Boeing 717-200
Service difficulty reports · 18,771
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 DALA2023022201322None · noneCORROSION ON L-22LH, Y STA 845 AT FILLET FAIRING STRUCTURE. SUMMARY OF NRC 00277: CORROSION LEVEL 2. LONGERON STA 845 STR 22LH WAS REPLACED PER DWG 5911420 REV: AE AND B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2636166)SDR DALA2023022201321None · noneSECONDARY NRC, IN REF NRC 00618: CORROSION ON MEMBRANE ON WEB BTW STA Y=180 - 200 UNDER OF FLOOR SUPPORT RH. SUMMARY OF NRC 00650: CORROSION LEVEL 2. REPAIR OF MEMBRANE ON WEB BTW STA Y=180 - 200 UNDER OF FLOOR SUPPORT RH WAS PERFORMED PER B-717 SRM 53-00-55-2SDR DALA2023022001259None · noneSECONDARY NRC IN REF NRC #00493: SEVERAL DINGS ON DIAPHRAGM AT STA Y=176, BTW (-X)=15 TO (-X)=42. SUMMARY OF NRC 00660: DINGS ON DIAPHRAGM AT STA Y=176, BTW (-X)= 15 TO (-X)=42 WERE REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 2 REPAIR 2. (LP #2636349)SDR DALA2023022001258None · noneCRACK ON CUSP MEMBRANE WEB AT STA 696 L-18 LH. SUMMARY OF NRC 0209: CUSP MEMBRANE WEB WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIGURE 203. (LP #2636060)SDR DALA2023022201327None · noneFOUND OVER WING INTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE #7 EMERGENCY LIGHT BATTERY POWER SUPPLY, LOCATION 685R, PER B717 AMM 33-51. OPERATION CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (LP #4026293)SDR DALA2023022001257None · noneA.A. A.D. CRACK WAS FOUND OF 0.437" LENGTH ON FRAME STA Y=715 RH SIDE IN REF CARD 5310-01436-04D JOB #074-0004 STEP: 13. SUMMARY OF NRC 00329: FRAME STA Y=715 RH SIDE WAS REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05-0G IN REF. A.A. WORK CARD: 5310-01436-03B.SDR DALA2023022001256None · noneCORROSION ON FLOOR SUPPORT X=20 STA Y=236 PASSENGER CABIN (W1). SUMMARY OF NRC 00531: CORROSION LEVEL 2. FLOOR SUPPORT X=20 STA Y=236 PASSENGER CABIN (W1) WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2633854)SDR DALA2023022201320None · noneLONGERON TEMPORARY REPAIR INSTALLED AT 25R BETWEEN STA 1022 AND STA 1042. COMPLIED WITH LONGERON SPLICE REPAIR PER B717 SRM 53-00-05-2R REPAIR 2 LONGERON REPAIR. A/C WAS DAMAGED BY BELTLOADER ON 13FEB22, REF LOG PAGE 9046786. (LP #2633018)SDR DALA2023022001260None · noneSHIP 9512 -ATB/GEAR/DE- DURING CLIMB OUT AFTER TAKEOFF, THE RIGHT MAIN LANDING GEAR "UNSAFE" LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE CREW COMPLIED WITH THE QRH AND ATTEMPTED ANOTHER RETRACTION. WHEN IT WAS DETERMINED THAT THE RIGHT LANDING GEAR WSDR DALA2023022001255None · noneWEAR ON CABLE TAIL CONE ASSEMBLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY NRC 00290: CABLE TAIL CONE ASSEMBLY WAS REPLACED PER B717-200 AMM 53-52-01. (LP #2633730)SDR DALA2023022001254None · noneCRACK ON LONGERON 2RH ON STA Y=1144 AT AFT ACCESSORIES COMPARTMENT (CAT). SUMMARY OF NRC 00414- LONGERON 2RH ON STA Y=1144 AT AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-05- 2R REPAIR 2. (LP #2633164)SDR DALA2023021701234None · noneTHE F/O SIDE EXIT SIGN AT THE EMERGENCY ROW FELL OFF DURING TURBULENCE. MAINTENANCE RESECURED THE EXIT SIGN LENSE COVER AT THE EMERGENCY EXIT ROW CROWN. (LP #8566510)SDR DALA2023021701233None · noneCORROSION ON RH CUSP WEB BTW STA Y=385 AND Y=399, BL (-X)=55 AT CPAX. SUMMARY OF NRC 00649: CORROSION LEVEL 2. RH CUSP WEB BTW STA Y=385 AND Y=399, BL (-X)=55 WAS CUT PER B-717-200 SRM 53-00-55-2R REPAIR 4 FIG.212 SHEET 1 AND 51-41-05-0G. (LP #2632222)SDR DALA2023021701232None · noneIN REF NRC #00492: CORROSION ON RH CUSP WEB BTW STA Y=385 AND Y=399, BL (-X)=55 AT CPAX. SUMMARY OF NRC 00649: CORROSION LEVEL 2. RH CUSP WEB BTW STA Y=385 AND Y=399, BL (-X)=55 WAS CUT PER B-717-200 SRM 53-00-55-2R REPAIR 4 FIG 212 SHEET 1 AND 51-41-05-0G. (LSDR DALA2023021701231None · noneA.A. A.D. CRACK WAS FOUND OF 0.250" LENGTH ON FRAME STA Y=737 RH SIDE IN REF CARD 5310-01439-01D JOB# 094-0004 STEP: 4. SUMMARY NRC 00154: OVER WING FRAME STA Y=737 BTW LONG 8 TO 18 RH WAS REPLACED PER WORK CARD 5310-01439-02B. ASSOCIATED AA 5310-01439 ADDED FSDR DALA2023021701230None · noneCRACK ON INTERCOSTAL FROM STA Y=1002 TO Y=1022 ON PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00584: INTERCOSTAL FROM STA Y=1002 TO Y=1022 ON PASSENGER CABIN FLOOR STRUCTURE WAS REPLACED AND REPAIRED PER B717-200 SRM 53-00-00-2R REPAIR 2, 51-41-02-0G, AND SDR DALA2023021701229None · noneCRACK ON INTERCOSTAL BTW STA 1002 TO STA 1022, X=22 TO X=-22, PASSENGER CABIN. SUMMARY OF NRC 00442: INTERCOSTAL BTW STA 1002 TO STA 1022, X=22 TO X=-22 WAS REPAIRED PER B717-200 SRM 51-70-11-2R-1. (LP #2631096)SDR DALA2023021701228None · noneSEVERAL HIDDEN CRACKS ON RH CUSP WEB UNDER RH SEAT TRACK RBL 44 BTW STA Y=674 AND Y=715 IN REF NRC 00154. SUMMARY OF NRC 00514: RH CUSP WEB UNDER RH SEAT TRACK RBL 44 BTW STA Y=674 AND Y=715 WAS PERMANENTLY REPAIRED PER B717-200 SRM 53-00-55-2 R REP 4 PAR 5 FISDR DALA2023021501184Unknown · unknownCORROSION ON SUPPORT WEB AT STA 579 TO 598 L17 RH FWD CARGO COMPARTMENT. SUMMARY OF NRC 00331: CORROSION LEVEL 2. SUPPORT WEB AT STA 579 TO 598 L17 RH FWD CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2629599)SDR DALA2023022201325None · none"FAA APPROVAL PENDING" FOR ERA 605849-14 REV ORIG. FUSELAGE SKIN / STA 1002-1022 / L-24-L-26 / GROUND DAMAGE SECTION I PERMANENT REPAIR INSTRUCTIONS. SUMMARY SEE NRC 003-0001:0514-2001/005 00005: COMPLIED WITH ER/A PRI 605849-14 REV A PRI REV 0 REPAIR INSTRUCTSDR DALA2023021501183Unknown · unknownCORROSION ON LH CENTER SEAT TRACK X=44 FROM STA Y=200 TO Y=256. SUMMARY OF NRC 00523: CORROSION LEVEL 2. LH CENTER SEAT TRACK AND SPLICE WAS REPLACED ON X=44 FROM STA Y=200 TO Y=256 PER B717-200 SRM 53-20-52-2R-PROCEDURE 5. (LP #2629217)SDR DALA2023021501185Unknown · unknownCORROSION AT LWR FLAP FITTING ATTACH POINTS ON FWD INBD DRIVE FITTING ASSY RH SIDE. REMOVED HINGE FLAP FITTING NONROUTINE CARDS #09 & 01. REMOVED DAMAGE AT HOLE #12 BORE AND #13 BORE AND SPOT FACE WITHIN LIMITS PER B717 OHM 27-50-5 FIG 602. PERFORMED MPI INSPESDR DALA2023021501182None · noneAIRCRAFT FUSELAGE DAMAGED BY BELT LOADER STA 1002 STR 25R. C/W FUSELAGE TEMPORARY SKIN REPAIR STA 1002 STR 25R PER ERA 605962-14 REV A SECTION 1. RII C/W. ASSOCIATED ER/A 14-605962 ADDED FOR AC 9570. (LP #9046786)SDR DALA2023021501181None · noneSECONDARY NRC, IN REF NRC 00488 CORROSION ON LH CUSP WEB BTW STA Y=560 - 579 AND BTW Y=609 TO 617. SUMMARY OF NRC 00612: CUSP WEB LH BTW STA Y=560 TO 579 AND BTW Y=609 TO 617 WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REP. 4 AND 51-41-02-0G. (LP #2SDR DALA2023021501180None · noneCORROSION OUT OF LIMITS ON FLOOR SUPPORT AT STA Y=200 X=-9 TO X=-44. ORIGINAL THICKNESS WAS 0.070 IN AND MINIMUM REMAINING THICKNESS IS 0.045 IN, THEREFORE THE AREA IS OUT OF LIMITS IN REF NRC 00431 AT PAX CABIN (CPAX)(W1). SUMMARY OF NRC 00484: CORROSION LEVESDR DALA2023021501179None · noneIN REFERENCE TO NRC 00066, AFTER REMOTION OF RETAINER SEALS, CRACK WAS FOUND ON PAN STRUCTURE AFT CARGO DOOR, FWD EDGE BTW CL STOP #1 AND CL STOP #2. SUMMARY OF NRC 00511: PAN STRUCTURE AFT CARGO DOOR, FWD EDGE BTW CL STOP #1 AND CL STOP #2 WAS REPAIRED PER B7SDR DALA2023021501178None · noneCOMPLY WITH FUSELAGE SKIN PERMANENT REPAIR STA 1002 TO STA 1022 L-24 TO L-26 PER ER/A 605849-14 REV ORIG. C/W ER/A 605849-14 REV ORIG. PERMANENT REPAIR AND ER/A 605849-14 REV A. RII C/W. ASSOCIATED ER/A 14-605849 ADDED FOR AC 9521. (LP #4025639)SDR DALA2023021501177None · noneCORROSION ON RH INBD SEAT TRACK -X=22 FROM STA Y=200 TO Y=256. SUMMARY OF NRC 00524: CORROSION LEVEL 2. RH INBD SEAT TRACK -X=22 FROM STA Y=200 TO Y=256 WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #2625411)SDR DALA2023021401137Unknown · unknownC/W ERA 605849-14 REV ORIG, FUSELAGE SKIN PERMANENT REPAIR STA 1002 TO STA 1022 L-24 TO L26. SUMMARY NRC 003-0001:0514-2001/001 00001: COMPLIED WITH ER/A PRI 605849-14 REV "0","1","2","3". ALL REPAIR INSTRUCTION STEPS, ENSURE FINALE ER/A 605849-14 REV. ORIG. SSDR DALA2023021401136Unknown · unknownCORRODED DIAPHRAGM ON STA Y=200 X=-22. ORIGINAL THICKNESS WAS 0.020 IN AND MINIMUM REMAINING THICKNESS IS 0.012 IN, THEREFORE IT IS OUT LIMITS IN REF NRC 00424 AT PAX CABIN (CPAX)(W1). SUMMARY OF NRC 00510: CORROSION LEVEL 2. DIAPHRAGM (WEB) ON STA Y=200 X=-22SDR DALA2023021401135Unknown · unknownLONGERON 24R CORRODED FROM STA 1000-1035. SUMMARY NRC 003-0001:0514-2001/002 00002: REPLACED LONGERON REF DAC DWG 5911424. (LP #2625262)SDR DALA2023021401134Unknown · unknownCORRODED FLOOR SUPPORT STA Y=157-200 AND X=44.5, STA Y=180 AND X=12 TO X=38. ORIGINAL THICKNESS WAS 0.070 IN AND MINIMUM REMAINING THICKNESS IS 0.035 IN, THEREFORE THE AREA IS OUT LIMITS IN REF NRC 00434 AT PAX CABIN (CPAX)(W1). SUMMARY OF NRC 00485: CORROSIONSDR DALA2023021401129Unknown · unknownCRACK ON WEB OF FUSELAGE DOOR FRAME, STA. 208, OVER LONGERON 11 LH AND LONGERON 15 LH. (CPAX). SUMMARY OF NRC 00394: WEB OF FUSELAGE DOOR FRAME, STA. 208, OVER LONGERON 11 LH AND LONGERON 15 LH WAS REPAIRED PER B717-200 SRM 53-10-15-2R PROCEDURE 1 REPAIR 1. (LSDR DALA2023021401128Unknown · unknownCORROSION ON ANGLE AT L1 DOOR JAMB (LWR SIDE) BTW STA Y=157 TO 186, BL -X=55 AT CPAX. SUMMARY OF NRC 00476: CORROSION LEVEL 2. ANGLE AT L1 DOOR JAMB (LWR SIDE) BTW STA Y=157 TO 186, BL -X=55 AT CPAX WAS REPLACED PER B717-200 SRM 53-10-51-0I-2 AND 51-41-02-0G. SDR DALA2023021401127Unknown · unknownCRACKS (2EAS, FWD AND AFT SIDES) WERE FOUND ON BEAM 1 DURING THE WORK PROCESS ON NRC 00081 AT L1 PASSENGER DOOR. (PTAS). SUMMARY OF NRC 00487: FWD AND AFT SIDES OF BEAM 1 AT L1 PASSENGER DOOR WERE REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LPSDR DALA2023021401126Unknown · unknownCORROSION IS OUT OF LIMITS AT THE LH CUSP WEB MEMBRANE AT STA 395 X=54 TO X=59. ORIGINAL THICKNESS WAS 0.020 INCHES AND REMAINING THICKNESS AT STA 395 IS 0.008 INCHES. THEREFOR AREA IS OUT LIMITS. REF NRC 00293 AT PAX CABIN (CPAX). SUMMARY OF NRC 00509: CORROSSDR DALA2023021401132Unknown · unknownREMOVED LT OUTER WING FIXED TRAILING EDGE REF ERA 604993-14 REV ORIG SECTION V. BLENDED DAMAGE AREA PER ERA 604993-14 REV A. PERFORMED HFEC OF CUTOUT PER STEP 5 OF ERA 604993-14 REV A SECTION 5. NO CRACK INDICATIONS NOTED. QC2013. FILLER & DOUBLER MADE, DRILLESDR DALA2023021401131Unknown · unknownC/W ERA 597013-14 REV A FUSELAGE SKIN REPAIR AT LAV WASTE VENT. SUMMARY NRC 001-0002:2040-0015/001 00026: COMPLIED WITH ERA 597013-14 REV A FUSELAGE SKIN REPAIR AT LAV WASTE VENT. (LP #2621093)SDR DALA2023021401125Unknown · unknownPUNCTURES (2EA) WERE FOUND ON FLOOR WEB STA Y=128 AND X=17 AT FLIGHT DECK IN REF CARD 2060-1007. SUMMARY OF NRC 00503: WEB STA Y=128 AND X=17 AT FLIGHT DECK WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2. (LP #2622123)SDR DALA2023021401124Unknown · unknownCRACK ON FWD PAN OF FWD CARGO DOOR BTW BEAM 2 AND 3. SUMMARY OF NRC 00294: FWD PAN OF FWD CARGO DOOR BTW BEAM 2 AND 3 WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #2622016)SDR DALA2023021401123Unknown · unknownCRACK ON INTERCOSTAL ON L1 DOOR INTERNAL STRUCTURE (BEHIND OPEN/CLOSURE HANDLE). SUMMARY OF NRC 00315: INTERCOSTAL ON L1 DOOR INTERNAL STRUCTURE (BEHIND OPEN/CLOSURE HANDLE) WAS FABRICATED AND REPLACED PER DWG 9955763 REV. M, B717-200 SRM 51-41-01-0G, 51-41-02SDR DALA2023021401122Unknown · unknownIN REF NRC 00294: CRACK ON FWD PAN OF FWD CARGO DOOR ON BEAM 5. SUMMARY OF NRC 00628: FWD PAN OF FWD CARGO DOOR ON BEAM 5 WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #2621821)SDR DALA2023021401121Unknown · unknownSCRATCH (2 EA) ON DIAPHRAGM STA Y=189 AND X=45 (CPAX) (W1). SUMMARY OF NRC 00423: DIAPHRAGM STA Y=189 AND X=45 WAS PERMANENTLY REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 PAR. 4 FIG. 201 (SHEET 2). (LP #2621668)SDR DALA2023021401120Unknown · unknownCORROSION ON RH TIE TRACK UPPER SURFACES FROM STA Y=900 TO Y=954. SUMMARY OF NRC 0556: CORROSION LEVEL 2. TIE TRACK RH ON STA Y=900 TO Y=954 WAS REPLACED PER B717-200 SRM 51-41-08-0G, 51-41-02 -0G, AND 51-41-01-0G. (LP #2620761)SDR DALA2023021401119Unknown · unknownELONGATED AND BENT HOLE ON RH CUSP WEB STA Y=715 TO 756 X-44 TO X-60 IN REF NRC 00154. SUMMARY OF NRC 00446: RH CUSP WEB STA Y=715 TO 756 X-44 TO X-60 WAS REPAIRED PER B717-200 SRM 53-00-55-2R REP. 4 FIGURE 221. (LP #2620447)SDR DALA2023021401118Unknown · unknownCORROSION ON FLOOR SUPPORT BTW STA 1022 TO STA 1053, X=44.5 LAVORATORY FLOOR STRUCTURE (PAX CAB) (W2). SUMMARY OF NRC 00445: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA 1022 TO STA 1053, X=44.5 LAVORATORY FLOOR STRUCTURE WAS REPLACED PER B717-200 SRM 53-20-51-0I,SDR DALA2023021401117Unknown · unknownSECONDARY IN REFERENCE NRC 496: CORROSION ON LH TIE TRACK UPPER SURFACES FRON STA Y=900 TO Y=1028. SUMMARY OF NRC 00555: CORROSION LEVEL 2. TIE TRACK SECTION FROM Y=900 TO Y=1028 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-01-0G. (LP #2620158)SDR DALA2023021401133Unknown · unknownWORN ON PREVIOUS REPAIR (2EA) OF FWD CARGO DOOR BARRIER LATCHES. SUMMARY OF NRC 00547: REPAIR DOUBLERS WERE REPLACED PER ER/A 559579-14MA REV ORIGINAL, SECTION I. PERMANENT REPAIR ASSOCIATED ER/A 14-559579 ADDED FOR AC 9553. (LP #2618071)SDR DALA2023020800983Not Reported · not reportedSECONDARY NRC 00428: FLOOR SUPPORT STA Y=180 AND X=-9 TO X=-43 HAS CORROSION. ORIGINAL THICKNESS IS 0.070 IN AND MINIMUM REMAINING THICKNESS IS 0.020 IN, THEREFORE THE AREA CORROSION IS OUT LIMITS AT PAX CABIN. (CPAX)(W1). SUMMARY OF NRC 00489: CORROSION LEVELSDR DALA2023020800982Not Reported · not reportedCORROSION ON FLOOR SUPPORTS (3 EA) STA Y=196 TO 200 FROM X=16 TO X=55.5 AT PAX CABIN FLOOR STRUCTURE. CPAX. SUMMARY OF NRC 00435: CORROSION LEVEL 2. FLOOR SUPPORTS (3 EA) AT STA Y=196 TO 200 FROM X=16 TO X=55.5 WERE REPLACED PER B717-200 SRM 51-41-05 PAR 8, 51
Back to Boeing 717-200