N922TS
Registered owner: AERO MICRONESIA INC DBA, GU (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.
80 reports on file, 1995-05-13 – 2022-07-26.
Part: SHUTOFF VALVE — FAULTY · airframe 102,704 hrs · 27,053 cycles
THE RIGHT ENG BLEED SHUT OFF WITH THE USE OF THE COWL ANTI ICE SYSTEM. THE LEFT ENG BLEED WAS UTILIZED FOR THE RIGHT SYSTEM PER THE QRH CAUSING THE LEFT ENG BLEED TO SHUT OFF. CABIN PRESSURE WAS LOST AND THE CREW DIVERTED TO BNA. THE RIGHT ENG HPSOV WAS FOUND FAULTY WHICH WAS DEFERRED. THE LEFT ENG BLEED OFF IS CONSIDERED NORMAL PER THE FIM.
Part: FCU — FAULTY (L ENG) · airframe 102,700 hrs · 27,050 cycles
CREW REPORTED LEFT ENGINE FAILURE ON SHORT FINAL INTO GSO. TROUBLESHOOTING STEPS TAKEN CONFIRMED A FAULTY FUEL CONTROL UNIT. FCU WAS REPLACED IAW AMM 73-21-04. PERFORMED ENGINE RUNS AND CONFIRMED OPERATIONAL. AIRCRAFT RETURNED TO SERVICE.
Part: EEC — FAULTY (L ENG) · airframe 102,700 hrs · 27,050 cycles
CREW REPORTED LEFT ENGINE FAILURE ON SHORT FINAL INTO GSO. L ENG PRI CONT AND L ENG SEC CONT MESSAGES WERE DISPLAYED ON THE EICAS STATUS PAGE. THE MESSAGES CONFIRMED A FAULTY EEC. THE EEC WAS REPLACED IAW 73-21-01. PERFORMED ENGINE RUNS AND CONFIRMED OPERATIONAL. AIRCRAFT RETURNED TO SERVICE.
Part: PUMP — FAULTY (LEFT WHEEL WELL) · airframe 102,488 hrs · 26,999 cycles
LEFT CENTER FUEL BOOST PUMP INOP. R/R LEFT CENTER FUEL BOOST PUMP PER AMM 28-22-03.
Part: ACTUATOR — FAULTY (RH PACK BAY) · airframe 102,488 hrs · 26,999 cycles
RH PACK TEMP ON TAXI. R/R RAM INLET ACTUATOR PER AMM 21-53-03. OPS CHECK NORMAL.
Part: CONTROL VALVE — FAULTY (RH PACK BAY) · airframe 102,488 hrs · 26,999 cycles
RIGHT PACK TEMP EICAS MSG ON TAXI. R/R RIGHT TEMP CONTROL VALVE PER AMM 21-51-12. OPS CHECK NORMAL.
Part: SHUTOFF VALVE — FAULTY (R ENG) · airframe 102,480 hrs · 26,997 cycles
R ENG PRSOV INOP. R/R R ENG PRSOV PER AMM 36-11-19.
Part: COOLING TURBINE — FAULTY (R ENG) · airframe 102,437 hrs · 26,987 cycles
R ENG HCC/EEC AND 351-26 MSG ON EPCS PAGE. R/R R ENG HIGH PRESSURE TURBINE COOLING VALVE PER AMM 75-24-03.
Part: CABIN PRESSURE — FAULTED · airframe 102,415 hrs · 26,982 cycles
EVENT: CABIN ALT ALERT AT FL240 RAPID DEPRESSURIZATION EMERGENCY DECLARED. MX PERFORMED CABIN AUTO 1 & 2 BITE TEST PER FIM 21-30 F/T 803. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE.
Part: BLEED ACTUATOR — FAULTY (L ENG) · airframe 102,403 hrs · 26,979 cycles
L ENG 2.5 BLEED MSG ON EPCS PAGE. R/R L ENG 2.5 BLEED ACTUATOR PER AMM 75-32-01.
Part: ACTUATOR — FAULTY (RH PACK BAY) · airframe 102,265 hrs · 26,947 cycles
RH PACK TEMP ON TAXI OUT, STBY SELECTED. SECURED RH PACK IAW MEL 21-51-01. R/R RAM INLET ACTUATOR PER AMM 21-53-01 IN REF TO FIM 21-51-14.
Part: PRESSURE SWITCH — FAULTY (FWD RIGHT STRUT) · airframe 101,963 hrs · 26,876 cycles
RIGHT AFT FUEL PUMP PRESSURE LIGHT ILLUMINATED... REPLACED FUEL PRESS. SWITCH.
Part: VALVE — FAULTY (FWD CARGO BIN) · airframe 101,902 hrs · 26,862 cycles
FWD CABIN AUTO EICAS MSG... REPLACED TRIM AIR MOD VALVE.
Part: ENGINE — NONE (L ENG) · airframe 101,383 hrs · 26,741 cycles
LEFT ENGINE REPLACEMENT FOR MX PLANNING PURPOSES.
Earlier reports · 1995–2021 · 66 reports
2021
Part: NONE — FAILED (APU) · airframe 101,375 hrs · 26,736 cycles
APU PNEUMATICS INOP DUE TO A FAILED P2 SENSOR. PNEUMATIC SYSTEM PLACED BACK INTO SERVICE AFTER P2 SENSOR REPLACEMENT.
Part: START VALVE — FAULTY (L ENG) · airframe 101,189 hrs · 26,648 cycles
DISCREPANCY: L ENG START VALVE INOP. CORRECTIVE ACTION: REMOVED AND REPLACED L ENG START CONTROL VALVE IAW AMM 80-11-02. OPS CHECK OK.
Part: NONE — FAULTY (R WING) · airframe 101,152 hrs · 26,641 cycles
DISCREPANCY: R WING ANTI-ICE VALVE FAILED ON TEST. CORRECTIVE ACTION: REMOVED AND REPLACED R WING TAI VALVE IAW AMM 30-11-02. OPS AND LEAK CHECK OK.
Part: ENGINE — OVERTEMP (LT ENGINE) · airframe 100,729 hrs · 26,541 cycles
LEFT ENGINE EGT RISING AFTER START AND IMPENDING OVERTEMP DURING TAKE OFF ROLL. LCC WAS REPLACED WITH NO FURTHER ISSUES.
Part: COMPUTER — FAULTED (LEFT HCC) · airframe 100,729 hrs · 26,541 cycles
LEFT ENGINE EGT RISING AFTER START AND IMPENDING OVERTEMP DURING TAKE OFF ROLL. HCC WAS REPLACED WITH NO FURTHER ISSUES.
Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 100,462 hrs · 26,481 cycles
CABIN ALT AUTO 2 INOP. REMOVED AND REPLACED #2 CABIN PRESS CONTROLLER IAW AMM 21-31-02. BITE TEST PASS.
Part: SELECTOR — FAULTED (CABIN TEMP) · airframe 100,342 hrs · 26,455 cycles
THE FLIGHT DECK CABIN TEMP SELECTOR WAS REPALCED DUE TO A CABIN TEMP RUN AWAY IN FLIGHT. DURING A BITE CHECK OF THE ZONE TEMP CONTROLLER, A TEMP SELECTOR FAULT WAS FLAGGED WHICH REQUIRED REPLACEMENT OF THE UNIT. AFTER REPLACEMENT, THE SYSTEM WAS CONFIRMED OPERATIONAL.
Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 100,329 hrs · 26,452 cycles
CABIN PRESSURE CONTROLLER SYSTEM 2 WAS REPLACED DUE TO A REPEAT CONTROLLER FAULT DURING A BITE CHECK AND A CABIN AUTO 2 STATUS MESSAGE ON EICAS. AFTER REPLACEMENT, SYSTEM WAS CONFIRMED OPERATIONAL.
Part: ACTUATOR — WORN (APU INLET DOOR) · airframe 100,077 hrs · 26,396 cycles
APU INLET DOOR CB TRIPS DURING APU SHUTDOWN, RESTRICTING THE APU DOOR TO CLOSE. ISSUE WAS ISOLATED TO A WORN APU INLET DOOR ACTUATOR WHICH WAS REPLACED AND CONFIRMED OPERATIONAL.
Part: TRANSCEIVER — FAULTY (RT HF) · airframe 100,047 hrs · 26,390 cycles
RIGHT HF INOPERATIVE. REMOVED AND REPLACED THE RIGHT HF TRANSCEIVER IAW AMM 23-11-03. OPS CHECK OK.
Part: DISPLAY — FAULTY (COCKPIT) · airframe 99,696 hrs · 26,321 cycles
CAPT MCDU BRIGHTNESS SETTING INOP. MCDU WAS REPLACED AND CONFIRMED OPERATIONAL.
Part: CONTROL VALVE — INOPERATIVE (RT A/C PACK) · airframe 99,664 hrs · 26,315 cycles
RIGHT PACK FLOW CONTROL VALVE WAS FOUND FAULTY DURING THE PACK OPERATIONAL CHECK. PART WAS REPLACED AND PACK WAS PLACED BACK IN OPERATION.
Part: CIRCUIT CARD — FAULTED (RT A/C PACK) · airframe 99,664 hrs · 26,315 cycles
RIGHT PACK RESET SWITCH WAS PLACED ON MEL. ISSUE WAS ISOLATED TO A FAULTY PACK FLOW CONTROL CARD.
1999
Part: SMOKE DETECTOR — FAILED (AFT LAVATORY)
RIGHT AFT LAV SMOKE DETECTOR WON'T TEST. REPLACED SMOKE DETECTOR, CHECKS OK PER MM 26-10-0. (M)
Part: BATTERY — DISCHARGED (AFT AIRSTAIR)
FLT 6530 - DCA-LGA - AFT AIRSTAIR EXIT LIGHT INOP. REPLACED BATTERIES, CHECKS OK. (M)
Part: PT7 TUBE — BROKEN (NR 2 ENGINE)
FLT 6410 - DCA-LGA - ON TAKEOFF ROLL, NR 2 ENGINE EPR DROPPED TO 1.7 AT 100 KNOTS. TAKEOFF ABORTED. ENGINE ANTI-ICE ON. CI NR M81495 ASSIGNED PER MEL SEQ 77-1. NR 2 ENGINEER INDICATION INOP. CI NR M841495 CLEARED, REPLACED NR 2 ENGINE REPLACED BROKEN PT7 LINE IN TURBINE EXHAUST AT 12 O'CLOCK POSITION, LEAK CHECKS OK. (M)
1998
Part: BATTERY PACK — DISCHARGED (CABIN)
FLT 6100 - LGA-BOS - EMERGENCY EXIT LIGHT INOPERATIVE ON RIGHT AFT EXTERIOR LIGHT. REPLACED BATTERY PACK AND LIGHT ASSEMBLY, OPERATIONAL CHECK NORMAL. (M)
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)
FLT 6531 - LGA-DCA - AFT LAVATORY SMOKE ALARM SOUNDED IN FLIGHT, NO EVIDENCE OF SMOKE HEAT OR FUMES. REPLACED AFT LAVATORY SMOKE DETECTOR, OPERATIONAL CHECK NORMAL. (M)
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)
FLT 6110 - LGA-BOS - AFT LAV SMOKE DETECTOR CAME ON IN FLIGHT. REPLACED AFT LAV SMOKE DETECTOR PER MM 25-60-01. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
FLT 6141 - BOS-LGA - AFT EXIT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK OPERATIONAL CHECK NORMAL. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
FLT 6530 - DCA-LGA - RIGHT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY CHARGER AND BATTERY PACK, OPERATIONAL CHECK NORMAL. (M)
Part: CHARGER UNIT — INOPERATIVE (CABIN)
FLT 6790 - DCA-LGA - RIGHT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY BASE CHARGER UNIT, OPERATIONAL CHECK NORMAL PER MM 33-50. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
FLT 6790 - DCA-LGA - RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL PER MM 33-50. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
EMERGENCY EXIT LIGHT AT AFT EXIT DOOR IS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL PER MM 33-50-0 (FLIGHT 6541 FOUND ON L/S CHECK DCA). (X)
Part: FLT/GND SENSOR — FAILED (LT MLG)
FLT 6081 - BOS-LGA - AIRCRAFT AT GATE SMOKE IN CABIN BEFORE DEPARTURE, BOTH AIRCRAFT PACKS OVERHEATED WITH PACK GROUND COOLING FAN DOORS FULL OPEN. SMOKE IN CABIN, PASSENGERS DEPLANED. REPLACED FLT/GROUND SHIFT SENSOR ON LEFT MAIN LANDING EAR PER MM 32-31-0. OPERATIONAL CHECK NORMAL. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
FLT 6530 - LEFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED CHARGING UNIT AND BATTERY PACK. OPERATIONAL CHECK NORMAL PER MM CHAPTER 33-50. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
FLT 6512 - DCA-LGA - LEFT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECKS NORMAL PER MM 33-50. (M)
Part: ACTUATOR — JAMMED (NR 2 LE FLAP)
ON CLIMB-OUT, WHILE RETRACTING FLAPS FROM 5 DEGREES TO 10 DEGREES NR 2 LEADING EDGE FLAP REMAINED FULLY EXTENDED, CYCLED FLAPS NO HELP. REPLACED NR 2 LEADING EDGE FLAP ACTUATOR. OPERATIONAL CHECKS NORMAL PER MM CHAPTER 27-81-22. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
FLT 6500 - OVERNIGHT L/S LGA, LEFT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL PER MM CHAPTER 33-50. (M)
1997
Part: BATTERY CHARGER — FAILED (CABIN)
FLT 6480 - FOUND ON OVERNIGHT L/S, FIRST TEN EMERGENCY PATH LIGHTS INOPERATIVE. REPLACED CHARGER DUE TO BLOWN FUSE, OPERATIONAL CHECK NORMAL. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
FLT 6681 - FOUND ON OVERNIGHT L/S, LEFT INTERIOR OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REPLACED LEFT OVERWING BATTERY PACK ASSEMBLY, OPERATIONAL CHECK NORMAL. (M)
Part: BATTERIES — DISCHARGED (CABIN)
FLT 6540 - DCA-LGA - AFT AIRSTAIR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
DCA/LGA - FLT 6540 - AFT ENTRY EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
DCA/LGA - FLT 6540 - LEFT HAND OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
RIGHT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONALC HEC CHECK NORMAL. FOUND ON L/S CHECK OVERNIGHT LGA. OFF FLIGHT 6460 DCA TO LGA. (X)
Part: BATTERY CHARGER — INOPERATIVE (CABIN)
LEFT OVERWING EMERGENCY EXIT SIGNS INOPERABLE. REPLACED BATTERY CHARGER UNIT, OPERATIONAL CHECK NORMAL. FOUND AN OVERNIGHT L/S CHECK OFF FLIGHT 6460 (DCA TO LGA). (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
AFT ENTRY EMERGENCY EXIT SIGN INOPERABLE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. (FOUND AN OVERNIGHT L/S CHECK OF FLIGHT 6460 DCA TO LGA. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
BOS/LGA - FLT 6141 - DURING L/S CHECK, DISCOVERED LEFT HAND AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
FOUND L/S CHECK, AFT ENTRY EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL PER MM 33-50-0. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
LGA/DCA - FLT 6531 - DURING L/S CHECK, DISCOVERED EMERGENCY EXIT LIGHT INOPERTIVE AT AFT ENTRY DOOR. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL IAW MM 33-50-0. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
LGZ/DCA - FLT 6531 - DURING L/S CHECK, DISCOVERED LEFT AFT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL IAW MM 33-50-0. (X)
Part: LIGHT — INOPERATIVE (CABIN)
FLT 6140 - LGA-BOS - FOUND ON L/S CHECK, L-1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS NORMAL IAW MM CHAPTER 33-50. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
FLT 6531 - DCA-LGA - LEFT AFT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK. (M)
Part: COFFEEMAKER — SHORTED (NR 1 POSITION)
ON FLT 6100, THERE WAS A STRONG SMELL OF ELECTRICAL SMOKE IN THE FORWARD GALLEY AREA. CREW PULLED ALL C/B'S FOR THE GALLEY AND LAV'S, SMELL DISIPATED. INSPECTION FOUND NR 1 COFFEEMAKER WITH TWO SHORTED WIRES AT H20 HEATER. REPLACED NR 1 COFFEEMAKER OPERATION CHECKED OK PER MM 25-30-00. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
FLT 6540 - DCA-LGA - LEFT EXTERIOR AFT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECKS NORMAL IAW MM 33-50-0. (M)
Part: BATTERY PACK — DISCHARGED (AFT ENTRY DOOR)
FLT 6530 - DCA-LGA - EMERGENCY EXIT LIGHT OVER AFT ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECKS NORMAL IAW MM 33-35-0. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
FLT 6500 - DCA-LGA - LEFT FORWARD OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECKS NORMAL IAW MM 33-50-00. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
FOUND ON OVERNIGHT L/S, FORWARD CABIN EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL IAW MM 33-50. (M)
Part: BATTERY PACK — DISCHARGED (LEFT EXTERIOR)
FLT 6141 - BOS-LGA - LEFT SIDE AFT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK OPERATIONAL CHECK NORMAL PER MM 33-50. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
LGA - FLT 6540 - ON OVERNIGHT INSPECTION, THE AFT LEFT HAND EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY PACK FOR THE AFT LEFT HAND EXTERIOR EMERGENCY LIGHT. OPERATION CHECKED OK. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
FLT 6530 - DCA-LGA - FOUND ON L/S CHECK, RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
FLT 6540 - LGA - ON OVERNIGHT INSPECTION, THE RIGHT EMERGENCY EXIT SIGNS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK, OPERATION CHECKED OK. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
FLT 6540 - LGA - ON OVERNIGHT INSPECTION, THE LEFT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY PACK OPERATION CHECKED OK. REFERENCE TAOA019708.
Part: BATTERY PACK — DISCHARGED (CABIN)
FLT 6081 - BOS-LGA - FOUND ON LS CHECK, OVERHEAD EMERGENCY EXIT LIGHTS INOP AT ROWS 17, 22, 30. REPLACED BATTERY PACKS AT ROWS 17, 22 AND 30. OPERATIONAL CHECK NORMAL.
Part: RIB — CRACKED (WS 70.5)
DURING D-CHECK, A 2 INCH CRACK AT 70.5 WING RIB UPPER CHORD RIGHT SIDE AT TWO MOST FORWARD HOLES, WERE FOUND DURING EDDY CURRENT INSPECTION. INSTALLED BOEING REPAIR KIT ON WING RIB UPPER CHORD RIGHT SIDE STATION 70.5 AS PER SERVICE BULLETING 727-57-0112 AND BOEING DRAWING 65C33202. (M)
1996
Part: WIRE — BROKEN (CABIN)
EMERGENCY PATH LIGHTING TRACK DISPLACED AND WIRE BROKEN AT 2 DEF. RED INDICATOR LIGHTS INOP AT L1 AND R1 DOOR. REPAIRED BROKEN WIRE AT 2 DEF, OPERATIONAL CHECK OF LIGHTS NORMAL. REPLACED TRACK SECTION. (M)
Part: SENSE TUBE — BENT (CABIN PRESS)
AT ALTITUDE OF 21,000 FEET AS THE THROTTLES WERE RETARDED TO CRUISE, THE CABIN BEGAN TO CLIMB. AS POWER WAS INCREASED, CABIN PRESSURIZATION CONTROL OPERATED NORMALLY. REPLACED BENT SENSE LINE, SYSTEM TESTED NORMAL PER MM, CHAPTER 21-30-0. REPLACED FLOW CONTROL VALVE, OPS OK PER MM, CHAPTER 21-30-0. (X)
Part: SMOKE DETECTOR — FAILED (FORWARD LAV)
FORWARD LAVATORY SMOKE DETECTOR WARNING WENT OFF ON CLIMB-OUT. REPLACED AND TESTED DETECTOR PER MM 25-60-00. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
AFT ENTRY OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (X)
1995
Part: BASE — CRACKED (AFT OVERWING)
AFT RIGHT OVERWING EMERGENCY EXIT LIGHT BASE CRACKED. REPLACED BASE ASSEMBLY FOR AFT RIGHT OVERWING EMERGENCY EXIT LIGHT. OPS CHECKED GOOD. (M)
Part: SWITCH — STUCK (NR 1 ENGINE)
FLT NR 6450 - DCA-LGA - IN CRUISE, EXPERIENCED A NR 1 OIL PRESSURE/FILTER BYPASS LIGHT ILLUMINATE. RETARDED NR 1 THROTTLE, LIGHT STAYED ON. SHUTDOWN NR 1 ENGINE, OIL PRESSURE REMAINED IN THE GREEN BAND. NR 1 OIL PRESSURE SWITCH STUCK IN THE ON POSITION. REPLACED OIL PRESSURE SWITCH, RAN CHECKED, OPS OK PER MM 79-33-1. (M)
Part: EEL BATT PACK — DISCHARGED (CABIN)
OVERHEAD EMERGENCY LIGHT AT ROW 9 INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M)
Part: EEL BATTERY PACK — DISCHARGED (CABIN)
OVERHEAD EMERGENCY LIGHT AT FWD CPR AREA INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (X)
Part: EEL LENS COVER — MISSING (CABIN)
ROW 16 EMERGENCY LIGHT LENS COVER MISSING. REPLACED LENS COVER. OPERATIONAL CHECK OK. (X)
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)
EMERGENCY LIGHTS AT CEILING OVERWING AND AT AFT OF LIFE RAFT COMPARTMENT FOUND INOPERABLE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS - OPS CK OK. (X)
Part: APU — LEAKING OIL (WHEEL WELL)
PRIOR TO BOARDING, APU FILLED CABIN WITH SMOKE. FOUND OIL ON GROUND AROUND APU AND APU COVERED WITH OIL. M841141 ASSIGNED PER MEL SEQ 49-1. MAINTENANCE LATER REPLACED APU ASSEMBLY. (W)