N801SY
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
AFTER REMOVAL FLOOR MOUNTED ESCAPE SLIDE BRACKETS, BRACKETS (8 EAS) WAS FOUND WITH CORROSION. OPEN
CRACK IN FRAME AT BS 312 & BTW S-5L & S-6L, PASSENGER CABIN. CRACK IN FRAME AT BS 312 & BTW S-5L & S-6L, PASSENGER CABIN WAS REPAIRED PER SRM 53-10-07-2R-1 REPAIR 1.
ROW 24-25 DEF EMERGENCY LIGHTNING PANEL FALLING DOWN. REATTACHED LOOSE PANEL REF MM 25-21-00. OK FOR SERVICE.
LEFT FWD EMERG EXIT DOOR OVERWING LIGHT INOPERATIVE. REMOVED AND REPLACED LT FWD EMERG DOOR OVERWING LIGHT LAMP IAW 33-51-04. OPS CHECKED GOOD.
R2 DOOR GIRT BAR STOWAGE RING BROKEN. INSPECTED GIRT BAR STOWAGE RING IAW AMM 25-66-01, FOUND TO BE DIRTY. CLEANED THE RING, NO OTHER DEFECTS FOUND. OK FOR SERVICE.
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED IN 2 SPOTS, 1 3/8, 1 1/4 AT STAB STATION 147.90 APPROX 24" AND 31" AFT OF FRONT SPAR. ACCOMPLISHED REPAIR OF CRACKED SPOTS ON 2 AREAS ON LEFT HORIZONTAL STABILIZER IAW B737 SRM 55-10-01-2R-11 AT STAB STATION 147.90 APPROX 24" & 31" AFT OF FRONT SPAR.
EMERGENCY LIGHT PANEL AT SEAT ROW 24, 25 DEF SAGGING / LOOSE. REPLACED MISSING BROKEN ATTACH CLIPS IAW MM 25-21-00. REATTACHED PANEL. OK FOR SERVICE.
ROWS 12-22 DEF FAILED EMERGENCY BATTERY PACK FUNCTIONAL CHECK. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-06. OPS CHECKS GOOD. OK FOR SERVICE.
EMERGENCY LIGHTING FAILS 15 MINUTE MINIMUM ILLUMINATION CHECK ROWS 16-23 L/H CABIN. REMOVED AND REPLACED BATTERY PACK (M1694) AT ROW 13 ABC REF: AMM 33-51-06, REQUIRES OPERATIONAL CHECK. EMERGENCY BATTERIES ON CHARGE UNTILL 1630 HRS. OPS CHECKED IAW MM 33-51-06. OPS CHECKS GOOD. OK FOR SERVICE.
EMERGENCY LIGHTING FAILS 15 MINUTE MINIMUM ILLUMINATION CHECK ROWS 13-23 R/H CABIN. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-06. OPS CHECKS GOOD. OK FOR SERVICE
EMERGENCY LIGHTS AT ROW 16-21 ABC FAILED EMERGENCY LIGHT BATTERY FUNCTION CHECK REMOVED AND REPLACED BATTERY PACK (M1694) AT ROW 13 ABC REF: AMM 33-51-06, REQUIRES OPERATIONAL CHECK. NOTE: EMERGENCY BATTERIES ON CHARGE UNTILL 1630 HRS. OPS CHECKED IAW MM 33-51-06. OPS CHECKS GOOD. OK FOR SERVICE.
EMERGENCY LIGHTING FAILS 15 MINUTE MIMIMUM ILLUMINATION CHECK AT DOOR 1L. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-06. OPS CHECKS GOOD. OK FOR SERVICE.
BOARDING DOOR GIRT BARS ARE LOOSE AND THE APRON IS TOO LONG ON THE RIGHT. - RESOLUTION: TIGHTENED CLIP AND SECURED L1 DOOR GIRT BAR IAW AMM 25-66-01. GIRT BAR IS SECURED TO DOOR. OK FOR SERVICE.
BOARDING DOOR GIRT BARS ARE LOOSE AND THE APRON IS TOO LONG ON THE RIGHT - TIGHTENED CLIP AND SECURED L1 DOOR GIRT BAR IAW AMM 25-66-01. GIRT BAR IS SECURED TO DOOR. OK FOR SERVICE.
14ABC EMERGENCY EXIT ROW SIDE WALL LIGHT INOP. REPLACED LIGHT ASSY FOR 14ABC EMERGENCY EXIT ROW SIDE WALL LIGHT OPS CHECK GOOD REF AMM 33-21-00-960-807
DEFECT 808881: DURING APPROACH WHEN FLAPS SET TO FLAPS 30S, FLAP STOPPED AT 25 AND SHOWED AN ASSEMTRY QRH COMPLETED AND FLAPS LEFT IN POSITION AFTER LANDING (EMERGENCY DECLARED) - RESOLUTION: PERFORMED FSEU BITE NO ACTIVE FAULTS FOUND REF FIM 27-51 TASK 801 FOUND FAULT #27-52261 IN HISTORY TO BE INTERMITTANT. PERFORMED FLAP OPS TEST REF AMM 27-51-00 OPS CHECK GOOD AC OK SERVICE (FURTHER TROUBLESHOOTING IN PROGRESS)
DEFECT684360: BOARDING DOOR GIRT BAR HOOK ON DOOR (RT SIDE) NEEDS TIGHTINING. - - RESOLUTION: ADJUSTED L1 DOOR AFT GIRT BAR RETAINTER REF AMM 25-66-01. OK FOR SERVICE
L1 GIRT BAR HOLDER IS LOOSE. ADJUSTED FWD GIRT BAR HOLDER ON L1 SLIDE CANISTER. REF AMM 25-66-00.
DEFECT 758319: - L1 SLIDE COMING OUT OF THE TOP BOTTOM OF DOOR - - - RESOUTION - GIRT BAR HANGING OUT TO FAR RESECURED GIRT BAR VELCRO. REINSTALLED SLIDE PACK AND COVER IAW AMM 25-66-01
DEFECT 701216: CABIN ALTITUDE CLIMBING AT 300-400 FEET PER MINUTE AT FL240. WE CAUGHT THE RISING ALTITUDE. EMERGENCY DESCENT STARTED AND CABIN ALTITUDE WARNING SOUNDED. CABIN ALTITUDE CLIMBING AT 300-400 FEET PER MINUTE AT FL240. WE CAUGHT THE RISING ALTITUDE. EMERGENCY DESCENT STARTED AND CABIN ALTITUDE WARNING SOUNDED.
DEFECT 745168: 2L EVACUATION SLIDE GRIT BAR WILL NOT STAY IN THE RETAINER. RESOLUTION: ADJUSTED RETAINER REF. AMM 25-61-00.
LOSS OF CABIN ALTITUDE, DIVERTING TO KMSY, MASKS WERE DEPLOYED. NO INJURIES TO PAX OR CREW. FLIGHT LANDED SAFELY, TAXIED TO GATE WITHOUT FURTHER ISSUE. MX ARRIVING ON SCENE TO TROUBLESHOOT.
CABIN ALTITUDE LIGHT ILLUMINATED IN FLIGHT WITH ACCOMPANYING CABIN DECOMPRESSION, UNABLE TO MANUALY MAINTAIN CABIN PRESSURE. PERFORMED FIM TASK 21-31 TASK 823 LEFT PACK PRESSURE SYSTEM WITHIN THE CHART ALSO DUAL PACK PRESSURIZE SYSTEM LEAK DOWN WAS HIGH ON THE GOOD SIDE. OF THE GRAPH OK FOR SERVICE.
DEFECT 740681: F/A REPORTS DOOR 1R GIRT BAR BRACKET NEEDS TIGHTENING. RESOLUTION: SECURED GIRTBAR CLIPS REF AMM 25-66-01 OK FOR SERVICE.
DEFECT 721342: 15A EMERGENCY EXIT WALL LIGHT INOP. RESOLUTION: REPLACED 15A EMERGENCY WALL LAMP REF AMM 33-20-00. THIS CLEARS MEL 33-15-02 MDDR# 114273
DEFECT 721342 : 15A EMERGENCY EXIT WALL LIGHT INOP RESOLUTION: (IN PROGRESS)
DEFECT: EMERGENCY EXIT LIGHTS GUARD OVER SWITCH DAMAGED. RESOLUTION: REMOVED AND REPLACED EMERGENCY EXIT LIGHT SW. GUARD. OPS CHECK NORMAL
FLAP DISAGREE ON APPROACH. SELECTED FLAPS 30 AND FLAPS WERE VERIFIED AT 30. LATER WITHOUT EXCESSIVE SPEED FLAPS WENT TO 25 AND LOCKED OUT. PERFORMED FSEU BITE PROCEDURE. FOUND FAULT TE FLAP UC MSG NO. 27-51351. RESET FAULT AND PERFORMED TE ASSYM SKEW INDICATION TEST AND FLAP LOAD RELIEF TEST. NO FAULTS NOTED. REF FIM TASKS 27-51-801, 27-51-802 AND 27-51-803 8675 MCO-CUN, A/C 801, CREW EXPERIENCED A FLAP DISAGREE GOING INTO CUN. EMERGENCY DECLARED. FLIGHT LANDED SAFELY IN CUN.
FLAP DISAGREE UNCOMMANDED FLAP RETRACTI0ON FROM,30 TO 25 AT 200 ON LANDING PERFORMED FIM TASK 27-51 TASK 830, NO DEFECTS NOTED. R & R FSEU PRECATUINARY REF AMM 27-51-01. OPS CHECKS GOOD FLAP DISAGREE- GO AROUND EXECUTED. LANDED SAFELY IN RFD
AFT LEFT LAVATORY SMOKE DETECTOR WHEN OFF ON APPROACH IN TO PUJ ABOUT 3000 AGL DECLAFRED EMERGENCY. FLIGHT ATTENDANT RESET SMOKE DETECTOR AND ALARM SILENCED. FLIGHT ATTENDANT SAID THERE WAS A SMELL ALSO ( LAVATORY SMOKE DETECTION SYSTEMS ) R+R AFT LEFT SMOKE DETECTOR REF AMM 26-14-01. OPS CK GOOD. THIS CLEARS MEL 26-16-01. MDDR# 106247 MC NOTIFIED
FRAME STA 440 IS CRACKED AT ATTACH FITTING FASTENER HOLE AT STR 8L. REPAIRED FRAME STA 440 STRINGER 8 LT, PER ATS ER 20-03227 REV IR AND SUN COUNTRY T/C ENG-53SCA-10615 REV 00.
CORROSION FWD SERVICE DOOR INNER CHORD, INBOARD ATTACH STRAP BS 277-300 RBL 50 WL 207. REMOVED AND REPLACED FWD SERVICE DOOR INNER CHORD, INBOARD ATTACH STAP AT BS 277-300 RBL 50 WL 207, IAW DWG 141A8310 REV L AND SRM 51-40-02-0G-0.
FRAME STA 480 IS CRACKED AT ATTACH FITTING FASTENER HOLE AT STR 8L. REPAIRED FRAME BS 480 STRINGER 8 LT, PER ATS ER 20-03227 REV IR AND SUN COUNTRY T/C 53SCA-10615 REV 00.
FRAME STA 400 IS CRACKED AT ATTACH FITTING FASTENER HOLE AT STR 8R. REPAIRED FRAM STA 400 STRINGER 8 RT, PER ATS ER 20-03227 REV IR AND SUN COUNTRY T/C ENG-53SCA-10615 REV 00.
FRAME STA 500D IS CRACKED AT ATTACH FITTING FASTENER HOLE AT STR 8L. REPAIRED FRAME BS 500D STRINGER 8 LT, PER ATS ER 20-03227 REV IR AND SUN COUNTRY T/C 53SCA-10615 REV 00.
FRAME STA 480 IS CRACKED AT ATTACH FITTING FASTENER HOLE AT STR 8R. REPAIRED FRAME BS 480 RT STRINGER 8, PER ATS ER 20-03227 REV IR AND SUN COUNTRY T/C ENG-53SCA-10615 REV 00.
FRAME STA 440 IS CRACKED AT ATTACH FITTING FASTENER HOLE AT STR 8R. REPAIRED FRAME BS 440 STR 8 RT, PER ATS ER 20-03227 REV IR AND SCA ENG-53SCA-10615 REV 00.
FRAME STA 400 IS CRACKED AT ATTACH FITTING FASTENER HOLE AT STR 8L. REPAIRED FRAME BS 400 STRINGER 8 LT, PER ATS ER 20-03227 REV IR AND SUN COUNTRY T/C ENG-53SCA-10615 REV 00.
FLOOR BEAM AT BS 947.5 HAS CORROSION AT RBL 5. REMOVED & REPLACED BS 947.5 UPPER T CAP PREVIOUS REPAIR AT RBL 5, IAW SCA EA 53-0054 REV 00 AND ATS ER 20-03209 REV IR.
FLOOR BEAM AT BS 947.5 HAS CORROSION ON PREVIOUS REPAIR AT LBL 4. REMOVED & REPLACED BS 947.5 UPPER T CAP PREVIOUS REPAIR AT LBL 4, IAW SCA EA 53-0054 REV 00 AND ATS ER 20-03209 REV IR.
CORROSION FLOOR BEAM UPPER CAP BS 947 RBL 50 WL 208. REMOVED & REPLACED UPPER T CAP PREVIOUS REPAIR AT STA 947.5 RBL 50 WL 208, IAW SCA EA 53-0054 REV 00 AND ATS ER 20-03209 REV IR.
FLOOR BEAM AT BS 986.5 HAS CORROSION FROM LBL 43 TO RBL 47.5. ACCOMPLISHED FLOOR BEAM REPAIR STA 986.5 RBL 50-LBL 50, IAW ATS ER 20-03204 REV IR DATED 09/24/2020 AND SUN COUNTRY EA 53-0053 REV 00.
AFT GALLEY FLOOR STRAP AT BS 1016 + 11" TO BS 1016 + 13", RBL 3 HAS CORROSION. REMOVED AND REPLACED AFT GALLEY FLOOR STRAP AT BS 1016+11-1016+13 RBL 3 WITH NEW REPLACEMENT PART PO NR 801412, IAW SRM 51-40-02 AND BOEING DWG 147A5700 57111U.
FORWARD CARGO BAY LEFT HAND Z CHANNEL MULTIPLE SPOTS OF CORROSION NEAR SCREW HOLES STA 500C-500I, MARKED. REMOVED FWD CARGO LT Z-CHANNEL FS 500B+10-500I DUE TO OUT OF LIMITS CORROSION, IAW SRM 51-40-02-0G-0 AND 53-00-53-1A-2. FABRICATED REPLACEMENT Z-CHANNEL AND INSTALLED FROM FS 500B+10-500I USING BAC 1496-444-7075T6 LOT NR 5095931-1, IAW SRM 51-40-02-0G-0 AND 53-00-53-2R-5.
RT MOP SILL HAS CORROSION FROM BS 947.5 TO BS 986.5 RBL 56. CORROSION ON RT MOP SILL BS 947.5 TO 986.5 FOUND TO BE OUT OF LIMITS, IAW SRM 53-70-15-1A-1 FIG 103 DETAIL E. REMOVED AND REPLACED MOP SILL PO 801719, IAW SRM 51-40-02-0G-0 BOEING DWG 147A8501 REV B.
FLOOR STRUCTURE AT BS 947 + 11" RBL 25 HAS CORROSION AROUND HOLE. REMOVED FLOOR SUPPOT STRUCTURE AT BS 947+11 DUE TO BE OUT OF LIMITS, PER SRM 53-70-51-1A-1 FIG 104. LOCATED, DRILLED, AND INSTALLED NEW INTERCOSTAL ITEM NR 147A5660U3 PER DWG 47A5650 AND SRM 51-40-02-0G-0.
AFT GALLEY LT AND RT MOUNTS ARE CORRODED. INSTALLED NEW AFT GALLEY LT AND RT MOUNTS.
AFT GALLEY FLOOR PAN AT BS 986.5 + 2", RBL 43.5 HAS CORROSION. CORROSION ON AFT GALLEY FLOOR PAN (SHEAR WEB) AT STA 986.5+2, RBL 43.5 IN AN AREA OF 1.5" X 1.0" FOUND TO BE OUT OF LIMITS, DUE TO NO SRM ALLOWABLE LIMITS FOUND. REMOVED AND REPLACED SHEAR WEB STA 986.5-1016 RBL 30.5-47 WL 208, IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A5700.
GOUGE FOUND ON STA 986.5 FRAME AT RBL 46 WL 209. FOUND GOUGE TO BE OUT OF LIMITS, PER SRM 53-00-07-1A-1 4(A)1. REPLACED DAMAGED FRAME SECTION BS 986.5 JUST BELOW STRINGER 17 TO STRINGER 24 RH, PER SRM 51-40-02 AND DRAWING 147A1086 SHEET 29 AND DRAWING 147A0002 SHEET 42.
FORWARD CARGO BAY LEFT HAND AFT CARGO WEBBING MOUNT 3" FORWARD OF STA 500I HAS CORROSION AROUND FLOOR BOLTS, MARKED. REMOVED AND INSTALLED NEW FORWARD CARGO BAY LEFT HAND AFT CARGO TRACK AT STA 500G+12-500I, IAW SRM 53-00-53-2R-3 AND DWG 143A7500.
FORWARD CARGO BAY CORROSION ON INTERCOSTAL UNDER LEFT CARGO FLOOR Z CHANNEL STA 500F-500G LBL 25 WL 160 NEAR SCREW HOLES, MARKED. CORROSION ON FWD CARGO BAY INTERCOSTAL UNDER LEFT CARGO FLOOR Z-CHANNEL STA 500E TO 500G LBL 25 WL 160 FOUND TO BE OUT OF LIMITS, DUE TO FASTENER HOLE'S LOCATION, IAW SRM 53-00-53-1A-2 FIG 103 DETAIL (D). REMOVED INTERCOSTAL, IAW SRM 51-40-02-0G-0. INSTALLED NEW INTERCOSTAL NR 802535/6 AND REAIR PART LOT NR 5088298-1, IAW SRM 51-40-02-0G-0, SRM 53-30-53-2R-1 AND BOEING DWG 143A7505 REV B.
LT HORIZONTAL STABILIZER RIB AT STAB STA 92.7 HAS A CRACKED ON 2ND STIFFENER AT THE BOTTOM. REPAIRED LT HORIZ STAB AT STA 92.7 2ND STIFFENER, IAW SRM 55-10-09-2R-4.
FLOOR STRUCTURE AT BS 947.5+11" LBL 25 HAS CORROSION AROUND HOLES. REMOVED AND REPLACED FLOOR SUPPORT 947-967 LBL 25, DUE TO OUT OF LIMITS. CORROSION BLEND AREA 1" L X 1" W X .017" D, IAW SRM 53-70-51-1A-1, SRM 51-40-02-0G-0 AND DWG 147A5650 AND SRM 51-40-05.
RT HORIZONTAL STABILIZER RIB AT STAB STA 92.7, 2ND STIFFENER ARE CRACKED AT THE BOTTOM. REPAIRED RT HORIZ STAB RIB AT STAB STA 92.7, 2ND STIFFENER, IAW SRM 55-10-09-2R-4.
FORWARD CARGO BAY AFT LOWER WALL MOUNT STA 500I HAS MULTIPLE AREAS OF CORROSION BETWEEN STR 24L-24R, MARKED. REMOVED AND REPLACED FORWARD CARGO BAY AFT LOWER WALL MOUNT STA 500I, IAW SRM 51-40-02 AND DWGS 143A7902 AND 143A9481.
FORWARD CARGO BAY CORROSION ON INTERCOSTAL UNDER LEFT CARGO FLOOR Z CHANNEL STA 500G-500H LBL 25 WL 160 NEAR SCREW HOLES, MARKED. FORWARD CARGO BAY INTERCOSTAL FROM BS 500G TO 500H LBL 25 FOUND TO BE OUT OF LIMITS, IAW B737-800 SRM 53-00-53-1A-2 FIG 103. REMOVED AND REPLACED INTERCOSTAL, IAW B737-800 SRM 51-40-02-0G-0 AND BOEING DRAWING 143A7505 REV B.
CORROSION FORWARD CARBO BAY CORROSION ON INTERCOSTAL UNDER LEFT CARGO FLOOR Z CHANNEL STA 500D-500E LBL 25 WL 160 NEAR SCREW HOLES, MARKED. FORWARD CARGO BAY INTERCOSTAL AT BS 500D TO 500E LBL 25 UNDER Z-CHANNEL FOUND TO BE OUT OF LIMITS, IAW B737-800 SRM 53-00-53-1A-2 FIG 103. REMOVED AND REPLACED INTERCOSTAL, IAW B737-800 SRM 51-40-02-0G-0 AND BOEING DRAWING 143A7505 REV A.
FORWARD CARGO BAY CORROSION ON INTERCOSTAL UNDER LEFT CARGO FLOOR Z CHANNEL STA 500E-500F LBL 25 WL 160 NEAR SCREW HOLES, MARKED. FORWARD CARGO BAY INTERCOSTAL FROM BS 500E TO 500F LBL 25 UNDER Z CHANNEL FOUND TO BE OUT OF LIMITS, IAW B737-800 SRM NO ALLOWABLE LIMITS. REMOVED AND REPLACED INTERCOSTAL, IAW B737-800 SRM 51-40-02-0G-0 AND BOEING DRAWING 143A7505 REV B.
CORROSION FOUND AT STA 1016, STR 24R TERMINAL FITTING. CORROSION ON STR 24R TERMINAL FITTING BS 1016 FOUND TO BE OUT OF LIMITS, DUE TO NO SRM ALLOWABLE DAMAGE LIMITS FOR THIS PART. REMOVED TERMINAL FITTING. LOCATED, DRILLED AND INSTALLED NEW FITTING, PER SRM 51-40-05, SRM 51-40-02 AND BOEING DRAWING 147A0070.
FORWARD CARGO BAY RIGHT HAND Z CHANNEL HAS MULTIPLE AREAS OF CORROSION STA 500C-500I, MARKED. FORWARD CARGO BAY RIGHT HAND Z-CHANNEL BS 500C TO BS 500I FOUND TO BE OUT LIMITS, IAW B737-800 SRM 53-00-53-1A-2 FIG 103 DETAIL D. REMOVED AND REPLACED Z CHANNEL, IAW B737-800 SRM 51-40-02-0G-0, 53-00-53-2R-5 AND BOEING DRAWING 143A7500 REV.
AFT GALLEY FLOOR STRUCTURE AT BS 1006 +8, LBL 31.5 HAS CORROSION. REMOVED AND REPLACED AFT GALLEY WALL SUPPORT FLOOR STRUCTURE STA 991-1015 LBL 31 WL 208, IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A5700.
CORROSION ON GALLEY WALL SUPPORT WL 208 BS 993 RBL 34-RBL 47. CORROSION ON AFT GALLEY WALL SUPPORT STA 992 RBL 33-45 WL 208 FOUND TO BE OUT OF LIMITS, DUE TO NO SRM ALLOWABLE LIMITS FOUND. REPLACED PART NR 147A5710U2.
CORROSION FOUND ON AFT GALLEY WALL SUPPORT AT STA 1015 RBL 31 WL 208. REMOVED AND REPLACED DAMAGED AFT GALLEY WALL SUPPORT STA 991-1015 RBL 31 WL 208, IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A5700.
CORROSION FOUND ON BRACKET ATTACHED TO INTERNAL SURFACE OF FUSELAGE SKIN AT AFT SIDE OF OUTFLOW VALVE STA 981 BETWEEN S24R AND S25R. REMOVED AND REPLACED OUTFLOW VALVE MOUNT BRACKET STA 981 AFT INBOARD SIDE, IAW SRM 51-40-02 AND DWG 147A0002 REV.
LT AFT ENTRY DOOR MOP SILL CORRODED FROM BS 947.5 TO BS 986.5 LBL 56. CORROSION FOUND ON LT AFT ENTRY DOOR MOPSILL STA 947-986 LBL 56 FOUND TO BE OUT OF LIMITS, IAW SRM 53-70-15-1A-1 FIG 103 DET D. REMOVED AND REPLACED WITH NEW PART PO 801720, IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0 AND DWG 147A8501 SHEET 78 REV B 57901U.
VERTICAL STIFFENER CRACKED AT BS 663 LBL 25 WL 150. REMOVED AND REPLACED VERTICAL STIFFENER AT BS 663 LBL 25 WL 150 WITH PO 802748, IAW SRM 51-40-02-0G-0 AND BOEING DWG 111A1000 REV B 57828U.
RT HORIZONTAL STABILIZER RIB AT STAB STA 92.7, 3RD STIFFENER CRACKED. REPAIRED RT HORIZ STAB AT STAB STA 92.7, 3RD STIFFENER, IAW SRM 55-10-09-2R-4.
LOWER MAIN SILL WEB STA 947 TO 992 WL 208 RT HAS MULTIPLE AREAS OF CORROSION. LOWER MAIN SILL WEB STA 947 TO 992 WL 208 RT FOUND TO BE OUT OF LIMITS, IAW SRM 53-70-15-1A-1 FIG 103 DETAIL (D). REMOVED SILL WEB, IAW SRM 51-40-02-0G-0. INSTALLED NEW WEB P/O 801504/2, IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A8501 REV B. REINSTALLED LOWER CORNER REVEALS.
RT FWD SERVICE DOOR MOP SILL CORRODED BS 312 + 7.5" TO 328 + 5 " RBL 58. RT FWD SERVICE DOOR MOP SILL CORRODED BS 312 + 7.5" TO 328 + 5 " RBL 58.
FORWARD CARGO BAY CORROSION ON INTERCOSTAL UNDER LEFT CARGO FLOOR Z CHANNEL STA 500C-500D LBL 25 WL 160 NEAR SCREW HOLES, MARKED. REMOVED DAMAGED FWD CARGO BAY INTERCOSTAL UNDER LEFT CARGO FLOOR Z CHANNEL BS 500C-500D LBL25. LOCATED, DRILLED, AND INSTALLED NEW INTERCOSTAL, IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0 AND DWG 143A7505 81142U 09/16/2020. CORROSION FOUND OUT OF LIMITS, IAW SRM 53-00-53-1A-2 FIG 103 DETAIL D.
FORWARD CARGO BAY INTERCOSTAL UNDER RIGHT HAND Z CHANNEL STA 500B+2 CRACKED AT SCREW HOLE, MARKED. REMOVED AND REPLACED FWD CARGO BAY INTERCOSTAL STA 500B TO 500C RBL 25 PO 802809, IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A7505 REV B 57828U.
FORWARD CARGO BAY CORROSION ON INTERCOSTAL UNDER LEFT HAND CARGO FLOOR Z CHANNEL STA 500H-500I NEAR SCREW HOLES, MARKED. FOUND CORROSION ON FWD CARGO BAY INTERCOSTAL UNDER LT CARGO FLOOR Z CHANNEL BS 500H-500I TO BE OUT OF LIMITS, IAW SRM 53-00-53-1A-2 PARA 4 C FIG 103 DETAIL E. REMOVED INTERCOSTAL, LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL, IAW SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 AND DWG 143A7505 81142U.
FWD ENTRY DOOR MOP SILL CORRODED BS 312 + 5" TO BS 344 LBL 58. NDED CORROSION ON FWD ENTRY CHORD (MOPSILL) BS 312+5 TO 344 LBL 58 WL 208, FOUND OUT OF LIMITS DUE TO CROSSING OVER FASTENER HOLES, PER SRM 53-10-15-1A-2 (DETAIL D&G). REMOVED AND REPLACED INNER CHORD (MOPSILL), PER B737-800 SRM 51-40-02 AND DRAWING 141A8110 REV G.
FLOOR BEAM CORRODED BS 328 RBL 39 TO RBL 58. CORROSION ON FS 328 FLOOR BEAM RBL 39-58 UPPER CHORD FOUND TO OUT OF LIMITS, DUE TO EXISTING REPAIR. REMOVED AND REPLACED UPPER CHORD OF FS 328 FLOOR BEAM, IAW SRM 53-10-51 REF EA 15794.
WING TO BODY SUPPORT HAS CHAFE DAMAGE BS 651-673 LBL 25 WL 150. WING TO BODY SUPPORT BS 651-673 LBL 25 WL 150 FOUND TO BE OUT OF LIMITS, IAW SRM 53-40-71-1A-1 FIG 103 DETAIL (C). REMOVED SUPPORT IAW SRM 51-40-02-0G-0. INSTALLED NEW WING TO BODY SUPPORT, IAW SRM 51-40-02-0G-0 AND BOEING DWG 149A7216 REV- P/O 745891.
PUNCTURE IN LT SIDE OF APU TAILCONE 22 INCHES FROM LEADING EDGE, STA 1178 APPROXIMATELY 16.5 INCHES FROM BOTTOM CENTERLINE. REPAIRED PUNCTURE IN LT SIDE OF APU TAIL CONE 22" FROM LEADING EDGE, STA 1178 AND APPROXIMATELY 16.5" FROM BOTTOM CENTER LINE, PER SRM 53-80-70-2R-1 TABLE 201 AND SRM 51-70-05-2R-2.
AFT GALLEY FLOOR STRAP AT BS 1016 + 4" TO BS 1016 + 14.5" LBL 3 HAS CORROSION. REMOVED AFT GALLEY FLOOR STRAP AT BS 1016+4" TO 1016+14.5" LBL 3 AND FOUND TO BE OUT OF LIMITS. RECEIVED NEW GALLEY STRAP PN 147A5714YR AND LOCATED, DRILLED, AND INSTALLED NEW PART. ALL WORK PERFORMED IAW DWG 147A5700 AND SRM 51-40-02.
INTERCOSTAL ATTACH BRACKET TO FRAME BS 500H RBL 25 CRACKED ON AFT SIDE OF FRAME. REMOVED AND REPLACED ATTACH BRACKET BS 500H RBL 25, IAW SRM 51-40-02-0G-0 DRG 143A7505 PO 801210 57309U.
FWD CARGO, RT ZEE CHANNEL BAFFLE CRACKED WHERE IT ATTACHES TO CLIP, INBOARD SIDE, STA 500A+1 RBL 24. REMOVED CRACKED BAFFLE AT BS 500A TO 500B RBL 24. FOUND TO BE OUT OF LIMITS, IAW SRM 51-10-02-0G-0. INSTALLED REPLACEMENT BAFFLE PO 802809 FROM BS 500A TO 500B, IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A7505 REV B 57828U.
CORROSION FORWARD CARBO BAY CORROSION ON INTERCOSTAL UNDER RIGHT HAND CARGO FLOOR Z CHANNEL STA 500H-500I NEAR SCREW HOLES, MARKED. REMOVED AND REPLACED INTERCOSTAL STA 500H-500I RBL 25 WITH REPLACEMENT PO 801182, IAW SRM 51-40-02-0G-0 DRG 143A7505 57309U.
CORROSION FORWARD CARGO BAY CORROSION ON INTERCOSTALS UNDER LEFT CARGO FLOOR Z CHANNEL STA 500B-500C LBL 25 WL 160 NEAR SCREW HOLES, MARKED. REMOVED FWD CARGO BAY INTERCOSTAL UNDER LEFT CARGO FLOOR 2 CHANNEL BS 500B-500C LBL 25. LOCATED AND DRILLED NEW INTERCOSTAL AND INSTALLED, IAW SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 AND DWG 143A7505 81142U.
INTERCOSTAL CRACKED BETWEEN BS 312 AND BS 328 RBL 31. REMOVED CRACKED INTERCOSTAL BETWEEN BS 312 TO BS 328 RBL 31 FOUND TO BE OUT OF LIMITS, PER SRM 53-10-51-1A-1. INSTALLED REPLACEMENT INTERCOSTAL PO 801703, IAW SRM 51-40-02 AND BOEING DWG 141A5400 REV - ID 39 57828U.
AFT CARGO BAY RIGHT HAND Z CHANNEL HAS MULTIPLE AREAS OF CORROSION STATION 727B-767, MARKED. CORROSION ON AFT CARGO BAY RT Z CHANNEL FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY OF FASTENER HOLES, IAW SRM 53-00-53-1A-2 FIG 103 DETAIL D. REMOVED Z CHANNEL, IAW SRM 51-40-02-0G-0. INSTALLED FABRICATED Z CHANNEL, IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A2500 REV C.
FWD CARGO, Z CHANNEL BAFFLE CLIP HAS CORROSION AT 500C 25LBL OUTBOARD OF S-26L. REMOVED FWD CARGO 2 CHANNEL BAFFLE CLIP BS 500C LBL 25 OUTBOARD OF S-26L. LOCATED, DRILLED, AND INSTALLED NEW BAFFLE CLIP, IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0 AND DWG 143A7505 81142U.
CORROSION FOUND ON OUTBOARD SIDE OF INTERCOSTAL STA 991 S21L LBL 39 WL 185. REMOVED AND REPLACED DAMAGED INTERCOSTAL AT STA 991 STR 21L LOL 39 WL 185 WITH NEW PART NR 147A8801U85 IAW SRM 51-40-02-0G-0 AND DWG 147A8801.
TOOLING MARKS ON FLOOR STRUCTURE BS 328 TO BS 344 LBL 11. REMOVED TOOLING MARKS ON FLOOR STRUCTURE STA 328-344 LBL 11 IN AN AREA OF L 2" X W .6" X D .017", IAW SRM 51-10-02-0G-0. DAMAGE FOUND TO BE OUT OF LIMITS, IAW SRM 53-10-51-1A-1 FIGURE 105 DETAIL C. REMOVED AND REPLACED PANEL BREAK STA 328-344 LBL 11, IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0 AND DWG 141A5400 SHEET 29 REV- 57901U.
CORROSION FOUND ON SHIELD AFT OF AFT CARGO COMPARTMENT DOOR STA 856 TO 867 RBL 21 WL 159. CORROSION ON AFT CARGO AFT SHIELD STA 856 TO 867 RBL 21 WL 159 FOUND TO BE OUT OF LIMITS, DUE TO NO LIMITS FOUND IN SRM 53-60-15-1A-1. REMOVED SHIELD, IAW SRM 51-40-02-0G-0. FABRICATED SHEILD FROM 7075-0 LOT NR 5042508, IAW BOEING DWG 146A8127 7075-0 REV B .050. HEAT TREATED TO 7075 T62, IAW BOEING DWG 146A8127. INSTALLED SHIELD, IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A0081 REV A.
TOOLING DAMAGE ON LAV HARD POINT SUPPORT BS 294.5 TO 312 LBL 11.16 WL 208. TOOLING DAMAGE ON LAV HARD POINT SUPPORT BS 294.5-312 LBL 11.16 WL 208 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS, PER SRM. REMOVED AND REPLACED LAV HARD POINT SUPP BS 294.5-312 LBL 11.16 WL 208, IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0 AND DWG 141A5600 SHEET 2 REV N 57901U.
WASTE TANK ENCLOSURE LOWER STANCHION SUPPORT BROKEN BS 867 LBL 10 WL 160. REMOVED BROKEN STANCHION SUPPORT AT BS 867 LBL 10 WL 160, IAW SRM 51-40-02-0G-0. INSTALLED NEW STANCHION P/O 802020/1, IAW SRM 51-40-02-0G-0 AND BOEING DWG 149A8102 REV C.
FOUND TOOLING DAMAGE ON SURFACE OF UPPER CHORD AT STA 312 LBL 10 TO LBL 53 WL 208. TOOLING DAMAGE FOUND ON SURFACE OF UPPER CHORD STA 312 FLOOR BEAM LBL 12 1" L X .7" W X .011" D LBL 16.5 1" L X .7" W X .013" D BOTH FOUND TO BE OUT OF LIMITS, IAW SRM 53-10-51-1A-1 FIGURE 105 DETAIL C. REPAIRED STA 312 FLOOR BEAM UPPER CHORD LBL 12-LBL 16.5, IAW SRM 53-10-51-2R-15. TOOLING DAMAGE FOUND ON STA 312 FLOOR BEAM UPPER CHORD LBL 29-LBL 52 REMOVED IN AN AREA OF 23" L X .7" W X .011" D FOUND TO BE WITHIN LIMITS, IAW SRM 53-10-51-1A-1 FIGURE 105 DETAIL C. APPLIED CHEMICAL CONVERSION COATING AND PRIMED BLEND AREA LBL 29-LBL 52, IAW AMM 51-21-41-370-803 AND AMM 51-21-72-370-804 57901U.
INTERCOSTAL BETWEEN BS 312 AND BS 328 LBL 11 CRACKED. REMOVED AND REPLACED CRACKED INTERCOSTAL STA 312-328 LBL 11, IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0 AND DWG 141A5400 SHEET 27 REV- 57901U.
TOOLING MARK ON FLOOR STRUCTURE BS 277 TO BS 294.5 LBL 11. TOOLING MARK ON FLOOR STRUCTURE BS 277-294.5 LBL 11 FOUND TO BE OUT OF LIMITS, DUE TO NO ALLOWABLE LIMITS, PER SRM. REMOVED AND REPLACED INTERCOSTAL, IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0 AND DWG 141A5600 SHEET 1 REV N 53901U.
AFT CARGO BAY STRINGER CLIP STA 727D STR 22L HAS CORROSION ON SURFACE, MARKED. STRINGER CLIP AT BS 727D STR 22C FOUND TO BE OUT OF LIMITS, DUE TO NO ALLOWABLE LIMITS, IAW B737-800 SRM. REMOVED AND REPLACED STR CLIP, IAW B737-800 SRM 51-40-02-0G-0 AND BOEING DRAWING 146A1220 REV.
AFT CARGO BAY LEFT HAND Z CHANNEL HAS MULTIPLE AREAS OF CORROSION STATION 727B-827, MARKED. REMOVED AND REPLACED AFT CARGO LEFT HAND Z CHANNEL FROM BS 727B-827, IAW B737-800 SRM 51-40-02-0G-0 AND BOEING DRAWING 146A7502 REV. NOTE: CORROSION WAS FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS AT FASTENER LOCATIONS, PER SRM 53-00-53-1A-2.
FLOOR STRUCTURE AT BS 947 + 3" RBL 18 TO RBL 46 HAS CORROSION ON UPPER AND LOWER SURFACES OF TOP AROUND HOLES. REMOVED AND REPLACED FLOOR STRUCTURE AT BS 947+3 RBL 18 TO RBL 46 WITH NEW FLOOR STRUCTURE ITEM NR 147A5676U6 PO 801297, IAW SRM 51-40-02 AND DWG 147A5650 59568U. CORROSION MEASUREMENTS AS FOLLOWS L=1.0" W=1.0" D=.024". CORROSION FOUND TO BE OUT OF LIMITS, IAW SRM 53-70-51-1A-1 59568U.
SEAT TRACK FLOOR STRUCTURE CORRODED AROUND HOLE BS 328 +5", LBL 43. CORROSION FOUND ON SEAT TRACK FLOOR STRUCTURE STA 328+5 LBL 43 FOUND TO BE OUT OF LIMITS, IAW SRM 51-10-02-0G-0 9C. REMOVED AND REPLACED FLOOR STRUCTURE WITH NEW, IAW SRM 51-40-02 AND DWG 141A5730 09/08/2020 57111U PART 141A5770U3.
FWD ENTRY INNER CHORD SCUFF PLATE ATTACH ANGLE STA 287 TO STA 335 LBL 59 WL 208 CORROSION DAMAGE. FWD ENTRY INNER CHORD SCUFF PLATE ATTACH ANGLE BS 287-335 LBL 59 FOUND TO BE OUT OF LIMITS, DUE TO NO ALLOWABLE LIMITS, IAW B737-800 SRM. REMOVED AND REPLACED ATTACH ANGLE, IAW B737-800 SRM 51-40-02-0G-0 AND BOEING DRAWING 141A8110 REV-A.
FLIGHT DECK FLOOR PANEL 211AF HAS LIGHT SURFACE CORROSION AT OUTER EDGE AREA. FLIGHT DECK FLOOR PANEL 211AF HAS LIGHT SURFACE CORROSION AT OUTER EDGE AREA. BLENDED AREA W=1.0" X L=19" X D=.006" ORIGINAL .050" REMAINING .043 FOUND TO BE OUT OF LIMITS, IAW SRM 51-10-51-1A-1 PARA J STEP 2(C) DETAIL 1. LOCATED AND DRILLED REPLACEMENT PANEL PO 801957, IAW SRM 51-40-05 AND BOEING DWG 141A0631. APPLIED TOPCOAT, IAW AMM 51-21-73-370-801 57828U.
CORROSION FOUND WHERE TOP EDGE OF APU AIR INLET PLENUM ATTACHES TO FWD SIDE OF BULKHEAD STA 1088, MARKED. REMOVED AND REPLACED STIFF NEW AT BS 1088 AT PPU AIR INLET PLENUM ATTACH POINT, IAW B737-800 SRM 51-40-02-0G-0 AND BOEING DRAWING 148A0924 REV B.
FWD WET AREA FLOOR PANEL P/N 141A5810-159 HAS 2 DAMAGED AREAS ON PANEL. REPAIRED 2 DAMAGED AREAS ON FWD WET AREA FLOOR PANEL P/N 141A5810-159, IAW 737 SRM 53-00-50-2R-0 AND SRM 53-00-50-2R-4 BOEING DWG 141A5810 ID: 0159.
CORROSION FOUND ON AFT CARGO COMPARTMENT AFT BULKHEAD LOWER CENTER SUPPORT STA 947 RBL 9.5 TO LBL 21 WL 157. CORROSION ON AFT CARGO AFT LOWER BULKHEAD SUPPORT OUT OF LIMITS, IAW SRM 51-10-02. REMOVED AND REPLACED AFT CARGO AFT LOWER BULKHEAD SUPPORT WITH NEW P/N 149A8118U29, IAW SRM 51-40-02 AND DWG 149A8117.
CORROSION FLOOR SUPPORT HAS CORROSION IN HOLES BS 312 TO BS 328 RBL 11. REMOVED DAMAGED FLOOR SUPPORT BS 312-328 RBL 11 AND INSTALLED NEW FLOOR SUPPORT P/N 141A5410U14 PO 801506, IAW SRM 51-40-02 DWG 141A5400. FINAL INSTALL TO BE ACCOMPLISHED ON CUSTOMER CARD 00344.
AFT CARGO BAY TIE DOWN BRACKET CORRODED NEAR SCREW HOLES STA 792 STR 23-24L, MARKED. REMOVED AND REPLACED AFT CARGO BAY TIE DOWN BRACKETS AT STA 792 STR 23-24L, IAW SRM 51-40-02 AND DWG NR 146A7550 59568U 09/03/2020. CORROSION FOUND TO BE OUT OF LIMITS, DUE TO NO PUBLISHED LIMITS IN SRM 59568U.
LT 663 UPPER ATTACH ANGLE CRACKED AT APPROXIMATELY LBL 8. REPAIRED LT 663 UPPER ATTACH ANGLE, IAW SRM 57-10-10-2R-5 LBL 8.
FWD WET AREA FLOOR PANEL P/N 141A5810-56 MISSING INSERT AND HAS A PUNCTURE. REPAIRED PUNCTURE, IAW SRM 53-00-50 REPAIR 6 + INSTALLED INSERT, IAW SRM 53-00-50 REPAIR GENERAL PARA 5S(1) ON FWD WET AREA FLOOR PANEL P/N 141A5810-56 80733U.
AFT CARGO BAY FLOOR SUPPORT STATION 772 2" LEFT OF CENTERLINE HAS CORROSION NEAR BOLT HOLES, MARKED. CORROSION ON AFT CARGO BAY FLOOR SUPPORT FOUND TO BE OUT OF LIMITS, IAW SRM 53-00-53-1A-1 FIG 103 DETAIL D. CORROSION FOUND AROUND FASTER HOLES. REMOVED FLOOR SUPPORT, IAW SRM 51-40-02-0G-0. INSTALLED NEW FLOOR SUPPORT, IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A7500 REV C.
CORROSION RT SHIELD FWD OF AFT CARGO DOOR FROM STA 767-794.5, RBL 25, WL 155. RT SHIELD FWD OF AFT CARGO DOOR FROM STA 767-794.5, RBL 25, WL 155. CORROSION ON RT SHIELD FWD OF AFT CARGO DOOR FOUND TO BE OUT OF LIMITS, DUE TO NO LIMITS FOUND IN SRM, IAW SRM 53-60-15-1A-1. REMOVED AFT CARGO FWD SHIELD, IAW SRM 51-40-02-0G-0. INSTALLED NEW SHIELD P/O 801703/3, IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A0081 REV A.
TOOLING MARK ON FLOOR STRUCTURE BS 270 TO 270 + 5", LBL 11. TOOLING MARK ON FLOOR STRUCTURE BS 270+6" LBL 11 FOUND TO BE OUT OF LIMITS, IAW NO SRM ALLOWABLE LIMITS. REMOVED AND REPLACED TEE, IAW SRM 51-40-02 AND BOEING DWG 141A5600 REV N 57828U.
AFT WET AREA FLOOR PANEL P/N 147A5810-28 EDGE HAS DELAMINATION, DAMAGED INSERTS AND PUNCTURE. REPAIRED DELAMINATION AND PUNCTURE ON AFT WET AREA CABIN FLOOR PANEL 147A5810-28 AND REPLACED DAMAGED INSERTS, PER SRM 53-00-50-2R-1.
LT LOWER 663 VAPOR BARRIER CRACKED BY THE EXHAUST CUTOUT APPROXIMATELY LBL 14 BELOW THE HORIZONTAL STIFFENER. REPAIRED CRACKS BY EXHAUST CUTOUT APPROXIMATELY LBL 14 BELOW THE HORIZONTAL STIFFENER ON LT LOWER 663 VAPOR BARRIER, PER SRM 57-10-10-2R-2 PARA 1 NOTE AND SRM 51-70-04-2R-10.
TOOLING MARKS ON FLOOR BEAM BS 294.5, LBL 11 TO RBL 41. BLENDED ON UPPER SURFACE OF FLOOR BEAM 294.5 AT RBL 24.5 AREA 1.75" L X .7" W X .015" D. FOUND TO BE OUT OF LIMITS, IAW SRM 53-10-51-1A-1 DET C. ALL OTHER BLEND AREAS .012" OR LESS WITHIN LIMITS, IAW SRM 53-10-51-1A-1 DET C. REPAIRED OUT OF LIMIT AREA, IAW SRM 53-10-51-2R-14 WITH 7075T6#0. .100" LOT# 5065468-1. 57828U.
LEFT WING PANEL 521 QB HAS EROSION NEXT TO FASTENER HOLE. REPAIRED EROSION NEXT TO FASTENER HOLE ON LEFT WING PANEL 521QB, IAW 737 SRM 57-41-01-2R-1 AND SRM 51-70-05 REPAIR 8.
RT WING LEADING EDGE PANEL 621EB HAS EROSION AT DRAIN HOLE. REPAIRED RT WING LEADING EDGE PANEL 621EB EROSION AT DRAIN HOLE, IAW 737 SRM 57-41-01-2R-1 AND SRM 51-70-05 REPAIR 8.
RT WING LEADING EDGE PANEL 621LB HAS EROSION AT DRAIN HOLE. REPAIRED EROSION AT DRAIN HOLE ON RT WING LEADING EDGE PANEL 621LB, IAW 737 SRM 57-41-01-2R-1 AND SRM 51-70-05 REPAIR 8.
AFT CARGO BAY DOOR FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION, MARKED, STA 808-827 RBL 26.5 WL 160. AFT CARGO BAY DOOR FLOOR SILL PLATE FOUND TO BE OUT OF LIMITS, IAW SRM 53-60-15-1A-1. REMOVED FLOOR SILL PLATE, IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A13410. INSTALLED NEW SILL PLATE, IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A8340 REV: A. NOTE: SILL PLATE WAS OUT OF LIMITS DUE TO PROXIMITY OF FASTENER HOLES.
AFT WET AREA FLOOR PANEL P/N 147A5810-23 HAS SEVERAL INSERTS DAMAGED. FABRICATED REPLACEMENT AFT WET AREA FLOOR PANEL P/N 147A5810-23, PER B737 SRM 53-00-50-2R-0 PARA 4A(1) TABLE 204 AND PARA 5A AND PER BOEING DRAWING 147A5810 REV A. BMS 4-17 TY6 LOT 5085150-1; SL5182A3 INSERTS; BMS 5-107 LOT AK9GP5303K. IDENIFIED PANEL, IAW B737 SRM 53-00-50-01-1 FIG 6 TABLE 6. FLOOR PANEL NOT ECONOMICALLY FEASIBLE TO REPAIR.
AFT CARGO BAY FLOOR SUPPORT TEE SPLICE STA 727I+5 HAS CORROSION AROUND MULTIPLE NUTPLATES. AFT CARGO BAY FLOOR SUPPORT TEE SPLICE STA 727I+5 HAS CORROSION AROUND MULTIPLE NUTPLATES. FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED LIMITS IN SRM. REMOVED AND REPLACED TEESPLICE WITH PO 774863 AT STA 727I+5, IAW SRM 51-40-02 AND BOEING DWG 146A7500 ID: 41 REV: C 57828U.
EMERG LIGHTS AT ROWS 5, 6, 7, 9, AND 10 DO NOT WORK. REMOVED AND REPLACED LT AND RT BATTERY PACKS AT ROW 7AC/7FD. OPS CHECK NORMAL.
NR 6 SLAT HAD A SMALL CRACK AT A FASTENER HOLE FOR ACTUATOR ATTACH FITTING. REMOVED AND REPLACED THE NR 6 LEADING EDGE SLAT. OK FOR SERVICE.
NR 8 LEADING EDGE SLAT HAS CRACK IN THE SKIN AT THE ACTUATOR ATTACH POINT. ACCCOMPLISHED AN INTERM REPAIR. REMOVED AND REPLACED THE NR 8 SLAT. PERFORMED A SLAT ADJUSTMENT. OK FOR SERVICE.
FOUND WIGGLE PLATE ASSY DAMAGED AT T/E PANEL 651EB. REMOVED 5 EACH RIVETS COMMON TO WING PLANK AND WIGGLE PLATE. NEW PLATE DRILLED AND CLECO'D IN PLACE. READY TO INSTALL. INSTALLED FASTENERS IN WIGGLE PLATE.
NR 6 FLAP FAIRING AFT LINK ASSEMBLY UPPER ROD END BOLT AND SPACER WORN. REMOVED AFT CANOE FAIRING TIP 642EB. PART IN AREA. REMOVED AND REPLACED AFT LINK ASSEMBLY. FOUND UPPER ROD END BOLT AND SPACER WORN. ORDERED BOLT. NEW SPACER AND OLD BOLT REINSTALLED TILL NEW BOLT ARRIVES. BOLT IS TAGGED. REPLACED UPPER ROD END BOLT AND SPACER AND AFT CANOE FAIRING TIP.
RIGHT WING LOWER INBD FIXED TE ATTACHED TO PANEL 651EB, FOUND A BEAM WORN AND ROD END MISSING. REMOVED PANEL 651EB. REMOVED THE WORN BEAM. INSTALLED A NEW BEAM.
FOUND A SMALL HOLE ON THE NR 1 OTBD NACELLE COWL. REPLACED WITH SERVICEABLE COWL.
DURING AN EMERGENCY LIGHT SWITCH OPS TEST, FOUND THE L2 DOOR ESCAPE SLIDE LIGHT INOPERATIVE. REPLACED A BLOWN FUSE IN THE AFT POWER SUPPLY FOR THE L2 SLIDE LIGHT. OPS CHECKED GOOD.
LEFT WING OUTBOARD MAIN FLAP INBOARD END TOP SIDE SKIN HAS WEAR DAMAGE. LEADING EDGE PANEL 113A3432-11 REMOVED FROM LT. FLAP FOUND WEAR OUT OF LIMITS. REPLACEMENT PANEL ORDERED FROM BOEING. FLAP PANEL # 113A3411-7 REMOVED DUE TO WEAR, FOUND TO BE WITHIN LIMITS. WEAR REQUIRES TREAT PRIME AND PAINT. DRILLED AND INSTALLED LEADING EDGE PANEL 113A3432-11. INSTALLED FLAP PANEL 113A3411-7. PRIMED AND PAINTED PANELS.
LEFT OTBD FLAP PHENOLIC CHAFE MATERIAL MISSING FROM T/E OF FORE FLAP. REMOVED ALL OLD PHENOLIC AND ADHESIVE. CLEANED BOTTOM SIDE OF THE O/B FLAP. REPAIRED.
THE AFT, LT, TE, OTBD FLAP, INBD FLAP TRACK HAS SIDE SCUFFING ON THE UPPER AND LOWER TRACK FLANGES FROM THE CARRIAGE RUB PLATES. ROLLER IS OUT OF LIMIT. BLENDED DAMAGE. NO CRACKS NOTED.
RIGHT OTBD FLAP PHENOLIC CHAFE MATERIAL MISSING FROM T/E OF FORE FLAP. REPAIRED.
ON APPROACH, AT FLAPS 1, THE LEADING EDGE FLAPS TRANSIT LIGHT ILLUMINATED, NR 3 SLAT AMBER LIGHT ILLUMINATED. RAN QRH 9.14 STILL AT FLAP 1, LEADING FLAP TRANSIT LIGHT AND OVERHEAD AMBER LIGHT WENT OUT AFTER APPROXIMATELY 5 MINUTES AND LEADINGE EDGE FLAPS EXTENTION LIGHT ILLUMINATED. PERFORMED FSEU BITE TEST. NO FAULTS NOTED. CYCLED FLAPS FULL UP AND FULL DOWN, NO DEFECTS NOTED. OK FOR SERVICE. INSPECTED WIRING HARNESS. NO DEFECTS NOTED. INSPECTED WIRING FROM NR 3 SLAT SENSORS TO FUSELAGE. CHECKED CONTINUITY FROM SENSORS TO D728A AT FSEU. CHECKED WIRING WITH MEGGAR AND UNDER LOAD. FOUND NO LOOSE CONNECTORS OR DEFECTS. FOUND BENT PIN IN RETRACT SENSOR S1095. REPLACED SENSOR.
WITH FLAPS EXTENDED TO 5 ON APPROACH. THE NR 3 SLAT ON THE LEFT WING FAILED TO EXTEND. REPLACED THE NR 3 LEADING EDGE EXTEND PROXIMITY SWITCH. R & R FSEU. OPS CHECKED GOOD. REPLACED THE LE FLAP/SLAT POSTION ANNUNCIATOR PANEL. OPS CHECKED GOOD. REMOVED AND REPLACED FLAP LOAD LIMITER SOLENOID. OPS CK GOOD. INSPECTED #3 LEADING EDGE SLAT TRACKS AND ACTUATOR WITH NO DEFECTS NOTED. PERFORMED FSEU BITE. ALL TESTS PASS, OK FOR SERVICE.
NR 3 SLAT STAYED IN TRANSIT AFTER SELECTING FLAPS FIVE. ACP BITE OF FSEU WITH NO FAULTS FOUND. OPERATED FLAPS WITH NO FAULTS. OK FOR SERVICE. PERFORMED LEADING EDGE FLAP AND SLAT POSITION INDICATING SYSTEM TEST. NO FAULTS FOUND. PERFORMED FSEU BITE TEST. NO FAULTS FOUND. PERFORMED VISUAL INSPECTION. NO FAULTS FOUND.
LT WING, UPPER PANEL L/E INBD OF ENGINE HAS LOOSE, SMOKING RIVETS. REPLACED FASTENERS.
RT WING, UPPER PANEL L/E INBD OF ENGINE HAS LOOSE, SMOKING RIVETS. REPLACED FASTENERS.
FLAPS WOULD NOT MOVE FROM 25 POSITION DURING GO AROUND AT AIRPORT, WHEN FLAP LEVER WAS MOVED TO FLAPS 15 POSITION. R & R T/E FLAP CONTROL VALVE. R & R FLAP LEVER POSITION SWITCH. ALL TESTS REQUIRED PASSED NORMALLY.
EMERGENCY LIGHTS ON OVERHEAD BIN BULLNOSE BETWEEN SEATS 15 ABC AND 20 ABC AND LIGHT AFT OF LT AFT OVERWING EXIT DOOR FAILED BATTERY PACK CAPACITY FUNCTIONAL TEST. R & R POWER SUPPLY M1670, BATTERY PACK IAW AMM 33-51-06. OPS CHECKS GOOD.
EMERGENCY LIGHTS ON OVERHEAD BIN BULLNOSE BETWEEN SEATS 16 DEF AND 20 DEF AND LIGHT AFT OF RT AFT OVERWING EXIT DOOR FAILED BATTERY PACK CAPACITY FUNCTIONAL TEST. R & R POWER SUPPLY M1671 BATTERY PACK IAW AMM 33-51-06. OPS CHECKS GOOD.
R2 EMERGENCY LIGHTS INOPERATIVE. R & R R2 EMERGENCY LIGHT CHARGER ASSY, AND BATTERY PACK.
R1 DOOR SLIDE EMERGENCY LIGHT INOPERATIVE AND KEEPS POPPING THE FUSE IN THE CHARGER. REPAIRED WIRING FROM CONNECTOR, D10748, PIN 12 TO CONNECTOR, D12052, PIN 2 AT ROW 1, SEAT AB.
PASSENGER CABIN FWD WET AREA BS 328 FLOORBEAM CORRODED AT SEVERAL SPOTS. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED THE FLOORBEAM.
FLOORBEAM BS 328 GOUGED DOWN THE AFT SIDE UNDER THE CUSP INSTALLATION ON THE RT SIDE, REPAIRED THE FLOORBEAM.
FWD CARGO BAY, LT SIDE FROM BS 400-500A FLOOR SUPPORT IS CORRODED. BLENDED CORROSION AND FOUND OUT OF LIMITS. R & R THE FLOOR SUPPORT.
FWD CARGO BAY, LT SIDE FROM BS 500A - 5000H FLOOR SUPPORT CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R THE FLOOR SUPPORT.
AFT CARGO DOOR CUTOUT BOTTOM WEB HAS LARGE AREA OF CORROSION ON TOP AND BOTTOM SURFACES. CORROSION FOUND TO BE 100 PERCENT MATERIAL LOSS. R & R WEB.
DURING FWD CARGO LT TRANSITION PANEL REPAIR, SPLICE FOUND CORRODED AT INTERCOSTAL BS 500F - 500G. R & R INTERCOSTAL.
DURING FWD CARGO LT TRANSITION REPAIR SPLICE FOUND CRACKED INTERCOSTAL BS 500G - 500H. R & R THE INTERCOSTAL.
AFT CARGO BAY, RBL 14 FLOOR SUPPORT STRUCTURE LOCATED AT BS 794 - 887 HAS SEVERAL AREAS OF SURFACE CORROSION. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION.
PASSENGER CABIN AFT WET AREA FS 986.5, 2.5 INCHES INBD OF MOP SILL AT L2 DOOR, CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REPAIRED.
DISCOVERED CRACKED FLOOR SUPPORT AT BL 0 BETWEEN BS 344 - 360 FLOORBEAMS. R & R FLOOR SUPPORT.
PASSENGER CABIN FWD WET AREA FROM BS 312 - 328, RBL 10 FLOOR SUPPORT CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. R & R FLOOR SUPPORT.
PASSENGER CABIN AFT WET AREA AT L2 DOOR MOP SILL HAS CORROSION IN SEVERAL AREAS. CORROSION EXTENDS UNDER L2 DOOR THRESHOLD. FOUND TO BE OUT OF LIMITS. R & R MOP SILL AT L2.
PASSENGER CABIN AFT WET AREA BS 947.5 AT LBL 4 & 12 AND RBL 4 HAS SURFACE CORROSION LOCATED ON TOP OF FRAME. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED.
PASSENGER CABIN AFT WET AREA AFT & INBD OF R2 DOOR AT FS 992, RBL 32 TO 42, G4 GALLEY FLOOR SUPPORT HAS SURFACE CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW FLOOR SUPPORT.
PASSENGER CABIN AFT WET AREA INBD OF L2 DOOR AT BS 967, LBL 36 HAS CORROSION ON TOP SURFACE OF BEAM . BLENDED CORROSION IAW EA 15791 FOUND TO BE OUT OF LIMITS.
PASSENGER CABIN FWD WET AREA FROM BS 328 - 344 AND ABOUT LBL 10 FLOOR SUPPORT CORRODED. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. R & R FLOOR SUPPORT.
FOUND TWO CRACKS IN LT WING CENTER SECTION REAR SPAR BETWEEN LBL 24.92 AND LBL 45.64. CRACK OUT OF LIMITS. REPAIRED LT WING CENTER SECTION REAR SPAR.
PASSENGER COMPARTMENT FWD WET AREA FROM BS 312 - 328 AND ABOUT LBL10 FLOOR STRUCTURE CORRODED. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. R & R FLOOR SUPPORT.
AFT CARGO BAY BS 887 FLOORBEAM HAS CORROSION BETWEEN RBL 3 & 10. FOUND TO BE OUT OF LIMITS. FABRICATED NEW FLOORBEAM ANGLE.
PASSENGER CABIN FWD WET AREA FROM BS 294.5 - 312 AND ABOUT RBL 10 FLOOR SUPPORT STRUCTURE CORRODED. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT.
MAJOR REPAIR. REPLACED SEAT TRACKS LBL 45.5 & RBL 24.75 AND FASTENERS AT THE FWD END.
SELECTED FLAPS 1 AT APPROX 230 KIAS AND FLAPS INDICATED T/E ASYMMETRY.
DURING CLIMBOUT, A LOUD BANG AND FLASH, NR 2 ENGINE FAILURE. RETURNED TO DEPARTURE.
THE 2AC SEAT MISSING EMERGENCY LIGHTING. INSTALLED EMERGENCY LIGHTING AS REQUIRED ON SEAT 2AC.
RIGHT AFT OVERWING EXIT HATCH DOORWAY LIGHT BULB BURNED OUT. RELAMPED RIGHT AFT OVERWING EXIT HATCH DOORWAY LIGHT.
CABIN SEAT TRACK AT STA 727D, 727F, 727G, 727J IS OUT OF LIMITS. REPAIRED SEAT TRACK.
CABIN SEAT TRACK AT STA 500+18" & 500C+19" LBL 44 IS OUT OF LIMITS. REPAIRED SEAT TRACK.
EMERGENCY FLOOR PROXIMITY LIGHTING AT ROW 9, 19, AND 26 INOP (FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM; INCANDESCENT LIGHTING SYSTEM). REPLACED ECECTRICAL CONNECTORS AT SEATS 9, 19 AND 26 AND CHECKS GOOD.
STA 986.5 FLOOR SUPPORT CORRODED JUST I/B OF R2 DOOR. BLENDED CORROSION & FOUND TO BE OUT OF LIMITS. REPAIRED AREA & REMOVED CORROSION.
STA 986.5 FLOOR SUPPORT CORRODED JUST I/B OF L2 DOOR. BLENDED CORROSION & FOUND TO BE OUT OF LIMITS. REPAIRED AREA & REMOVED CORROSION.
LBL 24 CABIN SEAT TRACK IS OUT OF LIMITS AT STA 727A. REPAIR TO BE ACCOMPLISHED ON THIS CARD NO DOT. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW TRACK & REPAIRED.
FORWARD CARGO PIT LEFT SIDE STA 500I SIDE WALL SUPPORT ANGLE AT AFT BULKHEAD IS CORRODED BETWEEN STR 23L TO 25L. REMOVED CORROSION FOUND TO BE OUT OF LIMITS.
LONGITUDINAL FLOOR SUPPORT CORRODED AT STA 947.5 ABOUT RBL 27. REMOVED & REPLACED DAMAGED FLOOR SUPPORT.
FORWARD CARGO LEFT TRANSITION (ZEE) ANGLE CORRODED BETWEEN FRAME STA 500G TO 500H ABOVE STR 25. BLENDED CORROSION FOUND TO BE OUT OF LIMITS.
FWD CARGO PIT LEFT SIDE TRANSITION (ZEE) ANGLE CORRODED BETWEEN STA 500H TO 500I AT STR 25L.
FORWARD CARGO FLOORBOARD TRANSITION (ZEE) ANGLE CORRODED BETWEEN FRAME STA 500H TO 500I ABOVE STR 25. BLENDED CORROSION FOUND TO BE OUT OF LIMITS.
FWD CARGO PIT LEFT SIDE STA 500E, 500F, 500G,& 500H GRAY WATER DRAIN HOSE SUPPORT BRACKETS HAVE CORROSION AROUND NUT PLATES. REMOVED CORRODED SUPPORT BRACKETS & INSTALLED NEW BRACKETS.
CORROSION ON FWD WET AREA FLOOR SUPPORT AT FS 327 LBL 10. 234-004. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED CORROSION. REMOVED AND REPLACED FLOOR SUPPORT.
EVIDENCE OF CORROSION ON FLOOR SUPPORT IN FWD WET AERA AT FS 325 RBL 10 234-002.
DURING REMOVAL OF TRANSITION PNL FOUND FWD CARGO BAY AFT RIGHT BULKHEAD LWR SUPPORT CORRODED. REMOVED CORROSION ON FWD CARGO BAY AFT RIGHT LOWER SUPPORT. CORROSION FOUND TO BE OUT OF LIMITS.
PASS CABIN SEAT TRACK LBL 44 BETWEEN BS 727D AND 727J HAS SEVERAL AREAS OF CORROSION ON INNER SURFACE. REMOVED CORROSION. OUT OF LIMITS.
CABIN SEAT TRACK LBL 44 FROM STA 520 TO 480 HAS MULTIPLE AREAS OF CORROSION. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED SEAT TRACK.
PASS CABIN SEAT TRACK LBL 24 AT STA 727A HAS CORROSION ON INNER SURFACE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED SEAT TRACK.
CABIN SEAT TRACK BETWEEN STA 727B-727J AT RBL 24 HAS GOUGED SPOTS. REMOVED CORROSION. REMAINING MATERIAL FOUND TO BE OUT OF LIMITS. REPAIR ACCOMPLISHED.
CREASE BEAM CORRODED FROM FS 318 TO 328 AT R1 DOOR. REMOVED AND REPLACED CREASE BEAM AT R1 DOOR.
FLOOR SUPPORT AT RBL 49 CORRODED AT STA 964. REMOVED CORROSION. REMAINING MATERIAL FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED FLOOR SUPPORT.
FLOOR SUPPORT AT STA 992.8 CORRODED JUST INBOARD OF R2 DOOR. REMOVED CORROSION. REMAINING MATERIAL FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT.
EMERGENCY LIGHT BATTERY ROW 20 RIGHT SIDE FAILED CAPACITY CHECK.
EMERGENCY LIGHT BATTERY ROW 11 RIGHT SIDE FAILED CAPACITY CHECK.
EMERGENCY LIGHT BATTERY AFT OVERHEAD LEFT SIDE FAILED CAPACITY CHECK.
EMERGENCY LIGHT BATTERY ROW 20 LEFT SIDE FAILED CAPACITY CHECK.
DURING SCHEDULED MAINTENANCE L-1 SLIDE DEPLOYMENT, SLIDE FAILED TO INFLATE. MAINTENANCE REMOVED AND REPLACED L-1 DOOR SLIDE PER TASK CARD 252400000.
THE 6ABC AND 19ABC EMERGENCY LIGHTS ARE INOP. FOUND CONNECTOR AT 6 ABC HAD A PIN PUSHED BACK. RESEATED PIN AND LOCKED IN CONNECTOR. RELAMPED 19ABC EMERGENCY LIGHT AND ALL EMERGENCY ESCAPE PATH LIGHTING OPS CKS GOOD.
DURING MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT SEATS 4-10 NOT WORKING. MAINTENANCE FOUND POWER SUPPLY AT ROW 6 LEFT FAULTY AND NOT CHARGING BATTERY PACK. FUSES AND POWER TO POWER SUPPLY CHECKS GOOD. REMOVED AND REPLACED POWER SUPPLY AND BATTERY AND OPERATIONAL CHECK IS GOOD.
DURING A FUNCTIONAL CHECK MAINTENANCE FOUND THE EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY CHECK AT DOORS L1, L2, AND R2. MAINTENANCE REPLACED THE BATTERY PACKS AT THE L1, R1, R2 DOORS.
DURING A FUNCTIONAL CHECK MAINTENANCE FOUND THE EMERGENCY LIGHT BATTERY BACKS AT R1, R2, AND L2 DOORS FAILED CAPACITY CHECK. MAINTENANCE THEN REPLACED THE BATTERY PACKS AT THE R1, R2, AND L2 DOOR.
MAINTENANCE FOUND THE L1 DOOR EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE THEN REPLACED THE EMERGENCY LIGHT BATTERY PACK.
RIGHT FWD OVERWING EMERGENCY EXIT LIGHT IN WINDOW LIGHT ASSY INOP. MAINTENANCE INSTALLED NEW LAMPS & OPERATIONALLY CHECKS GOOD.
EMERGENCY EXIT LIGHT ASSY ABOVE L2 DOOR HAS ONE LAMP INOP. MAINTENANCE INSTALLED NEW LAMP & OPERATIONALLY CHECKS GOOD.
WITH SYSTEM NOT ARMED, CARGO FIRE DISCHARGE LIGHT ILLUMINATED. SYSTEM CHECKED NORMAL PER FIM TASK 26-23-00-810-802. OK FOR SERVICE.
AFTER TAKEOFF TO RSW, CARGO DISCHARGE LIGHT ILLUMINATED FOR 1 HOUR, THEN WENT OUT. MAINTENANCE ACCOMPLISHED FIM TASK 26-23 TASK 802, NO DISCREPANCIES FOUND. SYSTEM CHECKS NORMAL.
AMBER CARGO FIRE (DISCH) LITE ILLUMINATED ON CLIMBOUT. EXTINGUISHED AFTER ABOUT 10 MINUTES. MAINTENANCE OPERATED TEST SEVERAL TIMES COULD NOT DUPLICATE IAW 26-16-00-710-801. OK FOR SERVICE.
AMBER CARGO FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED ON CLIMBOUT. NO CARGO WARNING WAS RECEIVED. THE CARGO FIRE EXTINGUISHING SYSTEM WAS NEVER ARMED AND THE CARGO FIRE DISCHARGE SWITCH WAS NEVER PUSHED. GREEN EXTINGUISHER TEST LIGHTS INDICATED NORMAL SQUIB CIRCUIT CONTINUITY. CARGO FIRE BOTTLE DISCHARGE LIGHT SUBSEQUENTLY EXTINGUISHED ON ITS OWN AFTER APPROX 15 MINUTES. MAINTENANCE CHECKED AND INSPECTED CONNECTOR PLUGS AND CHECKED SYSTEM IAW AMM 26-16-00-710-801. ALL CHECKED NORMAL. NO DEFECTS NOTED. RELEASED TO SERVICE.
PILOT REPORTED R1 DOOR SLIDE FELL OUT OF SLIDE CASE, DOOR WAS DISARMED. MAINTENANCE INSTALLED R1 DOOR ESCAPE SLIDE PACK AND COVER PER TASK 25-66-01-400-801 RII ACCOMPLISHED 2083126.
R1 DOOR SLIDE FELL OUT OF SLIDE CASE, DOOR WAS DISARMED. INSTALLED R1 DOOR ESCAPE SLIDE PACK AND COVER TASK 25-66-01-400-801 RII ACCOMPLISHED 2083126.
PILOT DISCOVERED AUTO BRAKE DISARM LIGHT ILLUMINATED. MAINTENANCE PLACED ON MEL 32-7 AND PERFORMED FIM TASK 32-42 TASK 828. DETERMINED FAULT TO BE INTERMITTENT. REMOVED MEL 32-7.
FWD RIGHT EMERGENCY EXIT WINDOW LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER AMM 33-21-00, OPS CHECKS GOOD.
FOUND LENS FOR EMERGENCY EXIT SIGN MISSING AFT SIDE OF L2 DOOR. INSTALLED A NEW LIGHT LENS ASSY OPS CHECKED EMERGENCY LIGHT SYSTEM, OPS CHECKED GOOD.
BULL NOSE EMERGENCY EXIT LIGHT AT ROW 13ABC INOP. RELAMPED - OPS CHECKED GOOD
Hydraulic "A" system RF after landing. Fault code 293 180 00. Found filter bowl assembly disengaged from filter. Removed & replaced hydraulic system "A" return filter IAW Task 2-11-61-000-802, ops checks good.