# Service difficulty reports: N811AL, cancelled Jan 29, 2018

A list on [N811AL, cancelled Jan 29, 2018](https://openairdocs.org/deregistered/N811AL-2018-01-29.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 4 · 170 reports

- [SDR RRXA010055](https://openairdocs.org/sdr/RRXA010055.md): Warning System · activated · Jun 27, 2001 · N811AL · Doug DC871 · Fire Detection
  > JUST PRIOR TO STARTING APPROACH EXPERIENCE FIRE WARNING ON NR 1 ENGINE FOLLOWED QRH. SHUT DOWN ENGINE AND BOTH BOTTLES FIRED. REPAIRED DAMAGED WIRING AT P10-7000 TO AFT FIRE LOOP ON NR 1 ENGINE IAW DC-8 M/M 20-50-1. CK'D ALL WIRING AND FIRE LOOPS ON NR 1 EN
- [SDR RRXA011047](https://openairdocs.org/sdr/RRXA011047.md): Element · faulty · Jun 13, 2001 · N811AL · Doug DC871 · Fire Detection
  > INTERMITTENT FIRE INDICATION ON NR 1 ENG FIRED BOTH BOTTLES AND SHUT DOWN ENG FIRE INDICATIONS STILL WERE INTERMITTENT. WHEN FIRE LIGHT IN HANDLE INTERMITTENT WENT OUT, FIRE TEST WOULD NOT TEST. REMOVED AND REPLACED NR 1 ENG FIRE SENSING ELEMENTS IAW DC-8
- [SDR RRXA010008](https://openairdocs.org/sdr/RRXA010008.md): Tire · failed · Feb 6, 2001 · N811AL · Doug DC871 · Tire
  > RIGHT MAIN GEAR TIRES BLEW ON LANDING. REMOVED AND REPLACED RT MLG WHEEL AND TIRE ASSYS IAW M/M 32-40-1 (TIRE POSITIONS 4, 5, 7, 8).
- [SDR RRXA001084](https://openairdocs.org/sdr/RRXA001084.md): Landing Gear · vibration · Dec 6, 2000 · N811AL · Doug DC871 · Nose/Tail Landing Gear
  > AFTER RETRACTION OF GEAR LOUD NOISE AND VIBRATION FROM NOSE GEAR AREA CYCLED GEAR NO NOISE WHEN EXTENDED. JACKED AIRCRAFT IAW DC-8 M/M CH 7-11-0 PERFORMED GEAR SWING IAW DC-8 M/M CH 32-30-0 NOSE GEAR STRUT/DOOR'S OPS NORMAL
- [SDR RRXA001080](https://openairdocs.org/sdr/RRXA001080.md): Fire Loop · malfunctioned · Nov 8, 2000 · N811AL · Doug DC871 · Fire Detection
  > AT TOP WHEN RETARDED THROTTLES #3 ENG HAD STEADY FIRE WARNING (BELL & LIGHT) SHUT DOWN ENG. AFTER SHUT DOWN AND DISCHARGING AGENT, FIRE WARNING CONTINUED. ***CORRECTIVE ACTION *** FOUND FIRE ELEMENT READING LOW RESISTANCE PER MM 26-11-2. R&R FIRE ELEMENT IAW
- [SDR RRXA001064](https://openairdocs.org/sdr/RRXA001064.md): Warning System · malfunctioned · Oct 10, 2000 · N811AL · Doug DC871 · Elevator Control System
  > REJECTED T/O DUE TO NO ELEVATOR CHECK, ASKED FOR FREIGHT REWEIGH (120 KNOTS). PERFORMED REJECTED T/O INSPECTION IAW EWA WORK CARD SP001. NO DEFECTS NOTED. INSPECTED ELEVATOR IAW MM 27-30-1. NO DEFECTS NOTED.
- [SDR RRXA003051](https://openairdocs.org/sdr/RRXA003051.md): Trunnion · cracked · Sep 15, 2000 · N811AL · Doug DC871 · Main Landing Gear Attach Section
  > DURING A MAINTENANCE VISIT FOUND A CRACK AND CORROSION DAMAGE TO THE NOSE W/W RT. TUNNEL NOSE GEAR TRUNNION ATTACH FITTING AT STA X=+20, Y=-12 Z=-25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 S
- [SDR RRXA003053](https://openairdocs.org/sdr/RRXA003053.md): Seat Track · corroded · Sep 8, 2000 · N811AL · Doug DC871 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND BROKEN OFF SCREWS AND CORROSION DAMAGE TO THE SEAT TRACK FLANGE AT STA Y=70-280 & X=+60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART A
- [SDR RRXA003766](https://openairdocs.org/sdr/RRXA003766.md): Doubler · corroded · Sep 6, 2000 · N811AL · Doug DC871 · Fuselage Main, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT SURFACE REAR SPAR LWR CAP AT STA XRS -578, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALL
- [SDR RRXA003055](https://openairdocs.org/sdr/RRXA003055.md): Splice · cracked · Sep 6, 2000 · N811AL · Doug DC871 · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND A 1/2 INCH CRACK LEADING FROM FASTENER HOLE ON THE THROUGH ACCESS HOLE 506A AT STA XW 408 AND XW 393 NR 8 UPPER STRINGER SPLICE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FAB
- [SDR RRXA003054](https://openairdocs.org/sdr/RRXA003054.md): Retainer · cracked · Sep 6, 2000 · N811AL · Doug DC871 · Cargo/Baggage Doors
  > DURING A MAINTENANCE VISIT FOUND CRACKED, BROKEN AND CORROSION DAMAGE TO THE MAIN CARGO DOR SEAL RETAINERS, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED
- [SDR RRXA003052](https://openairdocs.org/sdr/RRXA003052.md): Panel · corroded · Sep 6, 2000 · N811AL · Doug DC871 · Fuselage Main, Floor Beam
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMGE TO THE SUB-FLOOR PANEL AT STA 220-360 FROM RBL 45 TO RBL 49, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED
- [SDR RRXA002983](https://openairdocs.org/sdr/RRXA002983.md): Panel · corroded · Aug 31, 2000 · N811AL · Doug DC871 · Fuselage Main, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMGE TO THE SUB FLOOR PANEL AT STA 80-220 AND LBL 25 - LBL 45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 53-2-0.
- [SDR RRXA002982](https://openairdocs.org/sdr/RRXA002982.md): Panel · corroded · Aug 31, 2000 · N811AL · Doug DC871 · Fuselage Floor Panel
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMGE TO THE SUB FLOOR PANEL FROM STA 220-360 AND RBL 25 - RBL 45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-
- [SDR RRXA002991](https://openairdocs.org/sdr/RRXA002991.md): Threshold · cracked · Aug 29, 2000 · N811AL · Doug DC871 · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND A CRACKED, BENT AND RIVET DRILLED OFF THE LT L3 DOOR SILL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002990](https://openairdocs.org/sdr/RRXA002990.md): Fastener · damaged · Aug 29, 2000 · N811AL · Doug DC871 · Wing Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND A PARTIAL HI-LOK DRILLED AT RT LWR WING I/B NR 4 PYLON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002989](https://openairdocs.org/sdr/RRXA002989.md): Boss · corroded · Aug 29, 2000 · N811AL · Doug DC871 · Main Landing Gear Strut/Axle/Truck
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MLG SHOCK STRUT ASSY RETRACT PIN BOSS WHICH MEANS MA-AI-3210-01:03 NEEDS TO BE C/W, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002987](https://openairdocs.org/sdr/RRXA002987.md): Angle · cracked · Aug 29, 2000 · N811AL · Doug DC871 · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND A CRACKED TO THE CUSP KICK PLATE LT ANGLE AT STA 1560 - 1580, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002986](https://openairdocs.org/sdr/RRXA002986.md): Spar · damaged · Aug 29, 2000 · N811AL · Doug DC871 · Wing Spar
  > DURING A MAINTENANCE VISIT FOUND 7 DEFORMED BOLT HOLES TO THE RT CENTER AUX TANK AFT LT INNER ACCESS HOLE UPPER REAR SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002985](https://openairdocs.org/sdr/RRXA002985.md): Spar · damaged · Aug 29, 2000 · N811AL · Doug DC871 · Wing Spar
  > DURING A MAINTENANCE VISIT FOUND 4 DEFORMED BOLT HOLES TO THE LT CENTER AUX TANK AFT RT INNER ACCESS HOLE UPPER REAR SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002984](https://openairdocs.org/sdr/RRXA002984.md): Threshold · damaged · Aug 29, 2000 · N811AL · Doug DC871 · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND SEVERAL ELONGATED HOLES TO THE THRESHOLD ON THE B PIT DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002999](https://openairdocs.org/sdr/RRXA002999.md): Door · misrepaired · Aug 28, 2000 · N811AL · Doug DC871 · Landing Gear Doors
  > DURING A MAINTENANCE VISIT FOUND A BAD REPAIR TO THE LT MAIN LANDING GEAR DOOR AFT LWR CORNER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002998](https://openairdocs.org/sdr/RRXA002998.md): Frame · cracked · Aug 28, 2000 · N811AL · Doug DC871 · Fuselage Main, Frame
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FRAME UNDER PRESSURE DECK AT STA -99 AND LBL 60 BELOW L22L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002997](https://openairdocs.org/sdr/RRXA002997.md): Panel · damaged · Aug 28, 2000 · N811AL · Doug DC871 · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND A TORN CAMLOCK HOLE AT STA 683A, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002996](https://openairdocs.org/sdr/RRXA002996.md): Seat Track · broken · Aug 28, 2000 · N811AL · Doug DC871 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND A BROKEN SEAT TRACK AT STA 680 AND RBL 25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002995](https://openairdocs.org/sdr/RRXA002995.md): Seat Track · broken · Aug 28, 2000 · N811AL · Doug DC871 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND A BROKEN SEAT TRACK AT STA 1040 AND RBL 25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002994](https://openairdocs.org/sdr/RRXA002994.md): Seat Track · broken · Aug 28, 2000 · N811AL · Doug DC871 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND A BROKEN SEAT TRACK AT STA 1450 AND RBL 25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002993](https://openairdocs.org/sdr/RRXA002993.md): Longeron · cracked · Aug 28, 2000 · N811AL · Doug DC871 · Fuselage Main, Longeron/Stringer
  > DURING A MAINTENANCE VISIT FOUND A POSSIBLE CRACK TO THE LONGERON AT STA 857 AND L4R AFT SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002992](https://openairdocs.org/sdr/RRXA002992.md): Seat Track · broken · Aug 28, 2000 · N811AL · Doug DC871 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND A BROKEN SEAT TRACK AT X=0 Y=1477 Z=0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002988](https://openairdocs.org/sdr/RRXA002988.md): Skin · corroded · Aug 28, 2000 · N811AL · Doug DC871 · Fuselage Main, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN AT MARKER BEACON AT STA 680 - 660 AND L36L TO L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002914](https://openairdocs.org/sdr/RRXA002914.md): Support · cracked · Aug 26, 2000 · N811AL · Doug DC871 · Fuselage Main, Bulkhead
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BULKHEAD MIDDLE RT SUPPORT (HORIZONTAL) AT STA 70, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-4.
- [SDR RRXA002917](https://openairdocs.org/sdr/RRXA002917.md): Panel · corroded · Aug 25, 2000 · N811AL · Doug DC871 · Fuselage Main, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE R/H LWR. ACCESS PANEL 547, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0 AND EO 00-196.
- [SDR RRXA002916](https://openairdocs.org/sdr/RRXA002916.md): Panel · delaminated · Aug 25, 2000 · N811AL · Doug DC871 · Fuselage Main, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND FASTENERS PULLING THROUGH THE CENTER PANEL BETWEEN MAIN GEAR DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-
- [SDR RRXA002915](https://openairdocs.org/sdr/RRXA002915.md): Web · cracked · Aug 25, 2000 · N811AL · Doug DC871 · Fuselage Main, Bulkhead
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO BOTH SIDES ON THE L/H FLOOR BEAM PRESS WEB AT STA 857 AND LONGERON 0 TO =60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-
- [SDR RRXA002880](https://openairdocs.org/sdr/RRXA002880.md): Trunnion · corroded · Aug 24, 2000 · N811AL · Doug DC871 · Main Landing Gear Strut/Axle/Truck
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE TOP LT. SIDE OF NLG TRUNNION FITTING. ------------------------CX----------------------------
- [SDR RRXA002879](https://openairdocs.org/sdr/RRXA002879.md): Seat Track · damaged · Aug 24, 2000 · N811AL · Doug DC871 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND ELONGATED LOCK HOLES TO THE F/E LT. SEAT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0.
- [SDR RRXA002878](https://openairdocs.org/sdr/RRXA002878.md): Angle · corroded · Aug 24, 2000 · N811AL · Doug DC871 · Fuselage Floor Panel
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SUB-FLOOR ANGLE AT STA -99 FO'S SIDE RBL 48" 12" BELOW AND RT. OF FO'S RUDDER PEDELS, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1
- [SDR RRXA002877](https://openairdocs.org/sdr/RRXA002877.md): Seat Track · worn · Aug 24, 2000 · N811AL · Doug DC871 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND DEEP WEAR AREAS TO THE CAPT. FWD RT. SEAT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0.
- [SDR RRXA002876](https://openairdocs.org/sdr/RRXA002876.md): Web · corroded · Aug 24, 2000 · N811AL · Doug DC871 · Fuselage Main, Floor Beam
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON SUB-FLOOR WEB BELOW RELAY CONTROL PANEL AT STA 8 0 TO -12 FROM CL TO RBL 68", DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. ---------------------CX----------------------
- [SDR RRXA002875](https://openairdocs.org/sdr/RRXA002875.md): Skin · dented · Aug 24, 2000 · N811AL · Doug DC871 · Fuselage Main, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND A DENT TO THE EXTERIOR SKIN AT STA 1586 BETWEEN L21R-L22R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1
- [SDR RRXA002874](https://openairdocs.org/sdr/RRXA002874.md): Skin · corroded · Aug 24, 2000 · N811AL · Doug DC871 · Fuselage Main, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN AT STA 1296 AND L21R-L20R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. --------------------CX--------------------
- [SDR RRXA002873](https://openairdocs.org/sdr/RRXA002873.md): Frame · cracked · Aug 24, 2000 · N811AL · Doug DC871 · Fuselage Main, Frame
  > DURING A MAINTENANCE VISIT FOUND A CRACK AND SHEARED FASTENERS TO THE EXTERIOR FRAME/WEB AT STA 816 AND XCW 69, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALL
- [SDR RRXA002872](https://openairdocs.org/sdr/RRXA002872.md): Skin · dented · Aug 24, 2000 · N811AL · Doug DC871 · Fuselage Main, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND A DENT TO THE EXTERIOR SKIN AT STA 120 AND L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-1, 53-2-0.
- [SDR RRXA002871](https://openairdocs.org/sdr/RRXA002871.md): Skin · corroded · Aug 24, 2000 · N811AL · Doug DC871 · Fuselage Main, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE EXTERIOR SKIN BETWEEN STA 742-781 AND L35L-L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA002883](https://openairdocs.org/sdr/RRXA002883.md): Floorbeam · cracked · Aug 23, 2000 · N811AL · Doug DC871 · Fuselage Main, Floor Beam
  > DURING A MAINTENANCE VISIT FOUND A 1 1/4 INCH CRACK TO THE TOP FLOORBEAM AT STA -10 IN COCKPIT AND LBL -10, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0.
- [SDR RRXA002882](https://openairdocs.org/sdr/RRXA002882.md): Seat Track · damaged · Aug 23, 2000 · N811AL · Doug DC871 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND ELONGAGED LOCK HOLES AND SCALOPED WEAR AREAS ON THE 2ND OBS SEAT TRACK (RIGHT), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0.
- [SDR RRXA002881](https://openairdocs.org/sdr/RRXA002881.md): Intercostal · cracked · Aug 23, 2000 · N811AL · Doug DC871 · Fuselage Floor Panel
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND A CRACK TO THE RIVETS ON INTERCOSTAL AT STA 5 AND L29R. ----------------------------CX-----------------------------
- [SDR RRXA002912](https://openairdocs.org/sdr/RRXA002912.md): Seat Track · corroded · Aug 22, 2000 · N811AL · Doug DC871 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMGE AND BROKEN OFF SCREWS IN TRACK FLANGE ON SEAT TRACK AT STA Y=1360-1580 AND X-60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATE
- [SDR RRXA002911](https://openairdocs.org/sdr/RRXA002911.md): Seat Track · corroded · Aug 22, 2000 · N811AL · Doug DC871 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND BROKEN OFF SCREWS IN TRACK FLANGE TO SEAT TRACK AT STA Y=1360-1580 AND X-46, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICAT
- [SDR RRXA002910](https://openairdocs.org/sdr/RRXA002910.md): Seat Track · broken · Aug 22, 2000 · N811AL · Doug DC871 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND A LUG BROKEN OUT ON THE SEAT TRACK AT STA 1483 AND X=0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-3-0 AND STC SA180250 A

Next page: https://openairdocs.org/deregistered/N811AL-2018-01-29/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 = 'N811AL' AND deregistration_id = 'N811AL-2018-01-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N811AL-2018-01-29/reports

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