# Service difficulty reports: N5147A A list on [N5147A](https://openairdocs.org/aircraft/N5147A.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SCNA20260623256](https://openairdocs.org/sdr/SCNA20260623256.md): Smoke Goggles · broken · Jun 20, 2026 · N5147A · Boeing 73783N · Emergency Equipment > CAPTAINS SMOKE GOGGLES BROKEN INSTALLED NEW SMOKE GOGGLES PER AMM 25-64-00 - [SDR SCNA20260623262](https://openairdocs.org/sdr/SCNA20260623262.md): Smoke Goggles · missing · Jun 8, 2026 · N5147A · Boeing 73783N · Emergency Equipment > SMOKE GOGGLES MISSING FROM FWD FLT ATTENDENT SEAT I/B & O/B POS ( SUPERNUMERARY SEATS) INSTALLED 2 MISSING SMOKE GOGGLES IN THE AFT FACING SEAT REFERENCING AMM 25-64-00 THIS CLEARS MEL 25-31 MDDR # 139353 - [SDR SCNA20251230512](https://openairdocs.org/sdr/SCNA20251230512.md): Screw · missing · Dec 29, 2025 · N5147A · Boeing 73783N · Escape Slide > L1 SLIDE COVER MISSING SCREW. INSTALLED SCREW ON L1 SLIDE IAW AMM 25-66-01 - [SDR UIEA2025030400197](https://openairdocs.org/sdr/UIEA2025030400197.md): Cargo Track · corroded · Mar 4, 2025 · N5147A · Boeing 73783N · Fuselage, Seat/Cargo Attach Fittings > FORWARD CARGO COMPARTMENT - FLOOR STRUCTURE STA 500H TO STA 500I LBL17" CARGO TRACK CORRODED AROUND ANCHOR NUTS.(

PERFORMED PERMANENT REPAIR AT TIEDOWN TRACK FROM STA 500G +6" TO STA 500I AT LBL 17 IAW B737-800 BCF SRM 53-00-53-2R-3 REPAIR 3 FIGURE 201. THIS - [SDR UIEA2025030400196](https://openairdocs.org/sdr/UIEA2025030400196.md): Cargo Track · corroded · Mar 4, 2025 · N5147A · Boeing 73783N · Fuselage, Seat/Cargo Attach Fittings > FWD CARGO COMPARTMENT FROM STA 400 TO STA 460 LBL 18.2" TIE DOWN TRACK WITH CORROSION.(

PERFORMED PERMANENT REPAIR AT TIEDOWN TRACK SECTION FROM STA 360 TO STA 500A + 15 INCH AT LBL18.2 IAW B737-800 BCR SRM 53-00-53-2R-3 REPAIR 3 FIGURE 201. THIS REPAIR IS C - [SDR UIEA2025030400195](https://openairdocs.org/sdr/UIEA2025030400195.md): Channel · corroded · Mar 4, 2025 · N5147A · Boeing 73783N · Fuselage Miscellaneous Structure > FWD CARGO COMPARTMENT FROM STA 420 TO STA 500D LBL 24" ZEE CHANNEL WITH CORROSION INCLUDING SPLICE AREA AND AROUND ANCHOR NUTS.(

PERFORMED PERMANENT REPAIR AT SIDE PLATE SUPPORT ZEE FROM STA 360 TO STA 500I IAW B737-800 BCF SRM 53-00-53-2R-6 REPAIR 6 FIGURE - [SDR UIEA2025030400194](https://openairdocs.org/sdr/UIEA2025030400194.md): Stringer · corroded · Mar 4, 2025 · N5147A · Boeing 73783N · Fuselage Main, Longeron/Stringer > FWD CARGO COMPARTMENT FROM STA 500C+5" TO STA 500F STRINGER 28LH WITH CORROSION AROUND SOLID RIVETS DRIVEN HEAD.(

PERFORMED PERMANENT REPAIR AT STRINGER 28LH FROM STA 500A + 1 INCH TO STA 500E + 21 INCH IAW B737-800BCF SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206, - [SDR UIEA2025030400193](https://openairdocs.org/sdr/UIEA2025030400193.md): Stringer · corroded · Mar 4, 2025 · N5147A · Boeing 73783N · Fuselage Main, Longeron/Stringer > FWD CARGO COMPARTMENT FROM STA 500+12" AND FROM STA 500C + 12" TO STA 500F STRINGER 26LH WITH CORROSION AROUND SOLID RIVETS DRIVEN HEAD.(

PERFORMED PERMANENT REPAIR AT STRINGER 26L FROM STA 500 +6" TO STA 500 +19" IAW B737-800 BCF SRM 53-00-03-02-1 REPAIR 1 - [SDR UIEA2025030400192](https://openairdocs.org/sdr/UIEA2025030400192.md): Floor Support · corroded · Mar 4, 2025 · N5147A · Boeing 73783N · Fuselage Miscellaneous Structure > FWD CARGO COMPARTMENT STA 495 LBL 8.10" CARGO FLOOR BEAM WITH CORROSION AROUND ANCHOR NUTS.(

PERFORMED PERMANENT REPAIR AT FLOOR SUPPORT CHANNEL ON FWD CARGO COMPARMENT FROM STA 480 + 6" TO STA 500 + 15", LBL8.10 IAW B737-800 BCF SRM 53-00-53-2R-4 REPAIR 4 P - [SDR UIEA2025030400191](https://openairdocs.org/sdr/UIEA2025030400191.md): Floor Support · corroded · Mar 4, 2025 · N5147A · Boeing 73783N · Fuselage Miscellaneous Structure > FWD CARGO COMPARTMENT STA 495 RBL 8.10" CARGO FLOOR BEAM WITH CORROSION AROUND ANCHOR NUTS.(

PERFORMED PERMANENT FLOOR SUPPORT CHANNEL REPAIR AT FWD CARGO COMPARTMENT FROM STA 480 +6" TO STA 500 +15" AT RBL 8.10" IAW B737-800 SRM BCF 53-00-53-2R-4 REPAIR 4 P - [SDR UIEA2025030400190](https://openairdocs.org/sdr/UIEA2025030400190.md): Cargo Track · corroded · Mar 4, 2025 · N5147A · Boeing 73783N · Fuselage, Seat/Cargo Attach Fittings > FORWARD CARGO COMPARTMENT - FLOOR STRUCTURE FROM STA 460 TO STA 500 AND STA 500H TO STA 500I RBL13" CARGO TRACK CORRODED AROUND ANCHOR NUTS.(

PERFORMED PERMANENT REPAIR AT TIEDOWN SECTION FROM STA 360 TO STA 500B +15" AND FROM STA 500G +6" TO STA 500I IAW B7 - [SDR UIEA2025030400189](https://openairdocs.org/sdr/UIEA2025030400189.md): Stringer · corroded · Mar 4, 2025 · N5147A · Boeing 73783N · Fuselage Main, Longeron/Stringer > FWD CARGO COMPARTMENT FROM STA 500B+12" TO STA 500C+13" AND FROM STA 500D TO STA 500F STRINGER 27LH WITH CORROSION AROUND SOLID RIVETS DRIVEN HEAD.(

PERFORMED PERMANENT REPAIR AT STRINGER 27LH FROM STA 500 +3 INCH TO STA 500G + 10 INCH IAW B737-800BCF SRM 53 - [SDR UIEA2025030400188](https://openairdocs.org/sdr/UIEA2025030400188.md): Stringer · corroded · Mar 4, 2025 · N5147A · Boeing 73783N · Fuselage Main, Longeron/Stringer > FWD CARGO COMPARTMENT AT STA 500D+2", STA 500D+18" AND BETWEEN STA 500E-STA 500G STRINGER 26RH WITH CORROSION AROUND SOLID RIVETS DRIVEN HEAD.(

PERFORMED PERMANENT REPAIR AT STRINGER 26 RH FROM STA 500A TO STA 500H + 3 INCH IAW B737-800BCF SRM 53-00-03-2R-1 - [SDR UIEA2025030400187](https://openairdocs.org/sdr/UIEA2025030400187.md): Stringer · corroded · Mar 4, 2025 · N5147A · Boeing 73783N · Fuselage Main, Longeron/Stringer > FWD CARGO COMPARTMENT FROM STA 500B+10" TO STA 500E+16" STRINGER 27RH WITH CORROSION AROUND SOLID RIVETS DRIVEN HEAD.(

PERFORMED PERMANENT REPAIR AT STRINGER 27 RH FROM STA 500A +3 INCH TO STA 500G + 14 INCH IAW B737-800BCF SRM 53-00-03-2R-1 REPAIR 1 FIGURE - [SDR UIEA2025030100186](https://openairdocs.org/sdr/UIEA2025030100186.md): Floor Support · corroded · Mar 4, 2025 · N5147A · Boeing 73783N · Fuselage Miscellaneous Structure > FWD CARGO COMPARTMENT STA 495 RBL 3" CARGO FLOOR BEAM WITH CORROSION AROUND ANCHOR NUTS.(

PERFORMED PERMANENT REPAIR AT FLOOR CARGO STRUCTURE ZEE SUPPORT FROM STA 480+6 INCH TO STA500+15 INCH, RBL 3" DUE TO CORROSION OUT LIMITS IAW COOPESA EO N°: COO-EO-202 - [SDR UIEA2025030100185](https://openairdocs.org/sdr/UIEA2025030100185.md): Floor Support · corroded · Mar 4, 2025 · N5147A · Boeing 73783N · Fuselage Miscellaneous Structure > FWD CARGO COMPARTMENT STA 495 LBL 3" CARGO FLOOR BEAM WITH CORROSION AROUND ANCHOR NUTS. PERFORMED PERMANENT REPAIR AT FLOOR CARGO STRUCTURE ZEE SUPPORT FROM STA 480+6 INCH TO STA 500+15 INCH, LBL 3" DUE TO CORROSION OUT LIMITS IAW COOPESA EO N°: COO-EO-2025 - [SDR UIEA2025022700179](https://openairdocs.org/sdr/UIEA2025022700179.md): Stringer · corroded · Mar 4, 2025 · N5147A · Boeing 73783N · Fuselage Main, Longeron/Stringer > LOWER FUSELAGE, FWD CARGO COMPARTMENT FROM BS 440 TO BS 490 STRNGER-27R WITH CORROSION. PERFORMED PERMANENT REPAIR AT STRINGER 27R DUE TO CORROSION OUT LIMITS IAW SRM 53-00-03-2R-1 REPAIR 1 FIG 205 FROM STA 440 TO STA 500 AND SPLICE INSTALLED ON STA 460+8 INC - [SDR UIEA2025022700177](https://openairdocs.org/sdr/UIEA2025022700177.md): Stringer · corroded · Mar 4, 2025 · N5147A · Boeing 73783N · Fuselage Main, Longeron/Stringer > LOWER FUSELAGE, AFT CARGO COMPARTMENT FROM BSTA 727H TO BSTA 727I AND BSTA 727F TO BSTA 727G STRINGER 26R WITH CORROSION. PERFORMED PERMANENT REPAIR ON STRINGER SECTION (STR 26R) FROM BS 727E+2.5 INCH TO BS727G+20.5 INCH DUE TO CORROSION OUT LIMITS IAW B737 B - [SDR UIEA2025022700175](https://openairdocs.org/sdr/UIEA2025022700175.md): Floor Support · corroded · Mar 4, 2025 · N5147A · Boeing 73783N · Fuselage Miscellaneous Structure > LOWER FUSELAGE AFT CARGO COMPARTMENT FLOOR STRUCTURE FROM BS 727 TO BS 767 AT RBL 21 SIDE PLATE WITH CORROSION. REPAIRED SIDEPLATE FROM BS 727 TO BS 767 AT RBL 21 SPLICE INSTALLED FROM BS 727F+1.5 INCH TO BS 727F+12 INCH IAW SRM 53-00-53-2R-6 REPAIR 6 FIG 203 - [SDR UIEA2025022700170](https://openairdocs.org/sdr/UIEA2025022700170.md): Floor Support · corroded · Mar 4, 2025 · N5147A · Boeing 73783N · Fuselage Miscellaneous Structure > LOWER FUSELAGE AFT CARGO COMPARTMENT FLOOR STRUCTURE FROM BS 757+4 TO BS 847 AT LBL 25,SIDE PLATE WITH CORROSION. PERFORMED PERMANENT REPAIR AT SIDE PLATE FROM BS 727 TO BS 787 AT LBL 25 (SPLICE LOCATED BETWEEN BS 727J+2 INCH AND BS 727J+12 INCH AND BETWEEN B - [SDR UIEA2025022700169](https://openairdocs.org/sdr/UIEA2025022700169.md): Skin · dented · Mar 4, 2025 · N5147A · Boeing 73783N · Cargo/Baggage Doors > LOWER FUSELAGE, FWD COMPARMENT CARGO DOOR EXTERNAL SKIN AT BS 462 BETWEEN BEAM B AND BEAM C SKIN WITH DENT.(

PERFORMED PERMAMENT REPAIR AT AFT CARGO DOOR COMPARTMENT EXTERNAL SKIN I/A/W B737-800 BCF SRM 52-30-01-2R-3 REPAIR 3 (REPLACED EXTERNAL SKIN) REV 22 - [SDR UIEA2025022700167](https://openairdocs.org/sdr/UIEA2025022700167.md): Skin · dented · Mar 4, 2025 · N5147A · Boeing 73783N · Cargo/Baggage Doors > LOWER FUSELAGE, AFT CARGO COMPARTMENT DOOR EXTERNAL SKIN AT BS 821 BETWEEN BEAM D AND BEAM E SKIN WITH DENT.
(

PERFORMED PERMANENT REPAIR AT AFT CARGO DOOR COMPARTMENT EXTERNAL SKIN IAW B737-800 BCF SRM 52-30-01-2R-3 REPAIR 3 (REPLACED EXTERNAL SKIN) REV - [SDR UIEA2023021100104](https://openairdocs.org/sdr/UIEA2023021100104.md): None · none · Feb 16, 2023 · N5147A · Boeing 73783N · Communications System > WHILE PERFORMING ELT FIXED TYPE OPERATIONAL TEST, IT FAILED DURING TEST "THE LED FLASHES 4 TIMES"(

CLEANED ELT COAX CONNECTOR ANTENNA CABLE I/A/W B737-800 SWPM: 20-60-01 PAGE 2B, PAGES 3-4, AND PERFORM ELT SYSTEM TEST I/A/W B737-800 AMM TEST 23-24-00-730-804 - [SDR UIEA2023021100105](https://openairdocs.org/sdr/UIEA2023021100105.md): None · none · Feb 16, 2023 · N5147A · Boeing 73783N · Fuselage Structure (General) > LOWER EXTERNAL FUSELAGE AT BS 218.500, WL 192.750 LEFT SIDE SKIN FASTENER WITH DOUBLE HOLE(

PERFORM REPAIR AT SECTION 41, FUSELAGE BS 218, WL192.750, L/H SIDE SKIN AND FRAME OUTER CHORD DOUBLE HOLE REPAIR I/A/W COOPESA EO COO-EO-2023-17119-R00 DATED 07/FEB/2 - [SDR UIEA2023021100106](https://openairdocs.org/sdr/UIEA2023021100106.md): None · none · Feb 16, 2023 · N5147A · Boeing 73783N · Fuselage Structure (General) > LOWER EXTERNAL FUSELAGE AT BS 188, WL 194 LEFT SIDE SKIN FASTENER WITH DOUBLE HOLE( / / /
PERFORM - [SDR Q2SA20210909455](https://openairdocs.org/sdr/Q2SA20210909455.md): Transmitter · faulted · Sep 9, 2021 · N5147A · Boeing 73783N · Trailing Flap Position Indicating System > WHEN COMPLETING BEFORE LANDING CHECKLIST, FLAP HANDLE SELECTED TO 30, FLAP INDICATOR NEEDLE INDICATED 8 + 10 DEGREES. ON THE GO AROUND, THE FLAP NEEDLES MATCHED AT 10 DEGREE. COMPLETED THE QRH PROCEDURE, USING ALTERNATE FLAP MASTER SWITCH AND ELECTRICALLY MOVE - [SDR Q2SA20210804450](https://openairdocs.org/sdr/Q2SA20210804450.md): Inlet · contaminated · Aug 4, 2021 · N5147A · Boeing 73783N · Cabin Cooling System > ON DESCENT, PASSING THROUGH 11,000 FEET, SMELLED CHLORINE. PUT ON OXYGEN MASK. INSPECTED PACKS WITH APU BLEED AND ALSO WITH BOTH ENGINES RUNNING. COULD NOT DUPLICATE CHLORINE SMELL IN THE CABIN. FURTHER INSPECTION FOUND PETROLEUM JELLY RESIDUAL UNDERNEATH PANE - [SDR Q2SA20210712448](https://openairdocs.org/sdr/Q2SA20210712448.md): Flap System · malfunctioned · Jul 12, 2021 · N5147A · Boeing 73783N · Trailing Edge Flap Control System > AIRCRAFT LANDED WITHOUT INCIDENT. CREW REPORTED ON APPROACH SELECTED FLAP 30 AND THEY REMAINED AT FLAP 15. CYCLED FLAP LEVER TO 15 THEN BACK TO 30, FLAPS WOULD NOT MOVE FROM FLAP 15. MAINTENANCE VISUALLY INSPECTED FLAPS AND SLATS AND CYCLED FLAPS FULL UP AND D - [SDR Q2SA20210331445](https://openairdocs.org/sdr/Q2SA20210331445.md): Switch · out of adjust · Mar 31, 2021 · N5147A · Boeing 73783N · Landing Gear Door Retract Section > AIRCRAFT GROUNDED. GEAR WOULD NOT RETRACT AFTER TAKE-OFF. RAN QRH, GEAR WOULD NOT RETRACT. RETURNED TO AFW. INSPECTED AND FOUND MANUAL RELEASE EXTENSION DOOR SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH AS PER AMM 32-34-00 TASK 820-802. PERFORMED OPERATIONAL AND ## 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 = 'N5147A' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N5147A/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.