N324UP
Service difficulty reports · 155
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 = 'N324UP' 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 = 'N324UP' 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 IPXA10663562Floor Panel · damagedREF D 434408, POSITION 2L HAS 1 X 1 HOLE IN FLOOR PANEL. REMOVED FLOOR PANEL AND MFG NEW PANEL IAW EO B767-5320-9693G AND INSTALLED IAW AMM 51-01-01.SDR IPXA10663560Floor Panel · damagedREF D-4344202 POSITION 2L HAS 1 X 1 HOLE IN FLOORBOARD. REMOVED FLOOR PANEL AND MFG NEW PANEL IAW EO B767-5320-9693 AND INSTALLED IAW AMM 51-01-01.SDR IPXA10662787Skin · damagedON ARRIVAL FOUND DAMAGE TO OTBD FLAP L/E SKIN PANEL 666FT, 3.5"X0.75" LOCATED 1.5" FROM L/E OF PANEL AND 1.5" FROM OTBD EDGE OF PANEL. REPAIRED IAW SRM 57-53-01-2R FIG 201 AND SRM 51-70-03.SDR IPXA0660659Switch · looseEMERGENCY EXIT LIGHT SWITCH IS LOOSE. SECURED SWITCH AS REQUIRED.SDR IPXA10658705Unknown · odorINSPECTION TYPE:ETOP WHEN LANDING GEAR EXTENDED APPROACH A STRONG ODOR OF BURNING RUBBER ENTERED THE COCKPIT. ODOR DISSIPATED BY LANDING. PERFORMED VISUAL INSPECTION OF INLET AND EXHAUST ON LEFT AND RIGHT PACK. RAN BOTH PACKS AT FULL HOT NO DISCREPANCIES NOSDR IPXA09657853Skin · crackedINSPECTION TYPE:ETOP RHW NR 9 SLAT OTBD NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED RHW NR 9 SLAT OTBD AREA AT OSS641.62 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV45 ORG MAT'L IS CLAD7075T6-0063IN CRACK LENGTH IS 0.090 INCH DAMAGED CUTOUT IS 7.7SDR IPXA09657852Skin · crackedINSPECTION TYPE:ETOP RHW NR 9 SLAT INBD NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED RHW NR 9 SLAT INBD AREA AT OSS572.9 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV45 ORG MAT'L IS CLAD7075T6-0063 IN CRACK LENGTH IS 0.125IN DAMAGED CUTOUT IS 7.25 ISDR IPXA09657851Skin · crackedINSPECTION TYPE:ETOP LHW NR 4 SLAT OTBD NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED LHW NR 4 SLAT OTBD AREA AT OSS641.6 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 ORG MAT'L IS CLAD7075T6-0063IN, CRACK LENGTH IS 0.125 INCH DAMAGED CUTOUT IS 7.735 INCSDR IPXA09657850Skin · crackedINSPECTION TYPE:ETOP LHW NR 4 SLAT INBD NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED LHW NR 4 SLAT INBD AREA AT OSS572.9 NOSE SKIN REPAIRED AS PER SRM 57-43-01 2R2 FIG 201 REV45 ORG MAT'L IS CLAD 7075T6-0063 IN, CRACK LENGTH IS 0.090IN. DAMAGED CUTOUT IS 7.SDR IPXA09657884Support Angle · crackedINSPECTION TYPE:C NR 1 PYLON RT INTERNAL VERTICAL FRAME UPPER ATT SUPPORT CLIP CRACKED AT NAC STA 285.45 (CRACK LENGTH 1 INCH). NR 1 PYLON RT INTERNAL VERTICAL FRAME UPPER ATT SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45 SDR IPXA09657859Floor Support · crackedINSPECTION TYPE:C BULK CARGO COMPT STA 1439 LBL 24 INCH FLOOR PANEL SUPPORT FOUND CRACK (CRACK LENGTH 1.75 INCH), BULK CARGO STA 1439 LBL 22.33 INCH FLOOR SUPPORT REPAIRED AS PER SRM 51-70-11-0G FIG 1 REV 45 ORG, MATERIAL IS 7075T6-0.040IN, CRACK LENGTH 1.75 ISDR IPXA09657876Stiffener · deformedINSPECTION TYPE:6C BULK CARGO COMPT STA 1439 LBL 24 INCH STIFFENER FOUND DEFORM. BULK CARGO COMPT STA 1439 LBL 24 INCH STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.SDR IPXA09657875Stiffener · deformedINSPECTION TYPE:6C BULK CARGO COMPT STA 1480 RBL 8 INCH FLOOR PANEL STIFFENER FOUND DEFORMED. BULK CARGO COMPT STA 1480 RBL 8 INCH FLOOR PANEL STIFFENER REPLACE AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.SDR IPXA09657874Stiffener · deformedINSPECTION TYPE:6C BULK CARGO COMPT STA 1502 LBL 8 INCH FLOOR PANEL STIFFENER FOUND DEFORM. BULK CARGO COMPT STA 1502 LBL 8 INCH FLOOR PANEL STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.SDR IPXA09657873Stiffener · deformedINSPECTION TYPE:6C BULK CARGO COMPT STA 1480 LBL 8 INCH FLOOR PANEL STIFFENER FOUND DEFORM. BULK CARGO COMPT STA 1480 LBL 8 INCH FLOOR PANEL STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.SDR IPXA09657866Frame · crackedINSPECTION TYPE:C NR 1 PYLON INTERNAL FRAME CRACKED AT NAC STA 285.45 RT SIDE, (CRACK LENGTH 2 INCHES) NR 1 PYLON INTERNAL FRAME REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45 JUST AT NAC STA 285.45 RT SIDE.SDR IPXA09657863Stiffener · deformedINSPECTION TYPE:C BULK CARGO COMPT STA 1502 LBL 16 INCH FLOOR PANEL STIFFENER FOUND DEFORM. STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.SDR IPXA09657883Panel · damagedINSPECTION TYPE:C LT WING I/B MAIN FLAP O/B EDGE UPPER SURFACE FOUND CHAFED. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5H REV 45.SDR IPXA09657882Panel · damagedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B EDGE UPPER SURFACE FOUND CHAFE. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5H REV 45.SDR IPXA09657878Fairing · delaminatedINSPECTION TYPE:C LT WING O/B FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5C FIG 2 REV 45.SDR IPXA09657865Slat · chafedINSPECTION TYPE:C RHW - NR 9 SLAT OTBD UPPER EDGE FOUND CHAFE. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REV 45, REPAIR 4, FIG 202 SHEET 8.SDR IPXA09657881Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-02 PAR 5C FIG 2 REV 45.SDR IPXA09657880Bracket · crackedINSPECTION TYPE:C LT WING L/E LES 155 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR BRACKET FOUND CRACKED (1.125 INCH). LT WING L/E LES 155 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR BRACKET REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.SDR IPXA09657879Panel · delaminatedINSPECTION TYPE:C LEFT I/B ELEVATOR UPPER SURFACE O/B T/E AREA DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PAR 4A FIG 10 REV 45.SDR IPXA09657877Angle · crackedINSPECTION TYPE:6C AFT CARGO COMPT STA 1087 RBL 24 BELOW FLOOR CLIP FOUND CRACK. AFT CARGO COMPT STA 1087 RBL 24 BELOW FLOOR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.SDR IPXA09657864Doubler · delaminatedINSPECTION TYPE:C LHW INBD AFT FLAP UPPER SURFACE OTBD T/E AREA DELAMINATED FOUND ON EXISTING REPAIR PATCH. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REV 45, REPAIR 4 FIG 201 SHEET 1.SDR IPXA09657837Slat · chafedINSPECTION TYPE:C LEFT WING NR 4 SLAT I/B UPPER EDGE FOUND CHAFE. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10, REV 45 REPAIR 4 FIG 202 SHEET 8 AND SHEET 9 NOTES.SDR IPXA09657833Fitting · crackedINSPECTION TYPE:C AFT CARGO STA 1087 LBL 24 BELOW FLOOR CLIP FOUND CRACK (CRACK LENGTH 0.75 INCH). AFT CARGO STA 1087 LBL 24 BELOW FLOOR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.SDR IPXA09657827Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGED AT STA 412 TO 540, LBL 11 TO RBL 11. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53-01-01.SDR IPXA09657826Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGED AT STA 412 TO 540, RBL 33 TO RBL 55. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53-01-01.SDR IPXA09657825Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGED AT STA 1197+108 TO 1263, RBL 77 TO RBL 88. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53-01-01.SDR IPXA09657824Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGED AT STA 283 TO 412, RBL 33 TO RBL 55. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53-01-01.SDR IPXA09657823Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGED AT STA 1425 TO 1540, LBL 55 TO LBL 77. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53-01-01.SDR IPXA09657822Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGED AT STA 833 TO 930, LBL 11 TO RBL 11. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53- 01-01.SDR IPXA09657821Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PNL FOUND DAMAGE AT STA 654+22 TO 690 RBL 33 TO RBL 55. FLOOR PNL FABRICATED PER EO B767-5320-9693F & INSTALLED AS PER MM 53- 01-01.SDR IPXA09657860Angle · crackedINSPECTION TYPE:C AFT BULK CARGO STA 1562-1582 RBL 76 INCH FLOORBEAM ANGLE FOUND CRACK (CRACK LENGTH 0.25 I NCH), AFT BULK CARGO STA 1562-1582 RBL 76 FLOORBEAM ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45SDR IPXA09657858Angle · crackedINSPECTION TYPE:C AFT BULK CARGO STA 1562-1582 LBL 76 INCH FLOORBEAM ANGLE FOUND CRACK (CRACK LENGTH 0.5 INCH), AFT BULK CARGO STA 1562-1582 LBL 76 FLOORBEAM ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.SDR IPXA09657857Angle · crackedINSPECTION TYPE:C AFT BULK CARGO STA 1562-1582 LBL 75 INCH FLOORBEAM ANGLE FOUND CRACK (CRACK LENGTH 1.375 INCH), AFT BULK CARGO STA 1562-1582 LBL 75 INCH FLOORBEAM ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.SDR IPXA09657836Web · crackedINSPECTION TYPE:C LEFT WING NR 3 SLAT O/B NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED (CRACK 0.090 INCH). LEFT WING NR 3 SLAT O/B AREA AT OSS792.3 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45, ORG MATERIAL IS CLAD 7075T6-0.063IN, CRACK LENGTH SDR IPXA09657835Web · crackedINSPECTION TYPE:C LEFT WING NR 3 SLAT I/B NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED (CRACK .0625 INCH). LEFT WING NR 3 SLAT I/B AREA AT OSS724.24 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45 ORG MATERIAL IS CLAD 7075T6-0.063IN, CRACK LENGTH SDR IPXA09657834Web · crackedINSPECTION TYPE:C RIGHT WING NR 10 SLAT I/B NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED (CRACK 0.090 INCH). RIGHT WING NR 10 SLAT I/B AREA AT OSS724.24 NOSE SKIN REPAIRED AS PER SRM 57- 43-01-2R2 FIG 201 REV 45 ORG. MATERIAL IS CLAD 7075T6-0.063IN, CRACK LSDR IPXA09657820Fitting · crackedINSPECTION TYPE:C MEC COMPT STA 246 RBL 10 FLOORBEAM CLIP FOUND CRACK (CRACK LENGTH 1.5 INCH). MEC COMPT STA 246 RBL 10 FLOORBEAM CLIP REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.SDR IPXA09657816Fitting · crackedINSPECTION TYPE:C MEC COMPT STA 246 LBL 50 FLOORBEAM CLIP FOUND CRACKED CRACK 0.875 INCH. MEC COMPT STA 246 LBL 50 FLOORBEAM CLIP REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.SDR IPXA09655194Floor Panel · damagedINSPECTION TYPE:N/A POS 9 RBL 5 STATION 1134 DAMAGED 1.7 X 1.2 PUNCTURE. REPAIRED PER EO B767-5320-32928-A.SDR IPXA09655193Floor Panel · damagedINSPECTION TYPE:N/A POS 9R RBL 8 STATION 1160 DAMAGED 1 INCH CUTOUT. REPAIRED PER EO B767-5320-32929-A.SDR UPS08653329Unknown · noisyINSPECTION TYPE:N/A 30 SECS AFTER GEAR RETRACTION THERE WAS A NOISE UNDER C/P SIMILAR TO A COMPRESSOR STALL WITH NO OTHER INDICATIONS. DURING DESCENT FROM FL 390 PASSING FL 390 PASSING FL 250 SAME SOUND WAS HEARD THROTTLES AT IDLE. CREW REQUESTED EMERGENCY ESDR UPS08652290Light · inoperativeINSPECTION TYPE:ETOP ENTRY DOOR EMERGENCY LIGHT IS OUT. REMOVED AND REPLACED EMERGENCY DOOR LIGHT PER MM 33-51-03-2.SDR UPS07650331Charger · unknownINSPECTION TYPE:ETOP AT ENG SHUTDOWN RECEIVED ADVISORY LEVEL EICAS MESSAGE "MAIN BAT CHGR". ACCOMPLISHED FIM PROCEDURE 31-41-00/101 SYSTEM CHECKS OK.SDR UPS05645552Window · smokeSTRONG ODOR & SMOKE IN COCKPIT. CREW DECLARED AN EMERGENCY. T/S - FOUND SMOKE COMING FROM F/O FRONT WINDOW ELECT. CONNECTOR ON AFT LWR CORNER OF WINDOW. F/O FRONT WINDOW REPLACED IAW MM 56-11-01 WINDOW HEATING SYS TEST PERFORMED IAW 30-41-00-5. ALL OPS OK NO SDR UPS05645551A/C Pack · malfunctionedINSPECTION TYPE: ETOP IN FLT FL350 M80 AFTER AND DURING TRANSMITTING NOTICE ACRID ODOR IN COCKPIT, NO OTHER INDICATIONS NOTED. COULD NOT ISOLATE OR IDENTIFY SOURCE OF ODOR 1 PACK OPS, PRIOR TO COAST OUT HF COULD NOT BE OPERATED FOR 45 MINS EVENTUALLY TO WORK
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