N12125
Service difficulty reports · 123
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 = 'N12125' 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 = 'N12125' 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 CALA2022042501059Frame · misrepairedSUPPORT TASK, MAIN CABIN STA 760 L/H FUSELAGE FRAME AT FLOORBEAM HAS A DRILL START, TRANSCRIBED FROM HAECO GSO NRC 9285440 REPAIRED DRILL START ON MAIN CABIN STA 760 L/H FUSELAGE FRAME AT FLOORBEAM IAW UAL ECRA 5332-01026 AND HAECO REO-G23725, HAECO G SO MECH SDR CALA2022041801003Shear Web · noneSUPPORT TASK-- MAIN CABIN SHEAR WEB STA 700-720 RBL25 REQUIRES F ABRICATION. TRANSCRIBED FROM HAECO GSO NRC 9285902 REMOVED AND REPLACED -4 SHEAR WEB IAW B757-200 SRM 51-40-02 AND BOEING DWG 143N5140 REV B. HAECO GSO MECH V917499 INSP QC302SDR CALA2022041801002Deck Plate · corroded(SUPPORT TASK) MAIN CABIN DECK PLATE STA 1716 RBL50 HAS CORROSIO N ON WEB, TRANSCRIBED FROM HAECO GSO NRC 9285434 REMOVED CORROSION ON THE AFT DECK PLATE AT STA 1716 RBL50. REMAI INSP QC302 NING THICKNESS FOUND TO BE .027, REMOVED .044, ORIG .071 PER B75 7-200SDR CALA2022041400957Skin · corroded(B757-06-3-0246) LOWER FUSELAGE SKIN INTERNAL ANTENNA DOUBLER HA S CORROSION IN BULK PIT AT STA 1510 BETWEEN S28L AND 29L (MARKED ). TRANSCRIBED FROM N/R 9284791SDR CALA2022041100946Frame · cracked(SUPPORT TASK) MAIN CABIN STA 1540 BETWEEN STRINGER 8-9 L/H FRAM E CRACKED AT OVER HEAD BIN ATTACH POINT, TRANSCRIBED FROM HAECO GSO NRC 9285436 RE-INSPECTED AT 12,000 FLIGHT CYCLES FROM REPAIR INSTALLATION OR INSPECTION REQUIRED AT INTERVALS OF 12,000 FLIGHT SDR CALA2022041100940Floorbeam · corrodedSUPPORT TASK- MAIN CABIN FLOOR BEAM T-CAP STA 720 RBL25-45 HAS C ORROSION ON UPPER SURFACE, TRANSCRIBED FROM HAECO GSO NRC 928497 5SDR CALA2022041100939Floorbeam · corrodedSUPPORT TASK- MAIN CABIN FLOOR BEAM STA 365 RBL65 CORRODED ON UP PER SURFACE, TRANSCRIBED FROM HAECO GSO NRC 9285582 TRANSCRIBED FROM HAECO NR 9285582. REMOVED CORROSION ON BEAM UPPER CHORD RBL-12 TO RBL-65 IAW B757-200 SRM 53-00-51- FLOOR BEAM UPPER SURFACE ASDR CALA2022041100938Floor Support · corroded(SUPPORT TASK) MAIN CABIN FWD OF STA 700 PANEL SUPPORT HAS CORRO SION ON UPPER SURFACE. REF HAECO GSO NRC 9285442 REMOVED CORROSION ON PANEL SUPPORT FWD OF STA 700 IAW B757- STA 680-700 IAW B757-200 SRM 51-40-02 AND BAC DWG 143N5400 200 SRM 53-00-51 ORIGINAL SDR CALA2022040400867Floor Support · corrodedB757-53-3-0579 CBN AFT WET FLOOR BEAM CORRODED AT FASTENER HOLE BS 1640, BL L3, REFERENCE HAECO GSO NR 9284816SDR CALA2022040400866Floor Support · corrodedSUPPORT TASK- MAIN CABIN FLOOR STA 720-740 RBL65 HAS CORROSION O N UPPER SURFACE. TRANSCRIBED FROM HAECO GSO NRC 9284976SDR CALA2022040400865Floor Support · noneSUPPORT TASK- MAIN CABIN STA 700-720 RBL65 GUTTER SUPPORT REQUIR ES REPLACEMENT DUE TO OFFSET CREATED BY FLOOR BEAM REPAIR. TRANS CRIBED FROM HAECO GSO NRC 9285579SDR CALA2022032800796Seat Track · corrodedSUPPORT TASK, MAIN CABIN STA 730 RBL24 SEAT TRACK SUPPORT HAS CO RROSION, TRANSCRIBED FROM HAECO GSO NRC 9285765SDR CALA2022032500774Floor Support · corrodedTRANSCRIBED FROM HAECO NR 9284825. B757-53-3-0579/CBN AFT WET AREA FLOOR SUPPORT CHANNEL CORRODED AT FASTENER HOLE BS 1675, BL 0. DOT: T679. REMOVED AND REPLACED FLOOR SUPPORT CHANNEL IAW B757-200 SRM 51-4 0-02 AND BAC DWG 146N5230 REV-. REMOVED AND REINSTALLESDR CALA2022031400643Skin · noneTRANSCRIBED FROM HAECO NR # 9285363. SUPPT. TASK: FWD CARGO DOOR EXTERIOR SKIN HAS REPAIR DOUBLER NEAR FWD BOTTOM CORNER 10 IN. FROM DOOR FWD EDGE, 11.75 IN. BELOW HANDLE (APPROX.). DOUBLER MEASURES 11 X 8 IN. FOUND IN GOOD CONDITION WITH NO OBVI OUS DISCREPANSDR CALA2022031400638None · corrodedB757-53-3-0579- CABIN AFT WET AREA FLOOR WEB CORRODED AT FASTENE R HOLE BS1680 BL R4, TRANSCRIBED FROM HAECO GSO NRC 9284826SDR CALA2022030700592None · corrodedSUPPORT TASK; MAIN CABIN STA 1714 RBL 1 HAS CORROSION ON WEB (DE CK PLATE), TRANSCRIBED FROM HAECO GSO NRC 9285454 BLENDED AREA TO REMOVE CORROSION, FOUND TO BE OUT OF LIMITS CREATED SDR # 1027917. TRANSCRIBED FROM HAECO NR 9285454. HAECO IAW B757-200 SRM 53-6SDR CALA2021120102215Skin · wornSKIN WRINKLE AND WORN BETWEEN STA.1720 AND STA.1743 AFT OF APB BETWEEN S-27RT AND S-27LT. ( REF. L/P 7137422 ) REF COLLECTOR ECRA 5380-01303 FOR MAJOR REPAIR ACCOMPLISHED BY BOEING CONTRACTORS. NO FURTHER MX REQ''D AT THIS TIME. REF COLLECTOR ECRA 5380-01303 FSDR CALA2021120102214Bulkhead · noneREF ECRA 5380-01304, NEED TO INITIATE A DTA DIP PER PART 1 STEP #2 IN REGARDS TO A REPAIR ON THE APB CENTER WEB & FWD LOWER CHORD. ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 ON OR BEFORE THE AIRCRAFT REACHES 50,000 TOTAL CYCLES. ITEM PLACED ON DIP. PER ECRASDR CALA2021120102213Skin · noneREF ECRA 5360-01621, NEED TO INITIATE A DTA DIP PER PART 1 STEP #7 TO ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 ON OR BEFORE THE AIRCRAFT REACHES 50,000 TOTAL CYCLES. ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 ON OR BEFORE THE AIRCRAFT REACHES 50,000 TOSDR CALA2021101101853Bulkhead · buckledREF AVO#ESC210928-0125-3 STEP 4 DETAILED VISUAL INSPECTION- FOUND AFT PRESSURE BULKHEAD BUCKLED AT BL 0 BETWEEN STR.29R AND STR.29L. PREVIOUS WRITEUP LOCATION IS AT FUSELAGE STA. 1720.SDR CALA2021100601800Skin · damagedPER CREW, POSSIBLE TAIL STRIKE ON LANDING. ATTACHED PICTURES OF DMAGED AREAS PERFORMED VISUAL INSPECTIONS STEPS 4&5 REF AVO# PERFORMED DETAIL VISUAL INSPECTION REF AVO ESC210928-0125-1 STEP ESC210928-0125-1. 4. NO INTERNAL STRUCTURE DAMAGE NOTED ON THE INTERIOSDR CALA2021100601799Skin · gougedFUSELAGE SKIN WORN AND GOUGED AT AND BETWEEN STA.1720 - STA.1712 AT S-29RT AND S-29LT FWD OF APB ( REF. L/P 7137422 ) C/W RII INSP OF INSURANCE CUT REF DISPOSITION A.2 STEP 1 AVO ESC 210928-0125-3. TRIMMED OUT DAMAGE SKIN AT STA. 1713 TO 1720, BETWEEN S29L & PSDR CALA2021010400007Pressure Switch · faultedAPU OIL QTY EICAS S THE APU OIL QUANTITY IS LOW NOTE: APU AUTO EVENT ALSO-APU OIL ADD ON EICAS STATUS PAGE ON ARRIVAL SERVICED APU OIL, RAN APU AND TWICE WAS AUTO SHUTDOWN. BITE THE CONTROLLER FAULTED LOW OIL PRESSURE SWITCH. REPLACE OIL PRESSURE SWITCH AND SDR CALA2020010600010Skin · dentedDENT ON FUSELAGE LEFT SIDE BETWEEN PRESSURE RELIF VALVE AND ELEV.STATIC PORT ABOUT 36" BELOW PUNCTURE THROUGH FUSELAGE SKIN AT APPROX STA 1445 AND 1" ABOVE S-25L REMOVED DAMAGE TO THE AFFECTED SKIN AERA STA 1445 AND STR 25 L REF 53-00-01. INSPECTION WILL NEEDSDR CALA2019061400937Door · missingPDA 2 ON ARRIVAL FOUND #1 ENG IDG SERVICE DOOR MISSING C/W ECRA 7111-02030 PART 1 INTERIM REPAIR PERMANT REPAIR PER PART 3 DUE IN 1 CYCLE ADD EMP:U166362,U114806 PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 1 FLT CYCLE. TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPSDR CALA2019051700775Life Raft · unserviceableFOUND LIFE RAFT AT SEAT 21ABC UNRAVELING WHILE PREFORMING PRE-DEPARTURE CHECK REMOVED AND REPLACED LIFE RAFT. REF. AMM SUBTASK 25-64-00-962-005 AT STOWAGE BIN 21ABC. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1317377 SN OFF 5326 RAFT, 46 MAN, 7 OFF 29-2581-9-SDR CALA2018111402366Floorbeam · stainedB757-53-3-0488 HEAVY BLUE WATER ON FLOOR BEAM STRUCTURE BELOW L1 ENTRY FLOOR BOARD AND BELOW LAV A. STA 297 TO STA 377 BL-0 TO L BL-62. REV VTSAA N/R 0027691. CLEANED,NEUTRALIZED, PERFORMED DUI OF AND APPLIED CIC TO FLOOR B EAM STRUCTURE BELOW L1 ENTRY FLOOR BSDR CALA2018111202349Floor Support · none(B757-53-3-0488) HEAVY BLUE WATER ON FLOORBEAM STRUCTURE BELOW R 1 ENTRY FLOORBEAM AND ABOVE NLG WW UPPER WEB STA 350 TO STA 365 BL-0 TO RBL 25. REF VTSAA NR 0027692. CLEANED, NEUTRALIZED, PERFORMED DVI AND APPLIED CIC TO FLOOR BEA M STRUCTURE BELOW R1 ENTRY FSDR CALA2018110502307Support Channel · corroded(B757-06-3-0371) CORROSION ON RIGHT FWD OVERWING EXIT DOOR SUPPO RT CHANNEL. REF VTSAA NR 0027751. BLENDED CORROSION AT RH FWD OVERWING EXIT DOOR SUPPORT CHANNEL A ND FOUND DIMENSIONS D=.025 W=1 L=2 TO BE OUT OF LIMITS IAW B757- 2 SRM 52-20-02 AD1 FIG 101 REMOSDR CALA2018110302259Skin · corrodedCORROSION BETWEEN STA 900 BULKHEAD CHORD AND FUSELAGE SKIN IN AREA AFT OF FWD CARGO COMPARTMENT, STA 900 BETWEEN STR 27R. SKIN FOUND OUT OF LIMITS PER SRM 5300-00-01-A1. L+8.0,W+4.0,D-.120. CUTOUT DAMAGE AND ACCOMPLISHED REPAIR PER ECRA 5330-06451.SDR CALA2018110302258Stop Fitting · brokenAFT CARGO DOOR CUTOUT UPPER FWD DOOR STOP FITTING BROKEN AT STA 1400 RG23. REMOVED BROKEN STOP FITTING WITH MISSING BEARING PLATE AND INSTALLED NEW STOP FITTING P/N 69-45580U3 AND BEARING PLATE P/N 140N2850-1 AT AFT CARGO DOOR CUTOUT UPPER FWD STA 1400 IAW SRSDR CALA2018092401993Unknown · odorAIRCRAFT DIVERTED INTO DEN (FLT1640 LAX/EWR) DUE TO SMELL LIKE GAS IN AFT GALLEY AREA. WARRANT SMOKE/ODOR CONDITION INSPECTION 05-51-58-910-801C RAN APU, PACKS TOGETHER AND ISOLATED. RAN ALL OVENS, COFFEEMAKERS, WARMERS, LIGHTS, LAV MOTORS. ACCOMPLISHED HIGH SDR CALA2018053101354Actuator · leakingDUE TO RIGHT ENGINE HYDRAULIC LOST, AIRCRAFT REQUIRES RIGHT MAIN HYDRAULIC SYSTEM FLUSH AND FILTER REPLACEMENTS. REPLACED THE FILTER ELEMENTS IN THE PRESSURE AND CASE DRAIN MODULE FILTERS FOR THE RIGHT HYDRAULIC SYSTEM IAW AMM 29-11-00, PAGEBLOCK 201, CONDITISDR CALA2017120404320Lens · missingAFT RIGHT EXIT DOOR MISSING SLIDE ARM LIGHT. REPLACED MISSING LENSE ON AFT RT EXIT DOOR SLIDE ARM LIGHT,OPS CHECKED NORMAL.SDR CALA2017120104265Lens · missingEMERGENCY EXIT SIGN IN CENTER AISLE AFT COACH IS MISSING PLASTIC COVER AT BOTTOM OF SIGN. RE-INSTALLED AFT EMERGENCY EXIT LENS COVER. OK TO CONTSDR CALA2017101603640Adc · malfunctionedAFTER TAKEOFF, SHORTLY AFTER GEAR RETRACT, RECEIVED A FIRST EICAS MESSAGE ALT DISAGREE,THEN AIRSPEED DISAGREE, THEN RUDDER RATIO, MACH/SPEED TRIM, THEN BOTH LT & RT EEC STATUS MESSAGE, ELEVATOR ASYM. EMERGENCY DECLARED. LANDING WAS MADE. TAXIING IN, WITHSDR CALA2017042801177Sign · unsecure21A LOWER EMER EXIT SIGN IS HANGING BY WIRES. RESECURED EXIT SIGN. OPS GOOD.SDR CALA2017040700896Skin · damagedON ARRIVAL DISCOVERED FUSELAGE SKIN TORN, ONE INCH LONG, BS 293 BETWEEN STRINGERS 21 - 22R. REPAIRED IAW AVO 125-17-04-04-01, STEP 4.SDR CALA2015111600932Intercostal · corrodedCENTER INTERCOSTAL WEB ANGLE ATTACHES ON AFT CARGO DOOR LOWER END IS CORRODED. FOR PREVIOUS WORK ACCOMPLISHED SEE WIPS ABOVE. INSTALLED NEW CTR INTERCOSTAL WEB AT AFT CARGO DOOR IAW DWG 146N6 603 & SRM 51-40-02.SDR CALA2015111600931Stiffener · corrodedAFT CARGO DOOR LOWER END, AFT TEE STIFFENER IS CORRODED. FOR PREVIOUS WORK ACCOMPLISHED SEE WIPS ABOVE. R & R AFT CARGO DOOR LOWER END AFT TEE STIFFENER IAW DWG 146N6603 & SRM 51-40-02.SDR CALA2015111600930Intercostal · corrodedCENTER INTERCOSTAL ANGLE ON AFT CARGO DOOR LOWER END IS CORRODED OUT OF LIMITS. FOR PREVIOUS WORK ACCOMPLISHED SEE WIPS ABOVE. INSTALLED NEW CTR INTERCOSTAL ANGLE ASSEMBLY IAW DWG 146N6603 & SRM 51-40-02.SDR CALA2015111000908Frame · crackedFORWARD CARGO COMPARTMENT, RT FRAME DENTED AT STATION 680, ABOVE STRINGER 24L. CUT OUT DAMAGED AREA OF FRAME & INSTALLED REPAIR DOUBLER & INITIATED A ZONE 2 DIP TO REINSPECT AT 25K FLIGHT CYCLES AFTER REPAIR INSTALLATION OR 50K AIRFRAME FLIGHT CYCLES, WHICHEVSDR CALA2015111000907Frame · dentedFORWARD CARGO COMPARTMENT, LT FRAME IS DENTED AT STATION 800 ABOVE STRINGER 24L. CUT OUT DAMAGED AREA OF FRAME & INSTALLED REPAIR DOUBLER & INITIATED A ZONE 1 DIP TO REINSPECT AT 37,500 AFTER REPAIR INSTALLATION OR 50K AIRFRAME FLIGHT CYCLES, WHICHEVER COMES SDR CALA2015111000906Frame · dentedFORWARD CARGO COMPARTMENT, LT FRAME IS DENTED AT STATION 700 ABOVE STRINGER 23L. CUT OUT DAMAGED AREA OF FRAME & INSTALLED REPAIR DOUBLER & INITIATED A ZONE 2 DIP TO REINSPECT AT 25K FLIGHT CYCLES AFTER INSTALLATION OR 50K AIRFRAME FLIGHT CYCLES, WHICHEVER COSDR CALA2015111000905Floorbeam · corrodedMAIN CABIN FLOOR STRUCTURE FLOORBEAM 345 HAS CORROSION IN SEVERAL AREAS, FROM BL 0 TO LBL 1. SEE WIP & TASK STEPS FOR REPAIR OF FLOORBEAM AT STATION 345, BETWEEN LBL 51.8 & RBL-54.1 IAW SRM 53-00-51 REPAIR 10 & ECRA 5 310-06644 REV A.SDR CALA2015110600896Frame · dentedFORWARD CARGO COMPARTMENT, RT FRAME IS DENTED AT STATION 700, ABOVE STRINGER 24R, D9244 USED FOR SCEPTER PURPOSES ONLY. CUT OUT DAMAGED AREA OF FRAME & INSTALLED REPAIR DOUBLER & INITIATED A ZONE 2 DIP TO INSPECT REPAIR AT 25000 FLIGHT CYCLES AFTER REPAIR INSDR CALA2015110600895Frame · dentedFORWARD CARGO COMPARTMENT, LT FRAME IS DENTED AT STATION 660, ABOVE STRINGER 23L, D9244 WAS USED FOR SCEPTER ENTRY ONLY. CUT OUT DAMAGED AREA & INSTALLED REPAIR DOUBLER & INITIATED A ZONE 2 DIP TO INSPECT FRAME REPAIR AT 25000 FLIGHT CYCLE AFTER INSTALLATION SDR CALA2015110200893Frame · dentedABB FRAME AT STATION 1400, STRINGER 25 LT SHOWS DENT. INSTALLED FRAME REPAIR, TWO EACH STRINGER CLIPS, COLD WORKED TWO EACH HOLES & APPLIED CIC IAW SRM 53-00-07.SDR CALA2015110200889Frame · crackedCABIN INTERIOR, LT SIDEWALL FRAME AT STATION 1580 SHOWS SIGN OF CRACK AT FASTENER, BETWEEN STRINGER 8L & 9L. CUT OUT DAMAGE & INSTALLED REPAIR DOUBLERS IAW SRM 53-00-07 REPAIR 1. INITIATED DIP FOR DETAIL VISUAL INSPECTIONS 12000 FC FROM REPAIR INSTALLATION, SDR CALA2015102600875Frame · crackedCABIN INTERIOR, RT SIDEWALL FRAME AT STATION 800, SHOWS SIGN OF A CRACK AT FASTENER, BETWEEN STRINGER 8R & 9R, FOR SFR ENTRY PURPOSES ONLY. REPAIRED CABIN RT FRAME IAW SRM 53-00-07 REPAIR 1.
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