# Service difficulty reports: N701UP, cancelled Apr 1, 2010 A list on [N701UP, cancelled Apr 1, 2010](https://openairdocs.org/deregistered/N701UP-2010-04-01.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 · 283 reports - [SDR UPS08853554](https://openairdocs.org/sdr/UPS08853554.md): Wire · broken · Oct 9, 2008 · N701UP · Doug DC871F · Light System Wiring > EMERGENCY EXIT LIGHT SWITCH DOES NOT ILLUMINATE THE AMBER LIGHT WHEN SWITCH IS IN THE DISARM POSITION. FOUND BROKEN WIRE AT EMERGENCY LIGHTS BATTERY PACK. REPAIRED AS REQUIRED AND TESTED PER M/M 33-50-02-2. OK FOR SERVICE. - [SDR UPS08852550](https://openairdocs.org/sdr/UPS08852550.md): Slide · inoperative · Jun 19, 2008 · N701UP · Doug DC871F · Escape Slide > MAIN ENTRY DOOR SLIDE INOP 378344. REMOVED MAIN ENTRY DOOR SLIDE AND ROUTED TO S/M. RIVET INSTALLED ON LOOSE BRACKET SRM 51-1-21 AND FWD ENTRY SLIDE REINSTALLED IAW MM 25- 60-01-2. THIS CLEARS M378344. - [SDR UPS08851447](https://openairdocs.org/sdr/UPS08851447.md): Indicator · damaged · Jan 17, 2008 · N701UP · Doug DC871F · Escape Slide > ESCAPE SLIDE PRESSURE UNREADABLE. REMOVED AND REPLACED ESCAPE SLIDE PER MM 25-60-01. OPS CKD, SLIDE GIRT BAR INSTALLED. THIS CLOSES DEFERRAL M367121. - [SDR UPS08851428](https://openairdocs.org/sdr/UPS08851428.md): Indicator · out of position · Jan 12, 2008 · N701UP · Doug DC871F · Escape Slide > ESCAPE SLIDE PRESSURE GAUGE UNREADABLE, TOO LOW IN SIGHT WINDOW. REMOVED AND REPLACED SLIDE CONTAINER PER DC8 AMM 25-60-01-2 - [SDR UPS07850336](https://openairdocs.org/sdr/UPS07850336.md): Control Valve · leaking · Jul 28, 2007 · N701UP · Doug DC871F · Hydraulic System, Main > INSPECTION TYPE:N/A DURING DESCENT INTO SDF THE CREW RECEIVED AN AILERON LIGHT MESSAGE & BEGAN LOSING HYDRAULIC FLUID. THE CREW LATER DECLARED AN EMERGENCY. REMOVED AND REPLACED WING SLOT CONTROL VALVE WHILE RIGHT MANIFOLD WAS REMOVED IN REF TO AMM 27-80-04- - [SDR UPS07850490](https://openairdocs.org/sdr/UPS07850490.md): Girt Bar · unknown · Jul 25, 2007 · N701UP · Doug DC871F · Emergency Equipment > INSPECTION TYPE:N/A CAN'T STOW GIRT BAR ON ESCAPE SLIDE. STOWED GIRT BAR ON SLIDE. - [SDR UPS07849979](https://openairdocs.org/sdr/UPS07849979.md): Slide · out of position · Jun 16, 2007 · N701UP · Doug DC871F · Escape Slide > INSPECTION TYPE:N/A ESCAPE SLIDE PRESSURE UNREADABLE. REPOSITION SLIDE INSIDE OF COVER. - [SDR UPS07849800](https://openairdocs.org/sdr/UPS07849800.md): Battery · no test · May 13, 2007 · N701UP · Doug DC871F · Emergency Lighting > INSPECTION TYPE:N/A EMERGENCY LIGHTS WON'T TEST. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT PER MM 33-50-01-2. - [SDR UPS07849776](https://openairdocs.org/sdr/UPS07849776.md): Engine · flamed out · May 8, 2007 · N701UP · Doug DC871F · Powerplant System > INSPECTION TYPE:AS-E AT FLIGHT LEVEL 360 NR 3 ENGINE FLAMED OUT. RAN FLAME OUT CHECKLIST & RESTART IN FLIGHT CHECKLIST WHILE DESCENDING TO FLIGHT LEVEL 240 RESTART SUCCESSFUL OPERATED NORMALLY REMAINDER OF FLIGHT. PERFORMED ENGINE FLAME-OUT T/S REF MM 71-00- - [SDR UPS07849343](https://openairdocs.org/sdr/UPS07849343.md): Attach Fitting · cracked · Feb 20, 2007 · N701UP · Doug DC871F · Nacelle/Pylon, Main Frame > INSPECTION TYPE:C3 1ST CLIP FROM FWD C/S IS CRACKED NR 4 PYLON O/B SKATE ANGLE. REMOVED, FABRICATED AND INSTALLED CLIP IAW SRM 51-1-20D, DWG 5804007. - [SDR UPS07849288](https://openairdocs.org/sdr/UPS07849288.md): Skin · cracked · Feb 20, 2007 · N701UP · Doug DC871F · Fuselage Main, Plate/Skin > INSPECTION TYPE:C3 HFEC & VISUAL INSPECTION DETECTED A CRACK ON THE R-2 DOOR FWD UPPER CORNER APPROX.50 INCH IN LENGTH. CUT OUT DAMAGED AREA OF THE R-2 DOOR FWD UPPER CORNER IAW SRM 53-02-00 FIG 16, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW S - [SDR UPS07849243](https://openairdocs.org/sdr/UPS07849243.md): Web · cracked · Feb 20, 2007 · N701UP · Doug DC871F · Wing Miscellaneous Structure > INSPECTION TYPE:C3 NR 2 MAIN TANK THRU PNL 506C WEB IS CRACKED FWD OF CTR/SPAR XRS -6. STOP DRILLED CRACK AT NR 2 MAIN TANK WEB AT STA XRS -6 IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLER AT NR 2 MAIN TANK WEB AT STA XRS -6 IAW SRM 57-02- - [SDR UPS07849370](https://openairdocs.org/sdr/UPS07849370.md): Floorbeam · corroded · Feb 17, 2007 · N701UP · Doug DC871F · Fuselage Main, Floor Beam > INSPECTION TYPE:C3 HEAVY CORROSION & EXFOLIATION ON AFT SIDE OF FLOORBEAM, C-PIT TUNNEL LT SIDE STA 1260 LBL 59. REPAIRED FLOORBEAM AT STA 1260 LBL 59 IAW SAA EA 008-5310-01-A0693 UPS RAA DC8-53-20612, AND FAA FORM 8100-9. - [SDR UPS07849289](https://openairdocs.org/sdr/UPS07849289.md): Floorbeam · corroded · Feb 17, 2007 · N701UP · Doug DC871F · Fuselage Main, Floor Beam > INSPECTION TYPE:C3 HEAVY CORROSION ON TOP OF FLOORBEAM AFT ACCY COMPT STA 1580 RBL 50-60, FWD SIDE. CUT OUT CORRODED AREA ON FLOORBEAM AT STA 1580 RBL 50-60 IAW SRM TR 51-2-1. FABRICATED AND INSTALLED REPAIR FILLER, REPAIR ANGLES AND SPLICE ANGLES IAW SRM TR - [SDR UPS07849266](https://openairdocs.org/sdr/UPS07849266.md): Frame · corroded · Feb 16, 2007 · N701UP · Doug DC871F · Fuselage Main, Frame > INSPECTION TYPE:C3 C-PIT STA 1040 FRAME FROM L35L-L35R HAS EXFOLIATION CORROSION. REMOVED DAMAGED AREA OF FRAME CAP AT STA 1040 IAW SRM 51-1-21, AND DWG 53A-011-A. FABRICATED AND INSTALLED REPAIR ANGLE AND STRAP AT STA 1040 FROM L35L-L35R IAW DWG 2537716, DW - [SDR UPS07849372](https://openairdocs.org/sdr/UPS07849372.md): Floorbeam · cracked · Feb 15, 2007 · N701UP · Doug DC871F · Fuselage Main, Floor Beam > INSPECTION TYPE:C3 CRACKED END FITTING ON FLOORBEAM AT STA 280, RBL 48 A-PIT DOORWAY UPPER FWD CORNER REMOVED FLOORBEAM END FITTING AT STA 280, RBL 48 A-PIT DOORWAY UPPER FWD CORNER IAW SRM 51-1-20D. FABRICATED AND INSTALLED FLOORBEAM END FITTING AT STA 2 - [SDR UPS07849280](https://openairdocs.org/sdr/UPS07849280.md): Support Angle · missing · Feb 15, 2007 · N701UP · Doug DC871F · Fuselage Main, Structure > INSPECTION TYPE:C3 MAIN CABIN CENTER WING BOX SUB FLOOR FRAME FITTING SUPPORT ANGLE MISSING AT STA 740 L22R. FABRICATED AND INSTALLED SUPPORT ANGLE IAW SRM 51-3-2, 51-1-20D AND DWG 2892086. - [SDR UPS07849240](https://openairdocs.org/sdr/UPS07849240.md): Support Channel · cracked · Feb 15, 2007 · N701UP · Doug DC871F · Fuselage Miscellaneous Structure > INSPECTION TYPE:C3 SUPPORT CHANNEL CRACKED AT STA 1730 RBL 20. REMOVED SUPPORT CHANNEL AT STA 1730 RBL 20 IAW SRM 51-01-21. FABRICATED AND INSTALLED SUPPORT CHANNEL AT STA 1730 RBL 20 IAW SRM 51-3-0, AND DWG 5755032. - [SDR UPS07849249](https://openairdocs.org/sdr/UPS07849249.md): Web · cracked · Feb 14, 2007 · N701UP · Doug DC871F · Fuselage Miscellaneous Structure > INSPECTION TYPE:C3 CABIN STA 3.0 RBL 45 SUBFLOOR WEB IS CRACKED. STOP DRILLED CRACK ON WEB AT STA 3.0 RBL 45 IAW SRM 53-2-00 FIG 001B. FABRICATED AND INSTALLED REPAIR DOUBLER AT SUBFLOOR STA 3.0 RBL 45 IAW SRM 53-02-00-0 FIG 001D, AND SRM 51-1-20D. - [SDR UPS07849245](https://openairdocs.org/sdr/UPS07849245.md): Beam · cracked · Feb 14, 2007 · N701UP · Doug DC871F · Fuselage Miscellaneous Structure > INSPECTION TYPE:C3 CRACK IN RADIUS OF NR 3 J-BEAM, 60 COMPT RBL 2. STOP DRILLED CRACK IN RADIUS OF NR 3 J-BEAM IN THE 60 COMPT IAW SRM 53-02-05. FABRICATED AND INSTALLED REPAIR DOUBLER, AND ANGLE IN RADIUS OF THE NR 3 J-BEAM IN THE 60 COMPT IAW SRM 53-02-05- - [SDR UPS07849232](https://openairdocs.org/sdr/UPS07849232.md): Floor Support · cracked · Feb 14, 2007 · N701UP · Doug DC871F · Fuselage Miscellaneous Structure > INSPECTION TYPE:C3 CABIN SUBFLOOR STA 25-48 RBL 10 FLOOR SUPPORT ANGLE IS BROKEN. REMOVED FLOOR SUPPORT ANGLE AT CABIN SUBFLOOR AT STA 25-48 RBL 10, REPAIRED FLOOR SUPPORT ANGLE AT STA 25-48 RBL10 IAW SRM 51-01-19, AND SRM 51-3-2. - [SDR UPS07849413](https://openairdocs.org/sdr/UPS07849413.md): Frame · cracked · Feb 13, 2007 · N701UP · Doug DC871F · Wing Spar > INSPECTION TYPE:C3 CRACK IN DRILL START IN FRAME ON OUTBOARD LWR SIDE OF NR 3 ENG STUB WING. STOP DRILLED CRACK IN FRAME AT RIGHT STUB WING STA 252.351 IAW SRM 54-2-0, AND SRM TR 54-38. FABRICATED AND INSTALLED REPAIR ANGLE AND DOUBLER AT RIGHT STUB WING STA - [SDR UPS07849371](https://openairdocs.org/sdr/UPS07849371.md): Boss · corroded · Feb 13, 2007 · N701UP · Doug DC871F · Fuselage, Landing Gear Attach Fittings > INSPECTION TYPE:C3 LEFT MLG RETRACT PIN BOSS HAS PITTING AND TOOLING MARKS. REMOVED AND REPLACED LEFT MLG SHOCK STRUT ASSY IAW 32-11-00, RETRACT AND EXTENSION CHECKS GOOD IAW 32-11-00. - [SDR UPS07849233](https://openairdocs.org/sdr/UPS07849233.md): Bracket · cracked · Feb 13, 2007 · N701UP · Doug DC871F · Wing, Attach Fittings > INSPECTION TYPE:C3 LEFT WING FLAP WELL FUEL DUMP CHUTE HORSE SHOE BRACKET CRACKED. REMOVED CRACKED HORSE SHOE BRACKET FROM LEFT WING DUMP CHUTE IAW SRM 51-1-20D. FABRICATED AND INSTALLED HORSE SHOE BRACKET AT LEFT WING FUEL DUMP CHUTE IAW DWG 5649654, AND SR - [SDR UPS07849210](https://openairdocs.org/sdr/UPS07849210.md): Doubler · cracked · Feb 13, 2007 · N701UP · Doug DC871F · Wing Miscellaneous Structure > INSPECTION TYPE:C3 LEFT WING CENTER L/E UPPER INNER DOUBLER CRACKED AT STA XOLDI 6.2246. REMOVED CRACKED DOUBLER AT LEFT WING CENTER L/E STA XOLDI 6.2246 IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT DOUBLER AT LEFT WING CENTER UPPER L/E STA XOLDI 6. - [SDR UPS07849209](https://openairdocs.org/sdr/UPS07849209.md): Rib · cracked · Feb 13, 2007 · N701UP · Doug DC871F · Wing, Rib/Bulkhead > INSPECTION TYPE:C3 LT WING CENTER LEADING EDGE UPPER RIB CRACKED AT XFS 366. STOP DRILLED CRACK AT LEFT WING L/E AT STA XFS 366 IAW SRM 57-02-00 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER ON LEFT CENTER L/E AT STA XFS 366 IAW SRM 57-02-00 AND SRM 51-01-2 - [SDR UPS07849344](https://openairdocs.org/sdr/UPS07849344.md): Skin · cracked · Feb 12, 2007 · N701UP · Doug DC871F · Wing, Plate/Skin > INSPECTION TYPE:C3 LEFT WING UPPER SKIN 1 INCH CRACK AT XRS 107.000 UPPER FRONT SPAR SKIN. REPAIRED UPPER WING SKIN AT XRS 107.000 FRONT SPAR IAW SAA EA 008-5710-01-A0685 AND UPS RAA DC8-57-20211. - [SDR UPS07849224](https://openairdocs.org/sdr/UPS07849224.md): Longeron · corroded · Feb 12, 2007 · N701UP · Doug DC871F · Fuselage Main, Longeron/Stringer > INSPECTION TYPE:C3 CORROSION UNDER SPLICE FITTING AND LONGERON 33L IN AFT ACCESSORY COMPT AT STA 1550. REMOVED SPLICE FITTING AND CUT OUT CORRODED SECTION OF L33L FROM STA 1530-1550 IAW SRM 51-1-21. LOCATED, DRILLED UP, AND INSTALLED NEW SPLICE FITTING AND L - [SDR UPS07849211](https://openairdocs.org/sdr/UPS07849211.md): Bulkhead · cracked · Feb 12, 2007 · N701UP · Doug DC871F · Fuselage Main, Bulkhead > INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD CRACKED AT STA 1766 LBL 24 L10L AREA. CUT OUT DAMAGED AREA AT AFT PRESSURE BULKHEAD STA 1766 LBL 24 L10L IAW SRM 53-2-5 FIG 14A. FABRICATED AND INSTALLED FINGER DOUBLER, FILLER AND REPAIR DOUBLER AT AFT PRESSURE BULK - [SDR UPS07849242](https://openairdocs.org/sdr/UPS07849242.md): Longeron · corroded · Feb 10, 2007 · N701UP · Doug DC871F · Fuselage Main, Longeron/Stringer > INSPECTION TYPE:C3 HEAVILY CORRODED LONGERON IN AFT ACC COMPT STA 1570 L34L. REMOVED CORRODED LONGERON SECTION L34L STA 1560-1570 IAW SRM 51-01- 20D, AND SRM 51-01-21-0. FABRICATED AND INSTALLED LONGERON SPLICE SECTION AND NEW END FITTING AT STA 1560-1570 L3 - [SDR UPS07849223](https://openairdocs.org/sdr/UPS07849223.md): Skin · dented · Feb 10, 2007 · N701UP · Doug DC871F · Rudder, Plate/Skin > INSPECTION TYPE:C3 RUDDER RT SIDE LEADING EDGE STA ZR 140 SKIN HAS DENT. FOUND DENT OUT OF LIMITS AT RUDDER STA ZR 140 IAW SRM 55-02-00-0 FIG 001. REMOVED AND REPLACED SKIN AT RUDDER BAY NR 2 STA ZR 140 IAW SRM 51-3-0, 51-1-21, AND SRM 55-06-01-0. NO WEIGHT - [SDR UPS07849241](https://openairdocs.org/sdr/UPS07849241.md): Skin · dented · Feb 8, 2007 · N701UP · Doug DC871F · Fuselage Main, Plate/Skin > INSPECTION TYPE:C3 LEFT FUSELAGE STA 1580 BETWEEN L24L & L25L EXT SKIN HAS DENT WITH GOUGE 6 INCHES LONG 1.5 INCH WIDE AND APPROX..100 INCH DEEP. CUT OUT DAMAGED AREA AT STA 1580 BETWEEN L24L & L25L EXTERIOR SKIN IAW SRM 53-2-1 FIG 7. FABRICATED AND INSTALL - [SDR UPS06848792](https://openairdocs.org/sdr/UPS06848792.md): Battery Pack · discharged · Dec 20, 2006 · N701UP · Doug DC871F · Emergency Lighting > INSPECTION TYPE:N/A ON PRE-DEPARTURE, EMERGENCY ARM/DISARM LIGHT WILL NOT GO OUT WHEN SWITCH IS POSITION TO ARM. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK GOOD PER MM 33-50-01-2. - [SDR UPS06848787](https://openairdocs.org/sdr/UPS06848787.md): Battery Pack · inoperative · Dec 18, 2006 · N701UP · Doug DC871F · Emergency Lighting > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS NO TEST ON PREFLIGHT. REPLACED EMERGENCY LIGHTING BATTERY PACK. OPS CHECK GOOD. - [SDR UPS06847306](https://openairdocs.org/sdr/UPS06847306.md): Battery Pack · discharged · Jul 10, 2006 · N701UP · Doug DC871F · Emergency Lighting > EMERGENCY LIGHTS WOULD NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-50-01-2. OPS CHK GOOD. - [SDR UPS05843866](https://openairdocs.org/sdr/UPS05843866.md): Frame · corroded · Feb 1, 2005 · N701UP · Doug DC871 · Fuselage Main, Frame > FRAME AND SPLICE CORRODED BEYOND LIMITS AT STA 1420 L34R-L36. REMOVED SPLICE FTG AND CUT OUT CORRODED FRAME SECTION BETWEEN L36 AND L34R. FAB REPLACMENT SPLICE FROM SHT 7075-0-.063 HEAT TREAT TO T6. FAB FRAME SECTION FROM EXTR 2641520. INSTALLED PARTS REF - [SDR UPS05843782](https://openairdocs.org/sdr/UPS05843782.md): Fitting · cracked · Jan 13, 2005 · N701UP · Doug DC871F · Fuselage Main, Attach Fittings > INSPECTION TYPE:C1 INTERCOSTAL-TO-FRAME ATTACH FITTING CRACKED AT STA 1140 LONGERON 35R. REMOVED AND REPLACED FITTING REF SRM 51-1-20D, 51-1-8, 51-1-15. - [SDR UPS05843781](https://openairdocs.org/sdr/UPS05843781.md): Fitting · cracked · Jan 13, 2005 · N701UP · Doug DC871F · Wing, Attach Fittings > INSPECTION TYPE:C3, CLIP CRACKED IN NR 1 ALT TANK AT NR 1 PYLON SKATE ANGLE BETWEEN STR 62 & 63 XRS508.997 LT WING INT. FAB REPLACEMENT CLIP PER DWG5804007 FROM BAR7075T6. DYE-PEN INSP PER DPS 4.707; NO CRACKS NOTED. REMOVED AND REPLACED FITTING REF SRM 51- - [SDR UPS05843780](https://openairdocs.org/sdr/UPS05843780.md): Fitting · corroded · Jan 13, 2005 · N701UP · Doug DC871F · Wing, Attach Fittings > INSPECTION TYPE:C3 RT WING STA XW97 CANOE SUPPORT FITTING ATTACH BOLT HOLES CORRODED & GOUGED. REMOVED AND REPLACED FITTING REF SRM 51-3-2, 51-1-20D, 51-3-0, MM 20-16-00, 27-51-12. - [SDR UPS05843848](https://openairdocs.org/sdr/UPS05843848.md): Support Fitting · corroded · Jan 12, 2005 · N701UP · Doug DC871F · Trailing Edge Flaps > RT STA 98 FLAP SUPPORT FITTING (CANOE) HAS CORROSION UNDER FLAP TRACK AREA, O/B SURFACE.025 DEEP I/B SURFACE IS.006 DEEP. UNDERCUT AND REMOVED CORROSION.050 AND FABRICATED AND INSTALLED REPAIR FILLERS PER SB 27-164 PAGE 8. - [SDR UPS05843789](https://openairdocs.org/sdr/UPS05843789.md): Web · cracked · Jan 10, 2005 · N701UP · Doug DC871F · Fuselage Main, Structure > INSPECTION TYPE:C1, R1 DOOR JAMB TORQUE WEB CRACKED ABOVE UPPER DOOR HINGE ARM STA 150- 155, NEXT TO L14R. CUT OUT DAMAGE, NDT VERIFIED REF NDT/SPM06-10-01.001. FAB DOUBLER FROM SHT2024T3-.050, TREAT, PRIME & INSTALLED SAME REF SRM 53-2-0 FIG 1F, 51-1-8, 51- - [SDR UPS05843787](https://openairdocs.org/sdr/UPS05843787.md): Fitting · cracked · Jan 10, 2005 · N701UP · Doug DC871F · Aerodynamic Fairings > INSPECTION TYPE:C1, TAIL CONE ATTACH FITTING CRACKED ON L36, STA 1875. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-1-20D, 51-1-8, 51-3-0. - [SDR UPS05843846](https://openairdocs.org/sdr/UPS05843846.md): Attach Fitting · cracked · Jan 8, 2005 · N701UP · Doug DC871F · Fuselage Main, Attach Fittings > MAIN CABIN STA 835.5 L18L, FRAME ATTACH FITTING CRACKED. REMOVED AND REPLACED FRAME ATTACH FITTING AT STA 853.5 L18L, IAW SRM 51-1-20D. - [SDR UPS05843837](https://openairdocs.org/sdr/UPS05843837.md): Attach Fitting · cracked · Jan 8, 2005 · N701UP · Doug DC871F · Fuselage Main, Attach Fittings > MAIN CABIN AT STA 702 LBL (LONGERON 13LH) FRAME ATTACH FITTING CRACKED. REMOVED, FABRICATED AND REPLACED FRAME ATTACH FITTING AT F/S 702 L13L IAW 51-1-20-D, DWG3779978 AND SAA TRAVELER 0035. - [SDR UPS05843835](https://openairdocs.org/sdr/UPS05843835.md): Longeron · cracked · Jan 8, 2005 · N701UP · Doug DC871F · Fuselage Main, Longeron/Stringer > LONGERON 36 HAS 1 INCH CRACK ON RT UPPER FLANGE IN RADIUS BETWEEN F/S 1260-1280. REMOVED AND REPLACED DAMAGED LONGERON SECTION IAW DWG 5750322 AND SRM 51-1-20D FROM F/S 1260-1360 L36. - [SDR UPS05843786](https://openairdocs.org/sdr/UPS05843786.md): Fitting · cracked · Jan 8, 2005 · N701UP · Doug DC871F · Fuselage Main, Attach Fittings > INSPECTION TYPE:C1, LONGERON 8R END FITTING CRACKED AT STA 676. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D, 51-1-8. - [SDR UPS05843867](https://openairdocs.org/sdr/UPS05843867.md): Frame · corroded · Jan 7, 2005 · N701UP · Doug DC871F · Fuselage Main, Frame > A-PIT FRAME CORRODED AND MISDRILLED AT STA 280 L32R. CUT OUT DAMAGE, NDT VERIFIED ALL DAMAGE REMOVED PER NDTSPM 06-10-01.001. FAB REPAIR ANGLE FROM SHT 7075-0-.080 HEAT TREAT TO T6 PER DPS7.00-1. FAB FILLERS FROM SHT 7075T6-.080. INSTALLED ALL PARTS REF'S - [SDR UPS05843838](https://openairdocs.org/sdr/UPS05843838.md): Pressure Blkhd · cracked · Jan 7, 2005 · N701UP · Doug DC871F · Fuselage Main, Bulkhead > MAIN CABIN, AFT PRESSURE BULKHEAD CRACKED, RBL 50 UPPER SIDE. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER, FILLERS AND FINGER DOUBLER IAW SRM'S 53-2-5 FIG 14A, 51-1-21, 51-1-20D AND DWG SRO8530007. - [SDR UPS05843836](https://openairdocs.org/sdr/UPS05843836.md): Longeron · cracked · Jan 7, 2005 · N701UP · Doug DC871F · Fuselage Main, Longeron/Stringer > MAIN CABIN LONGERON CRACKED AT STA 1760 L15L. REMOVED DAMAGED SECTION OF LONGERON AND FABRICATED SPLICE AND LONGERON SECTION INSTALLED IAW SRM'S 53-2-2 FIG10, 51-1-21, 53-2-0,51-1-20D AND DC8-53B-OO9-39. - [SDR UPS05843834](https://openairdocs.org/sdr/UPS05843834.md): Fitting · cracked · Jan 7, 2005 · N701UP · Doug DC871F · Fuselage Main, Structure > LWR CARGO PIT STA 1140 L34R UPPER FWD FITTING CRACKED ON THE FRAME. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. Next page: https://openairdocs.org/deregistered/N701UP-2010-04-01/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 = 'N701UP' AND deregistration_id = 'N701UP-2010-04-01' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N701UP-2010-04-01/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.