N628AA
Registered owner: EDGE AIR LLC, DE (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.
85 reports on file, 1996-01-21 – 2014-03-26.
Part: WIRE HARNESS — DISCONNECTED (CABIN) · airframe 72,984 hrs · 25,974 cycles
SEAT 25D EMERGENCY LIGHTS INOPERATIVE. RECONNECTED SEAT 25D EMERGENCY LIGHTS WIRE BUNDLE NEXT TO WALL. OPERATIONS CHECKED NORMAL.
Part: WIRE HARNESS — DISCONNECTED (CABIN) · airframe 72,984 hrs · 25,974 cycles
SEAT 17D BOTH RED LIGHT EMERGENCY LIGHTS INOPERATIVE. RECONNECTED SEAT 17D EMERGENCY LIGHT WIRE BUNDLE NEXT TO BULKHEAD. OPERATIONS CHECKED NORMAL.
Part: HYDRAULIC LINE — RUPTURED (RT MLG) · airframe 72,447 hrs · 25,790 cycles
MIA CREW REPORTED LT HAND HYD RESERVOIR ANNUNCIATOR LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND HYD PRESSURE LINE TO RT GEAR TILT ACTUATOR LEAKING. REPLACED HYD LINE. SYSTEM GND CHECKED NORMAL OPERATION CLOSED.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,723 hrs · 25,887 cycles
ESCAPE PATH LIGHTS FROM ROWS 9D - 15D INOPERATIVE. REPLACED BATTERY PACK & CONTROL MODULE. OPERATIONS CHECKED NORMAL.
Earlier reports · 1996–2013 · 81 reports
2013
Part: BLADE — DAMAGED (NR 1 ENGINE) · airframe 71,707 hrs · 25,517 cycles
NR 1 ENG HAS FAN BLADE TIP DAMAGE TO NR 9 & 10 BLADE FROM A BIRD STRIKE. REPLACED 9 & 10 BLADE.
Part: BATTERY — DISCHARGED (CABIN) · airframe 71,477 hrs · 25,432 cycles
ROWS 9 TO 15 SEAT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY FOR EMERGENCY LIGHT MODULE M01799. OPERATIONS CHECKED NORMAL.
Part: GUIDE — GOUGED (RADOME) · airframe 69,859 hrs · 24,857 cycles
FRAME STATION 200 STRINGER 30 LOWER RADOME GUIDE GOUGED ON LOWER SIDE OF GUIDE ON PRESSURE BULKHEAD. REMOVED AND REPLACED GUIDE PER SRM 51-40-02 AND BAC DRAWING 141N7838 REV K.
Part: SHIM — EXPOSED (LT PYLON) · airframe 69,859 hrs · 24,857 cycles
SHIM PLIES ARE EXPOSED ON LEFT PYLON MID BULKHEAD. REMOVED AND REPLACED FORWARD INBOARD AND OUTBOARD SHIM AND HI-LOK ON NUMBER 1 PYLON MID BULKHEAD PER AARD 54-50-02-3.
2012
Part: RETAINER — BROKEN (EXIT SIGN) · airframe 69,350 hrs · 24,682 cycles
RIGHT SIDE FORWARD OVERWING EXIT SIGN RETAINER IS BROKEN. REMOVED AND REPLACED RIGHT SIDE FORWARD OVERWING EXIT SIGN. OPS CHECK NORMAL.
Part: OXYGEN MASK — UNSERVICEABLE (COCKPIT) · airframe 69,091 hrs · 24,595 cycles
DFW - INFLIGHT MIA-LAS. CREW REPORTED FIRST OFFICER OXYGEN MASK UNUSABLE. FLIGHT DIVERTED DFW LANDED WITHOUT INCIDENT. REPLACED FIRST OFFICER O2 MASK ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,146 hrs · 24,256 cycles
LEFT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR LEFT OVERWING EMERGENCY EXIT SIGN. OPS CHECK NORMAL.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,396 hrs · 23,588 cycles
SEAT 36D EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SEAT 36D MOUNTED EMERGENCY LIGHT ASSEMBLY. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,396 hrs · 23,588 cycles
FORWARD SEAT MOUNTED EMERGENCY LIGHT AT 9D INOPERATIVE. REPLACED LAMP FOR FORWARD SEAT 9D MOUNTED EMERGENCY LIGHT. OPS CHECKS NORMAL.
Part: SHROUD — BROKEN (CABIN) · airframe 66,396 hrs · 23,588 cycles
SEAT 1E AFT EMERGENCY LIGHT SHROUD BROKEN. REPLACED AFT SEAT 1E EMERGENCY LIGHT SHROUD. OPS CHECK NORMAL.
Part: DOOR — CRACKED (CABIN) · airframe 66,099 hrs · 23,483 cycles
RIGHT NUMBER 2 DOOR HAS A CRACK IN THE UPPER HINGE CUTOUT AREA. REMOVED DAMAGED AREA OF FORWARD FRAME. FABRICATED AND INSTALLED DOUBLER PER EA COMP-52-018996.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,190 hrs · 22,814 cycles
SEAT 19D EPL HAS ONE LAMP INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT 19D ESCAPE PATH LIGHT. OPS CHECK NORMAL.
2010
Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,226 hrs · 22,100 cycles
ESCAPE PATH LIGHTING AT 25D HAS TWO LAMPS INOPERATIVE. REPLACED ONE OF TWO LAMPS FOR ESCAPE PATH LIGHTING AT 25D. OPS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,226 hrs · 22,100 cycles
ESCAPE PATH LIGHTING AT 25D HAS TWO LAMPS INOPERATIVE. REPLACED ONE OF TWO LAMPS FOR ESCAPE PATH LIGHTING AT 25D. OPS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,226 hrs · 22,100 cycles
ESCAPE PATH LIGHTING AT 20D HAS TWO LAMPS INOPERATIVE. REMOVED AND REPLACED ONE OF TWO LAMPS FOR ESCAPE PATH LIGHTING AT 20D. OPS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,226 hrs · 22,100 cycles
ESCAPE PATH LIGHTING AT 20D HAS TWO LAMPS INOPERATIVE. REPLACED ONE OF TWO LAMPS FOR ESCAPE PATH LIGHTING AT 20D. OPS CHECKED NORMAL.
Part: PLACARD — PEELING (OVERWING EXIT) · airframe 62,226 hrs · 22,100 cycles
AFT LEFT OVERWING LATCH EXIT STICKER PEELING. REMOVED AND REPLACED EXIT STICKER AT AFT LEFT OVERWING LATCH.
Part: SHROUD — DAMAGED (CABIN) · airframe 62,085 hrs · 22,048 cycles
SEAT MOUNTED EMERGENCY LIGHT AT 10D DAMAGED. REPLACED SHROUD FOR SEAT MOUNTED EMERGENCY LIGHT AT 10D. OPS CHECKED NORMAL.
Part: LIGHT — DAMAGED (CABIN) · airframe 62,085 hrs · 22,048 cycles
SEAT MOUNTED EMERGENCY LIGHT AT 10D DAMAGED. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT 10D. OPS CHECKED NORMAL.
Part: BATTERY PACK — WEAK (CABIN) · airframe 62,085 hrs · 22,048 cycles
FOUND EMERGENCY LIGHTS FOR FIRST CLASS SECTION TO BE VERY DIM. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS. OPS CHECKED NORMAL.
Part: BATTERY PACK — WEAK (CABIN) · airframe 62,085 hrs · 22,048 cycles
EMERGENCY LIGHTS FOR RIGHT NUMBER 1 DOOR TO BE VERY DIM. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT NUMBER 1 DOOR. OPS CHECKED NORMAL.
Part: LENS — DAMAGED (CABIN) · airframe 62,085 hrs · 22,048 cycles
SEAT MOUNTED EMERGENCY LIGHT AT 10D DAMAGED. REPLACED LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT 10D. OPS CHECKED NORMAL.
Part: BATTERY PACK — WEAK (CABIN) · airframe 62,085 hrs · 22,048 cycles
EMERGENCY LIGHTS FOR LEFT NUMBER 1 DOOR TO BE VERY DIM. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT NUMBER 1 DOOR. OPS CHECKED NORMAL.
Part: CONTROL UNIT — FAULTY (BLEED VALVE) · airframe 61,356 hrs · 21,798 cycles
MIA - INFLIGHT TPA-SJU. CREW REPORTED DURING CLIMB RIGHT ENGINE BEGAN SURGING EGT INTO AMBER RANGE, HIGH NOTED AT 835 DEGREES. FLIGHT DIVERTED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BLEED VALVE CONTROL UNIT THAT HAD FAULTED. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
AFT DECK DOUBLERS BUT UP AGAINST 1720 CHORD. AFT DECK DOUBLERS HAD CORROSION. REMOVED AFT PART OF AFT DECK, AND SPLICED IN A NEW DECK PIECE PER SRM 53-60-51-2R REPAIR 2 AND EA B757-53-008716.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
CORROSION ON PRESSURE BULKHEAD SUPPORT RING AT STATION 1720, STRINGER 27 RIGHT. BLENDED OUT CORROSION PER SRM 51-10-02-0G. FLAP PEENED CORRODED AREA IAW SOPM 20-10-03 AND EA B757-53-008595.
Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
CORROSION DAMAGE WAS FOUND AT THE AFT CARGO DOOR THRESHOLD INNER T-CAP FROM STATION 1380 TO 1440. REMOVED AND REPLACED THE T-CAP EXTRUSION.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
CORROSION ON PRESSURE BULKHEAD SUPPORT RING AT STATION 1720, STRINGER 24 RIGHT. REMOVED CORROSION PER SRM 51-10-02-G. FLAP PEENED CORRODED AREA IAW SOPM 20-10-03 AND EA B757-53-008595. MSR/MRT 024185.
Part: ATTACH ANGLE — BENT (CARGO BAY) · airframe 61,266 hrs · 21,767 cycles
CARGO FLOOR INTERCOSTAL AFT VERTICAL ATTACH ANGLE BENT AND BUCKLED AT STATION 1415 TO 1420 AT LEFT BUTTLINE 1 INCH. REMOVED AND REPLACED VERTICAL ANGLE AND WEB.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
CORROSION ON PRESSURE BULKHEAD SUPPORT RING AT STATION 1720, STRINGER 25 LEFT. BLENDED OUT CORROSION PER SRM 51-10-02-0G. FLAP PEENED CORRODED AREA IAW SOPM 20-10-03 AND EA B757-53-008595.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
CORROSION ON PRESSURE BULKHEAD SUPPORT RING AT STATION 1720, STRINGER 28 LEFT. BLENDED OUT CORROSION PER SRM 51-10-02-0G. FLAP PEENED CORRODED AREA IAW SOPM 20-10-03 AND EA B757-53-008595.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,266 hrs · 21,767 cycles
THE INTERCOSTAL AT BUTTLINE 0 BETWEEN STATIONS 660-680 TOP L-ANGLE IS CRACKED OFF IN AREAS. REPLACED ANGLE IAW SRM 51-10-02-G8.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
CORROSION FOUND IN FOUR PLACES ON TOP OF THE FLOOR SUPPORT AT STATION 1661 TO 1681 AT BUTTLINE 0. REPLACED FLOOR SUPPORT WITH NEW PART.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
THE NUMBER 3 SEAT TRACK IS CORRODED AT STATION 682. REPLACED NR 3 SEAT TRACK STATION 640 TO 780.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
CORROSION ON WEB AT STATION 1077 TO 1079 AT LEFT BUTTLINE 67 TO 68 ALONG LONGERON 17 LEFT. REPLACED WITH NEW WEB.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
CORROSION FOUND AT THE NUT PLATE HOLE AT STATION 1640, RIGHT BUTTLINE 2. REPLACED FLOORBEAM T-CAP PER SRM 53-00-51-2R 4.
Part: GATE — CRACKED (L2 DOOR) · airframe 61,266 hrs · 21,767 cycles
LEFT NUMBER TWO DOOR UPPER GATE CRACKED. INSTALLED NEW GATE PER ESO 90282.
Part: SLAT — DAMAGED (RT WING) · airframe 61,266 hrs · 21,767 cycles
RIGHT WING SLAT NUMBER 10 HAS 2 AREAS WITH CHERRY MAX INSTALLED IN DEEP BLENDS. REMOVED DAMAGED AREAS AND INSTALLED DOUBLERS PER SRM 57-43-01.
Part: CONTROL BOX — CRACKED (L1 DOOR) · airframe 61,266 hrs · 21,767 cycles
LEFT NUMBER ONE DOOR HANDLE CONTROL BOX CRACKED. REMOVED OLD BOX AND INSTALLED FORWARD AND AFT CRANK ARMS WITH NEW BEARINGS PER ESO 90283.
Part: SKIN — DENTED (LE SLAT) · airframe 61,266 hrs · 21,767 cycles
LEFT WING SLAT NUMBER 1 TOP SURFACE, INBOARD END HAS BLENDED DENT AROUND FASTENER. REMOVED DAMAGED AREA OF SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.
Part: SLAT — CORRODED (RT WING) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
RIGHT WING SLAT NUMBER 8 HAS CORRODED AREA BLENDED WITH CHERRY MAX FASTENERS INSTALLED. REMOVED CORROSION INSTALLED DOUBLER PER AARD 57-43-00-3.
Part: GATE — CORRODED (L1 DOOR) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
LEFT NUMBER ONE DOOR, LOWER GATE CORRODED. INSTALLED NEW LOWER GATE PER ESO 90283.
Part: PAN — DAMAGED (L1 DOOR) · airframe 61,266 hrs · 21,767 cycles
LEFT NUMBER ONE DOOR HANDLE PAN GOUGED. REMOVED AND REPLACED LEFT NUMBER ONE HANDLE PAN WITH NEW HANDLE PAN PER ESO 90283.
Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
RIGHT INBOARD LAVATORY MOUNT IS CORRODED AT STATION 1600. REPLACED WITH NEW MOUNT.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
AT STATION 324 THE RIGHT OUTBOARD FLOOR BOARD SUPPORT IS CORRODED. REPLACED WITH NEW PART.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
CORROSION ON FLOORBOARD SUPPORT AT STATION 377 TO 395 AT RIGHT BUTTLINE 54. REPLACED WITH NEW PART.
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
RIGHT WING SLAT NUMBER 7 LEADING EDGE SKIN HAS ONE BLENDED AREA WITH CHERRY MAX FASTENER INSTALLED. INSTALLED DOUBLER ON SLAT PER SRM 57-43-01-2 AND ESO 90309.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
THE LONGITUDAL FLOOR SUPPORT INBOARD OF THE RIGHT NUMBER ONE DOOR AT STATION 345-365 IS CORRODED. REPLACED WITH NEW PART.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
THE LONGITUDAL FLOOR SUPPORT INBOARD OF THE RIGHT NUMBER ONE DOOR AT STATION 324 TO 345 IS CORRODED. REPLACE WITH NEW PART.
Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
RIGHT INBOARD LAVATORY MOUNT IS CORRODED AT STATION 1640. REPLACED WITH NEW PART.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
RIGHT AFT OUTBOARD LOWER DOOR DRAIN SUPPORT CORRODED AROUND FASTENERS. REPLACED WITH NEW PART.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
RIGHT FORWARD OUTBOARD LOWER DOOR DRAIN SUPPORT CORRODED AROUND FASTENERS AT STATION 1640 TO 1661. REPLACED WITH NEW PART.
Part: TORQUE BOX — CRACKED (R4 DOOR) · airframe 61,266 hrs · 21,767 cycles
RIGHT NUMBER FOUR DOOR TORQUE BOX CRACKED. REPLACED TORQUE BOX PER ESO 90108.
Part: GATE — CRACKED (R4 DOOR) · airframe 61,266 hrs · 21,767 cycles
RIGHT NUMBER FOUR DOOR UPPER GATE CRACKED. REPLACED UPPER GATE PER ESO 90108.
Part: SKIN — DENTED (LE SLAT) · airframe 61,266 hrs · 21,767 cycles
BLENDED DENT ON LEFT SLAT NUMBER 2 ON TOP OF LEADING EDGE AT IDLER FASTENER WAS FOUND TO BE BEYOND LIMITS. DAMAGED AREA WAS REMOVED AND FINISH DOUBLER REPAIR WAS INSTALLED PER SRM 57-43-01-2.
Part: SLAT — DENTED (LT WING) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
LEFT WING SLAT NUMBER THREE AT TOP LEADING EDGE INBOARD END BY INBOARD TRACK DENTED. INSTALLED DOUBLER REPAIR PER 57-43-00-1 AND ESO90246.
Part: GATE — CRACKED (R2 DOOR) · airframe 61,266 hrs · 21,767 cycles
RIGHT NUMBER TWO DOOR CRACKED AT GATE. REMOVED CRACKED GATE AND REPLACED WITH NEW PER ESO 90282.
Part: TORQUE BOX — CRACKED (L2 DOOR) · airframe 61,266 hrs · 21,767 cycles
L2 PASSENGER DOOR HANDLE TORQUE BOX CRACKED AT 2 CAM BASKET HOLES. REMOVED AND REPLACED WITH NEW DOOR HANDLE TORQUE BOX AND RECONNECTED ALL ASSOCIATED LINKAGES PER ESO 90282.
Part: GATE — GOUGED (PAX DOOR) · airframe 61,266 hrs · 21,767 cycles
NUMBER FOUR PASSENGER DOOR LOWER GATE HAS DEEP GOUGE. REMOVED AND REPLACED LOWER GATE PER ESO 90108.
Part: GATE — WORN (L2 DOOR) · airframe 61,266 hrs · 21,767 cycles
LEFT NUMBER TWO PASSENGER DOOR LOWER GATE WORN AND CORRODED AT LOWER EDGE. REMOVED LOWER GATE, TRANSFERRED HINGE ASSEMBLY AND EMERGENCY OPERATION ASSEMBLY FROM OLD GATE TO NEW GATE AND INSTALLED ON LEFT NUMBER TWO DOOR PER ESO 90282. ADJUSTMENT AND CHECK TO BE COMPLETED ON ROUTINE TASK CARD 8614.
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
CORROSION ON UPPER SKIN OF SLAT 26 INCHES FROM OUTBOARD END. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 57-43-00-3.
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 61,266 hrs · 21,767 cycles
CORROSION ON UPPER SKIN OF SLAT 26 INCHES FROM OUTBOARD END. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 57-43-00-3.
2009
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,632 hrs · 21,538 cycles
AFT CARGO DOOR MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK M10699, OPS OK.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,632 hrs · 21,538 cycles
EMERGENCY EXIT LIGHT SIGN ABOVE SEAT ROW 18ABC INOPERATIVE. REPLACED BATTERY PACK M10699, OPS OK.
Part: LENS — MISSING (CABIN) · airframe 60,632 hrs · 21,538 cycles
EMERGENCY EXIT AISLE LIGHT AT SEAT ROW 33DEF MISSING LENS. REPLACED LENS FOR AISLE EMERGENCY EXIT LIGHT AT ROW 33DEF, OPS OK.
Part: SHROUD — DAMAGED (CABIN) · airframe 60,632 hrs · 21,538 cycles
EMERGENCY LIGHT AT SEAT 22D HAS SHROUD DAMAGED. REPLACED SHROUD AT SEAT 22D, OPS OK.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,632 hrs · 21,538 cycles
EMERGENCY EXIT AISLE LIGHT AT SEAT ROW 27ABC INOPERATIVE. REPLACED BATTERY PACK M10699, OPS OK.
Part: LENS — MISSING (CABIN) · airframe 60,632 hrs · 21,538 cycles
EXIT MARKER AFT OF LEFT NUMBER TWO DOOR MISSING. REPLACED LENS FOR EMERGENCY EXIT LIGHT MARKER AT LEFT NUMBER TWO DOOR AFT, OPS OK.
2008
Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,725 hrs
DFW - EMERGENCY LIGHT AT SEAT ROW 17D INOPERATIVE. REPAIRED CONNECTION FOR EMERGENCY LIGHT AT SEAT ROW 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
2007
Part: BATTERY PACK — DISCHARGED (CABIN)
MIA - EMERGENCY LIGHTS FROM SEAT ROWS 17 TO 25 INOPERATIVE. CHARGED BATTERY PACKS FOR EMERGENCY LIGHTS FROM SEAT ROWS 17 TO 25. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: LIGHT — MISSING (CABIN)
SFO - EMERGENCY LIGHT AT SEAT 9D IS MISSING. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)
LAX - EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)
DFW - OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 12ABC AND 33DEF INOPERATIVE. REPLACED LAMPS FOR INOPERATIVE OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 12ABC AND 33DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT)
DFW - EMERGENCY LIGHTS AT SEATS 12ABC AND 33DFG INOPERATIVE. REPLACED LAMPS IN INOPERATIVE EMERGENCY LIGHTS AT SEATS 12ABC AND 33DFG. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: SPLICE — UNSECURE (CABIN)
LAX - RIGHT EMERGENCY LIGHTS AT SEATS 1E TO 6E INOPERATIVE. RESECURED WIRE SPLICE AT EMERGENCY EXIT SIGN AT THE L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: TRANSMITTER — MALFUNCTIONED (RT ENGINE)
DFW - FLT 823 - EN ROUTE MIA-LAX, JUST PRIOR TO LEVELING FORM A CLIMB TO FL390, RIGHT ENGINE EPR WENT TO FULL INDICATION RESULTING IN A LOSS OF RIGHT ENGINE POWER. A DESCENT BACK TO FL350 WAS NECESSARY BECAUSE OF DECAYING AIRSPEED. AT FL350, SAME PROBLEMS REMAINED WITH ENGINE MATCHING ENGINE INDICATORS. RIGHT THROTTLE FOUR INCHES AHEAD OF LEFT THROTTLE DUE TO INABILITY TO GET NORMAL THRUST. LANDED IN DFW WITHOUT INCIDENT. ACCOMPLISHED MAINTENANCE CHECK MANUAL CARD 4228. NO LEAKS FOUND. ACCOMPLISHED BITE CHECK AND FOUND CODE 47. REPLACED EPR TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1999
Part: LIGHT — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT FORWARD COACH INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP AT FORWARD COACH CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1998
Part: WIRE — BROKEN (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN FIRST CLASS AND COACH WERE FOUND INOPERABLE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING WIRE BETWEEN FIRST CLASS AND COACH. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: LIGHT — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR LIGHT FOUND INOPERATIVE. REPLACED LIGHT STRIP AT EMERGENCY EXIT FLOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1996
Part: HANDLE PAN — GOUGED (R4 DOOR)
AFW - FOUND R-4 DOOR HANDLE PAN HAS SMALL GOUGE. REF MRB 757-971. REFINISH THE BLEND OUT PER REF C SRM SECTION. (M)
Part: BOLT — MISSING (L1 DOOR)
SAN - FLT 0509 - AT THE GATE AFTER ARRIVAL, UNABLE TO OPEN L1 DOOR. PASSENGERS DEPLANED THROUGH R1 DOOR. REPLACED BOLT AND BUSHING FOUND MISSING FROM UPPER END OF L1 DOOR HANDLE LINKAGE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)