N266JB
Registered owner: TVPX AIRCRAFT SOLUTIONS INC TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
54 reports on file, 2008-02-02 – 2022-11-08.
Part: NONE — FAILED (LH-BCV-1) · airframe 41,129 hrs · 26,650 cycles
FLT#42, PBI-LGA. (AIRCRAFT DIVERTED TO JFK) 'BRAKE RH FAULT AND BRAKE LH FAULT; REMOVED AND REPLACED MAIN BRAKE CONTROL VALVE 4. OPS AND LEAK CHECKS ARE GOOD. REF TO AMM 32-41-09.'
Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 40,285 hrs · 26,026 cycles
DURING HEAVY MAINTENANCE, CORROSION ON FLOORBEAM AT PASSENGER CABIN FLOOR STRUCTURE FRAME 87 Y=-300; ALL WORK ACCOMPLISHED ON TOMEX NRC 00383, CORROSION ON FLOORBEAM AT PASSENGER CABIN FLOOR STRUCTURE FRAME 87 Y=-300 WAS REMOVED AND EVALUATED, THEREFORE IT IS OUT LIMITS. THE FLOOR BEAM WAS REPLACED PER EMB190 SRM 51-41-01 AND SRM 51-43-01. (CONSIDERED AS A MAJOR REPAIR) (SUPPLEMENTAL INFORMATION ADDED TO DESCRIPTION)
Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 40,285 hrs · 26,026 cycles
DURING HEAVY MAINTENANCE, CORROSION ON SHEAR CLIP AT FR 72 AND STGR 27-28 LH, AFT CARGO; ALL WORK ACCOMPLISHED ON TOMEX NR 00420, CORROSIÃN ON SHEAR CLIP AT FR 72 AND STGR 27-28 LH AFT CARGO WAS REMOVED AND EVALUATED, THEREFORE IT IS OUT LIMITS PER EMB 190 SRM 51-12-01 AND SRM 51-10-03 AND WAS INSTALLED NEW SHEAR CLIP PER EMB 190 SRM 51-41-02, SRM 51-41-01 AND SRM 51-43-01. DURING HEAVY MAINTENANCE, CORROSION ON SHEAR CLIP AT FR 72 AND STGR 27-28 LH, AFT CARGO; ALL WORK ACCOMPLISHED ON TOMEX NR 00420, CORROSIÃN ON SHEAR CLIP AT FR 72 AND STGR 27-28 LH AFT CARGO WAS REMOVED AND EVALUATED, THEREFORE IT IS OUT LIMITS PER EMB 190 SRM 51-12-01 AND SRM 51-10-03 AND WAS INSTALLED NEW SHEAR CLIP PER EMB 190 SRM 51-41-02, SRM 51-41-01 AND SRM 51-43-01. (CONSIDERED AS A MAJOR REPAIR) (SUPPLEMENTAL INFORMATION ADDED TO DESCRIPTION)
Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 40,285 hrs · 26,026 cycles
DURING HEAVY MAINTENANCE, CORROSION ON SHEAR CLIP AT FR 73 AND STGR 27-28 LH, AFT CARGO; ALL WORK ACCOMPLISHED ON TOMEX NRC 00410, SHEAR CLIP AT FR 73 AND STGR 27-28 LH, AFT CARGO WAS REPLACED PER. EMB 190 SRM 51-41-02, SRM 51-41-01 AND SRM 51-43-03 (CONSIDERED AS A MAJOR REPAIR)
Part: FLOOR SUPPORT — CORRODED · airframe 40,285 hrs · 26,026 cycles
DURING HEAVY MAINTENACE, CORR LATERAL FLOOR SUPPORT Y -1200 FR16; REF ALL WORK ACP ON TOMX W/O N266JB-1946 NR 00636 RPL FLOOR SUPPORT PER SRM 51-41-02.
Part: FASTENER — DAMAGED · airframe 40,285 hrs · 26,026 cycles
DURING HEAVY MAINTENACE, LIGHTNING STRIKE FR 24 BTW STR 13L-14L CTR FUSELAGE; RE TOMX NR 1946-00023 - LIGHTNING STRIKE AT FASTENER FR 24 STR 13L-14L REPAIRED IAW EMB 190 SRM 53-00-00 REPAIR 53.
Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 40,285 hrs · 26,026 cycles
DURING HEAVY MAINTENANCE, CORROSION ON SHEAR CLIP FR 87 AND STGR 27-28 RH, AFT CARGO; ALL WORK ACCOMPLISHED ON TOMEX NRC 00395, SHEAR CLIP FR 87 AND STGR 27-28 RH, AFT CARGO WAS REPLACED PER. EMB 190 SRM 51-41-02, SRM 51-41-01 AND SRM 51-43-01. (CONSIDERED AS A MAJOR REPAIR)
Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 40,285 hrs · 26,026 cycles
DURING HEAVY MAINTENANCE, CORROSION ON SHEAR CLIP FR88 AND STGR 27-28 RH, AFT CARGO; ALL WORK ACCOMPLISHED ON TOMEX NRC 394, CORROSION ON SHEAR CLIP FR 88 AND STGR 27-28 RH WAS REMOVED AND EVALUATED, THEREFORE IT IS OUT LIMITS. THE SHEAR CLIP WAS REPLACED PER EMB190 SRM 51-41-02 AND SRM 51-43-03. (CONSIDERED AS A MAJOR REPAIR) (SUPPLEMENTAL INFORMATION ADDED TO DESCRIPTION)
Part: DOOR SILL — CORRODED · corrosion level 2 · airframe 40,285 hrs · 26,026 cycles
DURING HEAVY MAINTENANCE, ALL WORK ACCOMPLISHED ON TOMEX NR 00293, CORROSION IN LOWER SILL WHERE HOLD SLIDE FITTINGS IN FWD SERVICE DOOR CUTOUT FWD FUSELAGE STRUCTURE; ALL WORK ACCOMPLISHED ON TOMEX NR 293, CORROSION IN LOWER SILL WAS REMOVED AND EVALUATED, THEREFORE IT IS OUT LIMITS. THE LOWER SILL WAS REPLACED PER EMB190 SRM 51-41-01, SRM 51-43-01, AND SRM 51-43-02. (CONSIDERED AS A MAJOR REPAIR)
Part: SPAR — CRACKED · airframe 40,285 hrs · 26,026 cycles
DURING HEAVY MAINTENACE, A CRACK WAS FOUND AFT BUSHING BORE RH PYLON I/B SPAR; MAJOR REPAIR - REF TOMX NR 1946-00564 - RH PYLON I/B SPAR WAS REPLACED PER EMB 190 SRM 51-43-03.
Part: SEAT — DAMAGED · airframe 40,285 hrs · 26,026 cycles
DURING HEAVY MAINTENANCE, E/F - SEATS - DIAPHRAGM FRONT TUBE HOLES - PERMANENT REPAIR - N266JB. (CONSIDERED AS A MAJOR REPAIR)
Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 40,285 hrs · 26,026 cycles
DURING HEAVY MAINTENANCE, CORROSION ON SHEAR CLIP AT FR 76 AND STGR 27-28 LH, AFT CARGO; WORK ACCOMPLISHED ON TOMEX NR # 00398, SHEAR CLIP AT FR 76 AND STGR 27-28 LH, AFT CARGO WAS REPLACED PER EMB 190 SRM 51-41-02, SRM 51-41-01, AND SRM 51-43-01. (CONSIDERED AS A MAJOR REPAIR)
Part: RIB — CRACKED · airframe 40,285 hrs · 26,026 cycles
DURING HEAVY MAINTENANCE, WINGS / LH WING / FIXED LEADING EDGE RIB 17 / CRACK - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
Part: HYDRAULIC LINE — LEAKING · airframe 40,161 hrs · 25,941 cycles
FLT#2259, BOS-PHL. (AIRCRAFT DECLARED AN EMERGENCY) 'ON APPROACH WE RECEIVED A HYD 2 LO PRESS EICAS MESSAGE. WE WENT AROUND AND COMPLETED QRH. LANDED WITHOUT INCIDENT; FOUND LH LG ACTUATORS HYD HOSES LEAKING. REMOVED AND REPLACED BOTH HOSES IAW AMM 29-10-13. ALSO REMOVED AND REPLACED #2 SYS CASE DRAIN FILTER AND PRESSURE FILTER IAW AMM 29-11-05. SERVICED HYD SYS IAW AMM 12-12-01. PERF ENG RUN OPS TEST AND LEAK CHECK GOOD. NO FAULTS ARE NOTED AT THIS TIME. AC OK FOR SERVICE. CW ENG 2 DRIVEN PUMP EDP RUND DRY INSP CHECK IAW AMM 05-50-23. ALL CHECKS ARE NORMAL. BOTH FILTERS WERE REPLACED.'
Earlier reports · 2008–2020 · 40 reports
2020
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 37,535 hrs · 24,253 cycles
DURING HEAVY MAINTENANCE, INOPERABLE ELPU FWD LT IN PASSENGER CABIN, REF AEROMAN N/R 2020-360662. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT, IAW E190 AMM 33-50-01-000-801-A. OPERATIONS CHECK GOOD, IAW E190 AMM 33-50-00-710-801-A.
Part: RIB — CRACKED (LT WING) · airframe 37,535 hrs · 24,253 cycles
DURING HEAVY MAINTENANCE, CRACK RIB 22 LEADING EDGE INERNAL AREA ON LT WING, REF AEROMAN N/R 2020-360662. REMOVED AND REPLACED RIB 22 AND FASTENERS LOCATED ON LEADING EDGE LT WING, IAW E190 SRM 51-40-08 AND DRAWING 190-31005-409.
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 37,535 hrs · 24,253 cycles
DURING HEAVY MAINTENANCE, INOPERABLE AFT RT OUTBOARD ELPU IN PAX CABIN, REF AEROMAN N/R 2020- 360657. REMOVED AND REPLACED RT OUTBOARD ELPU, IAW E190 AMM 33-50-01-400-801-A. OPERATIONS CHECK GOOD, IAW E190 AMM 33-50-01-710-801-A.
2019
Part: POWER UNIT — FAILED (CABIN) · airframe 34,141 hrs · 21,872 cycles
FLT 2167, HPN-PBI. RT AFT EXTERIOR OVERWING EMERG. LIGHT INOP ( EXTERNAL EMERGENCY-OPS NOT CONDUCTED AT NIGHT ); R & R EMERGENCY LIGHT POWER UNIT 243GLC PER AMM 33-50-01 OPS CHECKS OK. MDDR 375476 CLEARED, MX-4 UPDATED. PLACARD REMOVED.
2018
Part: SKIN — CRACKED (LT WING) · airframe 33,410 hrs · 21,367 cycles
DURING HEAVY MAINTENANCE CHECK AT SAL DATED 10/2018, CRACK WAS FOUND COMMON TO THE LT WING REAR LOWER SKIN PN 190-33065-009 AFT EDGE AT RIB 10. SEE REF /1/FOR DETAILS. CONTACTED FOR REPAIR DISPOSITION, AND PROVIDED THE REF /1/ ETD REPAIR, CONSISTING OF CUTTING OUT THE CRACKED SKIN AND INSTALLING A REPAIR DOUBLER AND FILLER. THIS EC INCORPORATES THE REF /1/ ETD WITHOUT DEVIATIION. THIS EC E18-821-01 EMBODIES PERMANENT REPAIR INSTRUCTIONS PER REF /2/ EA. EC E18-821-02 TRACKS FOLLOW-UP DETAILED INTERNAL AND EXTERNAL VISUAL INSPECTIONS AT A THRESHOLD OF 7,500 FC AND INTERVAL OF 7,500 FC. THRESHOLD IS COUNTED SINCE THE REPAIR ACCOMPLISHMENT; THIS REPAIR HAS BEEN APPROVED VIA THE REF /1/ ETD AND REF /3/ ANAC FORM. THIS REPAIR IS CLASSIFIED AS A MAJOR PERMANENT REPAIR REQUIRING FOLLOW-UP INSPECTIONS AS NOTED ABOVE.
2017
Part: GIRT BAR — OUT OF ADJUST (R1 DOOR SLIDE) · airframe 30,731 hrs · 19,378 cycles
R1 DOOR WILL NOT DISARM. ADJUSTED GIRT BAR FLOOR FITTINGS IAW 52-41-00. DOOR OPS CHECKED OK, NO FURTHER DEFECTS NOTED.
Part: STOP FITTING — OUT OF ADJUST (R1 DOOR) · airframe 30,731 hrs · 19,377 cycles
R1 DOOR WILL NOT DISARM. ADJUSTED THEUPPER & AFT STOPS IAW AMM 52-41-00. OPS CHECKED GOOD.
2016
Part: SEAL REST — CORRODED (FRAME 25) · corrosion level 2 · airframe 27,640 hrs · 17,146 cycles
CORROSION FWD CARGO DOOR CENTER SEAL REST AT FRAME 25 APROX. 12 INCHES AFT. REMOVED AND REPLACED FWD CARGO DOOR SEAL REST IAW SRM 51-41-01.
Part: SKIN — CORRODED (FRAME 77) · corrosion level 2 · airframe 27,640 hrs · 17,146 cycles
CORROSION AFT CARGO DOOR LOWER CUTOUT AT FRAME 77, 16' AFT. REMOVED CORROSION IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.
Part: FINGER DOUBLER — CORRODED (FRAME 24) · corrosion level 2 · airframe 27,640 hrs · 17,146 cycles
CORROSION FWD CARGO DOOR AFT FINGER DOUBLER AT FRAME 27, 1.5 INCHES AFT. REMOVED AND REPLACED THE FINGER DOUBLER. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.
Part: FINGER DOUBLER — CORRODED (FRAME 78) · corrosion level 2 · airframe 27,640 hrs · 17,146 cycles
CORROSION ON AFT CARGO DOOR FWD FINGER DOUBLER FRAME 78. REMOVED THE CORROSION IAW SRM 51-10-03, AND FOUND OUT OF LIMITS. REPLACED THE FINGER DOUBLER IAW NR00103.
Part: FINGER DOUBLER — CORRODED (FRAME 80) · corrosion level 2
AFT CARGO DOOR AFT LOWER FINGER DOUBLER FRAME 80 CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-10-03. DOUBLER REPLACED.
Part: FINGER DOUBLER — CORRODED (FRAME 77) · corrosion level 2
CORROSION ON THE AFT CARGO DOOR FWD LOWER FINGER DOUBLER AT FRAME 77. REMOVED THE CORROSION IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS. REPLACED THE FINGER DOUBLER.
Part: FINGER DOUBLER — CORRODED (FRAME 26) · corrosion level 2 · airframe 27,640 hrs · 17,146 cycles
CORROSION FWD CARGO DOOR AFT FINGER DOUBLER AT FRAME 26, 1 INCH AFT. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.
Part: STRUCTURE — CORRODED (FRAME 13) · corrosion level 2 · airframe 27,640 hrs · 17,146 cycles
FWD RIGHT STRUCTURE CORRODED 4.75 INCHES AFT OF FRAME 13 AND RBL 37. REMOVED CORROSION IAW SRM 51-12-01.
Part: FINGER DOUBLER — CORRODED (FRAME 79) · corrosion level 2
CORROSION AFT CARGO DOOR AFT LOWER FINGER DOUBLER FRAME 79. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-75-16. REPLACED THE FINGER DOUBLER IAW NR 00105.
Part: FINGER DOUBLER — CORRODED (FRAME 77) · corrosion level 2
CORROSION AFT CARGO DOOR FORWARD LOWER FINGER DOUBLER FRAME 77. REPLACED THE FINGER DOUBLER IAW SRM 51-43-03, 51-43-04, AND 51-23-06.
Part: SKIN — CORRODED (FRAME 78) · corrosion level 2 · airframe 27,640 hrs · 17,146 cycles
CORROSION AFT CARGO DOOR LOWER CUTOUT AT FRAME 78, 5' AFT. REMOVED CORROSION IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.
Part: FINGER DOUBLER — CORRODED (FRAME 25) · corrosion level 2 · airframe 27,640 hrs · 17,146 cycles
CORROSION FWD CARGO DOOR AFT FINGER DOUBLER AT FRAME 25, 15.5 INCHES AFT. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-23-04, 51-23-05, AND 51-23-06.
Part: BEAM — CORRODED (FRAME 26) · corrosion level 2 · airframe 27,640 hrs · 17,146 cycles
FWD CARGO LOWER BEAM HAS CORROSION UNDER NR 4 DOOR LATCH FITTING 10 INCHES AFT OF FRAME 26. REMOVED AND REPLACED THE BEAM IAW SRM 51-43-04.
Part: SKIN — CORRODED (FRAME 77) · corrosion level 2 · airframe 27,640 hrs · 17,146 cycles
CORROSION AFT CARGO DOOR LOWER CUTOUT AT FRAME 77, 14' AFT. REMOVED CORROSION IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.
Part: SKIN — CORRODED (FRAME 77) · corrosion level 2 · airframe 27,640 hrs · 17,146 cycles
CORROSION AFT CARGO DOOR LOWER CUTOUT AT FRAME 77, 6' AFT. REMOVED CORROSION IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.
Part: SKIN — CORRODED (FRAME 78) · corrosion level 2 · airframe 27,640 hrs · 17,146 cycles
CORROSION AFT CARGO DOOR LOWER CUTOUT AT FRAME 78, 5' AFT. REMOVED CORROSION IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.
Part: STRUCTURE — CORRODED (FRAME 12) · corrosion level 2 · airframe 27,640 hrs · 17,146 cycles
FWD RT STRUCTURE CORRODED 5.25 INCHES AFT OF FRAME 12 AND RBL 36.25. REMOVED AND REPLACED IAW SRM 51-43-04, AND 51-41-02.
Part: FINGER DOUBLER — CORRODED (FRAME 24) · corrosion level 2 · airframe 27,640 hrs · 17,146 cycles
CORROSION FWD CARGO DOOR AFT FINGER DOUBLER AT FRAME 24, 13.5 INCHES AFT. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.
Part: SHEAR TIE — CORRODED (FRAME 84) · corrosion level 2 · airframe 27,640 hrs · 17,146 cycles
SHEAR TIE CORRODED AT FRAME 84 STRINGERS 27-28L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-41-01, 51-41-02, AND 51-21-01.
Part: MOUNT — CORRODED (FRAME 15) · corrosion level 2 · airframe 27,640 hrs · 17,146 cycles
FWD LAVATORY MOUNT FITTING CORRODED 6.5 INCHES AFT OF FRAME 15 AND LBL 44. REMOVED AND REPLACED THE MOUNT FITTING IAW SRM 51-43-03.
Part: FINGER DOUBLER — CORRODED (FRAME 79) · corrosion level 2
CORROSION ON AFT CARGO DOOR AFT LOWER FINGER DOUBLER FRAME 79. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-43-03, 51-43-04, AND 51-23-06.
Part: FINGER DOUBLER — CORRODED (FRAME 77) · corrosion level 2
CORROSION ON AFT CARGO DOOR FWD FINGER DOUBLER AT FRAME 77. REMOVED THE CORROSION, AND FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.
2014
Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 21,621 hrs · 13,084 cycles
ACFT DIVERTED DUE TO "AVNX MAU 1A FAIL" ON EICAS IN FLIGHT. ACCOMPLISHED EBIT, PBIT AND RETURN TO SERVICE TEST IAW AMM 27-00-00-070-801-A. NO FURTHER FAULTS NOTED. ACFT GOOD FOR SERVICE.
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 21,094 hrs · 12,727 cycles
ON MAINTENANCE CHECK, FOUND R1 DOOR LOWER EXIT LIGHT INOPERATIVE. TROUBLESHOOTING FOUND POWER SUPPLY OUTPUT BAD. R & R RT FWD EMERGENCY LIGHT POWER SUPPLY, REF AMM 33-50-00. OPS CHECKS NORMAL.
Part: PROCESSOR — FAILED · airframe 20,305 hrs · 12,215 cycles
AIRCRAFT DIVERTED, AVNX MAU 3 FAIL, YD OFF. APPLIED T/S PROCEDURES, FOUND NIC PROC 6 FAILED. R & R NIC PROC 6 IAW AMM 31-41-04. NO FAULTS, OP'S CHECK OK.
2013
Part: SLIDE — DEFECTIVE (L2 DOOR) · airframe 18,227 hrs · 10,884 cycles
CREW REPORTED L2 DOOR WILL NOT DISARM. R & R L2 DOOR VENT FLAP CAM IAW AMM 52-12-25 AND L2 DOOR SLIDE IAW AMM 25-65-01. OPS CHECK OK.
Part: CONTROLLER — FAILED (NR 2) · airframe 17,217 hrs · 10,290 cycles
FLT 1731 JFK-BDA, AIR TURNBACK TO JFK DUE TO BLEED 1 AND 2 FAILED ON TAKEOFF AT TO-1. RESET SUCCESSFUL REPEAT AT 11000FT. FAILED AGAIN BLEEDS 1 AND 2. REMOVED AND REPLACED ENGINE NR 1 PRSOV AS PER AMM 36-11-03. REMOVED AND REPLACED HP BLEED VALVE NR 2 AS PER 36-11-01 AND AMS CONTROLLER IN SPDA NR 2 SLOT 23 IAW 21-00-02, OPS CHECK NORMAL.
Part: SHUTOFF VALVE — FAILED (BLEED AIR SYS) · airframe 17,217 hrs · 10,290 cycles
FLT 1731 JFK-BDA, AIR TURNBACK TO JFK DUE TO BLEED 1 AND 2 FAILED ON TAKEOFF AT TO-1. RESET SUCCESSFUL REPEAT AT 11000FT. FAILED AGAIN BLEEDS 1 AND 2. REMOVED AND REPLACED ENGINE NR 1 PRSOV AS PER AMM 36-11-03. REMOVED AND REPLACED HP BLEED VALVE NR 2 AS PER 36-11-01 AND AMS CONTROLLER IN SPDA NR 2 SLOT 23 IAW 21-00-02, OPS CHECK NORMAL.
Part: BLEED VALVE — FAILED (BLEED AIR SYS) · airframe 17,217 hrs · 10,290 cycles
FLT NR 1731 JFK-BDA, AIR TURNBACK TO JFK DUE TO BLEED 1 AND 2 FAILED ON TAKEOFF AT TO-1. RESET SUCCESSFUL REPEAT AT 11000F. FAILED AGAIN BLEEDS 1 AND 2. REMOVED AND REPLACED ENGINE NR 1 PRSOV AS PER AMM 36-11-03. REMOVED AND REPLACED HP BLEED VALVE NR 2 AS PER 36-11-01 AND AMS CONTROLLER IN SPDA NR 2 SLOT 23 IAW 21-00-02 OPS CHECK NORMAL.
2012
Part: POWER UNIT — FAILED (CABIN) · airframe 15,553 hrs · 9,245 cycles
FLT 1018 JFK-BOS, ON GROUND CHECK FOUND R2 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT FOR R2 DOOR IAW AMM 33-50-01-04. OPS CHECK GOOD.
2010
Part: BLEED AIR SYS — FAILED (NR 1) · airframe 10,478 hrs · 6,216 cycles
FLT 331 IAD-MCO, AIR RETURN TO IAD DUE TO SMOKE AND HAZE IN ENTIRE AIRCRAFT PRIOR TO ROTATION FOLLOWED BY BLEED 1 FAIL AT APPROX 1000 FEET. CREW DECLARED EMERGENCY AND A/C RETURN TO FIELD. PERFORMED VISUAL INSPECTION PER FIM 21-20-00-810-801-A AND NO DEFECTS NOTED IN AIRCRAFT. SUSPECT CONTAMINATION OF BLEED SYS DURING R/R OF NAPRSOV. A/C OK TO CONTINUE SERVICE.
2008
Part: ELECTRONIC UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 3,533 hrs · 2,119 cycles
AT GATE, NR 2 TRU FAILED UPON SHUTDOWN. FOLLOWED BY RECIRC, SMOKE AND SMELL OF SMOKE IN FWD CABIN. OCCURRED FOLLOWING ENGINE SHUTDOWN AFTER GPU CONNECTED. PERFORMED FIM TASK 21-20-00-810-801-A AND FOUND HS-ACE IMPLODED. NO DAMAGE FOUND IN SURROUNDING AREA. REMOVED AND REPLACED HS-ACE REF MM 27-43-01, OPS CHECK GOOD AFTER HS-ACE REPLACED REF FIM 24-31-00.
Part: CONTROL VALVE — FAULTED (BREAKS) · airframe 2,786 hrs · 1,714 cycles
FLT NR 611, PWM-JFK, MESSAGES AT GEAR EXTENSION- BRK LH FAULT, BRK RT FAULT, REDUCED BRAKE EFFECTIVENESS ON ROLL OUT AND TAXI IN NOTED. DE/RE-ENERGIZE A/C PER FIM 32-41-00. REPLACED NR 4 BRAKE CONTROL VALVE PER AMM 32-41-00. OPS OK, LEAK CHECKED OK.