# Service difficulty reports: N105WP, cancelled May 16, 2006

A list on [N105WP, cancelled May 16, 2006](https://openairdocs.org/deregistered/N105WP-2006-05-16.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 2 · 90 reports

- [SDR RRXA10694](https://openairdocs.org/sdr/RRXA10694.md): Nut Plate · damaged · Apr 9, 2001 · N105WP · Doug DC873 · Wing Miscellaneous Structure
  > DURING MAINTENANCE VSIT FOUND LT WING L/E FUEL TANK ATTACH SCREW TO LONG DAMAGE TO NUT PLATE AT XW-0 TO XW200 (EO), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10720](https://openairdocs.org/sdr/RRXA10720.md): Seat Track · damaged · Mar 28, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND BROKEN LOBE DAMAGE TO SEAT TRACK AT STA 120 AND X+23, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10719](https://openairdocs.org/sdr/RRXA10719.md): Seat Track · damaged · Mar 28, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND BROKEN LOBE DAMAGE TO SEAT TRACKS AT STA 640 AND X+47, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10723](https://openairdocs.org/sdr/RRXA10723.md): Seat Track · worn · Mar 26, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1120 - 1140 AND X+47.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10722](https://openairdocs.org/sdr/RRXA10722.md): Skin · dented · Mar 26, 2001 · N105WP · Doug DC873 · Aileron Tabs
  > DURING A MAINTENANCE VISIT FOUND DENT DAMAGE TO RT AILERON AT O/B CONTROL TAB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10721](https://openairdocs.org/sdr/RRXA10721.md): Stiffener · cracked · Mar 26, 2001 · N105WP · Doug DC873 · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND CRACKED DAMAGE TO W/W VERT STIFFENER AT STA 940 AND WING ROOT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10718](https://openairdocs.org/sdr/RRXA10718.md): Floorbeam · cracked · Mar 22, 2001 · N105WP · Doug DC873 · Fuselage Main, Floor Beam
  > DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO MAIN CARGO COMP FLOOR BEAM AT STA 200 LT OF L22, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10717](https://openairdocs.org/sdr/RRXA10717.md): Seat Track · worn · Mar 22, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 767 - 780 AND X+23, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10716](https://openairdocs.org/sdr/RRXA10716.md): Seat Track · worn · Mar 22, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 767 - 780 AND X+47, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10715](https://openairdocs.org/sdr/RRXA10715.md): Seat Track · worn · Mar 22, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 520 - 540 AND X+47, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10714](https://openairdocs.org/sdr/RRXA10714.md): Seat Track · worn · Mar 22, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1120 - 1140 AND X+23, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10713](https://openairdocs.org/sdr/RRXA10713.md): Seat Track · worn · Mar 22, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1030 - 1050 AND X+23, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10712](https://openairdocs.org/sdr/RRXA10712.md): Seat Track · damaged · Mar 22, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND ELONGATED HOLE DAMAGE TO SEAT TRACK LOCK HOLE AT F/E RIGHT SEAT DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10711](https://openairdocs.org/sdr/RRXA10711.md): Seat Track · worn · Mar 22, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT F/E''S LT SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10708](https://openairdocs.org/sdr/RRXA10708.md): Seat Track · worn · Mar 21, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 970 - 978 AND X+23, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10707](https://openairdocs.org/sdr/RRXA10707.md): Seat Track · worn · Mar 21, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACKS AT STA 930 - 980 AND X+47.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10706](https://openairdocs.org/sdr/RRXA10706.md): Seat Track · worn · Mar 21, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1540 - 1560 AND X=0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10705](https://openairdocs.org/sdr/RRXA10705.md): Seat Track · worn · Mar 21, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1402 - 1412 AND X-47, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10704](https://openairdocs.org/sdr/RRXA10704.md): Seat Track · worn · Mar 21, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1390 AND X-47, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10703](https://openairdocs.org/sdr/RRXA10703.md): Skin · chafed · Mar 20, 2001 · N105WP · Doug DC873 · Elevator, Plate/Skin
  > DURING A MAINTENANCE VISIT FOUND 8 INCHES WEAR/RUBB SPOT DAMAGE TO LT ELEVATOR AT MID SECTION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10702](https://openairdocs.org/sdr/RRXA10702.md): Doubler · cracked · Mar 20, 2001 · N105WP · Doug DC873 · Cargo/Baggage Doors
  > DURING A MAINTENANCE VISIT FOUND CRACK BEYOND STOP DRILL DAMAGE TO B-PIT DOOR AT BOTTOM FWD DOUBLER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10701](https://openairdocs.org/sdr/RRXA10701.md): Seat Track · worn · Mar 20, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1125 - 1135 AND X-47, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10700](https://openairdocs.org/sdr/RRXA10700.md): Seat Track · worn · Mar 20, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1568 - 1620 AND X+47, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM.
- [SDR RRXA10699](https://openairdocs.org/sdr/RRXA10699.md): Seat Track · worn · Mar 20, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1542 - 1546 AND X+22.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10698](https://openairdocs.org/sdr/RRXA10698.md): Seat Track · worn · Mar 20, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1123 - 1131 AND X-22.5, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM.
- [SDR RRXA10697](https://openairdocs.org/sdr/RRXA10697.md): Seat Track · worn · Mar 20, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 1125 - 1135 AND X-0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10696](https://openairdocs.org/sdr/RRXA10696.md): Seat Track · worn · Mar 20, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT RAIL AT STA 972-979 AND X-47.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10695](https://openairdocs.org/sdr/RRXA10695.md): Seat Track · worn · Mar 20, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 952-957 AND X-57, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10710](https://openairdocs.org/sdr/RRXA10710.md): Seat Track · worn · Mar 19, 2001 · N105WP · Doug DC873 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 765 - 779 AND X=0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA10709](https://openairdocs.org/sdr/RRXA10709.md): Floor Panel · corroded · Mar 19, 2001 · N105WP · Doug DC873 · Fuselage Floor Panel
  > DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CARGO COMP FLOOR PANEL AT STA 505 - 506 AND X-1.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
- [SDR RRXA991479](https://openairdocs.org/sdr/RRXA991479.md): Depressor · bent · Sep 27, 1999 · N105WP · Doug DC873 · Cargo/Baggage Doors
  > DURING A MAINTENANCE VISIT, FOUND AFT LOWER MAIN CARGO DOOR SEAL DEPRESSOR BENT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RETURNED TO ORIGINAL CONTOUR AND WELDED IAW COTNEY DRAWING NR J40-R01 WITH APPROVED 8110-
- [SDR RRXA99662](https://openairdocs.org/sdr/RRXA99662.md): Pressurization · malfunctioned · Apr 17, 1999 · N105WP · Doug DC873 · Cabin Pressure Control System
  > UNABLE TO PRESSURIZE AIRCRAFT. AIRCRAFT FERRIED TO BIRMINGHAM FOR DOOR MAINTENANCE.
- [SDR RRXA991071](https://openairdocs.org/sdr/RRXA991071.md): Spar · misdrilled · Feb 15, 1999 · N105WP · Doug DC873 · Wing Spar
  > DURING A MAINTENANCE VISIT FOUND DOUBLE DRILLED, WING, FWD LWR SPAR CAP AT PYLON NR 1, STA XW 467.0, ONE EACH HOLE DOUBLE DRILLED IN SPAR, INTERNAL DOUBLER, AND LOWER WING SKIN IN TEE DOUBLER OUT OF ROUND, PAST 3RD OVERSIZE. DAMAGE EXCEEDED LIMITS IAW DC-8 SR
- [SDR RRXA991080](https://openairdocs.org/sdr/RRXA991080.md): Fitting · damaged · Feb 12, 1999 · N105WP · Doug DC873 · Rudder, Spar/Rib
  > DURING A MAINTENANCE VISIT FOUND AN OVERSIZED HOLE, RUDDER SPAR FITTING AT STA ZR=61.156. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR BUSHING IAW FAA APPROVED TIMCO DER ENGINEERING S
- [SDR RRXA991079](https://openairdocs.org/sdr/RRXA991079.md): Bore · oversized · Feb 11, 1999 · N105WP · Doug DC873 · Landing Gear Retraction/Extension System
  > DURING A MAINTENANCE VISIT FOUND BORE OVERSIZED, MAIN LANDING GEAR LINK BORE, AND HAS ONE LOCATION OF LOCAL BLENDING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR BUSHINGS IAW FAA AP
- [SDR RRXA991066](https://openairdocs.org/sdr/RRXA991066.md): Mount · misdrilled · Feb 10, 1999 · N105WP · Doug DC873 · Wing Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND NUMEROUS OVERSIZED HOLES, NR 4 PYLON MOUNT AREA. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH
- [SDR RRXA991078](https://openairdocs.org/sdr/RRXA991078.md): Jamb · misdrilled · Feb 9, 1999 · N105WP · Doug DC873 · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND DOUBLE DRILLED IN VARIOUS LOCATIONS, L-2 ENTRY DOOR AFT JAMB AT STA 1666 AND STA 1660. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FAA
- [SDR RRXA991077](https://openairdocs.org/sdr/RRXA991077.md): Floorbeam · gouged · Feb 9, 1999 · N105WP · Doug DC873 · Fuselage Main, Floor Beam
  > DURING A MAINTENANCE VISIT FOUND GOUGE, FLOORBEAM, FUSELAGE, AT STA 52, UPPER AFT FLANGE HAS DEEP TOOL GOUGE AT BL 36 LEFT ON UNDERSIDE OF FLANGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED IAW FAA APPRO
- [SDR RRXA991076](https://openairdocs.org/sdr/RRXA991076.md): Floorbeam · misdrilled · Feb 9, 1999 · N105WP · Doug DC873 · Fuselage Main, Floor Beam
  > DURING A MAINTENANCE VISIT FOUND MISDRILLED, FLOORBEAM, AT STA 660, UPPER FLANGES. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-06273 AND DC08-53-0351,
- [SDR RRXA991075](https://openairdocs.org/sdr/RRXA991075.md): Door Pan · misdrilled · Feb 8, 1999 · N105WP · Doug DC873 · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND MISDRILLED, AFT SERVICE DOOR, AFT LWR DOOR PAN, IN TWO PLACES. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE, FILLER, AND DOUBLERS IAW FAA APPRO
- [SDR RRXA991074](https://openairdocs.org/sdr/RRXA991074.md): Frame · misdrilled · Feb 4, 1999 · N105WP · Doug DC873 · Fuselage Main, Frame
  > DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLE, FUSELAGE, FRAME AT STA 1140, LONGERON 35 LEFT AT AN INTERCOSTAL LOCATION. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW
- [SDR RRXA991073](https://openairdocs.org/sdr/RRXA991073.md): Floorbeam · damaged · Feb 4, 1999 · N105WP · Doug DC873 · Fuselage Main, Floor Beam
  > DURING A MAINTENANCE VISIT FOUND DAMAGE, FUSELAGE, FLOORBEAM AT STA 1140, BL 0.0, NO SRM. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SHIM, ANGLE, AND DOUBLER IAW FAA APPROVED TIMCO
- [SDR RRXA991072](https://openairdocs.org/sdr/RRXA991072.md): Floorbeam · misrepaired · Feb 4, 1999 · N105WP · Doug DC873 · Fuselage Main, Floor Beam
  > DURING A MAINTENANCE VISIT FOUND TWO CUTOUTS, FUSELAGE, FLOORBEAM, UPPER FORWARD FLANGE, AT STA 680. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW FAA APPROVED TIMCO DER ENGINE
- [SDR RRXA991061](https://openairdocs.org/sdr/RRXA991061.md): Fitting · misdrilled · Feb 3, 1999 · N105WP · Doug DC873 · Vertical Stabilizer, Spar/Rib
  > DURING A MAINTENANCE VISIT FOUND OVERSIZED HOLE, RUDDER SPAR FITTING AT STA ZR 61.156 HAS OVERSIZED ATTACH HOLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW OVERSIZED BUSHING IAW FAA A
- [SDR RRXA991063](https://openairdocs.org/sdr/RRXA991063.md): Floorbeam · cracked · Feb 2, 1999 · N105WP · Doug DC873 · Fuselage Main, Floor Beam
  > DURING A MAINTENANCE VISIT FOUND CRACKS, FUSELAGE, FLOORBEAM AT STA 160 AND STA 180, BL 40 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED STRAPS, ANGLES, AND DOUBLERS IAW FAA APPROVED T
- [SDR RRXA991062](https://openairdocs.org/sdr/RRXA991062.md): Floorbeam · cracked · Feb 2, 1999 · N105WP · Doug DC873 · Fuselage Main, Floor Beam
  > DURING A MAINTENANCE VISIT FOUND CRACKS, FUSELAGE, FLOORBEAM, AT STA 160 AND STA 180, CRACKED AT APPROX BL 40 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED STRAPS, ANGLES, AND DOUBLERS
- [SDR RRXA991070](https://openairdocs.org/sdr/RRXA991070.md): Floorbeam · damaged · Feb 1, 1999 · N105WP · Doug DC873 · Fuselage Main, Floor Beam
  > DURING A MAINTENANCE VISIT FOUND A TRIM OUT, FUSELAGE, LONGITUDINAL FLOORBEAM AT BL 11.5 RIGHT FROM STA 21 TO STA 25 IN THE UPPER HORIZONTAL FLANGE AND A BLEND OUT IN THE VERTICAL FLANGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW
- [SDR RRXA991069](https://openairdocs.org/sdr/RRXA991069.md): Fitting · mismanufactured · Feb 1, 1999 · N105WP · Doug DC873 · Wing Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND MATERIAL SUBSTITUTION, P/N: 3616112-3 FITTING IS MADE FROM P/N: 3616111 7075-T6 FORGING. REQUEST TO FAB FROM ALUMINUM BAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED A
- [SDR RRXA991160](https://openairdocs.org/sdr/RRXA991160.md): Longeron · cracked · Jan 29, 1999 · N105WP · Doug DC873 · Fuselage Main, Longeron/Stringer
  > DURING A MAINTENANCE VISIT FOUND A CRACK AND CORROSION, FUSELAGE, LONGERON 36 BETWEEN STA 260 AND STA 300. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SECTION OF LONGERON IAW DAC DW
- [SDR RRXA991068](https://openairdocs.org/sdr/RRXA991068.md): Fitting · cracked · Jan 29, 1999 · N105WP · Doug DC873 · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE VISIT FOUND CRACKED SPLICE FITTING AT STA 510, LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPLACEMENT SPLICE IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH

Next page: https://openairdocs.org/deregistered/N105WP-2006-05-16/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 = 'N105WP' AND deregistration_id = 'N105WP-2006-05-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N105WP-2006-05-16/reports

---
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