# Service difficulty reports: N470WN

A list on [N470WN](https://openairdocs.org/aircraft/N470WN.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 · 315 reports

- [SDR SWAA2026101935213](https://openairdocs.org/sdr/SWAA2026101935213.md): Hook · loose · Oct 14, 2026 · N470WN · Boeing 7377H4 · Emergency Equipment
  > ESCAPE SLIDE GIRT BAR HOOKS WERE LOOSE AT THE FWD BOARDING DOOR. ADJUSTED THE SLIDE COVER HOOKS IAW SIP. OPS CHKD NORMAL.
- [SDR SWAA2026090427229](https://openairdocs.org/sdr/SWAA2026090427229.md): Strap · cracked · Aug 25, 2026 · N470WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > RIGHT STUB BEAM STRAP FOUND CRACKED, BS 639, OTBD LAYER. REMOVED THE STRAP ASSY STUB BEAM BS 639 IAW SRM 51-40-02-0G-0. INSTALLED A NEW STUB BEAM STRAP
- [SDR SWAA2026082510937](https://openairdocs.org/sdr/SWAA2026082510937.md): Clamp · unsecure · Aug 21, 2026 · N470WN · Boeing 7377H4 · Airfoil Anti/De-ice System
  > LEFT WING BODY OVERHEAT LIGHT. PERFORMED QRH PROCEDURES. AFTER SOME TIME THE LIGHT EXTINGUISHED. PERFORMED BITE PROCEDURE IAW FIM 26-18, TASK 806. FOUND FAULT NR 14. FOUND LEAK UNDER PANEL 521AB JUST OTBD OF ENG. RESECURED CLAMP OTBD OF WING ANTI-ICE VALVE
- [SDR SWAA2026081172360](https://openairdocs.org/sdr/SWAA2026081172360.md): Screw · missing · Aug 7, 2026 · N470WN · Boeing 7377H4 · Emergency Lighting
  > ROW 15 FO SIDE EXIT SIGN MISSING SCREW. REMOVED AND REPLACED R/H OVERWING EXIT DOOR LOWER EMERGENCY EXTI DOOR SIGN IAW SRM 51-40-02.
- [SDR SWAA2026041789145](https://openairdocs.org/sdr/SWAA2026041789145.md): Light · damaged · Apr 14, 2026 · N470WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT ASSEMBLY ON HEADER PANEL JUST AFT OF FLIGHT DECK DAMAGED INTERNALLY. REMOVED, REPLACED, AND PERFORMED A GOOD OPS TEST OF EMERGENCY LIGHT IAW AMM 33-51-01-960-802.
- [SDR SWAA2026042085505](https://openairdocs.org/sdr/SWAA2026042085505.md): Threshold Web · corroded · Apr 1, 2026 · N470WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY SUB WEB THRESHOLD AT BS 794 - 847, RBL 25, WL 155. REMOVED AND REPLACED ON AFT CARGO BAY SUB-THRESHOLD WEB IAW SRM 51-40-02, AND DWG 146A8340, REV-.
- [SDR SWAA2026042085514](https://openairdocs.org/sdr/SWAA2026042085514.md): Seat Track · corroded · Apr 1, 2026 · N470WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LBL 25 AT BS500+6; BS500A+17; BS500B+18; BS500D+10. SEAT TRACK WILL BE REPLACED ON FAULT TTG8Q01BFPBT.
- [SDR SWAA2026042085523](https://openairdocs.org/sdr/SWAA2026042085523.md): Seat Track · corroded · Apr 1, 2026 · N470WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LBL 45 AT BS480+17; BS500+6; BS500A+17; BS500B+18; BS550D+1; BS500D+10. SEAT TRACK WILL BE REPLACED ON FAULT# TTG8Q01BFPBJ.
- [SDR SWAA2026041784730](https://openairdocs.org/sdr/SWAA2026041784730.md): Nonskid · peeling · Mar 31, 2026 · N470WN · Boeing 7377H4 · Passenger Compartment Equipment
  > LEFT AND RIGHT WING INBD UPPER SURFACE EMERGENCY EXIT NONSLIP WALKWAYS HAVE PEELING PAINT. TOUCHED UP AREAS OF MISSING OR WORN PAINT ON THE LEFT AND RIGHT WING I/B UPPER SURFACE EMERGENCY EXIT NONSLIP WALKWAYS IAW AMM 51-21-97-370-802.
- [SDR SWAA2026041685176](https://openairdocs.org/sdr/SWAA2026041685176.md): Floor Panel · debonded · Mar 31, 2026 · N470WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231ZF UPPER SKIN HAS A LARGE DISBOND NEAR AFT END OF PANEL. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026041685173](https://openairdocs.org/sdr/SWAA2026041685173.md): Floor Panel · pulled · Mar 31, 2026 · N470WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026041685174](https://openairdocs.org/sdr/SWAA2026041685174.md): Floor Panel · pulled · Mar 31, 2026 · N470WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026041685179](https://openairdocs.org/sdr/SWAA2026041685179.md): Floor Panel · pulled · Mar 31, 2026 · N470WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATION OF A NEW FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026041685180](https://openairdocs.org/sdr/SWAA2026041685180.md): Floor Panel · pulled · Mar 31, 2026 · N470WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 241FF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATION OF A NEW FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026041685178](https://openairdocs.org/sdr/SWAA2026041685178.md): Floor Panel · pulled · Mar 31, 2026 · N470WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026041685182](https://openairdocs.org/sdr/SWAA2026041685182.md): Floor Panel · pulled · Mar 31, 2026 · N470WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026041685172](https://openairdocs.org/sdr/SWAA2026041685172.md): Floor Panel · pulled · Mar 31, 2026 · N470WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED A NEW 231XF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026041685177](https://openairdocs.org/sdr/SWAA2026041685177.md): Floor Panel · pulled · Mar 31, 2026 · N470WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026041685181](https://openairdocs.org/sdr/SWAA2026041685181.md): Floor Panel · damaged · Mar 31, 2026 · N470WN · Boeing 7377H4 · Fuselage Floor Panel
  > FLOOR PANEL 242AF UPPER SKIN HAS LARGE FAILED PREVIOUS REPAIR NEAR FWD EDGE. FABRICATION OF NEW 242AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.
- [SDR SWAA2026042784717](https://openairdocs.org/sdr/SWAA2026042784717.md): Skin · pulled · Mar 30, 2026 · N470WN · Boeing 7377H4 · Nacelle/Pylon, Plate/Skin
  > FOUND PULLED THRU FASTENER ON NR 2 ENG INLET LIP SKIN AT THE 4 O'CLOCK POSITION.
- [SDR SWAA2026031678775](https://openairdocs.org/sdr/SWAA2026031678775.md): Coffeemaker · odor · Mar 12, 2026 · N470WN · Boeing 7377H4 · Buffet/Galleys
  > B FA REPORTED A SMOKY ODOR COMING FROM AFT COFFEEMAKER NR 2. R & R AFT NR 2 COFFEEMAKER PER AMM 25-30-01.
- [SDR SWAA2025122942804](https://openairdocs.org/sdr/SWAA2025122942804.md): Stiffener · cracked · Dec 5, 2025 · N470WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > VERTICAL STIFFENER CRACKED BS 540, RBL 24 UPPER SECTION. REPLACED THE LBL 24 AND RBL 24 STIFFENERS AT BS 540 IAW SRM 51-40-02 IAW DRAWINGS. FABRICATION DEVIATION IAW EA 25-157-03419.
- [SDR SWAA2025122942805](https://openairdocs.org/sdr/SWAA2025122942805.md): Stiffener · cracked · Dec 5, 2025 · N470WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > VERTICAL STIFFENER CRACKED BS 540, LBL 24 UPPER SECTION. REFER TO FAULT TTG8Q0197Q2R WHERE EA 25-157-03419 WAS ADDED AS A SUBTASK. C/W REPLACEMENT STIFFENER AT LBL 24 IAW SRM 51-40-02-0G-0 & DWG 111A2001 REV -. REMOVED AND REPLACED VERTICAL STIFFNER AT BS 54
- [SDR SWAA2025120942771](https://openairdocs.org/sdr/SWAA2025120942771.md): Lamp · burned out · Dec 5, 2025 · N470WN · Boeing 7377H4 · Emergency Lighting
  > RIGHT EMERGENCY EXIT CUTOUT OVERHEAD LIGHTS ARE BURNED OUT. R & R CABIN EMERGENCY EXIT LIGHTS IAW AMM 33-51-01. INSPECTED IAW AMM 33-51-01-960-801-NG. EXIT SIGN - LAMP REPLACEMENT.
- [SDR SWAA2025120942768](https://openairdocs.org/sdr/SWAA2025120942768.md): Light · inoperative · Dec 5, 2025 · N470WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS ABOVE OVERHEAD BINS ARE INOP ON LEFT SIDE. R & R CABIN CEILING NIGHT LIGHTS IAW AMM 33-22-00.
- [SDR SWAA2025112639209](https://openairdocs.org/sdr/SWAA2025112639209.md): Handle · broken · Nov 23, 2025 · N470WN · Boeing 7377H4 · Passenger/Crew Doors
  > L1 DOOR ASSIST HANDLE BROKEN. SWAPPED ASSIST HANDLE FROM FWD LAV TO L1 DOOR PER AMM 52-11-31. L1 DOOR ASSIST HANDLE OPS CHECKS NORMAL. OK TO CONTINUE IAW MEL 25-10-01. C/W SP NR 1B. AUTH 294378. INSTALLED NEW ASSIST HANDLE IN FWD LAVATORY. CHECKED GOOD.
- [SDR SWAA2025090811792](https://openairdocs.org/sdr/SWAA2025090811792.md): Handle · loose · Sep 5, 2025 · N470WN · Boeing 7377H4 · Passenger/Crew Doors
  > FWD ENTRY DOOR HANDLE LOOSE. SECURED FWD ENTRY DOOR HANDLE IAW AMM 52-11-00.
- [SDR SWAA2025070186569](https://openairdocs.org/sdr/SWAA2025070186569.md): Girt Bar · loose · Jun 29, 2025 · N470WN · Boeing 7377H4 · Emergency Equipment
  > FWD SERVICE DOOR GRIT BAR RETENTION BRACKET LOOSE. ADJUSTED FWD SERVICE DOOR GRIT BAR RETENTION BRACKET REF B737 SIP.
- [SDR SWAA2024112772235](https://openairdocs.org/sdr/SWAA2024112772235.md): Limiter · faulty · Nov 26, 2024 · N470WN · Boeing 7377H4 · Hydraulic System, Main
  > B HYD SYSTEM ENG AND ELEC LOW PRESSURE; QUANTITY DROPPED TO ZERO IN FLIGHT; STBY HYD LOW QTY AT GATE<[01] 01 - REMOVED AND REPLACED PER [AMM 27-51-67-401-NG (TRAILING EDGE FLAP FLOW LIMITER - REMOVAL/INSTALLATION - PERMANENT)]. OPPS CHECK GOOD
- [SDR SWAA2024102851744](https://openairdocs.org/sdr/SWAA2024102851744.md): Panel · cracked · Oct 22, 2024 · N470WN · Boeing 7377H4 · Wing Main, Frame Structure
  > PANEL CRACKED AT FASTENER HOLE. RIGHT WING INBOARD FLAP TRACK LOWER WING SKIN PANEL. PANEL CRACKED AT FASTENER HOLE. APPROX. 0.5 IN. LENGTH TO EDGE OF PANEL. RIGHT WING INBOARD FLAP TRACK LOWER WING SKIN PANEL. ITEM (8) 115A2723 SRM 57-51-01-0I-1.<[01] 04 - RE
- [SDR SWAA2024053083446](https://openairdocs.org/sdr/SWAA2024053083446.md): Stringer · cracked · May 8, 2024 · N470WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK INDICATION FOUND IN OPEN HOLE LOC ON BS 727 INNER CHORD AT STRINGER 18A LEFT SIDE; CRACK DIRECTION IS: 2 O CLOCK( VIEW LOOKING INSIDE TO OUTSIDE) 2024-270318<[01] ON STEP 2. TOOL USED: ET INSTRUMENT. P/N: NORTEC 600D. S/N: 210136503. DUE DATE: 23-MAY-24.
- [SDR SWAA2024052982211](https://openairdocs.org/sdr/SWAA2024052982211.md): Power Supply · inoperative · May 3, 2024 · N470WN · Boeing 7377H4 · Emergency Lighting
  > INOP EMERGENCY LIGHT POWER SUPPLY M1668 AT MIDDLE PAX CABIN 2024-270302<[01] REPLACED EMERGENCY LIGHT POWER SUPPLY M1668 AT MIDDLE PAX CABIN I.A.W B737-700 AMM 33-51-06-960-806. TEST IS OK. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED STEP 1 COMPLETED
- [SDR SWAA2024053081333](https://openairdocs.org/sdr/SWAA2024053081333.md): Scuff Plate · cracked · May 1, 2024 · N470WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2024-269854<[01] TOOL USED: DIGITAL CALIPER P/N: 500-196-30; S/N: A23325649; DUE DATE: 31-DEC-24.;[02] TOOL USED; RADIOMETER/PHOTOMETER KIT; P/N:XRP-3000; S/N:1859843; DUE DATE: 24/JUL/24;[03] REPAIRED AF
- [SDR SWAA2024053179613](https://openairdocs.org/sdr/SWAA2024053179613.md): Stringer · cracked · Apr 26, 2024 · N470WN · Boeing 7377H4 · Wing, Longeron/Stringer
  > CRACK FUEL TANK LOC. BTW RIB 19 AND RIB 20 STRINGER 8 UPPER SKIN LOWER SURFACE AFT AREA AT RT WING. REPAIRED UPPER STRINGER U8 - WSTA 564.5 TO WSTA 591.5 AND SKIN ATTACHMENT FLANGE RH WING IAW EA# 24-157-01169 WIP1 AND EA# 24-157-01169 SEE INDIVIDUAL SIGNOFF
- [SDR SWAA2024053179614](https://openairdocs.org/sdr/SWAA2024053179614.md): Stringer · cracked · Apr 26, 2024 · N470WN · Boeing 7377H4 · Wing, Longeron/Stringer
  > CRACK FUEL TANK LOC. BTW RIB 19 AND RIB 20 STRINGER 8 UPPER SKIN LOWER SURFACE AFT AREA AT LT WING. REPAIRED UPPER STRINGER U8 - WSTA 564.5 TO WSTA 591.5 AND SKIN ATTACHMENT FLANGE IAW EA# 24-157-01168-WIP1 AND EA# 24-157-01168 SEE INDIVIDUAL SIGNOFF BELOW.;
- [SDR SWAA2024052979616](https://openairdocs.org/sdr/SWAA2024052979616.md): Light · deteriorated · Apr 26, 2024 · N470WN · Boeing 7377H4 · Emergency Lighting
  > DETERIORATED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2024-270205<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-15-400-802;[02] REPLACED STRIP PHOTOLUMINESCENT
- [SDR SWAA2024053078998](https://openairdocs.org/sdr/SWAA2024053078998.md): Scuff Plate · cracked · Apr 25, 2024 · N470WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON THRESHOLD SCUFF PLATE AT AFT CARGO COMPARTMENT 2024-270149<[01] REPLACED THRESHOLD SCUFF PLATE AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02; DRAWING # 146A8340 REV.- SEE INDIVIDUAL SIGN OFFS BELOW;[02] CORRECTED STEP 1.<BR>REPLACED THRESHOLD SCU
- [SDR SWAA2024053079250](https://openairdocs.org/sdr/SWAA2024053079250.md): Stringer · cracked · Apr 25, 2024 · N470WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 25L LOCATED BS540 FWD CARGO COMPARTMENT 2024-270152<[01] TOOL USED ON STEP 3 UT EQUIPMENT P/N: 45MG; S/N: 130061901; CAL DUE DATE: 09-JUN-24;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPER
- [SDR SWAA2024053079249](https://openairdocs.org/sdr/SWAA2024053079249.md): Stringer · cracked · Apr 25, 2024 · N470WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 26L LOCATED BS540 FWD CARGO COMPARTMENT 2024-270153<[01] TOOL USED ON STEP 3 UT EQUIPMENT P/N: 45MG; S/N: 130061901; CAL DUE DATE: 09-JUN-24;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPER
- [SDR SWAA2024053079251](https://openairdocs.org/sdr/SWAA2024053079251.md): Stringer · cracked · Apr 25, 2024 · N470WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 25R LOCATED BS540 FWD CARGO COMPARTMENT 2024-270154<[01] TOOL USED ON STEP 3 UT EQUIPMENT P/N: 45MG; S/N: 130061901; CAL DUE DATE: 09-JUN-24;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPER
- [SDR SWAA2024053078996](https://openairdocs.org/sdr/SWAA2024053078996.md): Web · cracked · Apr 25, 2024 · N470WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB-INTERCOSTAL LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26R AT FWD CARGO COMPARTMENT 2024-270146<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; P/N P3015GOES00000 S/N 142820025 DUE DATE 22 JAN 25.;[02] R
- [SDR SWAA2024053079390](https://openairdocs.org/sdr/SWAA2024053079390.md): Angle · cracked · Apr 25, 2024 · N470WN · Boeing 7377H4 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ANGLE LOCATED STA 1016 AT VERTICAL STABILIZER 2024-270178<[01] REPLACED ANGLE LOCATED STA 1016 AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DRAWING # 176A3001;REV D.SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED WORK PERFORMED
- [SDR SWAA2024053079394](https://openairdocs.org/sdr/SWAA2024053079394.md): Support Bracket · corroded · Apr 25, 2024 · N470WN · Boeing 7377H4 · Rudder Structure
  > CORROSION BONDING JUMPER SUPPORT BRAKET LOC APROX AT RUD STA 257.9 AT VERTICAL STABILIZER 2024-270179<[01] REPLACED SUPPORT BRACKET AND FASTENERS LOC. APROX AT RUD STA 257.9 AT VERTICAL STABILIZER I.A.W B737-700 SRM 51-40-02 AND INSTALLED BONDING JUMPER LOC. N
- [SDR SWAA2024053078987](https://openairdocs.org/sdr/SWAA2024053078987.md): Frame · cracked · Apr 24, 2024 · N470WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK ON FRAME LOCATED BS 807 BTW STR 8L TO STR 9L AT PASSENGER CABIN 2024-270110 CRACK ON FRAME LOCATED BS 787 BTW STR 8L TO STR 9L AT PASSENGER CABIN<[01] TOOL USED ON STEP 5 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24;[02] PERFOR
- [SDR SWAA2024053078986](https://openairdocs.org/sdr/SWAA2024053078986.md): Frame · cracked · Apr 24, 2024 · N470WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK ON FRAME LOCATED BS 727B BTW STR 8L TO STR 9L AT PASSENGER CABIN 2024-270111<[01] TOOL USED ON STEP 6 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24;[02] PERFORMED PERMANENT REPAIR ON FRAME LOCATED BS 727B BTW STR 8L TO STR 9L AT
- [SDR SWAA2024053078988](https://openairdocs.org/sdr/SWAA2024053078988.md): Frame · cracked · Apr 24, 2024 · N470WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK ON FRAME LOCATED BS 727B BTW STR 8R TO STR 9R AT PASSENGER CABIN 2024-270112<[01] TOOL USED ON STEP 6 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24;[02] PERFORMED PERMANENT REPAIR ON FRAME LOCATED BS 727B BTW STR 8R TO STR 9R AT
- [SDR SWAA2024053077810](https://openairdocs.org/sdr/SWAA2024053077810.md): Light · broken · Apr 22, 2024 · N470WN · Boeing 7377H4 · Emergency Lighting
  > BROKEN SIDEWALL PANEL 231YHW BASE EMERGENCY EXIT LIGHT AT PASSENGER CABIN (1 EA) 2024-270063<[01] REPLACED SIDEWALL PANEL 231YHW BASE EMERGENCY EXIT LIGHT AT PASSENGER CABIN (1 EA) I.A.W. B737-700 AMM 33-51-01-960-802 OPERATIONAL TEST IS OK;[02] REPLACED SIDEW
- [SDR SWAA2024053078116](https://openairdocs.org/sdr/SWAA2024053078116.md): Angle · corroded · Apr 22, 2024 · N470WN · Boeing 7377H4 · Nacelle/Pylon Miscellaneous Structure
  > CORROSION FWD STRUT FAIRING BONDING JUMPER SUPPORT ANGLE ON ENGINE 2 2024-270074<[01] REPLACED SUPPORT ANGLE AT FWD STRUT FAIRING BONDING JUMPER ON ENGINE 2 IAW B737-700 SRM 51-40-02.;[02] REPLACED SUPPORT ANGLE AT FWD STRUT FAIRING BONDING JUMPER ON ENGINE 2
- [SDR SWAA2024053078117](https://openairdocs.org/sdr/SWAA2024053078117.md): Access Panel · cracked · Apr 22, 2024 · N470WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK LEADING EDGE RIB ACCESS PANEL 331B LE STA 114.55 LT HORIZONTAL STAB 2024-270077<[01] REPLACED LEADING EDGE CHORD RIB OF ACCESS PANEL 331B LE STA 114.55 AT LT HORIZONTAL STABILIZER I.A.W. B737-700 SRM 51-10-02; SRM 51-40-02. DWG 186A1305 SHEET 1 REV. 5 AN
- [SDR SWAA2024053078115](https://openairdocs.org/sdr/SWAA2024053078115.md): Vapor Barrier · cracked · Apr 22, 2024 · N470WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACK ON WEB VAPOR BARRIER LOCATED BS 663.75 LBL 16 AT CENTER WING BOX 2024-270075<[01] TOOL USED: CALIPER P/N: 500-196-30; S/N: B21141522; DUE DATE: 07-NOV-24.;[02] TOOL USED= HOT BONDER P/N:HCS9200B; S/N: 16122983; DUE DATE: 15-FEB-25. REPAIRED VAPOR BARRIE

Next page: https://openairdocs.org/aircraft/N470WN/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 = 'N470WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N470WN/reports

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