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.

SDR DALA2018021500939Structure · crackedA CRACK WAS FOUND AT CF 1200, RT FWD SIDE JUST FORWARD OF THE RUDDER HYD SHUTOFF VALVE. REPAIRED IAW ER/A 565689-14, REV ORG.Feb 14, 2018 · N945AT · Boeing 717200 · Vertical StabilizerSDR DALA2018021500905Skate Angle · crackedFOUND A CRACK ON THE FORWARD CANTED FRAME BS 1189, AT THE LEFT SKATE ANGLE. REPAIRED IAW ER/A 565522-14, REV ORG.Feb 14, 2018 · N945AT · Boeing 717200 · Nacelle/Pylon Miscellaneous StructureSDR DALA2018021500904Frame Angle · crackedCRACKED FRAME ANGLE AT BS 1022, LONGERON 7L. THE FRAME ANGLE WAS REPAIRED IAW ETI-17-18-008, REV 1, AND ER/A 565874-14, REV ORIGINAL.Feb 14, 2018 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018021400884Light · inoperativeRIGHT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT IAW AMM 33-50, OPS CHECKED GOOD.Feb 14, 2018 · N997AT · Boeing 717200 · Emergency LightingSDR DALA2018021400883Wire · shortedDURING SLAT RETRACTION, AFTER TAKEOFF RECEIVED A PSEU FAIL CAUTION INDICATION. DURING APPROACH, EXTENSION OF SLATS, DOWN ARROW STAYED ON, THOUGH INTERMITTENT. PERFORMED A NO FLAP, NO SLAT LANDING IAW QRH. REPLACED THE LT SLAT A SENSOR D1-65 IAW AMM 27-84 WFeb 14, 2018 · N896AT · Boeing 717200 · Flight Control System WiringSDR HALA2018021400041Cotter Pin · out of positionAT FLAP POSITION, SLATS EXTENDED 8, FLAPS 13, RECEIVED A DISAGREE 3, & 4 ALERT. DURING TROUBLESHOOTING, FOUND NO CABLE MOVEMENT WHEN SELECTING FLAPS 0 TO 13. FOUND A COTTER KEY ON K-2 DRUM BINDING ON CABLE GUIDE. REPOSITION COTTER KEY. OPS CHECKED GOOD. AFeb 13, 2018 · N477HA · Boeing 717200 · Trailing Edge Flap Control SystemSDR DALA2018021400882Battery Pack · inoperativeDURING CHECK, FOUND THE AFT OVERWING INTERNAL UPPER EMERGENCY EXIT LIGHTS INOPERATIVE FOR BOTH SIDES. MAINTENANCE REPLACED THE BATTERY PACK IAW AMM 33-51. OPS CHECKED GOOD.Feb 13, 2018 · N925AT · Boeing 717200 · Emergency LightingSDR DALA2021122908127Skate Angle · crackedA CRACK WAS FOUND FORWARD OF THE VERTICAL STABILIZER CANTED FRAME AT STA 1189 AT LH SKATE ANGLE ATTACH FASTENER. ACCOMPLISH SECTION II: INITIAL INSPECTION 3800 FLIGHT CYCLES AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR. ACCOMPLISH SECTION III: REPETITIVFeb 11, 2018 · N945AT · Boeing 717200 · Vertical StabilizerSDR DALA2018021100860Frame Angle · crackedCRACK ON THE FRAME ANGLE BS 1022, BETWEEN LONGERONS 16L TO 17L. CRACK WAS FOUND TO BE 0.750 INCH IN LENGTH. REPLACED THE FRAME ANGLE IAW DWG 9912243, REV JS, SRM 51-41-02, AND 51-41-05.Feb 10, 2018 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR HALA2018021200037Packing · odorFOUL ODOR IN COCKPIT AND CABIN FROM PREVIOUS WRITE UPS. OCCURS DURING SLOW AIRSPEEDS, HIGH POWER SETTINGS, SMELLS LIKE PETROLLIUM JELLY OR OIL IN PACKS. REMOVED REPLACED BOTH LT AND RT COALESCER BAGS IAW 21-54-08, PULLED AND COLLARED CIRCUIT BREAKERS U35, &Feb 10, 2018 · N495HA · Boeing 717200 · Air Distribution SystemSDR DALA2018021600979Grill · corrodedCORROSION ON FRAME GRILL R1. THE FRAME GRILL WAS REPAIRED IAW SRM 53-00-00-2R-1, FIG.201.Feb 9, 2018 · N998AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018021000859Frame Angle · crackedCRACK FOUND ON THE ON THE FRAME ANGLE BS 1022 BETWEEN LONGERONS 13R TO 14R. THE CRACK IS 0.250" LONG. REPAIRED IAW SRM 53-00-06-2R-2, FIG 201.Feb 9, 2018 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR HALA2018021200036Unknown · odorSTRONG ODOR IN COCKPIT AND , SMELLS LIKE OIL OR PLASTIC DURING TAKEOFF AND DESCENT, STRONG ODOR. CHECKED TI SENSORS IAW AMM 36-11-07 ON BOTH ENGINES, NO SIGHTS OF OIL OR UNWANTED MATERIAL, RAN BOTH PACKS OFF APU BLEED & COULD NOT DUPLICATE ODOR. REMOVED EXCFeb 9, 2018 · N495HA · Boeing 717200 · Air Distribution SystemSDR DALA2018020900791Access Panel · corrodedCORROSION ON THE ACCESS PANEL. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION III.Feb 8, 2018 · N998AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018020900790Rub Strip · corrodedCORRODED RUB STRIP ON THE RT WING. REPLACED THE RUB STRIP IAW SRM 57-10-01-2R, REP 3, PAR 6.Feb 8, 2018 · N998AT · Boeing 717200 · Wing Miscellaneous StructureSDR DALA2018020900789Structure · corrodedBEHIND THE FORWARD MOUNT OF THE UPPER RIGHT FAIRING, A FASTENER BARREL NUT SHOWED SIGNS OF CORROSION ON THE RIGHT HORIZONTAL STABILIZER. REMOVED THE FASTENER, AND REPAIRED THE BARREL NUT HOLE IAW PRI 565416-14, REV ORG.Feb 8, 2018 · N945AT · Boeing 717200 · Horizontal Stabilizer StructureSDR DALA2018020700755Sign · brokenEXIT SIGN IN FIRST CLASS IS BROKEN. RE-SECURED EXIT SIGN PER AMM 33-22.Feb 7, 2018 · N910AT · Boeing 717200 · Emergency LightingSDR DALA2018020700730Battery Pack · inoperativeTAILCONE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IAW AMM 33-51-03. OPS CHECKED GOOD.Feb 7, 2018 · N955AT · Boeing 717200 · Emergency LightingSDR DALA2018020700729Access Panel · corrodedCORROSION ON THE ACCESS PANEL. REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.Feb 6, 2018 · N998AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018020700728Access Panel · corrodedCORROSION IN THE COUNTERSINK OF THE ACCESS PANEL 520DB. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.Feb 6, 2018 · N998AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018020700727Access Panel · corrodedCORROSION ON THE ACCESS PANEL 520HB. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.Feb 6, 2018 · N998AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018020700726Rub Strip · corrodedCORROSION POINTS ON FUEL ACCESS PANEL RUB STRIP, LT WING. REPLACED IAW SRM 57-10-01.Feb 6, 2018 · N998AT · Boeing 717200 · Wing Miscellaneous StructureSDR DALA2018020700725Cusp Web · crackedCRACKED CUSP WEB, BS 665 TO 684, LBL 44 TO 54. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 222.Feb 6, 2018 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018020500687Frame · crackedUPPER RADIUS OF FRAME TAB AT STA 715.0 FOUND CRACKED REF STEP 13 OF WC 5310-01436-04B 95771310. C/W CARD 5310-01436-02A.Feb 4, 2018 · N895AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018020500649Access Panel · corrodedCORROSION IN THE COUNTERSINK OF THE ACCESS PANEL 520FT. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5,Feb 4, 2018 · N998AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018020500648Access Panel · corrodedCORROSION ON THE COUNTERSINK OF THE FUEL ACCESS PANEL 620EB. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01, REPAIR 2, PAR 5.Feb 4, 2018 · N998AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018020500647Floor Panel · delaminatedDELAMINATED FLOOR PANEL 211ANF. A NEW FLOOR PANEL WAS FABRICATED, AND INSTALLED IAW SRM 53-20-50-2R-3.Feb 4, 2018 · N998AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2018020400645Floor Panel · delaminatedDELAMINATED PASSENGER CABIN FLOOR PANELS #222ARF, 222VF, 221KF, 221AF. NRC 00454: FLOOR PANELS #222ARF, 222VF, 221KF, AND 221AF WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717 SRM 53-20-50-2R-3 AND WERE INSTALLED WITH CARD JIC 2040-0023. (LP #0410341)Feb 3, 2018 · N996AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2018020400644Pan · crackedCRACK ON RING PAN AFT LOWER CORNER BS 908. THE PAN WAS REPAIRED IAW SRM 56-20-02-2R-1, FIG 202.Feb 3, 2018 · N998AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018020400643Pan · crackedCRACK ON RING PAN FWD LOWER CORNER BS 446 . REPAIRED PER B717 SRM 56-20-02-2R-1 FIG 202 . LONG CRACK 0.100" INCH. (LP #0410120)Feb 3, 2018 · N998AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018020400642Former · crackedCRACKED EGDE FORMER BS 694 IN THE KEEL BEAM AREA. THE FORMER WAS REPAIRED IAW SRM 51-70-11, REP 1.Feb 3, 2018 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018020400641Former · crackedCRACKED RT EGDE FORMER BS 679 AT THE KEEL BEAM AREA REPAIRED IAW SRM 51-70-11, REP 1.Feb 3, 2018 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018020300640Frame · crackedCRACK IN UPPER RADIUS OF FRAME BS 674 . REPLACED THE FRAME IAW 5310-01436-03A.Feb 3, 2018 · N953AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018020300639Floor Support · corrodedCORROSION ON FLOOR SUPPORTS Y=150 TO 200 X=-44, Y=150 X=-32 TO X=-44 AND Y=150 X=-44 TO X=-50 PAX CABIN IS OUT OF LIMITS (W1) (AMDS 5300-2010). NRC 00453: LEVEL CORROSION 2, FLOOR SUPPORTS Y=150 TO 200 X=-44, Y=150 X=-32 TO X=-44 AND Y=150 X=-44 TO X=-50 WERE Feb 2, 2018 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018020600724Intercostal · damagedHOLES DAMAGED IN THE INTERCOSTAL, LONGERON 12L, BS 696 TO 715. REPLACED THE INTERCOASTAL IAW SRM 51-41-02.Feb 2, 2018 · N895AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2018020600031Fuel Line · leakingAFTER STARTING APU, NOTICE A STRONG FUEL ODOR, SHUT APU DOWN AND FUEL ODOR WENT AWAY. FOUND FUEL LEAKING FROM APU FCU HARD LINE TO FUEL NOZZLE. REMOVED AND REPLACED FCU HARD LINE PER AMM 49-32-01. LEAK CHK OPS OK. ODOR NO LONGER PRESENT. OK FOR SVC.Feb 2, 2018 · N486HA · Boeing 717200 · APU Engine Fuel and ControlSDR DALA2018020300637Frame · crackedCRACKED NOSE LANDING GEAR WHEEL WELL FRAME. REPAIRED IAW SRM 53-10-14-2R, REP 2, FIGURE 201.Feb 2, 2018 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018020200607Pan · crackedCRACKED PAN 5 BEAM POSITION, ON AFT CUTOUT AT FWD CARGO DOOR INNER STRUCTURE. PAN 5 BEAM POSITION ON AFT CUTOUT AT FWD CARGO DOOR INNER STRUCTURE WAS REPAIRED PER SRM 52-30-02 FIG 201.Feb 1, 2018 · N998AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018020100606Cusp Web · corrodedCORROSION ON CUSP WEB BTW STA Y=465 TO Y=446 AND X=-54 TO X=-60 AT CAB PAX (CPAX). CORROSION LEVEL 2. CUSP WEB BTW STA Y=465 TO Y=446 AND X=-54 TO X=-60 WAS REPAIRED PER SRM 53-00-55-2R-4.Feb 1, 2018 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2018013100028Switch · failedAIR TURNBACK DUE TO CAPTAIN`S TRIM CONTROL INOPERATIVE. ALTERNATE TRIM & FIRST OFFICER TRIM WORKED NORMAL, AUTOPILOT 1 & 2 WOULD NOT CONNECT. REMOVED & REPLACED THE CAPTAIN`S AND FIRST OFFICER`S PRIMARY TRIM SWITCHES S1-321 & S1-322 IAW AMM 27-41-01.Jan 31, 2018 · N495HA · Boeing 717200 · Stabilizer Position IndicatingSDR DALA2018020100587Pan · crackedCRACKED PAN NR 5 BEAM POSITION, ON FWD CUTOUT AT FWD CARGO DOOR INNER STRUCTURE. CRACKED PAN NR 5 BEAM POSITION, ON FWD CUTOUT WAS REPAIRED PER SRM 52-30-02-2R REPAIR 1 FIG 201.Jan 31, 2018 · N998AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018013100585Tail Cone · out of rigREQUIRED TO RELEASE THE COMPLETELY RIGGED TAILCONE IS 30+/- 5LBS. THE TAIL CONE IS OUT OF RIG AND RELEASING TOO EARLY USING THE INSIDE TAIL CONE RELEASE HANDLE. CHECKED & ADJUSTED TAILCONE RIG REF AMM 53-52-01. CHECK IS NOW WITHIN LIMITS.Jan 30, 2018 · N953AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2018013100584Tail Cone · out of rigTHE TAIL CONE IS OUT OF RIG AND RELEASING TOO EARLY DURING USE OF THE EXTERNAL TAIL CONE RELEASE HANDLE. CHECKED & ADJUSTED TAILCONE RIG REF AMM 53-52-01. CHECK WITHIN LIMITS.Jan 30, 2018 · N953AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2018013100583Support Bracket · crackedFLOOR SUPPORT BRACKET CRACKED AT STA 715 LBL 38. REPLACED BRACKET REF DWG 9923417.Jan 30, 2018 · N953AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018013100526Cusp Web · crackedCRACK ON CUSP WEB BTW STA Y=655 TO Y=674 AND X=54 TO X=60 AT CAB PAX (CPAX). CUSP WEB WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 206. HFEC INSPECTION WAS PERFORMED ON CUSP WEB AFT CUT OUT. NO CRACKS WERE FOUND PER NDT SPM 06-10-01.001.Jan 30, 2018 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018013100525Cusp Web · puncturedPUNCTURE ON CUSP WEB STA Y=696 AND X=-54 AT CAB PAX (CPAX). CUSP WEB WAS REPAIRED PER SRM 53-00-55-2-4 FIG 203. (HFEC) WAS ACCOMPLISHED ON CUSP WEB AT CAB PAX, NO CRACKS WERE FOUND AFTER TRIM OUT PER NDTSPM PART 6, 06-10-01.001.Jan 30, 2018 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018013100524Angle · crackedCRACK ON ANGLE AT BEAM 1 AND STA 197 APPROX AT FWD PASSENGER DOOR INT STRUCTURE. BEAM 1 AT FWD PASSENGER DOOR PAN WAS REPAIRED PER SRM 52-10-02-2R PROCEDURE 7 FIG 201.Jan 30, 2018 · N998AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2018013100523Cusp Web · crackedCRACK ON CUSP WEB AT STA Y=256 AND X=-54 AT CAB PAX (CPAX). CUSP WEB WAS REPAIRED PER SRM 53-00-55-2R-4- FIG 221. HFEC WAS ACCOMPLISHED ON CUSP WEB, TRIM OUT AREA WAS FOUND AT STA Y=256 AND X=-49 AT CAB PAX AND NO CRACK INDICATION WAS FOUND PER NDTSPM PART 6. Jan 30, 2018 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018013100522Beam · crackedCRACKED PAN 3 BEAM POSITION, ON FWD CUTOUT AT FWD CARGO DOOR INNER STRUCTURE (PTAS). CRACKED PAN #3 BEAM POSITION, ON FWD CUTOUT AT FWD CARGO DOOR INNER STRUCTURE WAS REPAIRED PER SRM 52-30-02-2R REPAIR 1 FIG 201.Jan 30, 2018 · N998AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018013100521Intercostal · crackedCRACK ON INTERCOSTAL BTW BEAM 4/5 AND STA 185.0 APROX (L1). INTERCOSTAL WAS REPLACED PER SRM 51-41-02-0G AND DWG 9955763 REV L.Jan 30, 2018 · N998AT · Boeing 717200 · Fuselage Miscellaneous Structure
Back to Boeing 717-200