Boeing 737-301
Service difficulty reports · 4,797
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 = '737301' 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 = '737301' 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 USAA020468Skin · crackedSKIN, RIGHT SIDE STA 727E AT STR 23 RT, CRACKED. CUT OUT DAMAGE, INSTALLED EXTERNAL DOUBLER IAW SRM.SDR USAA020471Skin · crackedSKIN, 2.8 INCH CRACK, RIGHT SIDE STA 727E AT STR 23 RIGHT. CUT OUT DAMAGE, INSTALLED EXTERNAL DOUBLER IAW SRM.SDR AWXA200201158Light · brokenPHX - EEL - FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 LT WAS BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 17 LT, OPERATIONAL CHECK WAS GOOD.SDR USAASB02212Charger · inoperativeIND - MAINTENANCE FOUND THE EMERGENCY EXIT IDENTIFIER LIGHTS FOR THE LEFT OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)SDR USAASB02211Control Panel · faultyALB - FLT 342 - ON APPROACH TO ALB, FROM PHL, CREW REPORTED A BURNING SMELL IN THE COCKPIT. THE NR 1 NAV INDICATIONS ALL FLAGGED AND THE NR 1 NAV CIRCUIT BREAKER POPPED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 NAV CSDR USAASB02210Door · out of rigIND - FLT 338 - ON CLIMB-OUT FROM IND, EN ROUTE TO CLT, THE FORWARD MAIN ENTRY DOOR WARNING LIGHT ILLUMINATED. CREW REPORTED THE HANDLE COMES UP IN FLIGHT WHEN PRESSURIZED AND THE LIGHT WILL GO OFF AND ON AS HANDLE IS PRESSED DOWN TO CLOSED POSITION. FLIGHT SDR USAASB02209Control Cable · out of adjustPIT - FLT 1025 - PREPARING TO LAND AT PIT, CREW RECEIVED THREE GREEN AND THREE RED LANDING GEAR LIGHTS DURING GEAR EXTENSION. CREW RECYCLED GEAR AND RECEIVED NORMAL GEAR INDICATION OF 3 GREEN GEAR LIGHTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SDR USAASB02215Slide · bindingPHL - DURING ANNUAL OPERATIONAL CHECK OF THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE, THE SLIDE HAD DIFFICULTY RELEASING FROM THE COMPARTMENT COVER. AFTER DEPLOYMENT, THE FORWARD UPPER CORNER WAS BOUND UP AGAINST THE DOOR. SLIDE WAS ROLLED AFT AND WOULD NOT SDR USAASB02206Charger · failedIND - MAINTENANCE FOUND THE EMERGENCY LIGHTS FROM SEAT ROW 5 THROUGH THE OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)SDR USAA020463Skin · crackedPIT - FOUND SKIN CRACKED 1.650 INCHES LONG, BETWEEN STATION 727E AND 747 STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. ()SDR USAA020417Elevator · delaminatedPIT - FOUND LEFT ELEVATOR SPLINTERING AND DELAMINATED, STATION 95, 81, 100 INBOARD SIDE. ACCOMPLISHED SKIN AND CORE REPAIRS PER SRM 55-20-01, 51-70-17 AND EA 75277. (M)SDR USAA020438Stringer · crackedPIT - FOUND ANGLE CRACKED .5 INCH, LT SHELF 18A FORWARD OF STATION 727. FABRICATED NEW PART PER BOEING DWG 65-46877. (M)SDR USAASB02203Light · inoperativeIND - MAINTENANCE FOUND THE EMERGENCY LIGHT (ROUND BUTTON LIGHT) ON THE FORWARD CLOSET INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT (ROUND BUTTON LIGHT) ASSEMBLY. OPERATIONAL CHECK GOOD. (M)SDR USAA020418Stringer · crackedPIT - FOUND SHELF CRACKED 1 INCH LONG, AFT END OF RIGHT 18A SHELF, FED OF STATION 727. REMOVED AND REPLACED SHELF PER SRM 51-10-02. (M)SDR USAA020419Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH DIAMETER, S27L AND STATION 336 IN FRAME OF EYE OPENING. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)SDR USAA020421Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED .75 INCH LONG, STATION 357 AND STRINGER 16L. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)SDR USAA020422Stringer · crackedPIT - FOUND STRINGER CRACKED .375 INCH LONG, STRINGER 17R BETWEEN STATION 616-639. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)SDR USAA020423Shear Tie · crackedPIT - FOUND SHEAR TIE CRACKED .5 INCH LONG, SHEAR TIE S2L AT STATION 639. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)SDR USAA020424Frame · crackedPIT - FOUND FRAME CRACKED .375 INCH, STATION 663 AND STRINGER 2L. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE AND STRINGER SPLICES PER EA 74814. (M)SDR USAA020425Clip · crackedPIT - FOUND CLIP CRACKED .5 INCH LONG, STATION 663 STRINGER 10L. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)SDR USAA020426Bracket · crackedPIT - FOUND BRACKET CRACKED .5 INCH LONG, STATION 663 STRINGER 8L AND 9L. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)SDR USAA020427Stringer · crackedPIT - FOUND STRINGER CRACKED .5 INCH LONG, FS 663 STRINGER 4L. REMOVED TIE CLIP, HFEC INSPECTION OF STRINGER AND CLIP PER SRM 51-40-02 AND NDT 0-4-53-10. (M)SDR USAA020428Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH LONG, FS 480 STRINGER 8L AND 9L. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES PER EA 74802-A. (M)SDR USAA020429Frame · crackedPIT - FOUND FRAME CRACKED .125 INCH, STATION 480 STRINGER 8R AND 9R. REMOVED DAMAGED AND INSTALLED REPAIR ANGLES PER EA 74802-A. (M)SDR USAA020432Stringer · crackedPIT - FOUND SHELF WITH 1 INCH LONG CRACK, AFT END OF LEFT 18A SHELF, FORWARD OF STATION 727. REMOVED AND REPLACED 18A SHELF PER SRM 51-10-02. (M)SDR USAA020415Skin · crackedPIT - FOUND LEADING EDGE REMOVABLE SKIN WITH CRACKS, 1 INCH BY 1 INCH AREA BEYOND 25 PERCENT MAXIMUM LIMITS, 14 EACH BLENDED AREAS, LEFT HORIZ STABILIZER LEADING EDGE STATION 86.66-151.75. BLENDED AND POLISHED PER SRM 55-10-01. (M)SDR USAA020420Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED .5 INCH BY 7 INCH AREA, STATION 303 AND 310 AT STRINGER 4L. FABRICATED WEB, STRAP AND T-FITTING PER SRM 53-02-04. (M)SDR USAA020437Stringer · crackedPIT - FOUND ANGLE CRACKED .5 INCH, SHELF 18A RIGHT SIDE JUST FORWARD OF 727. ATTACHED PARTS PER BOEING DWG 65-46877. (M)SDR USAA020439Skin · crackedPIT - FOUND SKIN CRACKED 1.5 INCH, LOWER AFT RADIUS OF FORWARD SERVICE DOOR SKIN CUT OUT FS 32. REPAIRED IAW WITH SRM 53-10-01 AND PER EA 74911 AND 75007. (M)SDR USAA020404Skin · crackedPIT - FOUND SKIN CRACKED 2.25 INCH, STATION 967 STRINGER 21L. CUT OUT DAMAGE, INSTALLED DOUBLER PER SRM 53-00-0 PAGE 206. (M)SDR USAASB02192Safety Switch · failedPIT - FLT 1591 - EN ROUTE, SEVERAL DISCREPANCIES THAT INDICATE THE A/C LOGIC WAS IN GROUND MODE. CB`S WERE NORMAL. AIRCRAFT STARTED TO DEPRESSURIZE AT FL280. NO OFF TIME ON ACARS. NO TCAS. TRANSPONDER WAS REPORTED INOP BY ATC. ENGINE LOW IDLE WAS IN THE SDR AWXA200201044Reveal · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1" CRACK WAS FOUND ON THE R-1 DOOR UPPER AFT INTERIOR REVEAL AT BS 320, RBL 47. MAINTENANCE REMOVED DAMAGED REVEAL AT BS 320, RBL 47; FABRICATED A NEW REPLACEMENT REVEAL AND -9 STRAP; INSTALLED REPAIR PARTS IAW B737-300SDR AWXA200201043Reveal · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1" CRACK WAS FOUND ON THE R-1 DOOR UPPER FORWARD INTERIOR REVEAL AT BS 309, RBL 47. MAINTENANCE REMOVED DAMAGED REVEAL AT BS 309, RBL 47; FABRICATED A NEW REPLACEMENT REVEAL AND -9 STRAP; INSTALLED REPAIR PARTS IAW B737SDR 2003F00062Charger · inoperativeMCO - DURING OVERNIGHT CHECK, WHILE ACCOMPLISHING EMERGENCY LIGHT OPERATIONAL TEST, MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 11 THROUGH 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CSDR F3LA200200359Sill · corrodedDURING C 4 CHECK, CORROSION WAS FOUND ON THE R1 DOOR MOP SILL. INSPECTION, IAW SRM 53-10-15 FOUND THE SILL OUT OF TOLERANCE. NEW SILL WAS INSTALLED IAW SRM 53-10-15 AND SRM 51-40-02.SDR F3LA200200358Housing · wornDURING C 4 CHECK, TRACK HOUSING WAS FOUND TO HAVE A HOLE WORN THROUGH IT CAUSING FUEL LEAK. HOUSING IS LOCATED INSIDE THE WING TANK FOR NR 5 OUT BOARD SLAT TRACK, RT WING STA 497. REMOVED DAMAGED NR 5 OUT BOARD SLAT TRACK HOUSING IN ACCORDANCE WITH THE REQUSDR USAASB02190Landing Gear · malfunctionedDTW - FLT 1904 - IN PREPARATION FOR LANDING AT DTW FROM PHL, AT APPROXIMATELY 1,500 FEET, CREW RECEIVED AN UNSAFE GEAR INDICATION WITH THREE RED AND THREE GREEN GEAR LIGHTS ILLUMINATING. CREW INITIATED A GO-AROUND AND RESET THE GEAR SELECTOR HANDLE DOWN. A NSDR USAASB0219010Landing Gear · malfunctionedDTW - FLT 1904 - IN PREPARATION FOR LANDING AT DTW FROM PHL, AT APPROXIMATELY 1,500 FEET, CREW RECEIVED AN UNSAFE GEAR INDICATION WITH THREE RED AND THREE GREEN GEAR LIGHTS ILLUMINATING. CREW INITIATED A GO-AROUND AND RESET THE GEAR SELECTOR HANDLE DOWN. A NSDR F3LA200200354Skin · corrodedDURING C 4 CHECK, CORROSION WAS FOUND ON THE INTERIOR FUSELAGE SKIN AT BS 500 AND STR 26L. FUSELAGE SKIN WAS ROUTED OUT AND REPAIRED IN ACCORDANCE WITH ENGINEERING AUTHORIZATION EA 53-737-185, SRM 53-00-01 AND SRM 53-30-03.SDR F3LA20020053Skin · corrodedDURING C 4 CHECK, CORROSION WAS FOUND ON INTERIOR SURFACE OF FUSELAGE SKIN AT BS 500, STR 26L. CORRODED AREA WAS ROUTED OUT AND REPAIRED IAW EA 53-737-185, SRM 53-00-01 AND SRM 53-30-3.SDR F3LA200200352Intercostal · corrodedDURING C 4 CHECK, CORROSION WAS FOUND AROUND NUT PLATES ON INTERCOSTAL BETWEEN BS 847 AND BS 867, STRINGERS 25R AND 24R. REPAIR WAS PERFORMED IN ACCORDANCE WITH BOEING DRAWING NUMBER 65-47 AND SRM 51-40-02.SDR AWXA200201008Battery · dischargedFLIGHT CREW REPORTED THE FORWARD HORIZONTAL EMERGENCY FLASHLIGHT BATTERY WAS DEAD. MAINTENANCE REMOVED AND REPLACED THE FORWARD HORIZONTAL EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.SDR F3LA200200361Intercostal · crackedDURING C 4 CHECK, THE UPPER FLANGE OF FLOOR INTERCOSTAL WAS FOUND CRACKED AT BS 344 TO BS 360. REMOVED INTERCOSTAL. FABRICATED UPPER FLANGE OF THE INTERCOSTAL IAW SRM 53-10-51 AND INSTALLED ON INTERCOSTAL IAW SRM 53-30-01. INTERCOSTAL INSTALLED IAW SRM 51-4SDR F3LA200200360Intercostal · corrodedDURING C 4 CHECK, CORROSION WAS FOUND ON THE INTERCOSTAL LOCATED AT BS 867 TO BS 887. INSPECTION REVEALED THE INTERCOSTAL WAS OUT OF LIMITS IAW THE REQUIREMENTS OF SRM 53-60-04. REPLACEMENT PART WAS FABRICATED AND INSTALLED IAW THE REQUIREMENTS OF SRM 53-60-SDR F3LA200200356Panel · corrodedDURING C 4 CHECK, AFT CARGO COMPARTMENT TRANSITION PANEL WAS FOUND TO HAVE CORROSION. INSPECTION OF THE TRANSITION PANEL, IAW THE REQUIREMENTS OF SRM 53-60-53, REQUIRED FABRICATION OF REPAIR PARTS IAW SRM 53-60-53.SDR AWXA200201006Stiffener · crackedDURING C-17 CHECK A 1 3/4 INCH CRACK WAS FOUND ON THE LOWER AFT END OF STIFFENER AT LT WING NR 3 FLAP FAIRING, WS 184.40 TO WS 191.00. MAINTENANCE REMOVED THE DAMAGED STIFFENER AT WS 184.40 TO WS 191.00, FABRICATED A NEW REPLACEMENT STIFFENER, AND INSTALLED RSDR AWXA200201005Stiffener · crackedDURING C-17 CHECK A 1 1/4 INCH CRACK WAS FOUND ON THE FORWARD SIDE OF STIFFENER IN THE ELECTRONIC EQUIPMENT BAY BS 328, LBL 31, WL 205. MAINTENANCE REMOVED THE DAMAGED STIFFENER AT BS 328, LBL 31, WL 205, FABRICATED A NEW REPLACEMENT STIFFENER, AND INSTALLED RSDR F3LA200200329Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR BEAM UPPER CHORD, BS 344. REPAIRED FLOORBEAM PER SRM 53-10-51 AND EA 53-737-184.SDR F3LA200200328Floor Support · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT, BS 328 TO 344, RBL 11. REPLACED FLOOR SUPPORT PER SRM 53-10-01, FIG. 101, 51-40-02 AND EA 53-737-181.SDR F3LA200200327Floor Support · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT, BS 312 TO 328, LBL 12. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 51-40-02, 51-40-02, SOPM 20-41-02 AND EA 53-737-181.
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