# Service difficulty reports: N757LV

A list on [N757LV](https://openairdocs.org/aircraft/N757LV.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 · 283 reports

- [SDR SWAA2023071177258](https://openairdocs.org/sdr/SWAA2023071177258.md): Light · inoperative · Jul 11, 2023 · N757LV · Boeing 7377H4 · Emergency Lighting
  > RH AFT EMERGENCY EXIT LIGHT INOP<[01] RELAMPED AFT RH EMERGENCY EXIT PER AMM 33-51-03.
- [SDR SWAA2023052552088](https://openairdocs.org/sdr/SWAA2023052552088.md): Battery Pack · inoperative · May 25, 2023 · N757LV · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK AT LOCATION M1673 (AFT LEFT SIDE)<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION M1673 OPS CHECK GOOD PER AMM 33-51-06;[02] REMOVED BATTERY DUE TO FAILED CAPACITY TEST REPLACED WITH SERVICEABLE UNIT. OPS CHECK G
- [SDR SWAA2023020900860](https://openairdocs.org/sdr/SWAA2023020900860.md): Battery Pack · inoperative · Feb 9, 2023 · N757LV · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT BEHIND THE AFT SERVICE DOOR IS INOP.<[01] REMOVED AND REPLACED AFT EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06
- [SDR SWAA2022102764130](https://openairdocs.org/sdr/SWAA2022102764130.md): None · none · Oct 25, 2022 · N757LV · Boeing 7377H4 · Aircraft Fuel System
  > FUEL QTY DROPPED 1100 LBS IN LEFT WING IN 20 MINUTES; WITH IMBALANCE OF 1100LBS. SHUT ENGINE DOWN PER QRH. AFTER BURNING FUEL FROM ENG 2; BALANCE WAS ACHIEVED / [01] PERFORMED DRIP STICK MEASURE ON LEFT WING FOUND TO BE ACCURATE.ALSO PERFORMED CROSSFEED VALVE
- [SDR SWAA2022102161711](https://openairdocs.org/sdr/SWAA2022102161711.md): Panel · delaminated · Oct 20, 2022 · N757LV · Boeing 7377H4 · Wing, Fuselage Attach Fittings
  > LEFT WING PANEL 521 YB OUTBOARD EDGE DELAMINATED. 2INCHES FROM LEADING EDGE. 1.5 INCH WIDE BY 3 INCH LONG / [01] ACCOMPLISHED TEMP REPAIR PER EA-GENERAL CLEANED; TAP TESTED;INSTALLED 2 LAYERS OF SPEED TAPE AND REINSTALLED PANEL.;[02] COMPLIED WITH EA; #TTG8Q00
- [SDR SWAA2022082344459](https://openairdocs.org/sdr/SWAA2022082344459.md): Light · out of position · Aug 21, 2022 · N757LV · Boeing 7377H4 · Emergency Lighting
  > FA REPORTS AFT EXIT SIGN FELL OFF / [01] R/R'D AFT SIGN ASSY. PER MM 33-51-01.
- [SDR SWAA2022080839146](https://openairdocs.org/sdr/SWAA2022080839146.md): Tab · loose · Aug 5, 2022 · N757LV · Boeing 7377H4 · Escape Slide
  > FA ADVISES THAT THE FWD SERVICE DOOR SLIDE MANUEL INFLATION PULL TAB HANGS OUT WHEN THE GIRT BAR IS ARMED / [01] RESECURED VELCRO NEAR GIRT BAR ON FWD SERVICE DOOR ESCAPE SLIDE PER AMM 25-66-01
- [SDR SWAA2022072833419](https://openairdocs.org/sdr/SWAA2022072833419.md): Flap · delaminated · Jul 25, 2022 · N757LV · Boeing 7377H4 · Trailing Edge Flap Control System
  > FLAP WAS FOUND WITH DELAMINATION / [01] FLAP REMOVED AND REPLACED. OPS AND ADJUSTMENT CHECKS GOOD IAW AMM 27-51-12;[02] C/W OPS AND ADJUSTMENT CHECK
- [SDR SWAA2022012463246](https://openairdocs.org/sdr/SWAA2022012463246.md): Engine · failed · Jan 22, 2022 · N757LV · Boeing 7377H4 · Powerplant System
  > AT 38000 FT THE R/H #2 ENG OIL/QAUATIY SHOWS 20 % ENG INSTRURMENTS FLASHED WHITE BOX AND OTHER ENGINE INSTRUMENTS ARE NORMAL. DECENT #2 QUAITY SLOWY WENT DOWN TO 7 % ON FINAL APPROCH. AT GATE #2; SHOWS 20% / [01] REMOVED AND REPLACED #2 ENGINE PER MT 771-00-0
- [SDR SWAA2021111532131](https://openairdocs.org/sdr/SWAA2021111532131.md): Rib · cracked · Oct 21, 2021 · N757LV · Boeing 737* · Horizontal Stabilizer, Spar/Rib
  > CRACK LEADING EDGE RIB STA 86.66 AT RT HORIZONTAL STABILIZER; 2021-462044 / [01] REPLACED LEADING EDGE RIB STA 86.66 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 186A1001 SHEET 4 REV. A; [02] UPDATED CORRECTIVE ACTION <BR>REPLACED LEA
- [SDR SWAA2021111531785](https://openairdocs.org/sdr/SWAA2021111531785.md): None · cracked · Oct 19, 2021 · N757LV · Boeing 737* · Fuselage Miscellaneous Structure
  > CRACK ANGLE FLOOR STRUCTURE BETWEEN BS 685 TO BS 706 AT LEVEL RBBL 0.07 CENTER SECTION; 2021-462040 / [01] REPLACED ANGLE FLOOR STRUCTURE BETWEEN BS 685 TO BS 706 AT LEVEL RBBL 0.07 CENTER SECTION IAW DWG 273A9112 REV-AND SRM B737 51-10-02 ITEM 9; [02] CORREC
- [SDR SWAA2021111531786](https://openairdocs.org/sdr/SWAA2021111531786.md): Structure · cracked · Oct 19, 2021 · N757LV · Boeing 737* · Fuselage Miscellaneous Structure
  > CRACK ANGLE FLOOR STRUCTURE BETWEEN BS 685 TO BS 706 AT LEVEL RBBL 24.5 CENTER SECTION; 2021-462041 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22; TEMPERATURE CONTROLLER: P/N: 38615K71; S/N: AE-40585; DUE D
- [SDR SWAA2021111530902](https://openairdocs.org/sdr/SWAA2021111530902.md): None · corroded · Oct 16, 2021 · N757LV · Boeing 737* · Fuselage Miscellaneous Structure
  > CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 767 TO BS 794.3 STR 25R WL 156 RBL2184 AT AFT CARGO COMPARTMENT; 2021-461994 / [01] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS 767 TO BS 794.3 STR 25R WL 156 RBL 21.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM
- [SDR SWAA2021111530901](https://openairdocs.org/sdr/SWAA2021111530901.md): Support · corroded · Oct 16, 2021 · N757LV · Boeing 737* · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 767 STR 25R WL156 RBL21.84 AT AFT CARGO COMPARTMENT; 2021-461993 / [01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 767 STR 25R WL156 RBL21.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9;
- [SDR SWAA2021111530903](https://openairdocs.org/sdr/SWAA2021111530903.md): None · corroded · Oct 16, 2021 · N757LV · Boeing 737* · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 STR 25L WL156 LBL21.84 AT AFT CARGO COMPARTMENT; 2021-461995 / [01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 STR 25L WL156 LBL21.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9;
- [SDR SWAA2021111530898](https://openairdocs.org/sdr/SWAA2021111530898.md): Tie Clip · cracked · Oct 15, 2021 · N757LV · Boeing 737* · Fuselage Main, Longeron/Stringer
  > CRACK BILGE AREA TIE CLIP LOCATED STA 500D AND STR 26L AT FWD CARGO COMPARTMENT; 2021-461992 / [01] REPLACED TIE CLIP AND FASTENER LOCATED STA 500D AND STR 26L AT FWD CARGO COMPARTMENT; I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A1225 REV -.; [02] REPLAC
- [SDR SWAA2021111530899](https://openairdocs.org/sdr/SWAA2021111530899.md): Tie Clip · cracked · Oct 15, 2021 · N757LV · Boeing 737* · Fuselage Main, Longeron/Stringer
  > CRACK BILGE AREA TIE CLIP LOCATED STA 500D AND STR 26R AT FWD CARGO COMPARTMENT; 2021-461991 / [01] REPLACED TIE CLIP AND FASTENER LOCATED STA 500D AND STR 26R AT FWD CARGO COMPARTMENT; I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A1225 REV -.; [02] REPLAC
- [SDR SWAA2021111530900](https://openairdocs.org/sdr/SWAA2021111530900.md): Angle · cracked · Oct 15, 2021 · N757LV · Boeing 737* · Fuselage Miscellaneous Structure
  > CRACK ANGLE - CLIP LOCATED BS 400 AND STRINGER 26L AT FWD CARGO COMPARTMENT; 2021-461990 / [01] TOOL USED DIGITAL CALIPER<BR>P/N: 500-172-30 S/N: 15237811 DUE DATE:11 MAY 22; [02] REPLACED ANGLE CLIP LOCATED AT BS 400 AND STR 26L FWD CARGO COMPARTMENT IAW SRM
- [SDR SWAA2021111529726](https://openairdocs.org/sdr/SWAA2021111529726.md): Angle · cracked · Oct 13, 2021 · N757LV · Boeing 737* · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE BETWEEN WS 236 TO WS 285 ON REAR SPAR AT RT WING; 2021-461956 / [01] REPLACED ANGLE LOCATED TRAILING EDGE BETWEEN WS 236 TO WS 285 ON REAR SPAR AT RT WING. IAW B737-700 SRM 51-40-02 AND DWG #115A2930 SHEET 8 REV -.; [02] CERTIFIED WO
- [SDR SWAA2021111529730](https://openairdocs.org/sdr/SWAA2021111529730.md): Angle · cracked · Oct 13, 2021 · N757LV · Boeing 737* · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE AREA OF ACCESS PANEL 651GB AT RT WING; 2021-461958 / [01] REPLACED ANGLE TRAILING EDGE AREA OF ACCESS PANEL 651GB AT RT WING IAW SRM B737-700-51-10-02 ITEM 9; 51-40-02 AND DRAWING 115A3700 REF. Y REV. DATE 30NOV01; REPLACED ANGLE DUE
- [SDR SWAA2021111529703](https://openairdocs.org/sdr/SWAA2021111529703.md): Skin · cracked · Oct 12, 2021 · N757LV · Boeing 737* · Fuselage Miscellaneous Structure
  > CRACK ON INTERNAL SKIN CUT OUT LOWER POSITION GROUND SERVICE DOOR 114AR; 2021-461865 / [01] TOOL USED EDDY CURRENT EQUIPMENT P/N NORTEC 500D; S/N:00X12101V022233; DUE DATE: 02-JUN-22; [02] REPAIRED EXTERNAL SKIN CUT OUT LOWER POSITION (EGPR SURROUND DOUBLER)
- [SDR SWAA2021111529181](https://openairdocs.org/sdr/SWAA2021111529181.md): Battery Pack · inoperative · Oct 12, 2021 · N757LV · Boeing 737* · Emergency Lighting
  > INOP UPPER BATTERY PACK ON FWD AREA GALLEY (2EA); 2021-461844 / [01] REPLACED POWER SUPPLY-BATTERY PACK M1674; M1675 ON FWD PAX CABIN; LIGHTS TEST ARE OK. IAW AMM 33-51-06-960-805; [02] CERTIFIED STEP 1; TEST OK.<BR>TASK CARD COMPLETED
- [SDR SWAA2021111129710](https://openairdocs.org/sdr/SWAA2021111129710.md): Stringer · cracked · Oct 12, 2021 · N757LV · Boeing 737* · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 25R AT BS 540 FWD CARGO COMPARTMENT; 2021-461921 / [01] TOOL USED: ULTRASONIC EQUIPMENT: P/N: 45 MG; S/N: 130064101 DUE DATE: 11-MAR-22; [02] TOOL USED EDDY CURRENT PN/ NORTEC 600D; SN/60009161631; DUE DATE/ 01DEC21; [03] TOOL USED PRECISION RA
- [SDR SWAA2021111129709](https://openairdocs.org/sdr/SWAA2021111129709.md): Stringer · cracked · Oct 12, 2021 · N757LV · Boeing 737* · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 26R AT BS 540 FWD CARGO COMPARTMENT; 2021-461920 / [01] TOOL USED: P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 05-MAR-22; [02] TOOL USED PRECISION RADIUS GAUGE P/N: 2204A3; S/N: AE-408657 DUE DATE: 02-NOV-21; [03] TOOL USED: TEMPERATURE CONTR
- [SDR SWAA2021111129713](https://openairdocs.org/sdr/SWAA2021111129713.md): Stringer · cracked · Oct 12, 2021 · N757LV · Boeing 737* · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 26L AT BS 540 FWD CARGO COMPARTMENT; 2021-461919 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N 45MG; S/N: 130061901; DUE DATE: 11 MAY 22.; [02] TOOL USED: P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 05-MAR-22; [03] TOOL USED PRECISION RADIUS
- [SDR SWAA2021111129712](https://openairdocs.org/sdr/SWAA2021111129712.md): Stringer · cracked · Oct 12, 2021 · N757LV · Boeing 737* · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 25L AT BS 540 FWD CARGO COMPARTMENT; 2021-461918 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N 45MG; S/N: 130061901; DUE DATE: 11 MAY 22.; [02] TOOL USED: P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 05-MAR-22; [03] TOOL USED PRECISION RADIUS
- [SDR SWAA2021111129711](https://openairdocs.org/sdr/SWAA2021111129711.md): Stringer · cracked · Oct 12, 2021 · N757LV · Boeing 737* · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 21L AT BS 540 FWD CARGO COMPARTMENT; 2021-461917 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 35DL S/N: 091419910 DUE DATE: 30-NOV-21.; [02] TOOL USED PN NORTEC 600D SN 60009161631 DUE DATE 01-DEC-21; [03] TOOL USED PRECISION RADIUS GAUGE P
- [SDR SWAA2021111128672](https://openairdocs.org/sdr/SWAA2021111128672.md): Light · broken · Oct 10, 2021 · N757LV · Boeing 737* · Emergency Lighting
  > BROKEN GALLEY 1 EMERGENCY EXIT LIGHT ASSY AT FWD GALLEY AREA; 2021-461580 / [01] REPLACED GALLEY 1 EMERGENCY EXIT LIGHT ASSY AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 PERFORMED OPERATIONAL TEST IS OK; [02] TASK CARD COMPLETED
- [SDR SWAA2021111528655](https://openairdocs.org/sdr/SWAA2021111528655.md): None · cracked · Oct 9, 2021 · N757LV · Boeing 737* · Leading Edge Devices
  > CRACK EXTERNAL SKIN LOCATED SLAT 6 AT LEVEL SLAT STATION 202.45 AT RT WING; 2021-461484 / [01] REMOVED ACCESS PANEL 623DB AND FLEX SKIN LOC SLAT 6 AT LEVEL SLAT STATION 202.45 AT RT WING IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION AND NOT FOUND
- [SDR SWAA2021111528656](https://openairdocs.org/sdr/SWAA2021111528656.md): None · cracked · Oct 9, 2021 · N757LV · Boeing 737* · Leading Edge Devices
  > CRACK EXTERNAL SKIN LOCATED SLAT 4 AT LEVEL SLAT STATION 85.19 AT LT WING; 2021-461488 / [01] REMOVED ACCESS PANEL 522DB AND FLEX SKIN LOC SLAT 4 AT LEVEL SLAT STATION 85.19 LT WING IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION AND NOT FOUND DAMAG
- [SDR SWAA2021072997629](https://openairdocs.org/sdr/SWAA2021072997629.md): Line · broken · Jul 26, 2021 · N757LV · Boeing 7377H4 · Hydraulic System, Main
  > HAD A LOSS OF HYDRAULIC QTY. IN FLIGHT; COMPLIED WITH QRH FOR LOSS OF HYD A; NORMAL LANDING SPEED; TOUCH DOWN WAS NORMAL.; / [01] FOUND NOSE LANDING GEAR TRANSFER CYLINDER HYDRAULIC LINE BROKEN. REMOVED AND REPLACED HYDRAULIC LINE PER A.M.M. 29-11-00 AND A.M.
- [SDR SWAA2020122838588](https://openairdocs.org/sdr/SWAA2020122838588.md): Lens · detached · Dec 23, 2020 · N757LV · Boeing 7377H4 · Emergency Lighting
  > L1 DOOR LOWER EMERGENCY EXIT SIGN LENS FELL OFF. DMA # 0414460 R & R EXIT 1 BL ASSEMBLY ON L1 ENTRANCE, REF AMM 35-51-01 CL NR 64016.
- [SDR SWAA2020111630483](https://openairdocs.org/sdr/SWAA2020111630483.md): Slide · loose · Nov 12, 2020 · N757LV · Boeing 7377H4 · Escape Slide
  > L2 AFT EMERGENCY SLIDE IS LOOSE. INSPECTED L2 SLIDE, IAW AMM 25-66-01 NO DEFECTS FOUND R1 SLIDE SLIGHTLY LOOSE. REMOVED RESECURED, IAW MT 725-61-06, AIRCRAFT OK FOR SERVICE.
- [SDR SWAA2020082010007](https://openairdocs.org/sdr/SWAA2020082010007.md): Hmu · slow · Jun 18, 2020 · N757LV · Boeing 7377H4 · Fuel Controlling System
  > WAIVE DESCENDING FOR TURBULENCE 400-380 NO PROBLEMS NOTED AFTER DESCENT AND LEVELING @ 380 ENGINE WAS SLOW TO POWER UP (AUTO THROTTLES ON) DESCENDED TO 360 AND #1 ENGINE WAS HOVERING @ 55% AND SLOWLY ROLLING BACK/DECENDED @ IDLE ENG FAIL LIGHT CAME ON /DECENDE
- [SDR SWAA2020061291274](https://openairdocs.org/sdr/SWAA2020061291274.md): Light · loose · Jun 10, 2020 · N757LV · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTING FLOOR STRIP AT ROW 8 LOOSE. SECURED FLOOR PROXIMITY LIGHT STRIP PER AMM 33-51-15.
- [SDR SWAA2020022841918](https://openairdocs.org/sdr/SWAA2020022841918.md): Light · broken · Feb 26, 2020 · N757LV · Boeing 7377H4 · Emergency Lighting
  > CENTER AISLE EMERGENCY LIGHT BROKEN. / R&R LIGHT ASSEMBLY PER MM.
- [SDR SWAA2020012840829](https://openairdocs.org/sdr/SWAA2020012840829.md): Light · inoperative · Jan 26, 2020 · N757LV · Boeing 7377H4 · Emergency Lighting
  > L1 DOOR EMERGENCY LIGHT INOP. R&R LIGHT ASSEMBLY IAW AMM.
- [SDR SWAA2020011640495](https://openairdocs.org/sdr/SWAA2020011640495.md): Light · inoperative · Jan 14, 2020 · N757LV · Boeing 7377H4 · Emergency Lighting
  > LT OVERWING EXIT DOOR SIDEWALL LIGHT INOP. R&R LIGHT ASSEMBLY PER MM.
- [SDR SWAA2019120339300](https://openairdocs.org/sdr/SWAA2019120339300.md): Slide · loose · Dec 2, 2019 · N757LV · Boeing 7377H4 · Escape Slide
  > L1 DOOR SLIDE NEEDED REPACKED. / STOWED SLIDE PER MT.
- [SDR SWAA2019110638648](https://openairdocs.org/sdr/SWAA2019110638648.md): Light · inoperative · Nov 5, 2019 · N757LV · Boeing 7377H4 · Emergency Lighting
  > R/H EMERGENCY EXIT DOOR, LOWER AFT LIGHT IS INOP. / RELAMPED R/H EMERGENCY EXIT DOOR, LOWER AFT LIGHT.
- [SDR SWAA2022032385028](https://openairdocs.org/sdr/SWAA2022032385028.md): Doubler · debonded · Oct 25, 2019 · N757LV · Boeing 7377H4 · Aerodynamic Fairings
  > FAIRING PANEL #192F DME ANTENNA NUTPLATE DOUBLER COMMON TO FAIRING IS DISBONDED / INSTALLED FAIRING PANEL 192F DME ANTENNA NUTPLATE IAW AMM 51-31-00-390-801 AND BOEING DWG 149A7752
- [SDR SWAA2019102238125](https://openairdocs.org/sdr/SWAA2019102238125.md): Support Angle · corroded · Oct 15, 2019 · N757LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY BULKHEAD TO FLOOR PANEL LOWER SUPPORT ANGLE CORRODED AT BS. 947, RBL 24. / R&R ANGLE IAW SRM & DWG.
- [SDR SWAA2022040685020](https://openairdocs.org/sdr/SWAA2022040685020.md): Floor Support · cracked · Oct 14, 2019 · N757LV · Boeing 7377H4 · Fuselage Main, Structure
  > FLOOR SUPPORT CRACKED AT BS 277-294 BL 0 WL 208 / REMOVED CRACK DAMAGED FLOOR SUPPORT AT BS277-294 BL0 WL208 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-05-0G-0 LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-05-0G-0 OK TO INS
- [SDR SWAA2022040485019](https://openairdocs.org/sdr/SWAA2022040485019.md): Floor Panel · delaminated · Oct 14, 2019 · N757LV · Boeing 7377H4 · Fuselage Floor Panel
  > FLOORPANEL 221BF HAS DELAMINATION AND BROKEN INSERTS / REPLACED FLOOR PANEL 221BF DUE TO DELAMINATION AND BROKEN INSERTS. FLOOR PANEL 221BF WILL BE INSTALLED ON NRC T986172. PER SRM 51-10-02-0G-0 PARAGRAPH 9
- [SDR SWAA2019110638646](https://openairdocs.org/sdr/SWAA2019110638646.md): Skin · damaged · Oct 10, 2019 · N757LV · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > DAMAGED FUSELAGE SKIN BS 1040+6" TO 1040+13" STR 1" ABOVE 23R TO 2" ABOVE 24R REQUIRES SKIN REPAIR (REFERENCE CUSTOMER CARDS T986010,T986011,T986013, T986014, T986015, T986016, T986018). / REPAIR TO FUSELAGE SKIN AT BS 1040+6" TO BS 1040+13" 1" ABOVE
- [SDR SWAA2022040585008](https://openairdocs.org/sdr/SWAA2022040585008.md): Angle · cracked · Oct 8, 2019 · N757LV · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > FOUND CRACKED SUPPORT ANGLES BEHIND WATER SERVICE PANEL AT ACB BS907+9 RBL12 WL170. MARKED / REMOVED & REPLACED THE SUPPORT ANGLES BEHIND WATER SERVICE PAN A.C.B. BS 907+9 RBL 12 WL 170 INSTALLED PER SRM 51-40-02-0G-0 AND AIPC 52-49-00-02
- [SDR SWAA2022040585007](https://openairdocs.org/sdr/SWAA2022040585007.md): Strap · corroded · Oct 8, 2019 · N757LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ***CORROSION*** ON TENSION STRAP AT AFT CARGO BAY BS 847 RBL8 WL163. MARKED / AREAS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 FIG 103.D LOCATED AND DRILLED REPLACEMENT TENSION STRAP AT AFT CARGO BAY BS785- 862; RBL8; WL163; IAW SRM 51-40-05-0G-0; INSTALL
- [SDR SWAA2019110638644](https://openairdocs.org/sdr/SWAA2019110638644.md): Frame · dented · Oct 8, 2019 · N757LV · Boeing 7377H4 · Fuselage Main, Frame
  > DENT ON THE FRAME AT AFT CARGO BAY BS 727C 3" ABOVE S-22R WL173. / REPAIRED PER: EA 1-753-35959 REV IR AND ATS ER 19-05297 REV IR.
- [SDR SWAA2019102338153](https://openairdocs.org/sdr/SWAA2019102338153.md): Support · corroded · Oct 8, 2019 · N757LV · Boeing 7377H4 · Fuselage Main, Floor Beam
  > AFT CARGO BAY FLOOR PANEL SUPPORT SPLICE CORRODED AT BS. 727D+6, BETWEEN LBL 19 TO RBL 19. / R&R SUPPORT SPLICE PER PO.
- [SDR SWAA2019102338152](https://openairdocs.org/sdr/SWAA2019102338152.md): Splice · corroded · Oct 8, 2019 · N757LV · Boeing 7377H4 · Fuselage Main, Floor Beam
  > AFT CARGO BAY FLOOR PANEL SUPPORT SPLICE CORRODED AT BS. 767+6, BETWEEN LBL 19 TO RBL 19. / R&R SPLICE PER WO.

Next page: https://openairdocs.org/aircraft/N757LV/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 = 'N757LV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N757LV/reports

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