N13512

CESSNA 172M No injuries Part 91 — operator not named in the NTSB record

ATA 3350

Part: LIGHT — INOPERATIVE (CABIN)

ACY - FLT 391 - EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSY. OPS CHECK GOOD IAW DC9 MM 33-53-00. (M)

ATA 3350

Part: BATTERY PACK — DISCHARGED (LT NACELLE)

MYR - FLT 619 - LEFT EMERGENCY NACELLE FLOOD LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT EMERGENCY NACELLE FLOOR LIGHTS BATTERY PACK IAW MM CHAPTER 33-50-00, OPERATIONAL CHECK GOOD. (X)

ATA 3350

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY EXIT)

MLB - FORWARD OVERWING EXIT EMERGENCY LIGHTS WILL NOT GO OFF AFTER TEST. THEN WOULD NOT TEST AFTER CYCLING C/B. REPLACED FORWARD OVERWING EXIT EMERGENCY LIGHT, POWER SUPPLY. OPERATION CHECKS GOOD IAW DC-9 MM 33-51. (M)

ATA 5321

Part: FLOOR — CORRODED (BS 140)

MHV - STATION 140X=PLUS 35 TO PLUS 52, 9 BY 18 INCH AREA OF CORROSION DEEP POTTING .5 INCH PUNCTURE AND SURFACE CORROSION NUMEROUS AREAS TOP SURFACE COCKPIT FLOORBOARD. REMOVED CORRODED WEB FROM LOCATION REMOVING ALL ATTACH FASTENERS FABRICATED NEW FLOOR WEB WITH 7075-T6.025 MATERIAL REINSTALLED HAT CHANNELS WITH RIVETS ALODINE AND PRIMERED PER SRM 51-10-3 PAGE 16, PAGE 15 21E, 53-21-0 PAGE 4B, 4 4C, 51-20-0 PAGE 1, 51-30-2 PAGE 1. (M)

ATA 5753

Part: SKIN — DELAMINATED (LT TE FLAP)

MHV - LEFT WING FLAP LEADING EDGE INBOARD P/N 5913560-455 HAS DELAMINATION AND SURFACE CORROSION PART LOATED ON RACK. REMOVED FLAP CAP ASSY FOR FURTHER INSPECTION. FOUND TO BE OUT OF LIMITS. CAP ASSY REPLACED WITH NEW PART, BACK DRILLED SEALED AND INSTALLED NEW CAP ASSY PER DC0 SRM 51-10-4 AND SRM 51-30 DC9 SRM 57-00 AND SRM 27-00. SEALED CAP ASSY, INSTALLED FIXED FLAP VANE DC9 MM 27-51-3. (M)

ATA 5320

Part: WEB — CORRODED (BS 218)

MHV - REF8 W245 FLOOR WEB LBL 61-64 STATION 218 HAS CORROSION BEYOND LIMITS. MANUFACTURED REPLACEMENT PANEL REF TO DC9 SRM 51-10-2 PAGE 2 PAR 2 SOLUTION HEAT TREATED THEN AGE HARDENED PER AMS-H-6088 AND ISSUED TO AIRCRAFT FOR FIT AND LOCATION ON W/O A066-C03-W245. (M)

ATA 5320

Part: WEB — CRACKED (BS 225)

FLOOR WEB IS CRACKED AT FS 225 LBL 26 INSIDE MAIN CABIN 2ND CRACK AT FS 225 LBL 45. REMOVED DAMAGED CRACKED WEB PER DC9 SRM AND REPLACED WITH NEW WEB LOCATED AND DRILLED ALODINE AND PRIMED PER DC9 SRM 53-05 PAGE 1 27, 53-01 PAGE 2 53-21 PAG 6V 53-10-3 PAGE 16 (23) PAGE 18 (30). (M)

ATA 5720

Part: TRAP FITTING — DEFECTIVE (LT WING)

MHV - ULTRASONIC INPECTION SHOWS AN INDICATION OF A DEFECT ON THE INBOARD SIDE OF THE INBOARD VETICAL BOLT ON THE LEFT REAR SPAR TO TRAPEZOIDAL FITTING. REPLACED TRAP FITTING PER S/B NR 57-129 JACKED AND SHORED A/C. REMOVED AND REPLACED AILERON CABLE MIXER FITTINGS RIGGED AILERON BUS CABLE AILERON LATERIAL CONTROL MIXER AND TRIM TAB PER MM DC9 27-10-0 PAGE 17, 9, 10, 12, 13. (M)

ATA 3350

Part: BATTERY PACK — DISCHARGED (CABIN)

DTW - OVERWING EMERGENCY EXIT LIGHTS (UPPER ONE'S) INOPERATIVE. ALL FOUR OF THEM, FORWARD, AFT AND LEFT AND RIGHT. REMOVED AND REPLACED BATTERY PACK PATTERNS AND OPERATION CHECKED IAW DC-9 MM 33-50-0. NO DEFECTS NOTED AT THIS TIME. (M)

ATA 3350

Part: LIGHT — INOPERATIVE (CABIN)

DTW - FORWARD EMERGENCY TRACK LIGHTS OUT. RESECURED FORWARD EMERGENCY TRACK LIGHT IAW MM 33-50. (M)

ATA 3350

Part: BATTERY PACK — DISCHARGED (CABIN)

DTW - FORWARD CABIN EMERGENCY FLOOR LIGHTS OUT. REMOVED AND REPLACED FORWARD EMERGENCY BATTERY PACK. OPERATION CHECK GOOD ON RAMP AT THIS TIME IAW MM 33-50-0. (M)

ATA 5320

Part: WEB — CORRODED (BS 229)

MHV - CABIN FS 229 LBL 52 SEVERE CORROSION EMANATING FROM BETWEEN MEMBRANE WEB AND T-ANGLE. REMOVED AND REPLACED WEB AS REQ PER SRM DC9 51-30-02, 51-30-0 NEW WEB'S AREAS MANUFACTURED ON WORK CARD NR A066B03 WEB ALODINED AND PRIMED IAW DC9 51-10-3. INSTALLED WEB IAW DC9 SRM 51-30-02 AND 51-30-08. (M)

ATA 2612

Part: FIRE HANDLE — WORN (NR 2 ENGINE)

MHV - NR 2 ENGINE FIRE HANDLE SPINS TO LEFT AND RIGHT WHILE PUSHED IN AND DOES'NT CENTER IN DETENT. REMOVED AND REPLACED ENGINE FIRE HANDLE IAW DC9 MM 76-20-1 PAGE 401 PARA 3, OPS CHECK GOOD. (M)

ATA 2612

Part: FIRE HANDLE — OUT OF ADJUST (NR 1 ENGINE)

MHV - NR 1 ENGINE FIRE HANDLE WILL NOT PULL BACK TO STOP REF W/O L150. RIGGED NR 1 FIRE HANDLE SYSTEM PER DC9 MM 76-20-0 PAGE 201-208 ADJUSTED TENSION PER DC9 MM 76-00 PAGE 204 FIG 201. (M)

ATA 2620

Part: FIRE HANDLE — STUCK (NR 2 ENGINE)

MHV - NR 2 ENIGNE FIRE HANDLE WILL NOT TURN TO NR 1 FIRE AGENT. REPOSITIONED FUEL SHUTOFF VALVE LEVER PER MM DC9 76-20-0 PAGE 205. (M)

ATA 5315

Part: FLOORBEAM — CORRODED (LAVATORY)

MHV - TWO FLOORBEAM CORROSION REPAIRS REQUIRE REPLACEMENT TO ACCOMMODATE LAV FLOOR STRUCTURE MODERATE. REMOVED TWO EXISTING REPAIRS FABRICATED REPAIR ANGLE FROM 7075-T6 EXTRUSION NR S415615 CUST ORDER NR 12401 PO 30196 AND FILLERS FROM 7075T6.125 PO 62571 IAW SRM 53-05 FIG 20A ALODINED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED REPAIR WITH PR1422B2 AND HL18PB6 HI-LOCKS DC9 SRM 51-20 AND 51-30-5. (M)

ATA 5312

Part: BULKHEAD ANGLE — DAMAGED (BS 965)

MHV - AFT CABIN LT BULKHEAD STATION 965 WATER LINE AND BULKHEAD TO FLOORBEAM ANGLE HAS GOUGES OUT OF LIMIT. REMOVED AND REPLACED WITH NEW PART FASTENERS INSTALLED PER SRM 51-30-5 RIVETS 51-30-2. (M)

ATA 5321

Part: FLOOR — CRACKED (RT COCKPIT)

MHV - CO-PILOT RUDDER FLOOR PANEL HAS CRACKED STRUCTURE FORWARD END BOTTOM. CUT OUT CRACK INSTALLED ANGLE DOUBLER PER DC9 IAW SRM 53-01-0 PAGE 1 AND 10 EXAMPLED FORMED ANGLE DOUBLER PER DC9 SRM 51-10-2 PAGE 1 FIG 2. INSTALLED FASTENER PER DC9 SRN 51-30-2. (M)

ATA 5320

Part: SUPPORT — CORRODED (BS 220)

MHV - FLOOR SUPPORT AT STATION 220 RBL 48 TO RBL 56 IS SEVERELY CORRODED. REMOVED FLOOR SUPPORT FOR FURTHER INSPECTION FOUND TO BE OUT OF LIMITS PER 51-10-3. FABRICATED NEW SUPPORT PER DC9 SRM 51-10-1 SURFACE TREATMENT AND INSTALLED NEW SUPPORT PER DC9 SRM 51-10-3 AND 51-10-4. (M)

ATA 5320

Part: SKIN — DAMAGED (BS 218)

MHV - FS 218 264 LONGERON 15-18 SKIN REPAIR DAMAGED LEFT SIDE. REPLACED DAMAGED SKIN AND FINGER DOUBLERS PER DWG 53-99034 FAX SURFACED SEAL ALL PARTS PER 51-20-0. INSTALLED FASTENERS WET WITH PR1422-B2. INSTALLED HI-LOCKS PER SRM 51-30-5 AND SOLID RIVETS PER 51-30-2. (M)

ATA 5320

Part: WEB — GOUGED (BS 965)

REF PO88 - GOUGE ON SHEAR WALL WEB .010 DEEP MATERIAL .032 BEYOND LIMITS STATION 965 SBL. REMOVED DAMAGED WEB AND REPLACED WITH NEW 991224-3 WEB INSTALLED FASTENERS PER DC9 SRM 51-30-1 FOR BOLTS 51-30-5 FOR HI-LOCKS 51-30-2 RIVETS. (M)

ATA 5330

Part: SKIN — DAMAGED (BS 218-229)

TEMPORARY SKIN PANEL REPAIR AT STATION 218 TO 229 L-17 TO 18L. REMOVED SKIN AND REPLACED WITH FABRICATED SKIN AND DOUBLERS IAW DC9 SRM 53-04 FIG 47. ALL PARTS WERE FAY SURFACE SEALED AND INSTALLED WITH WET FASTENERS IAW DC9 SRM 53-04 FIG 47 HI-LOCK WERE INSTALLED PER DC9 SRM 51-30-5 SOLID RIVETS WERE INSTALLED PER SRM 51-30-2. (M)

ATA 5330

Part: SKIN — MISREPAIRED (BS 992)

STATION 992 LEFT STRINGER 22-23 THERE IS A CLASS III SKIN REPAIR WITH CHERRY RIVETS INSTALLED ALSO NUMEROUS FASTENERS WITH SHORT CENTER TO CENTER SPACING. REMOVED TEMP REPAIR FABRICATED DOUBLER TRIPLER AND FILLER TRIMMED OUT ADDITIONAL AREA ALODINED AND PRIMED ALL AREAS INSTALLED DOUBLER TRIPLER AND FILLER WET WITH SEAL PER DC9 SRMS 51-10-3, 51-30-5, 51-10-8, 51-10-4, 51-30-2, 51-30-8 AND ENG DRAWING NR 53-990344 REV 1 DATED 3-10-99. (M)

ATA 5311

Part: FRAME — CRACKED (BS 200)

MHV - NO REPAIR FOUND IN THE SRM 53-00 FOR CRACK IN FRAME AT STATION 200 R16. CUT OUT DAMAGED AREA REINSTALLED WEB FABRICATED AND INSTALLED DOUBLER AND TRIPLER BOEING ENGINEERING MSQ NR AVQ-MOJ-99-0005RR AND INSTALLED FASTENERS IAW DC9 SRM 51-30-2, 51-30-5, 51-30-8, REPAIR PARTS WERE FABRICATED IAW DC9 SRM 51-10-2 ALODINED AND PRIMED IAW DC9 SRM 51-10-3. (M)

ATA 5347

Part: SEAT TRACK — CRACKED (BS 420)

MHV - SEAT TRACK RIGHT SIDE OUTBOARD AT STAITON 420 IS CRACKED EXTENDING .250 FROM ONE OF THE TOP SURFACE HOLES. REMOVED AND REPLACED OF SEAT TRACK FROM STATION 350 TO STATION 470 PER SRM 53-05 FIG 4F PAGE 10K. (M)

ATA 5321

Part: FLOOR — CRACKED (BS 200-243)

MHV - FORWARD PASSENGER FLOOR PANEL FOR FS 200-243 LBL 21-42, CORNER CRACKED (TORN). FABRICATED FLOORBOARD IAW DC9 SRM 53-21-0 PAGE 6 INSTALLED STIFFENERS IAW DC9 SRM 51-30-2 PAGE 30. ALODINED AND PRIMED PER IAW DC9 SRM 51-10-3. INSTALLED RIVETS IAW DC9 SRM 51-30-2. (M)

ATA 5320

Part: WEB — CRACKED (BS 211)

MHV - FS 211 R61 WEB AT 1.5 INCH LIGHTNING HOLE IS CRACKED AND HAS CORROSION THATS OUT OF LIMITS PER N/RW25. CUSP HAS BEEN REPLACED PER SRM 53-05-00 FIG 55 FASTENERS INSTALLATION PER SRM 51-30-2 AND SRM 51-30-5. (M)

ATA 5330

Part: SKIN — DAMAGED (BS 293-313)

TEMPORARY REPAIRS ON RIGHT SIDE FUSELAGE AT STATION 293 AND STATION 313. REMOVED TEMPORARY REPAIRS FROM RIGHT SIDE FUSELAGE CUT OUT SECTION OF SKIN AND FABRICATED SKIN SECTION TITANUM DOUBLER AND INSTALLED USING HI-LOCK FASTENER AND SOLID RIVETS IAW ENG DRAWING 53-99034-3 AND CHAPTERS 53-00 51-00 OF THE DC9 SRM. (M)

ATA 5320

Part: WEB — CORRODED (BS 211)

MHV - FS 211 R61 WEB HAS CORROSION AND BULGING AREA UNDER EXISTING REPAIR. REMOVED WEB AND DOUBLER FABRICATED NEW WEB PER DC9 SRM 53-11-1 FIGURE 11 SHEET 1 AND 2 LOCATED AND DRILL HOLE TO EXISTING FASTENER HOLES ALODINED PER DC9 SRM 51-10-3 PAGE 15 (22A) PRIMED PER DC9 SRM 51-10-3 PAGE 16 (24A).

ATA 5347

Part: SEAT TRACK — CORRODED (BS 980)

MHV - AT STATION 980 LBL ONE FASTENER HOLE WAS FOUND TO BE OUT OF LIMITS AFTER CORROSION WAS REMOVED FROM SEAT TRACK REF W/O W195. CUT OUT DAMAGED AREA PER DC9 SRM 53-05 FIG 20A FABRICATED. EXTRUSION FILLER STEEL RUB STRIP TREATED PRIMED AREA PER DC9 SRM 51-10-3. INSTALLED FILLER STEEL RUB STRIP AND EXTRUSION PER DC9 SRM 53-05 FIG 20A AND INSTALLED FASTENERS IAW DC9 SRM 51-30-5. (M)

ATA 5320

Part: WEB — CRACKED (BS 211)

FS 211 R61 WEB AT 1.5 INCH LIGHTNING HOLE FORWARD OF OVAL DUCT IS CRACKED AT RIVET SIDEWALL AREA AFT OF FORWARD GALLEY DOOR. REPAIR OF WEB WILL BE ACCOMPLISHED ON A066C03W258 INSTALLATION OF 2 ANGLE AND OVAL DOCT TO BE INSTALLED ON A066S03 W255. (M)

ATA 5347

Part: SEAT TRACK — CORRODED (BS 200-240)

MHV - FORWARD PASSENGER COMPARTMENT SEAT TRACK FS 200-240 HAS CORROSION AFT CORROSION WAS REMOVED FOUND AREA TO BE OUT OF LIMITS REF W/C 147. REMOVED AND REPLACED SEAT TRACK AS REQUIRED PER SRM 51-30-01 AND MANUFACTURED NEW TRACK IAW DC9 SRM 51-10-02 ALODINED AND PRIMED IAW 51-10-3. INSTALLED NEW TRACK IAW DC9 51-30-5 AND 51-30-1. (M)

ATA 5412

Part: BULKHEAD FRAME — CRACKED (LT PYLON)

MHV - LEFT PYLON BULKHEAD FORWARD FACE BULKHEAD FRAME HAS A 3.5 INCH CRACK BETWEEN STRINGERS 15 AND 16. REMOVED ANGLE AND REPLACED WITH NEW ANGLE 9912243-9 PO NR 8125801 PER DC9 SRM 51-30-2 FOR RIVETS 51-30-5 FOR HI-LOCKS. (M)

ATA 5321

Part: FLOOR — CRACKED (BS 617)

MHV - FS 617 RBL 50 RIGHT SIDE FLOOR CHIME PLATE CRACKED ON BOTH SIDES OF LIGHTENING HOLE. REMOVED AND REPLACED FLOOR CHIME PLATE IAW SRM 51-00 AND 51-30-02 JOB COMPLETE. (M)

ATA 5522

Part: SKIN — LIGHTNING STRIKE (RT ELEVATOR)

MHV - RIGHT ELEVATOR TRAILING EDGE OUTBOARD SIDE HAS EVIDENCE OF LIGHTNING STRIKE. MATERIAL ID 10 DOUBLER 2024T3.020 MATERIAL ID FOR TRAILING EDGE 2024T3.040 , ALODINED AND PRIMED PER SRM DC9 51-10-3. INSTALLED FABRICATED PARTS PER SRM 55-20-0 FIG 2. (M)

ATA 5320

Part: ANGLE — CORRODED (BS 995)

MHV - AFT CABIN ANGLE FS 995 LBL 0-60 HAS CORROSION BEYOND LIMITS CORROSION. REMOVED TO .035 ONLY ALLOWED .025 OER SRM 53-01 PAGE 6. REMOVED CORRODED ANGLE. REPLACED WITH NEW EXTRUSION 7075-T6511 MATERIAL DRILLED AND LOCATED NEW PART ALODINE AND PRIMED INSTALLED PER DC9 SRM 51-10-3, 53-05, 51-10-01, 51-01, 53-01, 51-30-2, 51-30-5. (M)

ATA 5755

Part: SKIN — DELAMINATED (LT SPOILER)

LEFT WING UPPER SURFACE OUTBOARD SPOILER IS DELAMINATED AT UPPER INBOARD SECTION APPROX 6 INCH BY 5 INCH OF DELAM ON PART RACK. DELAMINATION AREA IS LARGER THAN ALLOWED LIMITS IN SRM REQUIRES OUTSIDE VENDOR REPAIR REMOVED AND REPLACED. (M)

ATA 5321

Part: FLOOR — CORRODED (BS 200-243)

MHV - FORWARD PASS CABIN FLOOR AT FS 200-243 RBL 21-42 LIGHT CORROSION AFTER CORROSION WAS REMOVED FOUND AREA TO BE OUT OF LIMITS REF CARD W144. REMOVED AREA MATERIAL ID 7075T6.040 PER SRM 53-10-0. FABRICATED REPAIR PARTS PER SRM 53-01 FIG 4 ALODINED AND PRIMED PER SRM 51-10-3. INSTALLED PER SRM 53-01 FIG 4. (M)

ATA 5320

Part: ANGLE — CORRODED (BS 160)

MHV - FORWARD PASS COMPARTMENT FS 160 FLOOR SUPPORT ANGLE CORRODED LBL 15 TO 55. REMOVED SUPPORT ANGLE, FABRICATED NEW SUPPORT FROM 60-2576 7075T6 PO NR 81278 ALODINED AND PRIMED IAW DC9 SRM 50-10-3. INSTALLED SUPPORT IAW DC9 SRM 51-30-0. (M)

ATA 5315

Part: FLOORBEAM — CORRODED (BS 955)

MHV - AFT CARGO FS 955 RBL 24 EVIDENCE OF MODERATE TO HEAVY LOAL CORROSION ON FLOORBEAM UPPER CAP. REMOVED AND REPLACED UPPER CAP FABRICATED NEW CAP FROM 7075T6511 EXTRUSION S912758T PO NR 81788. INSTALLED FASTENER PER DC9 SRM 51-30-1 FOR TORQUE OF BOLTS DC9 SRM 51-30-2 FOR RIVET DC9 SRM 51-30-5 FOR HI-LOCKS PART WAS FABRICATED IAW DC9 SRM 51-10-1. (M)

ATA 5330

Part: SKIN — GOUGED (BS 130)

MHV - COCKPIT FUSELAGE SKIN LEFT SIDE AT STATION 130 WATER LINE 0 HAS A COUPLE OF GOUGES. REMOVED DAMAGED AREA (CUT OUT) AND REPAIRED IAW DC9 SRM 53-04 FIG 38 SHT 21, 51-30-2 AND 51-30-5 JOB COMPLETE REPAIRED FRAME AT FS 130 PER BOEING MESSAGE AUQ-MQJ-99-004RA DATED 12-MAR-99. (M)

ATA 5320

Part: STIFFENER — CRACKED (BS 484)

MHV - LEFT INBOARD FLOOR STATION 484 HAS RIVETS PULLING THROUGH AND BOTH ENDS OF ALL STIFFENERS ARE CRACKED ON 484 AND 520. REMOVED DAMAGED STIFFENERS. FABRICATED NEW STIFFENERS LOCATED AND DRILLED IAW SRM 51-01 TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED STIFFENERS IAW SRM 51-30-2 DC9. (M)

ATA 5321

Part: FLOOR — CORRODED (BS 160-200)

MHV - FLOORBOARDS FS 160-200 BL 0 TO LBL 42 CORRODED AND SUPTS CRACKED. FABRICATED A NEW SKIN IAW DC9 SRM 53-21-0, 4B INST HAT SUPPORTS IAW DC9 SRM 53-21-0. ALODINE AND PAINT IAW DC9 SRM. INSTALLED RIVETS IAW SRM DC9. (M)

ATA 5347

Part: SEAT TRACK — CORRODED (BS 200-230)

MHV - FORWARD PASS COMPARTMENT FS 200 TO 230 RBL 42 SEAT TRACK HAS EXFOLIATION CORROSION ON UPPER SURFACE. REMOVED DAMAGED SECTION OF SEAT TRACK CUT NEW SECTION OF SEAT TRACK EXTRUSION 52914913 PO 81257. FABRICATED AND DRILLED IAW SRM 53-05 . TREATED AND PRIMED NEW TRACK SECTION IW SRM 51-10-3. INSTALLED TRACK IAW SRM 51-30-1. (M)

ATA 2560

Part: BRACKET — CRACKED (R1 DOOR SLIDE)

MHV - R1 DOOR SLIDE SUPPORT BRACKET IS CRACKED FORWARD EDGE. STOP DRILLED CRACK USING .25 INCH DIAMETER DRILL AND BAB DOUBLER IAW DC9 SRM 53-01 FIG 2 DRILLED AND COUNTER SINK RIVET HOLES IAW SRM DC9 51-10-4 AND 51-30-2 ALODINE AND PRIMED IAW DC9 SRM 51-10-3 EDDY CURRENT TEST AND NO DEFECTS FOUND ATTACHED DOUBLER IAW 53-01 FIG 2 INSTALLED ON A/C. (M)

ATA 5320

Part: ANGLE — CORRODED (BS 160-220)

MHV - FORWARD PASS COMPARTMENT FS 160-220 BL 0 FLOOR SUPPORT ANGLE HAS MILD TO HEAVY CORROSION ENTIRE LENGTH. FLOOR SUPPORT WAS FABRCIATED ALODINED PRIMED AND INSTALLED COMPLETE IAW DC9 SRM 51-10-3, 51-30-5. (M)

ATA 5347

Part: SEAT TRACK — CORRODED (BS 220)

MHV - FORWARD PASS COMPARTMENT FS 220 RBL 21 SEAT TRACK HAS EXFOLIATION CORROSION ON TOP SURFACE. REMOVED SEAT TRACK AND REPLACED NEW SEAT TRACK FOR DC9 SRM 53-05 FIG 4. (M)

ATA 5330

Part: SKIN — GOUGED (BS 148)

MHV - COCKPIT FUSELAGE SKIN LEFT SIDE AT STATION 148 WATER LINE 0 HAS A COUPLE OF GOUGES. CUT OUT AREA DAMAGE, FABRICATE DOUBLER AND FILLER AND INSTALLED DOUBLER AND FILLER IAW DC9 SRM 53-04 FIG 38 PAGE 218 AND IAW DC9 SRM 51-30-02 AND 51-30-05. INSTALLED FASTENERS. (M)

ATA 5330

Part: SKIN — GOUGED (BS 120)

MHV - COCKPIT FUSELAGE SKIN LEFT SIDE AT STATION 120 WATER LINE 0 HAS A DENT APPROX 1 INCH BY 1 INCH AND IS GOUGED. CUT OUT AREA DAMAGE, FABRICATED DOUBLER AND FILLER AND INSTALLED DOUBLER AND FILLER IAW DC9 SRM 53-04 FIG 38 218 AND INSTALLED FASTENERS IW SC9 SRM 51-30-2 AND 51-30-5. (M)