N228JB
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.
91 reports on file, 2006-12-28 – 2025-03-10.
Part: PINTLE PIN — INADEQUATE (ZONE 700) · airframe 4,641,062 hrs · 30,310 cycles
DURING THE MAINTENANCE INSPECTION, IT WAS FOUND THE LOWER RH MLG AFT PINTLE PIN AFFECTED BY THE ANAC AD 2019-11-07, DUE TO THIS FACT THE PIN WAS REPLACED, THE JOB WAS HANDLE AND DOCUMENTED UNDER COOPESA ITEM A1P296 1 85 AND 7 476.
Part: SKIN PANEL — DAMAGED (ZONE 600) · airframe 4,641,062 hrs · 30,310 cycles
DURING THE MAINTENANCE INSPECTION, WERE FOUND 7 HOLES ALREADY OVERSIZED COMMON TO THE EMBRAER SB 190-57-0056 COVER AREA, THE ISSUE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900584 AND THE COOPESA ENGINEERING ORDER COO-EO-2025-21654-R00.
Part: PINTLE PIN — INADEQUATE (ZONE 700) · airframe 4,641,062 hrs · 30,310 cycles
DURING THE MAINTENANCE INSPECTION, IT WAS FOUND THE LOWER RH MLG AFT PINTLE PIN AFFECTED BY THE ANAC AD 2019-11-07, DUE TO THIS FACT THE PIN WAS REPLACED, THE JOB WAS HANDLE AND DOCUMENTED UNDER COOPESA ITEM A1P296 1 86 AND 7 477.
Part: LINK — CORRODED (ZONE 400) · airframe 4,641,062 hrs · 30,310 cycles
DURING THE MAINTENANCE INSPECTION, PYLON #2, LOWER LINK FITTING, INBOARD & OUTBOARD LUG, INBOARD FACE WITH CORROSION THE DAMAGE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900325 AND THE COOPESA ENGINEERING ORDER COO-EO-2025-21594-R00
Part: SKIN PANEL — DAMAGED (ZONE 600) · airframe 4,641,062 hrs · 30,310 cycles
DURING THE MAINTENANCE INSPECTION, WERE FOUND 8 OVERSIZED HOLES COMMON TO THE EMBRAER SB 190-57-0056 COVER AREA, THE ISSUE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900055-A AND THE COOPESA ENGINEERING ORDER COO-EO-2025-21515-R00.
Part: SKIN PANEL — CRACKED (ZONE 600) · airframe 4,641,062 hrs · 30,310 cycles
DURING THE MAINTENANCE INSPECTION, DURING SEALANT REMOVAL FOR A FUEL LEAK CORRECTION, A CRACK AT THE R/H WING, REAR SPAR AREA, LOWER SKIN NEAR TO RIB20 WAS FOUND. THE DAMAGE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-903131 AND THE COOPESA ENGINEERING ORDER COO-EO-2025-21888-R00.
Part: SKIN PANEL — DAMAGED (ZONE 500) · airframe 4,641,062 hrs · 30,310 cycles
DURING THE MAINTENANCE INSPECTION, WERE FOUND 7 HOLES ALREADY OVERSIZED (5/16 2ND OVERSIZE) COMMON TO THE EMBRAER SB 190-57-0056 COVER AREA, THE ISSUE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900473 AND THE COOPESA ENGINEERING ORDER COO-EO-2025-21656-R00.
Part: SKIN PANEL — DAMAGED (ZONE 500) · airframe 4,641,062 hrs · 30,310 cycles
DURING THE MAINTENANCE INSPECTION, WAS IDENTIFIED EIGHT (8 EA) EXISTING FASTENER HOLES WITH OVERSIZED DIAMETERS COMMON TO LOWER SKIN AND SPAR I, BETWEEN RIB 9-10 AND WITHIN THE AREA COVERED BY EMBRAER SB190-57-0056 REV 00, THE ISSUE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900054 AND THE COOPESA ENGINEERING ORDER COO-EO-2025-21510-R00
Part: SKIN PANEL — CORRODED (ZONE 100) · airframe 4,641,062 hrs · 30,310 cycles
DURING THE MAINTENANCE INSPECTION, CORROSION WAS FOUND ON THE INNER SURFACE OF THE FUSELAGE SKIN AT FR82, BETWEEN STRG-27R AND STRG-28R. THE DAMAGE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900569 AND THE COOPESA ENGINEERING ORDER COO-EO-2025-21613-R00.
Part: SKIN — DAMAGED (ZONE 100) · airframe 4,641,062 hrs · 30,310 cycles
DURING THE MAINTENANCE INSPECTION TWO LIGHTNING STRIKE WAS FOUND AT (THROUGH DAMAGES 1) FR 20+42MM, STR 27LH+26MM AND (THROUGH DAMAGES 2) AT FR 20+22MM, STR 27LH+70MM, THE DAMAGES WERE CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900865 AND THE COOPESA ENGINEERING ORDER COO-EO-2025-21643-R00.
Part: SKIN PANEL — CRACKED (ZONE 600) · airframe 4,641,062 hrs · 30,310 cycles
DURING THE MAINTENANCE INSPECTION, IT WAS FOUND ON RH WING FIXED LEADING EDGE THE SKIN CRACKED AT LEADING EDGE SLAT TRACK #5 OUTBD TRACK UPPER CORNER AREA. THE DAMAGE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900948 AND THE COOPESA ENGINEERING ORDER COO-EO-2025-21666-R00
Part: SKIN PANEL — CRACKED (ZONE 500) · airframe 4,641,062 hrs · 30,310 cycles
DURING THE MAINTENANCE INSPECTION, IT WAS FOUND ON LH WING FIXED LEADING EDGE THE SKIN CRACKED AT LEADING EDGE SLAT TRACK #5 OUTBD TRACK UPPER CORNER AREA. THE DAMAGE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900947AND THE COOPESA ENGINEERING ORDER COO-EO-2025-21665-R00
Part: SKIN PANEL — MISREPAIRED (ZONE 100) · airframe 4,641,062 hrs · 30,310 cycles
DURING THE MAINTENANCE INSPECTION, IT WAS FOUND AT THE FORWARD FUSELAGE SKIN, FROM FR18+155MM TO FR19+60MM, BETWEEN STR-26LH AND STR-27LH+170MM, AN EXISTING DOUBLER THAT DOES NOT COMPLY WITH ETD2017-190-024715 DATED MARCH 20, 2017, GUIDELINES. THE ISSUE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900518 AND THE COOPESA ENGINEERING ORDER COO-EO-2025-21662-R00.
Part: CROSSBEAM — CORRODED (ZONE 100) · airframe 4,641,062 hrs · 30,310 cycles
DURING THE MAINTENANCE INSPECTION, CORROSION WAS FOUND ON THE CROSS BEAM FR84 WITH CORROSION (4 LOCATIONS) BETWEEN Y-330/-Y860, THE DAMAGE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900179-A AND THE COOPESA ENGINEERING ORDER COO-EO-2025-21565-R01.
Part: SKIN PANEL — SCRATCHED (ZONE 200) · airframe 4,641,062 hrs · 30,310 cycles
DURING THE MAINTENANCE INSPECTION, SCRATCHES WERE FOUND ON THE EXTERNAL SKIN PANEL OF THE CENTER FUSELAGE II, AFT PLUG, LOCATED BETWEEN FR67 AND FR72, BETWEEN STR 01 LH AND STR 01 RH, THE DAMAGE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900264 AND THE COOPESA ENGINEERING ORDER COO-EO-2025-21591-R00.
Part: SKIN — DAMAGED (ZONE 500) · airframe 4,641,062 hrs · 30,310 cycles
DURING THE MAINTENANCE INSPECTION IT WAS DISCOVERED THAT THERE IS AN EXISTING REPAIR ON THE L/H WING LOWER SKIN AT RIB 10, WITH NO MATERIAL TRACEABILITY, THE ISSUE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900721 AND THE COOPESA ENGINEERING ORDER COO-EO-2025-21668-R00.
Earlier reports · 2006–2023 · 75 reports
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,069 hrs · 29,319 cycles
DURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION IN SEAT TRAC LOCATED BETWEEN FR 39/43 AND Y= 270.0 IN CF II PASSENGER FLOOR STRUCTURE; REF TOMX WO 2313 NRC 00153 CORROSION IN SEAT TRACK LOCATED BETWEEN FR 39/43 AND Y= 270.0 IN CF II PASSENGER FLOOR STRUCTURE WAS REMOVED AND EVALUATED WITHIN LIMITS PER EMB 190 SRM 51-12-01 AND SRM 51-10-03 AND SRM 53-22-10 AD/51. (CONSIDERED AS A MAJOR REPAIR)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,069 hrs · 29,319 cycles
DURING HEAVY MAINTENANCE: EXTERNAL EMERGENCY LIGHT FOUND INOP DURING LIGHTS CHECK; ELPU'S #3 AND #6 FOUND TO BE INOP. REMOVED AND REPLACED #3 AND #6 ELPU'S IAW EMB 190 AMM 33-50-01-400-801-A. OPS TEEST GOOD. REF TOMX NRC 00318 FOR ALL WORK ACCOMPLISHED.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,069 hrs · 29,319 cycles
DURING HEAVY MAINTENANCE: CORROSION ON CUTOUT OF A/C WASTE SERVICE PANEL (REF TOMX NRC# 00009); CORROSION ON CUTOUT OF WASTE SERVICE PANEL WAS REMOVED AND FOUND TO BE OUT OF LIMITS PER EMB-190 SRM 53-23-60 PAR 4 TABLE 101. CUTOUT AREA OF WASTE SERVICE PANEL WAS REPAIRED PER EMB-190 SRM 53-23-60 REPAIR 51P REF TOMX NRC# 00009 FOR ALL WORK ACCOMPLISHED.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,069 hrs · 29,319 cycles
DURING HEAVY MAINTENANCE: BOTTOM TAIL CONE FITTING HAS CORROSION; REMOVED CORROSION ON BOTTOM FITTING OF TAIL CONE. FOUND TO BE OUT OF LIMITS PER EMB-190 SRM 53-31-02 AD/54 PAR 4 AND 5 FIG 101. REMOVED AND REPLACED BOTTOM TAIL CONE FITITING IAW EMB-190 SRM 51-41-01,SRM 51-42-03 AND SRM 51-43-03. REF. TOMX NRC# 00326 FOR ALL WORK ACCOMPLISHED.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,069 hrs · 29,319 cycles
DURING HEAVY MAINTENANCE: CORROSION ON FR 80 AT STR 27RH AND STR28RH AT AFT CARGO DOOR CUTOUT; REMOVED CORROSION ON FR 80 AT STR 27R TO STR 28R FOUND TO BE OUT OF LIMITS PER EMB SRM 53-23-60 PERFORMED A TEMPORARY REPAIR PER ETD 2023-190-018873 REV A, EC # E23-700-01 AND ETI-190-23-610 REV 3. REF TOMX NRC# 00162 FOR ALL WORK ACCOMPLISHED.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,069 hrs · 29,319 cycles
DURING HEAVY MAINTENANCE: WINGS / LH WING / BIRD STRIKE STRUCTURE ASSY / SKIN / RIB 10 TO RIB 11 / WEAR DAMAGE â PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,069 hrs · 29,319 cycles
DURING HEAVY MAINTENANCE: CORROSION ON FLOOR BEAM BTW FR87 AND FR88 AND Y: 300 RH AT FLOOR STRUCTURE (W2); (RESOLVED ON W/O: 1225110 TASKCARD: NR-00014 ) REMOVED CORROSION ON FLOORBEAM BTW FR 87 AND FR 88 AND Y: 300 RH BLEND OUT FROM ORIGINAL THICKNESS OF .063" WAS .026" WITH A REMAINING THICKNESS OF .036" WAS FOUND OUT OF LIMITS PER EMB 190 SRM 53-23-10AD/52 PAR 5 TABLE 101. REMOVED AND REPLACED FLOOR BEAM IAW EMB 190 SRM 51-42-01, SRM 51-43-03.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 45,069 hrs · 29,319 cycles
DURING HEAVY MAINTENANCE: CORROSION ON FLOOR BEAM BTW FR87 AND FR88 AND Y: 300 RH AT FLOOR STRUCTURE (W2); REMOVED CORROSION ON FLOOR BEAM BTW FR 87 AND FR 88 AND Y: 300 RH BLEND OUT FROM ORIGINAL THICKNESS OF .063" WAS .026" WITH A REMAINING THICKNESS OF .036" WAS FOUND OUT OF LIMITS PER EMB 190 SRM 53-23-10AD/52 PAR 5 TABLE 101. REMOVED AND REPLACED FLOOR BEAM IAW EMB 190 SRM 51-42-01, SRM 51-43-03. (CONSIDERED AS A MAJOR REPAIR)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,069 hrs · 29,319 cycles
DURING HEAVY MAINTENANCE: CORROSION ON EXTERNAL FUSELAGE SKIN AND FASTENERS AT AREA COVERED BY LIVE TV RADOME; REMOVED CORROSION FROM AREA UNDER LIVE TV RADOME FOUND TO BE WITHIN ALLOWABLE LIMITS BUT CORROSION ON DOUBLER WAS FOUND OUT OF LIMITS. REMOVED AND REPLACED DOUBLER PER EMB 190 SRM 53-22-01/AD51. ETD 2015-190-068762 REV A AND EC # E23-679-01 REF TOMX NRC# 00239 FOR ALL WORK ACCOMPLISHED.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,069 hrs · 29,319 cycles
DURING HEAVY MAINTENANCE: WEAR AND BARE SKIN FOUND ON LH WING FIXED LEADING EDGE BTW RIBS 10 AND 11; WEAR AND BARE SKIN ON LH WING L/E FIXED BTW RIB 10 AND 11 WAS REPAIRED PER ETD 2023-190-019820 REV B. AND EC# E23-737-01 REFERENCE TOMX NRC# 00291 FOR ALL WORK ACCOMPLISHED.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,069 hrs · 29,319 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FLOOR STRUCTURE CROSS BEAM X=3301.3 / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,069 hrs · 29,319 cycles
DURING HEAVY MAINTENANCE: CORROSION IN LONGITUDINAL FLOOR BEAM LOCATED IN Y=300.0 BETWEEN FR 13/18 NI FWD FUS PASSENGER CABIN STRUCTURE; (RESOLVED ON W/O: 1225110 TASKCARD: NR-00013 ) CORROSION IN LONGITUDINAL FLOOR BEAM LOCATED IN Y=300.0 BETWEEN FR 13/18 IN FWD FUS PASSENGER CABIN FLOOR STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS PER EMB 190 SRM 51-12-01 AND SRM 51-10-03 AND SRM 53-10-10/AD51. THEREFORE WAS REPLACED PER EMB 190 SRM 51-41-01, SRM 51-41-02, SRM 51-43-03 AND SRM 51-43-04. ALL WORK ACCOMPLISHED ON TOMX WO # 2313 N/R# 00134. ACCOMPLISHED BY TOMX TECH # 429021. RII BY TOMX QC # 299517.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,069 hrs · 29,319 cycles
DURING HEAVY MAINTENANCE: CRACK ON RH WING FIXED LEADING EDGE BTW RIB 19 AND RB20. SLAT TRACK # 5 CUTOUT; REF TOMX WO 2313 NR # 00024 RH WING FIXED LEADING EDGE BTW RIB 19 AND RB20. SLAT TRACK # 5 CUTOUT WAS REPAIRED PER EMB-190 SRM 57-49-01 REPAIR 5.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,069 hrs · 29,319 cycles
DURING HEAVY MAINTENANCE: CORROSION ON CROSSBEAM LOCATED AT FR 11 BETWEEN Y= -370.0 AND Y= 370.0 COCKPIT FLOOR STRUCTURE; REMOVED CORROSION AND REPAIRED AREA PER EMB 190 SRM 51-12-01, SRM 51-10-03 AND REPAIRED PER EC# E23-707-01 REF. TOMX NR# 00141 FOR ALL WORK ACCOMPLISHED.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,069 hrs · 29,319 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / FR80 BETWEEN STGR 27R-28R / CORROSION - TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,069 hrs · 29,319 cycles
DURING HEAVY MAINTENANCE: FUSELAGE / CTR FUSELAGE II / UPPER SKIN / LIVE TV RADOME AREA / BTW FR 63-64 / STGR 01L & STGR 02L / PREVIOUS DOUBLER / PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,069 hrs · 29,319 cycles
DURING HEAVY MAINTENANCE: CORROSION ON SEAT TRACK (RH) BTW FR 79 AND FR 81 Y -100 REFERENCE TOMX NRC# 00173; REMOVED CORROSION FROM SEAT TRACK (RH) BTW FR79 AND FR81 AT Y-100 FOUND TO BE OUT OF LIMITS PER EMB 190-SRM 53-23-10/AD51. REMOVED AND REPLACED SEAT RACK IAW SRM 51-41-02, SRM 51-43-03 AND SRM 51-43-04 REF TOMX NRC# 00173 FOR ALL WORK ACCOMPLISHED.
2021
Part: BLEED AIR SYS — LOOSE (RH ENGINE FAN) · airframe 41,152 hrs · 26,497 cycles
FLT # 1937, SJU-SDQ(AIR TURN BACK TO SJU). BLEED 2 INOP (FAIL) RESET TWICE PER QRH ; FOUND MULTIPLE BLEED LINES LOOSE. REAJUSTED CLAMP LINES IAW AMM 36-11-08. PERFORMED ENGINES RUN. OPS CHECK OKAY. SEE LOG PG. 3188041 ITEM 1 AND 2 FOR R/R OF RH ENG FAN AIR VLV/AMS MOTOR CARD. A/C OKAY TO CONT. IN SVC.
Part: UNKNOWN — ODOR (CABIN) · airframe 40,737 hrs · 26,236 cycles
FLT 718, MSP-JFK. ABNORMAL SMELL IN CABIN INSPECTION REQUIRED; ACCOMPLISHED INSPECTION REF 21-00-00-810-801-A. NO FAULTS NOTED AS FLIGHT CRW TURNED PACK 2 OFF. NO ODOR SMELL PRESENT. ACCOMPLISHED THE MAINTENANCE OPERATIONAL TEST OF THE ELECTRONIC EQUIPMENT RACK VENTILATION SYSTEM MAIN COMPONENTS PER AMM TASK 21-28-00/500. VERIFIED VENT SHUT OFF VALVE AND GROUND SHUT OFF VALVE OPERATE NORMALLY
Part: VALVE — FAILED (FAN AIR) · airframe 40,551 hrs · 26,113 cycles
FLT 1274, CHS-RDU. BLEED 2 FAILURE IN FLIGHT WHEN AI SYS CAME ON AT FL 260 ; REMOVED AND REPLACED #2 ENGINE FAN AIR VALVE IAW AMM 36-11-09 OPS CHK OK NO FAULTS NOTED AFTER ENGINE RUNS.
2020
Part: FLOORBEAM — CORRODED (FRAME 17) · airframe 39,347 hrs · 25,394 cycles
DURING HEAVY MAINTENANCE, CORROSION FLOOR STRUCTURE BEAM LT FRAME 17 IN PASSENGER CABIN. RESOLVED ON W/O: 1072873 TASKCARD: NR-00007, REF ARM N/R 2020-317342 W/O 2020-348/1 TECH 8611312 RII QC 172. PERFORMED REPAIR (3 EA) ON FLOOR BEAM AT LEVEL OF FRAME 16, FRAME 17 AND FRAME 19, IAW SRM E190 53-10-10 REPAIR 51. THIS REPAIR IS PERMANENT AND NOT REQUIRED RE-INSPECTION.
Part: SHEAR TIE — CORRODED (FRAME 35) · airframe 39,347 hrs · 25,394 cycles
DURING HEAVY MAINTENANCE, CORROSION FLOOR STRUCTURE SHEAR TIE ON FRAME 35 BETWEEN STR 28L TO STR 27L ON FWD CARGO COMPARTMENT (1 EA) CPCP RELATED 53-22-003. REMOVED AND REPLACED STRUCTURE SHEAR TIE ON FRAME 35 BETWEEN STR 28L TO STR 27L ON FWD CARGO COMPARTMENT (1 EA), IAW E190 SRM 51-40-08 AND DWG 190-23014-429. ACCOMPLISHED ON AEROMAN NCR 2020-317375. CLASSIFIED AS MAJOR.
Part: SHEAR TIE — CORRODED (FRAME 86) · airframe 39,347 hrs · 25,394 cycles
DURING HEAVY MAINTENANCE, CORROSION ON SHEAR TIE LOCATED FR 86 BETWEEN STR 27R TO STR 28R ON AFT CARGO COMPARTMENT. RESOLVED ON W/O: 1072873 TASKCARD: NR-00011, REF ARM N/R 2020-317456 W/O 2020-348/1 TECH 8627612 RII QC163. REMOVED AND REPLACED SHEAR TIE AND FASTENERS LOCATED FRAME 86 BETWEEN STR 27R TO STR 28R, IAW E190 SRM 51-40-08 AND DRAWING 170-65180-433.
Part: SHEAR TIE — CORRODED (FRAME 88) · airframe 39,347 hrs · 25,394 cycles
DURING HEAVY MAINTENANCE, CORROSION SHEAR TIE FLOOR STRUCTURE LOCATED FRAME 88 STRINGER 27R TO STR 28R ON AFT CARGO COMPARTMENT (1 EA) CPCP RELATED 53-23-018-0428. REMOVED AND REPLACED SHEAR TIE FLOOR STRUCTURE LOCATED FRAME 88 STRINGER 28R AT AFT GALLEY AREA, IAW E190 SRM 51-40-08 AND DRAWING 170-65180-433. TOOL USED CALIPER P/N: 500-193, S/N: 1116083, DUE DATE: SEP-10-2021. ACCOMPLISHED ON AEROMAN NRC 2020-317341 WO: 2020 348/1. CLASSIFIED AS MAJOR.
Part: SHEAR TIE — CORRODED (FRAME 87) · airframe 39,347 hrs · 25,394 cycles
DURING HEAVY MAINTENANCE, CORROSION FLOOR STRUCTURE SHEAR TIE FR 87 STR 28R STR 29R AT AFT GALLE Y AREA. RESOLVED ON W/O: 1072873 TASKCARD: NR-00012, REF ARM N/R 2020-317418 W/O 2020-348/1 TECH 8627612 RII QC248. REMOVED AND REPLACED SHEAR TIE AND FASTENERS LOCATED FR 87 FROM STGR 28R TO STGR 29R AT AFT GALLEY AREA, IAW E190 SRM 51-40-08 AND DRAWING 170-651.
Part: SHEAR TIE — CORRODED (FRAME 88) · airframe 39,347 hrs · 25,394 cycles
DURING HEAVY MAINTENANCE, CORROSION SHEAR TIE FLOOR STRUCTURE LOCATED ON FRAME 88 BETWEEN STR 28R TO STR 29R ON AFT CARGO COMPARTMENT. RESOLVED ON W/O: 1072873 TASKCARD: NR-00010, REF N/R 2020-317432 W/O 2020-348/1. REMOVED AND REPLACED SHEAR TIE AND FASTENERS LOCATED ON FRAME 88 BETWEEN STR 28R TO STR 29R, IAW E190 SRM 51-40-08 AND DRAWING 170-65180-433.
Part: STRINGER — CORRODED (FRAMES 87-88) · airframe 39,347 hrs · 25,394 cycles
DURING HEAVY MAINTENANCE, CORROSION STRINGER 28R BETWEEN FRAME 87 TO STR 88 ON AFT CARGO COMPARTMENT (1 EA). CPCP RELATED 53-23-018-0428. PERFORMED PERMANENT REPAIR ON STRINGER 28R BETWEEN FR 87 TO FR 88 AFT GALLEY AREA, IAW E190 SRM 53-23-03 REPAIR 51 ITEM 5. TOOL USED CALIPER P/N: 500-197-30, S/N: A18135089, DUE DATE: JUL-11-2021. ACCOMPLISHED ON AEROMAN NRC 2020-317400 W/O: 2020 348/1. CLASSIFIED AS MAJOR.
Part: SKIN — CRACKED (LT WING TE) · airframe 39,347 hrs · 25,394 cycles
DURING HEAVY MAINTENANCE, CRACK LOWER SURFACE EXTERNAL SKIN TRAILING EDGE BETWEEN RIB 9 TO RIB 10 ON LT WING. RESOLVED ON W/O: 1072873 TASKCARD: NR-00006, REF ARM N/R 2020-317262 W/O 2020-348/1. PERFORMED PERMANENT REPAIR ON LOWER SKIN TRAILING EDGE BETWEEN RIB 9 AND RIB 10 LT WING, IAW E190 SRM 57-10-01, REPAIR 54, ITEM 9. ACCOMPLISHED BY ARM TECH 8610912 RII QC 217.
Part: LIGHT — BURNED (CABIN) · airframe 39,347 hrs · 25,394 cycles
DURING HEAVY MAINTENANCE, BURNED SEGMENT FWD LAVATORY EMERGENCY LIGHT NEXT TO DOOR L1 AT FWD GALLEY AREA. RESOLVED ON W/O: 1072873 TASKCARD: NR-00013, REF ARM N/R 2020-317425 W/O 2020-348/1 TECH 8602112 RII QC 200. REMOVED AND REPLACED SEGMENT FWD LAVATORY EMERGENCY LIGHT NEXT TO DOOR L1 AT FWD GALLEY AREA, IAW E190 AMM 33-50-15-000-801-A ITEM 2G STEP (3) AND AMM 33-50-15-400-801-A.
Part: SHEAR TIE — CORRODED (FRAME 87) · airframe 39,347 hrs · 25,394 cycles
DURING HEAVY MAINTENANCE, CORROSION SHEAR TIE FLOOR STRUCTURE FRAME 87 BETWEEN STR 27R TO STR 28R ON AFT CARGO COMPARTMENT. RESOLVED ON W/O: 1072873 TASKCARD: NR-00008, REF ARM N/R 2020-317398 W/O 2020-348/1TECH 8627612 RII QC 248. REMOVED AND REPLACED SHEAR TIE FLOOR STRUCTURE FRAME 87 FROM STR 27R TO STR 28R AT AFT GALLEY AREA (1 EA), IAW E190 SRM 51-40-08 AND DRAWING 170-65180-433 AND 170-65720-433.
Part: SERVICE PANEL — CORRODED (FRAME 88) · airframe 39,347 hrs · 25,394 cycles
DURING HEAVY MAINTENANCE, CORROSION SURROUND WASTE SERVICE PANEL FRAME 88 STR 88 STR 27R TO STR 28R INTERNAL AREA ON AFT CARGO COMPARTMENT (CPCP RELATED 53-23-018-0428). REMOVED AND REPLACED SECTION FRAME AND FASTENERS LOCATED FROM STR 25L TO STR 26R AT INTERNAL AREA OF AFT GALLEY AREA, IAW E190 SRM 51-40-08 AND DRAWING 170-66000-435. TOOL USED CALIPER P/N: 500-197-30, S/N: A18234376, DUE DATE: JUL-30-2021; P/N: NORTEC 600D, S/N: 190023010, DUE DATE: NOV-11-2020; P/N 45MG , S/N: 130066701, DUE DATE: MAR-05-2021. ACCOMPLISHED ON AEROMAN NRC 2020-317339. ACCOMPLISHED ON AEROMAN NRC 2020-317339. CLASSIFIED AS MAJOR
Part: FRAME — CORRODED (FRM 87) · airframe 39,347 hrs · 25,394 cycles
DURING HEAVY MAINTENANCE, (ARM N/R 2020-317399 W/O 2020-348/1) CORROSION FLOOR STRUCTURE FRAME 87 AROUND STR 27R TO STR 28R ON AFT CARGO COMPARTMENT. RESOLVED ON W/O: 1072873 TASKCARD: NR-00009. REFARM N/R 2020-317399 W/O 2020-348/1 TECH 8627612 RII QC 172. REMOVED AND REPLACED SECTION FRAME 87 AND FASTENERS LOCATED FROM STR 25L TO STR 25R, IAW E190 SRM 51-40-08 AND DRAWING 170-65720-433.
Part: SENSOR — FAILED (AOA) · airframe 39,231 hrs · 25,317 cycles
FLT 2020. FLL-ORH. DIVERTED TO JFK. EMERGENCY FLIGHT DECLARED. ADS 1 FAIL IN FLIGHT TO ADS3 RH WAS BLOCKED OUT WITH LINES QRH TO ADS 2 COMMON SOURCE ATARUAL CONTINED FOR DURATION COULD NOT RESET ; R & R #1 PITOT/STATIC/AOA SENSOR IAW AMM 34-13-01 PERFORMED OPS CHK OF ADS IAW AMM 34-15-00 OPS CHK GOOD A/C OK FOR SVC
2019
Part: SKIN — CRACKED (RT WING) · airframe 38,581 hrs · 24,886 cycles
DURING HEAVY MAINTENANCE, CRACK LOWER SKIN PANEL BTW RIB 9 TO RIB 10 ON RH WING, 2EA. ACCOMPLISHED A REPAIR OF THE CRACK DAMAGE IAW EA 57-5052-19 & ETD 2019 - 190-161679, REV B, & EC E19-1061-01. CLASSIFIED AS MAJOR.
Part: SKIN — CRACKED (LT WING) · airframe 38,581 hrs · 24,886 cycles
DURING HEAVY MAINTENANCE, A CRACK ON THE LOWER SKIN PANEL, RIB 4, LT WING. ACCOMPLISHED A REPAIR OF THE CRACK DAMAGE IAW EA 57-5051-19 REV 0, ETD 2019-190-161652, REV A, & EC E19-1062-01. CLASSIFIED AS MAJOR.
2017
Part: SKIN — CORRODED (FRAMES 77-78) · corrosion level 2 · airframe 32,970 hrs · 20,890 cycles
CORROSION WAS DISCOVERED ON INTERNAL SKIN ON RIVET FROM FRAMES 77 TO 78, STRINGER 29R IN THE AFT CARGO BAY. PERFORMED A PERMANENT REPAIR IAW EC E17-1152-01, AND EA 53-0447-17, REV 0, PART 1,2.
Part: ACM — FAILED (RIGHT) · airframe 31,843 hrs · 20,026 cycles
AT LEVELE OFF DURING CRUISE FL300, UNCONTROLABLE HEAT IN CABIN FWD CABIN SENSOR LOOKS FAULTY. DIVERTED. R & R THE NR 2 PACK ACM IAW AMM 21-51-00. OPS CHECKED GOOD.
Part: DUCT — LEAKING (PNEUMATIC SYS) · airframe 31,786 hrs · 19,979 cycles
CLIMBING THROUGH 12000 FT MSL, RECEIVED A BLEED 2 LEAK EICAS, RAN CHECK LIST. BLEED ONE WAS ON MEL, RENDERING AIRCRAFT UNPRESSURIZED. DIVERTED. TROUBLESHOT PROBLEM TO A LEAKING PRECOOLER EXHAUST DUCT PANEL SEAL. REMOVED AND REPLACED THE SEAL IAW AMM 54-50-25.
Part: LATCH — DIRTY (R1 DOOR) · airframe 31,303 hrs · 19,619 cycles
R1 DOOR LATCH INDICATOR NOT GREEN WITH DOOR CLOSED AND LOCKED. CLEANED THE LATCH. OPS CHECKED OK.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 30,983 hrs · 19,389 cycles
DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT EMERGENCY FWD POWER UNIT WAS INOPERATIVE. REMOVED & REPLACED FWD BATTERY PACK IAW AMM 33-50-01. OPS CHECKED NORMAL.
Part: LIFE RAFT — UNSERVICEABLE (CABIN) · airframe 30,935 hrs · 19,350 cycles
JFK-BTV. LIFE RAFT PULL CORD TYPE ROPE THAT IS CORDED IS UNRAVELED AND HANGING DOWN TO THE FLOOR. PROTECTOR UN-FASTENED; REMOVED AND REPLACED LIFE RAFT AS PER AMM 25-66-01.
2015
Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 26,328 hrs · 16,249 cycles
DURING HEAVY MAINTENANCE, FOUND CORROSION SHEAR TIE AT FRAME 17, STR 27-28R. REMOVED CORROSION AND FOUND THE SHEAR TIE TO BE OUT OF LIMITS, REMOVED THE SHEAR TIE AND DRILLED A NEW SHEAR TIE. INSTALLED THE NEW SHEAR TIE IAW SRM 51-41-01, 51-41-02, AND 51-23-06.
Part: FINGER DOUBLER — CORRODED (FRAME 26) · corrosion level 2 · airframe 26,328 hrs · 16,249 cycles
DURING HEAVY MAINTENANCE, FOUND CORROSION FWD CARGO DOOR AFT FINGER DOUBLER. BLENDED AND OUT OF LIMITS. REMOVED THE FINGER DOUBLER IAW SRM 51-10-03, 51-43-03 AND 51-43-04. LOCATED, DRILLED, COUNTERSUNK, AND ALODINED NEW FINGER DOUBLER IAW SRM 51-40-02; 51-40-04; 51-23-04. INSTALLED THE NEW FINGER DOUBLER IAW SRM 51-43-04.
Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 26,328 hrs · 16,249 cycles
DURING HEAVY MAINTENANCE FOUND CORROSION SHEAR TIE AT FRAME 17, STR 25 -26R. REMOVED CORROSION, FOUND SHEAR TIE TO BE OUT OF LIMITS, REMOVED SHEAR TIE, DRILLED A NEW SHEAR TIE AND INSTALLED AND APPLIED FINISH REF SRM 51-41-01; 51-41-02 AND 51-23-06.
Part: BEAM — CORRODED (FRAMES 14-17) · corrosion level 2 · airframe 26,328 hrs · 16,249 cycles
DURING HEAVY MAINTENANCE, FOUND THE FWD SERVICE DOOR LOWER BEAM HAS CORROSION AT FWD AND AT GIRT BAR ATTACHMENT HOLES FRAME 14 - 17, STR 17R. REPAIRED IAW EA E15-692-01, BLENDED OUT, PERFORMED NDT AND TOPCOATED.
Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 26,328 hrs · 16,249 cycles
DURING HEAVY MAINTENANCE FOUND CORROSION SHEAR TIE AT FRAME 17, STR 24-25R. REMOVED CORROSION AND FOUND THE SHEAR TIE TO BE OUT OF LIMITS. REMOVED THE SHEAR TIE , DRILLED A NEW SHEAR TIE AND INSTALLED IAW SRM 51-41-01, 51-41-02 AND 51-23-06.
Part: BEAM — CORRODED (FRAME 77) · corrosion level 2 · airframe 26,328 hrs · 16,249 cycles
DURING HEAVY MAINTENANCE FOUND CORROSION ON AFT CARGO LOWER BEAM. REPAIRED IAW EA E15-709-01. PERFORMED SPOT FACING, NDT, AND TOPCOAT.
Part: BEAM — CORRODED (FRAME 86) · corrosion level 2 · airframe 26,328 hrs · 16,249 cycles
DURING HEAVY MAINTENANCE FOUND AFT SERVICE DOOR CUTOUT LOWER BEAM CORRODED. REPAIRED IAW EA E15-713-01. SPOTFACED, PERFORMED NDT, AND TOPCOATED.
Part: BEAM — CORRODED (FRAME 85) · corrosion level 2 · airframe 26,328 hrs · 16,249 cycles
DURING HEAVY MAINTENANCE, FOUND AFT PASSENGER DOOR CUTOUT LOWER BEAM HAS SEVERAL AREAS OF CORROSION. REPAIRED IAW EA E15-714-01. PERFORMED SPOT FACING. NDT AND TOPCOAT.
Part: BEAM — CORRODED (FRAME 24) · corrosion level 2 · airframe 26,328 hrs · 16,249 cycles
DURING HEAVY MAINTENANCE, FOUND CORROSION ON THE FWD CARGO DOOR LOWER BEAM. BLENDED AND FOUND OUT OF LIMITS. REMOVED THE BEAM IAW SRM 51-10-03, 51-43-03, 51-43-04, 51-41-01, AND 51-41-02. LOCATED, DRILLED, AND ALODINED THE NEW DOOR BEAM IAW SRM 51-40-02, AND 51-23-04. INSTALLED THE NEW BEAM IAW SRM 51-43-03, AND 51-43-04.
Part: FINGER DOUBLER — CORRODED (FRAME 25) · corrosion level 2 · airframe 26,328 hrs · 16,249 cycles
DURING HEAVY MAINTENANCE, FOUND FWD CARGO DOOR FWD FINGER DOUBLER CORRODED. BLENDED AND FOUND OUT OF LIMITS, REMOVED THE FINGER DOUBLER IAW SRM 51-10-03, 51-43-03, AND 51-43-04. LOCATED, DRILLED, COUNTERSUNK AND ALODINED THE NEW FINGER DOUBLER IAW SRM 51-40-02, 51-40-01, AND 51-23-04. INSTALLED THE NEW FINGER DOUBLER IAW SRM 51-43-04.
Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 26,328 hrs · 16,249 cycles
DURING HEAVY MAINTENANCE FOUND CORROSION THE SHEAR TIE AT FRAME 16 STR 27-28R. REMOVED CORROSION AND FOUND THE SHEAR TIE TO BE OUT OF LIMITS. REMOVED THE SHEAR TIE, DRILLED A NEW SHEAR TIE AND INSTALLED IAW SRM 51-41-01; 51-41-02; 51-23-06.
Part: FINGER DOUBLER — CORRODED (FRAME 77) · corrosion level 2 · airframe 26,328 hrs · 16,249 cycles
DURING HEAVY MAINTENANCE, FOUND CORROSSION ON AFT CARGO DOOR FWD FINGER DOUBLER. REMOVED AND REPLACED THE FINGER DOUBLE IAW SRM 51-43-03.
Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 26,328 hrs · 16,249 cycles
DURING HEAVY MAINTENANCE, FOUND CORROSION ON THE SHEAR TIE AT FRAME 17, STR 26-27R. REMOVED THE CORROSION AND FOUND THE SHEAR TIE TO BE OUT OF LIMITS, REMOVED THE SHEAR TIE, DRILLED UP NEW SHEAR TIE AND INSTALLED NEW SHEAR TIE AT FRAME 17, STR 26R-27R IAW SRM 51-41-01, 51-41-02, AND 51-23-06.
Part: FITTING — CORRODED (FRAME 16 GIRTBAR) · corrosion level 2 · airframe 26,328 hrs · 16,249 cycles
DURING HEAVY MAINTENANCE, FOUND THE FWD GIRT BAR FITTING CORRODED. REPAIRED IAW EA E15-722-01. BLENDED OUT, PERFORMED NDT, AND TOPCOATED.
Part: MOUNT — CORRODED (FRAME 16) · corrosion level 2 · airframe 26,328 hrs · 16,249 cycles
DURING HEAVY MAINTENANCE, FOUND FRAME 16 AND LAV MOUNT FITTING HAS CORROSION, LBL 48". REMOVED CORROSION ON MOUNT FITTING, IAW SRM 51-12-01. DAMAGE AT 1" FWD FRAME 16, LBL 48.0, 1.25 X 1.0 X .020 REQ. REPLACED PART. LOCATED AND DRILLED NEW FRAME 16 AFT LAV MOUNT FITTING, REF SRM 51-40-02 INSTALLED NEW MOUNT FITTING AND TOPCOATED IAW SRM 51-43-03; 51-23-06 .
2014
Part: DOOR — MALFUNCTIONED (R1) · airframe 22,015 hrs · 13,488 cycles
PILOT REPORTED R1 DOOR WILL NOT DISARM. FOUND REGULATOR IN ARMED POSITION, COULD NOT INSTALL SAFETY PIN. DEPLOYED SLIDE, CHECKED GOOD. R & R SLIDE ASSY AND ADJUSTED GIRT BAR, SERVICED R1 DOOR PNEUMATIC ASSY IAW AMM 25-65-01.
Part: GIRT BAR — FROZEN (R1 DOOR) · airframe 21,993 hrs · 13,473 cycles
CREW REPORTED THAT R1 DOOR ARMING HANDLE UNABLE TO MOVE UP. THE TECH FOUND AFT LOCK ON GIRT BAR FROZEN, UNFROZE GIRT BAR, OPS CHECKED GOOD IAW 52-12-40.
2013
Part: WATER HEATER — FAILED (FWD LAVATORY) · airframe 21,878 hrs · 13,408 cycles
CREW REPORTED ELECTRICAL ODOR NEAR FOWARD LAVATORY ENROUTE. TROUBLESHOOTING IAW FIM TASK 21-20-00 AND 25-40-00, ODOR COMING FROM FWD LAV WATER HEATER. R & R FWD LAV WATER HEATER IAW AMM 38-12-01. OPS CHECK GOOD.
Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 21,641 hrs · 13,256 cycles
CREW DECLARED AN EMERGENCY AND AIRCRAFT DIVERTED DUE TO L1 SLIDE DEPLOYED INFLIGHT. PERFORMED GVI OF SLIDE INSTALLATION SURFACES ON DOOR INCLUDING RODS AND MECHANICAL FUNCTIONS. NO DEFECTS NOTED. R & R SLIDE ON L1 DOOR IAW AMM 25-65-01. OPS CHECK GOOD.
Part: ACM — DAMAGED (NR 1) · airframe 21,306 hrs · 13,019 cycles
MOMENTARY ODOR, SMOKE BURNING, FOLLOWED BY PACK 1 FAIL. ODOR CLEARED IMMEDIATELY. REF FIM 21-20-00-810-801, ACCOMPLISHED INSPECTION AND IDENTIFY SOURCE OF ODOR. FOUND NR 1 ACM TURBINE BLADE DAMAGED. R & R NR 1 ACM IAW AMM 21-51-05. OPS & LEAK CHECKED GOOD.
Part: VALVE — FAILED (PARKING BRAKE) · airframe 21,264 hrs · 12,993 cycles
ACFT DIVERTED, AT 100KTS TAKE OFF CONFIGURATION WARNING ON EICAS FOLLOWED BY PARKING BRAKE NOT RELEASED ONCE AIRBORNE. MESSAGES WENT AWAY WHEN CLIMBING THROUGH 5000 FT. TAXI OK, NO BRAKE DRAGGING. FOLLOWING FIM TASK 32-41-00-810-852A & SHOWING ALREADY R & R EMERGENCY PARKING BREAK VALVE IAW AMM 32-44-01. R & R EMER PARK BREAK PRESS SWITCH NR 1 & NR 2 SYS REF 32-44-09. OPS CK IAW 32-44-09-720-801A GOOD. ALSO ACCOMP RIG PROC CHECK OF EMERGENCY PARKING BREAK VALVE REF 32-44-00-820-801A, CHECKED GOOD. EMERGENCY PARKING BRAKE ACCUMULATOR TEST GOOD IAW 32-44-13. ACFT OK FOR SVC.
Part: CONVERTER — FAILED (LEFT) · airframe 20,536 hrs · 12,479 cycles
DURING TAKEOFF AND CLIMBOUT, CREW REPORTED STRONG ODOR OF OZONE AND SMELL. SUBSIDED ON CLIMBOUT AND RETURNED TO A LESSER DEGREE ON APPROACH, NO OTHER EICAS OR SYS INDICATIONS IAW TASK 21-20-00-810-801A. REPLACED LT OZONE CONVERTER IAW MM 36-30-00.
Part: CONVERTER — FAILED (RIGHT) · airframe 20,536 hrs · 12,479 cycles
DURING TAKEOFF AND CLIMBOUT CREW REPORTED STRONG ODOR OF OZONE AND SMELL. SUBSIDED ON CLIMBOUT AND RETURNED TO A LESSER DEGREE ON APPROACH, NO OTHER EICAS OR SYS INDICATIONS IAW TASK 21-20-00-810-801A. REPLACED RT OZONE CONVERTER IAW MM 36-30-00.
Part: ENGINE — FIRE (NR 2) · airframe 19,668 hrs · 11,922 cycles
FLT 615 JFK-JAX, ENGINE NR 2 TAILPIPE FIRE EXTINGUISHED WITH PURPLE K DRY AGENT. REMOVED AND REPLACED NR 2 ENGINE ASSY PER TASK CARDS E190-71-00-01-400-801 + E190-71-00-01-000-801. LEAK CHECKS AND ENGINE RUNS ACCOMPLISHED, ALL OPS CHECK NORMAL.
2012
Part: WIRE HARNESS — DEFECTIVE (LE SLAT) · airframe 18,144 hrs · 10,998 cycles
FLT 956 MCO-BOS, RETURNED TO MCO DUE TO SLAT FAILED UPON RETRACTION. REMOVED AND REPLACED RIGHT OUTBOARD SLAT HARNESS IAW AMM 27-83-07 AND SLAT POSITION SENSOR IAW AMM 27-83-06. OPS CHECK NORMAL.
Part: PROXIMITY SENSOR — DEFECTIVE (NLG) · airframe 16,506 hrs · 9,964 cycles
FLT 1017, CREW DECLARED EMERGENCY AND AIRCRAFT RETURNED TO BOS DUE TO LANDING GEAR LEVER WOULD NOT COME UP ON TAKEOFF. FOUND INTERMITTENT CONNECTION AT RIGHT NOSE WEIGHT ON WHEELS PROX SENSOR. REPLACED HARNESS ASSY AND PROXIMITY SENSOR REFERENCE AMM 32-62-01-04.
2010
Part: FRAME — CORRODED (FUSELAGE) · airframe 11,395 hrs · 6,856 cycles
FLT 6428 JFK-BNA DURING HMV VISIT AT BNA FOUND FWD FUSELAGE FLOORBEAM HAS CORROSION AT APPROX FRAME 14 AND FRAME 19 ALONG LBL 12. REPAIRED IAW JB E10-175-01. STRUCTURAL CONDITION REPORT STATES ITEM WAS REPAIRED REF ETD2010-190/02525 REV B AND EA E10-175-01 REV 04/10/10.
2009
Part: ACTUATOR — FAILED (SLATS) · airframe 10,467 hrs · 6,289 cycles
FLT 658 MCO-ROC DECLARED AN EMERGENCY INTO ROC ON APPROACH WITH "SLAT FAIL" EICAS MESSAGE WHEN CREW SELECTED SLAT/FLAPS 1 THE SLATS REMAINED AT ZERO ALONG WITH A SPOILER FAULT MESSAGE PERFORMED QRH PROCEDURE AND LANDED UNEVENTFUL. MX PERFORMED FIM TASK 27-87-00-810-802-A SLAT SYSTEM RESET AND OPS CHECKS GOOD AND AIRCRAFT WAS FERRY FLIGHT TO JFK FOR FURTHER TROUBLESHOOTING AND OPS CHECK. AT JFK MX FOUND LEFT WING SLAT ACTUATORS NR 1 AND NR 3 TORQUE LIMITERS TRIPPED, REMOVED AND REPLACED SLAT ACTUATORS IAW 27-81-01 ACCOMPLISHED MECHANICAL AND ELECTRICAL RIGGING PER AMM 27-80-00-820, OPS TEST OK PER AMM 27-80-00-710-801. AIRCRAFT RETURNED TO SERVICE.
Part: SLAT — MALFUNCTIONED (WING) · airframe 10,416 hrs · 6,260 cycles
FLT 1211 BOS-BUF HAD A "SLAT FAIL" EICAS MESSAGE ON FINAL APPROACH TO BUF LANDED WITH SLATS 0 AND FLAPS 2. MX TROUBLESHOOTING FOUND FAULT CODE 27811021ACE PERFORMED FIM TASK 27-81-00-810-802-A. FOUND NO SLAT ACTUATOR TORQUE LIMITERS TRIPPED, FAULT CLEARED AND SLATS OPS CHECKS GOOD. PERFORMED RETURN TO SERVICE CHECK, NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE.
Part: ACTUATOR — FAILED (LE SLAT) · airframe 10,203 hrs · 6,131 cycles
FLT 87 - JFK-SLC SLAT FAIL EXECUTED QRH PROCEDURE. TROUBLESHOT SLAT SYSTEM FOUND TORQUE LIMITER OUTBOARD OF NR 1 ENG PYLON TRIPPED. ACCOMPLISHED RESET CHECK OK. TSI 2722 WAS ISSUED AT JFK TO REPLACED LT NR 2 SLAT INBOARD ACTUATOR. ALSO PERFORMED SLAT ACTUATOR INSPECTION/CHECK IAW AMM 27-81-01.
Part: WARNING SYSTEM — MALFUNCTIONED (LE SLAT) · airframe 7,977 hrs · 4,825 cycles
FLT 615, JFK-JAX, SLAT FAIL IN FLIGHT FLAP POSITION 2, RAN QRH LANDED. T/S PER FIM TASK 27-81-00-810-803-A. CLEARED INHIBITS. CYCLED SLATS/FLAPS SEVERAL TIMES. OPS CHECK GOOD. NO MESSAGE ON EICAS.
2008
Part: ACTUATOR — MALFUNCTIONED (L/E SLAT) · airframe 4,682 hrs · 2,989 cycles
FLT 1118, FLL-SYR, SLAT FAIL, AOA LIMIT FAIL, SPOILER FAULT, STICK SHAKER ANTICIPATED. EICAS MESSAGES UPON FLAP LEVER MOVEMENT FROM 0 TO 1, QRH PROCEDURES ACCOMPLISHED. LANDED SLAT 0, FLAPS 2. FAULT CODE 27811021ACE PRESENT. PERFORMED FIM TASK 27-81-00-810-802, FOUND LT NR 6 SLAT ACTUATOR TRIPPED. REMOVED AND REPLACED NR 6 LT SLAT ACTUATOR IAW 27-81-01, OPS CHECK OF SLAT SYS OK, NO FAULTS NOTED.
2007
Part: ACTUATOR — MALFUNCTIONED (L/E SLAT) · airframe 4,450 hrs · 2,870 cycles
FLIGHT 1264, AUS-BOS, SLAT FAIL EICAS MESSAGE ON APPROACH TO BOSTON. FOUND NR 3, 6 AND 8 SLAT ACTUATORS ON LEFT WING WITH TRIPPED TORQUE LIMITERS. REPLACED NR 3 AND 8 ACTUATORS PER 27-81-01. RESET NR 6 ACTUATOR, RAN SLAT SEVERAL TIMES, CHECK NORMAL PER 27-81-01. INSP CK ALL RIGGING, ELECTRIC CHECKS AND OPS CHECK NORMAL.
2006
Part: CIRCUIT CARD — FAILED (MAU 3) · airframe 1,633 hrs · 1,127 cycles
AVNX 3 MAU FAIL EICAS W/ASSOCIATED OTHER MESSAGES. AUTO CONFIG TRIM FAIL, AP FAIL, SPOILER FAULT, ADS 3 FAIL, EMS 2 FAIL. REMOVED AND REPLACED MAU 3 PSI CARD IAW AMM 31-41-02. SYSTEM OPS CHECK NORMAL. A/C OK FOR SERVICE.