# Service difficulty reports: N8528Q

A list on [N8528Q](https://openairdocs.org/aircraft/N8528Q.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 2 · 56 reports

- [SDR SWAA2026090821860](https://openairdocs.org/sdr/SWAA2026090821860.md): Lens · unsecure · Sep 3, 2026 · N8528Q · Boeing 7378H4 · Emergency Lighting
  > FWD ENTRY DOOR LOWER EMERGENCY LIGHT LENS NEEDS TO BE SECURED. SECURED THE LENS IAW SIP.
- [SDR SWAA2026070114067](https://openairdocs.org/sdr/SWAA2026070114067.md): Cover · missing · Jun 20, 2026 · N8528Q · Boeing 7378H4 · Emergency Lighting
  > FWD LEFT OVERWING EXIT DOOR EXIT SIGN INDICATOR ASSY MISSING COVER. INSTALLED NEW FWD L/H OWE SIGN INDICATOR ASSY LENS COVER IAW AMM 33-51-01-960-801 SECTION C.(3).
- [SDR SWAA2026060809684](https://openairdocs.org/sdr/SWAA2026060809684.md): Slide · loose · Jun 5, 2026 · N8528Q · Boeing 7378H4 · Escape Slide
  > FWD SERVICE DOOR SLIDE LOOSE. REMOVED AND REPLACED SLIDE ASSY IAW MT 725-61-06.
- [SDR SWAA2026032481918](https://openairdocs.org/sdr/SWAA2026032481918.md): Flashlight · no test · Mar 20, 2026 · N8528Q · Boeing 7378H4 · Emergency Equipment
  > AFT LT CABIN CREW FLASHLIGHT DOES NOT TEST. PERFORMED OPS CK OF L/H AFT CABIN CREW FLASHLIGHT PER AMM 25-64-00. NO DISCREPANCIES NOTED.
- [SDR SWAA2026030275207](https://openairdocs.org/sdr/SWAA2026030275207.md): Lamp · inoperative · Feb 28, 2026 · N8528Q · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY LIGHT AFT OF R2 DOOR INOPERATIVE. REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHT IAW AMM 33-51-04.
- [SDR SWAA2026020666029](https://openairdocs.org/sdr/SWAA2026020666029.md): Battery Pack · inoperative · Jan 30, 2026 · N8528Q · Boeing 7378H4 · Emergency Lighting
  > THREE EMERGENCY EXIT AISLE LIGHTS AT SEATS ROWS 6 DEF - 14 DEF INOPERATIVE. REMOVED AND REPLACED THE BATTERY AND POWER SUPPLY IAW AMM 33-51-06. OPS CHECKED GOOD.
- [SDR SWAA2026020663492](https://openairdocs.org/sdr/SWAA2026020663492.md): Scuff Plate · cracked · Jan 21, 2026 · N8528Q · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO, AFT CORNER SCUFF PLATE CRACKED. REMOVED AND REPLACED THE SCUFF PLATE IAW AMM 53-11-02.
- [SDR SWAA2026021062637](https://openairdocs.org/sdr/SWAA2026021062637.md): Blade · damaged · Jan 19, 2026 · N8528Q · Boeing 7378H4 · Elevator Structure
  > RIGHT ELEVATOR, INBD BLADE SEAL, AFT SCREW HOLE COUNTERSINK IS ELONGATED PREVENTING SCREW FROM HOLDING. REF TSR 202600338; ENGINEERING RECOMMENDS REPAIRING IAW SRM 51-70-04-2R-9. ADDED TSR TO MEASUREMENTS FIELD. REPAIRED HOLE IAW SRM 51-70-04-2R-9, REPAIR 9
- [SDR SWAA2026021060214](https://openairdocs.org/sdr/SWAA2026021060214.md): Attach Angle · cracked · Jan 11, 2026 · N8528Q · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED AT RBL 34. CUT, LOCATED, & DRILLED A NEW ATTACH ANGLE FROM APPROX RBL 30 TO RBL 65. FABRICATED A SPLICE ANGLE, LOCATED & DRILLED VERTICAL LEG ONLY OF REPAIR SPLICE IAW SRM 57-10-10-2R-5. COMPLETED DRILLING AND FINA
- [SDR SWAA2026020660213](https://openairdocs.org/sdr/SWAA2026020660213.md): Nut Plate · debonded · Jan 11, 2026 · N8528Q · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > AFT CARGO BAY, LT FLOOR TRANSITION ANGLE, BS 727H - 727J. DEBONDED NUT PLATES (QTY. 10). INSTALLED BONDED NUT PLATES ON THE TRANSITION ANGLE IAW SRM 51-40-10.
- [SDR SWAA2026020660209](https://openairdocs.org/sdr/SWAA2026020660209.md): Nut Plate · debonded · Jan 11, 2026 · N8528Q · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > AFT CARGO LT FLOOR TRANSITION ANGLE, BS 727J - 767, DEBONDED NUT PLATES (QTY. 10). INSTALLED BONDED NUT PLATES TO THE TRANSITION ANGLE IAW SRM 51-40-10.
- [SDR SWAA2026020660210](https://openairdocs.org/sdr/SWAA2026020660210.md): Nut Plate · debonded · Jan 11, 2026 · N8528Q · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > AFT CARGO BAY, LT FLOOR TRANSITION ANGLE, BS 767 - 807 DEBONDED NUT PLATES (QTY. 10). INSTALLED BONDED NUT PLATES TO THE AFT CARGO LT FLOOR TRANSITION ANGLE IAW SRM 51-40-10
- [SDR SWAA2026020660211](https://openairdocs.org/sdr/SWAA2026020660211.md): Nut Plate · debonded · Jan 11, 2026 · N8528Q · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > AFT CARGO BAY, RT FLOOR TRANSITION ANGLE, BS 727F - 727H, DEBONDED NUT PLATES (QTY. 10). INSTALLED BONDED NUT PLATES TO AFT CARGO RT FLOOR TRANSITION ANGLE IAW SRM 51-40-10.
- [SDR SWAA2026020660212](https://openairdocs.org/sdr/SWAA2026020660212.md): Nut Plate · debonded · Jan 11, 2026 · N8528Q · Boeing 7378H4 · Fuselage Main, Attach Fittings
  > AFT CARGO RT FLOOR TRANSITION ANGLE, BS 727H - 727J, DEBONDED NUTPLATES (QTY. 10). INSTALLED BONDED NUTPLATES TO AFT CARGO RT FLOOR TRANSITION ANGLE IAW SRM 51-40-10.
- [SDR SWAA2026021059870](https://openairdocs.org/sdr/SWAA2026021059870.md): Seal · cracked · Jan 9, 2026 · N8528Q · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STAB, UPPER FWD SLIDING SEAL IS CRACKED. REMOVED AND REPLACED THE LT STABILIZER TO BODY UPPER FRONT SLIDING SEAL IAW AMM 53-31-31. OPS CHECKED GOOD.
- [SDR SWAA2026021059869](https://openairdocs.org/sdr/SWAA2026021059869.md): Seal · cracked · Jan 9, 2026 · N8528Q · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STAB UPPER FWD SLIDING SEAL IS CRACKED. REMOVED AND REPLACED RT STABILIZER TO BODY UPPER FRONT SPAR SLIDING SEAL IAW AMM 53-31-31. OPS CHKD GOOD.
- [SDR SWAA2026020559866](https://openairdocs.org/sdr/SWAA2026020559866.md): Hook · loose · Jan 9, 2026 · N8528Q · Boeing 7378H4 · Emergency Equipment
  > FWD ENTRY DOOR SLIDE AFT GIRT BAR HOOK LOOSE. SECURED THE GIRT BAR HOOK IAW SRM 51-40-02.
- [SDR SWAA2025033119215](https://openairdocs.org/sdr/SWAA2025033119215.md): Indication Sys · malfunctioned · Mar 28, 2025 · N8528Q · Boeing 7378H4 · Landing Gear Position and Warning
  > AFTER SELECTING THE LANDING GEAR DOWN; ALL RED AND GREEN INDICATOR LIGHTS ON INSTRUMENT PANEL REMAINED ILLUMINATED. OVERHEAD INDICATOR LIGHTS ALSO ILLUMINATED. PERFORMED A GO AROUND AND RAN CHECKLIST GEAR OPERATED NORMALLY<[01] PERFORMED PSEU BITE PROCEDURE PE
- [SDR SWAA2023082191287](https://openairdocs.org/sdr/SWAA2023082191287.md): Girt Bar · out of adjust · Aug 17, 2023 · N8528Q · Boeing 7378H4 · Emergency Equipment
  > REFERENCE TTG8Q00MWSTU R1 GIRT BAR REQUIRES INSPECTION DUE TO REPORTS OF GIRT BAR FALLING OUT OF HOOKS.<[01] INSPECTED R1 DOOR GIRT BAR RETAINER HOOKS & GIRT BAR IAW AMM 25-66-01. REPLACED SHEARED RIVETS ON R1 DOOR ESCAPE SLIDE PACK AFT RETAINING HOOK IAW SRM
- [SDR SWAA2023032319889](https://openairdocs.org/sdr/SWAA2023032319889.md): Battery · faulty · Mar 22, 2023 · N8528Q · Boeing 7378H4 · Emergency Equipment
  > AFT JUMP SEAT FLASHLIGHTS ARE NOT CHARGING; WILL NOT TEST<[01] R&R AFT FLASHLIGHT BATTERIES PER AMM 25-64-00.
- [SDR SWAA2023032018062](https://openairdocs.org/sdr/SWAA2023032018062.md): Girt Bar · out of adjust · Mar 17, 2023 · N8528Q · Boeing 7378H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE GIRT BAR IS NOT PROPERLY STOWED.<[01] STOWED FED SLIDE GRIT BAR PER AMM 25-66-00-040-801 STEP 3.D.(2).(A;B);[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.
- [SDR SWAA2023031616030](https://openairdocs.org/sdr/SWAA2023031616030.md): Battery Pack · inoperative · Mar 14, 2023 · N8528Q · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS COMMON TO BATTERY PACK M2816 ARE INOP.<[01] REMOVED AND REPLACED BATTERY PACK M2816 AND PERFORMED GOOD TEST PER AMM 33-51-06-960-805.;[02] VERIFIED
- [SDR SWAA2023031616031](https://openairdocs.org/sdr/SWAA2023031616031.md): Battery Pack · inoperative · Mar 14, 2023 · N8528Q · Boeing 7378H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS COMMON TO BATTERY PACK M1675 ARE INOP.<[01] REMOVED AND REPLACED BATTERY PACK M1675 AND PERFORMED GOOD TEST PER AMM 33-51-06-960-805.;[02] VERIFIED
- [SDR SWAA2023032109544](https://openairdocs.org/sdr/SWAA2023032109544.md): Beam · corroded · Feb 23, 2023 · N8528Q · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON 947 FLOORBEAM UPPER SURFACE LBL 50; WL 208.<REMOVED CORROSION ON 947 FLOORBEAM UPPER SURFACE LBL 50; WL 208 PER SRM 51-10-02-0G-0. AREA BLENDED IS 3' BY.600';.050' ON EDGE PER SRM 51-10-02-0G-0.;[04] REJECTED CORRECTIVE ACTIONS STEP 3; CREATED S
- [SDR SWAA2023032109551](https://openairdocs.org/sdr/SWAA2023032109551.md): Angle · corroded · Feb 23, 2023 · N8528Q · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON Z ANGLE COMMON TO SHEARWEB UPPER SURFACE STA 993; LBL 37; WL 208.<[01] REMOVED CORROSION ON Z ANGLE COMMON TO SHEARWEB UPPER SURFACE STA 993; LBL 37; WL 208. AREA BLENDED.5' BY.5' AROUND FLOOR PANEL HOLE; FOUND TO BE 100% MATERIAL LOSS FROM.050
- [SDR SWAA2023032009557](https://openairdocs.org/sdr/SWAA2023032009557.md): Attach Angle · cracked · Feb 23, 2023 · N8528Q · Boeing 7378H4 · Fuselage Main, Plate/Skin
  > CRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 13; WL 208.<[01] REMOVED DAMAGED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 13; WL 208 IAW SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 13; WL 208 I
- [SDR SWAA2023032009543](https://openairdocs.org/sdr/SWAA2023032009543.md): Support · corroded · Feb 23, 2023 · N8528Q · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT STA 952; LBL 30; LBL 35; WL 208.<[01] COMPLETED STEP 1; SRM 51-10-02-0G-0 REPLACEMENT OF PART IS APPLICABLE.;[02] COMPLETED STEP 2;[03] STEPS 1;2 PARTIAL UPDATED.;[04] LOCATED AND DRILLED NEW FLOOR SUPPORT STA 952; LBL 24- LBL 49; WL
- [SDR SWAA2023032009549](https://openairdocs.org/sdr/SWAA2023032009549.md): Floor Support · corroded · Feb 23, 2023 · N8528Q · Boeing 7378H4 · Fuselage Internal Mounting Structure
  > CORROSION ON FLOOR SUPPORT STA 952; RBL 28- RBL 34; WL 208.<[01] REMOVED CORROSION ON FLOOR SUPPORT STA 952; RBL 28-RBL 34; WL 208. FOUND TO HAVE 100% MATERIAL LOSS AROUND FASTENER HOLE AT RBL 30 PER SRM 51-10-02-0G-0; REPLACEMENT OF PART IS APPLICABLE.;[02] R
- [SDR SWAA2023032009545](https://openairdocs.org/sdr/SWAA2023032009545.md): Beam · corroded · Feb 23, 2023 · N8528Q · Boeing 7378H4 · Fuselage Main, Floor Beam
  > CORROSION ON 947 FLOORBEAM UPPER SURFACE RBL 25; RBL 50; WL 208.<CUTOUT DAMAGE FLANGES OF THE UPPER CHORD OF THE FLOOR BEAM ON BS 947.5 FROM LBL58.60 TO RBL58.60 IAW SRM 53-70-51-2R-5 STEP 4.C.(1)FLAP PEEN ON THE FLOOR BEAM AT BS 947 FROM LBL58.60-RBL58.60 IAW
- [SDR SWAA2023032009550](https://openairdocs.org/sdr/SWAA2023032009550.md): Web · corroded · Feb 23, 2023 · N8528Q · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SHEAR WEB UPPER SURFACE STA 988-989; 991-992; LBL 32- LBL 33; WL 208.<[01] REMOVED G4-B FWD O/B L/H FLOOR MOUNT FITTING STA 990 LBL 32; WL FOR ACCESS PER SRM 51-40-02-0G-0.;[02] REMOVED CORROSION ON SHEAR WEB UPPER SURFACE STA 989-990; 991-992; LB
- [SDR SWAA2023031709696](https://openairdocs.org/sdr/SWAA2023031709696.md): Panel · cracked · Feb 23, 2023 · N8528Q · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CRACKED PANEL BREAK STA 540; BL0-RBL 25; WL 208.<[01] REMOVED BREAK PANEL AT STA 540; BL0-RBL25; PER SRM 51-40-02-0G-0.<BR>LOCATED AND DRILLED NEW PART; OK TO INSTALL.;[02] LOCATE AND DRILL IS ACCEPTED.. MISSING SHIM AT FWD INBD HOLE (BL 0).;[03] LOCATED AND I
- [SDR SWAA2023032005224](https://openairdocs.org/sdr/SWAA2023032005224.md): Floor Panel · delaminated · Feb 20, 2023 · N8528Q · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 221FF SURFACE IS DELAMINATED.<DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F AND WILL BE REPAIRED IAW SRM 53-00-50-2R-1. REMOVED FIVE INSERTS FROM THE PANEL AND REMOVED AN APPROX. 13'X24' AREA OF DAMGED TOOLSIDE PLIES S
- [SDR SWAA2023032005226](https://openairdocs.org/sdr/SWAA2023032005226.md): Floor Panel · delaminated · Feb 20, 2023 · N8528Q · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 222DF HAS SURFACE DELAMINATION AND CORRODED INSERTS.<FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>DAMAGE TO BE REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>REMOVED 33EA INSERTS TO FACILITATE REPAIR; REMOVED DAMAGED
- [SDR SWAA2023031605228](https://openairdocs.org/sdr/SWAA2023031605228.md): Floor Panel · delaminated · Feb 20, 2023 · N8528Q · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241D LOWER SURFACE IS DELAMINATED.<[01] IDENTIFIED PANEL 241D IAW SRM 53-00-50-0I-1 PARA. FIGURE 6; TABLE 6.<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR><BR>WILL PERFORM REPAIRS IAW SRM 53-00-50-2R-1<B
- [SDR SWAA2023031605227](https://openairdocs.org/sdr/SWAA2023031605227.md): Floor Panel · delaminated · Feb 20, 2023 · N8528Q · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 242E UPPER SURFACE IS DELAMINATED.<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 6 TABLE 6.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1.<BR>REMOVED
- [SDR SWAA2023031605231](https://openairdocs.org/sdr/SWAA2023031605231.md): Floor Panel · delaminated · Feb 20, 2023 · N8528Q · Boeing 7378H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241XF HAS SURFACE DELAMINATION.<[01] IDENTIFIED PANEL IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>DAMAGE TO BE REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>REMOVED 7EA INS
- [SDR SWAA2023032003531](https://openairdocs.org/sdr/SWAA2023032003531.md): Support · corroded · Feb 16, 2023 · N8528Q · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO BAY ON BULKHEAD SUPPORT BS 500I RBL 20 TO LBL 20 WL 156<[01] EVALUATED CORROSION AT ALL LOCATIONS OF BULKHEAD SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 500I RBL 19 WL 156; FOUND 0.020 REMOVED FROM ORIG 0.071 IN NUMEROUS 1'X1' AREAS; FOUND
- [SDR SWAA2023032003532](https://openairdocs.org/sdr/SWAA2023032003532.md): Support · corroded · Feb 16, 2023 · N8528Q · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FORWARD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT BS 500A+12 TO 500H+2 RBL 23 WL 156<[01] EVALUATED CORROSION AT ALL LOCATIONS OF FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 500E+10 RBL 23 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.04
- [SDR SWAA2023032003533](https://openairdocs.org/sdr/SWAA2023032003533.md): Support · corroded · Feb 16, 2023 · N8528Q · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 727F+6 TO 767 RBL 21 WL 156<[01] EVALUATED CORROSION AT ALL LOCATIONS OF FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 727I+4 RBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN NUMEROUS
- [SDR SWAA2023032003534](https://openairdocs.org/sdr/SWAA2023032003534.md): Support · corroded · Feb 16, 2023 · N8528Q · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT BS 727G+16 TO 847 LBL 21 WL 156<[01] EVALUATED CORROSION AT ALL LOCATIONS OF FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 727I+4 LBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN NUM
- [SDR SWAA2023032003536](https://openairdocs.org/sdr/SWAA2023032003536.md): Shield · corroded · Feb 16, 2023 · N8528Q · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO BAY SHIELD BS 847+12 RBL 21 WL 164<[01] EVALUATED CORROSION ON SHIELD BS 847+12 RBL 21 WL 164; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION 1 AND MEA
- [SDR SWAA2023032003903](https://openairdocs.org/sdr/SWAA2023032003903.md): Attach Angle · cracked · Feb 16, 2023 · N8528Q · Boeing 7378H4 · Wing Miscellaneous Structure
  > LEFT WING TRANSVERSE WEB O/B ATTACH ANGLE CRACKED AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT<[01] REMOVED LEFT WING TRANSVERSE WEB O/B ATTACH ANGLE CRACKED AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT IAW SRM 51-40-02-0G-0;[02] LOCATED AND DR
- [SDR SWAA2023032003904](https://openairdocs.org/sdr/SWAA2023032003904.md): Panel · corroded · Feb 16, 2023 · N8528Q · Boeing 7378H4 · Wing Miscellaneous Structure
  > SPR FUELING CONTROL PANEL IS CORRODED<[01] CORROSION ON BRACKET WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN IN THE SRM. PART REPLACEMENT REQUIRED.;[02] REMOVED AND REPLACED FUELING CONTROL PANEL ASSEMBLY IAW AMM 28-41-61-000-801.;[03] VERIFIED ACTION
- [SDR SWAA2023031603012](https://openairdocs.org/sdr/SWAA2023031603012.md): Megaphone · damaged · Feb 14, 2023 · N8528Q · Boeing 7378H4 · Emergency Equipment
  > FWD MEGAPHONE RUBBER END IS DISBONDED.<[01] REPLACED FWD MEGAPHONE PER AMM 25-64-00-710-801;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2023031602610](https://openairdocs.org/sdr/SWAA2023031602610.md): Angle · cracked · Feb 13, 2023 · N8528Q · Boeing 7378H4 · Wing Main, Frame Structure
  > L/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL8 WL167.68<[01] CORRECTION TO TSK DETAIL SHOULD STATE ' L/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL8 WL167.68 ';[02] VALIDATED APPLICABILITY OF SRM 57-10-10-2R-5;[03] INSTALLED EWIS P
- [SDR SWAA2023031602611](https://openairdocs.org/sdr/SWAA2023031602611.md): Angle · cracked · Feb 13, 2023 · N8528Q · Boeing 7378H4 · Wing Main, Frame Structure
  > R/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL8 WL167.68<[01] VALIDATED APPLICABILITY OF SRM 57-10-10-2R-5;[02] INSTALLED EWIS PROTECTION ON FWD AND AFT SIDE OF VAPOR BARRIER BS663 UPPER ATTACH ANGLE RBL8-RBL20 WL167.68 IAW AMM 20-60-07-913-801.
- [SDR SWAA2023010588327](https://openairdocs.org/sdr/SWAA2023010588327.md): Lamp · inoperative · Jan 5, 2023 · N8528Q · Boeing 7378H4 · Emergency Lighting
  > L1 DOOR EXTERIOR EMRGENCY SLIDE LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-04. OPS OK.
- [SDR SWAA2022110367532](https://openairdocs.org/sdr/SWAA2022110367532.md): Slide · loose · Nov 2, 2022 · N8528Q · Boeing 7378H4 · Escape Slide
  > FORWARD SERVICE DOOR EMERGENCY SLIDE FELL OUT OF CONTAINER. / [01] REPACKED FORWARD SERVICE DOOR EMERGENCY SLIDE. REF AMM 25-66-01.
- [SDR SWAA2021020846533](https://openairdocs.org/sdr/SWAA2021020846533.md): Angle · missing · Feb 2, 2021 · N8528Q · Boeing 7378H4 · Escape Slide
  > AFT SERVICE DOOR ESCAPE SLIDE MISSING FORWARD CLIP ON SIDE CONTAINER / REPLACED CLIP PER S.I.P SHOULD WAS NOT OPENED
- [SDR SWAA2021042339320](https://openairdocs.org/sdr/SWAA2021042339320.md): Scuff Plate · cracked · Jan 2, 2021 · N8528Q · Boeing 7378H4 · Fuselage Miscellaneous Structure
  > AFT CARGO OPENING; AFT CORNER SCUFF PLATE CRACKED. / REMOVED AND REPLACED AFT CARGO DOOR SCUFF PLATE AS PER AMM 53-11-02

Next page: https://openairdocs.org/aircraft/N8528Q/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 = 'N8528Q' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8528Q/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.