N730AS
Registered owner: BJAUP LLC, KS (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.
393 reports on file, 1995-01-03 – 2006-04-11.
Part: SEAT TRACK — CORRODED (FUSELAGE)
YXX-RT OB SEAT TRACK CORRODED AT BSTA 520-540. INSTALLED NEW SEAT TRACK. (K)
Part: REPAIR — DAMAGED (FRAME) · airframe 68,420 hrs · 61,487 cycles
AFT ACCY BAY FRAME REPAIR AT BS 967 BL 0 DOUBLER IS GAPPED AT BOTH ENDS OF UPPER FRAME. REPAIRED FRAME DOUBLER PER EA 5310 02566.
Part: SKIN — DENTED (BS 960) · airframe 68,420 hrs · 61,487 cycles
FOUND EXTERNAL DENT BETWEEN STR 27R 27L AT BSTA 960. CUTOUT DAMAGED SKIN FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53 30 3 FIG 48.
Part: INTERCOSTAL — CRACKED (BS 947) · airframe 68,420 hrs · 61,487 cycles
INTERCOSTAL CRACKED AND BENT AT LWR CENTER LINE OF ACFT AT BSTA 947.5. FABRICATED NEW INTERCOSTAL AND INSTALLED PER SRM 51-20-1.
Earlier reports · 1995–2005 · 389 reports
2005
Part: SHEAR TIE — CRACKED (FUSELAGE)
YXX - FOUND NDT CRACK INDICATION AT FASTENER HOLE ON SHEAR TIE ANGLE AT BS 480, BETWEEN STRINGER 18L AND 19L. REPLACED SHEAR TIE AND CRACK REMOVED IAW B737-200 SRM. (M)
Part: FUEL TANK — CORRODED (FUSELAGE)
YXX - FOUND FUEL CENTER TANK CORRODED AT UPPER STRUCTURE AT BS 578 LBL 67. CORROSION REMOVED IAW EA 5710-01119. (M)
Part: CHANNEL — CORRODED (FS)
YXX - AFT CARGO PIT FLOOR SUPPORT CHANNEL ANCHOR NUT HOLES HAVE CORROSION AT BS 847 PLUS 15 INCHES RBL 8. AFT CARGO PIT FLOOR SUPPORT CHANNEL ANCHOR NUT HOLES CORROSION REMOVED AT BS 847 PLUS 15 INCHES RBL 8 PER B737-200 SRM 53-10-5 FIG 5. (M)
Part: STRINGER — CRACKED (FUSELAGE)
YXX - NDT CRACK INDICATIONS AT FASTENERS HOLES ON STRINGER 19 LEFT, BS 460-480. CRACK REMOVED IAW B737-200 SRM 53-10-3 FIGURE 1. (M)
Part: STRINGER — CRACKED (FUSELAGE)
YXX - NDT CRACK INDICATION AT FASTENER HOLE BS 470, STRINGER 22L. REPAIRED AND REMOVED CRACK IAW B737-200 SRM 53-10-3 FIG 1. (M)
Part: STRINGER — CRACKED (FS)
YXX - FOUND STRINGER 13R AT BS 500A PLUS 15 INCHES CRACKED. CRACK REMOVED AT STRINGER 13R BS 500A PLUS 15 INCHES PER EA 5330-01918. (M)
Part: SKIN — CORRODED (FUSELAGE)
YXX - AROUND CARGO SKIN AT STRINGER 27L BS 817-837 CORROSION FOUND UPON REMOVAL OF STRINGER. CORROSION REMOVED IAW B737-200 SRM 53-30-3 FIG 48. (M)
Part: DOUBLER — CORRODED (FUSELAGE)
YXX - UPON REMOVAL OF PREVIOUS REPAIR AT BS 500B PLUS 17 INCHES CORROSION ON RT KEEL BEAM AT BS 535. REPAIRED IAW ERO 3838 AND 3846 AND EA 5310-02458. CORROSION REMOVED IAW ERO 3838 STEP 1.1 PARA 74. (M)
Part: WINDOW FRAME — CRACKED (FUSELAGE)
YXX - FOUND LOWER AFT CORNER OF WINDOW FRAME CRACKED IN FASTENER HOLE AT BS 500A PLUS 15 INCHES RT. REPAIRED IAW ERO 3774 CRACK REMOVED ERO 3774 STEP 1.1. (M)
Part: KEELBEAM — CORRODED (FUSELAGE)
YXX - FOUND LEFT KEEL BEAM CORROSION AT BS 535 ON LOWER FLANGE. REPAIRED IAW RO 3838 AND EA 5310-02458. (M)
Part: SKIN — CORRODED (FUSELAGE)
FOUND CORROSION ON FUSELAGE SKIN IN FORWARD BILGE AT BS 500B PLUS 17 INCHES OUTBOARD OF STRINGER 28 RT. REPAIRED IAW EA 5330-01925. (M)
Part: FRAME — GOUGED (FUSELAGE)
YXX - FORWARD CARGO FRAME ANGLE AT BS 4600, 3 INCHES BELOW STRINGER 20L HAS GOUGE. REPAIRED IAW B737-200 SRM 53-10-04 FIG 10 AND EA 5330-01923. (M)
Part: FUEL TANK — CORRODED (FUSELAGE)
YXX - FUEL CENTER TANK CORRODED AT UPPER SURFACE BS 578 RBL 67. REPAIRED IAW EA 5710-01118. (M)
Part: WEB — CORRODED (FUSELAGE)
YXX - FOUND FLOOR WEB AT RT BS 578-597 CORRODED. REPLACED FLOOR WEB RT BS 578-597 WITH MADE REPAIR PART IAW B737-200 SRM 51-20-1 AND 51-30-2 FIGURE 3. (M)
Part: SHEAR TIE — DAMAGED (FS)
YXX - FOUND SHEAR TIE AT BS 480 BETWEEN STRINGER 20L AND 21L HAS LOW EDGE MARGIN. REPLACED WITH FABRICATED REPAIR PART IAW B737-200 SRM 51-30-2 PARA 4.
Part: SHEAR TIE — DAMAGED (FUSELAGE)
YXX - FOUND BS 520 SKIN TO FRAME ATTACH ANGLE BETWEEN STRINGER 27R AND 28R DISPLACED FROM PREVIOUS REPAIRS. REPLACED ATTACH ANGLES IAW B737-200 SRM 53-10-4 FIGURE 6. (M)
Part: SHEAR TIE — DAMAGED (FS)
YXX - BS 520 FRAME TO SKIN ATTACHMENT AT STRINGER 28L TO STRINGER 27 HAS LOW EDGE MARGIN. REPLACED ATTACHMENT PER B737-200 SRM 53-10-4 FIGURE 6. (M)
Part: KEELBEAM — DAMAGED (FUSELAGE)
YXX - RIGHT KEEL BEAM SUPPORT ANGLE AT BS 520 TO 535 HAS PREVIOUS DAMAGE. REPLACED WITH FABRICATED REPAIR PART IAW B737-200 SRM 51-20-1 AND 51-10-1 PARAGRAPH 5A. (M)
Part: SKIN — CRACKED (BS 495 S13R)
CRACK AT FASTENER, WINDOW 8R BSA 495R - LOWER AFT CORNER. CRACKED FASTENER HOLE AT WINDOW 8R BSTA 495 LOWER AFT CORNER REPAIRED IAW EA. (K)
Part: SKIN — CRACKED (FUSELAGE)
CRACK AT FASTENER, WINDOW 10R BSTA 500A=15R-LOWER AFT CORNER. CRACKED FASTENER HOLE AT WINDOW 10R BSTA 500A=15R LOWER AFT CORNER REPAIRED IAW EA. (K)
Part: SKIN — CRACKED (FUSELAGE)
YXX- CRACK AT FASTENER, WINDOW 6R BSTA 455R - LOWER AFT CORNER. CRACKED FASTENER HOLE AT WINDOW 6R BSTA 455 LOWER AT CORNER REPAIRED IAW EA. (K)
Part: FRAME — CRACKED (BS 480 S22L)
FWD CARGO FRAME AT BSTA 480 NEAR STR 22L CRACKED. FWD CARGO FRAME AT BSTA 480 NEAR STR 22L CRACKED FRAME REPAIRED IAW SRM. (K)
Part: ATTACH ANGLE — CORRODED (FUSELAGE)
YXX- FWD CARGO SKIN-TO-FRAME ATTACH ANGLE AT BSTA 500 AND STR 28 LT CORRODED. REPAIRED WITH MADE REPAIR PART. (K)
Part: STRINGER — CORRODED (FUSELAGE)
YXX - FOUND CORROSION IN AFT CARGO PIT ON STRINGER 21L AT BS 940. REPAIRED PER B737-200 SRM 53-10-3 FIGURE 1. (M)
Part: SHEAR TIE — OUT OF TOLERANCE (FUSELAGE)
SHEAR TIE ANGLE BSTA 460 BETWEEN STR 19 AND 20 HAS LOW EDGE MARGIN AT FASTENER HOLE. REPAIRED IAW SRM. (K)
Part: SHEAR TIE — DAMAGED (BS 480 S20-21L)
BSTA 480 BETWEEN STR 20L AND 21L SHEAR TIE ANGLE HAS LOW EDGE MARGIN. REPLACED ANGLE IAW SRM. (K)
Part: SHEAR TIE — CRACKED (FUSELAGE)
YXX - NDT CRACK INDICATION AT FASTENER HOLE ON SHEAR TIE ANGLE AT BSTA 480 BETWEEN STR 19L AND STR 20L. REPLACED SHEAR TIE ANGLE IAW SRM. (K)
Part: FRAME — CRACKED (FUSELAGE)
YXX - NDT CRACK INDICATION AT FASTENER HOLE ON FRAME TO SKIN ATTACHMENT AT BSTA 460 BETWEEN STRINGER 20L AND STRINGER 22L. REPAIRE FRAME IAW SRM. (K)
Part: SHEAR TIE — CORRODED (FUSELAGE)
SHEAR TIE AT BSTA 967 BETWEEN STRINGER 27L THRU 27R HAS CORROSION. SHEAR TIE BETWEEN STRINGER 27L AND 22R REPAIRED IAW SRM. (K)
Part: FRAME — CRACKED (FUSELAGE)
YXX- NDT CRACK INDICATION AT FASTENER HOLE ON FRAME TO SKIN ATTACHMENT AT BSTA 480 BETWEEN STRINGER 19L AND STRINGER 20L. REPAIRED FRAME IAW SRM. (K)
Part: SHEAR TIE — DAMAGED (BS 460)
SHEAR TIE ANGLE BS 460 BETWEEN STR 20L AND 21L HAS LOW EDGE MARGIN AT FASTENER HOLE. REPAIRED IAW SRM. (K)
Part: STRINGER — CRACKED (FUSELAGE)
YXX - STRINGER 20L AT BSTA 390 CRACKED THROUGH FASTENER HOLE. REPAIRED IAW SRM. (K)
Part: FRAME — CRACKED (FUSELAGE)
YXX - NDT CRACK INDICATION AT FASTENER HOLE ON FRAME TO SKIN ATTACHMENT AT BSTA 480 BETWEEN STRINGER 20L AND STRINGER 21L. REPAIRED FRAME IAW SRM. (K)
Part: FRAME — CRACKED (FUSELAGE)
YXX - NDT CRACK INDICATION AT FASTENER HOLE ON FRAME TO SKIN ATTACHMENT AT BSTA 460 BETWEEN STRINGER 21L AND STRINGER 22L. REPAIRED FRAME IAW SRM. (K)
Part: STRINGER — CRACKED (FUSELAGE)
YXX- NDT CRACK INDICATION AT FASTENER HOLES ON STR 19L, BSTA 460-480. REPAIRED IAW SRM. (K)
Part: FRAME — CRACKED (FUSELAGE)
YXX - NDT CRACK INDICATION AT FASTENER HOLE ON FRAME TO SKIN ATTACHMENT AT BSTA 460 BETWEEN STRINGER 19L STRINGER 20L. REPAIRED FRAME IAW SRM. (K)
Part: STRINGER — CRACKED (FUSELAGE)
YXX - NDT CRACK INDICATION AT FASTENER HOLES ON STR 20L, BSTA 460-481. REPAIRED IAW SRM. (K)
Part: SKIN — TOOL DAMAGE (FUSELAGE)
YXX - BONDED DOUBLER AND AIRCRAFT SKIN DAMAGED AT BSTA 827 AT STR 21L BY TOOL. BONDED DOUBLER AND AIRCRAFT SKIN AT BSTA 827 AT STR 21L REPAIRED IAW SRM. (K)
Part: ATTACH FITTING — OUT OF TOLERANCE (FUSELAGE)
BSTA 460 BETWEEN STRINGER 20L AND 21L SKIN TO FRAME ATTACHMENT HAS LOW EDGE MARGIN. REPAIRED IAW SRM. (K)
Part: STRINGER — CRACKED (FUSEAGE)
YXX - NDT CRACK INDICATION AT FASTENER HOLE BSTA 470, STR 22L. REPAIRED IAW SRM. (K)
Part: SHEAR TIE — CRACKED (FUSELAGE)
YXX- NDT CRACK INDICATION AT FASTENER HOLE ON SHEAR TIE ANGLE AT BSTA 480 BETWEEN STR 18L AND STR 19L. REPLACED SHEAR TIE ANGLE IAW SRM. (K)
Part: STRINGER — CORRODED (FUSELAGE)
YXX- AFT CARGO PIT BSTA 827, STR 23L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 827, STR 23L REPAIRED IAW SRM. (K)
Part: ATTACH FITTING — CORRODED (FUSELAGE)
YXX - FRAME ATTACHMENT CORRODED AT BS 520 BETWEEN STRINGER 28L AND 28R. REPLACED SKIN TO FRAME ATTACHMENT IAW B737-200 SRM 51-10-1 PARAGRAPH 9A AND 51-30-2 FIGURE 3. (M)
Part: STRINGER — CORRODED (FUSELAGE)
YXX - AFT CARGO PIT BSTA 827, STR 21L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 827, STR 21L REPAIRED IAW SRM. (K)
Part: FRAME — CRACKED (FUSELAGE)
YXX - FWD CARGO BSTA 480 FRAME CRACKED NEAR STR 22L. FRAME REPAIRED IAW SRM. (K)
Part: STRINGER — CORRODED (FUSELAGE)
YXX- AFT CARGO PIT BSTA 907, STR 21L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 907, STR 21L REAPIRED IAW SRM. (K)
Part: SPLICE — CORRODED (BS 907 S26L)
AFT CARGO PIT BSTA 907, STR 26L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 907 STR 26L SPLICE REPALCED WITH MADE PART IAW SRM. (K)
Part: STRINGER — CORRODED (FUSELAGE)
YXX - AFT CARGO PIT BSTA 827-847, STR 27L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 827-847, STR 27L REPAIRED IAW SRM. (K)
Part: STRINGER — CORRODED (FUSELAGE)
YXX - AFT CARGO PIT BSTA 807-847, STR 26L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 807-847, STR 26L REPAIRED IAW SRM. (K)
Part: STRINGER — CORRODED (BS 827 S24L)
AFT CARGO PIT STR 24L HAS CORROSION FWD OF BST 827 FRAME. STRINGER 24L AT BS 827 CORROSION REPAIRED IAW SRM. (K)
Part: SPLICE — CORRODED (BS 907 S27L)
AFT CARGO PIT STR SPLICE AT BSTA 907 STR 27L HAS CORROSION. AFT CARGO PIT STR SPLICE @ BSTA 907 27L, REPLACED WITH MADE REPAIR PART IAW SRM. (K)
Part: CHANNEL — CORRODED (BS 847)
AFT CARGO PIT FLOOR SUPPORT CHANNEL ANCHOR NUT HOLES HAVE CORROSION AT BSTA 847=15, RBL 8. AFT CARGO PIT FLOOR SUPPORT CHANNEL ANCHOR NUT HOLES CORROSION AT BSTA 847=15, RBL 8 REPAIRED IAW SRM. (K)
Part: HYDRAULIC LINE — CRACKED (HYDRAULIC SYS)
SEA - WHILE EXTENDING FLAPS TO NR5 POSITION, HYDRAULIC LOW-PRESSURE LIGHTS ILLUMINATED. QUANTITY WENT TO ZERO. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED (A) SYSTEM HYDRAULIC PRESSURE LINE. ACCOMPLISHED CONDITIONAL INSPECTIONS. RETURNED TO SERVICE. (K)
2004
Part: HOUSING — INOPERATIVE (BATTERY)
ANC - FOUND ROW 8 EMERGENCY LIGHT INOPERATIVE, FLOOR TRACK. REPLACED BATTERY RECEIVER HOUSING. (M)
Part: THRESHOLD — CORRODED (FUSELAGE)
OKC - DURING C-CHECK, FOUND AFT GALLEY DOOR LOWER SILL THRESHOLD IS CORRODED. REMOVED DAMAGED SUPPORT ANGLE AND INSTALLED NEW IAW SRM 51-30-2. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DURING C-CHECK, FOUND FLOORBEAM LOWER SURFACE OF BOTTOM FLANGE AT STATION 420 IS CORRODED. REMOVED DAMAGED RPR STRAPS AND INSTALLED REPLACEMENT RPR STRAP IAW EA 5310-02346. (M)
Part: SEAT TRACK — NICKED (FUSELAGE)
DURING C-CHECK, FOUND SEAT TRACK AT STATION 604-610, RBL 45 IS NICKED AND GOUGED. REMOVED DAMAGED SECTION ANGLE AND INSTALLED REPLACEMENT SECTION IAW SRM 53-10-5. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
OKC - FOUND DURING C-CHECK, INTERCOSTAL TOP AND BTM SIDES AT STATION 1006-1016, RBL 45-50 IS CORRODED. REMOVED DAMAGED WEB AND INSTALLED REPLACEMENT WEB IAW SRM 51-20-1. (M)
Part: BULKHEAD — DENTED (FUSELAGE)
OKC - DURING C-CHECK, FOUND LOWER EXTERNAL SIDE OF AFT PRESSURE BULKHEAD AT SECTION 48, STATION 1040 IS DENTED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER IAW SRM 53-10-4. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DURING C-CHECK, FOUND FLOORBEAM AT STATION 1016, RBL 5-40 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT UPPER CHORD IAW EA5310-02354. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DURING C-CHECK, FOUND FLOORBEAM FLANGE AT STATION 1006, RBL 45 IS CORRODED. REMOVED DAMAGE AND INSTALLED UPPER T-CHORD IAW EA5310-02347. (M)
Part: SKIN — CHAFED (TE FLAP)
DURING C-CHECK, FOUND RIGHT OUTBOARD FLAP ASSEMBLY LOWER SURFACE HAS BARE METAL AND IS CHAFED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER IAW EA5750-01948. (M)
Part: FLOORBEAM — DAMAGED (FUSELAGE)
DURING C-CHECK, FOUND HOLE IN LONGITUDINAL FLOORBEAM, OUTBOARD FLANGE AT STATION 609, RLB 46. REMOVED DAMAGE AND INSTALLED RPR AND STUD BEAM IAW EA5310-02348. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
FOUND C-CHECK, FOUND FLOORBEAM AT STATION 807, LBL 24-44 IS CORRODED AT AFT END UPPER T-CAP. REMOVED DAMAGE AND INSTALLED RPR STRAPS IAW EA5310-02353. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
FOUND C-CHECK, FOUND FLOORBEAM AT STATION 727B, RBL 25-45 IS CORRODED AT NUTPLATES. REMOVED DAMAGE AND INSTALLED RPR ANGLES IAW EA5310-02357. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DURING C-CHECK, FOUND FLOORBEAM AT STATION 480 UPPER FLANGE SURFACES CORRODED. REMOVED DAMAGED AND INSTALLED RPR STRAPS IAW EA5310-02356. (M)
Part: SHROUD — PUNCTURED (NR 2 ENG T/R)
DURING C-CHECK, FOUND NR 2 ENGINE THRUST REVERSER LWR INBOARD SIDE SKIN IS PUNCTURED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER IAW EA7830-01329. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DURING C-CHECK, FOUND AFT AIRSTAIR COLUMN OUTBOARD FLOOR MOUNT HOLES CORRODED. REMOVED DAMAGE, REAMED HOLES AND INSTALLED REPLACEMENT BUSHINGS IAW EA5260-01142. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DURING C-CHECK, FOUND FLOORBEAM AT STATION 986, LBL 15 IS CORRODED. REMOVED DAMAGE AND INSTALLED RPR ANGLE AND STRAP IAW SRM 53-10-9. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
OKC - DURING C-CHECK, FOUND LONGITUDINAL FLOORBEAM AT STATION 540-727B, RBL 45 INBOARD FLANGE SURFACES CORRODED. REMOVED DAMAGED AND INSTALLED RPR STRAPS IAW EA5310-02356. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DURING C-CHECK, FOUND STATION 807 BEAM CAP AT RBL 24.75 TO LBL 24.75. REMOVED DAMAGE AND INSTALLED RPR STRAPS IAW EA5310-02353. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DURING C-CHECK, FOUND FLOORBEAM RPR AT STATION 520 UPPER CHORD IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT PRP CHORD SECTION IAW EA5310-02358. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
OKC - DURING C-CHECK, FOUND FLOORBEAM AT STATION 500A, LOWER FLANGE, LOWER SURFACE IS CORRODED. REMOVED DAMAGED RPR STRAP AND INSTALLED RPR STRAP IAW EA5310-02349. (M)
Part: NOSE COWL — CRACKED (NR 2 ENGINE)
DURING C-CHECK, FOUND NR 2 ENGINE NOSE COWL CRACK EMINATING FROM FASTENER HOLE. REMOVED DAMAGE AND INSTALLED RPR ANGLE IAW EA7110-01233. (M)
Part: STRINGER — CRACKED (FS)
DURING C-CHECK, FOUND LEFT STRINGER 18 AT STA 986 IS CRACKED. REMOVED DAMAGE AND INSTALLED RPR ANGLE IAW SRM 53-10-3. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
OKC - DURING C-CHECK, FOUND FLOORBEAM AT STATION 807, RBL 44-RBL 60 IS CORRODED. REMOVED DAMAGE AND INSTALLED RPR STRAPS IAW EA5310-02353. (M)
Part: SKIN — CHAFED (FLAP)
DURING C-CHECK, FOUND LT OUTBOARD FLAP ASSEMBLY LOWER SURFACE HAS BARE METAL AND IS CHAFED. REMOVED DAMAGE AND INSTALLED RPR DOUBLER IAW EA5750-01947. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM AT STATION 787 IS CORRODED AROUND FASTENER HOLES. REMOVED DAMAGE AND INSTALLED RPR STRAP, ANGLES AND STIFFENERS IAW EA5310-02360. (M)
Part: THRESHOLD — CORRODED (FUSELAGE)
FOUND C-CHECK MAIN CARGO DOOR THRESHOLD WEB IS CORRODED AROUND FASTENER HOLES. REMOVED DAMAGE AND INSTALLED RRR DOUBLER IAW EA 5310-02355. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
DURING C-CHECK- FOUND ANGLE ON INTERCOSTAL AT STATION 980-986, LBL 45 IS CORRODED. REMOVED DAMAGED INTERCOSTAL AND REPLACED INTERCOSTAL IAW 51-30-2. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
DURING C-CHECK, FOUND SHEAR TIE AT STATION 986, BETWEEN 17L AND 19L IS CORRODED. REMOVED DAMAGED SHEAR TIE AND INSTALLED REPLACEMENT SHEAR TIE IAW 51-20-1. (M)
Part: STRINGER — CORRODED (FUSELAGE)
FOUND C-CHECK, FOUND CORROSION UNDER LIP OF STRINGER 24L AT STATION 986. REMOVED DAMAGED SECTION AND INSTALLED REPLACEMENT SECTION IAW 53-10-2. (M)
Part: CREASE BEAM — CORRODED (FUSELAGE)
DURING C-CHECK, FOUND CREASE BEAM AT STATION 980-1016, LBL 45 IS CORRODED. REMOVED CREASE BEAM AND INSTALLED NEW IAW SRM 51-30-2. (M)
Part: SEAT TRACK — WORN (FUSELAGE)
FOUND DURING C-CHECK, SEAT TRACK AT STATION 480-400, RBL 62 IS NICKED AND WORN. REMOVED DAMAGED SECTION AND INSTALLED REPLACEMENT SECTION IAW 51-30-5. (M)
Part: STRUCTURE — DEBONDED (A/C DOOR)
OKC - FOUND DURING C-CHECK, LEFT AIR COND BAY DOOR IS DISBONDING. REBONDED ALUMINUM FOIL PLY IAW EA 5240-01114. (M)
Part: SEAL — CORRODED (LT MLG WW)
DURING C-CHECK, FOUND LEFT WHEEL WELL BLADE SEAL LANDING HAS CORROSION AND BARE METAL AT TOP SURFACE. REMOVED DAMAGED LANDING AND INSTALLED NEW IAW SRM 51-30-2. (M)
Part: CREASE BEAM — CORRODED (FUSELAGE)
DURING C-CHECK, FOUND CREASE BEAM DOUBLER AT STATION 1004-1012, RBL 45-46 IS CORRODED. REMOVED DOUBLER AND INSTALLED NEW IAW SRM 51-30-2. (M)
Part: MOUNT FITTING — CRACKED (AIRSTAIR)
OKC - DURING C-CHECK, FOUND AFT AIRSTAIR FORWARD MOUNT FITTING IS CRACKED. REMOVED DAMAGED FITTING AND INSTALLED REPLACEMENT FITTING IAW SRM 51-10-1. (M)
Part: SKIN — CRACKED (SLAT)
DURING C-CHECK, FOUND RT OUTBOARD SLAT CRACKED AND DELAMINATED AT UPPER TRAILING EDGE. REMOVED DAMAGE AND INSTALLED DOUBLER IAW EA 5740-01391. (M)
Part: STRAP — CORRODED (FUSELAGE)
DURING C-CHECK, FOUND LOWER SURFACE OF LOWER FLANGE AT STATION 500B, BETWEEN BL 0 AND LBL 45. REMOVED DAMAGED STRAP AND INSTALLED REPAIR STRAP IAW EA 5310-01464. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DURING C-CHECK, FOUND FLOORBEAM VERT WED AT STATION 1016, RBL 42 IS CORRODED. REMOVED DMG DOUBLER AND INSTALLED RPLC DOUBLER IAW 51-20-1. (M)
Part: SKIN — DEBONDED (A/C BAY DOOR)
DURING C-CHECK, FOUND RIGHT AIR CONDITIONING BAY DOOR IS DISBONDING. REBONDED ALUMINUM FOIL PLY IAW EA 5240-01114. (M)
Part: STRINGER CLIP — CORRODED (FUSELAGE)
OKC - DURING C-CHECK, FOUND STRINGER CLIP AT STATION 986, STRINGER 23L IS CORRODED. REMOVED DAMAGED STRINGER CLIP AND INSTALLED REPLACEMENT STRINGER CLIP IAW SRM 51-30-2. (M)
Part: TORQUE BOX — CORRODED (AIR STAIRS)
OKC - DURING C-CHECK, FOUND AIRSTAIR TORQUE BOX, BTM SIDE AT STATION 980-986, LBL 50 IS CORRODED. REMOVED DAMAGED WEBS AND INSTALLED REPLACEMENT WEBS IAW BOEING DWG 65-59658. (M)
Part: STRINGER CLIP — CORRODED (FUSELAGE)
OKC - DURING C-CHECK, FOUND STRINGER CLIP AT STATION 986, STRINGER 24L IS CORRODED. REMOVED DAMAGED CLIP AND INSTALLED REPLACEMENT CLIP IAW SRM 51-30-2. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES AT STATION 540-650. OPENED UP HOLES, INSPECTION WITH HFEC, TREATED AND PRIMED AREA IAW EA 5310-02341. (M)
Part: SEAT TRACK — GOUGED (FUSELAGE)
FOUND SEAT TRACK AT STATION 370-468 IS WORN AND GOUGED. REMOVED DAMAGED SECTION AND INSTALLED RPR SEAT TRACK SECTION IAW SRM 53-10-5. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
FOUND CABIN SEAT TRACK AT LBL 45, STATION 727-887 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT SECTION IAW SRM 51-20-1. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
DURING C-CHECK, FOUND SHEAR TIE AND FRAME AT STATION 986, BETWEEN STRINGER 18L AND 19L IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT SHEAR TIE AND NEW FRAME SPLICE IAW SRM 51-30-2. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING C-CHECK, FOUND SEAT TRACK AT STATION 827-947, RBL 25 IS CORRODED. REMOVED DAMAGED SECTION AND INSTALLED REPLACEMENT SECTION IAW SRM 51-30-2.
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING C-CHECK, FOUND CABIN SEAT TRACK AT LBL 25, STATION 887 IS CORRODED. REMOVED DAMAGE AND INSTALLED REPLACEMENT SECTION IAW SRM 51-30-2. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING C-CHECK FOUND SEAT TRACK INBOARD FLANGE AT STATION 420-480, RBL 24 IS CORRODED. REMOVED DAMAGED SECTION AND INSTALLED REPLACEMENT SECTION IAW SRM 51-30-2. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
FOUND SPOT CORROSON ON BEAM CAP SUPPORT JUNCTION AT STATION 360, RBL 12. REMOVED DAMAGE AND INSTALLED RPR SECTION IAW SRM 53-10-9. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
FOUND FLOORBEAM LOWER FLANGE AT STATION 500, BL 0 - LBL 45 HAS LIGHT CORROSION. REMOVED DAMAGED PRP STRAP AND INSTALLED REPLACEMENT RPR STRAP IAW SRM 51-30-2 AND EA 5310-01463. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
FOUND FLOORBEAM TOP SURFACE AT STATION 1006, RBL 1-LBL 12 IS CORRODED. REMOVED DAMAGED RPR, INSTALLED REPLACEMENT RPR ANGLES IAW SRM 53-10-9. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
FOUND FLOORBEAM RPR STRAP AT STATION 847 IS CORRODED. REMOVED DAMAGED RPR STRAP AND INSTALLED REPLACEMENT RPR STRAP IAW SRM 51-10-2 AND EA 5310-01478. (M)
Part: STRINGER CLIP — CORRODED (FUSELAGE)
FOUND STRINGER CLIP AT STATION 986, STRINGER 19L IS CORRODED. REMOVED DAMGAED CLIP AND INSTALLED REPLACEMENT CLIP IAW SRM 51-20-1. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
FOUND CORROSION ON FLOORBEAM RPR STRAP AT FS 767. REMOVED DAMAGED RPR STRAP AND INSTALLED REPLACEMENT RPR STRAP IAW EA 5310-01465. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
FOUND CORROSION ON FLOORBEAM RPR STRAP AT FS 747. REMOVED DAMAGED RPR STRAP AND INSTALLED REPLACEMENT RPR STRAP IAW EA 5310-01466. (M)
Part: SEAT TRACK — GOUGED (FUSELAGE)
FOUND SEAT TRACK IS NICKED AND GOUGED AT STATION 600-616, LBL 25. REMOVED DAMAGED SECTION AND INSTALLED REPLACEMENT FLOOR TRACK SECTION IAW SRM 53-10-5. (M)
Part: THRESHOLD — CORRODED (FUSELAGE)
FOUND L2 DOOR THRESHOLD WEB IS CORRODED AND GOUGED. REMOVED DAMAGED WEB AND INSTALLED REPLACEMENT WEB IAW SRM 51-30-2. (M)
Part: LIGHT — INOPERATIVE (SMOKE BARRIER)
ANC - DURING MAINTENANCE, FOUND SMOKE BARRIER EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED ILGHT ASSEMBLY. (M)
Part: BATTERY — DISCHARGED (SMOKER BARRIER)
ANC - DURING RECON INSPECTION, FOUND THE EMERGENCY EXIT SIGN ON THE SMOKE BARRIER INOPERATIVE. REPLACED BATTERY, THEN LIGHT TESTED NORMAL. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ANC - DURING RECON INSPECTION, FOUND THE EMERGENCY FLOOR TRACK LIGHTS ON PALLET 10-3 INOPERATIVE. REPLACED BATTERY PACK, THEN LIGHT TESTED NORMAL. (M)
Part: BATTERY — DISCHARGED (SMOKER BARRIER)
ANC - DURING RECON INSPECTION, FOUND THE EMERGENCY EXIT SIGN ON THE SMOKE BARRIER INOPERATIVE. REPLACED BATTERY, THEN LIGHT TESTED NORMAL. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING C-CHECK, FOUND SEAT TRACK AT STATION 887-940, BL 0 HAS SEVERE CORROSION. REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED REPLACEMENT SECTION IAW SRM 51-20-1. (M)
2003
Part: SKIN PANEL — CRACKED (FUSELAGE)
PAE - DURING A-CHECK, FOUND THE FUSELAGE SKIN PANEL AT BODY STATION 747-748, STRINGER 17R CRACKED. REPAIRED SKIN PER SRM. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ANC - DURING INSPECTION, FOUND OVERWING EXIT IDENTIFIERS WITH DISCHARGED BATTERY. REMOVED AND REPLACED BATTERIES, THEN EXIT IDENTIFIERS OPERATED NORMALLY. (M)
Part: KEELBEAM — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND THE KEEL BEAM AT FUSELAGE STATION 800, RIGHT BUTTOCK LINE 6 CORRODED. REPAIRED KEEL BEAM PER EA. (M)
Part: SKIN PANEL — BULGED (FUSELAGE)
PAE - DURING C-CHECK, FOUND THE SKIN PANEL AT FUSELAGE STATION 520, STRINGER 27L-28L BULGING. REMOVED DAMAGED AREA AND REPAIRED SKIN PANEL PER EA. (M)
Part: BEAR STRAP — CRACKED (FUSELAGE)
DURING C-CHECK, FOUND THE BEAR STRAP AT FUSELAGE STATION 360, LEFT BUTTOCK LINE 65 CRACKED. REPAIRED BEAR STRAP PER EA. (M)
Part: SKIN PANEL — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND THE INNER SKIN PANEL AT FUSELAGE STATION 492, STRINGER 27R-28R CORRODED. REPAIRED SKIN PANEL PER EA. (M)
Part: STRINGER — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND STRINGER 27L AT FUSELAGE STATION 807-827 CORRODED. REPAIRED STRINGER PER EA. (M)
Part: WEB — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND THE SUB THRESHOLD WEB AT FUSELAGE STATION 792-847, STRINGER 26R CORRODED. REPLACED WEB PER SRM. (M)
Part: CASE — CRACKED (AFT AIRSTAIR)
PAE - DURING C-CHECK, FOUND THE AFT AIRSTAIR HANDLE CASING AT FUSELAGE STATION 967, LEFT BUTTOCK LINE 65 CRACKED. REPAIRED HANDLE CASING PER EA. (M)
Part: FRAME — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND THE FRAME AT FUSELAGE STATION 887, STRINGER 24L-25L CORRODED. CUT OUT DAMAGED SECTION AND REPAIRED FRAME PER SRM. (M)
Part: SPLICE — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND THE STRINGER SPLICE AT FUSELAGE STATION 887-934, STRINGER 24L CORRODED. REPLACED STRINGER SPLICE PER SRM. (M)
Part: SKIN — CRACKED (R1 DOOR)
PAE - DURING C-CHECK, FOUND THE R1 DOOR SKIN AT FUSELAGE STATION 295, RIGHT BUTTOCK LINE 68 CRACKED. REPAIRED DOOR SKIN PER EA. (M)
Part: STRINGER — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND STRINGER 20R AT FUSELAGE STATION 767 CORRODED. REPAIRED STRINGER PER SRM. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND THE LONGITUDINAL BEAM AT FUSELAGE STATION 685, RIGHT BUTTOCK LINE 43 CORRODED. REPAIRED BEAM PER SRM. (M)
Part: SPLICE — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND STRINGER SPLICE AT FUSELAGE STATION 907, STRINGER 22L-23L CORRODED. REPLACED STRINGER SPLICE PER SRM. (M)
Part: DOOR FRAME — CRACKED (CARGO DOOR)
PAE - DURING C-CHECK, FOUND THE AFT CARGO DOOR FRAME AT FUSELAGE STATION 836, LEFT BUTTOCK LINE 60 CRACKED. REPLACED DAMAGED DOOR FRAME SECTION PER SRM. (M)
Part: FRAME — DENTED (FUSELAGE)
PAE - DURING C-CHECK, FOUND THE FRAME AT FUSELAGE STATION 420, STRINGER 23L-24L DENTED. REMOVED DAMAGE AND REPAIRED FRAME PER SRM. (M)
Part: DOOR FRAME — GOUGED (FUSELAGE)
PAE - DURING C-CHECK, FOUND THE AFT CARGO DOOR FRAME AT FUSELAGE STATION 727B, STRINGER 20L GOUGED. REMOVED DAMAGED AREA AND REPAIRED DOOR FRAME PER SRM. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND THE SHEAR TIE AT FUSELAGE STATION 987, STRINGER 24L-25L CORRODED. REPAIRED SHEAR TIE PER SRM. (M)
Part: STRINGER — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND STRINGER 26L, FUSELAGE STATION 807-827 CORRODED. REPAIRED STRINGER PER SRM. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND THE SHEAR TIE AT FUSELAGE STATION 987, STRINGER 25L-26L CORRODED. REPAIRED SHEAR TIE PER SRM. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND THE SHEAR TIE AT FUSELAGE STATION 727A, RIGHT BUTTOCK LINE 8 CORRODED. REPLACED SHEAR TIE PER SRM. (M)
Part: SPLICE — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND THE KEEL BEAM SPLICE ANGLES AT FUSELAGE STATION 727-727A, RIGHT BUTTOCK LINE 6 CORRODED. REPLACED SPLICE ANGLES PER SRM. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND THE SEAT TRACK AT BODY STATION 540-727B, WATERLINE 208 CORRODED. REPLACED SEAT TRACK PER SRM. (M)
Part: FRAME — DENTED (FUSELAGE)
PAE - DURING C-CHECK, FOUND THE FRAME AT BODY STATION 500, STRINGER 23R-25R DENTED. CUT OUT DAMAGED SECTION AND REPAIRED FRAME PER SRM. (M)
Part: GUSSET — CRACKED (NR 2 FAIRING)
PAE - DURING C-CHECK, FOUND NR 2 ENGINE FAIRING GUSSET AT NACELLE STATION 99.25 CRACKED. REPLACED GUSSET PER SRM. (M)
Part: FRAME — DENTED (FUSELAGE)
PAE - DURING C-CHECK, FOUND THE FRAME AT BS 727B, STRINGER 24L-25L DENTED. CUT OUT DAMAGED SECTION AND REPAIRED FRAME PER SRM. (M)
Part: STRINGER CLIP — CRACKED (FUSELAGE)
PAE - DURING C-CHECK, FOUND STRINGER CLIP AT BODY STATION 277, STRINGER 26L CRACKED. REPLACED STRINGER CLIP PER SRM. (M)
Part: SUPPORT — CORRODED (FUSELAGE)
PAE - DURING C-CHECK, FOUND SIDEWALL SUPPORT AT BS 500A-520, STRINGER 26R CORRODED. REPLACED SUPPORT PER SRM. (M)
Part: TORQUE TUBE — DAMAGED (R2 DOOR)
SEA - CREW REPORTED THE R2 DOOR WAS DIFFICULT TO OPERATE THROUGH THE OPEN AND CLOSE CYCLE. S/D REMOVED AND REPLACED AFT GALLEY DOOR TORQUE TUBE (P/N 65-45849-160) AND RIGGED R2 DOOR, THEN DOOR OPERATED WITHIN LIMITS. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ANC - DURING RECON INSPECTION, FOUND INSTALLED PALLET ARRIVED WITH DISCHARGED BATTERY. REMOVED AND REPLACED BATTERY PACK, THEN LIGHTS OPERATED NORMALLY. (M)
2002
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING PREFLIGHT CHECK FOUND EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE ON PALLET 8-9. REMOVED AND REPLACED THE BATTERY PACK. THE TRACK LIGHTS THEN OPERATED NORMALLY.
Part: BATTERY PACK — DISCHARGED (CABIN)
ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS WOULD NOT TEST AT ROW 15. REMOVED AND REPLACED THE BATTERY PACK. THE TRACK LIGHTS THEN OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT SEAT PALLET 8-9 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY THEN LIGHTS OPERATED NORMAL. (M)
Part: SKIN — CRACKED (FUSELAGE)
PAE - DURING SCHEDULED C-CHECK, FOUND AFT ENTRY DOOR (L2) SKIN PANEL CRACKED AT BS 986, STRINGER 7L-8L CRACKED. REPAIRED DENT PER SRM. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
PAE - DURING SCHEDULED C-CHECK, FOUND SHEAR TIE AT BS 520, STRINGER 28R CORRODED. REPAIRED DENT PER SRM. (M)
Part: SKIN — DENTED (GALLEY DOOR)
PAE - DURING SCHEDULED C-CHECK, FOUND FORWARD GALLEY DOOR SKIN DENTED. REPAIRED DENT PER SRM. (M)
Part: SKIN — DENTED (CARGO DOOR)
PAE - DURING SCHEDULED C-CHECK, FOUND INNER SKIN ON AFT CARGO DOOR DENTED AT BS 800, STRINGER 25R. REPAIRED DENT PER SRM. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS WOULD NOT TEST IN THE AFT CABIN. REMOVED AND REPLACED THE TWO MOST AFT REMOTE ASSEMBLY BATTERY THEN LIGHTS OPERATED NORMAL. (M)
Part: GUIDE — BROKEN (PAX DOOR)
SEA - DURING MAINTENANCE CHECK, FOUND L1 DOOR GUIDE ARM ASSEMBLY BROKEN. REMOVED AND REPLACED GUIDE ARM ASSEMBLY, THEN DOOR OPERATED NORMALLY. (M)
Part: BRACKET — BROKEN (L1 DOOR)
ANC - DURING MAINTENANCE CHECK, FOUND UPPER HINGE COVER BRACKET BROKEN CAUSING THE L1 DOOR TO BE DIFFICULT TO CLOSE. REMOVED AND REPLACED BRACKET, THEN DOOR OPERATED NORMALLY. (M)
2001
Part: WIRE — BROKEN (CABIN)
ANC - EMERGENCY FLOOR TRACK LIGHTING AT ROW 7, SEAT PALLET 4-9 INOPERATIVE DUE TO BROKEN WIRE. REPAIRED BROKEN WIRE, THEN LIGHT OPS CHECKED GOOD. (M)
Part: SWITCH — MALFUNCTIONED (AFT F/A PANEL)
ANC - SOME EMERGENCY EXIT LIGHTING WILL NOT EXTINGUISH WITH FLIGHT DECK SWITCH IN ARMED POSITION. REMOVED AND REPLACED AFT FLIGHT ATTENDANTS CONTROLS SWITCH THEN LIGHTS OPERATED NORMAL. (M)
Part: MECHANISM — LACK OF LUBE (AIRSTAIRS)
ANC - CREW REPORTED AIRSTAIR MECHANISM DIFFICULT TO OPERATE. LUBRICATED MECHANISM, THEN OPS CHECKED GOOD. (M)
Part: LATCH — LACK OF LUBE (L1 DOOR)
ANC - DURING LINE CHECK, FOUND L1 DOOR HOLD OPEN LATCH INOPERATIVE. LUBRICATED LATCH OPERATIONAL CHECK NORMAL. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
FAI - DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTING AT SEAT PALLET NR 4 INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT BATTERY PACK, OPERATIONAL CHECK NORMAL. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT SEAT PALLETS 6-9 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND RECEIVER THEN LIGHTS OPERATED NORMAL. REF ASAA0110313. (M)
Part: RECEIVER — INOPERATIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT SEAT PALLETS 6-9 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND RECEIVER THEN LIGHTS OPERATED NORMAL. (M)
Part: RECEIVER — INOPERATIVE (CABIN)
ANC - DURING A LINE MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE ON PALLETS 6 AND 7. REPLACED THE EMERGENCY LIGHTING REMOTE RECEIVER ON PALLETS 6 AND 7. THE LIGHTS THEN OPERATED NORMALLY. (M)
Part: HANDLE — LACK OF LUBE (L2 DOOR)
SEA - DURING MAINTENANCE CHECK, FOUND L2 DOOR HANDLE STIFF. LUBED HANDLE, THEN HANDLE OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT ON THE SMOKE BARRIER WOULD NOT TEST. REMOVED AND REPLACED LIGHT ASSEMBLY AND BATTERY, THEN LIGHT OPERATED NORMALLY. REF ASAA0110230. (M)
Part: BATTERY — DISCHARGED (MID CABIN)
SEA - DURING MAINTENANCE CHECK, FOUND EMEREGNCY EXIT LIGHT ON THE SMOKE BARRIER WOULD NOT TEST. REMOVED AND REPLACED LIGHT ASEMBLY AND BATTERY, THEN LIGHT OPERATED NORMALLY. (M)
Part: DOOR FRAME — CRACKED (FUSELAGE)
PAE - DURING MAINTENANCE, FOUND FRAME AROUND MAIN CARGO DOOR CUTOUT AT BS 472.4, STRINGER 24R CRACKED. REPAIRED PER EA. (M)
Part: A/C PACK — MALFUNCTIONED (A/C BAY)
ANC - IMMEDIATELY AFTER DEPARTURE, NOTED STRONG ODOR ONLY IN COCKPIT. ODOR DISSIPATED BUT RETURNED INTERMITTENTLY OVER THE NEXT SIXTY MINUTES. UNABLE TO ISOLATE THE CAUSE OF THE ODOR. BORESCOPED AND CLEANED BOTH ENGINE BLEED AIR DUCTS AND PACK COMPONENTS FROM ENGINE FIREWALLS TO AIR CONDITIONING DISTRIBUTION BAY. REPLACED BOTH CHECK VALVES JUST UPSTREAM FROM MIXER ASSY DUE TO CORROSION, RT PACK DUCT TRIP SENSOR DUE BENT PINS, AND COCKPIT MUFFLER ASSY DUE INSULATION WAS LOOSE. CLEANED OUT AIR DUCTS IN COCKPIT, WHICH CONTAINED MUFFLER INSULATION PARTS. SUSPECT WITH LT PACK NOT GETTING AIR TO COCKPIT RT PACK WAS GOING FULL HOT CAUSING BAD SMELL. ALSO, MUFFLER INSULATION WAS FOUND TO HAVE BAD SMELL. (M)
Part: SMOKE — DETECTED (COCKPIT)
ANC - ABORTED TAKEOFF OF FLT 151, BOTH THE FIRST OFFICERS AND OBSERVER NOTED SMOKE IN THE COCKPIT DURING TAKEOFF. BOTH PACKS WERE TURNED OFF AS AIRCRAFT CLEARED RUNWAY. ANC MAINTENANCE INSPECTED BOTH ENGINES AND APU INLETS AND EXHAUST, NO DEFECTS NOTED. RAN ENGINES AT TAKEOFF POWER AND ISOLATED PACKS, COULD NOT DUPLICATE SMOKE/SMELL. RAN APU, COULD NOT DUPLICATE SMOKE/SMELL. INSPECTED A/C BAY DUCTS AND E/E COMPARTMENT. NO DEFECTS NOTED. REPLACED BOTH WATER SEPARATOR BAGS, BOTH WERE FOUND TO BE CLEAN. AIRCRAFT WAS RELEASED FOR SERVICE. (M)
Part: O-RING — NICKED (LT ENGINE)
ANC - FLT 64 - FLIGHT ATTENDANT REPORTED CHEMICAL ODOR ON CLIMBOUT WHICH DISSIPATED AFTER A FEW MINUTES. NO OTHER REPORTS WERE NOTED. AIRCRAFT LANDED IN JNU WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND ENGINES FOR FERRY FLIGHT TO SEA FOR TROUBLESHOOTING OF REPEAT REPORT OF CABIN/FLIGHT DECK ODOR. MAINTENANCE TROUBLESHOT AND ISOLATED TO LEFT ENGINE. REMOVED AND REPLACED LEFT ENGINE. FOUND THE OIL FUMES IN THE CABIN WERE DUE TO THE CONDITION OF THE NR 3 BEARING HOUSING O-RING (NICKED) AND PISTON RINGS (STUCK) WHICH ALLOWED OIL TO LEAK BY THE LABYRINTH SEAL AND INTO THE 6TH STAGE AIR EXTRACTION USED FOR THE CABIN. THE ENGINE WAS REPAIRED PER THE MM AND RETURNED TO SERVICE. (M)
Part: HANDLE — STIFF (L2 DOOR)
ANC - DURING MAINTENANCE CHECK, FOUND L2 DOOR HANDLE STIFF TO OPERATE. CLEANED AND LUBED HANDLE AND HANDLE OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
SEA - DURING MAINTENANCE CHECK, FOUND WIRES DISCONNECTED TO LIGHTED EMERGENCY EXIT SIGN. RECONNECTED WIRES AND LIGHT OPERATED NORMALLY. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK AT BS 360-390, BL 0 CORRODED. REPAIRED PER SRM. (M)
Part: ANGLE — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND ANGLE AT BS 360, STRINGER 28L CORRODED. REMOVED AND REPAIRED PER BOEING DRAWING. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BS 270, LBL 11, RBL 11 CORRODED. REPAIRED PER BOEING DRAWING. (M)
Part: CLIP — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND SHEAR CLIP AT BS 360, STRINGER 26L-27L CORRODED. REPAIRED PER BOEING DRAWING. (M)
Part: ANGLE — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND TEE CAP ATTACHING ANGLE AT BS 312, STRINGER 27L-28L CORRODED. REPAIRED PER BOEING DRAWING. (M)
Part: STRINGER — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER 26R AT BS 270, CORRODED. REPAIRED PER SRM. (M)
Part: SUPPORT — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND SEAT TRACK SUPPORT AT BS 540-639, LBL 62 CORRODED. REPAIRED PER SRM. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT ANGLE AT BS 737-947, STRINGER 27L CORRODED. REPAIRED PER SRM. (M)
Part: FLOOR SUPPORT — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BS 410-510, STRINGER 27R CRACKED. REPAIRED PER SRM. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 500B, BL 0 - LBL 55 CORRODED. REPAIRED PER EA. (M)
Part: STRINGER CLIP — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 967, STRINGER 24L CORRODED. REPAIRED PER BOEING DRAWING. (M)
Part: ANGLE — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND ANGLE AT BS 357, LBL 15 CORRODED. REMOVED, FABRICATED AND REPLACED ANGLE PER BOEING DRAWING. (M)
Part: SKIN PANEL — CHAFED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND EXTERIOR SKIN PANEL HAS A DEEP CHAFE MARK AT BS 794 NEAR THE AFT DOOR EDGE. REPAIRED PER SRM. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBOARD SUPPORT TRACK AT BS 737-874, STRINGER 27L CORRODED. REPAIRED PER SRM. (M)
Part: STRAP — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND STRAP AT BS 500, BL 0 TO LBL 55 CORRODED. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 420, BL 0 TO LBL 55 CORRODED. REPAIRED PER EA. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BS 270-277, RBL 11 CORRODED. REMOVED, FABRICATED AND REPLACED FLOOR SUPPORT PER BOEING DRAWING. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBOARD SUPPORT TRACK AT BS 737-947, LEFT BUTTOCK LINE 10 CORRODED. REPAIRED PER SRM. (M)
Part: SHEAR TIE — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 727B, STRINGER 26L-28L CORRODED. REPAIRED PER SRM. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT ANGLE AT BS 767, STRINGER 27R CORRODED. REPAIRED PER SRM. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT ANGLE AT BS 727B, STRINGER 26L CORRODED. REPAIRED PER SRM. (M)
Part: STRINGER CLIP — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 727A, RBL 8 CRACKED. REPAIRED PER SRM. (M)
Part: STRINGER CLIP — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 597, RBL 5 CRACKED. REPAIRED PER SRM. (M)
Part: STRINGER CLIP — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 787, LBL 16 CRACKED. REPAIRED PER SRM. (M)
Part: STRINGER CLIP — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP BS 727B, RBL 9 CRACKED. REPAIRED PER SRM. (M)
Part: STRINGER CLIP — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 578, RBL 8 CRACKED. REPAIRED PER SRM. (M)
Part: STRINGER CLIP — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 597, RBL 8 CRACKED. REPAIRED PER SRM. (M)
Part: CLIP — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 727B, LBL 6 CRACKED. REPAIRED PER SRM. (M)
Part: STRINGER CLIP — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 747, RBL 6 CRACKED. REPAIRED PER SRM. (M)
Part: STRINGER CLIP — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 616, RBL 6 CRACKED. REPAIRED PER SRM. (M)
Part: STRINGER CLIP — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 727B, RBL 7 CRACKED. REPAIRED PER SRM. (M)
Part: STRINGER CLIP — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 747, RBL 7 CRACKED. REPAIRED PER SRM. (M)
Part: SPLICE — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND SHEAR TIE SPLICE STRAP AT BS 360-372, STRINGER 28L CORRODED. REPAIRED PER SRM. (M)
Part: STRINGER CLIP — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP AT BS 639, LBL 4 CRACKED. REPAIRED PER SRM. (M)
Part: INTERCOSTAL — DAMAGED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 340-360, BUTTOCK LINE 0 WITH ELONGATED HOLES. (M)
Part: STRINGER — CORRODED (FUSELAGE)
PHX - DURING D-CHECK FOUND STRINGER 27R, BS 360-430 CORRODED. REPAIRED PER SRM. (M)
Part: FRAME — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 440, STRINGER 26R CRACKED. REPAIRED PER SRM. (M)
Part: INTERCOSTAL — DAMAGED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL BS 342-350, LBL 42.5 HAS ELONGATED HOLES. REPAIRED PER SRM. (M)
Part: SKIN — DENTED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 440-480, STRINGER 26R DENTED. (M)
Part: BULKHEAD — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 178, LBL 7 CRACKED. REPAIRED PER SRM. (M)
Part: BULKHEAD — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 178, WL 200, LBL 7 CRACKED. REPAIRED PER SRM. (M)
Part: FLOOR SUPPORT — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BS 540, RIGHT BUTTOCK LINE 2-22 CORRODED. REPAIRED PER SRM. (M)
Part: INTERCOSTAL — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 302, STRINGER 27L CORRODED. REPAIRED PER SRM. (M)
Part: STIFFENER — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND STIFFENER AT BODY STATION 178, LEFT BUTTOCK LINE 6 CRACKED. REPAIRED PER SRM. (M)
Part: FRAME — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND CHORD AT BODY STATION 178, STRINGER 20L CRACKED. REPAIRED PER SRM. (M)
Part: FRAME — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND CHORD AT BS 294-366, STRINGER 27L CORRODED. REPAIRED PER SRM. (M)
Part: FRAME — CRACKED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND FRAME AT BS 597, STRINGER 13L-18R CRACKED. REPAIRED PER SRM. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
PHX - DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 294.5, RIGHT BUTTOCK LINE 24, LEFT BUTTOCK LINE 26 CORRODED. REPAIRED PER SRM. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, FOUND SMOKE BARRIER EMERGENCY EXIT LIGHT BATTERY WOULD NOT TEST. REMOVED AND REPLACED REMOTE ASSEMBLY BATTERY AND LIGHT OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, EMERGENCY LIGHT TRANSMITTER INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT TRANSMITTER BATTERY. LIGHTS OPERATED NORMALLY. (M)
2000
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHT RECEIVER WILL NOT TEST AT ROW 18. REPLACED BATTERY PACK, LIGHTS TESTED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (AFT CABIN)
ANC - DURING MAINTENANCE CHECK, FOUND AFT PALLET EMERGENCY EXIT LIGHTING INOPERATIVE. REPLACED REMOTE ASSEMBLY RECEIVER AND BATTERY PACK. LIGHTS TESTED NORMALLY. REF ASAA0010182. (M)
Part: RECEIVER — INOPERATIVE (AFT CABIN)
ANC - DURING MAINTENANCE CHECK, FOUND AFT PALLET EMERGENCY EXIT LIGHTING INOPERATIVE. REPLACED REMOTE ASSEMBLY RECEIVER AND BATTERY PACK. LIGHTS TESTED NORMALLY. (M)
Part: RECEIVER — INOPERATIVE (CABIN)
ANC - DURING MAINTENANCE CHECK, FOUND SECTION OF EMERGENCY EXIT TRACK LIGHTING WILL NOT SHUT OFF. REPLACED TRACK LIGHT REMOTE ASSEMBLY RECEIVER FOR INOPERATIVE SECTION. SECTION OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (MID CABIN)
SEA - DURING MAINTENANCE CHECK, FOUND ROW 12 RECEIVER WILL NOT PASS EMERGENCY EXIT LIGHT TEST. REMOVED AND REPLACED ASSY RECEIVER AND BATTERY PACK, OPS NORMAL. (M)REF ASAA0010178.
Part: RECEIVER — INOPERATIVE (MID CABIN)
SEA - DURING MAINTENANCE CHECK, FOUND ROW 12 RECEIVER WILL NOT PASS EMERGENCY EXIT LIGHT TEST. REPLACED REMOVE ASSY RECEIVER AND BATTERY PACK, OPS NORMAL. (M)
Part: BATTERY PACK — DISCHARGED (MID CABIN)
SEA - DURING MAINTENANCE CHECK, FOUND AFT ENTRY EMERGENCY ESCAPE LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPS NORMAL. (M)
Part: RECEIVER — INOPERATIVE (MID CABIN)
ANC - DURING MAINTENANCE CHECK, FOUND FLOOR EMERGENCY EXIT LIGHTS ON SEAT PALLET 5-8 WILL NOT EXTINGUISH. REPLACED REMOTE ASSY RECEIVER, OPS NORMAL. (M)
Part: BATTERY PACK — DISCHARGED (MID CABIN)
ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS ON SEAT PALLET 8-2 WOULD NOT EXTINGUISH AND L2 AND R2 EXTERIOR ESCAPE LIGHTS WERE INOPERATIVE. REMOVED AND REPLACED BATERY PACK ON SEAT PALLET 8-2, OPS NORMAL, AND REPLACED POWER SUPPLY TO L2 AND R2 EXTERIOR ESCAPE LIGHTS, OPS NORMAL. (M)
Part: POWER SUPPLY — INOPERATIVE (L2 AND R2 DOORS)
ANC - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS ON SEAT PALLET 8-2 WOULD NOT EXTINGUISH AND L2 AND R2 EXTERIOR ESCAPE LIGHTS WERE INOPERATIVE. REMOVED AND REPLACED BATERY PACK ON SEAT PALLET 8-2, OPS NORMAL, AND REPLACED POWER SUPPLY TO L2 AND R2 EXTERIOR ESCAPE LIGHTS, OPS NORMAL. (M)REF ASAA0010175.
Part: RECEIVER — FAILED (FWD CABIN)
SEA-DURING MAINTENANCE CHECK FOUND EMERGENCY EXIT LIGHTS AT ROWS 2 AND 6 WOULD NOT TEST. REPLACED REMOTE ASSEMBLY RECEIVER AT ROW 2 AND REMOTE ASSEMBLY BATTERY AT ROW 6. LIGHTS TESTED NORMALLY.
Part: BATTERY PACK — DISCHARGED (FWD CABIN)
SEA-DURING MAINTENANCE CHECK FOUND EMERGENCY EXIT LIGHTS AT ROW 8 WILL NOT EXTINGUISH. REPLACED BATTERY PACK. LIGHTS WORKED PROPERLY.
Part: BATTERY PACK — DISCHARGED (MID CABIN)
SEA - DURING MAINTENANCE CHECK, EMERGENCY EXIT LIGHTS AT ROW 16 WOULD NOT TEST. REPLACED BATTERY PACK, LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (SMOKE BARRIER)
SEA-DURING MAINTENANCE CHECK FOUND SMOKE BARRIER AND AFT SEAT PALLET EMERGENCY EXIT LIGHTS INOPERATIVE.REPLACED AFT SEAT PALLET AND SMOKE BARRIER REMOTE ASSEMBLY BATTERY. LIGHTS TESTED NORMAL.
Part: BATTERY PACK — INOPERATIVE (AFT CABIN)
SEA-DURING MAINTENANCE CHECK FOUNT AFT SERVICE DOORS EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK FOR AFT SERVICE DOORS AND THE LIGHTS OPERATED NORMAL.
Part: LIGHT — INOPERATIVE (MID CABIN)
ANC-DURING MX CHECK EMERGENCY LIGHTS ON SEAT PALLET 7-7 WOULD NOT ILLUMINATE. REPLACED EMERGENCY LIGHT RECEIVER ASSY.
Part: CHARGER — INOPERATIVE (MID CABIN)
YXD-DURING SERVICE CHECK THE RT OVERWING INTERIOR LOWER EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. RELEASED PER MEL 33-15A. SEA MAINTENANCE SUBSEQUENTLY REPLACED BATTERY CHARGER AND REPAIRED SHORTED WIRE. THE LIGHT OPERATED NORMALLY.
Part: SHEAR TIE — MISSING (FUSELAGE)
YXD-DURING SCHEDULED MAINTENANCE STA 480 FRAME SHEAR TIE MISSING BETWEEN STRINGER 4R AND 10R. REPAIRED PER BOEING DRAWING 65-46532.
Part: SHEAR TIE — MISSING (FUSELAGE)
YXD-DURING SCHEDULED MAINTENANCE STA 500B FRAME SHEAR TIE MISSING BETWEEN STRINGER 4R AND 13R. REPAIRED PER BOEING DRAWING 65-64958 REV. D.
Part: DOOR FRAME — CRACKED (PAX DOOR)
YXD-DURING SCHEDULED MAINTENANCE STA 480 FRAME WAS FOUND TO BE CRACKED THROUGH THE OUTBOARD FLANGE TERMINATING IN A FASTENER HOLE COMMON TO THE REINFORCEMENT STIFFNER VERTICAL LEG. REPAIRED PER EA 5310-01719.
Part: RECEIVER — INOPERATIVE (MID CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT BATTERY PACK AND RECEIVER WERE FOUND TO BE INOPERATIVE. REPLACED THE RECEIVER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. REF ASAA0010128. (M)
Part: BATTERY PACK — DISCHARGED (MID CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT BATTERY PACK AND RECEIVER WERE FOUND TO BE INOPERATIVE. REPLACED THE RECEIVER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (MID CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTING AT ROWS 10/11 AND 16/17 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACKS AND THE LIGHTS OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
ANC - DURING MAINTENANCE CHECK, TWO EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 16. REPLACED WIRING AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROW 18 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)
Part: RECEIVER — INOPERATIVE (ROW 16)
ANC - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS AT ROW 16 WERE INOPERATIVE. REPLACED RECEIVER AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (SEAT PALLET)
ANC - PRIOR TO FLT 143 - ONE SEAT PALLET EMERGENCY TRACK LIGHTS ILLUMINATED. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (ROW 15)
ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 15 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHTS AT ROWS 1, 3, 14 AND 18 WOULD NOT TEST PROPERLY. REPLACED ASSOCIATED BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT PALLETS 3-2 AND 6-6 WOULD NOT EXTINGUISH. REPLACED BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M)
Part: SIGN — INOPERATIVE (CABIN)
ANC - PRIOR TO FLIGHT 22, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WOULD NOT TEST. REPLACED SMOKE BARRIER EMERGENCY EXIT IDENTIFIER AND THE LIGHT OPERATED NORMALLY. (M)
Part: RECEIVER — INOPERATIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE AFT PALLET EMERGENCY EXIT TRACK LIGHTS REMAINTED ILLUMINATED. REPLACED THE RECEIVER AND BATTERY, LIGHTS OPERATED NORMALY. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE AFT PALLET EMERGENCY EXIT TRACK LIGHTS REMAINED ILLUMINATED. REPLACED THE RECEIVER AND BATTERY, LIGHTS OPERATED NORMALLY. REF ASAA0010064(M)
Part: RECEIVER — INOPERATIVE (CABIN)
ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS ON THE SEAT PALLET JUST AFT OF THE BULKHEAD WERE FOUND TO BE INOPERATIVE. REPLACED THE RECEIVER AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, ONE SEAT PALLET BATTERY PACK FOR EMERGENCY EXIT TRACK LIGHTS WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
Part: CONNECTOR — LOOSE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE AFT CABIN EXIT IDENTIFIER WAS FOUND TO BE INOPERATIVE. TIGHTENED LOOSE CONNECTION AND IDENTIFIER OPERATED NORMALLY. (M)
Part: RECEIVER — INOPERATIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROW 3 WERE FOUND TO BE INOPERATIVE. REPLACED RECEIVER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROW 3 WERE FOUND TO BE INOPERATIVE. REPLACED RECEIVER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WOULD NOT TEST AT ROWS 3 AND 8 AND 11. REPLACED BATTERY (P/N 86-2-1014-4)AT ROW 3, AND BATTERY AND RECEIVER (P/N 88-3-2003-1-2) AT ROWS 8 AND 11. LIGHTS OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
ANC - AFTER RECON AND PRIOR TO FLIGHT 22, THE EMERGENCY EXIT LIGHTS AT PALLET 8-6 WERE FOUND TO BE INOPERATIVE. RELEASED PER MEL 33-19B. MAINTENANCE SUBSEQUENTLY REPAIRED WIRING AND LIGHTS OPERATED NORMAL. (M)
Part: BATTERY — DISCHARGED (ROW 11)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHT RECEIVER AT ROW 11 WOULD NOT TEST. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (ROW 18)
ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROW 8 AND 18 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND RECEIVER AT ROW 8 AND BATTERY PACK AT ROW 18, ALL LIGHTS OPERATED NORMALLY. REFERENCE ASAA0010027. (M)
Part: BATTERY PACK — DISCHARGED (ROW 18)
ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT ROW 18 REMAINED ILLUMINATED. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
Part: RECEIVER — INOPERATIVE (ROW 8)
ANC - DURING MAINTENANCE CHECK, THE EMEREGNCY EXIT TRACK LIGHTS AT ROW 8 AND 18 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND RECEIVER AT ROW 8 AND BATTERY PACK AT ROW 18, ALL LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M)
Part: SEAT TRACK — DAMAGED (BS 639-727B)
SEA - DURING SCHEDULED C-CHECK, THE SEAT TRACK SUPPORT AT STATION 639 TO 727B, RBL 45.5 HAD FLOOR PANEL SCREW MARKS.. REPAIRED PER EA 5310-01787. (M)
Part: RIB — WORN (NR 2 ENGINE COWL)
SEA - DURING SCHEDULED C-CHECK, THE NR 2 ENGINE INBOARD COWL, 4TH RIB AFT, WAS FOUND WORN IN TWO PLACES. REPAIRED PER EA 5410-01044. (M)
Part: STRAP — CORRODED (BS 787)
SEA - DURING SCHEDULED C-CHECK, THE CARGO CEILING RETENTION STRAP WAS FOUND CORRODED STATIO N787 RBL 24. REPAIRED PER EA 5320-01397. (M)
Part: KEELBEAM — CORRODED (BS 720-727)
SEA - DURING SCHEDULED C-CHECK, THE RIGHT MLG WHEEL WELL KEEL BEAM WAS FOUND TO BE CORRODED ON THE UPPER FLANGE RIGHT SIDE STATION 720 TO 727. REPAIRED PER EA 5310-01786 AND BOEING TELEX ASA-SEA-00-00007H. (M)
Part: STRINGER — CORRODED (BS 760-767)
SEA - DURING SCHEDULED C-CHECK, STRINGER 27R AT BS 760 TO 767 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01793 AND BOEING TELEX ASA-SEA-00-00031H. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 14 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER AND BATTERY. LIGHTS OPERATED NORMALLY. (M)
Part: RECEIVER — INOPERATIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AT ROW 14 INOPERATIVE. REMOVED AND REPLACED REMOTE ASSEMBLY RECEIVER AND BATTERY. LIGHTS OPERATED NORMALLY. REF ASAA0110015. (M)
1999
Part: BATTERY — DISCHARGED (CABIN)
SEA - PRIOR TO FLT 65, THE SMOKE BARRIER EMERGENCY LIGHT WOULD NOT TEST. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (X)
Part: RECEIVER — INOPERATIVE (ROW 18)
ANC - DURING MAINTENANCE CHECK, THE BULKHEAD EMERGENCY EXIT TO REAR LIGHT AND THE EMERGENCY FLOOR TRACK LIGHTS AT ROW 18 WERE FOUND TO BE INOPERATIVE. REPLACED BULKHEAD AND ROW 18 RECEIVER AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (ROW 18)
ANC - PRIOR TO FLIGHT 21, THE EMERGENCY EXIT FLOOR TRACK LIGHTS NEAR ROW 18 ILLUMINATED. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
Part: LIGHT — INOPERATIVE (ROW 14)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 14. REPLACED LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT ON THE SMOKE BARRIER WAS FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHT ASSEMBLY, LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT ON THE SMOKE BARRIER WAS FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHT ASSEMBLY, LIGHTS OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (ROW 12)
ANC - DURING MAINTENANCE CHECK, 2 EACH EMERGENCY TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 12. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)
Part: turbine — FAILED (NR 1 engine)
ANC - ON TAKEOFF OF FLIGHT 7802, JUST AFTER REDUCING POWER FOR CLIMB CREW REPORTED THE NR 1 ENGINE POPPED AND WAS LOST. SHUTDOWN NR 1 ENGINE AND FOUND TURBINE BLADE DAMAGE. REPLACED NR 1 ENGINE. THE ENGINE WAS ROUTED TO AEROTHRUST CORP FOR INSPECTION AND REPAIR. AEROTHRUST DISASSEMBLED AND INSPECTED THE ENGINE. THE C-7, T-1, T-3, AND T-4 DISKS, ALONG WITH THE N2 SHAFT WERE REPLACED. THE ENGINE WAS THEN REASSEMBLED, TESTED, BOROSCOPE, AND RETURN TO ALASKA AIRLINES. (M)
Part: RECEIVER — INOPERATIVE (ROW 14)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS AT ROWS 12 AND 14 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AT ROW 12 AND RECEIVER AT ROW 14. LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (ROW 12)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS AT ROWS 12 AND 14 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AT ROW 12 AND RECEIVER AT ROW 14. LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (ROW 14)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 14 WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (NR 3 PALLET)
SEA - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS ON THE NR 3 PALLET WERE FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (ROW 10-11)
ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 10-11 WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING RECON, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE ON NR 1 SEAT PALLET. REPLACED BATTERY AND THE LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (ROW 3)
SEA - FLT 61 - AFTER RECON, THE EMERGENCY EXIT TRACK LIGHTS AT ROW 3 WOULD NOT EXTINGUISH. REPLACED BATTERY AND THE LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ANC - AFTER RECON, THE FORWARD EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED COLD SOAKED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY CHARGER — INOPERATIVE (CABIN)
ANC - PRIOR TO FLT 64, THE INTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY CHARGER AND LIGHTS OPERATED NORMALLY. (M)
Part: RECEIVER — INOPERATIVE (CABIN)
SEA - AFTER RECON AND PRIOR TO FLIGHT 61, SEVERAL EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED MID POSITION TRANSMITTER AND RECEIVER AT ROW 12, ALL LIGHTS OPERATE NORMALLY. (M)
Part: TRANSMITTER — INOPERATIVE (CABIN)
SEA - AFTER RECON AND PRIOR TO FLIGHT 61, SEVERAL EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED MID POSITION TRANSMITTER AND RECEIVER AT ROW 12, ALL LIGHTS OPERATE NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE OVERWING EXIT SIGNS WERE FLASHING WITH THE EMERGENCY LIGHTS ON. REPLACED BATTERY PACK AND THE LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ANC - AFTER RECON AND PRIOR TO FLIGHT 64, BOTH OVERWING EXIT LIGHT WERE FOUND TO BE INOPERATIVE. REPLACED THE BATTERY CHARGER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY CHARGER — INOPERATIVE (CABIN)
ANC - AFTER RECON AND PRIOR TO FLIGHT 64, BOTH OVERWING EXIT LIGHT WERE FOUND TO BE INOPERATIVE. REPLACED THE BATTERY CHARGER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (PALLET 5-3)
SEA - DURING MAINTENANCE CHECK, EMERGENCY EXIT TRACK LIGHTS AT PALLET 5-3 WERE FOUND INOPERATIVE. REPLACED BATTERY AND THE LIGHTS OPERATED NORMALLY. (X)
1998
Part: BATTERY PACK — DISCHARGED (OVERWING EXIT)
ANC - PRIOR TO FLIGHT 22, THE OVERWING EXIT LIGHTS WERE FLASHING. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
ANC - DURING MAINTENANCE CHECK, THE R2 DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (M)
Part: LIGHT — INOPERATIVE (ROW 18)
JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT AT ROW 18 WS FOUND INOPERATIVE. REPLACED LAMP HOLDER AND LENS. LIGHT OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
ANC - DURING AIRCRAFT RECON, THE SEAT PALLET FLOOR TRACK LIGHTS AT 6-11 AND SEAT PALLET LIGHTS AT 8-4 WERE FOUND TO BE INOPERATIVE. REPLACED RECEIVER ON 6-11 AND BATTERIES ON 6-11 AND 8-4, ALL LIGHTS OPERATED NORMALLY. (M)
Part: RECEIVER — INOPERATIVE (CABIN)
ANC - DURING AIRCRAFT RECON, THE SEAT PALLET FLOOR TRACK LIGHTS AT 6-11 AND SEAT PALLET LIGHTS AT 8-4 WERE FOUND TO BE INOPERATIVE. REPLACED RECEIVER ON 6-11 AND BATTERIES ON 6-11 AND 8-4, ALL LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (ROW 14)
ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS REMAINED ILLUMINATED AT ROW 14. REPLACED RECEIVER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. (M)
Part: RECEIVER — INOPERATIVE (ROW 14)
ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS REMAINED ILLUMINATED AT ROW 14. REPLACED RECEIVER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. (M)
Part: BATTERIES — DISCHARGED (CABIN)
ANC - PRIOR TO FLT 64, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 12 AND 14. REPLACED BATTERIES AT ROWS 12 AND 14, AND REPLACED RECEIVER AT ROW 12. EMERGENCY EXIT FLOOR TRACK LIGHTS OPERATED NORMALLY. (M)
Part: RECEIVER — INOPERATIVE (CABIN)
ANC - PRIOR TO FLT 64, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 12 AND 14. REPLACED BATTERIES AT ROWS 12 AND 14, AND REPLACED RECEIVER AT ROW 12. EMERGENCY EXIT FLOOR TRACK LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE DIM. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (M)
Part: LIGHT — INOPERATIVE (CABIN)
ANC - DURING MAINTENANCE CHECK, FOUND THE EMERGENCY EXIT LIGHT ABOVE THE AFT AIRSTAIRS INOPERATIVE. REPLACED LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
ANC - PRIOR TO FLT 30, THE EMERGENCY EXIT LIGHTS ON PALLET 8-2 WOULD NOT EXTINGUISH. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
ANC - DURING MAINTENANCE CHECK, THE NR 2 PALLET EMERGENCY EXIT TRACK LIGHTS WOULD NOT EXTINGUISH WHEN TURNED OFF. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)
Part: RECEIVER — INOPERATIVE (CABIN)
ANC - DURNG MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT NR 1 PALLET WOULD NOT EXTINGUISH. REPLACED NR 1 PALLET RECEIVER AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 10 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
1997
Part: BATTERY PACK — DISCHARGED (CABIN)
ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE ON SEAT PALLETT 4-3. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ANC - DURING RECON, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND INOPERATIVE AT SEAT PALLET 6-10. REPLACED BATTERY PACK AND LGIHTS OPERATED NORMALLY. (M)
Part: ALUMINUM FOIL — WORN (A/C COMP DOOR)
SEA - DURING C-CHECK, THE RIGHT A/C BAY DOOR ALUMINUM FOIL PLY WAS FOUND WORN AT VARIOUS LOCATIONS. REPAIRED PER EA 5240-01025 AND BOEING TELEX ASA-SEA-97-0443RR. (M)
Part: DOOR — GOUGED (LT MLG)
SEA - DURING C-CHECK, THE LT MLG DOOR WAS FOUND DAMAGED FROM THE LT MLG ACTUATOR ATTACH BOLT HEAD. REPAIRED PER EA 3210-01062 AND BOEING TELEX ASA-SEA-0047RR. (M)
Part: FLOORBEAM — CORRODED (BS 259)
SEA - DURING C-CHECK, FOUND CORROION ON THE AFT FLANGE UPPER SURFACE OF THE FLOORBEAM, AROUND THE NUTPLATE HOLES. REPAIRED PER EA 5310-01555 AND BOEING TELEX ASA-SEA-97-0432. (M)
Part: ANGLE — CORRODED (BS 692)
SEA - DURING C-CHECK, FOUND CORROSION ON THE KEEL BEAM LOWER CHORD AT RBL 6.3 ON THE LOWER SURFACE OF THE LOWER CHORD OUTBOARD LEG IN THE AREA OF THE EXISTING ATTACH HOLE AT STATION 692. REPAIRED PER EA 5310-01557 AND BOEING TELEX ASA-SEA-97-0437. (M)
Part: SKIN — CORRODED (BS 303-348)
SEA - DURING C-CHECK, FOUND CORROSION ON THE EXTERIOR SURFACE OF THE SKIN BELOW THE L1 ENTRY DOOR. REPAIRED PER EA 5330-01265 AND BOEING TELEX ASA-SEA-96-0429RR. (M)
Part: TAILPIPE — DENTED (NR 2 ENGINE)
SEA - DURING C-CHECK A DENT WAS FOUND IN THE NR 2 ENGINE OUTBOARD AFT TAIL PIPE COWLING. REPAIRED PER EA 5410-01022. (M)
Part: TRACK — GOUGED (NR 4 LE SLAT)
SEA - DURING C-CHECK, THE NR 4 SLAT INBOARD AUXILIARY TRACK AT STATION 41.29 WAS FOUND GOUGED. REPAIRED PER EA 5740-01130 AND BOEING TELEX ASA-SEA-97-0436RR. (M)
Part: RIB — CHAFED (ELEVATOR)
SEA - DURING C-CHECK, WEAR WAS FOUND AT THE HORIZONTAL STABILIZER TRAILING EDGE RIBS AT STATION 66.54, 94.07, AND 121.9. REPAIRED PER EA 5510-01066 AND BOEING TELEX ASA-SEA-91-0202RR. (M)
Part: ANGLE — WORN (VERT STABLE)
SEA - DURING C-CHECK, THE RIGHT VERTICAL FIN SKATE ANGLE WAS FOUND TO BE WORN. REPAIRED PER EA 5530-01041. (M)
Part: CHANNEL — CRACKED (RT MLG DOOR)
SEA - DURING C-CHECK, TWO CRACKS WERE FOUND IN THE RADIUS OF THE RT MLG CENTER DOOR CHANNEL ADJACENT TO THE CUTOUT FOR THE HINGE. REPAIRED PER EA 3210-01063. (M)
Part: DOOR — GOUGED (RT MLG)
SEA - DURING C-CHECK, THE RT MLG DOOR WAS FOUND DAMAGED FROM THE RT MLG ACTUATOR ATTACH BOLT HEAD. REPAIRED PER EA 3210-01062 AND BOEING TELEX ASA-SEA-0047RR. (M)
Part: A/C COMT DOOR — WORN (ALUMINUM FOIL)
SEA - DURING C-CHECK, THE LEFT A/C BAY DOOR ALUMINUM FOIL PLY WAS FOUND WORN AT VARIOUS LOCATIONS. REPAIRED PER EA 5240-01025 AND BOEING TELEX ASA-SEA-97-0443RR. (M)
Part: FITTING — CORRODED (LT HORIZ STAB)
SEA - DURING C-CHECK, THE LEFT HORIZONTAL STABILIZER NR 6 HINGE FITTING LUG HOLES WERE FOUND TO BE CORRODED AND WORN. REPAIRED PER EA 2740-01031 AND BOEING TELEX ASA-SEA-97-0438. (M)
Part: TAILCONE — DELAMINATED (AFT FUSELAGE)
SEA - DURING C-CHECK, THE TAILCONE WAS FOUND TO HAVE A SOFT SPOT DELAMINATED. REPAIRED PER EA 5350-01050 AND BOEING TELEX ASA-SEA-97-0431RR. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ANC - DURING MAINTENANCE CHECK, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED RIGHT OVERWING EMERGENCY EXIT BATTERY PACK AND LIGHT OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ANC - DURING MAINTENANCE CHECK, THE RIGHT AFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED RIGHT AFT OVERWING EMERGENCY EXIT BATTERY PACK AND LIGHT OPERATED NORMALLY. (M)
Part: ACTUATOR — FAILED (NR 2 SPOILER)
ANC - AFTER TAKEOFF FLT 30, CREW REPORTED REQUIRED 30 DEG RT CONTROL WHEEL DEFLECTION TO MAINTAIN WINGS LEVEL. FOUND NR 2 FLIGHT SPOILER STUCK HALF WAY UP. REPLACED ACTUATOR AND SPOILER OPERATED NORMALLY. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE RIGHT WING AND BODY FILLET EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE POWER SUPPLY AND THE LIGHTS OPERATED NORMALLY. (M)
Part: WIRE — BROKEN (CABIN)
ANC - DURING MAINTENANCE CHECK, THE SEAT PALLET EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 18. FOUND WIRE BROKEN AT SOCKET. REMOVED SEAT PALLET FROM AIRCRAFT TO FACILITATE REPAIR TO WIRE. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE CABIN SMOKE BARRIER 'EXIT TO REAR' EMERGENCY SIGN LIGHTS WERE FOUND TO BE VERY DIM. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - FLT 9300 - CREW REPORTED, AFT EMERGENCY EXIT FLOOR TRACK LIGHTS REMAINED ON AFTER TEST. REPLACED BATTERY PACK AT ROW 14 AND LIGHTS OPERATED NORMALLY. (M)
1996
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTING AT ROWS 10-11 WOULD NOT EXTINGUISH. REPLACED RECEIVER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. (M)
Part: RECEIVER — INOPERATIVE (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTING AT ROWS 10-11 WOULD NOT EXTINGUISH. REPLACED RECEIVER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. REFERENCE ASAA9610142.
Part: BATTERY — DISCHARGED (CABIN)
ANC - FLT 54 - ONE SECTION OF MID CABIN EMERGENCY EXIT FLOOR TRACK LIGHTS ILLUMINATED DURING FLIGHT. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 16 AND 17. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 2. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M)
Part: KEEL BEAM — CRACKED (BS 540)
SEA - DURING D-CHECK, A CRACK WAS IDENTIFIED ON THE HORIZONTAL FLANGE OF THE KEEL BEAM CHORD AT BS 540, RBL 6.30. REPAIRED PER EA 5310-01479 AND BOEING TELEX ASA-SEA-96-0404RR. (M)
Part: FLOOR BEAM — CRACKED (BS 520)
SEA - DURING D-CHECK, BS 520 LBL 24.75 FLOOR BEAM UPPER CHORD WAS FOUND CRACKED IN RADIUS. REPAIRED PER EA 5310-01485 AND BOEING TELEX ASA-SEA-96-0392RR. (M)
Part: FLOOR BEAM — CORRODED (BS 549-727)
SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE LEFT FLANGE OF THE LONGITUDINAL FLOOR BEAM AT RBL 45, BETWEEN BS 549 AND 727A. REPAIRED PER EA 5310-01489 AND BOEING TELEX ASA-SEA-96-0400RR. (M)
Part: FLOOR BEAM — CORROSION (BS 520)
SEA - DURING D-CHECK, THE FLOOR BEAM FORWARD FLANGE AT BS 520, LBL 35 TO LBL 43 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01487 AND BOEING TELEX ASA-SEA-96-0392RR. (M)
Part: FLOOR BEAM — CORROSION (BS 787)
SEA - DURING D-CHECK, THE FLOOR BEAM LOWER FORWARD FLANGE AT BS 787, LBL 25 AND RBL 3 WERE FOUND TO BE CORRODED. REPAIRED PER EA 5310-01484 AND BOEING TELEX ASA-SEA-96-0390RR. (M)
Part: FLOOR BEAM — CORROSION (BS 520)
SEA - DURING D-CHECK, THE FLOOR BEAM FORWARD LOWER FLANGE AT BS 520, LBL 40 TO LBL 45 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01487 AND BOEING TELEX ASA-SEA-96-0392RR. (M)
Part: FLOOR BEAM — CRACKED (BS 520)
SEA - DURING D-CHECK, BS 520 RBL 24.75 FLOOR BEAM UPPER CHORD WAS FOUND CRACKED IN RADIUS. REPAIRED PER EA 5310-01485 AND BOEING TELEX ASA-SEA-96-0392RR. (M)
Part: FLOOR BEAM — CORRODED (BS 500B)
SEA - DURING D-CHECK, THE LOWER FORWARD FLANGE OF THE FLOOR BEAM AT BS 500B, LBL 35 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01464 AND BOEING TELEX ASA-SEA-96-0340RR. (M)
Part: FLOOR BEAM — CORRODED (BS 867)
SEA - DURING D-CHECK, THE LOWER FORWARD FLANGE OF THE FLOOR BEAM AT BS 867, LBL 23 TO RBL 46 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01477 AND BOEING TELEX ASA-SEA-96-0354RR. (M)
Part: FLOOR BEAM — CORRODED (BS 767)
SEA - DURING D-CHECK, THE LOWER FORWARD FLANGE OF THE FLOOR BEAM AT BS 767, RBL 24 TO 30 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01465 AND BOEING TELEX ASA-SEA-96-0339RR. (M)
Part: FLOOR BEAM — CORRODED (BS 420)
SEA - DURING D-CHECK, THE FORWARD UPPER HORIZONTAL FLANGE OF THE FLOOR BEAM AT BS 420, LBL 46 TO 58 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01474 AND BOEING TELEX ASA-SEA-96-0372RR. (M)
Part: FLOOR BEAM — CORRODED (BS 420)
SEA - DURING D-CHECK, THE FORWARD LOWER HORIZONTAL FLANGE OF THE FLOOR BEAM AT BS 420, LBL 5.25 TO 46 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01480 AND BOEING TELEX ASA-SEA-96-0379RR. (M)
Part: FLOOR BEAM — CORRODED (BS 420)
SEA - DURING D-CHECK, THE UPPER FORWARD FLANGE OF THE FLOOR BEAM AT BS 500A, LBL 25 TO 43 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01472 AND BOEING TELEX ASA-SEA-96-0353RR. (M)
Part: DOOR BEAM — CRACKED (BS 465.5)
SEA - DURING D-CHECK, THE MAIN CARGO DOOR UPPER BEAM AFT END WAS FOUND TO HAVE A 1.3 INCH CRACK. REPAIRED PER EA 5230-01062 AND BOEING TELEX ASA-SEA-96-0302RR. (M)
Part: FLOOR BEAM — CORRODED (BS 400)
SEA - DURING D-CHECK, THE AFT LOWER HORIZONTAL FLANGE OF THE FLOOR BEAM AT BS400, LBL 55 TO 65 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01475 AND BOEING TELEX ASA-SEA-96-0374RR. (M)
Part: FLOOR BEAM — CORRODED (BS 1016)
SEA - DURING D-CHECK, THE UPPER FORWARD FLANGE OF THE FLOOR BEAM AT BS 1016, RBL 30 TO 40 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01481 AND BOEING TELEX ASA-SEA-96-0378RR. (M)
Part: SKIN — CRACKED (BS 360)
SEA - DURING D-CHECK, A 1.5 INCH CRACK WAS FOUND IN THE SKIN AT THE ELECTRONICS COMPARTMENT COOLING DUCT CUTOUT. REPAIRED PER EA 5330-01261 AND BOEING SERVICE BULLETIN 737-53-1117 REV 1. (M)
Part: FLOOR BEAM — CORRODED (BS 500)
SEA - DURING D-CHECK, THE LOWER FORWARD FLANGE OF THE FLOOR BEAM AT BS 500, LBL 5 TO 48 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01463 AND BOEING TELEX ASA-SEA-96-042RR. (M)
Part: FLOOR BEAM — CORRODED (BS 500)
SEA - DURING D-CHECK, THE UPPER FORWARD FLANGE OF THE FLOOR BEAM BS 500A, LBL 42 TO RBL 43 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01471 AND BOEING TELEX ASA-SEA-96-0355RR. (M)
Part: FLOOR BEAM — CORRODED (BS 887)
SEA - DURING D-CHECK, THE UPPER AFT FLANGE OF THE FLOOR BEAM BS 887, RBL 4 TO LBL 51 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01468 AND BOEING TELEX ASA-SEA-96-0348RR. (M)
Part: FLOOR BEAM — CORRODED (BS 967)
SEA - DURING D-CHECK, A PREVIOUS REPAIR OF THE UPPER FORWARD FLANGE OF THE FLOOR BEAM BS 967 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01457 AND BOEING TELEX ASA-SEA-94-0307RR. (M)
Part: FLOOR BEAM — CORRODED (BS 480)
SEA - DURING D-CHECK, THE LOWER FORWARD FLANGE OF THE FLOOR BEAM BS 480, LBL 42 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01461 AND BOEING TELEX ASA-SEA-96-0332RR. (M)
Part: FLOOR BEAM — CORRODED (BS 440)
SEA - DURING D-CHECK, THE LOWER FORWARD FLANGE OF THE FLOOR BEAM BS 440, LBL 42.75 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01460 AND BOEING TELEX ASA-SEA-96-0327RR. (M)
Part: STRINGER — CRACKED (BS 500)
SEA - DURING D-CHECK, A CRACK WAS IDENTIFIED AT THE ENDS OF STRINGER 16R, BS 500B, WHICH TERMINATES AT THE RIGHT WING LEADING EDGE LIGHT. REPAIRED PER EA 5310-1456 AND BOEING SERVICE BULLETIN 737-53-1145. (M)
Part: FLOOR BEAM — CORRODED (BS 460)
SEA - DURING D-CHECK, THE LOWER FLANGE OF THE FLOOR BEAM BS 460, LBL 42.5 WAS FOUND TO BE CORRODED. REPARIED PER EA 5310-01459 AND BOEING TELEX ASA-SEA-96-0326RR. (M)
Part: FLOOR BEAM — CORRODED (BS 328)
SEA - DURING D-CHECK, THE UPPER CHORD FLANGE OF STATION 328 FLOOR BEAM (CABIN) WAS FOUND CORRODED. REPLACED CHORD AND SPLICED AT LBL 33 PER EA 5310-01454 AND BOEING TELEX ASA-SEA-94-0292RR. (M)
Part: SOCKET — MISSING (CARGO COMPT)
ANC - DURING MAINTENANCE CHECK, ONE EMERGENCY EXIT LIGHT SOCKET WAS FOUND MISSING PALLET 9-6. REPLACED SOCKET AND LIGHTS OPERATED NORMALLY. (M)
Part: DOOR — OUT OF ADJUST (L1 DOOR)
SEA - FLT NR 64 - L1 DOOR DIFFICULT TO OPEN AND CLOSE. ADJUSTED UPPER HINGE GUIDE ARM, LUBRICATED UPPER AND LOWER HINGE FITTINGS AND ALL LATCH CAM ROLLERS. DOOR OPERATED NORMALLY. (M)
Part: NLG MODULE — DEFECTIVE (NLG)
OTZ - FLT NR 52 - ON DEPARTURE FROM OTZ, NOSE LANDING GEAR WOULD NOT RETRACT. SLOWED TO 140 KNOTS, CYCLED GEAR AND NOSE GEAR CAME UP. NORMAL INDICATION FOR REMAINDER OF FLIGHT AND AIRCRAFT LANDED IN ANC WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR MODULE, COMPLETED GEAR SWING AND GEAR OPERATED NORMALLY. (M)
Part: BATTERY — DISCHARGED (CABIN)
SEA - DURING CREW PREFLIGHT, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS ILLUMINATED AT ROW 18. REMOVED AND REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (W)
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CEHCK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE ROW 2 (PALLET 1-7). REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
Part: WIRE — DISCONNECTED (CABIN)
SEA - DURING MAINTENANCE CHECK, TWO WHITE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN THE AFT CABIN. REPAIRED FLOOR TRACK WIRING AND LIGHTS OPERATED NORMALLY. (M)
Part: RECEIVER — DEFECTIVE (CABIN)
ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 18 WOULD NOT EXTINGUISH. REPLACED EMERGENCY EXIT LIGHT RECEIVER AT ROW 18 AND LIGHTS OPERATED NORMALLY. (M)
Part: COFFEE MAKER — SMOKING (AFT GALLEY)
ANC - FLT NR 23 - CREW REPORTED, AFT GALLEY COFFEE MAKER STARTED SMOKING. TURNED OFF GALLEY POWER AND SMOKE SUBSIDED. REPLACED AFT GALLEY COFFEE MAKER AND OPERATED NORMALLY, NO ODORS DETECTED. (M)
1995
Part: BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 14 AND 15 REMAINED ILLUMINATED. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X)
Part: OVEN — DEFECTIVE (NR 1 GALLEY)
ANC - ON ARRIVAL OF FLIGHT 58, CREW REPORTED A STRONG ELECTRICAL ODOR EMINATED FROM OVEN IN FORWARD GALLEY WHILE IN USE. ODOR DISSIPATED WHEN GALLEY POWER TURNED OFF. REMOVED AND REPLACED DOUBLE OVEN IN NR 1 GALLEY AND OPERATED NORMALLY WITH NO ODORS NOTED. (M)
Part: FLOOR BEAM — CORRODED (BS 520)
SEA- DURING C-CHECK, CORROSION WAS FOUND ON THE UPPER FORWARD FLANGE OF THE FLOOR BEAM AT BS 520, RBL 9.50, 15.375 AND 20. PERFORMED INTERIM REPAIR PER EA 5310-01371 AND BOEING TELEX ASA-SEA-95-0440RR. (M)
Part: FLOORBEAM — CORRODED (BS 727B)
SEA - DURING C-CHECK, CORROSION WAS FOUND ON THE UPPER FORWARD FLANGE OF THE FLOORBEAM AT BS 727B AT LBL 4.00. PERFORMED INTERIM REPAIR PER EA 5310-01365 AND BOEING TELEX ASA-SEA 950429RR. (W)
Part: FLOORBEAM — CORRODED (BS 328)
SEA - DURING C-CHECK, CORROSION WAS FOUND ON THE UPPER CHORD FLANGE OF THE FLOORBEAM AT BS 328 BETWEEN RBL 14.5 TO 60. PERFORMED INTERIM REPAIR PER EA 5310-1367 AND BOEING TELEX ASA-SEA 95-0438RR. (W)
Part: GOVERNOR — DEFECTIVE (AFT AIRSTAIR)
SEA - DURING C-CHECK, THE AFT AIRSTAIR FAILED THE EMERGENCY EXTENSION TIME CHECK. REPLACED CENTRIFUGAL GOVERNOR AND OPERATED WITHIN EMERGENCY EXTENSION TIME LIMITS. (W)
Part: DOOR SEAL — MISSING (CARGO DOOR)
ANC - FLT NR 126 - CREW REPORTED LOSS OF PRESSURIZATION DURING CRUISE, PASSENGER OXYGEN MASKS AUTOMATICALLY DEPLOYED. CREW DESCENDED AIRCRAFT TO 10,000 FEET AND SUBSEQUENTLY LANDED WITHOUT INCIDENT. FOUND A LARGE SECTION OF THE AFT LOWER CARGO DOOR SEAL MISSING. REPLACED SEAL, RESTOWED OXYGEN MASKS, PRESSURIZED AIRCRAFT AND OPERATED NORMALLY. (M)
Part: EEL BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE BULKHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (M)
Part: EEL BATTERY PACK — DISCHARGED (CABIN)
SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHTS AT ROW 14 WERE FOUND ON AND REMAINED ON AFTER RESETTING. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
Part: EEL BATTERY PACK — DISCHARGED (CABIN)
ANC - DURING MAINTENANCE CHECK, THE SEAT PALLET EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M)
Part: ROD — OUT OF ADJUST (L1 DOOR)
SEA - FLT 61 - PRIOR TO DEPARTURE, THE CREW REPORTED L1 DOOR WAS DIFFICULT TO CLOSE. ADJUSTED UPPER DOOR HINGE ROD AND DOOR OPERATED NORMALLY. (W)
Part: FAN — INOPERATIVE (AIR COND SYS)
JNU - ON ARRIVAL OF FLIGHT 66 - CREW REPORTED, BURNING ODOR IN COCKPIT AND AIR CONDITIONING FAN CIRCUIT BREAKER TRIPPED. ODOR DISSIPATED. RELEASED PER MINIMUM EQUIPMENT LIST ITEM 21-30. SUBSEQUENTLY CONFIRMED ABNORMAL NOISE AND A BURNING ODOR WHEN FAN WAS OPERATED. REPLACED AIR CONDITIONING FAN AND OPERATED NORMALLY. (M)