Boeing 737-76N
Service difficulty reports · 4,807
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '73776N' 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 aircraft_model_key = '73776N' 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 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 SWAA2025020392062Girt Bar · brokenAFT SERVICE DOOR SLIDE BAR HOLDER NUT PLATE BROKEN.<[01] INSTALLED NEW NUT PLATE; @0530 REQUIRES CURE TIME OF 1 HOUR.;[02] NUT PLATE IS FULLY INSTALLED IAW SRM 51-40-10.SDR SWAA2025020392309Lamp · inoperativeLEFT O/W EXIT SIGN LIGHT INOP<[01] OK TO CONTINUE PER. MEL 33-2-03. SP1B AUTHORIZATION #235312. ALL EMERGENCY LIGHTS AND SIGN ILLIUNNATE ON LH OVERWING DOOR. FOUND SIDEWALL LIGHT UNDERNEATH EXIT SIGN TO BE INOP.; [02] REMOVED AND REPLACED L/H O/W EXIT SIGN LIGSDR SWAA2025021991720Stiffener · corrodedCORROSION ON STIFFENER AT MID CABIN BS692 RBL64 WL203. MARKED<[01] THIS CARD WILL BE ACCOMPLISHED ON CARD NBR TTG8Q00YEMTL;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2025022091296Skin · crackedCRACK FOUND ON LH HORIZONTAL STABILIZER LOWER SKIN AT STA193.90; 17.5' FROM FWD EDGE; L: 0.6' MARKED<[01] REPAIRED LH HORIZONTAL STABILIZER LOWER SKIN AT STA193.90; 17.5' IAW SRM 55-10-01-2R-11 REPAIR 11.;[02] VERIFIED RII ITEMS ARE COMPLETESDR SWAA2025021991051Floor Panel · pulledFLOOR PANEL 231XF HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 231XF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025021991052Floor Panel · pulledFLOOR PANEL 241DF HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241DF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025021991053Floor Panel · pulledFLOOR PANEL 241AF HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025021991281Web · corrodedCORROSION ON SUBTHRESHOLD WEB AT ACB BS807 - BS847 RBL28 WL160. MARKED<[01] REMOVED AND REPLACED SUBTHRESHOLD WEB IAW SRM 51-40-02 AND DWG 146A8340 ID:0028 REV: -.SDR SWAA2025021991297Strap · corrodedCORROSION ON STRAP AT MID CABIN BS692 RBL65 WL203. MARKED<[01] REMOVED AND REPLACED NEW INNER CHORD IAW SRM 51-40-02 & DWG 144A5900;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2025021991298Floor Panel · crackedCRACKED PANEL BREAK AT MID CABIN BS540 LBL1 WL208.<[01] REMOVED AND REPLACED NEW PANEL BREAK AT MID CABIN BS540 LBL1 TO LBL24 IAW SRM 51-40-02 AND DWG 143A0060 ID:0002 REV: B.<BR>APPLIED TO CIC ON DISCREPANCY AREA IAW AMM 51-21-91-620-802.<BR>CLOSED FLOOR PANESDR SWAA2025021990520Stiffener · crackedLEFT HAND HORIZONTAL STABILIZER #3 INSPAR RIB; AT STABILIZER STATION 111.10; 4TH VERTICAL STIFFENER IS CRACKED.<[01] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 111.10 RIB 4TH VERTICAL STIFFENER AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4;[02SDR SWAA2025021990521Stiffener · crackedRIGHT HAND HORIZONTAL STABILIZER #3 INSPAR RIB; AT STABILIZER STATION 111.10; 4TH VERTICAL STIFFENER IS CRACKED.<[01] REMOVED THE DAMAGED PART AT RH HORIZONTAL STABILIZER STA 111.10 RIB 4TH VERTICAL STIFFENER AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4;[0SDR SWAA2025021990370Connector · brokenBROKEN CONNECTOR AT FSD EXIT INDICATOR LIGHT; WIRE LABEL W4142 D03658 M/W L01186<[01] REPLACED CONNECTOR D03658 PER SWPM 20-30-12 AND WM 33-51-21.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2025021997681Wire · brokenBROKEN CONNECTOR AT FSD EXIT INDICATOR LIGHT; WIRE LABEL W4142 D03658 M/W L01186<[01] REPLACED CONNECTOR D03658 PER SWPM 20-30-12 AND WM 33-51-21.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.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;
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