N777FD

Part: DIAPHRAGM — UNKNOWN (L1 DOOR SLIDE) · airframe 77,331 hrs · 28,909 cycles

L1 SLIDE PACK FELL OUT OF DOOR RECESS WHEN DOOR OPENED FROM OUTSIDE. (DOOR NOT DISARMED FROM PREVIOUS FLIGHT). REPLACED DIAPHRAGM IN L1 DOOR EMERGENCY POWER RESERVOIR PER M.M. 12-15-10-3 & SERVICE SAME TO GREEN BAND PER M.M. 12-15-10-3, REINSTALLED L1 SLIDE PACK BACK IN DOOR COVER PER M.M. 25-66-01-4, SAFETY PIN REMOVED FROM SLIDE AND INSTALLED IN POUCH. VERIFIED NORMAL DOOR ARMING AND CLOSED INDICATION AND SLIDE PRESSURE. A/C OK FOR SERVICE.

Part: NOT REPORTED — UNKNOWN (HYDRAULIC SYS) · airframe 76,711 hrs · 28,471 cycles

LOST LEFT HYDRAULIC QUANITY & PRESSURE ON 5 MILE FINAL. RAN QRH AND LANDED. REMOVED AND REPLACED THE TEMP LINE IAW AMM 20-10-10-4-0. TESTED THE LT DOWNLOCK ACTUATOR AND LINES IAW AMM 32-32-02-4, NO LEAKS NOTED. RAN ENGINES IAW MM-3614 AND ACTUATED ALL FLIGHT CONTROLS MULTIPLE TIMES INCLUDING ALT T/E FLAP/SLAT OPS TEST IAW AMM 27-51-26-4, NO FAULTS FOUND.

Part: WIRE — DAMAGED (EVAC SLIDE) · airframe 76,506 hrs · 28,334 cycles

R1 SLIDE LIGHT INTERMITTENT, FOUND WIRE W3682-0003-20 AND WIRE W3682-0012-20 BROKEN APPROX 60 INCHES FROM SPLICE SP1478 AND SPLICE SP68. REPAIRED REF WDM 25-66-11 PG 901 AND SWPM. CKS OK. MEL CLEARED AND PLACARD REMOVED.

Part: PITOT TUBE — DAMAGED (PITOT/STATIC SYS) · airframe 75,429 hrs · 27,628 cycles

BIRDSTRIKE ON DEPARTURE. LOST ALL AIRSPEED INDICATIONS AND ASSOCIATED ITEMS ON F/O'S SIDE. R & R F/O'S PITOT TUBE REF 34-11-01-4, THROUGH STEP 29, STEP 30, LEAKAGE TEST NEEDS ACCOMPLISHED. PERFORMED PITOT LEAK CHECK OF F/O'S PITOT TUBE IAW AMM 34-11-01-5. LEAK CHECKS WITHIN LIMITS. ACFT OK FOR SERVICE.

Part: COLLAR — INOPERATIVE (L1 DOOR) · airframe 75,103 hrs · 27,391 cycles

L1 DOOR HOLD OPEN LOCK INOPERATIVE. DOOR OPENS & SHUTS NORMALLY. R & R L1 DOOR HOLD OPEN LOCK COLLAR & CATCH IAW MM 52-11-08-8. OPERATIONS CHECKED GOOD.

Part: BEARING — LOOSE (L1 DOOR) · airframe 75,031 hrs · 27,330 cycles

CABIN L1 DOOR, FWD EDGE LOWER LATCH CRANK FOUND LOOSEN AT SUPPORT BEARING AREA. L1 DOOR, FWD LOWER LATCH CRANK R & R IAW CMM 52-11-07 REV 114. L1 DOOR FWD LOWER LATCH CRANK SUPPORT BEARING R & R IAW SOPM 20-50-03 REV 127. ADJUSTMENT CHECK CARRIED OUT IAW AMM 52-11-00 REV 114. FOUND GOOD. REPAIR CLASSIFIED AS MINOR.

Part: STOP FITTING — GALLED (L1 DOOR) · airframe 75,031 hrs · 27,330 cycles

CABIN L1 DOOR, FWD EDGE NR 1 - 7 STOP PINS FOUND METAL GALLING. R & R IAW AMM 52-11-00 REV 114. ADJUSTMENT CHECK CARRIED OUT IAW AMM 52-11-00 REV 114. FOUND GOOD. REPAIR CLASSIFIED AS MINOR.

Part: SEAT TRACK — DAMAGED (BS 608) · airframe 74,981 hrs · 27,303 cycles

BS 608, RBL 45.5, SEAT TRACK INNER FLANGE, FOUND ONE ELONGATED HOLE. REPAIRED IAW EA F-5310-T0321333. REPAIR CLASSIFIED AS MAJOR.

Part: SUPPORT ANGLE — CORRODED (BS 1681) · corrosion level 2 · airframe 74,981 hrs · 27,303 cycles

BS 1681, R4 DOOR SCUFF PLATE SUPPORT ANGLE FOUND CORRODED. REPAIRED IAW EA F-5310-T0321518 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (BS 988) · airframe 74,981 hrs · 27,303 cycles

BS 988, BL 45.5, SEAT TRACK CROWN, SUPPORT INNER FLANGE FOUND ONE ELONGATED HOLE. REPAIRED IAW EA F-5310-T0321399 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,981 hrs · 27,303 cycles

BS 1640, FLOORBEAM HAS CORROSION. REPAIRED IAW EA F-5310-T0321037 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 74,981 hrs · 27,303 cycles

CABIN BS 1640, FLOORBEAM EXISTING REPAIR HAS CORROSION. COMPLIED WITH EA F-5310-T0321037 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN PANEL — CHAFED (RT WING) · airframe 749 hrs · 27,303 cycles

RIGHT WING, OTBD NOSE SKIN FOUND CHAFED AT 2.5" FROM OTBD EDGE. NOSE SKIN R & R IAW SRM 51-40-02 REV 116 & DWG 113N3500 SHT 3 REV D. REPAIR CLASSIFIED AS MAJOR.

Part: BEAM — GOUGED (CARGO DOOR) · airframe 749 hrs · 27,303 cycles

FORWARD CARGO DOOR LOWER EDGE BEAM HAS GOUGE MARKS. R & R WITH NEW LOWER EDGE BEAM IAW DWG NR 143N6603 SHT 9 REV F. REPAIR CLASSIFIED AS MAJOR.

Part: SUPPORT BEAM — WORN (NR 2 PYLON) · airframe 749 hrs · 27,303 cycles

NUMBER 2 PYLON, FAN COWL SUPPORT BEAM AFT WEB, OTBD DOUBLER AT NAC STATION 102.1, FOUND WEAR MARK.

Part: DOUBLER — DEBONDED (TE FLAP) · airframe 749 hrs · 27,303 cycles

EXISTING REPAIR, WINGS RT SIDE, THERE IS A RT INBD FLAP LOWER SURFACE INBD PANEL REPAIR. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-7-5001 A4 PT 1, ATTACHMENT B, NO HISTORY. EXISTING REPAIR WAS EVALUATED IAW ATTACHMENT B OF EO F-5100-7-5001 A4 PART 1. FOUND REPAIR DOUBLER DIS BONDED. EXISTING REPAIR WAS REMOVED & NEW REPAIR CARRIED OUT IAW SRM 51-70-10-2R REV 116. SEE EA F-5750-TO321516 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — DEBONDED (TE FLAP) · airframe 749 hrs · 27,303 cycles

EXISTING REPAIR, RT SIDE UPPER SIDE OF INBD MAIN FLAP PANEL. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-7-5001 A4 PT 1, ATTACHMENT B, NO HISTORY. EXISTING REPAIR WAS EVALUATED IAW ATTACHMENT B OF EO F-5100-7-5001 A4 PART 1. FOUND REPAIR DOUBLER DIS BONED IAW SRM 51-10-06-2R REV 116. EXISTING REPAIR WAS REMOVED & NEW REPAIR CARRIED OUT IAW SRM 51-70-10-2R REV 116. SEE EA F-5750-T0321516 TITLE. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

CABIN STATION 1480, STRINGER 1 FRAME TWO EACH FASTENER HOLES FOUND ELONGATED. FRAME REPAIR CARRIED OUT AT STATION 1480, LBL 3 & RBL 3 IAW SRM 53-00-07 FIG 201 REPAIR 3 REV 116. THIS IS A CAT B REPAIR WITH A THRESHOLD OF 10,000 FLIGHT CYCLES, AFTER REPAIR HFEC FOLLOW UP AT 12,000 FLIGHT CYCLES INTERVALS. ALTERNATE FOLLOW UP INSPECTION AT 9000 FLIGHT CYCLES DETAILED VISUAL INSPECTION INTERVALS. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

CABIN STATION 1460, STRINGER 1 FRAME WEB FOUND TWO EACH ELONGATED HOLES AFTER BRACKET REMOVED, REF SNRM N01466. CABIN FRAME REPAIR CARRIED OUT IAW SRM 53-00-07 FIG 201 REPAIR 3 REV 116. THIS IS A CAT B REPAIR WITH A THRESHOLD OF 10,000 FLIGHT CYCLES, AFTER REPAIR HFEC FOLLOW UP AT 12,000 FLIGHT CYCLES INTERVALS. ALTERNATE FOLLOW UP INSPECTION AT 9,000 FLIGHT CYCLES DETAIL VISUAL INSPECTION INTERVALS. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,980 hrs · 27,303 cycles

BS 680, RBL 24.75 SEAT TRACK CROWN SUPPORT FOUND CORRODED. REPAIRED IAW EA F-5310-T0321853 A PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 749 hrs · 27,303 cycles

CABIN STATION 1120 - 1140 LT, CREASE BEAM WEB FOUND CORROSION. FOUND OUT OF 10% LIMIT IAW SRM 53-40-13, ALLOWABLE DAMAGE 1 FIG 101 REV 116. CREASE BEAM WEB REMOVED IAW SRM 51-40-02 REV 116. NEW CREASE BEAM WEB FABRICATED IAW DWG 144N5210 SHT 1 REV. INSTALLED IAW DWG 144N5200 SHT 2 REV B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

CABIN STATION 932 RT, CREASE BEAM WEB FOUND O1 EACH ELONGATED HOLE. CREASE BEAM WEB REMOVED AT STATION 920 - 940, RBL 63 & 70.5 IAW SRM 51-40-02 REV 116. CREASE BEAM WEB FABRICATED & INSTALLED IAW DWG 144N5140 SHT 6 REV. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 749 hrs · 27,303 cycles

CABIN STATION 960 - 984 RT CREASE BEAM WEB FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 115. REWORKED AREA, EVALUATED MATERIAL THICKNESS, REMOVED 0.020 " FOUND OUT OF 10% LIMITS IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEB R & R IAW SRM 51-40-02 REV 116 & DWG 144N5140 SHT 3 REV D. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: CREASE BEAM — CHAFED (BS 1590) · airframe 749 hrs · 27,303 cycles

BS 1590 LT, CREASE BEAM INBD CHORD LOWER SURFACE CHAFED. COMPLIED WITH EA F-5310-T0321812 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

CABIN STATION 1110 RT, CREASE BEAM WEB FOUND 01 ELONGATED HOLE. CABIN CREASE BEAM WEB AT STATION 1100 - 1120, RBL 63 & RBL 70.5 REMOVED IAW SRM 51-40-02 REV 116. CREASE BEAM WEB FABRICATED IAW DWG 144N5210 SHT 1 REV. INSTALLED IAW DWG 144N5200 SHT 1 REV B REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

CABIN STATION 932 RT, CREASE BEAM INNER CHORD FOUND 01 EACH ELONGATED HOLE. CREASE BEAM INNER CHORD REMOVED AT STATION 900 - 1040 RT IAW SRM 51-40-02 REV 116. CREASE BEAM INNER CHORD FABRICATED IAW DWG 144N5152 SHT 1 REV. INSTALLED IAW DWG 144N5140 SHT 3 REV D & SHT 4 REV A. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 749 hrs · 27,303 cycles

CABIN STATION 1420 - 1440 RT, CREASE BEAM WEB UPPER SURFACE CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 115. REWORKED AREA EVALUATED, MATERIAL THICKNESS REMOVED 0.010", FOUND OUT OF 10% LIMIT IAW SRM 53-60-13 ALLOWABLE DAMAGE 1 FIG 101 REV 116. CREASE BEAM WEB REMOVED IAW SRM 51-90-02 REV 116. CREASE BEAM WEB REMOVED IAW SRM 51-40-02 REV 116. CREASE BEAM WEB FABRICATED & INSTALLED IAW DWG 146N5590 SHT 4 REV E. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: CREASE BEAM — CORRODED (BS 984-996) · corrosion level 2 · airframe 749 hrs · 27,303 cycles

BS 984 - 996 RT, CREASE BEAM INNER CHORD VERTICAL FLANGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 115. FOUND OUT OF 10% LIMIT IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM INNER CHORD R & R IAW DWG 144N5140 SHT 3 REV D & SHT 4 REV A REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 749 hrs · 27,303 cycles

CABIN STATION 1140 - 1160 RT, CREASE BEAM WEB FOUND CORROSION. CORROSION REMOVED IAW 51-10-02 REV 115. REWORKED AREA, EVALUATED MATERIAL & REMOVED 0.026" FOUND OUT 10% LIMIT IAW SRM 53-40-13, ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEB REMOVED IAW SRM 51-40-02 REV 116. CREASE BEAM WEB FABRICATED IAW DWG 144N5210 SHT 1 REV. INSTALLED IAW DWG 144N5200 SHT 2 REV B REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 749 hrs · 27,303 cycles

CABIN STATION 996 - 1020 RT CREASE BEAM WEB FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 115. REWORKED EVALUATED MATERIAL & REMOVED 0.014" FOUND OUT OF 10% LIMIT IAW SRM 53-40-12 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEB REMOVED IAW SRM 51-40-02 REV 116. CREASE BEAM WEB FABRICATED & INSTALLED IAW DWG 144N5140 SHT 4 REV A REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — DAMAGED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

CABIN STATION 1110 RT, CREASE BEAM INNER CHORD FOUND 01 EACH ELONGATED HOLE. REMOVED IAW SRM 51-40-02 REV 116 FROM STATION 1040 - 1180 RT. CREASE BEAM INNER CHORD FABRICATED IAW DWG 144N5124 SHT 1 REV. INSTALLED IAW 144N5200 SHT 1 REV B & SHT 2 REV B. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 749 hrs · 27,303 cycles

CABIN STATION 940 - 960 RT, CREASE BEAM WEB FOUND CORROSION. REMOVED IAW SRM 51-10-02 REV 116. REWORKED AREA, EVALUATED & REMOVED 0.006" & FOUND OUT OF 10% LIMIT IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEB REMOVED IAW SRM 51-40-02 REV 116. CREASE BEAM WEB FABRICATED & INSTALLED IAW DWG 144N5140 SHT 3 REV D. REPAIR CLASSIFIED AS MAJOR.

Part: BEAM — CRACKED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

FORWARD E & E COMPARTMENT, STATION 263 BHD, BL 0 VERTICAL BEAM UPPER END CRACKED. CRACKED VERTICAL BEAM REMOVED & NEW VERTICAL BEAM FABRICATED IAW DWG 141N2913 SHT 1 REV B & INSTALLED IAW DWG 141N2910 SHT 1 REV E. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

EXTERIOR SKIN NUMEROUS SMALL NICKS & SCRATCHES ALONG THE BELLY OF THE ACFT, BETWEEN STRINGER 26 LT & 26 RT, AT BS 520 - 540. EXTERIOR SKIN, NUMEROUS SMALL NICKS & SCRATCHES REMOVED, FOUND OUT OF LIMIT AT STATION 537, 2.5" TO STRINGER 28R IAW SRM 53-00-01 FIG 101 DETAIL II REV 116 & REPAIR CARRIED OUT IAW SRM 53-00-01 FIG 201 REPAIR 16 REV 116. THIS IS A CAT B REPAIR. THRESHOLD 37000 FC REQUIRE LFEC REPEAT INTERVAL INSPECTION AT 3000 FC. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

FUSELAGE UNDER SHORING LT SIDE, THERE ARE SEVERAL SMALL SCRATCHES AT THE SHORING PAD AREA, BS 200 - 210, FROM LBL 30 - BL 0. REMOVED & FOUND OUT OF LIMIT AT STATION 200, LBL 9.5 IAW SRM 53-00-01 FIG 101 DETAIL 11 REV 116 & COMPLIED WITH EA F-5330-T0321490 PART 1. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.

Part: SKIN — NICKED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

FUSELAGE EXTERIOR SKIN LT SIDE, AFTER SHORING REMOVAL & SKIN CLEAN UP, FOUND A NICK MARK AT BS 620 & STRINGER 28. EXTERIOR SKIN, NICK MARK REMOVED, FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 116. REPAIR CARRIED OUT AS IAW SRM 53-00-01 FIG 201 REPAIR 15 REV 116. THIS IS A CAT B REPAIR. THRESHOLD 37000 FC REQUIRE LFEC INTERVAL INSPECTION AT 3000 FC. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

CABIN STATION 780 - 790, RBL 45.5, SEAT TRACK CROWN FOUND CHAFED. COMPLIED WITH EA F-5310-T0322310 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

CABIN STATION 780 - 800, RBL 24.75 SEAT TRACK CROWN FOUND CHAFED. CHAFED MARK REMOVED IAW SRM 51-10-02 REV 115. REWORKED AREA, EVALUATED CLEAN UP DEPTH OF 0.493" ON SEAT TRACK, CROWN LIP EXCEED LIP LIMIT OF 0.48" IAW SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE 1 REV 116. SEAT TRACK REPAIR CARRIED OUT IAW SRM 53-00-52 FIG 201 REPAIR 1 OPTION 1 REV 116. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

CABIN STATION 700 - 720, RBL 24.75, SEAT TRACK CROWN FOUND CHAFED. CHAFED MARK REMOVED IAW SRM 51-10-02 REV 115. REWORKED AREA, EVALUATED CLEAN UP DEPTH OF 0.028" ON SEAT TRACK CROWN EXCEED CROWN LIMIT 0.02" IAW SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE 1 REV 116. SEAT TRACK REPAIR CARRIED OUT AT STATION 698 - 730, RBL 24.75 IAW SRM 53-00-52 FIG 201 REPAIR 1 OPTION 1 REV 116. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

CABIN STATION 560 - 564, RBL 24.75, SEAT TRACK CROWN FOUND CHAFED. COMPLIED WITH EA F-5310-T0322362 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

CABIN STATION 984 - 996, RBL 24.75, SEAT TRACK CROWN FOUND CHAFED. CHAFED MARK REMOVED IAW SRM 51-10-02 REV 115. REWORKED AREA MEASURED CLEAN UP DEPTH OF 0.028" ON SEAT TRACK CROWN EXCEEDS CROWN LIMIT OF 0.020" IAW SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE 1 REV 116. SEAT TRACK CROWN REPAIR CARRIED OUT, BETWEEN STATION 984 - 1075, RBL 24.75 IAW SRM 53-00-52 FIG 201 REPAIR 4 REV 116. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

FUSELAGE EXTERIOR SKIN RT SIDE AT BS 1530, BETWEEN STRINGER 27 - 28, THERE IS A DEEP BLEND. DEEP BLEND FOUND OUT OF LIMIT IAW SRM 53-00-01 FIG 101 DETAIL II REV 116 & REPAIR CARRIED OUT IAW SRM 53-00-01 FIG 201 REPAIR 16 REV 116. THIS IS CAT B REPAIR. INSPECTION THRESHOLD 16,000 FC FROM TIME OF REPAIR REQUIRED LFEC REPEAT INSPECTION AT 3,000 FC. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — CRACKED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

EXTERIOR SKIN NUMEROUS SMALL NICKS & SCRATCHES ALONG THE BELLY OF THE ACFT, BETWEEN STRINGERS 26 LT & 26 RT AT BS 1580 - 1600. REMOVED IAW SRM 51-10-02 REV 115, FOUND WITHIN LIMIT IAW SRM 53-00-01 FIG 101 DETAIL II REV 116, EXCEPT HFEC INSPECTED FOUND CRACK AT STATION 1596, 2 3/8 " FROM STRINGER 28R. REPAIR CARRIED OUT IAW SRM 53-00-01 FIG 201 REPAIR 16 REV 116. 16,000 FC FROM TIME OF REPAIR REQUIRED LFEC REPEAT INSPECTION AT 3,000 FC. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 749 hrs · 27,303 cycles

CABIN STATION 365, RBL 24.75 SEAT TRACK CROWN SUPPORT FOUND CORROSION. SEAT TRACK CROWN SUPPORT CORROSION REMOVED IAW SRM 51-10-02 REV 116 & FOUND CORROSION MORE THAN 50% THRU. SEAT TRACK CROWN & SUPPORT REMOVED, BETWEEN STATION 365 - 440, RBL 24.75 IAW SRM 51-40-02 REV 116. NEW SEAT TRACK SUPPORT & CROWN INSTALLED IAW DWG 141N5130 SHT 2 REV E. REPAIR CLASSIFIED AS MAJOR.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 749 hrs · 27,303 cycles

CABIN STATION 365, RBL 45.5 SEAT TRACK CROWN SUPPORT FOUND CORROSION. CABIN STATION 365, RBL 45.5 SEAT TRACK CROWN SUPPORT CORROSION REMOVED IAW SRM 51-10-02 REV 116 & FOUND CORROSION MORE THAN 50% THRU. SEAT TRACK CROWN & SUPPORT REMOVED BETWEEN STATION 365 - 440, RBL 45.5 IAW SRM 51-40-02 REV 116. NEW SEAT TRACK SUPPORT & CROWN INSTALLED IAW DWG 141N5130 SHT 2 REV E. REPAIR CLASSIFIED AS MAJOR.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 749 hrs · 27,303 cycles

BS 1080 RT CREASE BEAM INNER CHORD SPLICE FITTING FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 115. FOUND CORROSION MORE THAN 50% THROUGH. CORRODED SPLICE FITTING REMOVED IAW SRM 51-40-02 REV 116. SPLICE FITTING FABRICATED IAW DWG 144N5215 SHT 1 REV. INSTALLED IAW DWG 144N5200 SHT 1 REV B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

AFT CARGO DOOR CUT OUT LOWER SILL WEB, CORROSION AT STATION 1420. AFT CARGO DOOR CUT OUT CORRODED WEB AT STATION 1380 - 1440, STRINGER 27R, R & R WITH NEW FABRICATED WEB IAW DWG 146N8522 SHT 1 REV E. NEW WEB FABRICATED IAW DWG 146N8522 SHT 1 REV E. REPAIR CLASSIFIED AS MAJOR.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 749 hrs · 27,303 cycles

BS 1120 RT, CREASE BEAM INNER CHORD SPLICE FITTING, FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 115. FOUND MORE THAN 50% THROUGH. CORRODED SPLICE FITTING REMOVED IAW SRM 51-40-02 REV 116. SPLICE FITTING FABRICATED IAW DWG 144N5215 SHT 1 REV & INSTALLED IAW DWG 144N5200 SHT 1 REV B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 749 hrs · 27,303 cycles

EMPENNAGE RT SIDE, THE APU INLET PERIMETER HAS CORROSION ON THE FWD SIDE AT BS 1825, BETWEEN STRINGER 3 & 6. CORROSION REMOVED, FOUND OUT OF LIMIT IAW SRM 53-80-15 FIG 101 TABLE 101 REV 116 & REPAIR CARRIED OUT IAW EA F-5310-T0321253 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SPLICE — CRACKED (BS 1120) · airframe 749 hrs · 27,303 cycles

CABIN STATION 1120 LT, CREASE BEAM INNER CHORD SPLICE FITTING FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 115. AFTER CORROSION REMOVAL & FOUND SPLICE FITTING CRACK THROUGH. SPLICE FITTING REMOVED IAW SRM 51-40-02 REV 115. NEW SPLICE FITTING FABRICATED IAW DWG 144N5215 SHT 1 REV. INSTALLED IAW DWG 144N5200 SHT 1 REV B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 749 hrs · 27,303 cycles

BS 1681, RBL 30 - 49, FLOORBEAM UPPER FLANGE FWD LOWER SURFACE FOUND CORRODED. COMPLIED WITH EA F-5310-T0321782 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

CABIN STATION 1080 LT CREASE BEAM INNER CHORD SPLICE FITTING FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 115. AFTER CORROSION REMOVAL & FOUND SPLICE FITTING CRACKED THROUGH. SPLICE FITTING FABRICATED IAW DWG 144N5215 SHT 1 REV. INSTALLED IAW DWG 144N5200 SHT 1 REV B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

BS 1200, RBL 24.75, SEAT TRACK CROWN CHAFED. REPAIRED IAW EA F-5310-T0321331 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

BS 1540, RBL 24.75, SEAT TRACK CROWN CHAFED. REPAIRED IAW SRM 53-00-52 FIG 201 REPAIR 1 OPTION 1 REV 116. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CHAFED (BS 1555-1575) · airframe 749 hrs · 27,303 cycles

BS 1555 - 1575, RBL 24.75, SEAT TRACK CROWN CHAFED. CHAFE REMOVED IAW SRM 51-10-02 REV 116. REWORKED AREA, AND FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 101 REV 116. SEAT TRACK REMOVED, & FABRICATED IAW DWG 146N5137 SHT 1 REV & INSTALLED IAW DWG 146N5120 SHT 9 REV. REPAIR CLASSIFIED AS MAJOR.

Part: SKIN PANEL — CORRODED (LT WING) · airframe 749 hrs · 27,303 cycles

LEFT WING, AFTER FILL PORT REMOVAL, UPPER SKIN UPPER SURFACE FOUND CORROSION AT OVERWING FILL PORT ADAPTER MATING AREA. LT WING OVERWING FILL PORT CORROSION REPAIRED IAW EA F-5730-T0320974 P 1. REPAIR CLASSIFIED AS MINOR.

Part: SEAT TRACK — CHAFED (BS 1120-1140) · airframe 749 hrs · 27,303 cycles

BS 1120 - 1140, LBL 24.75 SEAT TRACK CROWN FOUND CHAFED. SEAT TRACK REMOVED AND REPLACED IAW DWG 114N5021 SHT 1 REV A AND DWG 144N5001 SHT 3 REV A. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

BS 960 - 970, LBL 24.75 SEAT TRACK CROWN FOUND CHAFED. CHAFED MARK REMOVED IAW SRM 51-10-02 REV 115. REWORKED EVALUATED CLEAN UP DEPTH OF 0.030". FOUND EXCEEDS 0.020" CROWN LIMIT IAW SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE 1 REV 116. SEAT TRACK REPAIR CARRIED OUT, BETWEEN STATION 900 - 980, LBL 24.75 IAW SRM 53-00-52 FIG 201 REPAIR 4 REV 116. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

CABIN STATION 420 - 440, LBL 24.75, SEAT TRACK CROWN FOUND CHAFED. CHAFED MARK REMOVED IAW SRM 51-10-02 REV 115. REWORKED AREA EVALUATED CLEAN UP DEPTH OF 0.038 " ON SEAT TRACK CROWN, FOUND EXCEEDS 0.020 " LIMIT IAW SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE I REV 116. SEAT TRACK REMOVED BETWEEN STATION 377 - 440, LBL 24.75. NEW SEAT TRACK FABRICATED IAW DWG 141N5131 SHT 1 REV A. INSTALLED IAW DWG 141N5130 SHT 1 REV F. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

CABIN STATION 880 - 897, LBL 24.75 SEAT TRACK CROWN FOUND CHAFED. REWORKED AREA EVALUATED CLEAN UP DEPTH OF 0.56" ON SEAT TRACK CROWN LIP EXCEED LIMIT OF 0.48" IAW SRM 53-0-52 FIG 101, ALLOWABLE DAMAGE 1 REV 116. SEAT TRACK CROWN AND SUPPORT REMOVED, BETWEEN STATION 879 - 900, LBL 24.75 IAW SRM 51-40-02 REV 116. SEAT TRACK CROWN FABRICATED IAW DWG 143N5481 SHT 2 REV. SEAT TRACK CROWN & SUPPORT INSTALLED IAW DWG 143N5405 SHT 2 REV. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 749 hrs · 27,303 cycles

CABIN STATION 1018 LT, CREASE BEAM WEB INNER CHORD, VERTICAL FLANGE FOUND CORROSION. COMPLIED WITH EA F-5310-T0321234 PART 1. REPAIR FOR CORROSION FOUND ON LT CREASE BEAM INBD CHORD VERTICAL FLANGE AT STATION 1018. ALTERATION IS CLASSIFIED AS MINOR

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 749 hrs · 27,303 cycles

CABIN STATION 960 - 984, LT CREASE BEAM WEB FOUND CORROSION. REMOVED IAW SRM 51-10-02 REV 115 & FOUND CORROSION THROUGHOUT. CREASE BEAM WEB REMOVED IAW SRM 51-40-02 REV 116. NEW CREASE BEAM WEB INSTALLED IAW DWG 144N5140 SHT 3 REV D REPAIR CLASSIFIED AS MAJOR.

Part: TIE — CRACKED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

COCKPIT STATION 200 - 205, LBL 35 - LBL 38, FLOOR TIE FOUND CRACK. FLOOR TIE REMOVED FROM STA 200 - 205 LBL 26 - LBL 40 AS PER SRM 51-40- 02 REV 116. NEW FLOOR TIE INSTALLED AS PER DWG 141N5810 SHT 1 REV G. REPAIR CLASSIFIED AS MAJOR.

Part: TIE — CRACKED (FUSELAGE) · airframe 749 hrs · 27,303 cycles

COCKPIT STATION 200 - 205, RBL 35 - RBL 38, FLOOR TIE FOUND CRACK. FLOOR TIE AT STA 200 - 205 RBL 26 - RBL 40 REMOVED AS PER SRM 51-40-02 REV 116. NEW FLOOR TIE INSTALLED AS PER DWG 141N5180 SHT 1 REV G. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — DENTED (FUSELAGE) · airframe 74,961 hrs · 27,300 cycles

AFT CARGO FRAME DENTED STATION 1540, STRINGER 26L. CUT OUT DAMAGED SECTION OF INBD FLANGE & FORMED REPAIR ANGLE IAW SRM 53-00-07 REPAIR 5. INSTALLED IAW SRM 53-00-07 REPAIR 5 TABLE II. THIS IS A CAT B REPAIR IN ZONE 1 & REQUIRES SUPPLEMENTAL INSPECTIONS BEGINNING AT 50,000 TOTAL AIRFRAME CYCLES WITH REPEAT INSPECTIONS EVERY 12,000 CYCLES THEREAFTER. AIRPLANE SOLD AS IS ON 09 JUL 2014. BUYER WAS AWARE OF THIS ITEM PRIOR TO SALE BEING FINALIZED.

Part: FRAME — DENTED (FUSELAGE) · airframe 74,961 hrs · 27,300 cycles

AIRCRAFT CARGO FRAME DENTED STATION 1420, STRINGER 27L. CUT OUT DAMAGED AREA OF FRAME INBD FLANGE & FORMED A REPAIR ANGLE IAW SRM 53-00-07 REPAIR 5 & INSTALLED. THIS IS A CAT B REPAIR IN ZONE 3 & REQUIRES SUPPLEMENTAL INSPECTIONS TO BEGIN 12,000 CYCLES AFTER REPAIR INSTALLATION, WITH REPEAT INSPECTIONS EVERY 11,000 CYCLES THEREAFTER. AIRPLANE SOLD AS IS ON 09 JUL 2014. BUYER WAS AWARE OF THIS ITEM PRIOR TO SALE BEING FINALIZED.

Part: FRAME — BENT (FUSELAGE) · airframe 74,961 hrs · 27,300 cycles

AFT CARGO FRAME BENT STATION 1400, STRINGER 26L TO 27L. REPAIR DAMAGE FRAME IAW SRM 53-00-07 REPAIR 5 DETAIL I. THIS REPAIR IS A CAT B REPAIR IN ZONE 3. REQUIRES SUPPLEMENTAL INSPECTIONS STARTING IN 12,000 FLIGHT CYCLES & 11,000 FLIGHT CYCLES THEREAFTER THIS INSPECTION CONSISTS OF BOTH DETAIL VISUAL & NDT. AIRPLANE SOLD AS IS ON 09 JUL 2014 BUYER WAS AWARE OF THIS ITEM PRIOR TO SALE BEING FINALIZED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,961 hrs · 27,300 cycles

MAIN CABIN FLOORBEAM CORRODED AT BS 324 BETWEEN RBL 40R - 64R. REMOVED DAMAGED SECTION OF T CAP. FABRICATED & INSTALLED T CAP SPLICE REPAIR ANGLES & STRAPS IAW REO G16382 REV A & SRM 53-10-08 REPAIR 1 IAW ECRA 5310-05795 THIS IS A CAT B REPAIR. THE THRESHOLD FOR THE INITIAL INSPECTION IS 37,500 PTC. AIRPLANE SOLD AS IS ON 09 JUL 2014. BUYER WAS AWARE OF THIS ITEM PRIOR TO SALE BEING FINALIZED.