CFM International CFM56-3B2
Service difficulty reports · 635
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 engine_model_key = 'CFM563B2' 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 engine_model_key = 'CFM563B2' 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 USAA050355Spar · chippedPIT - Q4 - RUDDER L/E SPAR, .2500 INCH X .1250 INCH DEEP CHIP IN EDGE CHIP, LT L/E SPAR TAB. BLEND OUT REPAIR, HFEC INSPECTION AND VISUAL, SEALED IAW EA 79967. (K)SDR USAA050336Stringer Clip · crackedCLT - Q6 - STRINGER CLIP, .5 INCH CRACK, STATION 706, STRINGER 11R. REPLACED TIE CLIP IAW SRM 51-10-02.SDR USAA050337Stringer Clip · crackedCLT - Q6 - TIE CLIP, .3750 INCH CRACK, STA 827, STRINGER 3R. REPLACED TIE CLIP IAW SRM. (K)SDR USAA050338Attach Angle · crackedCLT - Q6 - ATTACH ANGLE, .250 INCH CRACK, STATION 578 BETWEEN STRINGERS 8R AND 9R. REPLACED ATTACH ANGLE WITH FABRICATED PART IAW DWG.SDR USAA050358Skin · damagedPIT - Q4 - COMP SKIN LT ELEVATOR, 2.5 INCH LENGTH X .125 INCH WIDTH, COMPOSITE DAMAGE, STA 55 AT PANEL CENTER TOP SURFACE LT ELEV. INSTALLED REPAIR PLIES IAW SRM AND EA. (K)SDR USAA050353Skin · chafedPIT - Q4 - SLAT, 8 INCH LONG X 3 INCH WIDE AREA, CHAFED. NR 4 SLAT IB T/E LOWER SKIN SURFACE. INSTALLED FILLER AND INTERNAL DOUBLER, KEY CORE AND TOP DOUBLER, SEALED EDGE AND REFINISHED IAW SRM. (K)SDR USAA050357Skin · delaminatedPIT - Q4 - EXT COMPOSITE SURFACE, .500 INCH AREA OF DELAMINATION, LT ELEVATOR TAB TOP IB CORNER. PREPARED DAMAGED AREA, INSTALLED REPAIR PLYS, HARDWARE, REFINISHED IAW SRM 55-20-01 AND 51-70-05. (K)SDR USAA050356Attach Angle · wornPIT - Q4 - ATTACH ANGLE, 1 INCH X 2 INCH WEAR AREA, BS 1288 AT S2R. FABRICATED NEW ANGLE IAW TYP REP 53-20-05A. (K)SDR USAA050359Support Bracket · corrodedPIT - Q4 - BRACKETS, 1 INCH X 3 INCH CORROSION, 4 BRACKETS. CORROSION; LEVEL 1; TASK C53-107-02 THRESHOLD SUPPORT BRAKETS, FWD DOOR ENTRY FLOOR STRUCTURE. PARTS REPLACED IAW MFG DWG. (K)SDR USAA050352Skin · delaminatedPIT - C5 - SLAT, 3 INCH LONG X 2.5 INCH WIDE - 2 AREAS, DELAMINATION. NR 5 SLAT TOP SURFACE IB AND OB T/E. INSTALED NEW CORE, TOP DOUBLERS, SEAL AND REFINISH IAW SRM. (K)SDR AWXA200500102Tube · backed outPHX - AIR TURN BACK - FLT 0893 - AFTER TAKEOFF AT PHX EN ROUTE FOR SEA WHILE CLIMBING THROUGH FL 230 THE NR 2 ENGINE SPOOLED DOWN TO IDLE, LEVELED OFF AT FL 240, ALL ENGINE PARAMETERS NORMAL EXCEPT ENGINE AT IDLE AND NO RESPONSE TO THROTTLE MOVEMENT, TURNED BASDR SB05014Pmc · faultyIAD - FLT1187 - ON CLIMB-OUT FROM IAD, EN ROUTE TO CLT, THE NR 2 ENGINE SURGED AS N1 ROLLED BACK 10 PERCENT AND BEGAN TO FLUCTUATE 4-5 PERCENT THEREAFTER. AIRCRAFT BEGAN TO YAW AND ROLL. AT 11,000 FEET, CREW DISENGAGED AUTOPILOT BUT PROBLEM CONTINUED. FLIGHSDR USAA050085Threshold · corrodedPIT - Q3 - WEB PLATE, .2500 INCH AROUND, CORROSION; LEVEL 1; TASK NR C53-202-01; AFT CARGO DOOR THRESHOLD AROUND NUT PLATE HOLES. DEFECTIVE PART REPLACED WITH IDENT PART IAW DWG 65-47957 AND SRM 51-40-03. (K)SDR USAA050151Skin · crackedPIT - Q6 - PYLON STRUT SKIN, .7500 INCH CRACK; PYLON STRUT SKIN FOR LT ENGINE, ACCESS PANEL CUTOUT. STOP DRILL OF CRACK AND INSTALLATION AT DOUBLER IAW TYP REP 54-30-07. (K)SDR USAA050200Support Beam · gougedPIT - Q3 - MLG SUPPORT BEAM, .025 DEEP .250 X .125 (4 EA) GOUGE; LT MLG SUPPORT BEAM, LOWER FLANGE AFT EDGE 37 INCHES OB OF IB EDGE. (K)SDR USAA041049Skin · damagedPIT - Q1 - RUDDER SKIN, .1250 INCH X .2500 INCH AREA, DAMAGE, LT SIDE 5.5 INCH FWD OF T/E 62.5 INCH UP FROM BOTTOM. PREPARED DAMAGED AREA, LIGHT SANDING, INSTALLED MULTI LAYERED REPAIR IAW SRM AND EA.SDR USAA050162Bracket · crackedPIT - Q6 - BRACKET, 10 INCHES LONG CRACK; VHF COMM ANT BRACKET, STA 500-500A FWD BAGGAGE PIT; REMOVED AND REPLACED CRACKED BRACKET, BLENDED CORROSION IAW SRM. (K)SDR USAA050161Skin · crackedPIT - Q6 - INNER SKIN, APPROX .5 INCH LONG; MAIN ENTRANCE DOOR AFT SIDE AT NR 7 STOP; INSTALLED DOUBLER IAW TYP REP. (K)SDR USAA050163Keelbeam · crackedPIT - Q6 - KEELBEAM, 1 INCH CRACK; STA540 39R; REPLACED SECTION OF FWD KEELBEAM, SPLICES MFGD IAW TYP REP 53-60-09. (K)SDR USAA050090Frame · crackedPIT - Q6 - FRAME, .0625 INCH CRACK, CRACK RADIATING FROM RIVET AT STA 827S-9R. INSTALLED DOUBLER IAW SRM 53-10-20A. (K)SDR USAA050092Plate · fatiguedPIT - Q6 - MAIN LANDING GEAR FG; INSTALLATION OF REAR SPAR FATIGUE PLATE; INSTALLATION OF REAR SPAR FATIGUE PLATE; LT REAR SPAR UPPER CHORD BETWEEN WBL 150 AND 126. FABRICATED DOUBLER AND INSTALLED IAW EA 79629. (K)SDR USAA050108Skin · crackedPIT - Q6 - SKIN, 2.2500 INCH CRACK; FUSELAGE SKIN AT FWD SVC DOOR CUT OUT AFT; CUT OUT CRACKED AREAS AND INSTALLED REPAIR DOUBLERS IAW SRM 53-10-01 AND EA 79657. (K)SDR USAA050164Intercostal · crackedPIT - Q6 - BAFFLE, 1 INCH CRACK; AFT CARGO BIN STA 927 S-25L; FABRICATED AND INSTALLED NEW BAFFLE IAW SRM. (K)SDR USAA050199Intercostal · burnedPIT - Q3 - INTERCOSTAL UNK SIZE- ARC BURN DAMAGE; GROUND STUD GD 3252, STA 344-360, LBL60 WL 204. REPLACED INTERCOSTAL IAW EA. (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 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 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 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 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 USAA050091Frame · crackedPIT - Q6 - FRAME - .1250 INCH CRACK, RADIATING FROM RIVET HOLE AT STA 907 S-9R. DOUBLER INSTALLED IAW SRM 53-10-20A.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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 USAA050113Floor Support · corrodedPIT - Q6 - FLOOR SUPPORT, 20 INCH X 1.5 INCH AREA, CORROSION; TOP OF FLOOR SUPPORT BETWEEN STA 947-967, RBL 46; DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40-02-1 AND 51-40-03. (K)
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