Boeing 737-3B7
Service difficulty reports · 4,722
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 = '7373B7' 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 = '7373B7' 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 USAA050112Skin · delaminatedPIT - Q6 - SKIN, 6.5 INCH X 4.5 INCH AREA DELAMINATION; NR 5 SLAT OB END; REMOVED TOP SKIN AND CORE AND REPLACED IAW SRM. (K)SDR USAA050111Skin · delaminatedPIT - Q6 - SKIN, 4 INCH X 4 INCH AREA DELAMINATION; NR 5 SLAT IB END; REMOVED TOP SKIN, CORE, REPLACED CORE AND TOP SKIN IAW SRM 57-70-10. (K)SDR USAA050110Skin · delaminatedPIT - Q6 - SKIN, 4 INCH X 4 INCH AREA DELAMINATION; NR 2 SLAT, OB END; REMOVED TOP SKIN, CORE, REPLACED CORE, TOP SKIN IAW SRM 51-70-10. (K)SDR USAA050109Skin · delaminatedPIT - Q6 - SKIN - CORE, 4 INCH X 4 INCH DELAMINATION, NR 2 SLAT IB END. REMOVED DAMAGE, INSTALLED INTERNAL DOUBLER, CORE, TOP EXT DOUBLER IAW SRM 51-70-10. (K)SDR USAA050107Structure · crackedPIT - Q6 - NR 2 SLAT, .1250 INCH CRACKS (3 EA); LOWER T CHORD AFT ROW OF FASTENERS AT ACTUATOR MOUNT; INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206. (K)SDR USAA050106Intercostal · crackedPIT - Q6 - INTERCOSTAL, .5 INCH CRACK; LT AND RT SIDES OF FWD ATTACH ANGLE AND INTERCOSTAL BELOW CABIN FLOOR STA 254 BL0. MANUFACTURED NEW INTERCOSTAL IAW MFG DWG 65-45833 AND SRM 51-20-01, 51-40-00. (K)SDR USAA050105Frame · crackedPIT - Q6 - FRAME, .2500 INCH CRACK; BS 907 FRAME BETWEEN STRINGERS S-1 AND S-2R. DOUBLERS INSTALLED IAW SRM 53-00-07, FIG 201 WITH MINOR DEVIATION IAW EA 79620. (K)SDR USAA050104Channel · crackedPIT - Q6 - L CHANNEL, 2 INCH LONG BETWEEN NUT PLATES CRACKED; S5A STRINGER LT SIDE STA 1140 TO 1145. REMOVED AND REPLACED STRINGER AND DOUBLERS IAW SRM 53-00-01 AND FIG 221 AND TYP REP 53-80-40. (K)SDR USAA050103Stiffener · crackedPIT - Q6 - STIFFENER; .5 INCH CRACK; FLOORBEAM STIFFENER BS 328, LBL 28. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02 AND MFG DWG. (K)SDR USAA050102Skin · crackedPIT - Q6 - FWD ENT DOOR, .1250 INCH CRACKS (3 EA); INTER SKIN AND FRAME AT NR 6 AFT DOOR STOP AND INTER SKIN AT NR 7 DOOR STOP AFT. INSTALLED DOUBLERS IAW TYP. REP. 52-10-16. (K)SDR USAA050101Skin Panel · chafedPIT - Q6 - SKIN PANEL, .015 INCH X 4 INCH LONG; CHAFED; FWD OF STA 867 TO JUST AFT OF STA 887, STR 2L AND 2R. DOUBLER INSTALLED AND TRIPLER IAW TYP. REP.53-30-02, REV B. (K)SDR USAA050100Frame · damagedPIT - Q6 - FRAME, .1562 INCH IN RADIUS (2 HOLES); STA 440 S-24L (FWD CARGO BIN); INSTALLED FABRICATED REPAIR DOUBLER IAW SRM. (K)SDR USAA050099Structure · crackedPIT - Q6 - AFT CARGO DOOR, .4375 INCH CRACK; BOTTOM OUTER T-CHORD FASTENER HOLE, LOWER AFT END; INSTALLED FABRICATED PART IAW SRM. (K)SDR USAA050098Stiffener · crackedPIT - Q6 - STIFFENER, .5 INCH CRACK; STIFFENER CRACKED BETWEEN S-12R AND S13R AT STA 291. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM AND DWG. (K)SDR USAA050097Frame · crackedPIT - Q6 - FRAME, .2500 INCH LENGTH; FRAME TO SKIN BRACKET AREA IN FRAME STA 360, STR 14R. INSTALLED DOUBLER REPAIR IAW SRM. (K)SDR USAA050096Angle · crackedPIT - Q6 - L ANGLE, 1.2500 INCH CRACK; L ANGLE FOR 360 FRAME AT STR 14L. MANUFACTURED NEW L ANGLE IAW SRM. (K)SDR USAA050095Structure · crackedPIT - Q6 - NR 1 SLAT, .1250 INCH CRACKS-2 EA; LOWER T-CHORD, AFT ROW OF FASTENERS, APPROX 40 INCHES FROM IB EDGE. INSTALLED DOUBLER IAW SRM. (K)SDR USAA050094Strap · crackedPIT - Q6 - STRAP, CRACKED IN HALF, 3 INCH CRACK; LOWER FLOORBEAM STA 312 AND 328 LBBL 12. DEFECTIVE PART REPLACED WITH IDENT PART IAW DWG. AND SRM. (K)SDR USAA050093Skin · crackedPIT - Q6 - RIVET HOLES, .1250 INCH TO .2500 INCH - 7 RIVET HOLES, CRACKED; LWR SKIN AFT FASTENER ROW CENTERED ON SLAT ACT. AREA. INSTALLED DOUBLER IAW SRM 57-43-01.(K)SDR USAA050091Frame · crackedPIT - Q6 - FRAME - .1250 INCH CRACK, RADIATING FROM RIVET HOLE AT STA 907 S-9R. DOUBLER INSTALLED IAW SRM 53-10-20A.SDR USAA050089Floor Support · corrodedPIT - Q3 - FLOOR SUPPORT, 1 INCH X 2 INCH AT 3 AREAS; CORROSION; LEVEL 1; TASK NR C53-107-02, STA 947.5-966 RBBL. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-00.SDR USAA050088Intercostal · corrodedPIT - Q3 - INTERCOSTAL, 1 INCH DIA (4 EA AREAS) CORROSION ; LEVEL 1; TASK NR C53-107-01, RBBL 10 BS 312 TO 328. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02. (K)SDR USAA050087Angle · corrodedPIT - Q3 - ANGLE, 1 INCH DIA. SPOT; EXFOLIATED CORROSION; BS 530, RT AT KEELBEAM, S-27R. KEELBEAM SECTION, -2 DOUBLER, -1 STRAP IAW TYP. REP. 53-60-09.SDR USAA050086Floorbeam · corrodedFLOORBEAM, 1INCH X 1 INCH AREA (2 EA) CORROSION; LEVEL 1; TASK NR C53-107-01, STA 328 FROM RBBL TO IB SEAT TRACK. REMOVED CORRODED SECTION, FABRICATED NEW AND INSTALLED IAW 53-10-51. (K)SDR USAA050084Threshold · corrodedPIT - Q3 - WEB PLATE, .2500 INCH AROUND, CORROSION; LEVEL 1; TASK NR C53-20201, AFT CARGO DOOR THRESHOLD; CORROSION AROUND NUT PLATE HOLES. DEFECTIVE PART REPLACED WITH IDENT PART IAW DWG NR 65-47957. (K)SDR USAA050218ASkin · crackedCLT - FOUND SKIN CRACKED 1.375 INCH, FS 727D STRINGER 23R. INSTALLED DOUBLER IAW SRM 53-00-01. (M)SDR USAA041137Skin · crackedCLT - FOUND SKIN CRACKED 10 INCHES AFT OF STATION 727E BELOW STRINGER 18R AND STATION 749 S19R. INSTALLED DOUBLER IAW SRM 53-00-01. (M)SDR SB04174Charger · failedPHL - MAINTENANCE REPORTED THE RIGHT-HAND CENTER EMERGENCY EXIT SIGN AND THE LEFT-HAND OVERWING EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY POWER SUPPLY AND BATTERY M1160. OPERATIONAL CHECK GOOD.SDR SB04173Wire · brokenPHL - MAINTENANCE REPORTED THE EMERGENCY EXIT AISLE LIGHT AT ROW 19 INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UNDER THE SEAT. OPERATIONAL CHECK GOOD.SDR SB04171Wire · brokenMAINTENANCE FOUND A BROKEN WIRE FOR THE EMERGENCY LIGHT AT SEAT 8ABC. MAINTENANCE REPAIRED BROKEN WIRE. OPERATIONAL CHECK NORMAL.SDR SB04169Logic Card · dirtyALB - FLT1231 - ON APPROACH TO ALB FROM CLT, THE RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED. CREW PERFORMED MANUAL GEAR EXTENSION PROCEDURE AND RECEIVED ALL THREE GREEN GEAR LIGHTS. CREW REPORTED LIGHTS TESTED OK. FLIGHT LSDR USAA040894Tie Clip · crackedPIT - Q5 - STRINGER TIE CLIP, .7500 INCH CRACK, BS 500B, STR 13,LT. FABRICATED IAW MFG DWG 69-45156 AND INSTALLED IAW SRM 51-40-02.SDR USAA041101Strap · corrodedPIT - Q5 - STRAP, WEB, SKIN, 3 INCH X 4 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-208-01, STA 492.5 BTW, 26R, 27R SKIN SECTION. REMOVED CORROSION, INSTALLED FILLER, STRAPS AND DOUBLER IAW EA. (K)SDR USAA041075Skin · crackedPIT - A-CHECK - SKIN, 2 INCH CRACK, STA 760, STR 19R, INSTALLED DOUBLER IAW SRM.SDR USAA041077Skin · delaminatedPIT - WALKAROUND- WING T/E, 8 INCH X 12 INCH AREA, DELAMINATION, UPPER PANEL OB RT FIXED T/E OF WING. REPLACED PANEL IAW SRM AND EA.SDR SB04164Control Unit · faultyATL - FLT1203 - FLIGHT DEPARTED CLT, EN ROUTE TO IAH, WITH THE NR 2 CSD/GENERATOR ON MEL 24-1 FOR LEAKING OIL. AT FL350, JUST PASSING ATL, THE APU OVERSPEED LIGHT ILLUMINATED AND THE APU SHUTDOWN. FLIGHT DIVERTED TO ATL AND LANDED WITHOUT FURTHER INCIDENT. SDR USAA041100Support · crackedPIT - Q05 - SUPPORT, .075 INCH CRACK, AFT CARGO DOOR UPLOCK SUPPORT. REMOVED AND REPLACED SUPPORT IAW SRM.SDR SB04162Battery Pack · dischargedORD - MAINTENANCE REPORTED A FEW OF THE AFT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.SDR USAA041067Frame · corrodedPIT- Q5- FRAME, 1.5 INCH, CORROSION; LEVEL 1; TASK NR C53-208-01, STA 500D, STR 28L FRAME. MANUFACTURED ANGLE IAW MFG DWG 65C22910. (K)SDR USAA041066Mount · corrodedPIT-Q5-LAV MOUNTS, 2 INCHES X 2 INCHES (2 EA) CORROSION; LEVEL 1; TASK NR C53-107-02, STA 913, LBL 21 AND LBL 34. DEFECTIVE PART REPLACED WITH IDENT PART NR. (K)SDR USAA041065Mount · corrodedPIT-Q5-LAV MOUNTS (2), 2 INCHES X 2 INCHES (2 EA), CORROSION; LEVEL 1; TASK NR C53-107-02, STA 994, RBL 21 AND RBL 34. DEFECTIVE PART REPLACED WITH IDENT PART NR. (K)SDR USAA041071Skin · chafedPIT - Q5 - SKIN, 9 INCHES X .5 INCH X .0075 INCH DEEP, CHAFED, RT OF S1 AT STA 867 TO 887. DOUBLER AND TRIPLER REPAIR SCHEME IAW SRM. (K)SDR USAA041069Intercostal · crackedPIT- Q5- INTERCOSTAL, 2 INCH CRACK, IN RADIUS- FLOOR INTERCOSTAL, STA 380, BBL 0. REPLACED SUPPORT ANGLE IAW SRM. (K)SDR USAA041068Skin · corrodedPIT - Q5- SKIN, 1.25 INCH, CORROSION, LEVEL 1; TASK NR C53-208-01, STA 500C + 19 INCH IB OF STR 28L. REMOVED CORROSION IAW SRM. (K)SDR USAA041072Frame · corrodedPIT - Q5 - FRAME, 3 INCH X 3 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-208-01, STA 492.5 BETWEEN STR 27R AND 28R FRAME. INSTALLED DOUBLERS IAW SRM. (K)SDR USAA041070Frame · corrodedPIT - Q5 - FRAME, 1.5 INCH X 1 INCH AREA, CORROSION; LEVEL 1; TASK C53-107-02, FRAME AT STA 993.5, RBL 46. REMOVED CORROSION, PRIMED AND PAINTED ISW SRM. (K)SDR SB04159Odor · detectedPHL - FLT1227, EN ROUTE FROM BTV TO PHL, CREW REPORTED A STRONG OIL SMELL IN CABIN. CREW WAS ABLE TO ISOLATE SOURCE TO LEFT PACK/LEFT ENGINE. FLIGHT LANDED AT PHL WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED FAULT ISOLATION STEPS FROM MM 21-00-01, PROSDR USAA041074Floorbeam · corrodedPIT - Q5 - BEAM, 10 INCH L X 1 INCH WIDE, CORROSION; LEVEL 1; TASK NR C53-107-01, FLOORBEAM SCREW HOLES, STA 312, LBBL 13 TO RBBL13. 22 INCH REPAIR ANGLE WITH 10 INCH X 1 INCH W FILLER IAW SRM. (K)SDR USAA041033Spar · damagedPIT - Q2 - SPAR, .50 INCH X .25 INCH AREA COMPOSITE DAMAGE/ DELAMINATION. LT AILERON L/E SPAR 26 INCHES FROM OB END UPPER FLANGE. REMOVED DAMAGED AREA AND TAPER SANDED FLANGE, INSTALLED REPAIR PLYS IAW EA, SRM.SDR USAA041032Skin Panel · damagedPIT - Q2 - TOP SKIN PANEL, 2 INCH SQ SINGLE LAYER, COMPOSITE DAMAGE, LT AILERON TOP SKIN PANEL AT TAB CONTROL ROD FAIRING MOUNT SURFACE. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, RESTORES FINISH IAW SRM.
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