N816SY
Registered owner: SUN COUNTRY INC, MN (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
SMOKE GOOGLES HAVE CRACK ON NOSE. PRIMARY OBSERVER SMOKE GOGGLES R&R REF AMM 25-64-00 OK FOR SERVICE THIS CLEARS MEL 25-11-1 MDDR# 139614
PHOTOLUMINESCENT ESCAPE PATH MARKING SYSTEM ALONG FLOUR AT ROWS 13-14 STRIP IS LOSE. RESECURED PHOTOLUMINESCENT FLOOR PATH AT SEATS 13 AND 14 DEF REF AMM 33-51-16.
LIGHTING STRIKE STA 243.7 STR 1L. REMOVED AND REPLACED 1 SOLID RIVET AT FUSELAGE SKIN BS 234.7 STR 1L IAW SRM 53-00-01-2R-40 REPAIR 40 PARAG 4.
LIGHTNING STRIKE TRANSFERRED TO W/O 104619 N/R-0001. COMPLETED PHASE 1 AND 2 AMM 05-51-19-210-804 AND AMM 05-51-19-210-805. ALL LIGHTING STRIKES ARE ON NON-ROUTINES W/O 104619
FA REPORTS DIFFICULTY WITH UNSEATING FWD ENTRY GIRT BAR FROM HANGER DURING ARMING PROCEDURE - - REMOVED AND INSTALLED GIRT BAR SMOOTH OPERATION IAW AMM 25-66-01
EMERGENACY EXIT LIGHT SWITCH IN COCKPIT HAS BROKEN BLACK SWITCH GUARD. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH GAURD IAW AMM 33-51-00.
ROW 12 ABC EMERGENCY FLOOR LIGHTING STRIP NEEDS TO BE RESECURED TO FLOOR
FLOOR STRIP IN FWD GALLEY BETWEEN NICKLE BOARD AND AISLE RUNNER DAMAGED, TRIP HAZARD. REPLACED STRIP BETWEEN NICKLE BOARD AND AISLE RUNNER IAW AMM25-27-15 OK FOR SVC
FWD GALLEY EMERGENCY EQUIPMENT DOOR STUCK CLOSED- PUSHED IN TO FAR. UNJAMMED DOOR OPERATED NORMALLY. OK FOR SERVICE REF AMM 25-24-15
DEFECT 814016: GIRT BAR BRACKETS STIFF ON L1 AND R1 DOORS. ADJUSTED GIRT BAR BRACKETS AND OPS CHECKS GOOD REF AMM 25-66-01.
DEFECT 814002: BOTH FOWARD DOOR GIRT BAR BRACKETS LOOSE - RESOLUTION: ADJUSTED L1 AND R1 GIRT BAR BRACKETS REF AMM 25-66-01. OK FOR SERVICE
LOUD VIBRATION HEARD AFTER TAKEOFF SUSPECTED GROUND CREW HEADSET AUDIOPANEL DOOR WAS LEFT OPEN OR CAME OPEN. - RESOLUTION: GROUND CREW REPORTED GROUND SERVICE DOOR OPEN ON TAXI IN. INSPECTED DOOR PER AMM52-49-02 OK FOR SERVICE.
WORK ORDER 94406, NR00009: AFT GALLEY ENTRY DOOR , ESCAPE SLIDE SKIRT EXTENDS MORE THAN 10 INCHS AT BOTTOM OF DOOR AND CATCHES ON DOOR SILL. - RESOLUTION: REPOSITIONED SKIRT PER AMM REF 25-66-00,
SCNA20250321079 DEFECT 712156 AC 816: EXIT PATH FLOOR LIGHTING IS LOOSE NEAR 2 DEF. SECURED EXIT PATH FLOOR LIGHTING AT ROW 2 DEF REF AMM 35-27-31
DEFECT 794782: AC RIGHT ROW 12 EMERGENCY TRACK LIGHTING SEPERATING FROM FLOOR. RESOLUTION: RESECURED EMER. TRACK LIGHTING REF AMM 33-51-16.
CRACKS ON RIB STAB STA= 249.10 AT RH HORIZONTAL STABILIZER. CRACKS ON RIB STAB STA= 249.10 AT RH HORIZONTAL STABILIZER WERE REPAIRED PER ETI-737-24-176 REV 4 AND ENG-55SCA-11502.
WORKORDER 80746, NON-ROUTINE 00004: INITIAL INSPECTION: SIGN OF ARCING ON BRAID WIRE UPPER EDGE OF WINDOW 1 RH AT FLIGHT COMPARTMENT.
DOOR 2L SLIDE BUMPER PART BROKE OFF SLIDE BUMPER. (OPEN)
: DOOR 2L SLIDE BUMPER PART BROKE OFF SLIDE BUMPER - - RESOLUTION: (OPEN DEFECT)
DOOR 1L SLIDE DROPPED OUT OF CASEING WHILE DOOR WAS BEING OPENED. REINSTALLED SLIDE PACK AND COVER 1L DOOR REF AMM 25-66-01.
GIRT BAR ON MAIN DOOR LOOSE FALLS OUT. ADJUSTED TENSION ON GRIT BAR HOLD BRACKET REF AMM 25-66-02.
DEFECT 756124: NOSE GEAR CAME DOWN ON THE AFTER TAKEOFF CHECKLIST. NOSE GEAR LIGHT DISPLAYED RED THEN ONLY GREEN. LANDING GEAR DISAGREE CHECKLIST/QRH COMPLETE. RESOLUTION: PERFORMED FIM TASK 32-09 # PSEU BITE-NO FAULTS. JACKED A/C PERFORMED GEAR SWING REF M/M 32-32-00. OPS CKS NORMALLY. PERFORMED FIM TASK 32-30# 809. FOUND NO DEFECTS AT THIS TIME. OK FOR SERVICE.
SCNA20230202052 SUPPLEMENT
DEFECT 725184: OVEN SMOKING WHILE COOKING SMELLS ELECTRICAL. RESOLUTION: CATERING REPLACED OVEN RACKS AND INSERT WITH CLEAN UNITS OPS CHECK GOOD IAW AMM 25-30-61 NO ELECTRIC SMELL NOTED.
NR 2 ENGINE HIGH VIB (MORE THAN 4.0) AND MOMENTARY SURGE. PERFORMED BORESCOPE OF #2 ENGINE BOOSTER SECTION AND LPT BLADES REF. AMM 72-00-00-200-803-F00, AND AMM 72-00-00-200-808-F00. NO DEFECTS FOUND. REMOVED #2 ENG SPINNER CONES PER AMM 72-21-01, AND REMOVED #2 ENG FAN BLADES PER AMM 72-21-02. CLEANED AND INSPECTED FAN BLADES PER AMM 72-21-02. #2 ENG FAN BLADES INSTALLED ON TASK CARDS 729400000 AND T/C 720250100.ACCOMPLISHED FIM TASK 71-05 TASK 805 FOR ENG. SURGE THRU TO STEP (8). HMU TO BE REPLACED ON FOLLOWING N/R. ACCOMPLISHED FAN TRIM BALANCE REF MM 71-00-00-750-803-FOO AND VIBRATION SURVEY TEST 7 TASK 71-00-00-700-814-FOO HIGHEST READING WAS .3 UNITS AT ALL POWER SETTINGS. REMOVED ENGINE #2 HMU REF. 73-21-10-000-801-F00. PERFORMED INTERFACE INSPECTION. OK TO INSTALL NEW HMU. INSTALLED #2 HMU IAW 73-21-10. STILL REQUIRES OPS AND LEAK CHECK. OPS AND LEAK CHK'D PER AMM 71-00-00-800-811-F00. OPS CHK GOOD. NO LEAKS NOTED. RII INSPECTION OF HMU INSTALLTION COMPLETED.
DEFECT WORK ORDER N/R-00016: EMERGENCY BATTERY AT M1694 INOP RESOLUTION: REMOVED, REPLACED AND TESTED EMERGENCY BATTERY AT M1694 IAW AMM B737 33-51-06-960-805, TEST GOOD. 59705C 08JUN22
DEFECT: AT ROWS 10 AND 11, LUMINESCENT LIGHT STRIP IS LOOSE RESOLUTION: REINSTALLED EMERGENCY FLOOR PATH STRIP REF. AMM 33-51-16.
L2 GIRT BAR HOLDER LOOSE. RESOLUTION: ADJUSTED HOLDER REF AMM 25-66-00
TASK: TEMPORARY SKIN REPAIR INSTALLED STA 420 STR 20R. RESOLUTION: REMOVED TEMPORARY SKIN REPAIR AT BS 420 STR 20 AND INSTALLED 1 DOUBLER 2024-T3 .063", -2 TRIPLER 2020-T3 .063" AND -3 FILLER 2024-T3 .090" IAW SUN COUNTRY ENGINEERING TASK CARD ENG-53SCA-10913.
DEFECT SECTION 43 FUSELAGE SKIN GOUGED FROM BS414 TO BS438 AT S-20R. RESOLUTION: DAMAGE WAS TRIMMED OUT FROM BS414 TO BS438 AT STRINGER 20R. STRINGER 20R WAS FOUND CRAKCED ATHE THE AFT THREE FASTENER HOLES WHICH WAS TRIMMED AND REPAIRED. A REPLACEMENT STRINGER WAS ORDERED AND RECEIVED FOR PERMANENT REPAIR.
DEFECT: HAD TRAILING EDGE FLAP DISAGREE ON APPROACH AFTER VECTORS INDICATED 0 WHEN LEVER SAET AT 15 RAN QRH THEN RECEIVED ASYMETRY RAN QRH AND LANDED RESOLUTION: PERFORMED FIM 27-51 TASK 801. FOUND FAULT 27-53280 R28VAC EXC INV. FOUND RT SKEW AND IND BREAKER POPPED (C1443). RESET BREAKER. R&R #5,6, AND 8 SKEW SENSORS PER AMM 27-59-01. R&R FLAP INDICATOR PER AMM 27-58-02. R&R RT FLAP POS TX PER AMM 27-58-01. R&R (C1443) RT SKEW AND IND C/B PER SWPM 20-30-00. ADJUSTED RT FLAP POS TX PER AMM 27-58-01. OPERATED T.E.FLAP SYS PER AMM 27-51-00. ALL OPS & INDICATIONS NORMAL
VERIFY THE WIRE INTEGRITY AT THE BELOW LISTED CONNECTORS AND MEGGER THE WIRING LOOKING FOR SHORTS. WHILE USING THE MEGGER METER. FOUND 3 TWISTED SHIELDED PAIR WIRES AFFECTED. JUST INBD FROM #4 CANOE ON RT WING. WIRES THAT WHERE CHAFFED WHERE W1032-2006-R2, W1032-2007-R20. NOT SURE ABOUT THE LAST WIRE. TE FLAP SKEW SENSORS #5,#6,#7 AND #8 ARE STILL DISCONNECTED. ALONG WITH THE RT TE FLAP POSITION TRANSMITTER. C/B TE FLAP POS SKEW SNR AND IND R IS STILL OPEN AND TEH LOAD SIDE WIRE STILL DISCONNECTED. FSEU & FLAP POS INDICATOR STILL REMOVED.
ON ARRIVAL FLAPS FAILED TO EXTEND. PER THE QRH ALETERNATE FLAP EXTENISON WAS ATTEMPTED. LEADING EDGE DEVICES EXTENTED BUT TRAILING EDGE FLAPS DID NOT. NOTIFIED MC SR 8092. PERFORMED FIM 27-51 TASK 801 FOUND FAULT 27-53280 AND FOUND C/B P6-2 (A11) POPPED RESET C/B AND REMOVED AND REPLACED FSEU PER AMM 27-51-01-400-801 OPS CHECKS GOOD NO FAULTS AT THIS TIME
DEFECT: ON DEPARTURE THE FLAPS WOULD NOT RETRACT, PER QRH ALTERNATE FLAP EXTENSION WAS ATTEMPTED IMEDIATELY A TRAILING EDGE ASSYMETRY DEVELOPED ALT FLAP EXTENSION WAS STOPPED FLIGHT LANDED FLAPS 5 NOTIFIED MC RESOLUTION: PERFORMED FIM 27-59 TASK 807. FOUND # 7 FLAP SKEW SENSOR FAULT AND FOUND C/B P6-2 (A11) POPPED. RESET C/B AND REPLACED #7 FLAP SKEW SENSOR REF AMM 27-59-01. OPS CK GOOD.
DEFECT: LANDING GEAR LEVER WILL NOT MOVE UP AFTER TAKEOFF RESOLUTION: FOUND GROUND SPOILER INTERLOCK VALVE LOWER SLIDER ASSY. DISCONNECTED . CONEECTED LOWER SLIDER ASSY SLEEVE AND SAFTIED IAW AMM 27-62-51. ADJUSTMENT AND FUNCTIONAL CHECK GOOD . ACCOMPLISHED GEAR SWING AND GEAR RETRACTED NORMALLY. OK FOR SERVICE.
CORROSION ON SEVERAL POINTS AT LH CREASE BEAM WL 208 FROM STA 968 TO STA 1016 REMOVED AND REPLACED ON BS 1016 TO 900 LH CREASE BEAM PER B737-800 SRM 51-40-02.
CORROSION ON TCAP AT STA 986.5 FROM BL 0 TO BL 45L .REMOVED CORROSION ON T CAP BS986BL0TO BL45L FOUND TO BE OUT OFF LIMITS REPLACED T CAP PER WORK ORDERR 3500849/2400/0002
CORROSION FOUND AT AFT CARGO, AFT BULKHEAD UNDER WATER TANK.REPAIRED STRINGER CORROSION IN AFT CARGO UNDER WATER TANK PER B737-800 SRM 53-00-03 FIG 201 REINSTALLED WATER TANK IAW AMM 38-11-01-400-801.
LEFT WING INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB TURNBUCKLE LUG DAMAGED REPAIRED L/H WING I/B FIXED F/E DEFLECTION CONTROL RIB PER B737-800 SRM 57-51-02-2R REP 2
CORROSION ON SEVERAL POINTS AT R1 DOOR CREASE BEAM BTW STA 328 TO STA 291.5REMOVED AND REPLACED R1 DOOR CREASE BEAM AT STA 328 TO STA 291.5 ALL WORK DONE IAW B737-800 SRM 51-70-02, SRM 51-40-02 SRM 51-40-05 AND AMM 53-11-01
RUDDER COUNTER BALANCE HAS EVIDENCE OF CORROSION.REMOVED AND REPLACED RUDDER COUNTER BALANCE WEIGHT IAW B737 SRM 51-40-02 REFER TO NR 3500849/3000/0009 FOR BALANEC REQUIREMENTS.
CORROSION ON Z CHANNEL BTW STA 986.5 AND STA 1006 AT BL 40R WL 208.REMOVED AND REPLACED Z CHANNEL ON BS986.5 AND 1006. AT BL 40 WLZ08. PER B737-800 SRM 51-40-02.
CORROSION ON TCAP OF BEAM STA 986.5 FROM BL 0 TO BL 45R WL 208 REMOVED AND REPLACED TCAP ON BS 986.TO RBL 45 TO LBL 45, PER B7374 800 SRM 53-10-51 REP 4.
SURFACE CORROSION ON 3 EA FRAME ON COMPARTMENT FLOOR AT ST 767 REPAIRED 3EA CHANNEL FRAMES ON AFT COMPARTMENT AT S-1 767 ALL WORK DONE IAW B737-800 SRM 51-10-02, STEP 15, SRM 53-00-53 REP 3 TABLE 202 ALTERNATIVE 3, SRM 53-00-53 ALLOWABLE DAMAGE 2 AMM 51-21-41 AND AMM 51-21-72. TOOL #1115 D/D 5-10-2020 TOOL # 1494 D/D 6-6-2020.
RAIL CHANNELS AT ST 767 LBL 3.0, LBL 8.1, LBL 12.5 AND LBL 17.24 HAVE SURFACE CORROSION AFT CARGO BAY REPAIRED RAIL CHANNELS AT ST 767, LBL 3.0, LBL 8-1, LBL 12.5 AND LBL 17-24, ALL WORK DONE IAW B737-800 SRM 51-10-02 STEP 15, SRM 53-00-53 REP 3 TABLE 202 ALTERNATIVE 3, AMM 51-21-41 AND AMM 51-21-72 ID #98 D/D 5/6/2020
MULTIPLE CORRODED INSERTS ON FLOOR PANEL 242 UF REMOVED AND REPLACED INSERTS ON FLOOR PANEL 242UF IAW B737-800 SRM 53-00-50 STEP 5 (S) (1-2) SEE ARR-ASR FORM SHOP TRAVELLER FOR WORK PERFORMED.
CORROSION ON LWR FLANGE FROM T CAP BEAM AT STA 986.5 BL 447 REMOVED CORROSION ON T CAP BS 986.5 BL44.7 OUT OFF LIMITS REPLACED T CAP PER WORK ORDER 3500849/2400/0002
MULTIPLE CORRODED INSERTS ON FLOOR PANEL 221BF REMOVED AND REPLACED INSERTS ON FLOOR PANEL 221 BF IAW B737-800 SRM 53-00-50 STEP 5 CS) (1-27 SEE AAR ASR FORM SHOP TRAVELLER FOR WORK PERFORMED
CORROSION ON Z CHANNEL BTW STA 986.5 AND STA 1016 AT BL 32R WL 208 . REMOVED + REPLACED Z-CHANNEL @ STA 986.5 1016 RBL 32 IAW B737-800 SRM 51-40-02 + BOEING DRAWING 147A-5700.
R1 DOOR CUT OUT FRAME LOWER SIDE FWD IS CRACK. REMOVED AND INSTALLED R1 DOOR FRAME IAW B737-800 SRM 51-40-02 STEP 4 AND 7.
R1 SCUFF PLATE HAS A CRACK ON THE PLATE.R1 SCUFF PLATE P/N 141A8431-1 REPAIRED ON REPAIR ORDER 412614 IAW BAC5975 REV (N) DATED 12 SEP 2019 8130-3 FORM TRACKING 201076
MULTIPLE CORRODED INSERTS ON FLOOR PANEL ON FLOOR PANEL 222BF REMOVED AND REPLACED INSERTS ON FLOOR PANEL 222BF IAW B737-800 SRM 53-00-50 STEP 5 (S)(1-2) SEE AAR-ASR FORM SHOP TRAVELLER FOR WORK PERFORMED.
MULTIPLE CORRODED INSERTS ON PANEL 242TF REMOVED AND REPLACED INSERTS ON PANEL 242TF IAW B737-800 SRM 53-00-50 STEP 5 (S)(1-2) SEE AAR-ASR FORM SHOP TRAVELLER FOR WORK PERFORMED.
MULTIPLE CORRODED INSERTS ON FLOOR PANEL 241ABF REMOVED AND REPLACED INSERTS ON FLOOR PANEL 241ABF IAW B737-800 SRM 53-00-50 STEP 5 (S)(1-2) SEE AAR-ASR FORM SHOP TRAVELLER FOR WORK PERFORMED.
CORROSION ON LH WEB BTW STA 986.5 AND STA 1006 AT BL 45L .REMOVED AND REPLACED L/H WEB BS 986.5 TO 1006 L/H PER B737-800 SRM 51-40-02.
CORROSION ON Z CHANNEL BTW STA 1006 AND STA 986.5 AT BL 35L TO BL 40L REMOVED AND REPLACED Z CHANNEL ON BS 986.5 TO 1006 PER B737-800 SRM 51-40-02.
CORROSION ON SEVERAL POINTS AT RH CREASE BEAM WL 208 FROM STA 947.5 TO STA 1016 REMOVED AND REPLACED CREASE BEAM ON BS 947 TO 1016 PER B737-800 SRM 51-40-02.
CORROSION ON RH WEB ON STA 986.5 AT BL 45R WL 208 .REMOVED AND REPLACED WEB. ON BS 986.5 TO 1006 PER B737-800 SRM 51-40-02.
MULTIPLE CORRODE INSERTS ON FLOOR PANEL 221EF REMOVED AND REPLACED INSERTS ON FLOOR PANEL 221EF IAW B737-800 SRM 53-00-50 STEP 5 (S) (1-2) SEE AAR-ASR FORM SHOP TRAVELER FOR WORK PERFORMED
MULTIPLE CORRODED INSERTS ON FLOOR PANEL 221GF REMOVED AND REPLACED INSERTS ON FLOOR PANEL 221 GF IAW B737-800 SRM 53-00-50 STEP 5 (S) (1-2). SEE AAR-ASR FORM SHOP TRAVELER FOR WORK PERFORMED.
CORROSION ON T CAP BEAM ON STA 947.5 AT BL 25R TO BL 55R. REMOVED T CAP AND REPLACED T CAP ON STA 947.5 PER B737-800 SRM 53-70-51 REP 5.
CORROSION ON STRIP AT R1 DOOR CREASE BEAM BTW STA 312 AND STA 294.5 REMOVED AND REPLACED STRIP AT R1 DOOR CREASE BEAM BTW STA 312-294.5 ALL WORK DONE IAW B737-800 SRM 51-40-02, 51-40-05
CORROSION ON GALLEY SUPPORT FITTING ON STA 344 AT BL 47LH WL 208 REMOVE AND REPLACE GALLEY SUPPPORT FITTING ON STA 344 AT BL 47-LH WL 208 IAW B737-800 SRM 51-40-02 STEP 9 A AND B SCREW GUN 3879 DUE DATE 5-16-2020.
CORROSION ON FLOOR SUPPORT BTW STA 947.5 AND STA 968 AT BL 50R REMOVED AND REPLACED FLOOR SUPPORT BTW BS 947.5 TO 968 AT BL 50R PER B737-800 SRM 51-40-02.
MULTIPLE CORRODED INSERTS ON FLOOR PANEL 222CF REMOVED AND REPLACE INSERTS ON FLOOR PANEL 222CF IAW B737-800 SRM 53-00-50 STEP 5 (S) (1-2) SEE AAR-ASR FORM SHOP TRAVELER FOR WORK PERFORMED.
MULTIPLE CORRODED INSERTS ON FLOOR PANEL 222DF REMOVED AND REPLACED MULTIPLE INSERTS ON FLOOR PANEL 222DF IAW B737-800 SRM 53-00-50 STEP 5 (S) (1-2), SEE AAR-ASR FORM SHOP TRAVELER FOR WORK PERFORMED.
MULTIPLE CORRODED MISSING INSERTS ON FLOOR PANEL 241 ACF.REMOVED AND REPLACED INSERTS ON FLOOR PANEL 241 ACF IAW B737-800 SRM 53-00-50 STEP 5 (S) (1-2) SEE AAR-ASR FORM TRAVELER
MULTIPLE CORRODED INSERTS ON FLOOR PANEL 221DF REMOVED AND REPLACED INSERTS ON FLOOR PANEL 221DF IAW B737-800 SRM 53-00-50 STEP 5 (S) (1-2) SEE AAR-ASR FORM TRAVELER
MULTIPLE CORRODED INSERTS ON FLOOR PANEL 221CF REMOVED AND REPLACED INSERTS ON FLOOR PANEL 221CF IAW B737-800 SRM 53-00-50 STEP 5 (S) (1-2) SEE AAR-ASR FORM SHOP TRAVELER FOR WORK PERFORMED.
4 CORRODED INSERTS ON FLOOR PANEL 231AF REMOVED AND REPLACED 4 INSERTS ON FLOOR PANEL 231AF IAW B737-800 SRM 53-00-50 STEP 5 (S) (1-2), SEE AAR-ASR FORM SHOP TRAVELER FOR WORK PERFORMED.
MULTIPLE CORRODED INSERTS ON FLOOR PANEL 232AF REMOVED AND REPLACED INSERTS ON FLOOR PANEL 232AF IAW B737-800 SRM 53-00-50 STEP 5 (S) (1-2) SEE AAR-ASR FORM SHOP TRAVELER FOR WORK PERFORMED.
MULTIPLE CORRODED INSERTS ON FLOOR PANEL 232BF REMOVED AND REPLACED INSERTS ON FLOOR PANEL 232 BF IAW B737-800 SRM 53-00-50 STEP 5 (S) (1-2) SEE AAR-ASR FORM TRAVELER
MULTIPLE CORRODED INSERTS ON FLOOR PANEL 241 AAF.REMOVED AND REPLACE INSERTS ON FLOOR PANEL 241 AAF IAW B737-800 SRM 53-00-50 STEP 5 (S) (1-2) SEE AAR-ASR FORM SHOP TRAVELER FOR WORK PERFORMED.
MULTIPLE DAMAGED INSERTS ON FLOOR PANEL 241 ADF REMOVED AND REPLACE INSERTS ON FLOOR PANEL 241 ADF IAW B737-800 SRM 53-00-50 STEP 5 (S) (1-2) SEE AAR-ASR FORM SHOP TRAVELER FOR WORK PERFORMED.
MULTIPLE DAMAGED AND CORRODED INSERTS ON FLOOR PANEL 241ADF. REMOVED AND REPLACE INSERTS ON FLOOR PANEL 241 ADF IAW B737-800 SRM 53-00-50 STEP 5 (S) (1-2) SEE AAR-ASR FORM SHOP TRAVELER FOR WOEK PERFORMED
RT WING #8 SLAT ACTURATOR ATTACH POINT SKIN CRACKED, 5/8" LONG. PLACED ON GMM / MTI. ADDITIONAL INFORMATION TO BE PROVIDED.
ROW 24L EMERGENCY LIGHT INOP. ROW 14L EMERGENCY LIGHT INOP. R&R LAMP AT ROW 24L FOR THE EMERGENCY LIGHT. OPS CHECK GOOD AT THIS TIME. PLACED EMERGENCY LIGHT AT ROW 14L ON MEL. R&R LIGHT ASSY. OPS CHECK GOOD. THIS CLEARS MEL.
ACCOMPLISH RT INBOARD WING LEADING EDGE FASTENER HOLE DAMAGE REPAIR. REMOVED DAMAGE FROM SKIN. CUT OUT MEASUREMENT 4.250" X 1.250". HFEC INSPECTION OF THE TRIM EDGE REQUIRED. HFEC ACCOMPLISHED ON CUTOUT. NO CRACKS FOUND. STARTED TO FABRICATE FILLER OUT OF 2024 T3 .063 DOUBLER OUT OF 2024 T3.4EACH 1/4" HOLES REAMED TO .247. FINAL REAM IS .262. FINISHED REPAIR DOUBLER, ALODINED AND PRIMED, STARTED TO INSTALL DOUBLER, WORK REMAINING IS INSTALL RIVETS. INSTALLED REMAINING FASTENERS.
FOUND 31 LOOSE RIVETS ON LT WING UPPER INBOARD LEADING EDGE PANEL. REMOVED THE 31 LOOSE FASTENERS AND PREPARED AREA FOR NDT INSPECTION. HFEC OPEN HOLE AND COUNTERSINK INSPECTION ACCOMPLISHED. 4 EACH COUNTERSINKS CRACKED IN SKIN ONLY. MOVED PNEUMATIC MANIFOLD DUCT TO THE SIDE AND VACUUMED OUT SWARF. 4 CRACKED FASTENER HOLES WILL BE REPAIRED. FABRICATED FILLER BLOCK AND INSTALLED AT OUTBOARD FASTENER HOLE. STARTED INSTALLING FASTENERS REMOVED FOR INSPECTION. AWAITING FASTENERS THAT ARE AOG. INSTALLED REMAINING FASTENERS. NEEDS LEADING EDGE DUCT AND PANELS INSTALLED. PLACED NR 1 ENG STRUT PNEUMATIC DUCT INTO POSITION AND INSTALLED THE V-BAND CLAMP AT OUTTER CONNECTION POINT UNDER PNL. 431CR. PNL. 431CR REMAINS OFF FOR LEAK CHECK. INSTALLED PNEUMATIC STUT DUCT INBD OF NR 1 ENG. AND INSTALLED PANEL 511AB. PLACED NR 2 ENG. STRUT PNEUMATIC DUCT INTO POSITION AND INSTALLED THE OUTTER V- BAND CLAMP. ACCESS PNL. REMAINED OFF FOR LEAK CHECK. INSTALLED THE REST OF THE NR 2 STRUT PNEUMATIC DUCT. RESTORED ALL ACCESS AND LEAK CHECKED DUCT. INSTALLED PANEL 431CR. LEAK CHECKED NR 2 ENG. PNEUMATIC STRUT DUCT. INSTALLED NR 2 ENG. STRUT PNL.
ACCOMPLISH LT INBOARD WING LEADING EDGE FASTENER HOLE DAMAGE REPAIR. REMOVED SKIN DAMAGE. CUT OUT MEASUREMENT 4.250" X 1.250". HFEC INSPECTION REQUIRED. HFEC ACCOMPLISHED ON CUTOUT. NO CRACKS FOUND. FABRICATED REPAIR PARTS. .071" 2024-T3 DOUBLER AND .063" 2024-T3 FILLER. DRILLED AND REAMED FOR FASTENERS. RIVET HOLES ARE .192". !/4 HILOCKS ARE REAMED TO .262" AND 3/16 HILOCKS ARE REAMED TO.199". READY TO PRIME AND INSTALL. ALODINED AND PRIME BOTH DOUBLER AND FILLER. READY TO INSTALL. INSTALLED DOUBLER AND FILLER.
FOUND 28 LOOSE RIVETS ON R/H WING INBOARD UPPER LEADING EDGE PANEL. REMOVED THE 28 LOOSE FASTENERS AND PREPARED AREA FOR NDT INSPECTION. HFEC OPEN HOLE AND COUNTERSINK INSPECTION ACCOMPLISHED. 4 EACH COUNTERSINKS CRACKED IN SKIN ONLY. MOVED PNEUMATIC MANIFOLD DUCT TO THE SIDE AND VACUUMED OUT SWARF. 4 CRACKED FASTENER HOLES WILL BE REPAIRED. INSTALLED FASTENERS EXCEPT ONE, FABRACATED RADIUS BLOCK ALIDOINED AND PRIMED FOR THE REMAINING FASTNER. INSTALLED REMAINING FASTENER AND RADIUS BLOCK. ALL ACCESS RESTORED. LEAK CHECK OF DUCT WAS GOOD. CLOSED PANEL .
UPON FIRST SELECTION OF FLAPS A FLAP ASSEMTRY OCCURRED WITH LEFT FLAPS REMAINING IN THE UP POSITION RIGHT FLAP EXTEND ONE NEEDLES WIDTH. PERFORMED FSEU BITE TEST. FAULT CODE 27-53252 FLAP 3 SKEW. PERFORMED TE FLAP SUPPORT NR 3 SKEW PROBLEM. NO DEFECTS NOTED DURING VISUAL INSPECTION. ACCOMPLISHED FLAP SKEW DETECTION SYSTEM FUNCTION TEST. FOUND F3 SKEW SENSOR OUT OF RANGE. R&R NR 3 FLAP SKEW. SYSTEM OPS CHECK OK. NO FAULTS ON THE FSEU, ALL CLEAR.
NR 5 SLAT HAS A SMALL CRACK ON THE LOWER SKIN WHERE ACTUATOR BRACKET IS LOCATED. R & R THE NR 5 LE SLAT.
DURING WALKAROUND FOUND .45 INCH CRACK ON NR 1 L/E SLAT SKIN AT ACTUATOR ATTACH RIB. REMOVED AND REPLACED THE NR 1 L/E SLAT. OPS CHECKED GOOD.
DURING SPOILER INSPECTION FOUND RIGHT INBOARD AFT FLAP PROGRAMMING TRACK TO HAVE WEAR DAMAGE ON OUTER EDGES AND ON INNER SURFACE. DAMAGE IS PRESENT ON THE TOP EDGE OF THE PROGRAMMING TRACK EXTENDING ABOUT THREE INCHES. THE RUB BLOCK HAS WORN 1/16 OF AN INCH OF MATERIAL AWAY FROM THE TRACK AT ITS DEEPEST POINT AND IS NOT WITHIN REPAIRABLE LIMITS. THE BOTTOM OF THE TRACK HAS WEAR EXTENDING ABOUT FOUR INCHES AND HAS BEEN WORN AWAY BY THE RUB BLOCK THE SAME AS THE TOP. THE PROGRAMMING TRACK WILL REQUIRE REPLACEMENT. REMOVED INBOARD AFT FLAP TO FACILITATE REPAIR. INSTALLED NR 5 FLAP LINK. REPLACED NR 5 FLAP.
FOUND ANGLE UNDER PROGRAMING TRACK WORN RT FLAP. REPLACED FLAP.
DURING GROUND SPOILER INSPECTION, FOUND LEFT, AFT FLAP PROGRAM TRACK TO HAVE WEAR DAMAGE ON OUTER EDGES AND ON INNER SURFACE. DAMAGE IS PRESENT ON THE TOP EDGE OF THE PROGRAMMING TRACK EXTENDING ABOUT TWO AND A HALF INCHES. THE RUB BLOCK HAS WORN 1/16 OF AN INCH OF MATERIAL AWAY FROM THE TRACK AT ITS DEEPEST POINT AND IS NOT WITHIN REPAIRABLE LIMITS. THE BOTTOM OF THE TRACK HAS WEAR EXTENDING ABOUT THREE INCHES AND HAS BEEN WORN AWAY BY THE RUB BLOCK THE SAME AS THE TOP. THE PROGRAMMING TRACK WILL REQUIRE REPLACEMENT. REMOVED INBOARD AFT FLAP TO FACILITATE REPAIR. REMOVED FASTENERS FROM PROGRAMING TRACK. REMOVED AND REPLACED PROGRAM TRACK. REMOVED AND REPLACED RUB BLOCK. INSTALLED L/H INBOARD TRAILING EDGE FLAP.
FOUND ANGLE UNDER PROGRAMING TRACK WORN LT FLAP. REMOVED AND REPLACED WORN ANGLE.
APPEARS TO BE AN INCH & QUARTER CRACK IN THE LEFT LEADING EDGE DEVICE-LOCATED IN THE CENTER OF LE DEVICE NR 3. MC NOTIFIED. REFERENCE N/R ON W/O. REMOVED AND REPLACED NR 3 SLAT. SLAT PART NUMBER REMOVED IS 114A5030-3, SERIAL NUMBER IS 000794. DISASSEMBLED COVE PANELS AND REMOVED LOWER SKIN FASTENERS. CUT OUT DAMAGE. READY FOR NDT. MADE REPAIR PARTS (FILLER & DOUBLER)FROM .063 & .071 7075 T-6. NDT OF REPAIR CUTOUT AND OPEN HOLE INSPECTION AND COUNTERSINKS WAS PREFORMED, NO DEFECTS NOTED. OK TO INSTALL REPAIR. DRILLED UP AND STARTED TO COUNTERSINK DOUBLER. FASTENERS AND FILLER WASHERS IN AREA. ACCOMPLISHED RII INTERFACE INSPECTION OF AREA WHERE NR 3 SLAT WAS REMOVED. NO DISCREPANCIES NOTED. OK TO INSTALL REPLACEMENT SLAT. INSTALLED NR 3 SLAT. OPS CHECKS GOOD. COMPLETED RII OF NR 3 SLAT INSTALLATION.
FWD LAV FLOOR PANEL P/N 1415810-56 AFT O/B COMPOSITE IS BROKEN AND AFT EDGE SECTION MISSING POTTING MATERIAL, AN INSERT MISSING AND TOP SURFACE DELAM. REPAIRED FWD LAV FLOOR PANEL P/N 1415810-56 AND REPLACED MISSING INSERT.
RIGHT SIDE FRAME 951 INNER CHORD FWD SURFACE HAS A GOUGE. RT FRAME 951 MAIN PASSENGER CABIN INNER CHORD FWD SURFACE REPAIRED.
CREASE BEAM WEB BETWEEN FRAMES 927 TO 947 RIGHT SIDE HAS SEVERAL SPOTS OF CORROSION ON THE SURFACE AND IN THE FASTENER HOLES. FABRICATED NEW WEB BETWEEN FRAMES 927 TO 947 IN PASSENGER RT SIDE.
MAIN PASSENGER CABIN BS 947 RBL 59 UNDER AFT OUTBOARD LAV MOUNT CORRODED. REPAIRED MAIN PASSENGER CABIN STA 947 RBL 59.
MAIN PASSENGER CABIN FLOORBEAM BS 986 CORRODED IN MULTIPLE AREAS BL 0 TO RBL 24. REPAIRED THE FLOORBEAM.
MAIN PASSENGER CABIN BS 986 LBL 12 TO LBL 64 FLOORBEAM TEE CORRODED IN MULTIPLE AREAS. REPAIRED THE FLOORBEAM.
MAIN PASSENGER CABIN FWD FLOORBOARD HAS MULTIPLE INSERTS CORRODED. REMOVED AND REPLACED THE INSERTS.
MAIN PASSENGER L1 DOOR FWD GIRT BAR FITTING CORRODED AT BS 312 LBL 64. REMOVED AND REPLACED THE GIRT BAR FITTING .
MAIN PASSENGER CABIN FLOORBOARD FWD SIDE BROKEN. REPAIRED THE FLOORBOARD.
RIGHT SIDE HORIZ STAB PANEL 343AB FIN IS TORN. REPLACE FIN ON PANEL 343AB RT SIDE HORIZ STAB.
HORIZONTAL STAB PANEL 343AB, METAL SEALS WORN. REMOVED RT SIDE HORIZONTAL STAB PANEL 343AB METAL SEALS AND INSTALLED NEW SEALS.
VERTICAL STABILIZER LEADING EDGE NEEDS ATTACHING HARDWARE REPLACED. REPLACED DAMAGE OR MISSING HARDWARE ON VERTICAL STABILIZER LEADING EDGE.
RT WING LEADING EDGE PANEL 621CB HAS WEAR ON CORNERS. REPAIRED RT WING LEADING EDGE PANEL 621CB WEAR ON CORNERS.
RT WING PANEL 621KB HAS WEAR ON CORNERS. REPAIRED RT WING PANEL 621KB WEAR ON CORNERS.
RT WING PANEL 621 HB HAS WEAR ON CORNERS. REPAIRED RT WING PANEL 621 HB WEAR ON CORNERS.
RT UPPER WING TO BODY PANEL 195CR CRACKED IN LOWER TRAILING EDGE BEND. REPAIRED RT WING TO BODY PANEL 195CR.
RIGHT SIDE HORIZ STAB PANEL 343DB HAS A BAD NUT PLATE. REPLACED NUTPLATE RT SIDE HORIZ STAB PNL 343DB.
RIGHT SIDE HORIZ STAB PANEL 343AB METAL SEAL WORN THROUGH. REMOVED RT SIDE HORIZ STAB PANEL 343AB METAL GAP SEALS AND INSTALLED NEW SEALS.
RT FWD WET AREA, R1 DOOR ENTRY FLOOR PANEL P/N 1415810-76 HAS SEVERAL DENTS ON TOP SURFACE AND HAS SCRIBE LINES. REPAIRED RT FWD WET AREA R1 ENTRY FLOOR PANEL P/N 1415810-76.
RT FWD WET AREA, FLOOR PANEL P/N 1415810-228 TOP SURFACE DELAM AND MISSING AN INSERT. REPAIRED FWD WET AREA FLOOR PANEL P/N 1415810-228 AND REPLACED MISSING INSERTS.
RT FWD WET AREA, FLOOR PANEL P/N 1415810-141 FWD O/B INSERT HOLE DAMAGED AND INSERT MISSING, AND HAS SCRIBE LINES ON TOP SURFACE. REPAIRED RT FWD WET AREA FLOOR PANEL P/N 1415810-141 AND REPLACED MISSING INSERT.
RT FWD WET AREA, FLOOR PANEL P/N 1415810-142 TOP SURFACE DELAM. REPAIRED RT FWD WET AREA FLOOR PNL P/N 14115810-142 DELAMINATION. REPLACED ALL PANEL INSERTS.
RT FWD WET AREA, FLOOR PANEL P/N 141A5810-160 TOP SURFACE DELAM AND MISSING AN INSERT. REPAIRED RT FWD WET AREA FLOOR PANEL P/N 11A5810-160.
RT FWD WET AREA, AFT FLOOR PANEL P/N 1415810-144 SCRIBE MARKS ON TOP SURFACE. REPAIRED RT FWD WET AREA FLOOR PANEL P/N 1415810-144.
FWD WET AREA, AFT CENTER FLOOR PANEL P/N 141A5810-147 TOP SURFACE DELAM. REPAIRED FWD WET AREA AFT CENTER FLOOR PANEL TOP SURFACE DELAM.
LT FWD WET AREA, FLOOR PANEL P/N 1415810-158 TOP SURFACE DELAM AND POTTING MATERIAL MISSING ALONG THE O/B AND AFT EDGE SECTION. REPAIRED LT FWD WET AREA FLOOR PANEL TOP SURFACE DELAM + MISSING POTTING MATERIAL ALONG OB + AFT EDGE.
LT FWD WET AREA, FLOOR PANEL P/N 141A5810-158 TOP SURFACE DELAM AND POTTING MATERIAL MISSING AT FWD EDGE SECTION. REPAIRED LT FWD WET AREA FLOOR PANEL TOP SURFACE DELAM + POTTING MATERIAL AT FWD EDGE.
LT FWD WET AREA, L1 DOOR ENTRY FLOOR PANEL P/N 1415810-159 AFT AND I/B CORNER SECTION DELAM AND HAS SEVERAL NUT INSERTS ARE CORRODED. REPAIRED LT FWD WET AREA L1 DOOR ENTRY FLOOR PANEL AFT + 1B CORNER SECTION DELAM + INSERTS REPLACED.
LT FWD WET AREA, AFT OF L1 DOOR FLOOR PANEL P/N 1415810-183 FWD O/B CORNER AND TOP SURFACE DELAM. REPAIRED LT FWD WET AREA AFT OF L1 DOOR FLOOR PANEL FORWARD O/B CORNER + TOP SURFACE DELAM.
LEFT SEAT ROW 7 AND 9 OVERHEAD BIN BULL NOSE'S TWO EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHTS. OPS CHECKED GOOD.
L2 DOOR LOWER GATE PAN ASSY FWD BRACKET CRACKED. REMOVED AND REPLACED THE AFT BRACKET.
R2 DOOR LOWER GATE PAN ASSY AFT BRACKET CRACKED. REMOVED AND REPLACED THE GATE BRACKET.
FOUND LIGHTNING STRIKE DAMAGE ON FASTENER ON RT ELEVATOR T/E 8" FROM OTBD END. REMOVED FASTENER. INSTALLED RIVET.
FOUND LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT BS 285 BETWEEN STR 22R AND 23R. DRILLED OUT DAMAGE. NO CRACKS WERE NOTED. INSTALLED BLIND RIVET.
FOUND LIGHTNING STRIKE DAMAGE ON FASTENER AT BS 295.5 BETWEEN STR 22R AND 23R. DRILLED OUT FASTENER. NO CRACKS WERE NOTED. INSTALLED BLIND RIVET.
FOUND LIGHTNING STRIKE DAMAGE ON FASTENER AT BS 296.5 1" BELOW STR 21R. DRILLED OUT FASTENER. NO CRACKS WERE NOTED. INSTALLED BLIND RIVET.
FOUND LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT BS 311 BETWEEN STR 22R AND 23R. DRILLED OUT DAMAGED. NO CRACKS WERE NOTED. INSTALLED BLIND RIVET.
AFT LT OVERWING EMERGENCY LIGHTS FAILED CAPACITY FUNCTONAL CHECK. R & R BATTERY PACK AT POSITON AFT LT OVERWING.
R-1 EMERGENCY LIGHTS FAILED CAPACITY FUNCTONAL CHECK. R & R BATTERY PACK POSITION R-1.
FWD LT OVERWING EMERGENCY LIGHTS FAILED CAPACITY FUNCTONAL CHECK. R & R BATTERY PACK AT POSITON FWD LT OVERWING.
NINE INCHES OF GLOWSTRIP INOPERATIVE IN FRONT OF ROW 28DEF. R & R GLOWSTRIP AS REQUIRED.
CABIN WARNING HORN SOUNDED AT FL370. CABIN PRESSURE OBSERVED AT 10,000. RATE OF CABIN CLIMB WAS 500 FPM AND NOT CONTROLLABLE, O2 MASKS DEPLOYED. REMOVED ICE CONTAMINATION FROM OUTFLOW VALVE AND SURROUNDING AREA.
PLASTIC EXIT SIGN FELL OFF BETWEEN DOOR L1 AND FWD F/A JUMPSEAT. SECURED PLASTIC EXIT SIGN AT L1 DOOR.
DOOR EXIT SIGN FELL OFF BETWEEN L1 AND FWD F/A JUMPSEAT. SECURED PLASTIC SIGN.
DURING GVI IN FWD CARGO AFTER RT TRANSITION PANEL REMOVAL, FOUND INTERCOSTAL BS 500G-500H CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS. R & R THE INTERCOSTAL.
LEFT AFT LAVATORY HAS EVIDENCE OF CORROSION ON UNDERSIDE SURFACE OF FLOOR AND AFT WALL. BONDED PERMANENT REPAIRS TO LEFT AFT LAV, AFT INBD & OTBD, FWD INBD MOUNT BLOCKS AND AFT DOOR CELL REPAIR.
FLOORBEAM BS 296 HAS CORROSION ON UPPER SURFACE RBL 21 TO SIDE WALL. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED THE FLOORBEAM.
FLOORBEAM AT BS 887 IS CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED THE FLOORBEAM.
FLOORBEAM AT BS 986.5 IS CORRODED FROM L2 DOOR TO R2 DOOR ON TOP SURFACE. FOUND TO BE OUT OF LIMITS. REPLACED UPPER FLOORBEAM TEE.
FLOORBEAM IS CORRODED BS 360 RBL 48. BLENDED AND FOUND TO BE OUT OF LIMITS. REPAIRED THE FLOORBEAM.
FLOOR SUPPORT FROM BS 947.5 - 967 IS CORRODED. BLENDED CORROSION ON THE FLOOR SUPPORT AND FOUND IT TO BE OUT OF LIMITS. R & R THE FLOOR SUPPORT.
FWD CARGO BAY AFT BULKHEAD RT CAP STRIP LOCATED AT BS 500H-500I HAS SURFACE CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, R & R.
FWD LAVATORY FLOOR HAS CORROSION DAMAGE. REPAIRED.
FLOOR SUPPORT JUST AFT OF BS 947.5 LT SIDE IS CORRODED. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. R & R THE FLOOR SUPPORT.
AFT CARGO BAY RT FLOOR SUPPORT AT RBL 16 IS CORRODED FROM BS 767-887. REMOVED THE CORROSION AND FOUND IT TO BE OUT OF LIMITS. R & R THE FLOOR SUPPORT.
PASSENGER CABIN R1 DOOR SILL ANGLE IS CORRODED. BLENDED CORROSION AND FOUND IT TO BE OUT OF LIMITS. REMOVED AND REPLACED THE ANGLE.
FLOORBEAM BS 328 HAS CORROSION ON UPPER SURFACE AT APPROXIMATELY RBL 45. REPAIRED THE FLOORBEAM.
DURING GVI IN FWD CARGO BAY AFTER RT TRANSITION PANEL REMOVAL, FOUND RT AFT BULKHEAD LOWER SUPPORT INBD END CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R SUPPORT.
FLOOR SUPPORT FROM BS 947.5 - 986.5, RBL18 FOUND CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R THE FLOOR SUPPORT.
FLOORBEAM TEE AT BS 947.5 IS CORRODED AT LBL 6 AND RBL 6. BLENDED CORROSION AND FOUND IT TO BE OUT OF LIMITS. REPAIRED FLOORBEAM TEE.
CHANNEL CORRODED AT BS 990 INBD OF R2 DOOR. REMOVED CORROSION ON CHANNEL AND FOUND TO BE OUT OF LIMITS. R & R THE CHANNEL.
DURING GVI IN FWD CARGO AFTER RT TRANSITION PANEL REMOVAL, FOUND AN INTERCOSTAL BS 500H-500I CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R THE INTERCOSTAL.
DURING GVI IN FWD CARGO, AFTER RT TRANSITION PANEL REMOVAL, FOUND INTERCOSTAL BS 500E-500F CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. R & R INTERCOSTAL.
FLOOR WEB IS CORRODED IN CORNER AT BS 986.5 RBL30. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R THE WEB.
FLOOR SUPPORT AT R2 DOOR IS CORRODED FROM BS 947 - 996. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R THE FLOOR SUPPORT.
AFT CARGO BAY LT CAP STRIPS ARE CORRODED ON LOWER SURFACE. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED AND RESTORED FINISH.
AFT CARGO BAY LT FLOOR SUPPORT BS 727 - 727H HAD SEVERAL SPOTS OF SURFACE CORROSION. BLENDED CORROSION AND FOUND OUT OF LIMITS. R & R FLOOR SUPPORT.
AFT CARGO FLOOR SUPPORT AT BL 0 CORRODED AT BS 887. BLENDED THE CORROSION FOUND IT TO BE OUT OF LIMITS. FABRICATED AND INSTALLED A NEW FLOOR SUPPORT.
AFT CARGO BAY FLOOR SUPPORT BS 727H - 787 HAD SEVERAL SPOTS OF CORROSION. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R FLOOR SUPPORT.
AFT CARGO DOOR CUT OUT FWD WEB LOWER CLOSE OUT PLATE IS CORRODED ON LOWER SIDE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED NEW CLOSE OUT PLATE.
R2 DOORWAY HEADER EMERGENCY LIGHT HAS ONE BULB DAMAGED. R & R THE BULB.
AFT CARGO PIT FLOOR SUPPORT ATTACH STRAP BS 727D IS CORRODED. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED NEW STRAP.
AFT CARGO BAY FLOOR SUPPORT ATTACH STRAP BS 767 IS CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED NEW STRAP.
AFT CARGO PIT FLOOR SUPPORT ATTACH STRAP BS 727 IS CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED NEW STRAP.
AFT CARGO FLOOR SUPPORT AT RBL 22 IS CORRODED ON UNDERSIDE BETWEEN BS 787-793. THE FLOOR SUPPORT FOUND TO BE 100 PERCENT MATERIAL LOSS, R & R THE FLOOR SUPPORT.
AFT CARGO BAY TRANSITION PANEL AFT OF DOOR CUTOUT FROM BS 847-867 CORRODED ON UPPER AND LOWER SURFACE. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R TRANSITION PANEL.
DURING RT HORIZONTAL LOWER SKIN REPLACEMENT, FOUND NR 1 IN SPAR RIB STA 92.70 SECOND VERTICAL STIFFENER CRACKED. REPAIRED NR 1 IN SPAR RIB 2ND VERTICAL STIFFENER.
AFT CARGO BAY FLOORBEAM STRAP AT BS 887 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED A NEW STRAP.
AFT CARGO BAY RT TRANSITION PANEL BS 867-887 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R TRANSITION PANEL.
RIGHT FLOOR WEB IS CORRODED IN TWO PLACES BETWEEN BS 1006 & 1016. FLOOR WEB FOUND TO BE OUT OF LIMITS. R & R WEB.
FWD CARGO BAY RT FLOORBEAM CAP JUST AFT OF BS 500F HAS SURFACE CORROSION AND IS OUT OF LIMITS, R & R.
LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. ACCOMPLISHED FIM TASK & FOUND SWITCH S1060 STUCK IN DOOR OPEN POSITION WITH MANUAL EXT DOOR CLOSED. REPLACED S1060 & PERFORMED GEAR SWING. CHECKS GOOD.
EMERGENCY LIGHT INOPERATIVE. R & R THE EMERGENCY LIGHT POWER SUPPLY BATTERY PACK M1694 IAW AMM 33-51-06 BATTERY PACK TEST SATISFACTORY. R & R THE LT FORWARD OVERWING EXTERIOR EMERGENCY LIGHT LAMP.
MAIN RUDDER PCU BOLT BROKEN IN LINKAGE. FOUND DAMAGE TO HINGE RIB 66.42 AND 56.48. BLENDED OUT DAMAGE. RE-INSTALLED NEW MAIN RUDDER PCU. PERFORMED PENETRANT INSPECTION. AREA PREPPED AND PRIMED.
INTERCOSTAL FROM BS 312 TO 328 RBL 32 IS CRACKED AT FASTENER HOLE. CAN BE SEEN FROM MAIN E&E COMPARTMENT. REMOVED & REPLACED INTERCOSTAL.
AFT CARGO COMPARTMENT SMOKE DETECTION "A" LOOP WILL NOT TEST. MAINTENANCE RESET POPPED BREAKER. SYSTEM CHECKS GOOD.
R2 DOOR EMERGENCY LIGHTS INOP.