# Service difficulty reports: N779UP, cancelled May 20, 2010

A list on [N779UP, cancelled May 20, 2010](https://openairdocs.org/deregistered/N779UP-2010-05-20.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 · 174 reports

- [SDR UPS02839890](https://openairdocs.org/sdr/UPS02839890.md): Strap · cracked · Oct 25, 2002 · N779UP · Doug DC871F · Wing Main, Frame Structure
  > INSPECTION TYPE: C2, RT WING HAS A CRACKED LONGERON 64 END FITTING-STRAP, AND LOWER SPAR IS CRACKED 1/2 INCH FROM EDGE OF SPAR TO FASTENER HOLE AT XRS 450. NDT VERIFIED 1/2 INCH CRACK AT XRS 450 FROM EDGE OF SPAR TO FASTENER HOLE, REMOVED, FABRICATED AND INS
- [SDR UPS02839838](https://openairdocs.org/sdr/UPS02839838.md): Fitting · corroded · Oct 25, 2002 · N779UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2 STA 300 BETWEEN LONG 35L TO 36 BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755822, AND SRM 53-2-0 FIG 2D.
- [SDR UPS02839844](https://openairdocs.org/sdr/UPS02839844.md): Longeron · corroded · Oct 22, 2002 · N779UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2 STA 300-305 LONG 35L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON 35L SECTION BETWEEN STA 290 TO 330 IAW SRM 53-2-2 FIG 10.
- [SDR UPS02839843](https://openairdocs.org/sdr/UPS02839843.md): Longeron · corroded · Oct 22, 2002 · N779UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2 STA 300-305 LONGERON 35R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON SECTION BETWEEN STA 290 TO 330 AT LONG 35R IAW SRM 53-2-2 FIG 10.
- [SDR UPS02839832](https://openairdocs.org/sdr/UPS02839832.md): Fitting · cracked · Oct 22, 2002 · N779UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2 STATION 1040-1050 LONGERON 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 51-1-20D.
- [SDR UPS02839847](https://openairdocs.org/sdr/UPS02839847.md): Fitting · cracked · Oct 21, 2002 · N779UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2 STA 70 LONG 22L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4611159, AND SRM 51-1-20D.
- [SDR UPS02839840](https://openairdocs.org/sdr/UPS02839840.md): Fitting · corroded · Oct 21, 2002 · N779UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2 STA 320 BETWEEN LONG 33L TO 34L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755822, AND SRM 53-2-0 FIG 2D.
- [SDR UPS02839839](https://openairdocs.org/sdr/UPS02839839.md): Fitting · corroded · Oct 21, 2002 · N779UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2 STA 300 BETWEEN LONG 33L TO 34L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755822, AND SRM 53-2-0 FIG 2D.
- [SDR UPS02839828](https://openairdocs.org/sdr/UPS02839828.md): Longeron · corroded · Oct 16, 2002 · N779UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2 AFT ACCY COMPARTMENT LONG 33L CORRODED BEYOND LIMITS BETWEEN STATION 1540 TO 1545. REMOVED LONGERON SECTION FROM STA 1515 TO 1550 AT LONG 33L, FABRICATED AND INSTALLED LONGERON SECTION AND SPLICES IAW SRM 53-2-2, FIG 10, 53-4-1 FIG 43.
- [SDR UPS02839850](https://openairdocs.org/sdr/UPS02839850.md): Door Frame · cracked · Oct 15, 2002 · N779UP · Doug DC871F · Cargo/Baggage Doors
  > INSPECTION TYPE:C2 A-PIT DOOR FRAME IS CRACKED AFT SIDE OF 3RD UPPER HOOK FROM FWD END ON DOOR AT APPROX STA 300 AT LONG 23R ON DOOR. REMOVED FRAME SECTIONS, FABRICATED AND INSTALLED 2EA FRAME SECTIONS AND DOUBLERS IAW SRM 52-2-0 FIG 2 AND DWG 9754100.
- [SDR UPS02839829](https://openairdocs.org/sdr/UPS02839829.md): Fitting · cracked · Oct 15, 2002 · N779UP · Doug DC871F · Horizontal Stabilizer Miscellaneous Structure
  > INSPECTION TYPE:C2 RIGHT HORIZONTAL STAB LOWER PLANK FITTING IS CRACKED AT XFS 46. REMOVED AND REPLACED FITTING IAW DWG 3701427, AND SRM 51-1-21.
- [SDR UPS02839872](https://openairdocs.org/sdr/UPS02839872.md): Longeron · corroded · Oct 14, 2002 · N779UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2 STA 300-320 LONG 34L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED LONGERON REPAIR SECTION AND SPLICES IAW SRM 53-2-2 FIG 10.
- [SDR UPS02839845](https://openairdocs.org/sdr/UPS02839845.md): Skin · cracked · Oct 14, 2002 · N779UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C2 RADIOGRAPHIC (X-RAY) INSPECTION DETECTED 2 CRACKS ON THE L1 DOOR LOWER AFT CORNER APPROX 5.25 INCHES AND.419 INCH AT STA 60 LONG 20L. REMOVED EXISTING DOUBLER, CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED
- [SDR UPS02839831](https://openairdocs.org/sdr/UPS02839831.md): Skin · cracked · Oct 14, 2002 · N779UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE:C2 RIGHT WING CENTER L/E LOWER SKIN IS CRACKED AT FASTENER HOLE AT XFS 347.75. STOP DRILLED CRACK, NDT VERIFIED CRACK TERMINATES AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-4087-B.
- [SDR UPS02839827](https://openairdocs.org/sdr/UPS02839827.md): Skin · cracked · Oct 14, 2002 · N779UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE:C2 LEFT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGER 11. CUTOUT CRACKED SKIN, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-2-1 FIG 10.
- [SDR UPS02839836](https://openairdocs.org/sdr/UPS02839836.md): Longeron · cracked · Oct 13, 2002 · N779UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C2 STA 1766 LONG 17R AND END FITTING ARE CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON AND END FITTING IAW DWG 5649327, 4772397, SRM 51-1-20D, 51-1-21.
- [SDR UPS02839830](https://openairdocs.org/sdr/UPS02839830.md): Fitting · cracked · Oct 13, 2002 · N779UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C2 LONG 17L AND END FITTING IS CRACKED AT STA 1766 AFT SIDE OF BULKHEAD. REMOVED AND REPLACED LONGERON AND END FITTING IAW DWG 5649327, 4772397 AND SRM 51-1-20D, 51-1-21, LONGERON FABRICATED IAW DWG 5649327.
- [SDR UPS02839826](https://openairdocs.org/sdr/UPS02839826.md): Skin · cracked · Oct 13, 2002 · N779UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 75 AT STRINGER 9. CUTOUT CRACKED SKIN, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 10.
- [SDR UPS02839871](https://openairdocs.org/sdr/UPS02839871.md): Skin · cracked · Oct 11, 2002 · N779UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM THE L2 DOOR LOWER FWD CORNER AND REPAIR PER SRM 53-2-0 FIG 18, APPROX STA 1620 LONG 10L. REMOVED STEEL DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER I
- [SDR UPS02839849](https://openairdocs.org/sdr/UPS02839849.md): Skin · cracked · Oct 11, 2002 · N779UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM THE L2 DOOR UPPER AFT CORNER AND REPAIR PER SRM 53-2-0 FIG 18, STA 1660 AT LONG 10L. REMOVED STEEL DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 18.
- [SDR UPS02839848](https://openairdocs.org/sdr/UPS02839848.md): Skin · cracked · Oct 11, 2002 · N779UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM THE R2 DOOR UPPER AFT CORNER AND REPAIR PER SRM 53-2-0 FIG 16, STA 1660 LONG 11R AND SKIN AND INTERNAL DOUBLER ARE CRACKED. REMOVED STEEL DOUBLER, CUTOUT DAMAGED AREA ON SKIN AND INTERNAL DOUBLER, NDT VERIFIED NO C
- [SDR UPS02839837](https://openairdocs.org/sdr/UPS02839837.md): Skin · cracked · Oct 11, 2002 · N779UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM THE R1 DOOR UPPER FWD CORNER AND REPAIR PER SRM 53-2-0 FIG 14. REMOVE STEEL DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER,TRIPLER AND FILLER IAW SRM 53-2-0 FIG 14.
- [SDR UPS01837269](https://openairdocs.org/sdr/UPS01837269.md): Fastener · corroded · Nov 9, 2001 · N779UP · Doug DC871F · Stabilizer Actuator
  > INSPECTION TYPE:N/A SEVERAL FASTENERS CORRODED IN COMPARTMENT 60 HORZ STABILIZER ACTUATING MECHANISM AREA ITEM SUBMITTED BY FOG TEAM. REMOVED AND REPLACED FASTENERS. CLEANED CORROSION FROM MARKET BOTLS APPROX 120 EA HUCK FASTENERS EXTENDING THROUGH LIGHTENIN
- [SDR UPS01837254](https://openairdocs.org/sdr/UPS01837254.md): Stiffener · cracked · Nov 5, 2001 · N779UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:B COMPARTMENT 60 AFT PRESS BULKHEAD J-BEAM 5TH FROM BOTTOM OF LT SIDE HAS CRACK AS MARKED. STOP DRILLED CRACK REF DC8-5310-15663-A14596. FABRICATED UPPER REPAIR BRACKET PER PRELIMINARY EO DC8-5310-15663-A DP 70236.
- [SDR UPS01835062](https://openairdocs.org/sdr/UPS01835062.md): Bottle · discharged · Feb 24, 2001 · N779UP · Doug DC871F · Escape Slide
  > INSPECTION TYPE:IN, CABIN DOOR EMERGENCY SLIDE BOTTLE PRESS LOW. REMOVED AND REPLACED CABIN DOOR EMERGENCY SLIDE AS PER MM 25-60-00.
- [SDR UPS00834569](https://openairdocs.org/sdr/UPS00834569.md): Skin · damaged · Dec 27, 2000 · N779UP · Doug DC871F · Trailing Edge Flaps
  > INSPECTION TYPE:PFLT LT WING INBD FLAP T/E HAS A 1/2 HOLE 2 INCHES INBD OF OUTBD EDGE. REPAIRED HOLE IN FLAP AS PER SRM 57-2-1. INSTALL A REPAIR DOUBLER.
- [SDR UPS00834260](https://openairdocs.org/sdr/UPS00834260.md): Line · leaking · Oct 26, 2000 · N779UP · Doug DC871F · Crew Oxygen System
  > INSPECTION TYPE:N/A, COURIER''S O2 REGULATOR PROBLEM. *S/D* REPLACED BROKEN O2 LINE, OPS CK NORMAL.
- [SDR UPS00834259](https://openairdocs.org/sdr/UPS00834259.md): Slide · inoperative · Oct 26, 2000 · N779UP · Doug DC871F · Escape Slide
  > INSPECTION TYPE:N/A, ESCAPE SLIDE WILL NOT ARM. ATTACHED GIRT BAR.
- [SDR UPS00833850](https://openairdocs.org/sdr/UPS00833850.md): Longeron · cracked · Oct 6, 2000 · N779UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C1, STA 1350 LONG 34L IS CRACKED. REMOVED AND REPLACED LONGERON IAW DWG 3758593, AND SRM 51-1-20D, 51-1-21.
- [SDR UPS00833852](https://openairdocs.org/sdr/UPS00833852.md): Fitting · damaged · Oct 4, 2000 · N779UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1, STA 1690 LONG 32L END HAS HOLES WITH NO EDGE DISTANCE. REMOVED AND REPLACED FITTING IAW DWG 4641324, AND SRM 51-1-20D.
- [SDR UPS00833851](https://openairdocs.org/sdr/UPS00833851.md): Longeron · damaged · Oct 4, 2000 · N779UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C1, STA 1690 - 1776 LONG 32L HAS HOLES IN RADIUS. REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG 5649329, AND SRM 51-1-20D.
- [SDR UPS00833848](https://openairdocs.org/sdr/UPS00833848.md): Intercostal · cracked · Oct 4, 2000 · N779UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1, STA 240 - 260 LONG 33L INTERCOSTAL IS CRACKED. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 5750726, AND SRM 51-1-21.
- [SDR UPS00833859](https://openairdocs.org/sdr/UPS00833859.md): Longeron · corroded · Oct 3, 2000 · N779UP · Doug DC871F · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C1, STA 1705 LONG 30L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG 5649329, AND SRM 51-1-20D.
- [SDR UPS00833858](https://openairdocs.org/sdr/UPS00833858.md): Shear Tie · corroded · Oct 3, 2000 · N779UP · Doug DC871F · Fuselage Main, Structure
  > INSPECTION TYPE:C1, STA 1760 LONG 28L - 28R 8 SHEAR TIES ARE CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED SHEAR TIES IAW 5612148, AND SRM 51-1-21.
- [SDR UPS00833853](https://openairdocs.org/sdr/UPS00833853.md): Finger Doubler · cracked · Oct 3, 2000 · N779UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1, STA 1690 - 1890 FINGER DOUBLERS IS CRACKED AT LONG 28R. REMOVED, FABRICATED, AND REPLACED DOUBLERS IAW DWG 5649328, AND SRM 51-1-21.
- [SDR UPS00834221](https://openairdocs.org/sdr/UPS00834221.md): Doubler · cracked · Oct 2, 2000 · N779UP · Doug DC871F · Wing, Plate/Skin
  > INSPECTION TYPE:C1, LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 335.25. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-20D, 51-1-21.
- [SDR UPS00833849](https://openairdocs.org/sdr/UPS00833849.md): Rib · cracked · Oct 2, 2000 · N779UP · Doug DC871F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C1, LEFT WING L/E LOWER RIB IS CRACKED AT XFS 310.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.
- [SDR UPS00833703](https://openairdocs.org/sdr/UPS00833703.md): Battery Pack · inoperative · Sep 7, 2000 · N779UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:P/F, ON PREFLIGHT LIGHTS DO NOT COME ON DURNIG TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK GOOD.
- [SDR UPS00833630](https://openairdocs.org/sdr/UPS00833630.md): Gearbox · inoperative · Aug 21, 2000 · N779UP · Doug DC871F · Stabilizer Control System
  > INSPECTION TYPE:N/A, HORIZONTAL STABILIZER STOPPED MOVING AFTER LANDING AT 4.0 DEGREES. FOUND RIVET STUCK IN HORZ STAB GEARBOX ASSY. REMOVED AND REPLACED GEARBOX ASSY AND BOTH JACKSCREW ASSYS.
- [SDR UPS00833394](https://openairdocs.org/sdr/UPS00833394.md): Lanyard · broken · Jul 21, 2000 · N779UP · Doug DC871F · Escape Slide
  > INSPECTION TYPE:N/A, SLIDE COVER LANYARD BROKEN AT CABLE (SLIDE AT ENTRY DOOR). REPLACED MAIN ENTRY DOOR SLIDE COVER LANYARD AND SECURED SLIDE LANYARD INSTALLED PER IPC 25-62-00.
- [SDR UPS00832630](https://openairdocs.org/sdr/UPS00832630.md): Battery Pack · discharged · May 16, 2000 · N779UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTING WILL NOT TEST. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK.
- [SDR UPS00831537](https://openairdocs.org/sdr/UPS00831537.md): Clip · broken · Feb 7, 2000 · N779UP · Doug DC871F · Escape Slide
  > INSPECTION TYPE:N/A, MAIN CABIN ESCAPE SLIDE INOP, MOUNTING BRACKET BOTTOM CLIP BROKEN. REMOVED AND REPLACED CLIP AND INSTALLED ESCAPE SLIDE.
- [SDR UPS99831146](https://openairdocs.org/sdr/UPS99831146.md): Light · inoperative · Nov 22, 1999 · N779UP · Doug DC871F · Emergency Lighting
  > EMERGENCY EXIT LIGHTS FAILED TO COME ON DURING PREFLIGHT CHECK. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK PN ON 5208458-503, PN OFF 570845 8-503 SN ON 976 SN OFF 2054, OPS CHECK GOOD.
- [SDR UPS99830756](https://openairdocs.org/sdr/UPS99830756.md): Battery Pack · discharged · Sep 28, 1999 · N779UP · Doug DC871F · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY LIGHTS DID NOT OPERATE WHEN TESTED. REMOVED AND REPLACED EMERGENCY BATTERY PACK ASSY PER M/M 33-50-01, OPS CHECK GOOD.
- [SDR UPS99830588](https://openairdocs.org/sdr/UPS99830588.md): Skin · cracked · Sep 9, 1999 · N779UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:N/A, FUSELAGE SKIN DAMAGE JUST AFT OF THE NLG W/W HAS AN 11 INCH CRACK. DUE TO LEFT NOSE TIRE TREAD SEPARATION. *S/D* DAMAGE REMOVED AS REQ'D RHODES 75705 RSB 0596 1 QC 2, FABRICATED AND DRILLED DOUBLER PER UPS DRAWING UPS-SDF-9900296 F BPT
- [SDR UPS99829759](https://openairdocs.org/sdr/UPS99829759.md): Skin · cracked · Jun 4, 1999 · N779UP · Doug DC871F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:N/A, 13.25 INCH CRACK LOCATED AT LONGERON L28 ON SKIN OF AIPLANE FS 1704 TO FS 1717 (FOR AND AFT). *S/D* REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS IAW DC8 SRM 53-2-1 FIG 4. INSTALLED PARTS IAW SRM 53-2-1, 51-1-23 D AND 51-1-21.
- [SDR UPS98828159](https://openairdocs.org/sdr/UPS98828159.md): Doubler · cracked · Nov 4, 1998 · N779UP · Doug DC871F · Wing Miscellaneous Structure
  > INSPECTION TYPE-C3, RT WING L/E LWR SKIN AT XFS 598.375 THE INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLACED THE INTERNAL DOUBLER IAW DWG 5769600 AND SRM 51-1-20D & 51-1-21.
- [SDR UPS98828108](https://openairdocs.org/sdr/UPS98828108.md): Angle · cracked · Nov 3, 1998 · N779UP · Doug DC871F · Wing Miscellaneous Structure
  > INSPECTION TYPE-D, VERTICAL ATTACHMENT ANGLE ON THE I/B SIDE OF THE NR 1 STUB WING CRACKED IN RADIUS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-21 AND DWG 9753297.
- [SDR UPS98828112](https://openairdocs.org/sdr/UPS98828112.md): Jamb · cracked · Nov 1, 1998 · N779UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-D, DOOR JAMB AFT ENTRY DOOR AFT LOWER CORNER HAS 2 INCH CRACK. REPAIRED IAW SRM 53-2-0.
- [SDR UPS98828158](https://openairdocs.org/sdr/UPS98828158.md): Intercostal · cracked · Oct 29, 1998 · N779UP · Doug DC871F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C3, FS 1120 TO 1140 AT LONG 33L THE INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 9753792 AND SRM 51-1-20D & 51-1-21.

Next page: https://openairdocs.org/deregistered/N779UP-2010-05-20/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 = 'N779UP' AND deregistration_id = 'N779UP-2010-05-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N779UP-2010-05-20/reports

---
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