# Service difficulty reports: N778SW

A list on [N778SW](https://openairdocs.org/aircraft/N778SW.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 5 · 239 reports

- [SDR SWAA2023090898241](https://openairdocs.org/sdr/SWAA2023090898241.md): Sign · detached · Sep 7, 2023 · N778SW · Boeing 7377H4 · Emergency Lighting
  > FWD ENTRY DOOR EXIT SIGN DETACHED<[01] REATTACHED FWD ENTRY DOOR EXIT SIGN IAW AMM 33-51-03
- [SDR SWAA2023083094818](https://openairdocs.org/sdr/SWAA2023083094818.md): Sign · loose · Aug 28, 2023 · N778SW · Boeing 7377H4 · Emergency Lighting
  > RT OVERWING EXIT SIGN LOOSE<[01] RESECURED EXIT SIGN PER AMM 33-51-04 OPS CHECK GOOD
- [SDR SWAA2023080484479](https://openairdocs.org/sdr/SWAA2023080484479.md): Stiffener · corroded · Aug 1, 2023 · N778SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > IN FWD NOSE ACCESSORY COMPARTMENT; LEFT FWD NLG DOOR STOP INTERNAL STIFFENER CORRODED; (REF IPC 53-11-00-02; ITEM 445) CORROSION MEASURES APPROXIMATELY 1.20 INCHES IN WIDTH X 1.64 INCHES IN LENGTH.<[01] REMOVED INTERNAL STIFFENER (REF IPC 53-11-00-02; ITEM 445
- [SDR SWAA2023073182842](https://openairdocs.org/sdr/SWAA2023073182842.md): Nozzle · cracked · Jul 27, 2023 · N778SW · Boeing 7377H4 · Engine Collector/Tailpipe/Nozzle
  > DURING WALKAROUND FOUND A CRACK AT THE 12 OCLOCK POSITION ON THE PRIMRAY EXHAUST NOZZLE ON THE #1 ENGINE BETWEEN MID AND AFT DOUBLER MEASURING APPROX. 6 INCHES BY 7 INCHES.<[01] R&R PRIMARY NOZZLE ASSEMBLY PER AMM 78-11-01
- [SDR SWAA2023072080241](https://openairdocs.org/sdr/SWAA2023072080241.md): Floor Panel · cracked · Jul 19, 2023 · N778SW · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CARGO PIT FLOOR PANEL 120CF HAS 7 CRACK<[01] ACCOMPLISHED FWD CARGO PANEL 120CF PERMANENT REPAIR PER AMM 25-52-01.
- [SDR SWAA2023072080283](https://openairdocs.org/sdr/SWAA2023072080283.md): Light · loose · Jul 19, 2023 · N778SW · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY STRIP LIGHTING AT ROW 8 CREATING TRIP HAZARD<[01] RE-SECURED PHOTO LUMINESCENT STRIP PER SIP
- [SDR SWAA2023031715845](https://openairdocs.org/sdr/SWAA2023031715845.md): Light · inoperative · Mar 13, 2023 · N778SW · Boeing 7377H4 · Emergency Lighting
  > AFT SERVICE DOOR EXT EMERGENCY LIGHT INOP<[01] RELAMPED AFT SERVICE DOOR EXT EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD.
- [SDR SWAA2023012392383](https://openairdocs.org/sdr/SWAA2023012392383.md): Tab · cracked · Jan 18, 2023 · N778SW · Boeing 7377H4 · Wing Main, Frame Structure
  > LEFT WING DEFLECTION CONTROL RIB UPPER TAB CRACKED<[01] COMPLIED WITH REPAIR THROUGH STEP H; SRM 57-51-02-2R-3;[02] COMPLIED WITH HFEC INSP. PER NDT MANUAL PART 6; 51-00-00 PROCEDURE 23;[03] ACCOMPLISHED REPAIR OF L/H WING DEFLECTION CONTROL RIB UPPER TAB DAMA
- [SDR SWAA2023011992361](https://openairdocs.org/sdr/SWAA2023011992361.md): Battery Pack · no test · Jan 18, 2023 · N778SW · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACKS, M1672, M1669, M1675, M1671, M1674 FAILED A CAPACITY TEST. THE BATTERY PACKS WERE REMOVED AND REPLACED IAW AMM 33-51-06.
- [SDR SWAA2022070525313](https://openairdocs.org/sdr/SWAA2022070525313.md): Sign · missing · Jul 2, 2022 · N778SW · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT SIDE PANEL LIGHT COVER MISSING- F/O SIDE / [01] REPLACED RH OVERWING EXIT SIGN PER AMM 33-51-01
- [SDR SWAA2022060714670](https://openairdocs.org/sdr/SWAA2022060714670.md): Slide · out of adjust · Jun 2, 2022 · N778SW · Boeing 7377H4 · Escape Slide
  > ITEM R1 DOOR HAS EXCESSIVE GIRT MATERIAL HANGING LOW / [01] REMOVED R-1 DOOR (FS) SLIDE (P/N 63550-101; S/N 0358F) IN REF TO MT 725-61-06.;[02] OK TO INSTALL NEW SLIDE;[03] REPLACED R-1 DOOR (FS) SLIDE WITH NEW SLIDE (P/N 63550-101; S/N 0320F) IN REF TO MT 725
- [SDR SWAA2022060713856](https://openairdocs.org/sdr/SWAA2022060713856.md): Support Beam · broken · May 31, 2022 · N778SW · Boeing 7377H4 · Wing Miscellaneous Structure
  > LEFT WING TRAILING EDGE PANEL 561AB MOUNT SUPPORT ANGLE IS BROKEN AT INBOARD END / [01] REMOVED AND REPLACED L/W TRAILING EDGE PANEL 561AB MOUNT SUPPORT BEAM PER REF B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1.
- [SDR SWAA2022060713338](https://openairdocs.org/sdr/SWAA2022060713338.md): Panel · cracked · May 30, 2022 · N778SW · Boeing 7377H4 · Wing, Control Surfaces
  > L/H CENTER WING-TO-B0DY FAIRING ACCESS PANEL 193CR UPPER SECTION HAS CRACK L/H CENTER WING-TO-B0DY FAIRING ACCESS PANEL 193CL UPPER SECTION HAS CRACK REMOVED PANEL 193CL FOR ACCESS TO REAPIR IRW B737-700 AMM 53-51-21-000-802; REMOVED THE DAMAGED PLIES AND PRE
- [SDR SWAA2022060713336](https://openairdocs.org/sdr/SWAA2022060713336.md): Bracket · broken · May 30, 2022 · N778SW · Boeing 7377H4 · Wing Spar
  > RIGHT WING REAR SPAR I/B THROUGH ACCESS PANEL 651DB ATTACHED BRACKET TO SPAR IS BROKEN / [01] REMOVED DAMAGE BRACKET AT R/W REAR SPAR I/B THROUGH ACCESS PANEL 651DB PER REF B737-700 SRM 51-40-02-0G-0.;[02] REMOVED AND REPLACED DAMAGE BRACKET AT R/W REAR SPAR I
- [SDR SWAA2022051206684](https://openairdocs.org/sdr/SWAA2022051206684.md): Strap · loose · May 10, 2022 · N778SW · Boeing 7377H4 · Emergency Exits
  > PILOT SIDE OVERWING EXIT STRAP COVER LOOSE. / [01] RE-INSTALLED OVERWING EXIT STRAP COVER PER AMM 52-22-00.
- [SDR SWAA2022011861671](https://openairdocs.org/sdr/SWAA2022011861671.md): Bumper · broken · Jan 15, 2022 · N778SW · Boeing 7377H4 · Escape Slide
  > AFT SERVICE DOOR SLIDE BOX BUMPER END CAP BROKEN. R & R AFT SERVICE DOOR SLIDE END CAP PER SIP.
- [SDR SWAA2022011360426](https://openairdocs.org/sdr/SWAA2022011360426.md): Light · inoperative · Jan 11, 2022 · N778SW · Boeing 7377H4 · Emergency Lighting
  > EXTERIOR AFT RT SVC DOOR EMERGENCY LIGHT INOP; / [01] RELAMPED AFT RT DOOR SLIDE EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD.
- [SDR SWAA2021122045675](https://openairdocs.org/sdr/SWAA2021122045675.md): Stringer · cracked · Nov 18, 2021 · N778SW · Boeing 7377H4 · Wing Miscellaneous Structure
  > R/W L/E INB FRONT SPAR LOWER CHORD ATTACHED ANGLE BRACKET CRACKED I/B OF PYLON # 2. REMOVED ANGLE PER B737-700 SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW STRINGER ANGLE IAW SRM 51-40-05-0G-0; [03] VERIFIED STEP 2; VERIFIED STEP 1; OK TO TREAT AND PRIME;
- [SDR SWAA2021122043377](https://openairdocs.org/sdr/SWAA2021122043377.md): Baffle · cracked · Nov 13, 2021 · N778SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FWD CARGO BS 500B - 500C, WL 156, S25R BAFFLE CORRORED. REMOVED BAFFLE IAW SRM 51-40-02-0G-0, FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2, PARAGRAF 4.C.(2)(B), FIGURE 103, DETAIL 103. LOCATED AND DRILLED THE BAFFLE IAW SRM 51-40-05-0G-0. APPLIED ALODINE AND
- [SDR SWAA2021122041726](https://openairdocs.org/sdr/SWAA2021122041726.md): Strap · corroded · Nov 8, 2021 · N778SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT;CORROSION AT T STRAP STA 727 D +5; / [01] FOUND EXFOLIATION CORROSION ON T STRAP AT STA. 727 +5; OUT OF LIMITS PER SRM 53-00-53-1A-2; AND ORDERED AND RECEIVED NEW T STRAP P/N 146A9401-8; NEW T TO BE INSTALLED ON T/C 5360-E-16462-NG; [02
- [SDR SWAA2021122041239](https://openairdocs.org/sdr/SWAA2021122041239.md): Web · corroded · Nov 7, 2021 · N778SW · Boeing 737 · Fuselage Miscellaneous Structure
  > SUPPLEMENTAL INFORMATION: CORROSION.....R/H FWD CARGO COMPARTMENT FLOOR @ STA 440 - STA 492.4 STR 25R WL 155.5 WEB HAS CORROSION IN SEVERAL AREAS. (18-038); / [01] WEB REMOVAL AND INSTALLATION BEING ACCOMPLISHED ON CARD #TTG8Q004DXN5; [02] LOCATED AND DRILLED
- [SDR SWAA2021122041238](https://openairdocs.org/sdr/SWAA2021122041238.md): Channel · corroded · Nov 7, 2021 · N778SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > RT FWD CARGO FLOOR BS 500A - 500D, S25R, WL 155.5 Z CHANNEL HAS CORROSION IN SEVERAL AREAS. LOCATED AND DRILLED A NEW Z CHANNEL IAW SRM 51-40-05-0G-0. VERIFIED STEP 1. TREATED AND APPLIED PRIMER TO Z CHANNEL IAW SRM 51-20-01-0G-0. FOUND OUT OF LIMITS IAW
- [SDR SWAA2021122041237](https://openairdocs.org/sdr/SWAA2021122041237.md): Channel · corroded · Nov 7, 2021 · N778SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON L/H FWD CARGO FLOOR, BS 480 - 500D, S25L, WL155.5, Z CHANNEL HAS CORROSION IN SEVERAL AREAS. REMOVED THE ZEE CHANNEL IAW AD CARD 5330-E-16461-NG, TASK CARD TTG8Q004DXN5 STEP 11, LOCATED AND DRILLED THE NEW ZEE CHANNEL IAW SRM 51-40-05-0G-0. TRE
- [SDR SWAA2021122041235](https://openairdocs.org/sdr/SWAA2021122041235.md): Shield · corroded · Nov 7, 2021 · N778SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON RT FWD CARGO FLOOR, BS 492.4 - 500A, S25R, WL 155.5. AFT SHIELD HAS CORROSION. LOCATED AND DRILLED A NEW SHIELD IAW SRM 51-40-05-0G-0, APPLIED ALODINE AND PRIMER AT ALL NEW HOLES IAW SRM 51-20-01-0G-0. SHIELD REMOVAL AND INSTALLATION BEING ACC
- [SDR SWAA2021122041236](https://openairdocs.org/sdr/SWAA2021122041236.md): Support · corroded · Nov 7, 2021 · N778SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION.....FWD CARGO COMPARTMENT FLOOR @ STA 500D STR25L - STR25R WL155.5 ACCESS PANEL ANGLE SUPPORT HAS CORROSION IN SEVERAL AREAS. (18-033); / [01] RECEIVED NEW ANGLE SUPPORT P/N 143A9485-35 AAR ISSUE TAG WN4490 P.O 1684224 FOR FWD CARGO COMPARTMENT FLOO
- [SDR SWAA2021122041240](https://openairdocs.org/sdr/SWAA2021122041240.md): Shield · corroded · Nov 7, 2021 · N778SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION.....R/H FWD CARGO COMPARTMENT FLOOR @ STA 420 - STA 440 STR 25R WL 155.5 FWD SHIELD HAS CORROSION. (18-039); / [01] RECEIVED NEW SHIELD P/N 143A8126U21 AAR ISSUE TAG WN9098 P.O 1684224 FOR FWD CARGO COMPARTMENT FLOOR FS 420 TO FS 440 STR 25R WL 155.
- [SDR SWAA2021122041227](https://openairdocs.org/sdr/SWAA2021122041227.md): None · cracked · Nov 5, 2021 · N778SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > R1 DOOR FWD CORNER CUTOUT FRAME CRACKED. REMOVED FASTENERS ON FRAME IAW SRM 51-40-02-0G-0 REMOVED THE CORNER CUTOUT FRAME IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW UPPER FWD FRAME IAW SRM 51-40-05-0G-0. TREATED AND PRIME FRAME HOLES IAW SRM 51-20-01-
- [SDR SWAA2021122040675](https://openairdocs.org/sdr/SWAA2021122040675.md): Frame · cracked · Nov 4, 2021 · N778SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CABIN LT FUSELAGE SUPPORT FRAME FLANGE HAS SMALL CRACK ABOVE L-1 DOOR CUTOUT, BS 312. TRIMMED DAMAGED AREA IAW SRM 53-10-07-2R-1, FIGURE 202. REMOVED FASTENERS AT REPAIR LOCATION IAW SRM 51-40-02-0G-0. PERFORMED HFEC ROTO ON OPEN FASTENER HOLES WITHIN
- [SDR SWAA2021122040684](https://openairdocs.org/sdr/SWAA2021122040684.md): Support · cracked · Nov 4, 2021 · N778SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT BREAK CRACKED AT STA 540 LBL24 MKD DOT; / [01] REMOVED FLOOR SUPPORT BREAK REF B737-7 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW PANEL BREAK REF. B737-7 SRM 51-40-05-0G-0; TREATED AND PRIMED HOLES REF. SRM 51-20-01-0G-0; [03] VER
- [SDR SWAA2021122040686](https://openairdocs.org/sdr/SWAA2021122040686.md): Support · cracked · Nov 4, 2021 · N778SW · Boeing · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT BREAK CRACKED AT STA 540 RBL 1 MKD DOT; / [01] REMOVED MAIN CABIN FLOOR SUPPORT AT FS 540 RBL 1 IN REF B737-700 SRM 51-40-02-0G-0; [02] VERIFIED STEP 1; [03] OK TO INSTALL PART; [04] INSTALLED NEW FLOOR SUPPORT AT FS 540 BETWEEN RBL 1
- [SDR SWAA2021122040688](https://openairdocs.org/sdr/SWAA2021122040688.md): Bracket · cracked · Nov 4, 2021 · N778SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > L/H FWD CARGO COMPARTMENT SIDEWALL @ STA500D STR 18L HAS (1 EACH) SUPPORT BRACKET CRACKED. (18-030); LH FWD CARGO COMPARTMENT SIDEWALL @ STA 500D STR19 HAS (1 EACH) GUSSET CRACKED. (18-030) / [01] REMOVED LT FWD SUPPORT BRACKET AT FWD CARGO COMP.SIDE WALL STA
- [SDR SWAA2021122040689](https://openairdocs.org/sdr/SWAA2021122040689.md): Bracket · cracked · Nov 4, 2021 · N778SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FWD CARGO SIDEWALL, BS 500D S19R HAS ONE GUSSET CRACKED. REMOVED GUSSET IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED GUSSET IAW SRM 51-20-01-0G-0. TREATED AND PRIMED GUSSET IAW SRM 51-20-01-0G-0. LOCATED AND DRILLED GUSSET IAW SRM 51-40-05-0G-0. INSTALLED TH
- [SDR SWAA2021122040670](https://openairdocs.org/sdr/SWAA2021122040670.md): Channel · corroded · Nov 4, 2021 · N778SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RIGHT SIDE Z CHANNEL IS CORRODED BS 727-767. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. LOCATED AND DRILLED A NEW Z CHANNEL IAW SRM 51-40-05-0G-0. TREATED AND PRIMERED, AND FABRICATED RT Z CHANNEL IAW AMM 51-21-41-370-802, AND 51-21-72-370
- [SDR SWAA2021122040671](https://openairdocs.org/sdr/SWAA2021122040671.md): Channel · corroded · Nov 4, 2021 · N778SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO LEFT SIDE 'Z' CHANNEL IS CORRODED 727-847;; / [01] FOUND EXFOLIATION CORROSION ON L/H SIDE Z CHANNEL BETWEEN STA. 272 AND STA. 847; OUT OF LIMITS PER 737 SRM 53-00-53-1A-2; [02] CORRECTION; FOUND EXFOLIATION CORROSION ON L/H SIDE Z CHANNEL BETWEEN
- [SDR SWAA2021110840679](https://openairdocs.org/sdr/SWAA2021110840679.md): Channel · corroded · Nov 4, 2021 · N778SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RIGHT 'Z' CHANNEL HAS LIGHT CORROSION AND MISSING PAINT FROM 847-964 AFT CARGO CHANNEL CORRECT STATION IS FROM 847 TO 947. REMOVED CORROSION ON AFT CARGO RIGHT ' Z' CHANNEL FROM STA847 TO STA 964 IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP.
- [SDR SWAA2021122040297](https://openairdocs.org/sdr/SWAA2021122040297.md): Scuff Plate · cracked · Nov 3, 2021 · N778SW · Boeing 7377H4 · Fuselage Main, Structure
  > R1 DOOR CENTER SCUFF PLATE HAS A CRACK; / [01] CRACK AT R1 DOOR CENTER SCUFF PLATE REPAIRED AS PER B737-700 SRM 53-10-15-2R REPAIR 2 BY J.L.WELDING INC.; FAA REPAIR STATION JLWR146K. ROUTING TAG #397622.; [02] VERIFIED WORK PERFORMED
- [SDR SWAA2021122038667](https://openairdocs.org/sdr/SWAA2021122038667.md): Plate · elongated · Oct 29, 2021 · N778SW · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FWD CAP STRIP PLATE SCREWS PASS THRU; HOLES ELONGATED; / [01] INSTALLED NEW AFT CARGO CAP STRIP; FWD PLATE PER REF. 737 AMM 25-52-10-400-801; [02] VERIFIED STEP 1.
- [SDR SWAA2021122038665](https://openairdocs.org/sdr/SWAA2021122038665.md): Bear Strap · corroded · Oct 29, 2021 · N778SW · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > TYPICAL CRACK FOUND EMANATING FROM FASTENER OPPOSITE FITTING LATCH AT R1 DOOR BEAR STRAP BETWEEN STA.291.5 AND STA.294.5 BETWEEN S-8R AND S-9R. APPROXIMATE LENGTH OF CRACK: 1.457'; TYPICAL CRACK FOND EMANATING FROM FASTENER OPPOSITE FITTING LATCH AT R1 DOOR
- [SDR SWAA2021122033635](https://openairdocs.org/sdr/SWAA2021122033635.md): Angle · corroded · Oct 26, 2021 · N778SW · Boeing 7377H4 · Wing Miscellaneous Structure
  > RT WING I/B FRONT SPAR BOOST PUMP 2 FWD UPPER BONDING STRAP SURROUNDING STRUCTURE CORRODED. REMOVED BONDING STRAP IAW SRM 51-40-02-0G-0. INSTALLED EWIS PROTECTION IAW AMM 20-60-07-913-801. DISCONNECT CONNECTOR (D00076) AND CAPPED IAW AMM 28-22-41-000-801.
- [SDR SWAA2020030942244](https://openairdocs.org/sdr/SWAA2020030942244.md): Retaining Clip · loose · Mar 7, 2020 · N778SW · Boeing 7377H4 · Emergency Equipment
  > RH SERVICE DOOR GUIRT BAR LATCH LOOSE ADJUSTED FWD SVC DOOR GIRT BAR STOW CLIP ON DOOR LINER PER SIP OK FOR SVC
- [SDR SWAA2020020440986](https://openairdocs.org/sdr/SWAA2020020440986.md): Battery Pack · no test · Jan 31, 2020 · N778SW · Boeing 7377H4 · Emergency Lighting
  > 5 EACH CABIN EMERGENCY LIGHTING BATTERY PACKS FAIL CAPACITY TEST. / R&R BATTERY PACKS PER AMM AND DWG.
- [SDR SWAA2020010340102](https://openairdocs.org/sdr/SWAA2020010340102.md): Light · inoperative · Dec 30, 2019 · N778SW · Boeing 7377H4 · Emergency Lighting
  > CAPTAIN EMERGENCY EXIT LIGHT INOP. / RELAMPED LIGHT PER MM.
- [SDR SWAA2019102238086](https://openairdocs.org/sdr/SWAA2019102238086.md): Support Fitting · corroded · Oct 19, 2019 · N778SW · Boeing 7377H4 · Wing, Landing Gear Attach Fittings
  > L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.
- [SDR SWAA2019102238085](https://openairdocs.org/sdr/SWAA2019102238085.md): Support Fitting · corroded · Oct 19, 2019 · N778SW · Boeing 7377H4 · Wing, Landing Gear Attach Fittings
  > L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.
- [SDR SWAA2019102238084](https://openairdocs.org/sdr/SWAA2019102238084.md): Support Fitting · corroded · Oct 19, 2019 · N778SW · Boeing 7377H4 · Wing, Landing Gear Attach Fittings
  > L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD LUG BORE CORRODED. / REPAIRED LUG BORE PER EA.
- [SDR SWAA2019102238047](https://openairdocs.org/sdr/SWAA2019102238047.md): Support Fitting · corroded · Oct 19, 2019 · N778SW · Boeing 7377H4 · Wing, Landing Gear Attach Fittings
  > L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD LUG BORE CORRODED. / REPAIRED LUG BORE PER EA.
- [SDR SWAA2019102238046](https://openairdocs.org/sdr/SWAA2019102238046.md): Support Fitting · corroded · Oct 19, 2019 · N778SW · Boeing 7377H4 · Wing, Landing Gear Attach Fittings
  > L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD LUG BORE CORRODED. / REPAIRED LUG BORE PER EA.
- [SDR SWAA2019102238045](https://openairdocs.org/sdr/SWAA2019102238045.md): Support Fitting · corroded · Oct 19, 2019 · N778SW · Boeing 7377H4 · Wing, Landing Gear Attach Fittings
  > L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD LUG BORE CORRODED. / REPAIRED LUG BORE PER EA.
- [SDR SWAA2019102238044](https://openairdocs.org/sdr/SWAA2019102238044.md): Support Fitting · corroded · Oct 19, 2019 · N778SW · Boeing 7377H4 · Wing, Landing Gear Attach Fittings
  > L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD LUG BORE CORRODED. / REPAIRED LUG BORE PER EA.
- [SDR SWAA2019102238043](https://openairdocs.org/sdr/SWAA2019102238043.md): Support Fitting · corroded · Oct 19, 2019 · N778SW · Boeing 7377H4 · Wing, Landing Gear Attach Fittings
  > L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD HAT SIDE CORRODED. / REPAIRED FITTING PER EA.

Next page: https://openairdocs.org/aircraft/N778SW/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 = 'N778SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N778SW/reports

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