N328AG

Part: SKIN — DAMAGED (BS 827-830) · airframe 38,103 hrs · 42,648 cycles

FLIGHT# N/A REPORT: DURING REPO OF AC TO THE LINE , DAMAGE OCCURED TO THE RH SIDE ABOVE FIN. CORRECTIVE ACTION: PERFORMED REPAIR TO FRAME STATION 827 AND SKIN IAW EO 340B-5390-2019-001 ALL CHECKS GOOD

Part: ELECTRONIC UNIT — FAULTY (REMOTE) · airframe 37,985 hrs · 42,541 cycles

FLIGHT# 0078, CAPTAIN SIDE HAD NO ABILITY TO COMMUNICATE BY RADIO - NO AUDIO WAS AVAILABLE. CB E10 WAS TRIPPED- SMELL OF BURNING WIRING WAS NOTICED, NO SMOKE WAS VISIBLE. REMOVED AND INSTALLED REMOTE ELECTRONICS UNIT IAW AMM 23-50-05-04, OPS CHECK GOOD IAW AMM23-50-00

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHT) · airframe 37,951 hrs · 42,513 cycles

FLIGHT 0137 MCO/MCO REPORT: L 8 EMERGENCY LIGHT EXT CONTROL CB TRIPPED CORRECTIVE ACTION: PERFORMED RESET BREAKER IAW AMM 33-50-00. OP'S CHECK GOOD. NO DEFECT FOUND THIS TIME.

Part: PCU — FAILED (LT PROPELLER) · airframe 37,890 hrs · 42,457 cycles

SUPPLEMENTAL FLIGHT# 0117 FPO/FLL REPORT: LEFT PROP RPM FLUCTUATED FROM 1230 RPM TO 750 RPM ON LEVEL FLIGHT. CORRECTIVE ACTION: REMOVED & REPLACED LT ENGINE PCU IAW AMM 61-20-05-04.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 37,830 hrs · 42,393 cycles

FLIGHT# 0098 MCO/MHH REPORT: LEFT AFT EMERGENCY LIGHT INOP. CORRECTIVE ACTION: R&R AFT LEFT POWER SUPPLY IAW AMM 33-50-10-04 OPS CHECK GOOD.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 37,589 hrs · 42,154 cycles

FLIGHT 0091 MHH/FLL REPORT: HYDRAULIC FAILURE AFTER LANDING. CORRECTIVE ACTION: R/R MAIN HYDRAULIC PUMP MOTOR, OPERATIONAL CHECK NORMAL REF AMM 29-10-10-04. NO LEAKS FOUND. R/R 7ML RELAY IAW WMM 29-10-10, & MM 24-52-00.OPS CHECK GOOD IAW 29-10-10-04.

Part: CONTROL UNIT — FAULTY (LANDING GEAR) · airframe 37,587 hrs · 42,152 cycles

SUPPLEMENTAL TO CORRECT TAIL NUMBER FLIGHT# 0065 MMH/FLL REPORT:ON FINAL APPROACH, SELECTING GEAR DOWN, THE HYD (DOWN) LIGHT ON CWP CAME ON. GEAR DID NOT GO DOWN, ONLY NOSE GEAR, MAIN HYD PRESSURE WAS ZERO. FOLLOWED QRH. PROCEDURE WAS TO SWITCH TO OFF THEN TO OVERRIDE, PUMP CAME ON WITH NORMAL PRESSURE. PER QRH, PRIOR TO CONFIGURING FOR APPROACH, SWITCHED HYD PUMP TO OVERRIDE AND KEPT IN THAT POSITION UNTIL PARKED. CORRECTIVE ACTION: R/R HYDRAULIC AUTO & MANUAL SWITCH IAW MM 29-10-50 ON&OFF ON# MS27407-1. REQUIRES OPS CHECK. GEAR EXTENSION STILL FAILED. SUSPECT LANDING CONTROL UNIT AT FAULT. R/R LANDING CONTROL UNIT IAW AMM 32-31-05-02. GEAR EXTENSION AND RETRACTION OPS CHECKED NORMAL IAW AMM 32-30-00.

Part: DUCT — ODOR (ZONE 400) · airframe 37,402 hrs · 41,976 cycles

FLIGHT# 0064. R INTAKE ANNUNCIATOR ILLUMNATED QRH DIRECTED OFF THEN ON REMAINED ILLUMINATED ASSOCIATED LIGHT SMELL OF SMOKE IN COCKPIT PROMPED TURNING OFF RT ENG ANTI ICE. CORRECTIVE ACTION: R&R RH LOWER INTAKE DUCT AND RELAY 935HE ON SHOE BOX IAW CMM 30-21-03,OPS CHECK GOOD IAW AMM 30-20-00 RLEAY P/N SM15CXD4 NSN

Part: GAUGE — FAILED (COCKPIT) · airframe 37,039 hrs · 41,647 cycles

FLIGHT 142 FLL/FPO REPORT: DURING FLIGHT "R PROP" TEMPERATURE AND "R PROP" PRESSURE GAUGE WENT TO ZERO ALL WAY TO LAND SHUT DOWN ENGINE EMERGENCY DECLARED. CORRECTIVE ACTION: R&R RT PGB OIL PRESS/TEMP GAUGE IAW AMM 79-30-15-02 OPS CHECK GOOD.

Part: CONTROL PANEL — FAILED (LANDING GEAR) · airframe 36,819 hrs · 41,426 cycles

FLIGHT:129 TLH/FLL NOSE WHEEL LANDING GEAR INDICATION LIGHT INTERMITTENT. CORRECTIVE ACTION: REMOVED AND REPLACED LANDING GEAR CONTROL PANEL IAW SAAB AMM 32-31-05-02. PERFORMED GEAR SWING IAW SAAB 340 AMM 32-30-00-05 OPS CHECKED GOOD.

Part: BLEED VALVE — FAILED (NR 2 ENGINE) · airframe 36,227 hrs · 40,629 cycles

FLIGHT 0064 PNS/MCO REPORT, COMPRESSOR STALL NR 2 ENGINE AT 19,00 FT DURING CRUISE. OVERTEMP FOR A FEW SECONDS WITH RED BUTTON. SMELT FUMES AT THE STALL COMPLIED WITH QRC/QRH FOR COMPRESSOR STALL. FUMES DISSIPATED FOR 10 MINUTES AND CAME BACK AT THAT TIME MOVED TO MASK AND GOGGLES WITH QRC/QRH DECLARED EMERGENCY. R&R START BLEED VALVE IAW MM 75-00-00 OPS CHECKED GOOD.

Part: BATTERY — OVERHEATED (RT MASTER) · airframe 35,866 hrs · 40,455 cycles

NO BATTERY START LIGHT ILLUMINATED AFTER NR 2 ENGINE STARTED. TEMPERATURE RAISED DURING CRUISE AND RT BATTERY HOT LIGHT ILLUMINATED, PERFORMED AN EMERGENCY LANDING . R & R THE RT MAIN BATTERY IAW AMM 24-34-10-04. OPS CHECKED GOOD.

Part: PANEL — FAILED (F/A PANEL) · airframe 35,823 hrs · 40,409 cycles

EMERGENCY LIGHT STUCK IN ARMED POSITION ON THE F/A PANEL. R & R F/A PANEL WITH SERVICEABLE PANEL OPS CHECK GOOD IAW AMM 20-10-00, & PERFORMED AN OPS CHECK IAW AMM 33-50-00. OPS CHECKED GOOD .

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 35,512 hrs · 40,090 cycles

MAIN CABIN DOOR WILL NOT OPEN FROM THE OUTSIDE, IF AIRSTAIRS ARE NOT STOWED AND SLIDE IN. ADJUSTMENT AND APPLIED LUBRICANT TO THE DOOR ASSEMBLY. FUNCTIONAL AND OPERATIONAL CHECKED GOOD IAW AMM 52-10-00-05

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 35,223 hrs · 39,772 cycles

FA REPORTED THAT THE EMERGENCY LIGHT SWITCH ARM IN YELLOW DOES NOT ILLUMINATE. TROUBLESHOT THE SYSTEM AND FOUND THE F/A EMERGENCY LIGHT SWITCH 29LN AT FAULT. R & R F/A EMERGENCY LIGHT SWITCH IAW AMM 39-40-60-02. EMERGENCY LIGHTS OPS CHECKED NORMAL IAW AMM 33-50-00.

Part: HANDLE — BINDING (PAX DOOR) · airframe 34,887 hrs · 39,417 cycles

FLIGHT ATTENDANT HAD A HARD TIME TURNING THE HANDLE TO OPEN THE CABIN DOOR. WITH THE DOOR OPEN THE DOOR LEVER IS STUCK IN THE CLOSED POSITION. RESET THE DOOR HANDLE TO OPEN POSITION, PERFORMED AN OPERATIONAL CHECK IAW AMM 52-10-00-05, SYSTEM OPERATES NORMAL.

Part: UPLOCK SWITCH — DIRTY (MLG) · airframe 34,845 hrs · 39,372 cycles

FLIGHT 0147, HYD PUMP RUNS CONTINUOSLY AFTER GEAR IS UP AND LOCKED. CLEANED UPLOCK SWITCHES AND PERFORMEND FUNCTIONAL TEST OF LANDING GEAR AND NO FAULTS NOTED IAW AMM 32-30-00-05.

Part: LIGHT — BROKEN (SEAT 3A) · airframe 34,710 hrs · 39,231 cycles

EMERGENCY LIGHT ASSY BROKEN AT SEAT 3A. REPLACED THE EMERGENCY DOME LIGHT. OPS CHECKED GOOD IAW AMM 33-50-55-04.

Part: ENGINE — OIL CONSUMPTION (RIGHT) · airframe 34,455 hrs · 39 cycles

DURING CLIMB RT ENGINE OIL PRESSURE ON CWP ILLUMINATED, OIL PRESSURE WAS AROUND 40 PSI AND DECREAED BELOW THE YELLOW DOT AND WHEN IT REACHED RED LINE CLOSE TO ZERO SHUTDOWN WAS PERFORMED. INSPECTED RT ENGINE AND FOUND OIL LEVEL LOW. SERVICED THE OIL SYSTEM IAW AMM 12-10-79. PERFORMED POWER UNIT LOW OIL LEVEL CLEARING PROCEDURE AND OIL CHECK IAW AMM PROCEDURE 49 AND OIL COMSUMTION CHECK IAW AMM 72-00-00 SPECIAL PROCEDURE AND TEST CLEARING PROCEDURE AND OIL COMSUMPTION. OPS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,274 hrs · 38,771 cycles

EMERGENCY LIGHT ABOVE MAIN CABIN DOOR DOES NOT ILLUMINATE. R & R THE POWER SUPPLY 21LN IAW AMM 33-50-10. EMERGENCY LIGHTS OPS CHECKED NORMAL IAW AMM 33-50-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,941 hrs · 36,975 cycles

EMERGENCY LIGHT "ARM" LIGHT NOT ILLUMINATING WHEN EMERGENCY LIGHTS ARE ARMED. THIS IS THE LIGHT LOCATED ON THE F/A PANEL. R & R EMERGENCY LIGHT ARM BULB, OPS CHECK GOOD REF AMM 33-50-00.

Part: COVER — DETACHED (EMERGENCY EXIT) · airframe 32,693 hrs · 36,564 cycles

RIGHT SIDE EMERGENCY EXIT COVER FELL OFF. REINSTALLED COVER IAW AMM 52-20-05-04.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 32,679 hrs · 36,536 cycles

EMERGENCY LIGHTING POWER SUPPLY 24LN FAILS TESTING. LIGHT FLASHES IMMEDIATELY UPON STARTING TEST. R & R 24LN EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-50-10-04-1. OPS CHECKED GOOD.

Part: SEAL — UNSECURE (PAX DOOR) · airframe 32,587 hrs · 36,388 cycles

FLIGHT GROUND RUN, F/A REPORTS CABIN DOOR NOT SEALING AND DAYLIGHT VISIBLE THROUGH GAP IN DOOR SEAL. INSPECTED CABIN DOOR AND SEALS, NO DEFECTS NOTED, REF AMM 52-20-20-15.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,329 hrs · 36,078 cycles

FLIGHT 100: EMERGENCY LIGHTING FROM ROWS 2A TO 7A AND OVERHEAD EMERGENCY LIGHT AT 7A INOPERATIVE. R & R EMERGENCY BATTERY PACK 20LN IAW AMM 33-50-10-04-1. OPS CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 32,286 hrs · 36,034 cycles

RIGHT FRONT WINDSHIELD CRACKED. R & R RT FRONT WINDSHIELD IAW AMM 56-10-05. RT FRONT WINDSHIELD HEAT OPS CHECK NORMAL IAW 30-42-00. PAINT ON MCO, DEFECT 30264. SEALANT CURED AND SPEED TAPE REMOVED, DEFECT 30263.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 32,168 hrs · 35,883 cycles

IN CABIN LIGHTING PANEL EMERGENCY LIGHT, ARM PORTION OF LIGHT DOES NOT ILLUMINATE. REPLACED THE LIGHT SWITCH IAW AMM 33-50-00, OPS CHECKED NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 31,942 hrs · 35,654 cycles

LOUD NOISE AND BURNING ODOR FROM UNDER FLOORBOARD IN ROW 4.

Part: LATCH — OUT OF ADJUST (PAX DOOR) · airframe 30,221 hrs · 33,758 cycles

CABIN DOOR 208 WILL NOT LATCH CLOSED. CLEANED AND ADJUSTED LATCH, OPS CHECKED GOOD.