N609AS
Registered owner: ALASKA AIRLINES INC, WA (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
L1 DOOR BINDING WHILE CLOSING. GROUNDED - YES. PERFORMED L-1 DOOR ADJUSTMENT AND SYSTEM TEST, FINAL DOOR TORQUE WITHIN LIMITS, OPENING TORQUE 300INLBS, CLOSING TORQUE 578 INLBS. IAW AMM 52-11-00-820-801, AMM 52-11-00-700-804.
AFT CARGO PIT DOOR INTERNAL SKIN CORRODED @ BLANKET RETAINER STUD JUST AFT OF FWD HINGE ARM. REMOVED MAJORITY OF CORROSION. THICKNESS OF MATERIAL REMAINING LESS THAN 50% AND IS OUT OF ALLOWABLE LIMITS REF SRM 52-30-01/0101 FIGURE 104. GROUNDED - YES. REMOVED AND REPLACED INNER SKIN P/N 146A6114-1, 146A6110, EA CMPT-52EA-30289 REV 00 AND SRM B737-700 SRM 451-40-02-OG-0. THIS CLOSES OUT MCT. SEAMC CHRIS NOTIFIED. SRXR430X.
FA REPORTED L1 DOOR VERY DIFFICULT TO OPERATE DOOR HANDLE. GROUNDED - YES. ATTEMPTED GUIDE ARM ADJUSTMENT IAW AMM 52-11-00, NO HELP. REMOVED FWD ENTRY DOOR LINING IAW AMM 52-11-31. ADJUSTED HORIZONTAL ADJUSTMENT ROD. ADJUSTED BOTH TOP & BOTTOM GATE DOORS. ADJUSTED ALL DOOR STOPS & PROPER ADJUSTMENT. IAW AMM 52-11-00-820-801.
EXTERIOR EMERGENCY EXIT LIGHTS AFT OF THE WING ARE INOPERATIVE ON BOTH SIDES. GROUNDED - YES. TRANSFERRED ITEM TO MIG-5 S/N OK448557 ITEM #7 OF MIG-85 INFO ONLY RELAMPED LT & RT SLIDE LIGHT IAW AMM 33-51-04-960-801. OPS CHECKED GOOD.
R1 DOOR EMERGENCY EXIT LIGHTS FAILED OPS CHECK. GROUNDED - YES. REMOVED AND REPLACED WITH SERVIEABLE BATTERY OPS CHECK GOOD IAW B737-700 AMM 33-51-06-960-805. (S/N 425489)
UPON REMOVAL OF AFT PIT SIDEWALL PANEL FOUND L/H TRANSITION TO HAVE CORROSION AT BS 727-767. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO L/H TRANSITION PANEL FROM STA727 TO STA 767 IAW SRM 51-40-02-OG-OW= 1/2" O= .040 R= 0 L= 1/4" D= .040.
UPON REMOVAL OF SIDEWALL PANEL FOUND CORROSION ON SHIELD IN AFT PIT. GROUNDED - YES. REMOVED AND REMPLACED SHIELD IN AFT PIT IAW B737-700 SRM 51-40-02-OG-OW: 2 O: 0.050 R: 0.025 L: 2 D: 0.025.
UPON REMOVAL OF AFT PIT SIDEWALL PANEL FOUND CORROSION ON RT TRANSITION PANEL BS 727 - 767. GROUNDED - YES. REMOVED AND REPLACED AFT PIT SIDEWALL PANEL ON RT TRANSITION IAW SRM 51-40-02-0G-0. W: .150 0: .040" R: 0" L: 1 D: .040".
R1 DOOR HANDLE BOX BEAM IS CRACKED. GROUNDED - YES. REMOVED & REPLACED HANDLE BOX BEAM IAW SRM 51-40-02-0G-0.
FWD PIT TRANSITION PANEL RT SIDE HAS SPOTS OF CORROSION FROM BS 500A - 500D. GROUNDED - YES. REMOVED AND REPLACED FWD PIT TRANSITION PANEL IAW SRM 51-40-02-0G-0, W= 1" O= .040" R= .025" L= 1" D= .015".
AFT CARGO PIT LOWER SILL WEB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO BIT LOWER SILL WEB IAW B737-700 SRM 51-40-02-OG-OW: .045 O: 1 R: .038 L: 2 D: .007.
FWD PIT TRANSITION PANEL HAS CORROSION BETWEEN BS 500 - 500D. GROUNDED - YES. REMOVED AND REPLACED FWD LT TRANSITION PANEL IAW SRM 51-40-02-0G-0. W:1 0:.040' R:.034 L:1 D:.006.
FWD PIT AFT BULKHEAD LOWER SUPPORT FRAME HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED FWD PIT AFT BULKHEAD LOWER SUPPORT FRAME IAW SRM 51-40-02-OG-OW:.700 O:.071 R:.050 L:.750 D:.021.
DENT ON BELLY SKIN AT STATION 400. GROUNDED - YES. (RESOLVED ON W/O: 2071370 TASKCARD: N/R-00026 ) ACCOMPLISHED REPAIR IAW EA 700-53EA-29631.
FA REPORTS L1 DOOR DIFFICULT TO CLOSE. GROUNDED - YES. FA REPORTS L1 DOOR HANDLE BINDING WHEN TRYING TO CLOSE. PERFORMED L1 FWD DOOR SYSTEM TEST REF AMM 52-11-00-700-804 L1 DOOR FAILS DOOR CLOSE TORQUE. WILL NOT CLOSE AT 1000 IN LB OF FORCE. L1 DOOR BINDING DUE TO LACK OF GREASE, GREASED L1 DOOR REF AMM 12-25-11-640-801 & ACCOMPLISHED DOOR SYSTEM TEST TESTED GOOD. DOOR OPERATES SMOOTHLY NO BINDING CLOSES AT 600 IN POUNDS. REF AMM 52-11-00-700-804.
L-1 DOOR VERY HARD TO UNLATCH / OPEN FROM THE EXTERIOR. GROUNDED - YES. (RESOLVED ON W/O: 2055375 TASKCARD: N/R-00001 ) REMOVED L1 DOOR LINER REF AMM 52-11-31. ADJUSTED GUIDE ARM REF 52-11-00 AMM. ADJUSTED HORIZONTAL CONTROL ARM REF AMM 52-11-00. AIRCRAFT NEEDS TO BE PUT BACK INTO USUAL CONDITION. 1092780 06/04/2025 RII 1048815 06/04/2025. FOUND L1 DOOR STILL HARD TO OPEN, PERFORMED UPPER AND LOWER GATE ADJUSTMENT REF AMM 52-11-00. REINSTALLED L1 DOOR LINER REF AMM 52-11-31. L1 DOOR NOW OPENS SATISFACTORY. REINSTALLED L1 DOOR ESCAPE SLIDE REF AMM 25-66-01. THIS CLEARS MCT DEFERRAL SEAMC WILL NOTIFIED.
FLEET SERVICE REPORTED L1 DOOR HARD TO OPEN. GROUNDED - YES. L1 DOOR ROD END REMOVED AND NEW INSTALLED ON GUIDE ARM. DOOR LINER REMOVED AND SLIDE REMOVED. HORIZONTAL ROD END ADJUSTED A HALF A TURN AWAY FROM MYSELF - SMALL IMPROVEMENT BUT OVERALL NO HELP. REMOVED UPPER GATE ROD - NO HELP AND NO ADJUSTMENT MADE. REINSTALLED UPPER GATE ROD REF AMM 52-11-31, 52-11-21 AND 52-11-00. ADJUSTED GUIDE ARM 3/4 TURN CLOCKWISE REF AMM 52-11-00-820-801 PERFORMED LATCH/UNLATCH TORQUE CHECK REF AMM 52-11-00-700-804 PASSES TORQUE CHECK. INSTALLED FORWARD ENTRY DOOR LINING REF AMM 52-11-31-400-802 THIS CLEARS MCT.
ROWS 9,15,18 AND RH EMERGENCY LIGHTS INOP. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY PACK M1669 S/N 335883 IAW B 737 AMM 33-51-06-960-805 AND PERFORMED OPS CHECK IAW B737 AMM 33-51-06-960-805 TEST GOOD.
FA REPORTS L1 DOOR DIFFICULT TO CLOSE. GROUNDED - YES. OPERATED L1 DOOR NO DEFECTS NOTED. SUSPECT COLD WEATHER IN SCC MADE DOOR HARD TO CLOSE. CLEANED AND LUBED L1 DOOR COMPONENTS REF AMM 12-25-11. L1 DOOR OPERATES NORMALLY.
FLIGHT ATTENDANT REPORTS PLASTIC EXIT COVER BROKEN IN FORWARD FLIGHT ATTENDANT JUMPSEAT AREA. GROUNDED - YES. REPLACED THE EXIT COVER PLACARD IN THE FORWARD FLIGHT ATTENDANT JUMP SEAT AREA, REF AMM 33-51-01.
CREW REPORTS L1 DOOR HARD TO OPEN AND CLOSE. GROUNDED - YES. FOUND L1 DOOR HARD TO CLOSE FROM OUTSIDE. PREVIOUS FLT HAD SAME ISSUE. PERFORMED ADJUSTMENT OF GUIDE ARM AND HORIZONTAL CONTROL ROD IAW 52-11-00 DOOR OPEN AND CLOSE TEST WITHIN LIMITS IAW 52-11-00.
L1 DOOR EMERG EXIT LENS BROKEN. GROUNDED - YES. RELAMPED L1 DOOR EMERG EXIT LIGHT REF AMM 33-51-01.
FA'S REPORTED A PUNGENT ODOR ON RECENT THROUGH APPROACH. ODOR WENT AWAY WHEN WE LANDED FA'S SAY IT WAS LEVEL 1 SEVERITY LEVEL. FWD CABIN, A FLIGHT ATTENDANT MID CABIN AND AFT. NO SMELL IN COCKPIT. GROUNDED - YES. REMOVED AND REPLACED AIR RE-CIRCULATION HEPA FILTER REF. AMM 21-25-01 AND THE WATER COALESCER BAG REF. AMM 21-51-05. OPS CHECK AND LEAK GOOD. NO UNUSUAL ODOR PRESENT.
EXTERIOR LH SIDE EMERGENCY LIGHT IS INOP. LIGHT POSITION IS AFT/INBOARD OF LH WING REF B737-700 AMM 33-51-04. GROUNDED - YES. CHARGED EMERGENCY BATTERY AND CYCLED POWER REF B737-700 AMM 33-51-04.
FLIGHT DECK EMERGENCY DOME LIGHT INOP. GROUNDED - YES. RELAMPED. OP CK NORMAL.
#8 SLAT NOSE BEAM CRACKED AT 3EA FASTENER HOLES AT SLAT STA 451.42. GROUNDED - YES. REPAIRED #8 SLAT IAW B737-700 SRM 57-42-02-2R-4.
AFT PIT CARGO TRACK AT RBL 13.80 HAS AREAS OF CORROSION BETWEEN STA 937 TO STA 947. GROUNDED - YES. REPAIRED CARGO TRACK SECTION IAW B737-700 SRM 53-00-53-2R-3.W= 1." O= .075" R= .060" L= 4." D= .015".
AFT CARGO, BS 947 BOTH FLOOR LUGS HAS CORROSION. GROUNDED - YES. BLENDED CORROSION ON CARGO TRACKS REMAINING MATERIAL FOUND OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-2, REPAIRED TRACK A- LBL 3.8 IAW B737-700 SRM 53-00-53-2R-3. MIG 5 GENERATED RBL 13.8 REPAIRED ON WO 1020805-1000-0082 OK327973.W= 1." O= .075" R= .058" L= 4." D= .017".
STA 947.5 HAS CORROSION AT I/B AND O/B LAV ATTACH POINTS. GROUNDED - YES. REPAIRED FLOOR BEAM STA 947.5 IAW 737-700 SRM 53-70-51-2R-5 REPAIR 5.W= 2" O= .180 R= 0.000 L= 67.5" D= .180.
AFT CARGO SHIELD FWD OF DOOR HAS CORROSION. GROUNDED - YES. REMOVED & REPLACED SHIELD ON AFT CARGO FWD OF DOOR IAW B737-700 SRM 51-40-02-0G-0.W= 1" O= .050" R= .040" L= 2." D= .010".
LH TRANSISION IN AFT PIT HAS AREAS OF CORROSION FROM FS 727B TI0787. GROUNDED - YES. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS, REPAIRED L/H TRANSITION PNL IAW B737-700 SRM 53-00-53-2R-6.W= 2" O= .040 R= 0 L= 2" D= 100%.
RH TRANSISION HAS AREAS OF CORROSION FROM FS 727B TO 767. GROUNDED - YES. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS, REPAIRED TRANSITION IAW B737-700 SRM 53-00-53-2R-6.W= 2" O= .040 R= 0 L= 2" D= 100%.
R/H HORIZONTAL LOWER SKIN CRACKED AT STA 167, 24 INCHES FWD OF REAR SPAR. GROUNDED - YES. REPAIRED LOWER SKIN ON RH HOR. STAB. IAW B737-700 SRM 55-10-01-2R-11.
#8 SLAT LOWER SKIN 3 EA FASTENERS PULLING THROUGH SKIN WITH POSSIBLE CRACK INDICATION, MULTIPLE OTHER FASTENERS ALSO APPEAR TO BE LOOSE AND SMOKING AROUND ACTATOR ATTACH POINT. GROUNDED - YES. REPAIRED #8 SLAT LOWER SKIN IAW B737-700 SRM 57-42-01-2R-8 ALT. 1.
EMERGENCY LIGHTS IN AFT GALLEY AREA ARE INOP. GROUNDED - YES. REMOVED S/N 117141 AND S/N 85867. REPLACED WITH WORKING BATTERY PACKS.
AFT R/H EXIT SIGN LIGHTS OUT. GROUNDED - YES. RELAMPED IAW B737-700 AMM 33-51-01. OPS GOOD.
LH #3 EMERGENCY LIGHT INOP. GROUNDED - YES. RELAMPED LH#3 EMERGENCY LIGHT. OPS NORMAL.
DURING T/C 78233008 ACCOPLISHMENT, FOUND L/H OVERWING ER LIGHT NOT ILLUMINATED. GROUNDED - YES. REPLACED LAMP. OPS CHECK GOOD.
UPPER FUSELAGE FRAME IS CRACKED AT STA 727D & STR 8RT FLAGGED. GROUNDED - YES. REPAIRED LT FRAME STA 727D IAW ALASKA TC AD20090102-700-25-1R STEP 51.
UPPER FUSELAGE FRAME IS CRACKED AT STA 727D & STR 8 LT FLAGGED. GROUNDED - YES. REPAIRED FRAME IAW ASA TC AD20090102-700-25-1L.
UPPER FUSELAGE FRAME AT STA 400 CRACKED AT STR 8 L/H. GROUNDED - YES. REPAIRED FRAME IAW ASA TC AD20090102-700-25-1L.
UPPER FUSELAGE FRAME IS CRACKED AT STA 827 & STR 8 R/H. GROUNDED - YES. REPAIRED R/H FRAME STA 827 IAW ALASKA TC AD20090102-700-25-1R STEP 63.
UPPER FUSELAGE FRAME IS CRACKED AT STA 500A & STR 8 R/H. GROUNDED - YES. REPAIRED FRAME IAW ASA TC AD20090102-700-25-1R.
UPPER FUSELAGE FRAME IS CRACKED AT STA 500C & STR 8 R/H. GROUNDED - YES. REPAIRED FRAME IAW ASA TC AD20090102-700-25-1R.
UPPER FUSELAGE FRAME IS CRACKED AT STA 380 & STR 8 R/H. GROUNDED - YES. REPAIRED FRAME IAW ASA TC AD20090102-700-25-1R.
UPPER FUSELAGE FRAME IS CRACKED AT STA 787 & STR 8L/H. GROUNDED - YES. REPAIRED FRAME IAW ASA TC AD20090102-700-25-1L.
UPPER FUSELAGE FRAME CRACKED AT STA 500A & STR 8 L/H. GROUNDED - YES. REPAIRED FRAME IAW ASA TC AD20090102-700-25-1L.
UPPER FUSELAGE FRAME IS CRACKED AT STA 500C & STR 8 L/H. GROUNDED - YES. REPAIRED FRAME IAW ASA TC AD20090102-700-25-1L.
UPPER FUSELAGE FRAME IS CRACKED AT STA 867 AND STR 8L/H. GROUNDED - YES. REPAIRED L/H FRAME FS 867 AT STR 8 IAW ALASKA TC AD20090102-700-25-1L STEP 67.
UPPER FUSELAGE FRAME IS CRACKED AT STA 400 & STR 8 R/H. GROUNDED - YES. REPAIRED FRAME IAW ASA TC AD20090102-700-25-1R.
UPPER FUSELAGE FRAME CRACKED AT STA 480 & STR 8 LT. GROUNDED - YES. REPAIRED FRAME IAW ASA TC AD20090102-700-25-1L.
UPPER FUSELAGE FRAME CRACKED AT STA 440 & STR 8 LT. GROUNDED - YES. REPAIRED FRAME IAW ASA TC AD20090102-700-25-1L.
SHEAR TIE AT FS540 ON TOP OF WING BOX LBL 14 IS CRACKED. GROUNDED - YES. REMOVED & REPLACED SHEAR TIE IAW 737-700 SRM 51-40-02-0G-0.
SHEAR TIE AT FS 540 ON TOP OF WING BOX LBL 41 IS CRACKED. GROUNDED - YES. REMOVED & REPLACED SHEAR TIE IAW 737-700 SRM 51-40-02-0G-0.
SHEAR TIE AT FS 540 ON TOP OF WING BOX RBL 6 IS CRACKED. GROUNDED - YES. REMOVED & REPLACED SHEAR TIE IAW 737-700 SRM 51-40-02-0G-0.
SHEAR TIE AT FS 540 ON TOP OF WING BOX LBL 32 IS CRACKED. GROUNDED - YES. REMOVED & REPLACED SHEAR TIE IAW 737-700 SRM 51-40-02-0G-0.
SHEAR TIE AT FS 540 ON TOP OF WING BOX RBL 14 IS CRACKED. GROUNDED - YES. REMOVED & REPLACED SHEAR TIE IAW 737-700 SRM 51-40-02-0G-0.
SHEAR TIE AT FS 540 ON TOP OF WING BOX LBL 16 IS CRACKED. GROUNDED - YES. REMOVED & REPLACED SHEAR TIE IAW B737-700 SRM 51-40-02-0G-0.
SHEAR TIE AT FS 540 ON TOP OF WING BOX LBL 32 IS CRACKED. GROUNDED - YES. REMOVED & REPLACED SHEAR TIE IAW 737-700 SRM 51-40-02-0G-0.
SHEAR TIE AT FS 540 ON TOP OF WING BOX RBL 54 IS CRACKED. GROUNDED - YES. REMOVED & REPLACED SHEAR TIE IAW 737-700 SRM 51-40-02-0G-0.
SHEAR TIE AT FS 540 ON TOP OF WING BOX RBL 41 IS CRACKED. GROUNDED - YES. REMOVED & REPLACED SHEAR TIE IAW 737-700 SRM 51-40-02-0G-0.
AFT PIT R/H TRANSITION PANEL HAS MULTIPLE AREAS OF CORROSION FROM STA 727-767. GROUNDED - YES. REMOVED CORROSION AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-2, REPAIRED TRANSITION PANEL IAW B737-700 SRM 53-00-53-2R-5 REPAIR 5W=1 O=.040 R=.024 L=6 D=.016.
AFT PIT LH TRANSITION PANEL HAS MULTIPLE AREAS OF CORROSION FROM STA 727-807. GROUNDED - YES. REPAIRED AFT PIT LH TRANSITION IAW 737-700 SRM 53-00-53-2R-5 REPAIR 5 W=1 O=.040 R=.000 L=10 D=.040.
UPON GEAR RETRACTION WE GOT A WHEEL WELL FIRE WARNING. WARNING CONTINUED FOR ABOUT 15- 30 SECONDS AFTER LANDING GEAR EXTENDED. NO OTHER ABNORMALITIES OR INDICATIONS. GROUNDED-YES. WHILE DEBRIEFING CREW, FIRE BELL CAME ON ALONG WITH WHEEL WELL FIRE LIGHT. WHEEL WELL FIRE LIGHT CURRENTLY ON SOLID. REMOVED M237 COMPARTMENT OVERHEAT DETECTION CONT. FOUND RESISTANCE PIN 21. GROUND 1.06 M OHMS, PIN 24-GROUND OL, AFTER DISCONNECTING BOTH ENDS OF M270 WHEEL WELL FIRE DETECTOR. DISCONNECTED CONN D46042P, MEGGED PIN 9, FOUND 0.16M OHMS SHORT TO GRD. FOUND 110 M OHMS PIN 9 D46042J. DISCONNECTED CONN D46030P MEGGED PIN 8 OF PLUG AND JACK, FOUND 110 M OHMS AT BOTH ENDS. FOUND VARIABLE RESISTANCE OF 30K OHMS-110K OHMS WHILE SHAKING WIRES AT D840, D842 CENTER CONDUCTOR TO CONNECTOR, REF B737-700 WDM 26-12-11. BITE OF M237 FOUND FAULT CODE 84, UNABLE TO RESET, REF B737-700 FIM 26-18 TASK 801. SENSOR TEST FOR FAULT CODE 84 SHOWS 3.26V AT POS 21 AND 24, INDICATES BAD SENSOR M270, REF FIM 26-18 TASK 802 PARA I (13). REPLACED WIRE W8222-6001R-18 AND WIRE W7522-6001R-18, RING OUT CHECKS GOOD, REF WDM 26-12-11 PG1. INSTALLED CONNECTORS D46030P AND D46042P. REINSTALLED COMPT OVHT DET CONT M237. REMOVED AND REPLACED WHEEL WELL OVERHEAT SENSOR ELEMENT M270. ACCOMPLISHED WHEEL WELL, WING, AND LOWER AFT BODY OVERHEAT DETECTION SYSTEM OPERATIONAL TEST, NO DEFECTS NOTED. REF B737-700 AMM 26-18-01, 26-18-02, 26-18-00 AND WDM 26-12-11.
AFT CARGO DOOR SILL WEB IS CORRODED. GROUNDED-YES. REMOVED CORROSION ON SILL WEB AND FOUND TO BE OUT OF LIMITS, IAW 737-700 SRM 53-60-15-1A-1. REPLACED WEB WITH NEW WEB, IAW 737-700 SRM 51-40-02-0G-0 5. AND 51-40-05-0G-0 TABLE A FIG 3, W 2" O .045 R .039 L 3" D .006.
REF LOG PAGE 60063891 - DURING A/C LOADING FOUND DAMAGE TO A/C AT STA 811 AND AT STRINGER S26R & S27R JUST BELOW AFT CARGO DOOR THRESHOLD GROUNDED - YES. (RESOLVED ON W/O: 1855193 TASKCARD: N/R-00001 ) REPAIRED DAMAGE AT STA 811 BETWEEN STR 26R AND 27R BELOW AFT CARGO DOOR I.A.W. ALASKA AIRLINES EA 700-53EA-23054. THIS IS A CAT B REPAIR WITH FIRST AND SECOND STAGE APPROVAL. THE INSPECTION THRESHOLD FOR THIS REPAIR IS PROVIDED BUT FULL COMPLIANCE TO 14CFR25.571(B) [25-45] AND 26.43(D) HAS NOT BEEN EVALUATED. NEW FAA APPROVED DATA WHICH CONTAINS THE INSPECTION REQUIREMENTS MUST BE ISSUED FINDING COMPLIANCE WITH 14CFR25.57(B)[25-45] PRIOR TO THE INSPECTION THRESHOLD OF 50,000 TOTAL FLT. CYCLES SEAMC ANDY NOTIFIED
DURING A/C LOADING FOUND DAMAGE TO A/C AT STA 811 AND AT STRINGER S26R & S27R, JUST BELOW AFT CARGO DOOR THRESHOLD. GROUNDED-YES. REPAIRED DAMAGE AT STA 811 BETWEEN STR 26R AND 27R BELOW AFT CARGO DOOR, IAW ALASKA AIRLINES EA 700-53EA-23054.
L1 DOOR IS DIFFICULT TO OPEN. GROUNDED-YES. DOOR OPERATED NORMALLY THRU TWO CYCLES, OK FOR FURTHER SERVICE.
FLIGHT ATTENDANT REPORTS L-1 DOOR HARD TO OPEN. GROUNDED - YES. OPEN AND CLOSED DOOR AT L1, COULD NOT DUPLICATE. OPS CHECK GOOD, OK FOR SERVICE.
A/C REAR LEFT FUSELAGE EMERG EXIT LIGHT BULB OUT. GROUNDED - YES. RELAMPED A/C REAR LT FUSELAGE EMERGENCY LIGHT OP CHECK GOOD IAW AMM 33-51-00.
GROUNDED - YES. REPAIRED L1 DOOR EXT SKIN LOWER HINGE CUTOUT IAW SRM 52-10-10-2R-5 REV 66, REPAIR IS A CATEGORY B REPAIR.
RIGHT VERTICAL PRESSURE WEB IS CRACKED IN MACHINED WEB AT RBL 42. ACFT GROUNDED. REPAIRED THE DAMAGE IAW SRM 57-10-10-2R-3, REPAIR 3, ALTERNATE 2.
AFT CARGO BAY, RT CARGO TRACK IS CRACKED IN RADIUS OF VERTICAL LEG AT BS 727E. ACFT GROUNDED. REPAIRED THE CARGO TRACK IAW SRM 53-00-53-212-3.
AFT CARGO BAY, RT CARGO TRACK IS CRACKED IN RADIUS OF VERTICAL LEG AT BS 747. ACFT GROUNDED. REPAIRED THE CARGO TRACK IAW SRM 53-00-53-2R-3, REPAIR 3.
APU BAY RT SIDE STRINGER EDGE DAMAGE FWD OF APU INLET OPENING 19 INCHES AFT OF FWD BULKHEAD. ACFT GROUNDED. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-80-13-1A-2. REMOVED FABRICATED AND INSTALLED NEW STRINGER IAW SRM 51-40-05-0G0 AND 51-40-02-0G0.
CENTER AISLE OVERHEAD OVERWING EMERGENCY EXIT SIGN LAMPS INOPERATIVE & A BROKEN LENS. ACFT GROUNDED. REPLACED THE LAMPS & REPLACED THE LENS. OPS CHECKED NORMAL, IAW AMM 33-51-01.
RIGHT OVERWING EMERGENCY EXIT IDENTIFIER BROKEN. ACFT GROUNDED. REPLACED THE LIGHT ASSY. OPS CHECKED NORMAL, IAW AMM 33-51-01.
EMERGENCY LIGHT EXIT SIGN IN CABIN CEILING BETWEEN OVERWING EXITS HAS MULTIPLE LAMPS INOPERATIVE. ACFT GROUNDED. REPLACED LAMP AND TESTED IAW AMM 33-51-01-960-801. OPS NORMAL.
EMERGENCY LIGHT AISLE FLOODLIGHT INOPERATIVE AT ROW 22 LT. ACFT GROUNDED. R & R AND TESTED LIGHT ASSY IAW AMM 33-51-03-960-802. OPS NORMAL.
EMERGENCY LIGHTS AT SEATS 8 ABC, AND 9-18 DEF WENT OFF PRIOR TO 15 MINS. ACFT GROUNDED. R & R, AND TESTED EMERGENCY EXIT LIGHT BATTERY PACKS AT BS 603 LT & RT, SIDEWALL IAW MM 33-51-06-960-805. TESTS PASS, OK FOR SERVICE. BATTERIES INSTALLED AT 03:00.
AFT PRESSURE BULKHEAD INTERCOSTAL CORRODED BS 1016, RBL 8 - RBL 17. ACFT GROUNDED. REMOVED, FABRICATED, AND INSTALLED NEW INTERCOSTAL, PN 148A2261-14 ON AFT PRESSURE BULKHEAD AT BS 1016, RBL 8-RBL 17, WL 210 IAW SRM 51-40-02 AND DWG 148A0922, SHT 0011. SMAL GRANTED FOR FABRICATION OF PART, CONTROL NR P0252177, ENGINEERING ISSUED ME-04 609-0740 FOR USE OF PN 148A2261-14 ON ACFT.
AFT PRESSURE BULKHEAD INTERCOSTAL CORRODED BS 1016, BL 0-RBL 8. ACFT GROUNDED. R & R INTERCOSTAL, PN 148A2261Y18, PO 835952.1 ON AFT PRESSURE BULKHEAD AT BS 1016, BL 0-RBL 8 IAW SRM 51-40-02 AND DWG 148A0922, SHT 011. ENGINEERING ISSUED ME-04 ASA-609-0739 FOR USE OF PN 148A2261Y18 IN LIEU OF PN 65-54862-20.
AFT PRESSURE BULKHEAD INTERCOSTAL CORRODED BS 1016, RBL 17-RBL 27. ACFT GROUNDED. R & R INTERCOSTAL, PN148A2261Y25, PO 835954.1 ON THE AFT PRESSURE BULKHEAD AT BS 1016, RBL 17-RBL 27 IAW SRM 51-40-02 AND DWG 148A0922, SHT 0011. ENGINEERING ISSUED ME-04, ASA-609-0741 FOR USE OF PN 148A2261Y25 IN LIEU OF PN 148A2261-1.
AFT PRESSURE BULKHEAD INTERCOSTAL CORRODED, BS 1016, BL 0-LBL 9. ACFT GROUNDED. R & R AFT PRESSURE BULKHEAD INTERCOSTAL IAW SRM 51-40-02 AND DWG 148A0922, SHT 0011. ENGINEERING ISSUED ME-04, ASA-609-0738 FOR USE OF PN 148A2261Y17 IN LIEU OF PN 65-54862-19.
L-1 WINDSHIELD POST CRACKED AT LT UPPER CORNER, DOT ATTACHED. ACFT GROUNDED. REPAIR ACCOMPLISHED ON TASK CARD SB737-53-1336-NG-1. DOT REMOVED.
MAIN CABIN FLOORBEAM AT FS 304.986.5 UPPER T CAP REQUIRES REPLACEMENT DUE CORROSION BEYOND ALLOWABLE LIMITS CUSP TO CUSP. ACFT GROUNDED. REPAIRED MAIN CABIN FLOOR BEAM AT BS 986.5, LBL 50-RBL 50 UPPER T-CAP IAW SRM 53-70-51-2R-4, REPAIR 4. THIS IS A CATEGORY "A" REPAIR, NO FURTHER ACTION REQUIRED.
AFT PRESSURE BULKHEAD INTERCOSTAL CORRODED BS 1024, RBL 27-RBL 48, WL 210. ACFT GROUNDED. R & R INTERCOSTAL, PN 148A2261Y24, PO: 834966.1 ON THE AFT PRESSURE BULKHEAD AT BS 1024, RBL 27-RBL 48, WL 210 IAW EA 700-53EA-14839, REV NEW AND REO-G18810, REV A, DOT REMOVED.
AFT PRESSURE BULKHEAD INTERCOSTAL CORRODED, BS 1033, LBL 8-LBL 16, WL 210. ACFT GROUNDED. R & R AFT PRSSURE BULKHEAD INTERCOSTAL, PN 65-54862U18, PO:834948.2 AT BS 1033, LBL 8-LBL 16, WL 210 IAW SRM 51-40-02 AND DWG 148A0922, SHT 0011. DOT REMOVED.
AFT PRESSURE BULKHEAD INTERCOSTAL CORRODED BS 1030, LBL 16 - LBL 27, WL 210. ACFT GROUNDED. R & R AFT PRESSURE BULKHEAD AT BS 1030, LBL 16 - LBL 27, PN 149A2261Y15, PO: 834948.1 INTERCOSTAL IAW SRM 51-40-02 AND DWG 148A0922, SHT 0011. ISSUED ME-04 ASA-609-0732 FOR USE OF PN 149A2261T15 ON AC 609AS, DOT REMOVED.
MAIN CABIN INTERCOSTAL STA 312 T0 328, RBL 32 IS CRACKED AT FASTENER HOLES. ACFT GROUNDED. R & R INTERCOSTAL STA 312-328, RBL 32 IAW DWG 141A5410, REV A. DOT REMOVED.
MAIN CABIN CREASE BEAM FS 950-995 AT R2 DOOR CORRODED IN MULTIPLE PLACES. ACFT GROUNDED. R & R INNER CHORD BY THE R2 AFT GALLEY, SERVICE DOOR, PART 147A8540V8, PO: 834913.2 AT BS 896-BS 1006, RBL 42-RBL 62 IAW DWG 147A8501 SHT 0067. DOT REMOVED.
INTERCOSTAL IN THE FWD CABIN AREA CRACKED. BS 344-BS360, LBL 10. ACFT GROUNDED. REMOVED AND REINSTALLED INTERCOSTAL FOR ACCESS AT BS 344 TO BS 360 BL-0 IAW BAC DWG 141A5410, REV C. REMOVED CRACKED INTERCOSTAL IAW SRM 51-40-02. LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-02 AND BAC DWG 141A5410, REV C. INSTALLED NEW INTERCOSTAL IAW BAC DWG 141A5410. REV C.
MAIN CABIN INTERCOSTAL STA 264-284 RBL 2 IS CRACKED. ACFT GROUNDED. R & R INTERCOSTAL IAW DWG 141A5410, REV A, REMOVED DOT.
MAIN CABIN FLOORBEAM, STA 947.5 HAS CORROSION AROUND 3 EA FASTENER H0LES, LBL 10 TO RBL 10. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS IN 3 EA AREAS. ORIGINAL THICKNESS IN 3 EA AREAS IS .180. REMAINING THICKNESS AT RBL 4 IS .125, .035 WAS REMOVED. REMAINING THICKNESS AT LBL 4 IS .148, .032 WAS REMOVED. REMAINING THICKNESS AT LBL 12 IS .159, .021 WAS REMOVED. RBL 4 AND LBL 4 FOUND TO BE OUT OF LIMITS AND LBL 12 IS FOUND TO BE WITHIN LIMITS. REPAIRED RBL 4 AND LBL 4, REF 700 53-70-51-2R-6, REPAIR 6 ALLOWABLE LIMITS REF SRM 53-70-51-1A-1 ALODINED AND PRIMED REF SRM 51-20-01, PAINTED AND IDENTIFIED AREA REF AMM 51-05-01 DOT REMOVED.
MAIN CABIN FLOOR INTERCOSTAL, BS 328 TO 344, LBL 45.50 CRACKED. ACFT GROUNDED. R & R MAIN CABIN FLOOR INTERCOSTAL, BS 328 TO 344, LBL 45.50, PN 141A5410U16 IAW SRM 51-40-02 AND BAC DW 141A5410, DOT REMOVED.
MAIN CABIN FLOOR INTERCOSTAL, BS 312 TO 328, LBL 45.50 CRACKED. DOT B322. ACFT GROUNDED. R & R MAIN CABIN FLOOR INTERCOSTAL, BS312 TO 328, LBL 45.50 PN 141A5410U12 IAW SRM 51-40-02 AND BAC DWG 141A5410, DOT REMOVED.
.5" CRACK INDICATION ON LOWER SURFACE OF LT HORIZONTAL STABILIZER, STA 101, 11" FROM AFT SPAR. ACFT GROUNDED. REMOVED AND REINSTALLED LT HORIZONTAL STABILIZER L/E AND TOP IAW AMM 27-41-21. REPAIRED CRACKED LOWER SKIN IAW SRM 55-10-01-2R-11, REPAIR 11, PAINTED REPAIR AREA IAW AMM 51-21-99. THIS IS CLASS "B" REPAIR AND REQUIRES REINSPECT. DOT REMOVED. .
EXTERNAL FUSELAGE, FWD RT POWER RECEPTICLE INNER CUTOUT MATTING SURFACE CRACKED. ACFT GROUNDED. ACCOMPLISHED A CATEGORY B REPAIR TO THE EXTERNAL GROUND POWER RECEPTACLE DOOR SURROUND DOUBLER IAW EA 700-53EA-14870. REV NEW AND REO-G18811, REV B. DOT REMOVED. CATEGORY B REPAIR INITIAL INSPECTION, THRESHOLD 50,000 TOTAL FLIGHT CYCLES PENDING DTE, REPEAT INSPECTION INTERVAL PENDING DTE.
PAX O2 MASKS DEPLOYED AT FL400 ACFT, RIGHT. CABIN PRESSURE ALL NORMAL WITH NO WARNING. F/A INDICATED THAT SOME PAX PULLED LANYARDS. DESCENDED TO LOWER ALTITUDE IAW QRH. FLIGHT DIVERTED. ACFT GROUNDED. FOUND ROW 21 DEF CIRCUIT BOARD CONNECTOR BURNED WHICH SHORTED MASK DROP CIRCUIT AND CAUSED PSU MASKS TO DROP ON RT SIDE OF ACFT UNCOMMANDED. R & R PSU IAW AMM 25-23-61-000-861. ROW 6 DEF O2 HOSE CONNECTOR FOUND DETACHED FROM O2 CANISTER AND 3 OF 4 GREEN DUST PROTECTORS STILL INSTALLED ON O2 CANISTER. RESECURED O2 HOSE CONNECTOR TO GENERATOR. RESTORED O2 MASKS AND CANISTERS, AUTO ACTIVATION, OPS CHECK GOOD.
L2 DOOR LOWER EXIT LIGHT LENS CRACKED. ACFT GROUNDED. REPLACED THE LIGHT ASSY AND OPS NORMAL, IAW MM 33-51-01.
FRAME AT BS 727A IS CORRODED UNDER GROUND BLOCK BETWEEN STR 4 - 5R. ACFT GROUNDED. REMOVED CORROSION ON FRAME, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A-1, FIG 102, DETAIL C. REPAIRED FRAME IAW EA 700-53EA-13321, REV: NEW.
EXIT SIGN AFT OF L2 DOOR WILL NOT STAY ON. ACFT GROUNDED. SECURED EXIT SIGN LENS IAW AMM TASK 33-51-01-410-001.
LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. FOUND CONNECTOR D11078 NOT HOOKED UP. IAW WDM 33-51-13 PLUGGED CONNECTOR IN, OPS CHECKED EMERGENCY LIGHTS NORMAL, REF MM 33-51-00.
AFTER PRESSURIZATION OF ACFT, FOUND LT OVERWING EXIT DIFFICULT TO OPEN. ACFT GROUNDED. ACCOMPLISHED LT EMERGENCY EXIT DOOR ADJUSTMENT IAW MM 52-22-00-820-001.
BATTERY PACK FAIL CAPACITY CHECK, REF TASK CARD 78233000. ACFT GROUNDED. REPLACED BATTERY PACK IAW MM 33-51-06.
CHECK DENT AT STA NR 896 W/L236 ACFT GROUNDED. CHECKED LIMITS ON FUSELAGE SKIN AT STA 896 W/L 236 ORIGINAL THICKNESS IS .100 WIDTH IS .650 AND LENGTH IS 3 DEPTH IS .020 W/Y=32.5 FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01 TOPCOAT IAW AMM 51-21-44.
EMERGENCY PATH LIGHT INOPERATIVE. R & R M1674 BATTERY PACK AND ROW 7DEF. OPS CHECKED GOOD IAW AMM 3-51-06-960-805.
MAIN CABIN SEAT TRACK STA 727B, RBL45.50 OTBD FLANGE AFT HOLE HAS CRACK INDICATION. ACFT GROUNDED. REMOVED DAMAGE AREA IAW REO-G16099, REV A. ACCOMPLISHED HFEC OF CUT OUT IAW NDT PTG 51-00-00 PROCEDURE 23. NO CRACKS NOTED. PERFORMED INSURANCE CUT OF 0.040. FABRICATED AND INSTALLED REPAIR PARTS REO-G16099, REV A AND EA 700-53EA-10073, REV NEW.
GATE AGENT REPORTS SHE CANT OPEN THE L-1 DOOR. FOUND L1 OUTSIDE DOOR HANDLE HARD TO LATCH/UNLATCH,ALSO FOUND LOWER GATE STRIKING DOOR CUTOUT-NO GAP WHEN CLOSED. FOUND 3 DOOR STOP PINS OUT OF ADJUSTMENT CAUSING DOOR HANDLE TO BIND DURING OPENING. ADJUSTED STOP PINS IAW MM 52-11-00-820-801, PARA U. ADJUSTED UPPER GUIDE ARM IAW PARA H TO CLEAR LOWER GATE RIDING CONDITION. DOOR OPS CKS OK.
EMERGENCY LIGHT EXIT LOCATOR SIGN ADJACENT TO L 1 DOOR HAS BROKEN LENS. ACFT GROUNDED. R & R LENS AND TESTED IAW MM 33-51-01-960-801. OPS NORMAL.
NR 4 SLAT LOWER EDGE HAS A LARGE DENT WITH A CREASE JUST OUTBOARD OF THE SLAT ACTUATOR. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND BONDED IAW B737 700 SRM 51 70 10 REPAIR 4.
AFT PIT CARGO TRACK AT BS 945 LBL 3 IS CORRODED. REMOVED DAMAGED SECTION AND INSTALLED REPLACEMENT PART IAW B737 700 SRM 51 40 02.
FORWARD CARGO FLOOR PANEL HAS REPAIR DOUBLER MISLOCATED. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW B737 700 SRM 51 40 05.
FORWARD CARGO FLOOR SUPPORT ZEE AT BS 500C +4 RBL 3 HAS HOLES FROM FLOOR PANEL REPAIR. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS AND INSTALLED IAW B737 700 SRM 53 0053 REPAIR 2.
EXTERIOR FUSELAGE SKIN DENTED AT BS 261, 21 INCHES BELOW STR 23L AT BS 285 STR 22L. REPLACED SKIN.
CUSTOMER WALK ITEM: EMERGENCY LIGHT DIOD AT 21 ABC. RELAMPED EMERGENCY LIGHT AT 21ABC AND PERFORMED GOOD FUNCTIONAL TEST.
RIGHT WING NR 5 SLAT EXTERNAL SKIN CRACKED AT ACTUATOR MOUNT LOCATION APPROX .25. REPAIRED RIGHT WING NR 5 SLAT.
BOTTOM DISCHARGE BASE ON RUDDER IS BAD. REPAIRED DAMAGE.
NR 2 SLAT EXTERIOR SKIN AT ACTUATOR HAS CRACK COMING OUT OF RIVET. REPAIRED NR 2 SLAT EXTERIOR SKIN AT ACTUATOR FITTING.
FOUND CONNECTIVE FRAME TO HAVE AN EXCESSIVELY WORN AREA AT FASTENER HOLE IN T/E. REMOVED AND REPLACED CONDUCTIVE FRAME.
RIGHT WING NR 6 SLAT EXTERNAL SKIN CRACKED AT ACTUATOR MOUNT LOCATION APPROX .25. REPAIRED RIGHT WING NR 6 SLAT.
CORROSION AT A FASTENER ON LT CREASE BEAM WEB UPPER SURFACE. REMOVED CREASE BEAM WEB, FABRICATED NEW WEB AND INSTALLED.
DENTED FRAME BS 727B STR 23 RT. REPAIRED DENT.
FLOOR PANEL SPLICE BETWEEN FLOORS NR 1 AND 2 CORRODED. REMOVED AND REPLACED FLOOR PANEL SPLICE.
CORROSION AFT CARGO BAY THRESHOLD CLOSEOUT WEB MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED AFT CARGO BAY THRESHOLD.
DENTED FRAME BS 827 23L. DENTED FRAME AT 827 S 23L REPAIRED IAW EA.
DENTED FRAME BS 727C 23R. REPAIRED DENT.
CRACKED FLOOR SUPPORT AT UPPER ANGLE. REPLACED FLOOR SUPPORT WITH NEW PART.
CORROSION ON STIFFNER FWD SIDE OF 227.8 BULKHEAD LBL 4 WL 159. REMOVED CORRODED STIFFNER FABRICATED NEW AND INSTALLED.
CRACKED FLOOR SUPPORT AT UPPER ANGLE BS 393 BL 0 WL 208. REPAIRED FLOOR SUPPORT.
FLOOR PANEL SPLICE TEE HAS CORROSION AFT CARGO BAY. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND REPLACED FLOOR PANEL SPLICE TEE.
VERTICAL CRACK IN VAPOR BARRIER AT FASTENER ROW OUT OF LIMITS.
CORROSION ON FORWARD CARGO BAY FLOOR TO BULKHEAD SUPPORT. REMOVED AND REPLACED FLOOR TO BULKHEAD SUPPORT.
FWD CARGO DOOR CUTOUT 2ND FROM THE BOTTOM STOP FITTING CRACKED. REPLACED FWD CARGO DOOR CUTOUT 2ND FROM THE BOTTOM STOP FITTING.
SUPPORT ANGLE CRACKED. REMOVED AND REPLACED SUPPORT ANGLE.
FRETTING ON LOWER WING TO BODY FAIRING SUPPORT FRAME BS 727 BL 0 RBL 20. REMOVED AND REPLACED WITH FABRICATED SUPPORT FRAME.
FRETTING ON WHEEL WELL FAIRING SUPPORT FRAME BS 663-674 LBL 27. REMOVED AND REPLACED FAIRING SUPPORT.
FRETTING ON WHEEL WELL CUTOUT FAIRING SUPPORT ANGLE. REMOVED FRETTING AND FOUND TO BE OUT OF LIMITS. REPLACED AND INSTALLED WHEEL WELL CUTOUT FAIRING SUPPORT ANGLE.
FRETTING ON WHEEL WELL FAIRING SUPPORT TEE CHORD BS 663 674 RBL 27. FRETTING TO BE OUT OF LIMITS, REPLACED WHEEL WELL FRAME.
FLOOR PANEL SPLICE BETWEEN NR 3 AND NR 4 CORRODED. FABRICATED REPLACEMENT FLOOR PANEL SPLICE.
INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL.
BS 277-294 RBL 1 WL 208 INTERCOSTAL CRACKED OUT OF LIMITS. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW.
BS 312 328 RBL 34 WL 208 INTERCOSTAL CRACKED OUT OF LIMITS. REMOVED DAMAGED INTERCOSTAL INSTALLED NEW.
BS 312 328 LBL 47 WL 208 INTERCOSTAL CRACKED OUT OF LIMITS. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW.
LT HORIZONTAL STAB STA 92.7 RIB CRACKED 1 INCH FROM BOTTOM AT VERTICAL STIFFENER LOCATED 20 INCHES FROM FRONT SPAR. RIB WAS REAPIRED.
FLOOR SUPPORT CRACKED AT BS 540 WL 207 RBL 1. REMOVED AND REPLACED FLOOR SUPPORT AT BS 540 WL 207.
LT HORIZONTAL STAB STA 92.7 RIB CRACKED 1 INCH FROM BOTTOM AT VERTICAL STIFFENER LOCATED 39 INCHES FROM FRONT SPAR. RIB WAS REAPIRED.
RT HORIZONTAL STAB STA 92.7 RIB CRACKED 1 INCH FROM BOTTOM AT VERTICAL STIFFENER LOCATED 11 INCHES FROM FRONT SPAR. RIB WAS REAPIRED.
LT HORIZONTAL STAB STA 92.7 RIB CRACKED 1 INCH FROM BOTTOM AT VERTICAL STIFFENER LOCATED 30 INCHES FROM FRONT SPAR. RIB WAS REPAIRED.
LT HORIZONTAL STAB STA 92.7 RIB CRACKED 1 INCH FROM BOTTOM AT VERTICAL STIFFENER LOCATED 30 INCHES FROM FRONT SPAR. RIB WAS REPAIRED.
CORROSION ON FLOORBEAM UPPER SURFACE. REPAIRED FLOORBEAM.
FLOOR SUPPORT CRACKED AT BS 540 WL 207 LBL 1. REPAIRED PER SRM.
AFT ENTRY FLOOR SHEAR WEB CRACKED. REMOVED AND REPLACED SHEAR WEB.
LT HORIZONTAL STAB STA 92.7 RIB CRACKED 1 INCH FROM BOTTOM AT VERTICAL STIFFENER LOCATED 20 INCHES FROM FRONT SPAR. RIB WAS REAPIRED.
LT HORIZONTAL STAB STA 92.7 RIB FRONT SPAR UPPER CLEVIS AFT LUG AFT FACE UPPER EDGE GOUGED. REPAIRED PEER EA
RT HORIZONTAL STAB STA 92.7 RIB CRACKED 1 INCH FROM BOTTOM AT VERTICAL STIFFENER LOCATED 39 INCHES FROM FRONT SPAR. RT HORIZONTAL STAB STA 92.7 RIB WAS REAPIRED.
CORROSION ON FLOOR SUPPORT BS 992. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPLACED FLOOR SUPPORT.
LT HORIZONTAL STAB STA 92.7 RIB CRACKED 1 INCH FROM BOTTOM AT VERTICAL STIFFENER LOCATED 11 INCHES FROM FRONT SPAR. LT HORIZONTAL STAB STA 92.7 RIB WAS REPAIRED.
AFT CARGO BAY BS 747-767 RBL 21 CORROSION ON INTERCOSTAL OUT OF LIMITS. REMOVED AND REPLACED INTERCOSTAL.
FWD CARGO BAY INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL.
CORROSION ON FLOOR SUPPORT BS 992. REMOVED AND REPLACED FLOOR SUPPORT.
BS 747 FRAME CRACKED AT BIN RAIL ATTACH BRACKET. CUTOUT FRAME AND REPAIRED WITH DOUBLER.
FWD CARGO BAY INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL.
FWD CARGO BAY INTERCOSTAL CRACKED BS 500C+19.5. REMOVED CRACKED INTERCOSTAL, INSTALLED NEW.
DENT IN FUSELAGE IN LINE WITH L1 DOOR SILL AND 36 INCHES AFT. REMOVED INTERIM REPAIR, FABRICATED PERMANENT REPAIR AND INSTALLED.
BS 480 FRAME CRACKED AT BIN RAIL BRACKET. CUTOUT FRAME AND REPAIRED WITH DOUBLER.
BS 440 FRAME CRACKED AT BIN RAIL BRACKET. REPAIRED WITH DOUBLER.
BS 867 FRAME CRACKED AT BIN RAIL ATTACH BRACKET. CUTOUT FRAME AND REPAIRED WITH DOUBLER.
FWD CARGO BAY FLOOR TO SIDEWALL SHIELD HAS CORROSION. REMOVED FLOOR TO SIDEWALL SUPPORT AND INSTALLED NEW.
BS 344 CORROSION ON FLOORBEAM. REMOVED DAMAGE FROM FLOORBEAM, FABRICATED REPAIR PARTS AND INSTALLED.
FWD CARGO BAY FRAME GOUGED. REPAIRED FRAME PER EA.
CORROSION ON FLOOR TO SIDEWALL SUPPORT AFT CARGO BAY RT SIDE. REMOVED CORROSION FABRICATED NEW ZEE SUPPORT AND INSTALLED.
CORROSION AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT. REMOVED SUPPORT, FABRICATED NEW SUPPORT AND INSTALLED.
RESKIN FWD CARGO DOOR DUE TO NUMEROUS DENTS. REMOVED AND REPLACED FWD CARGO DOOR SKIN.
RESKIN AFT CARGO DOOR DUE TO NUMEROUS DENTS. REMOVED AND REPLACED AFT CARGO DOOR SKIN.
AFT CARGO BAY CORROSION ON FLOOR TRACK. REMOVED AND REPLACED FLOOR TRACK.
AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT HAS CORROSION. REMOVED AND INSTALLED NEW SIDEWALL SUPPORT.
FWD CARGO DOOR CUTOUT FWD LOWER STOP FITTING GOUGED. FWD CARGO DOOR STOP FITTING FOUND TO BE OUT OF LIMITS.
MAIN CABIN FLOORBOARD SUPPORT CHANNEL CRACKED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM.
AFT CARGO BAY FLOOR PANEL NR 5 HAS CORROSION.
FOUND CLIP 143A75OU159 CRACKED. INSTALLED NEW CLIP 143A75OU159.
CARGO BAY FLOOR PANEL NR 3 HAS EXCESSIVE DENTS AND PUNCTURES. FABRICATED REPLACEMENT PANEL ASSY.
MAIN CABIN FLOORBOARD SUPPORT CHANNEL CRACKED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM.
BAFFLE BRACKET IS CRACKED. REMOVED AND REPLACED BAFFLE BRACKET IAW SRM 53 00 53.
BAFFLE BRACKET IS CRACKED. REMOVED AND REPLACED BAFFLE BRACKET IAW SRM 53 00 53.
BAFFLE BRACKET IS CRACKED.
FLOOR PANEL SPLICE PLATE CORRODED. REMOVED AND REPLACED SPLICE PLATE.
APPROX 1500' AGL ON TAKEOFF RT ENG SURGE/STALL APPROX 3 TIMES RIGHT AFTER POWER REDUCTION. SLIGHTLY HIGH EGT RT ENG A/T OFF AND POWER REDUCTION PER QRH ENG RAN NORMALLY J HOOK INSPECTION FAILED. DAMAGE NOTED ON THE HPC BLADES. EVIDENCE OF BIRDSTRIKE. NR 2 ENGINE REPLACED.
L2 DOOR SLIDE CATCHING ON DOOR. REMOVED & REPLACED SLIDE REF MM 25 66 01 000 801.
UNUSUAL VIBRATION FELT IN FLOOR OF AC DURING FLIGHT, STRONGEST VIBRATION IN OVERWING AREA AT CABIN. ALSO A SUBTLE YAWING MOTION FELT IN REAR GALLEY AREA EVERY FEW SECONDS. PASSENGER OBSERVED LT IB FLAP TRACK FAIRING WAS VIBRATING. PRECAUTIONARY EMERGENCY DECLARED & AC DIVERTED. (CREW REPORTED NO NOISE ASSOCIATED WITH VIBRATION) DURING CONDITIONAL INSPECTION OF MLG WING DOORS, FOUND LT MLG WING DOOR OUT OF ADJUSTMENT. ADJUSTED LT MLG WING DOOR IAW MM TASK 32-12-21-000-801
UNUSUAL VIBRATION FELT IN FLOOR OF AC DURING FLIGHT, STRONGEST VIBRATION IN OVERWING AREA AT CABIN. ALSO, A SUBTLE YAWING MOTION FELT IN REAR GALLEY AREA EVERY FEW SECONDS. PRECAUTIONARY EMERGENCY DECLARED & AC DIVERTED. REF LP 6428995, DURING CONDITIONAL INSPECTION FOUND RT ELEVATOR TAB CONTROL VALVE FAILED IN FLAP DOWN POSITION. REMOVED & REPLACED OER 27-31-35-000-801. OPS GOOD.
FA REPORTS FWD ENTRY DOOR DIFFICULT TO CLOSE AND LOCK ADJUSTED GUIDE ARM REF MM 52 11 00 820 801 "H". OPS CKS NML. OK FOR CONT SVC.
L N WING RSS 260 FITTING FOUND WITH DRILL HOLD. REPLACED WITH NEW PART.
BS 727B 787 RBL 21 ZEE CHANNEL CORRODED RE-PLUGGED ZEE CHANNEL WITH REPAIR PART IAW B737 700 SRM 51 40 05 51 40 08 AND 51 40 02.
BS 767 787 RBL 21 SUPPORT SHIELD IS CRACKED. SUPPORT SHIELD AT BS 767 787 RBL 21 REPLACED IAW B737 700 SRM 51 40 02.
AFT CARGO BS 767+S FLOOR PANEL "T" SPLICE CORRODED COLLISION ON TEE ASSY IN AFT CARGO BS 767+5 BLENDED OUT BEYOND LIMITS. REPLACED WITH REPAIR PART IAW B737 700 SRM 53 60 53.
BS 747 + 767 RBL 21 INTERCOSTAL HAS CORROSION COMMON TO ANCHOR NUTS. REPLACED INTERCOSTAL WITH REPAIR PART.
BS 727B TO BS 787 RBL 21 2 CHANNEL HAS CORROSION. REPLACED 2 CHANNEL WITH REPAIR PART.
PREVIOUS LIGHTNING STRIKE REPAIR AT RT FUSELAGE SKIN STA 500 + 16.5", 0.5" BELOW STR 20R REQUIRE HFEC OR DYE PENETRANT INSPECTION PER SRM 53 00 01 REPAIR 13 PARA 6. MATERIAL LOSS FROM PREVIOUS LIGHTNING DAMAGE REMOVAL 0.020" ORIGINAL THICKNESS IS 0.080" PER B737 700 SRM 53 30 01 FIG 2. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW B737 700 SRM 53 00 01 REPAIR MAT. MADE IAW B737 700 SRM 53 00 01. REPAIR PARTS INSTALLED IAW B737 700 SRM 51-40-02.
BS 1112 FRAME CRACKED AT UPPER END IN THE RADIUS. STUB TORSION BAY COMPARTMENT RT VERTICAL FRAME AT BS 1112 REPAIRED IAW B737 700 SRM 51 70 11 FIG 201.
AFT PIT FLOOR SUPPORT BEAM AT BS 792 CORRODED. REPAIRED IAW SRM 53-00-53.
AFT PIT FLOOR PANEL NR 4 IS CORRODED REPAIRED IAW SRM 51 40 08.
AFT PIT FLOOR PANEL NR 1 CORRODED REPAIRED IAW SRM 51 40 05 AND 53 60 53.
FWD PIT FLOOR PANEL NR 2 CORRODED REPAIRED IAW SRM 51-40-05 FIG 2 PG 2.
AFT CABIN FLOORBEAM IS CORRODED AT BS 994 WL 208 LBL 38-48 REPAIRED IAW SRM 51 40 02.
AFT CABIN FLOORBEAM CORRODED AT BS 1016 RBL 32 WL 208. REPAIRED IAW SRM 51 40 2.
AFT CABIN INTERCOSTAL IS CORRODED AT BS 950 REPAIRED IAW SRM 51 40 2.
AFT PIT FLOOR PANEL NR 3 IS CORRODED. REPAIRED IAW SRM 51 40 08 AND 53 60 53.
AFT PIT FLOOR PANEL NR 2 IS CORRODED REPAIRED IAW SRM 51 40 05 AND 53 60 53.
FWD PIT FLOOR PANEL NR3 CORRODED REPAIRED IAW SRM 51 40 08 AND 53 30 53.
FWD PIT FLOOR PANEL NR 1 CORRDED REPAIRED IAW SRM 51 40 05 AND51 40 08.
FLOOR SUPPORT AT BS 344 IS CORRODED REPAIRED IAW SRM 53 10 15.
FOUND SMALL DENT NEAR L1 DOOR AT BS 259. REPAIRED IAW SRM 53 00 01 PG 201 REPAIR 1.
CENTER FLOOR BOARD 2 STA 244 IS GOUGED REPAIRED IAW SRM 53 00 50
E/E BAY DOOR SKIN AFT OF ANGLE WAS DENT AT BS 323 REPAIRED IAW SRM 52 00 01.
OAK - DURING MAINTENANCE CHECK, THE MID CABIN EMERGENCY TRACK LIGHTS WERE INOPERATIVE. ADJUSTED THE EMERGENCY TRACK LIGHT WIRES. THE TRACK LIGHTS THEN OPERATED NORMALLY. (M)
SEA - DURING LINE MAINTENANCE, EMERGENCY TRACK LIGHTING COVER WAS FOUND MISSING AND WIRING WAS DISCONNECTED. REPLACED COVER AND WIRING. LIGHTS THEN OPERATED NORMALLY. (M)