# Service difficulty reports: N797UP, cancelled Dec 13, 2012

A list on [N797UP, cancelled Dec 13, 2012](https://openairdocs.org/deregistered/N797UP-2012-12-13.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 · 195 reports

- [SDR UPS03840165](https://openairdocs.org/sdr/UPS03840165.md): Landing Gear · collapsed · Feb 11, 2003 · N797UP · Doug DC871F · Nose/Tail Landing Gear
  > NOSE LANDING GEAR COLLAPSED AFTER ENGINE SHUT DOWN, APPROX. 4 FT FRO M BLOCK. AIRCRAFT SOLD IN "AS IS" CONDITION
- [SDR UPS02839620](https://openairdocs.org/sdr/UPS02839620.md): Skin · cracked · Oct 5, 2002 · N797UP · Doug DC871F · Cargo/Baggage Doors
  > INSPECTION TYPE:N/A PIT 31 DOOR AFT TOP CORNER OUTER SKIN HAS 4 INCH CRACK THROUGH 3 RIVETS. REMOVED DAMAGED REPAIRED IAW 52-2-0 FIG 2.
- [SDR UPS02839619](https://openairdocs.org/sdr/UPS02839619.md): Web · cracked · Oct 5, 2002 · N797UP · Doug DC871F · Cargo/Baggage Doors
  > PIT NR 31 CARGO DOOR WEB CRACKED. AT STA 40, APPROX. 12 INCHES BELOW MAIN DECK FLOOR. REMOVED DAMAGED SECTION OF WEB. T G 35574 10-6-02 FABRICATED & INSTALLED REPLACEMENT SECTION OF WEB PER DC-8 SRM 53-2-0
- [SDR UPS01836191](https://openairdocs.org/sdr/UPS01836191.md): Battery Pack · discharged · Jun 25, 2001 · N797UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERY PACK DISCHARGED. REMOVED AND REPLACED EMERGENCY BATTERY PACK, CKS OK P/N ON-OFF 5708458-503, S/N OFF FT L 158 ON 2085.
- [SDR UPS01835643](https://openairdocs.org/sdr/UPS01835643.md): Skin · cracked · Apr 11, 2001 · N797UP · Doug DC871F · Horizontal Stabilizer Structure
  > INSPECTION TYPE:C2,3 LEFT HORIZONTAL STAB. L/E. SKIN IS CRACKED AND DENTED BEYOND LIMITS XFS 150. REPAIRED SKIN I.A.W. SRM. 55-2-1 FIG. 4
- [SDR UPS01835680](https://openairdocs.org/sdr/UPS01835680.md): Floorbeam · corroded · Apr 5, 2001 · N797UP · Doug DC871F · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C2,3 STA. 140 FLOORBEAM IS CORRODED BEYOND LIMITS BETWEEN RBL. 50 AND RBL. 60. REPAIRED FLOORBEAM I.A.W. 8110-3 APPROVED DH SK 779-363
- [SDR UPS01835594](https://openairdocs.org/sdr/UPS01835594.md): Rib · cracked · Apr 4, 2001 · N797UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 327. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2
- [SDR UPS01835771](https://openairdocs.org/sdr/UPS01835771.md): Doubler · cracked · Apr 2, 2001 · N797UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE: C2,3. RIGHT WING OB L/E. INTERNAL WRAPAROUND DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED, AND REPLACED DOUBLER I.A.W. DWG. 5769600,AND SRM. 51-1-21
- [SDR UPS01835606](https://openairdocs.org/sdr/UPS01835606.md): Shear Tie · cracked · Apr 2, 2001 · N797UP · Doug DC871F · Fuselage Main, Structure
  > INSPECTION TYPE:C2,3 STA. 660 SHEAR TIE CLIP IS CRACKED BETWEEN LONG. 26L-27L REPAIRED SHEARTIE I.A.W. SRM. 53-2-0 FIG. 2A
- [SDR UPS01835773](https://openairdocs.org/sdr/UPS01835773.md): Fitting · corroded · Mar 31, 2001 · N797UP · Doug DC871F · Fuselage Main, Structure
  > INSPECTION TYPE:C2,3 STA 320 BATHTUB FITTING IS CRACKED BETWEEN LONG. 29L-30L REMOVED AND REPLACED FITTING I.A.W. DWG. 3755822,AND SRM.51-1-20D
- [SDR UPS01835770](https://openairdocs.org/sdr/UPS01835770.md): Fitting · cracked · Mar 31, 2001 · N797UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2,3 STA. 450 LONG. 36 SPLICE FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 3750330,AND SRM. 51-1-20D
- [SDR UPS01835653](https://openairdocs.org/sdr/UPS01835653.md): Fitting · corroded · Mar 31, 2001 · N797UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2,3 STA. 300 BETWEEN LONG. 28L-29L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755822,AND SRM.51-1-20D
- [SDR UPS01835652](https://openairdocs.org/sdr/UPS01835652.md): Fitting · corroded · Mar 31, 2001 · N797UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2,3 STA. 300 BETWEEN LONG. 29L-30L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755822,AND SRM. 51-1-20D
- [SDR UPS01835644](https://openairdocs.org/sdr/UPS01835644.md): Strap · cracked · Mar 31, 2001 · N797UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2,3 STA. 465 STRAP IN MIDDLE OF LONG. 33R IS CRACKED REMOVED,FABRICATED,AND REPLACED STRAP I.A.W. DWG. 3750349,AND SRM. 51-1-20D,51-1-21
- [SDR UPS01835642](https://openairdocs.org/sdr/UPS01835642.md): Fitting · cracked · Mar 31, 2001 · N797UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2,3 STA. 100 UPPER FRAME TO CUSP FITTING IS CRACKED AND CORRODED BEYOND LIMITS AT LONG. 21R REMOVED AND REPLACED FITTING I.A.W. DWG. 4597643,AND SRM. 51-1-20D
- [SDR UPS01835598](https://openairdocs.org/sdr/UPS01835598.md): Angle · cracked · Mar 31, 2001 · N797UP · Doug DC871F · Wing Miscellaneous Structure
  > INSPECTION TYPE:C2,3 LEFT WING L/E. ATTACH ANGLE IS CRACKED AT XW454. REMOVED, FABRICATED, AND REPLACED ANGLE I.A.W. DWG. 9753297,AND SRM. 51-1-20D,51-1-21
- [SDR UPS01835769](https://openairdocs.org/sdr/UPS01835769.md): Fitting · cracked · Mar 30, 2001 · N797UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C2,3 STA. 390 LONG. 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3754473-1N,AND SRM. 51-1-20D
- [SDR UPS01835745](https://openairdocs.org/sdr/UPS01835745.md): Skin · corroded · Mar 30, 2001 · N797UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C2,3 FUSELAGE EXTERNAL SKIN IS CORRODED BEYOND LIMITS AT STA. 857 BETWEEN LONGERON 16R-17R. REPAIRED SKIN I.A.W. SRM. 53-2-0 FIG. 22A
- [SDR UPS01835711](https://openairdocs.org/sdr/UPS01835711.md): Fitting · corroded · Mar 30, 2001 · N797UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2,3 STA. 70 LOWER CUSP TO FRAME FITTING IS CORRODED BEYOND LIMITS AT LONGERON 21R. REMOVED AND REPLACED FITTING I.A.W. DWG. 3610130,AND SRM. 51-1-21, 51-3-0
- [SDR UPS01835679](https://openairdocs.org/sdr/UPS01835679.md): Skin · corroded · Mar 30, 2001 · N797UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C2,3 STA. 920 LONG. 18R EXTERNAL SKIN IS CORRODED BEYOND LIMITS. REPAIRED SKIN I.A.W. 8110-3 APPROVED DH SK 797-908
- [SDR UPS01835651](https://openairdocs.org/sdr/UPS01835651.md): Longeron · cracked · Mar 30, 2001 · N797UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2,3 STA. 879-902,LONG. 24L IS CRACKED. REPAIRED LONG. I.A.W. SRM. 53-2-2 FIG. 5
- [SDR UPS01835604](https://openairdocs.org/sdr/UPS01835604.md): Rib · cracked · Mar 30, 2001 · N797UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 366.5 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2
- [SDR UPS01835603](https://openairdocs.org/sdr/UPS01835603.md): Rib · cracked · Mar 30, 2001 · N797UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XS 448.581. REPAIRED RIB I.A.W. SRM.57-2-0 FIG.2
- [SDR UPS01835602](https://openairdocs.org/sdr/UPS01835602.md): Rib · cracked · Mar 30, 2001 · N797UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XW 466.651. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2
- [SDR UPS01835601](https://openairdocs.org/sdr/UPS01835601.md): Rib · cracked · Mar 30, 2001 · N797UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 372.750. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2
- [SDR UPS01835600](https://openairdocs.org/sdr/UPS01835600.md): Rib · cracked · Mar 30, 2001 · N797UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 347.75. REPAIRED RIB I.A.W. SRM. 57-2-0,FIG. 2
- [SDR UPS01835599](https://openairdocs.org/sdr/UPS01835599.md): Rib · cracked · Mar 30, 2001 · N797UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XFS. 360.250. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2
- [SDR UPS01835597](https://openairdocs.org/sdr/UPS01835597.md): Rib · cracked · Mar 30, 2001 · N797UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XS 442.185. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2
- [SDR UPS01835595](https://openairdocs.org/sdr/UPS01835595.md): Doubler · cracked · Mar 30, 2001 · N797UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE:C2,3 LEFT WING L/E. INTERNAL DOUBLER IS CRACKED AT XW 257.5. REMOVED,FABRICATED,AND REPLACED DOUBLER I.A.W. DWG. 5769589,AND SRM. 51-1-20D,51-1-21
- [SDR UPS01835593](https://openairdocs.org/sdr/UPS01835593.md): Rib · cracked · Mar 30, 2001 · N797UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C2,3 RIGHT WING L/E. UPPER RIB IS CRACKED AT FASTENER END AT XFS 722.5. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2
- [SDR UPS01835592](https://openairdocs.org/sdr/UPS01835592.md): Rib · cracked · Mar 30, 2001 · N797UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C2,3 RIGHT WING L/E. UPPER RIB IS CRACKED AT FASTENER END AT XFS 772.5. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2
- [SDR UPS01835747](https://openairdocs.org/sdr/UPS01835747.md): Skin · corroded · Mar 29, 2001 · N797UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE:C2,3 RIGHT WING AUX. TANK UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 193. REPAIRED SKIN I.A.W. SRM. 57-2-1 FIG. 37 & 38
- [SDR UPS01835746](https://openairdocs.org/sdr/UPS01835746.md): Skin · corroded · Mar 29, 2001 · N797UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE:C2,3 RIGHT WING L/E. UPPER SKIN IS CORRODED BEYOND LIMITS BETWEEN XFS 341 TO XOLDI 6.225. REPAIRED SKIN I.A.W. 8110-3 APPROVED DH SK 797-486
- [SDR UPS01835710](https://openairdocs.org/sdr/UPS01835710.md): Pan · cracked · Mar 29, 2001 · N797UP · Doug DC871F · Cargo/Baggage Doors
  > INSPECTION TYPE:C2,3 C-PIT DOOR PAN IS CRACKED AT STA. 1180 AT LONG. 32R APPROX. REPAIRED PAN I.A.W. SRM. 52-2-0 FIG. 4
- [SDR UPS01835709](https://openairdocs.org/sdr/UPS01835709.md): Floorbeam · corroded · Mar 29, 2001 · N797UP · Doug DC871F · Fuselage Main, Floor Beam
  > INSPECTION TYPE: C2,3 STA. 1580 FLOORBEAM IS CORRODED BEYOND LIMITS AT RBL. 48. REPAIRED FLOORBEAM I.A.W. 8110-3 APPROVED DH SK 797-605
- [SDR UPS01835660](https://openairdocs.org/sdr/UPS01835660.md): Longeron · cracked · Mar 29, 2001 · N797UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2,3 STA. 1766 LONG. 17L IS CRACKED AND CORRODED REPAIRED LONGERON I.A.W. SRM.53-2-2 FIG. 10
- [SDR UPS01835611](https://openairdocs.org/sdr/UPS01835611.md): Skin · corroded · Mar 29, 2001 · N797UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE:C2,3 RT. WING L/E. UPPER SKIN IS CORRODED BEYOND LIMITS XFS 603.75 AT IB SLING ATTACH POINT. REPAIRED SKIN I.A.W. SRM. 57-3-0 FIG. 18,AND E.O. DC8-5720-7767-A
- [SDR UPS01835610](https://openairdocs.org/sdr/UPS01835610.md): Skin · corroded · Mar 29, 2001 · N797UP · Doug DC871F · Horizontal Stabilizer, Plate/Skin
  > INSPECTION TYPE:C2,3 RT. H-STAB. L/E. SKIN IB. SIDE OF STA. XFS 178 IS CORRODED BEYOND LIMITS. REPAIRED SKIN I.A.W. SRM. 55-2-1 FIG. 4
- [SDR UPS01835609](https://openairdocs.org/sdr/UPS01835609.md): Skin · corroded · Mar 29, 2001 · N797UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE:C2,3 RT AUX TANK UPPER SKIN IS CORRODED BEYOND LIMITS BETWEEN XFS 20-26.25 REPAIRED SKIN I.A.W. SRM. 57-2-0 FIG. 37 & 38,AND DHM. ENGINEERING RESPONSE.
- [SDR UPS01835768](https://openairdocs.org/sdr/UPS01835768.md): Skin · cracked · Mar 28, 2001 · N797UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE: C1, 3, LEFT WING CENTER L/E SKIN IS CRACKED AT XW 257.5 REPAIRED SKIN I.A.W. E.O. DC8-5720-7767-A
- [SDR UPS01835748](https://openairdocs.org/sdr/UPS01835748.md): Skin · corroded · Mar 28, 2001 · N797UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE:C2,3 LEFT WING L/E. UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 760. REPAIRED SKIN I.A.W. SRM. 57-2-1 FIG. 38
- [SDR UPS01835708](https://openairdocs.org/sdr/UPS01835708.md): Fitting · corroded · Mar 28, 2001 · N797UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2,3 STA. 1160 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG. 36 TO 35R. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755845,AND SRM. 53-2-0 FIG. 2D
- [SDR UPS01835659](https://openairdocs.org/sdr/UPS01835659.md): Fitting · corroded · Mar 28, 2001 · N797UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2,3 STA. 879 RBL. 63 CUSP TO FRAME FITTING BELOW FLOOR PANEL IS CORRODED BEYOND LIMITS REMOVED AND REPLACED FITTING I.A.W. DWG. 5643483,AND SRM. 51-1-20D, 51-1-21
- [SDR UPS01835649](https://openairdocs.org/sdr/UPS01835649.md): Longeron · cracked · Mar 28, 2001 · N797UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2,3 STA. 1260-1280 LONG. 35L IS CRACKED. REPAIRED LONGERON I.A.W. 8110-3 APPROVED DH SK 797-370
- [SDR UPS01835647](https://openairdocs.org/sdr/UPS01835647.md): Keelbeam · cracked · Mar 28, 2001 · N797UP · Doug DC871F · Fuselage Main, Keel
  > INSPECTION TYPE:C2,3 LT. KEEL BEAM WEB IS CRACKED AT STA. 879. REPAIRED WEB I.A.W. SRM. 53-2-0 FIG. 23
- [SDR UPS01835645](https://openairdocs.org/sdr/UPS01835645.md): Fitting · cracked · Mar 28, 2001 · N797UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2,3 STA. 1150 BETWEEN LONG. 35R-34R BATHTUB FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 3755843,AND SRM. 53-2-0 FIG. 2D
- [SDR UPS01835596](https://openairdocs.org/sdr/UPS01835596.md): Fitting · cracked · Mar 28, 2001 · N797UP · Doug DC871F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C2,3 STA. 1240, LONG. 35L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG.3758495,AND SRM. 51-1-20D
- [SDR UPS01835608](https://openairdocs.org/sdr/UPS01835608.md): Skin · corroded · Mar 28, 2001 · N797UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE:C2,3 LEFT WING AUX. TANK UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 193, 8-10 INCHES AFT OF L/E. REPAIRED SKIN I.A.W. SRM. 57-2-0 FIG. 2A
- [SDR UPS01835607](https://openairdocs.org/sdr/UPS01835607.md): Fitting · cracked · Mar 28, 2001 · N797UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2,3 STA. 1180 LONG. 34R BATHTUB FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 3755841,AND SRM. 53-2-0 FIG. 2D
- [SDR UPS01835605](https://openairdocs.org/sdr/UPS01835605.md): Fitting · cracked · Mar 28, 2001 · N797UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2,3 STA. 1180 BATHTUB BETWEEN LONG. 27L-28L IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 3755842,AND SRM. 53-2-0 FIG. 2D

Next page: https://openairdocs.org/deregistered/N797UP-2012-12-13/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 = 'N797UP' AND deregistration_id = 'N797UP-2012-12-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N797UP-2012-12-13/reports

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