N938DN

Part: LIGHT — DAMAGED (CABIN) · airframe 45,345 hrs · 36,861 cycles

EMERGENCY FLOOR LIGHTING DAMAGED. SECURED LIGHT STRIP. OPERATION CHECKS GOOD.

Part: BATTERY PACK — ABNORMAL (EMERGENCY LIGHTS) · airframe 44,859 hrs · 36,574 cycles

LEFT AFT OVERWING EXIT SIGN AND RIGHT AFT OVERWING EXIT SIGN INOPERATIVE. REPLACED THE BATTERY PACKS.

Part: SKIN — DENTED (TAILCONE) · airframe 44,857 hrs · 36,573 cycles

TAIL CONE SKIN DENTED. COMPLIED WITH PRI 540706-14, REV B, REVISION 0, 1, & 2 IAW ERA 540706-14, REV B.

Part: LENS — MISSING (CABIN) · airframe 44,721 hrs · 36,486 cycles

EMERGENCY EXIT LENS COVER MISSING AT DOOR 1R. INSTALLED NEW EMER EXIT LENS COVER.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 44,369 hrs · 36,288 cycles

L1 DOOR SLIDE UNSECURED. REMOVED AND REPLACED IAW MM.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 43,429 hrs · 35,766 cycles

EXIT SIGN COVER OVER CABIN MAIN ENTRANCE DOOR KEEPS FALLING DOWN. SECURED THE COVER. (LP# 9461452)

Part: COVER — LOOSE (EXIT SIGN) · airframe 43,354 hrs · 35,730 cycles

EMERGENCY EXIT SIGN COVER LOOSE. RE INSTALLED COVER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,102 hrs · 35,595 cycles

EMERGENCY FLOOR LIGHTING INOPERATIVE. RESECURED 17A - 20A FLOOR LIGHTING. OKAY FOR SERVICE.

Part: SKIN — CRACKED (BS 1437) · airframe 41,716 hrs · 34,747 cycles

AIRCRAFT SKIN HAS CRACK AT BS 1437. REPAIRED IAW PRI/ERA 549478-14.

Part: SKIN — CRACKED (FWD FUSELAGE) · airframe 41,716 hrs · 34,747 cycles

FUSELAGE SKIN CRACKED AT NOSE WHEEL WELL AFT DOOR HINGE CUTOUT. REPAIRED IAW SRM 53-30-01.

Part: ATTACH ANGLE — BROKEN (VERTICAL STAB) · airframe 41,723 hrs · 34,751 cycles

VERTICAL STABILIZER LEADING EDGE LOWER RIGHT INNER ATTACH ANGLE BROKEN. REPLACED THE ATTACH ANGLE IAW DWG 5912188.

Part: ATTACH ANGLE — BROKEN (VERTICAL STAB) · airframe 41,716 hrs · 34,747 cycles

VERTICAL STABILIZER LOWER LEFT INNER ATTACH ANGLE IS BROKEN. REPLACED IAW DWG 5912188.

Part: THRESHOLD — CORRODED (L1 DOORWAY) · airframe 41,712 hrs · 34,745 cycles

L1 DOOR THRESHOLD STRIP CORRODED. REPLACED IAW SRM 51-30-00.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 41,712 hrs · 34,745 cycles

CAPTAIN'S SLIDING WINDOW FRAME CRACKED AT UPPER AFT CORNER. REPAIRED IAW DWG 5911356 AND 5644324 AND PRI/ERA 549506-14.

Part: LONGERON — CRACKED (BS 1475) · airframe 41,712 hrs · 34,745 cycles

LONGERON 2R CRACKED AT BS 1475. REPAIRED IAW SRM 53-30-01, FIG 14.

Part: LIGHT — SHORTED (COCKPIT) · airframe 41,634 hrs · 34,705 cycles

FLIGHT CREW REPORTS SPARKS WHILE MOVING CAPTAIN'S LIGHT. CIRCUIT BREAKER TRIPPED AND WAS NOT RESET. INSTALLED NEW LIGHT. OPS CHECKED GOOD.

Part: STRUCTURE — DAMAGED (L1 DOOR) · airframe 41,286 hrs · 34,486 cycles

DAMAGE TO L1 DOOR LOWER LT CORNER FLANGE. REPAIRED DAMAGE IAW SRM 52-01-01.

Part: FRAME — DAMAGED (BS 1567) · airframe 39,604 hrs · 33,488 cycles

UPPER CANTED FRAME AT BS 1567.407 DAMAGED. REMOVED, FABRICATED AND INSTALLED FRAME IAW DWG 9911843.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 39,404 hrs · 33,371 cycles

DECLARED AN EMERGENCY ON APPROACH DUE TO RT HYD SYS LOW QTY. PERFORMED ALTERNATE GEAR EXTENSION. FOUND PYLON PRESSURE LINE CHAFING AND WORN THROUGH. CUT, REMOVED AND INSTALLED NEW LINE. LEAK CHECKS OK.

Part: UNKNOWN — HAZE (CABIN) · airframe 37,826 hrs · 32,431 cycles

F/A REPORTED ODOR AND HAZE IN CABIN JUST PRIOR TO DESCENT. LATER REPORTED HAZE AND MOST OF SMELL HAD CLEARED. TROUBLESHOT. NO TROUBLE FOUND. PERFORMED DUCT BURNOUT AND REPLACED COALESCER BAGS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,458 hrs · 31,592 cycles

EMERGENCY LIGHT INOPERATIVE VENTRAL STAIR AREA. REPAIRED IAW SWPM. OPS CHECKED GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,587 hrs · 31,074 cycles

FUSELAGE OUTER SKIN DAMAGE AT THE L1 DOOR GUST LOCK PIN CUTOUT. PERFORMED DVI. NO OTHER DAMAGE NOTED. TRIMMED OUT DAMAGED SKIN IAW RI 524991-14. COMPLETED IAW REPAIR INSTRUCTIONS 524991-14.

Part: BATTERY PACK — DISCONNECTED (EMERGENCY LIGHTS) · airframe 34,378 hrs · 30,363 cycles

DURING SERVICE CHECK, EMERGENCY EXIT LIGHTS IN CEILING AT ROWS 24 AND 25 INOPERATIVE. FOUND BATTERY PACK NOT CONNECTED. RECONNECTED AT LOCATION B5-243. OPS CHECKS GOOD.

Part: STRUCTURE — CRACKED (BS 1520) · airframe 32,520 hrs · 29,310 cycles

AFT ACCESSORY BAY AREA, CRACK AROUND FASTENER AREA BS 1520, LBL 10. ROUTED OUT CRACKED AREA AND FABRICATED REPAIR DOUBLER & SHIMS IAW ER/A 504832-14.

Part: SKIN — CORRODED (BS 954) · airframe 32,520 hrs · 29,310 cycles

DURING HMV, CORROSION WAS FOUND ON THE RT WING CENTER SECTION UPPER WING SKIN AT STA 954 AND BL 0. SUBSEQUENTLY, THE CORROSION WAS R & R IAW ER/A 504829-14. ACCOMPLISHED SECTION 1 OF REPAIR IAW ER/A 504829-14, REV O. REMOVED CORROSION FROM CENTER TANK, RBL 58, BS 955 IAW SRM 51-10-03, PARA 26 VOL II UT AREA AND FOUND TO BE OUT OF LIMITS IAW NDT SPM, PART 4 04-00-07, & SRM 53-00-01, FIG 3, VOL I. ORIG .235 AND LOWEST DEPTH IS .112 HFEC AREA IAW NDTSPM PART 6, 06-10-01 AND FOUND NO ADDITIONAL DEFECT OR CRACKS. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW ER/A 504829-14, REV 14, SEC 1 CAPPED SEAL ALL TANK FASTENERS IAW SRM 51-20-00, PARA 9, VOL II.

Part: BEAM — CRACKED (PAX DOOR) · airframe 32,520 hrs · 29,310 cycles

FORWARD ENTRY DOOR INTERNAL UPPER BEAM CRACKED IN RADIUS SIDE VIEWED THROUGH LIGHTNING HOLE STA 167. STOP DRILLED CRACK .250 DIAMETER IAW ERA 504823-14 AND SRM 51-00-01. LOCATED AND DRILLED NEW ANGLE IAW ERA 504823-14, REV 0 AND DWG 9955752. INSTALLED REPAIR ANGLE IAW SRM 51-40-01 AND 51-40-05. ASSOCIATED ER/A 14-504823 ADDED FOR AC 9238.

Part: FITTING — CRACKED (BS 1060 L20R) · airframe 32,520 hrs · 29,310 cycles

FUSELAGE LONGERON FITTING CRACKED. REPAIRED AT BS 1060, L20R IAW ER/A 14-509933 ADDED FOR AC 9238.

Part: BEAM — CRACKED (L1 DOOR) · airframe 32,520 hrs · 29,310 cycles

L1 DOOR INTERIOR BEAM CRACKED IN RADIUS AFT SIDE VIEWED THROUGH LIGHTNING HOLE STA 198. STOP DRILLED CRACK .250 DIA, LOCATED AND DRILLED NEW ANGLE AND INSTALLED IAW ERA 504823-14 REV 0, DWG 9955752 AND SRM 51-40-01, 51-40-02 AND 51-40-05. ASSOCIATED ER/A 14-504823 ADDED FOR AC 9238.

Part: HORN — GOUGED (LT WING) · airframe 32,520 hrs · 29,310 cycles

DURING CHECK, FOUND LT WINGTIP L/E HORN GOUGED, WS 560. FOUND HORN OUT OF LIMITS. REMOVED HORN FROM L/E. WELDED, GROUND WELD FLUSH, HFEC AND MT. NO DAMAGE NOTED. ALODINED, PRIMED AND INSTALLED HORN ON LEFT WINGTIP L/E SRM 51-30-02, 51-10-03 AND ER/A 468102-14 MA, ADDED FOR AC 9238. ACFT OK FOR SERVICE.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 32,520 hrs · 29,310 cycles

AFT AIRSTAIR (3RD STAIR FROM THE TOP, ABOVE THE APU ENCLOSURE) AFT RT CORNER HAS EVIDENCE OF CORROSION. R & R LOWER TEE ANGLE IAW SRM 51-10-05, 51-30-02, 51-30-05, 51-10-03 AND AMM 51-10-00-370-802.

Part: FRAME — CORRODED (BS 1379) · corrosion level 2 · airframe 32,520 hrs · 29,310 cycles

CORROSION AT AFT CARGO BS 1379 FRAME. AFT SIDE AT L30. REMOVED CORROSION. AREA FOUND OUT OF LIMITS WITH 100 PERCENT MATERIAL LOSS. CUT OUT DAMAGED AREA. FABRICATED TWO REPAIR SPLICES AND NEW FORMER. REPAIR INSTALLED IAW SRM 53-00-01, FIG 1 AND 51-10-03 PARA 26, PARA 21, PARA 1, VOL II AND 53-10-02, FIG 3, VOL I.