# Service difficulty reports: N788AT, cancelled Apr 11, 2011

A list on [N788AT, cancelled Apr 11, 2011](https://openairdocs.org/deregistered/N788AT-2011-04-11.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 · 58 reports

- [SDR DHL2008F00002](https://openairdocs.org/sdr/DHL2008F00002.md): Structure · cracked · Jul 9, 2008 · N788AT · Boeing 727214 · Leading Edge Devices
  > L/E SLAT HAS 2 SMALL CRACKS AT IB SLAT TRACK ATTACH POINT. CRACKS WERE BURNISHED OUT WITH MINIMAL MATERIAL LOSS IAW SRM 51-10-01. (K)
- [SDR DHLA200800048](https://openairdocs.org/sdr/DHLA200800048.md): Light · inoperative · May 13, 2008 · N788AT · Boeing 727214 · Emergency Lighting
  > FLT NR 177, FORWARD ENTRY DOOR EMERGENCY LIGHT INOP DURING STBY PWR CHECK. REMOVED AND REPLACED LIGHT ASSY IAW AMM 33-50-01. OPS CHECK NORMAL. AIRCRAFT WAS GROUNDED.
- [SDR DHL2008788003](https://openairdocs.org/sdr/DHL2008788003.md): Structure · cracked · May 2, 2008 · N788AT · Boeing 727214 · Leading Edge Devices
  > NR 3 L/E K-FLAP HAS SMALL CRACK ON THE BOTTOM I/B CORNER. REPAIRED SMALL CRACK PER SRM 51-40-0.
- [SDR DHL2008788001](https://openairdocs.org/sdr/DHL2008788001.md): Skin · gouged · Mar 25, 2008 · N788AT · Boeing 727214 · Leading Edge Devices
  > NR 3 K-FLAP HAS SMALL GOUGE ON LOWER I/B EDGE. DEFECT WAS BLENDED IAW B727SRM 57-50-1 DETAIL 4 GOUGE REMOVED, MINIMAL MATERIAL LOSS.
- [SDR DHLA200800011](https://openairdocs.org/sdr/DHLA200800011.md): Switch · lack of lube · Jan 30, 2008 · N788AT · Boeing 727214 · Door Warning System
  > FLT 194, FWD ENTRY DOOR LIGHT DOES NOT ILLUMINATE WITH DOOR OPEN TEST. TRANSFERED TO DMI 31565 IAW MEL 52-4 CAT C PLACARD INSTALLED. CLEANED AND LUBED L1 DOOR WARNING SWITCH, OPS CHK GOOD IAW MM 52-11-01. DMI 31565 CLEARED PLACARDS REMOVED. ACFT GROUNDED.
- [SDR DHLA200700055](https://openairdocs.org/sdr/DHLA200700055.md): Torque Box · cracked · Nov 6, 2007 · N788AT · Boeing 727214 · Fuselage Main, Structure
  > DURING AN"A" CHECK, TORQUE BOX AREA, LIGHTING HOLES AT STA 1223 LT AND RT HAVE SMALL CRACKS 2 AFT AIR STAIR AREA (PREVIOUSLY REJECTED ON NR 138359). CUT OUT DAMAGED AREA AT TORQUE BOX AREA LIGHTING HOLES/H DIMENSION CUTOUT 3/4" BY 1/4" IAW B727 SRM 53-10-1 FI
- [SDR DHLA200700054](https://openairdocs.org/sdr/DHLA200700054.md): Skin · damaged · Oct 10, 2007 · N788AT · Boeing 727214 · Fuselage Main, Plate/Skin
  > DURING PUSHBACK TOWBAR BROKE AND A/C HIT TUG. REPAIRED DAMAGED SKIN AREA IAW BOEING 727 SRM 53-30-03. REPLACED 2 INTERCOSTALS IAW BOEING 727SRM 51-30-02. FABRICATED INTERCOSTALS PER BOEING DWG 69-16996.
- [SDR DHL2007788526](https://openairdocs.org/sdr/DHL2007788526.md): Nose Cowl · worn · May 18, 2007 · N788AT · Boeing 727214 · Nacelle/Pylon, Main Frame
  > WHILE IN C CHECK AT FLIGHT STAR, NR 1 ENG NOSE COWLING 9:00 POS AFT END COWLING FAYING SURFACE IS WORN AWAY AND KNIFE EDGED. CUT OUT DAMAGED AREA ON NR 1 ENGINE NOSE COWLING AFT END 9:00 POSITION IAW B727 SRM 54-10-03 FIG3. CUTOUT AREA 5" BY 75", FABRICATED
- [SDR DHL2007788525](https://openairdocs.org/sdr/DHL2007788525.md): Skin · gouged · May 17, 2007 · N788AT · Boeing 727214 · Trailing Edge Flaps
  > WHILE AT C CHECK AT FLIGHTSTAR, RT I/B FORE FLAP I/B UPPER SURFACE GOUGED. REMOVED DAMAGED AREA 5" DIA CLEANED AND PREPPED REPAIR AREA, FABRICATED FILLER 5" AND DOUBLER 8" FROM.016" 2024-T3 PO NR 9003189 ALODINED, PRIMED AND APPLIED ADHESIVE FILM IAW B727 SR
- [SDR DHL2007788528](https://openairdocs.org/sdr/DHL2007788528.md): Skin · dented · May 10, 2007 · N788AT · Boeing 727214 · Trailing Edge Flaps
  > WHILE IN "C" CHECK, 3 DENTS ON R/W I/B AFT FLAP UPPER SURFACE 31", 55", AND 82" FROM I/B END. EVALUATED 3 DENTS AT 31" A=1.5, Y=.032, A/Y=46.37. 55" A=1.5", Y=.038, A/Y=39.47. 82" A=1.8, Y=.028, A/Y=64.28. AREA FOUND WITHIN LIMITS IAW B727 SRM 53-10-1 FIG 1.
- [SDR DHL2007788517](https://openairdocs.org/sdr/DHL2007788517.md): Skin · cracked · May 9, 2007 · N788AT · Boeing 727214 · Trailing Edge Flaps
  > RT IB AFT FLAP IS CRACKED 3 PLACES. CUT OUT 3 CRACKED AREAS ON RT IB AFT FLAP UPPER SKIN (1) 1.2" DIA. (2) 1" DIA (3) 1.8" DIA. CUTOUT 2 DELAMINATED AREAS ON LOWER SKIN (1) 8" BY 8" (2) 8 1/2" BY 23". FABRICATED UPPER DOUBLERS (1) 4.2" DIA (2) 4" DIA. (3) 4
- [SDR DHL2007788510](https://openairdocs.org/sdr/DHL2007788510.md): Stringer · corroded · May 4, 2007 · N788AT · Boeing 727214 · Fuselage Main, Longeron/Stringer
  > EXFOLIATION ON STRINGER 27R STA 510. CUT OUT DAMAGED AREA OF STR 27R 7 INCHES IN LENGTH IAW B727 SRM 53-10-3, FIG 1. FABRICATED STRINGER FILLER FROM 7075T6, 7" BY.040", CHORD FROM BAC 1493-412-7075T6, 15 INCHES LONG TWO EACH, ANGLE FROM BAC 1498-140-7075T6,
- [SDR DHL2007788511](https://openairdocs.org/sdr/DHL2007788511.md): Skin · delaminated · May 3, 2007 · N788AT · Boeing 727214 · Trailing Edge Flaps
  > LEFT WING INBD FORE FLAP, LWBL 74 UPPER SURFACE DELAMINATED AT EXISTING REPAIR. REMOVED DELAMINATED AREA 2.5" BY 7" CLEANED AND PREPPED AREA TO BOND IAW B727 SRM 51-40-20, PAR 7, FIG 3. FABRICATED DOUBLER 10" BY 5.7" AND FILLER 2.5" BY 7" FROM.016, 2024T3,
- [SDR DHL2007788516](https://openairdocs.org/sdr/DHL2007788516.md): Skin · delaminated · May 1, 2007 · N788AT · Boeing 727214 · Ailerons
  > LT OB AILERON TAB HAS AREA OF DELAMINATION AT OB END UPPER SURFACE. CUTOUT DELAMINATED AREA ON LT OB AILERON TAB UPPER OB END APPROX 1" BY 3 1/2". FABRICATED FILLER APPROX 1" BY 3 1/2" AND DOUBLER APPROX 2 1/2" BY 5" FROM 2024T3 PO NR 9003621. CLEANED, PREP
- [SDR DHL2007788515](https://openairdocs.org/sdr/DHL2007788515.md): Door Frame · corroded · Apr 29, 2007 · N788AT · Boeing 727214 · Fuselage Main, Structure
  > C2 DOOR CUTOUT AFT FRAME INNER CHORD IS CHORDED WITH EXFOLIATION BETWEEN STR 25R-26R. CUTOUT DAMAGED AREA IAW AD39-53-101 IR. FABRICATED NEW STRAP, FILLER, AND TWO ANGLES IAW DWG AD39-53-101IR. TREATED AND PRIMED ALL REPAIR PARTS AND AREA IAW B727 SRM 51-10
- [SDR DHL2007788512](https://openairdocs.org/sdr/DHL2007788512.md): Skin · delaminated · Apr 29, 2007 · N788AT · Boeing 727214 · Trailing Edge Flaps
  > LEFT WING, INBD FORE FLAP LOWER SURFACE DELAMINATED AT LWBL 125. CUT OUT DELAMINATED AREA 8.4" BY 9.4" CLEANED AND PREPPED AREA TO BOND IAW B727 SRM 51-40-20, PAR 7, FIG 3 AND 51-40-24, FIG 1. FABRICATED DOUBLER 10" BY 12.4" AND FILLER 8.4" BY 9.4" FROM.016
- [SDR DHL2007788522](https://openairdocs.org/sdr/DHL2007788522.md): Cargo Track · corroded · Apr 24, 2007 · N788AT · Boeing 727214 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK SEAT TRACK BBL 24L FROM BS 790 - 840 SHOWS CORROSION. FOUND SEAT TRACK CORRODED OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 3. REMOVED SEAT TRACK SECTION AT MAIN CARGO DECK STA 759.45L - 852.45L BBL24L IAW B727 SRM 51-30-2. FABRICATED NEW SEAT TR
- [SDR DHL2007788514](https://openairdocs.org/sdr/DHL2007788514.md): Skin · delaminated · Apr 24, 2007 · N788AT · Boeing 727214 · Trailing Edge Flaps
  > LEFT WING, INBD FORE FLAP, LOWER SURFACE NEAR TRACK FITTING, LWBL 90, AREA DELAMINATED. CUT OUT DELAMINATED AREA 13" BY 15.5" FABRICATED FILLER, 13" BY 15.5" AND DOUBLER, TWO EACH, 3" BY 15.5" FROM.016, 2024T3. ANODIZED, PRIMED AND APPLIED ADHESIVE FILM IAW
- [SDR DHL2007788507](https://openairdocs.org/sdr/DHL2007788507.md): Seat Track · corroded · Apr 24, 2007 · N788AT · Boeing 727214 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK, SEAT TRACK LBL 45L, FROM BS 850 TO 950C, SURFACE CORROSION, STA 868 TO 950C REMOVED.009 MATERIAL, ORIGINAL MATERIAL THICKNESS.230, MATERIAL REMAINING.221 WITHIN LIMITS IAW B727 SRM 53-10-1, FIG 3. TREATED AND PRIMED AREA IAW B727 SRM 51-10
- [SDR DHL2007788508](https://openairdocs.org/sdr/DHL2007788508.md): Seat Track · corroded · Apr 24, 2007 · N788AT · Boeing 727214 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK, SEAT TRACK LBL 45L, AT 750F, SURFACE CORROSION. REMOVED SEAT TRACK BS 690 TO 740 IAW B727 SRM 51-30-2. FABRICATED TWO NEW SEAT TRACKS FROM BAC 1520-792-7178T6511, 7'.8" LONG AND 6'.8" LONG AND TWO ANGLES FROM BAC 1503-100122-7178T6311, 1'.2"
- [SDR DHL2007788501](https://openairdocs.org/sdr/DHL2007788501.md): Skin · gouged · Apr 24, 2007 · N788AT · Boeing 727214 · Trailing Edge Flaps
  > RIGHT WING, INBD FOREFLAP, INBD UPPER SURFACE GOUGED, WS 198, RWBL 84. REMOVED DAMAGED AREA APPROX 5" DIA IAW B727 SRM 51-40-20,PAR 7, FIG 3. FABRICATED FILLER 5" DIA AND DOUBLER 8" DIA FROM 2024T6 IAW B727 SRM 51-40-24, FIG 1 AND 57-50-2 FIG 3. CLEANED, PR
- [SDR DHL2008788501](https://openairdocs.org/sdr/DHL2008788501.md): Skin · gouged · Apr 24, 2007 · N788AT · Boeing 727214 · Trailing Edge Flaps
  > RIGHT WING, INBD FOREFLAP, INBD UPPER SURFACE GOUGED, WS 198, RWBL 84. REMOVED DAMAGED AREA APPROX 5" DIA IAW B727 SRM 51-40-20, PAR 7, FIG 3. FABRICATED FILLER 5" DIA AND DOUBLER 8" DIA FROM 2024T6 IAW B727 SRM 51-40-24, FIG 1 AND 57-50-2 FIG 3. CLEANED, P
- [SDR DHL2007788513](https://openairdocs.org/sdr/DHL2007788513.md): Skin · delaminated · Apr 23, 2007 · N788AT · Boeing 727214 · Leading Edge Devices
  > RIGHT WING, LWS 383.5, L/E SLAT AERO FENCE, LOWER AFT COMPOSITE SURFACE AREA IS CRACKED, LAYERS ARE SPLITTING. SANDED, CLEANED AND PREPPED 9" BY 5" DAMAGED AREA IAW B727 SRM 51-40-9, PAR 4, FIG 1. FABRICATED, IMPREGNATED (7781-50) FIBERGLASS AND 50A RESIN.
- [SDR DHL2007788505](https://openairdocs.org/sdr/DHL2007788505.md): Skin · cracked · Apr 23, 2007 · N788AT · Boeing 727214 · Wing, Plate/Skin
  > RIGHT WING FIXED L/E NR 5 SLAT, INBD TRACK CUTOUT FOR SLAT TRACK SEAL, AFT INBD RADIUS,.5"-.75" LONG CRACK W/S 383.5. CUTOUT DAMAGED AREA 7" BY 2.25" IAW B727 SRM 57-30-4. FABRICATED NEW DOUBLER 7" BY 5.375 BY.040, 301 1/2 HARD AND FILLER 7" BY 2.25 BY.04
- [SDR DHL2007788506](https://openairdocs.org/sdr/DHL2007788506.md): Skin · gouged · Apr 21, 2007 · N788AT · Boeing 727214 · Trailing Edge Flaps
  > LEFT W/S 464, OUTBD FOREFLAP, INBD L/E AT PREVIOUS REPAIR DOUBLER GOUGED. REMOVED GOUGED DOUBLER IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER 5" BY 6" BY.063 FROM 2024T3 AND FILLER 2.20" BY 1.90" BY.063 FROM 2024T3 IAW B727 SRM 57-50-4, FIG 4. TREATED
- [SDR DHL2007788502](https://openairdocs.org/sdr/DHL2007788502.md): Stringer · corroded · Apr 20, 2007 · N788AT · Boeing 727214 · Fuselage Main, Longeron/Stringer
  > FWD LWR CARGO COMPARTMENT BS 700-720, STR 28L CORROSION ON STR. CUTOUT DAMAGED STR APPROX 30.25" LONG IAW B727 SRM 53-10-3 FIG 1. FABRICATED REPAIR PARTS, 2 HAT SECTIONS 12" AND 18.25" LONG FROM BAC1498-131-7075T6 AND 2 EACH SPLICES 12.25 AND 12.625" LONG FR
- [SDR DHL2007788503](https://openairdocs.org/sdr/DHL2007788503.md): Hinge Fitting · cracked · Apr 19, 2007 · N788AT · Boeing 727214 · Spoilers
  > LEFT WING UPPER T/E, NR 3 SPOILER PANEL, CENTER OUTBD HINGE FITTING IS CRACKED. STOP DRILLED CRACK.250 DIA AT END OF CRACK IAW B727 SRM 51-10-1, VERIFIED WITH NTD HFEC IAW B727 NDTM PT6-51-00-00, FIG 23, CRACK TERMINATED IN STOP DRILL HOLE. FABRICATED 6' BY
- [SDR DHL2007788509](https://openairdocs.org/sdr/DHL2007788509.md): Skin · cracked · Apr 18, 2007 · N788AT · Boeing 727214 · Trailing Edge Flaps
  > LEFT INBD MID FLAP LWBL 85-100, LOWER T/E CHORD CRACKED THREE PLACES ON CUTOUTS. CUTOUT DAMAGE AREA 46.625" BY 2" IAW B727 SRM 51-40-3, FIG 1. FABRICATED NEW ANGLE FROM BAC1503-100046-7075T6, 46.625" BY 2" AND TWO EACH SPLICES FROM BAC 1503-100046-7075T6, 7.
- [SDR DHL2007788504](https://openairdocs.org/sdr/DHL2007788504.md): Skin · debonded · Apr 18, 2007 · N788AT · Boeing 727214 · Trailing Edge Flaps
  > LEFT INBD AFT FLAP, UPPER SURFACE LWBL 244, UPPER SURFACE CRACKED AND DISBONDED. REMOVED DAMAGED AREA 12.5" BY 15", CLEANED, PREPPED AREA IAW B727 SRM 51-40-20, PAR 7, FIG 3. FABRICATED DOUBLER 3" BY 15" AND SKIN 12.5" BY 15" FROM 7075T6,.012, PRIMED, APPLI
- [SDR DHL2007788521](https://openairdocs.org/sdr/DHL2007788521.md): Panel · cracked · Apr 17, 2007 · N788AT · Boeing 727214 · Horizontal Stabilizer, Plate/Skin
  > VERTICAL LE PANEL NR 9502 LOWER INTERIOR PANEL BENT AND CRACKED. REMOVED PREVIOUS REPAIR ON PANEL NR 9502 IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER 7075T6.025 (16.5" BY 8.5") PO NR 9004219 IAW B727 SRM 55-30-2 FIG 2 AND 51-40-2 FIG 1. TREATED AND PRI
- [SDR DHL2007788519](https://openairdocs.org/sdr/DHL2007788519.md): Nose Cowl · cracked · Apr 17, 2007 · N788AT · Boeing 727214 · Nacelle/Pylon, Main Frame
  > NR 1 ENG NOSE COWL 7:30 POS AFT EDGE SKIN IS WORN AND CRACKED. CUTOUT DAMAGED AREA (3.50" BY.90"). FABRICATED REPAIR DOUBLER 2024T3.050 PO 9004690 (11.25" BY 3.50") AND FILLER 2024T3.040 PO NR 9004779 (3.50" BY.90") IAW B727 SRM 54-30-3 FIG 8. TREATED A
- [SDR DHL2007788518](https://openairdocs.org/sdr/DHL2007788518.md): Skin · damaged · Apr 17, 2007 · N788AT · Boeing 727214 · Nacelle/Pylon, Main Frame
  > NR 1 ENG NOSE COWL 9:00 POSITION AFT EDGE SKIN IS BROKEN OUT. CUTOUT DAMAGED AREA (3.50" BY.90"). FABRICATED REPAIR DOUBLER 2024T3.050 PO NR 9004690 (8.25" BY 2.65") AND FILLER 2024T3.040 PO NR 9004779 (3.50" BY.90") IAW B727 SRM 54-30-3 FIG 8. TREATED
- [SDR DHL2007788527](https://openairdocs.org/sdr/DHL2007788527.md): Torque Box · cracked · Apr 14, 2007 · N788AT · Boeing 727214 · Fuselage Main, Structure
  > WHILE IN "C" CHECK, AFT STAIRWELL RT TORQUE BOX HAS CRACK AT INBD WEB LIGHTENING HOLE STA 1223. STOP DRILLED CRACK IAW B727 SRM 51-10-1, FABRICATED REPAIR DOUBLER 7075T6.025 PO NR 9004219 6.6" BY 3.75" IAW B727 SRM 53-10-2 FIG 6. TREATED AND PRIMED IAW B727
- [SDR DHL2007788001](https://openairdocs.org/sdr/DHL2007788001.md): Skin · debonded · Jan 18, 2007 · N788AT · Boeing 727214 · Trailing Edge Flaps
  > LT WING OUTBOARD AFT FLAP SHOW DISBONDED SPOT TEMPORARY REPAIR FROM TE OUTBOARD END. REMOVED DELAMINATED AREA APPROX 9.75" BY 3.8" (UPPER SKIN) AND 3" BY 8.6" (LOWER SKIN), CLEANED AND PREPPED REPAIR AREA TO BOND. FABRICATED UPPER FILLER (9.75" BY 3.9") UPP
- [SDR DHL2006788004](https://openairdocs.org/sdr/DHL2006788004.md): Light · inoperative · Oct 19, 2006 · N788AT · Boeing 727214 · Emergency Lighting
  > DURING STANDBY POWER CHECK, FWD ENTRY DOOR EMERGENCY LIGHT DOES NOT ILLUMINATE. RESEATED COCKPIT EMERGENCY LIGHT ASSY AND OP'S CHECKED SATISFACTORY IAW B727 M/M 33-50-00.
- [SDR DHL2006788003](https://openairdocs.org/sdr/DHL2006788003.md): Battery · inoperative · Mar 7, 2006 · N788AT · Boeing 727214 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS NOT TESTING. REPLACED BATTERYS, OPS CK NORMAL IAW MM 33-50-101, PN-MISC062.
- [SDR DHL2006788002](https://openairdocs.org/sdr/DHL2006788002.md): Battery · inoperative · Feb 21, 2006 · N788AT · Boeing 727214 · Emergency Lighting
  > BOTH EMERGENCY EXIT LIGHTS ARE INOP. R&R BATTERIES IN EMERGENCY EXIT LIGHT ASSY IN COCKPIT OPSCK NORMAL IAW M/M 33-50-101. R&R EMERGENCY LIGHT ASSY IN FWD ENTRY OPS CK NORMAL IAW M/M33-50-101.BATTERIES P/N MISC-062
- [SDR DHL2006788001](https://openairdocs.org/sdr/DHL2006788001.md): Switch · out of adjust · Jan 14, 2006 · N788AT · Boeing 727214 · Landing Gear Position and Warning
  > DURING CRUISE AND LIGHT TURBULENCE NOSE GEAR WARN DOOR LIGHT ILLUMINATED. FOLLOWED AOM PROCEDURE (RAISE GEAR HANDLE) AND LIGHT WENT OUT, BUT FLICKERED IN TURBULENCE. FOUND RIGHT NOSE GEAR DOOR SWITCH OUT OF ADJUSTMENT. ADJUSTED SAME. OPS CHECKS GOOD IAW B7
- [SDR DHL2005788019](https://openairdocs.org/sdr/DHL2005788019.md): Door · out of adjust · Oct 11, 2005 · N788AT · Boeing 727214 · Landing Gear Position and Warning
  > FWD GEAR DOOR LIGHT AND NOSE GEAR DOOR LIGHT ILLUMINATED DURING CLIMB-OUT (14,000 + 320K) WITH GEAR HANDLE IN OFF POSITION LIGHT GOES OUT WITH GR LEVER IN UP POSITION. ENTERED ON DMI 22767 IAW MEL 32-1 CAT"C". PLACARD INSTALLED. TRANSFER TO DMICONT 22767, G
- [SDR DHL2005788018](https://openairdocs.org/sdr/DHL2005788018.md): Bungee Cord · damaged · Oct 9, 2005 · N788AT · Boeing 727214 · Landing Gear Position and Warning
  > FORWARD GEAR DOOR LIGHT AND S/O NOSE GEAR DOOR LIGHT ON WITH GEAR HANDLE IN OFF POSITION. GOES OUT IN UP POSITION. TRANSFERRED TO DMI LOG ITEM NR 22747 IAW ASTAR MEL 32-1 CAT "C". PLACARDS INSTALLED. REF DMI NR 22747 FWD GEAR DOOR LIGHT AND T/O NOSE GEAR D
- [SDR DHL2005788017](https://openairdocs.org/sdr/DHL2005788017.md): Warning Light · illuminated · Oct 6, 2005 · N788AT · Boeing 727214 · Landing Gear Position and Warning
  > GEAR DOOR WARNING LIGHT ILLUMINATED AFTER TAKEOFF WITH GEAR LEVER UP. PERFORMED ABNORMAL AND AFTER CYCLING GEAR RESULTED IN DOORS LIGHT AND LT AND RT GEAR RED DOOR LIGHTS ILLUMINATED.
- [SDR DHL2005788016](https://openairdocs.org/sdr/DHL2005788016.md): Door · out of adjust · Oct 4, 2005 · N788AT · Boeing 727214 · Landing Gear Door Retract Section
  > DURING CLIMBOUT AFTER COMPLETION OF AFTER LANDING CHECKLIST, NOSE GEAR DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT SLOWED BELOW 280 KIAS AND LIGHT WENT OUT. TRANSFER LANDING GEAR DOOR WARNING SYSTEM TO DMI LOG IAW MEL 32-1 CAT C ITEM DMI NR 22691 PLACARD INSTAL
- [SDR DHL2005788015](https://openairdocs.org/sdr/DHL2005788015.md): Door · out of rig · Oct 1, 2005 · N788AT · Boeing 727214 · Landing Gear Door Retract Section
  > RED NOSE GEAR DOOR LIGHT ON FRONT PANEL & AMBER NOSE GEAR DOOR LIGHT ON SO PANEL ILLUMINATED FLASHED DURING CLIMB. ABNORMAL PROCEDURE COMPLETED CONDITION NORMAL LIGHT EXTINGUISHED W/ GEAR HANDLE UP. DOOR WARNING SYS DEFFERRED IAW MEL 32-1 DMI 22651 CAT C PLA
- [SDR DHL2005788013](https://openairdocs.org/sdr/DHL2005788013.md): Switch · out of adjust · Sep 27, 2005 · N788AT · Boeing 727214 · Landing Gear Position and Warning
  > AT 340 KIAS RED LANDING GEAR DOORS LIGHT ON FWD PANEL ILLUMINATED & AMBER NOSE GEAR DOOR WARNING LIGHT ON S/O PANEL ILLUMINATED. FOUND NOSE GEAR DOOR SWITCH OUT OF ADJ. ADJ SWITCH IAW MM 32-62-11, OPS CHECK GOOD.
- [SDR DHL2005788014](https://openairdocs.org/sdr/DHL2005788014.md): Warning Light · false activation · Sep 27, 2005 · N788AT · Boeing 727214 · Landing Gear Position and Warning
  > RED NOSE GEAR DOOR AND AMBER NOSE GEAR DOOR ON S/O PANEL CAME ON DURING CLIMB. ABNORMAL PROCEDURE COMPLETED. CONDITION RETURNED TO NORMAL WITH GEAR HANDLE UP. INSP NOSE GEAR DOOR'S IAW 727 MM CH 32-22-1, NO DEFECTS FOUND AT THIS TIME. INDICATION PLACED ON
- [SDR DHL2005788012](https://openairdocs.org/sdr/DHL2005788012.md): Wire · loose · Aug 10, 2005 · N788AT · Boeing 727214 · Landing Gear Position and Warning
  > LEFT GEAR LIGHT DID NOT COME ON DURING EXTENSION. APPLIED APPROPRIATE ABNORMAL PROCEDURES AND LANDED SAFELY. TIGHTEND LOOSE WIRE ON BACK OF KOREY LIGHT ASSY. SYSTEM CHECKED NORMAL ON SEVERAL DUMMY GEAR RETRACTIONS IAW B727 M/M 32-61-01.
- [SDR DHL2005788011](https://openairdocs.org/sdr/DHL2005788011.md): Cap · loose · Aug 9, 2005 · N788AT · Boeing 727214 · Landing Gear Position and Warning
  > LEFT GEAR GREEN LIGHT DID NOT COME ON DURING EXTENTION. APPLIED APPROPRIATE ABNORMAL PROCEDURE AND LANDED SAFELY. FOUND L/MLG GREEN LIGHT CAP ASSEMBLY NOT FULLY ENGAGED IN LIGHT ASSY. PROPERLY INSTALLED PER MM 33-10-51 & L/MLG GREEN LIGHT OPS CKS NORMAL.
- [SDR DHL2005788010](https://openairdocs.org/sdr/DHL2005788010.md): Bulb · intermittent · Aug 2, 2005 · N788AT · Boeing 727214 · Landing Gear Position and Warning
  > LEFT MAIN GEAR LIGHT ILLUMINATES INTERMITTENTLY. RELAMPED LEFT GEAR GREEN LIGHT BULB. CKS GOOD IAW MM 32-61-01, (BULB NR387).
- [SDR DHL2005788009](https://openairdocs.org/sdr/DHL2005788009.md): Switch · out of adjust · Aug 2, 2005 · N788AT · Boeing 727214 · Landing Gear Position and Warning
  > RED "DOORS" LIGHT ON FWD PANEL AND "NOSE GEAR DOOR" AMBER LIGHT ON S'OFFICER'S PANEL FLICKERS DURING TURBULANCE. ADJUSTED NOSE GEAR DOOR LIGHTS SWITCHES, OPS CKECK GOOD IAW MM 32-62-00.
- [SDR DHL2005788008](https://openairdocs.org/sdr/DHL2005788008.md): Bulb · loose · Aug 2, 2005 · N788AT · Boeing 727214 · Landing Gear Position and Warning
  > RIGHT GEAR "RED" LIGHT ON FWD PANEL DOESN'T ILLUMINATE ON GEAR EXTENSION. RE-SEATED RT MLG RED LIGHT IN SOCKET. OPS CHECK GOOD IAW MM 32-61-01.

Next page: https://openairdocs.org/deregistered/N788AT-2011-04-11/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 = 'N788AT' AND deregistration_id = 'N788AT-2011-04-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N788AT-2011-04-11/reports

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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.