Boeing 717-200
Service difficulty reports · 18,756
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 = '717200' 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 = '717200' 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 DALA2024071006986Battery · inoperativeON SERVICE CHECK FOUND OVERWING EMERGENCY EVACUATION LIGHTS NOT ILLUMINATING. REPLACED OVERWING EMERGENCY EVACUATION LIGHT BATTERY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. LIGHTS NOW ILLUMINATE CORRECTLY. (LP #6026764)SDR DALA2024071006982Cusp Web · corrodedCORROSION ON CUSP WEB STA 397-406 AND X=-59. ORIGINAL THICKNESS 0.020" AND MINIMUM REMAINING THICKNESS 0.003", THEREFORE IT IS OUT OF LIMITS PER B717-200 SRM 53-00-55-1A PROCEDURE 1 ALLOWABLE DAMAGE 1. SUMMARY OF NRC 00690: CORROSION LEVEL 2. CUSP WEB STA 397-SDR HALA20240709033Seal · leakingATB -AFTER GEAR RETACTION IN LOUD SOUND FROM NOSE GEAR FOLLOWED BY DISSARM SPOILER MESSAGE. THE CLIMB/RECORD NLG STRUT.REPLACED NLG STRUCTSEALS PER AMM 32-21-01.NLG REQUIRES INSTALLSTARTING @3.AOF AMM32-21-01-400-801.INSTALLED NOSE SHOCK STRUT CYLINDER PER AMMSDR DALA2024071006987Skin · puncturedON WALKAROUND FOUND PUNCTURE IN SKIN AT STATION Y256 BETWEEN LONGERONS L18 AND L17. REMOVED THE PUNCTURED REPAIR SKIN AT FR 229-FR245 BETWEEN STGR L16L & L18L PER B717 SRM 51-40-02. C/W HFEC OF DAMAGED AREA. NO CRACK INDICATIONS. FABRICATED AND INSTALLED SKIN SDR DALA2024070806854Battery Pack · no testTHE AFT LEFT AND AFT RIGHT OVERWING EXIT LIGHTS (LOWER) ARE INOPERATIVE. DISCONNECTED R5-4255A FOR T/S. RE-CONNECTED R5-4255A AND REPLACED BATTERY POWER SUPPLY AND BATTERY ASSEMBLY B5-119 PER B717 AMM 33-51. ALL CHECKS ARE GOOD.SDR DALA2024070806852Skin · crackedCRACK ON INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW CUTOUT AREA. INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW CUTOUT AREA WAS REPAIRED PER B717-200 SRM 56-10-02-2R REPAIR 1.SDR DALA2024070806853Battery Pack · no testTHE FLIGHT COMPARTMENT EMERGENCY FLOOD LIGHT, L2-785, DOES NOT ILLUMINATE IN EMERGENCY LIGHT TEST. REPLACED EMERGENCY LIGHT BATTERY ASSEMBLY REF B717 AMM 33-51-04. OPERATIONAL CHECK WAS GOOD.SDR DALA2024070806851Longeron · crackedCRACK ON LONGERON 2L AT STA Y=1133 ON AFT ACCESORY COMPARTMENT. LONGERON 2L AT STA Y=1133 ON AFT ACCESORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2.SDR DALA2024070506804Bulb · no testAIRCRAFT 9547, TAIL CONE SLIDE EMER LIGHT L2-941 (MIDDLE BULB OF 3) DOES NOT ILLUM IN EMER LTS TEST. CORRECTIVE ACTION: FOUND EMER LIGHT L2-941 MIDDLE BULB HOLDER LOOSE AND CORRODED. SECURED AND CLEANED HOLDER REF B717 SWPM 20-10-10. (LP 5943933)SDR DALA2024070506805Battery Pack · no testAIRCRAFT 9511, DURING SVC CHECK FOUND MID CABIN EMER LIGHTS INOP.CORRECTIVE ACTION: REPLACED MID CABIN EMER LIGHTS BATTERY PACK. (LP 6209356)SDR DALA2024070506803Seat Track · corrodedAIRCRAFT 9524, CORROSION ON INB SEAT TRACK X22 STA Y=200 TO STA Y= 218 AT PAX CABIN (W1). CORRECTIVE ACTION: CORROSION LEVEL 2, SEAT TRACK WERE REPAIRED ON X= 22 STA Y= 200 TO STA Y= 294 PER B717-200 SRM 53-20-52-2R PROCEDURE 5, REPAIR 5. (LP 0428722)SDR DALA2024070506802Frame · crackedAIRCRAFT 9502, INITIAL INSPECTION: CRACKED ON CANTED FRAME AFT FACE STA 1200 CANTED, PROJECTION LONG 8LH AFT ACCESSORY COMPARTMENT. CORRECTIVE ACTION: CANTED FRAME AFT FACE STA 1200 CANTED, PROJECTION LONG 8LH AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717-20SDR DALA2024070306744Cusp Web · corrodedCORROSION ON PREVIOUS REPAIR DOUBLERS OF CUSP WEB STA Y=568-577 RH/LH SIDES AND X=55 AT PASSENGER CABIN (CPAX). CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLERS OF CUSP WEB STA Y=568-577 RH/LH SIDES AND X=55 AT PASSENGER CABIN(CPAX) WERE REPLACED PER B717-200 SRMSDR DALA2024070306745Skin · crackedWHILE IN ATL FOR SCHEDULED MAINTENANCE AND DURING ACCOMPLISHMENT OF WORKCARD 5530-01048-02, MAINTENANCE REPORTED CRACK INDICATIONS AT TWO EXISTING FASTENER LOCATIONS IN THE RH FRONT SPAR CAP LAYER FORWARD FLANGE. SUBJECT FASTENERS ARE IDENTIFIED AS HOLE 4 AND SDR DALA2024070306743Frame · crackedCRACK ON CANTED FRAME Y=1200 AND LONG 17R AT AFT ACCESORY COMPARTMENT. CANTED FRAME Y=1200 AND LONG 17R AT AFT ACCESORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1 REPAIR 1.SDR DALA2024070306742Frame · crackedAIRCRAFT 9502, INITIAL INSPECTION: CRACK ON CANTED FRAME Y=1200 AND LONG 17L AT AFT ACCESORY COMPARTMENT. CORRECTIVE ACTION: CANTED FRAME Y=1200 AND LONG 17L AT AFT ACCESORY COMPARTMENT WAS REPAIRED PER SRM 53-00-00-2R PROCEDURE 1 REPAIR 1.SDR DALA2024070306741Frame · crackedAIRCRAFT 9502, INITIAL INSPECTION: CRACK AT FRAME STA 715 AND L27R CANTED KEEL AREA. CORRECTIVE ACTION: FRAME STA 715 AND L27R CANTED KEEL AREA WAS REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. (LP 0425118)SDR DALA2024070206724Frame · crackedCRACKS ON FRAME BTW STA Y=1037 L13L & L14L AT AFT CABIN PAX. FRAME BTW STA Y=1037 L13L & L14L AT AFT CABIN PAX. WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 1 TABLE 203 FIG 201.SDR DALA2024070206725Skin · crackedAIRCRAFT 9567, DURING HCK AT QRO, WHILE PERFORMING THE AFT FUSELAGE AND EMPENNAGE INSPECTION PER WC 5300-2019, A CRACK WAS FOUND AFFECTING THE FUSELAGE SKIN AT Y=1087 AND L-14R. AN EXISTING SKIN SPLICE REPAIR IS ADJACENT TO THE DAMAGE REPORTED. CORRECTIVE ACTISDR DALA2024062906604Seat Track · corrodedAIRCRAFT 9524, CORROSION ON SEAT TRACK AT STA Y=898 X=44.5 AT PAX CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2, SEAT TRACK SECTION BTW STA Y=898 TO STA Y= 935 X=44.5 AT PAX CABIN WAS REPAIRED PER B717 SRM 53-20-52-2R REPAIR 5. (LP 0418906)SDR DALA2024062906603Seat Track · corrodedAIRCRAFT 9567, CORROSION ON INBOARD SEAT TRACK BTW STA= 200 TO STA= 256 UNDER GALLEY 2 AREA RH SIDE W-1 CPAX. CORRECTIVE ACTION: CORROSION ON INBOARD SEAT TRACK BTW STA= 200 TO STA= 256 UNDER GALLEY 2 AREA RH SIDE W-1 CPAX WAS REPAIRED PER B717 SRM 53-20-52-2RSDR DALA2024062906602Skin · damagedAIRCRAFT 9502, INITIAL INSPECTION: ELONGATED HOLES 6 E/A ON PAN AND INTERNAL SKIN ON LH FWD EMERGENCY EXIT DOOR. CORRECTIVE ACTION: HOLES 6 E/A ON PAN AND INTERNAL SKIN ON LH FWD EMERGENCY EXIT DOOR WERE REPAIRED PER ERA 618743-14 REV. ORIGINAL. (LP 0417200)SDR DALA2024062906601Pan · corrodedAIRCRAFT 9524, CORROSION ON PAN DOOR JAMB STA Y=994 TO Y= 954 BTW LONG 24 AND 28 RH AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: CORROSION LEVEL 2, PAN DOOR JAMB STA Y=994 TO Y=954 BTW LONG 24 AND 28 RH WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPSDR DALA2024062906600Longeron · corrodedAIRCRAFT 9502, INITIAL INSPECTION: CORROSION ON LONGERON 25R STA Y=323 AT FWD CARGO COMPARTMENT (C1). CORRECTIVE ACTION: LONGERON 25R STA Y=323 AT FWD CARGO COMPARTMENT (C1) WAS REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2, PAR 5, FIG 201. (LP 041654SDR DALA2024062906599Seat Track · corrodedAIRCRAFT 9567, CORROSION ON CENTER SEAT TRACK BTW STA= 200 TO STA= 256 UNDER GALLEY 2 AREA RH SIDE W-1 CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2. SECTION CENTER SEAT TRACK BTW STA= 200 TO STA= 256 WAS REPLACED PER B717-200 SRM 51-41-01-0G AND SRM 53-20-52-2R SDR DALA2024062906598Longeron · crackedAIRCRAFT 9567, INITIAL INSPECTION: CRACK ON LONGERON END L2R AND STA 1133 ALSO BRACKET SUPPORT LOWER SECTION CANTED BULKHEAD 1103 RH SIDE AFT ACCESORY COMPARTMENT. CORRECTIVE ACTION: CRACK ON LONGERON END L2R AND STA 1133 WAS REPAIRED PER B717-200 SRM 53-00-05SDR DALA2024062706576Angle · crackedAIRCRAFT 9567, CORROSION ON LOWER CUSP ANGLE FROM STA Y= 210/212 PROJECTION LONG 18R AT PAX CABIN FLOOR STRUCTURE. W1. CORRECTIVE ACTION: CORROSION LEVEL 2. CORROSION ON LOWER CUSP ANGLE FROM STA Y= 210/212 PROJECTION LONG 18R AT PAX CABIN FLOOR STRUCTURE WAS SDR DALA2024062706575Longeron · crackedAIRCRAFT 9502, INITIAL INSPECTION: CRACK ON LONGERON 6R, LONGERON 4L AND LONGERON 5L ON STA Y=1022 AT AFT CABIN PAX. CORRECTIVE ACTION: LONGERON 6R, LONGERON 4L AND LONGERON 5L ON STA Y=1022 AT AFT CABIN PAX WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURESDR HALA20240628032Autothrottle Sys · faultedREJECTED TAKEOFF AUTO THROTTLE FAIL TO ENGAGE ON TAKEOFF. PERFORMED BITE TEST ON FCC 1 & 2 NO FAULTS NOTED PER TASK 22-31-804 PLACARD REMOVED AND MIC CLEARED OK FOR SVC.SDR DALA2024062706578Skin · crackedAIRCRAFT 9508, WHILE ACCOMPLISHING HFEC INSPECTION PER WORK CARD 5530-01048-02 IN COMPLIANCE WITH FAA AD 2018-10-08, MTC FOUND THREE (3) FASTENER HOLES IN THE VERTICAL STABILIZER LEADING EDGE SKIN (P/N 5910189-15) BELOW ZFS 52.267 WITH CRACK INDICATIONS. THE DSDR DALA2024062706574Skin · crackedAIRCRAFT 9502, INITIAL INSPECTION: CRACK (2EA) ON ANGLE AND INTERNAL SKIN ON LOWER AFT CORNER AT EMERGENCY EXIT DOOR FWD LH. CORRECTIVE ACTION: INTERNAL SKIN ON LOWER AFT CORNER AT EMERGENCY EXIT DOOR FWD LH WAS REPAIRED PER B717-200 SRM 52-20-02-2R PROCEDURE SDR DALA2024062706573Fitting · corrodedAIRCRAFT 9524, CORROSION ON MAIN FRAME FITTING STAY=560 L18L AT PAX CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2. MAIN FRAME FITTING STAY= 560 L18L AT PAX CABIN WAS REPLACED PER B717 SRM 51-41-01-0G AND SRM 51-41-05-0G. (LP 0414381)SDR DALA2024062606519Battery Pack · inoperativeTHE EMERGENCY LIGHT IN CEILING PANELS FROM ROW 2 TO ROW 11 ARE INOPERATIVE. MAINTENANCE FOUND THE EMERGENCY BATTERY #5 B5-227 TO BE INOPERATIVE PER B717 FRMFIM 33-50. THE #5 EMERGENCY BATTERY WAS REPLACED PER AMM 33-51. OPERATIONAL CHECK WAS GOOD. NO FURTHER DSDR DALA2024062606518Skin · crackedCRACK INDICATION NOTED WORKING STEP 12 OF CARD 5530-01048-02 (AD 2018-10-08) WHILE PERFORMING OPEN HOLE HFEC. RH STAB L/E CRACK INDICATION IN SKIN LAYER ONLY. COMPLIED WITH N/R CARD 001 AND ER/A 619015-14AD REV ORIGINAL SECTION I PERMANENT REPAIR.SDR DALA2024062706579Hpc · damagedSHIP 9538 -ATO- ABORTED TAKEOFF AT APPROXIMATELY 80 KNOTS DUE TO SUSPECTED RIGHT ENGINE SUSPECTED COMPRESSOR STALL. CORRECTIVE ACTION: PERFORMED BORESCOPE INSPECTION AND FOUND DAMAGE TO 3RD AND 4TH STAGE HPC. REPLACED RIGHT ENGINE. (LP 5271438)SDR DALA2024062706577Skin · damagedAIRCRAFT 9567, FUSELAGE/SKIN/L1 DOOR GUST LATCH/CUTOUT/EDGE DAMAGE REPAIR. CORRECTIVE ACTION: ACCOMPLISH ER/A 618643-14 SECTION II INSPECTION WITHIN EVERY 8000 CYCLES AFTER ACCOMPLISHMENT OF SECTION I REPAIR. (LP 0413016)SDR DALA2024062706572Skin · crackedAIRCRAFT 9567, CRACK ON DOOR SKIN ADJACENT TO EXTERNAL DOOR HANDLE HOUSING AT LEFT PASSENGER ENTRANCE DOOR. SUMMARY OF NRC SERIAL 00370: DUE TO SEVERAL DAMAGE ON FWD PASSENGER DOOR (L1) WILL BE REPLACED WITH SERVICEABLE DOOR; PER TRACKING PURPOSE ONLY; FWD PASSDR DALA2024062606514Skin · gougedGOUGE WAS FOUND ON SKIN BS 1013. THE SKIN WAS REPAIRED IAW SRM 53-02-01-2R REP 1 PAR 5.B(5)(C) FIG 202 SHEET 15. PERFORMED VISUAL INSPECTION, INITIAL AND REPETITIVE, EVERY 8,000 CYCLES PER B717-200 SRM 53-02-01-2R PROCEDURE 1, REPAIR 1, STEP 6.A, TABLE 202. MSDR DALA2024062506491Web · nickedNICK ON MEMBRANE WEB BTW STA Y=172/173, AND X46 APROX AT CABIN PAX. SUMMARY OF NRC 00434: MEMBRANE WEB BTW STA Y=172/173, AND X46 APROX AT CABIN PAX WAS REPAIRED PER B717-200 SRM 51-70-10-2R-2 REPAIR 2. (LP #0411983)SDR DALA2024062506490Cusp Web · corrodedCORROSION OUT OF LIMITS ON CUSP WEB BTW STA Y=739-745 AND X=59 AT PASSENGER CABIN. SUMMARY OF NRC 00744: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER ON CUSP WEB BTW STA Y=739-745 AND X=59 AT PASSENGER CABIN WAS REPLACED PER B717-200 SRM 53-00-55-2R-4 PAR 5 FIGUSDR DALA2024062506489Longeron · corrodedCRACK ON LONGERON 6L STA Y=1022 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00544: LONGERON 6L STA Y=1022 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 AND 51-41-05-0G. (LP #0411816)SDR DALA2024062506488Longeron · corrodedCORROSION OUT OF LIMIT ON LONGERON END STA Y 1002 LONG 26 RH AT AFT CARGO COMPARTMENT. C2. SUMMARYOF NRC 00857: CORROSION LEVEL 2. LONGERON END ON STA Y 1002 LONG 26 RH AT AFT CARGO COMPARTMENT C2 WAS REPLACED PER B717 SRM 51-41-05-0G PAR 8. (LP #0411089)SDR DALA2024062406344Skin · crackedCRACK ON INTERNAL SKIN NEAR TO ANGLE, BEAM 1, AT LH FWD OVERWING EMERGENCY EXIT DOOR. SUMMARY OF NRC 00307: INTERNAL SKIN NEAR TO ANGLE, BEAM 1, AT LH FWD OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER B717-200 SRM 52-20-02-2R-1, CATEGORY A REPAIR. (LP #0409764SDR DALA2024062406343Cusp Web · crackedCRACKS WERE FOUND ON MEMBRANE OF PASSENGER CABIN AT CUSP WEB BTW STA 218/237 AND BTW STA X=-56/-22. SUMMARY OF NRC 00678: CUSP WEB BTW STA 218/237 AND BTW STA X=-56 /-22 WAS REPAIRED PER B717 53-00-55-2R-4 CONFIGURATION 7015 FIG 210 PAR 40 AND 51-41-02-0G. (LPSDR DALA2024062406342Floorbeam · crackedELONGATED HOLE ON FLOOR BEAM, STA 1022 BTW X=22 TO X=44 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00701: ELONGATED HOLE ON FLOOR BEAM, STA 1022 BTW X=22 TO X=44 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 2 REPAIR 2. (LP #04SDR DALA2024062406341Beam · crackedCRACK ON BEAM #2 STA Y=196 APROX IN PASSANGER DOOR (L1) AT CABIN PAX. SUMMARY OF NRC 00090: AREA ON BEAM #2 STA Y=196 IN PASSANGER DOOR L1 AT CABIN PAX WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 8 REPAIR 8. (LP #0406350)SDR DALA2024062406340Hinge Fitting · damagedELONGATED HOLE AND DAMAGED BOLT WAS FOUND AT RH FLAP HINGE #3. SUMMARY OF NRC 00776: ELONGATED HOLE AND DAMAGED BOLT AT RH FLAP HINGE #3 WAS REPAIRED PER PRI 617866-14 REV 1 & ER/A PRI 617866-14 REV ORIG. DTE REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM MAY 18SDR DALA2024062406339Frame · crackedA.D. CRACK WAS FOUND ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=715.000 RH IN REFERENCE CARD 5310- 01436-01D JOB# 082-0004. (SM) SUMMARY OF NRC 00508: OVERWING FRAME AT STA Y=715 WAS REPLACED PER CARD 5310-01436-03B AND B717-200 SRM 51-41-SDR HALA20240621031Power Supply · no testOVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLCAED OVERWING EMERGENCY LIGHTS POWER SUPPLY PER AMM 33-51-05. OPS CHECK GOOD. OK FOR SERVICESDR DALA2024062106297Longeron · crackedCRACK ON LONGERON 8L STA Y=1022 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00543: LONGERON 8L STA Y=1022 AT PASSENGER CABIN (CPAX) WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 FIG. 201. (LP #0404336)
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