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 SWAA2026092538079Scuff Plate · crackedREMOVED THE R1 GALLEY DOOR LOWER MAIN SILL SCUFF PLATE FOR PERMANENT REPAIR IAW AMM 53-11-01. REPLACED THE SCUFF PLATE IAW 51-40-02. PERFORMED A CABIN PRESSURE LEAK TEST IAW AMM 05-51-91. LEAK TESTED GOOD.SDR SWAA2026092132982Threshold · crackedR1 DOOR THRESHOLD IS CRACKED. COMPLIED WITH EA 26-153-02576. REF. TTG8Q01EQU8CSDR SWAA2026072778728Handle · brokenCAPTAIN`S SIDE GRAB HANDLE, JUST BELOW HUD, IS BROKEN. R & R CAPTAIN GRAB HANDLE IAW SOPM 20-50-01.SDR SWAA2026041788905Battery Pack · no testEMERGENCY LIGHT BATTERY PACK M01672 FAILED A CAPACITANCE CHECK. REMOVED AND REPLACED EMX BATTERY BACK M01672 IAW AMM 33-51-06-960-805-NG.SDR SWAA2025092216323Engine · failedNR 2 ENG FAIL ON T/O ROLL. NR 2 ENGINE FAILURE AND RTO AT 100KTS METAL IN THE TAILPIPE. REPLACED NR 2 ENGINE IAW MT 771-00-01 REF TTG8Q00YY43D.SDR SWAA2025072193095Lens · missing12 DEF EXIT/SALIDA COVER MISSING. INSTALLED NEW EMERG EXIT LENS PER AMM 33-51-01.SDR SWAA2025071792169Doubler · debondedL/H O/B UPPER SURFACE DISBOND ON EXISITING REPAIR DOUBLER. REMOVED DAMAGE PER SRM 57-53-01-2R14; PERFORMED TAP TEST PER 737 NET MANUEL PART 1 51-05-01 . PREPED AREA ;FABRICATED REPAIR PARTS INSTALLED REPAIR PARTS PER SRM 57-53-01-2R-14. AND SRM 51-70-05-2R-0 SDR SWAA2025061079517Girt Bar · looseR1 GIRT BAR LOOSE<[01] INSTALLED NEW RIVET ON R1 DOOR GIRT BAR BRACKET PER SRM 51-40-02.SDR SWAA2025032408355Engine · bird ingestionHIGH SPEED REJECTED TAKEOFF DUE TO LARGE BIRD STRIKE ON #2 ENGINE. NO ABNORMAL INDICATIONS; HOWEVER PAX AND FLIGHT ATTENDANTS COMPLAINED OF AN ODOR. <[01] C/W BIRD STRIKE INSPECTION ON ACFT PER 05-51-18 BIRD REMAINS FOUND IN NUMBER TWO ENGINE EVIDENCE OF BIRD SDR SWAA2025021996412Handle · brokenFWD ENTRY DOOR AFT DOOR ASSIST HANDLE IS BROKEN<[01] REMOVED AND INSTALLED IAW AMM 25-21-31-420-802<BR><BR>WN49860<BR>WN49856;[02] VERIFIED ITEM 1<BR>AUDIT C/WSDR SWAA2025021995295Battery Pack · inoperativeEMERGENCY EXIT BATTERY PACK M1674 WILL NOT CHARGE<[01] REMOVED AND REPLACED M1674 BATTERY PACK IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD<BR>WN49843;[02] VERIFIED ITEM 1<BR>C/WSDR SWAA2025021995296Battery Pack · inoperativeEMERGENCY EXIT BATTERY PACK M1675 WILL NOT CHARGE<[01] OPS CHECKED M1675 BATTERY IAW AMM 33-51-06-960-805; NO FAULT FOUND; OPS CHECK GOOD;[02] VERIFIED ITEM 1<BR>C/WSDR SWAA2025021995297Battery Pack · inoperativeEMERGENCY EXIT BATTERY PACK M2335 WILL NOT CHARGE<[01] REMOVED AND REPLACED M2335 BATTERY PACK IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD<BR>WN49840;[02] VERIFIED ITEM 1<BR>C/WSDR SWAA2025021995298Battery Pack · inoperativeEMERGENCY EXIT BATTERY PACK M1668 WILL NOT CHARGE<[01] REMOVED AND REPLACED M1668 BATTERY PACK IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD<BR>01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] WN4SDR SWAA2025021995299Battery Pack · inoperativeEMERGENCY EXIT BATTERY PACK M1670 WILL NOT CHARGE<[01] REMOVED AND REPLACED M1670 BATTERY PACK IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD.<BR>WN49839;[02] VERIFIED ITEM 1<BR>C/WSDR SWAA2025022092140Support Bracket · cracked(152-02) PASSENGER CABIN STA 867 STR 1R; FEEDER CABLE SUPPORT BRACKET IS CRACKED.<[01] REMOVED BRACKET AT BS867; BETWEEN S-1 AND S-2R; IAW SRM 51-40-02-0G-0. FABRICATED NEW BRACKET IAW BOEING DWG 287A4015 REV. -; BOEING PL 287A4015 REV. K; AND EA 25-153-00335.SDR SWAA2025022089840Intercostal · crackedDOT A24-77 FORWARD PIT. VERTICAL INTERCOSTAL AT STATION 480+15 BETWEEN STRINGERS 23L AND 25L CRACKED AT UPPER EDGE. BLENDED DAMAGE IAW SRM 51-10-02-0G-0. FOUND ADJACENT TO BLEND .040'; LOSS .007'; REMAINING .033' USING NDT TO VERIFY IN STEP 5. UPON FURTHER SDR SWAA2025021989045Floor Panel · pulledDOT#55 A-043 CABIN FLOOR PANEL 241KF HAS PULLED FIBERS ON TOP SIDE OF PANEL<[01] AUDIT C/W;[02] REFER TO FAULT TTG8Q00YBAGR WHERE EA 25-153-00203 WAS ADDED AS A SUBTASK..SDR SWAA2025021989044Floor Panel · pulledDOT#54 A-043 CABIN FLOOR PANEL 242GF HAS PULLED FIBERS ON TOP SIDE OF PANEL<[01] AUDITED;[02] REFER TO FAULT TTG8Q00YBAGR WHERE EA 25-153-00203 WAS ADDED AS A SUBTASK.SDR SWAA2025021989043Floor Panel · pulledDOT#53 A-043 CABIN FLOOR PANEL 231WF HAS PULLED FIBERS ON TOP SIDE OF PANEL<[01] REPAIRED PER EA 25-153-00203.SDR SWAA2025022088437Stringer · crackedFASTENER TAB FOR LEFT WING INBOARD UPPER FIXED LEADING-EDGE STRINGER P/N 116A4531-5 IS BROKED OFF. REMOVED AND REPLACED -5 STRINGER ON LEFT WING INBOARD UPPER FIXED LEADING-EDGE P/N 116A4531-5 ATAG WN49678 IAW BOEING DWG 116A4008 REV - SRM 51-40-02. VERIFIESDR SWAA2025022086137Stub Frame · crackedFWD GALLEY DOOR CUTOUT; UPPER FWD STUB FRAME HFEC SURFACE INSPECTION; FOUND 1' CRACK IN STUB FRAME AT JOGGLE; .70' ABOVE SEAL DEPRESSOR. MARKED IN BLACK. REF. CARD TTG8Q00TSZ8V INSP - FORWARD GALLEY DOOR (R1) BEAR STRAP BS 290-296 BETWEEN S-8R AND S-9R - GROUPSDR SWAA2025021986335Floor Panel · pulledFLOOR PANEL 222DF HAS PULLED FIBERS ON TOP SURFACE<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/WSDR SWAA2025021985676Floor Panel · crackedFLOOR PANEL 221BF HAS 5EA PLACES OF PANEL BEING CRACKED/BROKEN ON LOWER SURFACE.<[01] REPLACED FLOOR PANEL 221BF WITH SERVICEABLE FLOOR PANEL ON SHELF I.A.W REFERENCE TO AIPC 53-21-51-75 PG 14 SHEET 01 ITEM A;[02] INFO ONLY: PANEL 221BF WAS REPLACED ON #TTG8Q0SDR SWAA2025021985674Floor Panel · pulledFLOOR PANEL 221BF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] REPLACED FLOOR PANEL 221BF WITH SERVICEABLE FLOOR PANEL ON SHELF I.A.W REFERENCE TO AIPC 53-21-51-75 PG 14 SHEET 01 ITEM A;[02] INFO ONLY: PANEL 221BF WAS REPLACED ON #TTG8Q00Y4M8W & INSTALLED ON #TTSDR SWAA2025021985682Floor Panel · corroded(A204 DOT 93) FLOOR PANEL 221BF HAS 8EA FASTNER INSERTS WITH CORROSION; MARKED IN RED.<[01] REPLACED FLOOR PANEL 221BF WITH SERVICEABLE FLOOR PANEL ON SHELF I.A.W REFERENCE TO AIPC 53-21-51-75 PG 14 SHEET 01 ITEM A;[02] INFO ONLY: PANEL 221BF WAS REPLACED ON #SDR SWAA2025021985681Floor Panel · pulledFLOOR PANEL 231UF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.SDR SWAA2025021985671Floor Panel · pulled(A204 DOT 97) FLOOR PANEL 231KF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/WSDR SWAA2025021985680Floor Panel · debonded(A204 DOT 98) FLOOR PANEL 231KF; AFT LH CORNER OF FLOOR PANEL IS DISBONDED.<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/WSDR SWAA2025021985670Floor Panel · pulled(A204 DOT 99) FLOOR PANEL 231GF; UPPER FACE SHEET HAS MISSING FIBERS.<[01] 'REFER TO FAULT TTG8Q00Y4M65 WHERE EA 25-153-00105 WAS ADDED AS A SUBTASK.';[02] VERIFIED ITEM 1<BR>C/W;[03] C/WSDR SWAA2025021985668Floor Panel · pulled(A204 DOT 101) FLOOR PANEL 231DF; UPPER SURFACE FACE SHEET MISSING FIBERS.<[01] C/W EA 25-153-00105. VERIFIED ALL STEPS COMPLETE.;[02] VERIFIED C/W;[03] C/WSDR SWAA2025021985679Handle · out of adjust(A204 DOT 86) RH EMERGENCY EXIT DOOR 843 PULL CLOSE HANDLE RECESS HAS 2EA MISSING QUARTER TURN STUDS.<[01] REPLACED MISSING QUARTER TURN STUDS IN HANDLE RECESS ON DOOR 843 I/A/W 52-22-51-400-801 .;[02] VERIFIED STEP 1<BR>AUDIT C/WSDR SWAA2025022085662Winglet · corrodedDOT#42 A-043 RH WINGLET HAS CORROSION ON LOWER OTBD T/E 18' FROM BOTTOM EDGE<[01] 04 - REPAIRED PER [SRM 57-30-01-1A-2-APB-AP37.1-0632-A01611 (PERMANENT (NON-DENT DAMAGE TYPES)-WINGLETS)];[02] VERIFIED STEP 1<BR>AUDIT CWSDR SWAA2025022085661Winglet · corrodedDOT#43 A-043 RH WINGLET HAS CORROSION ON UPPER INBD T/E 42' FROM BOTTOM EDGE<[01] 04 - REPAIRED PER [SRM 51-10-02-0G-0-A00248 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - AIRFRAME - PERMANENT)] AND IAW APB 57-30-01 FIGURE 102 (D);[02] 04 - REPAIRED PER [SRM 5SDR SWAA2025021985451Receiver · crackedDOT#38 A-043 FWD CARGO COMPARTMENT AFT BKHD UPPER STAINTION RAIL CAMLOCK RECIVER CRACKED STA 500D LBL 39 WL 193<[01] REMOVED AND REPLACED CAMLOCK AT AFT BULKHEAD UPPER RAIL IAW SRM 51-40-02-0G-0;[02] VERIFIED ITEM 1<BR>AUDIT C/WSDR SWAA2025021985667Sidewall Support · corroded154-86 AFT CARGO COMPARTMENT STA 907 STR 24R+4 SIDEWALL PANEL SUPPORT CORRODED NEAR THE FASTENER HOLE<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]<BR> BOEING DWG 147A9409 ID:SDR SWAA2025022085126Seal · cracked(DOT 152-1) LEFT HORIZONTAL STABILIZER GAP COVER 333AB; SLIDING SEAL IS CRACKED.<[01] REMOVE AND REPLACED LEFT HORIZONTAL STABILIZER GAP COVER 333AB; SLIDING SEAL I.A.W SRM STEP 4.<BR>ISSUE TAG WN49657;[02] REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER GAP CSDR SWAA2025022085127Seal · cracked(DOT 152-2) LEFT HORIZONTAL STABILIZER PANEL 333AB; SLIDING SEAL SUPPORT BRACKET IS CRACKED.<[01] REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER PANEL 333AB; SLIDING SEAL I.A.W SRM 51-40-02-0G<BR>ISSUE TAG WN49657;[02] VERIFIED TASK COMPLETE<BR><BR>AUDIT C/WSDR SWAA2025021984885Floor Panel · corrodedDOT#27 A-043 FLIGHT COMPARTMENT FLOOR PANEL 211AF HAS CORROSION ON BOTTOM FWD EDGE STA 259.5 BL 0 WL 208<[01] REPLACED IAW SRM 51-40-02-0G-0 & BOEING DWG: 141A631 REV: B<BR>ATAG: WN 49596<BR>P/N: 141A5133U15ATSMR0;[02] FAULT RESOLVED ON OTHER FAULT. SEE FAULT SDR SWAA2025022084619Frame · crackedMAIN CABIN STA 440 FRAME HAS EVIDENCE OF CRACK AROUND FASTENER OF RAIL SUPPORT BRACKET I/B OF STR 8 L/H. REMOVED DAMAGE AND REPAIRED FRAME AT STA 440 S-8L IAW EA 25-153-00218.SDR SWAA2025022084621Frame · crackedMAIN CABIN STA 380 FRAME HAS EVIDENCE OF CRACK AROUND FASTENER OF RAIL SUPPORT BRACKET I/B OF STR 8 L/H. REPAIRED PER EA 25-153-00153 TTG8Q00YDMJL;[02] REPAIRED FRAME AT BS380; BETWEEN S-7L AND S-8L; IAW EA 25-153-00153.SDR SWAA2025022084618Frame · cracked(DOT#147-48) MAIN CABIN STA 400 FRAME HAS EVIDENCE OF CRACK AROUND FASTENER OF RAIL SUPPORT BRACKET I/B OF STR 8 L/H<[01] REPAIRED FRAME AT BS400; BETWEEN S-7L AND S-8L; IAW EA 25-153-00154.;[02] VERIFIED ITEM 1<BR>C/W;[03] C/WSDR SWAA2025022084613Crease Beam · corrodedCABIN FWD WET AREA R1 CREASE BEAM CRRODED AT STA 312+15' LBL 60 WL 208<[01] REMOVED DAMAGE FROM CABIN FWD WET AREA R1 CREASE BEAM CORRODED AT STA 312+15' LBL 60 WL 208; FOUND IT OUT OF LIMITS ; ORIG T . ADJACENT TO BLEND .085'; LOSS .017'; REMOVED DAMAGED PARTSDR SWAA2025021984610Floor Panel · corrodedDOT L7-010: AFT CARGO COMPARTMENT FLOOR PANEL 140AF IS CORRODED AT FASTENER HOLES<[01] EVALUATED CORROSION ON AFT CARGO COMPARTMENT FLOOR PANEL 140AF; FOUND TOTAL ACCUMULATED CORROSION DAMAGE TO BE MORE THAN THE 20IN ALLOWED; OUT OF LIMITS IAW SRM 53-00-53-1A-SDR SWAA2025021984611Floor Panel · corrodedDOT L7-012: AFT CARGO COMPARTMENT FLOOR PANEL 140CF IS CORRODED AT FASTENER HOLES<[01] VERIFIED LIMITS ON AFT CARGO COMPARTMENT FLOOR PANEL 140CF; DISTANCE BETWEEN DAMAGE IS 2' (MINIMUM ALLOWABLE DISTANCE BETWEEN DAMAGE IS 5') THEREFORE IS FOUND OUT OF THE LIMSDR SWAA2025022083950Angle · buckled(A204 DOT 73) FORWARD CARGO STA 500 TO 500A; STR 26L; BAFFLE PLATE UNDER Z-ANGLE IS BUCKLED ON FORWARD SIDE.<[01] REMOVED AND INSTALLED NEW RIVETS AT FORWARD CARGO STA 500 TO 500A STR 26L BAFFLE PLATE UNDER Z ANGLE I/A/W SRM 51-40-02-0G-0;[02] VERIFIED STEP 1;SDR SWAA2025021983951Shield · corroded(A204 DOT 78) FWD CARGO STA 492; RBL 21; WL 155; SPLASH SHIELD HAS CORROSION ON UPPER SURFACE<[01] REMOVED CORROSION AND VERIFIED WITH A 10-POWER MAGNIFYING GLASS ON FWD CARGO STA 492; RBL 21; WL 155; SPLASH SHIELD UPPER SURFACE I.A.W SRM 51-10-02-0G-0 VERIFIESDR SWAA2025021984185Floor Panel · corrodedFWD CARGO FLOOR PANEL 120CF HAS CORROSION AT FASTENER HOLES<[01] UPON FURTHER INVESTIGATION FOUND THAT CORROSION WAS 30 INCHES IN LENGTH WITH A MAX ALLOWED LENGTH OF 3 INCHES FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1; RECEIVED REPLACEMENT MATERIAL PN 202SDR SWAA2025022083595Rib · cracked(A204 DOT 64) LH HORIZONTAL STAB LEADING EDGE 331B; LE STA 114.5; RIB IS CRACKED NEXT TO BEND RADIUS AT LOWER AFT HOLE.<[01] REMOVED L/H L/E HORZ STAB RIB AT STA114.5 IAW SRM 51-40-02-0G-0 AND DWG 186A1305 REV - VERIFIED PART USING P/N 186A1352-9 AND ATAG WN49SDR SWAA2025022083596Rib · buckledLH HORIZONTAL STAB LEADING EDGE 331B; LE STA 198.25; RIB IS BUCKLED AT AFT RADIUS.<[01] REMOVED L/H HORZ STAB L/E 331B RIB IAW SRM 51-40-02-0G-0 AND DWG 186A1001 REV A VERIFIED PART USING P/N 654A0004-685 ATAG A285988 AND DWG 186A1001 REV A INSTALLED RIB IAW S
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