N920FD

Service difficulty reports · 222

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 = 'N920FD' 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 FDEA201203140935Lamp · inoperativeR1 DOOR SLIDE ILLUMINATION LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.Mar 14, 2012 · N920FD · Boeing 75723A · Emergency LightingSDR FDEA201202160590Shear Tie · damagedON REMOVAL OF AFT PIT NR 2 FLOOR PANEL, SHEAR TIE AT BS 1400 BETWEEN STR 27R AND 29R FOUND TO BE DAMAGED. REMOVED DAMAGED SHEAR TIE IAW SRM 51-40-02. FABRICATED NEW SHEAR TIE IAW SRM 51-30-01, FIG 7 AND DWG 140N2002. INSTALLED NEW PART IAW SRM 51-40-02.Feb 16, 2012 · N920FD · Boeing 75723A · Fuselage Internal Mounting StructureSDR FDEA201201130144Girt Bar · lack of lubeLEFT FWD DOOR WILL NOT ARM SLIDE. LUBED SLIDE MECHANISM L1 DOOR, SLIDED ARMS OPS CHECKED NORMAL, REF MM 52-11-00-0-0.Jan 13, 2012 · N920FD · Boeing 75723A · Emergency EquipmentSDR FDEA201108023065Indicator · reads lowON TAKEOFF ROLL F/O AIRSPEED LAGGED BADLY. INFLIGHT A/S CAME BACK TO MATCH CAPT, THEN SHOWED FAST. EVENTUALLY STABILIZED ABOUT 5KTS FAST ON FINAL. FLUSHED F/O'S PITOT SYSTEM USING AMM 34-11-00-3-0 AND REMOVED AND REPLACED RIGHT HAND ADC PER MM 34-12-01-4-0Aug 2, 2011 · N920FD · Boeing 75723A · Airspeed/Mach IndicatorSDR FDEA201010124018Skin · dentedFUSELAGE SKIN DENTED STA 1340 STR 29R. EVALUATED DENT AND FOUND OUT OF LIMITS DUE TO CROSSING A FRAME IAW SRM 53- 00-01. REMOVED DAMAGED SHEAR TIE, CUT OUT DAMAGED AREA DIMS 3 3/4" X 2 1/4", FABRICATED NEW SHEAR TIE, HEAT TREATED SHEAR TIE TO 7075T-6 CONDIOct 12, 2010 · N920FD · Boeing 75723A · Fuselage Main, Plate/SkinSDR FDEA200908072934Switch · burnedFL 410 '160 MILES FROM ICT SMELLED ELECTRICAL SMOKE IN COCKPIT, AFTER 15 MINUTES SMOKE WENT AWAY. AT 240 ODOR OF SMOKE AGAIN. FOUND LIGHT OVERRIDE SWITCH STUCK. NO ICAS MESSAGES AND NO STATUS MESSAGE, NO C.B. POPPED. COMPLIED WITH FIM 21-00-01 PGS 101 THAug 7, 2009 · N920FD · Boeing 75723A · Flight Compartment LightingSDR FDEA200907152644Wire · brokenAT APPLICATION OF STD TAKEOFF POWER ON TAKE OFF ROLL, RED CONFIG LIGHT AND RED EICAS MESSAGE "SPOILERS" ACCOMPANIED BY WARNING HORN. TAKEOFF ABORTED AT 50KTS. QRH PROCEDURES ACCOMPLISHED FOR BOTH ITEMS. FOUND B-BK WIRE FROM SPOILER HANDLE POSITION SWITCH SJul 15, 2009 · N920FD · Boeing 75723A · Flight Control System WiringSDR FDEA200907142643Relay · malfunctionedAT TAKEOFF POWER, EICAS MESSAGE "SPOILER" (RED MESSAGE) & RED "CONFIG" LIGHT. TAKE OFF ABORTED AT 56KTS. MOVED SPOILER HANDLE FULL-UP. TROUBLESHOT IAW FIM 31-51-00 & WDM 31-51-41. WHEN SPOILERS ACTUATED IN AUTO OR MANUAL NR 5, 6, 7, & 8 SPOILER PANELS DON`Jul 14, 2009 · N920FD · Boeing 75723A · Drag Control SystemSDR FDEA200905271811Window · crackedAT LEVEL FLIGHT 340 CAPTAIN`S WINDOW CRACKED. RETURNED. WINDOW HAD ARCING AT TOP BEFORE WINDOW CRACKED. REMOVED AND REPLACED CAPT'S L1 WINDOW REF MM 56-11-01-4 AND SUPP 56-11-01-4. COMPLETED WINDOW INSTALL (SEALED AND TORQUED) AS PER MM 56-11-01-4. OPS CHMay 27, 2009 · N920FD · Boeing 75723A · Flight Compartment WindowsSDR FDEA200901090109Crease Beam · corrodedMAIN CABIN, STA 1220-1240, RT OTBD CREASE BEAM CHORD HAS CORROSION. COMPLIED REPAIR OF RT OTBD CREASE BEAM STA 1220-1240 IAW EA NR F-5310-123914. MAJOR REPAIR NO FOLLOW-UP REQUIRED.Jan 9, 2009 · N920FD · Boeing 75723A · Fuselage Main, StructureSDR FDEA200812165179Crease Beam · corrodedMAIN CABIN FLOOR SUPPORT, RT CREASE BEAM, INBD CHORD, BS 600-620, HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. CORROSION OUT OF LIMITS PER SRM 53-30-13, DETAIL 2; D=.025". REMOVED AND REPLACED BS 600-620, RBL 63-70, INBD CREASE BEAM WEB, THAT WAS FABRDec 16, 2008 · N920FD · Boeing 75723A · Fuselage Main, StructureSDR FDEA200811184910Angle · crackedLT FUSELAGE FRAME RE-INFORCING ANGLE ( DOUBLER ) HAS A CRACK STA-700, LBL 65 WL-200. REMOVED FRAME RE-INFORCING ANGLE/DOUBLER IAW SRM 51-40-02, RECEIVED NEW ANGLE/DOUBLER AND INSTALLED IAW SRM 51-40-02AND DWG NR 143N1014. MAJOR REPAIR, NO FOLLOW-UP INSP REQUNov 18, 2008 · N920FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200811184909Floorbeam · corrodedCABIN FLOORBEAM, STA 1661, LBL 58 TO RBL 58 HAS CORROSION AT SEVERAL PLACES. REMOVED AND REPLACED FLOORBEAM UPPER CAP AT STA 1661, LBL 58, RBL 58 IAW SRM 51-40-02 MAJOR REPAIR. NO FOLLOW-UP INSP REQUIRED.Nov 18, 2008 · N920FD · Boeing 75723A · Fuselage Main, Floor BeamSDR 08FDEA04910Doubler · crackedLT FUSELAGE FRAME RE-INFORCING ANGLE (DOUBLER) HAS A CRACK BS-700, LBL 65 WL-200. REMOVED FRAME RE-INFORCING ANGLE/DOUBLER IAW SRM 51-40-02, RECEIVED NEW ANGLE/DOUBLER AND INSTALLED IAW SRM 51-40-02 AND DWG NR 143N1014 MAJOR REPAIR. NO FOLLOW-UP INSPECTION RNov 18, 2008 · N920FD · Boeing 75723A · Fuselage Main, FrameSDR 08FDEA04909Floorbeam · corrodedCABIN FLOORBEAM STA 1661, LBL 58 TO RBL 58 HAS CORROSION AT SEVERAL PLACES. REMOVED AND REPLACED FLOORBEAM UPPER CAP AT STA 1661 LABL 58-RBL 58 IAW SRM 51-40-02, MAJOR REPAIR NO FOLLOW-UP INSPECTION REQUIRED.Nov 18, 2008 · N920FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA200811124867Frame · damagedAFTER REMOVAL OF DOUBLER FROM TV MONITOR SPT AT BS 395, S-3L - S-3R, FOUND SEVERAL HOLES ON FRAME. COMPLIED WITH EA 757-2550-16-F1312, REV E, FRAME ALTERATION BS 395, B/T S-3L - S-3R. REMOVED SHEAR TIES AND STRINGER CLIPS PER EA STEP 2A1. REMOVED DAMAGE PNov 12, 2008 · N920FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA200811054763Frame · damagedAFTER REMOVAL OF DOUBLER FROM TV MONITOR SUPPORT AT BS 1000, FOUND SEVERAL HOLES IN FRAME. REMOVED DAMAGED SECTION OF FRAME, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS, BS 1000, S-5L-R, IAW SRM 53-00-07, REPAIR NR 3. THIS REPAIR IS CLASSIFIED AS A CAT.Nov 5, 2008 · N920FD · Boeing 75723A · Fuselage Main, FrameSDR 08FDEA04763Frame · damagedAFTER REMOVAL OF DOUBLER FROM TV MONITOR SUPPORT AT BS 1000, FOUND SEVERAL HOLES IN FRAME. REMOVED DAMAGED SECTION OF FRAME, FABBED REPAIR PARTS AND INSTALLED REPAIR PARTS, BS 1000, S-5L - S-5R, IAW SRM 53-00-07, REPAIR NR 3. THIS REPAIR IS CLASSIFIED AS A CNov 5, 2008 · N920FD · Boeing 75723A · Fuselage Main, FrameSDR 08FDEA04760Skin · corrodedNR 1 PYLON INBD AFT 311N5046-34 SKIN PANEL ASSY HAS CORROSION ON INNER SURFACE. REMOVED AND INSTALLED REPAIRED NR 1 PYLON INBD AFT SKIN PANEL ASSY IAW DWG 311N5002 AND SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKINov 5, 2008 · N920FD · Boeing 75723A · Nacelle/Pylon, Plate/SkinSDR FDEA200811044713Web · damagedNR 2 PYLON CENTER WEB BETWEEN PPS 146-154 HAS HEAT DAMAGE. PREFORMED HARDNESS TEST ON NR 2 PYLON CENTER WEB IAW SRM 51-20-02, FIG 3 AND FOUND TO BE ABOVE LIMITS. COMPLIED WITH F-5450-123904A DATED 09/03/08. THIS IS CAT "A" REPAIR . "MAJOR REPAIR"Nov 4, 2008 · N920FD · Boeing 75723A · Nacelle/Pylon Miscellaneous StructureSDR FDEA200811044712Web · wornNR 2 PYLON UPPER WEB AT PPS 146-154 HAS WORN AREA CAUSED BY LOOSE SUPPORT BRACKETS. BLENDED DAMAGED WORN AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL III COMPLIED WITH EA F-5450-123904A DATED 09/03/08. THIS IS A CAT "A" REPAIR. "Nov 4, 2008 · N920FD · Boeing 75723A · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA04713Web · damagedNR 2 PYLON CENTER WEB BETWEEN PPS 146-154 HAS HEAT DAMAGE. PREFORMED HARDNESS TEST ON NR 2 PYLON CENTER WEB PER SRM 51-20-02 FIG.3 AND FOUND TO BE ABOVE LIMITS. COMPLIED WITH F-5450-123904A DATED 09/03/08. THIS IS CAT "A" REPAIR . "MAJOR REPAIR"Nov 4, 2008 · N920FD · Boeing 757200 · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA04712Web · damagedNR 2 PYLON UPPER WEB AT PPS 146-154 HAS WORN AREA CAUSED BY LOOSE SUPPORT BRACKETS. BLENDED DAMAGED WORN AREA AND FOUND TO BE OUT OF LIMITS PER SRM 54-50-01 FIG. 101 DETAIL III . COMPLIED WITH FED EX E.A. F-5450-123904A DATED 09/03/08. THIS IS A CAT. "A" Nov 4, 2008 · N920FD · Boeing 757200 · Nacelle/Pylon Miscellaneous StructureSDR FDEA200810274585Fitting · mislocatedNR 1 PYLON , WHEN THE 311N5220-52 BATHTUB FITTING WAS LOCATED AND DRILLED C/M TO THE INBD LOWER SPAR 3 EA HOLES WERE MISLOCATED CAUSING A MISALIGNMENT C/M TO THE LWR SPAR. REAMED OTBD HOLE "A" TO 0.3267 DIA. AND INSTALLED 1 EA. BACB30US5K(*) X BOLT. REAMED OTOct 27, 2008 · N920FD · Boeing 75723A · Nacelle/Pylon, Attach FittingsSDR FDEA200810274583Frame · damagedAFTER REMOVAL DOUBLER FROM TV MONITOR SUPPORT AT STA 1320. FOUNDED SEVERAL HOLES ON FRAME. REMOVED DAMAGE AT STA 1320 FROM STR 4L-4R IAW SRM 53-00-07. FABBED ZEE FRAME FROM MAE TRAVELER T8/763299. FABBED SPLICES IAW MAE TRAVELER T8/761975. DRILLED REPAIOct 27, 2008 · N920FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA200810274582Frame · damagedAFTER REMOVAL DOUBLER FROM TV MONITOR SUPPORT AT STA 980 SEVERAL HOLES ON FRAME. REMOVED DAMAGE BETWEEN STR 5L AND 5R IAW SRM 53-00-01 REPAIR NR 3. FABBED NEW ZEE-FRAME REPAIR IAW MAE TRAVELER T8/763340. FABBED NEW SPLICES IAW MAE TRAVELER T8/761973. LOCAOct 27, 2008 · N920FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA200810274581Frame · damagedAFTER REMOVAL DOUBLER FROM TV MONITOR SUPPORT AT STA 800, S-4L- S-4R, FOUND SEVERAL HOLES ON FRAME. REMOVED DAMAGE AT STA 800 FROM STR 4L TO 4R IAW SRM 53-00-07. FABBED NEW ZEE-FRAME IAW MAE TRAVELER T8/763342. FABRICATED NEW SPLICES IAW MAE TRAVELER T8/76Oct 27, 2008 · N920FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA200810274580Frame · damagedAFTER REMOVAL DOUBLER FROM TV MONITOR SUPPORT AT STA 760 FOUND SEVERAL HOLES ON FRAME. REMOVED DAMAGE FRAME STA 760 BETWEEN STR.5R AND 4L IAW 53-00-07. FABRICATED NEW ZEE-FRAME IAW MAE TRAVELER T8/763343. FABRICATED NEW SPLICES IAW MAE TRAVELER T8/76190. Oct 27, 2008 · N920FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA200810274579Skin · damagedEXTERNAL LOWER FUSELAGE SKIN, LIGHTNING STRIKES (2EA) BS500- BS520, STR 28R- 27R. CHECKED LIMITS IAW SRM 53-00-01, FIG 201, REPAIR 6, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 201, REPAIR 16 , FIG 101. REMOVED DAMAGE IAW SRM 50-00-01. REPAIR 16, NFEC COct 27, 2008 · N920FD · Boeing 75723A · Fuselage Main, Plate/SkinSDR 08FDEA04585Spar · misinstalledNR 1 PYLON, WHEN THE 311N5220-52 BATHTUB FITTING WAS LOCATED AND DRILLED C/M TO THE INBD LOWER SPAR 3 HOLES WERE MISLOCATED CAUSING A MISALIGNMENT C/M TO THE LWR SPAR. REAMED OTBD HOLE "A' TO 0.3267 DIA AND INSTALLED 1 BACB30US5K(*) X BOLT. REAMED OTBD HOLE Oct 27, 2008 · N920FD · Boeing 75723A · Nacelle/Pylon, Frame/Spar/RibSDR 08FDEA04583Frame · damagedAFTER REMOVAL DOUBLER FROM TV MONITOR SUPPORT AT STA 1320. FOUNDED SEVERAL HOLES ON FRAME. REMOVED DAMAGE AT STA 1320 FROM STR 4L-4R IAW SRM 53-00-07. FABRICATED ZEE FRAME FROM MAE TRAVELER T8/763299. FABRICATED SPLICES PER MAE TRAVELER T8/761975. DRILLEDOct 27, 2008 · N920FD · Boeing 75723A · Fuselage Main, FrameSDR 08FDEA04582Frame · damagedAFTER REMOVAL DOUBLER FROM TV MONITOR SUPPORT AT STA 980 SEVERAL HOLES ON FRAME. REMOVED DAMAGE BTW STR 5L AND 5R IAW SRM 53-00-01 REPAIR NR 3. FABRICATED NEW ZEE FRAME REPAIR PER MAE TRAVELER T8/763340. FABRICATED NEW SPLICES PER MAE TRAVELER T8/761973. LOct 27, 2008 · N920FD · Boeing 75723A · Fuselage Main, FrameSDR 08FDEA04581Frame · damagedAFTER REMOVAL DOUBLER FROM TV MONITOR SUPPORT AT BS 800, FOUND SEVERAL HOLES ON FRAME. REMOVED DAMAGE AT BS 800 FROM S4R TO 4L IAW SRM 53-00-07. FABRICATED NEW ZEE FRAME PER MAE TRAVELER T8/763342. FABRICATED NEW SPLICES PER MAE TRAVELER T8/761971. DRILLOct 27, 2008 · N920FD · Boeing 75723A · Fuselage Main, FrameSDR 08FDEA04580Frame · damagedAFTER REMOVAL DOUBLER FROM TV MONITOR SUPPORT AT STA 760 FOUND SEVERAL HOLES ON FRAME. REMOVED DAMAGE FRAME STA 760 BTW STR 5R AND 4L IAW 53-00-07. FABRICATED NEW ZEE FRAME PER MAE TRAVELER T8/763343. FABRICATED NEW SPLICES PER MAE TRAVELER T8/76190. TREOct 27, 2008 · N920FD · Boeing 75723A · Fuselage Main, FrameSDR 08FDEA04579Skin · damagedEXTERNAL LOWER FUSELAGE SKIN, LIGHTNING STRIKES BS 500- BS 520 STR 28R- 27R. CHECKED LIMITS IAW SRM 53-00-01 FIGURE 201 REPAIR 6, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIGURE 201 REPAIR 16, FIGURE 101. REMOVED DAMAGE IAW SRM 50-00-01, REPAIR 16, NFEC CUOct 27, 2008 · N920FD · Boeing 75723A · Fuselage Main, Plate/SkinSDR 08FDEA04542Frame · damagedAFTER REMOVAL DOUBLER FROM TV MONITOR SUPPORT FOUNDED SEVERAL HOLES ON FRAME AT STA, 1020 REPAIRED FRAME IAW SRM 53-00-07 REPAIR NR 3, THIS IS A CATEGORY "B" REPAIR WITH THE FOLLOW-UP INSPECTION. HFEC INSPECTION EVERY 12,000 F/C AS GIVEN IN NDT PART. 6 ,51-0Oct 25, 2008 · N920FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA200810244533Frame · damagedAFTER REMOVAL OF DOUBLER FROM TV MONITOR SUPPORT, BS1340, S-4L - S-4R, FOUND SEVERAL HOLES ON FRAME. REMOVED DAMAGE IAW SRM 53-00-07, REPAIR 3. FABRICATED AND INSTALLED REPAIR PARTS AT BS 1340, S-4L - S-4R, IAW SRM 53-00-07, REPAIR 3. REPAIR PARTS FABRICATEOct 24, 2008 · N920FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA200810244532Frame · damagedAFTER REMOVAL OF DOUBLER FROM TV MONITOR SUPPORT, AT BS 1360, FOUND SEVERAL HOLES ON FRAME. REMOVED DAMAGE AT BS 1360, S-4L - S-4R, IAW SRM 53-00-07, REPAIR 3. FABRICATED AND INSTALED REPAIR PARTS, BS 1360, S-4L - S-4R, IAW SRM 53-00-07, REPAIR 3. REPAIR PAROct 24, 2008 · N920FD · Boeing 75723A · Fuselage Main, FrameSDR 08FDEA04329Frame · damagedAFTER REMOVAL OF DOUBLER FROM TV MONITOR SUPPORT, AT BS 1460, S4L TO S4R, FOUND SEVERAL HOLES ON FRAME. REMOVED AND REPLACED FUSELAGE FRAME, BS 1460, S4L TO S4R, IAW SRM 53-00-07. REPAIR PARTS FABRICATED ON MAE TRAVELERS T8/761978, T8/763298. THIS REPAIR IS Oct 13, 2008 · N920FD · Boeing 75723A · Fuselage Main, FrameSDR 08FDEA04325Skin Panel · corrodedNR 2 PYLON I/B AFT SKIN PANEL ASSY HAS CORROSION ON INNER SURFACE. REMOVED AND REPLACED SKIN PANEL ASSY PER DWG 311N5002 AND SRM 51-40-02. CORROSION ON SKIN WAS APPROXIMATELY 80% THROUGH MATERIAL. REPAIRED SKIN WAS RECEIVED ON TAG 031B66. THIS REPAIR IS CLASOct 13, 2008 · N920FD · Boeing 75723A · Nacelle/Pylon, Plate/SkinSDR 08FDEA04262Bulkhead · corrodedCABIN FLOOR , FWD. OF AFT PRESSURE BULKHEAD STA. 1720 .LBL 52 TO RBL 52 HAS CORROSION AT SEVERAL PLACES. REMOVED CORROSION , CHECKED LIMITS ON 6 REWORKED AREAS FOUND ALL 6 AREAS TO BE OUT OF LIMITS IAW SRM 53-00-51. REMOVED DAMAGED PANEL, FABRICATED NEW PREOct 7, 2008 · N920FD · Boeing 75723A · Fuselage Main, BulkheadSDR 08FDEA04255Floorbeam · corrodedMAIN CABIN FLOORBEAM, BS 1320, RBL 12-25, HAS CORROSION. REPAIRED MAIN CABIN FLOORBEAM, BS 1320, RBL 12-25, IAW SRM 53-00-51. CORROSION WAS DETERMINED TO BE OUT OF LIMITS PER SRM 53-00-51. THIS REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOWOct 7, 2008 · N920FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA200810064248Crease Beam · corrodedCREASE BEAM ANGLE FITTING ATTACHMENT AND CHORD HAS CORROSION AT S-17R, BS 520-540. REMOVED AND REPLACED CREASE BEAM ANGLES, 2EA, ANGLE SPLICES, 4EA, AND O/B CHORD IAW MAE TRAVELERS T8/760009, T8/760007, T8/760010 AND EA F-5310-110929, REV-, DATED 10/03/08.Oct 6, 2008 · N920FD · Boeing 757236 · Fuselage Main, StructureSDR 08FDEA04248Crease Beam · corrodedCREASE BEAM ANGLE FITTING ATTACHMENT AND CHORD HAS CORROSION AT S17R, BS 520-540. REMOVED AND REPLACED CREASE BEAM ANGLES, ANGLE SPLICES, AND O/B CHORD IAW MAE TRAVELERS T8/760009, T8/760007, T8/760010 AND EA F-5310-110929. THIS REPAIR IS CLASSIFIED AS A CATEGOct 6, 2008 · N920FD · Boeing 75723A · Fuselage Main, StructureSDR FDEA200810034185Panel · corrodedNR 2 PYLON PNL 443 FR CUT OUT HAS SURFACE CORROSION. BLENDED AREA IAW 54-50-71 CHECKED LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 54-50-71 FIG 101 DETAIL IV. REMOVED MACHINE DOUBLER IAW SRM 51-40-02. REPLACED MACHINE DOUBLER IAW SRM 51-10-02. FABRICATED DOUOct 3, 2008 · N920FD · Boeing 75723A · Nacelle/Pylon, Plate/SkinSDR FDEA200810034182Crease Beam · corrodedMAIN CABIN, STA 1620-1640, RT SIDE INBD CREASE BEAM CHORD HAS CORROSION. REMOVED CORROSION AND CHECK LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-03 FIG 101 DETAIL III. REMOVED CREASE BEAM INBD CHORD, FABRICATED CREASE BEAM INBD CHORD IAW SRM 51-10-02 SECOct 3, 2008 · N920FD · Boeing 75723A · Fuselage Main, StructureSDR 08FDEA04186Crease Beam · corrodedMAIN CABIN CREASE BEAM , BS 663-756 LBL 62 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02, CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13. REMOVED, FABRICATED AND INSTALLED CREASE BEAM IAW SRM 51-40-02 AND DWG 143N5520.Oct 3, 2008 · N920FD · Boeing 75723A · Fuselage Main, StructureSDR 08FDEA04185Doubler · corrodedNR 2 PYLON PANEL 443 FRAME CUT OUT HAS SURFACE CORROSION. BLENDED AREA IAW 54-50-71 FOUND TO BE OUT OF LIMITS IAW SRM 54-50-71. REMOVED MACHINE DOUBLER IAW SRM 51-40-02 REPLACED DOULBER IAW SRM 51-10-02.Oct 3, 2008 · N920FD · Boeing 75723A · Nacelle/Pylon, Plate/SkinSDR 08FDEA04184Seat Track · misalignedMAIN CABIN SEAT TRACK FLANGE 1620-1640, LBL 45 HAS 2 SCREW HOLES ELONGATED. REMOVED DAMAGED SEAT TRACK PER SRM 51-40-02, FABRICATED NEW SEAT TRACK PER MAE TRAVELER T8/752959. LOCATED AND DRILLED PER SRM 51-40-05, TREATED AND PRIMED PER SRM 51-20-01, PAINTED PEOct 3, 2008 · N920FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04183Seat Track · crackedSEAT TRACK BS 1540 LBL 45 FLANGE CRACKED. REMOVED SEAT TRACK PER SRM 51-40-02. RECEIVED NEW SEAT TRACK PER MAE TRAVELER T8/759349. LOCATED AND DRILLED PER SRM 51-40-05, TREATED AND PRIMED PER SRM 54-20-01 ,PAINTED PER SRM 51-21-00-7, AND INSTALLED PER SRM 51-4Oct 3, 2008 · N920FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
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