# Service difficulty reports: N806UP, cancelled Aug 12, 2010 A list on [N806UP, cancelled Aug 12, 2010](https://openairdocs.org/deregistered/N806UP-2010-08-12.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 7 · 343 reports - [SDR UPS08852686](https://openairdocs.org/sdr/UPS08852686.md): Skin · corroded · Jul 7, 2008 · N806UP · Doug DC873F · Fuselage Main, Plate/Skin > CORROSION RT LWR FUSE AFT OF THE E&E DOOR APPROX. STA 70. STARTED ECA FORM 011382. INSTALLED TIME LIMITED REPAIR IAW EO DC8-5330-29905A. ALL WORK PERFORMED ON ECA FORMS 011382 AND 011385. REPAIR DEFERRED FOR 24 MONTHS. - [SDR UPS08852628](https://openairdocs.org/sdr/UPS08852628.md): Battery Pack · failed · Jul 2, 2008 · N806UP · Doug DC873F · Emergency Lighting > ON PRE-DEPARTURE CK, EMERGENCY EXIT LIGHT CK FAILED. FOUND SW IN ON POSITION. REPLACED AND TESTED BATTERY PACK IAW 33-50-01-2 CKS OK. - [SDR UPS08852014](https://openairdocs.org/sdr/UPS08852014.md): Battery Pack · inoperative · Apr 11, 2008 · N806UP · Doug DC873F · Emergency Lighting > EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-50-01-2 PARA 4. OPS CHECK GOOD. - [SDR UPS08851953](https://openairdocs.org/sdr/UPS08851953.md): Light · intermittent · Mar 31, 2008 · N806UP · Doug DC873F · Emergency Lighting > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INTERMITTENT ON OPS CHECK. PERFORMED OPS CHECK OF EMERGENCY LIGHTS REF MM 33-50-02-2. OPS CHECK. - [SDR UPS07851308](https://openairdocs.org/sdr/UPS07851308.md): Battery Pack · inoperative · Dec 14, 2007 · N806UP · Doug DC873F · Emergency Lighting > EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-50-01-2 AND TESTED. - [SDR UPS07851275](https://openairdocs.org/sdr/UPS07851275.md): Battery Pack · discharged · Dec 8, 2007 · N806UP · Doug DC873F · Emergency Lighting > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD PER MM 33-50-02-2. - [SDR UPS07851058](https://openairdocs.org/sdr/UPS07851058.md): Slide · unsecure · Oct 26, 2007 · N806UP · Doug DC873F · Escape Slide > ESCAPE SLIDE CAME LOOSE. RESECURED ESCAPE SLIDE TO FWD ENTRY DOOR B DC8 25-60. - [SDR UPS07848853](https://openairdocs.org/sdr/UPS07848853.md): Light · no test · Jan 11, 2007 · N806UP · Doug DC873F · Emergency Lighting > EMERGENCY LIGHTS WOULD NOT TEST. INSTALLED SERVICEABLE EMERGENCY LIGHT BATTERY AND RELAY UNIT ASSY PER AMM 33-50-01. OPS CK NORMAL. - [SDR UPS07848852](https://openairdocs.org/sdr/UPS07848852.md): Battery · inoperative · Jan 2, 2007 · N806UP · Doug DC873F · Emergency Lighting > EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND TESTED OK PER MM 33-50-01-2. - [SDR UPS06848801](https://openairdocs.org/sdr/UPS06848801.md): Light · inoperative · Dec 27, 2006 · N806UP · Doug DC873F · Emergency Lighting > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK GOOD PER MM 3-50-01-2. - [SDR UPS06847782](https://openairdocs.org/sdr/UPS06847782.md): Doubler · gouged · Aug 22, 2006 · N806UP · Doug DC873F · Trailing Edge Flaps > INSPECTION TYPE:C1-3 STA 219 LT FLAP FOUND O/B VERT DOUBLER AND LWR ATTACH ANGLE GOUGED OUT OF LIMITS. REMOVED DAMAGED DOUBLER AND ATTACH ANGLE AT LT FLAP STA 219 IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPLACEMENT REPAIR WEB, STRAP AND REPAIR ANGLE IAW D - [SDR UPS06847665](https://openairdocs.org/sdr/UPS06847665.md): Fitting · cracked · Jul 31, 2006 · N806UP · Doug DC873F · Wing, Longeron/Stringer > INSPECTION TYPE-C1-3 BOTH STRINGER END FITTINGS ON STRINGER 51 AT XRS 74 ARE CRACKED NR 2 MAIN TANK. REMOVED BOTH STRINGER END FITTINGS AT STR 51 XRS 74 NR 2 MAIN TANK IAW SRM 51-1-20D. LOCATED AND DRILLED UP, AND INSTALLED 2 END FITTINGS AT STR 51 AT STA XR - [SDR UPS06847663](https://openairdocs.org/sdr/UPS06847663.md): Fitting · corroded · Jul 29, 2006 · N806UP · Doug DC873F · Fuselage Main, Attach Fittings > BATH TUB FITTING EXFOLIATED OUT OF LIMITS AT A-PIT TORQUE BOX STA 280 L33L-L34L. REMOVED BATHTUB FITTING AT STA 280 L33L-L34L IAW SRM 53-02-00, AND SRM 51-1-20D. DRILLED UP AND INSTALLED BATHTUB FITTING AT STA 280 L33L-L34L IAW SRM 53-02-00-0. - [SDR UPS06847710](https://openairdocs.org/sdr/UPS06847710.md): Skin · corroded · Jul 27, 2006 · N806UP · Doug DC873F · Fuselage Main, Plate/Skin > INSPECTION TYPE: C1-3 D-PIT BELLY SKIN REQUIRES REPLACEMENT DUE TO OUT OF LIMITS CORROSION AT L35R-36 STA 1490-1350. REMOVED AND REPLACED BELLY SKIN AT STA 1490-1350 L31L-L31R IAW SRM 51-1-20D, 51-1-21. - [SDR UPS06847648](https://openairdocs.org/sdr/UPS06847648.md): Attach Fitting · cracked · Jul 26, 2006 · N806UP · Doug DC873F · Wing, Attach Fittings > INSPECTION TYPE:C1/3 NR 1 MAIN TANK REAR SPAR ATTACH TEE FITTING AT XW-408 HAS A 4 INCH CRACK. REMOVED AND REPLACED ATTACH TEE FITTING AT XCW-408 NR1 MAIN TANK. - [SDR UPS06847640](https://openairdocs.org/sdr/UPS06847640.md): Splice · cracked · Jul 25, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/Stringer > INSPECTION TYPE: C1,3 LONGERON SPLICE FITTING CRACKED AT STA 1260 TO 1280 L35L. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-20D - [SDR UPS06847603](https://openairdocs.org/sdr/UPS06847603.md): Fitting · cracked · Jul 21, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/Stringer > INSPECTION TYPE:C1-3 60 HOLE APPROX STA 1800 LONGERON 24L END FITTING IS CRACKED. REMOVED DRILLED UP, AND INSTALLED END FITTING AT STA 1800 L24L IAW SRM 51-1-21, AND SRM 51-1-20D. - [SDR UPS06847574](https://openairdocs.org/sdr/UPS06847574.md): Longeron · cracked · Jul 21, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/Stringer > INSPECTION TYPE:C1-3 CRACKED LONGERON L34R FS 1270 IN C-PIT. REMOVED AND REPLACED LONGERON AT STA 1270 - 1350 L34R IAW SRM 51-1-20D. - [SDR UPS06847651](https://openairdocs.org/sdr/UPS06847651.md): Drag Angle · cracked · Jul 19, 2006 · N806UP · Doug DC873F · Nacelle/Pylon, Main Frame > INSPECTION TYPE:C1, 3 POSSIBLE CRACKS ON BULKHEAD FWD OF CENTER SPAR UPPER BOLT IB DRAG ANGLE. REMOVED, FABRICATED AND INSTALLED DRAG ANGLE IAW SRM 51-1-21, DWG 5615767 AND 51-1-20D. - [SDR UPS06847521](https://openairdocs.org/sdr/UPS06847521.md): Longeron · cracked · Jul 18, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/Stringer > INSPECTION TYPE:C1-3 MAIN CABIN LONGERON END FITTING CRACKED AT STA 905 L9L. REMOVED AND REPLACED LONGERON END FITTING AT STA 905 L9L IAW SRM 51-1-20D, AND SRM 51-01-23-0. - [SDR UPS06847441](https://openairdocs.org/sdr/UPS06847441.md): Longeron Splice · cracked · Jul 18, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/Stringer > INSPECTION TYPE:C1-3 LONGERON SPLICE FITTING CRACKED AT STA 900 TO 920 L1. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 900 TO 920 LONGERON 1 IAW SRM 51-01-20D, AND SRM 51-01-20D. - [SDR UPS06847583](https://openairdocs.org/sdr/UPS06847583.md): Longeron · cracked · Jul 17, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/Stringer > INSPECTION TYPE:C1-3 CRACKED LONGERON L35L FS 1270 C-PIT. REMOVED AND REPLACED LONGERON AT STA 1270 L35L IAW SRM 51-1-20D. - [SDR UPS06847581](https://openairdocs.org/sdr/UPS06847581.md): Longeron · cracked · Jul 17, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/Stringer > INSPECTION TYPE:C1-3 CRACKED LONGERON AT L36 FS 1270 IN C-PIT. REMOVED AND REPLACED LONGERON FROM STA 1270 - 1350 L36 IAW SRM 51-1-20D. - [SDR UPS06847522](https://openairdocs.org/sdr/UPS06847522.md): Finger Doubler · corroded · Jul 17, 2006 · N806UP · Doug DC873F · Fuselage Main, Structure > INSPECTION TYPE:C1-3 9 SHEARED RIVETS ON FINGER DOUBLER IN COCKPIT SUBFLOOR, STA -130 LBL 20. REMOVED CORRODED FINGER DOUBLER IN COCKPIT SUBFLOOR AT STA -130 LBL 20 IAW SRM 51-01-21. FABRICATED AND INSTALLED FINGER DOUBLER IN COCKPIT SUBFLOOR AT STA -130 LBL - [SDR UPS06847747](https://openairdocs.org/sdr/UPS06847747.md): Skin · corroded · Jul 16, 2006 · N806UP · Doug DC873F · Fuselage Main, Structure > INSPECTION TYPE:C1 3 HEAVY CORROSION BETWEEN FUSE SKIN AND FINGER DOUBLER AT STA 1670 L31R IN AFT ACC COMPT. REPAIRED FUSELAGE SKIN FROM FS 1660 TO 1680 IAW SAA EA 008-5330-01- A0329 REV A AND UPS RA DC8-53-20579. - [SDR UPS06847639](https://openairdocs.org/sdr/UPS06847639.md): Fitting · cracked · Jul 15, 2006 · N806UP · Doug DC873F · Fuselage Main, Attach Fittings > INSPECTION TYPE: C1, 3 CRACKED BATHTUB FITTING AT FS 270 L34R IN A-PIT. REMOVED AND REPLACED BATHTUB FITTING. IAW SRM 51-1-20D - [SDR UPS06847638](https://openairdocs.org/sdr/UPS06847638.md): Longeron · corroded · Jul 15, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/Stringer > INSPECTION TYPE: C1,3 AT STA. 270 L33L IS BLOWN OUT. REMOVED WEB, BATHTUB FITTING AND LONGERON. FABRICATED AND INSTALLED LONGERON, SPLICE FITTING,BATHTUB FITTINGS AND REPAIR ANGLES. IAW SRM 51-1-20D, 51-1-21,53-02-00 FIG. 10,51-3-2,53-02-02, DWG 9754913 - [SDR UPS06847526](https://openairdocs.org/sdr/UPS06847526.md): Splice · cracked · Jul 15, 2006 · N806UP · Doug DC873F · Fuselage Main, Plate/Skin > INSPECTION TYPE:C1-3 L31L AT STA 200 TO STA 180 SPLICE IS CRACKED. REMOVED AND REPLACED SPLICE FITTING AT STA 200-180 L31L IAW SRM 51-1-20D, AND SRM 51-03-02. - [SDR UPS06847646](https://openairdocs.org/sdr/UPS06847646.md): Doubler · broken · Jul 14, 2006 · N806UP · Doug DC873F · Cargo/Baggage Doors > INSPECTION TYPE: C1/3 INTERNAL DOUBLER BROKEN AT 6:00 AND 12:00 POSITION UNDER EXTERIOR MAIN CARGO DOOR ACCESS PLATE FOR NR 4 LATCH FABRICATED AND INSTALLED -1 AND -2 INTERNAL DOUBLERS IAW SAA EA 008-5320-01-A0331 DTD.05 AUG 2006 MFG DRAWING NR 5772790-637 REV - [SDR UPS06847584](https://openairdocs.org/sdr/UPS06847584.md): Shear Tie · cracked · Jul 14, 2006 · N806UP · Doug DC873F · Fuselage Internal Mounting Structure > INSPECTION TYPE:C1-3 MAIN CABIN STA 1740 L14L SHEAR TIE CRACKED. REMOVED SHEAR TIE AT STA 1740 L14L IAW SRM 51-01-20D. FABRICATED AND INSTALLED SHEAR TIE AT STA 1740 L14L IAW SRM 51-03-02, 51-1-20D AND DWG 5772706. - [SDR UPS06847439](https://openairdocs.org/sdr/UPS06847439.md): Seat Track · worn · Jul 14, 2006 · N806UP · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings > C1-3 FE'S FWD SEAT TRACK LOCK PINS HOLES WORN. REMOVED AND REPLACED FE'S FWD SEAT TRACK IAW SRM 51-03-00,51-01-22 AND SRM 51-03-00. - [SDR UPS06847435](https://openairdocs.org/sdr/UPS06847435.md): Seat Track · worn · Jul 14, 2006 · N806UP · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings > C1-3 2ND OBSERVERS AFT SEAT TRACK LOCKPIN HOLES WORN. REMOVED AND REPLACED 2ND OBSERVERS AFT SEAT TRACK IAW SRM 51-3-0 51-01-24. - [SDR UPS06847696](https://openairdocs.org/sdr/UPS06847696.md): Spar Cap · cracked · Jul 13, 2006 · N806UP · Doug DC873F · Wing Spar > INSPECTION TYPE:C1-3 LT MLG WHEEL WELL FRONT SPAR CAP STA 857 LBL 36 HAS A CRACK BETWEEN BOLTS. REPAIRED LT MLG WHEEL WELL FRONT SPAR CAP AT STA 857 LBL 36 IAW SAA EA NR 008-5710-01-A0299, UPS EO NR DC8-5710-24870, DOUGLAS DWG SRO 8570009. - [SDR UPS06847641](https://openairdocs.org/sdr/UPS06847641.md): Longeron · corroded · Jul 13, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/Stringer > INSPECTION TYPE: C1,3 AIR CONDITIONING COMPT, L36 IS CORRODED AND CRACKED AT STA.35. REMOVED, FABRICATED AND INSTALLED LONGERON AT FS 35 L36. - [SDR UPS06847582](https://openairdocs.org/sdr/UPS06847582.md): Fitting · cracked · Jul 13, 2006 · N806UP · Doug DC873F · Fuselage Miscellaneous Structure > INSPECTION TYPE:C1-3 LONGERON END FITTING CRACKED AT STA 65 L31L. REMOVED AND REPLACED LONGERON END FITTING AT STA 65 L31L IAW SRM 51-3-0, 51-1-21, AND SRM 51-3-2. - [SDR UPS06847527](https://openairdocs.org/sdr/UPS06847527.md): Rib · cracked · Jul 13, 2006 · N806UP · Doug DC873F · Wing, Rib/Bulkhead > INSPECTION TYPE:C1-3 LT CENTER WING L/E UPPER RIB CRACKED AT XFS 497. STOP DRILLED CRACKED RIB AT LT L/E WING STA XFS 497 IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED DOUBLERS ON RIB AT LT L/E WING STA XFS 497 IAW SRM 57-03-03 FIG 5, AND SRM 51-1-20D. - [SDR UPS06847447](https://openairdocs.org/sdr/UPS06847447.md): Rib · cracked · Jul 13, 2006 · N806UP · Doug DC873F · Wing, Rib/Bulkhead > RT CENTER L/E UPPER RIB AT XFS 415 IS CRACKED. STOP DRILLED CRACK ON RIB AT LT L/E STA XFS 415 IAW SRM 57-2-0. FABRICATED AND INSTALLED REPAIR ANGLES AT LT L/E STA XFS 415 IAW SRM 57-03-03 FIG 5 AND SRM 57-02-00. - [SDR UPS06847446](https://openairdocs.org/sdr/UPS06847446.md): Longeron · cracked · Jul 13, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/Stringer > INSPECTION TYPE:C1-3 RT AFT MAIN CABIN FS 1750 L14R CRACKED AT CANTED FRAME REMOVED CRACKED LONGERON SECTION AT STA 1750 L14R IAW SRM 53-02-02-0 FI FIG 10. FABRICATED AND INSTALLED LONGERON SECTION AT STA 1750 L14R IAW SRM 53-02-02-0 FIG 10, AND SRM 53-05 - [SDR UPS06847444](https://openairdocs.org/sdr/UPS06847444.md): Rib · cracked · Jul 13, 2006 · N806UP · Doug DC873F · Wing, Rib/Bulkhead > LEFT WING CENTER L/E RIB CRACKED AT XFS 328. STOP DRILLED CRACK AT LT WING L/E RIB AT STA XFS 328 IAW SRM 51-03-02. FABRICATED AND INSTALLED REPAIR ANGLES AT LT L/E WING STA XFS 328 IAW SRM 57-03-03 FIG 5, AND SRM 57-02-00. - [SDR UPS06847438](https://openairdocs.org/sdr/UPS06847438.md): Rib · cracked · Jul 13, 2006 · N806UP · Doug DC873F · Wing, Rib/Bulkhead > LT CENTER LE UPPER RIB CRACKED AT XFS 304. STOP DRILLED CRACK ON RIB ANGLE IAW SRM 57-2-0 AT STA XFS 304. FABRICATED AND INSTALLED REPAIR ANGLES AT STA L/WING STA XFS304 IAW SRM 57-02-0, AND 51-01-20D. - [SDR UPS06847410](https://openairdocs.org/sdr/UPS06847410.md): Rib · cracked · Jul 13, 2006 · N806UP · Doug DC873F · Leading Edge Devices > FOUND LT CTR LE UPPER RIB CRACKED AT XS 491. SET HOLE TERMINATED CRACK. FABRICATED AND INSTALLED 2. REPAIR DOUBLERS IAW SRM 57-02-00 FIG 002 SHT 2, 51-01-20D AND 51-1-15. - [SDR UPS06847409](https://openairdocs.org/sdr/UPS06847409.md): Rib · cracked · Jul 13, 2006 · N806UP · Doug DC873F · Leading Edge Devices > INSPECTION TYPE:C1,3 LT WING CTR LE LWR IB CRACKED AT XFS 347. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-02-00 FIG 002, 57-02-03 FIG 005 AND 51-1-20D. - [SDR UPS06847407](https://openairdocs.org/sdr/UPS06847407.md): Rib · cracked · Jul 13, 2006 · N806UP · Doug DC873F · Leading Edge Devices > RT CENTER LE UPPER RIB AT XFS 415 IS CRACKED. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 002, 51-1-21 AND 51-1-20D. SAT PREVIOUSLY SENT THIS WRITEUP WITH WRONG TAIL NR. - [SDR UPS06847406](https://openairdocs.org/sdr/UPS06847406.md): Rib · cracked · Jul 13, 2006 · N806UP · Doug DC873F · Leading Edge Devices > LT CENTER LE UPPER RIB CRACKED AT XFS 334. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLES 2 IAW SRM 57-02-00 FIG 002, 57-03-03 FIG 005 AND 51-1-20D. - [SDR UPS06847405](https://openairdocs.org/sdr/UPS06847405.md): Rib · cracked · Jul 13, 2006 · N806UP · Doug DC873F · Leading Edge Devices > FOUND LT CENTER LE UPPER RIB CRACKED AT XS454. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2 AND 51-1-20A. - [SDR UPS06847371](https://openairdocs.org/sdr/UPS06847371.md): Rib · cracked · Jul 13, 2006 · N806UP · Doug DC873F · Leading Edge Devices > C1, 3 RT CENTER LEADING EDGE UPPER RIB CRACKED AT XFS409. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 51-1-21, 57-02-00 FIG 2, 57-03-03 FIG 5. - [SDR UPS06847647](https://openairdocs.org/sdr/UPS06847647.md): Fitting · cracked · Jul 12, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/Stringer > INSPECTION TYPE: C 1-3 MAIN CABIN STA.1690 LONGERON 35L END FITTING CRACKED REMOVED AND REPLACED LONGERON 35L END FITTING AT STA.1690 IAW SRM 51-1-21 AND SRM 51-1-20D. - [SDR UPS06847602](https://openairdocs.org/sdr/UPS06847602.md): Pressure Panel · cracked · Jul 12, 2006 · N806UP · Doug DC873F · Fuselage Main, Bulkhead > INSPECTION TYPE:C1-3 LT MLG WHEEL WELL STA 940 LBL 63 PRESSURE DECK SKIN IS CORRODED AND CRACKED. CUT OUT DAMAGED AREA IAW SRM 53-2-0. FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS IAW SAA EA 008-5320-01-A0300, UPS EO DC8-5330- 24740-A, DOUGLAS DWG 564 - [SDR UPS06847572](https://openairdocs.org/sdr/UPS06847572.md): Fitting · cracked · Jul 12, 2006 · N806UP · Doug DC873F · Fuselage Main, Longeron/Stringer > INSPECTION TYPE:C1-3 LT MAIN CABIN FS 680 FWD LONG END FITTING 6L IS CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 680 L6L IAW SRM 51-03-00, 51-1-20D, AND SRM 51-02-23. - [SDR UPS06847370](https://openairdocs.org/sdr/UPS06847370.md): Rib · cracked · Jul 12, 2006 · N806UP · Doug DC873F · Leading Edge Devices > C1, 3 LT OB LEADING EDGE RIB CRACKED AT XFS 746 UPPER RIB. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EACH DOUBLERS IAW SRM 57-02-00 FIG 2 SHT 2, 51-01-20D AND 51-01-15. Next page: https://openairdocs.org/deregistered/N806UP-2010-08-12/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 = 'N806UP' AND deregistration_id = 'N806UP-2010-08-12' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N806UP-2010-08-12/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.