N14106

Service difficulty reports · 158

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N14106' AND registry_match = 'registration'
  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 CALA2026101620413O-Ring · leakingC-HYD QTY EICAS, LEAK COMING FROM DUAL PRESS/CASE DRAIN MODULE-C LOCATED IN HYD SERVICING BAY. LEAKING COMING FROM UPPER SWITCH BASE ASSY SEE PIC. PULLED AND COLLARED BOTH CENTER HYD PUMP CBS. REMOVED AND REPLACED O-RING ON UPPER PRESSURE SWITCH OF FILTER MODOct 15, 2026 · N14106 · Boeing 757224 · Hydraulic System, MainSDR CALA2026081418628Circuit Card · faultyRIGHT ENG OVHT EICAS, FL410 EGT SHOWED 587 AFTER ENG BLEED & PACK OFF. THRUST REDUCED. OVERHEAT LIGHT WENT OUT AT 1.39 EGT IAW FIM 26-11 FT 802. R & R AFOLTS CARD M10274, AMM 26-10-01/401.Aug 8, 2026 · N14106 · Boeing 757224 · Engine (Turbine/Turboprop)SDR CALA2026051816338Warning Message · false activationTE FLAP DISAGREE AFTER FLAP 25 SELECTION PERFORMED OPERATIONAL CHECK OF THE TE FLAPS. OPS CHECK GOOD. REF: AMM TASK 27-51-00-715-001. PERFORMED BITE TEST OF ALL THREE FSEUS. NO PRESENT FAULTS FOUND (SEE PICTURES). REF: FIM 27-51 FAULT TREE 805.May 14, 2026 · N14106 · Boeing 757224 · Trailing Flap Position Indicating SystemSDR CALA2026042815806Door Seal · wornLOUD SQUEAL OMMITTING FROM DOOR 1L TOP LEFT OF DOOR SEAL IMMEAD IATLY AFTER/T/O PERFORMED LEAK CHECK AND FOUND LEAK SOUND FROM BOTH UPPER CORNERS OF DOOR FRAME SEALS. UPON FURTHER INSPECTION FOUND DOOR FRAME WITH UNEVEN SURFACE FOR SEAL TO MATE WITH. APPLIED Apr 26, 2026 · N14106 · Boeing 757224 · Passenger/Crew DoorsSDR CALA2026030414305Plug · damagedREMOVED PLUG HPNGVN IN REF TO L/P4936131 FOUND PLUG DAMAGE INSTALLED PLUG HPNGVN IN REF TO AMM 72-00-00-846-191-R02 VERIFIED INSTALLATION OF PLUG HPNGVN IN REF TO AMM 72-00-00-846-191-R02Mar 4, 2026 · N14106 · Boeing 757224 · Turbine SectionSDR CALA2025120811827Slide · faultyFOUND R1 DOOR SLIDE PRESSURE LOW. REMOVED R1 SLIDE. PARTIALLY INSTALLED NEW SLIDE, NEW SLIDE CAME WITH INCORRECT GIRT BAR. GIRT BAR NEEDS REPLACED IAW AMM TASK 25-66-01-404-044 UP TO AND INCLUDING STEP H(17). VERIFIED SLIDE INSTALLATION UP TO AND INCLUDINDec 5, 2025 · N14106 · Boeing 757224 · Escape SlideSDR CALA2025112111377Anti-Ice Valve · no discrepancyTIA VALVE LIGHT WITH EICAS WHEN THRUST IS BELOW 30 N1 ON TAXI NORMAL INDICATION PER CONDITIONS DESCRIBED. NO FURTHER ACTION NEEDED. IAW AMM 30-21-00.Nov 19, 2025 · N14106 · Boeing 757224 · Air Intake Anti/De-Ice SystemSDR CALA2025100209521None · noneLIQUID OF UNKNOWN ORIGIN ALL ALONG RIGHT SIDE COCKPIT FLOOR. STRONG COFFEE SMELL ALSO. FLIGHT CREW SPILLED COFFEE DURING FLIGHT. SPILLAGE MOSTLY DRY UPON ARRIVAL. INSPECTED E+E NO FLUIDS FOUND.Oct 2, 2025 · N14106 · Boeing 757224 · Standard Practices/StructuresSDR CALA2025091008728Wire · burnedMAIN EQUIPMENT CENTER AT BS 395 RT UPPER POWER FEEDER IS BURNED. REMOVED AND REPLACED POWER FEEDER WIRE W3412-0003-210 AND W3412- 0010-210 IAW WDM 24-21-21 AND SWPM 20-10-21 21-30-13 AND 20-10-20 T97654 OPS CHECK OK IAW AMM 71-00-00-795-032 -R03.Sep 8, 2025 · N14106 · Boeing 757224 · Electrical Power System WiringSDR CALA2025091008724Wire Harness · burnedREF EA3611-01469. ENGINE 2 STRUT, UPPER SURFACE, RH SIDE, BY STA PPS 174.30, WIRE BUNDLE HAS CHAFING AND BURN MARKS. ESDR COMPLETED. REMOVED AND REPLACED POWER FEEDER WIRE W3412-0006-110 ON ENG #2 IAW AND M 24-21-21 AND SWPM 20-10-11 AMM 24-11-20-404-01 2 T011Sep 8, 2025 · N14106 · Boeing 757224 · Turbine Engine System WiringSDR CALA2025090808587Bulkhead Web · gougedAFTER RADOME HOLD SUPPORT BRACKET REMOVED, FOUND A GOUGE A T BULKHEAD FRONT FACE SKIN BS 200 LBL 15. ACCOMPLISHED REPAIR ON FWD BULKHEAD FRONT FACE SKIN WITH NO DEVI ARIOUS PER VT MAE EA 757-5310-13-A4089 REV- AND EC/RA #5310-0868 9. DIP BY PAGES CREATED PERSep 6, 2025 · N14106 · Boeing 757224 · Fuselage Main, BulkheadSDR CALA2025090508509Skin · crackedRIGHT WING SKIN AND DRAG FITTING. HAD A CRACK INDICATION, NOTED AT HOLE NR 3 IN BOTH LAYERS. ACCOMPLISHED REPAIR PER ECRA 5720-03563 AND EA 757-572 -13-A4083 WITH NO DEVIATIONS.Sep 3, 2025 · N14106 · Boeing 757224 · Wing, Plate/SkinSDR CALA2025090508507Skin · crackedRIGHT WING SKIN AND DRAG FITTING. CRACK INDICATION NOTED AT HOLE NR 5 IN BOTH LAYERS. ACCOMPLISHED REPAIR PER ECRA 5720-03563 AND EA 757-572-13-A4083 WITH NO DEVIATIONS.Sep 3, 2025 · N14106 · Boeing 757224 · Wing, Plate/SkinSDR CALA2025090508505Skin · crackedRIGHT WING SKIN & DRAG FITTING HAD A CRACK INDICATION NOTED AT HOLE NR 4 IN BOTH LAYERS. ACCOMPLISHED A REPAIR IAW ECRA 5720-03563 AND EA 757-572-13-A4083 WITH NO DEVIATIONS.Sep 3, 2025 · N14106 · Boeing 757224 · Wing, Plate/SkinSDR CALA2025090508503Drag Fitting · crackedRIGHT WING SKIN AND DRAG FITTING. A CRACK INDICATION NOTED AT HOLE NR 2 IN BOTH LAYERS. ACCOMPLISHED A REPAIR IAW ECRA 5720-03563 AND EA 757-572-13-A4083 WITH NO DEVIATIONS.Sep 3, 2025 · N14106 · Boeing 757224 · Wing, Attach FittingsSDR CALA2025082908259Skin · corrodedTAIL AREA, APU INLET DOOR FWD SIDE, CUTOUT H AS EVIDENCE OF CORROSION. REPAIRED STRAP FOR THE AUXILIARY POWER UNIT AIR STA 1825.00 BETW EEN STG 3 TO STA 6 R/H IAW B757-200 53-80-15-2R-1.Aug 24, 2025 · N14106 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2025082908258Bear Strap · crackedL1 DOOR SUROUND THE 7TH CRITICAL FASTENER HOLE. COUNTING RT TO LT IAW FIGURE -00 2 OF EA5330-04213 REV D, HAD A CRACK INDICATION AT THE BEAR STRAP L AYER. ACCOMPLISHED REPAIR IAW EA 757-5310-A4078 AND EA 5330-04213 REV D. OPERATION 2 & EC/RA # 5330-07569.Aug 24, 2025 · N14106 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2025082808230Tee Fitting · corrodedDURING BODY FAIRING REMOVAL FOUND EXFOLIATED T-CHORD AT BS 900, LOWER AREA. R & R TEE FITTING BS 900 BETWEEN LBL65 IAW SRM 51-40-02-0G-0, AND SRM 51-70-12-0G-0, STEP C, TABLE II.Aug 23, 2025 · N14106 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025082508090Stop Fitting · damaged(SDR) 53-5305-1-2060 - TAIL AREA, AFT POTABLE WATER SERVICE DOOR FWD CUTOUT DOORSTOP IS DAMAGED. DOT 23-059. REF: NR 130314. C/W SDR/SFR REPORTING ONLY REPAIRED AFT POTABLE WATER SERVICE DOOR FWD CUTOUT DOOR STOPS PE R EC/RA# 5361-01126 AND VT MAE EA 757-5360-Aug 23, 2025 · N14106 · Boeing 757224 · Fuselage Main, StructureSDR CALA2025082508089Support Channel · corrodedAFTER OPENING ACCESS PANEL 197LL, FOUND SUPPORT CHANNEL WTB L BL 6 WITH EXFOLLIATION, STA 1180 TO STA 1220. DOT 68-18. REF: NR 129950. C/W SDR/SFR REPORTING ONLY REMOVED AND REPLACED SUPPORT CHANNEL AT STA 1180 TO STA 1220 LBL 6 IAW B757-200 SRM 51-40-02-OG-0 Aug 23, 2025 · N14106 · Boeing 757224 · Fuselage Miscellaneous StructureSDR CALA2025082508072Skin · dented(SDR) LP#5082799 DENT ON LHS FUSELAGE STA 620-STA 640, S21L TO S 22L(REPAIR PER SRM) REF:NR130571 SFR REPORTING ONLY SDR REPORTING SFR #1610 HAS BEEN UPDATED. RII VERIFIED JOB PERFORMED.Aug 13, 2025 · N14106 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2025060605330Pressure Switch · faultedSTAB TRIM LIGHT ON O/H PANEL AND EICAS ILLUM AFTER T/O. ACCOMPLI SHED NON NORMAL. REMOVED AND REPLACED RIGHT BRAKE PRESSURE SWITCH IN REF AMM 27-41-07. LEAK CHECK GOOD. PERFORMED THE STABILIZER TRIM MODULE TEST IN REF 27-09-00-712-037 UP TO AND INCLUDING (4)(Jun 4, 2025 · N14106 · Boeing 757224 · Flight Control SystemSDR CALA2025031302747Relief Valve · damagedFOUND LOWER CABIN POSITIVE PRESSURE RELIEF VALVE MISSING LOWER FLAPPER. UPPER FLAPPER WAS REMOVED AND DEFERED ON LOG 3881765. FLAPPER SHAPE IS HALF CIRCLE OF 3 INCHES RADIUS. LOWER CABIN PRESSURE RELIEF VALVE CDL ON LOG 3881765Mar 10, 2025 · N14106 · Boeing 757224 · Cabin Pressure Control SystemSDR CALA2025010301775Cover · detachedEMERGENCY EXIT COVER SNAPPED OFF SEAT 27C RESECURRED EXIT ROW COVER AT SEAT 27CJan 1, 2025 · N14106 · Boeing 757224 · Emergency LightingSDR CALA2024110801078Elec Connector · dirtyCTRL SW ENG DID SHUT DOWN BUT STRONG FUEL SMELL IMMED AFTERWARD SEE LP 9791798 - FOLLOWING MULTIPLE ENGINE RUNS AND NORMAL SHUTD OWNS, NO SMELL OR ODOR WAS NOTICED FOLLOWING ENGINE 1 SHUTDOWNS. OK TO CONTINUE. SEE REFERENCED LP FOR PARENT WRITE UP. ON LEFT ENGNov 6, 2024 · N14106 · Boeing 757224 · Engine Fuel System WiringSDR CALA2024093000721Skin · damagedNR 6 LEADING EDGE SLAT DAMAGE, APPROXIMATELY 66 SQUARE INCH SECTION OF THE INBOARD TRAILING EDGE WEDGE DEPARTED THE AIRCRAFT.Sep 25, 2024 · N14106 · Boeing 757224 · Leading Edge DevicesSDR CALA2024010500043Plate · crackedRT WING TE WIGGLE PLATE IS CRACKED, LOCATED JUST AFT OF RT WING JACK PAD. REF AMES NR 165960-0600-0001 REMOVED AND REPLACED RT WING TE WIGGLE PLATE IAW B757 SRM 51-40- 02 PARA 4. SEE BACK FOR PARTIAL WORK ACCOMPLISHED.Jan 4, 2024 · N14106 · Boeing 757224 · Wing Main, Frame StructureSDR CALA2023121103621Cowling · damagedPDA 1 UPON ARRIVAL, PILOT FOUND OIL ACCESS SERVICING DOOR RIPPED OFF FROM #1 ENGINE, SEE ORIGINAL LOG PAGE 6497592. ALSO, COMPLETED AN ESFR (SDR # 1034535) REPORT CONSULTED TOMC AND ORD ENGINEERING. NO CDL RELIEF, HOWEVER, POSSIBLE RELIEF WITH TRM 7110-01125 Dec 8, 2023 · N14106 · Boeing 757200 · Nacelle/Pylon, Main FrameSDR CALA2023030900669Bearing · noneDOOR 1R VERY DIFFICULT TO ARM GIRT BAR BINDING DURING ARM/DISARM. FOUND FORWARD ROD END BEARING ASSY SHEARED BETWEEN GIRT BAR MECHANISM AND DOOR LOWER TORQUE TUBE. REMOVED ROD END BEARING ASSY. REF IPC 52-11-20-20A ITEMS 290 & 295. INSTALLED NEW SERVICEABLEMar 9, 2023 · N14106 · Boeing 757* · DoorsSDR CALA2023022700560Cowling · missingPDA 2 MISSING MASTER CHIP DETECTOR ACCESS PANEL 424CR ON ENG 2. DIMENSIONS 5X7 INCHES. AIPC REF 71-11-04. REMOVED AND REPLACED ENGINE #2 FAN COWL RH OUTBOARD PER EC/RA #5420-01600. REF AMM 71-11-04.Feb 27, 2023 · N14106 · Boeing 757200 · Nacelle/Pylon StructureSDR CALA2023010600047Stringer · damagedUPON DAMAGE REMOVAL OF FUSELAGE SKIN SECTION REF. L/P: 3443028, BETWEEN STA. 620 - 640, STRINGER S9L ALSO FOUND DAMAGED COMPLIED WITH INSPECTION REQUIREMENTS FOR VERIFICATION OF MAT''L FOR HAT SECTION DOUBLER AND FILLER MAT''L PER SRM: 53-00-03-2R-1 STEP 3. CUJan 5, 2023 · N14106 · Boeing 757224 · Fuselage Main, Longeron/StringerSDR CALA2023010600046Skin · dentedDURING JETBRIDGE CONNECTION TO THE AIRCRAFT THE JETBRIGDE CONTACTED THE AIRCRAFT FUSELAGE FWD OF D2L . INSPECTED DENT REF SRM 53-00-01 SHEET 3 PARA B,F,I,J.. DENT IS OUT OF LIMITS BUT MEETS ALL CRITERIA LISTED IN PARAGRAPH "I". APPROVED FOR DIP PER THIS SRM WIJan 5, 2023 · N14106 · Boeing 757224 · Fuselage Main, Plate/SkinSDR CALA2023010200011Skin · handler errorDURING JETBRIDGE CONNECTION TO THE AIRCRAFT THE JETBRIGDE CONTACTED THE AIRCRAFT FUSELAGE FWD OF D2L . INSPECTED DENT REF SRM 53-00-01 SHEET 3 PARA B,F,I,J.. DENT IS OUT OF LIMITS BUT MEETS ALL CRITERIA LISTED IN PARAGRAPH "I". APPROVED FOR DIP PER THIS SRM WIJan 2, 2023 · N14106 · Boeing 757200 · Standard Practices/StructuresSDR CALA2023010200010Toilet · leakingRIGHT AFT LAV LEAKING BLUE WATER.CARPETS SOAKED RH AFT LAV LEAK INSPECTED. NO ISSUES NOTED.Jan 2, 2023 · N14106 · Boeing 757224 · Waste Disposal SystemSDR CALA2022123003525Anti-Ice Valve · faultedRTO AT 90KTS FOR R ENG ANTI-ICE CAUTION RETURNED TO GATE. REMOVED & REPLACED PRESS REGULATOR ANTI-ICE SHUTOFF VALVE. OPS CHK GOOD.Dec 30, 2022 · N14106 · Boeing 757224 · Engine Anti-Icing SystemSDR CALA2022081902121Floorbeam · corrodedSUPPORT TASK: MAIN CABIN FLOORBEAM STA 720 RBL24 UPPER SURFACE CORRODED. TRANSCRIBED FROM HAECO GSO NRC# 9282606 REMOVED CORROSION ON FLOORBEAM AT STA 720 PER B757-200 SRM 51-1 HAECO GSO MECH V934114 INSP QC470 0-02. ORIGINAL MATERIAL THICKNESS .125, MATERIALAug 17, 2022 · N14106 · Boeing 757200 · Fuselage Main, Floor BeamSDR CALA2022081602103Doubler · none(SUPPORT TASK) RIGHT HORIZONTAL STAB INSPECTED PER EA 5100-02345 -017, FOUND 1EA REPAIR DOUBLER APPROX WIDTH=5", LENGTH= 10.5" BE TWEEN RIB 8 AND RIB 9, LOWER SKIN AUX AND FRONT SPAR. SKIN DOUBLER IS IN GOOD CONDITION. NO HISTORY OF DOCUMENTATION. TRANSCRIB EAug 15, 2022 · N14106 · Boeing 757200 · Horizontal Stabilizer, Plate/SkinSDR CALA2022081602102Lamp · inoperative(SUPPORT TASK) L1 DOOR EXTERIOR SLIDE LIGHT INOP. TRANSCRIBED GF FROM HAECO NR 9283359.Aug 15, 2022 · N14106 · Boeing 757200 · DoorsSDR CALA2022081002031Skin · none(SUPPORT TASK) R1 DOOR INSPECTED PER EA-5100-02345-017, FOUND 1E A SKIN DOUBLER APPROX WIDTH=8" X HEIGHT=9". SKIN DOUBLER IS IN GOOD CONDITION WITH NO DEFECTS NOTED. TRANSCRIBED FROM HAECO GSO NRC# 9282054 LOW FREQUENCY EDDY CURRENT (LFEC) INTERVAL 3,000 DOORAug 9, 2022 · N14106 · Boeing 757224 · Passenger/Crew DoorsSDR CALA2022080501958Seat Track · corrodedSUPPORT TASK: MAIN CABIN STA 745 RBL45 SEAT TRACK SUPPORT UPPER FLANGE HAS CORROSION. TRANSCRIBED FROM HAECO GSO NRC# 9282392Aug 3, 2022 · N14106 · Boeing 757224 · Fuselage Main, StructureSDR CALA2022080501957Attach Angle · crackedSUPPORT TASK: LW ADAPTER PLUG HAS A CRACKED ANGLE. TRANSCRIBED FROM HAECO GSO NRC# 9282883 REPAIRED LW ADAPTER PLUG UPPER ATTACH ANGLE PER UAL EC/RA 5730-0 3543. HAECO GSO MECH V900579, INSP QC004Aug 3, 2022 · N14106 · Boeing 757224 · Wing, Attach FittingsSDR CALA2022080101925Floor Support · corrodedSUPPORT TASK: 1602. MAIN CABIN FLOOR SUPPORT FRAME HAS CORROSION TOP & BOTTOM. MARKED IN RED). DOT B871. STA 740 OR APPROX LBL 56. TRANSCRIBED FROM HAECO GSO NR 9282532Jul 31, 2022 · N14106 · Boeing 757200 · Fuselage Main, Floor BeamSDR CALA2022072901916Frame · gougedTHE REPAIR INCORPORATED VIA ECRA 5362-01038 AT STA 1640 S-5R TO S-6R IS APPROVED AS TIME LIMITED FOR 18 MONTHS PENDING THE RESUL TS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE THE ACFT FROM SE RVICE ON JANUARY 15,2024 UNLESS ANOTHER 8110-3 FORM IS RECEIVED FIJul 27, 2022 · N14106 · Boeing 757224 · Fuselage Main, FrameSDR CALA2022072701892Flange · gougedTHE REPAIR INCORPORATED VIA ECRA 5362-01038 AT STA 1640 S-5R TO S-6R IS APPROVED AS TIME LIMITED FOR 18 MONTHS PENDING THE RESUL TS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE THE ACFT FROM SE RVICE ON JANUARY 15,2024 UNLESS ANOTHER 8110-3 FORM IS RECEIVED FIJul 27, 2022 · N14106 · Boeing 757200 · Fuselage Main, FrameSDR CALA2022072501864Intercostal · none(B757-53-3-0492) FWD PIT RH SIDE INTERCOSTAL HAS 1EA ELONGATED HOLE AT APPROX STA 725 BETWEEN S27R AND S28R. STREAMER ATTACHED. TRANSCRIBED FROM HAECO GSO NR 9282942 MAT''L ID 7075-0 .032 PO NO. 857 IAW BAC DWG 143N5375 REV C, FORM 51-21-10. INSTALLED INTECOSTJul 22, 2022 · N14106 · Boeing 757 · Fuselage Miscellaneous StructureSDR CALA2022072001825Frame · damaged(B757-53-3-05770 FRAME STA. 1220RH - STR.1 - TOOLING MARK/DAMAGE/BARE METAL EXPOSED ON EXTERNAL SRUFACE OF FRAME HAECO GSO NR 9283098 MAT ID 7075.0 .080 IAW B757-200 SRM 53-00-07-1A-1, FORMED AND HE AT TREATED IAW BAC5602 REV A. LOCATED/DRILLED IAW B757-200 SRJul 19, 2022 · N14106 · Boeing 757200 · Fuselage Main, FrameSDR CALA2022071801780Intercostal · corrodedB757-53-3-0553: INTERCOSTAL UPPER SURFACE CORRODED AT RBL45 BS 3 25, TRANSCRIBED FROM HAECO GSO NRC# 9283132Jul 15, 2022 · N14106 · Boeing 757224 · Fuselage Main, StructureSDR CALA2022071501751Floor Support · corrodedSUPPORT TASK MAIN CABIN STA 345-365 LBL 65 GUTTER SUPPORT HAS CO RROSION ON UPPER SURFACE, TRANSCRIBED FROM HAECO GSO NR 9283207Jul 14, 2022 · N14106 · Boeing 757200 · Fuselage Miscellaneous StructureSDR CALA2022071501739Intercostal · corrodedSUPPORT TASK: MAIN CABIN STA 399 RBL 45-61 FLOOR SUPPORT INTERCOSTAL HAS CORROSION ON BOTTOM. TRANSCRIBED FROM HAECO GSO NRC# 9 283237 REMOVED AND REPLACED FLOOR SUPPORT FROM STA 399 RBL-45 TO 61 IAW B757-200 SRM 51-40-02 , SRM 51-40-05 AND BAC DWG 141N5162. Jul 13, 2022 · N14106 · Boeing 757200 · Fuselage Main, StructureSDR CALA2022071501738Stringer · elongatedSUPPORT TASK; MAIN CABIN STATION 1560-STR-16 R HAS AN ELONGATED FASTENER HOLE AT STRINGER CLIP ATTACH POINT TRANSCRIBED FROM HAECO GSO NR 9283268 B757 200 SRM 51 20 01 TOP COATED IAW B757 200 AMM 51 21 15 INSTALLED STRINGER REPAIR FR 1560 S16 R, ZONE 1 TYPE 1 Jul 13, 2022 · N14106 · Boeing 757200 · Fuselage Main, Structure
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