANE BETWEEN XFS 430 TO XFS 440. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM - [SDR RRXA001034](https://openairdocs.org/sdr/RRXA001034.md): Skin · corroded · Jan 3, 2000 · N832AL · Doug DC873F · Wing, Plate/Skin > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, UPPER SKIN AT XFS 390 AND STRINGER 11. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED - [SDR RRXA001032](https://openairdocs.org/sdr/RRXA001032.md): Skin · corroded · Jan 3, 2000 · N832AL · Doug DC873F · Leading Edge Devices > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, OUTBOARD SLOT VANE BETWEEN XFS 430 TO XFS 440. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW D - [SDR RRXA001024](https://openairdocs.org/sdr/RRXA001024.md): Fitting · corroded · Jan 3, 2000 · N832AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACHMENT FITTING AT STA 1020 AND LONGERON 21 LEFT. CORROSION DAMAGE BEYOND 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- - [SDR RRXA001023](https://openairdocs.org/sdr/RRXA001023.md): Fitting · corroded · Jan 3, 2000 · N832AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACHMENT FITTING AT STA 1040 AND LONGERON 21 LEFT. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING P/N:4640162-501N AND INSTALLED - [SDR RRXA001031](https://openairdocs.org/sdr/RRXA001031.md): Attach Angle · corroded · Jan 2, 2000 · N832AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM ATTACHMENT ANGLE AT STA 260, BL 65R AND WL-1. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM - [SDR RRXA001029](https://openairdocs.org/sdr/RRXA001029.md): Splice · corroded · Jan 2, 2000 · N832AL · Doug DC873F · Fuselage Miscellaneous Structure > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 33 LEFT SPLICE, BETWEEN STA 380 TO STA 440. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW SPLICE AND INSTALLED IAW DC-8 SRM 51- - [SDR RRXA000287](https://openairdocs.org/sdr/RRXA000287.md): Seat Track · corroded · Dec 30, 1999 · N832AL · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FE'S FORWARD SEAT TRACK. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC-8 SRM 51-3-0. - [SDR RRXA99005](https://openairdocs.org/sdr/RRXA99005.md): Switch · failed · Jan 15, 1999 · N832AL · Doug DC873F · Landing Gear Position and Warning > ON GEAR EXTENSION RIGHT MAIN GEAR LIGHTS WOULD NOT COME ON. SWAPPED BULBS FROM LEFT WITH NO HELP. REMOVED AND REPLACED RIGHT MAIN GEAR DOWNLOCK SWITCH, OPS CHECKS GOOD. ## 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 = 'N832AL' AND deregistration_id = 'N832AL-2006-02-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N832AL-2006-02-21/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.