N307UP

Service difficulty reports · 212

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 = 'N307UP' 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 IPXA2019071344390Stiffener · crackedINSPECTION TYPE:C12 CRACK WAS FOUND ON STIFFENER (P/N:111T2005-8) OF CTR WING TANK FWD BULKHEAD, AT STA 785 RBL 11. REPAIR IAW SRM 57-10-10-2R-2 REPAIR 2 REV.74.00 SRID:#4-4545545432M EO B767-5740-58151-B AND B767-5710-73240-A.Jul 3, 2019 · N307UP · Boeing 76734AF · Fuselage Main, BulkheadSDR IPXA2019071344389Stiffener · crackedINSPECTION TYPE:C12 CRACK WAS FOUND ON STIFFENER (P/N:111T2008-12) OF CTR WING TANK FWD BULKHEAD, AT STA 785 RBL 33. REPAIR IAW SRM 57-10-10-2R-2 REPAIR 2 REV.74.00 SRID:#4-4545545432M EO B767-5740-58151-B AND B767-5710-73240-A.Jul 3, 2019 · N307UP · Boeing 76734AF · Fuselage Main, BulkheadSDR IPXA2019012438263Warning System · activatedINSPECTION TYPE:ETOP RIGHT AFT FUEL PUMP INOP PRESS LIGHT ON WITH FUEL PUMP. DEFERRED RT AFT FUEL PUMP REF MEL 28-22-1 PLACARD INSTALLED DMP C/W C/B P6 6 21 PULLED N COLLARD R AFT FUEL BOOST PUMP. **ETOPS FILED OPEN**Jan 24, 2019 · N307UP · Boeing 76734AF · Aircraft Fuel Distribution SystemSDR IPXA201809244287Floorboard · damagedMAIN CARGO DECK POS 4 CENTER FLOORBOARD HAD A HOLE. FABRICATED A NEW FLOORBOARD IAW EO B767-5320-9693-I.Sep 23, 2018 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2017101822754Shutoff Valve · malfunctionedEMERGENCY DECLARED, C HYD QTY, ENROUTE THE HYD SYS PRESSURE HYD C . 45 - .1 FLAPS EXTENDED ALTERNATE GEAR EXTENDED ALTERNATE RESERVE BRAKES AND STEERING ON.FOUND FLAP / SLAT SHUTOFF VALVE MODULE LEAKING. R/R FLAP / SLAT SHUTOFF VALVE MODULE WITH REF TO 767 AOct 17, 2017 · N307UP · Boeing 76734AF · Hydraulic System, MainSDR IPXA2017021714138Relay · failedAFT LOWER CARGO DOOR WILL NOT CLOSE ELECTRICALLY. R & R THE K36 RELAY IAW FIM 52-37-00-815-810. OPS CHECKED NORMAL.Feb 17, 2017 · N307UP · Boeing 76734AF · Cargo/Baggage DoorsSDR IPXA2016110610297Switch · malfunctionedAT FL 330, CARGO DOOR EICAS MESSAGE DISPLAYED WITH AURAL WARNING ACCOMPLISHED AOM PROCEDURE AND RETURNED TO DEPARTURE. PERFORMED BITE & HISTORY CHECK OF PSEU IAW FIM 32-09-03 FIG 103. HISTORY SHOWED S892, MAIN CARGO DOOR LOCKED SWITCH. SWITCH IS CLEAN AND WNov 6, 2016 · N307UP · Boeing 76734AF · Cargo/Baggage DoorsSDR IPXA2016110710376Sensor · out of alignmentINSPECTION TYPE:N/AATB - FL340 "CARGO DOOR" EICAS MESSAGE, MASTER CAUTION LIGHT ILLUMINATED, AND AN AURAL WARNING ZONE. COMPLETED QRH CARGO DOOR PROCEDURE (P. 145) DESCENDED TO 10000'. CONSULTED FLT CONTROL AND MAINT-RETURN SDF.MAIN DECK CARGO DOOR INDICATION Nov 5, 2016 · N307UP · Boeing 76734AF · Door Warning SystemSDR IPXA2016110310216Sensor · out of alignmentDOOR WARNING SYSTEM CARGO DOORS LIGHT ON STEADY EICAS MESSAGE. ACCOMPLISHED QRH. LT STAYED ON. DIVERTED. FOUND DOOR CLOSED. SENSOR S890 AND TARGET GAP .133" WITH DOOR CLOSED, AND UNLATCHED. ADDED SHIMS TO SENSOR IAW AMM 52-71-09-822-037 TO BRING CLEARANNov 3, 2016 · N307UP · Boeing 76734AF · Cargo/Baggage DoorsSDR IPXA2016070905614Unknown · odorDURING APPROACH, SMELLED STRONG ODOR LASTING APPROXIMATELY 10 SECONDS, BOTH EVAS UNITS AND FIRE EXTINGUISHER REPLACED. TROUBLESHOT IAW FIM 21-00-21 PAGE BLOCK 301. ENG RUN IDLE CHECK BOTH ENGINES WITH PACKS ON IAW AMM 71-00-00-862-053-H03. NO SMOKE, FUMES ORJul 9, 2016 · N307UP · Boeing 76734AF · Air Distribution SystemSDR IPXA2016050502958Lamp · inoperativeEMERGENCY EXIT LIGHT NEEDS BULB IN UNARMED LIGHT. REPLACED THE LAMP IAW AMM 33-13-00, OPS CHECKED NORMALMay 4, 2016 · N307UP · Boeing 76734AF · Emergency LightingSDR IPXA2016020298790Drain · leakingEMERGENCY DECLARED, CTR HYD SYSTEM QTY DECREASED SLOWLY TO 0.15. THEN AFTER GEAR EXTENSION QTY DECREASED TO .02 AND SYS PRESSURE LIGHT AND EICAS MSG ILLUMINATED. WERE ABLE TO EXTEND FLAPS TO 20 AND EXTEND GEAR W/NORMAL HYDRAULICS. FOUND ACMP PRESSURE AND CAJan 30, 2016 · N307UP · Boeing 76734AF · Hydraulic System, MainSDR IPXA2016010997565Container · damagedVACUUM PACKAGE OF LIFE VEST OF CENTER PASSENGER SEAT DAMAGED. LIFE VEST REPLACED IAW AMM 25-62-00, REV 116.03 DATED 12-08-15. PN OFF-ON: P01074-201C, SN OFF: 14031350236, SN ON: 15081710084. EFF REF IPC: 25-64-55-05A ITEM 010W REV 79.00 DATED 11-12-15.Jan 8, 2016 · N307UP · Boeing 76734AF · Life JacketSDR IPXA2016010497412Fmc · inoperativeATB CAPTAIN'S CDU FAILED. R & R LT FMC CDU IAW AMM 34-61-02. OPS CK NORMAL.Dec 29, 2015 · N307UP · Boeing 76734AF · Flight Management Computing Hardware SystemSDR IPXA2015120296321Valve · inoperativeINSPECTION TYPE: FWD CABIN TEMP EICAS MESSAGE AND INOPERATIVE LIGHT. R & R TRIM AIR VALVE, V2 IAW AMM 21-61-07-40. OPS CK NORMAL,Dec 1, 2015 · N307UP · Boeing 76734AF · Cabin Temperature Control SystemSDR IPXA2015062390447Floor Panel · crackedINSPECTION TYPE:C10, FOUND CRACK ON M/D CARGO FLOOR PANEL, 241QFF AT BS 933 TO BS 985, LBL 78 TO LBL 88. FABRICATED THE REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693-H.Jun 13, 2015 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA2015012185287Floor Support · corrodedMAIN CARGO DECK FLOOR SUPPORT CORRODED BS 1263, RBL 47.5. REPLACED THE FLOOR SUPPORT IAW MM 53-01-06.Jan 13, 2015 · N307UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA2014102084649Stringer · crackedSKIN FOUND CRACKED APPROXIMATELY 2.8 INCHES AT BS 1552 AND S20R AND ADJACENT STRINGER. REPAIRED IAW EO B767-5330-55753.Oct 6, 2014 · N307UP · Boeing 76734AF · Fuselage Main, Longeron/StringerSDR IPXA2013101800612Warning Message · false activationFWD CARGO DOOR EICAS MESSAGE. LIGHT EXTINGUISHED AFTER APPROXIMATELY FIVE MINUTES WITH ACFT DEPRESSURIZED. EMERGENCY DECLARED VERIFIED FWD CARGO DOOR CLOSED AND LOCKED IAW DMP 52-71-1-1. PERFORMED BITE PROCEDURE FOR THE PSEU. NO CODE FOUND RELATED TO THE FWOct 15, 2013 · N307UP · Boeing 76734AF · Door Warning SystemSDR IPXA3680236Actuator · inoperativeLIFE RAFT STOWAGE COMP. DOOR GAS ACTUATOR INOPERATIVE. R & R WITH NEW DOOR ACTUATOR IAW MM INTRO PG 1, PAR 1.Sep 12, 2013 · N307UP · Boeing 76734AF · Life RaftSDR IPXA3679015Floor Panel · delaminatedINSPECTION TYPE:C9, FOUND DELAMINATION DAMAGE ON M/D CARGO FLOOR PANEL AT BS 482-490 ,LBL 78.5-88, DIMENSIONS OF DAMAGE: 9" X 7". REPAIR IAW EO B767-5320-9693-H.Jun 20, 2013 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA3679014Floor Panel · dentedINSPECTION TYPE:C9, FOUND DENT DAMAGE ON CARGO FLOOR PANEL AT BS 573-584, LBL 75. DIMENSION OF CRACK DAMAGE: 9 INCHES LONG. REPAIR IAW EO B767-5320-9693-H.Jun 20, 2013 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA3679026Shear Web · corrodedINSPECTION TYPE:C9, FOUND CORROSION ON SHEAR WEB AT BS 286, RBL 45.0. REPAIR IAW EO B767-5310-51174-A.Jun 19, 2013 · N307UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA11668279Indicator · inoperativeEHSI WENT BLANK SOON AFTER TAKEOFF. REPLACED CAPTAIN'S EHSI AND OPS TEST COND. NORMAL IAW AMM 34-22-04-4.Jul 27, 2011 · N307UP · Boeing 76734AF · Turn and Bank/Rate of Turn IndicatorSDR IPXA11668219Failsafe · misinstalledINSPECTION TYPE:C, REMOVE FASTENERS / PARTS IDENTIFIED IN EO B767-5350-17922-I APPENDIX 'D', FIG 6 AS NECESSARY TO INSTALL A PROTECTIVE SHIM BETWEEN THE SKIN AND THE FAIL SAFE STRAP. FASTENERS/ PARTS REMOVED AND REINSTALLED IAW EO NR B767-5350-17922-I APPENDIJul 13, 2011 · N307UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA11668218Failsafe · misinstalledINSPECTION TYPE:C, REMOVE FASTENERS/ PARTS IDENTIFIED IN EO B767-5350-17922-I APP 'C' FIG 6 AS NECESSARY TO INSTALL A PROTECTIVE SHIM BETWEEN THE SKIN AND THE FAIL SAFE STRAP. FASTENER / PARTS REMOVED AND REINSTALLED EO NR B767-5350-17922-I APP. 'C' FIG 6 AT Jul 13, 2011 · N307UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA11668217Tee Fitting · corrodedINSPECTION TYPE:C, FUSELAGE RT BS 955 T-FITTING FRETTING FOUND JUST AT INTERNAL SURFACE AROUND THE MOST LOWER FASTENER HOLE. FUSELAGE RT BS 955 REAR SPAR BULKHEAD FITTING AREA 'T-FITTING REPLACED AND REINSTALL IAW EO NR B767-5350-17922-I APP 'D' FIG 6 ORG MATJul 13, 2011 · N307UP · Boeing 76734AF · Fuselage Main, BulkheadSDR IPXA11668181Floorbeam · corrodedINSPECTION TYPE:C, M/D BELOW FLOOR BS 1518, LBL 80 FLOORBEAM FOUND CORROSION. REPAIRED IAW RS R-53-65-37175 REV A & EO B767-5310-43604-A ORIG MAT IS BAC1506-4177-0775T6511 EXTRUSION, TOP FLANGE THICKNESS IS 0.0150, CORROSION BLENDED AREA IS 0.063" DEPTH, 1" Jul 13, 2011 · N307UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA11668179Floorbeam · corrodedINSPECTION TYPE:C, M/D BELOW FLOOR BS 1540 LBL 75 FLOORBEAM FOUND CORROSION. REPAIRED IAW HX RS R-53-65-37170 REV A & EO B767-5310-43603-A. ORIG MAT IS BAC1506-4177-7075T6511 EXTRUSION, TOP FLANGE THICKNESS IS 0.150, CORROSION BLENDED AREA IS 0.050" DEPTH, 1Jul 13, 2011 · N307UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA11668122Skin · dentedINSPECTION TYPE:C, LT WING INBD AFT FLAP LWR SURFACE FOUND DENT MARK. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4 FIG 202, SHEET 1, REV 50.Jul 13, 2011 · N307UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1668007Floor Support · corrodedINSPECTION TYPE:C, M/D BELOW FLOOR, BS 1583-1597, LBL 54, CLIP FOUND CORROSION. M/D BELOW FLOOR AT BS 1583-1597, LBL 54 CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 & SRM 51-40-02, REV 50. ORG MAT'L THICKNESS 0.090" BLEND OUT DEPTH 0.065" WIDTH 0.5" LENGTH 0Jul 13, 2011 · N307UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA11668216Tee Fitting · crackedINSPECTION TYPE:C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD, CRACK FOUND AT T-FITTING 7 O'CLOCK POSITION APPROX .0625". FUSELAGE LT BS 955 REAR SPAR BULKHEAD AREA 'T' FITTING REPLACED AND REINSTALL IAW EO NR B767-5350-17922-I APP 'C' FIG 6 ORIGIANAL MATERIAL IS Jul 11, 2011 · N307UP · Boeing 76734AF · Fuselage Main, BulkheadSDR IPXA11668215Failsafe · crackedINSPECTION TYPE:C, FUSELAGE LT BS 955 B/H, CRACK FOUND AT FAIL SAFE STRAP 3 O'CLOCK POSITION APPROX 0.040". FUSELAGE LT SIDE BS 955 REAR SPAR BULKHEAD FITTING FAIL SAFE STRAP REPAIED EO NR B767-5350-17922-I APP 'C' ORIGINAL MAT'L IS 2024T351-0750" MACHINED STJul 11, 2011 · N307UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA11668150Fairing · delaminatedINSPECTION TYPE:C, RT WING OTBD T/E FLAP MID L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A(1), FIG 5, REV 50.Jul 11, 2011 · N307UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1667973Fairing · delaminatedINSPECTION TYPE:8C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5, REV 50.Jul 11, 2011 · N307UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA11668214Failsafe · crackedINSPECTION TYPE:C, FUSELAGE LT BS 955 REAR SPAR B/H SIDE FTG FAIL SAFE STRAP ULTRASONIC INSP FOUND CRACK INDICATION , REMOVE FASTENER FOR CRACK CONFIRMATION. FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP ATT MOST LOWER BOLT REMOVED AND REJul 9, 2011 · N307UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA11668213Failsafe · crackedINSPECTION TYPE:C, FUSELAGE RT BS 955 REAR SPAR B/H SIDE FTG FAILSAFE STRAP ULTRASONIC INSP FOUND CRACK INDICATION, REMOVE FASTENER FOR CRACK CONFIRMATION. FASTENER RT BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP ATT MOST LWR BOLT REMOVED AND REINSTJul 9, 2011 · N307UP · Boeing 76734AF · Fuselage Main, StructureSDR IPXA1667366Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL POS 4, CENTER HAS 3 EA .2500" HOLES. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Jun 19, 2011 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667363Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL POS 4L HAS HOLE. FABRICATED NEW PANEL IAW EO B767-5320-9693-H.Jun 19, 2011 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667362Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL, POS NR 6 CTR HAS 2 EA HOLES. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Jun 19, 2011 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667361Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL POS 6/7R HAS 2 EA .2500" HOLES. FABRICATED NEW PANEL IAW EO B767-5320-9693-H.Jun 19, 2011 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667360Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL POS NR 5R HAS .2500" HOLE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693.Jun 19, 2011 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667018Floor Panel · damagedHOLE IN MCD FLOOR PANEL 4" FED OF 3RD LOCK FROM AFT END, 6 0" FROM FWD EDGE OF POS 10L. REPAIRED IAW SRM 53-00-50-2R, PARA 4.C.Jun 5, 2011 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667017Floor Panel · damaged.7500" HOLE IN FLOOR PANEL, POS 14L. REPAIRED IAW SRM 53-00-50-2R.Jun 5, 2011 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667015Floor Panel · damagedMAIN CARGO POS 9R FLOOR PANEL 1 EA .250 HOLE. REPAIRED IAW EO B767-5320-9693-H.Jun 5, 2011 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667014Floor Panel · damagedMCD FLOOR PANEL POS 9 CENTER HAS 5 EA .2500" HOLES. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Jun 5, 2011 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11665172Floorboard · damagedFLOORBOARD DAMAGED. FABRICATED NEW FLOORBOARD IAW EO B767-5320-9693-H.Mar 7, 2011 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11665165Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL FROM POS 5/6 RT HAS NUMEROUS .2500 HOLES IN UPPER SKIN. FAB NEW FLOOR PANEL REF EOB767-5320-9693-H.Mar 7, 2011 · N307UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10660719Arm · inoperativeRT SLIDING WINDOW WILL NOT CLOSE PROPERLY. REPLACED AND ADJUSTED LOWER LINK ARM (REF FIG 501, AMM 56-11-02-5 ITEM 7) PERFORMED SATISFACTORY OPS CHECK OF WINDOW REF AMM 56-11-02-6.Jun 25, 2010 · N307UP · Boeing 76734AF · Flight Compartment WindowsSDR IPXA10658912Handle · out of adjustF/O'S SLIDING WINDOW R2 IS DIFFICULT TO OPEN. SEEMS TO BE BINDING WHEN OPENING OR CLOSING. ADJUSTED F/O R2 WINDOW HANDLE. PERFORMED ADJ/TEST IAW MM 56 11 02 5. OPS NORMAL AT THIS TIME.Mar 23, 2010 · N307UP · Boeing 76734AF · Flight Compartment Windows
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