N229JB

Part: CABIN PRESSURE — FAILED (CPCS-CTRL) · airframe 41,942 hrs · 27,004 cycles

FLT#6107, TPA-FLL. 'CABIN PRESSURE OVERPRESSURIZING DURING CLIMB AT 15000 SHOWING -300; AS PER TECH SUPPORT RECOMMENDATION AFTER FHDB/DVDR ANALYSIS, REMOVED AND REPLACED CABIN PRESSURE CONTROLLER AS PER M.M. 31-31-01. ACCOMPLISHED OPS TEST OF CPCS CONTROLLER AS PER M.M. 21-31-00-710-801. ALL OPS/IND. CHECK IS NORMAL AT THIS TIME. NO FAULTS /DEFECTS WERE NOTED. OK TO CONTINUE.'

Part: OUTFLOW VALVE — FAILED (OUTFLOW-VLV) · airframe 41,941 hrs · 27,003 cycles

FLT#2024, MCO-TPA. 'CABIN ALT HI DURING CLIMB OUT (10,500). RAN QRH; REF FIM 21-31-00 ACCOMPLISHED GVI PACK BAY DUCTS NO LEAKS NOTED PER AMM 21-51-21. GVI AIR MIX DUCTS AND VALVES NO LEAKS NOTED PER AMM 21-20-03. ACCOMPLISHED CABIN LEAK TEST PER AMM 21-31-00-720-802-A. TEST OK WITHIN LIMITS. DOWNLOADED DFDR AND QAR PER AMM 31-31-00. ITEM CONTINUES ON L/P 3343574-2 (ACCOMPLISHED FIM TASK 21-31-00-810-801A, COMPLIED WITH ALL WIRING CHECKS NO FAULTS FOUND, REMOVED AND REPLACED CPCS OUTFLOW VALVE IAW AMM 21-31-02 OPS CHECKS GOOD.).'

Part: PRESSURE SWITCH — FAILED · airframe 41,531 hrs · 26,747 cycles

FLT#441, BOS-CLE .(AIRCRAFT PREFORMED AN AIR TURN BACK, BOS-BOS). ' AFTER TAKEOFF BLEED 2 OVERPRESS DID NOT RESET RAN QRH. AIR RETURN BACK AIRCRAFT HAS HISTIRY OF BLEED ISSUES AND APU; ITEM RESOLVED ON LOG PAGE 3327106 ITEM 1. 3327106 ITEM 1: REPLACED RH BLEED PRESSURE SWITCH REF AMM 36-14-01. OPS TEST GOOD NO FAULTS NOTED. RH BLEED PRESSURE SWITCH REMOVED AND REPLACED.'

Part: BLEED VALVE — FAILED (FUS-FRNG-FWD-PNL) · airframe 41,529 hrs · 26,745 cycles

FLT#1354, DCA-BOS. (AIRCRAFT PREFORMED AN AIR TURN BACK DCA-DCA). 'BLEED 1 OVERPRESS COULD NOT RESET PER QRH; PERFORMED LEAK CHECK OF THE BLEED 1 HP SENSE LINE. FOUND SENSE LINE BROKEN.REMOVED ADN REPLACED HP VALVE SENSE LINE IN REFERENCE E190 AMM 36-11-01.LEAK CHECK GOOD AND OPS CHECK GOOD AT THIS TIME.AC OK TO CONTINUE AND FOUND CROSS BLEED VALVE LEAKING.REMOVED AND REPLACED CROSS BLEED VALVE IAW E190 AMM 36-10-01 OPS CHECK GOOD.

Part: NONE — NONE · airframe 41,506 hrs · 26,729 cycles

FLT#1552, RSW-HPN. 'A/C DIVERTED INTO MCO DUE TO BLEED 2 LEAK, SLIGHT ODOR MID CABIN AND IN COCKPIT. SECURED BLEED PER QRH; PERFORMED OPERATIONAL TEST OF ENGINE 2 BLEED SYSTEM AFTER REPAIR OF PRECOOLER SEAL. CHECKS GOOD IAW AMM 36-11-00. NO ODORS NOTED. SUSPECT ODOR WAS DUE TO LEAK. AIRCRAFT OKAY FOR SERVICE.'

Part: NONE — NONE · airframe 41,322 hrs · 26,600 cycles

FLT # 1393, FLL-NAS. (EMERGENCY DECLARED) ON DESCENT INTO NAS 9000 BRH LH/RH FAULT APPEARED FOLLOWED BY BRH LH/RH FAIL COMPLIED E/QRH AND LANDED IN NAS NO BRAKES ON IDG USED FULL T/R TO STOP; PERFORMED TSM 32-41-00-810-848-A FOUND TO BE TRANSITORY CONDITION MAIN BCM 1 NO FAULTS AT THIS TIME BNRAKE CHECK PERFORMED IAW AMM 32-41-00 AC GOOD FOR SVC (SUPPLEMENTAL INFORMATION ADDED MORE INFORMATION INTO DESCRIPTION)

Part: SKIN — CRACKED (LT WING) · airframe 40,301 hrs · 25,896 cycles

DURING HEAVY MAINTENANCE, CRACK ON LH WING FIXED LEADING EDGE SLAT TRACK# 5 CUTOUT; TEMPORARY REPAIR WAS PERFORMED PER EMB- 190 EC E21-809-01 ETI-190-21-788 REV1 AND ETD 2021-190-023168 REVA (7500FC) REPLACED SKIN WITH 750FC REINSPECTS UNTIL REPLACEMENT.

Part: SKIN — WORN (LT WING LE) · airframe 40,301 hrs · 25,896 cycles

DURING HEAVY MAINTENANCE, WEAR ON LH WING FIXED LEADING EDGE SKIN FROM RIB 12 TO RIB 13; LH WING FIXED LEADING EDGE SKIN 12 TO RIB 17 WAS REPLACED PER EMB190 SRM 51-41-02 AND ARM 51-43-04. PER CRACK FOUND OT=0.080"", RT= 0.080"" THEREFORE OUT OF LIMITS PER EMB 190 SRM 57-49-01 AD 51 PAR 5 TABLE 102 FIG 1 SHEET 5 PER TECHOPSMX WO#020000390739

Part: UNKNOWN — ODOR (CABIN) · airframe 39,815 hrs · 25,600 cycles

FLT 1394, NAS-FLL. DURING TAKEOFF AT APPROX 100KTS THE COCKPIT AND FWD CABIN FILLED WITH A STRONG EXHAUST/FUEL SMELL. THE ODOR DISSIPATED GRADUALLY AND WAS INPERCEPTABLE CLIMBING THROUGH 10000FT. THERE WAS NO VISABLE SMOKE OR MIST ASSOCIATED WITH THE ODOR; DURING T/S FOUND EXCESSIVE OIL IN APU COMPT. CLEANED APU INLET, COMPONENTS AND COMPT AS REQUIRED. PERFORMED HIGH POWER RUN WITH PACKS RUNNING REF GE LMM 72-00-00. NO FUMES / ODOR NOTED. A/C OK TO CONT.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 39,803 hrs · 25,593 cycles

FLT 1583, RSW-DCA. EMERGENCY LT POWER UNIT #2 FAILED FUNCTIONAL TEST ; REMOVED AND REPLACED #2 POWER UNIT IAW AMM 33-50-01. OPS CKS OK.

Part: VALVE — FAILED (FAN AIR) · airframe 39,520 hrs · 25,437 cycles

FLT 2323, DCA-MCO. RETURNED TO FIELD. BLEED 2 FAIL IN FLIGHT AFTER APU SHUT OFF (BLEED 1 WAS ON MEL). R & R FAN AIR VALVE, IAW E190 AMM 36-11-09. OPERATIONS CHECK GOOD. A/C OK FOR CONTINUED SERVICE.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 39,404 hrs · 25,378 cycles

DURING HEAVY MAINTENANCE, INOPERABLE EMERGENCY LIGHT POWER UNIT (ELPU) FWD LT SIDE, REF AEROMAN N/R 2020-349934. R & R EMERGENCY LIGHT POWER UNIT (ELPU), FWD LT SIDE, IAW E190 AMM 33-50-01-400-801-A. PERFORMED OPERATIONAL TEST, IAW E190 AMM 33-50-00-710-801-A/500. OPERATIONS CHECK GOOD.

Part: ACTUATOR — FAILED (HORIZ STAB) · airframe 37,273 hrs · 23,884 cycles

FLT 2002, JFK-BUF. DURING CLIMB AUTOPILOT OFF, PITCH TRIM ACTIVATED ON ITS OWN. PITCH TRIM FAIL, AUTOPILOT FAIL CAUTION EICAS ALONG WITH MACH TRIM FAIL, AUTOPILOT/TRIM DISCONNECT HELD DOWN. COMPLIED WITH QRH. SYSTEM RESET AFTER QRH PROCEDURE. ON FINAL APPROACH AUTO PILOT OFF, PITCH TRIM ACTIVATED ON ITS OWN, AP/TRIM DISCONNECT HELD DOWN UNTIL TOUCHDOWN,SYS 1 SYS 2 CUTOUT SWITCHES TO OFF. ACTIVE MESSAGES AP FAIL PITCH TRIM FAIL STALL PROTECT FAULT MACH TRIM FAULT; REMOVED AND REPLACED HSACE IAW AMM 27-43-01 PERFORMED OPS CHECK PER 27-40-00. OPS CHECK GOOD NO FAULTS NOTED. PERFORMED RTS PER AMM 27-00-00-070-801. NO FAULTS NOTED. A/C OK TO CONTINUE.

Part: SKIN — CRACKED (LT WING) · airframe 33,492 hrs · 21,181 cycles

DURING CURRENT (03/2018) HMV AT SAL, DAMAGE WAS FOUND ON THE LT WING AFT REAR SPAR LOWER SKIN (P/N: 190-33065-009) AFT EDGE, AT RIB 10+1” LEVEL. THE DAMAGE CONSISTS OF A CRACK MEASURING APPROXIMATELY 1.332” IN LENGTH (REF. /1/ FOR DETAILS). THE DAMAGE WAS ASSESSED USING THE APPLICABLE SRM SECTIONS AND DETERMINED TO BE OUT OF ANY ALLOWABLE/REPAIRABLE DAMAGE LIMITS. CONTACTED FOR REPAIR DISPOSITION WHICH CONSISTS OF A SERIES OF INSPECTIONS, TRIM-OUT REPAIR, FILLER & DOUBLER FABRICATION, INSTALLATION, AND SURFACE PROTECTION RESTORATION. EC E18-168-01 PROVIDES TEMPORARY REPAIR INSTRUCTIONS FOR THE NOTED DAMAGE. EC E18-168-02 IS A PLACE HOLDER EC TO TRACK THE PERMANENT REPAIR, DUE WITHIN 12 MONTHS, PENDING DAMAGE TOLERANCE ANALYSIS; THIS REPAIR HAS BEEN APPROVED BY VIA THE ATTACHED REF. /1/ ETD. THE REPAIR HAS BEEN DETERMINED TO BE 'MAJOR' AS PER THE GUIDELINES ESTABLISHED IN GMM. THIS REPAIR, ONCE COMPLETED PER THE INSTRUCTIONS ATTACHED TO THIS EC, IS TEMPORARY WITH NO ADDITIONAL POST REPAIR INSPECTIONS REQUIRED.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 32,998 hrs · 20,828 cycles

FT # 1038, AUS-BOS. AFT OVERHEAD EMERGENCY LIGHT INOP; R & R #5 POWER SUPPLY, EMERGENCY LIGHT, IAW AMM 33-50-01. OPS CHECK GOOD.

Part: ENGINE — CONTAMINATED (NR 1) · airframe 31,418 hrs · 19,667 cycles

RETURN TO FIELD DUE TO A DIRTY SOCK ODOR DURING TAKEOFF. THE ACFT DID NOT PRESSURIZE. OUTFLOW VALVE WAS FULL OPEN. PERFORMED FIM TASK 21-20-00. VERIFIED THE NR 1 ENGINE COMP WASH WAS PERFORMED. PERFORMED DECONTAMINATION ON PNEUMATIC SYS WITH ENGINE IAW AMM 21-20-00-810-803A. NO ABNORMAL ODORS NOTED, OK FOR SERVICE.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 31,016 hrs · 19,417 cycles

DURING ROUTINE MAINTENANCE, DISCOVERED THAT EMERGENCY LIGHT IN CEILING PANEL NR 5 WILL NOT ILLUMINATE. R & R EMERGENCY LIGHT POWER SUPPLY NR 2 IAW AMM 33-50-01. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: CONVERTER — FAILED (ELECTRICAL SYS) · airframe 29,159 hrs · 18,157 cycles

DIVERTED, AT 39,000 FT FLIGHT CREW EXPERIENCED SMOKE IN THE COCKPIT AND AN ELECTRICAL BURNING ODOR. CONDITIONS WERE EXPERIENCED ONLY IN THE COCKPIT, NOT THE CABIN; PERFORMED INSPECTION OF SMOKE OF COCKPIT. ALSO, DID FAULT ISOLATION INSPECTION OF ELECTRICAL OUTLETS. R & R COCKPIT OUTLETS CONVERTER. R & R CAPTAINS ACFT POWER OUTLET. PERFORMED DOUBLE ENGINE RUN FOR 20 MINUTES. ALL CHECKS NORMAL. NO DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE.

Part: SENSOR — FAILED (SLAT SYS) · airframe 28,373 hrs · 17,612 cycles

EMERGENCY DECLARED. RECEIVED SLAT FAIL IN FLIGHT. R & R BOTH INBD/OTBD RT SLAT SKEW SENSORS IAW AMM 27-83-01-000-801-A. OPS CHECK GOOD.

Part: FINGER DOUBLER — CORRODED (FRAME 77) · corrosion level 2 · airframe 26,628 hrs · 16,459 cycles

DURING HEAVY MAINTENANCE FOUND AFT CARGO DOOR FWD FINGER DOUBLER HAS CORROSION AT FRAME 77. REMOVED CORROSION IAW SRM 51-12-01. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-43-01, 51-23-02, SRM 51-40-02, SRM 51-43-03 AND SRM 51-40-04.

Part: STRINGER — CORRODED (FRAMES 23-24) · corrosion level 2 · airframe 26,628 hrs · 16,459 cycles

DURING HEAVY MAINTENANCE, FOUND CORROSION AT STRINGER 21R BETWEEN FRAMES 23 & 24. R & R THE STRINGER IAW SRM 51-41-02, 51-43-04.

Part: BEAM — CORRODED (FRAME 79) · corrosion level 2 · airframe 26,628 hrs · 16,459 cycles

DURING HEAVY MAINTENANCE, FOUND THE AFT GARGO LOWER BEAM HAS TWO PLACES OF CORROSION BLISTERS. CORROSION OUT OF LIMITS. R & R LOWER AFT CARGO DOOR BEAM IAW SRM 51-43-02 & 51-43-03.

Part: BEAM — CORRODED (FRAME 77) · corrosion level 2 · airframe 26,628 hrs · 16,459 cycles

DURING HEAVY MAINTENANCE, FOUND BEFORE REMOVAL AFT GARGO LOWER BEAM HAS 2 PLACES OF CORROSION BLISTERS AS MARKED, BOTH CORROSION SPOTS OUT OF LIMITS. R & R AFT CARGO BEAM IAW SRM 190-51-43-002 & 51-43-03.

Part: FINGER DOUBLER — CORRODED (FRAME 79) · corrosion level 2 · airframe 26,628 hrs · 16,459 cycles

DURING HEAVY MAINTENANCE, FOUND AFT CARGO DOOR, AFT FINGER DOUBLER HAS CORROSION AT FRAME 79. R & R THE FINGER DOUBLER IAW 51-43-0351-43-04.

Part: BEAM — CORRODED (FRAME 25) · corrosion level 2 · airframe 26,628 hrs · 16,459 cycles

DURING HEAVY MAINTENANCE, FOUND FWD CARGO DOOR HAS CORROSION ON BEAM AT AREA BY AFT DOOR LATCH. R & R THE BEAM IAW SRM 51-43-02 51-21-02 & 51-23-06.

Part: ACM — CONTAMINATED (NR 2) · airframe 24,677 hrs · 15,192 cycles

AIR RETURN TO DEPARTURE DUE TO LAV SMOKE EICAS WARNING. INFLIGHT, REPORTED SMOKE DETECTED IN BOTH LAV "CHIRPED" WENT INTO ALARM. PERFORMED FIM TASK 21-20-00-810-803-A. NO ODOR WHEN RUNNING PACK NR 1. NR 2 PACK DOES HAVE ODOR. OPENED PACK BAY NR 2 INSPECTED NR 2 ACM AND COOLER AND FOUND COFFEE RESIDUE. REPLACED NR 2 ACM, HEAT EXCHANGER AND FAN BYPASS CHECK VALVE IAW AMM 21-51-05 AND 21-51-04. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,549 hrs · 13,821 cycles

DURING MAINTENANCE IT WAS NOTED THE EMERGENCY BATTERY PACK AT POSITION NR 6 WAS BAD. R & R BATTERY PACK IAW AMM 33-50-01. OPS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 22,497 hrs · 13,788 cycles

ON MAINTENANCE CHECK, FOUND EMERGENCY EXIT CEILING LIGHT INOPERATIVE BETWEEN L1 AND R1. FOUND CONNECTOR P0314 DISCONNECTED ABOVE CEILING PANEL. CONNECTED, PERFORMED OPS CHECK IAW AMM 33-50-01 FOUND SATISFACTORY.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 22,497 hrs · 13,788 cycles

DURING MAINTENANCE IT WAS DISCOVERED, EMERGENCY LIGHT FOR L1 DOOR FOUND INOPERATIVE. R & R THE EMERGENCY POWER SUPPLY IAW AMM 33-50-01. OPS CHECKED NORMAL.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 22,497 hrs · 13,788 cycles

DURING MAINTENANCE, IT WAS DISCOVERED THE EMERGENCY LIGHTS FOR L2 DOOR FOUND INOPERATIVE. R & R EMERGENCY LIGHTS POWER SUPPLY IAW AMM 33-50-01, OPS CHECKED NORMAL.

Part: POWER SUPPLY — FAILED (NR 3 MAU) · airframe 19,678 hrs · 11,945 cycles

FLT 241 BOS-MCO, AIR RETURN TO BOS DUE TO "AVNX MAU 3A FAIL" ON EICAS 15 MINS INTO FLT WITH ASSOCIATED EICAS MSGS. "AVNX MAU 2A FAIL" TEN MINUTES LATER WITH ASSOCIATED EICAS MSGS. MAU 2 PWR 1 & MAU 3 PWR 1 CB'S POPPED. REPLACED MAU 2-1 PWR SPLY AND MAU 3-1 PWR SPLY IAW 31-41-02. ALL INDICATIONS NORMAL.

Part: POWER SUPPLY — FAILED (NR 2 MAU) · airframe 19,678 hrs · 11,945 cycles

FLT 241 BOS-MCO, AIR RETURN TO BOS DUE TO "AVNX MAU 3A FAIL" ON EICAS 15 MINS INTO FLT WITH ASSOCIATED EICAS MSGS. "AVNX MAU 2A FAIL" TEN MINUTES LATER WITH ASSOCIATED EICAS MSGS. MAU 2 PWR 1 & MAU 3 PWR 1 CB'S POPPED. REPLACED MAU 2-1 PWR SUPPLY AND MAU 3-1 POWER SUPPLY IAW 31-41-02. ALL INDICATIONS NORMAL.

Part: CONNECTOR — LOOSE (VIBRATION SYS) · airframe 17,869 hrs · 10,838 cycles

FLT 1152 FLL-RIC, AIRCRAFT DIVERTED TO MCO DUE TO NR 2 ENGINE LP VIBRATION 4.1 ABOVE 89.0 N1. N1 78% = 1.9 VIB LP, 82% = 3.2, 89% = 4.1. PERFORMED FIM TASK 77-31-00-810-816. FOUND W9B HARNESS CONNECTOR P91 LOOSE. SECURED CONNECTOR & PERFORMED HIGH POWER ENGINE TEST IAW GE EMM 72-00-00, TESTING 03. VIBRATIONS WELL WITHIN PARAMETERS. NIL FAULTS NOTED FURTHER.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 16,863 hrs · 10,211 cycles

FLT 6406 JFK-BNA, ON HEAVY MAINTENANCE CHECK FOUND FWD CABIN CROSS BEAM FR 17 RIGHT HAS NUMEROUS PIN SIZE SPOTS CORRODED. REPAIRED BY INSTALLING TWO MANUFACTURED "L" ANGLES DRILLED AND CUT TO CROSSBEAM LIGHTNING HOLES IAW EA E12-273-01.

Part: BLADE — MISSING (NR 1 ENGINE) · airframe 13,883 hrs · 8,409 cycles

FLT 1107 JFK-RDU DIVERTED TO IAD AT FLT 360 NOTICED CONTINUOUS RUMBLE FOLLOWED BY NR 1 VIBS AT 4.5, PERFORMED ENGINE ABNORMAL QRH. NR 1 ENGINE THRUST LEVER WAS AT 1/2 POWER LEVEL WITH VIBS GREEN. VIB'S CONTINUED TO INCREASE INTO AMBER RANGE UNTIL THRUST LEVER AT OR NEAR IDLE. VIB'S WERE IN GREEN RANGE FOR APPROACH AND LANDING. ALL OTHER INDICATIONS ON NR 1 ENGINE NORMAL. FOUND NR 1 ENGINE 4TH STAGE BLADES MISSING (4) AND DAMAGED. PERFORMED THE FOLLOWING EXTERNAL VISUAL INSPECTIONS WITH NO FINDINGS. GVI WING TO FUSELAGE FAIRING IAW AMM 05-21-00-212-802-A. CENTER FUSELAGE III BOTTOM EXTERNAL GVI 0521-00-212-803-A. REAR FUSELAGE GVI EXTERNAL 05-21-00-212-806-A. LT WING LOWER SURFACE GVI EXTERNAL 05-24-00-212-806-B. LT MLG 05-24-00-212-B. FLAP LT LOWER SURFACE GVI 05-24-00-212-804-B. REMOVED AND REPLACED NR 1 ENGINE IAW AMM 71-00-01-401. OPS CHECK/LEAK CHECK OK.

Part: UNKNOWN — FAILED (ELECTRICAL SYS) · airframe 12,850 hrs · 7,826 cycles

FLT 418 PBI-BOS, CREW DECLARED EMERGENCY DUE TO SPDA FAIL CYAN IN AIR ON ELECTRICAL SYNOPTIC PAGE RT SIDE AMBER DASHES QRH COMPLETED. PER FAULT CODE 24610048SP1, FIM 24-61-00-810-887A. REMOVED AND REPLACED SPDA 2 MICRO COMMS MOD SLOT 12 PER AMM 24-61-07. ACCOMPLISHED TARGET LOAD, OPS CHECKS NORMAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,654 hrs · 7,105 cycles

FLT 6420 ON HEAVY MAINTENANCE VISIT AT BNA, UPON INSPECTION FOUND CORROSION ON RT FLOORBEAM TRACK AT FRAME 13, FRAME 14, FRAME 15, FRAME 16 AND FRAME 17. FABRICATED, REPAIRED DOUBLER AND REPAIRED CABIN FLOORBEAMS AS PER EA E10-342-01 REF EAMS NR H14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,654 hrs · 7,105 cycles

FLT 6420, ON HEAVY MAINTENANCE VISIT AT BNA, UPON INSPECTION FOUND CORROSION ON LT FLOORBEAM TRACK AT FRAME 14, FRAME 15, FRAME 16 FRAME 17, AND FRAME 19. FABRICATED REPAIRED DOUBLER AND REPAIRED CABIN FLOORBEAMS AS PER EA E10-342-01 REF EAMS NR H1479.

Part: SLIDE — UNWANTED DEPLOY (L2 DOOR) · airframe 10,679 hrs · 6,579 cycles

FLT JB7--AFTER FLT, L-2 DOOR SLIDE DEPLOYED BY CATERING. R & R L-2 DOOR SLIDE IAW AMM 25-65-01 & ASSIST ACTUATOR DIAPHRAGM REPLACED IAW AMM 52-42-53. FOUND THAT THE CATERING CREW & FLT CREW FOLLOWED PROPER DOOR OPENING PROCEDURES. DURING L2 DOOR OPENING CATERING NOTICED THE SLIDE CASING & A STRING AT LOWER AFT CORNER HANGING DOWN & STOPPED OPENING DOOR. CATERING ATTEMPTED TO FREE THE STRING THEN SLIDE UNRAVELED & INFLATED BETWEEN FUSELAGE & PARTIALLY OPENED DOOR. FOUND A MECHANICAL MALFUNCTION OF SLIDE, STRING HANGING DOWN BUSTLE BRACKET RELEASE PIN LANYARD WITH PIN TORN OFF. CATERING PULLING ON LANYARD RELEASED SLIDE CASING CAUSING DEPLOYMENT.

Part: ACTUATOR — FAILED (SLATS) · airframe 9,725 hrs · 6,011 cycles

FLT NR 1703 BOS-BDA, SLAT FAIL EICAS MESSAGE WITH SLATS AT ZERO ON APPROACH TO BDA DIVERTED TO JFK. MX AT JFK PERFORMED SLAT ACTUATOR INSPECTION CHECK PER FIM 27-81-00-810-802A IAW AMM 27-81-01, FOUND LEFT WING SLAT ACTUATOR NR 8 AND RIGHT WING SLAT ACTUATORS NR 1, 2,3, 5 AND 6 TORQUE LIMITER INDICATORS TRIPPED. RESET TORQUE LIMITS IAW 45-45-00-970-805-A/200, NR 2 RIGHT SLAT ACTUATOR TORQUE LIMITER DID NOT RESET. REPLACED THIS ACTUATOR IAW 27-81-01 ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SLAT SYSTEM — FAILED (ZONE 100) · airframe 9,685 hrs · 5,985 cycles

FLT NR 448 TPA-BOS, WHEN EXTENDING FLAPS FOR LANDING SLAT FAIL EICAS MESSAGE APPEARED, LANDED BOS WITH FLAP HANDLE AT POS.2. FDE DETAIL SLAT FAIL SURFACE JAMMED. FAULT CODE 27811021ACE. FIM REF 27-81-00-810-802-A, RELEASED PDU, BRAKE RELEASE NORMAL SMOOTH OPERATION NOTED. REPLACED S/F ACE NR 1 PER AMM 27-53-02 CK GOOD.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 9,631 hrs · 5,958 cycles

FLT 1791 CABIN DID NOT PRESSURIZE ON DEPARTURE NOTICED AT 9500 FT LEVELED 10,000 FT OUTFLOW VALVE WAS FULLY OPEN DID NOT DEPLOY VALVE DID NOT MOVE. PERFORMED IAW AMM TASK 21-31-710-801 OK FOR SERVICE. AS PRECAUTIONARY A TSI WAS ISSUE TO REPLACE THE OUTFLOW VALVE AND MODULE IN MCO.

Part: UNKNOWN — SMOKE (CABIN) · airframe 9,623 hrs · 5,954 cycles

FLT 582 - APPROX 15000 FT F/A SMELLED SMOKE IN REAR CABIN. PERFORMED CHECK IAW WITH FIM 21-20-00-810-801A, NO DEFECTS NOTED. OPS CHECK PERFORMED IAW LTV 44-20-10. NO DEFECTS NOTED.

Part: HINGE — WORN (COCKPIT DOOR) · airframe 9,583 hrs · 5,932 cycles

FLT 461 BOS-RSW - COCKPIT DOOR CAME OFF HINGES WHEN CREW PUSHED OUT ON IT DURING A BREAK. CREW RESEATED DOOR, DOOR WORK OK AFTER RESEATING. REMOVED AND REPLACED COCKPIT UPPER DOOR HINGE GROUND OPS OK IAW AMM 52-51-01.

Part: DOOR — DISLODGED (COCKPIT) · airframe 9,497 hrs · 5,875 cycles

FLT 421 BOS-PBI COCKPIT DOOR FELL OFF HINGES DURING FLIGHT. CLEANED DEBRI FROM LOWER HINGE. SECURED OPS CHECK NORMAL 52-51-01.

Part: FMU — FAILED (NR 2 ENGINE) · airframe 8,357 hrs · 5,187 cycles

FLT 31, JFK-MCO, JUST PRIOR TO ROTATION SLIGHT ROLL BACK ON NR 2 ENG. ENG MADE COMMAND THRUST, AFTER LIFT OFF, THEN ROLLED BACK TO 31.3 N1. RETURN TO JFK. UPON LANDING ENG 2 NO DISPATCH. THEN ENG, FAILED AFTER CLEARING RUNWAY. YAW CORRELATED WITH ROLL BACK. REMOVED AND REPLACED FMU IAW AMM CH 73-21-03. OPS & LEAK CHECK GOOD. AS PER ENGINEERING REQUEST REMOVED AND REPLACED NR 2 ENG FADEC AS PER CF3410E ENG MM 73-00-00-800-812. OPS CHECK OK.

Part: DEFLECTOR — NOISY (R2 DOOR) · airframe 8,299 hrs · 5,153 cycles

FLT 1263, BOS-AUS, RETURNED TO BOS, VERY LOUD R2 DOOR NOISE IN FLIGHT. DOOR DEFLECTORS, PASSENGER AND SERVICE, RELEASED ON CDL C-52-10-01, PERFORMED DOOR DEFLECTOR DEACTIVATION PROCEDURE. A/C OK FOR SERVICE.

Part: TRANSCEIVER — FAILED (RADAR SYS) · airframe 8,173 hrs · 5,079 cycles

FLT 584, FLL-HPN, RADAR FAILED AFTER TAKEOFF, RETURNED TO FLL. REMOVED AND REPLACED RTA ASSY IAW REF 34-42-01, OPS CHECK PER AMM 34-42-00. OPS CHECK GOOD.

Part: PUMP — FAILED (NR 2 HYD SYSTEM) · airframe 6,751 hrs · 4,284 cycles

HYD 2 EDP FAIL IN FLT LOSS OF HYD 2 WAS DUE TO EDP NR 2, HYD 2 LO QTY AND PRESSURE EICAS MSGS. VISIBLE GAUGE LOSS OF FLUID QTY AT 0. QRH PROCEDURES FOLLOWED MANUAL GEAR RELEASE. REMOVED AND REPLACED NR 2 HYD EDP IAW 29-11-01, SERVICED NR 2 HYD SYS IAW 12-12-01-03, PERFORMED RETURN TO SERVICE TEST IAW 27-00-00, CHECK HYD SYS NR 2 FILTERS, OPS CHECK GOOD. PERFORMED LANDING FREE-FALL INSP, OPS CHECK OK, PERFOMED NR 2 ENG RUN LEAK CHECK GOOD. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (L/E SLAT) · airframe 6,357 hrs · 4,053 cycles

FLT NR 293, SEA-LGB, SLAT FAIL ON APPROACH TO LGB, FOUND LT NR 5 SLAT ACTUATOR TRIPPED. R/R LT SLAT ACTUATOR IAW AMM 27-81-01. PERFORMED SLAT CTL MECH RIGGING PER 27-80-00-820-801 & SLAT CTL ELEC RIGGING PER 27-80-00-820-802A/200. NO FAULTS NOTED. OPS TEST OF SLAT CTL SYS CKS NORMAL AT THIS TIME. ACFT OK FOR SERVICE.

Part: ROD — BENT (NLG DOOR)

LG NOSE DOOR OPEN CAUTION ON EICAS AFTER GEAR LEVER WAS SELECTED UP ON TAKEOFF, PERFORMED QRH MESSAGE, EXTINGUISHED AFTER GEAR WAS LOWERED DURING AIR RETURN, INDICATIONS WERE NORMAL WITH GEAR DOWN, REMOVED AND REPLACED LT AFT DOOR SENSOR IAW AMM 32-61-13, PG 401, ADJUSTED NLG DOOR POSITION SENSOR IAW AMM 32-61-13-820-802A. REMOVED AND REPLACED NLG AFT DOOR LINKAGE ROD IAW 32-22-03, ACCOMPLISHED NLG GEAR SWING IAW AMM 32-61-13. OPS CHECK OK. (K)

Part: WARNING MESSAGE — ILLUMINATED (NLG STEERING) · airframe 983 hrs · 695 cycles

STEER FAIL EICAS MSG ON SHORT FINAL. TOTAL LOSS OF STEERING AFTER LANDING. ACCOMPLISHED RESET OF MAU2 PWR IAW FIM 32-53-00-810-819-A TRANSITATORY CONDITION. OPS CHKS OF NOSE WHEEL STEERING IAW AMM 32-52-00 CHKS NORMALLY.

Part: FIRE BOTTLE — FAILED (CARGO BAY) · airframe 28 hrs · 12 cycles

AT FL 410, 44 MINUTES INTO FLIGHT THE FOLLOWING CAS AMBER MESSAGES. CARGO AFT FIRE SYS FAIL. CARGO FWD FIRE SYS FAIL. REPLACED HIGH RATE FIRE BOTTLE PER AMM 26-23-01. CLOSED MID E-BAG HATCH PER 52-46-00-000-801. OPS OK.

Part: MODULE — FAULTY (WARNING SYSTEM) · airframe 26 hrs · 11 cycles

CRG AFT FIRE SYS FAIL AND CRG FWD FIRE SYS FAIL EICAS ILLUMINATED IN FLIGHT. PERFORMED EXTENSIVE TROUBLESHOOTING OF MAU NR 3 GEN I/O AND ASSOCIATED CONNECTORS. PERFORMED CONTINUITY CHECK OF FIRE BOTTLE WIRING FROM RESPECTIVE CONNECTORS TO MAU NR 3. NO DEFECTS NOTED. REMOVED AND REPLACED GEN I/O 3 MODULE. PERFORMED SOFTWARE TARGET LOAD OF MODULE. SOFTWARE LOAD GOOD. NO DEFECTS OR EICAS MESSAGE NOTED. A/C IS OK FOR RETURN TO SERVICE IAW EMB190 AMM 31-41-06-400-801-A, 31-41-00-970-801A AND 45-45-40-470-801-A.