Boeing 757-24APF

Service difficulty reports · 16,054

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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 aircraft_model_key = '75724APF'
  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 IPXA2022091086092Shear Web · corrodedINSPECTION TYPE:SEG3MAIN CABIN FLOOR STA 340-368 LBL 25, AROUND HOLES HAS CORROSION. CORROSION LOCATED AT THE SHEAR WEB BETWEEN STA 330.8 AND STA 395 LBL 35.0.AFTER THE BLENDOUT ALL AREAS, SHEAR WEB WAS FOUND TO BE IN LIMITS PER SRM 53-10-51-1A-2.Sep 10, 2022 · N441UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2022091086099Shear Web · corrodedINSPECTION TYPE:SEG3MAIN CARGO COMPT UNDER FLOOR PANEL 222 XCF HAS AREAS OF CORROSION BETWEEN STA 418 AND STA 440. CORROSION LOCATED AT THE SHEAR WEB BETWEEN STA 398.5 AND STA 431.75 RBL 49AFTER THE BLENDOUT ALL AREAS, SHEAR WEB WAS FOUND TO BE IN LIMITS PER SSep 10, 2022 · N441UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2022091086091Shear Web · corrodedINSPECTION TYPE:SEG3MCC LEFT UNDER FLOOR PANEL 221 XAF HAS VARIOUS AREAS OF CORROSION. THE CORROSION IS ON THE SHEAR WEB STA 395 LBL 35.00 AND LBL 45.50.BLENDOUT WAS FOUND TO BE IN LIMITS PER SRM 53-10-51-1A-2.Sep 10, 2022 · N441UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2022091086088Shear Web · corrodedINSPECTION TYPE:SEG3MAIN CABIN FLOOR STA 394 LBL 38, FLOOR HAS CORROSION. *CORROSION WAS FOUND AT THE SHEAR WEB FROM STA 365 TO STA 395 LBL 38WORKED PER RCD 283541, BLEND OUT AREA FOUND TO BE WITHIN LIMITS PER SRM 53-10-51-1A-2Sep 10, 2022 · N441UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2022091086095Shear Web · corrodedINSPECTION TYPE:SEG3MAIN CABIN FLOOR STA 360-380 RBL 40 TO RBL 45.50, HAS CORROSION. CORROSION LOCATED AT THE SHEAR WEB BETWEEN STA 365.00 AND STA 395 RBL 40.00 TO RBL 45.50AFTER THE BLENDOUT ALL AREAS, SHEAR WEB WAS FOUND TO BE IN LIMITS PER SRM 53-10-51-1A-2Sep 10, 2022 · N441UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2022090986070Deck Plate · corrodedINSPECTION TYPE:SEG3MAIN CABIN DECK AFT SHEAR PLATE AT FS1700 BL 0 REMOVED CORROSED AREA 2.00" BY 1.50" WITH ONLY .037" OF MATERIAL REMAINING FINDING DECK PLATE TO BE OUT OF LIMITS PER SRM 53-0-51-1A-AREPAIRED DECKPLATE PER SRM 53-60-51-2R-7 REPAIR 7Sep 9, 2022 · N441UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2022090886040Skin · corrodedINSPECTION TYPE:SEG3#2 ENIGNE O/B SKIN ASSY P/N 311N5046-52 HAS CORROSION AT PP STA 144.425 AND PP STA 153.90REPAIRED O/B SKIN PER EA# 757-5450-27-A3019Sep 8, 2022 · N441UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2022090886039Shear Web · crackedINSPECTION TYPE:SEG3MAIN CABIN SHEAR WEB AT FS 365.25 LBL 12.5 HAD MULTIPLE CRACK DAMAGESREPAIRED SHEAR WEB PER SRM 53-10-51-2R-12 DETAIL 2Sep 8, 2022 · N441UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2022090685940Skin · crackedINSPECTION TYPE:SEG3LEFT WING FIXED LEADING EDGE AREA BETWEEN SLAT #3 AND SLAT #4 IS CRACKEDREPAIRED PER EO #B757-5740-11855E WING-OUTBOARD FIXED LEADING EDGE UPPER SKIN PANEL CRACK REPAIRS (SREO) APPENDIX BSep 6, 2022 · N441UP · Boeing 75724APF · Wing, Plate/SkinSDR IPXA2022090485888Skin · puncturedINSPECTION TYPE:N/ARIGHT ELEVATOR LOWER SKIN PUNCTUREDREPAIRED DAMAGED SKIN IAW EO B757-5520-84504-ASep 4, 2022 · N406UP · Boeing 75724APF · Elevator StructureSDR IPXA2022090585899Lamp · inoperativeINSPECTION TYPE:N/AL1 ENTRY DOOR EMERGENCY LIGHT HAS SEVERAL BULBS BURNT OUTRELAMPED 11 EA BULBS ON ENTRY DOOR EMERGENCY LIGHT IAW AMM 33-51-01 OPS CK GOODSep 3, 2022 · N404UP · Boeing 75724APF · Emergency LightingSDR IPXA2022092086428Frame · dentedINSPECTION TYPE:SEG1** SUPPLEMENTAL SDR ** FRAME AT STA 1500 RH HAS A DENT AT THE TOP OF THE FLANGE AT STR 25-26R. PERFORMED CUTOUT OF DAMAGED AREA. DIMENSIONS L=1.15" W=1.00"ACCOMPLISHED REPAIR PER SRM 53-07-2R-5 DETAIL I AND RCD 284695. ORIG SUB DATE: 9/20Sep 1, 2022 · N402UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2022090185804None · noneINSPECTION TYPE:**SDR FILED OPEN** L FWD ENTRY DOOR EICAS AFTER LANDING \, DURING TAXI, ILLUMINATED. WENT OUT AFTER 1 MINUTE. DEFERRED LEFT FWD ENTRY DOOR INDICATION SYSTEM IAW MEL 52-71-1.. DMP C/W. PLACARD INSTALLED.Sep 1, 2022 · N411UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2022092086426Frame · dentedINSPECTION TYPE:SEG1FRAME AT STA 1560 RH HAS A DENT AT THE TOP OF THE FLANGE AT STR 25-26R. PERFORMED CUTOUT OF DAMAGED AREA. DIMENSIONS L=.778" W=1.00"ACCOMPLISHED REPAIR PER SRM 53-07-2R-5 DETAIL I AND RCD 284612Aug 31, 2022 · N402UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2022091586283Frame · dentedINSPECTION TYPE:SEG1, FRAME AT STA 1520 RH HAS A DENT AT THE TOP OF THE FLANGE AT STR 25-26R. PERFORMED CUTOUT OF DAMAGED AREA. DIMENSIONS L=3.65" W=1.00"ACCOMPLISHED REPAIR PER SRM 53-07-2R-5 DETAIL III AND RCD 284607Aug 31, 2022 · N402UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2022091286142Support · crackedINSPECTION TYPE:C15NO 2 ENGINE I/B TR UPPER SEAL RETAINER CRACKED. CRACKED AREA FOUND AT THE UPPER BIFURCATION FIREWALL SEAL SUPPORT INNER FLANGE PPS 139.5ACCOMPLISHED REPAIR PER RR RB211-535E4-37/10 EM: 78-31-28-300-086 AND VT MAE EA# 757-7831-27-A3020 REV-Aug 31, 2022 · N441UP · Boeing 75724APF · Engine Thrust ReverserSDR IPXA2022092086458Stringer · corrodedINSPECTION TYPE:SEG1, STR 28R HAS CORROSION ON THE BOTTOM SURFACE OF STRINGER APPROX. 6 INCHES LONG. LOCATED AT THE FACTORY SPLICE FWD OF STA 1460.ACCOMPLISHED REPAIR PER SRM 53-00-03-2R-1 DETAIL IV AND RCD 284546.Aug 30, 2022 · N402UP · Boeing 75724APF · Fuselage Main, Longeron/StringerSDR IPXA2022083085766None · noneINSPECTION TYPE:C18NEEDED AN ALTERNATIVE METHOD OF INSPECTION ON AN EXISTING REPAIR TO FS 1560 BETWEEN STR 25R AND STR 27R AS PER EO#B757-5310-73926-AFOLLOWED ENGINEERING INSTRUCTIONSD PER EO#B757-5310-26562-CAug 30, 2022 · N419UP · Boeing 75724APF · Standard Practices/StructuresSDR IPXA2022082985706Floor Panel · damagedINSPECTION TYPE:C15CABIN FLOOR PANEL #231XCF BROKEN AT THE CORNER DOT 70.25FABBED PANEL 231XCF FROM 5024N400001SS-G, BATCH# 3489461 PER SR EO B757-5320-9692-KAug 29, 2022 · N441UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2022090886049Floor Panel · damagedINSPECTION TYPE:C15, MAIN CARGO COMPARTMENT , FLOOR PANEL #232XFF DAMAGED. - THIS IS A MINOR REPAIRREPLACED BROKEN INSERT I.A.W. UPS E.O. NO: M-5320-38342-C. ORIG SUB DATE: 9/9/2022Aug 26, 2022 · N441UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2022091086089Shear Web · corrodedINSPECTION TYPE:SEG3MAIN CABIN STA 340 LBL 10, FLOOR HAS CORROSION IN SEVERAL AREAS. CORROSION WAS FOUND AT THE SHEAR WEB.WORKED PER RCD 283543, BLENDED OUT AREA FOUND TO BE WITHIN LIMITS PER SRM 53-10-51-1A-2.Aug 26, 2022 · N441UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2022091286144Shear Web · corrodedINSPECTION TYPE:C15MAIN CABIN FLOOR STA 345, LBL 6 HAS CORROSION. CORROSION AREA IS LOCATED AT SHEAR WEB STA 345 LBL 6AFTER BLENDOUT THE AREA FOUND TO BE WITHIN ALLOWABLE LIMITS PER SRM 53-10-51-1A-2Aug 26, 2022 · N441UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2022082985705Power Lever · inoperativeINSPECTION TYPE:N/A**DIVERSION** SIGNIFICANT THRUST LEVER SPLIT ON CLIMBOUT RT THRUST LEVER AT MECHANICAL STOP PASSING FL 320 LT THRUST LEVER 5-6 AFT OF RT LEVER RT ENGINE EPR REQUESTED 1.34 THRUST LEVER COULD ONLY GET TO 1.3R&R D RT ENG EEC REF MM 7321-04-401Aug 26, 2022 · N433UP · Boeing 75724APF · Power LeverSDR IPXA2022091286145Deck Plate · corrodedINSPECTION TYPE:C15MAIN CABIN STA 1720 LBL 17 CORROSION LOCATED AT AFT SHEAR WEB CORROSION LOCATED AT STA 1720 BETWEEN BL 0 AND LBL 24.75BLEND WAS FOUND TO BE WITHIN ALLOWABLE LIMITS PER SRM 53-60-51-1A-1Aug 25, 2022 · N441UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2022082785658Skin · delaminatedINSPECTION TYPE:CLEFT HOR. STAB. LWR SKIN HAS A NEW DENT 41 IN. FROM INBD EDGE AND 14 IN. FROM L/E.REPAIRED PANEL IAW B757 SRM 51-70-10-2R -4 PER SRM 55-10-01-1A.Aug 25, 2022 · N463UP · Boeing 75724APF · Horizontal Stabilizer, Plate/SkinSDR IPXA2022082585594Floor Panel · damagedINSPECTION TYPE:C18FLOOR PANEL #241 XDF HAS BROKEN EDGES IN 2 PLACES DOT 70-15FABBED PANEL 241 XDF FROM 5024N400001SS-G, BATCH# 3855547 PER SREO B757-5320-9692-KAug 19, 2022 · N419UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2022081985408Doubler · corrodedINSPECTION TYPE:SEG2#2 ENGINE PYLON O/B SIDE INSIDE SKIN CORRODED FWD OF THE PRE-COOLER.WORK PER UPS EO B757-5430-84516-A, UPS RCD 279265, AND VT MAE EA 757-545-27-A3001 REV-Aug 19, 2022 · N455UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2022081985412Skin · dentedINSPECTION TYPE:SEG2EXTERIOR CROW AREA STA 620-640 BL 0 RIVET HEAD HAS A LIGHTNING STRIKE. DURING AN IDT INSPECTION FOUND A DENT IN THE AREA.WORK PER UPS EO B757-5330-84515-A, UPS RCD 279212 AND VT MAE EA 757-5330-27-A3000 REV-Aug 19, 2022 · N455UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2022081985411Controller · false indicationINSPECTION TYPE:N/A**DIVERSION - EMERGENCY DECLARED**IN CRUISE AT FL390, RECEIVED CABIN ALTITUDE WARNING. CABIN SHOWED APPROXIMETLY 11,000'. RAN CHECKLIST AND DESCENDED TO FL210, CABIN ALTITUDE WENT DOWN TO 6000. BEFORE DESCENT CABIN SHOWED 11,500' AND RATE WAAug 17, 2022 · N422UP · Boeing 75724APF · Cabin Pressure ControllerSDR IPXA2022081785360Frame · dentedINSPECTION TYPE:SEG2FRAME STA 1480 IN THE AFT CARGO AREA IS DENTED ON TOP OF THE FRAME FLANGE BY S-26R. DAMAGE MARKED IN REDWORKED PER UPS RCD 279468, REPAIR IAW SRM 53-00-07-2R-5 DETAIL IIIAug 17, 2022 · N455UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2022081485215None · noneINSPECTION TYPE:DIRH LOWER FUSELAGE AT STA 700, S-24R HAS A TEMPORARY LIGHTINING STRIKE REPAIR. REQUIRES PERMANENT REPAIR. SKIN P/N: 143N3691-2, ORIGINAL MAT: STOCK 0.080" THICKNESS, 2024-T3 CLAD SHEETACCOMPLISHED REPAIR PER 757-200PF SRM REV 114.0, CHAPTER 53Aug 13, 2022 · N413UP · Boeing 75724APF · Standard Practices/StructuresSDR IPXA2022081285170Skin Panel · corrodedINSPECTION TYPE:SEG2#2 ENGINE PYLON FWD LOWER SKIN HAS CORROSION. FROM PP STA 109.00 TO PP STA 112.00REMOVED CORROSION IAW SRM 51-10-02-0G, 10X DVI WITH NO CORR/CRACKS NOTED. NOMINAL THICKNESS .350, AFTER REMOVAL .245, MATERIAL LOSS .005 WITHIN LIMITS IAW SRM Aug 12, 2022 · N455UP · Boeing 75724APF · Crew Oxygen SystemSDR IPXA2022082585608Skin · corrodedINSPECTION TYPE:SEG1#1 ENGINE INBD PYLON INNER SKIN FWD OF PRECOOLER HAS CORROSION OUT OF LIMITSWORK PER UPS EO B757-5430-84537-A, UPS RCD 279961 AND VT MAE EA 757-5450-27-A3005 REV-Aug 11, 2022 · N463UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2022082585607Skin · corrodedINSPECTION TYPE:SEG1#2 ENGINE OUTBD PYLON FWD OF PRECOOLER (INTERNAL) BETWEEN NAC STA 105.66 - 169.8 HAS CORROSION.WORK PER UPS EO B757-5430-84529-A, UPS RCD 279930 AND VT MAE EA 757-5450-27-A3002 REV-Aug 11, 2022 · N463UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2022082585606Skin · corrodedINSPECTION TYPE:SEG1#1 ENGINE PYLON OUTBD INNER SKIN FWD OF VENT PANEL $443CL HAS CORROSIONWORK PER UPS EO B757-5430-84530-A, UPS RCD 279965 AND VT MAE EA 757-5450-27-A3003 REV-Aug 11, 2022 · N463UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2022082585593Frame · dentedINSPECTION TYPE:SEG1FRAME STA 1460 AT S-26L IS DENTED ON TOP OF FRAME FLANGE IN THE RADIUSACCOMPLISHED REPAIR IAW SRM 53-00-07-2R-5 DETAIL 1 AND RCD 279873Aug 10, 2022 · N463UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2022082785650Strap · corrodedINSPECTION TYPE:C13MAIN CARGO DOOR CUTOUT LOWER STRAP REPAIR AT STA 620, BETWEEN STR 24L AND STR 26L.WORKED, PER UPS EO B 757-5330-84558-A, UPS RCD 279834, AND VT MAE EA 757-5330-27-A3007 REV- FAA 8100-9Aug 9, 2022 · N463UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2022080384864Light · inoperativeINSPECTION TYPE:N/AWHILE TAKING THE RUNWAY FOR DEPARTURE WE HAD A BURNING SMELL IN COCPIT. TURNED OF LIGHT & SMELL DISAPATED. BLOCK TURN BACK. RUNWAY TAXI LIGHTS.R&R R RUNWAY TURNOFF LIGHT TRANSFORMER (T138) PER MM33-42-05-004-001 AS A PRECAUTION. R&R LIGHTINGAug 2, 2022 · N426UP · Boeing 75724APF · Air Distribution SystemSDR IPXA2022081485224Skin · corrodedINSPECTION TYPE:DVI#2 PYLON WING SKIN/DRAG FTG HOLE #2 HAS CORROSION INDICATION INSIDE HOLE FOUND DURING INSP OF THE E.O. B757-5720-69617-I APPENDIX EREPAIRED IAW UPS E.O. B757-5720-84376-A DATED 08/14/2022Jul 31, 2022 · N444UP · Boeing 75724APF · Wing, Plate/SkinSDR IPXA2022072784612Frame · damagedINSPECTION TYPE:SEG1EXISTING REPAIR FOUND AT AFT CARGO COMPARTMENT FRS 1240 R/H BETWEEN STR 24R TO STR 27RWORK PER UPS EO B757-5310-84316-A, UPS RCD 256300 AND VT MAE EA 757-5360-27-A2979 REV -Jul 27, 2022 · N424UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2022081285169Tie Clip · corrodedINSPECTION TYPE:CK17FWD CARGO DOOR AT APPROX FS 580 LOWER INNER T CHORD IS CORRODEDREMOVED AND REPLACED T CHORD USING AN 10136-1503 PER SRM 51-40-02 PAR 9Jul 26, 2022 · N444UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2022072684580Panel · delaminatedINSPECTION TYPE:SEG1DRY BAY PANEL (632 FZ) FLAME SPRAY PEELING OFF AROUND FASTENER HOLES.PANEL 632 FZ (DOOR) SENT OUT FOR FLAME SPRAY REPAIR. VENDOR VT-SAN ANTONIO. REINSTALLED ON SERVICEABLE PARTS TAG #914270. SRM 51-70-14-0G PARA 10.BJul 26, 2022 · N424UP · Boeing 75724APF · Wing Main, Frame StructureSDR IPXA2022072684579Stringer · corrodedINSPECTION TYPE:SEG1AGING AIRCRAFT INSPECTION AT STA 1625 L, S 26L, SEVERAL RIVETS WITH CORROSIONWORKED PER UPS RCD 256496, REPAIRED IAW B757-SRM 53-00-03-2R-1Jul 26, 2022 · N424UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2022072384465Frame · corrodedINSPECTION TYPE:SEG1DURING ACCOMPLISHMENT OF E.O. B757-5310-73926-A, FOUND EXISTING REPAIR AT STA 1560 BETWEEN S-24L AND S-27LWORKED PER UPS EO B757-5310-83788-A, UPS RCD 256301, AND VT MAE EA 757-5360-27-A2978 REV-Jul 23, 2022 · N424UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2022080284840Floor Panel · corrodedINSPECTION TYPE:SEG2FLOOR BEAM AT STA 1100 LBL4 HAS CORROSION OUT OF LIMITS. ORIGINAL THICKNESS .200" MATERIAL REMAINING .140" MATERIAL LOSS .060"REPLACED SECTION OF UPPER FLANGE FROM RBL 13.0 TO LBL 12.0 PER EO B757-5310-27-A2990Jul 22, 2022 · N453UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2022080684960Skin · corrodedINSPECTION TYPE:CK14#1 PYLON AFT SKIN INNER DOUBLER HAD 2 LOCATIONS OF CORROSION DAMAGE. THE FWD CORROSION LOCATION IS LOCATED BETWEEN PP STA 153 AND PP STA 160. THE AFT CORROSION LOCATION IS LOCATED BETWEEN PP STA 182.2 AND PP STA 185.35. BOTH LOCATIONS ARE OJul 21, 2022 · N453UP · Boeing 75724APF · Nacelle/Pylon, Main FrameSDR IPXA2022072184408Frame · dentedINSPECTION TYPE:SEG1AFT CARGO COMPARTMENT, LOWER FRAME STA 1300 L/H BETWEEN STR 25L TO STR 26L HAS A DENTWORK PER RCD 256338, REPAIRED PER 757-200PF SRM REV 114.00 53-00-07-2R-6 DETAIL III PER SRM 53-60-07-2RJul 21, 2022 · N424UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2022072984678Frame · damagedINSPECTION TYPE:SEG2DURING ACCOMPLISHMENT OF EO B757-5310-73926-A FOUND AN EXISTING FRAME REPAIR AT STA 1560 BETWEEN S-24R AND S-27R. ALTERNATE INSPECTION REQUIREDACCOMPLISHED REPAIR PER EO B757-5310-83923-A, UPS RCD 277195 AND VT MAE 757-5360-27-A2984Jul 20, 2022 · N453UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2022072084384Frame · dentedINSPECTION TYPE:SEG1AFT CARGO COMPARTMENT, LOWER FRAME UPPER FLANGE AT STA 1500 R/H HAS A DENT BETWEEN STR 25R TO STR 26RWORKED PER RCD 256340. ACCOMPLISHED REPAIR IAW 757-200PF SRM REV 114.00 CHAPTER 53-00-07-2R-5 DETAIL III PER SRM 53-60-07-2RJul 20, 2022 · N424UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2022080584952Skin Panel · dentedINSPECTION TYPE:CK14DEFERRAL ITEM# 762227. FUSELAGE SKIN DOUBLER HAS DENT AT STA 400-405 BETWEEN S3L AND S4LREPLACED EXISTING DOUBLER IAW UPS EO B757-5330-45385-C AND VT MAE EA 757-5310-27-A2993Jul 19, 2022 · N453UP · Boeing 75724APF · Fuselage Main, Structure
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