# Service difficulty reports: N958FD

A list on [N958FD](https://openairdocs.org/aircraft/N958FD.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 92 reports

- [SDR FDEA202209222359](https://openairdocs.org/sdr/FDEA202209222359.md): Fitting · corroded · Sep 22, 2022 · N958FD · Boeing 757236 · Nacelle/Pylon, Attach Fittings
  > #1 ENGINE PYLON SKIN BOLT INSPECTON NDT FOUND HOLE #1 AND #6 HAS CORROSION IN HOLE. REPAIR OF HOLES #1 AND #6 ACCOMLISHED PER EA F-5730-T0370635 PT1 WINGS - PLATES AND SKINS - LH WING, UPPER SKIN AT DRAG FITTING, CORROSION FINDINGS - EO F-5730-E0340076 R
- [SDR FDEA202209222358](https://openairdocs.org/sdr/FDEA202209222358.md): Fitting · corroded · Sep 22, 2022 · N958FD · Boeing 757236 · Nacelle/Pylon, Attach Fittings
  > #2 ENG PYLON DRAG FITTING HOLE #5 CORROSION INDICATION REPAIR OF HOLE #5 ACCOMPLISHED PER EA F-5730-T0370623 PT1 WINGS - PLATES AND SKINS - RH WING, UPPER SKIN AT DRAG FITTING, CORROSION FINDINGS - EO 5730-E0340076 REV H PT2 MAJOR REPAIR
- [SDR FDEA202110012445](https://openairdocs.org/sdr/FDEA202110012445.md): Support Angle · corroded · Oct 1, 2021 · N958FD · Boeing 757236 · Wing Main, Frame Structure
  > UPON REMOVAL OF LH WING, TRIALING EDGE, UPPER SKIN PANEL, DISCOVERED THE FORWARD LAND AT REAR SPAR HAD CORROSION. STARTED REMOVAL OF CORROSION AT T/E OF LEFT WING UPPER SKIN PANEL, BETWEEN WS 150-180 & WS 194.5 IAW SRM 57-20-01-1A. FOUND CORROSION EXTEND
- [SDR FDEA202012173183](https://openairdocs.org/sdr/FDEA202012173183.md): Stop Fitting · out of rig · Dec 17, 2020 · N958FD · Boeing 757236 · Doors
  > "CABIN ALT" MESSAGE AND LIGHTS AT FL 390 30 MIN AFTER "L EMER DOORS" MESSAGE. RT COMPLIED DESCENT TO 10,000 FT AT AROUND 11,000 FT BOTH MESSAGES EXTINGUISHED. DECLARDED EMERGENCY/DIVERT TO ICT FOUND "LOW INFLOW" ON THE NR 1 CONTROLLER. ICT U FOUND LOWER FO
- [SDR FDEA202012173182](https://openairdocs.org/sdr/FDEA202012173182.md): Sensor · out of alignment · Dec 17, 2020 · N958FD · Boeing 757236 · Emergency Exits
  > "EMER DOORS" OVERHEAD LIGHT. "L EMER DOOR" MESSAGE AT FL 390 30 MIN INTO CRUISE. FOUND FWD SENSOR OUT OF ALIGNMENT. ADJUSTED AND SHIMMED WITH REF TO B757 MM 52-71-00-5. OPERATIONS CHECKED GOOD, AC OK TO CONTINUE.
- [SDR FDEA202012173181](https://openairdocs.org/sdr/FDEA202012173181.md): Stop Fitting · out of rig · Dec 17, 2020 · N958FD · Boeing 757236 · Doors
  > "CABIN ALT" MESSAGE AND LIGHTS AT FL 390 30 MIN AFTER "L EMER DOORS" MESSAGE. QRH COMPLIED DESCENT TO 10,000 FT, AT AROUND 11,000 FT BOTH MESSAGES EXTINGUISHED. DECLARDED EMERGENCY/DIVERT TO ICT. FOUND LOWER FORWARD ADJUSTING STOP PIN OUT OF RIG. ADJUSTED
- [SDR FDEA202010092453](https://openairdocs.org/sdr/FDEA202010092453.md): Power Supply · inoperative · Oct 9, 2020 · N958FD · Boeing 757236 · Emergency Lighting
  > ON AMT PREFLIGHT COURIER AREA, CENTER EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. L1 ADN R1 INTERIOR DOOR, SLIDE LIGHTS AND COCKPIT LIGHTS OPS NORMAL. REF. 757 WDM 33-51-12, DURING T/S FOUND BLOWN FUSE ON POWER SUPPLY BATTERY CHARGER TRAY ASSY SUPPLYING POWE
- [SDR FDEA2020090312080](https://openairdocs.org/sdr/FDEA2020090312080.md): Frame · cracked · Sep 1, 2020 · N958FD · Boeing 757236 · Doors
  > L-3 DOOR UPPER MAIN FRAME CRACKED FROM EDGE TO FASTENER IN RADIUS AT SPLICE END. REMOVED AND REPLACED L-3 DOOR PER EA F-5220-T0356544 P1.
- [SDR FDEA202008292069](https://openairdocs.org/sdr/FDEA202008292069.md): Intercostal · corroded · Aug 29, 2020 · N958FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > AFT CARGO BILGE AREA, CORROSION ON FWD END OF INTERCOSTAL STA 1420 BETWEEN S27L AND S28L. UPON EVAL FOUND TO BE OUT OF ALLOWABLE LIMITS, IAW B757 SRM 53-00-04-1A FIG 101 DETAIL V. REMOVED, FABRICATED, & INSTALLED NEW AFT CARGO BILGE INTERCOSTAL STA 1420 BETW
- [SDR FDEA202009092070](https://openairdocs.org/sdr/FDEA202009092070.md): Floor Support · corroded · Aug 29, 2020 · N958FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > CORROSION IN THE FWD CARGO FLOOR SUPPORT INTERCOSTAL LOWER ATTACH ANGLE, APPROX BS645 LBL 16.5 DOT 129-053. REMOVED, FABRICATED, AND INSTALLED INTERCOSTAL IN FWD CARGO AT BS645 LBL16.5, IAW B757 SRM 51-40-02-0G AND BOEING DWG 143N5367 REV A/REV F. UPON FURTH
- [SDR FDEA2020009092068](https://openairdocs.org/sdr/FDEA2020009092068.md): Floor Support · corroded · Aug 29, 2020 · N958FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > CORROSION IN THE FWD CARGO FLOOR SUPPORT INTERCOSTAL LOWER FLANGE, APPROX BS.738 RBL 7.5 DOT 129-047. REMOVED CORROSION ON INTERCOASTAL, APPROX STA 738 RBL 7.5 IAW B757 SRM 51-10-02-0G. UPON EVAL FOUND INTERCOASTAL TO BE WRONG MATERIAL, IAW BOEING DWG 143N53
- [SDR FDEA2020083192070](https://openairdocs.org/sdr/FDEA2020083192070.md): Floor Support · corroded · Aug 29, 2020 · N958FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > CORROSION IN THE FWD CARGO FLOOR SUPPORT INTERCOSTAL LOWER ATTACH ANGLE, APPROX BS645 LBL. 16.5 DOT 129-053 REMOVED FABRICATED AND INSTALLED INTERCOSTAL IN FWD CARGO AT BS645 LBL16.5 IAW B757 SRM 51-40-02-0G AND BOEING DWG 143N5367 REV A / REV F. UPON FUR
- [SDR FDEA2020083192069](https://openairdocs.org/sdr/FDEA2020083192069.md): Intercostal · corroded · Aug 29, 2020 · N958FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > AFT CARGO BILGE AREA, CORROSION ON FWD END OF INTERCOSTAL STA 1420 BETWEEN S27L AND S28L. UPON EVAL FOUND TO BE OUT OF ALLOWABLE LIMITS IAW B757 SRM 53-00-04-1A FIG 101 DETAIL V. REMOVED FABRICATED & INSTALLED NEW AFT CARGO BILGE INTERCOSTAL STA 1420 BTWN
- [SDR FDEA2020083192068](https://openairdocs.org/sdr/FDEA2020083192068.md): Floor Support · corroded · Aug 29, 2020 · N958FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > CORROSION IN THE FWD CARGO FLOOR SUPPORT INTERCOSTAL LOWER FLANGE, APPROX BS.738 RBL.7.5 DOT 129-047 REMOVED CORR ON INTERCOASTAL APPROX STA 738 RBL7.5 IAW B757 SRM 51-10-02-0G. UPON EVAL FOUND INTERCOASTAL TO BE WRONG MATERIAL IAW BOEING DWG 143N5367 REV
- [SDR FDEA202008221984](https://openairdocs.org/sdr/FDEA202008221984.md): Angle · corroded · Aug 22, 2020 · N958FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > MAIN CABIN L/H CUSP WEB ANGLE (MOP SILL) UPPER SURFACE HAS CORROSION AT BS 1623. REMOVED CORROSION AT MAIN CABIN L/H CUSP WEB ANGLE MOP SILL (CREASE BEAM)IAW B 757 SRM 51-10-02-OG.EVALUATED AREA ORIGINAL MAT.070" MAT REM.061",MAT LOSS.009" FOUND TO BE O
- [SDR FDEA202004080719](https://openairdocs.org/sdr/FDEA202004080719.md): Unknown · malfunctioned · Apr 8, 2020 · N958FD · Boeing 757236 · Cabin Pressure Control System
  > CRZ FL340, CABIN ALTITUDE WARNING. CABIN APPROX 10,000FT WITH APPROX 200FPM CLIMB, DIFFERENTIAL 6.4 DESCENDED TO FL320 NO HELP DUCT PRESSURE OVER 40PSI. DECDEN
- [SDR FDEA201909142241](https://openairdocs.org/sdr/FDEA201909142241.md): Governor · faulty · Sep 14, 2019 · N958FD · Boeing 757236 · Turbine Governor
  > PDIS 958 72-00 6611 14SEP19 TLH OPEN U LOGPAGES: 3112691 DURING TAKEOFF RIGHT ENGINE DID NOT REACH FULL POWER. LEFT ENGINE 1.6 EPR RIGHT ENGINE 1.3 EPR. AFTER TAKEOFF RIGHT ENGINE REMAINED AT REDUCED POWER UNTIL LANDING. RIGHT POWER MATCHED LEFT AT SE
- [SDR FDEA201909032083](https://openairdocs.org/sdr/FDEA201909032083.md): Battery · out of position · Sep 3, 2019 · N958FD · Boeing 757236 · Emergency Lighting
  > DURING SERVICE CHECK FOUND EMERGENCY LIGHT ABOVE R1 DOOR AND EXTERIOR R1 DOOR LIGHT INOP. PROPERLY INSTALLED BATTERIES IN BOTH FWD CHARGER UNITS M730, M731 PER MM 33-51-07-2. FWD LEFT AND RIGHT EMERG LIGHTS CHECK NORMAL PER MM 33-51-00-5.
- [SDR FDEA201811103173](https://openairdocs.org/sdr/FDEA201811103173.md): Light · inoperative · Nov 10, 2018 · N958FD · Boeing 757236 · Emergency Lighting
  > L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED THE L1 SLIDE LIGHT, OPS CHECK GOOD IAW AMM 33-51-06-2-1.
- [SDR FDEA2018082182124](https://openairdocs.org/sdr/FDEA2018082182124.md): Floor Support · cracked · Aug 18, 2018 · N958FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BS 325 TO 345, LBL 2 WAS CRACKED IN AFT LWR CORNER. FABRICATED A REPLACEMENT FLOOR SUPPORT IAW DWG 141N5150, REV BN.
- [SDR FDEA2018081422018](https://openairdocs.org/sdr/FDEA2018081422018.md): Floorbeam · corroded · Aug 12, 2018 · N958FD · Boeing 757236 · Fuselage Main, Floor Beam
  > CORROSION PREVIOUS REPAIR IN THE MAIN CABIN WET AREA FLOOR BEAM UPPER SURFACE,BS.345 BETWEEN RBL. 5.0 TO LBL. 7.5. REMOVED THE EXISTING REPAIR IAW SRM 51-40-02-0G, FABRICATED, HEAT TREATED AND INSTALLED A NEW REPAIR IAW SRM 53-00-51-2R.
- [SDR FDEA2018081422019](https://openairdocs.org/sdr/FDEA2018081422019.md): Seat Track · corroded · Aug 12, 2018 · N958FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON THE MAIN CABIN FWD WET AREA SEAT TRACK, UPPER SURFACE, BETWEEN BS 345 TO 365, RBL 14.50. FOUND TO BE OUT OF LIMITIS IAW SRM 53-00-52. REMOVED THE SEAT TRACK, FABRICATED A REPLACEMENT SEAT TRACK IAW DWG 3504-NC-2. INSTALLED THE NEW SEA
- [SDR FDEA201805261324](https://openairdocs.org/sdr/FDEA201805261324.md): Transceiver · malfunctioned · May 26, 2018 · N958FD · Boeing 757236 · Ground Proximity System
  > CAPTAINS RADAR ALT BREAKS LOCK REPEATLY DURING CLIMB AND DECSENT THROUGH APPROX FL 200. REMOVED AND REPLACED THE LEFT RADIO ALTIMETER TRANSCEVER IAW MM 34-33-01-4. COMPLETED MCDP TEST 30/40 WITH NO FAULTS. IAW 22-00-02-2. OK FOR SERVICE.
- [SDR FDEA201805241314](https://openairdocs.org/sdr/FDEA201805241314.md): Indicator · malfunctioned · May 24, 2018 · N958FD · Boeing 757236 · Trailing Flap Position Indicating System
  > DURING APPROACH AFTER F/O CALLED FLAPS 15, NOTICED A SPLIT IN THE FLAP INDICATOR WITH RIGHT NEEDLE AT FLAP 1 AND LEFT NEEDLE AT FLAP 15. DISCONTINUED APPROACH. NO EICAS OR OTHER INDICATIONS OF A FLAP PROBLEM. F/O SAID THERE WAS NO LATERAL CONTROL ISSUES HE COU
- [SDR FDEA201804070906](https://openairdocs.org/sdr/FDEA201804070906.md): Indicator · malfunctioned · Apr 7, 2018 · N958FD · Boeing 757236 · Trailing Flap Position Indicating System
  > NOTED FLAP ASSYMETRY WHEN FLAPS 30 SELECTED. ONE FLAP REMAINED AT 20. FLAPS CAME UP TOGETHER DURING GO-AROUND. FLAPS CAME DOWN NORMALLY FOR SUBSEQUENT LANDING. NO EICAS OR STATUS MESSAGE NOTED. EMERGENCY DECLARED. REMOVED AND REPLACED FLAP POSITION INDIC
- [SDR FDEA201803130673](https://openairdocs.org/sdr/FDEA201803130673.md): Gear · broken · Mar 13, 2018 · N958FD · Boeing 757236 · Passenger/Crew Doors
  > DURING PREFLIGHT FOUND L1 LOCKING OPEN MECHANISM GEAR BROKE, DOOR OPENS AND CLOSES NORMALLY, LOCKING CLOSED MECHANISM GOOD. REMOVED AND REPLACED THE L1 DOOR HOLD OPEN LOCK IAW AMM 52-11-08-4-0. OPS CHECKED NORMAL. ACFT OK FOR SERVICE.
- [SDR FDEA201703180956](https://openairdocs.org/sdr/FDEA201703180956.md): Fseu · malfunctioned · Mar 18, 2017 · N958FD · Boeing 757236 · Trailing Edge Flap Control System
  > DURING ARRIVAL, AT SELECTION OF FLAPS TO 20, ONE FLAP POINTER REMAINED AT 15 WHILE OTHER CONTINUED TO 20. NO EICAS MESSAGE OR TRAILING EDGE LIGHT ILLUMINATED. LANDING EXECUTED AT FLAPS 20. DURING APPROACH BOTH POINTERS RESET TO 20. UNEVENTFUL LANDING AND R
- [SDR FDEA201409182663](https://openairdocs.org/sdr/FDEA201409182663.md): Skin · corroded · Sep 18, 2014 · N958FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE SKIN HAS AN AREA OF CORROSION AT BS 535 BL 0 UNDER ATC ANTENNA AREA. REPAIRED IAW EA F-5330-T0311516 REV PSP1.
- [SDR FDEA201409172705](https://openairdocs.org/sdr/FDEA201409172705.md): Skin · delaminated · Sep 17, 2014 · N958FD · Boeing 757236 · Trailing Edge Flaps
  > RIGHT WING TE AFT FLAP TAPS DELAMINATION ON LOWER SURFACE, APPROX WING STATION 537, AFT OF NR 11 SPOILER BOARD. REMOVED DAMAGE, DIMENSION 6 X 6, SANDED, CLEANED, PREPPED RT WING AFT FLAP, APPLIED REPAIR, PRIMED & TOP COATED AREA ALL IAW SRM 51-70-17, 51-20-01
- [SDR FDEA201409172638](https://openairdocs.org/sdr/FDEA201409172638.md): Seat Track · corroded · Sep 17, 2014 · N958FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT COURIER AREA SEAT TRACK IS CORRODED BS 345 - 378. REMOVED, FABRICATED & INSTALLED NEW SEAT TRACK IAW SRM 51-40-02, 51-20-01 DWG 3504-NC-2.
- [SDR FDEA201409042454](https://openairdocs.org/sdr/FDEA201409042454.md): Charger · failed · Sep 4, 2014 · N958FD · Boeing 757236 · Emergency Lighting
  > R1 DOOR INTERIOR & EXTERIOR EMER LIGHTS INOPERATIVE. R & R FWD EMER BATTERY & CHARGER IAW MM 33-51-07-2. ACFT OK TO CONTINUE.
- [SDR FDEA201407291997](https://openairdocs.org/sdr/FDEA201407291997.md): Battery Pack · discharged · Jul 29, 2014 · N958FD · Boeing 757236 · Emergency Lighting
  > R1 DOOR EMER EXIT SIGN WILL ONLY ILLUMINATE FOR A FEW SECONDS ON PREFLIGHT TEST. R & R R1 DOOR EMER SIGN BATTERY PACK IAW MM 33-51-07-2. OPERATIONS CHECKED NORMAL OK FOR SERVICE.
- [SDR FDEA201312142983](https://openairdocs.org/sdr/FDEA201312142983.md): Unknown · malfunctioned · Dec 14, 2013 · N958FD · Boeing 757236 · Landing Gear Brake System
  > PARKED AT GATE, SET PARKING BRAKE, PARKING BRAKE SHOWED ON EICAS. ACFT ROLLED FWD ANYWAY. SET PARKING BRAKE SEVERAL TIMES, FUNCTIONS NORMAL. PERFORMED ADJUSTMENT TEST IAW 757-200 MM 32-44-00-5. OPERATIONS CHECKED OK, NO HISTORY, OK FOR SERVICE.
- [SDR FDEA201306181334](https://openairdocs.org/sdr/FDEA201306181334.md): Control Rod · loose · Jun 18, 2013 · N958FD · Boeing 757236 · Emergency Equipment
  > L1 DOOR ARMED KNOCKER LOOSE. REMOVED & REPLACED AND ADJUSTED L1 DOOR RETRACTABLE DOOR MECHANISM ROD ASSY IAW MM 52-11-20-5. OP'S CHECKED NORMAL.
- [SDR FDEA201211144021](https://openairdocs.org/sdr/FDEA201211144021.md): Switch · arced · Nov 14, 2012 · N958FD · Boeing 757200 · Exterior Lighting
  > BURNING RUBBER ODOR AT INITIAL POWER UP ON TAXI OUT. THEN ON TAKE OFF ROLL. ODOR GOES AWAY IN ABOUT 10 SECONDS. TURNED ON ALL EXTERIOR LIGHTS. DETECTED A BURNING ODOR. TURNED OFF LIGHTS WOULD DIMINISH THE ODOR. PULLED DOWN LIGHT OVERRIDE PANEL, AND NOTI
- [SDR FDEA201211144015](https://openairdocs.org/sdr/FDEA201211144015.md): Switch · arced · Nov 14, 2012 · N958FD · Boeing 757236 · Light System Wiring
  > BURNING RUBBER ODOR AT INITIAL POWER UP ON TAXI OUT. ON TAKEOFF ROLL, ODOR GOES AWAY IN ABOUT 10 SECONDS. ODOR BOTH TIMES WAS WITH THE APU OFF. RAN BOTH ENGINES AT THE GATE AND ISOLATED THE APU AND RAN WITH ONE PACK AT A TIME, AND THEN WITH BOTH PACKS
- [SDR FDEA201210173655](https://openairdocs.org/sdr/FDEA201210173655.md): Web · corroded · Oct 17, 2012 · N958FD · Boeing 75728A · Wing, Center Box
  > LEFT WING CENTER TANK FUEL QTY HARNESS FEED THRU JUST OTBD OF WBL 79.50 ON L/E SPAR CORRODED. COMPLIED WITH EA F-5710-162408 (WING-SPAR WEB CORROSION AT FUEL GAUGE CONNECTOR). CAT "A" REPAIR REF: FAA FORM 8100-9. CORROSION WAS DETERMINED TO BE OUT OF LIMITS
- [SDR FDEA201209263467](https://openairdocs.org/sdr/FDEA201209263467.md): Spar · corroded · Sep 26, 2012 · N958FD · Boeing 757236 · Wing Spar
  > LT OTBD MAIN FLAP FRONT SPAR AFT FACE CORRODED AT APPROX WS 600. COMPLIED WITH EA F-5750-162538, MAJOR REPAIR.
- [SDR FDEA201209253440](https://openairdocs.org/sdr/FDEA201209253440.md): Crease Beam · corroded · Sep 25, 2012 · N958FD · Boeing 757236 · Fuselage Main, Structure
  > SURFACE CORROSION AROUND FASTENERS ON LT OTBD CREASE BEAM REPAIR ANGLE BS 1500-1520 AT BS 1460-1540, STR 17L. REPAIRED IAW EA 757-5361-16-F3872. MAJOR REPAIR.
- [SDR FDEA201209213386](https://openairdocs.org/sdr/FDEA201209213386.md): Spar · corroded · Sep 21, 2012 · N958FD · Boeing 757236 · Wing Spar
  > RT AFT WING SPAR WEB SURFACE BOTTOM SURFACE HAS CORROSION AT IRSS 183. COMPLIED WITH EA F-5710-162544-WINGS-MAIN FRAME-OUTER TANK-REAR SPAR CORROSION IRSS 183.0. RTS (AFT BOOST PUMP) REF FAA FORM 8100-9. MAJOR REPAIR.
- [SDR FDEA201209123303](https://openairdocs.org/sdr/FDEA201209123303.md): Skin · damaged · Sep 12, 2012 · N958FD · Boeing 757236 · Fuselage Main, Plate/Skin
  > TCAS ANTENNA STRUCTURE, EXTRANEOUS FASTENER HOLES IN SKIN BETWEEN BS 418 AND 439, STR 1 TO 2R. REPAIRED IAW EA 757-5311-16-F3842, REV. MAJOR REPAIR.
- [SDR FDEA201208213096](https://openairdocs.org/sdr/FDEA201208213096.md): Seat Track · damaged · Aug 21, 2012 · N958FD · Boeing 757236 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO TRACK BS 440- 640, RBL 24 HAS SEVERAL NICKS, GOUGES, SCRATCHES AND CORROSION. EVALUATED GOUGED FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL I. R & R SEAT TRACK IAW SRM 51-40-02 AND DWG 143N5080. MAJOR REPAIR.
- [SDR FDEA201208203086](https://openairdocs.org/sdr/FDEA201208203086.md): Skin · damaged · Aug 20, 2012 · N958FD · Boeing 757236 · Passenger/Crew Doors
  > L4 DOOR FWD EDGE EXTERIOR SKIN IS DEFORMED APPROX ABOUT TWO INCHES OPPOSITE OF DOOR FWD STOP FITTING NR 3. REPAIRED ON 48208890001 AND EA 757-5210-16-F3857, REV -.
- [SDR FDEA201208183073](https://openairdocs.org/sdr/FDEA201208183073.md): Stringer · damaged · Aug 18, 2012 · N958FD · Boeing 757200 · Fuselage Main, Longeron/Stringer
  > STRINGER HAS SEVERAL FASTENERS HOLES BLOWN OUT (DAMAGED) BETWEEN STA 1640-1661, STR 4L. REMOVED STRINGER FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03, NOTE A, FIG 101 PAGE 101. INSTALLED NEW STRINGER IAW SRM 53-00-03 FIG 201 (SHEET 1 OF 8) REPAIR 2 PA
- [SDR FDEA201208173065](https://openairdocs.org/sdr/FDEA201208173065.md): Stringer · damaged · Aug 17, 2012 · N958FD · Boeing 757200 · Fuselage Main, Longeron/Stringer
  > SEVERAL FASTRNER HOLES DAMAGED & CRACKED BETWEEN BS 1640-1661, STR 4R. REPAIRED STRINGER IAW SRM 53-00-03, FIG 201, REPAIR 2. CATEGORY A REPAIR.
- [SDR FDEA201208163031](https://openairdocs.org/sdr/FDEA201208163031.md): Rib · corroded · Aug 16, 2012 · N958FD · Boeing 757200 · Wing, Rib/Bulkhead
  > RT WING AT STATION 806.50, AILERON B. WIRE ATTACHMENT POINT CORRODED. REMOVED CORROSION IAW SRM 51-10-02, CHECKED LIMITS ORIGINAL MATERIAL.070, MATERIAL REMAINING.040, MATERIAL LOSS.030. FOUND OUT OF LIMITS IAW SRM 57-51-09, PG 106, DETAIL IV, FIG.101.
- [SDR FDEA201208163034](https://openairdocs.org/sdr/FDEA201208163034.md): Beam · dented · Aug 16, 2012 · N958FD · Boeing 757236 · Fuselage Main, Structure
  > AFT CARGO DOOR LOWER SUPPORT EDGE BEAM HAS MULTIPLE DENTS. CHECKED LIMITS LOWER EDGE BEAM BS 1380 -1440 FOUND TO BE OUT OF LIMITS IAW SRM 52-30-02, R & R LOWER EDGE BEAM, IAW SRM 51-40-02 AND DWG 146N6603.
- [SDR FDEA201208163026](https://openairdocs.org/sdr/FDEA201208163026.md): Spar Cap · corroded · Aug 16, 2012 · N958FD · Boeing 757200 · Wing Spar
  > CORROSION ON LT WING REAR SPAR UPPER ANGLE AT WS 160, ALSO BETWEEN ANGLE AND SKIN. REPAIRED IAW EA F-5710-162424. MAJOR REPAIR.
- [SDR FDEA201208132974](https://openairdocs.org/sdr/FDEA201208132974.md): Frame · gouged · Aug 13, 2012 · N958FD · Boeing 757200 · Fuselage Main, Frame
  > FRAME BS1280 S11 - 14R, DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, DETAIL II FIG 101 SH. 3. INSTALLED NEW FRAME REPAIR IAW SRM 51-40-02 AND SRM 53-00-07 REPAIR 3, DETAIL II, FIG 201, SHEET 3. MAJOR REPAIR
- [SDR FDEA201208112951](https://openairdocs.org/sdr/FDEA201208112951.md): Channel · gouged · Aug 11, 2012 · N958FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > CHANNEL HAS GOUGES AT FRAME BS 1280, S11L. DAMAGE FOUND OUT-OF-LIMITS IAW SRM 53-00-07, FIG 101 DETAIL V. INSTALLED NEW FRAME REPAIR IAW SRM 53-00-07, FIG 201, REPAIR 3.

Next page: https://openairdocs.org/aircraft/N958FD/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N958FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N958FD/reports

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