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 SWAA2022053105997Scuff Plate · crackedAFT CARGO BAY; FWD CORNER SCUFF PLATE IS CRACKED / WELDED CRACK ON FLANGE OF AFT CARGO BAY FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-60-15-2R-1 PARA 4.B. (2) AND (4) WELDING MACHINE CALIBRATION ID: E10583; DUE DATE 12/2022;[02] VESDR SWAA2022053105996Skin · crackedLH HORIZONTAL STAB; LWR STAB SKIN CRACKED AT STAB STA 193.90; CUTOUT LOWER HORIZONTAL SKIN OF L/H HORIZONTAL STAB PER SRM 55-10-01-2R-11 STEP 4 (B) 2. AND DRILLED OUT EXISTING FASTENERS IN REPAIR AREA PER STEP 4 (F) 1. FABRICATED REPAIR DOUBLER PER SRM 55-10-0SDR SWAA2022051205555Smoke Detector · no testAFT LAV SMOKE DETECTOR WILL NOT TEST / [01] REMOVED AND REPLACED AFT LAV SMOKE DETECTOR. TEST RESULTS PASS AT THIS TIME. REF AMM. 26-14-01. -END-SDR SWAA2022053105507Vapor Barrier · crackedL/H VAPOR BARRIER DOUBLER (111A1511-27) LBL 6-31; BS 663 HAS A CRACK. (MARKED) / [01] FABRICATED DOUBLER FROM 2024-0 #0.040 LOT 1313418-1 IAW DWG 11A1511-27 REV.-A AND DWG 111A1000 REV:A;[02] VERIFIED CORRECTIVE ACTION 1.;[03] RECIVED DOUBLER ON CUSTOMER RO NOSDR SWAA2022051005171Battery Pack · inoperativeCUSTOMER WALK: LH OVER WING EMERGENCY EXIT LIGHTS TOP AND FWD. BOTTOM SIGNS WILL NOT ILLUMINATE. / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACK M1668 AS PER REF B737 AMM 33-51-01-960-801. TEST OK.;[02] VERIFIED STEP 1.SDR SWAA2022051005173Light · inoperativeCUSTOMER WALK: LT WING OVER WING EMERGENCY EXIT LIGHT INOP / [01] RELAMPED LT WING EMERGENCY EXIT LIGHT AS PER REF B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP 1.SDR SWAA2022053105038Support · crackedFLOOR SUPPORT CRACKED AT STA 540+1; WL 208; RBL1. / [01] COMPLETED STEP 1;<BR>REMOVED AND REPLACED CRACKED FLOOR SUPPORT AT BS 540+1 WL20 AND MATCHED DRILLED FLOOR BOARD HOLES IAW BOEING DWG 143A0060 AND SRM 51-40-02 AND SRM 51-40-05.;[02] VERIFIED;[03] VERIFISDR SWAA2022053105039Support · crackedFLOOR SUPPORT CRACKED AT STA 540+1; WL 208; LBL1. / [01] REMOVED AND REPLACED FLOOR SUPPORT AT STA 540+1 WL 208 LBL 1 IAW SRM 51-40-02 AND BOEING DWG 143A0060;[02] EDITED FOR PROPER SIGN OFF REQUIREMENT.;[03] VERIFIED;[04] PICKED UP HOLES COMMON TO FLOOR PANELSDR SWAA2022051004958Battery Pack · inoperativePASSENGER CABIN EMERGENCY EXIT SIGNS AT L2 AND R2 DOORS INOP. / [01] PERFORMED CHARGE OF THE BATTERY PACKS M1672 ; M1673 AND PERFORMED OPERATIONAL TEST ;TEST PASS. REF. TO B 737 AMM 35-51-06-610-602; AMM 33-51-00-710-801.;[02] VERIFIED OP CHECK OK.SDR SWAA2022051006053Battery Pack · inoperativePASSENGER CABIN EMERGENCY EXIT SIGNS AT L2 AND R2 DOORS INOP. / [01] PERFORMED CHARGE OF THE BATTERY PACKS M1672 ; M1673 AND PERFORMED OPERATIONAL TEST ;TEST PASS. REF. TO B 737 AMM 35-51-06-610-602; AMM 33-51-00-710-801.;[02] VERIFIED OP CHECK OK.SDR SWAA2022051004959Light · inoperativePASSENGER CABIN EMERGENCY OVERHEAD BIN LIGHTS INOP AT POSITIONS 16R/H; 18R/H AND 19L/H. / [01] PERFORMED CHARGE OF THE BATTERY PACKS M1672; M1673; AND PERFORMED OPERATIONAL TEST; TEST PASS. REF. TO B737 AMM 33-51-06-610-802 AND AMM 33-51-00-710-801.;[02] VERIFSDR SWAA2022053104837Frame · crackedCRACK IN RADIUS OF FRAME AT B.S. 312 JUST ABOVE FORWARD ENTRY DOOR CUT OUT. / [01] TRIMMED OUT DAMAGE AT STA 312 FRAME LBL32 WL282 IAW SRM 51-10-02-0G-0;[02] SRM 53-10-15-1A-1 IS APPLICABLE FOR ALLOWABLE DAMAGE.;[03] TRIMMED .250 FROM EDGE OF FRAME. FOUND TO BSDR SWAA2022053103655Bulkhead · crackedCRACKED LOWER L/H COMPOSITE BULKHEAD AT BS663 LBL32 WL156. IDENTIFIED LOWER L/H COMPOSITE BULKHEAD AT BS663 LBL32 WL156 IAW SRM 57-10-10-0I-2 FIGURE 2; SHEET 1; TABLE 2; ITEM 4.DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PAR 4D(1).REPASDR SWAA2022053103657Bulkhead · crackedCRACKED LOWER R/H COMPOSITE BULKHEAD AT BS663 RBL34 WL158.DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PAR 4D(1).REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-04-2R-10 PER SRM 57-10-10-2R-2 PAR 1C.STARTED DAMAGE REMOVAL ON BOTH FWD AND AFT FASDR SWAA2022051100169Container · elongatedFWD SERVICE DOOR SLIDE CONTAINER FWD MOUNTING BRACKET HAS HOLE ELONGATED. / [01] REMOVED AND REPLACED FWD SERVICE DOOR SLIDE CONTAINER AND ACCOMPLISHED LATCH RELEASE TEST ; TEST PASSED SCALE B/C 161549 REF B 737-700 AMM 25-66-01-400-804;[02] VERIFIED STEP 1SDR SWAA2022051097543Gusset · crackedFWD CARGO COMP. L/H SIDE STR 19L BETW. STA 500C THRU 500D GUSSET CRACKED / [01] REMOVED GUSSET FROM FWD CARGO STA 500C-500D STR 19L PER B737-700 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW GUSSET PER B737-700 SRM 51-10-02-0G-0.;[03] VERIFIED STEP #1.;[04] SDR SWAA2022051097544Gusset · crackedFWD CARGO COMP. R/H SIDE STR 19R BETW. STA 500C THRU 500D GUSSET CRACKED / [01] REMOVED CRACKED GUSSET FROM FWD CARGO STA 500C-500D STR 19R PER B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED;[03] LOCATED AND DRILLED NEW GUSSET PER B737-700 SRM 51-10-02-0G-0.;[04] VSDR SWAA2022051197300Rib · crackedLH HORIZONTAL STABILIZER LE ACCESS PANEL RIB CRACK AT LE STA 300.51 / [01] PERFORMED HFEC INSP ON LH HORIZONTAL STAB L/E ACCESS PNL RIB AT L/E STA 300.51 IAW B737 NDT P6 51-00-00 PROC.23; CRACK NOTED LENGTH 0.600'<BR>TOOL USED : NORTEC 600 B/C 166317 10/22;[02SDR SWAA2022051097301Shield · corrodedFWD CARGO COMP.R/H SIDE SHIELD BETWEEN STA 500 THRU 500AHAS CORROSION / [01] REMOVED CORROSION AT FWD CARGO AFT SHIELD BETW. STA 500 THRU 500A R/H SIDE PEER B737-700 SRM 51-10-02-0G-0 (WORKED BY HUMBERTO MEDINA 26340);[02] VERIFIED STEP 1.;[03] PERFORMED UT THSDR SWAA2022042797397Battery Pack · defectiveEMERGENCY LIGHTS INOP AT POSITIONS: 6 ABC; 8 DEF; 9 ABC; 12 ABC; 12 DEF AND R2 DOOR; UPPER EMERGENCY EXIT LIGHT. / [01] DURING TROUBLESHOOTING FOUND BATTERY PACK POS. M2335 DEFECTIVE AS PER REF. B737 AMM 33-51-00-710-801.;[02] REMOVED AND REPLACED EMERGENCY BASDR SWAA2022042696625Light · inoperativeEMERGENCY LIGHT ON ROW 18DEF IS INOP / [01] RELAMPED EMERGENCY LIGHT ON ROW 18DEF IAW AMM 33-51-03. OPS CHECK GOOD.SDR SWAA2022051196385Rib · crackedRIGHT HORIZONTAL STAB. RIB # 4 AT FWD LOWER CORNER CRACK. / [01] PERFORMED HFEC INSP ON RT HORIZ STAB RIB#4 FWD LWR CORNER IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED (CRACK LENGTH 0.625') <BR>TOOL USED : NORTEC 600 B/C 166317 CALDUE: 10/22;[02] REMOVED SDR SWAA2022051196236Rib · crackedFOUND RIB #8 P/N 174A1008-2 OF DORSAL FIN ASSEMBLY CRACKED / [01] REMOVED RIB AT DORSAL FIN AS PER REF B737-700 SRM 51-40-02-0G-0. PERFORMED BY RS # 35463;[02] LOCATED AND DRILLED NEW RIB AS PER REF B737-700 SRM 51-10-05-0G-0. PERFORMED BY RS # 35463;[03] VERISDR SWAA2022051195849Channel · corrodedAFT CARGO COMPARTMENT LH Z CHANNEL FROM STA 727 TO STA 874 HAS SEVERAL CORROSION. CORRERCTION. AFT CARGO COMPARTMENT LH CHANNEL FROM STA 727 TO STA 847 HAS SEVERAL CORROSION. / [01] REMOVED CORROSION AT AFT CARGO COMP. L/H SIDE 'Z' CHANNEL FROM STA 727 TO STA SDR SWAA2022051095848Strip · corrodedAFT CARGO COMPARTMENT;CAP STRIP PLATE AT FWD POSITION OF AFT CARGO DOOR STA 794 ;S25R HAS CORROSION AND DEEP GOUGE. / [01] REMOVED CORROSION AT AFT CARGO COMPT. CAP STRIP AT FWD POSITION.PER B 737-700 SRM 51-20-01-0G-0. FOUND OUT OF LIMITS.MORE THAN 50 % OF MASDR SWAA2022051095850Channel · corrodedAFT CARGO COMPARTMENT RH Z CHANNEL FROM STA 727 TO STA 767 HAS SEVERAL SPOTS OF CORROSION. / [01] REMOVED CORROSION AT AFT CARGO COMP. R/H SIDE 'Z' CHANNEL FROM STA 727 TO STA 767 PER B737-700 SRM 51-10-02-0G-0 (WORKED BY HUMBERTO MEDINA);[02] VERIFIED STEP 1.SDR SWAA2022051095851Shield · corrodedAFT CARGO COMPARTMENT FWD WEB SHIELD FROM STA 767 TO STA 794 HAS SPOTS OF CORROSION. / [01] REMOVED CORROSION AT AFT CARGO COMP. FWD WEB SHIELD FROM STA 767 TO STA 794 PER B737-700 SRM 51-10-02-0G-0 (WORKED BY HUMBERTO MEDINA);[02] VERIFIED STEP 1.;[03] PERFORSDR SWAA2022051195274Angle · crackedCRACK FOUND ON FRAME AT STA 312 ABOVE L1 DOOR CUTOUT. / [01] CONFIRMED CRACK AT STA 312 FRAME ABOVE L1 DOOR CUTOUT IAW NDTM PART 6;51-00-00 PROCEDURE 23.<BR>CRACK LENGTH : 0.315';11] FABRICATED ANGLE AT REPAIR AREA AS PER REF B737-700 SRM 53-10-07-2R-1. MATERISDR SWAA2022051195449Web · out of positionFORWARD CARGO COMPARTMENT DOOR CUT-OUT THRESHOLD HAS SPOTS OF CORROSION BETWEEN STA.440 AND STA.500 RBL27 TO RBL29. / [01] REMOVED CORROSION AT FWD CARGO COMP. DOOR CUTOUT THRESHOLD BETW. STA 440 THRU STA 500 RBL 27 THRU RBL29 (WORKED BY HERNANDEZ MEDINA #2634SDR SWAA2022051095273Door Frame · crackedCRACK FOUND ON FRAME AT STA 328 ABOVE L1 DOOR CUTOUT. / [01] CONFIRMED CRACK AT STA 328 FRAME ABOVE L1 DOOR CUTOUT IAW NDTM PART 6;51-00-00 PROCEDURE 23.<BR>CRACK LENGTH : 0.157';[02] TRIMMED OUT FRAME INNER CHORD TO REMOVE DAMAGE AT STA 328 BETWEEN S-5L AND SSDR SWAA2022051095452Drip Tray · crackedE&E COMPARTMENT DRIPSHIELD P/N 284A2830-1 IS CRACKED / [01] REMOVED/REPLACED DRIPSHIELD (SHROUD ASSY ) IN REF SOPM 20-50-01;[02] VERIFIED STEP 1.SDR SWAA2022041994985Light · inoperativeEMERGENCY LIGHTS POWER SUPPLY M1673 WILL NOT POWER LIGHTS OR TAKE A CHARGE. / [01] REMOVED & REPLACED EMERGENCY LIGHTS POWER SUPPLY M1673 PER AMM 33-51-06.SDR SWAA2022041994987Light · inoperativeLH OVERWING EMERGENCY EXIT SIGN HAS TWO BULBS INOP. / [01] RELAMPED LH OVERWING EMERGENCY EXIT SIGN PER AMM 33-51-01.SDR SWAA2022051194870Stiffener · crackedRH HORIZONTAL STABILIZER RIB #4 STIFFENER 2 CRACK. / [01] REMOVED DAMAGE AT RH HORIZONTAL STAB. RIB #4 ; STIFFENER #2 S PER REF B737-700 SRM 55-10-09-2R-4 FIGURE 202;[17] INSTALLED REPAIR PARTS AT RH HORIZONTAL STAB. RIB # 4 STIFFENER #2 AS PER REF B737-700 55SDR SWAA2022051194219Pressure Web · crackedCRACK FOUND AT MAIN WHEEL WELL VERTICAL PRESSURE WEB BETWEEN RBL40.00 AND RBL 45.64 IAW NDTM PART 6;51-00-00 PROCEDURE 23. CRACK LENGTH :0.843'. CRACK FOUND AT MAIN WHEEL WELL VERTICAL PRESSURE WEB BETWEEN RBL40.00 AND RBL 45.64 IAW NDTM PART 651-00-00 PROCEDUSDR SWAA2022041893843Lanyard · missingLEFT OVER WING EXIT DOOR ASSIST LANYARD COVER MISSING VELCRO. / [01] REMOVED AND REPLACED VELCRO PER SIP;[02] C/W INSPECTION.SDR SWAA2022041492958Battery Pack · inoperativeL1 EMERGENCY LIGHTS INOP BOTH INSIDE AND OUTSIDE / [01] R&R FWD EMERGENCY LIGHTS BATTERY PACK; OPS CHECK GOOD REF AMM 33-51-06SDR SWAA2022042791212Scuff Plate · crackedFWD CARGO DOOR AFT SCUFF PLATE CORNER WITH A CRACK. / [01] ACCOMPLISHED WELD REPAIR AT FWD CARGO DOOR AFT SCUFF PLATE AS PER SRM 53-3015-1A-2. SCUFF PLATE WILL BE INSTALL ON (TTG8Q003E4Z5).SDR SWAA2022022275541Handle · looseL2 DOOR LINER ASSIST HANDLE LOOSE / [01] TIGHTEN UP LOOSE L2 DOOR ASSIST HANDLE I.A.W. AMM 52-13=31-400-802;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.SDR SWAA2022022273031Flange · crackedGROUND POWER RECEPTACLE LOWER FLANGE IS CRACKED AT FORWARD FASTENER. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-5 FIG-102 ZONE B. REMOVED DAMAGE AREA IAW SRM 53-10-15-2R-4 STEP 4( A;B & C). HFEC INSPECTED TRIMMED EDGE IAW NDT PART 6 51-00-00 PROCEDURSDR SWAA2022022272123Light · inoperativeLEFT HAND OVER WING EMERGENCY LIGHT INOP. / [01] RELAMPED WINDOW LIGHT AT L/H OVERWING EMERGENCY EXIT AND PERFORMED INSTALLATION TEST PER AMM 33-21-00-960-801; LIGHT IS DIM AND DOES NOT CHANGE WITH SWITCH SETTINGS;[02] CORRECTION FOR ITEM 1; PERFORMED GOOD OPESDR SWAA2022022272124Light · inoperativeFWD SERVICE DOOR EMERGENCY SLIDE LIGHT IS INOP. / [01] REMOVED AND REPLACED SLIDE LIGHT BULB AND PERFORMED GOOD OP CHECK AS PER AMM 33-51-04-960-801. NO OTHER FAULTS NOTED.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.SDR SWAA2022022367099Skin · corrodedCORROSION ON FUSELAGE EXTERNAL SKIN AT BS 1088 AND S-24L / [01] REMOVED DECORATIVE EXTERIOR PAINT AT DISCREPANCY AREA TO FOM PER AMM 51-21-11ICKNESS 0.080' [REF SRM 53-80-01-0I-1 FIG 9;12] REMAINING 0.076'. DAMAGE OUT OF LIMITS DUE TO MATERIAL REMOVAL IS NOT PSDR SWAA2022022367097Skin · corrodedCORROSION ON EXTERNAL SKIN AT BS 1085 AND S-26R FWD SIDE OF JACK POINT C. REMOVED CORROSION ON SKIN. L=3.5' X W=3.2' PER SRM 53-00-01-1A-1 PARARGRAPH 2.E. ACCOMPLISHED HFEC INSPECTION OF EXISTING HOLES AND COUNTERSINKS NO CRACK NOTED IAW 737 NDTM PART 6; 51SDR SWAA2022022367098Skin · corrodedCORROSION ON FUSELAGE EXTERNAL SKIN FWD EDGE BUTT JOINT BS1016 AND STR 21L / [01] REMOVED DECORATIVE EXTERIOR PAINT AT DISCREPANCY AREA TO FOM PER AMM 51-21-11;[10] EVALUATED DAMAGE ON FUSELAGE SKIN L=5.7'; W=2.0'; D=0.011'. ORIGINAL THICKNESS 0.071' [REF SRM SDR SWAA2022022267100Intercostal · crackedDAMAGED INTERCOSTAL AT BS500-500A STR 25 LBL25 / [01] REMOVED INTERCOSTAL CRACKED FCB AT BS500 TO BS500A S-25L LBL25 IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW FCB INTERCOSTAL AT BS 500 - 500A STR 25L ; LBL 25 IAW SRM 51-40-05 AND DWG # 143A7510 ; OK TSDR SWAA2022022366939Bulkhead · crackedBS 663 LOWER BULKHEAD IS CRACKED AT R.B.L. 50 W.L. 158. DAMAGE OUT OF LIMITS IAW SRM 57-10-10-1A-2 PARA 4.D. REMOVED AN APPROXIMATE 13'X.01' LENGTH OF CRACK DAMAGE FROM AN AREA LOCATED 46.5' FROM THE IN BOARD EDGE AND 5.5' FROM UPPER EDGE IAW SRM 51-70-04-2SDR SWAA2022022266579Floor Support · crackedCRACKED TRANSITION LINK BS 520 TO 540 BL 0 WL 208.1 / [01] REMOVED CRACKED TRANSITION LINK FROM BS 520 T0 BS 540 BL 0 WL 208.1 IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED PASSENGER CABIN FLOOR SUPPORT P/N 143A5595-21 LOT#1481259-1 AT BS 520 TO BS 540; BL 0 SDR SWAA2022022366577Skin · crackedON ACCOMPLISHING INSPECTION ON CCN:5510-I-15029-NG#1; FOUND 1 INCH CRACK AT HORIZONTAL STAB LOWER IN-SPAR SKIN AT HSS 193.90 RIB, 16" FROM REAR SPAR. REMOVED THE DAMAGED PART IAW SRM 51-40-02. HFEC INSPECTED CUT OUT IAW 737 NDTM PART 6 51-00-00 PROCEDURE 2SDR SWAA2022022266573Beam · crackedUPON ACCOMPLISHING INSPECTION OF CCN:5241-I-14079-NG; FOUND 1 INCH CRACK OF #4 BEAM COMMON TO THE FORWARD SERVICE DOOR. / [01] FSD #4 BEAM WAS REMOVED AND REPLACED ON WORK ORDER: 546753 PER SRM 51-40-02-0G-0 PARA 4; 7 AND BOEING DWG: 141A6516.;[02] VERIFIED CO
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