# Service difficulty reports: N714CB, cancelled Oct 15, 2024

A list on [N714CB, cancelled Oct 15, 2024](https://openairdocs.org/deregistered/N714CB-2024-10-15.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 6 · 270 reports

- [SDR SWAA2021122154114](https://openairdocs.org/sdr/SWAA2021122154114.md): Flap System · faulted · Dec 17, 2021 · N714CB · Boeing 7377H4 · Trailing Edge Flap Control System
  > ON APPROACH SELECTED FLAPS 15 AND THEN 30. AT WHICH TIME WE NOTICED FLAP INDICATOR WAS AT 5. EXC. GO AROUND AND USED QRH ALT FLAP EXT PROCEDURES. PERFORMED FSEU BITE REF FIM 27-51 TASK 801; FAULT HISTORY SHOWED FAULTS 27-52261 AND 27-53280. CLEANED CONNECTORS
- [SDR SWAA2021122053486](https://openairdocs.org/sdr/SWAA2021122053486.md): Panel · elongated · Dec 15, 2021 · N714CB · Boeing 737 · Aerodynamic Fairings
  > SUPPLEMENTAL INFORMATION: AFT WING-TO-BODY FAIRING PANEL 194E HAS ELONGATED FASTENER HOLES.; / [01] TRIMMED; DRILLED; AND PAINTED NEW PNL; [02] REMOVED & REPLACED PANEL PER AMM 53-51-21
- [SDR SWAA2021122053205](https://openairdocs.org/sdr/SWAA2021122053205.md): Panel · elongated · Dec 15, 2021 · N714CB · Boeing 7377H4 · Aerodynamic Fairings
  > CENTER WHEEL WELL PANEL 193D FASTENER HOLES ELONGATED.; / [01] TRIMMED; DRILLED AND PAINTED NEW PNL; [02] REMOVED &REPLACE PANEL PER AMM 53-51-21
- [SDR SWAA2021092119554](https://openairdocs.org/sdr/SWAA2021092119554.md): Handle · loose · Sep 17, 2021 · N714CB · Boeing 7377H4 · Escape Slide
  > AFT ENTRY DOOR SLIDE HANDLE EXPOSED; / [01] SECURED AFT ENTRY DOOR SLIDE HANDLE IAW AMM 25-66-01
- [SDR SWAA2021092120453](https://openairdocs.org/sdr/SWAA2021092120453.md): Handle · loose · Sep 17, 2021 · N714CB · Boeing 7377H4 · Escape Slide
  > AFT ENTRY DOOR SLIDE HANDLE EXPOSED; / [01] SECURED AFT ENTRY DOOR SLIDE HANDLE IAW AMM 25-66-01
- [SDR SWAA2021061682904](https://openairdocs.org/sdr/SWAA2021061682904.md): Light · inoperative · Jun 13, 2021 · N714CB · Boeing 7377H4 · Emergency Lighting
  > LH EMERGENCY EXIT SIDEWALL LIGHT INOP; / OK TO CONTINUE PER MEL 33-2-03 SP1B; RR'D RH OVERWING EXIT SIDEWALL FUSE IAW AMM 33-51-01
- [SDR SWAA2021042967409](https://openairdocs.org/sdr/SWAA2021042967409.md): Light · inoperative · Apr 26, 2021 · N714CB · Boeing 7377H4 · Emergency Lighting
  > ROW 12 DEF SIDEWALL LIGHT INOP; ROW 12 DEF SIDEWALL LIGHT INOP /
- [SDR SWAA2021040159266](https://openairdocs.org/sdr/SWAA2021040159266.md): Lens · missing · Mar 28, 2021 · N714CB · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY AISLE LIGHT BEZEL/LENS MISSING AT 13DEF / CLEARED ON DMA 0718865 REPLACED MISSING EMERGENCY LIGHT LENS AT SEAT ROW 13DEF IAW AMM 33-51-03 CL NO 74301
- [SDR SWAA2020112331793](https://openairdocs.org/sdr/SWAA2020112331793.md): Linkage · broken · Nov 20, 2020 · N714CB · Boeing 7377H4 · Escape Slide
  > R1 DOOR SLIDE LINKAGE BROKEN. REPLACED LINKAGE, REF MT 725-61-06 AMM 25-66-01.
- [SDR SWAA2021051204424](https://openairdocs.org/sdr/SWAA2021051204424.md): Skate Angle · corroded · Jul 28, 2020 · N714CB · Boeing 7377H4 · Nacelle/Pylon Miscellaneous Structure
  > #2 ENG FWD ENG STRUT FAIRING STRUCTURE INBD SKATE ANGLE HAS CORROSION AT APPROX NAC STA 252-256 UNDER PANEL 441DL. / REPAIRED PER EA 20-154-01219
- [SDR SWAA2020080304426](https://openairdocs.org/sdr/SWAA2020080304426.md): Battery Pack · no test · Jul 28, 2020 · N714CB · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY FUNCTIONAL CHECK AT LOCATION M01669. R&R EMERGENCY LIGHTING BATTERY PACK AND POWER SUPPLY AS PER AMM 33-51-06.
- [SDR SWAA2020072702817](https://openairdocs.org/sdr/SWAA2020072702817.md): Battery Pack · inoperative · Jul 22, 2020 · N714CB · Boeing 7377H4 · Emergency Lighting
  > EXIT LIGHTS CONNECTED TO M1674 BATTERY PACK DO NOT COME ON / REMOVED AND REPLACED M1674 BATTERY PACK AND OPS CHECKED PER AMM 33-51-06-960-805 CHECKED GOOD
- [SDR SWAA2020072702351](https://openairdocs.org/sdr/SWAA2020072702351.md): Housing · damaged · Jul 20, 2020 · N714CB · Boeing 7377H4 · Emergency Lighting
  > AFT ENTRY WAY CENTER EMERGENCY EXIT LIGHT HOUSING IS DAMAGED. / REPLACED AFT ENTRY WAY CENTER EMERGENCY LIGHT HOUSING; OPS CHECK WAS GOOD IAW AMM 33-51-01-960-802. 57193U 23JUL20
- [SDR SWAA2020072700652](https://openairdocs.org/sdr/SWAA2020072700652.md): Skin · corroded · Jul 14, 2020 · N714CB · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > UPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 679 RBL 5 AT FASTENER HOLE. INBETWEEN STRINGER 1R AND 2R. / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 20-153-01151 REV IR (ATS ER 20-02895 REV IR). REFER TO NRC U186768 FOR TRACKING.
- [SDR SWAA2020072700651](https://openairdocs.org/sdr/SWAA2020072700651.md): Skin · corroded · Jul 14, 2020 · N714CB · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > UPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 683 RBL 2;RBL 9 AT FASTENER HOLES. INBETWEEN STRINGER 1R AND 2R / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 20-153-01151 REV IR (ATS ER 20-02895 REV IR). REFER TO NRC U186768 FOR TRACKING.
- [SDR SWAA2020072700650](https://openairdocs.org/sdr/SWAA2020072700650.md): Skin · corroded · Jul 14, 2020 · N714CB · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > UPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 694;RBL 9 AT FASTENER HOLE. INBETWEEN STRINGER 1R AND STR2R / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 20-153-01151 REV IR (ATS ER 20-02895 REV IR). REFER TO NRC U186768 FOR TRACKING.
- [SDR SWAA2020072700649](https://openairdocs.org/sdr/SWAA2020072700649.md): Skin · corroded · Jul 14, 2020 · N714CB · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > UPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 701; RBL3 AT FASTENER HOLE. INBETWEEN STRINGER 1R AND 2R. / REPAIRED UPPER EXTERIOR FUSELAGE SKIN PER ATS ER 20-02895; REV IR; PER EA 20-153-01151; REV IR.
- [SDR SWAA2020072797632](https://openairdocs.org/sdr/SWAA2020072797632.md): Frame · corroded · Jul 4, 2020 · N714CB · Boeing 7377H4 · Fuselage Main, Frame
  > BS 847 FRAME UPPER SURFACE CORRODED. LBL20; WL156. REPAIRED THE FRAME IAW ER20-02837, REV IR, AND EA 20-153-01157, REV IR.
- [SDR SWAA2020072797627](https://openairdocs.org/sdr/SWAA2020072797627.md): Bulkhead Web · corroded · Jul 2, 2020 · N714CB · Boeing 7377H4 · Fuselage Main, Bulkhead
  > ***CORROSION*** ON BS 259.5 BULKHEAD WEB WL 207 LBL 10 - RBL 2. / BS 259.5 WEB REPAIRED IAW EA # 20-153-01002 REV IR AND ER # 20-02836 REV IR.
- [SDR SWAA2021080397612](https://openairdocs.org/sdr/SWAA2021080397612.md): Floorbeam · cracked · Jul 1, 2020 · N714CB · Boeing 7377H4 · Fuselage Main, Floor Beam
  > BREAK PANEL IS CRACKED STA 540; RBL 1; WL 208. (MARKED) / REMOVED AND REPLACED BREAK PANEL AT STA540 RBL1 IAW SRM 51-40-02 AND AIPC 53-31-00-05
- [SDR SWAA2021080397611](https://openairdocs.org/sdr/SWAA2021080397611.md): Floorbeam · cracked · Jul 1, 2020 · N714CB · Boeing 7377H4 · Fuselage Main, Floor Beam
  > BREAK PANEL IS CRACKED STA 540; LBL 1; WL 208. (MARKED) / REMOVED AND REPLACED BREAK PANEL AT STA540 LBL1 IAW SRM 51-40-02 AND AIPC 53-31-00-05
- [SDR SWAA2020072797614](https://openairdocs.org/sdr/SWAA2020072797614.md): Structure · corroded · Jul 1, 2020 · N714CB · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON AFT CHORD OF BS 259.5 BULKHEAD WL 207 LBL 10-RBL 6. / THE DAMAGE IS REPAIRED PER EA 20-153-01002 REV IR AND ER #20-02836 REV IR. REFER TO NRC U186702 FOR TRACKING.
- [SDR SWAA2020072797613](https://openairdocs.org/sdr/SWAA2020072797613.md): Structure · corroded · Jul 1, 2020 · N714CB · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD CHORD OF BS 259.5 BULKHEAD, WL 207, LBL 10 - RBL 3. REMOVED AND REPLACED CHORD IAW SRM 51-40-02-0G-0, DWG 141A5133, REV C, AND DWG 141A7430, REV B.
- [SDR SWAA2020072797623](https://openairdocs.org/sdr/SWAA2020072797623.md): Stiffener · corroded · Jul 1, 2020 · N714CB · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON VERTICAL STIFFENER AT BS 225 RBL 5 WL 160. FOUND CORROSION ON VERTICAL STIFFNER AT BS225 RBL5 WL160 TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM. REMOVED AND REPLACED VERTICAL STIFFNER AT BS225 RBL5 WL160 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0;
- [SDR SWAA2020072797624](https://openairdocs.org/sdr/SWAA2020072797624.md): Stiffener · corroded · Jul 1, 2020 · N714CB · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON VERTICAL STIFFENER AT BS 225 LBL 5 WL 160. FOUND CORROSION ON VERTICAL STIFFNER AT BS 225, LBL 5, WL 160 TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM. REMOVED AND REPLACED VERTICAL STIFFNER IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, & DWG 141A7410.
- [SDR SWAA2020072797602](https://openairdocs.org/sdr/SWAA2020072797602.md): Stringer · corroded · Jul 1, 2020 · N714CB · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > FWD CARGO BAY STRINGER 23R HAS CORROSION AT END OF STRINGER BS536 WL164 RBL46 / REPAIRED STRINGER IN FWD CARGO BAY BS536. STR 23R WL164; RBL46 PER ER 20-02826 REV IR AND EA 20-153-01129 REV IR.
- [SDR SWAA2021081997560](https://openairdocs.org/sdr/SWAA2021081997560.md): Beam · cracked · Jun 30, 2020 · N714CB · Boeing 7377H4 · Wing Main, Frame Structure
  > LT WING AFT LWR T/E PANEL BEAM JUST O/B OF THE #1 PYLON IS CRACKED. / REMOVED AND REPLACED LT WING AFT LWR T/E PANEL BEAM JUST O/B OF THE NO 1 PYLON IAW SRM 51-40-02-0G-0 AND IPC 57-50-00-17 59779U 6JUL20
- [SDR SWAA2021081797590](https://openairdocs.org/sdr/SWAA2021081797590.md): Support · corroded · Jun 30, 2020 · N714CB · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS CORROSION AROUND NUT PLATE HOLES BS727 TO BS767 RBL23 WL156 / REMOVED CORROSION DAMAGED FLOOR TO SIDEWALL SUPPORT BS727-767 RBL23 WL156 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPOR
- [SDR SWAA2021081797589](https://openairdocs.org/sdr/SWAA2021081797589.md): Support · corroded · Jun 30, 2020 · N714CB · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS CORROSION AROUND NUT PLATE HOLES BS727 TO BS847 LBL23 WL156 / EVALUATED CORROSION ON ACB L/H FLOOR TO SIDEWALL SUPPORT; BS727 847; REMOVED.015' FROM ORIG.040'; FOUND TO BE OUT OF LIMITS; IAW SRM 53-00-53-
- [SDR SWAA2021081797591](https://openairdocs.org/sdr/SWAA2021081797591.md): Splice Strap · corroded · Jun 30, 2020 · N714CB · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR SPLICE STRAP AT BS767+4 HAS CORROSION AROUND NUT PLATE HOLES RBL10 TO LBL10 WL156 / RECEIVED NEW ACB FLOOR SPLICE STRAP BS767+4 ON PO# 796202. NEW SPLICE STRAP TO BE INSTALLED ON CUST CARD# JPANEL-141-CLOSE
- [SDR SWAA2021081797592](https://openairdocs.org/sdr/SWAA2021081797592.md): Splice Strap · corroded · Jun 30, 2020 · N714CB · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR SPLICE STRAP AT BS887 HAS CORROSION AROUND NUT PLATE HOLES RBL10 TO LBL10 WL156 / EVALUATED CORROSION ON ACB FLOOR SPLICE STRAP; BS887; FOUND TO BE OUT OF LIMITS; DUE TO NO LIMITS IN SRM.51-10-02-0G-0. REMOVED DAMAGED SPLICE STRAP; LOCATED;
- [SDR SWAA2021081597593](https://openairdocs.org/sdr/SWAA2021081597593.md): Support · corroded · Jun 30, 2020 · N714CB · Boeing 7377H4 · Fuselage Main, Bulkhead
  > AFT CARGO BAY LOWER BULKHEAD SUPPORT BS847 TO BS867 LBL10 TO WL156 HAS CORROSION / REMOVED AND REPLACED AFT CARGO BAY LOWER BULKHEAD SUPPORT BS847 TO 867 LBL10 WL156 IAW SRM 51-40-05; SRM 51-40-02; AND AIPC 53-42-51-06.
- [SDR SWAA2021081397594](https://openairdocs.org/sdr/SWAA2021081397594.md): Web · corroded · Jun 30, 2020 · N714CB · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY WEB BETWEEN BS787 TO BS807 RBL6 WL150 HAS CORROSION / EVALUATED CORROSION ON WEB BETWEEN BS787-807; RBL6; FOUND TO BE OUT OF LIMITS; DUE TO NO LIMITS IN SRM. LOCATED; DRILLED; AND INSTALLED NEW WEB; IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 1
- [SDR SWAA2021072997552](https://openairdocs.org/sdr/SWAA2021072997552.md): Bolt · broken · Jun 30, 2020 · N714CB · Boeing 7377H4 · Rudder, Plate/Skin
  > BROKEN NUTPLATE FOR MOUNT BOLT ON DORSAL FIN. / REMOVED AND REPLACED NUT PLATE FOR MOUNT BOLT ON DORSAL FIN IAW SRM 51-40-02-0G-0 AND IPC 55-32-11-02. DWG #174A0101. 59769U 1JUL20
- [SDR SWAA2020072797574](https://openairdocs.org/sdr/SWAA2020072797574.md): Seat Track · corroded · Jun 30, 2020 · N714CB · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK IN MULTIPLE AREAS AT PASSENGER CABIN BS480 - BS520 LBL45 WL208. MARKED / REMOVED CORROSION AND SEAT TRACK WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1. SEAT TRACK WAS FABBED AS PER ATS HFAB-100-307 AND REPLACED IAW SRM 51-40-02
- [SDR SWAA2020072797575](https://openairdocs.org/sdr/SWAA2020072797575.md): Seat Track · corroded · Jun 30, 2020 · N714CB · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK IN MULTIPLE AREAS AT PASSENGER CABIN BS 480 - 520, RBL 45, WL 208. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02-0G-0.
- [SDR SWAA2020072797598](https://openairdocs.org/sdr/SWAA2020072797598.md): Floor Panel · damaged · Jun 30, 2020 · N714CB · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 231XF UPPER SURFACE WAS DAMAGED. DUE TO THE EXTENT OF DAMAGE, FABRICATED A NEW CABIN FLOOR PANEL IAW SRM 53-00-50-2R-0 PARA 1A, AND DWG 144A5810-7.
- [SDR SWAA2020072797599](https://openairdocs.org/sdr/SWAA2020072797599.md): Floor Panel · damaged · Jun 30, 2020 · N714CB · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241AF UPPER SURFACE WAS DAMAGED. DUE TO THE EXTENT OF DAMAGE, FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-50-2R-0 PARA 1A AND DWG 144A5810-8.
- [SDR SWAA2020072797600](https://openairdocs.org/sdr/SWAA2020072797600.md): Floor Panel · damaged · Jun 30, 2020 · N714CB · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241DF UPPER SURFACE WAS DAMAGED. DUE TO THE EXTENT OF DAMAGE, FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-50-2R-0, PARA 1A, AND DWG 144A5810-9.
- [SDR SWAA2020072797551](https://openairdocs.org/sdr/SWAA2020072797551.md): Skin · corroded · Jun 29, 2020 · N714CB · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION ON CROWN SKIN EXTERNAL SURFACE IN MULTIPLE AREAS FROM APPROXIMATELY BS 887- BS 996 STR 3L - STR 3R / REPAIRED DAMAGE ON CROWN SKIN EXTERNAL SURFACE IN MULTIPLE AREAS FROM APPROXIMATELY BS887-996; STR3L- STR3R PER ER# 20-02823 REV IR AND EA # 20-153-0
- [SDR SWAA2020072703504](https://openairdocs.org/sdr/SWAA2020072703504.md): Floor Skin · dented · Jun 29, 2020 · N714CB · Boeing 7377H4 · Fuselage Main, Structure
  > FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. / REPAIRED FLIGHT DECK FLOOR EA #1-A53-33179 REV IR.
- [SDR SWAA2020012874817](https://openairdocs.org/sdr/SWAA2020012874817.md): Fuse · inoperative · Jan 24, 2020 · N714CB · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT ON CEILING IN FORWARD GALLEY AND LIGHT NEXT TO FORWARD JUMPSEAT INOP. REMOVED AND REPLACED BATTERY PACK AND FUSES FOR EMERGENCY LIGHT POWER SUPPLY M01675 PER AMM 33-51-06.
- [SDR SWAA2020012874775](https://openairdocs.org/sdr/SWAA2020012874775.md): Battery Pack · inoperative · Jan 24, 2020 · N714CB · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT ON CEILING IN FORWARD GALLEY AND LIGHT NEXT TO FORWARD JUMPSEAT INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AND FUSES FOR EMERGENCY LIGHT POWER SUPPLY M01675 IAW AMM 33-51-06.
- [SDR SWAA2019121739763](https://openairdocs.org/sdr/SWAA2019121739763.md): Slide · out of position · Dec 16, 2019 · N714CB · Boeing 7377H4 · Escape Slide
  > L2 DOOR SLIDE LOOSE AND WAS HANGING ON DOOR. / REPOSITIONED SLIDE PER MT.
- [SDR SWAA2019103138404](https://openairdocs.org/sdr/SWAA2019103138404.md): Lamp · inoperative · Oct 30, 2019 · N714CB · Boeing 7377H4 · Emergency Lighting
  > R/H AFT EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.
- [SDR SWAA2019103138403](https://openairdocs.org/sdr/SWAA2019103138403.md): Lamp · inoperative · Oct 30, 2019 · N714CB · Boeing 7377H4 · Emergency Lighting
  > L/H AFT EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.
- [SDR SWAA2019100237460](https://openairdocs.org/sdr/SWAA2019100237460.md): Wire · broken · Sep 29, 2019 · N714CB · Boeing 7377H4 · Emergency Lighting
  > FORWARD LT EXTERIOR EMERGENCY LIGHT INOPERATIVE. FOUND A BROKEN WIRE, AFT OF THE FORWARD ENTRY DOOR, RETAINING LANYARD. REPAIRED LIGHT PER AMM. R&R LENS RETAINER WIRE PER AMM.
- [SDR SWAA2019100137431](https://openairdocs.org/sdr/SWAA2019100137431.md): Oil System · low pressure · Sep 27, 2019 · N714CB · Boeing 7377H4 · Engine Oil Pressure
  > INFLIGHT SHUTDOWN, DIVERTED, AND DECLARED AN EMERGENCY, OIL QUANTITY FOR THE NR 2 ENGINE DECREASED TO ZERO, FOLLOWED BY A LOW OIL PRESSURE LIGHT AND OIL PRESSURE DECREASING BELOW 13 PSI FOR 15 SECONDS. FLASHING YELLOW THEN RED. PERFORMED ENGINE SHUTDO
- [SDR SWAA2019091036733](https://openairdocs.org/sdr/SWAA2019091036733.md): Girt Bar · loose · Sep 5, 2019 · N714CB · Boeing 7377H4 · Emergency Equipment
  > R1 DOOR GIRT BAR LOOSE. SECURED GIRT BAR IAW AMM.
- [SDR SWAA2022031569917](https://openairdocs.org/sdr/SWAA2022031569917.md): Bracket · cracked · Aug 22, 2019 · N714CB · Boeing 7377H4 · Wing Miscellaneous Structure
  > LEFT WING FIXED UPPER TRAILING EDGE PANEL CENTER INNER BRACKET CRACKED ABOVE NACELLE STRUT FAIRING / REMOVED AND REPLACED PER SRM 51-40-02.

Next page: https://openairdocs.org/deregistered/N714CB-2024-10-15/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 = 'N714CB' AND deregistration_id = 'N714CB-2024-10-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N714CB-2024-10-15/reports

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