# Service difficulty reports: N852UP, cancelled Sep 15, 2014

A list on [N852UP, cancelled Sep 15, 2014](https://openairdocs.org/deregistered/N852UP-2014-09-15.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 6 · 285 reports

- [SDR IPXA09856179](https://openairdocs.org/sdr/IPXA09856179.md): Doubler · damaged · Jun 1, 2009 · N852UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV SURVEY SEQ 852-W3-07 LT WING XFS 270.5 EDGE REPAIR HAS WRINKLING AT THE FWD MOST POINT OF REPAIR AREAS FASTENERS. REPAIR ACCOMPLISHED PER TIMCO REO-G12679 AND EO DC8-5730-33484-A.
- [SDR IPXA09856170](https://openairdocs.org/sdr/IPXA09856170.md): Skin · misrepaired · May 30, 2009 · N852UP · Doug DC873F · Vertical Stabilizer, Plate/Skin
  > INSPECTION TYPE:SV SURVEY SEQ 852-S4-30418 RT SIDE OF VERTICAL STAB L/E AT STATION XFS 74. 00 EXTERNAL DOUBLER DOES NOT CORRELATE TO SRM. ACCOMPLISHED REPAIR PER TIMCO REO-G12834 REV B AND EO DC8-5530-33667-A.
- [SDR IPXA09856169](https://openairdocs.org/sdr/IPXA09856169.md): Skin · misrepaired · May 30, 2009 · N852UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV SURVEY SEQ 852-W3-28 REPAIR DOUBLER HAS FASTENERS WITH LESS THAN AD SPACING AND LESS THAN 1.5D EDGE DISTANCE. LEFT O/B LEADING EDGE UPPER SKIN XFS 710 TO 761 AT WING FRONT SPAR. REPAIR ACCOMPLISHED PER TIMCO REO-G12772 REV C AND EO DC8-573
- [SDR IPXA09855925](https://openairdocs.org/sdr/IPXA09855925.md): Skin · misrepaired · May 18, 2009 · N852UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:SV SURVEY SEQ 852-W3-33 REPAIR AT LT OTBD FLAP LE LOWER SKIN SAT XF333 20' FWD OF FLAP SPAR DOES NOT CORRELATE TO A SRM REPAIR. REPAIR ACCOMPLISHED PER TIMCO REO-G12642 REV A AND EO DC8-5750-33476-A.
- [SDR IPXA09855879](https://openairdocs.org/sdr/IPXA09855879.md): Structure · misrepaired · May 15, 2009 · N852UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV SURVEY SEQ 852-F1-13 FUSE REPAIR AT STA 430 BETWEEN L26L, DOES NOT COR RELATE TO SRM REPAIR. REPAIR ACCOMPLISHED PER TIMCO REO G12817 REV IR AND EO DC8-5330-3346OA.
- [SDR IPXA09855877](https://openairdocs.org/sdr/IPXA09855877.md): Structure · misrepaired · May 15, 2009 · N852UP · Doug DC873F · Elevator Structure
  > INSPECTION TYPE:SV SURVEY SEQ 852-S2-02 L/E REPAIR DOES NOT CORRELATE TO AN SRM. REPAIR ACCOMPLISHED PER TIMCO REO-G12757 REV B AND EO DC8 5520-33391.
- [SDR IPXA09855876](https://openairdocs.org/sdr/IPXA09855876.md): Skin · dented · May 15, 2009 · N852UP · Doug DC873F · Horizontal Stabilizer, Plate/Skin
  > INSPECTION TYPE:SV SURVEY SEQ 852-SI-05 LT HORIZ STAB L/E DENTED AT REPAIR AT STA XFS 91-2 50. REPAIR ACCOMPLISHED PER DC8-SRM 55-2-1 FIG 4 TR 55-2.
- [SDR IPXA09855858](https://openairdocs.org/sdr/IPXA09855858.md): Skin · misrepaired · May 13, 2009 · N852UP · Doug DC873F · Ailerons
  > INSPECTION TYPE:SVC SURVEY SEQ 852-W3-31 REPAIR DOUBLER AT LT INBD AILERON UPPER EDGE DOES NOT CORRELATE TO SRM REPAIR. REPAIR ACCOMPLISHED PER TIMCO REO-G12538 REV C AND UPS EO DC8-5720-33337-A
- [SDR IPXA09855840](https://openairdocs.org/sdr/IPXA09855840.md): Skin · misrepaired · May 12, 2009 · N852UP · Doug DC873F · Emergency Exits
  > INSPECTION TYPE:SV SURVEY SEQ 852-F1-50 EFN 85219991021 DATA DOES NOT CORRELATE SRM 52-2-0, CENTER OF REPAIR WAS ONE FASTENER ROW, TWO REQUIRED IAW 52-02-00 FIG 2 SHT 3 REV 78. RT OVERWING DOOR FWD REPAIR ACCOMPLISHED PER TIMCO REO-G12761 REV AND EO DC8-5220-
- [SDR IPXA09855839](https://openairdocs.org/sdr/IPXA09855839.md): Skin · damaged · May 12, 2009 · N852UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV SURVEY SEQ 852-W3-06 LT WING L/E SURFACE EDGE DOUBLER XFS 300-341 SEVERAL FASTENERS ARE LESS THAN 1.5 DIAMETERS FROM EDGE OF REPAIR MARKED XFS 320. REPAIR ACCOMPLISHED PER TIMCO REO-G12705 AND EO DC8-5730-33332.
- [SDR IPXA09855859](https://openairdocs.org/sdr/IPXA09855859.md): Skin · misrepaired · May 11, 2009 · N852UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV SURVEY SEQ 852-W4-11, RT CTR LE LWR SKIN STA XFS 303 PREVIOUS REPAIR DID NOT PASS APPENDIX H. REMOVED EXISTING REPAIR, INSTALLED NEW REPAIR IAW REO-G12763 AND UPS EO DC8-5710-33325-A.
- [SDR IPXA09855856](https://openairdocs.org/sdr/IPXA09855856.md): Skin · gouged · May 11, 2009 · N852UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:SV SURVEY SEQ 852-W4-16 RT INBD FLAP INBD END OF LEADING EDGE, PREVIOUS REPAIR DOUBLER GOUGED AND REPAIR FASTENER HAS LESS THAN I.5D EDGE DISTANCE. REMOVED REPAIR. INSTALLED NEW REPAIR IAW REO-G12633 AND UPS EO DC8-5730-33323-A.
- [SDR IPXA09855855](https://openairdocs.org/sdr/IPXA09855855.md): Skin · damaged · May 11, 2009 · N852UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:SV SURVEY SEQ 852-W3-21, LT OTBD FLAP UPPER SURFACE STA XF 346 PREVIOUS REPAIR DOUBLER GOUGED AND FASTENER HIGH WITH SHORT ED. REMOVED PREVIOUS REPAIR, REMOVE DAMAGE. INSTALLED NEW REPAIR IAW REO-G 12688 AND UPS EO DC8-5730-33322-A.
- [SDR IPXA09855853](https://openairdocs.org/sdr/IPXA09855853.md): Skin · damaged · May 11, 2009 · N852UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:SV SURVEY SEQ 852-W3-32, LT OTBD FLAP LWR SKIN STA 220 20 INCH FWD OF FLAP SPAR HAS SHEARED FASTENER AND LESS THAN 4D SPACING. REMOVED EXSITING REPAIR, REMOVED DAMAGE. INSTALLED NEW REPAIR IAW REO-G12751 AND UPS EO DC8-5720-33343-A.
- [SDR IPXA09855804](https://openairdocs.org/sdr/IPXA09855804.md): Structure · misrepaired · May 8, 2009 · N852UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV SURVEY SEQ 852-F1-46 REPAIR DOES NOT CORRELATE TO A SRM REPAIR. REPAIR ACCOMPLISHED PER DC8 SRM 53-2-1 FIG7 SHT 15 TR 53/203.
- [SDR IPXA09855803](https://openairdocs.org/sdr/IPXA09855803.md): Structure · misrepaired · May 8, 2009 · N852UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV SURVEY SEQ NUMBER 852-F1-44 REPAIR CONFIGURATION DOES NOT CORRELATE TO A SRM REPAIR, FS 133 L10R-L11R. REPAIR ACCOMPLISHED PER DC8 SRM 53-2-1 FIG 7 SHT 15 TR 53-203.
- [SDR IPXA09855854](https://openairdocs.org/sdr/IPXA09855854.md): Skin · misrepaired · May 7, 2009 · N852UP · Doug DC873F · Cargo/Baggage Doors
  > INSPECTION TYPE:SV SURVEY SEQ 852-F1-35. D PIT CARGO DOOR EXTERIOR SKIN STA 1034 EXISTING REPAIR DOES NOT CORRELATE TO AN SRM REPAIR. REPAIR FASTER SPACING IS LESS THAN 4D SRM MINIMUM. REMOVED EXISTING REPAIR, REMOVED DAMAGE. INSTALLED NEW REPAIR IAW DC8 SR
- [SDR IPXA09855676](https://openairdocs.org/sdr/IPXA09855676.md): Structure · misrepaired · Apr 24, 2009 · N852UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV SURVEY SEQ 852-F1-27 REPAIR DOUBLER AT STA 1748.5 L20R AND L21R, DOES NOT CORRELATE TO SRM REPAIR. REPAIR ACCOMPLISHED PER DC8 SRM 53-2-1 FIG 7 SHT 12 AND TR 53-203.
- [SDR IPXA09855675](https://openairdocs.org/sdr/IPXA09855675.md): Structure · misrepaired · Apr 24, 2009 · N852UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV SURVEY SEQ 852-F1-28 REPAIR DOUBLER AT STA 1717 TO 1720 L20R AND L49R DOES NOT CORRELATE TO SRM REPAIR. REPAIR ACCOMPLISHED PER DC8-SRM 53-2-1 FIG 7.
- [SDR IPXA09855674](https://openairdocs.org/sdr/IPXA09855674.md): Skin · misrepaired · Apr 24, 2009 · N852UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SV SURVEY SEQ 852-F1-04 LT FUSE STA 57-50 L29L-L30L DOUBLER HAS SEVERAL FASTENERS WITH LESS THAN 1.5 DIA EDGE DISTANCE. REPAIR ACCOMPLISHED PER DC8 SRM DC8 SRM 53-2-0 FIG 13.
- [SDR IPXA09855673](https://openairdocs.org/sdr/IPXA09855673.md): Skin · misrepaired · Apr 24, 2009 · N852UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SV SURVEY SEQ 852-F1-36, FUSE PLUG REPAIR ATTACH FASTENERS SPACING LESS THAN 4D STA 1364 BETWEEN L22R-L23R. REPAIR ACCOMPLISHED PER DC8 SRM 53-2-1 FIG 7 SHT 11 AND T/R53-203.
- [SDR IPXA09855672](https://openairdocs.org/sdr/IPXA09855672.md): Structure · misrepaired · Apr 24, 2009 · N852UP · Doug DC873F · Horizontal Stabilizer Structure
  > INSPECTION TYPE:SV SURVEY SEQ 852-S1-04, LT HORIZ STAB L/E, DOES NOT CORRELATE TO SRM, DOUBLER GAGE THICKER THAN SRM CALLOUT. REPAIR ACCOMPLISHED PER DC8 SRM 55-2-1 FIG 4.
- [SDR IPXA09855610](https://openairdocs.org/sdr/IPXA09855610.md): Skin · damaged · Apr 20, 2009 · N852UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV SURVEY SEQ 852-W4-15 REPAIR DOUBLER HAS FASTENERS WITH SHORT EDGE DISTANCE, RT OTBD L/E LOWER SKIN XFS 712. REPAIR ACCOMPLISHED PER REO-G12675 REV A AND EO DC8-5720-33123-A.
- [SDR IPXA09855608](https://openairdocs.org/sdr/IPXA09855608.md): Access Panel · damaged · Apr 20, 2009 · N852UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV SURVEY SEQ 852-WS-35 LT WING L/E LOWER SURFACE ACCESS PANEL XFS 502 RE PAIR DOUBLER IS.071 BASE STRUCTURE IS.100. INSTALLED REPAIR PER DAC DWG 5761041-3.
- [SDR IPXA09855607](https://openairdocs.org/sdr/IPXA09855607.md): Access Panel · damaged · Apr 20, 2009 · N852UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV SURVEY SEQ 852-W3-34-LT WING L/E LOWER SURFACE ACCESS PANEL, XFS 476 EX EXISTING REPAIR DOUBLER IS.071 AND BASE MATERIAL IS.100. INSTALLED REPAIR PER DAC DWG 5761041.
- [SDR IPXA09855654](https://openairdocs.org/sdr/IPXA09855654.md): Skin · misrepaired · Apr 19, 2009 · N852UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV 852-W4-13 REPAIR DOUBLER CRACKED. RIGHT L/E LOWER SKIN ABOVE NR 4 PYLON XFS 530 35 INCHES FWD OF WING FRONT SPAR. REPAIRED PER DC8 SRM 57-2-01A FIG 2.
- [SDR IPXA09855638](https://openairdocs.org/sdr/IPXA09855638.md): Skin · misrepaired · Apr 19, 2009 · N852UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SV SSN 852-F1-03 REPAIR CONFIGURATION DOES NOT CORRELATE TO A SRM REPAIR. REPAIR ACCOMPLISHED IAW SRM 53-2-0 FIG 1D SHT 3.
- [SDR IPXA09855637](https://openairdocs.org/sdr/IPXA09855637.md): Skin · cracked · Apr 19, 2009 · N852UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV SSN 852-W4-13 REPAIR DOUBLER CRACKED RT LEAD EDGE LWR SKIN ABOVE NR 4 PYLON XFS 530 35 INCH FWD OF WING FWD SPAR. REPAIR ACCOMPLISHED IAW DC8 SRM 57-02-01A FIG 2 SHT 1.
- [SDR IPXA09855640](https://openairdocs.org/sdr/IPXA09855640.md): Cusp Web · cracked · Apr 18, 2009 · N852UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV MAIN CABIN CUSP MEMBRANE CRACKED AT FS 1613 RBL57. REPAIR ACCOMPLISHED IAW DC8 SRM 53-2-0 FIG 25 SHT 4 AND TR53-166.
- [SDR IPXA09855635](https://openairdocs.org/sdr/IPXA09855635.md): Web · cracked · Apr 18, 2009 · N852UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV EFN 85220011042 C PIT RT TUNNEL SUBFLOOR MEMBRANE IS EXFOLIATED AND CRACKED AT RBL 60 BETWEEN FS 1100 AND FS 1120. REMOVED DAMAGE AND FABRICATED DOUBLER PER EO DC8-5330-2159-B. REPAIR ACCOMPLISHED IAW DC8 SRM 53-2-0 FIG 25 SHEETS 4 AND 5 A
- [SDR IPXA09855634](https://openairdocs.org/sdr/IPXA09855634.md): Cusp Web · cracked · Apr 18, 2009 · N852UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV EFN 85220011031 RT UPPER CUSP MEMBRANE CRACKED BETWEEN FS 1600 TO FS 1620. REPAIRED CRACK IN CUSP MEMBRANE PER EO DC8-5330-2159 -B. REPAIR ACCOMPLISHED IAW DC8 SRM 53-2-0 FIG 25 SHT 4 TR53-166.
- [SDR IPXA09855633](https://openairdocs.org/sdr/IPXA09855633.md): Web · punctured · Apr 18, 2009 · N852UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV EFN 85219971087 MAIN CABIN.75 IN PUNCTURED IN MEMBRANE FS 132 RBL65. FABBED AND INSTALLED REPAIR DOUBLER AT CUSP MEMBRANE PER DC8 -5332-2159. REPAIR ACCOMPLISHED IAW SRM 53-2-0 FIG 25 SHT 4 TR53-166.
- [SDR IPXA09855632](https://openairdocs.org/sdr/IPXA09855632.md): Cusp Web · damaged · Apr 18, 2009 · N852UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV EFN 85219971055 LT CUSP FROM FS 120 TO FS 130 DAMAGED. REPAIRED DAMAGED CUSP PER UPS EO DC8-5330-2159-B. REPAIR ACCOMPLISHED IAW DC8 SRM 53-2-0 FIG 25 SHT 4 TR53-166.
- [SDR IPXA09855631](https://openairdocs.org/sdr/IPXA09855631.md): Web · cracked · Apr 18, 2009 · N852UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV EFN 85219971054 HEAVY CORROSION AND CRACK IN FLOOR WEB LT CUSP AREA EXTENDING UNDER FLOOR SUPPORT FITTING FROM FS 260 TO FS 280. REPAIR ACCOMPLISHED IAW SRM 53-2-0 FIG 25 SHT 4 TR53-166.
- [SDR IPXA09855630](https://openairdocs.org/sdr/IPXA09855630.md): Cusp Web · cracked · Apr 18, 2009 · N852UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV EFN 852 19971053 CUSP IS CRACKED FROM LT FS 80 TO FS 100 IN FWD PIT. REPAIRED DAMAGE TO CUSP MEMBRANE PER UPS EO DC8-5330-2159 -B. REPAIR ACCOMPLISHED IAW DC8 SRM 53-20-0 FIG 25 SHT 4 TR53-166.
- [SDR IPXA09855645](https://openairdocs.org/sdr/IPXA09855645.md): Skin · misrepaired · Apr 17, 2009 · N852UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SV SEQ NR 852-F1-33 DOES NOT CORRELATE TO SRM REPAIR. REPAIRED PER DC8 SRM 53-2-1 FIG 7 SHEETS 13 AND 14, TR 53-203.
- [SDR IPXA09855644](https://openairdocs.org/sdr/IPXA09855644.md): Skin · misrepaired · Apr 17, 2009 · N852UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SV SURVEY SEQUENCE 852-F1-25, REPAIR DOUBLER AT STA 1749 BETWEEN L19L AND L20L, DOES NOT CORRELATE TO SRM REPAIR. REPAIRED PER DC8 SRM 53-2-1 FIG 7 SHEETS 11 AND 13 + TR 53-203.
- [SDR IPXA09855643](https://openairdocs.org/sdr/IPXA09855643.md): Skin · misrepaired · Apr 17, 2009 · N852UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SV SURVEY SEQUENCE 852-F1-24, VENT REPAIR DOUBLER, STA 1718.5 BETWEEN L18 L AND L19L DOES NOT CORRELATE TO SRM REPAIR. REPAIRED PER DC8 SRM 53-2-1 FIG 7 SHEET 11 AND 13 + TR 53-203.
- [SDR IPXA09855655](https://openairdocs.org/sdr/IPXA09855655.md): Doubler · damaged · Apr 16, 2009 · N852UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV 852-W4-10 REPAIR DOUBLER CHAFED/GOUGED AND HAS FASTENERS WITH SHORT E D RT WING LEADING EDGE LOWER SKIN XFS 257, 47 INCHES FWD OF WING FRONT SPAR (ABOVE NR 3 PYLON). REPAIRED PER DC8 SRM 57-2-1A FIG 2.
- [SDR IPXA09855653](https://openairdocs.org/sdr/IPXA09855653.md): Skin · misrepaired · Apr 16, 2009 · N852UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:SV SURVEY SEQUENCE 852-W3-20, REPAIR DOUBLER AT LEFT I/B FLAP UPPER SKIN DOES NOT CORRELATE TO SRM. REPAIRED PER DC8 SRM 57-02-01 FIG 002Q SHT 1.
- [SDR IPXA09855641](https://openairdocs.org/sdr/IPXA09855641.md): Skin · misrepaired · Apr 16, 2009 · N852UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:SV SURVEY SEQ 852-W3-20 REPAIR DOUBLER AT LT INBD FLAP UPPER SKIN DOES NOT CORRELATE TO SRM. REPAIR ACCOMPLISHED IAW DC8 SRM 57-2-1 FIG 2Q SHT 1.
- [SDR IPXA09855639](https://openairdocs.org/sdr/IPXA09855639.md): Skin · misrepaired · Apr 16, 2009 · N852UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SV SSN 852-F1-01 REPAIR DOES NOT CORRELATE WITH SRM REFERENCES. REPAIR ACCOMPLISHED IAW DC8 SRM 53-2-0 FIG 1D SHT 3.
- [SDR IPXA09855636](https://openairdocs.org/sdr/IPXA09855636.md): Skin · damaged · Apr 16, 2009 · N852UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV SSN 852-W4-10 REPAIR DOUBLER CHAFED/GOUGED AND HAS FASTENERS WITH SHORT ED RT WING LEAD, EDGE LWR SKIN XFS 257 47 INCH, FWD OF WING FWD SPAR ABOVE NR 3 PYLON. REPAIR ACCOMPLISHED IAW DC8 SRM 57-2-1A FIG 2.
- [SDR IPXA09855642](https://openairdocs.org/sdr/IPXA09855642.md): Skin · misrepaired · Apr 14, 2009 · N852UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SV SEQ NR 852-F1-05, FLUSH REPAIR, FASTENERS 2 IN FILLER COUNTERSINKS DEEP. REPAIRED PER DC8 SRM 53-2-1 FIG 7 SHT 15 (TR 53-203) ESTABLISH REPETITIVE INSPECTIVE PER SRM 53-2-1 FIG 5 (TR 53-190) 53-2-1 PF 35 AND 51-5-5 PG 1 PAR 2A(1).
- [SDR IPXA09855795](https://openairdocs.org/sdr/IPXA09855795.md): Rib · cracked · Apr 10, 2009 · N852UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:SV LT WING L/E (XFS 309) SUPPORT RIB CRACKED AND REPAIR DOUBLER IS CRACKED. REMOVED AND REPLACED REPAIR PER DC8 SRM 57-2-0 FIG 2 SHT 2.
- [SDR IPXA09855183](https://openairdocs.org/sdr/IPXA09855183.md): Support Angle · damaged · Mar 28, 2009 · N852UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV CUSP SUPPORT ANGLE BETWEEN STA 1600 TO 1620 RBL 60 HAS DRILL DAMAGE ON SUB FLOOR LEG. INSTALL REPAIR PER DAC DWG 9750448.
- [SDR IPXA09855973](https://openairdocs.org/sdr/IPXA09855973.md): Frame · cracked · Feb 18, 2009 · N852UP · Doug DC873F · Wing Spar
  > INSPECTION TYPE:SV CRACKED FORMER AT RT WING LE STA XFS 303 BOTTOM AFT. FABRICATED NEW FORMER AND INSTALLED PER DAC DWG 5769530 REV F, AND DC8 SRM 51-1-20D REV 78.
- [SDR IPXA09855721](https://openairdocs.org/sdr/IPXA09855721.md): Skin · misrepaired · Feb 18, 2009 · N852UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SV SS 852-F1-46, REPAIR DOES NOT CORRELATE TO A SRM, FS 92 - FS 100, L20R - L21R. ACCOMPLISHED THE FOLLOWING: ADDED ADDITIONAL FASTENERS REQUIRED BY DC8-SRM 53-2-1 FIG 7 SHT 15 AND TR 53-203.
- [SDR IPXA09856125](https://openairdocs.org/sdr/IPXA09856125.md): Skin · misrepaired · Feb 17, 2009 · N852UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:SV SS 852-W4-24, RT O/B FLAP LOWER SKIN REPAIR AT XF 215, DOES NOT HAVE.5 MINIMUM CORNER. REPAIRED PER TIMCO REO-G12754 REV B, AND UPS DC8-5750-33544-A.
- [SDR IPXA09856130](https://openairdocs.org/sdr/IPXA09856130.md): Skin · misrepaired · Feb 16, 2009 · N852UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SV SS 852-F1-39, REPAIR DOES NOT CORRELATE TO A SRM, NO FASTENER CALL OUT FOR DOUBLER THICKNESS FS 351-FS 368, L18R-L21R. REPAIRED PER REO-G12770 REV C, AND UPS DC8-5330-33639-A.

Next page: https://openairdocs.org/deregistered/N852UP-2014-09-15/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 = 'N852UP' AND deregistration_id = 'N852UP-2014-09-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N852UP-2014-09-15/reports

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