JASC 5753

Service difficulty reports · 31,513

Reports filed under 5753 · Trailing Edge Flaps, 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 = '5753'
  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 FDEA202105051108Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABMay 5, 2021 · N525FE · Doug MD11FSDR FDEA202105051107Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 4May 5, 2021 · N525FE · Doug MD11FSDR FDEA202105051106Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-09. OVERSIZMay 5, 2021 · N525FE · Doug MD11FSDR FDEA202105051105Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 May 5, 2021 · N525FE · Doug MD11FSDR FDEA202105051104Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57May 5, 2021 · N525FE · Doug MD11FSDR FDEA202105051103Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED REPAIR BUSHIMay 5, 2021 · N525FE · Doug MD11FSDR SCNA20210514050Skin · delaminatedLEFT HAND OUTBOARD AFT FLAP INBOARD LOWER CORNER DELAMINATED. REPAIRED DELAMINATION AT INBOARD LOWER CORNER ON LEFT HAND OUTBOARD AFT FLAP PER 737-800 SRM 57-53-01-2R-4 AND SRM 51-70-10-2R-4May 5, 2021 · N815SY · Boeing 7378BKSDR SCNA20210514029Rub Strip · missingLH O/B FWD FLAP WORN WHERE I/B EDGE OF AFT FLAP MAKES CONTACT, AND RUB STRIP MISSING. REPAIRED WORN AREA ON L/H O/B FWD FLAP AT I/B EDGE OF LOWER SURFACE AND REPLACED MISSING RUB STRIP PER EA 57-0062May 5, 2021 · N815SY · Boeing 7378K2SDR SWIA2021062859121Slat Track · chafedLH SLAT TRACK AT 1-3 LOCATION IS CHAFFED ON UPPER AND LOWER SURFACES (C-CHECK RO 6/22/2021) LH SLAT TRACK 1-3 BLENDED AND REPAIRS PER REO 690-57-42-803-REV -- DATE 2021-05-06. ALL STEPS COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS. SKY CARD 51-900-Apr 30, 2021 · N800SK · Cndair CL6002D24SDR SWAA2021062368893Skin · debondedL/H O/B AFT FLAP I/B END LOWER SURFACE HAS A DISBOND / REMOVED AND REINSTALLED L/H O/B AFT FLAP IAW AMM 27-51-22-000-801 AND AMM 27-51-22-400-801 AND PERFORMED FUNCTIONAL TEST ALL TESTS GOOD (POS:L/H O/B; TAG NO:793983; P/N OFF/ON:113A3700-21; S/N OFF/ON:00159Apr 30, 2021 · N938WN · Boeing 7377H4SDR SWIA202158131Skin · dentedRH INBOARD FLAP HAS ONE DENT ON LOWER SKIN, APPROX 13 INCHES IN FROM OUTBOARD EDGE. (FILED CLOSED) REPAIRED DENT TO RH I/B FLAP ON LOWER SKIN, APPROX 13 INCHES IN FROM OUTBOARD EDGE IN REF TO SRM 57-52-00-02, REPAIR 3. / COMPLIED WITH TASK CARD 51-900-1Apr 29, 2021 · N472CA · Cndair CL6002B19SDR SWIA2021072159672Hinge · damagedREMOVE AND INSTALL RT WING OTBD FLAP HINGE BOX ASSY WS178.00, WS220.00 AND WS264.00 TO FOM PER AMM (C-CHECK RO 7/18/2021) REMOVED AND REINSTALLED RT WING OTBD FLAP HINGE BOX'S WS178.00, WS220.00 AND WS264.00 REF. CRJ200 AMM 57-21-37-400-801Apr 26, 2021 · N878AS · Cndair CL6002B19SDR SWIA2021062859111Skin · dented* LH INBD FLAP DENTED ON LOWER SKIN IN MULTIPLE LOCATIONS (MARKED) (C-CHECK RO 6/22/2021) INSTALLED NEW LH INBD FLAP LOWER SKIN INSERT, JOINT STRAPS, AND FILLER IAW CRJ900 SRM 57-52-01-201-005-A01, SPLICE REPAIR FIGURE 57-52-01-995-802 .C/W SKY CARD 51Apr 26, 2021 · N800SK · Cndair CL6002D24SDR SWAA2021060166872Skin · debondedDEBONDED OB AFT FLAP SKIN T/E ON INBOARD EDGE AT LT WING / REPAIRED O/B AFT FLAP SKIN T/E ON INBOARD EDGE AT LT WING ASPER B737-700 SRM 57-53-01-2R-16 REP 16 AND B737-700 SRM 51-70-10-2R-0 REPAIR GENERAL.TOOL USED CALIPER P/N 500-197-30 S/N A18135103 DUE DATE Apr 26, 2021 · N7835A · Boeing 737752SDR SWIA202158290Skin · dentedLEFT WING, INBOARD FLAP LOWER SKIN IN THE WHEEL SPLASH AREA HAS THE APPEARANCE OF DENTING IN MARKED AREAS. (C-CHECK RO 5/20/2021) INSTALLED NEW LOWER SKIN SECTION ON LEFT WING INBOARD FLAP IAW CRJ700 SRM 57-52-01-201-005-A01, SPLICE REPAIR OF FLS75.600 Apr 26, 2021 · N658CA · Cndair CL6002C10SDR SWAA2021051966388Wedge · debondedRH INBD MAIN FLAP OUTBD T/E DISBONDED / REMOVED AND REPLACED R/H INBD MAIN FLAP T/E WEDGE PER SOPM 20-50-02 (SA-M 326 A1303346)Apr 26, 2021 · N8665D · Boeing 7378H4SDR IPXA2021051269329Vane · delaminatedINSPECTION TYPE:3CRT WING I/B FLAP VANE LOWER SURFACE IS DELAMINATED.REPAIRED DELAMINATED RT WING I/B FLAP VANE LOWER SURFACE 3" DIA., 16.34" FROM T/E AND 71.31" FROM I/B END IAW SRM 57-50-80, REPAIR 2, PARA. 4, FIGURE 201, SHEET 4. (MAJOR)Apr 26, 2021 · N265UP · Doug MD11FSDR IPXA2021050569045Vane · delaminatedINSPECTION TYPE:3CLT WING I/B FLAP VANE LOWER SURFACE IS DE-LAMINATED IN 2 AREAS.REMOVED AND REPLACED DE-LAMINATED LT WING I/B FLAP VANE IAW AMM 27-50-22. (MINOR)Apr 26, 2021 · N265UP · Doug MD11FSDR REXA2021050300281Fairing · chafedR/H FLAP STUB FAIRING CHAFED BEYOND REPAIR NEEDS REPLACED. REMOVED AND REPLACED R/H FLAP STUB FAIRING IAW CRJ 200 SRM'S 51-40-11, 51-42-06 AND 51-42-21. Apr 26, 2021 · N924EV · Cndair CL6002B19SDR CALA2021042600550Seal · missingPAX INFORMED US WHEN FLAPS WERE LOWERED ON FINAL A PIECE OF RUBBER CAME OFF LT WING INSPECTED LEFT WING FOR MISSING SEALS. FOUND UPPER SEAL LOCATED NEXT TO OUTBOARD SIDE OF THE INBOARD AILERON MISSING, LOCATED AT APPROX WING STATION 534. REF L/P 6194234 FOR MIApr 26, 2021 · N642UA · Boeing 767322SDR UIEA2021042100954Skin · damagedRT WING OB FLAP UPR SURFACE PREVIOUSLY INSTALLED REPAIR HAS MNULTIPLE DAMAGES AT IB CORNE. (CAUSED BY #9 SPOILER ACTUATOR ROD END FITTING BOLTS)(<P>ACCOMPLISHED FAB NEW DOUBLER, BONDED DOUBLER, TAP TEST, PROTECTIVE TREATMENT, CLEANED, PREPPED AND APPLIED TEFLOApr 25, 2021 · N655GT · Boeing 767205SDR SWIA2021072859770Hinge · chafedR/H OUTBOARD FLAP OUTBOARD HNIGE BOX HAS CHAFE/GOUGE DAMAGE AT THE AFT ATTACHMENT POINT (C-CHECK RO 7/24/2021) REPAIRED R/H OUTBOARD FLAP OUTBOARD HNIGE BOX AT W.S 264.00 CHAFE/GOUGE DAMAGE AT THE AFT ATTACHMENT POINT IAW MHIRJ REO 601R-57-21-3466 REV--Apr 22, 2021 · N909EV · Cndair CL6002B19SDR IPXA2021042968753Structure · corrodedINSPECTION TYPE:C12CORROSION ON UPPER CHORD(P/N:113T2225-5) OF L/H WING INBD MAIN FLAP REAR SPAR NEAR IFS 248.REPAIR I.A.W BOEING SR:4-5057440694 AND UPS EO B767-5750-80191-A.Apr 21, 2021 · N327UP · Boeing 76734AFSDR DALA2021042802442Strut · corrodedSHIP 3244 CORROSION TRAILING EDGE INTERCONNECT STRUT AND ALL ELECTRICAL PLUG BTW IB AND OB FLAP. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT ON RH WING PER A320 AMM 27-51-44. AND REPLACED CONDUIT OF HARNESS 7540VC AND 7542VC ON INTERCONNECTING STRUT. (17Apr 21, 2021 · N344NW · Airbus A320212SDR FDEA202104201259Seal · crackedRH WING OUTBD FLAP OUTBD HINGE XW638 - METAL SEAL CRACKED AT PANEL 636JL. REMOVED AND INSTALLED NEW METAL SEAL PN ARC2148-9 ON ARC2148-504(636JL)FAIRING REF SRM 51-31-01 VOL 2 AND DWG ARC2148Apr 20, 2021 · N316FE · Doug MD1030FSDR SWIA2021080960139Fairing · chafedRH FLAP STUB FARING IS CHAFED AND SEALS ARE WORN (C-CHECK RO 8/5/2021) REMOVED AND REPLACED R/H STUB FAIRING SKIN AND SEALS IAW CRJ200 SRM 51-42-06.Apr 19, 2021 · N693BR · Cndair CL6002B19SDR SWIA202157732Skin · dentedRH INBOARD FLAP LOWER SKIN HAS DENT APPROX. 6" INBOARD OF INBOARD EDGE AND 2" FWD OF TRAILING EDGE. (FILED CLOSED)COMPLIED WITH PERMANENT REPAIR OF THE RH INBOARD FLAP LOWER SKIN 6" INBOARD OF THE INBOARD EDGE AND 2" FWD OF THE TRAILING EDGE IN REFERENCE TApr 18, 2021 · N438SW · Cndair CL6002B19SDR SWIA202157728Skin · dentedRH INBOARD FLAP HAS DENT ON LOWER SKIN APPROX. 12" FROM TRAILING EDGE AND 27" FROM INBOARD EDGE. (FILED CLOSED) COMPLIED WITH THE PERMANENT REPAIR OF THE RH INBOARD FLAP LOWER SKIN APPROX 12" FROM THE TRAILING EDGE AND 27" FROM THE INBOARD EDGE IN REApr 18, 2021 · N438SW · Cndair CL6002B19SDR SWIA2021070759313Skin · chafedTHE R/H INBOARD FLAP LOWER SKIN IS CHAFED WHERE BOTH THE INBOARD AND OUTBOARD CANOE FAIRING SEALS CONTACT IT. (C-CHECK RO 7/5/2021) COMPLIED WITH THE BLENDOUT REPAIR TO THE R/H INBOARD FLAP LOWER SKIN BETWEEN FLAP STA 48.000 AND FLAP STA 64.000 PER REO Apr 16, 2021 · N612QX · Cndair CL6002C10SDR SWIA2021070759312Skin · chafedTHE L/H INBOARD FLAP LOWER SKIN IS CHAFED WHERE THE INBOARD CANOE FAIRING SEAL CONTACTS IT. (C-CHECK RO 7/5/2021) COMPLIED WITH THE BLENDOUT REPAIR TO THE L/H INBOARD FLAP LOWER SKIN BETWEEN FLAP STA 48.000 AND FLAP STA 64.000 PER REO 670-57-52-483 REV Apr 16, 2021 · N612QX · Cndair CL6002C10SDR FDEA202104160938Hinge Fitting · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING FROM INBOARD CCENTRIC HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING FROM INBOARD ECCENTRIC HOLE BORE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS Apr 16, 2021 · N529FE · Doug MD11FSDR FDEA202104160937Hinge Fitting · corrodedRIGHT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04. OVERSIZApr 16, 2021 · N529FE · Doug MD11FSDR FDEA202104160936Hinge Fitting · corrodedLEFT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04. OVERSIZEDApr 16, 2021 · N529FE · Doug MD11FSDR SCNA20210514045Fairing · eroded#1 FWD FLAP FAIRING 544AB, EROSION AT AFT MOUNT HOLES. REPAIRED EROSION AT AFT MOUNT HOLES ON #1 FWD FLAP FAIRING 544AB PER 737-800 SRM 57-53-70-2R-3 TABLE 203 AND SRM 51-70-05-2R-8Apr 15, 2021 · N815SY · Boeing 7378BKSDR SWIA2021090360718Attach Bolt · corrodedL/H OUTBOARD FLAP, OUTBOARD FLAP HINGE LUG LOWER FITTING ATTACH BOLT NUT IS CORRODED. (C-CHECK RO 8/31/21) REMOVED AND REPLACED LH OUTBOARD FLAP, OUTBOARD HINGE LUG LOWER FITTING ATTACH NUT AND WASHER IAW CRJ700 AMM 57-53-27-400-803-A01.Apr 14, 2021 · N703SK · Cndair CL6002C10SDR SWIA2021070159274Bolt · corrodedR/H O/B FLAP ( CENTER HINGE AREA ) O/B SPOILER ACTUATOR MOUNTING BOLT STOP PLATE HARDWARE BOLT CORRODED. (C-CHECK RO 6/29/2021) REMOVED AND REPLACED R/H O/B FLAP(CENTER HINGE AREA) O/B SPOILER ACTUATOR MOUNTING BOLT STOP PLATE HARDWARE IAW CRJ700 AMM RApr 14, 2021 · N656CA · Cndair CL6002C10SDR SWIA2021070159273Bolt · corrodedR/H O/B FLAP O/B HINGE WING MOUNTING HARDWARE ( 4 BOLTS ) ARE CORRODED. (C-CHECK RO 6/29/2021) REMOVED AND INSTALLED 4 EA NEW SERVIEABLE MOUNT BOLTS IN R/H WING OUTBD HINGE BOX FWD ATTACHMENT FITTING IAW CRJ 700 AMM 57-54-02-400-808-A01. REF CONTINUAApr 14, 2021 · N656CA · Cndair CL6002C10SDR SCNA20210514046Fairing · eroded#2 FWD FLAP FAIRING 543AB, EROSION AT AFT MOUNT HOLES. REPAIRED EROSION AT AFT MOUNT HOLES ON #2 FWD FLAP FAIRING 543AB IAW B737 SRM 51-70-05-2R-0Apr 14, 2021 · N815 · Boeing 7378BKSDR 2021F00071Skin · puncturedRRL LH IN-BOARD FLAP DAMAGE REF ENGINEERING MEMO DQ29618M1 RRLApr 14, 2021 · N802QS · Cessna 750SDR U2RA2021041300012Skin · crackedREFER TO NAL LP 44320-3: DURING FLAP OVERSPEED INSPECTION, FOUND DAMAGE TO THE R/H INBD. FORE-FLAP TRAILING EDGE. DAMAGE WAS FOUND TO BE APPROXIMATELY 8" PARALLEL TO THE TRAILING EDGE AND 3" PERPENDICULAR TO THE TRAILING EDGE: DAMAGE FOUND TO EXCEED SERVICEApr 13, 2021 · N702CA · Boeing 747412SDR IPXA2021051069257Skin · puncturedINSPECTION TYPE:SEGR/H WING I/B FLAP LOWER SURFACE HAS A PUNCTURE LOCATED 63.5" FROM I/B SIDE AND 23.5" FROM THE T/EREPAIRED RH I/B FLAP LOWER SURFACE IAW EA# A300-5752-27-A2577Apr 12, 2021 · N133UP · Airbus A300F4622RSDR IPXA2021050368946Skin · dentedINSPECTION TYPE:SEGLH WING CENTER FLAP LE EDGE NOSE SKIN HAS A 6.64" LONG BY 1.850" WIDE BY .400" DEEP DENTACCO,PLISHED REPAIR IAW A300-600 SRM 57-50-00 FIG 208Apr 12, 2021 · N133UP · Airbus A300F4622RSDR FDEA202104120894Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM Apr 12, 2021 · N529FE · Doug MD11FSDR FDEA202104120893Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57 Apr 12, 2021 · N529FE · Doug MD11FSDR FDEA202104120892Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FAApr 12, 2021 · N529FE · Doug MD11FSDR FDEA202104100881Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. Apr 10, 2021 · N529FE · Doug MD11FSDR FDEA202104100879Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMApr 10, 2021 · N529FE · Doug MD11FSDR FDEA202104100878Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57Apr 10, 2021 · N529FE · Doug MD11FSDR FDEA202104100877Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED OVERSIZEDApr 10, 2021 · N529FE · Doug MD11FSDR FDEA202104100876Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE HOLE SURFACE REWORKED AS PER MD-11 CMM 57-44-09 AND FOUND BARREL NUT WALL THICKNESS TApr 10, 2021 · N529FE · Doug MD11F
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