N7732A
Service difficulty reports · 265
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 = 'N7732A' 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 = 'N7732A' 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 SWAA2023110917224Battery Pack · inoperativeAFT LEFT WET AREA EMERGENCY LIGHTS ARE INOP / [01] AFT LEFT WET AREA POWER SUPPLY - BATTERY PACK REMOVED & REPLACED IAW AMM 33-50-06-960-805 OPS-CHECK FOR EMERGENCY LIGHT GOOD;[02] AFT LEFT WET AREA POWER SUPPLY - BATTERY PACK REMOVED & REPLACED IAW AMM 33-51-SDR SWAA2023110917225Battery Pack · inoperativeAFT RIGHT WET AREA EMERGENCY LIGHTS ARE INOP / [01] AFT RIGHT WET AREA POWER SUPPLY - BATTERY PACK REMOVED & REPLACED IAW AMM 33-50-06-960-805 OPS CHECK FOR EMERGENCY LIGHT GOOD.;[02] AFT RIGHT WET AREA POWER SUPPLY - BATTERY PACK REMOVED & REPLACED IAW AMM 33SDR SWAA2023092102060Light · inoperativeEXTERIOR LEFT AFT EMERGENCY LIGHT INOP<[01] RELAMPED EXT LEFT AFT EMERGENCY LIGHT PER AMM 33-51-00 AND WDM 33-51-11.SDR SWAA2023090596945Handle · looseLEFT EMERGENCY EXIT ASSIST HANDLE CONTAINER LOOSE<[01] INSTALLED MISSING 1/4 TURN FASTENER PER AMM 52-22-51SDR SWAA2023081588340Bulb · inoperative16 DEF EMERGENCY LIGHT INOP<[01] RE-LAMPED AREA LIGHT ON 16DEF PER AMM 33-51-03. OPS CHECK GOOD.SDR SWAA2023072581295Vapor Barrier · crackedL/H VAPOR BARRIER IS CRACKED AT BS 663 LBL 40 EIGHT INCHES FROM TOP OF BARRIER 5.5IN IN LENGTH.<[01] C/W EA M-21-157-00675SDR SWAA2023072581296Vapor Barrier · crackedL/H VAPOR BARRIER IS CRACKED AT BS 663 LBL 51 SIX INCHES FROM TOP OF BARRIER 5 INCHES IN LENGTH.<[01] C/W M 21-157-00675SDR SWAA2023072480859Bracket · brokenFWD KEEL BEAM FWD RH BRACKET BROKEN<[01] REMOVED AND REPLACED BRACKET REF SRM 51-40-02SDR SWAA2023062872478Slide · out of adjustSLIDE PACK FELL OUT OF FWD SERVICE DOOR.<[01] RE-INSTALLED FWD SERVICE DOOR SLIDE PER MT 725-61-06.SDR SWAA2023061960522Slide · out of adjustFWD ENTRY DOOR SLIDE PARTIALLY OUT OF CASE<[01] REINSTALLED FWD ENTRY DOOR SLIDE PER MT 725-61-06SDR SWAA2022072730900Radome · delaminatedC/R REPLACE NOSE RADOME DUE TO DELAMINATION / [01] REMOVED NOSE RADOME. REF B737-700 AMM 53-52-00-000-801;[02] VERIFIED STEP 1<BR>OK TO INSTALL SERVICEABLE RADOME;[03] INSTALLED SERVICEABLE RADOME. B737-700 AMM 53-52-00-400-801<BR><BR>TORQUE WRENCH <BR>B/C: 16SDR SWAA2022072730361Battery Pack · inoperativeL1 DOOR EXTERIOR EMERGENCY LIGHT INOP. / [01] REMOVED AND REPLACED FWD L EMERGENCY BATTERY PACK; OPS TEST PERFORMED AND TEST PASSED AS PER B737 AMM 33-51-06-960-805.;[02] VERIFIED STEP 1SDR SWAA2022072729653Shield · corrodedITEM GENERATED TO CAPTURE CORROSION MEASUREMENT TABLE FOR NR CORROSION**AFT CARGO DOOR CUTOUT SHIELD JUST AFT OF CARGO DOOR CUTOUT; CORRODED. STA 847-867; WL-156; BL-33 [TTG8Q00D7SJM] / [01] CHART WAS GENERATED AND FILLED OUT FOR ITEM TTG8Q00D7SJM;[02] VERIFIESDR SWAA2022072729485Stiffener · crackedR/H HORIZONTAL STABILIZER RIB #4 STIFFENER #2; LOWER FLANGE WITH A CRACK. / [01] CRACK CONFIRMED IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK LENGTH : 0.945'<BR>[NORTEC 600 ; B/C 166317 ; CALIB.DUE- 10/22];[02] CUTOUT THE DAMAGE AREA AT RH HORIZONTAL STAB RIBSDR SWAA2022072728472Angle · ratchetingRH STAB RIB #5 (STA 129.50) HAS CRACK AT LWR I/B FLANGE BETWEEN STIFFENERS #1 AND #2. / [01] PERFORMED HFEC INSP ON RIB#5 STA 129.50 LOWER INBD FLANGE BETWEEN STIFFENER#1 AND #2 B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED MARKED<BR>TOOL USED : NORTEC 600 B/CSDR SWAA2022072728473Angle · crackedRH STAB RIB #5 (STA 129.50) HAS CRACK AT LWR O/B FLANGE BETWEEN STIFFENERS #1 AND #2. / [01] PERFORMED HFEC INSP ON RIB#5 STA 129.50 LOWER O/B FLANGE BETWEEN STIFFENER#1 & 2 B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED MARKED<BR>TOOL USED : NORTEC 600 B/C 172SDR SWAA2022072728475Angle · crackedRH STAB RIB #5 (STA 129.50) HAS CRACK AT LWR FWD SECTION PARALLEL TO LWR FLANGE / [01] PERFORMED HFEC INSP ON FWD LWR AREA OF RIB#5 IAW B737 NDT P6 51-00-00 PROC.23; CRACK CINFIRMED MARKED<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] CUT OUT DAMAGEDSDR SWAA2022072728474Angle · crackedRH STAB RIB #5 (STA 129.50) HAS CRACK AT LWR O/B FLANGE AT STIFFENER #2. / [01] PERFORMED HFEC INSP ON RIB#5 STA 129.50 LOWER O/B FLANGE AT STIFFENER#2 B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED MARKED<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[07]SDR SWAA2022072728958Stiffener · crackedR/H HORIZONTAL STABILIZER RIB #4 STIFFENER #3 LOWER FLANGE WITH A CRACK / [01] CRACK CONFIRMED IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK LENGTH : 1.339'<BR>[NORTEC 600 ; B/C 166317 ; CALIB.DUE- 10/22];[02] CUTOUT THE DAMAGE AREA AT RH HORIZONTAL STAB RIB #SDR SWAA2022072729277Support Angle · crackedFOUND T SUPPORT ANGLE CRACKED AT RT STAB RIB #5 / [01] REMOVED FWD T SUPPORT ANGLE FROM RT STAB RIB #5 AS PER B737-700 51-40-02-0G-0;[02] CORRECTION FOR STEP #1 SHOULD READ: REMOVED FWD T SUPPORT ANGLE FROM RT STAB RIB #5 AS PER B737-700 SRM 51-40-02-0G-0;[03]SDR SWAA2022072727977Splice Plate · corrodedAFT CARGO COMPARTMENT R/H SPLICE PLATES FOUND WITH EXFOLIATED CORROSION / [01] REMOVED AND REPLACED SPLICE PLATES AT AFT CARGO COMP.R/H AS PER B-737-700 SRM # 51-10-02-OG-0.;[02] VERIFIED STEP 1.SDR SWAA2022072726079Rib · crackedFOUND CRACK AT FWD LOWER RIB #4 AFTER REMOVAL OF RIB #4 FOUND A CRACK AT THE LOWER FWD SIDE OF THE RIB / [01] PERFORMED HFEC INSP ON FWD LWR AREA OF RIB#4 IAW B737 NDT P6 51-00-00 PROC.23; CRACK CINFIRMED MARKED<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/SDR SWAA2022072724552Baffle · crackedFWD CARGO COMP. LEFT SIDE BAFFLE IS CRACK AT FWD END BETWEEN STA 500A AND 500B LBL-24. / [01] REMOVED FWD CARGO LT.SIDE BAFFLE AT STA 500A AND 500B LBL 24 IN REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1;[03] PEROFRMED HFEC ROTO INSP ON FASTENER OPEN HOLES; IAW BSDR SWAA2022072734896Baffle · crackedFWD CARGO COMP. LEFT SIDE BAFFLE IS CRACK AT FWD END BETWEEN STA 500A AND 500B LBL-24. / [01] REMOVED FWD CARGO LT.SIDE BAFFLE AT STA 500A AND 500B LBL 24 IN REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1;[03] PEROFRMED HFEC ROTO INSP ON FASTENER OPEN HOLES; IAW BSDR SWAA2022072724554Channel · crackedFWD CARGO COMP. RIGHT/Z-CHANNEL HAS A CRACK BETWEEN STA 500C-STA 500D RBL-24. / [01] LOCATED AND DRILLED NEW FWD CARGO RT. SIDE 'Z' CHANNEL IN REF SRM 51-40-05-0G-0;[02] VERIFIED STEP # 1;[03] TREATED AND PRIMED FWD CARGO RT. Z CHANNEL AS PER SRM 51-20-01-0G-0SDR SWAA2022072724547Angle · crackedAFT CARGO COMP. FWD BULKHEAD CENTER LOWER SUPPORT ANGLE IS CRACK AT STA 727+4 RBL-5. / [01] REMOVED DAMAGED SUPPORT ANGLE FROM AFT CARGO FWD BULKHED AT STA 727+4 RBL-5;[02] CORRECTION. REMOVED DAMAGED SUPPORT ANGLE FROM AFT CARGO FWD BULKHED AT STA 727+4 RBL-5SDR SWAA2022072724543Channel · corrodedAFT CARGO COMP. RIGHT/Z-CHANNEL HAS CORROSION AROUND FASTENERS HOLE FROM STA 727B TO STA 767 RBL-22. / [01] FOUND EXFOLIATED CORROSION TO BE OUT OF LIMITS AS PER B737 SRM 53-00-53-1A-2;[02] RECIEVED NEW PART 146A7502-51; NEW PART WILL BE INSTALLED UNDER TASK CSDR SWAA2022072724546Channel · corrodedAFT CARGO COMP. LEFT/Z-CHANNEL HAS CORROSION AROUND FASTENERS HOLE FROM STA 727C TO STA 787 LBL-22. / [01] FOUND EXFOLIATED CORROSION TO BE OUT OF LIMITS AS PER B737 SRM 53-00-53-1A-2;[02] RECIEVED NEW PART 146A7502-27; PART WILL BE INSTALLED UNDER TASK CARD: SDR SWAA2022072723940Stiffener · crackedL/H HORIZONTAL STABILIZER RIB #2 STIFFENER #2 LOWER FLANGE HAS A CRACK. / [01] PERFORMED HFEC INSP ON RIB STIFFENER LOWER FLANGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] PERFORMED HFEC INSP ON RSDR SWAA2022072723941Stiffener · crackedL/H HORIZONTAL STABILIZER RIB #5 STIFFENER #2 LOWER FLANGE; WITH A CRACK. STAB. STA-129.50 / [01] PERFORMED HFEC INSP ON RIB STIFFENER LOWER FLANGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[06] CUT OSDR SWAA2022072723942Stiffener · crackedL/H HORIZONTAL STABILIZER RIB #5 STIFFENER #3 LOWER FLANGE; WITH A CRACK. STAB. STA-129.50 / [01] PERFORMED HFEC INSP ON RIB STIFFENER LOWER FLANGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] CUT OSDR SWAA2022072723943Stiffener · crackedL/H HORIZONTAL STABILIZER RIB #5 STIFFENER #4 LOWER FLANGE; WITH A CRACK. STAB. STA-129.50 / [01] PERFORMED HFEC INSP ON RIB STIFFENER LOWER FLANGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] CUT OSDR SWAA2022072723921Stiffener · crackedR/H HORIZONTAL STABILIZER RIB #4 STIFFENER #3 LOWER FLANGE WITH A CRACK. / [01] PERFORMED HFEC INSP ON RIB STIFFENER LOWER FLANGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] RT STABILAIZER RIB 4 STSDR SWAA2022072723923Stiffener · crackedR/H HORIZONTAL STABILIZER RIB #4 STIFFENER #4 LOWER FLANGE WITH A CRACK. / [01] PERFORMED HFEC INSP ON RIB STIFFENER LOWER FLANGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] CUTOUT THE DAMAGE AREA SDR SWAA2022072722896Shield · corroded**CORROSION**AFT CARGO DOOR CUTOUT SHIELD JUST AFT OF CARGO DOOR CUTOUT; CORRODED. STA 847-867; WL-156; BL-33 / [01] RECIEVED NEW PART P/N: 146A8127Y10ATSMRO. NEW PART WILL BE INSTALLED UNDER TASK CARD: TTG8Q0048PN3;[02] CORRECTION FOR STEP #1 SHOULD READ: RECSDR SWAA2022072722895Shield · crackedAFT CARGO DOOR CUTOUT SHIELD JUST FWD OF CARGO DOOR CUTOUT; CRACKED. / [01] RECIVED NEW SHIELD P/N 453A2611-1; NEW HIELD WILL BE INSTALL <BR>ON EA MOC CARD TTG8Q0043PN3;[02] VERIFIED STEP 1.SDR SWAA2022072722893Web · crackedL/H MAIN W/W FWD WALL; VERTICAL PRESSURE WEB HAS A CRACK. STA-663 LBL-40 / [01] MEASUREMENTS;[02] REMOVED PREVIOUS REPAIR AND PERFORMED VISUAL INSPECTION FOUND CRACK SIZE 16' AND FOUND UNWANTED MATERIAL ON VAPOR BARRIER PER B737NTM51-05-01 PART 1;[03] PREPAREDSDR SWAA2022072722748Slat · crackedRIGHT WING L/E SLAT #5 LOWER SURFACE SKIN HAS VISUAL CRACK INDICATION AT ACTUATOR FITTING SLAT STATION 85.19. (51-002) / [01] PERFORMED HFEC INSP. ON A POSSIBLE CRACK IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. CRACK NOTED AND MARK (CRACK LENGTH .156') <BR>TOSDR SWAA2022072722752Slat · crackedRIGHT WING L/E SLAT #7 LOWER SURFACE SKIN HAS VISUAL CRACK INDICATION AT ACTUATOR FITTING SLAT STATION 322.71. (51-004) / CRACK NOTED AND MARK (CRACK LENGTH .156') <BR>TOOL: NORTEC 600 B/C: 166317 DUE: 10/20/22;[02] REMOVED COVE PANELS 624CB; 624DB; 624EB AND SDR SWAA2022072722751Slat · crackedRIGHT WING L/E SLAT #6 LOWER SURFACE SKIN HAS VISUAL CRACK INDICATION AT ACTUATOR FITTING SLAT STATION 202.45. (51-003) / CRACK NOTED AND MARK (CRACK LENGTH .125') <BR>TOOL: NORTEC 600 B/C: 166317 DUE: 10/20/22;[02] REMOVED EXISTING FAST. LOCATED AND DRILLED NSDR SWAA2022062220069Sign · inoperativeLH OVERWING EMERGENCY EXIT SIGN FWD BULB INOP. / [01] RELAMPED LH OVERWING EXIT EXIT SIGN LIGHT IAW AMM 33-51-01.SDR SWAA2021122355685Pump · faultyENGINE 1 HYDRAULIC COW PRESSURE LIGHT ILLUMINATED ; LP #2061637 / [01] R&R #1 ENG ENGINE DRIVE HYDRAULIC PUMP PER AMM 29-11-11. REPLACED BOTH CASE DRAIN FILTERES & RETURN FILTER PER AMM 29-11-51 & AMM 29-11-61. SEE LOG PAGE 2061638 FOR LEAK & CHECK FILTER REPLSDR SWAA2021122756023Pump · failedNO1 ENG HYDRAULIC LOW PRESS LIGHT ; / [01] REPLACED #1 ENGINE HYDRAULIOC PUMP PER M/M 29-11-11. REPLACED #1 ENGINE HYDRAULIC SUPPLY AND PRESSURE LINES AS PRECAUTIONARY PER M/M 20-10-52. REPLACED #1 ENGINE ?A? SYSTEM CASE DRAIN FILTER; ?A? SYSTEM ENGINE PRESSURSDR SWAA2021081004909Support Bracket · crackedCRACKED BRAKET AT PNEUMATIC DUCT SUPPORT AT RH WING CENTER BOX FWD BULKHEAD FWD FACE; STA 540; WL 154; S- 24R / REMOVED AND REPLACED PNEUMATIC DUCT SUPPORT BRACKET AT CENTER BOX FWD BULKHEAD FWD FACE STA 540 WL 154 STR 24RSDR SWAA2020081303643Floor Panel · crackedFLOOR PANEL # 242AF CRACKED AT AFT END UPPER AND LOWER SURFACE MAIN CABIN CENTER WING R/ H SIDE. CLEANED & REPAIRED IAW SRM 53-00-50-2R-1 REPAIR 1.SDR SWAA2020061291283Seat Track · defectiveFO SEAT JAMMS FORE AND AFT MOVEMENT. R&R FO SEAT TRACKS REF AMM 25-11-11. OPS CHECKS NORMALLY AT THIS TIME.SDR SWAA2020060188050Battery Pack · dischargedEMERGENCY LIGHTS AT ROWS 14ABC AND 17ABC ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT STATION 727C IAW AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2020050574340Battery Pack · dischargedRH OVERWING EXIT EMERGENCY LIGHTS AND 2EA OVERHEAD BIN EMERGENCY LIGHTS INOP. / REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECKS GOOD NO FURTHER DEFECTS NOTED.SDR SWAA2022030492667Support Bracket · crackedRIGHT WING TRAILING EDGE FIXED PANEL SUPPORT BRACKET CRACKED. / REMOVED AND REPLACED BRACKET REF SRM 51-40-02.SDR SWAA2022030492657Fairing · crackedPANEL 193B HAS DELAMINATION; CRACKING AND EVIDENCE OF FASTENERS PULLING THROUGH ON INNER SURFACE OF PANEL AT FASTENER LOCATION 1; 2; 5; 34; 36; AND 38 / R&R PANEL 193B PER AMM 53-51-21.
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