N552WN
Registered owner: UMB BANK N A TRUSTEE, UT (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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
197 reports on file, 2010-10-12 – 2020-03-23.
Part: SPAR — CORRODED (RT WING) · airframe 59,169 hrs · 33,658 cycles
**CORROSION*** EVIDENCE OF CORROSION AT RIGHT WING FRONT SPAR WEB AT IFSS 119 COMMON TO BOOST PUMP UPPER AND LOWER BONDING JUMPER FASTENER HOLES / REPAIRED CORROSION PER EA 20-157-00171 AND ATS ER 20-02273; REV IR AT RIGHT WING FRONT SPAR WEB AT IFSS 119..
Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,169 hrs · 33,658 cycles
EMERGENCY EXIT LIGHT ASSEMBLY L1063 OVER FORWARD SERVICE DOOR HAS BULBS OUT. REPLACED BULB ON EMERGENCY EXIT LIGHT ASSEMBLY L1063 AND PERFORMED GOOD TEST PER AMM 33-51-01-960-801 93105U 20MAR20
Part: WIRE — DAMAGED (CABIN) · airframe 59,169 hrs · 33,658 cycles
EMERGENCY EXIT AISLE LIGHT AT SEAT ROW 17ABC IS OUT. RE-TERMINATED W3142-0455-20 INTO GD3756 AND PERFORMED GOOD OPERATIONAL TEST OF EMERGENCY EXIT AISLE LIGHT AT SEAT ROWN 17ABC AS DOCUMENTED ON SA-M 326 A1292282.
Part: PANEL — DENTED (VERTICAL STAB) · airframe 59,169 hrs · 33,658 cycles
DENT ON VERTICAL STAB L/E PANEL AT L/E STA 262 TRIMMED OUT THE DAMAGE PART OF THE SKIN ON VERTICAL STAB L/E PANEL AT L/E STA 262. DIMENSIONS 1.6" X 1.25" AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-01-2R-1. 88920U 14 MAR 20
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
FLOOR PANEL 241ACF HAS DAMAGED INSERTS. REPAIRED ADDITIONAL DAMAGE TO LOWER SURFACE AND REPLACED DAMAGED INSERTS IAW SRM 53-00-50-2R-1 AND DWG 147A5810-13. 59198U, 3.9.20.
Part: PANEL — CRACKED (LE SLAT) · airframe 59,169 hrs · 33,658 cycles
#7 SLAT COVE PANEL 624DB IS CRACKED REMOVED AND REPLACED #7 SLAT COVE PANEL 624DB. FABRICATED FROM 7075 T6 BARE 0.063" LOT # 5057680 IAW. SRM 51-40-02. AND DWG 114A8121 88920U 21MAR20
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
FLOOR PANEL 242UF HAS SURFACE DAMAGE 7" FROM AFT EDGE 6" FROM OB EDGE. FLOOR PANEL 242UF SURFACE DAMAGE ENTIRE PANEL TOP SURFACE WAS REPAIRED IAW SRM 53-00-50-2R-1
Part: FITTING — CORRODED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON AFT DRAIN MAST FITTING AT B.S. 990; BETWEEN STRINGERS 24 AND 25 LEFT; AROUND GROUND WIRE ATTACH POINT / REMOVED AFT DRAIN MAST FITTING AT BS 990 BETWEEN STRINGERS 24-25 LH AND REPLACED DUE TO NO ALLOWABLE DAMAGE IN SRM. IAW SRM 51-40-02 AND DRAWING 197A7443
Part: RIB — NOT REPORTED (RH HORIZ STAB) · airframe 59,169 hrs · 33,658 cycles
(SKYLINE DTIP) RH HORIZONTAL STAB STA 120.3 RIB LOWER OUTER FLANGE REPAIR 6TH FASTENER FROM FRONT OF REPAIR REQUIRES REPLACEMENT. (REF ESR# 20-01893) MOD / REPAIRED RH HORIZ. STAB STA 120.3 RIB LOWER OUTER FLANGE IAW SWA EA 1-755-4669 REV IR AND ATS ER 20-0194 REV IR PERMANENT ACTION REQUIRED: THE RIB REPAIR IS CLASSIFIED AS CATEGORY C PER 737-700 SRM 51-00-06. PERFORM A CATEGORY A REPAIR ON THE RIB WITHIN 2 YEARS FROM THE DATE OF THIS APPROVAL. RECOMMEND 737-700 SRM 55-10-09 REPAIR 5. REF: TCO-SWA-20-0187 REMOVABLE COMPONENT: P/N: 186A2000-32 S/N: IC0105
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
CRACKED SUPPORT ANGLE AT ACB BEHIND WATER SERVICE PANEL BS918 RBL11 WL170. REMOVED AND REPLACED SUPPORT ANGLE AT ACB BEHIND WATER SERVICE PANEL BS 918, RBL 11, WL 170 P/N 7531385 PO# 785210 IAW SRM 51-40-02 AND DWG 147A7221 89004U 06MAR20
Part: SPLICE — CORRODED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON FLOOR PANEL SUPPORT SPLICE AT AFT CARGO BAY BS887 RBL20 TO LBL6 WL172. REMOVED AND INSTALLED NEW FLOOR PANEL SUPPORT SPLICE AT ACB B.S. 887 RBL 20 TO LBL 6 WL 172 ITEM # 7530863 IAW SRM 51-40-02-0G-0 STEP 2. DWG # 146A7500, AIPC 53-42-11-30 57319U 03-06-20
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS794 - BS847 RBL23 WL160. REMOVED DAMAGE FROM ACB SUBTHRESHOLD WEB IN AREAS OF 13" X 8" ORIGINAL MATERIAL THICKNESS 0.045" MORE THAN 50% MATERIAL LOST FOUND TO BE OUT OF LIMIT IAW SRM 53-60-15-1A-1 LOCATED AND DRILLED NEW SUBTHRESHOLD WEB ITEM # 7531818 IAW SRM 51-40-05-0G-0 AND DWG # 146A8123 AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG # 146A8120
Part: ANGLE — CORRODED (APU BAY) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON APU CAVITY LEFT HAND INSULATION BLANKETS LOWER ATTACH POINT AT B.S. 1090-1154. LBL 23 / REMOVED AND REPLACED LH LOWER ANGLE ON APU CAVITY PO# 784374-1 IAW SRM 51-40-02; DWG 148A8600 AND DWG 148A8615
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS827 - BS727 LBL21 WL158. REPLACED FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS 847 LBL 21 WL 158 IAW SRM 51-40-02-0G-0 AND DRAWING # 146A7502 P/N 146A7502-3 DUE TO REMOVED CORROSION ON MULTPLE AREA ON FLOOR TO SIDEWALL SUPPORT AT ACB BS 727 - BS 827 LBL 21 WL 158, AREA 40" X 2" MAX MAT. LOSS 0.027" ORIGINAL THICKNESS 0.040", FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 DETAIL 4.A.(2) FIG. 103. 54861U,
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
CRACKED FLOOR SUPPORT AT PASSENGER CABIN BS540 RBL1 WL208. REMOVED, LOCATED AND DRILLED FLOOR SUPPORT STA. 540 RBL 1 PER SRM 51-40-02 PAR 7D, SRM 51-40-05 FIG. 4 AND DWG. 143A0060. OK TO INSTALL. LEAD 59 29FEB20 INSP 45 27FEB20 INSTALLED FLOOR SUPPORT PER SRM 51-40-02 PAR 7D AND DWG. 143A0060. 91195U 2.29.20
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 500A-500D, R.B.L. 22, W.L. 155. REMOVED CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500A-500D RBL22 AREAS: 1.2"X0.8"; 1"X0.7"; 0.8"X0.6" AND 1.4"X0.8" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 STEP 4.A.(3) FIG 103 DETAIL D. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BS500A-500D RBL 22, FABRICATED FROM EXTRUSION BAC 1496-444 #7075T6 LOT #1426040-1 IAW SRM 51-40-02 AND DWG 143A7500 REV A 89008U 05MAR20
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
CRACKED STRINGER CLIP AT PASSENGER CABIN BS727E S-6R. MARKED REJECTION: OF O/B FASTENER DAMAGED ON STR CLIP BS 72 7E S-6R. INSP 345 02MAR20 REMOVED AND REPLACED STRINGER CLIP AT PASSENGER CABIN B.S 727E S-6R IAW SRM 51-40-0G-0 DWG 146A112 REV. C SH .1 AND SRM 51-40-02-0G-0 STEP 4(B). 92430U 02MAR2020
Part: SHIELD — CORRODED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON FORWARD CARGO BAY SHIELD AT B.S. 420-440, R.B.L. 22, W.L. 155. REPLACED FWD CARGO BAY SHIELD AT BS 420-440, RBL 22 AS PER SRM 51-40-02-0G-0 AND DRAWING # 143A0080 ID: 0019, SHIELD WAS EVALUATED AND NO FOUND ALLOWABLE DAMAGE ON SRM, PART REPAIRABLE BY REPLACEMENT AS PER 51-70-02-0G-0 SRM STEP. 9. C.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 400-420, R.B.L. 22, W.L. 155. REMOVED AND REPLACED FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 400-420 RBL 22 IAW SRM 51-40-02-0G-0 AND DWG 143A7505
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 500A-500D; R.B.L. 22; W.L. 155. / REMOVED CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT BS 500A-500D RBL22 AREAS: 1.2'X0.8'; 1'X0.7'; 0.8'X0.6' AND 1.4'X0.8' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 STEP 4.A.(3) FIG 103 DETAIL D. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BS500A-500D RBL 22; FABRICATED FROM EXTRUSION BAC 1496-444 #7075T6 LOT #1426040-1 IAW SRM 51-40-02 AND DWG 143A7500 REV A 89008U 05MAR20
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON FORWARD CARGO BAY SUB WEB THRESHOLD AT B.S. 440-494, R.B.L. 28, W.L. 155. REMOVED CORROSION ON FCB SUBTHRESHOLD WEB BS 440-494, AREAS 4.3" X 2". 1." X 0.7" AND 1.2" X 1", ORIGINAL THICKNESS 0.045", LOWEST REMAINING THICKNESS 0.040" FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15-1A-1. REMOVED AND REPLACED FCB SUBTHRESHOLD WEB P/N 7530597 PO# 763003, BS 440-494 IAW SRM 51-40-02 REF DWG 143A8330 REV A. 89004U, 03MAR20.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON INTERCOSTAL AT ACB BS787 - BS794 RBL23 WL157. REPLACED INTERCOSTAL AT ACB BS 787-794 RBL 23 WL 157 AS PER SRM 51-40-02-0G-0 AND DRAWING # 146A8320 I.D 0008, THE REMOVED PART WAS EVALUATED AND FOUND TO BE OUT OF LIMITS DUE TO NO HAVE ALLOWABLE DAMAGE ON SRM, PART REPAIRABLE BY REPLACEMENT.
Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
CRACKED BULKHEAD SUPPORT BRACKET AT ACB BS865 LBL10 WL165. / REPLACED; BULHEAD SUPPORT BRACKET AT BS. 865 LBL 10 WL 165. REPLACED. I.A.W. SRM. 51-10-02-0G-0; SRM 51-40-05-0G-0 AND. SRM 51-40-02-0G-0 59868U. 02-MAR-20; INSTALLED I.A.W. I.P.C. 53-42-51-06. DETAIL. 'P' AND. SRM 51-40-02-0G-0. 59868U. 02-MAR-20.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT B.S. 500D, R.B.L. 22 - L.B.L. 22, W.L. 155. REMOVED AND REPLACED FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT BS 500D, RBL 22-LBL 22 IAW SRM 51-40-02-0G-0 AND DWG 143A9481
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON AFT FLOOR TO BULKHEAD PANEL SUPPORT ANGLE AT ACB BS947 RBL20 TO LBL7 WL180. REMOVED AND INSTALLED NEW AFT FLOOR TO BULKHEAD PANEL SUPPORT ANGLE AT ACB BS 947 IAW SRM 51-40-02-0G-0,. SRM 51-10-02-0G-0 PAR 9C AIPC 53-11-51-01, DWG # 149A8118, DWG # 149A8117, DWG # 149A8110
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS887 TO BS947 RBL21 WL172. REMOVED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 887 TO BS 947 RBL 21 WL 172 ITEM # BAC 1496-377 # 7075T62 LOT # 1419996-1 IAW SRM 53-70-53-01-2, SRRM 53-00-53-1A-2, SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, SRM 51-40-05-0G-0 SRM 51-20-01-0G-0, SOPM 20-41-02, DWG # 147A7501. DWG # 147A7500
Part: SHIELD — CORRODED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON AFT SHIELD AT AFT CARGO BAY BS847 -BS867 RBL20 WL164. REMOVED AND REPLACED AFT SHIELD AT ACB BS 847 TO BS 867 RBL 20 WL 164 IAW SRM 51-40-02-0G-0 AND DWG 146A0081
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 400-500D, L.B.L. 22, W.L. 155. SIDE PLATE CHANNEL FOUND IT OUT OF LIMITS IAW SRM 53-00-53 IN MULTIPLES AREAS 1 X 1 OVER 50% MATERIAL LOSS. FABRICATED FLOOR TO SIDEWALL SUPPORT AT BS 400-500D LBL 22 FROM BAC 1496-444 #7075 T62 LOT # 1426040-1 LOCATED AND DRILLED IAW DWG 143A7501 REV B AND FABRICATED ZEE CHANNEL SPLICE BS 490 LBL 22 FROM BAC 1496-444 # 7075 T62 CLAD LOT # 1426040-1 LOCATED AND DRILLED IAW SRM 53-00-53-2R-6 REPAIR 6. APPLI
Part: FRAME — CRACKED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
CRACKED FRAME AT PASSENGER CABIN BETWEEN S-8R AND S-9R BS727B WL273. REPAIRED CRACKED FRAME OF BS 727B BETWEEN STR 8R AND 9R PER EA 1-A53-12114 REV 4.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS767 - BS727 RBL21 WL157. REMOVED AND REPLACED SIDEWALL SUPPORT FLOOR ACB AT BS 767-727 RBL 21 WL 157 IAW SRM 51-40-02-0G-0 DWG 146A7500
Part: SHIELD — CORRODED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON FWD SHIELD AT AFT CARGO BAY BS767 - BS794 RBL21 WL157. REMOVED CORRODED FWD SHIELD IN AFT CARGO BAY AT BS 767-794 RBL 21 WL 157 IAW SRM 51-40-02-0G-0 AND REPLACED SHIELD IAW SRM 51-40-02-0G-0 STEP 4 AND 5, DRAWING 146A0081 80570U 9MAR20
Part: SHIELD — CORRODED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
***CORROSION*** ON FORWARD CARGO BAY SHIELD AT B.S. 494-500A, R.B.L. 22, W.L. 155. REMOVED AND REPLACED ON FORWARD CARGO BAY SHIELD AT BS 494 TO BS 500A, RBL 22, WL155 PO# 784772-1
Part: SKATE ANGLE — CHAFED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
CHAFING ON THE RIGHT SKATE ANGLE AT VERTICAL STAB BS 1011 RBL14. REMOVED, LOCATED, DRILLED AND INSTALLED SKATE ANGLE STA. 1011 RBL 14 PER SRM 51-40-05 FIG.4, SRM 51-40-02 PAR 4B, DWG. 147A3200 AND DWG. 147A0030. 91195U 3-4-20
Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 59,169 hrs · 33,658 cycles
CHAFING ON THE LEFT SKATE ANGLE AT VERTICAL STAB BS1011 LBL14. / REMOVED; LOCATED; DRILLED AND INSTALLED SKATE ANGLE STA. 1011 LBL 14 PER SRM 51-40-05 FIG.4; SRM 51-40-02 PAR 4B; DWG. 147A0030 AND DWG. 147A3200. 91195U 3-4-20
Part: SKATE ANGLE — CHAFED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
CHAFING ON THE LEFT SKATE ANGLE IN MULTIPLE AREAS AT VERTICAL STAB BS1016 TO BS1128 LBL14. REPAIRED SKATE ANGLE STA. 1016 LBL 14 PER SRM 53-80-71-2R-6 AND DWG, 148A8300. -1 ANGLE MADE OUT OF 2024-0 1063 LOT # 1375061-1 HEAT TREATED TO T42, -2 STRAP MADE OUT OF 2024-T3 .080 LOT # 1375061-1 HEAT TREATED TO T42, -2 STRAP MAKE OUT OF 2024-T3 .080 LOT # 1422866-1. 91195U 3.5.20 INSTALLED -1 ANGLE AND -2 STRAP PER SRM 53-80-71-2R6 AND DWG. 148A8300. 91195U 3.5.20
Part: ANGLE — CHAFED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
CHAFING ON THE RIGHT SKATE ANGLE IN MULTIPLE AREAS AT VERTICAL STAB BS1016 TO BS1128 RBL14. REPAIRED AND INSTALLED -1 ANGLE AND -2 STRAP AT SKATE ANGLE STA. 1016 RBL 14 PER SRM 53-80-71-2R-6 AND DWG. 148A8300. -1 ANGLE FABRICATED OUT OF 2024-0 H/T TO T42 .063 CLAD LOT # 1375061-1. -2 STRAP FABRICATED OUT OF 2024-T3 .080 CLAD LOT # 1422866-1. 91195U 3.6.20
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 59,169 hrs · 33,658 cycles
R/H HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS. 193.9, 9IN AFT OF FRONT SPAR. / REPAIRED SKIN PER EA.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
FWD CARGO; AFT PIT; STA540; STR23; LBL42. STR HAS A CRACK AT THE LAST TWO FASTENERS. MARKED /
Part: STRINGER — CRACKED (AFT CARGO FLOOR) · airframe 59,169 hrs · 33,658 cycles
SUPPLEMENTAL INFORMATION: FWD CARGO; AFT PIT; STA540; STR23; LBL42. STR HAS A CRACK AT THE LAST TWO FASTENERS. MARKED / CRACKED STRINGER AT BS540; S23L; RBL42 WAS REPAIRED IAW ATS ER 20-02188 REV IR DATED 30MAR20 AND EA20-153-00026 REV IR.
Part: STRUCTURE — DENTED (FUSELAGE) · airframe 59,169 hrs · 33,658 cycles
FLIGHT DECK FL IS DENTED AT B.S. 255, R.B.L. 4 - L.B.L. 14, W.L. 207.54. REPAIRED FLIGHT DECK FLOOR AT B.S. 255 RBL 4 - RBL 14 PER E.A. 1-A53-33179 REV IR, DWG. 141A0631, SRM 51-40-02 PAR 4,7(D), SRM 51-40-05 FIG. 4, AMM 20-60-07-913-801. -1 WEB FABRICATED OUT OF 2024-T3 .040 LOT # 1418247-1. -3 DOUBLERS FAVRICATED OUT OF 2024-73 .050 LOT # 1425168-1. 91195U 2.29.20
Earlier reports · 2010–2019 · 157 reports
2019
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 57,235 hrs · 32,464 cycles
FORWARD CABIN EMERGENCY FLASHLIGHT INOP. R&R BATTERY PER AMM.
Part: HOOK AND LOOP — WORN (EMERGENCY EXIT) · airframe 57,171 hrs · 32,423 cycles
LT EMERGENCY EXIT RED PULL STRAP COMPARTMENT COVER HOOK AND LOOP WORN. R&R VELCRO PER SIP.
Part: RUB STRIP — DELAMINATED (EVAC SLIDE) · airframe 56,066 hrs · 31,771 cycles
L1 DOOR ESCAPE SLIDE SKIRT RUB STRIP DELAMINATED. R&R SLIDE PER MT.
2018
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 54,545 hrs · 30,844 cycles
BATTERY PACK INOP AT LOCATION M1672. R&R BATTERY PACK PER AMM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
STRINGER CLIP CRACKED AT BS 986, LBL 55. R&R CLIP IAW SRM AND DWG.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
FLOORBEAM CRACKED AT BS 294, RBL 52. REPAIRED CHORD IAW EA & ER.
Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
SHEAR WEB CRACKED AT BS 986, RBL 45. R&R SHEAR WEB PER SRM & DWG.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
SEAT TRACK CROWN CORRODED BETWEEN BS 694 TO BS 727A+12, LBL 45. R&R SEAT TRACK IAW DWG AND SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
SEAT TRACK CROWN CORRODED BETWEEN BS 727B TO BS 887, LBL 25. R&R SEAT TRACK PER SRM AND DWG.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
SEAT TRACK CROWN CORRODED BETWEEN BS 679 TO BS 727A+8, RBL 45. R&R SEAT TRACK IAW DWG AND SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
SEAT TRACK CROWN CORRODED BETWEEN BS 727B TO BS 887, LBL 45. R&R SEAT TRACK PER SRM AND DWG.
Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
FORWARD CARGO BAY, RT FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 500A TO BS 500D, RBL 22. R&R SUPPORT PER SRM & DWG.
Part: SHIELD — CORRODED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
FORWARD CARGO BAY SHIELD CORRODED BETWEEN BS 492 TO BS 500A, RBL 22. R&R SHIELD PER SRM & DWG.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
SEAT TRACK CROWN CORRODED BETWEEN BS 727B TO BS 887, RBL 45. R&R SEAT TRACK IAW DWG AND SRM.
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
FORWARD CARGO BAY SUBTHRESHOLD WEB CORRODED BETWEEN BS 440 TO BS 480, RBL 23. R&R WEB PER SRM & DWG.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
SEAT TRACK CROWN CORRODED BETWEEN BS 663 TO BS 713, RBL 25. R&R SEAT TRACK IAW DWG AND SRM.
Part: SHIELD — CORRODED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
AFT CARGO BAY SHIELD CORRODED BETWEEN BS 847 TO BS 867, RBL 22. R&R SHIELD PER SRM & DWG.
Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
AFT CARGO BAY, RT FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 727+10 TO BS 767, RBL 23. R&R SUPPORT PER DWG & SRM.
Part: DOOR SILL — CORRODED (L1 DOOR) · airframe 54,545 hrs · 30,844 cycles
L1 DOOR MOP SILL CORRODED BETWEEN BS 312 TO BS 328, LBL 56. R&R MOPSILL IAW DWG AND SRM.
Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 54,545 hrs · 30,844 cycles
AFT CARGO BAY RT CARGO TIE DOWN TRACK CRACKED AT BS 747, RBL 13.84. R&R TRACK PER SRM AND DWG.
Part: FITTING — CORRODED (L1 DOOR) · airframe 54,545 hrs · 30,844 cycles
L1 DOOR GIRT BAR FITTING CORRODED AT BS 312, LBL 54. R&R FITTING IAW SRM & DWG.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
FLOOR SUPPORT CORRODED BETWEEN BS 967 TO BS 986, RBL 19. R&R SUPPORT IAW ER & EA.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
BEAM UPPER AND LOWER SURFACE CORRODED AT BS 986, RBL48. REPAIRED BEAM PER ER AND EA.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
R2 DOOR MOP SILL CORRODED AT BS 986, RBL 53. R&R MOP SILL PER SRM & DWG.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
R1 DOOR MOPSILL BETWEEN BS 300 TO BS 328, RBL 32. R&R MOPSILL IAW DWG AND SRM.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 54,545 hrs · 30,844 cycles
AFT CARGO BAY, RT CARGO TIED OWN TRACK CORRODED BETWEEN BS 794 TO BS 867, RBL 13. R&R TRACK PER SRM.
Part: FITTING — CORRODED (L1 DOOR) · airframe 54,545 hrs · 30,844 cycles
L1 DOOR GIRT BAR FITTING CORRODED AT BS 344, LBL 56. R&R FITTING IAW SRM & DWG.
Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 727E+10 TO BS 807, LBL 23. R&R PLATE PER SRM & DWG.
Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 54,545 hrs · 30,844 cycles
LOWER VAPOR BARRIER CRACKED AT BS 663, LBL 27. REPAIRED BARRIER IAW SRM.
Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
ATTACH CLIP CRACKED BETWEEN BS 289 TO BS 294, WL 208. R&R CLIP IAW SRM & DWG.
Part: FORMER — CHAFED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
LT FAIRING FORMER CHAFFED ON LOWER SIDE OF FORMER BETWEEN BS 663 TO BS 673, LBL 28. R&R FORMER IAW SRM AND DWG.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, LBL 8. REPAIRED ANGLE PER ER AND EA.
Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 54,545 hrs · 30,844 cycles
LOWER VAPOR BARRIER BULKHEAD WEB CRACKED AT BS 663, BETWEEN LBL 30 TO LBL 40. REPAIRED WEB IAW SRM.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 54,545 hrs · 30,844 cycles
VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, RBL 8. REPAIRED ANGLE PER ER AND EA.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,731 hrs · 29,755 cycles
RT OVERWING EXIT DOOR LIGHT INOP. RELAMPED LIGHT PER MM.
Part: SLIDE — DISCONNECTED (L1 DOOR) · airframe 52,495 hrs · 29,631 cycles
L1 DOOR SLIDE DISCONNECTED. CONNECTED THE SLIDE IAW MT.
2017
Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 52,385 hrs · 29,549 cycles
RT WHEEL WELL BEADED WEB CRACKED AT BS 663. REPAIRED WEB PER EA.
Part: COVER — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,938 hrs · 95,343 cycles
FORWARD GALLEY EMERGENCY EXIT LIGHT COVER INOP. REPAIRED THE COVER PER EA.
Part: BATTERY — FAILED (CABIN) · airframe 50,266 hrs · 28,268 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1674. R&R BATTERY PER AMM.
Part: BATTERY — FAILED (CABIN) · airframe 50,266 hrs · 28,268 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER AMM.
Part: BATTERY — FAILED (CABIN) · airframe 50,266 hrs · 28,268 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R&R BATTERY PER AMM.
Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 50,266 hrs · 28,268 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R & R THE BATTERY IAW AMM.
2016
Part: SWITCH — BROKEN (COCKPIT) · airframe 48,919 hrs · 27,463 cycles
AIR TURNBACK/DECLARED EMERGENCY. PASSING FL 350 CABIN LOST PRESSURIZATION. R&R SWITCH S128 PER MM.
Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 48,500 hrs · 27,235 cycles
VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 47. R&R WEB PER SRM & DWG.
Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 48,500 hrs · 27,235 cycles
VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN LBL 45 TO LBL 47. REPAIRED WEB IAW EA & ER.
Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 48,500 hrs · 27,235 cycles
VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 26. R&R WEB IAW EA.
Part: SLAT — CRACKED (RT WING) · airframe 48,500 hrs · 27,235 cycles
RT WING NR 5 SLAT INBOARD ACTUATOR ATTACH FITTING COVE CHORD FASTENER HOLES CRACKED. R&R NR 5 SLAT IAW AMM.
Part: BRACKET — CRACKED (RT WING SPOILER) · airframe 48,500 hrs · 27,235 cycles
RIGHT WING OUTBOARD NR 7 SPOILER UPPER PANEL MID SUPPORT BRACKET CRACKED. R & R THE BRACKET IAW SRM.
Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 48,500 hrs · 27,235 cycles
MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 27. REPAIRED WEB IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 48,500 hrs · 27,235 cycles
LT BULKHEAD FRAME CRACKED AT BS 727, WL 200. REPAIRED FRAME IAW EA.
Part: SKIN — CRACKED (LE SLAT) · airframe 48,500 hrs · 27,235 cycles
RT WING NR 8 SLAT NOSE SKIN CRACKED AT STA 451.97. REPAIRED SKIN IAW SRM AND DWG.
Part: SKIN — CRACKED (LT WING SLAT) · airframe 48,500 hrs · 27,235 cycles
LT WING NR 4 SLAT NOSE SKIN CRACKED AT STATION 85.19. REPAIRED SKIN IAW SRM.
Part: STIFFENER — CRACKED (RT MLG WW) · airframe 48,408 hrs · 27,173 cycles
RIGHT MLG CENTER WING SECTION REAR SPAR BULKHEAD STIFFENER CRACKED AT STA 663, RBL 25. R & R STIFFENER IAW SRM.
Part: STIFFENER — CRACKED (LT MLG WW) · airframe 48,408 hrs · 27,173 cycles
LEFT MLG CENTER WING SECTION REAR SPAR BULKHEAD STIFFENER CRACKED AT STA 663, LBL 10.54. R & R STIFFENER IAW SRM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 48,310 hrs · 27,112 cycles
LEFT OVERHEAD BIN EMERGENCY LIGHT INOPERATIVE BETWEEN ROW 3 TO ROW 6. R & R BATTERY IAW MM.
Part: LENS — BROKEN (EXIT SIGN) · airframe 47,795 hrs · 26,826 cycles
FORWARD ENTRY DOOR EMERGENCY EXIT SIGN LENS BROKEN. R & R LIGHT ASSEMBLY IAW MM.
Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 47,561 hrs · 26,696 cycles
L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MAINTENANCE.
Part: SKIN — DELAMINATED (TE FLAP) · airframe 47,377 hrs · 26,576 cycles
LEFT WING OTBD AFT FLAP AFT INBD CORNER SKIN DELAMINATED. R & R AFT FLAP IAW AMM.
Part: GIRT BAR — OUT OF POSITION (R1 DOOR) · airframe 47,092 hrs · 26,410 cycles
R1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED GIRT BAR IAW MT.
Part: COVER — MISSING (EXIT SIGN) · airframe 46,429 hrs · 26,024 cycles
RIGHT LOWER OVERWING EXIT SIGN COVER MISSING. R & R SIGN ASSEMBLY IAW MM.
2015
Part: BATTERY — FAILED (CABIN) · airframe 44,191 hrs · 24,753 cycles
FORWARD RT EMER BATTERY PACK FAILED FUNCTIONAL CHECK. R & R BATTERY IAW MM.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 44,061 hrs · 24,685 cycles
THE R2 DOOR EXIT LIGHT LENS FOUND TO BE MISSING. R & R THE EXIT LIGHT ASSY IAW MM.
Part: RELAY — FAILED (FUEL SYSTEM) · airframe 435,600 hrs · 24,407 cycles
AIR TURN BACK LT CTR FUEL PUMP INOPERATIVE. R & R UNIVERSAL FAULT INTERRUPTER RELAY IAW MM.
Part: CONTROL VALVE — FAULTY (BLEED AIR SYS) · airframe 42,640 hrs · 23,897 cycles
DECLARED EMER DUAL BLEED TRIPPED. R & R NR 1 PRECOOLER CONTROL VLV IAW MM.
Part: CONTROL VALVE — FAULTY (BLEED AIR SYS) · airframe 42,640 hrs · 23,897 cycles
DECLARED EMER DUAL BLEED TRIPPED. R & R NR 2 PRECOOLER CONTROL VLV IAW MM.
Part: LENS — BROKEN (CABIN) · airframe 42,571 hrs · 23,858 cycles
R1 DOOR EMER EXIT SIGN LENS BROKEN. R & R LENS IAW AMM.
2014
Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,243 hrs · 23,667 cycles
EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 17 ABC. RELAMPED LIGHT IAW MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,243 hrs · 23,667 cycles
AFT ENTRY EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,243 hrs · 23,667 cycles
MAIN CABIN SEAT TRACK CRACKED FWD OF BS 727B, LBL 45, OTBD FLANGE FWD & AFT FASTENER HOLES. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,243 hrs · 23,667 cycles
MAIN CABIN SEAT TRACK CRACKED FWD OF BS 727B, RBL 45, OTBD FLANGE FWD & AFT FASTENER HOLES. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,243 hrs · 23,667 cycles
MAIN CABIN SEAT TRACK CRACKED FWD OF BS 727B, LBL 25, OTBD FLANGE FWD & AFT FASTENER HOLES. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,243 hrs · 23,667 cycles
MAIN CABIN SEAT TRACK CRACKED FWD OF BS 727B, RBL 25, INBD FLANGE FWD & AFT FASTENER HOLES. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,243 hrs · 23,667 cycles
MAIN CABIN SEAT TRACK CRACKED FWD OF BS 727B, RBL 25, OTBD FLANGE FWD & AFT FASTENER HOLES. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,243 hrs · 23,667 cycles
MAIN CABIN SEAT TRACK CRACKED FWD OF BS 727B, LBL 45, INBD FLANGE FWD & AFT FASTENER HOLES. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,243 hrs · 23,667 cycles
MAIN CABIN SEAT TRACK CRACKED FWD OF BS 727B, LBL 25, INBD FLANGE FWD & AFT FASTENER HOLES. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 42,243 hrs · 23,667 cycles
MAIN CABIN SEAT TRACK CRACKED FWD OF BS 727B, RBL 45, INBD FLANGE FWD & AFT FASTENER HOLES. REPAIRED SEAT TRACK IAW EA.
Part: SKIN — CRACKED (RT WING) · airframe 42,243 hrs · 23,667 cycles
RIGHT WING NR 1 WINGLET UPPER LE SKIN CRACKED AT COUNTERSUNK HOLE UPPER SURFACE 1.5 FROM BUTT PLATE. REPAIRED SKIN IAW SRM.
Part: POST — CRACKED (FUSELAGE) · airframe 42,243 hrs · 23,667 cycles
RIGHT NR 1 WINDOW POST CRACKED FROM EDGE OF RADIUS TOWARDS LUG. REPAIRED POST IAW EA.
Part: POST — CRACKED (FUSELAGE) · airframe 42,243 hrs · 23,667 cycles
LEFT NR 3 WINDOW POST NR 2 CIRCLE NOTE HOLE CRACKED. REPAIRED POST IAW EA.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 42,243 hrs · 23,667 cycles
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 193.90, 9 INCHES AFT OF FRONT SPAR. REPAIRED SKIN IAW SRM.
Part: SLIDE — UNSECURE (R1 DOOR) · airframe 41,539 hrs · 23,246 cycles
R1 DOOR EMER EVAC SLIDE FELL OUT, DID NOT DEPLOY & STILL OPERATIONAL. INSTALLED SLIDE IAW MT.
Part: LENS — BROKEN (CABIN) · airframe 40,116 hrs · 22,385 cycles
AFT ENTRY DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R & R LENS IAW MM.
Part: BATTERY — FAILED (CABIN) · airframe 39,740 hrs · 22,168 cycles
FWD CABIN EMERGENCY EXIT LIGHTS FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.
2013
Part: BALLAST — INOPERATIVE (CABIN) · airframe 38,655 hrs · 21,522 cycles
LT EMERGENCY LIGHT INOPERATIVE. R & R BALLAST IAW MM.
Part: WIRE — OUT OF ADJUST (R2 DOOR) · airframe 36,645 hrs · 20,329 cycles
R2 DOOR EMERGENCY EVAC SLIDE TEST WIRE FELL OUT. RE-INSTALLED WIRE PER M/M.
Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 36,309 hrs · 20,117 cycles
L1 DOOR SLIDE OUT OF ADJUST. REPOSITIONED L1 DOOR SLIDE PER MT.
Part: SIGN — MISSING (CABIN) · airframe 36,267 hrs · 20,092 cycles
EXIT SIGN AT ROW 12 DEF MISSING. REMOVED AND REPLACED LIGHT ASSY PER WDM.
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 36,237 hrs · 20,072 cycles
EMERGENCY DOME LIGHT IN COCKPIT INOP. REMOVED AND REPLACED BULB PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,894 hrs · 19,854 cycles
EMERGENCY LIGHT BELOW EXIT LIGHT FWD BULB IS INOP. RELAMPED FWD EMERGENCY LIGHT BELOW EXIT LIGHT RT SIDE. FUNCTION TEST GOOD PER AMM 33-51-00-710-801 89195U 25JAN13 AND AMM 33-51-01-960-801.
2012
Part: CONNECTOR — LOOSE (CABIN) · airframe 35,699 hrs · 19,739 cycles
AFT ENTRY DOOR EMERGENCY EXIT SLIDE LIGHT IS INOP. RECONNECTED CONNECTOR D11086 PER SWPM 20-60-06. OPERATIONAL CHECK OF AFT ENTRY DOOR EMERGENCY EXIT SLIDE LIGHT PERFORMED PER 33-51-00-720-801 AND CHECK IS GOOD.
Part: BULKHEAD — DELAMINATED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
REPAIR DISBONDED ON BS 663 BULKHEAD RBL 11 WL 153. REPAIRED DISBOND ON BS 663 BULKHEAD RBL 11 WL 153 PER SRM 51-70-04-2T-10 AND SRM 51-70-04-2R-0.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
STRINGER CLIP AT BS 500D STR 19LT CRACKED. REMOVED CRACKED GUSSET BS 500D STR 19LT IAW SRM 51-40-02, FABRICATED REPLACEMENT GUSSET IAW DRWING 143A7902 INSTALLED NEW GUSSET IAW SRM 51-40-02 87529U 07DEC12.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FRAME CRACKED BS 296 WL 208.5 RT SIDE. REPAIRED FRAME BS 296 WL 208 RT SIDE STUB FRAME IAW ER 12-03669 AND EA 1-753-21271.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FLOOR PANEL 242DF FWD EDGE DAMAGE AND INSERT MISSING. FABRICATED NEW FLOOR PANEL IAW BOEING DWG 144A5810. INSTALLED INSERTS PER BAC 5085 PARA 8.4.1.2 & PART MARKED AS GIVEN IN DRAWING 144A5810 SHEET 16.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FLOOR SUPPORT BS 537 BBL 0 - RBL 25 WL 208 CRACKED AT I/B CORNER. REMOVED AND REPLACED SUPPORT PER SRM AND BOEING DRAWING.
Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
VERTICAL PRESSURE WEB CRACKED BS 663 RBL 34 WL 197. REPAIRED CRACK AT BS 663 RBL 34 WL 197 PER SRM 57-10-10 2R3 REPAIR 3.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FUSELAGE FRAME CRACKED AT AIR CONDITIONING ATTACH BRACKET BS 827 STR 8LT. REPAIRED CRACKED FRAME BS 827 STR 8LT IAW EA 1-A53-12114.
Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 35,699 hrs · 19,739 cycles
LEFT MLG WHEEL WELL VAPOR BARRIER STA 663 LBL 36 CRACKED 20+INCH. REPAIRED CRACK ON LEFT MLG WHEEL WELL VAPOR BARRIER STA 663 LBL 36 PER SRM 51-70-04-2R-10 AND SRM 51-70-04-2R-0.
Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 35,699 hrs · 19,739 cycles
RIGHT MLG WHEEL WELL VAPOR BARRIER STA 663 RBL 11 CRACKED 30+INCH. REPAIRED CRACK ON RIGHT MLG WHEEL WELL VAPOR BARRIER AT STA 663 RBL 11 PER SRM 51-70-04-2R-10 AND SRM 51-70-04-2R-0.
Part: ATTACH BRACKET — CRACKED (RT MLG WW) · airframe 35,699 hrs · 19,739 cycles
RIGHT MLG WHEEL WELL VAPOR BARRIER DIAGONAL BRACE ATTACH BRACKET CRACKED THRU ON HORIZONTAL STIFFENER. REMOVED & REPLACED RIGHT MLG WHEEL WELL UPPER BARRIER DIAGONAL BRACE ATTACH BRACKET PER SRM 51-40-02 & DWG 111A1000.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FLOOR SUPPORT CORRODED BETWEEN BS 983 TO BS 985, BETWEEN RBL 16.5 TO RBL 19.5. REMOVED AND REPLACED INTERCOSTAL PER EA AND SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FUSELAGE FRAME CRACKED AT AIR CONDITIONING ATTACH BRACKET BS 480 STR 8-9R. REPAIRED FRAME AT BS 480 BETWEEN STR 8R & 9R IAW EA 1-A53-12114.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS 727B STR 8-9L. REPAIRED FUSELAGE FRAME AT AIR CONDITIONING BRACKET ATTACHMENT BS 727B STR 8-9L PER EA 1-A53-12114.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FUSELAGE FRAME CRACKED AT AIR CONDITIONING ATTACH BRACKET BS 787 STR 8-9R. REPAIRED FUSELAGE FRAME AT AIR CONDITIONING ATTACH BRACKET AT BS 787 STR 8-9R PER EA 1-A53-12114.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS 500A STR 8-9L. REPAIRED FRAME AT BS 500A BETWEEN STRINGER 8L TO 9L IAW EA 1-A53-12114 REV 2.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FUSELAGE FRAME CRACKED AT AIR CONDITIONING ATTACH BRACKET BS 867 STR 8-9R. REPAIRED CRACKED FRAME BS 867 STR 8R-9R PER EA 1-A53-12114.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS 440 STR 8-9L. REPAIRED FRAME AT BS 440 BETWEEN STRINGER 8L & 9L IAW EA 1A-53-12114.
Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
ATTACH TEE CLIP CORRODED AT BS 1090, RBL 14. REMOVED AND REPLACED CLIP IAW SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FUSELAGE FRAME CRACKED AT AIR CONDITIONING ATTACH BRACKET BS 500A STR 8-9R. REPAIRED BS 500A FRAME AT STR 8-9RT PER EA 1-A53-12114.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FUSELAGE FRAME CRACKED AT AIR CONDITIONING ATTACH BRACKET BS 500C STR 8-9R. REPAIRED FRAME BS 500C STR 8-9RT PER EA 1-A53-12114.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS 500C STR 8-9L. REPAIRED FRAME BS 500C STR 8-9L PER EA 1-A53-12114.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FUSELAGE FRAME CRACKED AT AIR CONDITIONING ATTACH BRACKET BS 727D STR 8-9R. FRAME WAS REPLACED ON CARD T166212.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BS 480 STR 8-9L. REPAIRED FRAME BS 480 STR 8-9LT PER EA 1-A53-12114.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FUSELAGE FRAME CRACKED AT AIR CONDITIONING ATTACH BRACKET BS 400 STR 8. REPAIRED FRAME AT BS 400 STR 8-9RT PER EA 1-A53-12114.
Part: FRAME — CRACKED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FUSELAGE FRAME CRACKED AT AIR CONDITIONING ATTACH BRACKET BS 360 STR 8-9R. REPAIRED CRACK AT A/C BRACKET BS 360 STR 8-9 RT IAW ER 12-03651 EA 1-753-21219.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
AFT WET AREA FLOOR PANEL IS DELAMINATED, PANEL 241 ZF. PANEL 241ZF WAS REPAIRED IAW SRM 53-00-50-2R-9.
Part: PANEL — DELAMINATED (RT WING) · airframe 35,699 hrs · 19,739 cycles
RIGHT WING L/E PANEL 621CB DELAMINATED AT FWD I/B CORNER. REPAIRED RIGHT WING L/E PANEL 621CB I/B FWD CORNER IAW SRM 51-70-05.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
AFT WET AREA FLOOR PANELS IS DELAMINATED, PANEL 241 YF. PANEL 241YF REPAIRED IAW SRM 53-00-50-2R-9.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
AFT WET AREA FLOOR PANEL IS DELAMINATED, PANEL 241 ABF. REPAIRED DELAMINATED AFT WET AREA ON FLOOR PANEL 241ABF IAW SRM 53-00-50-2R-1 87210U 03DEC12.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
AFT WET AREA FLOOR PANEL IS DELAMINATED, PANEL 241 ADF. REPAIRED DELAMINATION ON AFT WET AREA FLOOR PANEL 241ADF IAW SRM 53-00-50-01-1 AND SRM 53-00-50-2R-1.
Part: PANEL — DELAMINATED (LT WING) · airframe 35,699 hrs · 19,739 cycles
LEFT WING L/E PANEL 521WB FWD I/B CORNER IS DELAMINATED. REPAIRED DELAMINATION ON FWD I/B CORNER OF LEFT WING L/E PANEL 521WB IAW SRM 51-70-05-2R-6, 57-40-01, 51-40-02, AND 51-70-14-2R-3 89215U 08DEC2012.
Part: RETAINER — CRACKED (RT WING) · airframe 35,699 hrs · 19,739 cycles
RIGHT WING TRAILING EDGE VERTICAL SEAL RETAINER CRACKED AT STA 275. REMOVED AND REPLACED RETAINER IAW SOPM.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
AFT WET AREA FLOOR PANEL DISBONDED PANEL 242SF. REPAIRED DISBONDED AFT WET AREA ON FLOOR PANEL 242SF IAW SRM 53-00-50-2R-1 89216U 02DEC12.
Part: RETAINER — CORRODED (RT WING) · airframe 35,699 hrs · 19,739 cycles
RIGHT WING TRAILING EDGE UPPER SEAL RETAINER CORRODED BETWEEN STA 255 TO STA 261. REMOVED AND REPLACED RETAINER IAW SRM.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
AFT WET AREA FLOOR PANEL IS DELAMINATED, PANEL 241 AEF. REPAIRED PANEL 241AEF, AFT WET AREA FLOOR PANEL DELAMINATION IAW SRM 53-00-50-01-1 AND SRM 53-00-50-2R-1.
Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 35,699 hrs · 19,739 cycles
LEFT WING UPPER TRAILING EDGE PANEL SUPPORT ANGLE IS CRACKED AT ORSS 270. REMOVED ANGLE IAW SRM 51-40-02-0G-0. LOCATED, DRILLED, AND INSTALLED NEW ANGLE AT LEFT WING UPPER T/E PANEL AT ORSS 270 IAW SRM 51-40-05-0G-0 & SRM 51-40-02-0G-0. 55774U, 03DEC
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
AFT WET AREA FLOOR PANEL IS DELAMINATED, PANEL 242 VF. REPAIRED DELAMINATION ON PANEL 242VF AFT WET AREA FLOOR PANEL IAW SRM 53-00-50-01-1 AND SRM 53-00-50-2R-1.
Part: SEAL DEPRESSOR — BROKEN (NR 1 PYLON) · airframe 35,699 hrs · 19,739 cycles
NR 1 ENGINE PYLON O/B AFT FIRE SEAL DEPRESSOR IS BROKEN. REMOVED NR 1 ENGINE PYLON O/B AFT UPPER FIRE SEAL DEPRESSOR PER SRM 51-40-02-0G-0. 3091C 28NOV12. INSTALLED NEW O/B AFT UPPER FIRE SEAL DEPRESSOR PER SRM 51-40-02-0G-0 STEP 5.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
CORROSION, ON INTERCOSTAL AT BS 996.8 BELOW STRINGER 14L. REMOVED CORROSION ON INTERCOSTAL BS 996.8 BELOW STR 14 LEFT FOUND TO BE IN LIMITS PER SRM 53-70-15-1A-1. ALODINED AND PRIMED BARE METAL PER MM 51-21-41-370-802. 7020U 29NOV12.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
AFT WET AREA FLOOR PANEL IS DELAMINATED, PANEL 241 AAF. REPAIRED AFT WET AREA FLOOR PANEL 241AAF IAW SRM 53-00-50 6490U 30NOV12.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
AFT WET AREA FLOOR PANEL IS DELAMINATED, PANEL 242 UF. REPAIRED DELAMINATED AFT OUT AREA FLOOR PANEL 242UF IAW SRM 53-00-50-2R-1 89216U 01DEC2012.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
AFT WET AREA FLOOR PANEL IS DELAMINATED, PANEL 242 TF. REPAIRED DELAMINATION ON AFT WET AREA FLOOR PANEL 242TF IAW SRM 53-00-50-2R-1. 89216U, 01DEC2012.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
SIDEWALL SUPPORT CORRODED AT BS 859, RBL22. REMOVED AND REPLACED SUPPORT IAW DWG.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 35,699 hrs · 19,739 cycles
CORROSION, ON CARGO TRACK AT STA 797-825, RBL 15 AND WL 159. REPAIRED CARGO TRACK BS 779.5-887 RBL 13.8 IAW EA 1-A53-8210 AND SRM 53-00-53-2R-3.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
INTERCOSTAL CORRODED AT BS 777, RBL 19. REMOVED AND REPLACED INTERCOSTAL PER SRM.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT STA 769, RBL 21 AND WL 146. CORRODED FLOOR SIDEWALL SUPPORT AT BS 769 RBL 21, WL 146, WAS REPLACED WITH CFE ON # 7531132, BS 767 TO 794 RBL 21 PER SRM 51-40-05, SRM 51-40-02.
Part: SUPPORT — PUNCTURED (FUSELAGE) · airframe 35,699 hrs · 19,739 cycles
FLOOR TO SIDEWALL SUPPORT PUNCTURED BETWEEN BS 757 TO BS 747E+3, RBL 21. REMOVED AND REPLACED SUPPORT PER SRM.
Part: RETAINER — CRACKED (LT WING) · airframe 35,699 hrs · 19,739 cycles
LEFT WING FAIRING 542BB LEF FWD BULB SEAL RETAINER P/N 113A9375-1 IS CRACKED. REMOVED AND REPLACED CRACKED LEFT WING FAIRING 542BB SEAL RETAINER IAW SOPM 20-50-01. 89264U 29NOV12.
Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 35,699 hrs · 19,739 cycles
CAPTAINS NR 1 WINDOW FRAME IS CRACKED AT UPPER AFT CORNER MOD. INSTALLED REPAIR DOUBLER IAW ER 12-03637 AND EA 1-753-21274.
Part: SEALANT — DETERIORATED (RT PYLON) · airframe 35,699 hrs · 19,739 cycles
SEALANT CRACKED AND DETERIORATED RT PYLON AT BOTTOM EDGE OF ENGINE MOUNT BULKHEAD AND O/B DIAGONAL BRACE LOWER ATTACH LUG. REMOVED AND REPLACED SEALANT PER AMM PER BOEING DRAWING.
Part: POUCH — OUT OF ADJUST (EVAC SLIDE) · airframe 35,620 hrs · 19,691 cycles
F/A REPORTS DIFFICULTY ENGAGING FWD ENTRY DOOR GIRT BAR. ADJUSTED FWD ENTRY DOOR EVACUATION SLIDE MANUAL D RING VELCRO STOW POUCH PER AMM. CLEARANCE NOW ACHIEVED TO PROPERLY STOW GIRT BAR, OPS CHECK GOOD PER AMM.
Part: RETAINER — MISSING (L1 DOOR) · airframe 35,585 hrs · 19,670 cycles
L1 DOOR ESCAPE SLIDE GIRT BAR RELEASE STOP SLEEVE PLASTIC RETAINER MISSING. REMOVED AND REPLACED RETAINER PER AMM.
Part: RETAINER — MISSING (L2 DOOR) · airframe 35,585 hrs · 19,670 cycles
L2 DOOR ESCAPE SLIDE GIRT BAR RELEASE STOP SLEEVE PLASTIC RETAINER MISSING. REMOVED AND REPLACED RETAINER PER AMM.
Part: RETAINER — MISSING (R2 DOOR) · airframe 35,585 hrs · 19,670 cycles
R2 DOOR ESCAPE SLIDE GIRT BAR RELEASE STOP SLEEVE PLASTIC RETAINER MISSING. REMOVED AND REPLACED RETAINER PER AMM.
Part: RETAINER — MISSING (R1 DOOR) · airframe 35,585 hrs · 19,670 cycles
R1 DOOR ESCAPE SLIDE GIRT BAR RELEASE STOP SLEEVE PLASTIC RETAINER MISSING. REMOVED AND REPLACED RETAINER PER AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,543 hrs · 19,645 cycles
LEFT BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 9. RELAMPED LIGHT PER MM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,802 hrs · 17,984 cycles
EXTERIOR LT OVERWING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED LAMP PER MM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,802 hrs · 17,984 cycles
EXTERIOR AFT ENTRY EMERGENCY LIGHT IS INOP. RELAMPED LIGHT PER M/M.
Part: LIGHT — BROKEN (CABIN) · airframe 32,730 hrs · 17,937 cycles
L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.
2011
Part: COVER — MISSING (CABIN) · airframe 31,904 hrs · 17,464 cycles
OVERWING EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.
Part: SIGN — BROKEN (CABIN) · airframe 31,697 hrs · 17,347 cycles
L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,419 hrs · 16,631 cycles
DURING SCHEDULED CV CHECK, FOUND EMERGENCY EXIT DOOR SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.
Part: LIGHT — MISSING (CABIN) · airframe 30,180 hrs · 16,495 cycles
EEPLS MISSING. REMOVED AND REPLACED EEPLS PER MM.
2010
Part: COVER — CRACKED (CABIN) · airframe 29,361 hrs · 196,024 cycles
DURING SCHEDULED SPV CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 7 TO ROW 18. REMOVED AND REPLACED COVER PER MM.
Part: SKIN — CORRODED (CARGO DOOR) · airframe 29,361 hrs · 16,024 cycles
DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR INNER SKIN CORRODED. REPAIRED SKIN PER SRM.
Part: SLAT — DELAMINATED (RT WING) · airframe 29,361 hrs · 16,024 cycles
DURING SCHEDULED SPV CHECK, FOUND RT WING NR 8 SLAT DELAMINATED. REPAIRED SLAT PER MM.
Part: FLAP — DELAMINATED (LT WING) · airframe 29,361 hrs · 16,024 cycles
DURING SCHEDULED SPV CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER MM.