N19141
Service difficulty reports · 138
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 = 'N19141' 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 = 'N19141' 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 CALA2023063002084Bear Strap · unknownAS REQUIRED BY AD 2012-25-11 ACCOMPLISH AN NDT INSPECTION OFTHE BEAR STRAP AND INNER CORD IN THE AREA OF THE REPAIR BEFORE 50,000 TOTAL AIRCRAFT CYCLES.AFTER THE ACCUMULATION OF 46,500 TOTAL A IRCRAFT FLIGHT CYCLES BUT BEFORE 47,000 TOTAL AIRCRAFT FLIGHT CY CLSDR CALA2023062802070Fitting · unknownREMOVE AND REPLACED FLOOR SUPPORT FITTING AT STA 395-418 I/A/W 5 1-40-05 REMOVED AND REPLACED FLOOR SUPPORT FITTING AT 395-415 I/A/W SRM 51-40-02 AND ECRA 5316-01014.SDR CALA2023062802069Frame · damagedCUTOUT DAMAGE AND REPAIRED FUSELAGE FRAME AT STA 1280 BETWEEN S8 R AND S9R REF SRM 53-00-07 REPAIR 8 THE INSPECTION GIVEN IN TABLE 203/REPAIR 8. THRESHOLD ZONE 3 12, FLIGHT CYCLES WHICHEVER COMES FIRST. METHOD OF INSPECTION DETAIL 000 FLIGHT CYCLES FROM REPAIRSDR CALA2023062802067Frame · damagedCUTOUT DAMAGE AND REPAIRED FUSELAGE FRAME AT STA 1580 BETWEEN S8 L AND S9L REF SRM 53-00-07 REPAIR 8 IS GIVEN IN TABLE 203/REPAIR 8.DO THE INSPECTION THRESHOLD 12,00 FLIGHT CYCLES WHICHEVER COMES FIRST.METHOD OF INSPECTION DETAILE 0 FLIGHT CYCLES FROM REPAIR ISDR CALA2023062802066Frame · damagedCUTOUT DAMAGE AND REPAIR FUSELAGE FRAME AT STA 1580 BETWEEN S8R A ND S9R REF SRM 53-00-07 REPAIR 8 5 TABLE 203/REPAIR 8. DO THE INSPECTION REQUIREMENTS AS GIVEN IN TABLE 203/ CUTOUT DAMAGE AND REPAIRED FUSELAGE FRAME AT STA 1580 BETWEEN S8 R AND S9R REF SRM 53SDR CALA2023062802065Frame · damagedCUTOUT DAMAGE AND REPAIRED FUSELAGE FRAME AT STA 760 BETWEEN S8R AND S9R REF SRM 53-00-07 REPAIR 8 STEP 5 TABLE 203/REPAIR 8.DO THE INSPECTION AS GIVEN IN TABLE 20 OR 50,000 AIRFRAME FLIGHT CYCLES WHICHEVER COMES FIRST. METHOD O INSPECTION INTERVAL 3/REPAIR 8 SDR CALA2023062802075Beam · unknownREPAIRED UPPER CHORD OF FLOOR BEAM AT STA 1640 RBL 48 TO RBL 58 REF SRM 53-00-51-2R-8 REPAIR 8 SDR WAS COMPLETED AND ALL WORK ACCOMPLISHED I/A/W SRM 53-00-51-2 R-8 REPAIR 8.SDR CALA2023062802074Bracket · crackedCUSP WEB FORWARD LOWER FRAME CLIP CRACKED. LOCATED JUST AFT STA. 1120 LEFT SIDEWALL, FLOOR LEVEL, VIEW WITH MIRROR AND FLASHLIGHT UNDER CUSP WEB. (K. JONES V932161) CUSP WEB FORWARD LOWER FRAME CLIP CRACKED. LOCATED JUST AFT STA. 1120 LEFT SIDEWALL, FLOOR LEVESDR CALA2023062802073Frame · damagedCUTOUT DAMAGE AND REPAIR FUSELAGE FRAME AT STA 1520 BETWEEN S8R AND S9R REF SRM 53-00-07 REPAIR 8 DO THE INSPECTION IN TABLE 203/REPAIR 8.ZONE 3 INSPECTION THRESH AIRFRAME FLIGHT CYCLES WHICHEVER COMES FIRST.METHOD DETAILED VIS OLD 12,00FLIGHT CYCLES FROM REPASDR CALA2023062802072Unknown · unknownLOCATED AND DRILLED NEW SERVICEABLE NEW GALLEY SUPPORT AT R4 DOOR DRAIN PAN AT STA 1640-1660 I/A/W SRM 51-40-05 SDR WAS COMPLETED AND ALL WORK ACCOMPLISHED I/A/W SRM 51-40-05SDR CALA2023062802071Frame · damagedCUTOUT DAMAGE AND REPAIRED FUSELAGE FRAME AT STA 1080 BETWEEN S8 L AND S9L REF SRM 53-00-07 REPAIR 8 STEP 5 TABLE 203/REPAIR 8.INSPECTION REQUIREMENTS TABLE 203 ZONE 50,000 AIRFRAME FLIGHT CYCLES WHICHEVER COMES FIRST. METHOD OF I CYCLES. 3 INSPECTION THRESHOLSDR CALA2023061601886Frame · crackedCUSP WEB FORWARD LOWER FRAME CLIP CRACKED. LOCATED JUST AFT STA. 1120 LEFT SIDEWALL, FLOOR LEVEL, VIEW WITH MIRROR AND FLASHLIGHT UNDER CUSP WEB. (K. JONES V932161) CUSP WEB FORWARD LOWER FRAME CLIP CRACKED. LOCATED JUST AFT STA. 1120 LEFT SIDEWALL, FLOOR LEVESDR CALA2022032500785Service Door · missingPDA 1 UPON ARRIVAL TO JFK FOUND PNEUMATIC GROUND SERVICE DOOR MISSING.(DOOR 25X13) ADDED IMAGES ADDED IMAGES UPON ARRIVAL FOUND RH PNEUMATIC ACCESS PANEL MISSING. REQUEST COMPLYED WITH DDP PLACED ON CDL CDL DISPATCH DESK: 001 .LEFT SIDE AIR CONDITIONING ACCESSDR CALA2021102601976Skin · noneSUPPORT TASK: EXISTING MAJOR REPAIR INSTALLED AT BS620 STRINGER 18L NOT LISTED FOR INSP FROM AIRCRAFT RECORDS REVIEW. REPAIR IS INSTALLED ADJACENT AND BELOW MAJOR REPAIR BETWEEN BS620-640 AND BETWEEN STRINGERS 16L-17L. REPAIR IS NOTED IN ECRA 5330-05371. T RANSDR CALA2021102001928None · noneTRANSCRIBED FROM ECRA 5311-02651 HAECO GSO NR 9284641. PLANNING TO CONTACT ENGINEERING AFTER 15-JAN-2023 BUT BEFORE 15-FEB-2023 AND REQUEST THAT UPDATED INSPECTION INSTRUCTIONS BE PROVIDED FOR ECRA 5311-02651. PLANNING TO CONTACT ENGINEERING AFTER 15-JAN-2023 SDR CALA2021082701440Rib · damagedSUPPORT TASK-LEFT ELEVATOR OUTBD, RIB P/N 183N2505-31 AFT VERTIC AL EDGE HAS DAMAGE. REPAIRED L/H ELEVATOR OBD RIB IAW B757-200 SRM 55-20-02, SRM 51- 70-04, DWG 183N2505SDR CALA2018022000701Coffeemaker · shortedCOFFEE MAKER HAD ELEC POP/SPARK WITH A LITTLE SMOKE. PULLED CB NO FURTHER ISSUES. T/S FOUND C/M HEATER ELEMENT WIRE BROKEN AND SHORTING. REPLACED COFFEE MAKER OPS AND LEAK CKS GOOD.SDR CALA2018011200146Coffeemaker · odorMID GALLEY COFFEEMAKER SMELLED OF BURNING RUBBER. ODOR CLEARED, NO PROBLEM FOUND. OPS CHECKED NORMAL.SDR CALA2017122904676Floorbeam · corrodedCORROSION ON MAIN CABIN FLOORBEAM UPPER SURFACE, BS 324, RBL 53 TO 62. REPAIRED THE FLOORBEAM IAW SRM 53-10-08-R1, FIG 201.SDR CALA2017122904675Skin · chafedLEFT INBD MAIN FLAP BULLNOSE SKIN CHAFED AT OTBD LANDING GEAR AFT FAIRING. REPAIRED IAW ECRA 5750-05013, PART 1, TO LEFT INBD MAIN FLAP BULLNOSE SKIN.SDR CALA2017122904674Floor Support · crackedAFT CABIN FLOOR SUPPORT, BS 1580 AND 1600, BL 0, FOUND CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, P2-3, AND DWG 146N5180, REV A.SDR CALA2017122904673Floor Support · corrodedCARGO FLOOR SUPPORT CORRODED AT BS 1510. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-53, REPAIR 1, TABLE 201, FIG 201.SDR CALA2017122904672Floor Support · corrodedAFT CARGO FLOOR SUPPORT CORRODED UNDER NUTPLATE AT BS 1330. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-53, REPAIR 1, TABLE 201, DETAIL X.SDR CALA2017122904671Floor Support · crackedAFT CABIN FLOOR SUPPORT, BS 1320 AND 1340, BL 0 FOUND CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PAR 4.SDR CALA2017122904670Floor Support · crackedMAIN MID CABIN FLOOR SUPPORT BETWEEN BS 700 AND 720, AT RBL 24.75 FOUND CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PAR 4, AND 70SDR CALA2017122904669Strap · crackedFWD ACCESSORY BAY LT TUNNEL STABILIZATION STRAP AT LBL 25 IS CRACKED BS 365 AND ONE INCH FWD OF BS 377. REPAIRED THE STRAP IAW SRM 53-00-51, FIG 201, REPAIR 12, AND 13.SDR CALA2017122904668Skin · chafedLEFT INBD MAIN FLAP BULLNOSE SKIN CHAFED AT INBD LANDING GEAR AFT FAIRING. ACCOMPLISHED INTERIM REPAIR.SDR CALA2017122904667Floor Support · corrodedMAIN MID CABIN FLOOR SUPPORT BETWEEN BS 720 AND 740, RBL 63 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PG 2, AND DWG 143N8322.SDR CALA2017121704485Oven · dirtyAFT OVEN 3 NEEDS TO BE CLEANED SMOKES AFT OVEN 3 IS CLEANED AND OPS CHECKED GOOD. OK TO CONTINUESDR CALA2017120904379Battery · disconnectedFOUND 2 EMERGENCY FLASHLIGHTS IN FIRST CLASS & 3 EMERGENCY FLASHLIGHTS INOPERATIVE. FOUND FIRST CLASS & COACH EMERGENCY FLASHLIGHTS BATTERIES UNPLUGGED. PLUGGED IN ALL BATTERIES FOR FIRST & COACH FLASHLIGHTS. OPS CK GOOD. OK TO CONTINUE.SDR CALA2017120804340Skin · dented(B757-06-3-0221) LOWER FUSELAGE SKIN BETWEEN STA 520 AND STA 540 , STGR 27R AND 28R HAS SCUFFED DENTS 3EA 209-029 ACCOMPLISED EC/RA 5330-06240 REV-INSTALLED DECAL PER EC/RA 2060- 01042 ON SKIN BETWEEN STA 520 AND STA 540, STR 27FR AND STR 28R FOR AREAS MARKED SDR CALA2017120804339Skin · dented(B757-06-3-0269) LOWER FUSELAGE BETWEEN STA 560 AND STA 520, STGR 27R AND STGR 28R HAS 2EA DENTS 209-013 ACCOMPLISHED PERMANENT REPAIR ON FUS.SKIN BETWEEN ST500 & STA520 . STR27R & STR28R IAW EC/RA5330-06240 REV- & EC/RA5330-06241 REV -.SDR CALA2017120804338Spar · cracked(B757-57-3-0463) R/H I/B MAIN FLAP FWD SPAR LWR CHORD HAS CRACK ACCESS THROUGH O/B AFT FLAP TRACK CAVITY (FLAP STA. 220). 090-055 REMOVED AND REPAIRED R/H I/B MAIN FLAP IAW. ECRA 5750-05012. INT ITIATED DIP TO"ACCOMPLISH INSPECTION REQUIREMENTS ON OR BEFORE T SDR CALA2017120804337Skin · dented(B757-06-3-0337) RH I/B MAIN FLAP UPPER SURFACE SKIN HAS DENT AT I/B SECTION. 090-056 REPAIRED DENT DAMAGE ON R/H IB MAIN FLAP UPPER SURFACE SKIN I/B SECTION IAW B757-200 SRM 51-70-10.SDR CALA2017120804336Stringer · mechanic errorFWD CARGO COMPT. STRINGER 27R ON I/B SIDE HAS DRILL MARK ON EDGE OF RADIOUS DURING LOCATING AND DRILLING OF DOUBLER AT STA500-540 ACCOMPLISHED INTERIM REPAIR ON FUSE STRINGER 27R BETWEEN 500-520 IAW ECRA5330-06254 REV-. SEE PART 2 FOR INSPECTION REQUIREMENTS ASDR CALA2017120804335Skin · dentedB757-06-03-0221 LOWER FUSELAGE SKIN AT STA 500 STA 520 STGR 27R AND 28R HAS GAUGE DENT 209-028 ACCOMPLISHED INTERIM REPAIR ON FUSELAGE STRINGER 27R BETWEEN B.S 500 AND B.S. 520 IAW ECRA 5330-06254 REV-.PART1. SEE PART 2 FOR INSPECTION REQUIREMENTS AND PART 3 FSDR CALA2017120404318Skin · chafed(B757-06-3-0323) R/H I/B MAINFLAP BULLNOSE SKIN CHAFED I/B OF LANDING GEAR AFT FAIRING ACCOMPLISHED INTERIM REPAIR OF R/H I/B MAINFLP BULLNOSE SKIN PER ECRA5750-05018 PART1. INITIATED DIP TO "ACCOMPLISH INSPECTION R EQUIREMENTS ON/BEFORE A/C REACHIN 75000 TOTASDR CALA2017120404317Skin · chafed(B757-06-3-0323) R/H I/B MAIN FLAP BULLNOSE SKIN CHAFED AT O/B OF L/G AFT FAIRING. 090-046 PERFORMED INTERIM REPAIR TO R/H I/B MAIN FLAP BULLNOSE AT LANDING GEAR AFT FAIRING. IAW ECRA 5750-05018 PART1. INITIATED DIP TO " ACCOMPLISH INSPECTION REQUIREMENTS ON OSDR CALA2017120404316Skin · cracked#3 SLAT COVE SKIN HAS CRACK AT I/B AND O/B SIDE OF I/B SLAT TRACK MOUNT FITTING. ACCOMPLISHED INTERIM REPAIR ON #3 SLAT COVE SKIN AT I/B AND O/B SIDE OF I/B SLAT TRACK MOUNT IAW SRM 57-43-01 REPAIR 4 PAGE 201. INITIATED DIP TO INSPECT THESE BLIND RIVETS 3000FCSDR CALA2017120404314Floor Support · corrodedB757-53-3-0480 MAIN AFT CABIN FLOOR SUPPORT BOX BEAM HAS CORROSION BETWEEN BS 1660 AND BS 1681, LBL 58,209-108. REMOVED AND REPLACED FLOOR SUPPORT BOX BEAM P/N 146N5246US, PO N O. SAG1722589 AT MAIN AFT CABIN BTW BS1660 AND BS1681 AND LBL 58 . IAW B757-200 SRMSDR CALA2017120404313Floor Support · corrodedB757-06-3-0243 AFT CARGO FLOOR SUPPORT STGR RBL 7.55 HAS CORROSION UNDER NUT PLATE AT BS 1330, 209-075. ACCOMPLISHED REPAIR ON AFT CARGO FLOOR SUPPORT STGR RBL 7.55 BS 1330. IAW B757-200 SRM 53-00-53 REPAIR 1 TABLE 201 DETAIL X.SDR CALA2017120404312Floor Support · corrodedB757-53-3-0480 MAIN AFT CABIN FLOOR SUPPORT GUSSET AT BS 1680BL0 HAS CORROSION 209-124 REMOVED CORROSION FROM PLATE GUSSET AT MAIN AFT CABIN BS1680 BL0 , REMANING MATERIAL OUT OF LIMITS. IAW 757-200 SRM 53-00-51 FIG 101 DETAIL VI PAGE 104. REMNOVED, FABRICATEDSDR CALA2017120404311Skin · cracked#3 SLAT COVE SKIN HAS CRACK AT O/B SIDE OF O/B SLAT TRACK MOUNT FITTING. ACCOMPLISHED INTERIM REPAIR ON #3 SLAT COVE SKIN AT O/B SIDE OF O/B SLAT TRACK MOUNT FITTING IAW SRM 57-43-01 REPAIR 4 PAGE 201. INITIATED DIP TO REINSPECT BLIND RIVETS 3000FC AFTER INSTASDR CALA2017120304309Floor Support · corrodedFLOORBEAM IN MAIN CABIN AT STA700 RBL 58 HAS CORROSION ON UPPER SURFACE. COMPLIED WITH ECRA 5310-07284 ON FLOORBEAM IN MAIN CABIN AT STA 700 RBL 58 UPPER SURFACE.SDR CALA2017120304308Floor Support · corrodedCORROSION ON MAIN CABIN FLOOR SUPPORT UPPER SURFACE AT STA 330 RBL-4. BLEND OUT DAMAGE FITTING FOUND OUT OF LIMITS IAW SRM 53 -00-51. ALLOWABLE DAMAGE 1 FIG 101 DETAIL III. REMOVED AND REPLACED FITTING AT MAIN CABIN BTW STA 334-345 RBL 4 IAW SRM 51-40-02.SDR CALA2017120304307Floor Support · corrodedCORROSION ON MAIN CABIN FLOOR BOX BEAM UPPER SURFACE AT STA 378 RBL-62. REMOVED AND REPLACED THE FLOOR BOX BEAM ON MAIN CABIN AT STA 378 RBL 62 IAW SRM 51-40-02 PAG 2 AND 9.SDR CALA2017120304306Floor Support · corrodedAFT CARGO FLOOR SUPPORT STR RBL 16.10 HAS CORROSION UNDER NUT PLATE AT BS 1330. ACCOMPLISHED REPAIR ON AFT CARGO FLOOR SUPPORT STR RBL 16.10 BS 1330 IAW SRM 53-00-53 REPAIR 1TABLE 701 FIG 201 DETAIL X.SDR CALA2017120304305Intercostal · crackedAFT CABIN FLOOR SUPPORT STRUCTURE INTERCOSTAL BETWEEN BS 1420 AND BS 1440 AT BL 0 CRACKED. REMOVED SUPPORT ANGLES AND INSTALLED NEW SUPPORT ANGLE AT AFT CABIN FLOOR BETWEEN BS1420-1440 BL0 IAW SRM 51-40-02 PAG 1-4/ P/N 140N2505432.SDR CALA2017120304304Floor Support · corrodedAFT CARGO FLOOR SUPPORT STR RBL 10.45 HAS CORROSION UNDER NUT PLATE AT BS 1330. ACCOMPLISHED REPAIR AT AFT CARGO FLOOR SUPPORT STR RBL 10.45 BS 1330 IAW SRM 53-00-53 REPAIR 1 TABLE 201 FIG 201 DETAIL XL.SDR CALA2017120304303Floor Support · corrodedMAIN FWD CABIN FLOOR SUPPORT BOX BEAM BETWEEN BS 345 AND BS 365, RBL 58 HAS CORROSION ON UPPER SURFACE. BLENDED OUT CORROSION ON MAIN CABIN FLOOR SUPPORT BOX BEAM AT STA 345 TO STA365, RBL 58 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 10
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