N315UP

Service difficulty reports · 146

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 = 'N315UP' 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 IPXA10658152Floor Support · crackedAFT CARGO COMPT STA 1087 LBL 25" FLOOR SUPPORT CLIP FOUND CRACKED. AFT CARGO COMPT STA 1087 LBL 25" FLOOR SUPPORT CLIP REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 45.Jan 14, 2010 · N315UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA10658151Floor Support · crackedAFT CARGO COMPT STA 1087 RBL 25" FLOOR SUPPORT CLIP FOUND CRACKED. AFT CARGO COMPT STA 1087 RBL 25" FLOOR SUPPORT CLIP REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV 45.Jan 14, 2010 · N315UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA10658195Floor Panel · damagedINSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 654+22 TO 690, L11 TO R11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.Jan 13, 2010 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658221Skin · crackedINSPECTION TYPE: 7C NO,1 PYLON - EXTERNAL SKIN CRACKED AT PYLON PANEL NR 432AL CUTOUT AREA. SKIN REPAIRED IAW HX RS NR R54-50-36587 A MATERIAL 2024T3-0.080" CRACK LENGTH 0.5",0.1875"DIA STOP HOLE DRILLED AT THE CRACK END. THIS REPAIR IS CLASSIFIED AS A MAJOR Jan 12, 2010 · N315UP · Boeing 76734AF · Nacelle/Pylon, Plate/SkinSDR IPXA10658219Fitting · crackedINSP TYPE: C LT WING - INBD MAIN FLAP INBD AFT FLAP HINGE FTG FOUND CRACKED LT WING INBD MAIN FLAP INBD HINGE FTG REPAIRED IAW SRM 57-53-02-2R1 FIG201 REV45 ORG MATL IS 7075T73 FORGING, CRACK LENGTH IS 1.5" AT INBD FLANGE & 0.5" AT OTBD FLANGE. DAMAGED CUJan 12, 2010 · N315UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10658214Floor Support · crackedINSPECTION TYPE:C, AFT BULK CARGO STA 1581 LBL 70" FLOOR ANGLE FOUND CRACKED. AFT BULK CARGO STA 1581 LBL 70" CABIN FLOOR SUPPORT ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 45.Jan 12, 2010 · N315UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA10658213Floor Support · crackedINSPECTION TYPE:C, AFT BULK CARGO STA 1581 RBL 70" CABIN FLOOR ANGLE FOUND CRACKED. AFT BULK CARGO STA 1581 RBL 70" CABIN FLOOR SUPPORT ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 45.Jan 12, 2010 · N315UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA10658194Skin · crackedINSPECTION TYPE:7C, RT WING NR 9 SLAT L/E OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT OTBD AREA AT OSS 641.74 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG201, REV 45. ORG MATL IS CLAD 7075T6-0.063", CRACK LENGTH IS 0.14", DAMAGED CUTOUT IS 8.Jan 12, 2010 · N315UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658193Skin · crackedINSPECTION TYPE:7C, LT WING NR 4 SLAT L/E OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT OTBD AREA AT OSS 641.6 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, REV 45, ORG MATL IS CLAD 7075T6-0.063", REPAIR LENGTH IS 0.15", DAMAGED CUTOUT IS 9" Jan 12, 2010 · N315UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658192Skin · crackedINSPECTION TYPE:7C, LT WING NR 4 SLAT L/E INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT INBD AREA AT OSS 572.875 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG201, REV 45 ORG MATL IS CLAD 7075T6-0.063", CRACK LENGTH IS 0.13", DAMAGED CUTOUT IS 9" Jan 12, 2010 · N315UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658190Skin · crackedINSPECTION TYPE:7C, LT WING NR 3 SLAT L/E OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR3 SLAT OTBD AREA AT OSS792.4 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201 REV45 ORG MATL IS CLAD 7075T6-0.063" CRACK LENGTH IS 0.09" DAMAGED CUTOUT IS 8.875"X7.12Jan 12, 2010 · N315UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10658189Skin · crackedLT WING NR 3 SLAT L/E INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 3 SLAT INBD AREA AT OSS724.4 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201 REV 45 ORG MATL IS CLAD7075T6-0063" CRACK LENGTH IS 0.125" DAMAGED CUTOUT IS 9" X 7.125" THIS REPAIR IS CLJan 12, 2010 · N315UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10658178Fairing · delaminatedINSPECTION TYPE: C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.Jan 12, 2010 · N315UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10658177Fairing · delaminatedINSPECTION TYPE:C, RT WING OTBD T/E FLAP INBD L/E FAIRING DELAMINATION COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.Jan 12, 2010 · N315UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10658220Stiffener · crackedINSP TYPE: 7C AFT OF FWD CARGO CENTER TANK FW LBL 10.94" STIFFENER UPPER FOUND CRACKED STIFFENER UPPER AREA REPAIRED IAW HX RS NR R57-10-36582A MATERIAL BAC1518-749-2024T3511,CRACK LENGTH 0.7" CUT OFF LENGTH 19.5" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WIJan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA10658206Floor Panel · damagedINSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 283 TO 412, L33 TO L55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658205Floor Panel · damagedINSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 1207 TO 1344, L11 TO R11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658204Floor Panel · damagedINSPECTION TYPE: 7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 731 TO 833, L33 TO L55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658203Floor Panel · damagedINSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 1114 TO 1197+22, L11 TO L33. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658202Floor Panel · damagedINSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 1207 TO 1344, R33 TO R55. FLOOR PANEL FABRICATE IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658201Floor Panel · damagedINSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 283 TO 412, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658200Floor Panel · damagedINSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 283 TO 412, RBL 11 TO RBL 33. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658199Floor Panel · damagedINSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 372 TO 412, LBL 55 TO LBL 77. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658198Floor Panel · damagedINSPECTION TYPE:7C, MCD FLOOR PANEL FPIMD DAMAGED AT STN 654+22 TO 690, R11 TO R33. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658197Floor Panel · damagedINSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 833 TO 930, L11 TO L33. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658196Floor Panel · damagedINSPECTION TYPE:7C, MCD FLOOR PANEL FOUND DAMAGED AT STN 654+22 TO 690, L33 TO L55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-06.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10658159Stiffener · crackedINSPECTION TYPE:C, AV COMPT STA 246 FWD RBL 10" CABIN FLOOR STIFFENER FOUND CRACKED. AV COMPT STA 246 FWD RBL 10" CABIN FLOOR STIFFENER REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 45.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA10658157Stiffener · crackedINSPECTION TYPE: 7C, AV COMPT STA 246 AFT LBL 50 CABIN FLOOR STIFFENER FOUND CRACKED. AV COMPT STA 246 AFT LBL 50" CABIN FLOOR STIFFENER REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 45.Jan 11, 2010 · N315UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657617Floor Panel · damagedINSPECTION TYPE:N/A REF D407584 CENTER CARGO FLOOR POS 6 HAS FOUR HOLES MCD. FABRICATED 2 FLOOR PANELS PER B767-5320-9693-F.Oct 11, 2009 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657616Floorboard · dentedINSPECTION TYPE:N/A D407591: MCD POS 11L FLOOR HAS 2 DENTS. FABRICATED NEW FLOORBOARDS PER B767-5320-9693-F.Oct 11, 2009 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657615Floorboard · dentedINSPECTION TYPE:N/A REF D407590: TWO DENTS IN MAIN CARGO DECK FLOORBOARDS POS 4R TRANSFERRED FROM LOG PG 297108 ITEM 3. FABRICATED 2 NEW FLOOR PANELS PER EO B767-5320-9693-F.Oct 11, 2009 · N315UP · Boeing 76734AF · Fuselage Floor PanelSDR UPS08652238Shuttle Valve · malfunctionedINSPECTION TYPE:N/A A/C PULLED LEFT USING AUTOBRAKES. RIGHT BRAKES INOP. REMOVED AND REPLACED AUTOBRAKE SHUTTLE VALVE PER MM 32-42-10-4, NO HELP. REMOVED AND REPLACED NORMAL AUTO SKID MODULE PER MM 32-42-02-4. GROUND OPS CHECKS GOOD AND LEAK CHECKS GOOD, OMay 12, 2008 · N315UP · Boeing 76734AF · Master Cylinder/Brake ValveSDR UPS08651670Yaw Damper · inoperativeA/C YAWED CONTINUOUSLY LT AND RT AT HIGH SPEEDS. T/S FOUND M509 RT UPR YAW DAMPER SERVO LVDT RESISTANCE VALUE ABNORMAL AND M317 O/B SPOILER NR 12 PCA LVDT PIN 8 SHROTED TO CASING. BOTH M509 RT UPPER YAW DAMPER SERVO AND M317 O/B SPOILER NR 12 PCA REPLACED. YFeb 14, 2008 · N315UP · Boeing 76734AF · Rudder Control SystemSDR UPS08651395Valve · malfunctionedINSPECTION TYPE:N/A BTB - A/C TURNS LEFT DURING BRAKING. REMOVED AND REPLACED PARKING BRAKE VALVE IAW AMM 32-44-04-4.Jan 11, 2008 · N315UP · Boeing 76734AF · Landing Gear Brake SystemSDR UPS07650450Computer · inoperativeINSPECTION TYPE:ETOP BTB - LT FMC SINGLE SOURCE MESSAGE. (08-17-07] ACCOMPLISHED FIM 34-61-00 FIG 108A, ALL TESTS PASSED. THE SYSTEM IS OK.Aug 15, 2007 · N315UP · Boeing 76734AF · Flight Management Computing Hardware SystemSDR UPS07649629Window · defectiveINSPECTION TYPE:N/A CREW PREFLIGHT - CAPTAIN'S SIDING WINDOW HARD TO OPEN. A/C REMOVED FROM SERVICE. REMOVED AND REPLACED L2 WINDOW PER 56-11-02-4.Apr 17, 2007 · N315UP · Boeing 76734AF · Flight Compartment WindowsSDR UPS06647997Acars · inoperativeACARS - NO COMMUNICATION. TRANSMISSION ON LT HF INOP AT ALL STATIONS. T/S FOUND LT HF TRANSCEIVER FAULT. R/R LT TRANSCEIVER. OP CHECK NORMAL PER MM 23-11-03.Sep 13, 2006 · N315UP · Boeing 767300 · HF Communications SystemSDR UPS06646621Seat Track · corrodedAREAS OF CORROSION ON SEAT TRACK AT BS 512, BS 556, BS 576, BS 619 LBL 88 WL 200. REMOVED AND REPLACED SEAT TRACK PER DWG 143T5242 AND SRM 51-40-02, 51-40-03.Mar 14, 2006 · N315UP · Boeing 767300 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05645480Generator · leakingATB - RT GENERATOR FAILED, EMERGENCY DECLARED. SERVICE RT IDGE WITH 2 QTS OIL GWL 0558164/REMOVED NR 2 ENG IDG IAW MM 24-11-01 DW 0558595\ TRANSFERRED FITTINGS WITH NEW O-RINGS TW 1229598 REF MM 24-11-01 INSTALLED NEW IDGE ON NR 2 ENG OPS AND LEAK CK GOOD.Sep 23, 2005 · N315UP · Boeing 767300 · AC Generation SystemSDR UPS05645401Generator · disconnectedINSPECTION TYPE: ETOP ATB - DUE RT GEN DRIVE MSG DISPLAYED ON T/O AT 100 KTS. ONE ELEC SOURCE REMAINING. FOUND RT GEN DISCONNECTED AND OIL LEVEL LOW AND FILL UNION LOOSE. RECONNECTED IDG IAW 24-11-01. TIGHTENED FILL UNION AND SERVICED IDG IAW 12-13-03-3 ENSep 10, 2005 · N315UP · Boeing 76734AF · Alternator-Generator DriveSDR UPS05643993Control Panel · inoperativeEMERGENCY LIGHT SWITCH PANEL ANNUNCIATOR DOES NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL PANEL AND PERFORMED CHECK OK IAW 33-51-08.Mar 1, 2005 · N315UP · Boeing 76734AF · Emergency LightingSDR UPS04642147Engine · flamed outINSPECTION TYPE: ETOP, RT ENGINE FLAMED OUT WHEN POWER WAS REDUCED FOR LANDING. OBVIOUSLY NO RE-START ATTEMPTED. NO ENG PARAMETER EXCEEDENCE OBSERVED. REPLACED RIGHT ENG PER TC 6002 & TC 6001 OP'S CHECK SATISFIED.Apr 16, 2004 · N315UP · Boeing 76734AF · Engine (Turbine/Turboprop)SDR UPS03641620Clamp · brokenINSPECTION TYPE:ETOP ATB - LT PACK INOPERATIVE LIGHT ILLUM AND LT (PACK TEMP) EICAS MESSAGE. LIGHT DID NOT EXTINGUISH WHEN STBY SELECTED AND RESET PUSHED. REMOVED AND REPLACED BROKEN CLAMP TO HEAT EXCHANGER RVM, LT PACK. OPS CHECK NORMAL IAW MM 21-50-0Dec 2, 2003 · N315UP · Boeing 767300 · Cabin Cooling SystemSDR UPS03640413Light · inoperativeINSPECTION TYPE: ASV, EMERGENCY LIGHT ABOVE LT SUPERNUMERARY SEAT INOP. RELAMPED, OPS CHECKS OK.Apr 5, 2003 · N315UP · Boeing 76734AF · Emergency LightingSDR UPS00632550Skin · crackedINSPECTION TYPE:N/A, MX INSPECTION - LT WING UPPER SKIN PANEL CRACKED INC NR RSOO-118. *S/D* REMOVED AND REPLACED PANEL IAW SRM 51-40-0 (P/N 113T1654-235).May 9, 2000 · N315UP · Boeing 767300 · Wing, Plate/SkinSDR UPS99631232Gear Lever · malfunctionedGEAR LEVER WOULD NOT MOVE TO UP POS INFLT WAS FREE TO MOVE TO UP POS WHEN LOCK OVRH PUSHER. FLIGHT RETURNED TO SDF PER AMC. AIR TURN BACK, FOUND LEVER LOCK CIRCUIT BREAKER NOT COMPLETELY IN. RESET BREAKER AND OPS CHECKED LANDING GEAR CONTROL PER MM 32-31-00Dec 21, 1999 · N315UP · Boeing 76734AF · Landing Gear Retraction/Extension System
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