Boeing 737-247
Service difficulty reports · 1,009
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 = '737247' 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 = '737247' 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 DL73E971453Skin · gougedTHE FUSELAGE SKIN AT STA 490 WAS FOUND DAMAGED AT THE LAP SPLICE AT STRINGER 26R. THE DAMAGE CONSISTED OF A GOUGE THAT PENETRATED THE UPPER SKIN AND BONDED DOUBLER OF THE OVERLAPPING SKIN IN THE SPLICE AREA. THE OVERLAPPED SKIN WAS UNDAMAGED. DAMAGE REMOVALSDR 97ZZZX3397Bulb · failedLEFT EXTERIOR OVERWING EMERGENCY LIGHT 1 EACH OF 2 LIGHT BULBS INOPERATIVE. REPLACED LIGHT BULB IAW BOEING 737 MM 33-51-22. OPS CHECK NORMAL. (X)SDR DL73E971308Prox Sensor · out of adjustUPON GEAR EXT, THE NOSE GEAR DOWN GREEN LIGHT FAILED TO ILLUMINATE. RED LIGHTS NML DURING EXT AND REMAINED OUT AFTER GEAR EXT. REQUIRED MISSED APPROACH. RECYCLED GEAR AND GOT NML INDICATIONS ON EXT. CHECKED NOSE GEAR THROUGH VIEWER APPROACH AND LANDING NMLSDR DL73E971259Bearing · failedSTAB TRIM JAMMED IN FLT AT 2 DEGS NOSE DOWN TRIM. FOUND CROSSOVER SHAFT AND BEARINGS SEVERLY DAMAGED. REPLACED SHAFT, BEARINGS AND STAB TRIM SPROCKET PER M/M, CKS NML.SDR USVA69702Accy Gear Box · failedNR 2 ENGINE OIL QUANTITY DROPPED TO ZERO AND WHEN OIL PRESSURE DROPPED BELOW RED RADIAL ENGINE WAS SHUT DOWN. OIL TEMP WAS NORMAL. SINGLE TIME WAS ABOUT TEN MINUTES. WITH ENGINE SHUT DOWN ABOUT 10 PSI WAS NOTED ON GAUGE. TROUBLE SHOT NR 2 ENGINE, REMOVED ASDR DL73E971226Skin · gougedA GOUGE WAS FOUND IN THE SKIN AT STA 1088 BETWEEN STR 8 AND 9R. THE DAMAGE WAS TRIMMED OUT AND REPAIRED WITH AN INTERNAL DOUBLER. THIS REPAIR WAS APPROVED BY FAA/DER FORM 8110-3, DER DESIGNATION SO-889, DATED 06-19-97.SDR DL73E971225Skin · dentedA 4 BY 9 BY .173 DENT AT STA 1006 BETWEEN STR 13R AND 14R. THE DENT IS LOCATED AT A LAP SPLICE. THE DENT WAS REPAIRED PER B737 SRM 53-30-3, FIGURE 9. IT IS NOTED THAT THE UPPER ROW OF FASTENERS IN THE UPPER ROW OF THE LAP SPLICE WOULD NOT MAINTAIN 2D EDGE MSDR DL73E971200Generator · overtempNR 1 GEN DISCONNECTED IN FLIGHT DUE TO HIGH OIL TEMP.SDR DL73E971122Fuel Pump Plug · looseFUEL LEAK ON NUMBER ONE ENGINE. FOUND TEST PLUG ON FUEL PUMP FILTER HOUSING BACKED OUT. SECURED, SAFTIED SYSTEM LEAK CKS GOOD.SDR DL73E971099Oxygen Mask · defectiveJUMPSEAT O2 MASK FITTING WILL NOT SEAT. REPLACED MASK ASSY.SDR DL73E971120Tee Cap · corrosionCORROSION ON UPPER SURFACE OF FS 312 FLOOR. REMOVED LIGHT SURFACE CORROSION PER SRM 51-10-6. REMOVED DAMAGED SECTION OF TEE CAP. FABRICATED REPLACEMENT SECTION PER M/M 53-21-0. INSTALLED REPAIR FROM LBL 25 TO RBL53 PER M/M 53-21-0 COMPLETED INSTALLATION OFSDR P2EA97059Door Frame · crackedPAE - FOUND FLT C-CHECK MAINTENANCE VISIT, FORWARD CARGO DOOR FRAME CRACK INDICATIONS AT FOLLOWING LOCATIONS, FORWARD FRAME BS 440 STRS 21R PLUS 6 INCH, 21R PLUS 8 INCH, TO 22R PLUS 5 INCH STRINGERS 23R PLUS 3 INCH, TO 24R PLUS 6 INCH, 24R PLUS 8 INCH, AND STRSDR P2EA97056Doubler · tornPAE - FOUND C-CHECK MAINTENANCE VISIT, NR 1 ENGINE SLIPPER FAIRING OUTBOARD LATCH DOUBLER TORN. REMOVED AND REPLACED LATCH DOUBLER AND FILLER PER SRM 54-30-2. (M)SDR P2EA97055Fairing · crackedPAE - FOUND C-CHECK MAINTENANCE VISIT, NR 1 ENGINE SLIPPER FAIRING NR 4 AND NR 5 RIBS ARE CRACKED AT OUTBOARD LATCH ATTACH POINT. REMOVED AND REPLACED NR 4 AND NR 5 RIBS ON NR 1 ENGINE SLIPPER FAIRING IAW 51-10-3. (M)SDR P2EA97054Skin · damagedPAE - FOUND C-CHECK MAINTENANCE VISIT, RUDDER LOWER T/E HAD DAMAGE. REPAIRED RUDDER LOWER T/E IAW SRM 51-40-15 AND EWO 970452. RUDDER BALANCED WITHOUT REMOVAL FROM AIRCRAFT IAW SRM 51-80-07. (M)SDR P2EA97052Chord · corrodedPAE - FOUND ON C-CHECK MAINTENANCE VISIT, CORROSION ON PREVIOUS REPAIR ON RT NOSE CHORD, BS 244-250. CORROSION ON PREVIOUS REPAIR WAS OUT OF LIMITS IAW SRM 53-10-1. REMOVED RIGHT NOSE CHORD FROM STATION 227.8 TO 247. FABRICATED NEW NOSE CHORD AND SPLICE, INSDR P2EA97060'T' Bolt · corrodedPAE - DURING C-CHECK MAINTENANCE VISIT, RIGHT MLG 'T' BOLT CORRODED AND MISSING END DOME. REPLACED RIGHT MLG 'T' BOLT PER MM 32-11-42, AND FUNCTIONAL CHECK PER MM 32-32-00. THIS HAS BEEN CLASSIFIED LEVEL 2 CORROSION PER BAC CPCP. (M)SDR P2EA97058Torsion Links · corrodedPAE - FOUND C-CHECK MAINTENANCE VISIT, RIGHT MLG UPPER AND LOWER TORSION LINKS HAVE WORN BUSHING SAT STRUT ATTACH POINTS. REMOVED WHEELS AND BRAKES, DAMPER, UPPER AND LOWER TORSION LINKS. REPLACED UPPER AND LOWER TORSION LINKS. REPLACED UPPER LINK ATTACH BOSDR P2EA97057Rib · chafedPAE - FOUND C-CHECK MAINTENANCE VISIT, NR 1 ENGINE LEFT FORWARD COWL, NR 1 RIB IS CHAFED. CHAFED RIB IS OUT OF LIMIT PER SRM 54-10-1. REMOVED AND REPLACED NR 1 RIB PER SRM 51-30-2 AND 51-10-2. (M)SDR P2EA97051Bracket · crackedPAE - FOUND C-CHECK MAINTENANCE VISIT, NR 2 ENGINE OUTBOARD FORWARD COWL, FORWARD HORIZ LATCH ATTACH BRACKET IS CRACKED. REMOVED NR 2 ENGINE OUTBOARD FORWARD HORIZ LATCH ATTACH BRACKET, FABRICATED, TREATED, INSTALLED NEW ATTACH BRACKET IAW SRM 54-10-1. (M)SDR P2EA97035Aileron · damagedPAE - FOUND C-CHECK MAINTENANCE VISIT, RIGHT AILERON HAS SEVERAL DENTS AND CREASES ON LOWER SURFACE. DURING OPEN UP FOR DAMAGE REMOVAL FOUND DELAMINATION AND WATER CONTAMINATION EXCEEDING REPAIR LIMITS. REPLACED RIGHT AILERON PER MM 27-11-11. (M)SDR P2EA97049Web · corrodedPAE - FOUND C-CHECK MAINTENANCE VISIT, CORROSION ON INBOARD SIDE OF NOSE W/W WEB ABOVE LEFT CHORD BS 251. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED VERT STIFFENER AND REPAIRED FRAME WEB, INSTALLED WET PER SRM 53-30-5 AND 51-10-2. ALODISDR P2EA97048Bracket · misdrilledPAE - FOUND CHECK MAINTENANCE VISIT, PREEXISTING MIS-DRILLED HOLES TWO ON LEFT UPPER TANG BRACKET TO VERTICLE STAB. REPLACED LEFT UPPER AND LOWER TANG BRACKETS IAW MM 51-30-2. (M)SDR P2EA97047Hinge Fitting · brokenPAE - FOUND C-CHECK MAINTENANCE VISIT, LEFT WING AILERON, OUTBOARD HINGE FITTING AT RSS 610 HAS BROKEN FLANGE ON CORNER OF THE FITTING. REMOVED DAMAGED AND REPAIRED IAW EWO 97-0473. (M)SDR P2EA97053Skin · crackedPAE - FOUND C-CHECK MAINTENANCE VISIT, SKIN CRACK INDICATION NOTED AND MARKED, BS 540, 2 INCH ABOVE STRINGER 24L, FORWARD FASTENER. INSTALLED FREEZE PLUGS AT IN SKIN AT NOTED CRACK INDICATION, BS 540, 2 INCH ABOVE STRINGER 24L. FABRICATED REPAIR STRAP AND INSDR P2EA97050Cowl · crackedPAE - FOUND C-CHECK MAINTENANCE VISIT, NR 1 ENGINE NOSE COWL ANTI-ICE TUBE CUTOUT IS CRACKED. REMOVED NOSE COWL, ROUTED TO SHOP FOR REPAIRS, WORK ACCOMPLISHED PER WORK ORDER 217255-Z-5, FAA 8130-3/46001, REINSTALLED NOSE COWL PER MM 71-11-31A. (M)SDR P2EA97043Brace · corrodedPAE - FOUND C-CHECK MAINTENANCE VISIT, HORIZONTAL STABILIZER HINGE HOUSING LEFT UPPER THRUST BRACE IS CORRODED. REMOVED, REPLACED HORIZONTAL STABILIZER HINGE HOUSING LEFT UPPER THRUST BRACE IAW MM 55-10-10. INSTALLED BUSHINGS IAW OHM 55-10-5. THIS HAS BEEN SDR P2EA97042Stiffener · corrodedPAE - FOND C-CHECK MAINTENANCE VISIT, CORROSION ON VERTICLE STIFFENER, AFT SIDE OF FRAME, BS 243 STRINGER 24 RIGHT. REMOVED CORROSION ON VERTICLE STIFFENER, BS 243, STRINGER 24 RT, AREA REMOVED BEYOND LIMITS PER SRM 53-10-1. REPLACED STIFFENER PER SRM 51-10-SDR P2EA97046Web · wornPAE - FOUND C-CHECK MAINTENANCE VISIT, NR 1 ENGINE FORWARD WEB OF PYLON WORN THROUGH FROM SLIPPER FAIRING. REMOVED FORWARD WEB AND REPLACED WITH NEW WEB PER SRM 51-30-02 ON NR 1 ENGINE PYLON. (M)SDR P2EA97045Brace · corrodedPAE - FOUND C-CHECK MAINTENANCE VISIT, HORIZONTAL STABILIZER HINGE HOUSING RIGHT UPPER THRUST BRACE IS CORRODED. REMOVED, REPLACED HORIZONTAL STABILIZER HINGE HOUSING RIGHT UPPER THRUST BRACE IAW MM 55-10-10. INSTALLED BUSHINGS IAW OHM 55-10-5. THIS HAS BEESDR P2EA97044Brace · corrodedFOUND C-CHECK MAINTENANCE VISIT, HORIZONTAL STABILIZER HINGE HOUSING RIGHT LOWER THRUST BRACE IS CORRODED. REMOVED, REPLACED HORIZONTAL STABILIZER HINGE HOUSING RIGHT LOWER THRUST BRACE IAW MM 55-10-10. INSTALLED BUSHINGS IAW OHM 55-10-5. THIS HAS BEEN CLASSDR P2EA97041Splice · corrodedPAE - FOUND C-CHECK MAINTENANCE VISIT, WHILE WORKING N/R 0217 DISCOVERED STRINGER SPLICE, TO BE CORRODED AND CRACKED, BS 912, STRINGER 24 LEFT. REMOVED CORRODED STRINGER SPLICE, BS 904 TO 912 STRINGER 24 LEFT. INSTALLED NEW STRINGER SPLICE BS 904 TO 912 STRISDR P2EA97040Support · crackedPAE - FOUND C-CHECK MAINTENANCE VISIT, NON-ROUTINE WRITE-UP, WHILE WORKING (962753A062-R) DISCOVERED CRACKED FLOOR SUPPORT AT BS 663.75, RBL 60, WL 208. REMOVED CRACKED FLOOR SUPPORT FROM BS 52-672, RBL 60, WL 208. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40 ASDR DL73E970887Hsi · failedIN CRUISE, CAPTS HSI SPUN 360 DEG AND ENDED UP 180 DEG OUT, ACCOMPANIED BY ELECT SMELL AND C/B POPPING. EMERGENCY DECLARED AND A/C DIVERTED. REPLACED CAPTS HSI, OPS CHECKS NORMAL.SDR DL73E970882Oven · failedF/A REPORTED, BLUE SMOKE FROM FWD GALLEY OVEN. FLIGHT CREW SMELLED BURNING RUBBER SMELL. OVENS WERE ON. F/A REPORTED CRACKLING NOISE BEHIND OVEN. C/A REPLACED OVEN. WIRING OK. CKS NORMAL.SDR P2EA97033Carriage · brokenPAE - DURING C-CHECK MAINTENANCE, FOUND LEFT OUTBOARD FLAP INBOARD CARRIAGE BROKEN AT AFT SPINDLE. REMOVED AND REPLACED CARRIAGE ASSEMBLY. FLAPS TO BE RIGGED IAW MM PROCEDURES AS PART OF C-CHECK ACCOMPLISHMENT. (X)SDR DL73E970833Bulkhead Web · crackedTHREE CRACKS WERE DISCOVERED ON THE FWD FACE OF THE FS 178 BULKHEAD WEB. TRIMMED OUT CRACKS; 0.050 2024-T3 DOUBER, FILLER AND SHIMS AS REQUIRED; DTA ANALYSIS AT 60,000 CYCLES.SDR DL73E970807Power Supply · inoperativeAFT LEFT SERVICE DOOR EMERGENCY SLIDE ILLUMINATION LIGHT INOP. REPLACED M1197 EMERGENCY LIGHT POWER SUPPLY.SDR DL73E970834Floorbeam · crackedSTA 520 HAS DAMAGE ON THE FLOORBEAM, 1.5 CRACK ON BOTH THE LEFT INBD AND RT INBD SEAT TRACK LOCATION. BOTH THE CRACKS ARE IN THE RADIUS AND EXTEND INBD AND OUTBD. THIS IS A GROUP 3 A/C PER S/B 737-53-1120, REV 1. INSPECT FOR CRACKS, REPAIR SIMILAR TO S/B 73SDR DL73E970766Duct · rupturedNR 1 ENG OVERHEAT LIGHT CAME ON AT 1200 MSL, ALL ENG IND NORMAL. WHEN THROTTLE RETARDED LIGHT WENT OUT. FOUND DUCT TO NOSE COWL A/I VLV RUPTURED.SDR CALA9700582Hyd Line · leakingTHE A-SYSTEM HYD PRESSURE AND QTY DROPPED TO ZERO WHILE APPROACHING IAH. THE HYD LOSS WAS ACCOMPANIED BY ILLUMINATION OF BOTH A-SYSTEM PUMP LOW PRESSURE LIGHTS. MANUAL GEAR EXTENSION AND ALTERNATE FLAPS WERE USED AND THE A/C LANDED WITHOUT INCIDENT. MAINTENSDR DL73E970716Bulkhead Web · crackedDURING ACCOMPLISHMENT OF SI 3-69482-12, FOUR CRACKS WERE DISCOVERED ON THE FWD FACE OF THE FS 178 BULKHEAD WEB. THIS ER/A GIVES INSTRUCTIONS TO INSTALL A 0.050 2024-T3 REPAIR DOUBLER.SDR DL73E970644Floorbeam · corrodedAT HMV, THE FS 344 FLOORBEAM WAS FOUND TO BE CORRODED LBL 48 TO RBL 12. THE DAMAGE WAS REMOVED AND AT CAP WAS FABRICATED AND REPLACED PER MM 53-21-0 PG 806.SDR DL73E970643Floorbeam · corrodedAT HMV, THE FLOORBEAM AT FS 312 LBL 12 TO RBL 12 WAS FOUND TO BE CORRODED. THE CORROSION WAS REMOVED PER SRM 51-10-6 AND WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. THE DAMAGED SECTION WAS REMOVED AND A REPAIR FABRICATED AND INSTALLED PER MM 53-21-0.SDR 97ZZZM661Light · inoperativeASSEMBLY NOT PROVIDING POWER TO THE LAMPS. REMOVED AND REPLACED ASSEMBLY. OPS CHECKED NORMAL.SDR DL73E970673Bulkhead · fatiguedDURING INSPECTIONS PER SI 3-69482-12, THE STATION 178 BULKHEAD WAS FOUND CRACKED IN THREE LOCATIONS RBL 5.7, WL 202 LBL 5.7, WL 198, LBL 5.7, WL 202.SDR P2EA97009Ptt Button · dirtyFLT 403 - DEN - EMERGENCY DECLARED, LANDING UNEVENTFUL. NR 2 COMM HEAD PTT (PUSH TO TALK) BUTTON STUCK. LOST BOTH RADIOS ON APPROACH. CLEANED NR 2 COMM HEAD PTT BUTTON, SYSTEM OPERATES NORMAL PER MM 23-21-0. (M)SDR DL73E970444Csd · low oilDURING INITIAL ENGINE RUN-UP FOR TAKEOFF, NR 1 GEN BUS OFF LIGHT ILLUMINATED WITH ASSOCIATED LOSS OF ELECTRICAL POWER. SERVICED NR 1 CSD WITH 2 PINTS OF OIL, RAN NR 1 ENGINE AND CHECKED FOR LEAKS, NONE FOUND. NR 1 GEN OPS OK.SDR DL73E970442Floor Beam · crackedTHE BL ZERO FLOOR BEAM OF THE WING CENTER SECTION IS CRACKED AT F.S. 663. NO CRACKS WERE FOUND IN THE WEB. THE CRACK IS TYPCAL PER BOEING SERVICE BULLETIN 737-57-1210. ER/A 304926-14 AUTHORIZES THE SERVICE BULLETIN REPAIR FOR THIS CONDITION.SDR DL73E970508Floor Beam · corrodedFLOOR BEAM AT STA 344 CORRODED MANY PLACES SPAN - BEAM . TASK NR C53-107-02.
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