N7723E
Service difficulty reports · 270
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 = 'N7723E' 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 = 'N7723E' 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 SWAA2025022083779Angle · corrodedDOT#10 A-043 AFT CARGO COMPARTMENT LH Z ANGLE CORRODED STA 727E+6' TO 727D+3' LBL 24 WL 156<[01] REMOVED CORRSION IAW SRM 51-10-02-0G-0<BR>UT IAW B737 NDT PART 4; 51-00-00 PROC 2. ORIG .032'; LOSS .013'; REMAINING .019'. TOOL#40084; DUE 06AUG25<BR>EVALUATED ARSDR SWAA2025022083780Angle · corrodedDOT#11 A-043 AFT CARGO COMPARTMENT LH Z ANGLE CORRODED STA 727E+14' TO 787+5' LBL 24 WL 156<[01] REMOVED CORRSION IAW SRM 51-10-02-0G-0<BR>UT IAW B737 NDT PART 4; 51-00-00 PROC 2. ORIG .032'; LOSS .010'; REMAINING .022'. TOOL#40084; DUE 06AUG25<BR>EVALUATED ARSDR SWAA2025022083781Shield · corrodedDOT#13 A-043 AFT CARGO COMPARTMENT RH FWD SHIELD CORRODED STA 767 TO 787 RBL 24 WL 156<[01] REMOVED CORRSION ON TOP SIDE OF SHIELD IAW SRM 51-10-02-0G-0 EVALUATED AREA. ORGININAL THICKNESS 0.050'. LOSS 0.010'. REMAINING THICKNESS 0.040'. MAX. OF 10T ON ALLOWABSDR SWAA2025022083782Angle · corrodedDOT#14 A-043 AFT CARGO COMPARTMENT RH Z ANGLE CORRODED STA 727+4 TO 767 RBL 24 WL 156<[01] REMOVED CORRSION IAW SRM 51-10-02-0G-0; UT IAW B737 NDT PART 4; 51-00-00 PROC 2. ORIG .032'; LOSS .009'; REMAINING .023'. TOOL#40084; DUE 06AUG25; EVALUATED AREA. ORGINISDR SWAA2025022083772Web · corrodedDOT#03 A-043 AFT CARGO COMPARTMENT DOOR SILL WEB CORRODED STA 807+3' TO 827+4' RBL 27 WL 156<[01] VERIFIED ALL NDT TASK COMPLETE;[02] 01 - REMOVED AND REPLACED AFT CARGO PIT LOWER DOOR SILL WEB PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION ANDSDR SWAA2025022083776Web · corrodedFWD CARGO DOOR CUTOUT LOWER SILL WEB HAS EVIDENCE OF CORRION IN SEVERAL AREAS OF WEB<[01] 01 - REMOVED AND REPLACED PER SRM 53-30-15-1A-1-A00071.SDR SWAA2025021983778Strap · corrodedDOT#08 A-043 AFT CARGO COMPARTMENT FLOORBOARD 'T' STRAP CORRODED STA 727D RBL 2 WL 156<[01] REPLACED AFT CARGO COMPARTMENT FLOORBOARD 'T' STRAP P/N 146A9401-8 TAG#49635 IAW IPC 53-42-11-30 INSTALLED ON W/O TTG8Q00WXN8W;[02] VERIFIED ITEM 1<BR>C/WSDR SWAA2025021983777Angle · corrodedDOT#07 A-043 AFT CARGO COMPARTMENT RH 'Z' ANGLE CORRODED STA 887+8 RBL 24 WL 156<[01] EVALUATED AREA. ORGININAL THICKNESS 0.032'. LOSS 0.012'. REMAINING THICKNESS 0.020'. MAX. OF 10T ON ALLOWABLE DAMAGE. OUT OF LIMITS IAW SRM 53-00-53-1A-2<BR>FABRICATED NEW Z SDR SWAA2025021983773Attach Angle · corrodedDOT#05 A-043 AFT CARGO COMPARTMENT FWD BKHD LOWER CENTER FAIRING ATTACH ANGLE TOP STRAP CORRODED STA 727+4' RBL 20 WL 156<[01] REPLACED (PLATE) AFT CARGO COMPARTMENT P/N453A2611-12 TAG#A289211 IAW IPC 25-52-10-02 INSTALLED ON W/O TTG8Q00WXN8W;[02] REPLACED (PLSDR SWAA2025021983594Hook · corroded(A204 DOT 59) RIGHT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK HAS MINOR CORROSION<[01] 01 - REMOVED AND REPLACED R/H EMERGENCY EXIT DOOR LIFE LINE PER [AMM 25-61-10-400-802-NG (EMERGENCY EXIT DOOR LIFE LINE INSTALLATION - PERMANENT)]<BR><BR>STRAP P/N: 416A1531-17SDR SWAA2025021983593Hook · corroded(A204 DOT 60) LEFT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK HAS MINOR CORROSION<[01] LEFT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK WAS REMOVED AND REPLACED I.A.W. AMM 25-61-10-400-802-NG<BR><BR>TOOL USED: STAAR 39119; DUE 03/03/25;[02] VERIFIED STEP 1<BR>AUDIT CWSDR SWAA2025021983001Light · crackedEMERGENCY EXIT LIGHT ON FWD LAVATORY IS CRACKED<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT ON FWD LAVATORY IAW AMM 33-51-01-960-802 STEP 3A-3C(1-4)(5)(D) (6)(7)(10)(12).<BR>SIGNING FOR JOSEPH KREBS EMP#38394;[02] REMOVED AND REPLACED EMERGENCY EXIT LIGHT OSDR SWAA2025022082601Floorboard · pulled154-05 PASSENGER CABIN FLOOR BOARD 231XF HAS MULTIPLE AREAS OF PULLED FIBERGLASS FROM TAPE REMOVAL. REFER TO FAULT TTG8Q00XXV53 WHERE EA 25-153-00035 WAS ADDED AS A SUBTASK.SDR SWAA2025021982605Floorboard · pulled154-15 PASSENGER CABIN FLOOR BOARD 242DF HAS MULTIPLE DENTS AND PULLED FIBERGLASS ON SURFACE<[01] 'REFER TO FAULT TTG8Q00XXV53 WHERE EA 25-153-00035 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/WSDR SWAA2025021982604Floorboard · pulled154-10 PASSENGER CABIN FLOOR BOARD 232SF HAS MULTIPLE DENTS AND PULLED FIBERGLASS ON UPPER SURFACE<[01] 'REFER TO FAULT TTG8Q00XXV53 WHERE EA 25-153-00035 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/WSDR SWAA2025021982602Floorboard · pulled154-06 PASSENGER CABIN FLOOR BOARD 241AF HAS MULTIPLE AREAS OF PULLED FIBERGLASS ON SURFACE<[01] 'REFER TO FAULT TTG8Q00XXV53 WHERE EA 25-153-00035 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/WSDR SWAA2025021982851Scuff Plate · crackedFWD CARGO DOOR FWD CORNER SCUFF PLATE IS CRACKED<[01] CRACK ON FWD CARGO DOOR FWD CORNER SCUFF PLATE WAS REPIARED ON BACK SHOP WORK ORDER 46301/1400/0001 SERIAL NO: 9519433 IAW SRM 53-30-15-2R-1 (WELD REPAIR);[02] VERIFIED ITEM 1<BR><BR>AUDIT C/WSDR SWAA2025022082595Wedge · crackedR/H WING # 5 SLAT LOWER CENTER WEDGE HAS CRACK ON EDGE OF WEDGE. REMOVED R/H WING # 5 SLAT LOWER CENTER WEDGE IAW SRM 51-40-02-0G-0. UT IAW B737 NDT PART 4; 51-00-01. NO ADDITIONAL DEFECTS NOTED. TOOL#31896; DUE 29APR25. EVALUATED AND FOUND SMALL CRACK AT CESDR SWAA2025022082455Attach Fitting · crackedR/H WING TO BODY FAIRING PANEL 191AR AFT EDGE; CENTER ATTACH BEAM IS CRACKED AT UPPER END.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] VERIFIED STEP 1<BR>AUDIT CWSDR SWAA2025022081912Beam · corroded(A-204 DOT 29) LH WING FIXED LEADING EDGE CAVITY. FORWARD EDGE OF KRUEGER FLAP CUTOUT. NOSE BEAM HAS CORROSION IN RADIUS FROM #1 KRUEGER FLAP 2ND FROM I/B HINGE TO #2 KRUEGER FLAP 2ND FROM I/B HINGE<[01] REMOVED DAMAGE AND REPAIRED PER EA 25-157-00351;[02] COMSDR SWAA2025022081640Plate · corroded(A204 DOT 3) #1 FLAP TRACK FORWARD FAIRING. INNTER FORWARD MOUNT PLATE HAS EVIDENCE OF CORROSION<[01] 04 - REPAIRED PER [SRM 57-53-71-1A-1-A00978 (PERMANENT (NON-DENT DAMAGE TYPES))];[02] COMPLETE<BR>AUDIT C/WSDR SWAA2024122680673Lamp · inoperativeL1 DOOR AND R/H MID EMERGENCY EXIT SIGN SEVERAL LAMPS INOP<[01] R&R SEVERAL LAMPS ON L1 DOOR AND R/H EMERGENCY DOOR EXIT SIGNS PER AMM 33-51-01. OPS CHECK GOOD.SDR SWAA2024122680903Sign · inoperativeL1 DOOR AND R/H MID EMERGENCY EXIT SIGN SEVERAL LAMPS INOP<[01] R&R SEVERAL LAMPS ON L1 DOOR AND R/H EMERGENCY DOOR EXIT SIGNS PER AMM 33-51-01. OPS CHECK GOOD.SDR SWAA2024111858895Battery Pack · inoperativeL2 EMERGENCY LIGHT INOP.<[01] RELAMPED; REF. AMM 33-51-04. NO FIX. SWAPPED POWER SUPPLIES M1672 AND M1673; REF. AMM 33-51-06. NO FIX. SWAPPED BACK TO ORIGINAL. CHECK CONTINUITY FROM D10746 TO GND; REF. WDM 33-51-14-6. GOOD CONTINUITY. REQUIRES MORE T/S; SHORT-SDR SWAA2024111859058Lens · out of adjustL2 EMERGENCY LIGHT LENS ASSEMBLY MISSING 1 SCREW.<[01] REPLACED MISSING SCREW IAW SIP.SDR SWAA2024091236727Floor Support · crackedLH UPPER CENTER INTERCOSTAL FLOOR SUPPORT CRACKED ABOVE AIR CONDITIONING DISTRIBUTION BAY STA. 540<[01] REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02.SDR SWAA2024090332584Latch · damagedL1 DOOR SLIDE HAS SLIDE LATCHING MECHANISM TO BEZEL DAMAGED.<[01] REMOVED AND REPLACED L1 DOOR ESCAPE SLIDE IAW MT 725-61-06-FE.SDR SWAA2023112424029Girt Bar · brokenFWD SERVICE GIRT BAR BRACKET BROKEN<[01] R&R GIRT BAR RETAINING BRACKET FASTENER PER SRM 51-40-02. SLIDE REMOVAL NOT REQUIRED.SDR SWAA2023112123287Bracket · brokenFWD SERVICE DOOR GIRT BAR BRACKET BROKEN.<[01] MADE TEMPORARY REPAIR PER EA M-23-125-01839. PERMANENT REPAIR DUE BY 11/30/23. OK TO CONTINUE PER M-23-125-01839TLD. A/C OK FOR SERVICE.SDR SWAA2023051247341Power Supply · inoperativeINOP EMERGENCY LIGHT FWD ENTRY DOOR; FWD GALLEY; STOWAGE BIN 3 RH; EME RGENCY DOOR LH(2EA) AT PASSENGER CABIN 2023-238132<[01] PERFORMRD FIM 33-50 TASK 801 AND FOUND BURNED FUSE (3 3/A) ON POWER SUPPLY ;WERE REPLACED IAW B737-700 AMM 33-51-06-960-804 AND PERFOSDR SWAA2023051247438Girt Bar · out of adjustPASSENGER CABIN R1 DOOR SLIDE BAR HARD TO EXTEND AND CONNECT TO THE FLOOR 2023-238139<[01] INSTALLED CORRECTLY ESCAPE SLIDE FWD SERVICE DOOR IAW SWA TASK MT 725-61-06; STEP 3K(2)(3);[02] TASK CARD COMPLETE.SDR SWAA2023051527365Web · corrodedCORROSION WEB LOC ON FUELING STATION INTERNAL AREA OF PANEL 621GB AT RT WING 2023-238059<[01] REPLACED REFUEL STATION PANEL AND PERFORMED OPERATIONAL TEST IAW B737-700 AMM 28-41-61-400-801 TEST IS OK<BR>SEE INDIVIDUAL SIGN OFF STEP BELOW;[02] CORRECTED STEP 1<SDR SWAA2023051527364Angle · crackedCRACK BODY STA 663.75 ANGLE UPPER POSITION LBL 43 AT AIR CONDITIONING BAY 2023-238062<[01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23.;[02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 220272712; DUE DATSDR SWAA2023051527168Support Angle · brokenBROKEN ACCESS PANEL 651GB SUPPORT ANGLE AT RT WING 2023-238052<[01] REPLACED SUPPORT ANGLE AT RT WING LOC. ON ACCESS PANEL 651GB IAW B737-700 SRM 51-10-02 ITEM 9;[02] CORRECTED STEP 1 <BR>REPLACED SUPPORT ANGLE AT RT WING LOC. ON ACCESS PANEL 651GB IAW B737-70SDR SWAA2023051526181Plate · crackedCRACK INBOARD TRAILING EDGE CORRUGATED PLATE IRSS 215 AT RT WING 2023-237955<[01] REPLACED CORRUGATED PLATE LOC. IRSS 215 AT RT WING AND FASTENERS IAW B737-700 SRM 51-10-02 ITEM 9 . SEE INDIVIDUAL SIGN OFF BELOW.;[02] COMPLETE TASK CERTIFIEDSDR SWAA2023051525845Angle · crackedCRACK ANGLE LOCATED BS400 AND STR26L FWD CARGO COMPARTMENT 2023-237904<[01] REPLACED ANGLE LOCATED BS400 AND STR26L FWD CARGO COMPARTMENT IAW B737 -700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 143A7505 SHEET 2 REV: B SEE INDIVIDUAL SIGNOFFS BELOW.;[02] RISDR SWAA2023051525847Skin · crackedCRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 16.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.500 INCH 2023-237925<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500D; S/N: N500X1210V022240; SDR SWAA2023051225580Intercostal · crackedCRACK ON INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 328 TO BS 344 LBL47 AT FWD GALLEY AREA 2023-237863<[01] REPLACED INTERCOSTAL WEB AND FASTENERS LOCATED FLOOR STRUCTURE BTW BS 328 TO BS 344 LBL47 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 AND DWG 141SDR SWAA2023051225579Intercostal · crackedCRACK ON INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 LBL47 AT FWD GALLEY AREA 2023-237856<[01] REPLACED INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 LBL47 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 AND DWG 141A5400 SHEET 26SDR SWAA2023051525231Intercostal · crackedCRACK ON INTERCOSTAL LOCATED FWD ENTRY DOOR CUTOUT BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA 2023-237784<[01] REPLACED INTERCOSTAL LOCATED FWD ENTRY DOOR CUTOUT BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA IAW B737-700 SRM 51SDR SWAA2023051525340Floorbeam · crackedCRACK ON FLOOR BEAM LOCATED BS 294.5 AT LEVEL STR 17R RBL 53 AT FWD GALLEY AREA 2023-237816<[01] TOOL USED: EDDY CURRENT EQUIPMENT ; P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 27-MAR-24;[02] TOOL USED: RADIOMETER/PHOTOMETER P/N: XRP-3000; S/N:1859843; CAL DUESDR SWAA2023051525337Floorbeam · corrodedCORROSION ON FLOOR BEAM 986.5 RBL 44 WL 208.1 AT AFT GALLEY AREA 2023-237792<[01] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN 220272712; DUE DATE 17-DEC-23;[02] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 RBL44 AND WL208.1 AT AFT GALLEY AREA IAW B73SDR SWAA2023051525336Floorbeam · corrodedCORROSION ON FLOOR BEAM 986.5 LBL 44 WL 208.1 AT AFT GALLEY AREA 2023-237791<[01] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN 220272712; DUE DATE 17-DEC-23;[02] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 LBL44 AND WL208.1 AT AFT GALLEY AREA IAW B73SDR SWAA2023051225225Stub Frame · crackedCRACK ON STUB FRAME LOCATED BS 294.5 AT LEVEL STR 17R RBL 53 AT FWD GALLEY AREA 2023-237787<[01] TOOL USED EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220273012; DUE DATE: 17-DEC-23.;[02] REMOVED DAMAGE ON STUB FRAME LOC. BTW BS291.5 TO BS 294.5 AT LEVEL SSDR SWAA2023051225230Structure · crackedCRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2023-237783<[01] REPLACED TIE CLIP AND FASTENERS LOC. ON BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; DWG 141A1110 SHEET 18; REV - AND DWG 143A8380 SHEET 21; RSDR SWAA2023051724903Girt Bar · deterioratedDETERIORATED GIRT BAR FITTING SLEEVE (4 E/A) ON FLOOR PANEL 242UF AT AFT GALLEY AREA 2023-237740<[01] REPLACED GIRT BAR FITTING SLEEVE (4 E/A) ON FLOOR PANEL 242UF AT AFT GALLEY AREA AND CURED EPOXY ADHESIVE ON SLEEVES OF FLOOR PANEL IAW B737-700 SRM 53-00-50-SDR SWAA2023051524895Access Panel · delaminatedDELAMINATED ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2023-237730<[01] TOOL USED: CALIPER P/N: 500-193-30 S/N: 0000288 DUE DATE: 27-DEC-23.;[02] TOOL USED SCALE P/N SPX601 S/N 8340225441 DUE DATE 20 JUL 23;[03] TOOL USED: HOT BONDER PN: HCS9200B-AV SN: 18196SDR SWAA2023051524748Fitting · deterioratedDETERIORATED GIRT BAR FITTING HARDWARE LT AND RT AT FWD GALLEY AREA 2023-237710<[01] REPLACED GIRT BAR FITTING HARDWARE LT AND RT AT FWD GALLEY AREA IAW SOPM 20-50-01 REV 38;[02] REPLACED GIRT BAR FITTING HARDWARE LT AND RT AT FWD GALLEY AREA IAW SOPM 20-50-01SDR SWAA2023051525042Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED CEILING AREA OF BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2023-237749<[01] REPLACED SUPPORT ANGLE LOCATED CEILING AREA OF BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A7901 SHESDR SWAA2023051524899Support Angle · crackedCRACK TRAILING EDGE DEFLECTION CONTROL SUPPORT ANGLE LOCATED ORSS 261 PLUS 18 INCHES APROX. AT RT WING. REPLACED SUPPORT ANGLE LOCATED TRAILING EDGE DEFLECTION CONTROL; ORSS 261 PLUS 18 INCHES APROX. AT RT WING IAW SRM 51-10-02 ITEM 9 AND DRAWING 115A6200 SHE
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