N253UP
Service difficulty reports · 363
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 = 'N253UP' 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.
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 = 'N253UP' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IPXA2020100861077Angle · crackedINSPECTION TYPE: 2C MAIN CABIN T ANGLE AT STA 1339 AND LONG 15 L IS CRACKED. REMOVED, FABRICATED, AND REPLACED T ANGLE, IAW DWG AEA7568 AND SRM 51-35-01. (MINOR)SDR IPXA2020100861076Angle · crackedINSPECTION TYPE: 2C MAIN CABIN T ANGLE AT STA 1339 AND LONG 15R IS CRACKED. REMOVED, FABRICATED, AND REPLACED ANGLE, IAW DWG AEA7568 AND SRM 51-35-01. (MINOR)SDR IPXA2020100861067Angle · crackedINSPECTION TYPE: 2C MAIN CABIN "T" ANGLE AT STA 1221 AND LONG 15L IS CRACKED. REMOVED, FABRICATED, AND REPLACED T ANGLE, IAW DWG AEA7568 AND SRM 51-35-01. (MINOR)SDR IPXA2020100661008Doubler · crackedINSPECTION TYPE: 2C LT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 636.84 TO 643.5. REPAIRED CRACKED LT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 636.84 TO 643.5, IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)SDR IPXA2020101561325Floorbeam · crackedINSPECTION TYPE: 2C LOWER FWD CARGO FLOOR BEAM IS CRACKED AT STA 6-70 AND X= -57.5. REPAIRED CRACKED FLOOR BEAM AT STA 6-70 AND X= -57.50, IAW VT-SAA EA 011-5340-01-A8593 REV I/R AND UPS EO MD11-5340-78173-A. (MAJOR)SDR IPXA2020101161174Stanchion · corrodedINSPECTION TYPE: 2C CORROSION ON VERTICAL STANCHION AT FWD CARGO AFT BULKHEAD AT STA Y=6-73 X= -28.05 BETWEEN Z= -19 Z= -117. REMOVED, FABRICATED, AND INSTALLED VERTICAL STANCHION, IAW DWG A6A7094 (MINOR).SDR IPXA2020101161173Stanchion · corrodedINSPECTION TYPE: 2C FWD CARGO AFT BULKHEAD AT STA 6-70 LT THE 5TH VERTICAL BEAM HAS CORROSION. REMOVED, FABRICATED, AND INSTALLED VERTICAL STANCHION AT STA Y=6.73 AND X= -9.05 BETWEEN Z= -19 AND Z= -117, IAW DWG AGA7094 (MINOR).SDR IPXA2020101061137Stiffener · crackedINSPECTION TYPE: 2C RT WING TRAILING EDGE FALSE SPAR HAS 1 EA VERTICAL STIFFENER CRACKED JUST BELOW NR 1 SPOILER. REMOVED STIFFENER, FABRICATED, AND INSTALLED AT RT WING TRAILING EDGE FALSE SPAR JUST BELOW NR 1 SPOILER, IAW SRM 51-33-01 (MINOR).SDR IPXA2020100861072Stiffener · crackedINSPECTION TYPE: 2C RT MLG WHEEL WELL AFT LOWER WEB HAS 2 EA CRACKED VERTICAL STIFFENERS. REMOVED AND REPLACED 2 EA CRACKED VERTICAL STIFFENERS AT RT MLG WHEEL WELL AFT LOWER WEB, IAW MD-11 SRM 51-35-01. (MINOR)SDR IPXA2020100861068Stiffener · crackedINSPECTION TYPE: 2C CENTER CARGO ST STA 1841 AND LBL=24, THE VERTICAL STIFFENER IS CRACKED. REMOVED, FABRICATED, AND REPLACED STIFFNER, IAW DWG AGA7170 AND SRM 51-35-01. (MINOR)SDR IPXA2020100661021Channel · damagedINSPECTION TYPE: 2C LOWER FWD CARGO DOOR ENTRY WAY 1ST HAT CHANNEL IS DAMAGED. REMOVED, FABRICATED AND REPLACED CHANNEL, IAW DWG ADA8012 AND SRM 51-35-01. (MINOR)SDR IPXA2020100661009Doubler · crackedINSPECTION TYPE: 2C RT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 734.7 TO 740.8. REPAIRED CRACKED RT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 734.7 TO 740.8, IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)SDR IPXA2020100661007Doubler · crackedINSPECTION TYPE: 2C RT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 610 TO 616. REPAIRED CRACKED RT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 610 TO 616, IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)SDR IPXA2020100661006Doubler · crackedINSPECTION TYPE: 2C RT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 653 TO 658. REPAIRED CRACKED RT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 653 TO 658, IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)SDR IPXA2020100861085Doubler · crackedINSPECTION TYPE: 2C LT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 728 TO 740. REPAIRED CRACKED LT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 728 TO 740, IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)SDR IPXA2020100661011Doubler · crackedINSPECTION TYPE: 2C LT WING FIXED LEADING EDGE BEADED DOUBLER IS CRACKED BETWEEN STA XOS 643 TO 648. REPAIRED CRACKED LT WING FIXED LEADING EDGE BEADED DOUBLER BETWEEN STA XOS 643 TO 648, IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)SDR IPXA2020101061147Doubler · crackedINSPECTION TYPE: 2C RT MLG DOOR INNER LOWER FWD CORNER DOUBLER CRACKED AT RADUIS. REMOVED CRACKED DOUBLER AND INSTALLED NEW CORNER ASSEMBLYY AT RT MLG DOOR LOWER FWD CORNER, IAW SRM 51-31-01 (MINOR).SDR IPXA2020101061140Bracket · crackedINSPECTION TYPE: 2C RT MLG WHEEL WELL SYSTEM NR 1 HYD ACCUMULATOR LOWER SUPPORT BRACKET CRACKED AT BOTH ENDS. REMOVED CRACKED BRACKET, FABRICATED, AND INSTALLED IN RT MLG WHEEL WELL BELOW SYSTEM NR 1 ACCUMULATOR, IAW SRM 51-31-01 (MINOR).SDR IPXA2020101061138Angle · crackedINSPECTION TYPE: 2C RT MLG WW CUTOUT AT FWD END HAS A CRACKED ANGLE. REMOVED CRACKED ANGLE, FABRICATED, AND INSTALLED IN RT MLG WW FWD END CUT OUT, IAW SRM 51-35-01. MINORSDR IPXA2019072344788Unknown · odorINSPECTION TYPE:N/A DURING CLIMB STRONG ODOR OF OVERHEAT CONDITION COMING FROM THE DUCTING TO THE COCKPIT. AIR SYNOPTIC SHOWED THE #1 PACK RUNNING VERY HOT. OUTLET TEMP. WAS 120* F. COCKPIT SUPPLY DUCT TEMP WAS 123*F. COCKPIT TEMP WAS 80*F AND RISING TEMPPERFOSDR IPXA2019071944630Spring · defectiveINSPECTION TYPE:N/A L1 DOOR UPPER PANNEL STICKS WHILE CLOSING SLAMMING FORWARD TOWARDS THE DOOR FRAME. DEFERRED IAW MEL 52-10-3-1-2-1, M677304 ASSIGNED, PLACARD INSTALLED.. **SUPPLEMENTAL SDR** R/R L1 DOOR SLIDING CEILING PANEL SPRING IAW AMM 25-23-23-401. C/WSDR IPXA2019060542771Switch · inoperativeL1 DOOR EVACUATION SLIDE REMOTE PRESS TO TEST SWITCH INOP.R/R REMOTE PERESSURE INDICATOR ASSY IAW AMM 25-61-04. THIS CLEARS M671830SDR IPXA2019040140648Drive Chain · brokenL1 DOOR EMERGENCY DRIVE CHAIN BROKEN. REPLACED DRIVE CHAIN REF CMM 52-11-09SDR IPXA2019013038476Bottle · low pressureR1 DOOR PNEUMATIC BOTTLE PRESS FOR EMERGENCY OPENING IS LOW. DEFERRED R1 DOOR PER MEL 52-10-3-1-2-1. R/R R1 DOOR STORAGE RESERVOIR PER MD11 52-11-04 000-801 AND 52-11-04-0400-801 SYSTEM CHECKS OK.SDR IPXA2019012938433Bottle · low pressureDUE PREFLT FOUND RT SLIDE EMERGENCY BOTTLE PRESS LOW. DUE TIME OK TO DEF PER MEL52-10-3-1-2-1. REPLACED BATTERIES. OPS NORMAL REF AMM 25-61-01-710-802.SDR IPXA2018101735091Altimeter · malfunctionedPASSING FL 180 DURING CLIMB, THE FIRST OFFICER LOST ALL CONTROL OF HIS BARO ALTIMETRY, ALT DISPLAYED BOTH EAD'S, ALT WINDOW ON AFS PANEL WENT BLANK, NO CONTROL WITH ALTITUDE KNOB. AIRSPEED HDG ALSO BLANKED WITH NO CONTROL, AUTO THROTTLES LOCKED. AIR TURN BSDR IPXA2018100394638Bracket · crackedRT WING T/E BRACKET WAS CRACKED, BELOW THE NR 1 SPOILER, INBD MOUNT. REMOVED AND REPLACED THE BRACKET IAW SRM 51-33-01. MINOR.SDR IPXA2018100134602Spar Cap · corrodedRIGHT WING REAR SPAR UPPER CAP AFT FLANGE WAS CORRODED BETWEEN XORS 561 - 575. REPAIRED THE SPAR UPPER CAP AFT FLANGE IAW EA 011-5710-01-A7477, REV I/R, AND EO MD11-5710-70099-A. MINOR.SDR IPXA2018092874473Longeron Splice · crackedLONGERON SPLICE 1R WAS CRACKED AT STATION 5-123. REMOVED AND REPLACED THE LONGERON SPLICE IAW SRM 51-31-01, AND 51-33-01. MINOR.SDR IPXA2018100534697Fastener · looseNR 2 ENGINE INLET NOSE SKIN HAD LOOSE BLIND FASTENERS. REPAIRED IAW EA 011-7110-01-A7465, REV IR, AND EO MD11-7110-58061-B. MINOR.SDR IPXA2018100394641Inlet · crackedNR 2 ENGINE INLET LIP HAD A CRACK AT THE 1:00 O`CLOCK POSITION, AT A FASTENER. REPAIRED THE NR 2 ENGINE INLET LIP IAW SRM 54-10-01, REPAIR 4. MINOR.SDR IPXA2018100394619Trunnion · damagedNLG, RT TRUNNION, INBD HAT BUSHING WAS BROKEN. FOUND THE RT NLG TRUNNION, INBD BUSHING BORE SPOT FACE OUT OF LIMITS. REPAIRED THE NLG TRUNNION BUSHING BORE IAW EA 011-5310-01-A7469, REV IR, AND EO MD11-531070137-A. MINOR.SDR IPXA2018100124508Longeron · corrodedLONGERON 51L HAD CORROSION AT BS 1857. REPAIRED THE LONGERON BETWEEN BS 1862.47 TO 1887.0 IAW SRM 53-00-05, REPAIR 1, FIG 201, & 202. MAJOR.SDR IPXA2018100134604Skin · crackedNR 1 ENGINE, RT CORE COWL WAS CRACKED AND HAS A DOUBLER REPAIR AT THE AFT LATCH. REPAIRED IAW EA 011-5430-01-A7482, REV I/R, AND EO MD11-7110-70101-A. MINOR.SDR IPXA2018100134603Filler · damagedTAILCONE HAD CHAFE DAMAGE ON THE RT INTERNAL FILLERS AND LONGERONS BETWEEN BS 2163.685 AND 2165.061, Z=45 & Z=60.1. REPAIRED THE DAMAGED TAILCONE IAW EA 011-5350-01-A7464, REV I/R, AND EO MD11-5350-62358-B. MINOR.SDR IPXA2018092834501Spoiler · corrodedRT WING UPPER SURFACE SPOILER SILL WAS CORRODED BETWEEN XOSP 530 TO 564. REPAIRED THE SPOILER IAW SRM 57-50-05, REPAIR 10, FIG 201, AND 51-38-01, 6D. MAJOR.SDR IPXA2018092634437Stiffener · crackedNR 2 ENGINE RT THRUST REVERSER STIFFENER, FWD OF THE CASCADE VANE AT 2:30 POSITION WAS CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM 54-01-42. MINOR.SDR IPXA2018092434321Rib · chafedLEFT WING INBD FLAP, INBD TRACK FAIRING RIB WAS CHAFED. REMOVED AND REPLACED THE RIB IAW SRM 51-33-01, AND 51-35-01. MINOR.SDR IPXA2018092104202Tee Fitting · crackedLEFT WING, OTBD FLAP, INBD FWD HINGE FAIRING, OTBD FWD LOWER PANEL SUPPORT TEE FITTING WAS CRACKED. REMOVED AND REPLACED THE TEE IAW SRM 51-33-01. MINOR.SDR IPXA2018092834506Longeron Splice · corrodedLONGERON 51L SPLICE FITTING WAS CRACKED AT BS 1857. REMOVED, FABRICATED, AND REPLACED THE LONGERON SPLICE IAW DWG 7414, AND SRM 51-33-01. MINOR.SDR IPXA201809244282Former · crackedLEFT WING FIXED L/E FORMER WAS CRACKED AT XOS. 961. REMOVED, FABRICATED, AND REPLACED THE FORMER IAW DWG. ARB2920-13, AND SRM 51-33-01. MINOR.SDR IPXA2018100134601Frame · gougedNR 1 ENGINE, LT CORE COWL FRAME WAS GOUGED AT NAC STA 300.0 AND THE 8 O'CLOCK POSITION. REPAIRED THE DAMAGE IAW EA 011-7110-01-A7466, REV I/R, AND EO MD11-7110-70005-A. MINOR.SDR IPXA2018092634436Longeron Splice · corrodedLONGERON 48L SPLICE FITTING WAS CORRODED BETWEEN BS 1701 - 1721. REMOVED AND REPLACED THE LONGERON SPLICE IAW SRM 51-31-01, AND 51-33-01. MINOR.SDR IPXA2018092654387Floorbeam · crackedFLOORBEAM WAS CRACKED AT STATION 6-70 ABOVE LONGERON 43L. REPAIRED THE FLOORBEAM IAW SRM 53-40-51, REPAIR 1, FIGURE 201. MAJOR.SDR IPXA20180924283Support Angle · crackedRIGHT WING FUEL CONTROL PANEL OTBD MOUNT ANGLE WAS CRACKED. REMOVED, FABRICATED, AND REPLACED THE SUPPORT ANGLE IAW DWG ARB2382, AND SRM 51-35-01. MINOR.SDR IPXA20180924281Skin · crackedRIGHT WING FIXED L/E LOWER SKIN WAS CRACKED AT XOS. 827. REPAIRED THE WING L/E SKIN IAW SRM 57-40-02, REPAIR 7, FIG 201. MAJOR.SDR IPXA2018092134235Stiffener · crackedNR 3 ENGINE, INBD THRUST REVERSER SUPPORT STIFFENER, SECOND FROM THE BOTTOM WAS CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM 54-01-42. MINOR.SDR IPXA2018092134234Stiffener · crackedNR 3 ENGINE, INBD THRUST REVERSER SUPPORT STIFFENER, 4TH FROM THE BOTTOM WAS CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM 54-01-42. MINOR.SDR IPXA2018100594662Pan · crackedLEFT FWD CENTER GEAR DOOR PAN WAS CRACKED AT THE FWD CORNER. REPAIRED THE DOOR PAN IAW SRM 52-82-07, REPAIR 1, FIG 201. MINOR.SDR IPXA2018092834500Skin · gougedEXTERIOR FUSELAGE SKIN AT BS 1153, LONGERON 44R WAS GOUGED. REPAIRED THE SKIN IAW EA 011-5340-01-A7467, REV IR, AND EO MD11-5330-70087-A. MINOR.
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