# Service difficulty reports: N957R, cancelled Apr 24, 2002

A list on [N957R, cancelled Apr 24, 2002](https://openairdocs.org/deregistered/N957R-2002-04-24.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 3 · 122 reports

- [SDR RRXA003351](https://openairdocs.org/sdr/RRXA003351.md): Panel · delaminated · Oct 30, 2000 · N957R · Doug DC863F · Wing, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND A DELAMINATED PANEL ON THE LT WING LWR T/E AT STA XW 5.00 TO XW 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003350](https://openairdocs.org/sdr/RRXA003350.md): Panel · delaminated · Oct 30, 2000 · N957R · Doug DC863F · Wing, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND DELAMINATION AND A DENTED HOLE TO THE LT WING LWR SURFACE T/E PANEL UNDER HYD TANK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003349](https://openairdocs.org/sdr/RRXA003349.md): Panel · delaminated · Oct 30, 2000 · N957R · Doug DC863F · Wing, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LT WING LWR SURFACE T/E PANEL AT STA 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003348](https://openairdocs.org/sdr/RRXA003348.md): Panel · delaminated · Oct 30, 2000 · N957R · Doug DC863F · Wing, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LT WING LWR SURFACE T/E PANEL AT STA XW 98 TO XW 138, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003347](https://openairdocs.org/sdr/RRXA003347.md): Panel · delaminated · Oct 30, 2000 · N957R · Doug DC863F · Wing, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LT WING LWR SURFACE T/E PANEL AT STA 138 TO 214, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003346](https://openairdocs.org/sdr/RRXA003346.md): Skin · delaminated · Oct 30, 2000 · N957R · Doug DC863F · Wing, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND DELAMINATION TO THE LEFT WING LWR SURFACE T/E PANEL NR 577B, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003345](https://openairdocs.org/sdr/RRXA003345.md): Skin · cracked · Oct 30, 2000 · N957R · Doug DC863F · Trailing Edge Flaps
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE O/B FLAP O/B EXHAUST GATE FLANGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003344](https://openairdocs.org/sdr/RRXA003344.md): Angle · cracked · Oct 30, 2000 · N957R · Doug DC863F · Trailing Edge Flaps
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP RIB ANGLE AT THE LEFT O/B FLAP I/B SCISSOR LINK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003343](https://openairdocs.org/sdr/RRXA003343.md): Skin · cracked · Oct 30, 2000 · N957R · Doug DC863F · Trailing Edge Flaps
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE SKIN AT THE LEFT I/B FLAP BOTTOM, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003342](https://openairdocs.org/sdr/RRXA003342.md): Channel · cracked · Oct 30, 2000 · N957R · Doug DC863F · Trailing Edge Flaps
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LEFT I/B FLAP I/B TRAILING EDGE WEDGE CHANNEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003341](https://openairdocs.org/sdr/RRXA003341.md): Floor Panel · cracked · Oct 30, 2000 · N957R · Doug DC863F · Fuselage Floor Panel
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND A CRACK TO THE COCKPIT FLOOR PANEL NR 677, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003340](https://openairdocs.org/sdr/RRXA003340.md): Floor Panel · cracked · Oct 30, 2000 · N957R · Doug DC863F · Fuselage Floor Panel
  > DURING A MAINTENANCE VISIT FOUND CORROSION AND A CRACK TO THE TOP AND BOTTOM OF THE COCKPIT FLOOR PANEL 679, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003339](https://openairdocs.org/sdr/RRXA003339.md): Floor Panel · corroded · Oct 30, 2000 · N957R · Doug DC863F · Fuselage Floor Panel
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BOTH SIDES OF THE COCKPIT FLOOR PANEL UNDER F/E''S DESK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003338](https://openairdocs.org/sdr/RRXA003338.md): Floor Panel · corroded · Oct 30, 2000 · N957R · Doug DC863F · Fuselage Floor Panel
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE COCKPIT FLOOR PANEL UNDER FE''S CONSOLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003337](https://openairdocs.org/sdr/RRXA003337.md): Fitting · corroded · Oct 30, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CIRCUMFERENTIAL FRAME FITTING AT STA 1480 AND L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003336](https://openairdocs.org/sdr/RRXA003336.md): Fitting · corroded · Oct 30, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMGE TO THE FRAME TO CUSP FITTING AT STA 1460 AND L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003335](https://openairdocs.org/sdr/RRXA003335.md): Finger Doubler · corroded · Oct 30, 2000 · N957R · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND POPPED RIVET HEADS TO THE UPPER SURFACE W/W FINGER DOUBLER BETWEEN STA 902 - 920 AND LBL 4 LBL -4 Z AXIS -10, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003334](https://openairdocs.org/sdr/RRXA003334.md): Panel · delaminated · Oct 30, 2000 · N957R · Doug DC863F · Fuselage Floor Panel
  > DURING A MAINTENANCE VISIT FOUND THE COCKPIT FLOOR SEPARATED AT STA -12 TO -32, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003352](https://openairdocs.org/sdr/RRXA003352.md): Skin · corroded · Oct 25, 2000 · N957R · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ALONG THE MOUNTING SURFACE OF THE NR 2 ADF AT STA 145 - 170 AND L36 TO L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003290](https://openairdocs.org/sdr/RRXA003290.md): Rib · cracked · Oct 20, 2000 · N957R · Doug DC863F · Trailing Edge Flaps
  > DURING A MAINTENANCE VISIT FOUND CORROSION AT RIGHT I/B FLAP-RIB-LOC AT STA XW 64 18 - 20 INCHES AFT OF FLAP FRONT SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003289](https://openairdocs.org/sdr/RRXA003289.md): Angle · cracked · Oct 20, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE ATTACH ANGLE AT THE RIGHT W/W AT STA XWO ABOVE L24R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003291](https://openairdocs.org/sdr/RRXA003291.md): Fitting · misdrilled · Oct 18, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND A DRILLED AREA TO THE CIRCUMFERENTIAL FRAME FITTING AT STA 640 AND L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003292](https://openairdocs.org/sdr/RRXA003292.md): Fitting · cracked · Oct 16, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL ATTACH FITTING BETWEEN MLG DOORS AT STA 930, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003299](https://openairdocs.org/sdr/RRXA003299.md): Stringer · chafed · Oct 13, 2000 · N957R · Doug DC863F · Engine Thrust Reverser
  > DURING A MAINTENANCE VISIT FOUND A CHAFED STRINGER SIDEWALL AND HOLES ELONGATED ON THE NR 4 THRUST REVERSER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003298](https://openairdocs.org/sdr/RRXA003298.md): Bulkhead · cracked · Oct 13, 2000 · N957R · Doug DC863F · Fuselage Main, Bulkhead
  > DURING A MAINTENANCE VISIT FOUND A CRACK AND MISSING FASTENERS TO THE A & B PIT CENTER DIVIDER WALL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003297](https://openairdocs.org/sdr/RRXA003297.md): Intercostal · cracked · Oct 13, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND A CRACKED INTERCOSTAL BETWEEN MLG DOORS AND LT AND RT ATTACH FITTINGS AT STA 902, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003296](https://openairdocs.org/sdr/RRXA003296.md): Intercostal · cracked · Oct 13, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL BETWEEN MLG DOORS AT STA 940, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003295](https://openairdocs.org/sdr/RRXA003295.md): Fitting · cracked · Oct 13, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL ATTACH FITTINGS BETWEEN MLG DOORS AT STA 960, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003294](https://openairdocs.org/sdr/RRXA003294.md): Fitting · cracked · Oct 13, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL ATTACH FITTING BETWEEN MLG DOORS AT STA 950, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003293](https://openairdocs.org/sdr/RRXA003293.md): Fitting · cracked · Oct 13, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL ATTACH FITTINGS BETWEEN MLG DOORS AT STA 890, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003308](https://openairdocs.org/sdr/RRXA003308.md): Web · tool damage · Oct 12, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND DRILL HOLES AND DRILL STARTS IN WEB AT STA 1340 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003307](https://openairdocs.org/sdr/RRXA003307.md): Frame · misdrilled · Oct 12, 2000 · N957R · Doug DC863F · Fuselage Main, Frame
  > DURING A MAINTENANCE VISIT FOUND A DRILL START AT FLOOR LEVEL AT STA 1280 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003306](https://openairdocs.org/sdr/RRXA003306.md): Longeron · misdrilled · Oct 12, 2000 · N957R · Doug DC863F · Fuselage Main, Longeron/Stringer
  > DURING A MAINTENANCE VISIT FOUND DRILL STARTS AND HOLES IN STRINGER AT STA 440 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003305](https://openairdocs.org/sdr/RRXA003305.md): Web · misdrilled · Oct 12, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND HOLES IN WEB BETWEEN STA 260 - 280 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003304](https://openairdocs.org/sdr/RRXA003304.md): Link · worn · Oct 10, 2000 · N957R · Doug DC863F · Trailing Edge Flaps
  > DURING A MAINTENANCE VISIT FOUND EXCESSIVE PLAY IN THE LEFT O/B FLAP MID SCISSOR LINK BOLT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003303](https://openairdocs.org/sdr/RRXA003303.md): Link · worn · Oct 10, 2000 · N957R · Doug DC863F · Trailing Edge Flaps
  > DURING A MAINTENANCE VISIT FOUND EXCESSIVE PLAY TO THE LEFT O/B FLAP LWR SCISSOR LINK BOLT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003302](https://openairdocs.org/sdr/RRXA003302.md): Structure · cracked · Oct 10, 2000 · N957R · Doug DC863F · Landing Gear Doors
  > DURING A MAINTENANCE VISIT FOUND A CRACKED CORNER AT RIVET HOLE TO THE RT MAIN GEAR DOOR FWD LWR END, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003301](https://openairdocs.org/sdr/RRXA003301.md): Panel · delaminated · Oct 10, 2000 · N957R · Doug DC863F · Fuselage Main, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND A DELAMINATED AND DETERIORATED PANEL 632 TOP AND O/B SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003300](https://openairdocs.org/sdr/RRXA003300.md): Longeron · corroded · Oct 10, 2000 · N957R · Doug DC863F · Fuselage Main, Longeron/Stringer
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE BETWEEN STA 1080 - 1100 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003212](https://openairdocs.org/sdr/RRXA003212.md): Skin · dented · Oct 6, 2000 · N957R · Doug DC863F · Trailing Edge Flaps
  > DURING A MAINTENANCE VISIT FOUND SEVERAL DING AREAS ON THE LEFT I/B FLAP BOTTOM, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003176](https://openairdocs.org/sdr/RRXA003176.md): Structure · worn · Oct 6, 2000 · N957R · Doug DC863F · Nacelle/Pylon Structure
  > DURING A MAINTENANCE VISIT FOUND A WORN EDGE ON THE AFT NR 2 ENGINE LT PYLON SKIRT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003175](https://openairdocs.org/sdr/RRXA003175.md): Frame · corroded · Oct 5, 2000 · N957R · Doug DC863F · Fuselage Main, Frame
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FRAME LOWER CHORD IN -A- PIT AT STA 160 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003174](https://openairdocs.org/sdr/RRXA003174.md): Frame · corroded · Oct 5, 2000 · N957R · Doug DC863F · Fuselage Main, Frame
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FRAME IN -A- PIT AT STA 180 AND L36L TO L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003173](https://openairdocs.org/sdr/RRXA003173.md): Floorbeam · corroded · Oct 5, 2000 · N957R · Doug DC863F · Fuselage Main, Floor Beam
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND POPPED RIVETS AT BEAM LOWER CHORD/WEB AT STA 702 LBL 45 TO 52.5 & LBL 55.5 TO 61 Z AXIS -7 FWD AND AFT SIDE OF BEAM, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003177](https://openairdocs.org/sdr/RRXA003177.md): Mount · gouged · Oct 4, 2000 · N957R · Doug DC863F · Engine Mount Section
  > DURING A MAINTENANCE VISIT FOUND A GOUGED FWD MOUNT ON THE NR 3 ENGINE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003180](https://openairdocs.org/sdr/RRXA003180.md): Bracket · cracked · Oct 3, 2000 · N957R · Doug DC863F · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIGHT I/B LWR SCISSOR PANEL SUPPORT BRACKET, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003179](https://openairdocs.org/sdr/RRXA003179.md): Web · cracked · Oct 3, 2000 · N957R · Doug DC863F · Wing Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND A CRACK IN WEB WHERE WEDGE ATTACH POINT IS ON THE RIGHT I/B FLAP AT STA XW 75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003178](https://openairdocs.org/sdr/RRXA003178.md): Floorbeam · cracked · Oct 3, 2000 · N957R · Doug DC863F · Fuselage Main, Floor Beam
  > DURING A MAINTENANCE VISIT FOUND CORROSION EXFOLIATION TO THE FLOORBEAM AT STA 702 AND X+50, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003099](https://openairdocs.org/sdr/RRXA003099.md): Frame · cracked · Sep 22, 2000 · N957R · Doug DC863F · Trailing Edge Flaps
  > DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LEFT WING O/B FLAP I/B FRAME, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA003098](https://openairdocs.org/sdr/RRXA003098.md): Link · gouged · Sep 22, 2000 · N957R · Doug DC863F · Trailing Edge Flap Actuator
  > DURING A MAINTENANCE VISIT FOUND A GOUGE TO THE SUPPORT AFT LINK ON THE LEFT I/B FLAP SUPPORT AT STA 98 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.

Next page: https://openairdocs.org/deregistered/N957R-2002-04-24/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 = 'N957R' AND deregistration_id = 'N957R-2002-04-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N957R-2002-04-24/reports

---
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