N790FD

Service difficulty reports · 107

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 = 'N790FD' 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 FDEA202104210971Charger · no testL-1 DOOR OVERHEAD EXIT LIGHT DOES NOT ILLUMINATE DURING TEST. REPLACED EMERGENCY LIGHT BATTERY AND POWER SUPPLY ITEM M731 IAW AMM 33-51-07-2. OPS CHECKED EMERGENCY EXITS LIGHTS GOOD IAW AMM 33-51-01-2-0Apr 21, 2021 · N790FD · Boeing 757222 · Emergency LightingSDR FDEA202009172238Skin · delaminatedLT WING OUTBOARD FLAP UPPER TRAILING EDGE PANEL HAS DELAMINATED AREA AT WS 495.Sep 17, 2020 · N790FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA202009172240Skin · delaminatedRT WING OB MAIN FLAP EXTERNAL AREA T/E HAS ONE DENT. UPON FURTHER EVAL FOUND 1/2" DENT DELAMINATED, IAW B757 SRM 51-10-06-2R. ACCOMPLISHED REPAIR ON RT WING O/B MAIN FLAP EXTERNAL AREA T/E AT WS 560-565, IAW B757 SRM 57-53-01-2R REP 1 TABLE III SRM 51-70-07-Sep 17, 2020 · N790FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA202009172239Skin · delaminatedLT WING O/B FLAP UPPER T/E PANEL HAS DELAMINATED AREA AT WS 475. REPAIRED LT WING O/B FLAP UPPER T/E PANEL BY HOT-BONDING REPAIR PLYS, IAW B757 SRM 57-53-01-2R FIG 201 TABLE III AND B757 SRM 51-70-07-06 PARAG 5B AND B757 SRM 51-70-17-0G PARAG 3G AT WS 475.Sep 17, 2020 · N790FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA202009172237Skin · delaminatedLT WING O/B FLAP UPPER T/E PANEL HAS DELAMINATED AREA AT WS 495. REPAIRED LT WING O/B FLAP UPPER T/E PANEL BY HOT-BONDING REPAIR PLYS, IAW B757 SRM 57-53-01-2R FIG 201 TABLE III SRM 51-70-07-0G PAR 5B AND SRM 51-70-17-0G PAR 3G AT WS 495.Sep 17, 2020 · N790FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA202009172236Skin · delaminatedLT WING O/B FLAP UPPER T/E PANEL HAS DELAMINATED AREA AT WS 595. REPAIRED LT WING O/B FLAP UPPER T/E PANEL BY HOT-BONDING REPAIR PLYS, IAW B757 SRM 57-53-01-2R FIG 201 TABLE III SRM 51-70-07-0G PAR 5B AND SRM 51-70-17-0G PAR 3G AT WS 595.Sep 17, 2020 · N790FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA202009142210Skin · crackedMAIN CARGO DOOR FWD VENT DOOR BOX INTERIOR SKIN HAS PROTUDING DENT WITH VISUAL CRACK. REMOVED, FABRICATED, AND REPLACED PANEL ON MAIN CARGO DOOR FWD VENT DOOR BOX INTERIOR SKIN (PANEL), IAW B757 SRM 51-40-02-0G AND B DWG 65-49309, REV D AND REV H.Sep 14, 2020 · N790FD · Boeing 757222 · Cargo/Baggage DoorsSDR FDEA202009122187Seat Track · corrodedMAIN DECK STA 1180 RBL 24.75 SEAT TRACK FLANGE CORRODED. REMOVED CORROSION ON SEAT TRACK FLANGE AT STA 1180, RBL 24.75 IAW B757 SRM 51-10- 02-0G. EVALUATED DAMAGED AREA, ORIG. MAT=.070", REM. MAT= .032" MAT LOSS= .038" FOUND TO BE OUT OF LIMITS, IAW B757 SSep 12, 2020 · N790FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020031740223Battery · dischargedMDIS 790 33-50 3426 24JAN20 GSO FACT U L1 DOOR EXTERIOR EMERGENCY LIGHT AND L1 DOOR INTERIOR EXIT SIGN WON'T ILLUMINATE WHEN EMERGENCY LIGHTS ARE TESTED. R/I 24JAN20 05:26 GSO U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 2013-Jan 24, 2020 · N790FD · Boeing 757222 · Emergency LightingSDR FDEA2018122103587Stator · burnedCLIMBING THROUGH FL390, RIGHT ENGINE FAILED. SHUTDOWN RIGHT ENGINE PER QRH. BEFORE ACCOMPLISHING PROCEDURE CAPTAIN NOTED LACK OF OIL PRESSURE AND FUEL FLOW SHOWED 0 , 0. REPLACED RH ENGINE EEC ALTERNATOR (N2 TRANSDUCER) ROTOR AND STATOR PER AMM 73-21-05-4Dec 20, 2018 · N790FD · Boeing 757222 · Engine (Turbine/Turboprop)SDR FDEA201808232177Skin · delaminatedDISBOND RIGHT OUTBOARD AFT FLAP TRAILING EDGE. REPAIRED THE RT OTBD AFT FLAP TE, HOT-BOND REPAIR IAW SRM 57-53-01- 2R, FIG 201, TABLE II, AND SRM 512R, FIG 201, TABLE II, AND SRM 51-70-04-OG, PARA 6, 4. G, & EA TF-5750 -T0341994, P1.Aug 23, 2018 · N790FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201709022452Light · inoperativeRT EXTERIOR EMERG EXIT LIGHT INOP. FOUND AND CLEANED GROUND TERMINAL AT SLIDE LIGHT L30 AND RELAMPED (MPN 767, NSN BLUB) SAME REF AMM 33-51-06-21 AND TESTED LIGHT SEVERAL TIMES REF AMM 33-51-07-2. RT EMERGENCY SLIDE LIGHT OPS CHECK GOOD SEVERAL TIMES. A/C OK FSep 2, 2017 · N790FD · Boeing 757222 · Emergency LightingSDR FDEA201705271528Mechanism · dirtyL1 DOOR RELEASE LEVER STICKS WHEN CLOSING. EMOVED ACCESS PANEL FROM FUSELAGE FORWARD OF DOOR AND CLEANED DEBRIS FROM HOLD OPEN MECHANISM. LUBED THE HOLD OPEN MECHANISM IAW SMP. HOLD OPEN LATCH OPS CHECKED NORMAL.May 27, 2017 · N790FD · Boeing 757222 · Passenger/Crew DoorsSDR FDEA201705151437Gust Lock · lack of lubeLEFT CREW ENTRY DOOR'S GUSTLOCK DOES NOT RELEASE NORMAL. LUBRICATED THE GUST LOCK, OPS CHECKED GOOD IAW MM 52-11-08-6.May 15, 2017 · N790FD · Boeing 757222 · Passenger/Crew DoorsSDR FDEA201704161224Battery Pack · dischargedRT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED RT EMERGENCY LIGHT BATTERY PACK, REF WDM 33-51-12 AND AMM 33-51-07-2. OPS CHECK GOOD.Apr 16, 2017 · N790FD · Boeing 757222 · Emergency LightingSDR FDEA201704161205Battery Pack · dischargedRT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED RT EMERGENCY LIGHT BATTERY PACK, REF WDM 33-51-12 AND AMM 33-51-07-2. OPS CHECK GOOD.Apr 16, 2017 · N790FD · Boeing 757222 · Emergency LightingSDR FDEA201703080823Lamp · inoperativeLT EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.Mar 8, 2017 · N790FD · Boeing 757222 · Emergency LightingSDR FDEA201609083144Skin · damagedEXTERIOR SKIN NUMEROUS SMALL NICKS AND SCRATCHES ALONG THE BELLY OF THE AIRCRAFT BETWEEN STRINGER 26 LEFT AND 26 RIGHT AT BODY STATION 680 - 700. STA 680-700 STR 26L-26R EXTERIOR SKIN NUMEROUS SMALL NICKS AND SCRATCHES REMOVED FOUND WITHIN LIMIT AS PER SSep 8, 2016 · N790FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201609083143Skin · damagedEXTERIOR SKIN NUMEROUS SMALL NICKS AND SCRATCHES ALONG THE BELLY OF THE AIRCRAFT BETWEEN STRINGER 26 LEFT AND 26 RIGHT AT BODY STATION 700 - 720. STA 700-720 STR 26L-26R EXTERIOR SKIN NUMEROUS SMALL NICK AND SCRATCHES REMOVED FOUND WITHIN LIMIT AS PER SRM Sep 8, 2016 · N790FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201609083142Skin · damagedEXTERIOR SKIN NUMEROUS SMALL NICKS AND SCRATCHES ALONG THE BELLY OF THE AIRCRAFT BETWEEN STRINGER 26 LEFT AND 26 RIGHT AT BODY STATION 720 - 740. STA 720-740 STR 26L - 26R EXTERIOR SKIN NUMEROUS SMALL NICKS AND SCRATCHES REMOVED FOUND WITHIN LIMIT AS PERSep 8, 2016 · N790FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201609063120Skin · chafedLEFT WING INBD MAIN FLAP, INBD NOSE SKIN, FOUND WITH DEEP SPANWISE CHAFING MARK. COMPLIED WITH PART 1 OF EA F--5750-T0326940 TITLE: WINGS - FLIGHT SURFACES - LT WING INBOARD MAIN FLAP ASSY, CHAFE DAMAGE FOUND ON LEADING EDGE SKIN BETWEEN STA 74.00 AND STA 105Sep 6, 2016 · N790FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201608303067Floorbeam · corrodedBS 720, LBL 60 - 62 FLOORBEAM UPPER FLANGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02-0G, REV 118.0 AND FOUND EXCEEDED LIMIT IAW SRM 53-00-51-1A, REV 118.0. COMPLIED WITH EA F-5310-T0327426. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Aug 30, 2016 · N790FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201608283056Angle · corrodedEMPENNAGE AFTER REMOVAL OF APU INLET DOOR FOUND STRAP BETWEEN STA 1787 - 1825 AT S3R WITH CORROSION. STRAP ANGLE R & R WITH NEW ANGLE, PN: 654N0244-620 IAW DWG NR 148N3105, SHT 1, REV C. REPAIR CLASSIFIED AS MAJOR.Aug 28, 2016 · N790FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201608252974Floorbeam · damagedCABIN-STA 324, RBL 15-RBL 30 FOUND 02 EA ELONGATED FASTENER HOLES ON FLOORBEAM WEB. FLOORBEAM WEB REPAIRS COMPLIED WITH. REPAIR CLASSIFIED AS MAJOR.Aug 25, 2016 · N790FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201608252973Floorbeam · damagedCABIN - STA 324, RBL 5-15 FOUND 03 EA ELONGATED FASTERNER HOLES ON FLOORBEAM WEB. FLOORBEAM WEB REPAIR, BETWEEN RBL 4 AND RBL 20 AND BETWEEN RBL 21 AND 29 COMPLIED WITH REPAIR. CLASSIFIED AS MAJOR.Aug 25, 2016 · N790FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201608252972Floorbeam · damagedCABIN, STA 324, RBL 30-70 FOUND SEVERAL ELONGATED FASTENER HOLES ON FLOORBEAM WEB. FLOORBEAM WEB REMOVED IAW SRM 51-40-02-0G, REV 118.0. NEW FLOORBEAM WEB FABRICATED AND INSTALLED IAW DWG 141N2930, SHT 2, REV F AND EA F-5310-T0327532 A PART 1, P1. REPAIR CLAug 25, 2016 · N790FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201608172900Skin · damagedFUSELAGE EXTERIOR SKIN THERE ARE NUMEROUS LIGHTNING STRIKES AT BS 680 - 740 STRINGERS 27 - 28L. COMPLIED WITH EA F-5330-T0327528, PART 1. REPAIR RIVETS AND LIGHTNING DAMAGES ON FUSELAGE SKIN PANEL BETWEEN STA 680-STA 716 AND S-27L-S-28L. REPAIR CLASSIFIED AAug 17, 2016 · N790FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201608152890Spar · gougedHORIZONTAL STAB RIGHT SIDE AUX SPAR BETWEEN RIB 2 & 3 AUX SPAR FOUND ONE DENT WITH A GOUGE. COMPLIED WITH EA F-5510-T0327452. REPAIR CLASSIFIED AS MAJOR.Aug 15, 2016 · N790FD · Boeing 757222 · Horizontal Stabilizer, Spar/RibSDR FDEA201608152888Spar · gougedHORIZONTAL STABILIZER RT SIDE AUXILIARY SPAR BETWEEN RIB 2 & 3. EXISTING REPAIR DOUBLER FOUND WITH 1 EA GOUGE. RT HORIZONTAL STABILIZER AUXILIARY SPAR BETWEEN RIB 2 & 3 EXISTING REPAIR DOUBLER WITH 01 EA GOUGE, COMPLIED WITH EA F-5510-T0327452, PART 1, TITLEAug 15, 2016 · N790FD · Boeing 757222 · Horizontal Stabilizer, Spar/RibSDR FDEA201608032781Seat Track · corrodedSEAT TRACK BOTTOM AT BS 699.5 RBL 24.75, FOUND CORRODED. CORROSION EXCEEDS LIMIT IAW SRM 53-00-52-1A, REV 118.0. SEAT TRACK REMOVED AT STA 699- STA 780, RBL 24.75 IAW SRM 51-40-02-0G, REV 118.0, NEW SEAT TRACK FABRICATED IAW DWG 143N5085, SHT 2, REV B AND INAug 3, 2016 · N790FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201608022754Door Sill · corrodedAFT CARGO COMPARTMENT, STA 1440-1460, 27R CARGO DOOR CUT LOWER SILL WEB CORROSION. SILL WEB R & R WITH NEW FABRICATED LOWER SILL WEB IAW DWG 146N8522, SHT 1, REV E. NEW LOWER SILL WEB FABRICATED IAW DWG 146N8522, SHT 1, REV C. REPAIR CLASSIFIED MAJOR IAW GMAug 2, 2016 · N790FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201608022742Skin · corrodedLEFT WING, AFTER REMOVAL, UPPER SKIN UPPER SURFACE OVERWING FILL PORT CUTOUT FOUND CORRODED AT MATING AREA TO ADAPTER. LT WING AFTER REMOVAL UPPER SKIN SURFACE OVERWING FILL PORT CUTOUT COMPLIED WITH EA F-5730-T0327055 P1. LT WING SKIN UPPER SURFACE CORROSIOAug 2, 2016 · N790FD · Boeing 757222 · Wing, Plate/SkinSDR FDEA201608022739Skin · chafedRIGHT WING-OTBD T/E MAIN FLAP NOSE SKIN LE FOUND CHAULK MARK AT 3" FROM OTBD EDGE. COMPLIED WITH PART 1 OF EA F-5750-T0327084. RT WING OTBD MAIN FLAP ASSY, CHAFE DAMAGE FOUND ON L/E OTBD SKIN WBL 557. REPAIR CLASSIFIED AS MAJORAug 2, 2016 · N790FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201608012698Fitting · corrodedBS 1080 LT CREASE BEAM INNER SPICE FITTING FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02-0G, REV 118.0 AND FOUND EXCEED LIMIT IAW SRM 53-40-12-1A, REV 118.0 FITTING. REMOVED IAW SRM 51-40-02-0G, REV 118.0 AND REPLACED IAW DWG 144N5200, SHT 1, REV B WITHAug 1, 2016 · N790FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201607312684Skin · damagedEXTERIOR SKIN, NUMEROUS SMALL NICKS AND SCRATCHES ALONG THE BELLY OF THE ACFT BETWEEN STR 26 LT AND 26 RT AT BODY STA 620-STA 640. STA 620-STA 640, STR 26L-26R EXTERIOR SKIN NUMEROUS NICKS AND SCRATCHES REMOVED IAW SRM 51-10-02, REV 118. FOUND WITHIN LIMIT IAJul 31, 2016 · N790FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201607302661Web · corrodedBS 960 - 984 LT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02-0G REV 118.0 & FOUND OUT OF LIMITS IAW SRM 53-40-13-1A REV 118.0. CREASE BEAM WEB REMOVED AND REPLACED IAW SRM 51-40-02-0G REV 118.0 AND DWG 144N5140 SHT 3 REV D. REPAIR CLASJul 30, 2016 · N790FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201607302663Web · corrodedBS 1400 - 1420 RIGHT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 118. FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13-1A REV 118. CREASE BEAM WEB REMOVED IAW SRM 51-40-02 REV 118. A NEW CREASE BEAM WEB INSTALLED IAW DWG 146N5590 SHTJul 30, 2016 · N790FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201607302662Shear Web · corrodedBS 960 - 984, RIGHT SHEAR WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 118. FOUND OUT OF LIMITS IAW SRM 53-40-12-1A REV 118. THE SHEAR WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV 118, AND DWG 144N5140 SHT 3 REV D. MAJOR REPAIR.Jul 30, 2016 · N790FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201607282644Seat Track · chafedBS 1460 - 1480 LBL 24.75 SEAT TRACK CROWN CHAFED. SEAT TRACK REPAIR CARRIED OUT BETWEEN STA 1410-1540 LBL 24.75 IAW SRM 53-00-52-2R OPTION 1, REPAIR 1, REV 118.0. REPAIR CLASSIFIED AS MAJOR.Jul 28, 2016 · N790FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607282643Seat Track · chafedBS 1430-1450 LBL 24.75 SEAT TRACK CROWN CHAFED. CHAFE REMOVED IAW SRM 51-10-02-0G REV 118.0. REWORKED AREA MAXIMUM DISTANCE BETWEEN LIPS 0.510" EXCEEDED MAXIMUM LIMT 0.480" IAW SRM 53-00-52-1A, REV 118.0. SEAT TRACK REPAIR CARRIED OUT BETWEEN STA 1410-STA 1Jul 28, 2016 · N790FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201607282642Crease Beam · corrodedBS 982 - 983 LEFT CREASE BEAM INNER ANGLE VERTICAL FLANGE FOUND CORRODED. REMOVED IAW SRM 51-10-02-0G, REV 118.0. REWORKED AREA EVALUATED AND FOUND CORROSION MORE THAN 50 PERCENT THRU EXCEEDED 10 PERCENT LIMIT IAW SRM 53-40-13-1A, REV 118.0 INNER CHORD REMOVJul 28, 2016 · N790FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201607282641Crease Beam · corrodedBS 1360 - 1380 RT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02-0G, REV 118.0. REWORKED AREA EVALUATED ORIGINAL THK 0.040", REMAINING THICKNESS 0.026" AND MATERIAL THICKNESS REMOVED 0.014". FOUND EXCEED 10 PERCENT LIMIT IAW SRM 53-60-Jul 28, 2016 · N790FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201607282640Crease Beam · corrodedBS 1100 - 1120 LEFT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02-06, REV 118.0. ORIGINAL MATERIAL THICKNESS 0.063", REMAINING THICKNESS 0.044" AND MATERIAL THICKNESS REMOVED 0.019". FOUND EXCEEDED 10 PERCENT, LIMIT IAW SRM 53-40-13-1A,Jul 28, 2016 · N790FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201607282639Deck Plate · corrodedBS 1681 LBL 18 AFT DECK PLATE UPPER SURFACE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02-0G, REV 118.0. REWORK AREA ORIGINAL THICKNESS 0.071", REMAINING THICKNESS 0.044" AND MATERIAL THICKNESS REMOVED IS 0.027", FOUND EXCEEDED LIMIT IAW SRM 53-60-51-1Jul 28, 2016 · N790FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201607252611Frame · corrodedAFT CARGO BAY, BS 1380 STRINGER 28L TO 29R FRAME WEB CORRODED. FRAME OUT OF LIMITS. R & R WITH NEW FABRICATED FRAME WEB STR 28R-STR 24L IAW DWG 146N1010, SHT 3, REV C. NEW FRAME WEB FABRICATED IAW DWG NR 146N1028, SHT 09, REV C. REPAIR CLASSIFIED AS MAJOR.Jul 25, 2016 · N790FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201607202550Skin Panel · delaminatedRIGHT WING INBD TE MAIN FLAP INTERIOR UPPER INTERSPAR PANEL LOWER SURFACE FOUND DELAMINATED AT WFS 180. COMPLIED WITH PART 1 EA F-5750-T0327826, TITLE: WING FLIGHT SURFACES SRM REPAIRS ON RT WING INBD MAIN FLAP UPPER BONDED SKIN OUTER & INNER FACESHEETS, STA Jul 20, 2016 · N790FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201607202548Skin · dentedLEFT WING INBD MAIN FLAP UPPER OTBD PANEL UPPER SURFACE FOUND DENTED AND DELAMINATED AT 15" FROM OTBD EDGE, 10" FROM T/E. REPAIR CARRIED OUT IAW SRM 51-70-10-2R, REV 118.0, SEE PART 1 OF EA F-5750-T0327752. REPAIR TO UPPER SKIN PANEL, MULTIPLE REPAIRS TO BONJul 20, 2016 · N790FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201607202546Skin · dentedLEFT WING INBD MAIN FLAP UPPER OTBD PANEL UPPER SURFACE FOUND DENTED AND DELAMINATED AT 59.5-62.5" FROM OTBD EDGE, 6-11" FROM T/E. REPAIR CARRIED OUT IAW SRM 51-70-10-2R, REV 118.0, SEE PART 1 OF EA F-5750-T0327752. REPAIR TO UPPER SKIN PANEL, MULTIPLE REPAIJul 20, 2016 · N790FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201607202542Door Sill · corrodedBS 690 - 730 L2 DOOR CUTOUT LOWER SILL INNER FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02-0G, REV 118.0. REWORKED AREA EVALUATED AND FOUND CORROSION MORE THAN 50 PERCENT THRU, EXCEEDED LIMIT IAW SRM 53-30-15-1A, REV 118.0. INNER CHORD REMOVED BETWEEN SJul 20, 2016 · N790FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201607152459Strap · corrodedEMPENNAGE AFTER REMOVAL OF APU INLET DOOR FOUND STRAP AT BS 1825 BETWEEN S3 - 6R CORRODED. REMOVED FOUND OUT OF LIMIT IAW SRM 53-80-15-1A, FIG 101, TABLE 101, REV 118.0 AND REPAIR CARRIED OUT IAW SRM 53-80-15-2R, FIG 202, DETAIL 1, REV 118.0. REPAIR CLASSIFIJul 15, 2016 · N790FD · Boeing 757222 · Fuselage Miscellaneous Structure
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