N210FE

Part: INDICATOR — SHORTED (FUEL INDICATOR) · airframe 32,842 hrs · 18,824 cycles

DURING CLIMB-OUT OF FL220, NR 2 FUEL ICING LIGHT CAME ON. RAN QRH PROCEDURE, FUEL TEMP WAS 40 DEGREES, RETURNED TO MEMPHIS, DUMPED FUEL AND FUEL ICING LIGHT REMAINED ON THROUGH LANDING, WENT OUT WHILE WAITING TO PARK. FOUND BULB ASSY BENT CAUSING BULB TO SHORT OUT AND COME ON WHEN VIBRATION OCCURRED. RELAMPED WITH NEW BULB PER 727-200 MM SHAKING LIGHT ASSY BEFORE RELAMPING, LIGHT STAYED ON. LIGHT TEST GOOD, NR 2 FUEL HEAT VALVE OPS CHECK GOOD. ALL INDICATIONS FOR FUEL HEAT VALVES OPS CHECK.

Part: SWITCH — FAILED (NR 5 SLAT) · airframe 32,698 hrs · 18,738 cycles

UPON FLAP RETRACTION TO 2 THE NR 5 SLAT REMAINED EXTENDED WITH AMBER LIGHT ON FORWARD LED INDICATOR PANEL. S/O LED INDICATOR PANEL SHOWED NR 5 SLAT EXTENDED. QRH WAS FOLLOWED WITH ALL PROCEDURES COMPLIED WITH. RETURNED TO MEM FOR UNEVENTFUL LANDING. REMOVED AND REPLACED NR 5 SLAT SWITCH (REF 27-82-011-4). OP CHECKED GOOD (REF 27-82-011-4).

Part: FRAME — DAMAGED (BS 348) · airframe 32,621 hrs · 18,660 cycles

FS 348.2 6 INCHES ABOVE UPPER AFT DOOR STOP HAS A DRILL START ON FUSELAGE FRAME FOUND DURING REMOVAL OF COVER TO WORK DOOR STOP FITTING. INSTALLED FABRICATED REPAIR ANGLE REF SRM 51-40-3 VERIFIED MATERIAL 2024 .080 (O), HEAT TREATED ANGLE, FABRICATED VERIFIED MATERIAL FOR CLIP REF BAC1514-518. HEAT TREATED CLIP FORM TRACKING NR 2007-05-125. INSTALLED CLIP REF SRM 51-10-2 REF W/C, 53101127.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 32,621 hrs · 18,660 cycles

AGING A/C INSP, FOUND FRAME REPAIR AT STA 520, STR 16R-17R, DID NOT CONFORM TO SRM 51-40-3 FIG 1. REMOVED AND DISCARDED PREVIOUS REPAIR ANGLES AND INSTALLED NEW REPAIR PARTS REF. ALL WORK ACCOMPLISHED ON WO#36350/N00878.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 32,621 hrs · 18,660 cycles

FOUND ON AGING A/C INSP FOUND EXISTING REPAIR AT STA 760 FRAME DOES NOT CONFORM TO SB 727-53-0197. REMOVED AND DISCARDED EXISTING REPAIR. ACCOMPLISHED HFEC OF DAMAGE. FABRICATED REPAIR PARTS AND INSTALLED, REF FED EX EA 7-5310-113044.

Part: TAB — DELAMINATED (ZONE 600) · airframe 32,621 hrs · 18,660 cycles

RIGHT WING INBD AILERON TAB OTBD AFT AREA HAS 1" AREA OF DELAM REMOVED AND REINSTALLED R/W INBD AILERON TAB REF MM 27-10-011-4 ADJ/CHECK REF MM 27-10-000-5, OPS CHECK GOOD.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 32,621 hrs · 18,660 cycles

CABIN FLOORBEAM HAS CORROSION STA 344 LBL 36" TO 54" REMOVED CORROSION, ORIGINAL MATERIAL .107, REMAINING .086", ROTO PEENED AREA. TREATED AND PRIMED AREA REF 51-10-02, MM 51-20-151 AND SOPM 20-10-03, AND EA NR 7-5310-111639.

Part: STRUCTURE — MISREPAIRED (BS 520) · airframe 32,621 hrs · 18,660 cycles

ON AGING A/C INSPECTION, FOUND EXISTING REPAIR LOCATED AT STA 520, STR 16R-17-R, DID NOT CONFORM TO SRM. REMOVED AND DISCARDED PREVIOUS ANGLES & INSTALLED NEW REPAIR PARTS, EA I070369 ALL WORK ACCOMPLISHED ON WO 36352/N00878.

Part: SKIN — CRACKED (ZONE 600) · airframe 32,621 hrs · 18,660 cycles

RIGHT WING UPPER TE SKIN CRACKED AT NR 12 SPOILER IB CENTER HINGE CUTOUT REMOVED NR 12 SPOILER. REMOVED FASTENERS IN REPAIR AREA. STOP DRILLED CRACK, NDT VERIFY CRACK TERMINATION. FABRICATED REPAIR PLATE, TREATED AND PRIMED. INSTALLED REPAIR, APPLIED FILLET SEAL AND PAINTED REPAIR. INSTALLED NR 12 SPOILER, REF SRM 57-30-4.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 32,621 hrs · 18,660 cycles

LT AFT WING BODY FILLET B HYD SYS SVC BAY FRG FRAME INTERCOSTAL IS CRACKED AT NR 1 EMDP PRESSURE HOSE BHD FITTING CUTOUT OB HYD RESERVOIR BS 950A 5, STR 23L. REMOVED DAMAGED INTERCOSTAL REF SRM 51-30-2 MFG NEW INTERCOSTAL REF DWG 69-14299, AND INSTALLED NEW INTERCOSTAL REF SRM 51-30-2

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 32,621 hrs · 18,660 cycles

AFT PIT, AFT BULKHEAD SUPPORT FRAME IS CORRODED AT FASTENER RECEPTACLE BS 1166, LBL 19-RBL 36, WL 179 REMOVED CORROSION, FOUND 3 AREAS TO BE OUT OF LIMITS, IAW SRM 53-10-1. REMOVED DAMAGED AREA, FABRICATED REPAIR PART OUT OF 7075-T6 .063. FABRICATED FILLERS AND TREATED AND PRIMED, IAW SRM 51-40-4, INSTALLED IAW SRM 51-30-2.

Part: TAB — DELAMINATED (ZONE 600) · airframe 32,621 hrs · 18,660 cycles

RIGHT WING OTBD AILERON TAB HAS A 37" LONG AREA OF DELAM FROM OTBD EDGE. REMOVED AND REPLACED R/W OTBD AILERON TAB REF M/M 27-10-041-4. PERFORMED ADJ/TEST REF MM 27-10-000-5, OPS CHECK GOOD.

Part: SKIN — CRACKED (ZONE 100) · airframe 32,621 hrs · 18,660 cycles

LOWER FUSELAGE VHF NR 2 ANTENNA, SKIN ON FWD LIP DAMAGED, AND BASE PNL FOR ANTENNA IS CRACKED SRM 51-30-2. REMOVED VHF ANTENNA PANEL, REPLACED HAT CHANNEL AND INSTALLED PANEL SRM 51-30-2.

Part: ATTACH FITTING — CRACKED (ZONE 200) · airframe 32,621 hrs · 18,660 cycles

MAIN DECK BODY FRAME INTERCOSTAL ASSY CLIP IS CRACKED BS 351 FWD, STR 15L. REMOVED WEB, REMOVED CLIP, DRILLED AND INSTALLED NEW CLIP, REINSTALLED WEB REF SRM 51-30-2 FIG.

Part: ATTACH FITTING — CRACKED (ZONE 200) · airframe 32,621 hrs · 18,660 cycles

MAIN DECK BODY FRAME INTERCOSTAL ASSY CLIP IS CRACKED BS 348 AFT, STR 15L. REMOVED PANEL FWD OF STR 15L, STA 348, REMOVED DOOR STOP, REF SRM 51-30-2 FIG 1. REMOVED DAMAGE CLIP, NEW CLIP INSTALLED ON N/R N00991 WIP NR 4, DOOR STOP. REINSTALLED ON N/R N00991 WIP, NR 4.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 32,621 hrs · 18,660 cycles

AFT PIT, STA 1166, WL 200, RBL 48, AFT WALL SUPPORT ANGLE, IS CORRODED UPPER AFT CORNER. BLENDED CORROSION AND FOUND ANGLE TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW ANGLE, REF SRM 51-30-2 PG 1-4, AND BOEING DWG NR 65-67251.

Part: SKIN — CRACKED (ZONE 600) · airframe 32,621 hrs · 18,660 cycles

RT WING, UPPER WING SKIN CRACKS AT NR 12 I/B HINGE CUT OUT. STOP DRILLED CRACK, NDT VERIFIED CRACK TERMINATION, FABRICATED AND INSTALLED REPAIR DOUBLER REF SRM 57-30-4.

Part: SUPPORT ANGLE — CRACKED (ZONE 500) · airframe 32,621 hrs · 18,660 cycles

LT WING T/E ANGLE SUPPORT FOR JACKSCREW MOST OUTBD FAIRING IS CRACKED FROM FASTENER HOLE (INBD ANGLE). REPLACED WITH NEW DOUBLER REF 51-30-5 AND SRM 51-30-2.

Part: DEFLECTOR — CRACKED (ZONE 600) · airframe 32,621 hrs · 18,660 cycles

PNL RACK RT WING TO BODY RT WING TO BODY PLN UPPER SURFACE HAS A CRACKED BRACKET. PAINTED AND INSTALLED NEW PARTS, REF SRM 51-30-023 PG 1.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 32,621 hrs · 18,660 cycles

AT LWR CARGO BAY, BS 1137-1140, RBL 61-62, WL 208, FLOOR SUPPORT CHANNEL I/B FLANGE LOWER SURFACE IS CORRODED. REMOVED SEAT TRACK REF SRM 51-30-02. REMOVED SIDEWALL PANEL, REMOVED SEAT TRACK SUPPORT CHANNEL. FABRICATED NEW PARTS, TREATED, PRIMED AND PAINTED. INSTALLED NEW PARTS REF SRM 51-30-02.

Part: FLAP TRACK — WORN (ZONE 500) · airframe 32,621 hrs · 18,660 cycles

LT WING TE IB FLAP OB TRACK UPP OB FLG WEAR STEP HAS GOUGES/ HIGH METAL 5" - 32" FROM AFT END. LT WING INBD T/E FLAP OUTBD (NR 3) FLAP TRACK REPLACED ON W/C 27X5705-03.

Part: PANEL — DAMAGED (ZONE 300) · airframe 32,621 hrs · 18,660 cycles

RT LOWER I/B PNL NR 9214 IS DAMAGED ON HORIZ STAB. REPAIRED RT HORIZONTAL STAB PANEL NR 9214 REF SRM 55-20-3 FIG 1 AND SRM 55-10-2 PG 1, FIG 1, SHT 1.

Part: ATTACH ANGLE — CRACKED (NR 3 SPOILER) · airframe 32,621 hrs · 18,660 cycles

LT WING, LWR TE PANEL BELOW NR 3 SPOILER PANEL, INBD SET OF ATTACH ANGLES FOR PANEL SUPPORT ROD OTBD ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE REFERENCING SRM 51-30-2.

Part: SUPPORT ANGLE — CRACKED (ZONE 600) · airframe 32,621 hrs · 18,660 cycles

RT WING OB TE LWR SURFACE PANEL SUPPORT ANGLE CRACKED, 4" FWD OF TE, BELOW OB HINGE OF NR 12 SPOILER REPLACED PANEL SUPPORT ANGLE REF SRM 51-30-02 PAGE 19.

Part: FRAME — DENTED (BS 1130) · airframe 32,621 hrs · 18,660 cycles

AFT PIT STA 1130, LBL 25, STR. 26, FRAME IS DENTED CUT OUT DAMAGE, FABRICATED REPAIR ANGLE FROM 7075-0 .063 AND HEAT TREATED TO 7075-T-6 INSTALLED REPAIR ANGLE REF SRM 51-40-03.

Part: SPAR — CRACKED (RT STAB) · airframe 32,621 hrs · 18,660 cycles

RT STAB AFT SPAR 3RD BALANCE BAY FROM O/B END, HINGE PANEL FWD ATTACH BRACKET CRACKED AT I/B END REPLACED CHANNEL AND WEB REF SRM 51-30-3 PG 5.

Part: FLAP TRACK — CORRODED (ZONE 600) · corrosion level 2 · airframe 32,621 hrs · 18,660 cycles

RT WING TOP SIDE OF I/B FLAP O/B FLAP TRACK AT MOUNT HOLE IS CORRODED RT I/B FLAP TRACK (NR 6) REPLACED. NEW TRACK INSTALLED ON W/C 27X5708-03.

Part: FRAME — DENTED (ZONE 100) · airframe 32,621 hrs · 18,660 cycles

AFT CARGO PIT RT SIDE STA 1050 STR 25R FRAME IS DENTED DETERMINED DENT TO BE OUT OF LIMITS, PER SRM 53-10-01. FABRICATED REPAIR PARTS, TREATED AND PRIMED AND INSTALLED REF SRM 51-40-3 FIG 1, SRM 51-30-02.

Part: TEE FITTING — CRACKED (CARGO DOOR) · airframe 32,621 hrs · 18,660 cycles

MAIN UPPER CARGO DOOR S/N 9, TEE SUPPORT FITTING CRACKED AT LATCH HOOK 3RD FWD FROM AFT EDGE BY TORQUE TUBE BEARING FITTING. REMOVED AND REPLACED DAMAGED T- FITTING WITH NEW TEE CLIP FX797 IAE SRM 51-30-2.

Part: BRACKET — CRACKED (LT WING) · airframe 32,621 hrs · 18,660 cycles

LT WING TRAILING EDGE SMALL U SHAPE BRACKET FOR SUPPORT OF OUTBD TRACK FAIRING, IS CRACKED AT THE SERRATIONS INBD FLANGE REMOVED CLIP REF SRM 51-30-02 FIG.7 PG.32 INSTALLED NEW CLIP REF. SRM 51-30-02 PG 2

Part: SEAL DEPRESSOR — GOUGED (CARGO DOOR FRAME) · airframe 32,621 hrs · 18,660 cycles

FUSE LWR LOBE AFT CARGO DR FRAME INTERIOR SURFACE IS GOUGED AT LOWER AFT CORNER, BS 989, STR 26R. REMOVED AND INSTALLED NEW LOWER AFT CORNER, OF AFT CARGO PIT DOOR REF SRM 51-30-2 PG 1-12 (SEAL DEPRESSOR).

Part: FLAP TRACK — CORRODED (ZONE 500) · corrosion level 2 · airframe 32,621 hrs · 18,660 cycles

LT WING TE IB FLAP OB TRACK IS CORRODED AT FWD END AND SPOILER SPPT ATTACH POINT LT WING INBD T/E FLAP OUTBD (NR3) FLAP TRACK REPLACED ON FED EX W/C 27X5705-03.

Part: FRAME — DENTED (BS 720) · airframe 32,621 hrs · 18,660 cycles

FWD PIT FRAME, STA 720 DENTED BETWEEN STRINGER 23-24R REMOVED DAMAGE SECTION OF FRAME REF SRM 53-10-4 FIG 1. FABRICATED REPAIR PARTS REF SRM 53-10-4 FIG 1. DRILLED REPAIR PARTS REF 51-10-4, AND INSTALLED NEW REPAIR PARTS REF SRM 53-10-4 FIG 1.

Part: FRAME — CORRODED (TORQUE BOX) · corrosion level 2 · airframe 32,621 hrs · 18,660 cycles

FUSELAGE LOWER LOBE NH NOSE TUNNEL TORQUE BOX INTERIOR HORIZ WEB IB CHORD IS CORRODED/EXFOILATION, BS 295-301, LBL 15, WL168 BLENDED AND REMOVED CORROSION .018 MATERIAL LOSS, WITHIN LIMITS, APPLIED ALODINE AND PRIMER REF SRM 51-10-1 AND SRM 51-10-2, SRM 53-10-1 PG 1.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 32,621 hrs · 18,660 cycles

MAIN DECK BODY FRAME INTERCOSTAL ASSY CLIP IS CRACKED BS 351, STR 15L REMOVED AND REPLACED CLIP. REF SRM 51-30-2 PG 1-3 AND 5-7.

Part: STIFFENER — CRACKED (ZONE 300) · airframe 32,621 hrs · 18,660 cycles

ANGLE CRACKED ON THE VERTICAL STAB LEADING EDGE WEB LOCATED ON THE UPPER RIGHT ON THE AFT SIDE OF WEB AND THE UPPER STAB BULKHEAD REMOVED AND REPLACED STIFFENER ANGLE ON VERTICAL STAB. REFERENCE SRM 51-30-02, PG 3.

Part: HINGE — CRACKED (NR 4 SPOILER) · airframe 32,621 hrs · 18,660 cycles

UPPER WING CUT OUT FOR NR 4 SPOILER HINGE HAS TWO SMALL CRACKS, LOCATION OF HINGE IS SECOND HINGE INBOARD FROM OUTBOARD END OF SPOILER STOPPED DRILLED ENDS OF CRACKS AND INSTALLED DOUBLER. REF SRM 57-30-4, FIGURE NR 10, PAGES 27-31.

Part: FLAP TRACK — CORRODED (ZONE 500) · corrosion level 2 · airframe 32,621 hrs · 18,660 cycles

LEFT WING TE OB FLAP OB TRACK IS CORRODED AT AFT ATTACH POINT. TRACK ASSEMBLY REPLACED ON FED EX W/C 27X5707-01 REF MM 27-51-031-4.

Part: RIB — GOUGED (NR 7 SPOILER) · airframe 32,621 hrs · 18,660 cycles

NR 7 SPOILER INBOARD DOWN STOP BRACKET HAS LOOSE LOWER BOLT AND BRACKET IS GOUGED AT ATTACH BOLT BLENDED DAMAGED AREA, NDT FOR MATERIAL LOSS. ORIGINAL THICKNESS.215", MATERIAL REMAINING IS .081 REF SRM 57-20-1 FIG 2. FOUND TO BE OUT OF LIMITS, REF SRM 57-20-1 FIG 2. REMOVED AND REPLACED DOWN STOP BRACKET REF SRM 51-30-2 PG 2.

Part: SKIN — DELAMINATED (ZONE 600) · airframe 32,621 hrs · 18,660 cycles

RT FOREFLAP I/B END LOWER SURFACE AND EDGE ARE DELAMINATED REPAIRED DELAMINATION ON I/B END LOWER SURFACE OF FOREFLAP REF SRM51-40-20. TAP TEST GOOD, PRIMED AND PAINTED REPAIR AREA REF M/M 51-40-20-151-7 COOK TICKET ATTACHED.

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 32,621 hrs · 18,660 cycles

FOUND ON AGING A/C INSP AFT LOWER CARGO DOOR SKIN REPAIR ON AFT LWR CORNER DID NOT CONFORM TO CURRENT SRM 52-00-3 FIG 3. REMOVED EXISTING DOUBLER INSTALLED NEW EXTERNAL DOUBLER REPAIR REF SRM. 52-00-3 FIG 3.

Part: WEB — CRACKED (ZONE 300) · airframe 32,621 hrs · 18,660 cycles

VERTICAL STAB ELEVATOR FEEL CONTROL UNIT PLATFORM ASSY FWD LT VERTICAL WEB CRACKED ON INTERNAL SIDE AT THE 2 MOST FWD LWR FASTENERS. REPLACED LT VERTICAL WEB ON VERT STAB ELEVATOR FEEL CONTROL UNIT PLATFORM. REF SRM 51-30-2 PG 1-12.

Part: KEELBEAM — CORRODED (BS 950A S29L) · corrosion level 2 · airframe 32,621 hrs · 18,660 cycles

AFT PIT BILGE KEEL BEAM OB FLANGE IS CORRODED BS 950A 2, STR 29L, WL139. ACCOMPLISHED REPAIR OF KEEL BEAM CHORD OB FLG BD 950A 2, STR 29, REF FED EX EO NR 7-5310-7-2356 CARD 6 PG 2 FIG 3 NOTE 1.

Part: SKIN — CRACKED (NR 4 SPOILER) · airframe 32,621 hrs · 18,660 cycles

FOUND UPPER WING CUTOUT FOR NR 4 SPOILER HINGE HAS TWO SMALL CRACKS, LOCATION OF HINGE IS SECOND HINGE INBOARD END OF SPOILER. STOPPED DRILLED ENDS OF CRACK AND INSTALLED DOUBLER REF SRM 57-30-4/ FIGURE NR 10 PAGES 27-31.

Part: WEB — CRACKED (ZONE 400) · airframe 32,621 hrs · 18,660 cycles

VERTICAL STAB ELEVATOR FEEL CONTROL UNIT PLATFORM ASSY FWD RT VERTICAL WEB CRACKED ON INTERNAL SIDE AT THE TWO MOST FWD LWR FASTENERS. REMOVED RT VERTICAL WEB, PICKED UP HOLES IN NEW WEB, INSTALLED RIVETS AND HILOCKS IN NEW WEB, REF SRM 51-30-2.

Part: PRESSURE PANEL — CORRODED (BS 931-932) · corrosion level 2 · airframe 32,621 hrs · 18,660 cycles

LT W/W PRESSURE DECK LOWER SURFACE HAS SURFACE CORROSION AT WL 208, BS 931- 932, LBL 5"-7". REPAIRED LT W/W PRESSURE DECK LOWER SURFACE AT WL 208, BS 931-932, LBL 5"-7" IAW SRM 51-10-6 PAGE 12 AND IAW SRM 51-10-2

Part: FRAME — CRACKED (ZONE 200) · airframe 32,621 hrs · 18,660 cycles

MAIN DECK BODY FRAME IB CHORD IS CRACKED AT BS 930, STR 13R-14R. REPAIRED 2 FRAME BS 930 PER SRM 53-10-4 FIG 1.

Part: STOP FITTING — CRACKED (DOOR FRAME) · airframe 32,621 hrs · 18,660 cycles

MAIN DECK RT AFT OVER WING DOOR CUTOUT HAS 1 EA STOP PAD CRACKED AT FWD UPP POS BS 825 REMOVED AND REPLACED STOP PAD REF. 52-20-002-8 PG.1

Part: STOP FITTING — CRACKED (DOR FRAME) · airframe 32,621 hrs · 18,660 cycles

MAIN DECK RT RWD OVER WING DOOR CUTOUT HAS 4 EA CRACKED STOP PADS AT THE FOLLOWING POS: FWD UPP, AFT UPP, AFT MID, LWR BS 760-783. REMOVED AND REPLACED STOP PADS (4 EA) REF MM 52-20-002-8 PG1.

Part: SKIN — WORN (BS 720D S19L) · airframe 32,621 hrs · 18,660 cycles

AGING A/C INSPECTION FOUND EXISTING FLUSH REPAIR BETWEEN STA 720D-720E AT STR 19L, ON LAP SPLICE. REPAIR HAS ADDITIONAL WEAR ON THE FILLER. REMOVED WORN FILLER, FABRICATED FILLER AND INSTALLED REF SRM 53-30-3 FIG 14.

Part: SKIN — WORN (ZONE 100) · airframe 32,621 hrs · 18,660 cycles

AGING A/C INSPECTION FOUND EXISTING FLUSH REPAIR BETWEEN STA 720D-720E AT STR 19R ON LAP SPLICE. REPAIR HAD ADDITIONAL WEAR ON THE FILLER. REMOVED WORN FILLER, FABRICATED FILLER AND INSTALLED. REF SRM 53-30-3 FIG 14.

Part: BRACKET — CRACKED (RT WING) · airframe 32,621 hrs · 18,660 cycles

RT WING'S LOWER TRAILING EDGE PANELS OUTBD STRUT MOUNT BRACKET IS CRACKED BY NR 7 TRANSMISSION REMOVED AND REPLACED RT WING LOWER EDGE PANEL MOUNT BRACKET SRM 51-30-2 PG 1.

Part: FLOORBOARD — PUNCTURED (CARGO BAY) · airframe 32,621 hrs · 18,660 cycles

AFT LOWER CARGO PIT 1ST OR FWD FLOORBOARD HAS MANY PUNCTURES FABRICATED NEW PANEL REF 51-30-5. ALODINED AND PRIMED BOTTOM SIDE OF PANEL REF MM 51-20-021-7 AND MM 51-20-031-7.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 32,621 hrs · 18,660 cycles

FOUND EXISTING EXTERNAL REPAIR APPROX STA 1050 AT STR 20L. DID NOT CONFORM TO CURRENT SRM 53-30-3 ON AGING A/C INSPECTION. REMOVED EXTERNAL REPAIR, FABRICATED STRUCTURAL FILLER AND REPAIR DOUBLER AND INSTALLED REF SRM 53-30-3 FIG 5, PAGES 20-23

Part: DOOR — MISREPAIRED (ZONE 800) · airframe 32,621 hrs · 18,660 cycles

FWD CARGO DOOR AT 6'' FROM AFT EDGE AND 11'' FROM FROM BOTTOM EDGE. REPAIR DID NOT CONFORM TO CURRENT SRM 52-00-3, FOUND DURING AGING A/C INSPECTION REMOVED EXISTING REPAIR ON LOWER SKIN OF FWD CARGO DOOR 6'' FROM AFT AND 11''FROM BOTTOM EDGE. FABRICATED AND INSTALLED DOUBLER REF SRM 52-00-3 FIG 4.

Part: TRANSMITTER — FAILED (NR 1 ENGINE) · airframe 32,103 hrs · 18,341 cycles

NR 1 EPR WOULD NOT ADVANCE WHEN PUSHING THROTTLE UP FOR TAKEOFF. TROUBLE SHOT PER MTSI WRI 77-10/0562 AND PER B727-200 AMM CH 77-11-001-1. REMOVED AND REPLACED NR 1 ENGINE EPR TRANSMITTER. RAN PER B727-200 JRH. CHECKS GOOD. ALSO, SEE WRI 77-10/0565. A/C OK FOR SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 29,648 hrs · 16,821 cycles

RIGHT MAIN LANDING GEAR WHEEL WELL AFT BULKHEAD UPPER OUTBOARD HORZ SUPPORT ANGLE IS CRACKED. *S/D* REMOVED & REPLACED DAMAGED ANGLE IAW SRM 51-10-1 & SRM 51-30-2. NEW ANGLE FABRICATED ON MAE TRAVELER T5/486632.

Part: LINE — MISALIGNED (PITOT/STATIC SYS) · airframe 29,479 hrs · 16,723 cycles

F/O'S A/S AND ALT LAG BEHIND CAPT'S. CAPT'S A/S AND ALT MATCH W/ STBY. ENT BY: 220542 FACT 05DEC04 08:44 MEM T/S AND FOUND SPARE STATIC FLEX LINE QUICK DISC BEHIND F/O'S INST PNL LEAKING. LINE IS LOOSE AND NOT CONNECTED TO ANY INSTRS. THE QUICK DISC WAS MISALIGNED, REF IPC 34-10-00 62A ITEM 15. EA TO CAP AND STOW THE PITOT AND STATIC LINES WHICH USED TO RUN TO THE MACH AIRSPEED IND ON THE F/O'S SIDE. C/W EA 7-3410- 84482. VERIFIED NO UNCONNECTED LINES ON THE CAPTS SIDE. PERFORMED A FULL RANGE PITOT STATIC LEAK TEST TO 22,500 FEET LEFT AT ALT FOR 20 MINUTES NO LEAKAGE NOTED. A/S WAS 350 KTS, REF B727-200 AMM 34-11-000-5. CK F/O'S INST'S ALL OK.

Part: CONNECTOR — FAILED (NR 2 ENGINE) · airframe 26,831 hrs · 15,259 cycles

ON SHORT FINAL APPROACH TO MEM. NR2 ENGINE FIRE WARNING LIGHT ILLUMINATED AND FIRE BELL SOUNDED. NO INDICATION IN COCKPIT OTHER THAN LIGHT AND BELL. FOUND PIN A AND PIN E OF PLUG D352J SHORTING TOGETHER INTERMITTENTLY. REPLACED D352J IAW MFG STANDARD MAINTENANCE PRACTICES (SMP). CONNECTOR INSTALLED, SECURED, SAFETIED. OPS CHECKED NR2 ENG FIRE DETECTION I/A/W M/M CHAPTER 26-11-001-5 PAGE 1/2 OPS CHECKED NORMAL AT THIS TIME.

Part: WARNING LIGHT — ILLUMINATED (NR 2 ENG FIRE) · airframe 26,798 hrs · 15,228 cycles

FIRE WARNING BELL SOUNDED AND GLARE SHIELD FIRE WARNING LIGHT ILLUMINATED MOMENTARILY WHILE ADDING POWER IN A CLIMB FROM FL 290, ABOUT 1.7 EPR, HAPPENED AGAIN 10 MIN LATER AT FL 310, ABOUT 2.0 EPR, TO QUICK TO DETERMINE WHICH ENGINE.

Part: FIRE DETECTOR — MALFUNCTIONED (NR 2 ENGINE) · airframe 26,792 hrs · 15,225 cycles

RETARDED THROTTLES AT 13000 FT AND EXPERIENCED FIRE WARNING BELL, AND LIGHT ON NR 2 TEE HANDLE. NO OTHER ASSOCIATED INDICATIONS. LIGHT WENT OUT SHORTLY AFTER. RETURNED TO GTF AND LIGHT AND HORN CAME ON TWICE MORE DURING RETURN. R/R BOTH SENSING ELEMENTS ON NR 2 ENGINE PER FEDEX 727-200 M/M 26-11-012-4. ALSO R/R'D ENGINE FIRE DETECTION UNIT PER FEDEX 727-200 M/M 26-11-000-4. RAN #2 ENGINE PER FEDEX B727 CHAP.5. SYSTEM OPS CHECKS GOOD ON GROUND.

Part: SKIN — CHAFED (FUSELAGE) · airframe 26,283 hrs · 14,942 cycles

SKIN CHAFED AT BS 720D+12 AT STR 19L. R&R SKIN PER SRM 53-30-3 FIG 14.

Part: SKIN — CHAFED (FUSELAGE) · airframe 26,283 hrs · 14,942 cycles

SKIN CHAFED AT BS 720D+12 AT STR 19R. R&R SKIN PER SRM 53-30-03.

Part: FRAME — CORRODED (FUSELAGE) · airframe 26,283 hrs · 14,942 cycles

CORROSION ON BS 720E FRAME FWD SIDE STR 7L. R&R FRAME PER SRM 53-10-01 & EA 7-5310-67028 & SRM 53-10-14 FIG 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,283 hrs · 14,942 cycles

CORROSION ON UPR CHORD FLOORBEAM AT BS 344, LBL 3, WL 208.

Part: GASPER FAN — OVERHEATED (CABIN) · airframe 25,651 hrs · 14,606 cycles

IN RANGE TO LAS DETECTED A SLIGHT SMELL LIKE OVERHEATED EQUIPMENT. SMELL SEEMED TO DISSIPATE AFTER LANDING. RELEASED FOR SERVICE PER MEL/CDL. GASPER FAN INOP. REMOVED AND REPLACED GASPER FAN PER MM 21-23-011-4, OPS CHECK NORMAL.

Part: ADC — FAILED (E/E BAY)

NR 1 ADC FAILED DURING CLIMBOUT. REMOVED AND REPLACED NR 1 ADC PER MM 34-12-011-4.

Part: CONTROL UNIT — FAILED (ANTI-SKID SYS)

CAPT AND 1ST OFF LEFT BRAKE NOT FUNCTIONING. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT PER MM 32-42-061.

Part: ADC — FAULTY (E/E BAY)

ON ROTATION AIR DATA COMPUTER NR 2 C/B POPPED SEVERAL TIMES. REMOVED AND REPLACED CADC PER MM 34-12-011-4.

Part: BRAKE — OVERHEATED (MLG)

NR 3 MAIN WHEEL AND BRAKE HOT AND LONG ROLL OUT. REMOVED AND REPLACED NR 2 MAIN TIRE AND BRAKE PER MM 32-45-01 & 32-41-032-4.

Part: LIGHT — INOPERATIVE (COCKPIT)

RIGHT AND LEFT MLG IND LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT BULBS PER MAINT PRACT. OPS CK GOOD.

Part: LINE — CHAFED (B HYD SYST)

99-104 - LOST 'B' SYS HYD FLUID AND PRESS ON TAXI IN. A/C TOWED IN. INSTALLED NEW HYD PRESS LINE FROM NR 1 B PUMP TO B: MODULE PER 727-200 STANDARD MM 12-12-000. OPERATIONAL AND LEAK CK GOOD.

Part: PANEL — MISSING (HYD SERVICE)

98-0142, PANEL MISSING FOR HYDRAULIC SYSTEM B. INSTALLED MISSING HYDRAULIC ACCESS PANEL AND HARDWARE, OPERATIONAL CHECK GOOD.

Part: DOUBLER — DAMAGED (BS 540)

UPPER LOBE BS 540, RBL 66 FRAME DAMAGED APPROX 5 ABOVE FLOOR. INSTALLED DOUBLER PER SRM 51-40-3.

Part: DOUBLER — DAMAGED (PAX DOORWAY)

FWD ENTRY DOOR CUTOUT LOWER HINGE CUTOUT HAS BEEN CUTOUT BEYOND FUSELAGE SKIN AND DEEP INTO BEAR STRAP AT FWD SECTION OF HINGE CUTOUT. INSTALLED LOWER HINGE CUTOUT DOUBLER PER S/B 727-53-0198 REV 1 AND EA 7-5330-29333.

Part: DOUBLER — DAMAGED (BS 600)

UPPER LOBE, BS 600, RBL 66, FRAME DAMAGED APPROXIMATELY 5 ABOVE FLOOR. INSTALLED DOUBLER PER SRM 51-40-3.

Part: DOUBLER — DAMAGED (BS 520)

UPPER LOBE, BS 520, RBL 66 FRAME DAMAGED APPROX 5 ABOVE FLOOR. INSTALLED DOUBLER PER SRM 51-40-3.

Part: DOUBLER — DAMAGED (BS 500)

UPPER LOBE, BS 500, RBL 66 FRAME DAMAGED APPROX 5 ABOVE FLOOR. INSTALLED DOUBLER PER SRM 51-40-3.

Part: DOUBLER — DAMAGED (PAX DOORWAY)

FWD ENTRY DOOR CUTOUT UPPER HINGE AREA HAS BEEN CUTOUT PAST FUSELAGE SKIN AND DEEP INTO BEAR STRAP AT FWD SECTION OF HINGE CUTOUT. INSTALL UPPER HINGE CUTOUT DOUBLER PER S/B 727-53-0198 REV 1 AND EA 7-5330-29333.

Part: CONTROL UNIT — MALFUNCTIONED (E/E COMP)

98-0001 FIRE WARNING LIGHTS AND BELL ON FOR 1 SECOND AT CRUISE, (ON FORWARD INSTRUMENT PANEL) NO FURTHER INDICATIONS. ENGINE INSTRUMENTS ALL NORMAL. FOUND PIN PUSHED BACK IN FIRE DETECTOR CONTROL UNIT REMOVED AND REPLACED UNIT OPERATIONAL CHECKED GOOD.

Part: WIRE — LOOSE (NR 2 ENGINE)

ENGINE NR 2 FIRE WARNING LIGHT AND BELL ILLUMINATED AND SOUNDED PERIODICALLY AT BEGINNING OF DESCENT - IDLE POWER SETTING. LIGHT AND BELL COULD BE CANCELED. ENGINE OPERATION WAS NORMAL. INSPECTED ALL DUCTING OK. SECURED LOOSE WIRING AND BRACKETS AT VARIOUS POINTS AND CHECKS OK.

Part: CLAMP — LOOSE (NR 1 STRUT)

ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT DURING CLIMBOUT AT 15,000 MSL. FOLLOWED APPROPRIATE CHECK LIST AND LIGHT WENT OUT CONTINUED TO GEG. TIGHTENED LEAKING CLAMPS BOTH SIDES OF MODULATING SHUTOFF VALVE IN NR 1 ENGINE STUB WING TO STOP LEAKS NEAR SENSING ELEMENT.

Part: OVERHEAT UNIT — MALFUNCTIONED (NR 1 ENG STRUT)

DISCREPANCY: ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED WHEN NR 1 THROTTLE WAS RETARDED, LIGHT WENT OUT. FINISHED CHECK LIST RESULTING IN RIGHT PACK AND NR 3 BLEED ONLY USABLE. CORRECTIVE ACTION: RAN ENGINE NR 1 AT IDLE POWER, CHECKED PYLON AREA FOR ANY LEAKS, NONE FOUND. VISUALLY CHECKED TEMPERATURE SENSOR ALL SEEMS OK. REINSTALLED PROPERLY. REPLACED FIRE OVERHEAT DETECTOR ACCESSORY UNIT FOR PRECAUTION/TROUBLESHOOTING. TESTED OK FOR SERVICE PER MM 26-14-0. INSTALLED STUB WING PANEL.

Part: VALVE — LOOSE (NR 1 ENGINE)

ENGINE NR 1 STRUT OVERHEAT ILLUMINATED. WHEN NR 1 BLEED WAS CLOSED, LIGHT WENT OUT, FINISHED CHECKLIST RESULTING IN RIGHT PACK AND NR 3 BLEED ONLY USABLE. FOUND SENSE LINE ON NR 1 ENGINE BLEED AIR SHUTOFF VALVE LOOSE, (B-NUT WAS BACKED OFF). TIGHTENED SENSE LINE, RAN ENGINE ON GROUND. NO BLEED LEAKS NOTED. OK FOR SERVICE.