# Service difficulty reports: N812UP, cancelled Jan 11, 2011

A list on [N812UP, cancelled Jan 11, 2011](https://openairdocs.org/deregistered/N812UP-2011-01-11.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 5 · 228 reports

- [SDR UPS08851598](https://openairdocs.org/sdr/UPS08851598.md): Lamp · inoperative · Jan 31, 2008 · N812UP · Doug DC873F · Emergency Lighting
  > GLARESHIELD HAS ONE EMERGENCY LIGHT INOP. RELAMPED AND TESTED IAW MM 33-13-00-2. OPS CHECK GOOD.
- [SDR UPS07851077](https://openairdocs.org/sdr/UPS07851077.md): Tab · punctured · Oct 28, 2007 · N812UP · Doug DC873F · Elevator, Tab Structure
  > INSPECTION TYPE:N/A LEFT ELEVATOR INBOARD CONTROL TAB HAS A.3125 INCH PUNCTURE ON BOTTOM OF TAB. TRANS TO NRC 107944. CHECKED LEFT I/B ELEVATOR AREA ON AIRCRAFT SIDE FOR HARDWARE/ATTACH FITTING. NO DISCREPANCY FOUND. OK TO INSTALL ELEVATOR CONTROL TAB. I
- [SDR UPS07850635](https://openairdocs.org/sdr/UPS07850635.md): Battery Pack · faulty · Sep 8, 2007 · N812UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A DURING PREFLIGHT EMERGENCY LIGHTS BATTERY CHARGING C/B POPPED AND WOULD NOT RESET. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK PER MM 33-50-01-2. SYSTEM OPS CHECKS GOOD.
- [SDR UPS07850457](https://openairdocs.org/sdr/UPS07850457.md): Floor Panel · damaged · Aug 16, 2007 · N812UP · Doug DC873F · Fuselage Floor Panel
  > INSPECTION TYPE:N/A PIT 31 HAS HOLE IN FLOOR PANEL. A.375 INCH HOLE IN PIT 31 FLOOR PANEL IS LOCATED 33 INCHES AFT OF DOORSILL AND 41 INCHES LEFT OF CENTERLINE. ACCOMPLISHED INTERIM REPAIR PER EO DC8-5320-8724, APPROX A. DEFERRAL OPENED FOR PERMANENT REPAI
- [SDR UPS06848713](https://openairdocs.org/sdr/UPS06848713.md): Battery Pack · inoperative · Nov 22, 2006 · N812UP · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHT INOP. FOUND EMERGENCY EXIT LIGHT BATTERY PACK LOW DURING PREDEPARTURE CHECK
- [SDR UPS06846826](https://openairdocs.org/sdr/UPS06846826.md): Wire · chafed · May 9, 2006 · N812UP · Doug DC871F · Electrical Power System Wiring
  > SMOKE IN THE COCKPIT FROM BEHIND FE PANEL CLEARED AFTER 30 SECONDS DECLARED EMERGENCY AND LANDED ASAP. OCCURRED DURING DESCENT 12000' 275KTS. REPAIRED CHAFED WIRE L 893L20 BEHIND NR 4 M FUEL QUANTITY GAUGE IAW AMM 20 50 01 8 P 3.
- [SDR UPS06846766](https://openairdocs.org/sdr/UPS06846766.md): Doubler · cracked · Apr 23, 2006 · N812UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 EXTERIOR OF TAILSKID FAIRING JUST FWD OF DOUBLER HAS RIPPED FASTENER HOLE AND AFT EDGE IS GOUGED. REMOVED DOUBLER IAW SRM 53-2-0 FIG 1F. FABRICATED AND INSTALLED REPAIR DOUBLER,AND FILLER AT STA 1766 L34L TO L34R IAW SRM 53-02-01 FIG 7, 51
- [SDR UPS06846756](https://openairdocs.org/sdr/UPS06846756.md): Intercostal · cracked · Apr 20, 2006 · N812UP · Doug DC873F · Fuselage Miscellaneous Structure
  > FOUND CRACKED INTERCOSTAL AT FS 520 BELOW L31R. REMOVED CRACKED INTERCOSTAL AT FS 520 BELOW L31R IAW SRM 51-1-21. FABRICATED, DRILLED, REAMED AND INSTALLED INTERCOSTAL AT FS 520 L31R IAW DWG 51616520, SRM 51-3-2,51-01-08, AND SRM 51-01-20D-0.
- [SDR UPS06846745](https://openairdocs.org/sdr/UPS06846745.md): Structure · corroded · Apr 7, 2006 · N812UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION TYPE:C1 EXFOLIATION CORROSION FOUND AT STA 70 STRUCTURE BETWEEN L31R AND L32R. CUT OUT DAMAGED STRUCTURE AT STA 70 BETWEEN L31R AND L33R IAW SRO 08538006, AND SRM 53-02-05. FABRICATED AND INSTALLED DOUBLER CHORD, AND SPLICES IAW SRO 08538006, AND
- [SDR UPS06846765](https://openairdocs.org/sdr/UPS06846765.md): Skin · corroded · Apr 6, 2006 · N812UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C1 AFTER REMOVAL OF B-PIT SCUFF PLATE TO FOM NDT INSP IAW E0 DC8 5330-20206-D FOUND CORROSION ON SKIN STA 518 L27R. CUT OUT DAMAGED AREA AT STA 518 L27R IAW SAA EA NR 008-5330-01-A0150. FABRICATED AND INSTALLED -2 FILLER, -3 TAPERED SHIM, -4
- [SDR UPS06846764](https://openairdocs.org/sdr/UPS06846764.md): Fitting · corroded · Apr 1, 2006 · N812UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 STA 340 L30L FITTING EXFOLIATED, FINGER DOUBLER CORRODED AND MISSING HILOCK COLLAR. REMOVED FITTING AT STA 340 L30L IAW SRM 51-1-20D. REMOVED CORROSION FROM FINGER DOUBLER AND FOUND TO BE WITHIN LIMITS PER SRM 51-1-8. INSTALLED END FITTIN
- [SDR UPS06846746](https://openairdocs.org/sdr/UPS06846746.md): Frame · corroded · Mar 31, 2006 · N812UP · Doug DC873F · Fuselage Main, Frame
  > INSPECTION TYPE:CC1 STA 1120 AT L36 FRAME HAS EXFOLIATION CORROSION. CUT OUT DAMAGED SECTION OF FRAME AT STA 1120 L36 IAW SRM 53-2-0 FIG 2. FABRICATED AND INSTALLED FILLER, ANGLES, AND FRAME REPAIR ANGLE IAW SRM 53-02-00-002, 53-02-00 FIG 2, AND SRM 51-1-8.
- [SDR UPS06846744](https://openairdocs.org/sdr/UPS06846744.md): Fitting · corroded · Mar 31, 2006 · N812UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 STA 1150 BETWEEN L36 AND L35R BATHTUB FITTING CORRODED AND GOUGED. REMOVED BATHTUB FITTING AT STA 1150 L36 AND L35R IAW SRM 51-1-20D. FABRICATED REPAIR ANGLES IAW SRM 53-02-00. INSTALLED REPAIR ANGLES AND NEW BATHTUB FITTING AT STA 1150 L
- [SDR UPS06846748](https://openairdocs.org/sdr/UPS06846748.md): Cusp Web · cracked · Mar 29, 2006 · N812UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 STA 1280 CUSP CRACK AT LT FITTING. REMOVED DAMAGED CUSP AT STA 1260-1300 LT IAW SRM 53-02-05-0 FIG 015A. FABRICATED AND INSTALLED EXTERNAL DOUBLER, CUSP SEGMENT AND FRAME FITTINGS AT STA 1280 LT STA 1260-1300 IAW SRM 53-02-05-0 FIG 015A, A
- [SDR UPS06846691](https://openairdocs.org/sdr/UPS06846691.md): Frame · corroded · Mar 29, 2006 · N812UP · Doug DC873F · Fuselage Main, Frame
  > FOUND HEAVY CORROSION ON STA 1700 FRAME L36-L35L FWD SIDE. CUT OUT SECTION OF CORRODED FRAME FROM STA 1700 BETWEEN L36 AND L35R IAW SRM 53-2-0. FABRICATED AND INSTALLED 4 REPAIR SPLICES, -7 SPLICE AND FRAME SECTION REPAIR IAW DWG 5612142, AND SRM'S 53-02-00
- [SDR UPS06846689](https://openairdocs.org/sdr/UPS06846689.md): Fitting · cracked · Mar 29, 2006 · N812UP · Doug DC873F · Fuselage Main, Attach Fittings
  > FOUND STA 902 LONGERON 4R FITTING IS CRACKED. R & R END FITTING AT STA 902 LONGERON 4R IAW SRM 51-1-20D, AND SRM 51-1-21.
- [SDR UPS06846666](https://openairdocs.org/sdr/UPS06846666.md): Fitting · cracked · Mar 29, 2006 · N812UP · Doug DC873F · Fuselage Main, Attach Fittings
  > FOUND STA 1160 L20R FITTING CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW SRM 51-1-20D AND DWG NR 9750419.
- [SDR UPS06846662](https://openairdocs.org/sdr/UPS06846662.md): Attach Angle · corroded · Mar 29, 2006 · N812UP · Doug DC873F · Fuselage Main, Attach Fittings
  > ATTACH ANGLE AT STA 820 UNDER FLOOR AT RBL65 FWD OF FRAME HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING STA 820 RBL 65 IAW SRM 51-3-2 AND 51-1-20D.
- [SDR UPS06846642](https://openairdocs.org/sdr/UPS06846642.md): Angle · cracked · Mar 29, 2006 · N812UP · Doug DC873F · Fuselage Main, Structure
  > FOUND STA 1766 LONGERON 6R BRACKET CRACKED. REMOVED ANGLE BRACKET AT STA 1766 L6R IAW SRM 51-01-20D. FABRICATED AND INSTALLED ANGLE BRACKET AT STA 1766 L6R IAW DWG 5773844, AND SRM 51-1-20D.
- [SDR UPS06846688](https://openairdocs.org/sdr/UPS06846688.md): Fitting · cracked · Mar 28, 2006 · N812UP · Doug DC873F · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1 STA 902 LONGERON 4L FITTING IS CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 902 L4L IAW SRM 51-3-2, 51-1-20D AND SRM 51-1-21.
- [SDR UPS06846665](https://openairdocs.org/sdr/UPS06846665.md): Fitting · cracked · Mar 28, 2006 · N812UP · Doug DC873F · Fuselage Main, Attach Fittings
  > FOUND STA 680 L2L FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-1-20D AND 51-3-0.
- [SDR UPS06846664](https://openairdocs.org/sdr/UPS06846664.md): Fitting · cracked · Mar 28, 2006 · N812UP · Doug DC873F · Fuselage Main, Attach Fittings
  > FOUND STA 902 L9L FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0, 51-1-20D AND 51-1-21.
- [SDR UPS06846663](https://openairdocs.org/sdr/UPS06846663.md): Fitting · cracked · Mar 28, 2006 · N812UP · Doug DC873F · Fuselage Main, Longeron/Stringer
  > FOUND STA 1690 LONGERON END FITTING CRACKED LONGERON 24R. REMOVED AND REPLACED FITTING IAW SRM 51-1-21,51-1-21 AMD 51-3-0.
- [SDR UPS06846681](https://openairdocs.org/sdr/UPS06846681.md): Fitting · cracked · Mar 27, 2006 · N812UP · Doug DC873F · Fuselage Main, Attach Fittings
  > STA 680 LONGERON 6L FITTING IS CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 680 L6L IAW SRM 51-1-20D, SRM 51-1-21, 51-3-0.
- [SDR UPS06846641](https://openairdocs.org/sdr/UPS06846641.md): Fitting · cracked · Mar 27, 2006 · N812UP · Doug DC873F · Fuselage Main, Structure
  > FOUND STA 680 LONGERON 3L FITTING CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 680 L3L IAW SRM 51-01-20D, 51-03-00-0, 51-03-01-0.
- [SDR UPS06846747](https://openairdocs.org/sdr/UPS06846747.md): Stiffener · corroded · Mar 26, 2006 · N812UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1 RT W/W STA 857 BULKHEAD VERTICAL STIFFENER CORRODED BEYOND LIMITS RBL 46, 13" BELOW CEILING. REMOVED VERTICAL STIFFENER AT STA 857 RBL40 IAW SRM 51-01-21, AND SRM 51-01-20D. FABRICATED AND INSTALLED ANGLES,"L" ANGLES, AND VERTICAL STIFFENE
- [SDR UPS06846735](https://openairdocs.org/sdr/UPS06846735.md): Skin · cracked · Mar 26, 2006 · N812UP · Doug DC873F · Landing Gear Doors
  > INSPECTION TYPE:C1 EXTERIOR SKIN CRACK, TORN ON RMLG IB DOOR AT STRUT EXTENSION. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 52-06-03, 52-02-00-0, AND 51-1-21.
- [SDR UPS06846692](https://openairdocs.org/sdr/UPS06846692.md): Skin · corroded · Mar 26, 2006 · N812UP · Doug DC873F · Fuselage Main, Plate/Skin
  > FOUND STRUCTURE CORRODED FWD OF LT BOTTLE BOLT BARREL NUT, LT W/W FWD UPPER OB CORNER. REPAIRED EXTERNAL SKIN CORROSION AT STA 857 LONGERON 24L AT BAYONET FITTING IAW UPS ENGINEERING FILE NR DC8-53-20543, SAA EA NR 008-5320-01-A0137, BAC SERVICE REQUEST 1-176
- [SDR UPS06846690](https://openairdocs.org/sdr/UPS06846690.md): Stiffener · corroded · Mar 26, 2006 · N812UP · Doug DC873F · Fuselage Miscellaneous Structure
  > HEAVY CORROSION UNDER VERTICAL STIFFENER ON LT W/W 857 BULKHEAD LBL 45, 13" BELOW CEILING. REMOVED VERT STIFFENER AT FS 857 LBL45 IAW SRM 51-01-21. FABRICATED AND INSTALLED REPAIR ANGLE, REPLACEMENT STIFFENER AND SUPPORT ANGLES AT FS 857 LBL45 IAW DWG 564343
- [SDR UPS06846614](https://openairdocs.org/sdr/UPS06846614.md): Skin · corroded · Mar 25, 2006 · N812UP · Doug DC873F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT SPLICE BETWEEN FUSELAGE AND TAILCONE BETWEEN LONGERON 34L- 34R HAS CORROSION APPEARS TO GO UNDER DOUBLER ON FUSELAGE SIDE STA 1890. REMOVED DOUBLER, REMOVED CORROSION FROM SKIN AND FOUND TO BE WITHIN LIMITS. FABRICATED AND INSTALLED DOUBLER
- [SDR UPS06846615](https://openairdocs.org/sdr/UPS06846615.md): Skin · dented · Mar 23, 2006 · N812UP · Doug DC873F · Fuselage Main, Plate/Skin
  > DENTS 2 EACH AFT OF SERVICE DOOR L-2 AT STA 1670 L17L. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM53-2-1 FIG 10.
- [SDR UPS05845298](https://openairdocs.org/sdr/UPS05845298.md): Microphone · inoperative · Aug 31, 2005 · N812UP · Doug DC873F · Audio Integrating System
  > CAPTAINS O2 MASK MIC INOP.
- [SDR UPS04843415](https://openairdocs.org/sdr/UPS04843415.md): Battery Pack · discharged · Oct 26, 2004 · N812UP · Doug DC873F · Emergency Lighting
  > EMERGENCY LIGHTS BATTERY LOW ON PREFLIGHT CHECK. REPLACED EMERGENCY LIGHTS BATTERY PACK. OPS CK GOOD.
- [SDR UPS04843200](https://openairdocs.org/sdr/UPS04843200.md): Battery Pack · inoperative · Sep 27, 2004 · N812UP · Doug DC873F · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS INOP. ALL SWITCHES & BREAKERS WERE OFF PRIOR TO TEST. REPLACED BATTERY PACK, OPS CHECK OK.
- [SDR UPS04842991](https://openairdocs.org/sdr/UPS04842991.md): Slide · deteriorated · Aug 20, 2004 · N812UP · Doug DC873F · Escape Slide
  > GIRT BAR CABLE UNHOOKED FROM RAFT. UPON FURTHER INSPECTION FOUND SEVERAL AREAS OF DETERIORATION ON SLIDE. REMOVED AND REPLACED DOOR SLIDE IAW MM 25-60-01-2.
- [SDR UPS04842378](https://openairdocs.org/sdr/UPS04842378.md): Control Panel · failed · May 14, 2004 · N812UP · Doug DC873F · AC Generation System
  > N/A DURING TAXI OUR AND JUST BEFORE TAKEOFF, WE GOT A BUSS POWER FAIL LIGHT AND NR 4 GEN UNPARRALLED LIGHT ON. SMOKE BEGAN TO ACCUMULATE IN THE COCKPIT. TAXIED BACK TO RAMP. FOUND NR 4 GCP TO HAVE A HARD FAILURE. SUSPECT NR 4 GCP AS CAUSE OF SMOKE. RAN A/C PN
- [SDR UPS04842168](https://openairdocs.org/sdr/UPS04842168.md): Seat Track · corroded · Apr 8, 2004 · N812UP · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C3 STATION 786 TO 798 BL 0 SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED SEAT TRACK SECTION BETWEEN STATION 750 TO 810 IAW SRM 53-2-3 FIG 14.
- [SDR UPS04842125](https://openairdocs.org/sdr/UPS04842125.md): Web · corroded · Apr 6, 2004 · N812UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C3, STATION 1190 LONG 33L UPPER WEB IS CORRODED BEYOND LIMITS, WEB BELOW C-PIT DOOR. BLENDED OUT CORROSION, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 25.
- [SDR UPS04842121](https://openairdocs.org/sdr/UPS04842121.md): Fitting · corroded · Apr 4, 2004 · N812UP · Doug DC873F · Wing, Attach Fittings
  > INSPECTION TYPE: C3, LEFT WING FLAP HINGE 219 CANOE FITTING HAS PITTING CORROSION. MILLED OUT CORROSION, FABRICATED AND INSTALLED REPAIR FILLERS IAW SB 27-164.
- [SDR UPS04842224](https://openairdocs.org/sdr/UPS04842224.md): Intercostal · cracked · Apr 3, 2004 · N812UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C3 STATION 25 AT LONG 21L ANGLE IN FWD ENTRY DOOR FWD JAMB IS CRACKED. REMOVED, CRACKED INTERCOSTAL, FABRICATED AND INSTALLED INTERCOSTAL IAW DWG 5597646 AND SRM 51-1-20D, 51-1-21.
- [SDR UPS04842237](https://openairdocs.org/sdr/UPS04842237.md): Frame · corroded · Apr 2, 2004 · N812UP · Doug DC873F · Fuselage Main, Frame
  > INSPECTION TYPE: C3, STATION 1040 FRAME AND FRAME CAP ARE CORRODED BEYOND LIMITS AT LONG. 35L CUTOUT DAMAGED FRAME AT STATION 1040 LONG. 35L, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW DC8-53A-010 AND REPLACED FRAME CAP IAW SRM. 53-1-0,51-1-20D,51-1
- [SDR UPS04842231](https://openairdocs.org/sdr/UPS04842231.md): Splice · cracked · Apr 2, 2004 · N812UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C3 LONG 35L SPLICE FITTING IS CRACKED STATION 1040-1060. REMOVED AND REPLACED FITTING IAW DWG 3750545 AND SRM 51-1-20D.
- [SDR UPS04842230](https://openairdocs.org/sdr/UPS04842230.md): Attach Fitting · cracked · Apr 2, 2004 · N812UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C3 INTERCOSTAL ATTACH FITTING IS CRACKED AT STATION 1150 AT LONG 33R. REMOVED AND REPLACED INTERCOSTAL IAW DWG 4758514 AND SRM 51-1-20D.
- [SDR UPS04842229](https://openairdocs.org/sdr/UPS04842229.md): Attach Fitting · cracked · Apr 2, 2004 · N812UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C3 INTERCOSTAL ATTACH FITTING IS CRACKED AT STATION 1140 AT LONG 35R. REMOVED AND REPLACED FITTING IAW DWG 3758497 AND SRM 51-1-20D.
- [SDR UPS04842226](https://openairdocs.org/sdr/UPS04842226.md): Bracket · cracked · Apr 2, 2004 · N812UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C3 CIRCUMFERENTIAL TIE BRACKET IS CRACKED AT LONG 3L AND 3R AT APPROX STATION 1790. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW DWG 5612148 AND SRM 51-1-21, 51-1-20D.
- [SDR UPS04842167](https://openairdocs.org/sdr/UPS04842167.md): Frame · corroded · Apr 2, 2004 · N812UP · Doug DC873F · Fuselage Main, Frame
  > INSPECTION TYPE:C3 STATION 1060 FRAME IS CORRODED BEYOND LIMITS AT LONG 35L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8-53A-010.
- [SDR UPS04842166](https://openairdocs.org/sdr/UPS04842166.md): Shear Tie · corroded · Apr 2, 2004 · N812UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION TYPE:C3 STATION 1000 BETWEEN LONG 28L TO 29L SHEAR TIE IS CORRODED. REMOVED, FABRICATED AND REPLACED SPLICE PLATE AND FILLER IAW SRM 53-2-0 FIG 2A AND 2B.
- [SDR UPS04842124](https://openairdocs.org/sdr/UPS04842124.md): Frame · corroded · Apr 2, 2004 · N812UP · Doug DC873F · Fuselage Main, Frame
  > INSPECTION TYPE: C3, STATION 1040 FRAME IS CORRODED AT LONG 36. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8-53A-010.
- [SDR UPS04842266](https://openairdocs.org/sdr/UPS04842266.md): Fitting · corroded · Apr 1, 2004 · N812UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE: C3, RT WING FLAP HINGE 98 CANOE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED CANOE FITTING I.A.W. DWG. 5614372,M/M.27-51-12, SAA SK 812-411,AND UPS ENGINEERING FILE NUMBER DC8-57-20109
- [SDR UPS04842238](https://openairdocs.org/sdr/UPS04842238.md): Rib · cracked · Apr 1, 2004 · N812UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE: C3, LEFT WING INBOARD STUB WING UPPER RIB IS CRACKED AT XS 250. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED 2 ANGLE DOUBLERS IAW SRM. 57-2-0 FIG. 2

Next page: https://openairdocs.org/deregistered/N812UP-2011-01-11/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 = 'N812UP' AND deregistration_id = 'N812UP-2011-01-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N812UP-2011-01-11/reports

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