N804SY
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
R1 GIRT BAR HARD TO INSERT INTO BRACKET MC NOTIFIED JB 7665 ACTIVATED DOOR MOUNT ESCAPE SYSTEM THEN DEACTIVATED DOOR MOUNT ESCAPE SYSTEM AR R1 DOOR REF 25-66-00 NO ISSUE WITH INSERTS FOUND OK FOR SERVICE.
L2 LAV DOOR ASHTRAY IS LOOSE AND HAS SHARP EDGE. SECURED ASHTRAY AND REMOVED SHARP EDGES B737 CM 25-46-11
WHEN TROUBLESHOOTING INOP APU, DURING VOLTAGE CHECK OF FIM 49-40 TASK 816 THE WIRE LEAD SPARKED ON CONTACT WITH ELECTRICAL CONNECTOR D11114C SOCKET 55. PART OF THE LEAD FUSED TO THE INSIDE OF THE SOCKET. FORWARD LH FWD CARGO BULKHEAD REMOVED AS WELL AS THE LOWER BUNDLE TIE DOWNS ON THE BOTTOM OF E2-1 RACK TO PROVIDE ACCESS FOR THE BACK OF THE BLOCK. UNABLE TO REMOVE SOCKET 55 ON CONNECTOR D11114C.REMOVED LRU'S M279, M1653, M1710,M9 AND M1850. REMOVED E2-2 RACK ASSY F.O.M. PARTIAALY REMOVED CONNECTOR D11114C. CONNECTOR HAS DAMAGED SOCKET RETAINER. NEED NEW CONNECTOR P/N DPX3MA66565-252.
SEVERAL NO SMOKING / FASTEN SEAT BELT LIGHTS OUT. RELAMPED PER MM 33-25-00. OK FOR SERVICE.
1R DOOR PANEL COVERING SLIDE GAUGE FELL DOWN INSIDE PANEL. RESECURED ESCAPE SLIDE COVER WINDOW REF AMM 25-66-01. OK FOR SERVICE
DEFECT 815088: FLIGHT ATTENDANT REPORTS 1L WINDOW SAFTEY STRAP/SLIDE INDICATOR IS FRAYING RESOLUTION: RESECURED L1 WINDOW FLAG REF AMM 52-11-31 OKAY FOR SERVICE
1R SLIDE BRACKET LOOSE. ADJUSTED R1 DOOR SLIDE BRACKET REF AMM 25-66-01.
COFFEE HAS WEIRD/TOXIC/METALLIC TASTE. SERVICED H2O RAN FLUSHED COFFEE MAKER WATER NOW TASTE IS IK. REF 12-14-01 REV 86
ELONGATED HOLE ON FRAME STA 500D APPROX RBL 21 AT FWD CARGO COMPARTMENT FLOOR STRUCTURE. FRAME STA 500D APPROX RBL 21 AT FWD CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER B737-800 SRM 53-30-07-2R-1 REP. 1
HIDDEN DAMAGE: AFTER REMOVED RH SIDE PLATE, CORROSION AND ELONGATED HOLES ON INTERCOSTAL BTW STA 747 AND STA 767 S-25R WERE FOUND AT AFT CARGO COMPARTMENT IN REF NRC 00186 - - RESOLUTION: EMP 10001386 - INTERCOSTAL BTW STA 747 AND STA 767 S-25R WAS REPLACED PER B737-800 SRM 51-40-02-0G-0RE
AFTER REMOVED RH SIDE PLATE, ELONGATED HOLE WERE FOUND ON FRAME OF STA 727B, 727J, AND 747 BTW S-25R AND S-26R AT AFT CARGO COMPARTMENT IN REF NRC 00186 - HOLES ON FRAME OF STA 727B, 727J BTW S-25R AND S-26R WERE DRILLED TO NEXT SIZE PER B737-800 SRM 51-40-05-0G-0 AND FRAME STA 747 BTW S-25R AND S-26R AT AFT CARGO COMPARTMENT WAS REPAIRED PER B737-800 SRM 53-60-07-2R-2 REPAIR 2.
CORROSION IN ADAPTER PLATES (2EAS) OF FLOOR-MOUNTED ESCAPE SLIDE BRACKETS. ADAPTER PLATES OF FLOOR-MOUNTED ESCAPE SLIDE BRACKETS WAS REPLACED AND VERIFIED PER B737-800 AIPC 25-66-02-01 ITEM: 50.
INITIAL INSPECTION: PUNCTURE IN FLOOR CARGO ACCESS PANEL 140EF. - NEW FLOOR PANEL P/N 453A2610-20 WAS FABRICATED PER DWG: 453A2610 REV:K.
WO 80724, NR00046: BROKEN PLASTIC STRIP OF ESCAPE SLIDE PACK DOOR L2. PLASTIC STRIP OF ESCAPE SLIDE PACK DOOR L2 (2EA) WERE INSTALLED PER B737-800 SRM 51-40-02-0G-0.
CORROSION ON FITTING GIRT BAR FLOOR STRUCTURE OF DOOR L1 AT STA 312 ANDSTA 344, W1 AREA. FITTING GIRT BAR FLOOR STRUCTURE OF DOOR L1 AT STA 312 AND STA 344, W1 AREA WAS REPLACED PER B737-800 SRM 51-40-02-0G-0.
MISSING COTTER PIN ON ANCHOR FITTING OF BOTH EMERGENCY ESCAPE ROPE AT COCKPIT. COTTER PIN WAS INSTALLED ON BOTH EMERGENCY ESCAPE ROPE AT COCKPIT PER B737-800 AMM 25-61-10.
MISSING LADDER TIE & PIN OF ESCAPE SLIDE PACK DOOR L1, R1 & L2. LADDER TIE & PIN OF ESCAPE SLIDE PACK DOOR L1, R1 & L2 WERE VERIFIED AND INSTALED PER IPC 25-66-00-13 ITEMS 278 AND 280
INITIAL INSPECTION: CRACK ON FRAME STA 500H APPROX LBL 17.5 AT FWD CARGO COMPARTMENT FLOOR STRUCTURE - RESOLUTON:FRAME STA 500H APPROX LBL 17.5 AT FWD CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIR PER ETI-737-25-061 REV. 2 AND SCX MDDR 131702 LOG 812909 AND EA 11644
CRACK ON PRESSURE DECK WEB AT STA 663 & LBL 42, MLG WHEEL WELL. CRACK ON PRESSURE DECK WEB AT STA 663 & LBL 42, MLG WHEEL WELL WAS REPAIRED PER PER B737-800 SRM 57-10-10--2R-3 REPAIR. 3 AND B737-800 SRM 57-10-10-2R--6 REPAIR 6
EMERGENCY PATHWAY LIGHTS 28 C LOOSE. SECURED EMER PATHWAY LIGHTS 28C. REF: AMM 25-77-00
FLOOR LIGHTING STRIP ROW 27C LOOSE. RE-SECURED "GUIDE U" FLOOR TRACK LIGHTING STRIP AT SEAT ROW 27C REF AMM 27-51-00
CABIN 02 MASKS DEPLOYED DUE TO DEPRESSURIZATION. CLEANED AND RE-PACKED ALL CABIN O2 MASKS PER B737-800 AMM 35-22-31-100-801-001 AND REPLACED ALL DISCHARGED O2 GENERATORS IN CABIN PER B737-800 AMM 35-22-11-000/-400-801-101 ON SCA WO# 92890, N/R-00007.
CABIN DEPRESSURIZATION. BOTH PACK LIGHTS CAME ON, QRH CLEARED LIGHTS THEN THEY CAME ON AGAIN AT 1000MSL. PERFORMED DCPC BITE, FIM 21-53 TASK 820, FIM 21-31 TASK 803 NO FAULTS FOUND. C/W AMM 21-51-03-160-811 & TASK CARDS 21000001 & 21000002 HEAT EXCHANGER CLEANING. OPS CHECKS NORMAL. AMM 21-00-00-00-040-804 MMEL 21-1 DDG RESTORATION C/W. THIS CLEARS MEL 21-1-1-F
L1 DOOR FA MASK DIDN'T DEPLOY. EMERGENCY DECLARED. COMPLETED ALL T/S AND CLEANING OF BOTH AC PACKS ON NR0006. COMPLETED VISUAL INSPECTION OF CABIN O2 GENERATORS IAW B737 AMM 35-22-00-210-801, ALL GENERATORS DISCHARGED WITH THE EXCEPTION OF CABIN ROWS 9L/H, 18L/H, FWD LAV & AFT L/H LAV. COMPLETED CABIN PSU O2 GENERATOR REMOVAL & INSTALL IAW B737 AMM 35-22--11-000/400-801-001 COMPLETED ASU O2 GENERATOR REMOVAL & INSTALL ON L/H FWD, L/H & R/H AFT ASU'S, (R/H FWD NOT DISCHARGED) IAW B737 AMM 35-22-11-000/400-805-001 REMOVED AND REINSTALLED EMPTY LSU OXYGEN CYCLINDER PER SCA REP AFT RH LAV IS DEFERRED AND PART IS TO BE REPLACED AT MSP. COMPLETED INSPECTION OF ALL CABIN, F/A & LAV O2 MASKS IAW B737 AMM 25-22-31-- 210-801-001, NO DEFECTS NOTED COMPLETED CLEANING OF ALL CABIN F/A & LAV O2 MASKS IAW B737 AMM 35-22-31-100-801-001. COMPLETED PSU/ASU/LSU OXYGEN MASK PACKING IAW B737 AMM 35-22-31-100-801-001 ACTIVATED AND ARMED CABIN PSU O2 GENERATORS IAW B737 AMM 35-22-11-400-811-001 COMPLETED CABIN DEPRESSURIZATION CONDITIONAL INSPECTION IAW B737 AMM 05-51-81-210--801. GENERATOR R&R COMPLETED ON TASK STEP 2A. CONDITIONAL INSPECTION COMPLETED ON WIP STEP 6A.
DEFECT 794748: L1 DOOR FA MASK DIDN'T DEPLOY. (EMERGENCY DECLARED REF DEFECT 794747, ITEM 1 - CABIN DEPRESSURIZATION)
AFT LAV 2L MASK DIDN'T DEPLOY. EMERGENCY DECLARED. PERFORMED OPS CHECK ON SCA WO# 92890, N/R-00007, PER AMM 35-22-00-700-802. OPS CHECK GOOD.
DEFECT 719519: DOOR 1R GIRTBAR DIFFICULT TO STOW. RESOLUTION: 1R GIRT BAR NO DEFECTS NOTED REF AMM 25-66-01. OKAY FOR SERVICE
WORK ORDER 91005 NR00002: R/H EXTERNAL EMERGENCY SLIDE / WING LIGHTS ARE INOP. SEE TASK CARD 330100000 FIGURE 9 FOR LOCATIONS: R/H OVER WING EXIT LIGHTS AND LOWER AFT SLIDE LIGHT. - - RESOLUTION: RELAMPED PER AMM 33-51-04 . OPS CHECK GOOD
DEFECT 754311: DOOR 1L GIRT BAR BRACKET IS LOOSE - - - RESOLUTION: SECURED GIRT BAR BRACKET AT L-1 DOOR REF 25-66-02
DEFECT 754311: DOOR 1L GIRT BAR BRACKET IS LOOSE - - RESOLUTION: SECURED GIRT BAR BRACKET AT L-1 DOOR REF 25-66-02
DEFECT WO 85083 NRC00023: SLIDE L1 GIRT BRACKET SUPPORT RIVET SHEARED OFF, NEEDS REPLACEMENT. - RESOLUTION: REPLACED RIVIT PER SRM 51-40-02 AND INSTALLED PACK AND CLOSED CONTAINER PER AMM 25-66-01.
DEFECT WO 85083 NRC00018: R1 DOOR EXIT SIGN BATTERY PACK FAIL 15 MIN TEST. - RESOLUTION: REMOVED AND REPLACED FORWARD R/H BATTERY PACK FOR R1 DOOR EXIT SIGN NEW BATTERY TESTED GOOD REF WDM 33-51-12-3.
DEFECT WO 85083 NRC00019: L1 DOOR, SLIDE HOUSING, WINDOW FOR PRESSURE GAGE CRACKED. - RESOLUTION: INSTALLED NEW GAUGE COVER GLASS ON L1 DOOR, INSALLED PACK AND CLOSED CONTAINER PER 25-66-01.RII ACCOPLISHED DURING SLIDE PACK AND COVER BEING CLOSED, OK TO INSTALL ON DOOR. INSTALLED SLIDE PACK ON L1 DOOR PER AMM 25-66-01.
DEFECT WO 85083 NRC00021: L2 DOOR, SLIDE HOUSING,WINDOW FOR PRESSURE GAGE CRACKED. - RESOLUTION: INSTALLED GAUGE WINDOW GLASS, CLOSED CONTAINER PER AMM 25-66-01. RII ACCOMPLESED OF SLIDE IN CONTAINER AND CLOSING OF CONTAINER, OK TO INSTALL PACK ON DOOR. INSTALLED SLIDE PACK ON L2 DOOR PER AMM 25-66-01.
R1 DOOR, SLIDE HOUSING, WINDOW FOR PRESSURE GAGE CRACKED. - REMOVED L1 SLIDE PACK PER AMM 25-66-01, REPLACED GAUGE WINDOW PART # 69-45145-4. REINSTALLED SLIDE PACK PER AMM 25-66-01. VELCRO ON BOTTOM NEEDS TO BEATTACHED TO BOTTOM PLATE. INSPECTION NEEDED BEFORE CLOSING. RII ACOPLISHED DURING CLOSING OF SLIDE PACK, OK TO INSTALL PACK ONTO DOOR. INSTALLED SLIDE PACK ON R1 DOOR PER AMM 25-66-01.
DEFECT WO 85083 NRC00021: L2 DOOR, SLIDE HOUSING,WINDOW FOR PRESSURE GAGE CRACKED. - RESOLUTION: INSTALLED GAUGE WINDOW GLASS, CLOSED CONTAINER PER AMM 25-66-01. RII ACCOMPLESED OF SLIDE IN CONTAINER AND CLOSING OF CONTAINER, OK TO INSTALL PACK ON DOOR. INSTALLED SLIDE PACK ON L2 DOOR PER AMM 25-66-01.
ON APPRAOCH INSIDE T6 FINAL APPROACH WE SELECTED FLAPS FROM 30 TO 40 THE LEFT FLAP EXTENDED TO 40 + THE RIGHT ONLY TO 35 AFTER LANDING BOTH FLAPS WENT TO 40 AND BACK UP. PERFORMED FSEU BITE 27-51 TASK 802 FOUND FAULT MSG 27-52260 INTERMITTENT FAULT OF RH T/E FLAP SENSOR CYCLED T/E FPLAS NUMEROUS TIMES WITH ALL INDICATIONSNORMAL AND NO OTHER FAULTS DETECTED.
DEFECT WO 75103 NR00032: SUPPORT STIFFENER AT BS 663, LBL 30, WL 140 IS CRACKED ON THE LOWER END. P/N 111A1308-7 - - RESOLUTION: REMOVED STIFFENER P/N 111A1308 AT BS 663 LBL 30 WL 140 IAW SRM 51-40-02 57049R 10/17/2023 LOCATED AND DRILLED NEW STIFFENER P/N 111A1308-15 PO# 941846/1 IAW BOEING DWG 111A1000 REV:- OK TO INSTALL 57049R 10/17/2023 INSP 26 10/17/2023 INSTALLED NEW STIFFENER AT BS 663 LBL 30 WL 140 IAW SRM 51-40-02 AND BOEING DWG 111A1000 REV:-
DEFECT WO75105 NR00041: SECONDARY FINDING- RH WING LOWER TRAILING EDGE PANEL SUPPORT BEAM AT MID SPAN COMMON TO PANEL 661AB, BROKEN AT I/B END - - RESOLUTION: REMOVED AND REPLACED RH WING LOWER TRAILING EDGE PANEL, SUPPORT BEAM P/N: 115A3758Y10 PER SRM 51-40-02- G-0, REV 20, SRM 51-4-05-0G-0 REV 20, SRM 20-50-11-910-801 REV 20, BOEING DWG 115A3700 REV-, DWG 115A3712 REV B, (COMMON TC PANEL 661 AB).
DEFECT WO 75105 NR00007: N/R-00001 - DEFECT: MECH-676694: REPAIRED CRACK DAMAGE ON LH SIDE OF 663 BULKHEAD @ LBL 40 WL 160. - - RESOLUTION: REPAIRED CRACK DAMAGE ON LH SIDE OF 663 BULKHEAD AT LBL 40 WL 160 IAW SRM 51-70-04-2R-10.
DEFECT NRC00180: CORROSION ON WEB AT AFT WET AREA BS1016+10 LBL20 WL208. WORK TO BE ACCOMPLISHED ON CUSTOMER CARD ID 00210.
CORROSION ON WEB AT AFT WET AREA BS1016 TO BS1016+12 RBL6 TO RBL16 WL208. CORROSION ON WEB AT AFT WET AREA BS 1016 TO BS 1016 + 12 RBL 6 TO RBL 16 WL 208 WORK TO BE ACCOMPLISHED ON CUSTOMER CARD ID 00213, 728596 INTERIOR 5061 ATTACHED COPY
CORROSION ON FLOOR BEAM AT AFT WET AREA BS947 LBL4 TO RBL9 WL208. REMOVED & REPLACED THE DAMAGED T-CHORD & 1 EA ANGLE AND INSTALLED ALL THE REPAIR PARTS AT AFT WET AREA BS 947.5 LBL 4 - RBL 9 W/L 208 IAW SRM 53-70-51-2R-5 REPAIR 5
CORROSION ON WEB AT AFT WET AREA BS987+2 LBL44 WL208. FOUND CORROSION ON WEB AT BS 987 + 2, LBL 44, WL208 TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE LIMITS FUOND IN THE SRM. WEB IS REPAIRABLE BY REPLACEMENT. REMOVED AND REPLACED WEB AT AFT WET ATEA, BS 987 TO BS 1016, LBL 33 TO LBL 47, WL 208 PER SRM 51-40-02-OG-0 AND DWG 147A5700
CORROSION ON WEB AT AFT WET AREA BS987+2 RBL32 WL208. REMOVED & REPLACED THE DAMAGED WEB AT AFT WET AREA BS987 + 2, RBL 32 W/L 208 TO 1016 RBL 44 IAW SRM 51-40-02-OG-0 & DWG #147A5700
CORROSION ON TENSION STRAP AT AFT WET AREA BS1016+4 LBL27 WL208. REMOVED AND INSTALLED NEW STRAP AT AFT WET AREA BS 1016 + 4, LBL 27, WL 208 P/N 147A5714-3 I.A.W. SRM 51-40-02-OG-0 DWG NO 147A5700
CORROSION ON WEB AT AFT WET AREA BS1016 TO BS1016+14 LBL5 TO LBL16 WL208. REMOVED AND INSTALLED NEW WEB AT AFT WET AREA BS 1016 + 4, LBL5 - LBL16 WL208 P/N147A5712-5 I.A.W. ASRM 51-40-02-OG-0 DWG NO 147A5700
CORROSION ON TENSION STRAP AT AFT WET AREA BS1016+4 LBL17 WL208. REMOVED AND INSTALLED NEW STRAP AT AFT WET AREA BS 1016 + 4, LBL 17, WL 208 P/N 147A5714-4 I.A.W. SRM 51-40-02-OG-0 DWG NO 147A5700
CORROSION ON FLOOR SUPPORT AT AFT WET AREA BS947+10 LBL50 WL208. REMOVED & REPLACED THE DAMAGED FLOOR SUPPORT AT AFT WET AREA BS 947 + 10 LBL 50, W/L 208 IAW SRM 51-40-02 & DWG #147A5650
CORROSION ON FLOOR SUPPORT AT AFT WET AREA BS947+15 LBL25 WL208. REMOVED & REPLACED THE DAMAGED FLOOR SUPPORT AT AFT WET AREA BS 947 + 15 LBL 25 W/L 208 IAW SRM 51-40-02 & DWG #147A5650
FLOOR SUPPORT HAS MISS DRILL AT AFT WET AREA BS984 RBL15 WL208. REMOVED AND REPLACED FLOOR SUPPORT BTW B/S 967.00 TO B/S 986.50 RBL16. WL208 DUE TO FOUND OUT ALLOWABLE DAMAGE LIMITS IAW SRM 51-40-02 AND DWE 140A9870 REV:B.
CORROSION ON 987 FLOOR BEAM AT AFT WET AREA LBL44 TO RBL44 WL208. AIRCRAFT ARRIVED WITH CORROSION DAMAGE ON A PREVIOUS REPAIR THAT WAS ACCOMPLISHED TO THE TOP OF BS 987 FLOOR BEAM. FLOOR BEAM IS REPAIRABLE BY REPLACEMENT DUE TO NO ALLOWABLE DAMAGE FOR BS 987 FLOOR BEAM TOP CHORD REPAIR PARTS IN SRM REMOVED AND REPLACED BS 987 FLOOR BEAM TOP CHORD REPAIR PARTS, LBL 44 TO RBL 44, WL 208 PER SRM 53-70-51-2R-4 REPAIR 4
CORROSION ON TENSION STRAP AT AFT WET AREA BS1016+4 RBL27 WL208. REMOVED AND INSTALLED NEW STRAP AT AFT WET AREA BS 1016+4, RBL 27, WL 208 P/N 147A5714-3 I.A.W. SRM 51-40-02-0G-0 DWG NO. 147A5700
CORROSION ON TENSION STRAP AT AFT WET AREA BS1016+4 RBL3 WL208. REMOVED AND INSTALLED NEW STRAP AT AFT WET AREA BS 1016 + 4, RBL 3, WL 208 P/N 147A5714-4 I.A.W. SRM 51-40-02-OG-0 DWG NO 147A5700
CORROSION ON TENSION STRAP AT AFT WET AREA BS1016+10 RBL17 WL208. REMOVED AND INSTALLED NEW STRAP AT AFT WET AREA BS1016 + 10, RBL 17, WL 208 P/N 147A5714-5 I.A.W. SRM 51-40-02-OG-0 DWG NO 147A5700
CORROSION ON WEB AT AFT WET AREA BS1016+4 RBL25 WL208. REMOVED AND INSTALLED NEW WEB AT AFT WET AREA BS 1016 + 4 RBL 25, WL 208 P/N 147A5712-4 I.A.W. ASRM 51-40-02-OG-0 DWG NO 147A5700
CORROSION ON TENSION STRAP AT AFT WET AREA BS1016+4 LBL3 WL208. REMOVED AND INSTALLED NEW STRAP AT AFT WET AREA BS 1016 + 4, LBL 3, WL 208 P/N 147A5714-5 I.A.W. SRM 51-40-02-OG-0 DWG NO 147A5700
SCRATCH MARKS ON AFT WET AREA FLOOR SUPPORT BS947+4 LBL18 TO LBL38 WL208. REMOVED & REPLACED THE DAMAGED FLOOR SUPPORT AT THE AFT WET AREA BS947+4 LBL18 TO LBL38, W/L208 IAW SRM 51-40-02 & DWG #147A5650
CORROSION ON FLOOR SUPPORT AT AFT WET AREA BS947+3 RBL47 WL208. REMOVED & REPLACED THE DAMAGED FLOOR SUPPORT #147A5676-6 IAW SRM 51-40-02 & DWG #147A5650 BS 947 + 3 RBL 47, W/L 208
CORROSION ON WEB AT AFT WET AREA BS1016+6 RBL16 WL208. CORROSION ON WEB AT AFT WET AREA BS 1016 + 6 RBL 16 WL 208. WORK TO BE ACCOMPLISHED ON CUSTOMER CARD ID 00213. 728596 INTERIOR 5061 ATTACHED COPY
DEFECT 760473: 1R DOOR BRACKET THAT HOLDS SLIDE WHEN ITS DISARMED IS LOOSE. - - - RESOLUTION: ADJUSTED 1R DOOR GIRT BAR RETAINER CLIP. OPS CHECKS GOOD. REF AMM 25-66-01.
DEFECT 701410: AFTER TAKEOFF ALL 3 GEAR LIGHT STAYED RED WITH GREEN DOWN INDICATIONS COULD NOT GET GEAR UP. DECLARED EMERGENCY- - - RESOLUTION: REMOVED AND REPLACE LANDING GEAR SELECTOR VALVE IAW. AMM 32-31-51 PB. 401 OP[S CHK. GOOD NO DEFECTS NOTED AT PRESENT TIME.
DEFECT 742407: L1 DOOR SLIDE PACK SMALL STRING WITH PIN ATTACHED IS HANGING LOOSE FROM PACK. - - - RESOLUTION: INSTALLED PIN IAW AMM 25-66-00.
DEFECT WORK ORDER 77806: R2 DOOR EXTERNAL EMERGENCY LIGHT INOP. RESOLUTION: REMOVED AND REPLACED FUSE ON AFT GALLEY RH POWER PACK ASSY IAW AMM 33-51-03. OPS CHECK GOOD.
DEFECT WORK ORDER 77806: 4 FED CABIN EMERGENCY LIGHT INOP.. RESOLUTION: REMOVED AND REPLACED FUSE ON FWD GALLEY RH POWER PACK ASSY IAW AMM 33-51-03. OPS CHECK GOOD.
LH VAPOR BARRIER HAS A CRACKED ANGLE AT BS 663, LBL 10, WL 150. RECEIVED STIFFENER ITEM: HFAB53-SF-012 LOCATED AND DRILLED NEW STIFFENER IAW SRM 51-40-02 AND BOEING DWG 111A1301 REV:A, APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW AMM 51-21-41 AND AMM 51-21-72, THE INSTALLATION WILL BE CARRIED OUT UNDER THE WORK ORDER CARD ID #00106 728596 FUSELAGE 5002 ITEM NO. 22 ATTACHED COPY
DEFECT W/O 77393 NR00002: GALLEY DOOR L2 LEFT HAND ESCAPE SLIDE GIRT BAR SKIRT DRAGS ON LOWER DOOR SILL RESOLUTION: REPOSITIONED L2 DOOR SLIDE GIRT BAR SKIRT PER AMM 25-66-00
DAMAGE TO L/H O/B FLAP UNDER I/B FAIRING. REPAIRED 2.2"X1.5" GOUGE TO L/H O/B FLAP UNDER I/B FAIRING IAW B737-800 SRM 51-70-10-2R4 REPAIR 4& B737-800 SRM 5170-102R-0 REPAIR GENERAL. RESTORED FINISH IAW B737-800 AMM 51-21-73-370-803.
LEFT HAND SIDE WING,SEAL SUPPORT ASSEMBLY HAS GOUGE ON LOW SURFACE LOCATED INBOARD FLAP AT INBOARD SIDE BY THE FUSELAGE. REMOVED AND REPLACED SEAL SUPPORT ASSEMBLY AFT L/H SIDE WING PLATE PER B737-800 SRM 51-40-02.
GOUGE ON LOW SURFACE OF SEAL SUPPORT ASSEMBLY AT RIGHT HAND SIDE WING,INBOARD FLAP,INBOARD SIDE BY A FUSELAGE. REMOVED AND REPLACED SEAL SUPPORT ASSEMBLY AT R/H SIDE WING PLATE PER B737-800 SRM 51-40-02.
FWD CARGO RH FLOOR TO SIDEWALL SUPPORT HAS SIGNS OF CORROSION FROM STA 500E TO 500G. REMOVED AND REPLACED FWD CARGO R/H FLOOR TO SIDEWALL SUPPORT PER B737-800 SRM 51-40-02- ON BS 500B TO 500I.
A CRACK APPROXIMATELY 3/4 INCHES UNDERNEATH A WEATHER RADAR SUPPORT FLATFORM AT RIGHT SIDE IN EE BAY JUST FWD OF EE BAY DOOR. REPAIRED WEATHER REDAR SUPPORT PLATFORM IN EE BAY IAW B737-800 SRM 51-20-13-2R REP. 1.
6" CRACK ON BOTTOM SIDE OF PANEL 661AB. ONE PUNCTURE ON BOTTOM SIDE OF 661AB MEASURING 1"X1" AND A 1"X .5" GOUGE. REPAIRED 6" CRACK 1"X1" PUNCTURE AND 1.5"X.5" GOUGE ON BOTTOM SIDE OF PANEL 661AB IAW B737-800 SRM 51-70-04 REPAIR 11 AND SRM 51-70-04 REPAIR 2.
FOUND DENT IN AFT CARGO DOOR DENT IS 2" LONG BY 1" WIDE AND .070" DEEP. REMOVED AND REPLACED AFT CARGO DOOR EXTERIOR SKIN FOR B737-800 SRM 51-40-02.
#1 ENG R/H T/R AT NAS STA 235 AND WL 73" HAS BURN MARK. REPAIRED #1 ENG R/H T/R AT NAS STA 235 AND WL 73" IAW B737-800 SRM 51-70-08, PARA. 3., A,-6. RESTORED PAINT FINISH IAW 51-21-44-300-802 PARAGRAPH 3C(1)(A-C) AND AMM 51-21-73 PARAGRAPH E.
THERE IS GOUGE ON A DOUBLER AT FWD OF RIGHT SIDE OF PANEL 192CR-2 LOCATED BOTTOM SIDE FUSELAGE,AIR CONDITIONING BAY AREA. REMOVED AND REPLACED DOUBLER AT FWD R/H OF PANEL 192CR-2 PER B737-800 SRM 51-40-02.
FIBERGLASS PANEL HAS 2 CRACKS,ONE IS APPROXIMATELY 3" AT UPPER JUST ABOVE A LEFT HAND KEEL BEAM AND OTHER IS APPROXIMATELY 4" ADJACENT TO KEEL BEAM LOCATED LEFT MAIN WHEEL WELL FWD. REPAIRED 2 4" CRACKS ON VAPOR BARRIOR WEB PN:111A1141 IAW B737-800 SRM 57-10-10 ID AND ALLOWABLE DAMAGE #2 AND B737-800 SRM 51-70-04 REPAIR 10.
REPAIR TO CRACK ON WEB CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK WEB BETWEEN RBL 40 AND RBL 45 STA 663 IS TEMP REPAIR. REMOVED THE DAMAGED PART OF THE WEB, PERFORMED A DETAIL INSPECTION OF THE REPAIR AREA, FABRICATED, LOCATED, DRILLED, AND INSTALLED REPAIR PARTS INSPECTION REQUIREMENTS FOR A CATEGORY B REPAIR ALTERNATIVE 2 AS PER B737-800 SRM 57-10-10 REPAIR 3 AND TABLE 204.
AT L1 UNDER MOP SILL, CORROSION UNDER PANEL 221DF, SUPPORT STRUCTURE BETWEEN THE TWO DRAINS, MARKED A5/027. REMOVED AND REPLACED MOP SILL ON L-1.
STATION 986.5, IN FRONT OF R2, CORROSION ON THE "T" CAP OF STAATION ABOUT 3 FEET INBOARD, MARKED WITH STREAMER A5/038. REPAIRED FLOORBEAM @ STATION 986.5 FROM L-2 TO R-2 DOOR.
RIGHT WING PANEL 651FB ALL 5 OF THE ATTACH RODS ARE CORRODED. REMOVED AND REPLACED RIGHT WING PANEL 651FB ATTACHMENT RODS.
LEFT WING PANEL 551GB ATTACH RODS ARE CORRODED. REMOVED AND RELACED ATTACH RODS AT LEFT WING PANEL 551GB.
FWD CARGO DOOR SILL HAS CORROSION. DOT BC56. REMOVED DAMAGED WEB FWD CARGO DOOR. FABRICATED AND LOCATED AND DRLLED NEW WEB, TREATED AND PRIMED NEW WEB. INSTALLED NEW WEB.
PANEL 241VF, IN FRONT OF R2, PANEL IS DELAMENATED ON THE AFT SIDE OF PANEL, MAREKED WITH STREAMER A5/037. REPAIRED DELAMINATED ON AFT SIDE PANEL 241VF.
AFT LOWER CORNER OF AFT CARGO SEALPLATE CRACKED. REMOVED AND REPLACED AFT LOWER CORNER OF AFT CARGO SEAL PLATE.
CORROSION FOUND UNDER AFT CARGO DOOR SEALPLATE. REMOVED AND REPLACED WEB ON AFT CARGO DOOR SURROUND LWR MAIN SILL.
CORROSION ON FASTENER HOLES AT STA 807 AND ST 25L FLOORBEAM IN AFT CARGO. REMOVED AND REPLACED "2" ANGLE SUPPORT ON STA 807 AND 847.
CORROSION UNDER R-1 DOOR SCUFF PLATE SUPPORT STRUCTURE AT LOWER CUTOUT, FROM STA 222A TO STA 333.1 AT STRINGER 17-R. REMOVED AND REPLACED R-1 DOOR MOP SEAL.
R-2 DOOR SCUFF PLATE ATTACH STRIP HAS CORROSION. DOT BS57. REMOVED & REPLACED R-2 DOOR SCUFF PLATE ATTACH STRIP.
L-2 DOOR SCUFF PLATE ATTACH STRIP HAS CORROSION. DOT BC58. REMOVED AND REPLACED L-2 DOOR MOPSEAL.
FLOOR PANEL 241 ACF, AFT GALLEY, AFT OF L2 DOOR, CORNER IS BROKEN, MARKED WITH STREAMER A5032. REPAIRED FLOOR PANEL 241 ACF CORNER.
AFT GALLEY, LT SIDE, UNDER FLOOR PANEL 241 ACF, GALLEY SUPPORT MOUNT STRUCTURE IS CORRODED, MARKED WITH STREAMER A5/033. REMOVED AND REPLACED GALLEY SUPPORT MOUNT ON LT SIDE.
UNDER FLOOR PANEL 241ABF, STATION 986.5, THERE ARE FOUR SCREW HOLES THAT HAVE A LIGHT CORROSION ON TOP OF STATION, MARKED A5/034. T-CAP REPAIR COMPLETED.
PANEL 241ADF, RT SIDE, AFT GALLEY, AFT OF R2 DOOR, PANEL HAS 8 BAD INSERTS. ALL MARKED WITH STREAMER A5/035. REPLACED 8X BAD INSERTS IN PANEL 241 ADF.
PANEL 241VF, IN FRONT OF R2 DOOR, AFT SIDE OF PANEL, SEVERAL BAD INSERTS, MARKED WITH STREAMER A5/036. REMOVED AND REPLACED FIVE BAD INSERTS ON PANEL 241 VF.
PANEL 242TF HAS 3 SCREW INSERTS, HAS LIGHT SURFACE CORROSION ON TOP INSERTS, MARKED WITH STREAMER A5/041. REPLACED 3 INSERTS ON PANEL 242 TF.
PANEL 241ABF IN FRONT OF L2, SEVERAL SCREW INSERTS ARE CORRODED THROUGH OUT PANEL, LOOK ON BOTH SIDES OF PANEL AROUND THE DRAIN PAN, MARKED WITH STREAMER A5/044. REMOVED 12 SCREW INSERTS THAT WERE CORRODED ON PANEL 241 ABF AND INSTALLED 12 SCREW INSERTS.
PANEL 241AAF, HAS A COUPLE OF SCREW INSERTS THAT ARE CORRODED, MARKED WITH STREAMER A5/045. REPLACED 2X INSERTS IN PANEL 241 AAF.
FWD GALLEY, RT SIDE, AFT R1 FLOOR PANEL "SAM 1" HAVE SEVERAL BAD INSERTS, MARKED A5/020. REPLACED 10X INSERTS TO FWD GALLEY RT SIDE AFT R1 FLOOR PANEL.
FWD GALLEY, AFT OF R1 DOOR, FLOOR PANEL 220 BAD INSERT MARKED WITH STREAMER A5/021. REMOVED AND REPLACED ONE BAD INSERT ON PANEL 220DF.
FWD GALLEY, AFT OF R1 DOOR, GALLEY ATTACHING SUPPORT BRACKET SEVERLY CORRODED. LOCATED IN FWD GALLEY AFT OF R1 DOOR, LAYING ON THE FLOOR. MARKED A5/022. FABRICATED NEW SUPPORT BRACKET.
PANEL 221 CF, FWD GALLEY, CENTER OF AIRCRAFT HAS A BAD INSERT. MARKED A5/023. REMOVED AND REPLACED BAD INSERTS ON PANEL 221 CF.
PANEL 222BF HAS TWO BAD INSERTS MARKED WITH STREAMER, PANEL IS LOCATED IN AIRCRAFT A5/024. REMOVED AND REPLACED TWO BAD INSERTS ON PANEL 222BF.
PANEL 221DF HAS 3 BAD INSERTS; 2 BETWEEN THE TWO DRAINS ON PANEL AND ANOTHER BAD INSERT OPPOSITE END OF PANEL A5/025. REMOVED AND REPLACED 4 INSERTS ON PANEL 221DF.
UNDER THE L1 SCUFF PLATE, THERE IS CORROSION IN SEVERAL AREAS ON SUPPORT STRUCTURE FOR SCUFF PLATE. MARKED A5/026. REMOVED AND REPLACED ANGLE SUPPORT UNDER THE SCUFF PLATE.
AFT OF THE L1 DOOR, SMALL SKINNY PANEL HAS A BROKEN CORNER ON THE PANEL, MARKED WITH STREAMER A5/030. REPAIRED SMALL SKINNY PANEL BROKEN CORNER DELAMINATION ON PANEL; AFT OF THE L1 DOOR. INSTALLED 1 INSERT THAT WAS REMOVED.
THE R1 WINDOW FRAME HAS A CRACK ON THE UPPER OUTER CORNER, MARKED WITH STREAMER A5/046. REF W/O AND CUSTOMER CARD REPAIRED.
EMERGENCY ASILE LIGHTS AT ROWS 6 TO 11 INOP. EMERGENCY ASILE LIGHT AT ROW 4 AND R1 DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK @ ROW 8 DEF. EMERGENCY LIGHTS CHECK GOOD. REPLACED BATTERY CHARGER @ L1 OVERHEAD. EMERGENCY LIGHTS CHECK GOOD.
LEFT MLG FWD TRUNNION PIN HAS CORROSION. REPAIRED.
RT MAIN LANDING GEAR FWD TRUNNION PIN HAS CORROSION PITTING. REMOVED RT MLG TO FOM. REMOVED RT FWD TRUNNION BEARING ASSEMBLY TO FOM. REMOVED AND REPLACED RT MAIN LANDING GEAR FWD TRUNNION PIN. INSTALLED RT FWD TRUNNION BEARING ASSEMBLY. INSTALLED RT MLG. OPS CHECK AND LEAK CHECK IS GOOD.
FLOOR EMERGENCY LIGHT INOPERATIVE. R & R THE FEEDER CABLE ASSY. OPS CHECKED GOOD.
LT STABILIZER, RIB CRACKED AT BS 101.9, 3RD STIFFENER AFT. CUT OUT DAMAGE ON 3RD STIFFENER AFT AT STABILIZER BS 101.9 RIB AND REPAIRED.
CABIN, DOOR 2 LT, UPPER FORWARD STOP PIN FITTING IS GOUGED. R & R UPPER FWD DOOR STOP FITTING ON AFT ENTRY DOOR, L-2. PERFORMED ADJUSTMENT TEST TO STOP. OPS CHECK GOOD.
BS 344 TO 360, BL 0 INTERCOSTAL HAS CRACK AT AFT FLOORBOARD PANEL ATTACH HOLE. R & R CRACKED INTERCOSTAL AT BS 344-360, BL0.
RIGHT WING DEFLECTION, RIB LOWER ATTACH POINT IS BROKEN. REMOVED BROKEN LUG, EDDY CURRENT AFFECTED AREA, NO DEFECTS NOTED, ROTORY FLAP PEENED REPAIR AREA, TREATED AND PRIMED, DRILLED REPAIR FITTING AND INSTALLED.
LEFT WING DEFLECTION RIB LOWER ATTACH POINT IS WORN. LT WING DEFLECTION RIB LOWER ATTACH POINT IS WORN, REMOVED WORN EXISTING LUG, EDDY CURRENT AFFECTED AREA, NO DEFECTS NOTED, ROTORY FLAP PEENED AREA. TREATED & PRIMED, DRILLED REPAIR FITTING AND INSTALLED.
LAV A THRESHOLD INSERTS ARE CORRODED. REPLACED 4 EA LAV A THRESHOLD INSERTS.
LEFT WING DEFLECTION, RIB UPPER ATTACH POINTS ARE WORN. LT WING DEFLECTION RIB UPPER ATTACH POINTS ARE WORN, BLENDED WORN AREA, FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGED AREA, DRILLED & FABRICATED FILLER, DOUBLER, SERRATED PLATE, HFEC FOUND NO DEFECTS NOTED, TREATED, PRIMED TOP COAT, INSTALL ALL REPAIRS IAW SRMS.
FLOORBOARD, IN AFT WET AREA HAS A CRACK ON THE INBD AFT CORNER. REPAIRED FLOORBOARD.
RT HORIZONTAL STABILIZER, STAB STA 92.7, 20" FORWARD OF AFT SPAR. RIB IS CRACKED. TRIMMED OUT DAMAGE AT RIB STIFFENER 20" FWD OF AFT SPAR ON RT HORIZONTAL STABILIZER BS 92.7 AND REPAIRED RIB.
LEFT PACK BAY RAM AIR EXHAUST DUCT FUSELAGE SEAL BRACKET IS CRACKED. REPLACE CRACKED EXHAUST DUCT BRACKET WITH NEW.
LOWER FUSELAGE PANEL 193D HAS A BROKEN NUTPLATE. R & R LOWER FUSELAGE PANEL 193D BROKEN NUTPLATE.
CABIN FLOOR STRUCTURE BETWEEN BS 312 AND BS 328, LBL 47 FLOOR SUPPORT HAS CRACK AT HOLE ON TOP SIDE. R & R CRACKED FLOOR SUPPORT.
LT RAM AIR DOOR, GUIDE BRACKETS 1 WORN, 1 BROKEN. INSTALLED NEW GUIDE BRACKETS ON LT RAM AIR DOOR.
LEFT RAM AIR DOOR, 2 EA ATTACH LINKS CRACKED. INSTALLED NEW 2 NEW LT RAM AIR DOOR ATTACH LINKS.
AD DRIVEN, RT MLG INBD HINGE DOOR, AFT HINGE FITTING, 2 CRACKS IN HINGE FITTING AT ATTACH FASTENER, ENDS OF CRACKS MARKED IN BLACK, IAW TASK CARD INSTRUCTIONS; ACCOMPLISH TASK CARD. ACCOMPLISHED TASK CARD.
VAPOR BARRIER CRACKED, ABOVE LT RAM AIR EXHAUST. REPAIRED VAPOR BARRIER FIBERGLASS ABOVE LT RAM AIR EXHAUST.
RT WING LOWER T/E PANEL 651FB HAS A BENT SUPPORT ROD ON THE INBD FWD CORNER. R & R R/H WING LOWER T/E PANEL 651 FB INBD FWD SUPPORT ROD.
LT HORIZONTAL STABILIZER, RIB CRACKED AT BS 101.9, 2ND STIFFENER AFT. CUTOUT DAMAGE AT 2ND STIFFENER AFT ON STAB BS 101.9 RIB AND REPAIRED.
EMERGENCY LIGHT ON SEAT 16C INOPERATIVE. TIGHTENED CONNECTOR, OPS CHECK GOOD.
SEAT TRACK AT BS 727B, LBL 45 INBD AND OTBD FLANGES HAVE CRACKS. REPARIED.
BS 727B, SPLICE STRAP LOCATIONS AT LBL 24.75, RBL 24.75, AND RBL 45.50. REQUIRE REPAIR. REPAIRED DAMAGED COUNTERSINKS.
SEAT 29ABC EMERGENCY LIGHT INOPERATIVE. R & R SEAT 29ABC EMERGENCY LIGHT.
CABIN EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED THE LAMPS.
FOUND LT AND RT BATTERY PACKS AT STATION 727, FORWARD OF LT AND RT FORWARD ESCAPE HATCHES AND BATTERY PACKS THAT CONTROL THE LIGHT AROUND THE FORWARD ENTRY & SERVICE DOORS FAILED THE TEST.
LEFT FUSELAGE STA 500B FRAME HAS A GOUGED SPOT APPROX 12 IN ABOVE FLOOR. REPAIRED LT FUSELAGE FRAME STA 500B APPROX 12" ABOVE FLOOR.
AFT WET AREA AFT FLOOR SILL WEB UPPER SURFACE HAS SEVERAL CORROSION SPOTS. REPAIRED AFT SILL WEB.
AFT CARGO BAY RIGHT FLOORBEAM AT FRAME 794.3 TO 847 CORRODED. REMOVED AND REPLACED FRAME FROM 777 TO 859.
AFT CARGO BAY RIGHT FLOORBEAM AT FRAME 794.3 TO 847 CORRODED. REMOVED AND REPLACED FLOORBEAM.
FOUND INTERCOSTAL BETWEEN BS 500F - 500G CRACKED AT STRINGER. REMOVED AND REPLACED INTERCOSTAL.
AFT WET AREA RBL32 FLOOR SUPPORT FRAME STA 992.8 - 1016 HAS SEVERAL CORROSION SPOTS AROUND SCREW HOLE TOP UPPER AND LOWER SURFACES. REMOVED AND REPLACED FLOOR SUPPORT STA 992.8 - 1016 LBL32 AFT WET AREA.
FORWARD PIT BAFFLE CORRODED ON O/B SIDE AT S-27L AND STA 500H. REMOVED AND REPLACED BAFFLE AT STR-27L STA 500H.
WET AREA FLOOR SUPPORT FRAME STA 992.8 - 1016, LBL 32 HAS CORROSION SPOT ON UPPER SURFACE AND AROUND SEVERAL SCREW HOLES. REMOVED AND REPLACED FLOOR SUPPORT FRAME 992.8 - 1016 LBL 32.
AFT WET AREA FLOORBEAM STA 986 SEVERAL CORROSION SPOTS AROUND SCREW HOLE TOP AND BOTTOM SIDES. T-CAP REPAIR. REPAIRED FLOORBEAM.
FORWARD PIT S-26L STRINGER CLIP CRACKED AT STA 500I. REMOVED AND REPLACED STRINGER CLIP AT STA 500I S-26L.
FORWARD CARGO BAY LEFT INTERCOSTAL AFT SUPPORT BRACKET CRACKED FORWARD SIDE OF STA 500H AT LBL21. REMOVED CRACKED SUPPORT BRACKET. INSTALLED NEW BRACKET.
FWD CARGO BAY LEFT INTERCOSTAL FWD SUPPORT BRACKET CRACKED AFT OF STA 500G AT LBL21. REMOVED CRACKED SUPPORT BRACKET. INSTALLED NEW SUPPORT BRACKET.
FORWARD PIT S26R STRINGER CLIP CRACKED AT STA 500I. REMOVED AND REPLACED STRINGER CLIP AT STA 500I.
FORWARD PIT BAFFLE BRACKET CORRODED AT STA 500H AND S-27L. REMOVED AND REPLACED BAFFLE BRACKET AT 500H AND S-27L.
AFT WET AREA RBL 24 FLOOR SUPPORT BEAM STA 947.5 - 967 HAS CORROSION ON TOP SURFACE. REMOVED AND REPLACED FLOOR SUPPORT BEAM 947.5 - 967.
FORWARD CARGO BAY RIGHT INTERCOSTAL AFT SUPPORT BRACKET CRACKED FWD SIDE OF 500H RBL 21. REMOVED CRACKED AFT SUPPORT BRACKET AT STA 500H RBL 21. INSTALLED NEW SUPPORT BRACKET.
FORWARD PIT BAFFLE FWD BRACKET CRACKED AT S-26R AND 500H. REMOVED CRACKED BAFFLE AT S-26R AND 500H. INSTALLED NEW SUPPORT BRACKET.
WHILE REMOVING TRANSITION ZEE ANGLE FOR REPAIR, FOUND INTERCOSTAL AT STRINGER 25L BETWEEN STATION 500H-500I TO BE CRACKED IN THE RADIUS. FABRICATED NEW INTERCOSTAL.
FORWARD CARGO COMPARTMENT LEFT FWD STA 500I S-25L, TRANSITION SUPPORT ANGLE FOR SIDEWALL/FLOOR PANELS IS CORRODED OVER A LARGE AREA. REPAIRED FWD PIT LEFT TRANSITION SUPPORT STA 500I S-25L.
FORWARD CARGO BAY LEFT INTERCOSTAL AFT SUPPORT BRACKET CRACKED FWD SIDE OF STA 500G LBL21. REMOVED CRACKET BRACKET. INSTALLED NEW SUPPORT BRACKET.
FORWARD CARGO BAY RIGHT INTERCOSTAL FWD SUPPORT BRACKET CRACKED AFT SIDE OF STA 500G AT RBL 21. REMOVED CRACKED SUPPORT BRACKET AFT OF STA 500G AT RBL 21. INSTALLED NEW SUPPORT BRACKET.
FORWARD CARGO BAY RIGHT INTERCOSTAL AFT SUPPORT BRACKET CRACKED FWD SIDE OF STA 500G AT RBL 21. REMOVED CRACKED SUPPORT BRACKET FWD SIDE OF STA 500G AT RBL 21. INSTALLED NEW SUPPORT BRACKET.
FORWARD PIT RIGHT ZEE CHANNEL CORRODED SEVERAL PLACES FROM SLICE AFT OF STA 500D - 500I. REMOVED CORROSION STA 500D TO 500I+10. REMOVED OUT OF LIMITS ZEE CHANNEL AND INSTALLED NEW SECTION.
FORWARD CARGO BAY RIGHT INTERCOSTAL AFT SUPPORT BRACKET CRACKED FWD OF BS 500F AT RBL 21. REMOVED CRACKED SUPPORT BRACKET. INSTALLED NEW SUPPORT BRACKET.
AFT WET AREA RBL 49 SUPPORT FRAME STA 947.5-967 HAS CORROSION AREA. REMOVED SUPPORT AND INSTALLED NEW SUPPORT.
FWD PIT STR CLIP CORRODED AROUND FASTENERS AT STR 27R AND STA 500F. REMOVED AND REPLACED STRINGER CLIP AT STR 27R AND STA 500F.
IN FWD CARGO BAY, FOUND EXFOLIATION CORROSION ON STRINGER CLIP AT STA 500H STRINGER 27R. REMOVED AND REPLACED STRINGER CLIP AT STA 500H STRINGER 27R.
AFT CARGO BAY RIGHT TRANSITION ANGLE HAS SEVERAL AREAS OF CORROSION STA 727 TO STA 787. REPAIRED TRANSITION PANEL IN AFT CARGO FROM STA 727-727C+10, AND 727G+10 TO 767. FOUND ALL OTHER AREAS TO BE FOUND IN LIMITS.
STA 947.5 CABIN FLOOR SUPPORT FRAME HAS SEVERAL CORROSION SPOTS ON UPPER SURFACE AND AROUND SCREW HOLE UPPER/LOWER SIDES. REMOVED CORROSION ON STA 947.5 FLOORBEAM, FLOORBEAM FOUND OUT OF LIMITS. REPAIRED STA 947.5 FLOORBEAM.
PASSENGER CABIN LEFT STA 312-328, FLOOR SUPPORT INTERCOSTAL FOR FLOOR PANEL NO 221DF IS CRACKED IN TWO PLACES. REMOVED AND REPLACED CRACKED INTERCOSTAL WITH NEW.
FORWARD PIT S26L BAFFLE BRACKET CRACKED AT STA 500H. REMOVED AND REPLACED WITH NEW BRACKET.
AFT CARGO BAY LEFT TRANSITION ANGLE HAS SEVERAL AREAS OF CORROSION FROM STA 727 TO STA 847. REPAIRED DAMAGED SECTIONS OF AFT CARGO BAY LEFT TRANSITION ANGLE.
FORWARD CARGO BAY LEFT INTERCOSTAL FORWARD SUPPORT BRACKET CRACKED AFT OF STA 500F AT LBL 21. REMOVED CRACKED SUPPORT BRACKET AT STA 500F. INSTALLED NEW SUPPORT BRACKET.
ANGLE FOR INTERCOSTAL CRACKED AT STA 500F AND STR 25R. REMOVED CRACKED ANGLE STA 500F AND STRINGER 25R. REPLACED WITH NEW BRACKET.
FORWARD CARGO BAY SHEAR TIE FWD SIDE OF STA 500B AT LBL 21 IS CRACKED. REMOVED AND REPLACED SHEAR TIE.
FORWARD WET AREA L-1 DOOR SLIDE GIRT BAR FWD FLOOR ATTACH FITTING CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED L-1 GIRT BAR FITTING (FWD).
FORWARDD WET AREA RBL 30 SUPPORT FRAME STA 312-328 BARE METAL AROUND SCREW HOLES. REMOVED CRACKED FLOOR SUPPORT. FABRICATED NEW & INSTALLED.
CABIN EMERGENCY LIGHT INOP AT ROW 7ABC. RELAMPED AND OPS CHECKED GOOD.
AFTER R2 SLIDE DEPLOYMENT FOR TRAINING PURPOSES, EXTERIOR LIGHTING DID NOT ILLUMINATE ON THE SLIDE & THE SHEAR PIN RESTRAINT HAD NOT BEEN PACKED & STOWED PROPERLY. MAINTENANCE REPLACED SLIDE.
DURING CHECK OF EMERGENCY LIGHTS FOUND LIGHTS AT SEAT 6-12 ABC INOP. REPLACED BATTERY AND BATTERY CHARGER FOR EMERGENCY LIGHTS AT SEATS 6-12 ABC. OPS CHECKS NORMAL. REF AMM 33-51-06-960-806.
FOUND RT T/E FLAP L/E PAN 567AT CHAFED. BLENDED CHAFED AREA ON PANEL 567AT IAW B737-800 SRM 57-53-01, EA NO 14395.
LEFT WING O/B AFT FLAP BULLNOSE GOUGED (O/B OF NR 1 FAIRING). REPAIRED LT WING O/B AFT FLAP IAW SCA EA 57-8393.
LEFT WING I/B MAIN FLAP UPPER I/B SURFACE GOUGED. REPAIRED LT MAIN FLAP UPPER I/B SURFACE BY BLENDING IAW B737-800 SRM 57-53-01 FIG 103 & AAR EA NO 14398.
FOUND NR 6 SLAT L/E SKIN CRACKED 61 INCHES O/B OF I/B SIDE ON LWR SURFACE. REPAIRED NR 6 SLAT SKIN IAW EA 57-8391.
FOUND NR 7 SLAT L/E SKIN CRACKED 61 INCHES O/B OF I/B EDGE ON LWR SURFACE. REPAIRED NR 7 SLAT SKIN SCA EA 57-8389.
FOUND NR 8 SLAT LE SKIN CRACKED 61 INCHES OB OF IB EDGE ON LWR SURFACE. REPAIRED NR 8 SLAT.
FOUND NR 2 SLAT L/E SKIN LWR SURFACE CRACKED 61 INCHES O/B OF I/B SIDE MARKED. TWO CRACKS FOUND (.9375 & .25). REPAIRED NR 2 SLAT IAW SCA EA 57-8389.
DURING ROUTINE MAINTENANCE, FOUND FIRST CLASS EMERGENCY PROXIMITY LIGHTING FAILED CAP CHECK. REMOVED AND REPLACED BATTERY PACK FOR FIRST CLASS EMERGENCY PROXIMITY LIGHTING. OPS CHECK GOOD.
A CLEAR PLASTIC COVER ON THE R-1 DOOR SLIDE WAS FOUND TO BE LOOSE. MAINTENANCE REMOVED THE SLIDE AND REPAIRED THE WINDOW AND THEN REINSTALLED THE SLIDE IN THE R-1 POSITION.
DURING A FUNCTIONAL CHECK MAINTENANCE DISCOVERED THAT THE M1673 CHARGER / POWER SUPPLY WAS UNSERVICEABLE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY M1673.
DURING MAINTENANCE INSPECTION, FOUND THE RT AFT OVERWING EXIT EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE RELAMPED THE LIGHT. OPERATIONAL CHECK IS NORMAL.
MAINTENANCE FOUND LEFT FWD EMERGENCY EXIT SIDEWALL LIGHT INOP. MAINTENANCE REPLACED THE BALLAST FOR THE LIGHT.
MAINTENANCE FOUND R-2 DOOR EMERGENCY SIGN DAMAGED WITH LENS FALLING OFF. MAINTENANCE REMOVED AND REPLACED R-2 DOOR EMERGENCY EXIT SIGN AND LENS.
COCKPIT EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED & REPLACED FLIGHT DECK BULB AS REQUIRED. OPS CHECK NORMAL.
ENGINE NR 2 OIL PRESSURE AND QUANTITY LOW IN FLIGHT. FOUND LOOSE LINE ON ENGINE TGB. TIGHTENED LINE AND LEAK CHECKED GOOD.
EMERGENCY EXIT LIGHT FOUND BROKEN ABOVE DOOR R1. REPLACED LIGHT ASSEMBLY.
R-1 DOOR SLIDE DID NOT INFLATE AUTOMATICALLY DURING OPS CHECK SUN COUNTRY TASK CARD 25-220-00-02. ESCAPE SLIDE INFLATED MANUALLY AFTER PULLING THE MANUAL INFLATION HANDLE.
FORWARD LEFT POWER SUPPLY FOR EMERGENCY LIGHTS INOP.
DURING WALKAROUND FOUND EMERGENCY LIGHT FOR L2 EXTERIOR DOOR LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT ASSEMBLY AT DOOR L2. OPS CHECK GOOD.