N955AT

Service difficulty reports · 197

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N955AT' AND registry_match = 'registration'
  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 DALA2026101905722Oxygen Mask · faultedF/O O2 MASK-SETTINGS DO NOT ALIGN WITH INSIDE INDICATOR IE AT 100% THE INDICATOR READS EMERGENCY, R/R F/O O2 MASK PER B717 AMM 35-13. (9520956) (AIRCRAFT GROUNDED).Oct 18, 2026 · N955AT · Boeing 717200 · Crew Oxygen SystemSDR DALA2026081304644Strip · disconnectedFOUND METAL STRIP DISCONNECTED ON RIGHT WING LEADING EDGE, COMPLIED WITH ER/A 485300- 14. (9085798) (AIRCRAFT GROUNDED).Aug 12, 2026 · N955AT · Boeing 717200 · Wing Miscellaneous StructureSDR DALA2025032002095Pan · crackedCRACK ON PAN NEXT TO AFT HINGE DOOR (UPPER AREA) AT FWD CARGO DOOR. SUMMARY OF NRC 00193: PAN NEXT TO AFT HINGE DOOR (UPPER AREA) OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0866764)Mar 19, 2025 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2025032002093Pan · crackedCRACK ON OUTER PAN BTW BEAM 1 AND 2 (AFT EDGE) OF FWD CARGO DOOR WAS FOUND. SUMMARY OF NRC 00552: OUTER PAN AND INNER PAN BTW BEAM #1 AND BEAM #2 (AFT EDGE) AT FWD CARGO DOOR WERE REPAIRED PER ER/A 624433-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 624Mar 19, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025032002092Pan · crackedCRACK WAS FOUND ON INNER PAN AT AFT CARGO DOOR AT STOP FITTING ON BEAM 5 AFT EDGE. SUMMARY OF NRC 00577: INNER PAN ON BEAM 5 AFT EDGE OF AFT CARGO DOOR WAS REPAIRED PER ER/A 566665-14 REV A SECTION II: PERMANENT REPAIR AND PRI 566665-14 REV 4. ASSOCIATED ER/A Mar 19, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025031902064Beam · crackedCRACK WAS FOUND ON INNER/OUTER PAN BEAM 2 AND INNER PAN BEAM 1 FWD EDGE AT AFT CARGO DOOR. SUMMARY OF NRC 00578: INNER/OUTER PAN BEAM 2 AND INNER PAN BEAM 1 FWD EDGE AT AFT CARGO DOOR WAS REPAIRED PER PRI 624376-14 REV 2 AND ERA 624376-14 REV ORIGINAL SECTION Mar 19, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025031702028Pan · crackedCRACKS (2 EA) WERE FOUND ON INNER PAN AT AFT CARGO DOOR STOP FITTING ON BEAM 1 STA Y=990. SUMMARY OF NRC 00589: INNER PAN ON AFT SIDE BETWEEN STOP #1 AND STOP #2 AT AFT CARGO DOOR WAS REPAIRED PER ER/A 624383-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRIMar 15, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025031702019Pan · crackedCRACKS (2 EA) ON OUTER PAN IN BEAM 5 AT AFT CARGO DOOR FWD AND AFT EDGES. SUMMARY OF NRC 00111: DAMAGED AREA OF OUTER PAN IN BEAM 5 AT AFT CARGO DOOR FWD AND AFT EDGES WERE REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 6 REPAIR 6. (LP #0857625)Mar 14, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025031101890Beam · crackedCRACK WAS FOUND ON BEAM 5 AND INNER PAN (FWD EDGE) AT AFT CARGO DOOR. SUMMARY OF NRC 00574: BEAM 5 AND INNER PAN (FWD EDGE) AT AFT CARGO DOOR. WERE REPAIRED PER PRI 624316-14 REV 3 AND ERA 624316-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-6Mar 11, 2025 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2025031101888Skin · corrodedCORROSION ON INNER SKIN PANEL FROM STA Y=657 TO Y=636 BTW L29L AND L29R, STA Y=588 L30 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00183: CORROSION LEVEL 2. INNER SKIN PANEL FROM STA Y=657 TO Y=636 BTW L29L AND L29R, STA Y=588 L30 AT FWD CARGO COMPARTMENT WAS REPMar 10, 2025 · N955AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025030501711Hinge Fitting · damagedAN ELONGATED HOLE WAS FOUND AT THE RH WING FLAP HINGE FITTING #3 PIVOT POINT. SUMMARY OF NRC 00535: RH WING FLAP HINGE FITTING #3 WAS REPAIR PER PRI 624272-14 REV 1 AND ER/A 624272-14 REV ORIGINAL. ASSOCIATED ER/A 14-624272 ADDED FOR AC 9514. (LP #0840814)Mar 4, 2025 · N955AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2025030501710Hinge Fitting · corrodedAN ELONGATED HOLE INBD ON INBD FACE ON HINGE FLAP #3 AT LH WING, ALONG WITH CORROSION ON BOTH HOLES INBD/OUTBD HINGE. SUMMARY OF NRC 00543: HINGE FLAP #3 AT LH WING WAS REPAIRED PER PRI 624271-14 REV 1 AND ER/A 624271-14 REV ORIGINAL. ASSOCIATED ER/A 14-624271Mar 4, 2025 · N955AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2025030501709Frame · corrodedCORROSION ON FRAME BTW STA Y=1022 L28L TO L28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00177: CORROSION LEVEL 2. FRAME BTW STA Y=1022 L28L TO L28R AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3, REPAIR 3. PERFORM A DETAIL VISUAMar 4, 2025 · N955AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2025030401650Shear Tie · corrodedFRAME CLIP STA 1022 BTW LONG 28RH TO 28LH, AFT CARGO COMPARTMENT, WAS FOUND CORRODED OUT OF LIMITS WITH MINIMUM REMAINING THICKNESS 0.048 IN PER B717-200 SRM 53-00-01-1A ALLOWABLE DAMAGE PAR 4.C.(2) FIG 103. SUMMARY OF NRC 00633: CORROSION LEVEL 2. FRAME CLIP Mar 3, 2025 · N955AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2025030301647Angle · corrodedCORROSION ON ANGLE CUSP BTW STA Y=197 TO STA Y=210 OF FWD GALLAY SERVICE DOOR AT CABIN PASSENGER. SUMMARY OF NRC 00283: CORROSION LEVEL 2. ANGLE CUSP BTW STA Y=197 TO STA Y=210 OF FWD GALLEY SERVICE DOOR AT CABIN PASSENGER WAS REPAIRED PER PRI 624120-14 REV 4 Feb 28, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025030101571Cusp Web · crackedCRACK ON CUSP WEB (BELOW AREA) IN X=-54 AND STA 257, STA 277, STA 656, STA 674, STA 818, AND STA 937 AT CPAX. SUMMARY OF NRC 00336: CUSP WEB AT STA 277, STA 257, STA 818, STA 937 WERE REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4, CUSP WEB BTW STA 655 TO STA Feb 27, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025022601481Skin · damagedLH ELEVATOR WAS FOUND DENTED AND SCRATCHED ON UPPER SKIN. SUMMARY OF NRC 00575: LH ELEVATOR WAS REPAIRED PER B717-200 SRM 51-70-13-2R REPAIR 2. PERFORM DECAL CONDITION INSPECTION EVERY C CHECK PER TOPP MANUAL 30-10-70 PAR I PAGE 14. LOG PAGE DEFERRED TO DECAL Feb 26, 2025 · N955AT · Boeing 717200 · Elevator, Plate/SkinSDR DALA2025022601480Cusp Web · crackedCRACK ON CUSP WEBS (LOWER AND UPPER AREA) IN X=54 AND STA 225, STA 237, STA 258, STA 655, AND STA 663. ALSO, X=58 AND STA 668, STA 807 AT CPAX WAS CRACKED. SUMMARY OF NRC 00442: CUSP WEBS IN X=54 AND STA 225, STA 237, STA 258, STA 655, STA 663, ALSO X=58 AND SFeb 25, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025022601479Angle · corrodedCORROSION ON ANGLE CUSP BTW STA Y=190 TO STA Y=200 OF FWD ENTRY DOOR AT PASSENGER CABIN. SUMMARY OF NRC 00270: CORROSION LEVEL 2. ANGLE CUSP BTW STA Y=190 TO STA Y=200 OF FWD ENTRY DOOR AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 3 RFeb 25, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025022501469Door Frame · corrodedCORROSION ON DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00062: CORROSION LEVEL 2. DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED AND INSTALLED PER B717-200 SRM 53-20-15 -2R-7. (LP #0822834)Feb 22, 2025 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2025022501468Floor Support · corrodedCORROSION ON FLOOR SUPPORT BTW STA Y=194 TO STA Y=200 X=56 OF FWD ENTRY DOOR AT PASSENGER CABIN. SUMMARY OF NRC 00276: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=194 TO STA Y=200 X=56 OF FWD ENTRY DOOR AT PASSENGER CABIN WAS MANUFACTURATED PER DWG 9910078-173 Feb 21, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025022101363Web · corrodedCORROSION OUT OF LIMITS FOUND AT WEB STA 200 TO STA 216 X=25 TO X=54. SUMMARY OF NRC 00492: CORROSION LEVEL 2. WEB STA 200 TO STA 216 X=25 TO X=54 WAS FABRICATED PER DWG 9910078 REV JC. AND REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-08-0G. (LP #0821476)Feb 21, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025022101362Web · corrodedCORROSION ON WEB BTW STA Y=225 TO STA Y=228 X=56 AT FWD CABIN PASSENGER. SUMMARY OF NRC 00280: CORROSION LEVEL 2. CUSP WEB STA 216 TO 237 X=45 TO X=57 WAS FABRICATED PER DWG 993053 REV CF. AND WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #082Feb 20, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025022101359Pan · crackedCRACK WAS FOUND ON AFT SIDE ON BEAM 4 OUTER PAN AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00508: AFT SIDE ON BEAM 4 OUTER PAN AT FWD COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0819812)Feb 20, 2025 · N955AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2025022001286Cusp Web · corrodedCORROSION ON CUSP WEB, REWORKED AREAS AT X=58 STA 866 AND STA 840-847 WAS FOUND OUT OF LIMITS WITH MINIMUM REMAINING THICKNESS OF 0.010IN PER B717 SRM 53-00-55-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR 4.C. FIG 101. SUMMARY OF NRC 00531: CORROSION LEVEL 2. CUSP WEFeb 20, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025021801196Seat Track · corrodedCORROSION OUT OF LIMITS IN REF NRC 188: CORROSION ON SIDE TRACK (RH) BWT STA 644 TO 648 SEAT TRACK FLANGE: WITH ORIGINAL THICKNESS =0.060" AND MINIMUM REMAINING THICKNESS IS 0.025". THEREFORE, IT IS OUT LIMITS PER B717-200 SRM 53-20-52-1A PROCEDURE 2 ALLOWABLEFeb 18, 2025 · N955AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025021401141Cusp Web · crackedCRACK ON CUSP WEB BTW STA Y=218/Y=237 AND X-54/X-44 AND CUSP WEB BTW STA Y=200/Y=218 AND X-54/X-24 AT PAX CABIN. SUMMARY OF NRC 00495: CUSP WEB BTW STA Y=218/Y=237 AND X-54/X-44 AND CUSP WEB BTW STA Y=200/Y=218 AND X-54/X-24 WERE REPAIRED PER B717-200 SRM 53-0Feb 13, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025021401140Frame · crackedCRACK ON FRAME STA Y=1037, L-17L AND L-17R AT CPAX. SUMMARY OF NRC 00379: FRAME STA Y=1037, L-17L AND L-17R AT CPAX WERE REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0808878)Feb 13, 2025 · N955AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2025021401139Floor Support · corrodedCORROSION ON FLOOR SUPPORTS (3 EA) BTW STA Y=1022 TO STA Y=1074 AND -X=44 TO -X=56 AT AFT PASSENGER CABIN (W2). SUMMARY OF NRC 00271: CORROSION LEVEL 2. CORRODED FLOOR SUPPORTS (3 EA) BTW STA Y=1022 TO STA Y=1074 AND -X=44 TO -X=56 AT AFT CABIN (W2) WERE REPLAFeb 13, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025021401138Floor Support · corrodedCORROSION ON FLOOR SUPPORT BTW STA Y=1022 TO STA Y=1074 AND X=44 AT AFT PASSENGER CABIN (W2). SUMMARY OF NRC 00275: CORROSION LEVEL 2. CORRODED FLOOR SUPPORT BTW STA Y=1022 TO STA Y=1074 AND X=44 AT AFT CABIN (W2) WAS REPLACED PER DWG 9981474-15 REV L AND PER Feb 12, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025021001045Pan · crackedCRACK WAS FOUND ON INNER PAN OF THE AFT EDGE AT FWD CARGO DOOR. SUMMARY OF NRC-00306: AFT EDGE AT FWD CARGO DOOR CRACK ON INNER PAN WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 3 REPAIR 3. (LP #0800119)Feb 7, 2025 · N955AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2024032803862Drain · crackedCRACK ON DRAIN OF LH CLEAR VIEW WINDOW AT COCKPIT. SUMMARY OF NRC 00080: LH CLEAR VIEW WINDOW RETAINER AT COCKPIT WAS REPAIRED PER ERA 616781-14 REV ORIGINAL. ASSOCIATED ER/A 14-616781 ADDED FOR AC 9514. (LP #0264952)Mar 27, 2024 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024022102374Trunnion · corrodedRMLG FIXED STRUT OB ATTACH POINT BORE BUSHING CORRODED. REPLACED BUSHING PER BOEING DWG 5924841 ON NRC 008. (LP #0033263)Oct 25, 2023 · N955AT · Boeing 717200 · Fuselage, Landing Gear Attach FittingsSDR DALA2023091407536Unknown · unknownLWR FRAME SECTION STA 120 DAMAGED DURING LANDING. C/W PRI 610432-14 REV 0. C/W PRI 610432-14 REV 1. C/W PRI 610432-14 REV 2. C/W PRI 610432-14 REV 3. C/W PRI 610432-14 REV 4. C/W PRI 610432-14 REV 5. C/W ERA 610432-14 REV B PRIS 0-5 MATCH FINAL ERA. (LP #29683Sep 13, 2023 · N955AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023091207455Unknown · unknownLHS NLG SUPPORT BEAM DAMAGED ON LANDING. REMOVED DAMAGED NLG SUPPORT BEAM PER BOEING DWG 9910088. REPLACED NLG SUPPORT BEAM PER BOEING DWG 9910088. (LP #2963209)Sep 10, 2023 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2023090507180Unknown · unknownLOWER SKIN PANEL ASSY 5911401-537 DAMAGED DRUING LANDING. REMOVED -537 SKIN ASSY PER DWG 5911401. LOCATED AND DRILLED NEW SKIN ASSY PER DWG 5911401. APPLIED TOP COAT TO ASSEMBLY PARTS PER B717 SRM 51-22-01. INSTALLED DOUBLERS TO SKIN PER DWG 5911401. PRIMED EXAug 31, 2023 · N955AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023082907002Unknown · unknownLOWER FRAME SECTION AT STA 160 DAMAGED DURING LANDING. (REF PAPER NR 012) REMOVED LOWER FRAME SECTION STA 160 PER B717 SRM 51-40-02. C/W REV 0 OF PRI 610940-14. C/W REV 1 OF PRI 610940-14. C/W PRI 610940-14 REV 2. C/W ERA 610940-14 REV ORIG. PRIS 0-2 MATCH FINAug 28, 2023 · N955AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023082506912Unknown · unknownC/W ERA 610811-14 INTERNAL DOUBLER FABRICATION DAMAGED DURING LANDING. C/W PRI 610811-14 REV 0. C/W ERA 610811-14 REV ORIG. PRI REV 0 MATCHES FINAL ERA. (LP #2934596)Aug 24, 2023 · N955AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023081806720Unknown · unknownLH NLG SKIN PANEL 5911400-99 DAMAGED DURING LANDING. REF NR 066: C/W PRI 610190-14 REV 0. C/W PRI 610190-14 REV 1. C/W PRI 610190-14 REV 2. C/W PRI 610190-14 REV 3. C/W ERA 610190-14 REV ORIG. PRI REVS 0-3 MATCH FINAL ERA. (LP #2920961)Aug 16, 2023 · N955AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023081606675Unknown · unknown-39 AND -22 CHORDS AT STA 110 BULKHEAD DAMAGED DURING LANDING. REMOVED DAMAGED PORTION OF -39 AND -22 CHORDS PER B717 SRM 51-70 -11-2R-2. FABRICATED NEW -22 SECTION AND REPAIR ANGLES PER B717 SRM 51-70-11-2R-2 AND PRI 610765-14 REV 0. TREATED AND PAINTED PER BAug 15, 2023 · N955AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2023081606674Unknown · unknownRHS NLG SUPPORT BEAM WAS DAMAGED ON LANDING. C/W PRI 610297-14 REV 0. C/W PRI 610297-14 REV 1. C/W ERA 610297-14 REV ORIG. PRI REVS 0 AND 1 MATCH FINAL ERA. (LP #2919777)Aug 15, 2023 · N955AT · Boeing 717200 · Fuselage, Landing Gear Attach FittingsSDR DALA2023081606673Unknown · unknownE&E DOOR SURROUND JAMB PAN AND SUPPORT FRAMES DAMAGED DURING LANDING. REMOVED E&E DOOR SURROUND JAMB PAN PER B717 SRM 51-40-02. INSTALLED E&E JAMB PAN AND SUPPORT FRAMES PER B717 SRM 51-40-02 AND DWG 9911550. (LP #2919766)Aug 15, 2023 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2023081606672Unknown · unknownSTA 110 BULKHEAD AND LWR CHORD DAMAGED DURING LANDING. REMAINING SECTIONS OD ST110 CHORD REMOVED. REMOVED DAMAGE SECTION OF BULKHEAD PER B717 SRM 53-10-08-2R REPAIR 1. FABRICATED -3 THROUGH -23 REPAIR PARTS PER B717 SRM 53-10-08-2R REPAIR 1 AND ERA 610394-14 RAug 15, 2023 · N955AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023081606671Unknown · unknownLONGERON AT STA 160-STA 180 STR 30 DAMAGED DURING LANDING. REMOVED LONGERON AT STA 160 - STA 180 STR 30 PER B717 SRM 51-40- 02. REPLACED LONGERON AFT STA 160- STA 180 STR 30 PER B717 SRM 51-40-02 AND DWG 5911401. (LP #2919466)Aug 15, 2023 · N955AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023081606670Unknown · unknownSEVEN LONGERONS STA 110-120 STR 28L-28R WERE DAMAGED DURING LANDING. (REF BUFF NR 010) LOCATED AND DRILLED LONGERON SECTIONS PER B717 DWG 5911401. INSTALLED 7 EA LONGERON SECTIONS STA 110-120 STR 28L-28R PER B717 SRM 51-40-02 AND DWG 591140. (LP #2919459)Aug 15, 2023 · N955AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023072505984Unknown · unknownLOWER FRAME SECTION STA 132 WAS DAMAGED DURING LANDING. MAINTENANCE REMOVED LOWER FRAME SECTION PER B717 SRM 51-40-02. LOCATED AND DRILLED NEW SPLICES PER B717 DWG 9911512. INSTALLED NEW SPLICES AND REPLACEMENT 132 FRAME SECTION PER B717 SRM 51-40-02 AND DWG #Jul 24, 2023 · N955AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023063005265Unknown · unknownSHIP 9514 -GEAR/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC AFTER NOT BEING ABLE TO EXTINGUISH THE "NLG UNSAFE" INDICATION ON APPROACH. THE QRH WAS COMPLIED WITH AND COMMUNICATIONS WITH MCC WAS ESTABLISHED, BUT THE NOSE LANDING GEAR FAILED TO EXTEND. THJun 28, 2023 · N955AT · Boeing 717200 · Landing Gear SystemSDR DALA2023040402601Unknown · unknownWHILE REMOVING CEILING PANELS MAINTENANCE FOUND A BROKEN EMERGENCY LIGHT WIRE. THE WIRE WAS REPAIRED PER SWPM 20-30. THE OPERATIONAL CHECK WAS GOOD. (LP #4025352)Mar 29, 2023 · N955AT · Boeing 717200 · Emergency LightingSDR 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)Feb 18, 2023 · N955AT · Boeing 717200 · Emergency LightingSDR DALA2022040602329Frame · crackedFRAME AT STA Y1116 AND STR R11 CRACKED. REMOVED DAMAGED AREA PER B717SRM 53-00-07-2R-1. FABRICATED & INSTALLED REPAIR PARTS IAW B717 SRM53-00-07-2R-1. (LP #2182161)Apr 3, 2022 · N955AT · Boeing 717200 · Fuselage Main, Frame
Back to N955AT