JASC 5342

Service difficulty reports · 578

Reports filed under 5342 · Fuselage, Stabilizer Attach Fittings, newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE jasc_code = '5342'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR REXA2026052800812Drag Angle · crackedCRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM REPAIR ON CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WAS PERFORMED PESep 30, 2025 · N294PQ · Cndair CL6002D24SDR VNAA202510300005Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.0). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE ATSep 23, 2025 · N630NN · Cndair CL6002D24SDR REXA2026052800845Drag Angle · crackedINITIAL INSPECTION: CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL 0.00). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5Sep 19, 2025 · N605LR · Cndair CL6002D24SDR REXA2026052800840Drag Angle · crackedINITIAL INSPECTION: CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL 0.00) CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67Sep 19, 2025 · N605LR · Cndair CL6002D24SDR HNAA2025102100718Drag Angle · crackedF070245 VERTICAL STABILIZER RH DRAG ANGLE HAS POSSIBLE CRACK AT FR 76. REPAIRED VERTICAL STABILIZER RH DRAG ANGLE AT FR 76. IAW EMB 145 SRM 53-31-01RE DET B FIG 219 SH1 AND SRM 51-40-02.Sep 15, 2025 · N691AE · Emb EMB145LRSDR HNAA2025102100717Drag Angle · crackedF070244 VERTICAL STABILIZER LH DRAG ANGLE HAS POSSIBLE CRACK AT FR 76. RAR VERTICAL STABILIZER LH DRAG ANGLE AT FR 76. IAW EMB 145 SRM 53-31-01RE DET B FIG 219 SH1 AND SRM 51-40-02.Sep 15, 2025 · N691AE · Emb EMB145LRSDR SWI2025F01896Drag Angle · crackedRIGHT AFT VERTICAL STAB DRAG ANGLE HAS POSSIBLE CRACK (MARKED). (C-CHECK RO 12/24/2025)EVALUATED, REMOVED AND INSTALLED NEW RH AFT VERTICAL STAB DRAG ANGLE REF CRJ900 SRM 51-42-13-001-001-A01 , CRJ900 SRM 51-42-21-001-001-A01 , CRJ900 SRM 51-42-22-001-001-A01 Sep 10, 2025 · N820SK · Cndair CL6002D24SDR SWIA202512260910Drag Angle · crackedLEFT AFT VERTICAL STAB DRAG ANGLE HAS POSSIBLE CRACK. PERFORMED REPAIR ON LH AFT VERTICAL STAB DRAG ANGLE IAW SRM 55-31-00-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.Sep 10, 2025 · N820SK · Cndair CL6002D24SDR SWI2025F01793Drag Angle · crackedLEFT VERTICAL STAB TO FUSELAGE ATTACH AFT DRAG ANGLE POSSIBLY CRACKED. REMOVED CRACKED LT VERTICAL STAB TO FUSELAGE ATTACH AFT DRAG ANGLE IAW SRM 51-42-10-001-001-A01, SRM 51-42-21-001-001-A01, AND SRM 51-42-22-001-001-A01, AND INSTALLED -5 DOUBLER ANGLE ANAug 27, 2025 · N633SK · Cndair CL6002C10SDR SWIA2025120900827Drag Angle · crackedLH VERTICAL STAB TO FUSELAGE ATTACH FORWARD DRAG ANGLE POSSIBLY CRACKED. AFTER DETERMINING THE END OF THE CRACK BY NDT INSP IAW NDTM PART 1 51-20-08-230 ON REPORTED FWD DRAG ANGLE, IT WAS REPAIRED BY INSTALLATION OF REINFORCEMENT ANGLE IAW SRM 55-31-00-201-00Aug 27, 2025 · N633SK · Cndair CL6002C10SDR IPXA2025091850638Bracket · cracked-EXT TAIL-L/H SIDE WHERE FUSELAGE AND TAIL MEET-ANGLE CRACKED FOR UPPER APRON(333AT)-109 VWV 91195430. INSTALLED L/H HORIZONTAL STABILIZER LEADING EDGE 331AB IAW A300-600 AMM 55-12-11/401. REVIEWEDAug 25, 2025 · N142UP · Airbus A300F4622RSDR SWIA202511240808Drag Angle · crackedRH VERTICAL STAB-TO-FUSELAGE AFT DRAG ANGLE POSSIBLY CRACKED (MARKED) (C-CHECK RO 11/22/2025)REMOVED RH AFT DRAG ANGLE REF CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01,CRJ700 SRM 51-42-22-001-001-A01. INSTALLED NEW RH AFT DRAG ANGLE REF CAug 8, 2025 · N759EV · Cndair CL6002C10SDR SWIA20251124808Drag Angle · crackedLH VERTICAL STAB-TO-FUSELAGE AFT DRAG ANGLE POSSIBLY CRACKED (MARKED) (C-CHECK RO 11/22/2025)INSTALLED -5 AFT ANGLE DOUBLER & -7 AFT ANGLE FILLER ON L/H AFT DRAG ANGLE REPAIR REF CRJ 700 SRM 55-31-00-201-001-A01. COMPLIED WITH SKY WEST TASK CARD 51-900-1002-Aug 8, 2025 · N759EV · Cndair CL6002C10SDR VNA2025F00028Drag Angle · crackedCRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE LH/RH , BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE LH/RH , BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRAJul 15, 2025 · N640NN · Bombdr CL6002D15SDR REXA2025100200899Drag Angle · crackedR/H AFT DRAG ANGLE IS CRACKED. REMOVED UNSERVICEABLE RH AFT DRAG ANGLE P/N:AV670-21186-004. IAW CRJ900 SRM 51-42-13-001-001-A01,SRM 51-42-21-001-001-A01 AND SRM 51-42-22-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE RH AFT DRAG ANGLE PN# AV670-21186-004 IJul 7, 2025 · N133EV · Cndair CL6002D24SDR SWI2025F01502Drag Angle · crackedRH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE POSSIBLE CRACK (MARKED) (C-CHECK RO 11/01/2025)PERFORMED SRM REPAIR TO CRACKED RH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE. REF CRJ900 SRM 55-31-00-201-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.Jun 28, 2025 · N803SK · Cndair CL6002D24SDR SWI2025F01501Drag Angle · crackedLH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE POSSIBLE CRACK (MARKED) (C-CHECK RO 11/01/2025)REMOVED AND INSTALLED REPAIR ANGLES ON LH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE. REF. CRJ900 SRM 55-31-00-201-001-A01 REV 38 JUL 25/2020. COMPLIED WITH 51-900-1002-SKY.Jun 28, 2025 · N803SK · Cndair CL6002D24SDR SWIA202511030628Drag Angle · crackedRH VERT STAB-TO-FUSELAGE FORWARD DRAG ANGLE POSSIBLE CRACK (MARKED) (C-CHECK RO 11/01/2025)PERFORMED SRM REPAIR TO CRACKED RH VERT STAB-TO-FUSELAGE FORWARD DRAG ANGLE. REF CRJ900 SRM 55-31-00-201-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.Jun 28, 2025 · N803SK · Cndair CL6002D24SDR SWIA2025062300020Drag Angle · crackedDURING RH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE REMOVAL FIND CRACK ON RH VERT STAB-TO-FUSELAGE FWD DRAG ANGLE #30352476 (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSJun 20, 2025 · N898SK · Cndair CL6002D24SDR REXA2025062600699Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUMJun 19, 2025 · N601LR · Cndair CL6002D24SDR SWI2025F01636Drag Angle · crackedRIGHT VERT STAB-TO-FUSELAGE AFT DRAG ANGLE, THE AFT END POSSIBLE CRACKED. (C-CHECK) REMOVED AND REPLACED WITH NEW RT VERT STAB-TO-FUSELAGE AFT DRAG ANGLE. IAW DWG BA670-35002, REV -F, SRM 51-42-21-001-001-A01, SRM 51-42-13-001-001-A01 AND SRM 51-42-22-001-0May 24, 2025 · N898SK · Cndair CL6002D24SDR SWIA202511260524Drag Angle · crackedLH VERT STAB-TO-FUSELAGE AFT DRAG ANGLE, THE FWD END POSSIBLE CRACK (MARKED) (C-CHECK RO 11/25/2025)REMOVED AND INSTALLED NEW AFT DRAG ANGLE PN# AV670-21186-003 ON LH VERTICAL STABILIZER REF CRJ900 SRM 51-42-13-001-001-A01, CRJ900 SRM 51-42-22-001-001-A01, CMay 24, 2025 · N898SK · Cndair CL6002D24SDR AALA202506232953Lug · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND HORIZONTAL STABILIZER REAR SPAR LOWER LUG. REPAIRED PER EA 364945.May 15, 2025 · N963AN · Boeing 737823SDR AALA202506235379Lug · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND HORIZONTAL STABILIZER REAR SPAR LOWER LUG. REPAIRED PER EA 364946.May 15, 2025 · N963AN · Boeing 737823SDR SWI2025F01051Drag Angle · crackedLEFT VERTICAL STABILIZER DRAG ANGLE AFT CRACKED. PERFORMED REPIAR DRAG ANGLE AFT ON LT VERTICAL STABILIZER IAW REO 670-55-31-018 REV-A, & SRM 51-26-01, NDT PERFORMED.Apr 22, 2025 · N825SK · Cndair CL6002D24SDR SWIA2025072200422Drag Angle · crackedRIGHT VERTICAL STABILIZER DRAG ANGLE AFT CRACKED. PERFORMED REPAIR DRAG ANGLE AFT AT RH VERTICAL STABILIZER IAW REO 670-55-31-018 REV-A, SRM 51-26-01, NDT PERFORMED.Apr 22, 2025 · N825SK · Cndair CL6002D24SDR SWI2025F00940Drag Angle · crackedLH VERTICAL STAB - TO - FUSELAGE AFT DRAG ANGLE POSSIBLE CRACK AT LEADING EDGE OF ANGLE (MARKED) (C-CHECK RO 07/15/2025)REPAIRED LH VERTICAL STAB - TO - FUSELAGE AFT DRAG ANGLE PER CRJ900 SRM TASK 55-31-00-201-001-A01.COMPLETED SKYWEST TASK CARD 51-900-1002-Apr 4, 2025 · N802SK · Cndair CL6002D24SDR SWIA2025071600404Drag Angle · crackedLH VERTICAL STAB - TO - FUSELAGE FWD DRAG ANGLE CRACKED (MARKED) (C-CHECK RO 07/15/2025)REPAIRED LH VERTICAL STAB - TO - FUSELAGE FWD DRAG ANGLE PER CRJ900 SRM TASK 55-31-00-201-001-A01.COMPLETED SKYWEST TASK CARD 51-900-1002-SKY AND M-337.Apr 4, 2025 · N802SK · Cndair CL6002D24SDR REXA2026072801209Drag Angle · crackedIN REFERENCE TO CARD 700-53-900-310: CRACK ON AFT DRAG ANGLE AT VERTICAL STABILIZER RH SIDE. AFT DRAN ANGLE AT VERTICAL STABILIZER RH SIDE WAS REPAIRED PER CRJ-700 SRM 55-31-00-201-001-A01Mar 16, 2025 · N376CA · Cndair CL6002C10SDR SWI2025F01303Drag Angle · crackedLH VERTICAL STAB TO FUSELAGE ATTACH AFT DRAG ANGLE POSSIBLY CRACKED (MARKED) (C-CHECK RO 09/07/2025)REMOVED OLD AND INSTALLED NEW AFT DRAG ANGLE AT AFT LH VERTICAL STAB TO FUSELAGE ATTACH. REF CRJ900 SRM 51-42-13-001-001-A01 , CRJ900 SRM 51-42-21-001-001-A01Mar 13, 2025 · N896SK · Cndair CL6002D24SDR SWI2025F01301Drag Angle · crackedRH VERTICAL STAB TO FUSELAGE ATTACH AFT DRAG ANGLE POSSIBLY CRACKED (MARKED) (C-CHECK RO 09/07/2025)REMOVED OLD AND INSTALLED NEW AFT DRAG ANGLE AT AFT RH VERTICAL STAB TO FUSELAGE ATTACH REF CRJ900 SRM 51-42-13-001-001-A01 , CRJ900 SRM 51-42-21-001-001-A01 AMar 13, 2025 · N896SK · Cndair CL6002D24SDR DALA2025031802032Mount · corroded(LOG 0855497) VERTICAL STAB MOUNTING POINTS CORROSION PRI 624280 ISSUED. C/W VERTICAL STAB/MOUNTING POINTS/CORROSION FINDINGS ERA 624280-14 REV ORIGINAL SECTION 1 PERMANENT REPAIR. VERIFIED ERA 624280-14 HAS BEEN COMPLETED.Mar 13, 2025 · N3737C · Boeing 737832SDR YENA2025031200253Lug · crackedDURING HEAVY MAINTENANCE: REF AEROMAN WO# 2025 17/1 NR# 2025-120296. CRACK ON LUG O/B ACTUATOR ON RH HORIZONTAL STABILIZER, (RESOLVED ON W/O: 1353259 TASKCARD: NR-00014) REF AEROMAN WO# 2025 17/1 NR# 2025-120296. PERFORMED PERMANENT REPAIR ON LOCKING LUG LOCATMar 10, 2025 · N607JB · Airbus A320232SDR DALA2025031201944Lug · corroded(LOG 0849062) CORROSION LOCATED ON AFT FACE OF REAR LOWER LUG AT LT HORIZONTAL STABILIZER. COMPLIED WITH ER/A 623847-14 REV ORIGINAL, THIS MATCHES WITH ALL STEPS ON PRI 623847-14 REV 0, 1 AND 2, IT HAS BEEN VALIDATED.PERFORMED REPAIR INSTRUCTIONS ON HORIZONTALMar 9, 2025 · N3742C · Boeing 737832SDR DALA2025031201943Lug · corroded(LOG 0848130) CORROSION LOCATED ON AFT FACE OF REAR LOWER LUG OF RH HORIZONTAL STABILIZER. PERFORMED REPAIR INSTRUCTIONS ON RH HORIZONTAL STABILIZER, AS PER ER/A 623846-14 REV. ORIGINAL.Mar 9, 2025 · N3742C · Boeing 737832SDR REXA2025031300318Attach Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DAMar 3, 2025 · N348PQ · Cndair CL6002D24SDR REXA2025031300316Attach Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND ON FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SMar 3, 2025 · N348PQ · Cndair CL6002D24SDR DALA2025030301627Mount · corrodedAIRCRAFT 3737, ON VERTICAL STAB AFT MOUNT OUTBOARD LT FITTING LUG CORROSION ON FACE OF BUSHING. CORRECTIVE ACTION: REPLACED VERTICAL STAB AFT MOUNT OUTBOARD LT BUSHING PER PRI 624280-14 C/W ALL RII ITEMS. REF ERA 624280-14 REV 0 PRI REV5. (LP 0829461)Feb 26, 2025 · N3737C · Boeing 737832SDR SCNA20250415119Bushing · crackedRIGHT HOR. STAB AFT BOTTOM ATTACHMENT BUSHING CRACKED. UNABLE TO CONFIRM WHETHER IF BUSHING IS A SHRINKFIT OR FORCEMENT & P/N IS UNAVAILABLE PER EAR #12 RESPONSE STEP 1. PERFORMED A DVI IAW SRM 51-10-04-0G-0 REV 23 10MAR2025, GOUGE (POSSIBLE) CRACK NOTED AT Feb 25, 2025 · N8059A · Boeing 73786JSDR DALA2025030201589Mount · corroded(LOG 0829460) ON VERTICAL STAB AFT MOUNT OUTBOARD RT FITTING LUG CORROSION ON FACE OF BUSHING. R/R VERT STAB AFT MOUNT OUTBOARD RT BUSHING PER PRI 624280-14 C/W ALL RII ITEMS, REF ERA 624280-14 REV 0, PRI REV 5.Feb 25, 2025 · N3737C · Boeing 737832SDR SCNA20250505161Bushing · migratedLEFT AFT HORIZONTAL STAB UPPER AFT BUSHING MIGRATING. SAA034 027 - RESOLUTION: SUBMIT TO ENG. UNABLE TO CONFIRM IF BUSHING IS SHRRINK FIT OR FORCEMATE P/N CANNOT BEE CONFIRMED PER ENG RESPOSE STEP 1. BUSHING MIGRATED SEALANT WAS BROKEN AROUND ENTIRE CIRCFeb 24, 2025 · N8059A · Boeing 73783NSDR SCNA20250415120Bushing · crackedON CENTER BOX LEFT AFT LOWER HOR. STAB HAS BUSHING CRACKED. UNABLE TO CONFIRM WHETHE IF BUSHING IS SHRINKFIT OR FORCEMENT & P/N IS UNAVALIABKE, PER EAR #5 RESPONSE STEP 1. PERFORMED A DVI, IAW SRM 51-10-04-0G-0 REV 23 10MAR2025, GOUGE & CRAVK NOTED AT DEFEFeb 24, 2025 · N8059A · Boeing 73786JSDR 9WGA2025021234408Attach Fitting · damagedHORIZONTAL STAB ATTACH FITTING R/H OUTBOARD UPPER TENSION BOLT HOLE HAS EVIDENCE OF CORROSION/CRACK INDICATION, REPAIRED R/H OUTBOARD UPPER TENSION BOLT HOLE IAW B747-400 EAM 4453014 R3. NO DEFECTS NOTED. AIRCRAFT APPROVED FOR RETURN TO SERVICE.Feb 8, 2025 · N344KD · Boeing 747446SDR 9WGA2025021234407Attach Fitting · damagedHORIZONTAL STAB ATTACH FITTING R/H UPPER MIDDLE OUTBOARD TENSION BOLT HOLE HAS EVIDENCE OF CORROSION/CRACK INDICATION. REPAIRED R/H UPPER MIDDLE OUTBOARD TENSION BOLT HOLE IAW B747-400 EAM 4453014 R3. NO DEFECTS NOTED. AIRCRAFT APPROVED FOR RETURN TO SERVICFeb 8, 2025 · N344KD · Boeing 747446SDR 9WGA2025021234406Attach Fitting · corrodedHORIZONTAL STABILIZER ATTACH FITTING LEFT HAND LOWER INBD CROSSBOLT HOLE HAS EVIDENCE OF CORROSION.Feb 8, 2025 · N344KD · Boeing 747446SDR SWI2025F01042Drag Angle · crackedVERTICAL STAB. RH AFT DRAG ANGLE HAS SUSPECTED CRACK (MARKED). (C-CHECK RO 07/18/2025)REPAIRED VERTICAL STAB RH AFT DRAG ANGLE REF CRJ700 SRM 55-31-00-201-001-A01 REPAIR COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKYJan 24, 2025 · N723EV · Cndair CL6002C10SDR SCNA20250507170Bushing · wornRIGHT HAND HORIZONTAL STABILIZER, THE FORWARD LOWER MOUNT BUSHINGS PLATING IS WORN. (120-109) - RESOLUTION: SUBMIT TO ENG, REMOVED FORWARD LOWER MOUNT BUSHINGS AT RIGHT HAND HORIZONTAL STABILIZER IAW BOEING SERVICE BULLETIN 737-55-1074 FIG. 4 PAGE 1 TO 3. REVJan 23, 2025 · N5209A · Boeing 73783NSDR SCNA20250505163Bushing · wornRIGHT HAND HORIZONTAL STABILIZER, THE AFT MID MOUNT BUSHINGS PLATING IS WORN. REMOVED AFT MID MOUNT BUSHINGS AT R/H HORIZONTAL STABILIZER IAW BOEING SERVICE BULLETIN 737-55-1074 FIG 4 PG 1 TO 3 REV 2.Jan 23, 2025 · N5209A · Boeing 7378SDR SCNA20250505162Bushing · wornRIGHT HAND HORIZONTAL STABILIZER, THE FORWARD LOWER MOUNT BUSHINGS PLATING IS WORN. (120-109) - SUBMIT TO ENG, REMOVED FORWARD LOWER MOUNT BUSHINGS AT RIGHT HAND HORIZONTAL STABILIZER IAW BOEING SERVICE BULLETIN 737-55-1074 FIG. 4 PAGE 1 TO 3. REV. 2. DATE JUJan 23, 2025 · N5209 · Boeing 7378SDR SCNA20250415118Lug · gougedAIRCRAFT TAIL SECTION, RIGHT HAND HORIZONTAL STABILIZER, THE FORWARD UPPER MOUNT LUG HAS A GOUGE ON THE UPPER FORWARD SURFACE. . REMOVED DAMAGE ON TO AIRCRAFT TAIL SECTION R/H HORIZONTAL STABALIZER THE FWD UPPER MOUNT LUG ON THE UPPER FWD SURFACE IAW B737-800 Jan 23, 2025 · N5209A · Boeing 73783N
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