Boeing MD-11F

Service difficulty reports · 31,317

Newest first. General aviation reporting is voluntary.

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 = 'MD11F'
  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 IPXA2020052255590Doubler · crackedINSPECTION TYPE:2CLT WING FIXED L/E SKIN BEADED DOUBLER CRACK REPAIR BETWEEN STA XOS 740.8 - XOS 753.0 REQUIRES PERMANENT REPAIR.REPAIRED CRACKED LT WING FIXED L/E SKIN BEADED DOUBLER BETWEEN STA XOS 740.8 - XOS 753.0 IAW MD-11 SRM 57-40-02, REPAIR 15, FIGURE Apr 27, 2020 · N256UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020051855418Doubler · crackedINSPECTION TYPE:2CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BEWTEEN STA. XOS. 648.2 TO 653.0.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 648.2 TO 653.0 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)Apr 27, 2020 · N256UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020051855414Doubler · crackedINSPECTION TYPE:2CL/H WINF FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 616.8 TO 621.6.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 616.8 TO 621.6 IAW SRM 57-40-02 REPAIR 15 FIG, 205. (MAJOR)Apr 27, 2020 · N256UP · Doug MD11F · Wing, Plate/SkinSDR FDEA2020051570939Doubler · damagedCENTER CARGO DOOR LEFT LOWER AFT CORNER PREVIOUS DOUBLER REPAIR DAMAGED. REPLACED DOUBLER PER SRM 53-00-15-2R REPAIR 8Apr 27, 2020 · N593FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA202004270930Skin · crackedPACK #1 EXHAUST EXTERNAL FUSELAGE SKIN - UPPER AFT CORNER - CRACK EMANATING FROM FASTENER HOLE TO CUTOUT. CONFIRMED WITH NDT HFEC. REPAIRED / REMOVED CRACKED SKIN CONDITION. REF: MD-11 SRM 53-20-15-2R REPAIR #3 SHEET 1Apr 27, 2020 · N593FE · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020042954740Sense Line · looseINSPECTION TYPE:3CREJECTED TAKEOFF DUE TO ASYMMETRICAL ENGINE ACCELERATION.FOUND PT2 AND PT5 LINES LOOSE ON THE ENGINE EEC. TIGHTENED LINES AND PERFORMED ENG. RUNS,REF AMM 71-02-03-700-800. ENG. RUNS ARE GOOD.Apr 27, 2020 · N278UP · Doug MD11F · Fuel Controlling SystemSDR FDEA202004270806Seat Track · damagedCABIN SEAT TRACK CROWN AREA DAMAGED AT LEFT HAND STATION 5-2, X = 8.5. SEAT TRACK CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 5-8Apr 27, 2020 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202004270805Seat Track · damagedCABIN SEAT TRACK CROWN AREA DAMAGED AT LEFT HAND STATION 1421, X = 47.5 . SEAT TRACK CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1Apr 27, 2020 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202004270804Seat Track · damagedCABIN SEAT TRACK CROWN AREA DAMAGED AT LEFT HAND STATION 5-11 , X = 27.5. SEAT TRACK CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLApr 27, 2020 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202004270802Tire · failedAFTER CLEARING RUNWAY NBR 10 TIRE FAILURE ALERT APPEARED ASSOCIATED NOISE AND THUMP. DURING TAXI INTO GATE. FOUND NBR 10 M/W TIRE DAMAGED NO FURTHER DAMAGE FOUND. NBR 10 M/W TIRE ASSY REPLACED AS PER AMM 32-41-01-4 REV OCT 26/2018 .Apr 27, 2020 · N583FE · Doug MD11F · TireSDR IPXA2020052645700Former · crackedINSPECTION TYPE:2C, RT WING L/E RIB (FORMER) IS CRACKED AT STA XOS 584.8912.REMOVED AND REPLACED CRACKED RT WING L/E RIB (FORMER) AT SAT XOS 584.8912 IAW MD-11 SRM 51-33-01. (MINOR)Apr 26, 2020 · N256UP · Doug MD11F · Wing SparSDR IPXA2020052255570Rib · crackedINSPECTION TYPE:2CRT WING FIXED L/E RIB IS CRACKED O/BOF #14 SLAT TRACK.REMOVED AND REPLACED CRACKED RT WING FIXED L/E RIB AT STA XOS 906.5607 IAW MD-11 SRM 51-33-01. (MINOR)Apr 26, 2020 · N256UP · Doug MD11F · Wing, Rib/BulkheadSDR IPXA2020052255568Skin · crackedINSPECTION TYPE:2CLT WING FIXED L/E SKIN IS CRACKED I/B OF #16 SLAT TRACK.REPAIRED CRACKED LT WING FIXED L/E SKIN BETWEEN STA XOS 987.1 - 993.2 IAW MD-11 SRM 57-40-01, REPAIR 9, FIGURE 201. (MAJOR)Apr 26, 2020 · N256UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020042554629Skin · bentL1 DOOR AFT UPPER CORNER BENT OUTWARD INTO THE AIRSTREAM. REWORKED BENT SKIN & RMVD EFFECTED FASTNERS PER ENGINEER REQ. 4-25-20/C/W HFEC AND ROTO SCAN PER NDT SPM 06-10-01.001, 06-00-03, NO CRACKS NOTED AT THIS TIME. COMPLETED FAB OF REPLACMENT SKIN & REPAIRApr 25, 2020 · N293UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2020052635668Frame · crackedINSPECTION TYPE:C3AFT AVI COMP BILGE AREA L/H CANTED FRAME IS CRACKED AT STA 469.173.ACCOMPLISHED PERMANENT REPAIR ON CRACKED CANTED FRAME IN AFT AVIONICS COMPARTMENT AT STA 469.173 IAW MD11 SRM 53-10-07 REPAIR 1 FIGURE 201 REV. 66. (MAJOR)Apr 24, 2020 · N261UP · Doug MD11F · Fuselage Main, FrameSDR IPXA2020051855411Frame · crackedINSPECTION TYPE:3CFUSELAGE FRAME AT STA. 469.173 CANT AND X=60 IS CRACKED.REPAIRED CRACKED FUSELAGE FRAME AT STA. 469.173 CANT AND X=60 IAW SRM 53-10-07 REPAIR 1 FIG. 201. (MAJOR)Apr 24, 2020 · N261UP · Doug MD11F · Fuselage Main, FrameSDR FDEA2020042740784Tire · failed15 MINUTES PRIOR TO LANDING LEVEL 2 TIRE FAIL NUMBER #8 TIRE INDICATIONG ZERO AND CONFIRMED FLAT BY EMERGENCY SERVICES. REMOVED AND REPLACED #8 MAIN TIRE AS REQUIRED REF MD11 AMM 32-41-01-4. AIRCRAFT OK FOR SERVICEApr 24, 2020 · N589FE · Doug MD11F · TireSDR IPXA2020062977053Seat Track · corrodedINSPECTION TYPE:3CMAIN CABIN FLOOR SEAT TRACK STA 1381 -1521 X=8.50 HAS CORROSION.REPAIRED CORRODED SEAT TRACK IN MAIN CARGO BETWEEN STA 1371 AND 1531 X=8.50 IAW SRM 53-00-52 REPAIR 1 FIG 201 AND EA 011-5310-01-A8188 , EO MD11-5310-76615A. (MAJOR)Apr 23, 2020 · N261UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2020062977049Seat Track · corrodedINSPECTION TYPE:3C, MAIN CARGO RT FLOOR AREA SEAT TRACK HAS CORROSION BETWEEN STA 1401 TO STA 1501 X= -75.25REPAIRED CORRODED SEAT TRACK IN MAIN CARGO BETWEEN STA 1391 AND 1531 X= -75.25 IAW SRM 53-00-52 REPAIR 1 FIG 201 , EA 011-5310-01-A8188 AND EO MD11-5310Apr 23, 2020 · N261UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2020061056406Seat Track · corrodedINSPECTION TYPE:3C SEAT TRACK IS CORRODED BETWEEN STA 1401-1521 AT X=8.50. REMOVED AND REPLACED SEAT TRACK IAW EA 011-5310-01-A8188 REV IR AND EO MD-11-5310-76615-A. (MINOR)Apr 23, 2020 · N261UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2020060155979Floor Support · corroded3C MAIN CABIN RT FLOOR AREA AT STA 1481 FLOOR PANEL LANDING SUPPORT HAS SURFACE CORROSION. REMOVED CRACKED SUPPORT. FABRICATED AND INSTALLED IN MAIN CABIN RT FLOOR AREA AT STA 1481 IAW SRM 51-33-01.Apr 23, 2020 · N261UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020060155980Intercostal · cracked3C FWD CARGO COMPARTMENT. LT SIDE BILGE INTERCOSTAL, BETWEEN STATION 6 - 10 AND 6 - 30, UNDERNEATH Z-FRAME HAS A CRACK. REMOVED CRACKED INTERCOSTAL. FABRICATED AND INSTALLED BETWEEN STATION 6 - 10 AND 6 - 30, UNDERNEATH Z-FRAME IAW SRM 51-31-01.Apr 23, 2020 · N261UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020052635671Skin · corrodedINSPECTION TYPE:3CRT AFT FUSELAGE EXTERIOR SKIN HAS CORROSION BETWEEN STA 2140 - 2163.ACCOMPLISH PERMANENT REPAIR ON CORRODED RT AFT FUSELAGE SKIN BETWEEN STA 2140 - 2163 IAW MD-11 SRM 53-70-01 REPAIR 3 FIG 201. (MAJOR)Apr 23, 2020 · N261UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020042454603Charger · defectiveINSPECTION TYPE:N/A** DIVERSION ** LANDED WITHOUT INCIDENT ** AFTER 52 MIN. IN FLIGHT MULTIPLE LVL 1 ALERTS. "BATT CHARGING" @ 52 MIN., 1:45 MIN, 21, 21 MM ALERT REMAINED ILLUMINATED VARIOUS INTERVALS - 6MM - 2MM.REPLACED BATTERY CHARGER PER AMM 24-34-03-400-8Apr 23, 2020 · N289UP · Doug MD11F · Battery/Charger SystemSDR IPXA2020060856294Support · crackedINSPECTION TYPE:3C AFT CARGO BILGE AREA LOWER FRAME SUPPORT HAS A CRACK AT STA 1841 ABOVE LONGERON 43. REMOVED CRACKED FRAME SUPPORT, FABRICATED AND INSTALLED IN AFT CARGO AT STA 1841 ABOVE LONGERON 43 IAW SRM 51-35-01 AND DWG AGA7098. (MINOR)Apr 22, 2020 · N261UP · Doug MD11F · Fuselage Main, FrameSDR IPXA202005265731Bracket · crackedINSPECTION TYPE:3CCAC COMPARTMENT STA 1159 TRUSS BRACKET AT LONGERON 27 RH IS CRACKED IN 2 PLACES.REMOVED CRACKED TRUSS BRACKET, FABRICATED AND INSTALLED BETWEEN STA 1139 AND 1159 AT LONGERON 27 RH IN CAC COMP. IAW MD11 SRM 51-30-01 AND DRAWING AFA7605. (MINORApr 22, 2020 · N261UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2020052645694Intercostal · crackedINSPECTION TYPE:3CCENTER CARGO COMP L/H SIDE INTERCOSTAL UNDER Z-FRAME BETWEEN STA 1761 AND 1781 HAS A CRACK.REMOVED, FABRICATED CRACKED INTERCOSTAL AND INSTALLED IN CETER CARGO LH SIDE UNDER Z-FRAME BETWEEN STA 1761 AND 1781 IAW DRAWING ACA7046 AND AMM 20-50-Apr 22, 2020 · N261UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020051855407Intercostal · crackedINSPECTION TYPE:3CCENTER CARGO COMP MRH INTERCOSTAL UNDER Z-FRAME BETWEEN STA 5-11 AND 5-32 HAS A CRACK AT FWD SIDE.REMOVED, FABRICATED AND INSTALLED INTERCOSTAL IN CENTER CARGO COMP BETWEEN STA 5-11 - 5-32. IAW SRM 51-33-01. (MINOR)Apr 22, 2020 · N261UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020051855406Angle · corrodedINSPECTION TYPE:3CAFT CARGO DOOR JAMB LWR AFT ANGLE SUPPORT IS CORRODED.REMOVED, FABRICATED AND INSTALLED ZEE ANGLES ON AFT CARGO DOOR JAMB IAW SRM 51-31-01. (MINOR)Apr 22, 2020 · N261UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020051155174Intercostal · crackedINSPECTION TYPE:3CCENTER CARGO COMP R/H INTERCOSTAL UNDER Z FRAME BETWEEN STA 5-11 AND 5-32 HAS A CRACK AT FWD SIDE.REMOVED, FABRICATED AND INSTALLED CENTER CARGO COMP R/H INTERCOSTAL BETWEEN STA 5-11 AND STA 5-32 IAW SRM 51-33-01. (MINOR)Apr 22, 2020 · N261UP · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA2020042320770Tire · failedDURING LANDING ROOLOUT, TIRE FAILURE ALERT. #10 TIRE SHOWS 0 PSI. #10 BLOWN ON LANDING. NO OTHER DAMAGE NOTED. REMOVED AND REPLACED #10 TIRE AND #9 TIRE IAW AMM 32-41-01-4. OK FOR SERVICE.Apr 22, 2020 · N575FE · Doug MD11F · TireSDR FDEA2020042320769Tire · failedDURING LANDING ROOLOUT, TIRE FAILURE ALERT. #10 TIRE SHOWS 0 PSI. #10 BLOWN ON LANDING. NO OTHER DAMAGE NOTED. REMOVED AND REPLACED #10 TIRE AND #9 TIRE IAW AMM 32-41-01-4. OK FOR SERVICE.Apr 22, 2020 · N575FE · Doug MD11F · TireSDR IPXA2020061056405Skin · gougedINSPECTION TYPE:3C LT HORZONTAL STAB L/E SKIN IS GOUGED ON O/B SECTION BETWEEN XFS 351.215 AND XFS 357.032. REPAIRED GOUGED LT HORIZONTAL STAB L/E SKIN BETWEEN XFS 351.215 AND XFS 357.032 IAW EA 011-5510-01-A8186 AND EO MD11-5510-76731-A (MAJOR).Apr 21, 2020 · N261UP · Doug MD11F · Horizontal Stabilizer, Plate/SkinSDR IPXA2020061056404Skin · gougedINSPECTION TYPE:3C LT HORIZONTAL STAB L/E SKIN IS GOUGED ON O/B SECTION BETWEEN XFS 351.215 AND XFS 357.032. REPAIRED GOUGED LT HORIZONTAL STAB L/E SKIN BETWEEN XFS 391.933 AND XFS 397.749 IAW EA 011-5510-01-A8186 AND EO MD11-5510-76731-A (MAJOR).Apr 21, 2020 · N261UP · Doug MD11F · Horizontal Stabilizer, Plate/SkinSDR IPXA2020060155981Floorbeam · cracked3C SUB FLOORBEAM AT APPROX STATION 6 - 73, LONGERON 43, LT CORNER IS CRACKED AT ITS ANGLE CHANGE. REMOVED CRACKED SUB FLOORBEAM, FABRICATED AND INSTALLED AT STATION 6 - 73, LONGERON 43 LT IAW SRM 51-31-01.Apr 21, 2020 · N261UP · Doug MD11F · Fuselage Main, Floor BeamSDR IPXA2020052055529Frame · gougedINSPECTION TYPE:2C#3 ENGINE O/B CORE COWL LOWER AFT FRAME IS GOUGED.REMOVED AND REPLACED GOUGED #3 ENGINE O/B CORE COWL LOWER AFT FRAME IAW MD-11 SRM 54-01-42. (MINOR)Apr 21, 2020 · N256UP · Doug MD11F · Engine Cowling SystemSDR IPXA2020051155166Intercostal · crackedINSPECTION TYPE:3CFWD CARGO RT SIDE BILGE INTERCOSTAL BETWEEN STA 6-30 AND 6-50 CRACKED AT AFT UPPER SIDE.REMOVED , FABRICATED AND INSTALLED INTERCOSTAL AT FWD CARGO BETWEEN STA 6-30 AND 6-50 IAW SRM 51-33-01 AND DRAWING ACA7049. ( MINOR)Apr 21, 2020 · N261UP · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA2020042310773Fitting · crackedUPPER FUSELAGE LEFT SIDE STA1401 FILLET PANEL SUPPORT RIB, LOWER CLIP IS CRACKED. REMOVED AND REPLACED LOWER CLIP (ANB7143-11) AT LEFT SIDE STA 1361 REF SRM 51-31- 01-0G.Apr 21, 2020 · N594FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA2020042310772Fitting · crackedUPPER FUSELAGE LEFT SIDE STA 1381 FILLET PANEL SUPPORT RIB, LOWER CLIP IS CRACKED. REMOVED LOWER CLIP (ANB7142-7) CLIP AND INSTALLED NEW FABRICATED ANB7142-7 CLIP REF SRM 51-31-01-0G.Apr 21, 2020 · N594FE · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020042454537Bracket · out of adjustINSPECTION TYPE:N/AUNABLE TO ARM LEFT ENTRY DOOR & SLIDE BEFORE FLIGHTADJUSTED LEFT DOOR FWD ARMING "ARMED" BRACKET PER AMM 25-61-15Apr 21, 2020 · N296UP · Doug MD11F · Emergency EquipmentSDR IPXA2020052645696Support Frame · crackedINSPECTION TYPE:3CR/H WING TO BODY AT STRINGER 31 RH HAS VERTICAL ATTACHMENT SUPPORT FRAME CRACKED.REMOVED, FABRICATED CRACKED SUPPORT FRAME AND INSTALLED AT RH WING TO BODY AT STRINGER 31 IAW DRAWING ANB7143 AND SRM 51-35-01. (MINOR)Apr 20, 2020 · N261UP · Doug MD11F · Aerodynamic FairingsSDR IPXA2020052255603Panel · crackedINSPECTION TYPE:3CL/H UNDERWING BARREL CANTED PANEL CRACKED AT STA X=1236.8 Z=100.ACCOMPLISHED PERMANENT REPAIR OF CRACKED LH UNDERWING BARREL CANTED PANEL AT STA 1236.8 IAW EO.MD11-5310-76331-A REV 05/18/2020. (MAJOR)Apr 20, 2020 · N261UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020052255567Skin · dentedINSPECTION TYPE:2CL/H FUSELAGE SKIN DENT AT STA 337 REQUIRES PERMANENT REPAIR.REPAIRED L/H FUSELAGE SKIN DENT BETWEEN STA 322 - 339 AND BETWEEN Z=-2 - Z=-20 IAW MD-11 SRM 53-00-01, REPAIR 1, FIGURE 201. (MAJOR)Apr 20, 2020 · N256UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020052255626Skin · dentedINSPECTION TYPE:2CRT FUSELAGE SKIN DENT BETWEEN STA 330 - 348 AND Z=-2.9 - Z=9.312 REQUIRES PERMANENT REPAIR.REPAIRED RT FUSELAGE SKIN DENT BETWEEN STA 330 - 348 AND Z=-2.9 - Z=9.312 IAW VT-SAA EA 011-5330-01-A8172 REV IR AND UPS EO MD11-5330-76584-A. (MAJOR)Apr 20, 2020 · N256UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020052255625Skin · dentedINSPECTION TYPE:2CLT FUSELAGE SKIN HAS A DENT AT STA 357 ABOVE Z=-2.9 REQUIRES PERMANENT REPAIR.REPAIRED LT FUSELAGE SKIN DENT BETWEEN STA 339 - 357 ABOVE Z=-2.9 IAW VT-SAA EA 011-5330-01-A8179 REV IR AND UPS EO MD11-5330-76576-A. (MAJOR)Apr 20, 2020 · N256UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020052055526Doubler · crackedINSPECTION TYPE:2CLT WING FIXED L/E BEADED DOUBLER BETWEEN STA XOS 783 - 789 REQUIRES PERMANENT REPAIR.REPAIRED CRACKED LT WING FIXED L/E BEADED DOUBLER BETWEEN STA XOS 783 - 789 IAW MD-11 SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)Apr 20, 2020 · N256UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020052055525Doubler · crackedINSPECTION TYPE:2CLT WING FIXED L/E BEADED DOUBLER BETWEEN STA XOS 879 - 883 REQUIRES PERMANENT REPAIR.REPAIRED CRACKED LT WING FIXED L/E BEADED DOUBLER BETWEEN STA XOS 879 - 883 IAW MD-11 SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)Apr 20, 2020 · N256UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020052055565Skin · dentedINSPECTION TYPE:2CL/H FUSELAGE SKIN DENT AT STA 330 REQUIRES PERMANENT REPAIR.REPAIRED L/H FUSELAGE SKIN DENT BETWEEN STA 322 - 348 AND Z=-30 - Z=-40 IAW MD-11 SRM 53-00-01, REPAIR 1, FIGURE 201. (MAJOR)Apr 20, 2020 · N256UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020052055564Skin · dentedINSPECTION TYPE:2CL/H FUSELAGE SKIN DENT AT STA 283 REQUIRES PERMANENT REPAIR.REPAIRED L/H FUSELAGE SKIN DENT BETWEEN STA 280 - 308 AND BETWEEN Z=5 - Z=22 IAW MD-11 SRM 53-00-01, REPAIR 1, FIGURE 201. (MAJOR)Apr 20, 2020 · N256UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020051855409Longeron · corrodedINSPECTION TYPE:3CRH UPPER WING TO BODY AREA UNDER R3 DOOR AT LONGERON 28 RH HAS CORROSION.REPAIRED LONGERON 28 RH AT STA 1300 IAW EA 011-5300-01-A8170 I/R AND UPS EO MD11-5300-76521-A ( MINOR)Apr 20, 2020 · N261UP · Doug MD11F · Fuselage Main, Longeron/Stringer
Back to Boeing MD-11F