Boeing 737-7BX
Service difficulty reports · 579
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 = '7377BX' 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 = '7377BX' 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 COZA20131107034Sensor · inoperativeAFTER A FLAPS 40 LANDING, THE FLAPS SPLIT AND STOPPED WHILE BEING RETRACTED. THE LT FLAP SKEW SENSOR INDICATOR CIRCUIT BREAKER POPPED. TROUBLESHOOTING DETERMINED THE NR 3 FLAP SKEW SENSOR HAD FAILED. R & R THE FLAP SKEW SENSOR. OPS CHECKS WERE NORMAL.SDR ASMF201311080002Blades · damagedACFT RETURNED DUE TO THE LT ENGINE VIBRATION REACHING 6.0 UNITS. FLIGHT CREW ACCOMPLISHED QRH 7.24 PROCEDURE AND VIBRATION WAS STABILIZED IN 4.0 UNITS. MAINTENANCE DETECTED A CRACK ON FOUR FAN BLADES 1 INCH LONG AND 0.750 INCHES IN DEPTH, CRACKS OUT OF LIMITSDR SWAA2013092620545Handle · lack of lubeR2 WINDOW EXTERNAL RELEASE HANDLE INOPERATIVE. LUBED HANDLE IAW SIP.SDR COZA20130923033Control Panel · inoperativeDURING MX CHECKS IN COCKPIT, NR 2 NAV CONTROL PANEL FOUND BLINKING. "FAILED" SHOWED IN THE WINDOWS WHEN FREQUENCIES WERE TRANSFERRED. THE NAV CONTROL PANEL WAS REPLACED AND OPS CHECKED NORMAL.SDR COZA20130908032Start Valve · inoperativeDURING LT ENGINE START, LT "START VALVE OPEN" LIGHT REMAINED ILLUMINATED AFTER ENGINE START SWITCH WAS TURNED OFF. TROUBLESHOOTING IAW THE FAULT ISOLATION MANUAL, DETERMINED THE START VALVE HAD FAILED. REPLACED LT ENGINE START VALVE AND OPS CHECK NORMAL.SDR COZA20130830031Actuator · leakingDURING INSPECTION, THE NR 10 FLIGHT SPOILER ACTUATOR WAS FOUND STATICALLY LEAKING FROM THE INPUT LINKAGE ASSEMBLY. OPERATING THE FLIGHT SPOILER WITH HYD POWER DID NOT CHANGE THE LEAK RATE. REPLACED ACTUATOR AND OPERATIONALLY CHECKED WITH NO LEAKS FOUND.SDR SWAA2013082919682Bracket · crackedRT WING REAR SPAR SHELF PLATE BULB SEAL BRACKET CRACKED. R&R BRACKET IAW SRM.SDR COZA20130814030Display · inoperativeON GROUND, F/O PRIMARY FLIGHT DISPLAY UNIT WENT DARK. R & R THE DISPLAY UNIT. OPS CHECKED NORMAL.SDR SWAA2013080618869Bushing · missingR1 DOOR EMERGENCY EVAC SLIDE GIRT BAR PLASTIC BUSHING MISSING. R&R BUSHING IAW MM.SDR COZA20130708029Signal Cond Unit · inoperativeENGINE VIBRATION INDICATIONS WENT BLANK ON SECONDARY ENGINE DISPLAY. USING TROUBLESHOOTING INFORMATION FROM THE FIM, THE AIRBORNE VIBRATION MONITORING SIGNAL CONDITIONER WAS FOUND INOPERATIVE. REPLACED THE AVM SIGNAL CONDITIONER AND ENGINE VIBRATION INDICATISDR COZA20130618028Control Unit · inoperativeDURING GROUND CHECKS, "ELEC" LIGHT ILLUMINATED ON THE ELECTRIC METERS, BATTERY AND GALLEY POWER MODULE. BITE CHECK ON POWER MODULE P5-13 INDICATED "SPCU INOP". REPLACED THE STANDBY POWER CONTROL UNIT. OPS CHECK NORMAL AND "ELEC" LIGHT NOT ILLUMINATED.SDR COZA20130609027Fdau · inoperativeFLIGHT DATA RECORDER "OFF" LIGHT ILLUMINATED ON THE FDR/MACH AIRSPEED WARNING PANEL, P5. USING FAULT ISOLATION MANUAL TASKS, THE FLIGHT DATA ACQUISITION UNIT WAS FOUND FAILED INTERNALLY AND UNRESPONSIVE. REPLACEMENT FDAU, PN 967-0212-002 WAS INSTALLED AND OSDR COZA20130603026Control Unit · inoperativeACFT WAS ON THE GROUND AND "ELEC" LIGHT WAS ILLUMINATED ON THE ELECTRIC METERS, BATTERY AND GALLEY POWER MODULE. BITE CHECK ON POWER MODULE P5-13, INDICATED SPCU INOP. R & R STANDBY POWER CONTROL UNIT. OPS CHECK NORMAL WITH NO MX MESSAGES OR LIGHTS.SDR SWAA2013042415095Lens · missingLEFT EMERGENCY LIGHT LENS MISSING AT ROW 9. INSTALLED LENS PER MM.SDR SWAA2013041614874Wire · out of adjustR2 DOOR EMERGENCY EVAC SLIDE TEST WIRE FELL OUT. RE-INSTALLED WIRE PER M/M.SDR SWAA2013031413659Slide · out of positionL1 DOOR SLIDE OUT OF ADJUST. REPOSITIONED L1 DOOR SLIDE PER MT.SDR SWAA2013031213559Sign · missingEXIT SIGN AT ROW 12 DEF MISSING. REMOVED AND REPLACED LIGHT ASSY PER WDM.SDR SWAA2013030513340Light · inoperativeEMERGENCY DOME LIGHT IN COCKPIT INOP. REMOVED AND REPLACED BULB PER MM.SDR SWAA2013022813176Frame · brokenEXIT SIGN FRAME BROKEN FOR AFT GALLEY DOOR. REMOVED AND REPLACED LAMP ASSY PER M/M.SDR SWAA2013021512705Skin · crackedEXT POWER DOOR ACCESS CUTOUT AFT EDGE IS CRACKED. ACCOMPLISHED REPAIR ON EXT PWD DOOR ACCESS CUTOUT AFT EDGE IAW EA 1-A53-9269 88954U 13FEB13.SDR SWAA2013021412652Cover · brokenAFT FLIGHT ATTENDANTS CONTROL PANEL EMERGENCY LIGHT SWITCH COVER SPRING IS BROKE. REMOVED AND REPLACED AFT FLIGHT ATTENDANTS CONTROL PANEL EMERGENCY LIGHT SWITCH COVER IAW SWPM 20-84-14 PG 6 PARA F STEP 1 AND 2 AND PG 11 PARA F STEP 1.1 89318C 12FEB13.SDR COZA20130131024Control Panel · defectiveBACKLIGHTING ON AUDIO CONTROL PANEL P/N 5145-1-64 WAS INTERMITTENT. REPLACED PANEL AND OPERATIONAL CHECK NORMAL.SDR SWAA2013012811946Light · inoperative(QC) FWD ENTRY EMERGENCY EXIT LIGHT INOP. RELAMPED FWD ENTRY EMERGENCY EXIT LIGHT PER AMM 33-35-01-960-801 STEP 2.C. 1(A-4) & 2.C.1(C) & 2.C.4 AND PERFORMED GOOD TEST PER AMM 33-35-01-960-801 STEP 2.C.2 56138U 27JAN13.SDR SWAA2013012811945Light · inoperative(QC) AFT SERVICE DOOR EXIT LIGHT BULB BURNED OUT. RELAMPED AFT SERVICE DOOR EXIT LIGHT BULB PER AMM 33-51-01-960-801 STEPS 2.C.(A.1) & 2.C.4 AND PERFORMED GOOD OPS CHECK PER AMM 33-51-01-960-801 STEP 2.C.2 56138U 27JAN13.SDR SWAA2013012811944Slide · out of position(QC) AFT SERVICE DOOR ESCAPE GIRT IS CONTACTING FLOOR AND BINDING UPON CLOSE. REPOSITIONED AFT SERVICE DOOR SLIDE PACK IAW MT #725-61-06 POS SA 3695U 27JAN13.SDR COZA20130124022Hydraulic System · lowAIRCRAFT LANDED WITH "A" HYDRUALIC SYSTEM AT 64% AND REFILL ANNUNCIATED. INSPECTION FOUND SIGNS OF FLUID INBOARD OF RIGHT WING AND RIGHT SIDE OF FUSELAGE. RESERVOIR WAS SERVICED. LEAK CHECKS WERE PERFORMED BY ACTUATING LEADING EDGES, FLAPS, SPOILERS AND AILSDR COZA20130117021Actuator · leakingDURING INSPECTION, RIGHT INBOARD LEADING EDGE FLAP ACTUATOR FOUND LEAKING. REPLACED ACTUATOR P/N 382000-1001. OPERATIONAL CHECK, NO LEAKS FOUND.SDR SWAA2013012811941Light · inoperativeEMERGENCY LIGHT BELOW EXIT LIGHT FWD BULB IS INOP. RELAMPED FWD EMERGENCY LIGHT BELOW EXIT LIGHT RT SIDE. FUNCTION TEST GOOD PER AMM 33-51-00-710-801 89195U 25JAN13 AND AMM 33-51-01-960-801.SDR SWAA2013012311704Attach Bracket · crackedAFT CARGO BAY FWD BULKHEAD ATTACH BRACKET CRACKED BS 727, WL 163, RBL 5. REMOVED AND REPLACED ACB FWD BULKHEAD ATTACH BRACKET AT BS 727, WL 163 RBL 5 WITH NEW BRACKET PART NUMBER 7531203 IAW SRM 51-40-02. 56105U 17JAN13.SDR COZA20130117020Control Unit · faultyCREW REPORTED "AUTO BRAKE DISARM" LIGHT CAME ON IMMEDIATELY AFTER TOUCHDOWN. A BITE CHECK WAS PERFORMED ON THE ANTI-SKID/AUTO-BRAKE CONTROL UNIT (AACU). ACTIVE MAINTENANCE MESSAGE "BOX A/B" WAS DISPLAYED. FOLLOWING THE STEPS IN THE FIM, THIS MESSAGE INDICATSDR SWAA2013011411423Stop Pin · looseRIGHT EMERGENCY EXIT DOOR HATCH AFT UPPER STOP PIN IS LOOSE. TIGHTENED RIGHT EMERGENCY EXIT DOOR HATCH AFT UPPER STOP PIN JAM NUT IAW AMM 52-22-00-820-801 STEP 5.F.(1)10).SDR SWAA2013011011346Retaining Clip · looseFORWARD GALLEY DOOR FWD GIRT BAR RETAINING CLIP IS LOOSE. REMOVED & REPLACED FGD FWD GIRT BAR RETAINING CLIP IAW SRM 51-40-02 STEP 4A,B,C, & E.SDR SWAA2013012811943Connector · brokenELECTRICAL CONNECTOR BS 952 WL 300 LBL 16 IS BROKEN. REMOVED AND REPLACED CONNECTOR D40100J PER SWPM 20-72-24 & WDM 33-51-22, 33-51-14 4631U 09JAN13 8052C 9JAN13 307 09JAN13 PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS PER AMM 33-51-00-710-8.SDR SWAA2013012111600Floor Panel · corrodedCORROSION ON RIGHT EDGES OF FLOOR PANEL 140AF. REPLACED PANEL PER DWG SRM.SDR SWAA2013012111599Tee Fitting · corrodedCORROSION APU COMPARTMENT RT SIDE BS 1128. REMOVED AND REPLACED T-CHORD PER SRM AND DWG.SDR SWAA2013010811261Tee Fitting · corrodedBS 1088 RBL 32 O/B T-CHORD CORRODED. REMOVED AND REPLACED T-CHORD PER SRM AND DWG.SDR SWAA2013012311728Seal · crackedRIGHT HORIZONTAL STABILIZER FORWARD LOWER SLIDE SEAL IS CRACKED. REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER FORWARD LOWER SLIDE SEAL PER MM 55-31-31-000-801, MM 55-31-31-400-801 AND SOPM 20-50-01.SDR SWAA2013012311703Frame · crackedFRAME CRACKED STA 293, RBL 54, WL 209 (FSD FWD FRAME). REPAIRED BS 293 FWD SERVICE DOORWAY FWD LOWER STUB FRAME RBL 54 WL 209 IAW ER 13-01020 AND EA 1-753-21496.SDR SWAA2013012111598Stringer Clip · crackedSTRINGER CLIP IS CRACKED AT STA 360 STRINGER 8R. REMOVED STR CLIP BS 360 STR 8R IAW SRM 51-40-02. INSTALLED NEW STRINGER CLIP PO #LINE 422757 AT STA 360 STR 8R IAW SRM 51-40-02-0G-0.SDR SWAA2013011811561Fuse · blownBATTERY CHARGER AT STATION 597 RIGHT, M1669 HAS BLOWN FUSES. INSTALLED FUSES ON M1669 PER WDM 33-51-11 89229U 15JAN13 8052C 15JAN13 267 15JAN13 OPS CHECK OF EMERGENCY EXIT LIGHTS WILL BE ACCOMPLISHED ON DEFECT T169104 SAM 326 A 771917 ITEMSDR SWAA2013011811560Fuse · blownBATTERY CHARGER AT STATION 500C, M2335 HAS BLOWN FUSES. INSTALLED FUSES ON M2335 PER WDM 33-51-11 89229U 15JAN13 8052C 15JAN13 267 15JAN13 OPS CHECK OF EMERGENCY EXIT LIGHTS WILL BE ACCOMPLISHED ON DEFECT T169107 SAM 326 A771917 ITEM 1.SDR SWAA2013012811942Frame · crackedBS 360 FRAME IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE AT STR 8R. BS 360 FRAME AT STRINGER 8R REPAIRED PER EA 1-753-21532.SDR SWAA2013012311702Frame · crackedBS 360 FRAME IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE AT STR 8L. REPAIRED BS 360 FRAME AT AIR CONDITIONING ATTACH BRACKET STR 8L IAW EA 13-01010 AND EA 1-753-21499.SDR SWAA2013012111597Frame · crackedBS 727D FRAME IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE AT STR 8R. BS 727D FRAME REMOVED AND REPLACED ON CARD T169299.SDR SWAA2013012111596Frame · crackedBS 500A FRAME IS CRACKED AT AIR CONDITIONING ATTACH BRACKED I/B HOLE AT STR 8R. REPAIRED BS 500A FRAME AT AIR CONDITIONING ATTACH BRACKET STR 8R IAW EA 1-A53-12114R2.SDR SWAA2013010911285Mount · corrodedCORROSION ON L1 DOOR GIRT BAR FITTING MOUNT STA 344, LBL 58, WL 208. REMOVED AND REPLACED MOUNT IAW SRM.SDR SWAA2013010811260Frame · crackedBS 400 FRAME IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE AT STR 8R. REPAIRED BS 400 FRAME AT AIR CONDITIONING ATTACH BRACKET STR 8R IAW EA 1-A53-12114R2.SDR SWAA2013010811259Frame · crackedBS 787 FRAME IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE AT STR 8L. REPAIRED THE CRACK AT BS 787 STR 8L AT AIR CONDITIONING BRACKET I/B HOLE IAW EA 1-A53-12114.SDR SWAA2013010711167Frame · crackedBS 867 FRAME IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE AT STR 8R. BS 867 FRAME THAT IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE REPAIRED IAW EA 1-A53-12114. 89213C 02JAN13.SDR SWAA2013010711166Frame · crackedBS 827 FRAME IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE AT STR 8R. BS 827 FRAME THAT IS CRACKED AT AIR CONDITIONING ATTACH BRACKET I/B HOLE REPAIRED IAW EA 1-A53-12114 89213C 02JAN13.
Back to Boeing 737-7BX