Boeing 737-7CT
Service difficulty reports · 2,413
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 = '7377CT' 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 = '7377CT' 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 SWAA2025042320085Pressure Deck · crackedCRACKED HORIZONTAL PRESSURE DECK ABOVE MLG WHEEL WELL BS664 RBL41 WL203. <[01] REMOVED FASTENERS COMMON TO REPAIR AREA AND CUT AND REMOVED THE DAMAGE PART OF THE WEB PER SRM 53-40-51-2R-2 PAR. 4. C. FIG. 202. INSTALLED REPAIR PARTS AND APPLIED CIC PER SRM 53-SDR SWAA2025043055740Nut · deterioratedDETERIORATED ENTRY DOOR ASSIST HANDLE NUT FWD AND LOWER POSITION AT FWD GALLEY AREA (4 EA) 2025-237983<[01] REPLACED ENTRY DOOR ASSIST HANDLE NUT FWD AND LOWER POSITION AT FWD GALLEY AREA (4 EA) IAW SOPM 20-50-01 REV NO. 38;[02] CERTIFIED WORK PERFORMEDSDR SWAA2025043055745Doubler · corrodedDOUBLER BTW BS 400 TO BS 420 BETWEEN S-1 AND S-2L REQUIRES REMOVAL AND REPAIR. 2025-237993<[01] TOOL USED ON STEP 3: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 200048001; DUE DATE: 28-MAY-25;[02] PERFORMED REPAIR CATEGORY B IAW EA 25-153-00902. SEE INDIVIDUSDR SWAA2025033119511Cover · detachedFO OVERWING EXIT HANDLE COVER FELL OFF<[01] INSTALLED PER SIPSDR SWAA2025033119092Seat · inoperativeCABIN SEAT RECLINE IN EMERGENCY EXIT ROW NEEDS TO BE INOP AT 11D<[01] LOCKED OUT HYDRAULIC AT SEAT 11D IAW AMM 25-22-00.SDR SWAA2025032709804Light · inoperativeINOP EXTERNAL OVER WING EMERGENCY LIGHT LT 2025-186221<[01] REPLACED OVER WING EMERGENCY LIGHT ON LT IAW B737-700 AMM 33-51-04-960-801 STEP 2.F (3) (B) AND 2.F (4);[02] COMPLETED; TEST OKSDR SWAA2025031704784Battery Pack · failedR/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. <[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.SDR SWAA2025031704783Battery Pack · failedL/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. <[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.SDR SWAA2025031304356Seat Back · out of adjustSEATS RECLINING AT EMERGENCY EXIT ROW 12D; 12F. ADJUSTED 12D; 12F SEAT RECLINE REF AMM 25-22-00SDR SWAA2025040203135Scuff Plate · crackedCRACK AFT CORNER SCUFF PLATE AT AFT CARGO 2025-186142 <[01]. TOOL USED DIGITAL CALIPER P/N: 500-193-30; S/N: 0000293; DUE DATE: 01-NOV-25.; [02] TOOL USED RADIOMETER/ PHOTOMETER KIT P/N: XRP-3000; S/N :1753759 ; DUE DATE : 30/JUN/25; [03] REPAIRED AFT CORNER SDR SWAA2025040203457Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED TRAILING EDGE IRSS213 AT LT WING 2025-186156<[01] REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE IRSS213 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG115A2001 SHEET 24 REV A MEASURE OF CRAK IS: 0.609.SDR SWAA2025040203343Plate · crackedCRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING 2025-186146<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02. AND DWG 115A2001 SHEET 29 REV -. <BR>MEASURE OF CRACK L:SDR SWAA2025033115240Plate · crackedCRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT LT WING 2025-186155<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02. AND DWG 115A2001 SHEET 29 REV -.<BR>MEASURE OF CRACK L: 0.346SDR SWAA2025033115241Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED TRAILING EDGE IRSS213 AT LT WING 2025-186156<[01] REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE IRSS213 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG115A2001 SHEET 24 REV A MEASURE OF CRAK IS: 0.609 P/N: 500-19SDR SWAA2025033115239Plate · crackedCRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING 2025-186146<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02. AND DWG 115A2001 SHEET 29 REV -. <BR>MEASURE OF CRACK L:SDR SWAA2025032815236Scuff Plate · crackedCRACK AFT CORNER SCUFF PLATE AT AFT CARGO 2025-186142 <[01]. TOOL USED DIGITAL CALIPER P/N: 500-193-30; S/N: 0000293; DUE DATE: 01-NOV-25.; [02] TOOL USED RADIOMETE/PHOTOMETER KIT P/N: XRP-3000; S/N :1753759 ; DUE DATE : 30/JUN/25; [03] REPAIRED AFT CORNER SCSDR SWAA2025040103130Battery Pack · inoperativeINOP EMERGENCY EXIT LIGHT (BATTERY PACK) LT SIDE ON LOWERED CEILING PANEL AT FWD GALLEY AREA. REPLACED EMERGENCY EXIT LIGHT (BATTERY PACK) LT SIDE ON LOWERED CEILING PANEL AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-06-960-805 <BR>PERFORMED OPERATIONAL TESDR SWAA2025040103131Battery Pack · inoperativeINOP EMERGENCY EXIT LIGHT (BATTERY PACK) RT SIDE ON LOWERED CEILING PANEL AT FWD GALLEY AREA . REPLACED EMERGENCY EXIT LIGHT (BATTERY PACK) RT SIDE ON LOWERED CEILING PANEL AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-06-960-805 <BR>PERFORMED OPERATIONAL SDR SWAA2025032815234Battery Pack · inoperativeINOP EMERGENCY EXIT LIGHT (BATTERY PACK) RT SIDE ON LOWERED CEILING PANEL AT FWD GALLEY AREA (1 EA) 2025-186089 <[01]. REPLACED EMERGENCY EXIT LIGHT (BATTERY PACK) RT SIDE ON LOWERED CEILING PANEL AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-06-960-805. SDR SWAA2025032815233Battery Pack · inoperativeINOP EMERGENCY EXIT LIGHT (BATTERY PACK) LT SIDE ON LOWERED CEILING PANEL AT FWD GALLEY AREA (1 EA) 2025-186088 <[01]. REPLACED EMERGENCY EXIT LIGHT (BATTERY PACK) LT SIDE ON LOWERED CEILING PANEL AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-06-960-805. SDR SWAA2025040202895Lens · incorrectINCORRECTED LENS EMERGENCY EXIT ON DOOR L2 AT AFT GALLEY AREA 2025-186058 <[01]. REPLACED EMERGENCY LENS ON DOOR L2 AT AFT GALLEY AREA (1EA) IAW B737-700 AMM 33-51-01-960-802 STEP 3.C. ITEM (10); [02] REPLACED EMERGENCY LENS ON DOOR L2 AT AFT GALLEY AREA (1EA)SDR SWAA2025040202894Lens · incorrectINCORRECTED LENS EMERGENCY EXIT ON DOOR R1 AT FWD GALLEY AREA 2025-186070 <[01]. REPLACED EMERGENCY LENS ON DOOR R1 AT FWD GALLEY AREA (1EA) IAW B737-700 AMM 33-51-01-960-802 STEP 3.C. ITEM (10); [02] REPLACED EMERGENCY LENS ON DOOR R1 AT FWD GALLEY AREA (1EASDR SWAA2025040202551Web · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB BTW LBL 30 TO LBL 40 STA 675 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.375 INCH APPROXIMATELY. ) 2025-185995 <[01] ON STEP 4; TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 90023010; DUE DATE: 0SDR SWAA2025040202552Web · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB RBL 40 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.500 INCH APPROXIMATELY.) 2025-185996 <[01]. STEPS 6 AND 7 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 240497907; CAL DUE DATE: 27-AUGSDR SWAA2025040102892Lens · incorrectINCORRECT EMERGENCY EXIT LENS ON DOOR L1 AT FWD GALLEY AREA 2025-186056<[01] REPLACED EMERGENCY LENS ON DOOR L1 AT FWD GALLEY AREA (1EA) IAW B737-700 AMM 33-51-01-960-802 STEP 3.C. ITEM (10);[02] REPLACED EMERGENCY LENS ON DOOR L1 AT FWD GALLEY AREA (1EA) IAW SDR SWAA2025032815213Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB RBL 40 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.500 INCH APPROXIMATELY.) 2025-185996 <[01] STEPS 6 AND 7 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 240497907; CAL DUE DATE: 27-AUG-2SDR SWAA2025032815212Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB BTW LBL 30 TO LBL 40 STA 675 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.375 INCH APPROXIMATELY. 2025-185995 <[01] ON STEP 4; TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 90023010; DUE DATE: 05SDR SWAA2025040202341Sign · burnedBURNED EMERGENCY EXIT INDICATOR ASSY ON SIDEWALL PANEL 231YHW AT PASSENGER CABIN 2025-185968 <[01]. REPLACED EMERGENCY EXIT INDICATOR ASSY ON SIDEWALL PANEL 231YHW AT PASSENGER CABIN IAW B737-700 AMM 33-51-01-960-802 PERFORMED OPERATIONAL TEST IS OK; [02] TASSDR SWAA2025040202339Angle · crackedCRACK ANGLE TRAILING EDGE AREA AT LEVEL ORSS 270 AT RT WING 2025-185961<[01] REPLACED ANGLE AND FASTENERS LOCATED TRAILING EDGE AREA AT LEVEL ORSS 270 AT RT WING IAW B737-700 SRM 51-40-02-0G; SRM 51-10-02-0G-0 AND DWG 115A2982 SHEET 4. REV -;[02] CORRECTED STESDR SWAA2025033115201Angle · crackedCRACK ANGLE TRAILING EDGE AREA AT LEVEL ORSS 270 AT RT WING 2025-185961<[01] REPLACED ANGLE AND FASTENERS LOCATED TRAILING EDGE AREA AT LEVEL ORSS 270 AT RT WING IAW B737-700 SRM 51-40-02-0G; SRM 51-10-02-0G-0 AND DWG 115A2982 SHEET 4. REV -;[02] CORRECTED STESDR SWAA2025032815203Indicator · burnedBURNED EMERGENCY EXIT INDICATOR ASSY ON SIDEWALL PANEL 231YHW AT PASSENGER CABIN 2025-185968 <[01]. REPLACED EMERGENCY EXIT INDICATOR ASSY ON SIDEWALL PANEL 231YHW AT PASSENGER CABIN IAW B737-700 AMM 33-51-01-960-802 PERFORMED OPERATIONAL TEST IS OK; [02] TASDR SWAA2025030699109Scuff Plate · crackedFCB FWD SCUFF PLATE CRACKED<[01] REPLACED FCB FWD SCUFF PLATE PER SRM 51-10-02-0G-0; LOCATED AND DRILLED AND COUNTERSUNK PER SRM 51-40-02-0G-0; SRM 51-40-08-0G-0; REF IPC 53-13-00-08.;[02] INSTALLED ON BAR CODE TTG8Q00YP6R7;[03] VERIFIED CORRECTIVE ACTION ITEMSDR SWAA2025031098253Panel · crackedFSD FWD SURROUND PANEL IS CRACKED AT THE OUTLET CUTOUT<[01]. REPAIRED FSD FWD SURROUND PANEL CRACK AT OUTLET CUTOUT IAW CMM 25-00-66 REPAIR 1-1 SECTION 4.B.; REPAIR 2-1 SECTION 4.B; AND ENG. DWG 25200003 PG. 11 ITEM 1.12.SDR SWAA2025022498763O-Ring · leakingSUSPECTED HYDRAULIC LEAK IN MAIN WHEEL WELL. REMOVED AND REPLACED O-RING AT BOTTOM OF ALT. BRAKE SELECTOR VALVE REF AMM 32-41-93SDR SWAA2025031097012Angle · crackedDURING OPEN HOLE HFEC; 1 EA HOLE CRACKED; TITANIUM ANGLE UPPER FLANGE; BS 663; LBL 36; MARKED.<[01] REPAIRED CRACKED HOLE BY REAMING HOLE TO FIRST OVERSIZE PER SRM 53-40-51-2R-2 PARAGRAPH 2. J. AND SRM 51-10-02-0G-0 STEP 11. B. NDI ACCOMPLISHED PER 737 NDTM PASDR SWAA2025031096409Vapor Barrier · crackedR/H BS 663 LOWER VAPOR BARRIER CRACKED RBL 53 WL 159 <[01]. APPLIED INTERIM REPAIR AT THE LOWER VAPOR BARRIER RBL 53 BS663 WL 159 IAW SRM 57-10-10-2R-2; [02] VERIFIED ALL STEPS CORRECTION ACTION ITEM 1 MEASUREMENT FIELD COMPLETE; CARD COMPLETE.SDR SWAA2025030695755Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DAMAGE FOUND TO BE OUT OF ECONOMICAL REPAIR; FABRICATED NEW 231XF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2025030695757Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DAMAGE FOUND TO BE OUT OF ECONOMICAL REPAIR; FABRICATED NEW 241AF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2025030695759Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DAMAGE FOUND TO BE OUT OF ECONOMICAL REPAIR; FABRICATED NEW 241DF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2025030695760Floor Panel · pulledFLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DAMAGE FOUND TO BE OUT OF ECONOMICAL REPAIR; FABRICATED NEW 242AF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2025030696150Seat Track · corrodedCORROSION ON PAX CABIN SEAT TRACK BS372 LBL25 WL208. MARKED<[01] REMOVED CORROSION FROM CABIN SEAT TRACK BS372 LBL25 WL208.<BR>WELL: L= 7' W: .90' D: .030' CROWN: L=4'W: .45' D: .025'<BR>FOUND SEAT TRACK OUT LIMITS PER SRM 53-00--52-1A-1 PAR. 4 A. (2) FIG. 103SDR SWAA2025030696222Panel · crackedR/W T/E PANEL 651FB HAS A CRACKED L-CLIP ON FWD SIDE 27' FROM O/B END<[01] REMOVED CRACKED L-CLIP AND REPLACED WITH NEW IAW SRM 51-40-02-0G-0 AND DWG 115A2710 REV. B.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2025031095754Panel · crackedPANEL BREAK CRACKED AT HARDWARE - BS 540; RBL 47 AND RBL 63. <[01] REMOVED AND REPLACED PANEL BREAK AT BS 540; RBL 47 AND RBL 63 PER SRM 51-40-02-0G-0 AND DWG 143A5240 REV: -; [02] JOB COMPLETE.SDR SWAA2025031095752Web · crackedCRACK IN MAIN CABIN ABOVE MLG WHEEL WELL - BS 663; LBL 35; WL 196. <[01] THIS CARD WILL BE ATTENDED ON CUSTOMER CARD TTG8Q00YPFZ9; [02] VERIFIED. CARD COMPLETE.SDR SWAA2025030695751Stiffener · corrodedCORROSION NEAR FASTENER; BS 697; RBL 67; WL 203.5.<[01] CORROSION NEAR FASTENER; BS 697; RBL 67; WL 203.5 REPAIRED PER 25-153-00436-WIP1;[02] VERIFIED CORRECTIVE ACTION. CARD COMPLETE.SDR SWAA2025030695750Skin · crackedCRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.9; 17' FROM FWD EDGE; 0.5' IN LENGTH (MARKED)<[01] DUPLICATE WRITE UP. ALL WORK TO BE PERFORMED ON FAULT TTG8Q00YQ0L1;[02] VERIFIED. CARD COMPLETE.SDR SWAA2025030695749Skin · crackedCRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 17' FROM FWD EDGE; 0.5' IN LENGTH (MARKED)<[01] REPAIRED L/H HORIZONTAL STABILIZER LOWER SKIN IAW SRM 51-40-02-0G-0 AND SRM 55-10-01-2R-11; REPAIR 11; FIG. 204; DETAIL B AND TABLE 202.;[02] VERISDR SWAA2025030695375Pressure Deck · crackedCRACK IN LH HORIZ PRESSURE DECK BS 665 LBL 34 WL 202; .790' LONG. MARKED ENDS.<[01] REMOVED THE DAMAGE WEB; CUT AND REMOVED THE DAMAGED PART OF THE WEB PER SRM 53-40-51-2R-2 PAR. 4. C. (1)(2)(3)(B) FIG. 203. <BR><BR>INSTALLED L/H PRESSURE DECK BS663- BS773; L SDR SWAA2025030695743Scuff Plate · crackedAFT CARGO FWD CORNER SCUFF PLATE CRACKED<[01] REPAIRED AFT CARGO FWD CORNER SCUFF PLATE PER SRM 53-60-15-2R-1 PARA 4.B.(2); SOPM 20-30-02; SOPM 20-43-03; AMM 51-21-72-370-804.;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2025031095371Bulkhead · crackedB.S. 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT L.B.L. 19; W.L. 152. <[01] APPLIED INTERIM REPAIR AT THE LOWER VAPOR BARRIER LBL 19 BS663 WL 152 IAW SRM 57-10-10-2R-2; [02] VERIFIED ALL STEPS CORRECTION ACTION ITEM 1 MEASUREMENT FIELD COMPLETE; CARD COMPLETE.
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