# Service difficulty reports: N440LV

A list on [N440LV](https://openairdocs.org/aircraft/N440LV.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 7 · 304 reports

- [SDR SWAA2026100566166](https://openairdocs.org/sdr/SWAA2026100566166.md): Battery Pack · failed · Oct 1, 2026 · N440LV · Boeing 7377H4 · Emergency Lighting
  > LT EMERGENCY LIGHT BATTERY PACK M1668, FAILED A CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026100527632](https://openairdocs.org/sdr/SWAA2026100527632.md): Battery Pack · no test · Oct 1, 2026 · N440LV · Boeing 7377H4 · Emergency Lighting
  > AFT RT EMERGENCY BATTERY PACK M1672 FAILED A CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026100543416](https://openairdocs.org/sdr/SWAA2026100543416.md): Battery Pack · no test · Oct 1, 2026 · N440LV · Boeing 7377H4 · Emergency Lighting
  > FWD RT BATTERY PACK M1674 FAILED A CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026100549619](https://openairdocs.org/sdr/SWAA2026100549619.md): Battery Pack · no test · Oct 1, 2026 · N440LV · Boeing 7377H4 · Emergency Lighting
  > FWD LT EMERGENCY BATTERY PACK M1675 FAILED A CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2026072700354](https://openairdocs.org/sdr/SWAA2026072700354.md): Panel · delaminated · Jul 21, 2026 · N440LV · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > RT HORIZONTAL STAB UPPER TRAILING EDGE PANEL HAS DELAMINATION ON OTBD CORNER. FROM CORNER GOING INBD L=1.9 INCHES LONG W=1.5 CONDUCTIVE STRIP HAS HAS DAMAGE AND RIVET PULLED THROUGH AT DELAMINATION LOCATION ACCOMPLISHED EA 26-155-01964.
- [SDR SWAA2026072760264](https://openairdocs.org/sdr/SWAA2026072760264.md): Cap · damaged · Jul 21, 2026 · N440LV · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > RT HORIZONTAL END CAP DAMAGED. CRACK ON TOP 1.25 INCHES LONG AND CRACK ON BOTTOM MEASURES 2 INCHES LONG. ACCOMPLISHED EA 26-155-01964
- [SDR SWAA2026020667034](https://openairdocs.org/sdr/SWAA2026020667034.md): Battery Pack · no test · Feb 3, 2026 · N440LV · Boeing 7377H4 · Emergency Lighting
  > BATTERY PACK M01669 FAILED CHECK AT SEAT 15 DEF. R & R EMERGENCY BATTERY PACK IAW AMM 33-51-06.
- [SDR SWAA2025123056140](https://openairdocs.org/sdr/SWAA2025123056140.md): Girt Bar · out of position · Dec 28, 2025 · N440LV · Boeing 7377H4 · Emergency Equipment
  > R1 DOOR SLIDE GIRT BAR FLAP OUT OF POSITION. REPOSITION GIRT FLAPS IN SLIDE COVER REF AMM 25-66-00.
- [SDR SWAA2025102727286](https://openairdocs.org/sdr/SWAA2025102727286.md): Skin · delaminated · Oct 23, 2025 · N440LV · Boeing 7377H4 · Trailing Edge Flaps
  > RIGHT INBD FLAP HAS SKIN DELAMINATION AT THE OTBD AFT EDGE 7" FROM EDGE OF FLAP MEASURING 3.5 LONG AND 0.5 IN WIDTH. FOUND DAMAGE TO BE IN ZONE 3 & REPAIRABLE IAW SRM 57-53-01-1A-1, REPAIRED IAW SRM 57-53-01-1A-1 (4) (A) (7) (A).
- [SDR SWAA2025082105671](https://openairdocs.org/sdr/SWAA2025082105671.md): Slide · out of position · Aug 18, 2025 · N440LV · Boeing 7377H4 · Escape Slide
  > AFT LH DOOR SLIDE LOWER FLAP OUT OF CASE. REPOSITIONED SLIDE PER MT 725-61-06
- [SDR SWAA2025052374041](https://openairdocs.org/sdr/SWAA2025052374041.md): Cover · out of adjust · May 22, 2025 · N440LV · Boeing 7377H4 · Escape Slide
  > PAX CABIN AFT LEFT DOOR SLIDE COVER RUBBING AGAINST TO SCUFF PLATE TO CLOSE POSITION. 2025-296367 <[01]. INSTALLED CORRECTLY AFT LEFT SLIDE COVER IAW MT 725-61-06 TTG8Q010SL8G; [02] COMPLETED.
- [SDR SWAA2025052374046](https://openairdocs.org/sdr/SWAA2025052374046.md): Light · out of adjust · May 22, 2025 · N440LV · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ON OVERHEAD BIN AT SEAT 3DEF IS LOOSE 2025-296338 <[01]. INSTALLED CORRECTLY EMERGENCY EXIT LIGHT ON OVERHEAD BIN AT SEAT 3DEF IAW SOPM 20-50-12 REV 57; [02] CERTIFIED WORK PERFORMED.
- [SDR SWAA2025052374047](https://openairdocs.org/sdr/SWAA2025052374047.md): Handle · loose · May 22, 2025 · N440LV · Boeing 7377H4 · Galley Doors
  > PAX CABIN FWD SERVICE DOOR LINING ASSISTANT HANDLE LOOSE 2025-296356 <[01]. INSTALLED CORRECTLY FWD SERVICE DOOR LINING ASSISTANT HANDLE IAW B737-700 AMM 52-41-31-400-802 ITEM 3.F.(2); [02] TIGHTENED FWD SERVICE DOOR LINING ASSISTANT HANDLE IAW B737-700 AMM 5
- [SDR SWAA2025052368755](https://openairdocs.org/sdr/SWAA2025052368755.md): Web · corroded · May 8, 2025 · N440LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER SILL WEB LOCATED BS 460 AT FWD CARGO DOOR CUTOUT STRUCTURE 2025-296297 <[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE:
- [SDR SWAA2025052267151](https://openairdocs.org/sdr/SWAA2025052267151.md): Battery Pack · inoperative · May 5, 2025 · N440LV · Boeing 7377H4 · Emergency Lighting
  > INOP LOWERED CEILING PANEL BATTERY PACK LT POSITION AT AFT GALLEY AREA 2025-296223 <[01]. REPLACED BATTERY PACK LT POSITION AT AFT GALLEY AREA IAW B737-700 AMM 33-51-06-960-805 INSTALLATION TEST OK; [02] JOB COMPLETED AND TEST IS OK.
- [SDR SWAA2025052267152](https://openairdocs.org/sdr/SWAA2025052267152.md): Light · inoperative · May 5, 2025 · N440LV · Boeing 7377H4 · Emergency Lighting
  > INOP LOWERED CEILING PANEL BATTERY PACK RT POSITION AT AFT GALLEY AREA 2025-296224 <[01]. PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST IAW B737-700 AMM 33-51-00-710-801 TEST OK;[02] JOB COMPLETED; AND TEST IS OK.
- [SDR SWAA2025052366807](https://openairdocs.org/sdr/SWAA2025052366807.md): Splice · corroded · May 3, 2025 · N440LV · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION L SHAPE STRINGER SPLICE ON STR28L LOC BS 360 AT EQUIPMENT ELECTRONIC COMP 2025-296187<[01]. TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 29 JAN 26; P/N P3015GOES00000 S/N 112820025 DUE DATE 28 JAN 26.; [02] REPLACED SP
- [SDR SWAA2025052367145](https://openairdocs.org/sdr/SWAA2025052367145.md): Plate · cracked · May 3, 2025 · N440LV · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACK ON CORRUGATED PLATE LOCATED AT LEVEL IRSS 229 TRAILING EDGE AT RT WING 2025-296204 <[01]. REPLACED CORRUGATED PLATE LOCATED AT LEVEL IRSS 229 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02;SRM 51-10-02 ITEM 9 AND DWG 115A2001; SHEET 30; REV A.; [02]
- [SDR SWAA2025052266808](https://openairdocs.org/sdr/SWAA2025052266808.md): Web · corroded · May 3, 2025 · N440LV · Boeing 7377H4 · Fuselage Main, Structure
  > CORROSION WEB LOC ON STR28L AND BS 360 AT EQUIPMENT ELECTRONIC COMP 2025-296188 <[01]. REPLACED REPAIR WEB LOC. BS 351 TO BS 360; PLATE LOC BS 360;ANGLE LOC BS 351 ON STR 28L AT EQUIPMENT ELECTRONIC COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 141A8511 SHEET
- [SDR SWAA2025052766286](https://openairdocs.org/sdr/SWAA2025052766286.md): Access Panel · cracked · May 1, 2025 · N440LV · Boeing 7377H4 · Wing, Plate/Skin
  > CRACK COVER OF ACCESS PANEL 551FB AT LT WING 2025-296072<[01] REMOVED AND REPLACED COVER OF ACCESS PANEL 551FB AT LT WING IAW B737-700 SRM 51-40-02-0G-0 GENERAL AND DWG 115A2200. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] JOB COMPLETED.
- [SDR SWAA2025052366417](https://openairdocs.org/sdr/SWAA2025052366417.md): Strap · corroded · May 1, 2025 · N440LV · Boeing 7377H4 · Cargo Compartments
  > CORROSION ON STRAP LOCATED BS 794.3 BTW STR 25R TO STR 26R WL 256.1 AT CUTOUT AFT CARGO DOOR 2025-296096 <[01]. TOOL USED: POWER PACK FMK0003223 S/N PE0412/63335 DUE DATE 17 JUN 25; THERMOMETER P/N FLUKE 566 S/N 587770091WS DUE DATE 30 JUN 26; MULTIMETER P/N F
- [SDR SWAA2025052366281](https://openairdocs.org/sdr/SWAA2025052366281.md): Intercostal · cracked · May 1, 2025 · N440LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL LOCATED BS 540 BTW BL 0 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN 2025-296066 <[01]. REMOVED INTERCOSTAL LOCATED BS 540 BTW BL 0 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN DUE TO NO FOUND ALLOWABLE DAMAGE ON B737-700 SRM 53-30-51-1A-1 ALLOWAB
- [SDR SWAA2025052366282](https://openairdocs.org/sdr/SWAA2025052366282.md): Support Bracket · cracked · May 1, 2025 · N440LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BS 695 RBL 24.75 WL 208.1 AT PASSENGER CABIN 2025-296067 <[01]. REPLACED SUPPORT ANGLE REPAIR LOCATED BS 695 RBL 24.75 WL 208.1 AT PASSENGER CABIN IAW. B737-700 SRM 51-40-02-0G AND DWG 273A9112; SHEET:30; REV - AND DWG 111A6000 S
- [SDR SWAA2025052266285](https://openairdocs.org/sdr/SWAA2025052266285.md): Web · cracked · May 1, 2025 · N440LV · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 31 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.600 INCHES. 2025-296071<[01]. TOOL USED IN STEP 6: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 200053402 DUE DATE: 16-SEP-25; [02] TOOL USED IN STEP 7: E
- [SDR SWAA2025052365683](https://openairdocs.org/sdr/SWAA2025052365683.md): Scuff Plate · cracked · Apr 30, 2025 · N440LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2025-296011<[01]. TOOL USED DIGITAL CALIPER P/N: 500-193-30; S/N: 0000291; DUE DATE: 01-NOV-25.; [02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N: 1753759; DUE DATE: 30/JUN/25; [03] REPAIRED F
- [SDR SWAA2025052765680](https://openairdocs.org/sdr/SWAA2025052765680.md): Support Bracket · cracked · Apr 29, 2025 · N440LV · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING 2025-295979<[01] REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 6 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT BR
- [SDR SWAA2025052765679](https://openairdocs.org/sdr/SWAA2025052765679.md): Support Bracket · cracked · Apr 29, 2025 · N440LV · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK SUPPORT BRACKET INBOARD TRAILING EDGE ORSS 271 AT LT WING 2025-295977<[01] REPLACED SUPPORT BRACKET INBOARD TRAILING EDGE ORSS 271 AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 6 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[0
- [SDR SWAA2025052765678](https://openairdocs.org/sdr/SWAA2025052765678.md): Angle · cracked · Apr 29, 2025 · N440LV · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING 2025-295976<[01] REPLACED ANGLE AND FASTENERS LOC. TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET: 7 REV:-.
- [SDR SWAA2025052265256](https://openairdocs.org/sdr/SWAA2025052265256.md): Nut · deteriorated · Apr 28, 2025 · N440LV · Boeing 7377H4 · Passenger/Crew Doors
  > DETERIORATED ENTRY DOOR ASSIST HANDLE NUT UPPER AND LOWER POSITION AT FWD GALLEY AREA (4 EA) 2025-295954 <[01]. REPLACED ENTRY DOOR ASSIST HANDLE NUT UPPER AND LOWER POSITION AT FWD GALLEY AREA (4 EA) IAW B737-700 AMM 52-11-31-000-802 STEP 2. F (3) AND AMM 52-
- [SDR SWAA2025042859789](https://openairdocs.org/sdr/SWAA2025042859789.md): Isolator · cracked · Apr 22, 2025 · N440LV · Boeing 7377H4 · Escape Slide
  > FWD GALLEY SERVICE DOOR FWD LOWER SLIDE ISOLATOR IS CRACKED<[01] R&R FWD GALLEY SERVICE DOOR FWD LOWER SLIDE ISOLATOR IAW SRM 51-40-02.;[02] C/W INSPECTION
- [SDR SWAA2025042859779](https://openairdocs.org/sdr/SWAA2025042859779.md): Girt Bar · worn · Apr 22, 2025 · N440LV · Boeing 7377H4 · Escape Slide
  > AFT GALLEY SERVICE DOOR SLIDE GIRT WORN<[01] R&R AFT SERV DOOR EVAC SLIDE IAW AMM 25-66-01; REF. TTG8Q00ZZVW1.;[02] 02 - INSPECTED PER [AMM 25-66-01-401-NG (DOOR-MOUNTED ESCAPE SYSTEM - REMOVAL/INSTALLATION - PERMANENT)]
- [SDR SWAA2025042827188](https://openairdocs.org/sdr/SWAA2025042827188.md): Door Frame · cracked · Apr 22, 2025 · N440LV · Boeing 7377H4 · Fuselage Main, Structure
  > GROUND POWER CONNECTOR DOOR FRAME HAS A 2-INCH CRACK. REMOVED DAMAGE PER SRM 51-10-02. C/W EA 25-153-01032.
- [SDR SWAA2024123081269](https://openairdocs.org/sdr/SWAA2024123081269.md): Acm · seized · Dec 27, 2024 · N440LV · Boeing 7377H4 · Cabin Cooling System
  > ON CLIMB AND DESCENT LEFT PACK HAD WET SOCK SMELL IN COCKPIT AND FWD GALLEY. PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-56. FOUND SMELL TO BE FROM LEFT PACK. FWD LEFT PACK TO MEL 21-1-01. RAN LEFT PACK; PACK TRIP OFF LIGHT ILLUMINATED. FOUND ACM SEIZED.
- [SDR SWAA2024101547689](https://openairdocs.org/sdr/SWAA2024101547689.md): Connector · faulted · Oct 11, 2024 · N440LV · Boeing 7377H4 · Engine Indicating System Wiring
  > ON TAKEOFF #2. EGT TURNED RED AND 933 DEGREES WAS RECORDED. ALL OTHER ENGINE INDICATIONS WERE NORMAL. ON TAKEOFF #2. EGT TURNED RED AND 933 DEGREES WAS RECORDED. ALL OTHER ENGINE INDICATIONS WERE NORMAL. A/T WERE DISCONNECTED AND THRUST REDUCED AS EGT RETURNED
- [SDR SWAA2024101548828](https://openairdocs.org/sdr/SWAA2024101548828.md): Probe · out of limits · Oct 11, 2024 · N440LV · Boeing 7377H4 · Engine EGT/TIT Indicating System
  > ON TAKEOFF #2. EGT TURNED RED AND 933 DEGREES WAS RECORDED. ALL OTHER ENGINE INDICATIONS WERE NORMAL. ON TAKEOFF #2. EGT TURNED RED AND 933 DEGREES WAS RECORDED. ALL OTHER ENGINE INDICATIONS WERE NORMAL. A/T WERE DISCONNECTED AND THRUST REDUCED AS EGT RETURNED
- [SDR SWAA2024091136030](https://openairdocs.org/sdr/SWAA2024091136030.md): Transmitter · inoperative · Sep 10, 2024 · N440LV · Boeing 7377H4 · Trailing Flap Position Indicating System
  > FLAPS WOULD NOT EXTEND PAST AN INDICATION OF 2 DEGREES WITH THE FLAP HANDLE IN POSITION 5-30. FLAPS WOULD NOT EXTEND PAST 10 DEGREES USING ALTERNATE FLAP EXTENSION PROCEDURES<[01] R&R?D RIGHT WING FLAP POSITION TRANSMITTER AND OPS CHECKED PER MM 27-58-01. OPS
- [SDR SWAA2024082630193](https://openairdocs.org/sdr/SWAA2024082630193.md): Skin · delaminated · Aug 25, 2024 · N440LV · Boeing 7377H4 · Trailing Edge Flaps
  > LH OB AFT FLAP PREVIOUS REPAIR DELAM<[01] REMOVED LH OB AFT FLAP IAW AMM 27-51-22;[02] OK TO INSTALL LH OB AFT FLAP.SN 000856.;[03] INSTALLED L/H AFT.OUTBOARD FLAP PER M/M 27-51-22;[04] REMOVED AND REPLACED L/H AFT. OUTBOARD FLAP PER M/M 27-51-22;[05] C/W RII
- [SDR SWAA2024081625704](https://openairdocs.org/sdr/SWAA2024081625704.md): Bracket · cracked · Aug 14, 2024 · N440LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > RIGHT MAIN LANDING GEAR CENTER DOOR LOWER FWD MOUNT BRACKET CRACKED AT THE BARREL NUT.<[01] REMOVED RH MLG CENTER/INNER DOOR TO FOM IAW AMM 32-13-11. INSTALLED NEW SERRATED PLATE ON NEW CENTER DOOR FWD MOUNT IAW SRM 51-40-02.;[02] VERIFIED - REMOVED RH MLG CEN
- [SDR SWAA2024081625705](https://openairdocs.org/sdr/SWAA2024081625705.md): Plate · corroded · Aug 14, 2024 · N440LV · Boeing 7377H4 · Main Landing Gear
  > NLG HAS EXPOSED CORROSION AT AFT UPPER ASSY AREA WHERE IT BOLTS TO UPPER STEERING PLATE.<
- [SDR SWAA2024081525708](https://openairdocs.org/sdr/SWAA2024081525708.md): Bracket · cracked · Aug 14, 2024 · N440LV · Boeing 7377H4 · Galley Doors
  > CABIN R2 SERVICE DOOR LOWER LINER ATTACH PANEL; FWD BRACKET IS CRACKED.<[01] REMOVED AND REPLACED CABIN R2 SERVICE DOOR LOWER LINER ATTACH PANEL PER AMM 52-41-61
- [SDR SWAA2024081525706](https://openairdocs.org/sdr/SWAA2024081525706.md): Support · cracked · Aug 14, 2024 · N440LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT E&E L/H FWD GALLEY FLOOR BOARD SUPPORT BETWEEN STA. 312 & 328 CRACKED AT CENTER FASTENER HOLE.<[01] REMOVED AND REPLACED AFT E&E L/H FWD GALLEY FLOOR BOARD SUPPORT BETWEEN STA. 312 & 328 IAW SRM 51-40-02
- [SDR SWAA2024071713528](https://openairdocs.org/sdr/SWAA2024071713528.md): Fastener · loose · Jul 16, 2024 · N440LV · Boeing 7377H4 · Passenger/Crew Doors
  > FASTENERS LOOSE ON LEFT SIDE AFT ENTRY DOOR SLIDE COVER<[01] SECURED SLIDE COVER FASTENERS IAW SIP
- [SDR SWAA2023113025140](https://openairdocs.org/sdr/SWAA2023113025140.md): Charger · inoperative · Nov 27, 2023 · N440LV · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN LIGHTING EMER CHAR R AFT P18-3 B-10 CB POPPED<[01] REPLACED CHARGER IN AFT GALLEY OVERHEAD PER AMM 33-51-06
- [SDR SWAA2023102715117](https://openairdocs.org/sdr/SWAA2023102715117.md): Lamp · missing · Oct 25, 2023 · N440LV · Boeing 7377H4 · Emergency Lighting
  > EXIT SIGN COVER AT FORWARD SERVICE DOOR MISSING<[01] R&R FWD FWD SERVICE DOOR EMERGENCY EXIT LAMP ASSY PER AMM 33-51-02
- [SDR SWAA2023070563553](https://openairdocs.org/sdr/SWAA2023070563553.md): Panel · elongated · May 31, 2023 · N440LV · Boeing 7377H4 · Nacelle/Pylon, Plate/Skin
  > #2 ENG INLET COWL LOWER ANTI ICE VENT ACCESS PANEL HAS ELONGATED HOLES AT FASTENER LOCATIONS<[01] LOCATED; DRILLED AND PERFORMED COUNTERINK ON FASTENER HOLES REF. SRM 51-40-08-0G-0; REF. SRM 51-40-05-0G-0. APPLIED TOP COAT PAINT TO PANEL 422 AB REF. AMM 51-2
- [SDR SWAA2023070563549](https://openairdocs.org/sdr/SWAA2023070563549.md): Channel · corroded · May 28, 2023 · N440LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > LEFT 'Z' CHANNEL AT B/S 727A-727C IS CORRODED<[01] WORK WILL BE ACCOMPLISHED ON WOR CARD TTG8Q00LAZEK;[02] VERIFIED WORK CARD NOTE: NEW 'Z' CHANNEL WILL BE INSTALLED
- [SDR SWAA2023070563548](https://openairdocs.org/sdr/SWAA2023070563548.md): Channel · corroded · May 28, 2023 · N440LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO LEFT 'Z' CHANNEL IS CORRODED AT B/S 727C-807<[01] REMOVED AND REPLACED AFT CARGO LEFT 'Z' CHANNEL AT B/S 727C-807 PER REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1 Z CHANNEL REPLACED
- [SDR SWAA2023070563551](https://openairdocs.org/sdr/SWAA2023070563551.md): Support · corroded · May 28, 2023 · N440LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR SUPPORT STRINGER AT B/S 937 8 INCHES LEFT OF CENTER LINE IS CORRODED AT NUT PLATE HOLE. CORROSION IS AROUND NUT PLATE AT ABOUT B/S 937 AND LBL-3 (ON TIE-DOWN RAIL)<[01] REMOVE AND REPACED TRACK TIE D0WN L/ H SIDE FROM STA 887 TO STA 947.5 PER R
- [SDR SWAA2023070563550](https://openairdocs.org/sdr/SWAA2023070563550.md): Support · corroded · May 28, 2023 · N440LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR SUPPORT STRINGER IS CORRODED AT B/S 935 14 INCHES RIGHT OF CENTER LINE<[01] REMOVE AND REPLACED TRACK TIE D0WN R/ H SIDE FROM STA 887 TO STA 947.5 PER REF SRM 51-40-02-0G-0;[02] VERIFIED STEP # 1;[03] VERIFIED STEP # 1
- [SDR SWAA2023070552568](https://openairdocs.org/sdr/SWAA2023070552568.md): Intercostal · cracked · May 26, 2023 · N440LV · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CABIN WET AREA L/H SIDE WALL INTERCOSTAL CRACKED @ S-16L BETWEEN STA 259.5 & 303.8 MKD DOT CORRECTION FWD CABIN WET AREA L/H SIDE WALL INTERCOSTAL CRACKED @ S-16L BETWEEN STA 294.5 & 303.9<[01] REMOVE AND REPLACE DAMAGE INTERCOSTAL;[02] CORRECTION TO STEP#

Next page: https://openairdocs.org/aircraft/N440LV/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 = 'N440LV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N440LV/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.