N325UP

Service difficulty reports · 117

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 = 'N325UP' 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 IPXA3678341Flap System · inoperativeAT APPROXIMATELY 5000 FT WHEN CONFIGURED FOR LANDING, LEFT FLAP STAYED AT 5 AND RT FLAP WENT TO 20. RAN EMERGENCY NON NORMAL CHECKLIST AND LANDED WITH FLAPS 20. EMERGENCY DECLARED. FLAPS CHECKS IAW FIM 27-58-00-815-803. R & R INDICATOR FLAP POSITION IMay 14, 2013 · N325UP · Boeing 76734AF · Trailing Edge Flap Control SystemSDR IPXA12674933Adi · inoperativeAIR TURN BACK DUE TO CAPTAIN`S ADI INOPERATIVE, POPPING AND CRACKLING HEARD, AND AN ELECTRICAL ODOR FOR BRIEF PERIOD. WHEN BLOCK IN, FOUND CAPT ADI CIRCUIT BREAKER TRIPPED, TROUBLE SHOT IAW FIM 34-12, TASK 818. FOUND CAPTAIN`S ADI BAD. R & R AND TESTED OK IAug 18, 2012 · N325UP · Boeing 76734AF · Attitude Gyro and Indicating SystemSDR IPXA1669582Skin · dented7C CHECK, RT WING OTBD FLAP, OTBD AFT LWR PANEL AT OTBD AREA FOUND DENT MARK. METAL HOT BOND REPAIR PERFORMED IAW SRM51-70-10-2R, REPAIR 4, FIG 202, SHEET.3, REV.50.Sep 26, 2011 · N325UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1669581Rib · crackedC CHECK, RT WING NR 9 SLAT AT UP STOP FITTING INBD FLANGE FOUND CRACKED. RT WING- NR9 SLAT UP STOP SUPPORT RIB INBD FLANGE REPAIRED IAW HX RS R-57-41-37231 REV A & EO B767-5750-44540-A, ORG MAT'L 7075-T7351 PLATE, CRACK LENGTH 0.375" FINAL CUTOUT SIZE IS 0Sep 26, 2011 · N325UP · Boeing 76734AF · Wing, Rib/BulkheadSDR IPXA1669503Hinge Fitting · crackedINSPECTION TYPE: C, RT WING - INBD MAIN FLAP, INBD AFT FLAP HINGE ARM FOUND CRACKED RT WING - INBD MAIN FLAP HINGE ARM FITTING REPAIR IAW SRM 57-53-02-2R1, REPAIR 1, FIG 201, REV 50, ORG MAT'L 7075-T73 FORGING CRACK LENGTH AT INBD FLANGE IS 0.375" AND OTBD FLSep 23, 2011 · N325UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA1669556Floor Panel · gougedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DEEP GOUGES AND 10 DENTS AT STA 412 TO STA 540, LBL 11 TO LBL 33. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.Sep 22, 2011 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1669555Floor Panel · puncturedINSPECTION TYPE:7C, FLOOR PANEL FOUND 8 PUNCTURES AND 15 DENTS AT STA 654+22 TO STA 690, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-01.Sep 22, 2011 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA11668135Floor Panel · damagedFLOOR PANEL POS NR 3-4R HAS DAMAGED ON UPPER SKIN. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.Jul 23, 2011 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667348Floor Panel · damagedREF D431900, FLOOR PANEL 2L HAS 1" HOLE. FABRICATED & REPLACED PANEL IAW EO B767-5320-9693-H.Jun 18, 2011 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA1667347Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL POS 2/3 HAS 1EA HOLE. REF D432191, FABRICATED & REPLACED FLOOR PANEL IAW EO B767-5320-9693-H.Jun 18, 2011 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10661275Eadi · intermittentCAPT EADI AND EHSI BLANKED OUT, BOTH NORM AND ALT. R & R EADI AND EHSI SYS OPS NORMAL.Jul 25, 2010 · N325UP · Boeing 76734AF · Integrated Flight SystemSDR IPXA10659025Floor Support · crackedBULK CARGO PIT FLOOR SUPPORT STRINGER AT 22.33 LBL AT STA 1480 AFT FASTENER HOLE ON OTBD SIDE IS CRACKED. R & R STRINGER AND SUPORT ANGLES IAW DWG 146T1219.Apr 1, 2010 · N325UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657666Panel · delaminatedRT WING INBD MAIN FLAP UPPER SURFACE OTBD EDGE. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5H REV 45.Oct 14, 2009 · N325UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09657665Panel · delaminatedVERTICAL STAB L/E AREA LT UPPER PANEL. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-70 PAR 5C FIG 10 REV 45.Oct 14, 2009 · N325UP · Boeing 76734AF · Vertical Stabilizer, Plate/SkinSDR IPXA09657664Stiffener · crackedFWD CARGO COMPT STA 785.9 LBL10.94 CENTER FRONT SPAR STIFFENER FOUND CRACK. FWD CGO COMPT STA785.9 LBL10.94 CTR TANK FRONT SPAR STIFFENER REPAIRED AS PER RS R57-10-36448 AND EO B767-5710-35177. ORG MAT'L BAC1518-912 2024T3511 DAMAGED SECTION CUT LENGTH 18.75Oct 14, 2009 · N325UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657663Stiffener · crackedFWD CARGO STA 785.9 LBL32.94 CENTER TANK FWD B/H STIFFENER CRACK. FWD CARGO STA 785.9 LBL 32.94 CTR TANK FWD B/H STIFFENER REPAIRED AS PER HX RS R57-10-36449 & EO B767-5710-35176. ORG MAT'L BAC1518-749 2024-T3511, DAMAGED SECTION CUT LENGTH 16.5 INCH THIS REOct 14, 2009 · N325UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657662Stiffener · crackedBULK CARGO COMPT STA 1480 RBL 8 FLOOR PANEL SUPPORT VERTICAL STIFFENER CRACK. REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 14, 2009 · N325UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657660Floor Support · crackedBULK CARGO COMPT STA 1417 LBL15 FLOOR PNL SUPPORT FOUND CRACKED. BULK CARGO COMPT STA 1417 LBL 15 FLOOR PANEL SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 14, 2009 · N325UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657658Floor Support · crackedBULK CARGO COMPT STA 1417 LBL9 FLR PNL SUPPORT FOUND CRACK. BULK CARGO COMPT STA 1417 LBL9 FLOOR PANEL SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 14, 2009 · N325UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09657655Skin · damagedLIGHTNING STRIKE DMG TO FASTENER AT STA 325 STR 24R. DMI D363083 LIGHTNING STRIKE AT STA 325 STR 24R DAMAGE FASTENER REPLACED AS PER SRM 53-00-01-2R8 FIG 201 REV 45.Oct 14, 2009 · N325UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA09657654Skin · crackedRHW NR 10 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED JUST AT OSS792.24 RHW NR 10 SLAT AT OSS792.24 OTBD NOSE SKIN REPAIR AS SRM 57-43-01-2R2 FIG 201 REV45. ORG MAT'L CLAD 7075T6-0063IN, ORG CRACK LENGTH .125 INCH DAMAGED SKIN CUTOUT 7.25 INCH BY 9 INCH Oct 14, 2009 · N325UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657653Skin · crackedRT WING NR 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED JUST AT OSS724.24 RHW NR 10 SLAT AT OSS724.24 INBD NOSE SKIN REPAIRED AS PER SRM 57-43-01 -2R2 FIG 201 REV 45. ORG MAT'L CLAD 7075T6-0063IN, ORG CRACK LENGTH .125 INCH DAMAGED SKIN CUTOUT 7.125 INOct 14, 2009 · N325UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657652Skin · crackedLT WING NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED JUST AT OSS572.9. LHW NR 4 SLAT AT OSS572.9 INBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 SIG 201 REV 45. ORG MAT'L CLAD 7075T6-0063IN, ORG CRACK LENGTH .125 INCH DAMAGED SKIN CUTOUT 7.5 I NCH BY 8.Oct 14, 2009 · N325UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657651Skin · crackedLHW NR 3 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED JUST AT OSS792.24 LHW NR 3 SLAT AT OSS792.24 OTBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45. ORG MAT'L CLAD 7075T-600631N ORG CRACK LENGTH .125 INCH DAMAGED SKIN CUTOUT 7 INCH BY 9 INCHOct 14, 2009 · N325UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657650Skin · crackedLHW NR 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACK JUST AT OSS724.24. LHW NR 3 SLAT AT OSS 724.24 INBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45. ORG MAT'L CLAD 7075T6-00631N ORG CRACK LENGTH .125 INCH DAMAGED SKIN CUTOUT 7 INCH BY 9 INCH TOct 14, 2009 · N325UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657649Skin · crackedLHW NR 2 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACK AT OSS872, LHW NR 2 SLAT OSS872 INBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45. ORG MAT'L 7075T6-00631N CRACK LENGTH .125 INCH DAMAGED SKIN CUTOUT 6.875 INCH BY 9.125 INCH THIS REPAIR IS CLASOct 14, 2009 · N325UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09657690Floorbeam · crackedINSPECTION TYPE:C CABIN FLOOR SUPPORT INBD ATT SPLICE ANGLE FOUND CRACK JUST AT STA 1578 LBL 75 INCH CRACK LENGTH 1.75 INCH. BULK CARGO STA 1578 LBL 75 INCH FLOOR SUPPORT INBD ATTACH SPLICE ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657689Floorbeam · crackedINSPECTION TYPE:C CABIN FLOOR SUPPORT ATT INBD SPLICE ANGLE FOUND CRACK JUST AT STA 1578 RBL 75 INCH CRACK LENGTH 1.75 I NCH. BULK CARGO STA 1578 RBL 75" FLOOR SUPPORT I/B ATTACH SPLICE ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV.45Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657688Floorbeam · crackedINSPECTION TYPE:C CABIN FLOOR SUPPORT OTBD ATT SPLICE ANGLE FOUND CRACK JUST AT STA 1578 RBL 76 INCH CRACK LENGTH 1 INCH. CABIN FLOOR SUPPORT OTBD ATT SPLICE ANGLE REPLACED AS PER 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657687Floorbeam · crackedINSPECTION TYPE:C CABIN FLOOR SUPPORT OTBD ATT SPLICE ANGLE FOUND CRACK JUST AT STA 1578 LBL 76 INCH CRACK LENGTH 0.75 INCH. BULK CARGO STA 1578 LBL 76 INCH FLOOR SUPPORT OTBD ATTACH SPLICE ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657646Floorbeam · crackedMEC COMPT STA246 FLOORBEAM CLIP AT RBL 25 FOUND CRACK. MEC COMPT STA 246 RBL 25 FLOORBEAM ATTACH CLIP REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09657645Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 873 TO 933 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657644Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 975 TO 1114 LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657643Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 833 TO 930 RBL 11 TO RBL 33. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657642Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 985 TO 1090 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657641Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 1114 TO 1197+22 RBL 33 TO RBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657640Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 833 TO 930 LBL 55 TO LBL 77. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657639Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 690 TO 730 LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657638Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 540 TO 654+22 LBL 11 TO LBL 33. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657637Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 540 TO 654+22 LBL11 TO RBL11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657636Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 412 TO 540 RBL 33 TO RBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657635Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 690 TO 764 RBL 77 TO RBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657634Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 1425 TO 1540 LBL 55 TO LBL 77. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657633Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA1344 TO 1480 LBL77 TO LBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657632Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 975 TO 1114 RBL 55 TO RBL 77. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657631Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 412 TO 540 RBL 55 TO RBL 77. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657630Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 1197+22 TO 1207 LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657629Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 1207 TO 1344 LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657628Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 283 TO 412 RBL 77 TO RBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09657627Floor Panel · damagedMCD FLOOR PANEL FOUND DAMAGE AT STA 412 TO 540 LBL 55 TO LBL 77. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Oct 13, 2009 · N325UP · Boeing 76734AF · Fuselage Floor Panel
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