N7816B
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2018-10-15 – 2018-10-15 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2018-10-15 – 2018-10-15 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
6 EMERGENCY EXIT LIGHTS INOP. RIGHT HAND STOW BINS 7 AND 8; L2 DOOR HEADER PANEL; AFT ENTRY; G4 AND R2 EXTERIOR EMERGENCY EXIT LIGHTS / [01] PERFORMED A TEST OF EMERGENCY EXIT LIGHTS PER AMM 33-51-00-710 AND WDM 33-51-14. DETERMINED THAT BATTERY PACKS M1672 AND M1673 ARE NOT CHARGING.;[02] REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BATTERY PACKS M1672 AND M1673 AND PERFORMED A SATISFACTORY INSTALLATION TESTS IAW AMM 33-51-06-960-805.;[03] VERIFIED CORRECTIVE ACTION 1 AND 2 COMPLETED;[04] ALL MAINTENANCE COMPLETED FOR THE CARD.
6 EMERGENCY EXIT LIGHTS INOP. RIGHT HAND STOW BINS 7 AND 8; L2 DOOR HEADER PANEL; AFT ENTRY; G4 AND R2 EXTERIOR EMERGENCY EXIT LIGHTS / [01] PERFORMED A TEST OF EMERGENCY EXIT LIGHTS PER AMM 33-51-00-710 AND WDM 33-51-14. DETERMINED THAT BATTERY PACKS M1672 AND M1673 ARE NOT CHARGING.;[02] REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BATTERY PACKS M1672 AND M1673 AND PERFORMED A SATISFACTORY INSTALLATION TESTS IAW AMM 33-51-06-960-805.;[03] VERIFIED CORRECTIVE ACTION 1 AND 2 COMPLETED;[04] ALL MAINTENANCE COMPLETED FOR THE CARD.
PASSENGER CABIN AFT EMERGENCY EQUIPMENT CEILING LIGHT R/H FWD AT SEAT ROW 20FED IS INOP.(MARKED) / [01] FAULT GENERATED IN ERROR;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
SUPPLEMENTAL INFORMATION: FWD SAC DOOR SLIDE LOOSE ; / [01] COMPLETED INSPECTION OF FWD SVC DOOR SLIDE. REPOSITIONED GIRT BAR IN SLIDE APRON. REF AMM 25-66-01
GIRTBAR RETAINER ON FORWARD SERVICE DOOR BROKEN ; / RESECURED GIRTBAR RETAINER ON FWD SRV DOOR WITH 2 NEW RIVETS REF SRM 51-40-02. <BR>REF MT 725-61--06FOR SLIDE REMOVAL ANFD INSTALLATION TO FOM<BR>E136889
AFT SERVICE DOOR SLIDE GIRT BINDS IN DOOR WHEN CLOSING / RETUCKED AFT SERVICE DOOR SLIDE GIRT 2 - FOLD USING HAND PRESSURE. GIRT NOW CLEARS SCUFF PLATE WHEN CLOSING DOOR.
EMERGENCY ISLE ILLUMINATION LIGHT AT BIN 6 LH DOES NOT ILLUMINATE / RELAMPED AND REPLACED LENS OF ROW 6 LH EMERGENCY AISLE ILLUMINATION LIGHT PER AMM 33-51-03-960-801 AND PERFORMED A GOOD INSTALLATION TEST OF ROW 6 LH EMER LIGHT PER AMM 33-51-03-960-801
FWD SERVICE DOOR CUTOUT UPPER STUB FRAME IS CRACKED / REMOVED AND INSTALLED NEW FSD UPPER STAB FRAME; ALL WORK ACCOMPLISHED ON CUSTOMER CARD # U271289. SA-M 326 # A1289821
FSD CUTOUT FWD FRAME UPPER SEAL DEPRESSOR IS CRACKED BETWEEN WL 220 TO 230 / REMOVED & REPLACED FSD CUTOUT FWD FRAME UPPER SEAL DEPRESSOR BETWEEN WL220 TO WL230. PER SRM 51-40-02-0G-0 & IPC 53-11-00-80 PO#814612
VERTICAL STAB TO FUSELAGE SKATE ANGLE CHAFED BS 1090-1120 LT SIDE / REMOVED & REPLACED L/H VERTICAL STAB TO FUSELAGE SKATE ANGLE FROM BS1016-BS1132 PO#809203 PER SRM 51-40-02 & DWG# 148A8310
FWD SERVICE DOOR ; FWD SURROUND SIDEWALL PANEL IS CRACKED AT THE ELECTRICAL OUTLET CUTOUT / REPAIRED FWD SERVICE DOOR; FWD SURROUND PANEL IAW AMM 25-00-00-300-801 STEP 2.I. 59310U 01FEB21
CRACKED STRINGER AT B.S. 540; STRINGER 23 LEFT. / CRACKED STRINGER AT BS 540; STRINGER 23 LEFT REPAIRED IAW ATS ER 21-01193 REV IR. AND PER EA NO:21-153-00353 REV IR. 55981U 11FEB21
ROD ATTACH BRACKET IS BROKEN; LOCATED 5' O/B OF O/B HINGE FOR ACCESS PANEL 551DB / REMOVED AND INSTALLED NEW COLLARS (2) AND ROD ATTACH BRACKET LOCATED 5' O/B OF O/B HINGE FOR ACCESS PANEL 551DB IAW SRM 51-40-02-0G-0 57015U 08FEB21
LH WING FIXED SEAL RETAINER IS CRACKED AT UPPER FLANGE; ORSS 272; AFT OF LH PYLON TRAILING EDGE FAIRING / REMOVED & REPLACED L/H WIND FIXED SEAL RETAINER AT UPPER FLANG; ORSS 272 AFT OF L/H PYLON TRAILING EDGE FAIRING IAW SRM 51-40-02-0G-0 & DWG # 115A2930
CRACKED FLOOR SUPPORT AT B.S. 540; B.L. 0 TO L.B.L. 24.5; W.L. 208.1. / REMOVED AND REPLACED FLOOR SUPPORT AT B.S.540 B.L.0. LBL24.5 W.L.208.1 IAW SRM 51-40-02-0G-0 & SRM 51-40-05 & DWG 143A5240
***CORROSION*** MULTIPLE AREAS OF CORROSION GOUGES ON PASSENGER CABIN SEAT TRACKS AT B.S. 727B-887; R.B.L. 45; W.L. 208.1. / REMOVED AND INSTALLED NEW PASSENGER CABIN SEAT TRACK AT BS727B TO 887; RBL45; WL208.1 PER SRM 51-40-02-0G-0 AND BOEING DWG #146A5300
CORROSION ON FUSELAGE SKIN AT BS 860-1016; LBL 14 TO RBL 14; WL 306.
CORROSION MULTIPLE AREAS OF CORROSION ON PASSENGER CABIN SEAT TRACKS AT BS 727B-887; LBL. 45; WL. 208.1.
DURING INSPECTIONS ON CUSTOMER CARD 15021 A 1 INCH CRACK IN THE BEAR STRAP WAS NOTED AT BS 294. THREE INCHES BELOW STR 8R. ENGINEERING DISPOSITION REQUIRED.
CORROSION MULTIPLE AREAS OF CORROSION ON PASSENGER CABIN SEAT TRACKS AT BS 727B-887; L.BL 24.5; WL 208.1.
***CORROSION*** ON INTERCOSTAL SUPPORT CHANNEL FWD O/B CORNER BS 260 LBL 3 WL 208 / REMOVED AND REPLACED INTERCOSTAL SUPPORT CHANNEL BS360 TO BS270 LBL3 WL208 PER SRM 51-40-02; SRM 51-40-05 AND DWG 141A5210
DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #4 (LOWER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. / FORWARD SERVICE DOOR # 4 (LOWER) BEAM WAS REPLACED ON WORK ORDER: 537115.
SUPPORT INTERCOSTAL IS BENT AT BS 500D+8 LBL 7; WL 156 / REMOVED AND REPLACED INTERCOSTAL SUPPORT AT BS 500D TO 520 WL156 PER SRM 51-40-02; SRM 51-40-05 AND DWG 143A7902
NUT PLATE BROKEN AT BS 494 AT STRINGER 24R / REMOVED AND REPLACED NUT PLATE AT BS 494 STRINGER 24R FCB IAW AMM INTRODUCTION STEP 2SIP AND DWG 143A8321
SEVERAL FASTENERS PULLING THROUGH ONE FASTENER CRACKED 6 O'CLOCK POSITION #2 ENGINE INLET / REPAIRED SEVERAL FASTENERS PULLING THROUGH AND ONE FASTENER CRACKED AT 6 O'CLOCK POSITION ON #2 ENGINE INLET PER SRM 54-10-01-1A-2 ALLOWABLE DAMAGE 2.
FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. / REPAIRED FLIGHT DECK FLOOR DENT AT BS 255; RBL 4 - LBL 14; WL 207; PER SWA EA 1-A53-33179 REV 1
#2 ENGINE INLET COWL OUTER BARREL PANEL HAS DENT WITH GOUGE AT 3 O'CLOCK POSITION 8 INCHES FORWARD OF PANEL AFT EDGE / REPAIRED #2 ENGINE INLET COWL BARREL PANEL DENT WITH GOUGE PER SRM 54-10-01-2R-6 REPAIR 6
GIRT BAR TAB HANGING TO LOW AFT SERVICE DOOR. REPOSITIONED AFT SERVICE DOOR SLIFE, PER SWA MT 725-61-06.
AFT EMERG. BATTERY PACK INOP / R/R AFT EMERGENCY BATTERY PACK IAW AMM 33-51-06. OPS CK. GOOD.
R2 DOOR SLIDE LOOSE / SECURED R2 DOOR SLIDE REF MT 725-61-06; AMM 25-66-01
"Z" FOLD HAS COME OUT OF CONTAINER AT LH AFT SLIDE GIRT REPOSTIONED L2 SLIDE THAT IS HOOKED TO THE GERT BAR REF MM 25-66-01 (DID NOT REMOVE SLIDE FROM COVER) REF SA-M 767 H24793-3
EXIT DOOR SIGN ARROW POINTED AWAY FROM DOOR. / R&R LENS PER AMM.
R/H OVERWING EMERGENCY EXIT WINDOW LIGHT INOP. / FOUND JIFFY SPLICE D11076 DISCONNECTED. CONNECTED SPLICES IAW AMM & WDM.
DTIP- PREVIOUS OPERATOR; F000888; SPLICE REPAIR ON AFT CARGO COMPARTMENT FLOOR TRACK REPAIR SPLICE AT LBL 17.2 BS 767+11-787+13 REQUIRES REPLACEMENT DUE TO FASTENER COUNT 4 VERSUS 5 AND THICKNESS OF THE LOWER FLANGE OF THE TRACK SPLICE 0.080' VERSUS 0.090' IN ADDITION TO FASTENER SPACING IS BELOW THE MINIMUM OF .750' / REMOVED AND REPLACED CARGO TRACK STA 865 TO STA 756 LBL 17.2 PER DWG 146A7500 REV B. ACCOMPLISHED CARGO TRACK SPLICE REPAIR AT STA 756 PER SRM 53-00-53-2R-3
LEFT WING MIDSPAN FIXED TRAILING EDGE BULKHEAD AFT VERTICAL CURVED SEAL RETAINER IS CRACKED WITH PIECE BROKEN OFF / REMOVED AND REPLACED SEAL RETAINERS IAW B737 AIPC 57-50-00-25 AND B737 SRM 51-40-02-0G-0
DTIP PREVIOUS OPERATOR STRAP REPAIR (T402405) ON RH PASSENGER CABIN CREASE BEAM FROM BS 650 TO 673 - REQUIRES REPLACEMENT / PREVIOUS REPAIR AT STA 650-673 IAW EA 190095 IR AND SWA EA 1-753-34321 REV IR DATED 25MAR19.
HORIZONTAL PRESSURE DECK WEB CRACKED BETWEEN BS 663 TO BS 675, RBL 41. REPAIRED WEB IAW SRM.
HORIZONTAL PRESSURE DECK WEB CRACKED BETWEEN BS. 663 TO BS. 675, LBL 31, AT FORWARD SECTION OF BEAD. / REPAIRED DECK IAW EA AND SRM.
CABIN FLOOR STRUCTURE RT CREASE BEAM WEB LOWER SURFACE CORRODED BETWEEN BS 716 TO BS 727. R&R RT CREASE BEAM WEB IAW SRM AND DWG.
FLOOR SUPPORT L-ANGLE ATTACH WEB CRACKED AT BS 540, BETWEEN LBL 26 TO LBL 45. R&R SUPPORT BREAK ASSEMBLY IAW SRM.
COMMON TO STRINGER CIRCUIT BREAKER ATTACH ANGLE CORRODED AT BS 259.5+1.5, STR 12L, SLOTTED HOLE. R&R STRINGER CLIP IAW SRM AND DWG.
CIRCUIT BREAKER ATTACH ANGLE CRACKED IN RADIUS AT BS 259.5+1.5, STR 8L. R&R STRINGER CLIP IAW SRM AND DWG.
VERTICAL STABILIZER PANEL 322A HAS ELONGATED HOLE. MARKED. / VERTICAL STAB PANEL 322 A HAS ELONGATED HOLE EVALUATED HOLE SIZE AS .450' MAX ALLOWED HOLE SIZE = .312' IS OUT OF LIMITS IAW 737-700 SRM 51-40-0G-05-0 FIG 3 VERIFIED NEW VERTICAL STAB PANEL 322 A AS P/N 176A3009U9 IAW 737-700 AIPC 65-33-11-02 AND A TAG WN3941 PICKED UP HOLES IN NEW PANEL 322 A IAW 737-700 SRM 51-40-05-0G-0 *ABOVE PANEL WILL BE INSTALLED ON JPANEL-320-CLOSE SN # 1388 WO # 38939-3300-0015*
AFT CARGO; STA 787+5; STR 23L; TIEDOWN PLATE HAS CORROSION / CARGO TIEDOWN PLATE AT STA 787 STR 23L DOES NOT HAVE ENTRIES IN THE SRM. PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9C. REMOVED TIEDOWN PLATE IAW SRM 51-40-02-0G-0. FABRICATED; LOCATED; AND DRILLED NEW PLATE IAW BOEING DWG # 146A9403 REV AE AND SRM 51-40-05-0G-0; TREATED AND PRIMED NEW PLATE IAW AMM 51-21-45-370-803 A+D AMM 51-21-72-370-804; ACCOMPLISHED CONFORMITY INSPECTION ON PLATE P/N 146A9403-13 AND VERIFIED IT CONFORMS TO THE SPECIFICATIONS FOUND IN BOEING DWG# 146A9403 REV AE INSTALLED NEW TIE DOWN PLATE AT STA 792 STR 23L IAW SRM 51-40-02-0G-0 AND 146A9401 REV D.
AFT CARGO; STA 787+5; STR 22L; TIEDOWN PLATE HAS CORROSION / CARGO TIEDOWN PLATE AT STA 792 STR 22L DOES NOT HAVE ENTRIES IN THE SRM. PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9C. REMOVED TIEDOWN PLATE IAW SRM 51-40-02-0G-0. FABRICATED; LOCATED; AND DRILLED NEW PLATE IAW BOEING DWG # 146A9403 REV AE AND SRM 51-40-05-0G-0; TREATED AND PRIMED NEW PLATE IAW AMM 51-21-45-370-803 AND AMM 51-21-72-370-804; ACCOMPLISHED CONFORMITY INSPECTION AND VERIFIED PLATE P/N 146A9403-13 CONFORMS TO THE SPECIFICATIONS FOUND IN BOEING DWG# 146A9403 REV AE INSTALLED NEW TIE DOWN PLATE AT STA 792 STR 22L IAW SRM 51-40-02-0G-0 AND BOEING 146A9401 REV D.
PASSENGER CABIN; STA 294; FLOOR LINE; ATTACH ANGLE CRACKED IN RADIUS; COMMON TO CREASE BEAM WEB AND CREASE BEAM INNER CORD / REMOVED AND REPLACED PASSENGER CABIN STA 294; FLOOR LINE ATTACH ANGLE COMMON TO CREASE BEAM WEB AND INNER CHORD IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A8310 SHT 1 REV: D ATAG# 141831203 A06555
PAX CABIN LH SIDE AT STA-616 TO STA-639 AT STR-7L CHANNEL ASSY. IS CORRODED AT BOTH ENDS AND IN LIGHTENING HOLES. / REMOVED CHANNEL ASSY AT PASSENGER CABIN L/H SIDE AT STA 616 TO STA 639 STR 7L IAW B737-700 DWG 412A2250 REV: -; SRM 51-40-02-0G-0 AND INSTALLED CHANNEL. EA 190189 P1 CANCELLED ATAG # A24409
AFT CARGO; STA 787; STR 23L TO 25L; SIDEWALL SUPPORT ANGLE HAS CORROSION AT NUT PLATE HOLES / SIDEWALL SUPPORT ANGLE (-89) DOES NOT HAVE ENTRIES IN SRM. PART REPAIRABLE BY REPLACEMENT. PE SRM 51-10-02-0G-0 STEP 9.C. REMOVED AND REPLACED ANGLE PER SRM 51-40-02-0G-0 AND DWG 146A1262 REV -. ANGLE PART# 146A9403-89 P/N 146A9403-89
AFT CARGO; STA 727A+19; LBL 23; BAFFLE ANGLE HAS CORROSION ON LOWER SURFACE UNDER NUTPLATE / REMOVED AND EVALUATED CORROSION ORIGINAL THICKNESS .045' LOSS OF .011' WITH .034' REMAINING. BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 REMOVED AND REPLACED BAFFLE STA 727A - 727B LBL 23 PART # 146A7505-1 PER SRM 51-40-02-0G-0 AND DWG 146A7500 REV B
STRINGER CLIP CRACKED AT BS 277, STR 10R. R&R STRINGER CLIP IAW SRM & DWG.
AFT CARGO Z-ANGLE CORRODED BETWEEN BS 747+15 TO BS 807+5, LBL 21. R&R AFT CARGO Z-ANGLE PER SRM.
AFT CARGO, FLOOR SUPPORT RAIL CORRODED AROUND NUTPLATE HOLES BETWEEN BS 794 TO BS 847, RBL 14. R&R CARGO TRACK PER DWG AND SRM.
CENTER CABIN INBOARD RAIL ATTACH FASTENER CRACKED AT BS 827, STR 8L. REPAIRED FRAME IAW EA.
AFT CARGO STA 727 TO 767; RBL 21; Z-ANGLE HAS CORROSION / REMOVED AND EVALUATED CORROSION. ORIGINAL THICKNESS .040' LOSS OF .015' WITH .025' REMAINING. BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED AFT CARGO RH Z-ANGEL STA 727-767 PER SRM 51-40-02-0G-0 AND DWG 146A7502 REV A
AFT CARGO; STA 727 TO STA 747+15; LBL 21; Z-ANGLE HAS CORROSION / AFT CARGO LH Z-ANGEL REPLCED ON WORK CARD X896022. Z-ANGE REPLACED FROM STA 727-847
AFT CARGO; STA 767 TO 794; RBL 24; SPLASH SHIELD HAS CORROSION ON UPPER AND LOWER SURFACE / REMOVED AND EVALUATED CORROSION. ORIGINAL THICKNESS .051' LOSS OF .011' WITH .040' REMAINING BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1. REMOVED AND REPLACED AFT CARGO FWD SHILED PART # 146A8127-1 PER SRM 51-40-02-0G-0 AND DWG 146A0081 REV C P/N 146A8127-1 ATAG # WN1704
AFT CARGO; STA 787+5; STR 24L; TIEDOWN PLATE HAS CORROSION / CARGO TIEDOWN PLATE AT STA 792 STR 24L DOES NOT HAVE ENTRIES IN THE SRM. PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9C. REMOVED TIEDOWN PLATE IAW SRM 51-40-02-0G-0. FABRICATED; LOCATED; AND DRILLED NEW PLATE IAW DWG # 146A9403 REV AE AND SRM 51-40-05-0G-0; TREATED AND PRIMED NEW PLATE IAW AMM 51-21-45-370-803 AND AMM 51-21-72-370-804; ACCOMPLISHED CONFORMITY INSPECTION AND VERIFIED PLATE P/N 146A9403-13 AND VERIFIED IT CONFORMS TO THE SPECIFICATIONS FOUND IN BOEING DWG# 146A9403 REV AE INSTALLED NEW TIE DOWN PLATE AT STA 792 STR 24L IAW SRM 51-40-02-0G-0 AND BOEING 146A9401 REV D.
AFT CARGO FLOOR PANEL 140CF HAS CORROSION AROUND PERIMETER OF PANEL / PANEL 14OCF REPLACED ON CARD # X895804
AFT CARGO COMPARTMENT FLOOR SUPPORT BRACKET CRACKED AT BS 947, LBL 13, AFT BULKHEAD. R&R BRACKET IAW SRM.
STUB FRAME CRACKED AT BS 294, WL 208, COMMON TO INNER CREASE BEAM ANGLE. R&R STUB FRAME IAW DWG AND SRM.
RIGHT OUTBOARD AFT FLAP; INBOARD TRAILING EDGE CORNER HAS EVIDENCE OF DELAM / REPAIRED R/H WING O/B FLAP; I/B CORNER ON UPPER SURFACE OF SKIN IAW SRM 57-53-01-2R-4 AND SRM 51-70-10-2R-0
FORWARD CARGO PIT DOOR SURROUND AFT SHIELD ON UPPER AND LOWER SURFACE CORRODED BETWEEN BS 492 TO BS 500A, RBL 24. R&R SHIELD IAW SRM & DWG.
PAX CABIN FLOOR 231XF HAS MISSING FIBERS ON UPPER SURFACE / REPAIRED PAX CABIN FLOOR 231XF UPPER SURFACE IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 REV 66
AFT CARGO COMPARTMENT THRESHOLD; FWD OF DOOR; FLOOR TIE DOWN PLATE CORRODED / REPLACED PARTS ON TABLE P/N 450A1611-1 ON ATAG# A02816 IAW IPC 25-52-10-02P/N 456A2611-1 ATAG# A02816
FORWARD CARGO PIT L/H BAFFLE CLIP AFT SIDE OF STA 500C LBL25 IS CRACKED / REMOVED CLIP FWD CARGO STA 500C LBL 25 IAW SRM 51-4-02-09-0. RECEIVED NEW CLIP P/N -143A750245 ON A TAG# A17245 IAW BOEING DWG #143A7505 REV. A LOCATED AND DRILLED NEW CLIP IAW SRM 51-40-05-09-0 AND BOEING DWG #145A7505 REV A. INSTALLED NEW CLIP FWD CARGO AT STA 500C LBL 25 IAW BOEING DWG #143A7505 REV A. A TAG# A17245
FORWARD CARGO PIT L/H BAFFLE CLIP FORWARD SIDE OF STA 500C LBL25 IS CRACKED / REMOVED INTERCOSTAL FROM STA 500B-500C LBL25 IAW SRM 51-40-02-09-0. REMOVED CLIP IAW SRM 51-40-02-09-0. RECEIVED NEW CLIP P/N 143A75024159 ON ATAS #A56050 IAW BOEING DWG#143A7505 REV A. LOCATED AND DRILLED NEW CLIP IAW SRM 51-40-05-09-0 AND BOEING DWG #143A7505 REV A. INSTALLED NEW CLIP FWD CARGO AT STA 500C LBL25 IAW BOEING DWG#143A7505 REV A. INSTALLED INTERCOSTAL AT STA 500B-500C LBL25 IAW BOEING DWG#143A7505 REV A. A TAG# A56050
RH OVER WING TO BODY FAIRING 195CR FWD EDGE AT RADIUS HAS CRACK / REPAIRED RH OVERWING TO BODY FAIRING 195CR EDGE AT RADIUS IAW B737-700 SRM 53-60-70-2R-1 REPAIR 1 REV 66
FORWARD CARGO PIT LT BAFFLE CLIP FORWARD SIDE CRACKED AT BS 500B, LBL 25. R&R CLIP IAW SRM & DWG.
FORWARD CARGO PIT LT BAFFLE CLIP AFT SIDE OF FRAME CRACKED AT BS 400, LBL 25. R&R CLIP IAW SRM & DWG.
AFT CARGO COMPARTMENT THRESHOLD; AFT OF DOOR; FLOOR TIE DOWN PLATE CORRODED / REPLACED PART ON TABLE 143A2611-2 ON ATAG #A69675 IAW IPC 25-52-10-02
CABIN SIDEWALL PANEL 231YHW MISSING ESCAPE LENS. R&R SIGN LIGHT ASSEMBLY IAW AMM.
LT OVERWING EXIT SIGN INOP. R&R BATTERY PER AMM.
RT OVERWING EXIT SIGN INOP. R&R BATTERY PER AMM.
#6 FLAP TRACK FAIRING TAILCONE SEPERATING;MULTIPLE LOOSE FASTENERS / REPLACED FLAP TRACK FAIRING TAILCONE (#6) IAW AMM 27-51-28
SUPPLEMENTAL INFORMATION: R/H WING; I/B MAIN FLAP O/B LOWER SKIN IS SEPARATED; 23.5' W X 10.0' D / REMOVED AND REPLACED R/H I/B T/E FLAP WEDGE MPN 113A2500-14 ATAG WN5499 IAW BOEING DWG 113A2100 REV B737-700 SRM 51-40-02
EMERGENCY LIGHT BATTERY FAILED TEST AT ROW 15 DEF. R&R BATTERY PER MM.
TAIL LEFT ELEVATOR BAY #3 BALANCE BAY PANEL VERTICAL SIDE CRACKED UPPER RIGHT SIDE NEAR HINGE ASSY. / REMOVED AND REPLACED CRACKED PANEL ON L/H ELEVATOR #3 BALANCE BAY PANEL AND HINGE ASSY PER SRM 51-10-02. INSTALLED L/H ELEVATOR #3 BALANCE BAY PANEL AND HINGE ASSY PER AMM 27-31-41
EMERGENCY LIGHT BATTERY FAILED TEST AT ROW 1 ABC. R&R BATTERY PER MM.
EMERGENCY LIGHT BATTERY FAILED TEST AT ROW 3 DEF. R&R BATTERY PER MM.
EMERGENCY LIGHT BATTERY FAILED TEST AT ROW 6 DEF. R&R BATTERY PER MM.
EMERGENCY LIGHT BATTERY FAILED TEST AT ROW 16 DEF. R&R BATTERY PER MM.
R1 DOOR SLIDE GIRT BAR STOP BROKEN. INSTALLED A GIRT BAR STOP IAW MT.
AIR TURNBACK, LEFT OVERWING LIGHT ILLUMINATED DURING TAKE OFF ROLL. CLIMBED TO 19,000 FEET PRESSURIZATION ABNORMALITY FELT. R&R AFT EMERGENCY EXIT DOOR INDICATION SWITCH.
AIR TURNBACK, LEFT OVERWING LIGHT ILLUMINATED DURING TAKE OFF ROLL. CLIMBED TO 19,000 FEET PRESSURIZATION ABNORMALITY FELT. R&R FORWARD EMERGENCY EXIT DOOR INDICATION SWITCH.
R/H WING FIXED TRAILING EDGE UPPER PANEL ABOVE #2 PYLON AFT FAIRING HAS CRACKED VERTICAL SEAL RETAINER / R/R RETAINER IAW SRM 51-40-02.
LT EMERGENCY BULLNOSE LIGHT LENS MISSING AT ROW 9. INSTALLED LENS PER SIP.
DECLARED EMERGENCY, TRAILING EDGE FLAPS DID NOT EXTEND PAST 5 DEGREES WHEN FLAP LEVER WAS PLACED TO 15 AND 30 DEGREES ALTERNATE FLAP SWITCH USED TO EXTEND FLAP TO 15 DEGREES. R&R RIGHT FLAP POSITION TRANSMITTER PER AMM.
AFT GALLEY EMERGENCY EXIT SIGN PARTIALLY DETACHED FROM CEILING. R&R SIGN PER MM.
FORWARD ENTRY EMERGENCY EXIT LIGHT LENS BROKEN. INSTALLED LENS IAW AMM.
R2 DOOR EMERGENCY EVAC SLIDE LOOSE ON BOTTOM. SECURED THE SLIDE IAW AMM.
L2 DOOR SLIDE LOOSE ON BOTTOM. SECURED SLIDE IAW MT.
FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500 - 500D, LBL 23. R & R THE SIDEWALL SUPPORT IAW SRM.
FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500 - 500A, RBL 23. R & R THE SIDEWALL SUPPORT IAW SRM.
AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 - 947, RBL 25. R & R THE SIDEWALL SUPPORT IAW SRM.
AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT ANGLE CRACKED AT BS 727A+6. R&R SUPPORT IAW SRM AND DWG.
AFT CARGO BAY RT FLOOR TO SIDE WALL SUPPORT ANGLE CORRODED BETWEEN BS 727 TO BS 767. R&R SUPPORT IAW SRM AND DWG.
LT FLOOR TO SIDE WALL SUPPORT ANGLE CORRODED BETWEEN BS 727 TO BS 767. R&R SUPPORT IAW SRM AND DWG.
AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 794, RBL 25. R&R SUPPORT IAW SRM AND DWG.
AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT ATTACH CLIP CORRODED AT BS 768, RBL 25. R&R ATTACH CLIP IAW SRM AND DWG.
AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO 847, LBL 25. R & R SIDWALL SUPPORT IAW SRM AND DWG.
AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT SHIELD CORRODED BETWEEN BS 847 - 867, RBL 25. R & R THE SHIELD IAW SRM.
MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 39. REPAIRED THE BULKHEAD WEB IAW SRM.
LT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 40. REPAIRED WEB PER SRM.
FORWARD GALLEY FLASH LIGHT STRAP BROKEN. R&R STRAP IAW SIP.
R1 DOOR EXIT SIGN AT FLOOR LEVEL INOPERATIVE. R & R THE SIGN IAW MM.
R1 DOOR EMERGENCY EVAC SLIDE CONTAINER GIRT BAR HOOK LOOSE. R & R HOOK ASSY IAW SRM.
FORWARD NR 2 EMERGENCY FLASHLIGHT STATUS LIGHT INOPERATIVE. R & R BATTERY IAW MM.
R1 DOOR EMER EVAC SLIDE GIRT BAR BRACKET BROKEN. R & R BRACKET IAW SRM.
L1 DOOR EMER EVAC SLIDE LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.
R2 DOOR EXTERIOR EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.
RIGHT EMER EXIT LIGHT LENS DIRTY, FWD AFT CARGO BAY. CLEANED LENS IAW AMM.
DOME LIGHT BEHIND PILOTS SEAT GOING TO EMER EXIT LIGHT FIXTURE, WIRE BROKEN. R & R LIGHT IAW AMM.
LEFT STOW BIN EMER EXIT LIGHT INOPERATIVE AT ROW 12. ADJUSTED BATTERY PACK IAW AMM.
AFT CARGO DOOR CUT OUT AFT CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.
AFT CARGO BAY FLOOR STRAP CORRODED AT BS 727D+5.6 BETWEEN LBL 20 - RBL 20. R & R STRAP IAW SRM.
LEFT WING OTBD AFT FLAP OTBD AFT CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.
WHILE WORKING LT FILLET FAIRING MOD FOUND WEB ASSEMBLY TO BE CRACKED. R & R WEB IAW SRM & DWG.
LEFT CREASE BEAM WEB CORRODED AT BS 685, LOWER SURFACE NUT CLIP HOLE. R & R WEB IAW DWG & SRM.
LEFT CREASE BEAM WEB CORRODED BETWEEN BS 639 - 663, LOWER SURFACE NUTPLATE HOLES. R & R WEB IAW SRM & DWG.
RIGHT CREASE BEAM WEB CORRODED AT BS 685, LOWER SURFACE NUTPLATE HOLE. R & R WEB IAW DWG & SRM.
AREA AFT OF AFT CARGO BAY ON SUPPORT ANGLE CORRODED AT BS 967.5, BETWEEN STRINGER 27L - 27R. R & R ANGLE IAW DWG & SRM.
LEFT CREASE BEAM INNER CHORD CORRODED AT BS 727, UPPER SURFACE. REPAIRED CHORD IAW SRM.
LEFT CREASE BEAM INNER CHORD CORRODED AT BS 639, UPPER SURFACE. R & R CREASE BEAM IAW SRM.
RIGHT CREASE BEAM ANGLE CORRODED AT BS 698. R & R ANGLE IAW SRM.
AFT OF AFT CARGO BAY INTERCOSTAL CORRODED AT FWD SIDE OF FRAME BS 967.5, STRINGER 24R. R & R INTERCOSTAL IAW DWG & SRM.
LEFT CREASE BEAM INNER CHORD CORRODED AT BS 650, UPPER SURFACE. R & R CREASE BEAM IAW SRM & DWG.
AFT OF AFT CARGO BAY ON FRAME INNER FLANGE CORRODED AT BS 986.5, BETWEEN STRINGER 27L - 27R. REPAIRED FRAME IAW EA.
RIGHT WING SPAR FWD TRUNNION FITTING UPPER & LOWER INBD & OTBD BORE CHAMFERS CORRODED. REPAIRED FITTING IAW EA.
FRAME TO FLOOR SUPPORT ANGLE CRACKED AT BS 827, RBL 20. R & R ANGLE IAW SRM.
FRAME TO FLOOR SUPPORT ANGLE CRACKED AT BS 807, RBL 20. R & R ANGLE IAW SRM & DWG.
FLOOR TO SIDE WALL SUPPORT ANGLE CORRODED BETWEEN BS 727 - 767, RBL 22. R & R ANGLE IAW SRM.
FLOOR TO SIDEWALL SUPPORT ANGLE CORRODED BETWEEN BS 727 - 847, LBL 22. R & R ANGLE IAW SRM.
FRAME CORRODED AT BS 727D, STRINGER 23L. REPAIRED FRAME IAW SRM & DWG.
SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B, LBL 45. REPAIRED FLANGE IAW EA.
SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B, RBL 45. REPAIRED FLANGE IAW ER & EA.
SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B, RBL 25. REPAIRED FLANGE IAW ER & EA.
FUSELAGE SKIN EXTERNAL SURFACE DAMAGED UNDER FWD END OF DORSAL FIN BETWEEN BS 855 - 873, BETWEEN LBL 4 TO RBL 4. REPAIRED SKIN IAW ER & EA.
RIGHT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A - 500D. R & R SUPPORT IAW SRM & DWG.
STRINGER CLIP CRACKED AT BS 480+15, STRINGER 24L. R & R CLIP IAW DWG & SRM.
INTERCOSTAL WEB CORRODED AT BS 990, STRINGER 20L. R & R WEB IAW SRM & DWG.
FLOOR BULKHEAD WEB CRACKED AT BS 1016, RBL 35. R & R WEB IAW SRM.
BULKHEAD TO FLOOR WEB CORRODED AT BS 1016, BETWEEN RBL 17 - 27. R & R WEB IAW SRM & DWG.
BULKHEAD TO FLOOR WEB CORRODED AT BS 1016, BETWEEN RBL 8 - 16. R & R WEB IAW SRM & DWG.
LEFT WING NR 6 FLAP TRACK CANOE FAIRING CRACKED AT THE NR 13 FASTENER HOLE AFT END OF LOCATION. REPAIRED FAIRING IAW SRM & EA.
LEFT WING NR 6 FLAP TRACK CANOE FAIRING CRACKED AT THE NR 10 FASTENER HOLE AFT END OF LOCATION. REPAIRED FAIRING IAW SRM & EA.
L2 DOOR EMER EVAC SLIDE CASE END CAP ON BUMPER MISSING. R & R END CAP IAW SRM.
R1 DOOR EMER EVAC SLIDE Z FOLD OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
FUSELAGE FRAME CRACKED AT BS 747, STRINGER 8R. REPAIRED FRAME IAW EA.
LEFT CEILING PANEL EMER EXIT LIGHT HOUSING DAMAGED AT BS 627. R & R LIGHT IAW MM.
LEFT EMER EXIT LIGHT CONNECTOR D11088 DAMAGED. R & R D11088 IAW WDM.
LEFT EMER EXIT LIGHT CONNECTOR D11100 DAMAGED. R & R CONNECTOR IAW WDM.
LEFT EMER EXIT LIGHT CONNECTOR D11326 DAMAGED. R & R CONNECTOR IAW WDM.
LEFT EMER EXIT LIGHT CONNECTOR D11330 DAMAGED. R & R CONNECTOR IAW WDM.
LEFT EMER EXIT LIGHT CONNECTOR D11338 DAMAGED. R & R CONNECTOR IAW WDM.
LEFT EMER EXIT LIGHT CONNECTOR D11342 DAMAGED. R & R CONNECTOR IAW WDM.
RIGHT EMER EXIT LIGHT CONNECTOR D11098 DAMAGED. R & R CONNECTOR IAW WDM.
FUSELAGE FRAME CRACKED AT BS 520, STRINGER 8R. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED FRAME IAW EA.
RIGHT EMER EXIT LIGHT CONNECTOR D11102 DAMAGED. R & R CONNECTOR IAW WDM.
RIGHT EMER EXIT LIGHT CONNECTOR D11328 DAMAGED. R & R CONNECTOR IAW WDM.
RIGHT EMER EXIT LIGHT CONNECTOR D11332 DAMAGED. R & R CONNECTOR IAW WDM.
RIGHT EMER EXIT LIGHT CONNECTOR D11336 DAMAGED. R & R CONNECTOR IAW WDM.
FUSELAGE FRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 520, STRINGER 8L. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 360, STRINGER 8L. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 727D, STRINGER 8R. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 500C, STRINGER 8R. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 480, STRINGER 8R. REPAIRED FRAME IAW EA.
FORWARD CABIN FLOORBEAM CORRODED AT BS 328, BETWEEN RBL 45 - 58, UPPER & LOWER SURFACE. REPAIRED FLOORBEAM IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 344 - 360, RBL 1. REPAIRED INTERCOSTAL IAW ER & EA.
FORWARD CABIN FLOORBEAM CORRODED AT BS 344, BETWEEN RBL 6 TO LBL 56. REPAIRED FLOORBEAM IAW ER & EA.
FORWARD CABIN FLOORBEAM CORRODED AT BS 294, RBL 12. REPAIRED FLOORBEAM IAW EA.
LEADING EDGE OF RUDDER SKIN CRACKED NEAR NR 5 HINGE LOCATION ON RT SIDE. REPAIRED RUDDER IAW MM.
FUSELAGE LOWER BULKHEAD CHORD CRACKED AT BS 540, STRINGER 22L, FWD HOLE 2ND FROM TOP. REPAIRED CHORD IAW ER & EA.