N308UP

Service difficulty reports · 175

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N308UP' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA2018101094852Transceiver · inoperativeTRANSMISSION & RECEPTION ON LEFT HF WAS INOPERATIVE. DIVERTED. REPLACED THE LEFT HF TRANSCEIVER. OPS CHECKED OK IAW MM 23-11-03-401.Oct 7, 2018 · N308UP · Boeing 76734AF · HF Communications SystemSDR IPXA2018091033812Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL AT POS 1 AND 2 RT DAMAGED. FABRICATED NEW MAIN CARGO DECK FLOOR PANEL IAW SREO B767-5320-9693-I.Sep 10, 2018 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2018071631709Proximity Sensor · out of adjustCREW ENTRY DOOR PROXIMITY SENSORS 194 AND 195 ARE OUT OF LIMITS OF T/C 52 000 100, REQUIRES ADJUSTMENT. CORRECTED SENSORS S194 AND S195 PER AMM 52 71 01 964 211.Jul 15, 2018 · N308UP · Boeing 76734AF · Door Warning SystemSDR IPXA2018012725930Fire Loop · malfunctionedAFTER SHUTDOWN, THE RT ENGINE NR 2 FIRE LOOP MESSAGE. TROUBLESHOT IAW FIM 26-11-815-801. AFTER INSPECTING THE WIRING FOR THE RT B FIRE LOOP, FOUND TS 683-B2 PARTIALLY ATTACHED AT LOWER FWD LOOP. OPS CHECKED GOOD.Jan 27, 2018 · N308UP · Boeing 76734AF · Fire DetectionSDR IPXA2017092021905Switch · brokenEMERGENCY LIGHT ON/ARMED/OFF GUARDED SWITCH GUARD BROKEN. REMOVED AND REPLACED EMERGENCY LIGHTS P5 PANEL IAW AMM 33 51 08. OP CHECKS GOOD 31 12 11 51A ITEM 015.Sep 20, 2017 · N308UP · Boeing 76734AF · Emergency LightingSDR IPXA2017051617165Skin · crackedINSPECTION TYPE: C11, CRACK ON RT FUSELAGE SKIN AT BS 1725.5, STRINGER 7R. REPAIR IAW EO B767-5330-24301-D, APPX C, AND SRM 53-80-01-2R-5, REPAIR 5, DETAIL III, REV 68.May 15, 2017 · N308UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA2017051517090Floor Panel · damagedINSPECTION TYPE: C11, DAMAGE FOUND ON THE M/D CARGO FLOOR PANEL AT BS 287-412. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-IMay 5, 2017 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2017051517089Skin · crackedINSPECTION TYPE: C11, CRACK ON THE RT FUSELAGE SKIN AT BS 1662, STRINGERS 12 - 13AR. REPAIRED IAW SRM 53-80-01, REPAIR 7, REV.68.May 5, 2017 · N308UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA2017042816575Escape Rope · detachedEMERGENCY ESCAPE ROPE OVER MAIN ENTRY DOOR HANGING DOWN, COMPLIED WITH EO B767-2520-64068.Apr 27, 2017 · N308UP · Boeing 76734AF · Emergency EquipmentSDR IPXA2017031214999Skin · dentedLEFT WING INBD AFT FLAP T/E WEDGE LWR SKIN DENTED. REPAIRED IAW EO B767-5750-63362-B.Mar 11, 2017 · N308UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2016080906824Escape Rope · unsecureDURING A PREFLIGHT, THE MAIN CABIN DOOR ESCAPE ROPE CAME OUT OF HOLDER. REPACKED THE ESCAPE ROPE ASSY AND SECURED IAW AMM 25-61-04-502-010Aug 9, 2016 · N308UP · Boeing 76734AF · Emergency EquipmentSDR IPXA2016012498289Handle · inoperativeAT CREW ENTRY DOOR EXTERIOR HANDLE DISARM LEVER DOES NOT FAIR WITH HANDLE IN THE STOWED POSITION CHECKED FLUSHNESS OF HANDLE IAW AMM 52-12-00-835-126, STEP D, 5, C. CHECKS GOOD AT THIS TIME. SUSPECT THERE WAS ICE IN THE AREA PREVIOUSLY.Jan 24, 2016 · N308UP · Boeing 76734AF · Passenger/Crew DoorsSDR IPXA2015052789463Flap System · malfunctionedEMERGENCY DECLARED, RECEIVED EICAS FLAP DISAGREE AND DISCREET LIGHT. STATUS PAGE MSG T/E FLAP DRIVE OFF. CANCELLED EMERGENCY AFTER FLAPS CORRECTED, REF FIM 27-51-00-815-839, PFM FSEU AND FSPM BITE TEST NORMAL. NO FAULT FOUND IAW AMM 27-51-00-201 OPERATED FLMay 25, 2015 · N308UP · Boeing 76734AF · Trailing Edge Flap Control SystemSDR IPXA2015051489066Skin · dentedDURING MAJOR MAINTENANCE VISIT NR 6772, FOUND A DENT AT BS 433 , NEAR S24L ON BULK CARGO DOOR OUTER SKIN. EVALUATED DAMAGE IAW SRM 52-30-01-1A-1 REV 62.00.May 12, 2015 · N308UP · Boeing 76734AF · Cargo/Baggage DoorsSDR IPXA2015051489065Skin · dentedDURING MAJOR MAINTENANCE VISIT NR 6772, FOUND DENT, SKIN, BS 455, NEAR S-27L , BULK CARGO DOOR, EVALUATED DAMAGE IAW SRM 52-30-01-1A-1 REV 62.00.May 12, 2015 · N308UP · Boeing 76734AF · Cargo/Baggage DoorsSDR IPXA2015051989227Skin · crackedINSPECTION TYPE:C, 10 CRACK INDICATION WAS FOUND ON RT WING LOWER SKIN FASTENER HOLES AT STR 9.5L, NEAR WING STA 995, REPAIR IAW SR: 3-3263168689 AND EO B767-5730-57502-B.May 11, 2015 · N308UP · Boeing 76734AF · Wing, Plate/SkinSDR IPXA2015051989226Skin · crackedINSPECTION TYPE:C, 10 CRACK INDICATION WAS FOUND ON RT WING LOWER SKIN, FASTENER HOLE AT STR L-6.5 , NEAR WING FS 995 REPAIR IAW SR: 3-3263168689 WITH FAA APPROVED 8100-9 FORM DATED: 17MAY2015 AND EO B767-5730-57508-B.May 11, 2015 · N308UP · Boeing 76734AF · Wing, Plate/SkinSDR IPXA2015051989228Structure · crackedINSPECTION TYPE:C, 10 CRACK AND DISBOND ON THE LT WING OTBD FLAP L/E AT OTEF STA 61.98 - 75.23. REPAIR IAW SRM 57-53-01-2R-1, REPAIR 1, FIG 201, REV:62.00 & 767-300F, SRM 51-70-05-0G-0-GENERAL FIG REV:62.00.May 7, 2015 · N308UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2015051989225Stiffener · crackedINSPECTION TYPE:C, 10 CRACK ON THE CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT FS 785.9 , RBL 11, REPAIR IAW SRM 57-10-10, REPAIR 2, REV 62, SRID : 3-3262898378 AND EO: B767-5310-57469-A.May 7, 2015 · N308UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2015051989221Stringer · crackedINSPECTION TYPE:C 10, CRACK, 0.5", WAS FOUND ON STRINGER 20L AT FS 1511 REPAIR IAW SR 3-3253369211 AND EO B767-5310-57389-A.May 5, 2015 · N308UP · Boeing 76734AF · Fuselage Main, Longeron/StringerSDR IPXA2015051989224Stringer · crackedINSPECTION TYPE:C, 10 CRACK, 1.15" WAS FOUND ON THE STRINGER 20R AT BS 1504. REPAIR IAW SR 3-3253389894 AND EO B767-5310-57390-A.May 5, 2015 · N308UP · Boeing 76734AF · Fuselage Main, Longeron/StringerSDR IPXA2014072183667Switch · brokenEMERGENCY LIGHTS SWITCH ON OVERHEAD PANEL BROKEN. R & R LIGHT SWITCH.Jul 19, 2014 · N308UP · Boeing 76734AF · Emergency LightingSDR IPXA2014031782299Door Frame · dentedBULK CARGO DOOR LOWER FRAME DENTED AT CUTOUT. DENT .7 INCHES FWD AND AFT ON WITH OF RETURN FLANGE .7 X.375 ON THE WEB OF FRAME. REPAIRED IAW E0 B767-5230-53563-B.Mar 16, 2014 · N308UP · Boeing 76734AF · Cargo/Baggage DoorsSDR IPXA13678209Floor Panel · crackedINSPECTION TYPE:C9. FOUND M/D CARGO FLOOR PANEL CRACKED AT BS 497, RBL 51.5-54. REPAIRED IAW EO NO B767-5320-9693-H.May 5, 2013 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA13678208Floor Panel · dentedINSPECTION TYPE:C9, FOUND M/D CARGO FLOOR PANEL DENTED BETWEEN BS 412 AND 456, RBL 28. REPAIRED IAW EO NR B767-5320-9693-H.May 5, 2013 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA13678207Floor Panel · dentedINSPECTION TYPE:C9, FOUND M/D FLOOR PANEL DENTED BETWEEN BS 685 AND 690, RBL 17. REPAIRED IAW EO NR B767-5320-9693-H.May 5, 2013 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA13678206Floor Panel · dentedINSPECTION TYPE:C9, FOUND M/D CARGO FLOOR PANEL DENTED BETWEEN BS 654+22 AND 654+66, LBL 88. REPAIRED IAW EO NO B767-5320-9693-H.May 5, 2013 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA13678205Floor Panel · dentedINSPECTION TYPE:C9, M/D CARGO FLOOR PANEL DENTED BETWEEN BS 370 AND 412, RBL 28. REPAIRED IAW EO NR B767-5320-9693-H.May 5, 2013 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA13678203Skin · dentedINSPECTION TYPE:C9, LT WING NR 2 SLAT T/E WEDGE ASSY UPPER SKIN DENT AT OSS 916.DAMAGE SIZE IS MEASURED AS 0.5" (LENGTH) X 0.5" (WIDTH) AND THE CUTUOT IS MEASURED AS 0.6" DIAMETER. REPAIRED IAW SRM 57-43-02, REPAIR 1 AND 51-70-10, REPAIR 2, FIG 203, REV 56.Apr 30, 2013 · N308UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA3677601Floorboard · damagedPOS 6L 3RD FLOORBOARD IN FROM OTBD 3 INCHES FWD OF CTR LINE HAS .2500" HOLE INTERIM REPAIR. REPAIRED IAW EO B767-5320-50236-A AND EO B767-5320-9693-H.Mar 24, 2013 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2675122Doubler · damagedDOUBLER DAMAGED AT BS 450. REPAIR IAW EO B767-5330-48402-A.Sep 1, 2012 · N308UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA12671528Pressure Switch · inoperativeETOP C HYD SYS PRESS LIGHTS ILLUMINATED. R & R CTR HYD SYS PRESSURE SWITCH IAW AMM 29-1-09- 04. OPS GOOD AT THIS TIME.Feb 6, 2012 · N308UP · Boeing 76734AF · Hydraulic System, MainSDR IPXA11668270Hydraulic System · low pressureCENTER HYD SYS LOW PRESSURE LIGHT WITH ASSOSICATED ECIAS MSG. DEMAND PUMP IN AUTO AND LOW PRESSURE LIGHT ILLUMINATED, BOTH OCCURED WHEN SELECTING FLAPS TO 1. EMEREGENCY DECLARED AND LANDED WITHOUT INCIDENT. ACFT OUT OF SERVICE.Jul 29, 2011 · N308UP · Boeing 76734AF · Hydraulic System, MainSDR IPXA1667654Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5, REV 50.Jun 22, 2011 · N308UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1667661Fitting · crackedINSPECTION TYPE:C, FUSE RT BS 955 REAR SPAR B/H FITTING AREA 1EA FASTENER HOLE FOUND CRACK AT T-FITTING APPROX .1250" IN LENGTH ON 3 O/C POSITION. FUSE RT BS 955 REAR SPAR B/H FITTING AREA T-FITTING REPLACED AND INSTALL IAW EO B767-5350-17922-I APP D ORG MAT'Jun 21, 2011 · N308UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA1667660Failsafe · crackedINSPECTION TYPE:C, FUSE RT BS 955 REAR SPAR B/H FITTING AREA 1 EA FASTENER HOLE FOUND 2EA CRKS AT FAIL SAFE STRAP APPROX .1250" IN LENGTH ON 4 O/C POSITION AND THROUGH THICKNESS OM 10 O/C POSITION. FUSE RT BS 955 REAR SPAR B/H FITTING FAIL SAFE STRAP REPAIREDJun 21, 2011 · N308UP · Boeing 76734AF · Fuselage Main, FrameSDR IPXA1667659Failsafe · crackedINSPECTION TYPE:C, FUSE RT BS 955 REAR SPAR B/H SIDE FITTING FAIL SAFE STRAP 1 EACH HOLE CRACK INDICATION. FUSE RT BS 955 REAR SPAR B/H SIDE FITTING FAIL SAFE STRAP ATT MOST LWR BOLT REMOVED AND REINSTALLED IAW EO B767-5350-17922-I, APPENDIX D FIG 6 FOR FURTHJun 20, 2011 · N308UP · Boeing 76734AF · Fuselage Main, FrameSDR IPXA1667657Fitting · crackedINSPECTION TYPE:C, FUSELAGE LT BS 955 B/H REAR SPAR FITTING AREA CRACK FOUND AT T-FITTING HAT 9 O'CLOCK POSITION APPROX 1250" . FUSE LT BS 955 REAR SPAR B/H AREA T-FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-I APP C, ORG MAT'L IS 7075-T73 DIE FORGINJun 20, 2011 · N308UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA1667656Failsafe · crackedINSPECTION TYPE:C, FUSE LT BS 955 B REAR SPAR FITTING AREA 2EA CRACKS FOUND AT FAIL SAFE STRAP AT 3 O'CLOCK POSITION THROUGH THICKNESS AND 9 O'CLOCK POSITION APPROX. .1250" FUSE LT SIDE BS 955 REAR SPAR B/H FITTING FAIL SAFE STRAP REPAIRED AS IAW EO B767-5350Jun 20, 2011 · N308UP · Boeing 76734AF · Fuselage Main, FrameSDR IPXA1667655Failsafe · crackedINSPECTION TYPE:C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP, 1 EACH HOLE CRACK INDICATION. FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP ATT MOST LWR BOLT. REMOVED & REINSTALLED IAW EO B767-5350-17922-I APP C, FJun 20, 2011 · N308UP · Boeing 76734AF · Fuselage Main, FrameSDR IPXA11667604Floor Panel · dentedINSPECTION TYPE:C, FLOOR PANEL FOUND 8 EA DENTS TOGETHER WITH DEEP GOUGE RUNNING THROUGH FROM FWD TO AFT AT BS 598 TO 654+22 RBL 77 TO RBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.Jun 19, 2011 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11667603Floor Panel · dentedINSPECTION TYPE:C, FLOOR PANEL FOUND 9EA DENTS AND 2 TOGETHER WITH DEEP GOUGE RUNNING THROUGH FROM FWD TO AFT AT STN 654+22 TO STN 690 RBL 77 TO RBL 88. FLOOR PANEL FABRICATED EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.Jun 19, 2011 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11667580Stiffener · crackedINSPECTION TYPE:8C, FWD CARGO COMPT WING CENTER TANK FRONT SPAR VERTICAL STIFFENER UPPER AREA FOUND CRACKED JUST AT STA 785.9, LBL 10.94. ORIGINAL MATERIAL IS BAC1518-912-2024T3511, CRACK LENGTH IS 1.25", CUT OFF LENGTH IS 19.5". THIS REPAIR IS CLASSIFIED ASJun 19, 2011 · N308UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA11667578Stiffener · crackedINSPECTION TYPE:8C, FWD CARGO COMPT WING CENTER TANK FRONT SPAR VERTICAL STIFFENER UPPER AREA FOUND CRACKED JUST AT STA 785.9 LBL 32.94. ORIGINAL MATERIAL IS BAC1518-749-2024T3511, CRACK LENGTH IS 2.25", CUT OFF LENGTH IS 16.5", THIS REPAIR IS CLASSIFIED AS AJun 19, 2011 · N308UP · Boeing 76734AF · Wing Miscellaneous StructureSDR IPXA1666640Floor Panel · damagedFLOOR PANEL POS 8L HAS .5" HOLE ON FWD SIDE OF PANEL. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.May 15, 2011 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1666639Floor Panel · damagedFLOOR PANEL POS 9R HAS HOLE AT FWD RT SIDE .5" DIAMETER. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.May 15, 2011 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1666638Floor Panel · damagedFLOOR PANEL POSITION 2R RT AFT SIDE HAS A 2" X 1" HOLE REF D432651. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.May 15, 2011 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1665460Floor Panel · damagedDURING A/C UNLOAD POSITION, 11R LT SIDE CTR BUTTERFLY LOCK FLOOR PANEL DAMAGED AND SIDE LOCK DAMAGED. FLOOR PANEL R & R TO S/M SHOP. THIS IS A MAJOR REPAIR TRANSFERRED TO NRC 338942. INSPECTED AREA. INSTALLED NEW FLOOR PANEL IAW MM 53-01-06-4. FLOORBOARD IMar 15, 2011 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10663056Floorboard · damagedHOLE IN MCD FLOORBOARD POSITION 4 CTR FS.635, LBL3. REPAIRED IAW SRM 53-00-50-2R PARA 6.Oct 11, 2010 · N308UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10661155Floor Panel · damagedMAIN DECK FLOOR PANEL POS 4L HAS A .5" HOLE. IDENTIFIED AS MAJOR REPAIR. INSTALLED FLOOR PANEL, SEALANT & TAPE REF MM 53-01-06-4, THIS CLEARS D411572.Jul 17, 2010 · N308UP · Boeing 76734AF · Fuselage Floor Panel
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