N306AS
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.
214 reports on file, 2007-09-21 – 2024-06-06.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 74,437 hrs · 30,177 cycles
ROW 16 EXIT LIGHT MISSING. GROUNDED - YES. INSTALLED ROW 16 EXIT LIGHT COVER IAW AMM 33-51-01.
Earlier reports · 2007–2023 · 213 reports
2023
Part: BATTERY PACK — FAILED (MAIN PASSENGER C) · airframe 72,451 hrs · 29,240 cycles
DURING T/C 78233001( EMERGENCY BATTERY PACK FUNCTIONAL CHECK FOUND FWD AND AFT BATTERY PACK FOR L1065 AND L1207 AISLE LIGHT TEST FAIL. GROUNDED - YES. REMOVED AND REPLACED POWER PACK AT FWD AND AFT CABIN LOCATION AND OPS CHECK FOUND NORMAL, REF AMM 33-51-06-960-805 AND SSM 33-51-13.
Part: LENS — MISSING (MAIN PASSENGER C) · airframe 70,334 hrs · 28,293 cycles
ROW 6 ABC EMERGENCY AISLE LIGHT LENS COVER MISSING. GROUNDED - YES. REPLACED LENS, ROW 6 ABC, EMERGENCY AISLE LIGHT, REF B737-900 AMM 33-51-03.
2022
Part: LAMP — INOPERATIVE (MAIN PASSENGER C) · airframe 69,503 hrs · 27,931 cycles
INTERIOR EMERGENCY EXIT LIGHTS HAVE INOP BULBS AT R1 AND L OVERWING EMERGENCY EXITS. GROUNDED - YES. CORRECTIVE ACTION WAS PERFORMED AS FOLLOWS REPLACED INOPERATIVE INTERIOR EMERGENCY EXIT LIGHTS AT R1 DOOR & L OVERWING EXITS BY HAND.
Part: RIB — CRACKED · airframe 69,503 hrs · 27,931 cycles
R/H HORIZ STAB INSPAR RIB 4TH FROM I/B END IS CRACKED. GROUNDED - YES. REMOVED #4 RIB IAW B737-900 SRM 55-10-09-2R-4 REPAIRED RIB AIW B737-900 SRM 55-10-09-2R-4 REINSTALLED REPAIRED #4 RIB IAW B737-900 SRM 55-10-09-2R-4.
Part: SKIN — CRACKED · airframe 69,503 hrs · 27,931 cycles
R/H HORIZONTAL LOWER SKIN CRACKED AT STA 94.0 AND REAR SPAR. GROUNDED - YES. REMOVED EXISTING REPAIR PREFORMED CUTOUT OF DAMAGE AND ISNTALLED NEW REPAIR IAW B737-900 SRM 55-10-01-2R-11 CAT B REPAIR WITH AN INSPECTION THRESHOLD OF 56,000 FLT CYCLES.
Part: SKIN — CRACKED · airframe 69,503 hrs · 27,931 cycles
R/H HORIZONTAL LOWER SKIN IS CRACKED AT STA 147 AND REAR SPAR. GROUNDED - YES. REMOVED EXISTING REPAIR PREFORMED CUTOUT OF DAMAGE AND INSTALLED NEW REPAIR IAW B737-900 SRM 55-10-01-2R-11 CAT B REPAIR WITH AN INSPECTION THRESHOLD OF 56,000 FLT CYCLES.
Part: SKIN — CORRODED · corrosion level 2 · airframe 69,503 hrs · 27,931 cycles
FUSELAGE SKIN AROUND VACUUM LAV EXHAUST VENT AT FS917 IS CORRODED. GROUNDED - YES. DAMAGE FOUND TO BE OUT OF LIMITS CUT OUT DAMAGE AND REPAIRED SKIN IAW B737-900 SRM 53-70-01-2R-3 THIS IS A CAT B REPAIR WITH AN INSPECTION THRESHOLD OF 77,931 TOTAL FLIGHT CYCLES AND 5,000 CYCLE INTERVAL W=2 O=.125 R=.097 L=3 D=.028.
2021
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,370 hrs · 26,102 cycles
EMERGENCY EXIT LIGHT BULBS INOP ON FWD INTERIOR SIDE OF R1 DOOR. GROUNDED - YES. RELAMPED R1 DOOR EMERGENCY EXIT LIGHT OPS CHECK GOOD IAW B737-900 AMM 33-51-01-960-801.
Part: TRANSITION PANEL — CORRODED (AFT CARGO) · corrosion level 2 · airframe 65,370 hrs · 26,102 cycles
AFT CARGO LT TRANSITION PANEL CORRODED STA 727C-787. GROUNDED-YES. REPAIRED TRANSITION PANEL (ZEE ASSEMBLY), IAW B737-900 SRM 53-00-53-2R-6W1.2 O .040 R .033 L 1.5 D 3007.
Part: FLOOR SUPPORT — CRACKED (FWD WET AREA) · airframe 65,370 hrs · 26,102 cycles
FWD WET AREA INTERCOSTAL CRACKED BETWEEN STA 312-328 RBL 32. GROUNDED-YES. REMOVED & REPLACED INTERCOSTAL, IAW 737-900 SRM 51-40-02-0G-0.
Part: FLOOR SUPPORT — CRACKED (FWD WET AREA) · airframe 65,370 hrs · 26,102 cycles
FWD WET AREA INTERCOSTAL CRACKED BETWEEN STA 328-344 LBL 44. GROUNDED-YES. REMOVED & REPLACED INTERCOSTAL, IAW B737-900 SRM 51-40-02-0G-0.
Part: FLOOR SUPPORT — CRACKED (FWD WET AREA) · airframe 65,370 hrs · 26,102 cycles
FWD WET AREA INTERCOSTAL CRACKED BETWEEN STA 312-328 LBL 44. GROUNDED-YES. REMOVED & REPLACED INTERCOSTAL, IAW 737-900 SRM 51-40-02-0G-0.
Part: SHEAR TIE — CRACKED (BS 540) · airframe 65,370 hrs · 26,102 cycles
SHEAR TIE AT FS 540 LBL 32 IS CRACKED AT AFT FASTENER HOLE. GROUNDED-YES. REMOVED & REPLACED WITH NEW SHEAR TIE FS 540 LBL 32, IAW B737-900 SRM 51-40-02-0G-0. LEAK CHECK GOOD, IAW B737-900 AMM 28-11-00-300-803.
Part: SHEAR TIE — CRACKED (BS 540) · airframe 65,370 hrs · 26,102 cycles
SHEAR TIE AT FS 540 RBL 32 IS CRACKED AT AFT FASTENER HOLE. GROUNDED-YES. REMOVED & REPLACED WITH NEW SHEAR TIE AT FS 540 RBL 32, IAW B737-900 SRM 51-40-02-0G-0 PERFORMED LEAK CHECK, IAW B737-900 AMM 28-11-00-300-803.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,370 hrs · 26,102 cycles
SHEAR TIE AT FS 540 LBL 6 IS CRACKED AT AFT FASTENER HOLE. GROUNDED-YES. REMOVED & REPLACED WITH NEW SHEAR TIE FS 540 LBL 6, IAW B737-900 SRM 51-40-02-0G-0. LEAK CHECK GOOD, IAW B737-900 AMM 28-11-00-300-803.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 65,370 hrs · 26,102 cycles
SHEAR TIE AT FS 540 RBL 54 IS CRACKED AT AFT FASTENER HOLE. GROUNDED-YES. REMOVED & REPLACED WITH NEW SHEAR TIE AT FS 540 RBL 54 IAW B737-900 SRM 51-40-02-0G-0. PERFORMED LEAK CHECK, IAW B737-900 AMM 28-11-00-300-803.
Part: SHEAR TIE — CRACKED (BS 540) · airframe 65,370 hrs · 26,102 cycles
SHEAR TIE AT FS 540 RBL 15 IS CRACKED AT AFT FASTENER HOLE. GROUNDED-YES. REMOVED & REPLACED WITH NEW SHEAR TIE FS 540 RBL 15, IAW B737-900 SRM 51-40-02-0G-0. LEAK CHECK GOOD, IAW B737-900 AMM 28-11-00-300-803.
Part: SHEAR TIE — CRACKED · airframe 65,370 hrs · 26,102 cycles
SHEAR TIE AT FS 540 LBL 40 IS CRACKED AT AFT FASTNER HOLE. GROUNDED-YES. REMOVED & REPLACED WITH NEW SHEAR TIE AT FS 540 LBL 40, IAW B737-900 SRM 51-40-02-0G-0. PERFORMED LEAK CHECK, IAW B737-900 AMM 28-11-00-300-803, LEAK CHECK GOOD.
Part: SHEAR TIE — CRACKED (BS 540) · airframe 65,370 hrs · 26,102 cycles
SHEAR TIE AT FS 540 LBL 15 IS CRACKED AT AFT FASTENER HOLE. GROUNDED-YES. REMOVED & REPLACED WITH NEW SHEAR TIE FS 540 LBL 15, IAW B737-900 SRM 51-40-02-0G-0. LEAK CHECK GOOD, IAW B737-900 AMM 28-11-00-300-803.
Part: SHEAR TIE — CRACKED (BS 540) · airframe 65,370 hrs · 26,102 cycles
SHEAR TIE AT FS 540 RBL 6 IS CRACKED AT AFT FASTENER HOLE. GROUNDED-YES. REMOVED & REPLACED WITH NEW SHEAR TIE AT FS 540 RBL 6, IAW B737-900 SRM 51-40-02-0G-0. PERFORMED LEAK CHECK, IAW B737-900 AMM 28-11-00-300-803. LEAK CHECK GOOD.
Part: SKIN — CRACKED (HORIZONTAL STAB.) · airframe 65,370 hrs · 26,102 cycles
LEFT HORIZONTAL STABILIZER LOWER SKIN IS CRACKED AT STAB STA 101.90 BETWEEN 92.70 AND 101.90 APPROXIMATELY 12" FROM LEADING EDGE. GROUNDED-YES. REPAIRED LT HORIZONTAL STAB LOWER SKIN CRACKED AT STAB STA 101.90 BETWEEN 92.70 AND 1019.90, IAW 737-900 SRM 55-10-01-2R-11 REPAIR 11.
Part: SHIELD — CORRODED (FWD CARGO) · corrosion level 2 · airframe 65,370 hrs · 26,102 cycles
FWD PIT TRANSITION PANEL CORRODED AT STA 500 RBL 26. GROUNDED-YES. REMOVED CORROSION AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS, IAW B737-900 SRM 53-30-15-1A-1. REMOVED AND REPLACED TRANSITION PANEL (SHIELD), IAW B737-900 SRM 51-40-02-0G-0W.5 O .032 R .022 L 1.2 D .010.
2020
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,370 hrs · 26,102 cycles
ACCOMPLISH REPAIRS FOR THE DISCREPANCIES LISTED ON THE ATTACHED AAR MIG 85A(S) FOR EMERGENCY LIGHTS. GROUNDED - YES. ALL DISC LISTED ON THE ATTACHED AAR MIG 85A WERE CORRECTED. REMOVED AND REPLACE BATTERY PACKS (S/N: 128057, 122469, 128061, 15651, & 79591) REF B737-900 AMM 33-51-06-960-805.
2019
Part: UNKNOWN — ODOR (CABIN) · airframe 64,518 hrs · 25,718 cycles
ON CLIMBOUT FROM MCI FLIGHT ATTENDANTS REPORTED STRONG ODOR COMING FROM AFT GALLEY. NO VISIBLE SMOKE OR FUMES. OVENS WERE OFF. SHUT RECIRC FANS OFF AND HAD FAS SHUT COFFEE MAKERS OFF. AFTER LEVEL OFF ODOR WENT AWAY RECIRC FANS TURNED ON AND ODOR DID NOT RETURN. LEFT ALL COFFEE MAKERS OFF. AIRCRAFT HAD BEEN DEICED ON PREVIOUS LEG BUT NOT ON THIS SEGMENT. GROUNDED - YES. INSPECTED AFT GALLEY FOR ODOR , FOUND COFFEE GROUNDS AND COFFEE BURNT ON THE HEATERS. CLEANED OFF COFFEE MAKERS IAW B737-900 AMM 25-32-03.
Part: LENS — DETACHED (EXIT SIGN) · airframe 62,741 hrs · 24,904 cycles
F/A REPORTS EXIT SIGN LENS COVER MISSING @ 17A. GROUNDED - YES. INSTALLED NEW EXIT SIGN LENS COVER @ 17A.
2018
Part: NOT REPORTED — MALFUNCTIONED (AC BAY) · airframe 60,915 hrs · 24,035 cycles
WITH ONE PACK MEL'D ON TAKE OFF FRON SLC, RT PACK MADE 3 PSI DIFFERENTIAL PRESSURE UP TO 10,000 MSL THAN THE DIFF PRESSURE REDUCED TO 0 PSI AND THE CABIN CLIMBED TO 10,000 FEET RETURNED TO SLC AFTER REFERENCING QRH. GROUNDED - YES. ON DEFERRAL.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 60,901 hrs · 24,029 cycles
EMERGENCY EXIT LIGHT POWER SUPPLY M1670 REQUIRES REPLACEMENT. GROUNDED - YES. REMOVED AND REPLACED M1670 POWER SUPPLY IAW AMM 33-51-06. OPS CHECK GOOD MECH.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 60,901 hrs · 24,029 cycles
EMERGENCY EXIT LIGHT POWER SUPPLY M1695 REQUIRES REPLACEMENT. GROUNDED - YES. REMOVED AND REPLACED M1695 POWER SUPPLY IAW AMM 33-51-06. OPS CHECK GOOD. SUPPLY, EMERGENCY POWER ( BATTERY).
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 60,901 hrs · 24,029 cycles
MAIN CABIN EMERGENCY LIGHT NOT OPERATING CORRECTLY THRU OUT CABIN. GROUNDED - YES. REMOVED AND REPLACED 3 EMERGENCY LIGHTS POWER SUPPLIES IAW AMM 33-51-06. OPS CHECKS GOOD.
Part: POWER SUPPLY — DEFECTIVE (CABIN) · airframe 60,901 hrs · 24,029 cycles
MAIN CABIN EMERGENCY LIGHTS NOT OPERATING CORRECTLY GROUNDED - YES. REMOVED AND REPLACED M1675 AND M1694. OP CHECK GOOD IAW AMM 33-51-06.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 60,901 hrs · 24,029 cycles
RT NR 3 WINDOW POST 3RD HOLE FROM BOTTOM, HAS CRACK INDICATION MARKED IN FRAME AT 2:30 POSITION. GROUNDED - YES. REMOVED DAMAGE, FABRICATED EXTENDED REPAIR PARTS AND INSTALLED IAW 900-53EA-20690.
Part: STRINGER CLIP — CORRODED (BS 867) · corrosion level 2 · airframe 60,901 hrs · 24,029 cycles
AFT CARGO BAY STRINGER CLIP AT BS 867 S26L WAS CORRODED. ACFT GROUNDED. CORROSION FOUND BEYOND ALLOWABLE LIMITS DUE TO NO PUBLISHED LIMITS AVAILABLE, REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02, DWG 146A1282, SH 104, REV-, AND SHEET 103, REV-.
Part: TRANSITION PANEL — DAMAGED (BS 727C-727F) · airframe 60,901 hrs · 24,029 cycles
AFT CARGO TRANSITION PANEL NUTPLATE HOLES BS 727D - 727E WERE ELONGATED. ACFT GROUNDED. REAMED DAMAGED HOLES IAW DWG 146A7502. AFTER MAX ALLOWABLE HOLE REMAINING .2540 DAMAGE WAS STILL PRESENT, OUT OF LIMITS IAW DWG 146A7502, REV. REMOVED AND REPLACE THE DAMAGED SECTION OF THE TRANSITION PANEL IAW DWG 146A7500 REV-, SRM 53-00-53-2R-5, SRM 51-40-02, AND AMM 51-21-99.
Part: FLOORBEAM — CORRODED (BS 947.5) · corrosion level 2 · airframe 60,901 hrs · 24,029 cycles
MAIN CABIN, BS 947.5 CENTER FLOORBEAM WAS CORRODED. ACFT GROUNDED. REMOVED THE CORROSION IAW SRM 53-70-51. FOUND TO BE OUT OF LIMITS. REMOVED THE UPPER TEE IAW SRM 53-70-51-2R-5. FABRICATED A REPAIR TEE, FOUR SPLICE ANGLES, AND FOUR STRAPS IAW SRM 53-70-51-2R-5. ROTO PEENED THE TEED IAW SOPM 20-10-03. APPLIED ALODINE IAW SOPM 20-43-03. APPLIED PRIMER IAW SOPM 20-41-02. INSTALLED THE UPPER TEE, SPLICE ANGLES, AND STRAPS IAW SRM 53-70-51-2R-5.
Part: FLOOR SUPPORT — CORRODED (BS 950) · corrosion level 2 · airframe 60,901 hrs · 24,029 cycles
MAIN CABIN AFT BS 950, LT FLOOR SUKPPORT HAD CORROSION. ACFTGROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1, REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 147A5650, REV-.
Part: SKIN — DENTED (CARGO DOOR) · airframe 60,901 hrs · 24,029 cycles
REMOVED AND REPLACED FWD CARGO DOOR OUTER SKIN PN 143A6112-2 IAW BAC DWG 143A6112 REVD AND CMM 52-31-15 REV 29. REMOVED AND REPLACED HANDLE ASSY PN 149A6134-4 IAW BAC DWG 143A6110 REV A AND CMM 52-31-15. GROUNDED - YES.
Part: CHANNEL — CORRODED (BS 727I-767) · corrosion level 2 · airframe 60,901 hrs · 24,029 cycles
AFT CARGO RIGHT TRANSITION PANEL SURFACE CORRODED, BS 727K+5 - 767, RBL 24. ACFT GROUNDED. REMOVED THE CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. ACCOMPLISHED A SPLICE REPAIR IAW SRM 53-00-53-20-5, DWG 146A7500 54.77 REV-AND 54.80 REV-. APPLIED TOPCOAT TO REPAIR AREA IAW AMM 51-21-73.
Part: TRANSITION PANEL — CORRODED (AFT CARGO) · corrosion level 2 · airframe 60,901 hrs · 24,029 cycles
AFT CARGO RT TRANSITION PANEL SURRFACE CORRODED BS 767 787 RBL 24. GROUNDED - YES. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW ASA B737-90 SRM 53-60-15-1A-1. ORIGINAL MATERIAL THICKNESS IS 0.050 IN, REMAINING THICKNESS IS 0.038 IN, REMOVED 0.012 IN. REMOVED AND REPLACED DOOR SURROUND SHIELD (TRANSITION PANEL AREA) IAW ASA 737-900 SRM 51-40-02 AND BAC 146A0081 SH. 16 REV A. REMOVED DOT B293. APPLIED TOP COAT TO REPAIR AREA IAW ASA B737-900 AMM 51-21-73. REMOVED AND REINSTALLED 1 EA INTERCOSTAL STA 787 794 FOR ACCESS IAW ASA 737-900 SRM 51-40-02- AND BAC DWG 146A8320 SH. 10 REV. A.
Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 60,901 hrs · 24,029 cycles
RIGHT WING REAR SPAR VERTICAL PRESSURE DECK WEB STA 663 AT RBL 40 HAS EVIDENCE OF A CRACK, APPROX 1.0 INCH IN A VERTICAL POSITION. GROUNDED - YES. REPAIRED ON CARD SB737-57-1330-NG-2, OPS 7675.
Part: TRANSITION PANEL — CORRODED (BS 854-859) · corrosion level 2 · airframe 60,901 hrs · 24,029 cycles
AFT CARGO RT TRANSITION PANEL SURFACE CORRODED, BS 854 - 859 AFT OF DOOR CUT OUT. GROUNDED - YES. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW ASA 737-900 SRM 53-60-15-1A-1 ORIGINAL MATERIAL THICKNESS IS 0.050 IN, REMAINING THICKNESS IS 0.042 IN, REMOVED 0.008 IN. REMOVED AND REPLACED DOOR SURROUND SHIELD (TRANSITION PANEL AREA) IAW ASA 737-900 SRM 51-40-02 AND BAC DWG 146A0081 SH. 16 REV. REMOVED AND REINSTALED 1 EA INTERCOASTAL STA 847-855 FOR ACCESS UAW ASA 737-900 SRM 51-40-02 AND BAC DWG 146A2321 SH.4 REV A. APPLIED TOP COAT TO REPAIR AREA IAW ASA 737-900 AMM 51-2-73. REMOVED DOT B288. ORIGINAL THICKNESS .071 MATERIAL REMOVED .002 MATERIAL REMAINING .069
Part: SKIN — CORRODED (BS 460) · corrosion level 2 · airframe 60,901 hrs · 24,029 cycles
FWD CARGO COMPARTMENT DOOR SILL SKIN HAS SEVERAL AREAS OF LIGHT SURFACE CORROSION ALONG LENGTH OF OPENING. MARKED IN RED. GROUNDED - YES. REMOVED CORROSION ON CORRODED AREAS ON FWD CARGO DOOR SILL WEB IAW B737-900 SRM 51-10-02, ORIG THICK 0.045, IAW B737-900 SRM 53-30-15-0I-1. REMAINING THICKNESS/LOWEST READING 0.037, AT STA 460+10. REMOVED 0.008, FOUND TO BE OUT OF LIMITS IAW B737-900 SRM 53-30-15-1A-1 TOOLING ID: UT GAUGE: T8225M. REMOVED WEB IAW B737-900 SRM 51-40-02. LOCATED AND DRILLED WEB IAW B737-900 SRM 51-40-05 AND BAC DWG 143A8330-REV A. INSTALLED NUT PLATES ON WEB IAW B737-900 SRM 51-40-02, AND BAC DWG 143A8330-REV A. INSTALLED WEB IAW B737-900 SRM 51-40-02 AND BAC DWG 143A8330 REV A.REMOVED DOT: C786.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,901 hrs · 24,029 cycles
AFT CARGO FLOOR SUPPORT TIE DOWN SURFACE CORRODED, BS 796-826 RBL14. GROUNDED - YES. REMOVED CORROSION FROM AREA ORIGINAL THICKNESS .070 IAW BAC DWG 146A7501 REV - 100% MAT LOSS. FABRICATED NEW FLOOR SUPPORT IAW SRM 53-00-53-2R-3. JOGGLED TIE DOWN TRACK IAW BAC DWG 146A7501 ERV -. ALODINED IAW SRM 51-20-01, PRIMED IAW SOPM 20-41-02. INSTALLED IAW SRM 53-00-53-2R-3 AND BAC DWG 146A7501 REV-.
Part: CHANNEL — CORRODED (BS 727G-727I) · corrosion level 2 · airframe 60,901 hrs · 24,029 cycles
AFT CARGO RT TRANSITION PANEL SURFACE CORRODED BS 727G +9 - 727K, LBL24. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 51-00-53-1A-2. ACCOMPLISHED A SPLICE REPAIR IAW SRM 53-00-53-2R-5, AND DWG 146A7500, SH 77, REV-.
Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 60,901 hrs · 24,029 cycles
R1 DOOR SURROUND FWD UPPER CORNER INNER SKIN IS SEPARATED AND BENT. GROUNDED - YES. REMOVED STUB FRAME ASSY, DOOR STOP FITTING, ROLLER GUIDE FITTING AND DEPRESSOR ON R1 DOOR CUT OUT FWD CORNER UPPER IAW SRM 51-40-02, FABRICATED LOCATED & DRILLED STUB FRAME P/N 141A8371.7 IAW SRM 51-40-05 AND BAC DWG 141A8370 REV D, ID: 0011, INSTALLED STUB FRAME ASSY, DOOR STOP FITTING, ROLLER GUIDE AND NEW DEPRESSOR P/N 141A8372U1 IAW DWG 141A8370, REV C AND SRM 51-40-02. DOOR ADJUSTMENT (FITTINGS) ACCOMPLISHED ON ROUTINE CARD.
Part: BEARING — DETACHED (WINDOW) · airframe 60,781 hrs · 23,978 cycles
FIRST OFFICERS SIDE WINDOW WILL NOT CLOSE. GROUNDED - YES. RE-ATTACHED WINDOW BEARING PER AMM 56-12-11 OPS CHECK NORMAL.
Part: SIGN — UNSECURE (CABIN) · airframe 60,555 hrs · 23,878 cycles
EXIT SIGN CAME OFF EXIT ROW AREA AIRCRAFT LEFT. GROUNDED - YES. REATTACHED EXIT SIGN AT MID CABIN AC LEFT OK FOR SERVICE.
Part: ROLLER — STUCK (R2 DOOR) · airframe 59,895 hrs · 23,568 cycles
R2 DOOR IS STUCK IN POSITION. ACFT GROUNDED. FOUND UPPER RT ROLLER UNDER ROLLER TRACK. PUSHED CORNER OF DOOR TO GET ROLLER UNSTUCK. ADJUSTED THE GUIDE ARM IAW AMM 52-41-00-820-801, STEP 1. PERFORMED A GUIDE ARM ADJUSTMENT IAW AMM 52-41-00-820-003. OP CHECKED GOOD. COMPLETED 52-41-00-820-008 THROUGH 52-41-00-820-013. OP CHECKED GOOD. PERFORMED AMM 52-41-00-700-801. OP CHECKED GOOD. ADJUSTED THE 5195 SENSOR TO WITHIN LIMITS IAW AMM 52-71-11.
Part: ROLLER — BINDING (R2 DOOR) · airframe 59,709 hrs · 23,483 cycles
CREW REPORTED THE R2 DOOR DID NOT FULLY CLOSE. ACFT GROUNDED. FOUND THE UPPER HINGE ROLLERS JAMMED OVER DOOR CLOSED SWITCH. FREED THE DOOR. NO DEFECTS OR DAMAGE NOTED AMM 52-41-00. ACFT GOOD FOR SERVICE.
2016
Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 54,909 hrs · 21,332 cycles
L2 EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMPS, OPS CHECK GOOD IAW AMM 33-51-04-960-801.
Part: TRANSITION PANEL — CORRODED (BS 727-767) · corrosion level 2 · airframe 54,909 hrs · 21,332 cycles
AFT CARGO BAY RT TRANSITION PANEL HAS CORROSION SPOTS FROM BS 727+4 - 767. ACFT GROUNDED. REMOVED AND REPLACED THE TRANSITION PANEL IAW SRM 51-40-02 AND BAC DRAWING 146A7502 REV.- AND 146A7500 REV.- AND 146A7500 REV.
Part: TRANSITION PANEL — CORRODED (BS 727-847) · corrosion level 2 · airframe 54,909 hrs · 21,332 cycles
AFT PIT, L/H TRANSITION PANEL HAS CORROSION SPOTS FROM BS 727+4 - 847. ACFT GROUNDED. REMOVED AND REPLACED AFT CARGO LT TRANSITION PANEL IAW SRM 51-40-02 AND DRAWING 146A7500 REV.
Part: TRANSITION PANEL — CORRODED (BS 400-500L) · corrosion level 2 · airframe 54,909 hrs · 21,332 cycles
FWD CARGO BAY LT TRANSITION PANEL HAS CORROSION FROM BS 400 - 500L. ACFT GROUNDED. REMOVED CORROSION FROM THE TRANSITION PANEL IAW SRM 53-00-53-1A-2 2. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 4.A
Part: TRANSITION PANEL — CORRODED (BS 500F-500L) · corrosion level 2 · airframe 54,909 hrs · 21,332 cycles
FWD CARGO BAY RT TRANSITION PANEL HAS CORROSION FROM BS 500F+10 - 500L. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53.
Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 54,707 hrs · 21,246 cycles
R1 DOOR EMERGENCY EXIT SIGN BROKEN. ACFT GROUNDED. REMOVED AND REPLACED THE EXIT SIGN IAW AMM 33-51-01. OPS CHECKED GOOD.
2014
Part: LENS — DETACHED (EMERGENCY LIGHTS) · airframe 48,999 hrs · 18,873 cycles
EXIT SIGN FELL OFF AT 17F. ACFT GROUNDED. REATTACHED EXIT SIGN AT 17F.
Part: TORQUE TUBE — DAMAGED (TE FLAPS) · airframe 48,913 hrs · 18,842 cycles
RIGHT WING T/E FLAP DRIVE TORQUE TUBE OTBD OF NR 6 TRANSMISSION SCORED. ACFT GROUNDED. REPLACED TORQUE TUBE REF AMM 27-51-58, NO ADJUSTMENT REQ, NO TURNING OF TORQUE TUBE NOTED DURING REMOVAL AND INSTALLATION.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 48,913 hrs · 18,842 cycles
CRACK INDICATION FOUND LT HORIZONTAL LOWER SKIN, FWD OF AFT SPAR, 5' OTBD OF STABILIZER, STA 166.30. 2.120' LONG. ACFT GROUNDED. REPAIRED LT HORIZONTAL LOWER SKIN STA 171.30 IAW SRM 55-10-01-2R-11.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 48,913 hrs · 18,842 cycles
CRACK INDICATION FOUND RT HORIZONTAL STABILIZER LOWER SKIN, 9' FWD OF AFT SPAR & INBD OF STABILIZER STA 101.90. MARKED AT .680' LONGERON. ACFT GROUNDED. REMOVED DAMAGE ON SKIN FWD OF STAB DOOR CUTOUT IAW SRM 53-00-51-1A-1. DAMAGE AREA IS .45" X 5.65" ORIG THICKNESS .080, REMOVED .005, REMAINING THICKNESS .075, FOUND TO BE WITHIN LIMITS. ALODINED AND PRIMED AREA IAW SRM 53-00-01-1A-1. TOP COAT RESTORED ON JOB CARD 17, CUSTOMER CARD NR 74012000.
Part: SOCKET — DAMAGED (EMERGENCY LIGHT) · airframe 48,676 hrs · 18,754 cycles
F/A REPORTS EMERGENCY EXIT LIGHT COVER OFF AT RT AFT OVERWING EXIT. ACFT GROUNDED. FOUND RIGHT AFT LOWER OVERWING EXIT LIGHT BASE DAMAGED. REPLACED SAME, OPS NORMAL, IAW MM 33-51-00.
Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 47,952 hrs · 18,467 cycles
EMERGENCY LIGHT EXIT LOCATOR SIGN ADJACENT TO L1 DOOR HAS BROKEN LENS. ACFT GROUNDED. REPLACED LENS AND TESTED IAW MM 33-51-01-960-801. OPS NORMAL.
Part: SEAT TRACK — GOUGED (BS 520) · airframe 47,065 hrs · 18,130 cycles
CABIN SEAT TRACK AT BS 520 LBL 45.50 IS GOUGED. ACFT GROUNDED. BLENDED DAMAGE IAW SRM 51-10-02.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 47,061 hrs · 18,129 cycles
RT STABILIZER LOWER SURFACE, MIDSPAN, ALONG STA 142.45 IS CRACKED. ACFT GROUNDED. DAMAGE REPAIRED IAW SRM 55-10-01-2R-11, REPAIR NR 11 ON DEFECT 11190253. CATEGORY "B" REPAIR.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 47,061 hrs · 18,129 cycles
LT STABILIZER LOWER SURFACE, JUST OTBD OF STA 105.26, JUST FWD OF THE REAR SPAR IS CRACKED. ACFT GROUNDED. REMOVED AND LT STAB LOWER SKIN IAW SRM 55-10-01-2R-11, REPAIR NR 11 THIS REPAIR IS A CATEGORY "B" REPAIR.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 47,061 hrs · 18,129 cycles
RT STABILIZER LOWER SURFACE BETWEEN STA 142.45 AND 151.75, JUST FWD OF THE REAR SPAR IS CRACKED. ACFT GROUNDED. REPAIRED THE RT STABILIZER LOWER SKIN IAW SRM 55-10-01-2R-11, REPAIR 11. THIS IS A CATEGORY "B" REPAIR.
2012
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,358 hrs · 16,376 cycles
EMERGENCY EXIT AISLE LIGHTS ABOVE SEAT ROWS 6ABC, 8ABC, AND 11ABC INOPERATIVE. R & R EMERGENCY LIGHT POWER SUPPLY M2335 IAW MM 33-51-06. OPS CHECK OF POWER SUPPLY GOOD IAW MM 33-51-06.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 42,358 hrs · 16,376 cycles
EXTERIOR LT FWD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R & R EMERGENCY LIGHTS POWER SUPPLY M2335 IAW MM 33-51-06. OPS CHECK OF EXTERIOR LT FWD OVERWING EXIT LIGHT GOOD IAW MM 33-51-06.
Part: POWER SUPPLY — DISCHARGED (EMERGENCY ,IGHT) · airframe 42,358 hrs · 16,376 cycles
EMERGENCY EXIT AISLE LIGHTS ABOVE SEAT ROWS 26ABC, 28DEF, 29ABC, AND 30DEF INOPERATIVE. R & R EMERGENCY LIGHT POWER SUPPLIES M1899 AND M1898 IAW IAW MM 33-51-06. OPS CHECK OF EMERGENCY EXIT AISLE LIGHTS GOOD IAW MM 33-51-06.
Part: PLATE — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 42,358 hrs · 16,376 cycles
AFT CARGO BAY SIDE PLATE FOUND CORRODED. REPAIRED SIDE PLATE IAW SRM.
Part: DOUBLER — CORRODED (BS 500) · corrosion level 2 · airframe 42,358 hrs · 16,376 cycles
ANTENNA DOUBLER AT BS 500 FOUND TO BE CORRODED. R & R CORRODED ANTENNA DOUBLER.
Part: STRUCTURE — CORRODED (BS 500H-500L) · corrosion level 2 · airframe 42,358 hrs · 16,376 cycles
FWD CARGO BAY LEFT TRANSITION PANEL CORRODED NUMEROUS PLACE. BS 500H - 500L, STR 26L. REMOVED CORROSION AND CHECKED LIMITS. ORIGINAL THICKNESS IN ALL AREAS IS .040. REMAINING THICKNESS FROM 500H 5 IS .038, .002. REMOVED REMAINING THICKNESS FROM 500I TO 500J IS .037 .003 REMOVED. REMAINING THICKNESS FROM 500J TO 500K IS .037, .003 WAS REMOVED. REMAINING THICKNESS FROM 500K TO 5R00 K 10 IS .038, .002 WAS REMOVED. 500K 10 TO 500L FOUND TO BE OUT OF LIMITS. ALODINED AND PRIMED H5 TO 500K 10 REF SRM 51-20-01. PAINTED AND IDENTIFIED 500 H 5 TO 500K 10 REF AMM 51-21-99, 51-05-01. FABRICATED AND INSTALLED REPAIR FROM 500K 10 TO 500L REF SRM 53-00-53.
Part: FRAME SPLICE — CORRODED (BS 787) · airframe 42,358 hrs · 16,376 cycles
FUSELAGE FRAME SPLICE AT BS 787, STR 26R FOUND TO BE CORRODED. R & R FRAME SPLICE.
Part: SEAT TRACK — CRACKED (BS 500K-520) · airframe 42,358 hrs · 16,376 cycles
SEAT TRACK AT RBL 45, BS 518 HAS AT CRACK ON INBD TANG. ACFT GROUNDED. REPAIRED SEAT TRACK AT RBL-45, BS 500K12 - BS 520 IAW REO-G15690, REV A, IAW EA 900-53EA-09414, REV NEW DATE 12DEC2012.
Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 42,358 hrs · 16,376 cycles
MAIN CABIN UNDER FLOOR PANEL INTERCOSTAL CRACKED AROUND FASTENER. BS 312 - 328, LBL 45. R & R INTERCOSTAL IAW SRM 51-40-02 AND BAC DWG 141A5400.
Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 42,358 hrs · 16,376 cycles
MAIN CABIN FLOOR SUPPORT CRACKED AROUND FASTENER. BS 328 - 344, LBL 45, R & R FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 141A5400.
Part: FRAME — DENTED (BS 480 S24L) · airframe 42,358 hrs · 16,376 cycles
FWD CARGO BAY LT SIDEWALL FRAME DENTED BS 480, STR 24L -STR 25L. ACFT GROUNDED. PERFORMED DAMAGE REMOVAL AND INSPECTION IAW REO G15718, REV IR. FABRICATED REPAIR PARTS IAW REO G15718, REV IR. R & R 5-24L & S25L STRINGER TIES IAW REO G15718 REV IR. INSTALLED FRAME REPAIR PARTS IAW REO G15718 REV IR. ALODINED AND PRIMED REPAIR PARTS IAW REO G15718 REV IR. REMOVED AND REINSTALLED INTERCOSTAL AT STR 23L, STA 480L IAW SRM 51-40-02.
Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 42,358 hrs · 16,376 cycles
CABIN FLOOR SUPPORT CRACKED BS 312 - BS 328, RBL 31. R & R FLOOR SUPPORT.
Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 42,358 hrs · 16,376 cycles
CABIN FLOOR SUPPORT CRACKED AT BS 312 TO 328, RBL 31. R & R FLOOR SUPPORT IAW SRM 51-40-02.
2011
Part: TUBE — LOOSE (NR 1 HMU) · airframe 36,137 hrs · 14,126 cycles
INITIAL CLIMBOUT LEVELOUT AT 350. NR 1 ENGINE FAIL LIGHT ROLL BACK. UNCOMMANDED SHUT DOWN IN FLT RETURNED TO SEA. FOUND LOOSE DISCHARGE TUBE ON HMU OF NR 1 ENGINE. REPLACED NR 1 ENGINE PER T/C 78471001 78471000 REF W/O 109776.
2010
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,325 hrs · 13,835 cycles
RIGHT FWD OVERWING EXIT SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PACK M1676 IAW B737 900 MM 33 51 06 960 805.
Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 35,325 hrs · 13,835 cycles
TRAILING EDGE SUPPORT ANGLE CRACKED AT RIGHT WING. REMOVED AND REPLACED SUPPORT ANGLE IAW B737 900 SRM 51 40 02.
Part: BATTERY PACK — FAILED (CABIN) · airframe 35,325 hrs · 13,835 cycles
EMERGENCY LIGHT BATTERY PACK M1695 FAILED CAPACITY TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1695 IAW B737 900 AMM 33 51 06 960 806.
Part: BATTERY PACK — FAILED (CABIN) · airframe 35,325 hrs · 13,835 cycles
EMERGENCY LIGHTS BATTERY PACK M1671 FAILS CAPACITY TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1671 IAW B737 900 AMM 33 51 06 960 805 AND 33 51 06 960 806.
Part: BATTERY PACK — FAILED (CABIN) · airframe 35,325 hrs · 13,835 cycles
EMERGENCY LIGHT BATTERY PACK M1670 FAILED CAPACITY TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1670 IAW B737 900 AMM 33 51 06 960 806.
Part: BATTERY PACK — FAILED (CABIN) · airframe 35,325 hrs · 13,835 cycles
EMERGENCY LIGHT BATTERY PACK M1694 FAILED CAPACITY TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1694 IAW B737 900 AMM 33 51 06 960 806.
Part: BATTERY PACK — FAILED (CABIN) · airframe 35,325 hrs · 13,835 cycles
EMERGENCY LIGHTS BATTERY PACK M1674 FAILED CAPACITY TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1674 IAW B737 900 AMM 33 51 06 960 806.
Part: BATTERY PACK — FAILED (CABIN) · airframe 35,325 hrs · 13,835 cycles
EMERGENCY LIGHT BATTERY PACK M1673 FAILED CAPACITY TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1673 IAW B737 900 AMM 33 51 06 960 806.
Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 35,325 hrs · 13,835 cycles
LEFT WING UPPER TRAILING EDGE SUPPORT ANGLE AT RSS 277 IS CRACKED. REMOVED AND REPLACED THE LEFT WING UPPER TRAILING EDGE SUPPORT ANGLE IAW B737 900 SRM 51 40 02 PAR 5 51 40 05 TABLE F AND 51 20 01 PAR D.
2009
Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
FOUND ON INSTALLATION OF INBOARD FLAP ON LT SIDE FOUND O/B TRAILING EDGE TRACK FOUND CORROSION ON O/B TRACK. REMOVED AND REPLACED TRACK.
Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 29,975 hrs · 11,732 cycles
FWD CARGO BAY NR 1 FLOOR PANEL PUNCTURED. REMOVED AND REPLACED FLOOR PANEL.
Part: SLAT TRACK — CHAFED (LE SLAT) · airframe 29,975 hrs · 11,732 cycles
LEFT WING NR 4 SLAT UPPER TRAILING EDGE LOWER SURFACE CHAFING I/B AUX TRACK. REPAIR NR 4 SLAT T/E WEDGE LOWER SURFACE AT I/B AUX TRACK IAW EA 900 57EA 01140.
Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY NR 2 FLOOR PANEL IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOOR PANEL.
Part: SKIN — DENTED (CARGO DOOR) · airframe 29,975 hrs · 11,732 cycles
AFT CARGO DOOR OUTER SKIN HAS DENTS OUT OF LIMITS. REPLACED OUTER SKIN.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
CORROSION AFT CARGO BAY UPON REMOVAL OF FLOOR TO SIDEWALL SUPPORT FOUND CORROSION ON BS 727D FRAME RBL 20 22 WL 156. REMOVED CORROSION PER EA900 53EA 0159.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
CORROSION AFT CARGO BAY FRAME AND DOUBLER ASSY BS 767 RBL 23 27 WL 156 158. REMOVED CORROSION PER EA900 53EA 0159.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
CORROSION ON ACB FRAME TO SHIELD CLIP BS 767 WL 157 RBL 22. REPLACED CLIP.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFTER REMOVAL OF CORRODED SHIELD FOUND FRAME STA 787 CORRODED ON UPPER FLANGE BETWEEN STR 25R AND 26R.
Part: SKIN — CHAFED (LE SLAT) · airframe 29,975 hrs · 11,732 cycles
LEFT WING NR 4 SLAT UPPER TRAILING EDGE LOWER SURFACE CHAFING AT I/B CORNER. PER EA 900 STEA 01140 ACCOMPLISHED REPAIR IAW ER 09 2242 HAS BEEN COMPLETED.
Part: FLAP TRACK — CORRODED (TE FLAP) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
CORROSION ON I/B AFT FLAP I/B TRACK. REMOVED AND REPLACED TRACK.
Part: FRAME — CORRODED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
AFTER MOVING FLOOR SUPPORT FOR REPLACEMENT FOUND FRAME CAP BS 7271 ABOVE STR 25 TO BE CORRODED. REMOVED CORROSION PER EA900 53EA 0159.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
FLOOR SUPPORT CORRODED. REMOVED AND REPLACED FLOOR SUPPORT.
Part: FITTING — DAMAGED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
WHILE WORKING BS 986 FLOORBEAM REPAIR FOUND MECHANICAL DAMAGE TO T-CLIP AT BS 986 1006 RBL 48 WL 208. REPAIRED T-CLIP.
Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
FOUND 3 MISDRILLED HOLES IN TOP OF FLOOR SUPPORT BS 767 RBL 7. REMOVED DAMAGED FLOOR SUPPORT, FABRICATED AND INSTALLED NEW SUPPORT.
Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY FLOOR PANEL NR 4 HAS CORROSION. REMOVED, CORRODED PANEL, FABRICATED AND INSTALLED NEW PANEL PER SRM.
Part: FITTING — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
INTERCOSTAL TO SIDEWALL SUPPORT TIE CLIP CRACKED. REMOVED AND REPLACED TIE CLIP WITH NEW.
Part: FITTING — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
WHILE INSPECTING INSTALLATION OF INTERCOSTAL DISCOVERED CRACKED CLIP AT BS 500H RBL 24 WL 156 ATTACHING FWD SIDE OF FRAME TO INTERCOSTAL.
Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
FWD CARGO BAY NR 4 FLOOR PANEL IS PUNCTURED. FABRICATED NEW PANEL.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
INTERCOSTAL CRACKED BS 500L K RBL 24 WL 156. REMOVED AND REPLACED WITH FABRICATED INTERCOSTAL PER SRM 51 40 02.
Part: FLOOR PANEL — CORRODED · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY FLOOR PANEL NR 4 HAS CORROSION BEYOND LIMITS. REMOVED CORRODED PANEL, FABRICATED AND INSTALLED NEW PANEL PER SRM.
Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
FWD CARGO BAY NR 5 FLOOR PANEL IS PUNCTURED. FABRICATED NEW PANEL.
Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
FWD CARGO BAY FLOOR PANEL NR 4 IS PUNCTURED. FABRICATED NEW PANEL AND INSTALLED PER SRM 51 30 01.
Part: FLOOR PANEL — CORRODED · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY FLOOR PANEL NR 1 HAS CORROSION BEYOND LIMITS. FABRICATED AND INSTALLED NEW FLOOR PANEL.
Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY FLOOR PANEL NR 5 IS CORRODED BEYOND LIMITS. CORROSION OUT OF LIMITS. REPLACED WITH FABRICATED FLOOR PER SRM 51 40 05.
Part: FLOOR PANEL — CORRODED (BS 727J-773) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY FLOOR PANEL NR 3 HAS CORROSION BEYOND LIMITS. FABRICATED AND INSTALLED NEW FLOOR PANEL.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
INTERCOSTAL BAFFLE ASSY CRACKED. REMOVED CRACKED INTERCOSTAL FABRICATED AND INSTALLED NEW INTERCOSTAL.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
INTERCOSTAL BAFFLE ASSY CRACKED. FABRICATED NEW INTERCOSTAL.
Part: CARGO TRACK — DAMAGED (CARGO BAY) · airframe 29,975 hrs · 11,732 cycles
CARGO TIE DOWN TRACK HAS MECHANICAL DAMAGE. REMOVED AND REPLACED TRACK.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
FLOOR PANEL HAS CRACKED DELAMINATED CORNER. FABRICATED REPLACEMENT FLOOR PANEL.
Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
FWD CARGO BAY NR 3 FLOOR PANEL IS PUNCTURED. FABRICATED NEW FLOOR PANEL IAW SRM 51 40 05.
Part: SKIN — CRACKED (HORIZ STAB) · airframe 29,975 hrs · 11,732 cycles
LT HORIZONTAL STAB LOWER SKIN CRACKED STAB STA 101.9, 37 TO 38 INCHES AFT OF FRONT SPAR. REPAIRED PER ER 09-2321 AND EA 900-55EA-01178.
Part: SILL — CORRODED (EMERGENCY EXIT) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
CORROSION ON LT AFT OVERWING EXIT CUTOUT UPPER SILL LIFE LINE ATTACH POINT. REPAIRED PER EA 900-53EA-01152.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
FLOOR PANEL BS 887 917 WL 208 RBL 45 62 DELAMINATED. FABRICATED NEW FLOOR PANEL PER SRM 53 00 50.
Part: SKIN — CHAFED (LE SLAT) · airframe 29,975 hrs · 11,732 cycles
NR 3 SLAT UPPER T/E WEDGE LOWER SURFACE CHAFED AT ACTUATOR. REPAIRED PER EA 900 57EA 01080.
Part: SKIN — CHAFED (LE SLAT) · airframe 29,975 hrs · 11,732 cycles
NR 6 SLAT IS WORN AT LOWER SURFACE OF UPPER T/E WEDGE. REPAIRED PER EA 900 57EA 01080.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO FRAME CORROSION BS 727F RBL 20 22 WL 156. REPAIRED PER ATS ER 09 2320.
Part: SKIN — CHAFED (LE SLAT) · airframe 29,975 hrs · 11,732 cycles
NR 2 SLAT UPPER T/E WEDGE LOWER SURFACE CHAFED AT O/B CORNER. REPAIRED PER EA 900 57EA 01080.
Part: SKIN — CHAFED (LE SLAT) · airframe 29,975 hrs · 11,732 cycles
NR 7 SLAT IS WORN AT LOWER SURFACE OF UPPER T/E WEDGE. REPAIRED PER EA 900 57EA 01080.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO FRAME CORROSION BS 727H RBL 20 22 WL 156. REPAIRED PER ATS ER 09 2320.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO FRAME CORROSION BS 727K RBL 20 22 WL 156. REPAIRED PER ATS ER 09 2320.
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
FWD ENTRY AREA FLOOR PANEL BS 270-310 WL 208 LBL 45 CRACKED, DELAMINATED AND PUNCTURED. FABRICATED REPLACEMENT FLOOR PANEL.
Part: SKIN — CHAFED (LE SLAT) · airframe 29,975 hrs · 11,732 cycles
NR 3 SLAT UPPER T/E WEDGE LOWER SURFACE CHAFED AT I/B CORNER. REPAIRED PER EA 900 57EA 01080.
Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
FRAME TO INTERCOSTAL CLIP CRACKED. REMOVED CRACKED CLIP, FABRICATED AND INSTALLED NEW CLIP.
Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
FLOOR PANEL BS 294 312 RBL 10 45 WL 208 DELAMINATED AND PUNCTURED. FABRICATED NEW FLOOR PANEL PER SRM 53 00 50.
Part: FRAME — CORRODED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
AFT CARGO FRAME CORROSION BS 727L RBL 20 22 WL 156. REPAIRED PER ATS ER 09 2320.
Part: SKIN — CRACKED (HORIZ STAB) · airframe 29,975 hrs · 11,732 cycles
LT HORIZONTAL STAB LOWER SKIN CRACKED STAB STA 175 26 INCHES TO 27.5 AFT FRONT SPAR. REPAIRED PER ER 09-2321 AND EA 900-55EA-01178.
Part: SKIN — CHAFED (LE SLAT) · airframe 29,975 hrs · 11,732 cycles
NR 1 SLAT UPPER T/E WEDGE LOWER SURFACE CHAFED O/B END. REPAIRED PER EA 900 57EA 01080.
Part: SPLICE PLATE — CORRODED (FLOOR PANEL) · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY FLOOR PANEL SPLICE PLATE CORRODED. FABRICATED NEW SPLICE.
Part: FITTING — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
INTERCOSTAL CLIP CRACKED. REMOVED AND REPLACED CLIP.
Part: SKIN — CHAFED (LE SLAT) · airframe 29,975 hrs · 11,732 cycles
NR 2 SLAT UPPER T/E WEDGE LOWER SURFACE CHAFED AT ACTUATOR. REPAIRED PER EA 900 57EA 01080.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO FRAME CORROSION BS 747 RBL 20 22 WL 156. REPAIRED PER ATS ER 09 2320.
Part: SKIN — CHAFED (LE SLAT) · airframe 29,975 hrs · 11,732 cycles
NR 1 SLAT UPPER T/E WEDGE LOWER SURFACE CHAFED AT ACTUATOR. REPAIRED PER EA 900 57EA 01080.
Part: SKIN — CHAFED (LE SLAT) · airframe 29,975 hrs · 11,732 cycles
NR 5 SLAT UPPER T/E WEDGE LOWER SURFACE CHAFED. REPAIRED PER EA 900 57EA 01080.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO FRAME CORROSION BS 727E RBL 20 22 WL 156. REPAIRED PER ATS ER 09 2320.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO FRAME CORROSION BS 727G RBL 20 22 WL 156. REPAIRED PER ATS ER 09 2320.
Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
FLOOR PANEL BS 312 344 LBL 45 WL 208 DELAMINATED AND PUNCTURED. FABRICATED NEW FLOOR PANEL PER SRM 53 00 50.
Part: SKIN — CRACKED (HORIZ STAB) · airframe 29,975 hrs · 11,732 cycles
LT HORIZONTAL STAB CRACKED STAB STA 101.9 TO 28 TO 29 INCHES AFT OF FRONT SPAR. REPAIRED PER ER 09-2321 AND EA 900-55EA-01178.
Part: SKIN — CRACKED (HORIZ STAB) · airframe 29,975 hrs · 11,732 cycles
RT HORIZONTAL STAB LOWER SKIN CRACKED STAB STA 147.9 TO 32 - 25 INCHES AFT OF FRONT SPAR. REPAIRED PER ER 09-2321 AND EA 900-55EA-01178.
Part: SKIN — CRACKED (HORIZ STAB) · airframe 29,975 hrs · 11,732 cycles
RT HORIZONTAL STAB LOWER SKIN CRACKED STAB STA 141.2 TO 144.7. REPAIRED PER ER 09-2321 AND EA 900-55EA-01178.
Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
CORROSION ON FLOORBEAM UPPER CHORD BS 986 RBL 17 WL 208. REMOVED AND INSTALLED FABRICATED FLOORBEAM UPPER CHORD PER SRM 53-70-51.
Part: BRACKET — CRACKED (RT WING) · airframe 29,975 hrs · 11,732 cycles
RT WING FIXED T/E AFT AIR DAM BRACKET CRACKED RSS 261. REMOVED CRACKED AND INSTALLED NEW BRACKET PER SRM 51 40 02.
Part: SKIN — CRACKED (HORIZ STAB) · airframe 29,975 hrs · 11,732 cycles
RT HORIZONTAL STAB LOWER SKIN CRACKED STAB STA 101.9, 28 INCHES AFT OF FRONT SPAR. REPAIRED PER ER 09-2321 AND EA 900-55EA-01178.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
CORROSION ON FLOOR TO SIDEWALL SUPPORT ZEE IN AFT CARGO BAY. REMOVED AND REPLACED SUPPORT ZEE.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
FOUND CORROSION ON AFT FACE OF FRAME AT BS 500I STR 25L. CUT OUT DAMAGED AREA AND REPAIRED.
Part: INTERCOSTAL — CRACKED (BS 500C-500D) · airframe 29,975 hrs · 11,732 cycles
FWD CARGO BAY INTERCOSTAL CRACKED. REMOVED CRACKED INTERCOSTAL, FABRICATED AND INSTALLED NEW INTERCOSTAL.
Part: WEB — CORRODED (BS 847-867) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO DOOR CUTOUT SUPPORT WEB CORRODED. REMOVED AND REPLACED WITH NEW WEB.
Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY LOWER SILL THRESHOLD WEB HAS CORROSION BEYOND LIMITS. FABRICATED NEW WEB AND REPLACED CORRODED ONE.
Part: SUPPORT — CORRODED (BS 500G-500L) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 500L STR 25L. REMOVED AND INSTALLED FABRICATED FWD CARGO FLOOR TO SIDEWALL SUPPORT CHANNEL PLATE.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
FWD CARGO BAY INTERCOSTAL CRACKED. REPLACED INTERCOSTAL.
Part: WEB — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
HORIZONTAL FLOOR WEB FROM BS 986 1016 LBL 31 47 CRACKED. REMOVED CRACKED WEB, FABRICATED AND INSTALLED NEW WEB.
Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
CORRODED STRAP BS 787-794 STR 25-26R AT UPPER FLANGE OF INTERCOSTAL. REMOVED AND INSTALLED, FABRICATED STRAP PER SRM 51-40-02.
Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
FWD CARGO BAY INTERCOSTAL SUPPORT CLIP CRACKED. REMOVED CLIP, FABRICATED NEW CLIP AND INSTALLED.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY INTERCOSTAL CRACKED. FABRICATED NEW INTERCOSTAL IAW MANUFACTURERâS DRAWING 146A7505.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
CORROSION ON FLOOR STRUCTURE SUPPORT. INSTALLED NEW FLOOR SUPPORT P/N 141A521101.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
CRACKED VAPOR BARRIER STIFFENER BS 663 RBL 7 TO RBL 31 WL 160.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
INTERCOSTAL FOUND TO BE CRACKED. REPLACED INTERCOSTAL.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
CORROSION FWD CARGO BAY FRAME 500I AT STRINGER 25L. REPAIRED PER EA 900-53EA-01172.
Part: WEB — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
HORIZONTAL FLOOR WEB FROM BS 986-1016 LBL 31-47 CRACKED. REPAIRED CRACKED WEB.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
INTERCOSTAL CRACKED FWD CARGO BAY. REMOVED AND INSTALLED FABRICATED INTERCOSTAL PER SRM 51-30-01.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
FWD CARGO BAY INTERCOSTAL CRACKED. REPLACED INTERCOSTAL.
Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
STRINGER CLIP AT BS 500I STR 27R IS CORRODED. STRINGER CLIP IS FOUND OUT OF LIMITS, REMOVED AND REPLACED.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
CORROSION AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT. REPLACEMENT TO BE ACCOMPLISHED ON MIG 5.
Part: WEB — CORRODED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
CORROSION ON WEB JUST AFT OF AFT GALLEY AFT RT FOOT MOIST. REMOVED AND REPLACED WEB.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
BULKHEAD SUPPORT FWD CARGO BAY CORRODED. REMOVED AND REPLACED BULKHEAD SUPPORT.
Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
FWD CARGO BAY STRINGER CLIP CORRODED. REMOVED AND REPLACED CLIP.
Part: WEB — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY CLOSEOUT WEB CRACKED. REMOVED CRACKED WEB, FABRICATED AND INSTALLED NEW WEB.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT.
Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 29,975 hrs · 11,732 cycles
FWD CARGO BAY NR 2 FLOOR PANEL PUNCTURED. REPLACED FLOOR PANEL WITH FABRICATED NEW PANEL.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
FWD CARGO DOOR FLOOR TO SIDEWALL HAS CORROSION. REPLACED FLOOR TO SIDEWALL SUPPORT.
Part: SILL — GOUGED (BS 400-480) · airframe 29,975 hrs · 11,732 cycles
FWD CARGO DOOR LOWER SILL VERTICAL WEB GOUGED. BLENDED OUT GOUGES AT 16 LOCATIONS THAT WERE WITHIN LIMITS REPAIRED 2 LOCATIONS THAT WERE OUT OF LIMITS.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
CORROSION ON Z-CHANNEL BS 270 RBL 9 LBL 9. REMOVED AND REPLACED WITH NEW FABRICATED Z-CHANNEL.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT IS CORRODED BEYOND LIMITS.
Part: SKIN — DENTED (CARGO DOOR) · airframe 29,975 hrs · 11,732 cycles
DENT IN FWD CARGO DOOR.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT IS CORRODED.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT IS CORRODED. REMOVED AND REPLACED AFT CARGO FLOOR TO SIDEWALL SUPPORT BS 727C+10 TO 727I RBL 20 WL 156.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT IS CORRODED. REMOVED CORROSION PER EA900-53EA-01159.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT IS CORRODED.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT IS CORRODED. SDR WRITTEN IN ERROR SIDEWALL SUPPORT TO BE REPLACED ON MIG 5.
Part: SKIN — DENTED (CARGO DOOR) · airframe 29,975 hrs · 11,732 cycles
DENT IN FWD CARGO DOOR. REPAIRED DENT FOUND OUT OF LIMITS.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT IS CORRODED. SDR WRITTEN IN ERROR SIDEWALL TO BE REPLACED ON MIG 5.
Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
DRILL START IN INTERCOSTAL. REPAIRED INTERCOSTAL.
Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO BAY FLOOR SUPPORT SPLICE RAIL IS CORRODED. REPLACED FLOOR SUPPORT.
Part: RIB — DAMAGED (RT WING) · airframe 29,975 hrs · 11,732 cycles
LEADING EDGE NOSE RIB ON RT WING O/B MAIN FLAP HAS AN ELONGATED HOLE. FABRICATED AND INSTALLED NEW FITTING.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
INTERCOSTAL CRACKED BEYOND LIMITS AT FASTENER HOLE. REMOVED AND REPLACED WITH A NEW PART.
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
CORRODED FWD CARGO BAY DOOR SUB THRESHOLD BEYOND LIMITS. REMOVED AND REPLACED FWD CARGO BAY DOOR SUB THRESHOLD WEB.
Part: PANEL — DAMAGED (WING) · airframe 29,975 hrs · 11,732 cycles
PANEL 667ET HAS AN ELONGATED HOLE. REPAIRED HOLE PER EA 900-57EA-01164 / ER 09-2331 REV A.
Part: SKIN — DENTED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
DENT IN FUSELAGE SKIN BEYOND LIMITS OF SRM 53-00-01. REMOVED DENT 1X1 INCH AND REPAIRED WITH EXTERNAL SKIN DOUBLER.
Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO FLOOR SUPPORT IS CORRODED. REPAIRED FLOOR SUPPORT.
Part: SKIN — DENTED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
DENT BEYOND LIMITS IN FUSELAGE SKIN. REPAIRED FUSELAGE SKIN.
Part: WEB — GOUGED (CARGO BAY) · airframe 29,975 hrs · 11,732 cycles
FWD CARGO BAY CLOSE OUT WEB HAS EDGE DAMAGE GOUGES AND BARE METAL. REPLACED WEB.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
CRACKED INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL.
Part: SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
CORROSION AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 727I+10 TO 767 RBL 20 WL 156. REMOVED AND REPLACED AFT CARGO FLOOR TO SIDEWALL SUPPORT.
Part: PLATE — CORRODED (CARGO BAY) · airframe 29,975 hrs · 11,732 cycles
FWD CARGO BAY RT SIDE PLATE CORRODED. REMOVED AND INSTALLED FABRICATED RT SIDE PLATE BS 500B-500L PER SRM 53-00-53.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
CORROSION AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 797-847 LBL 20 WL 156. REMOVED AND REPLACED SUPPORT.
Part: FLOOR SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
CORROSION ON LBL 3 FLOOR SUPPORT BS 772 WL 156 ZEE. REMOVED AND REPLACED FLOOR SUPPORT.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
CORROSION AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT ZEE BS 727I+10 TO BS 797 LBL 20 WL 158. FABRICATED AND REPLACED SIDEWALL SUPPORT ZEE.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
CORROSION ON FLOOR SUPPORT G4 AFT O/B FOOT MOUNT. REMOVED AND REPLACED FLOOR SUPPORT.
Part: WEB — GOUGED (CARGO BAY) · airframe 29,975 hrs · 11,732 cycles
FWD CARGO BAY CLOSE OUT WEB REVEAL HAS EDGE DAMAGE GOUGES AND BARE METAL. REPLACED WEB.
Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 29,975 hrs · 11,732 cycles
LT HORIZONTAL STAB LEADING EDGE PREVIOUSLY REWORKED DENT ON I/B REMOVABLE LEADING EDGE SEGMENT AT L/E STA 113. REPAIRED LT HORIZONTAL LEADING EDGE.
Part: FLOOR PANEL — CORRODED (COCKPIT) · airframe 29,975 hrs · 11,732 cycles
CORROSION ON COCKPIT FLOOR PANEL BS 262-270 RBL 9 LBL 9. REMOVED FLOOR PANEL, FABRICATED NEW PANEL AND INSTALLED.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,975 hrs · 11,732 cycles
INTERCOSTAL CRACKED BS 336 LBL 45 WL 208. REPLACED INTERCOSTAL.
Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
CORROSION ON FSD THRESHOLD I/B SUPPORT CHANNEL. REMOVED AND REPLACED FSD THRESHOLD SUPPORT CHANNEL.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,975 hrs · 11,732 cycles
AFT CARGO LONGITUDINAL FLOOR SUPPORT ABOVE S26R HAS CORROSION BS 794-827. REMOVED DAMAGED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED NEW SUPPORT.
2007
Part: HOUSING — GOUGED (CARGO DOOR) · airframe 24,352 hrs · 9,524 cycles
AFT CARGO DOOR HOUSING GOUGED. REPAIRED IAW EA 5230 01123.
Part: HOUSING — GOUGED (CARGO DOOR) · airframe 24,352 hrs · 9,524 cycles
FWD CARGO DOOR HOUSING GOUGED. REPAIRED IAW EA 5230 01123.