N455UP

Service difficulty reports · 211

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 = 'N455UP' 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 IPXA1565280Floor Panel · corrodedINSPECTION TYPE:C4, MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 480 TO 560 RBL 46 TO RBL 61 HAS DELAMINATION, BROKEN AND CORRODED INSERT. FABRICATED NEW FLOOR PANEL IAW EO 757-5320-7692-6.Feb 28, 2011 · N455UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA1565279Floorboard · damagedINSPECTION TYPE:C4, MAIN CARGO COMPARTMENT FLOORBOARD AT STA 879 TO 900 RBL 1 TO RBL 26 HAS EDGE DAMAGE. FABRICATED NEW FLOORBOARD IAW EO B-757-5320-9692.Feb 28, 2011 · N455UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA11565194Floorboard · damagedINSPECTION TYPE:C4, MAIN CARGO COMPARTMENT FLOORBOARD 231 XSF AT STA 820 TO 879 LBL 26 TO LBL 45 HAS PUNCTURE AND EDGE DAMAGE. REPLACED FLOORBOARD IAW EO B757-5320-9692.Feb 28, 2011 · N455UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA1565728Floor Support · corrodedINSPECTION TYPE:C4, FWD CREW ENTRY STA 310-324 LBL 64, WL 208 SUPPORT CHANNEL NEAR DRAIN CORROSION UNDER NUTPLATES AND ON TOP AT AFT HOLE. REMOVED CORROSION ORIGINAL THICKNESS .050 LOSS .006 WITH .044 REMAINING IS OUT OF LIMITS IAW SRM 53-10-51 ACCOMPLISHED BFeb 22, 2011 · N455UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA1565727Floor Support · corrodedINSPECTION TYPE:C4, FWD CREW ENTRY STA 297-310, LBL 64, WL 208 SUPPORT CHANNEL NEAR DRAIN CORROSION UNDER NUTPLATES. REMOVED CORROSION ORIGINAL MATERIAL THICKNESS .050 LOSS OF .003 TO .01 0 WITH .043 TO .040 REMAINING OUT OF LIMITS IAW SRM 53-10-51 ACCOMPLISHFeb 22, 2011 · N455UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA1565717Floorbeam · corrodedINSPECTION TYPE:C4, MAIN DECK FLOOR STRUCTURES LT SIDE STA BS 1681.8 BETWEEN LBL 45. 5 TO LBL 54.9 HAS CORROSION. REMOVED CORROSION ORIGINAL THICKNESS .07K LOSS .025 WITH .046 REMAINING IS OUT OF LIMITS IAW SRM 53-00-51-1A . ACCOMPLISHED BLEND REPAIR FOR EFeb 22, 2011 · N455UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA11565548Floorbeam · corrodedINSPECTION TYPE:C4, MAIN DECK FLOOR STRUCTURE LT SIDE STA 1600 BETWEEN LBL 45.5 TO L BL 54.9 HAS CORROSION AROUND SEVERAL FASTENER HOLES. REPAIRED PER EA 110184 REV IRFeb 22, 2011 · N455UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA1565292Floorboard · damagedINSPECTION TYPE:C4, MAIN CARGO COMPARTMENT LT SIDE STATIONS BS 1600 TO BS 1681.8 FLOORBOARD 251 XQF HAS MULTIPLE DAMAGED/MISSING INSERTS AND EDGE DAMAGE FORWARD INBD SIDE. REPLACED PANEL IAW EO B757-5320-9692-G.Feb 22, 2011 · N455UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA1565287Floor Panel · damagedINSPECTION TYPE:C4, MAIN CARGO FLOOR PANEL NR 252 XHF DAMAGED ON LOWER SURFACE AT RT FWD EDGE. REPLACED MAIN CABIN FLOOR PANEL 252 XAF IN REF TO SRM 53-00-50-2R1 IAW B757-5320-9692-G.Feb 22, 2011 · N455UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA1565285Floor Panel · damagedINSPECTION TYPE:C4, MAIN CABIN FLOOR PANEL NR 251XHF DAMAGED ON LOWER SURFACE AT INSERT RT EDGE. FABRICATED NEW FLOOR PANEL IAW EO B757-5320-9692.Feb 22, 2011 · N455UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA1565724Seat Track · corrodedINSPECTION TYPE:C4, MAIN CARGO COMPARTMENT STA 1100 TO STA 1180 LBL 60" SEAT TRACK HAS LIGHT CORROSION. REMOVED SEAT TRACK FROM STA 1080 TO 1180 FABRICATED REPLACEMENT SEAT TRACK AND INSTALLED IAW SRM 51-40-02 AND DWG 144N5016 SEAT TRACK MADE FR OM BAC 1520-2Feb 20, 2011 · N455UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA1565609Seat Track · corrodedINSPECTION TYPE:C4, MAIN CARGO COMPARTMENT STA 1038 TO STA 1042, RBL 60" SEAT TRACKHAS LIGHT CORROSION AT FASTENER HOLES. REPLACED SECTION OF SEAT TRACK FROM STA 900 - 1080 IAW DWG 144N501 7 AND SRM 51-40-02.Feb 20, 2011 · N455UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA1565586Seat Track · corrodedINSPECTION TYPE:C4, MAIN CARGO COMPARTMENT STA 1120 TO STA 1200, LBL 26 SEAT TRACK HAS LIGHT CORROSION THROUGHOUT UPPER FLANGE. R & R SEAT TRACK.Feb 20, 2011 · N455UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA1565726Floorbeam · corrodedINSPECTION TYPE:C4, MAIN CARGO COMPARTMENT STA 1020 LBL 1 TO LBL 24 FLOORBEAM HAS LIGHT CORROSION. R & R FLOORBEAM IAW 51-40-02 AND DWG 144N5005 DUE TO CORROSION OUT OF LIMITS. ORIGINAL MATERIAL .050 LOSS .011 REMAINING .039.Feb 19, 2011 · N455UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA1565725Floorbeam · corrodedINSPECTION TYPE:C4, MAIN CARGO COMPARTMENT STA 900 LBL 6 TO LBL 16 FLOORBEAM HAS CORROSION. REMOVED CORROSION ORIGINAL MATERIAL .050 LOSS OF .009 REMAINING .041 OUT OF LIMITS IAW SRM 53-00-51-1A-1, FABRICATED AND REPLACED FLOORBEAM IAW SRM 51-40-02 AND DWG 14Feb 19, 2011 · N455UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA11565660Frame · crackedINSPECTION TYPE:C4, LOWER FWD FUSELAGE FRAME CRACKED AT WIRE BUNDLE SUPPORT ATTACH POINT INBD FASTENER HOLES, STA 345 BETWEEN STRINGERS 22L AND 21L. REMOVED DAMAGE AND REPAIRED FRAME IAW EA 110190 EO B757-5310-41 936-A.Feb 19, 2011 · N455UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA11565658Floorbeam · corrodedINSPECTION TYPE:C4, MAIN CARGO COMPARTMENT STA 1055, LBL 46 TO LBL 59, FLOOR SUPPORT HAS CORROSION. REPLACED FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 144N 5005.Feb 19, 2011 · N455UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA11565529Floorbeam · corrodedINSPECTION TYPE:C4, MAIN CARGO COMPARTMENT STA 1028, RBL 1 TO RBL 24 FLOOR SUPPORT HAS LIGHT CORROSION FABRICATED NEW AND INSTALLED.Feb 19, 2011 · N455UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA11565525Frame · gougedINSPECTION TYPE:C4, MAIN CABIN LT SIDE BS 1460 BELOW STRINGER 15L FRAME GOUGED ON INBOARD FLANGE. DRILLED OUT GOUGE TO .160 AND INSTALLED BACR15BB5AD RIVET IAW EO B757-5310-39560.Feb 18, 2011 · N455UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA11565524Stringer · gougedINSPECTION TYPE:C4, MAIN CABIN LT BS 1540 BELOW STRINGER 15L, FRAME GOUGES ON INBD FLANGE. DRILLED OUT DAMAGE AND INSTALL RIVET IAW EO B757-5310-39560.Feb 18, 2011 · N455UP · Boeing 75724APF · Fuselage Main, Longeron/StringerSDR IPXA11565523Stringer · gougedINSPECTION TYPE:C4, MAIN CABIN LT SIDE, BS 1340 BELOW STRINGER 15L FRAME GOUGED ON INBD FLANGE. DRILLED OUT DAMAGE AND INSTALLED 2 BACR15BB6AD RIVETS IAW EO B757-53 10-39560.Feb 18, 2011 · N455UP · Boeing 75724APF · Fuselage Main, Longeron/StringerSDR IPXA11565522Stringer · gougedINSP TYPE:C4 MAIN CABIN LEFT SIDE BS 1220 STRINGER 15L FRAME GOUGED ON INBD FLANGE. DRILLED OUT DAMAGE TO .186 AND INSTALLED BACR15BB6AD RIVET IAW EO -5310-39560Feb 18, 2011 · N455UP · Boeing 75724APF · Fuselage Main, Longeron/StringerSDR IPXA11565457Frame · dentedINSPECTION TYPE:C4, FWD PIT FRAME DENTED AT STATION 780 AT STRINGER 23L. CUTOUT DAMAGE AND INSTALLED DOUBLER IAW SRM 53-00-07-2R-J INSP R EQUIREMENTS 37,500 FLIGHT CYCLES AFTER REPAIR INSTALLED ON 50,000 AIRFRAME FLIGHT CYCLES WHICH EVER COMES FIRST, INTERNAFeb 17, 2011 · N455UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA1565719Frame · damagedINSPECTION TYPE:C4, DAMAGE TO FRAME 600 BELOW STR 16R MAIN CARGO DECK. REPAIRED IAW EA 110162, REV IR.Feb 15, 2011 · N455UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA11565659Frame · damagedINSPECTION TYPE:C4, DAMAGE TO FRAME 580 BELOW STR 16R MAIN CARGO DECK REPAIRED FRAME IAW EA 110172.Feb 15, 2011 · N455UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA11565588Frame · damagedINSPECTION TYPE:C4, DAMAGE TO FRAME 480, STR 15R, MAIN CARGO DECK. REPAIRED FRAME IAW EA 110171 EO B757-5310-41904-A.Feb 15, 2011 · N455UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA11565531Frame · damagedINSPECTION TYPE:C4, DAMAGE TO FRAME 820, STRINGER 15L MAIN CARGO DECK, DRILLED OUT DAMAGE TO .199 AND INSTALLED BACR15BB6AD RIVET IAW EO B757 -5310-39560.Feb 15, 2011 · N455UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA11565521Stringer · damagedINSPECTION TYPE:C4 DAMAGE TO FRAME 860 AT STRINGER 15R MAIN CARGO DECK DRILLED OUT DAMAGE TO .191 AND INSTALLED BAC R15BB6AD RIVET IAW EO B757 -5310-39560.Feb 15, 2011 · N455UP · Boeing 75724APF · Fuselage Main, Longeron/StringerSDR IPXA1565288Floor Panel · damagedINSPECTION TYPE:C4, EXPOSED CORE ON MAIN DECK FLOOR PANEL 232 MF. REPLACED PANEL 232 MF IAW EO B757-5320-9692-G.Feb 15, 2011 · N455UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA1565282Floorboard · brokenINSPECTION TYPE:C4, FLOORBOARD INSERT BROKEN OUT, PANEL NR 231 XEF. REPLACED FLOORBOARD NR 231XEF IAW EO B757-5320-9692-G.Feb 15, 2011 · N455UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA1564219Floor Panel · damagedINSPECTION TYPE:N/A MCD FLOOR PANEL AT POS 9R HAS 2 SMALL HOLE. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-50-2R, REPAIR 1.Jan 15, 2011 · N455UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA09557118Frame · dentedINSPECTION TYPE:C DENTS ON AFT PIT FRAME STA 1340 ABOVE STR 25R & 26R. DENT STA 1340 S25R OUT OF LIMITS IAW SRM 53-00-07-1A 1 FIG 101. HFEC CUTOUT IAW NDT PT6 51-00-16 NO CRACKS NOTED. FAB'D PART PER TRAVELER T9/801181. REPAIR INSTALLED IAW EA 757- 5362-27Aug 3, 2009 · N455UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA09555313Door Frame · damagedINSPECTION TYPE:C ("04 ITEM") FWD CARGO DOOR JAM AT STA 620 HAS 2EA MISDRILLED HOLES HOLES IN WEB & CHORD. REMOVED DAMAGED BRACKET PER SRM 51-40-02. DIM OF DAMAGE HOLES: A UPPER HOL .330" ORIG HOLE .250 B LWR HOLE .315 IRUG GIKE .250 PER DRW NT143N8522. REMMar 5, 2009 · N455UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA09555156Structure · chafedINSPECTION TYPE:C NR 2 V-BAND GROOVE HAS A CHAFED MARK AT 11 O'CLOCK POSITION. HAND BLEND CHAFE AREA IAW EO535-7230-32641 PG 4 APP A PG 1, 2 PER SP TASK70-42-11-300-001. HFEC REQRK IAW NTM51-00-19PT6 PER EO 535-7230- 32641P1 NO CRACK FOUND. APPLY CHROMATE CFeb 24, 2009 · N455UP · Boeing 75724APF · Turbine Engine Compressor SectionSDR IPXA09555155Structure · chafedINSPECTION TYPE:C NR 2 V-BAND GROOVE HAS A CHAFED MARK AT 11 O'CLOCK POSITION. HAND BLEND CHAFE AREA IAW EO535-7230-32641 PG 4 APP A PG 1, 2 PER SP TASK70-42-11-300-001. HFEC REQRK IAW NTM51-00-19PT6 PER E0535-7230- 32641P1 NO CRACK FOUND. APPLY CHROMATE COFeb 24, 2009 · N455UP · Boeing 75724APF · Turbine Engine Compressor SectionSDR IPXA09555047Structure · chafedINSPECTION TYPE:C NR 2 ENGINE V-BAND GROOVE HAS CHAFED MARK AT 1'OCLOCK POSITION. HAND BLENDED CHAFED AREA IAW EO535-7230-32641P4 APP Z PG 1, 2 ST 1 PER SPM TASK 70-42-11-300-001. HFEC REWORK AREA IAW NTM51-00-19PT6 PER EO 535-7230-32641 P1, NO CRACK FOUND. Feb 24, 2009 · N455UP · Boeing 75724APF · Turbine Engine Compressor SectionSDR IPXA09555046Structure · chafedINSPECTION TYPE:C NR 2 ENG V-BAND GROOVE HAS CHAFED MARK AT 1 O'CLOCK POSITION. HAND BLND CHAFED AREA IAW EO535-7230-32641 PG 4 APP A PG 1, 2 STP1 PER SPM TASK70-42-11-300-001. HFEC REWRK IAW NTM51-00-19PT6 PER EO535-7230- 32641P1, NO CRACK FOUND. APPLIED CFeb 24, 2009 · N455UP · Boeing 75724APF · Turbine Engine Compressor SectionSDR IPXA09555048Frame · dentedINSPECTION TYPE:C FRAME DENTED AT STA 1340 STR 25L. FOUND DAMAGE OUT OF LIMIT IAW SRM 53-00-07-1A1, FIG 101 SHT 1, NO DENT ALLOWED. DAMAGE IS .9"LX.6"WX.009"D. TRIMMED OUT DENT DAMAGE IAW SRM 53-00-07-2R, FIG 201 STEP 1. TRIMMED OUT AREA .905"L, 1.3"W. HFFeb 23, 2009 · N455UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA09554969Frame · dentedINSPECTION TYPE:C DENT AT FWD CARGO COMP FUSELAGE FRAME STA 700 S24R. DENT IS D=.015 W=.310 L=.520. TRIMMED OUT DENT DAMAGE IAW SRM 53-00-07- 2R, FIG 201 SHT 1, STEP 1. SIZE OF TRIM OUT IS L=.650" W=1.2". PERFORMED HFEC IAW NTM51-00-19PT6 OF DAMAGE CONTENTFeb 21, 2009 · N455UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA09554968Frame · dentedINSPECTION TYPE:C DENT AT FWD CARGO FUSELAGE FRAME STA 720, S23R-S24R. DENT IS W=.450 L=.620 D=.0250. TRIM OUT DENT DAMAGE IAW SRM 53-00-07- 2R FIG201 SHT 1 STEP 1 SIZE OF TRIM OUT L=.70" W=1.30". PERFORMED HFEC IAW NTM 51-00-19 PT6 OF DMG CUTOUT AREA. NO Feb 21, 2009 · N455UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA09555130Skin · gougedINSPECTION TYPE:C LEFT O/B FLAP I/B UPPER SKIN PREVIOUS REPAIR HAS 2 (EA) EVENLY SPACED GOUGES LOCATED BEHIND NR 3 SPOILER ACTUATOR 25 INCHES FWD OF T/E PER E.0. B757-5100-30760-B APPENDIX 'C' CONTACT ON SITE ENGR FOR DISPO. OUT OF LIMITS SRM 57-53-01-1A. REMFeb 20, 2009 · N455UP · Boeing 75724APF · Trailing Edge FlapsSDR IPXA09555129Skin · gougedINSPECTION TYPE:C LEFT O/B FLAP I/B UPPER SKIN PREVIOUS REPAIR HAS A GOUGE REPAIR LOCATE 35.0 INCHES FROM I/B EDGE 25 INCHES FWD OF T/E PER EO B757-5100-30760-B APPEN 'C', CONTACT ON SITE ENGR FOR DISPO. OUT OF LIMIT SRM 57-53-01-1A (2) REMOVED PREV REPAIR SRFeb 20, 2009 · N455UP · Boeing 75724APF · Trailing Edge FlapsSDR IPXA09555044Frame · dentedINSPECTION TYPE:C FRAME STATION 1300 HAS A DENT BETWEEN S22R TO S23R. DNT L=.991W=.490DPTH=.039. TRIM OUT DENT DAMAGE IAW EA757-5362-27-A1836 STP1 PRELIM2 TRM SZ:W=1.5"X L=1.09". REMOVED FASTENERS CMMN TO REPAIR FOR HFEC INSP IAW SRM 51-40-02, EA757-5362-27Feb 19, 2009 · N455UP · Boeing 75724APF · Fuselage Main, FrameSDR UPS09554277Floor Panel · dentedINSPECTION TYPE: N/A CENTER OF FLOOR PANEL AT POS 7/8 LT, 1 INCH DENT WITH CRACK IN TOP SHEET. REPAIRED IAW EO B757-5320-31573.Jan 5, 2009 · N455UP · Boeing 75724APF · Fuselage Floor PanelSDR UPS08554207Roller · out of adjustINSPECTION TYPE:N/A L2 WINDOW WILL NOT OPEN. ADJUSTED LOWER AFT ROLLER. ACCOMPLISHED NR 2 WINDOW LATCHING SYS HANDLE ALL WORK PER MM 56-11-02-5. OK FOR SERVICE.Dec 15, 2008 · N455UP · Boeing 75724APF · Flight Compartment WindowsSDR UPS08554188Flap · damagedINSPECTION TYPE:N/A LT OUTBOARD AFT FLAP T/E LWR SURFACE INTERIM REPAIR. REPAIRED FLAP PER B757-5750-31551-A.Dec 13, 2008 · N455UP · Boeing 75724APF · Trailing Edge FlapsSDR UPS08554135Window · out of adjustINSPECTION TYPE:N/A L2 WINDOW HARD TO OPERATE. ADJUSTED L2 WINDOW PER MM 56-11-02-5.Dec 9, 2008 · N455UP · Boeing 75724APF · Flight Compartment WindowsSDR UPS08553972Skin · damagedINSPECTION TYPE:N/A LIGHTNING STRIKE DAMAGE TO FASTENER LOCATED AT FUSELAGE BS 395.0 STRINGER 3 LEFT. DAMAGE BEYOND SRM LIMITS. DAMAGED REPAIRED PER EO B757-5330-31068-A.Oct 31, 2008 · N455UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR UPS08553421Seal · brokenINSPECTION TYPE:N/A 5TH & 6TH FROM FWD EMERGENCY DESCENT DEVICE HAS SEALS BROKEN. REMOVED AND REPLACED DESCENT DEVICE PER AMM 25-61-00-4 IN 5TH & 6TH POSITION.Sep 26, 2008 · N455UP · Boeing 75724APF · Emergency EquipmentSDR UPS08553422Seal · brokenINSPECTION TYPE:N/A FWD EMERGENCY DESCENT DEVICE HAS BOTH SEALS MISSING/BROKEN. REMOVED AND REPLACED DESCENT DEVICE PER MM 25-61-00-4.Sep 25, 2008 · N455UP · Boeing 75724APF · Emergency Equipment
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