Boeing 737-7BD
Service difficulty reports · 7,528
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 = '7377BD' 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 = '7377BD' 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 SWAA2024062789407Sidewall Support · corrodedCORROSION FWD CARGO FLOOR TO SIDEWALL SUPPORT BS500A+2-BS500A+10; BS500B+6; BS500B+18; BS500C+2 RBL 25 WL 156<[01] REMOVED AND REPLACED R/H FLOOR TO SIDEWALL FROM BS 500A TO BS 500D IAW SRM 51-40-02 AND DWG 143A7500 ID:0045 REV: -;[02] JOB COMPLETE.SDR SWAA2024062789412Shield · corrodedCORROSION FWD CARGO AFT SHIELD BS480+18; BS500+10-500A RBL 25 WL 156<[01] REMOVED AND REPLACED FWD CARGO BAY AFT SHIELD PER SRM 51-40-02-0G-0 AND DWG#143A0080.;[02] REJECT - STEP 7; 2EA FASTENERS TTG8Q00TU9R5;[03] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH STEPSSDR SWAA2024062689410Stringer · crackedAFT AREA OF FWD CARGO BS540 L/H STR 23 CRACKED WL 156<[01] REJECT: EA-24-153-01423-WIP1 STEP 2.<BR>FABRICATION PARTS DOES NOT MATCH THE 737-700 SRM 53-00-03 REPAIR 1;<BR>INCORRECT LOCATION OF DRAIN HOLE ON HAT-SECTION REPAIR.;[02] ACCOMPLISHED REPAIR PER SRM 5SDR SWAA2024062689399Attach Angle · crackedFWD CARGO INTERCOSTAL ATTACH ANGLE AFT OF BS 400 RBL 25 WL 152 CRACKED<[01] REMOVED AND REPLACED ON FCB INTERCOSTAL ATTACH ANGLE (CLIP) AFT OF BS400;RBL25;WL152 IAW SRM 51-40-02 AND DWG#143A7505. VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2024052489513Slide · out of positionAFT LEFT SERVICE DOOR SLIDE OUT OF POSITION<[01] REPACKED SIDE IAW MT 725-62-01 AC OK FOR SERVICESDR SWAA2024052389212Motor · faultedSTAB OUT OF TRIM LT ILLUMINATED DURING FLT. R & R STAB MOTOR PER MM 2741-71.SDR SWAA2024070388880Seal · crackedRT. HORIZ STAB PANEL 343AT SLIDE SEAL (SHARK FIN) CRACKED.<[01] REMOVED AND REPLACED RT. HORIZ STAB PANEL 343AT SLIDE SEAL (SHARK FIN) IAW SRM 51-40-02 AND AIPC 55-10-52-01H;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2024062888896Stiffener · deformedFLOOR SUPPORT STIFFENER SHIM WAS FOUND DEFORMED AT STA 540 BETWEEN RBL45 AND RBL63;WL208. (MARKED)<[01] REMOVED AND REPLACED FLOOR STIFFENER SUPPORT ANGLE IAW SRM 51-40-02 AND DWG 143A5240 ID:0021 REV: -;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASURESDR SWAA2024062788898Floor Support · crackedFLOOR STIFFENER SUPPORT ANGLE CRACKED AT STA685+8; RBL 24.5; WL203. (MARKED)<[01] REMOVED AND REPLACED FLOOR STIFFENER SUPPORT ANGLE AT STA 685+8; RBL 24.5; WL203 IAW SRM 51-40-02-0G-0 AND DWG 273A9110 REV A;[02] REMOVED AND REPLACED FLOOR STIFFENER SUPPORT ANSDR SWAA2024062788899Floor Support · crackedFLOOR STIFFENER SUPPORT ANGLE CRACKED AT STA540; LBL1; WL208. (MARKED)<[01] REMOVED AND REPLACED FLOOR STIFFENER SUPPORT ANGLE IAW SRM 51-40-02 AND DWG 143A5240 ID:0014 REV:;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2024062688897Floor Panel · pulledFLOOR PANEL 241CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241CF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 ID:0130.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.SDR SWAA2024062688137Floor Panel · pulledFLOOR PANEL 242BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024062688136Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024062688135Floor Panel · pulledFLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024062688134Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241AF FLOOR PANEL HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.;[02] CORRECTION TO CORRECTIVE ACTION STEP 1: 'FABRICATION OF NEW 241AF FLOOR PANEL HAS BEEN ACCOMPLISHED IAW SRM 53SDR SWAA2024062688133Floor Panel · pulledFLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 232SF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1553922-1; INSERTS INSTALLED USING BMS5-107 LOT#AK3BA2380A/A THEN CURED UNDER HEAT LAMP MONITORED WITH THERMOMETER ASDR SWAA2024062688132Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024062687923Vapor Barrier · crackedL/H B.S. 663 VAPOR BARRIER IS CRACKED AT MID SPAN.<[01] 04 - REPAIRED PER [SRM 51-70-04-2R-10-A00755 (REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES - AIRFRAME - PERMANENT)];[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024052287850Slide · dislodgedFORWARD SERVICE DOOR EMERGENCY ESCAPE SLIDE DISLODGED WHEN DOOR OPENED. GIRT BAR WAS NOT ENGAGED; SLIDE WAS NOT ACTIVATED.<[01] RE INSTALLED FWD SERVICE DOOR ESCAPE SLIDE PACK AND COVER PER AMM 25-66-01. OP CHECK GOOD.SDR SWAA2024052287242Panel · damagedWING-TO-BODY FAIRING PANEL 193B HAS SEVERAL ELONGATED FASTENER HOLES AND NUMEROUS COUNTERSINKS THAT ARE TOO DEEP.<[01] MATCH DRILLED NEW PANEL 193B PER SRM 51-10-02.SDR SWAA2024052086045Lamp · inoperativeINOP LAVATORY A EMERGENCY LIGHT AT FWD GALLEY AREA 2024-259404<[01] REPLACED LAMPS IN LAVATORY A EMERGENCY LIGHT AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 AND PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS IAW B737-700 AMM 33-51-00-710-801<BR>TEST ISDR SWAA2024050983733Handle · looseCABIN L1 DOOR CLOSE ASSIST HANDLE LOOSE.<[01] SECURED CABIN L1 DOOR CLOSE ASSIST HANDLE PER AMM 52-11-00.SDR SWAA2024050783320Fuel Sys · unbalancedERRATIC FUEL CONSUMPTION WITH ENGINE NUMBER TWO FUEL IMBALANCE OF 1000LBS IN 17 MINUTES ON CLIMB OUT AFTER BALANCING FUEL QUANTITY IN NUMBER TWO TANK WAS PLUS OR MINUS 60 POUNDS<[01] INSPECTED MOTORS FOR FUEL LEAKS NO DEFECTS FOUND PER AMM 71-71-00 PERFORMED FSDR SWAA2024042980168Lamp · inoperativeL1 DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] REPLACED LAMP FOR THE L1 DOOR EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHECK GOOD.SDR SWAA2024042579218Slide · dislodgedSLIDE FROM FWD SERVICE DOOR FELL OUT<[01] REPACKED FWD SERVICE DOOR SLIDE PER MT725-61-06SDR SWAA2024051578352Stub Frame · crackedCRACK INDICATION IN HOLE FROM STUB FRAME LOCATED BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. LOOKING FWD CRACK DIRECTION IS: 7 O CLOCK. 2024-259366 CRACK ON WEB LOCATED BTW BS 291.5 TO BS 340 AT LEVEL STR 17R AT FWD GALLEY AREA SEE PICTURES ON TASK INFORMATISDR SWAA2024042377514Light · inoperativeINOP EXTERNAL SKIN EMERGENCY EGRESS EXIT LIGHT NEXT TO AFT SERVICE DOOR AT UPPER FUSELAGE (1 EA) 2024-206689<[01] REPLACED FUSE AT POWER SUPPLY AND TEST IS OK IAW B737-700 AMM 33-51-06-960-804.;[02] TASK CARD COMPLETE.SDR SWAA2024042679508Actuator · faultedR/H LANDING GEAR RED LIGHT ILLUMINATED DURING GEAR EXTENSION<BR>NOSE GEAR AND L/H LANDING GEAR OPERATED NORMALLY<BR>CYCLED THE HANDLE. R/H RED LIGHT ILLUMINATED AGAIN.<BR>DURING GO AROUND AND QRH. EXTENDED THE GEAR A THIRD TIME AND ALL THREE GREEN LIGHTS ILLUMSDR SWAA2024042377111Bracket · brokenR/H MAIN LANDING GEAR BEAM CONDUIT GUIDE LOWER ATTACH BRACKET IS BROKEN.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]<BR>R&R R/H MAIN LANDING GEAR BEAM CONDUIT GUIDE LOWER ATSDR SWAA2024052084498Angle · perforatedPERFORATION ON ANGLE LOCATED BS540 PLUS 8INCH AND RBL41 AT AIR CONDITIONING BAY 2024-259288<[01] TOOL USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-OCT-24.;[02] PERFORMED PERMANENT REPAIR CATEGORY A LOCATED BS540 TO 540+13? AND RBL41 AT AIR CONDITIOSDR SWAA2024052076303Bracket · crackedCRACK BRACKET LOCATED BS540 AND RBL7 AT AIR CONDITIONING BAY 2024-259286<[01] REPLACED BRACKET LOCATED BS540 AND RBL7 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED BRACKET LOCATED BS540SDR SWAA2024052076304Bracket · crackedCRACK BRACKET LOCATED BS540 AND LBL7 AT AIR CONDITIONING BAY 2024-259287<[01] REPLACED BRACKET LOCATED BS540 AND LBL7 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED BRACKET LOCATED BS540SDR SWAA2024051676300Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS273 ON DEFLECTION CONTROL RIB AREA LT WING 2024-259282<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS273 ON DEFLECTION CONTROL RIB AREA LT WING TOOK MEASURE OF CRACK IS 0.835 INCH TOOL USED CALIPER P/N: 500-196-30 S/N: A22SDR SWAA2024051676302Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS217 AT LT WING 2024-259283<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS217 AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; MEASURED CRACK IS L: 0.799 INCH TOOL USED CALIPER P/N: 8647A4SDR SWAA2024051576306Light · brokenBROKEN EMERGENCY EXIT LIGHT ASSY ON BIN 6 LH SIDE 2024-259291<[01] REPLACED EMERGENCY EXIT LIGHT ASSY ON BIN 6 LH SIDE IAW B737-700 AMM 33-51-03-960-802; STEP 3.D. (1); EXCEPT 3.D. (1) (A) AND (I).;[02] REPLACED EMERGENCY EXIT LIGHT ASSY ON BIN 6 LH SIDE IAW BSDR SWAA2024052075514Angle · crackedCRACK ON ANGLE LOCATED BS 947.5 AT LEVEL STR 25L AT AFT CARGO COMPARTMENT 2024-259235<[01] REPLACED ANGLE AND FASTENERS LOCATED BS 947.5 AT LEVEL STR 25L AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG 149A8103 SHEET: 7 REV: A; SEE INDIVISDR SWAA2024052087949Angle · crackedCRACK ON ANGLE LOCATED BS 947.5 AT LEVEL STR 25L AT AFT CARGO COMPARTMENT 2024-259235<[01] REPLACED ANGLE AND FASTENERS LOCATED BS 947.5 AT LEVEL STR 25L AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG 149A8103 SHEET: 7 REV: A; SEE INDIVISDR SWAA2024052075513Floor Support · crackedCRACK ON ANGLE LOCATED FLOOR STRUCTURE BTW BS 907 TO BS 927 AFT POSITION AT AFT CARGO COMPARTMENT 2024-259237<[01] REPLACED ANGLE LOCATED FLOOR STRUCTURE BTW BS 907 TO BS 927 AFT POSITION AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 SDR SWAA2024052075516Strap · corrodedCORROSION ON STRAP LOCATED BS 887 BTW STR 26L TO STR 26R WL 156 AT AFT CARGO COMPARTMENT 2024-259238<[01] REPLACED STRAP LOCATED BS 887 BTW STR 26L TO STR 26R WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 146A9401 SHEETSDR SWAA2024051575692Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB RBL 41 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROXIMATELY: 0.327 INCH 2024- 259270<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL-24.;[02] TOOL USED: ESDR SWAA2024051575691Pressure Deck · crackedCRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK LBL 30 STA 663 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.437 INCH APPROX. 2024-259269<[01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 210138503; DUE DATE: 21-JUL-24;[02] TOOL USED: EDDY CURRSDR SWAA2024052074731Girt Bar · deterioratedDETERIORATED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AFT ENTRY DOOR AT AFT GALLEY AREA 2024-259164<[01] REPLACED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AFT ENTRY DOOR AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801;[02] CORRECTED STEP 1<BR><BR>REPLSDR SWAA2024052074739Bracket · deterioratedDETERIORATED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AFT SERVICE DOOR AT AFT GALLEY AREA 2024-259165<[01] REPLACED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AFT SERVICE DOOR AT AFT GALLEY IAW B737-700 AMM 25-66-02-400-801;[02] CORRECTED STEP 1<BR>REPLACED SDR SWAA2024051574729Lens · brokenBROKEN EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) 2024-259152<[01] REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-801 STEP 2.C. (1) (A) 4).;[02] COMPLETEDSDR SWAA2024051575178Light · brokenBROKEN LAVATORY A EMERGENCY EXIT LIGHT ASSY AT FWD GALLEY AREA (1 EA) 2024-259222<[01] REPLACED LAVATORY A EMERGENCY EXIT LIGHT ASSY AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-801 STEP 2.C. (1) (A) 4).;[02] COMPLETEDSDR SWAA2024051574737Girt Bar · deterioratedDETERIORATED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE FWD ENTRY DOOR AT FWD GALLEY AREA 2024-259162<[01] REPLACED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE FWD ENTRY DOOR AT FWD GALLEY AREA I.A.W B737-700 AMM 25-66-02-400-801;[02] CERTIFIED WORK PERFORMED.SDR SWAA2024051574738Girt Bar · deterioratedDETERIORATED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE FWD SERVICE DOOR AT FWD GALLEY AREA 2024-259163<[01] REPLACED GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE FWD SERVICE DOOR AT FWD GALLEY AREA I.A.W B737-700 AMM 25-66-02-400-801;[02] CORRECTED STEP 1<BR><BSDR SWAA2024052074621Access Panel · corrodedCORROSION WEB INDICATEDTOR FUEL LOCATED OFSS382 ACCESS PANEL 621GB AT RT WING 2024-259142 CORROSIN ON FUEL QUANTITY INDICATORS HOUSING LOCATED AT PANEL 621GB RT WING<[01] REPLACED INDICATEDTOR FUEL LOCATED OFSS382 ACCESS PANEL 621GB AT RT WING I.A.W B737-700 SSDR SWAA2024051474620Bracket · crackedCRACK EXTERNAL SKIN SUPPORT BRACKET LOCATED BS1016 AT LEVEL STR3L TO STR3R AT VERTICAL STABILIZER 2024-259139<[01] REPLACED SUPPORT BRACKET AND FASTENERS I.A.W. B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02; DRAWING# 176A3101 SHEET 4 REV: - AND DWG#SDR SWAA2024041874346Support Bracket · crackedRIGHT ENGINE STARTER VALVE DUCT SUPPORT BRACKET IS CRACKED AT 9 O'CLOCK POSITION.<[01] REMOVED AND REPLACED STARTER DUCT SUPPORT BRACKET AT #2 ENGINE 9 O'CLOCK POSITION (STARTER DUCT NOT DISCONNECTED). REF: B-737NG AMM 20-50-11-910-801 AND POWERPLANT BUILDUP M
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